MRO Network - airworthiness directive

The FAA has published an airworthiness directive (AD) adding special compliance items to maintenance and inspection programmes for a number of McDonnell Douglas aircraft and the 717-200.

Effective from March 5, the AD covers models of the DC-10, MD-10 and MD-81/82/83/87/88/90 and is expected to affect 716 aircraft registered in the US.

The FAA says the AD was developed in response to reports of latent air data transducer degradation and to prevent erroneous data being produced which could lead to a mid-air collision in certain circumstances.

The FAA estimates that the revision to MRO programmes will cost US operators a total of $60,860.

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Engine - Critical Parts - Identification / Replacement

RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37 engines, all serial numbers (s/n). These engines are known to be installed on, but not limited to, Boeing 757 series aeroplanes

EASA AD 2015-0058

N/A

Rolls-Royce Alert NMSB RB.211-72-AH792 Revision 1 dated 05 June 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
RR Worldwide (WW) Communication WW/11174/2, dated 22 January 2015. RR WW/11196/1 dated 01 May 2015

Wings - Wing Rear Spar - Inspection / Repair

Jetstream 4100 aeroplanes, all models, all serial numbers

EASA AD 2011-0096

N/A

BAE Systems (Operations) Ltd SB J41-A57-029 Revision 3 dated 08 April 2014.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Fuselage - Skin and Structure / Allowable Damage Limits - Records Check / Repair

Airbus A330-201, A330-202, A330-203, A330-223, A330-243, A330-223F, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes,
Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes,
all manufacturer serial numbers (MSN) up to MSN 1 600 inclusive.

N/A

Airbus SB A330-53-3232 original issue dated 04 November 2014.
Airbus SB A340-53-4222 original issue dated 25 November 2014.
Airbus SB A330-53-3233 original issue dated 26 September 2014.
Airbus SB A340-53-4223 original issue dated 26 September 2014.
Airbus SB A330-53-3234 original issue dated 08 December 2014.
Airbus SB A340-53-4224 original issue dated 15 December 2014
Airbus SB A330-53-3235 Revision 01 dated 14 January 2015.
Airbus SB A340-53-4225 Revision 01 dated 14 January 2015.
Airbus SRM dated April 2013.
Airbus SRM TR 53-001 dated 28 November 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Flight Controls - Elevator Trim Circuit - Inspection / Modification

Jetstream 4100 aeroplanes, all models, all serial numbers

N/A

BAE Systems (Operations) Ltd, ISB J41-27-068 original issue dated 21 January 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Flight Controls - Elevator Aileron Computers - Replacement / Software Update

Airbus A318-111, A318-112, A318-121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, all manufacturer serial numbers (MSN).

DGAC France AD 95-203-072 and 2001-508

N/A

Airbus SB A320-27-1135 original issue dated 29 June 2001, or Revision 01 dated 31 August 2001, or Revision 02 dated 18 April 2002.
Airbus SB A320-27-1151 original issue dated 09 March 2004, or Revision 01 dated 19 October 2004.
Airbus SB A320-27-1152 original issue dated 04 June 2004, or Revision 01 dated 19 October 2004, or Revision 02 dated 04 April 2006.
Airbus SB A320-27-1243 original issue dated 17 March 2015.
Airbus SB A320-27-1244 original issue dated 05 March 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

EMBRAER S.A. / 39-1394

This Airworthiness Directive (AD) applies to Embraer S.A. model ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD, ERJ 170-100 SU, ERJ 170-200 LR, ERJ 170-200 STD and ERJ 170-200 SU airplanes with manufacturer serial number 17000002, 17000004 through 17000013, and 17000015 through 17000453, inclusive.
Note (1): Airplanes with an original airworthiness certificate or original export certificate of airworthiness issued on or after February 23, 2015 must comply with the airworthiness limitations specified as part of the airworthiness certification of those airplanes, or in accordance with operations specifications approved under "Regulamento Brasileiro da Aviacao Civil" (RBAC) 121 or 135, or an inspection program approved under paragraph 91.409(e) of "Regulamento Brasileiro de Homologacao Aeronautica" (RBHA) 91.
Note (2): This AD requires revisions to certain operator maintenance documents to include new inspections or modification to the existing ones and its respective thresholds and intervals. Compliance with these inspections is required by RBHA 91.403(c). For airplanes that have been previously modified, altered, or repaired in the areas addressed by these inspections, the operator may not be able to accomplish the inspections described in the revisions. In this situation, to comply with RBHA 91.403(c), the operator must request approval for an alternative method of compliance according to paragraph (c) of this AD. The request should include a description of changes to the required inspections that will ensure the continued damage tolerance of the affected structure.

ANAC AD 2012-10-01

N/A

You must use the Appendix A, Airworthiness Limitations, of the Embraer 170 and 175 Maintenance Review Board Report, MRB 1621, Revision 10, dated February 23, 2015 to do the actions required by this AD, unless the AD specify otherwise.

Electrical Power - Ground Reference Connection - Retrofit / Rotorcraft Flight Manual - Amendment

MBB-BK117 A-1, MBB-BK117 A-3, MBB-BK117 A-4, MBB-BK117 B-1, MBB-BK117 B-2 and MBB-BK117 C-1 helicopters, all serial numbers.

N/A

ECD ASB-MBB-BK117-90-118 Revision 02 dated 04 May 2009.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
BK117 A-3 RFM, TR 9, dated 22 September 2006.
BK117 A-4 RFM, TR 5, dated 22 September 2006.
BK117 B-1 RFM, TR 6, dated 22 September 2006.
BK117 B-2 RFM, TR 1, dated 22 September 2006.
BK117 C-1 RFM, TR 2, dated 22 September 2006.
BK117 C-1C RFM, TR 1, dated 22 September 2006.

Tail Rotor Drive - Slider Assembly Pitch Control - Inspection

A109A and A109AII helicopters, all serial numbers

N/A

AgustaWestland BT 109-149 original issue dated 29 May 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Main Rotor Drive - Cross-Bar - Inspection

AS 350 B, BA, BB, B1, B2, B3 and D helicopters, and
AS 355 E, F, F1, F2, N and NP helicopters, and
EC130 B4 and T2 helicopters, all serial numbers

N/A

AH ASB AS350-05.00.84 original issue dated 21 May 2015.
AH ASB AS355-05.00.73 original issue dated 21 May 2015.
AH ASB EC130-05A021 original issue dated 21 May 2015.
AH ASB EC130-05A022 original issue dated 21 May 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Main Rotor Drive - Main Gear Box / Gleason Crown - Inspection / Replacement

EASA AD 2013-0118

N/A

AgustaWestland BT 109EP-128 Rev. A dated 28 May 2013 or Rev. B dated 20 May 2015 or Rev. C dated 26 May 2015.
AgustaWestland BT 109-K-57 Rev. A dated 28 May 2013 or Rev. B dated 20 May 2015 or Rev. C dated 26 May 2015.
AgustaWestland BT 119-058 Rev. A dated 28 May 2013 or Rev. B dated 20 May 2015 or Rev. C dated 26 May 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Flight Controls - Trimmable Horizontal Stabilizer Actuator - Identification / Replacement

Airbus A330-201, A330-202, A330-203, A330-223, A330-223F, A330-243, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes, all manufacturer serial numbers (MSN).
Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340-642 and A340-643 aeroplanes, all MSN.

EASA AD 2013-0144R1

N/A

Airbus SB A330-27-3199 dated 15 July 2014.
Airbus SB A340-27-4190 dated 15 July 2014.
Airbus SB A340-27-5062 dated 15 July 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Doors - Potable Water Service Panel Access Door Latching Mechanism - Modification

Airbus A330-201, A330-202, A330-203, A330-223, A330-243, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342, and A330-343 aeroplanes, all Manufacturer Serial Number (MSN), except those on which Airbus modification (Mod) 201715, or Airbus Mod 201796, or Airbus Mod 201938 has been embodied in production.
Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340-642 and A340-643 aeroplanes, all MSN.

N/A

Airbus SB A330-52-3086 original issue dated 27 April 2012, or Revision 01 dated 25 April 2014.
Airbus SB A340-52-4094 original issue dated 27 April 2012, or Revision 01 dated 25 April 2014.
Airbus SB A340-52-5019 original issue dated 29 May 2012, or Revision 01 dated 25 April 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Time Limits / Maintenance Checks - Maintenance Requirements / Airworthiness Limitations - Implementation

Falcon 7X aeroplanes, all serial numbers.

EASA AD 2009-0254 and 2010-0033

N/A

Dassault Aviation Falcon 7X AMM chapter 5-40 DGT 107838 revision 4, dated 02 February 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Navigation - Attitude Heading Reference System - Modification / Replacement

Northrop Grumman LITEF GmbH LCR-100 Attitude Heading Reference System (AHRS), Part Number (P/N) 145130-2000, P/N 145130-2001, P/N 145130-7000, P/N 145130-7001 and P/N 145130-7100.
These AHRS units are known to be installed on, but not limited to, Pilatus PC-12, Learjet 31A, Cessna 560XL, RUAG (Dornier) 228 series, and PZL Mielec M28 (Sky Truck) aeroplanes; and Bell Helicopter Textron Inc. 412EP, Bell Helicopter Textron Canada 407, and Sikorsky S-76C helicopters.

N/A

Northrop Grumman LITEF SB 145130-0017-845, issue C, dated 14 January 2015, or issue D, dated 1 April 2015, which can be downloaded from the NG LITEF GmbH website.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Power Plant - Turbocharger Hose - Inspection/Replacement

DA 40 D aeroplanes, all serial numbers (S/N), if equipped with a Thielert TAE 125-02-99 engine

N/A

DAI MSB D4-088 dated 30 January 2012.
DAI MSB D4-075/1 dated 30 January 2012 with WI MSB D4-075 Revision 1.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Fuselage - Intermediate Gear Box Fairing - Inspection / Replacement

AS 332 C, AS 332 C1, AS 332 L, AS 332 L1, AS 332 L2 and EC 225 LP helicopters, all serial numbers, if equipped with an Intermediate Gear Box (IGB) fairing Part Number (P/N) 332A24-0303-05XX or P/N 332A24-0303-06XX or P/N 332A08-1391-00 or P/N 332A08-1391-01.

EASA AD 2011-0189-E

N/A

Airbus Helicopters AS332 ASB 53.01.47 Revision 5 dated 09 March 2015.
Airbus Helicopters AS332 SB 53.01.78 original issue dated 09 March 2015.
Airbus Helicopters EC225 ASB 53A001 Revision 5 dated 09 March 2015.
Airbus Helicopters EC225 SB 53-041 original issue 09 March 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Flight Controls - Elevator Tension Control Regulator - Inspection

F28 Mark 0070 and Mark 0100 aeroplanes, all serial numbers

N/A

Fokker Services SBF100-27-095 original issue dated 22 April 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

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FAA Joint Aircraft System Component (JASC)/Air Transport Association (ATA) of America Code: 34, Navigation

Avidyne Corporation (Avidyne) Integrated Flight Displays (IFDs) part number (P/N) 700-00083-() loaded with software release 9.3.1.0 or earlier release (referred to as Model R9-10 inch), P/N 700-00171-() loaded with software release 9.2.5.0 or earlier release (referred to as Model R9-12 inch), and P/N 700-00182-() loaded with software release 10.0.3.0 or earlier release (referred to as Model IFD540). These IFDs are installed on, but not limited to, airplanes that are certificated in any category and are identified in the following:
(1) For Model R9-10 inch: AML STC SA00282BO.
(2) For Model R9-12 inch: Korea Aerospace Industries KC-100 (currently being type validated by the FAA).
(3) For Model IFD540: STC SAA00343BO.

N/A

None

CORRECTION - Air Transport Association (ATA) of America Code 27, Flight Controls.

This AD applies to The Boeing Company Model 777-200, -200LR, -300, and -300ER series airplanes, certificated in any category, as identified in paragraphs (c)(1) and (c)(2) of this AD.
(1) Airplanes having a Variable Number identified in paragraph 1.A., "Effectivity," of Boeing Special Attention Service Bulletin 777-27-0062, Revision 2, dated January 27, 2014.
(2) Airplanes having a date of issuance of the original airworthiness certificate or date of issuance of the original export certificate of airworthiness on or after January 27, 2014.

FAA AD 2007-13-05

N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Boeing Special Attention Service Bulletin 777-27-0062, Revision 2, dated January 27, 2014.
(ii) Reserved.

Air Transport Association (ATA) of America Code 57, Wings

This AD applies to the airplanes identified in paragraphs (c)(1) through (c)(5) of this AD, certificated in any category, all certified models, all serial numbers.
(1) Airbus Model A300 B2-1A, B2-1C, B2K-3C, B2-203, B4-2C, B4-103, and B4-203 airplanes.
(2) Airbus Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes.
(3) Airbus Model A300 B4-605R and B4-622R airplanes.
(4) Airbus Model A300 F4-605R and F4-622R airplanes.
(5) Airbus Model A300 C4-605R Variant F airplanes.

FAA AD 2008-06-18

EASA AD 2012-0203

(3) The following service information was approved for IBR on July 21, 2015.
(i) Airbus Service Bulletin A300-57-6029, Revision 08, dated April 25, 2013.
(ii) Reserved.
(4) The following service information was approved for IBR on April 23, 2008 (73 FR 14670, March 19, 2008).
(i) Airbus Service Bulletin A300-57-0177, Revision 05, dated March 23, 2007.
(ii) Airbus Service Bulletin A300-57-6029, Revision 06, dated March 23, 2007.

Air Transport Association (ATA) of America Code 53, Fuselage

This AD applies to Learjet Inc. Model 45 airplanes, certificated in any category, as identified in Bombardier Recommended Service Bulletin 40-56-03, Revision 1, dated October 15, 2012 (for airplanes having serial numbers (S/Ns) 45-2000 through 45-2120 inclusive, and S/Ns 45-2122 through 45-2130 inclusive); and Bombardier Recommended Service Bulletin 45-56-3, Revision 1, dated October 15, 2012 (for airplanes having S/Ns 45-005 through 45-427 inclusive).

N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Bombardier Recommended Service Bulletin 40-56-03, Revision 1, dated October 15, 2012.
(ii) Bombardier Recommended Service Bulletin 45-56-3, Revision 1, dated October 15, 2012.

Air Transport Association (ATA) of America Code 57, Wings.

This AD applies to all The Boeing Company Model 747-8F and 747-8 series airplanes, certificated in any category.

N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Boeing Special Attention Service Bulletin 747-57-2338, dated January 14, 2014.
(ii) Reserved.

Air Transport Association (ATA) of America Code 35, Oxygen.

This AD applies to the Airbus airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers.
(1) Model A318-111, -112, -121, and -122 airplanes.
(2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes.
(3) Model A320-211, -212, -214, -231, -232, and -233 airplanes.
(4) Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes.

N/A

EASA AD 2013-0278

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Airbus Service Bulletin A320-35-1069, dated April 26, 2013.
(ii) Reserved.

No subject

This AD applies to all Pratt & Whitney Division (PW) PW6122A and PW6124A turbofan engines with high-pressure compressor (HPC) 7th stage integrally bladed (IB) rotor, part number (P/N) 5495637, installed.

N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Pratt & Whitney Division (PW) Engineering Authorization No. 15MM008, Revision A, dated March 24, 2015.
(ii) PW Service Bulletin No. PW6ENG 72-46, dated March 5, 2015.

CORRECTION - Air Transport Association (ATA) of America Code 52, Doors

This AD applies to The Boeing Company airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category.
(1) Model 767-200, -300, -300F, and -400ER series airplanes, as identified in Boeing Service Bulletin 767-52A0100, Revision 3, dated January 19, 2015.
(2) Model 777-200, -200LR, -300, -300ER, and 777F series airplanes, as identified in Boeing Service Bulletin 777-52-0053, Revision 2, dated January 19, 2015.

N/A

service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Boeing Service Bulletin 767-52A0100, Revision 3, dated January 19, 2015.
(ii) Boeing Service Bulletin 777-52-0053, Revision 2, dated January 19, 2015.
(iii) Eaton Service Bulletin 692D100-52-4, Revision 3, dated August 14, 2014.

Air Transport Association (ATA) of America Code 51, Standard Practices/Structures

This AD applies to Fokker Services B.V. Model F.28 Mark 0070 and 0100 airplanes, certificated in any category, all serial numbers

N/A

EASA AD 2013-0140

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Fokker Service Bulletin SBF100-51-021, dated April 23, 2013, including the attachments identified in paragraphs (j)(2)(i)(A) through (j)(2)(i)(E) of this AD.
(A) Fokker Parts List Local SB10051021-XU-B, Revision A, Sequence 1, dated April 10, 2013.
(B) Fokker Parts List Supply SB10051021-XU-B, Revision A, Sequence 1, dated April 10, 2013.
(C) Fokker Parts List Local SB10051021-XU-A, Revision B, Sequence 1, dated April 10, 2013.
(D) Fokker Parts List Supply SB10051021-XU-A, Revision B, Sequence 1, dated April 10, 2013.
(E) Fokker Manual Change Notification MCNM F100-160, dated April 23, 2013.
(ii) Reserved.

Air Transport Association (ATA) of America Code 27, Flight Controls

This AD applies to airplanes specified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category.
(1) ATR-GIE Avions de Transport Régional Model ATR42-500 airplanes having manufacturer serial number (MSN) 671 through 815 inclusive, except MSN 811.
(2) ATR-GIE Avions de Transport Régional Model ATR72-212A airplanes having MSN 769 through 914 inclusive, except MSN 826, 905, 908, and 911

N/A

EASA AD 2012-0064

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) ATR Service Bulletin ATR42-27-0104, Revision 01, dated August 30, 2011.
(ii) ATR Service Bulletin ATR42-27-0105, Revision 01, dated August 30, 2011.
(iii) ATR Service Bulletin ATR72-27-1065, Revision 02, dated August 30, 2011.
(iv) ATR Service Bulletin ATR72-27-1066, Revision 01, dated August 30, 2011.

Air Transport Association (ATA) of America Code 26, Fire protection

This AD applies to Bombardier, Inc. Model DHC-8-400, -401, and -402 airplanes, certificated in any category, serial numbers 4001 through 4424 inclusive.

N/A

TC AD CF-2014-06

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Bombardier Service Bulletin 84-26-15, Revision A, dated January 15, 2014.
(ii) Reserved.

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FAA Air Transport Association (ATA) of America Code 30, Ice and Rain Protection.

This AD applies to all Dassault Aviation Model FALCON 2000EX airplanes, certificated in any category.

N/A

EASA AD 2015-0102-E

None

Air Transport Association (ATA) of America Code 52, Doors

This AD applies to Bombardier, Inc. Model DHC-8-400, -401, and -402 airplanes, certificated in any category, serial numbers 4001 through 4411 inclusive.

N/A

TC AD CF-2014-08

None

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EASA Flight Controls - Rudder Control Pedal Torque Tubes - Inspection / Replacement

F 406 aeroplanes, serial numbers from 0001 to 0098 inclusive

N/A

ASI Aviation SB F406-104 original issue dated 28 July 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Fin Forward Pickup - Inspection

Model PAL 750XL aircraft, S/N all through to 193, 195 and 197.

NZCAA AD DCA/750XL/16A

N/A

Pacific Aerospace Limited Mandatory Service Bulletin (MSB)PACSB/XL/068

Fuel Control - Fuel Control Unit Bellow Leak

Pratt and Whitney Canada (P&WC) - Engine models as listed in the AD

N/A

P&WC SB 14389
P&WC SB 13473

Propellers - Rear Half Hub Dowel Holes - Inspection / Replacement

Model R352/6-123-F/1, R352/6-123-F/2 and R410/6-123-F35 propellers, all serial numbers.
These propellers are known to be installed on, but not limited to, Fokker F27 Mk 050, F27 Mk 0502 and F27 Mk 0604 aeroplanes.

N/A

Dowty Propellers SB F50-61-165 initial issue dated 19 November 2012, or ASB F50-61-A165 Revision 1 dated 12 May 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD

Doors - Jettisoning System of the Pilot and Co-pilot Doors - Functional Check

EC 155 B1 helicopters, all serial numbers delivered after manufacturing before 30 June 2015, and equipped with pilot or co-pilot doors jettisoning system in accordance with Airbus Helicopters modification POST MOD 0752C05, except helicopters on which Aircraft Maintenance Manual (AMM) task 52-11-00-712 was accomplished on both pilot and co-pilot doors since last crew door installation.

N/A

Airbus Helicopters ASB EC155-52A032 revision 0, dated 22 July 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Doors - Cabin Sliding Plug Doors / Emergency Jettisoning System - Inspection

AS 332 C, AS 332 C1, AS 332 L, AS 332 L1 and AS 332 L2 helicopters, all manufacturer serial numbers with a manufacturing date before 14 July 2014 and equipped with cabin sliding plug doors modified in accordance with Airbus Helicopters modification (mod) AL25612 or mod 0725870.
EC 225 LP helicopters, all manufacturer serial numbers with a manufacturing date before 14 July 2014 and equipped with cabin sliding plug doors.

EASA AD 2014-0263R1

N/A

Airbus Helicopters ASB AS332-53.01.86, dated 18 August 2014 or Revision 1 dated 29 June 2015.
Airbus Helicopters ASB EC225-53A048, dated 18 August 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Engine - Front Support Pins - Inspection / Replacement

ARRIEL 1E2 turbo-shaft engines, all serial numbers.
These engines are known to be installed on, but not limited to, Airbus Helicopters Deutschland (formerly Eurocopter Deutschland) MBB-BK117-C1 and MBB-BK117-C2 helicopters.

N/A

Turboméca MSB 292 72 0842 version A dated 25 March 2015 or version B dated 08 July 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Fuselage - Missing Shims Between Longerons and Longeron Joint Fittings

Bombardier Inc. model DHC-8-400, -401 and -402 aeroplanes, serial numbers 4156 through 4453, 4456 and 4457.

N/A

Bombardier Service Bulletin (SB) 84-53-65

Ice and Rain Protection- Full Ice Protection System Tail Rotor Slip Ring - Inspection / Replacement

AB139 and AW139 helicopters, all serial numbers (S/N), if equipped with Full Icing Protection System (FIPS).
Note 1: Helicopters equipped with FIPS and have one of the kits "Partial Removal Arrangement" with Part Number (P/N) from 4G3000F00311 to P/N 4G3000F00319 inclusive are affected by the requirements of this AD.

N/A

AgustaWestland BT 139-404 original issue dated 22 December 2014.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Air - Carburettor Heated Air Intake Box - Modification

DR 400/100, DR 400/120 and DR 400/120D aeroplanes, all serial numbers, if modified in accordance with STC EASA.A.S.01266 (renumbered EASA STC 10014147) at original issue.

N/A

Atelier Chabord SB BS-DR420-12-01 Revision A dated 10 December 2012.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Equipment and Furnishings - VHF Antenna for Emergency Flotation Gear Protection - Installation

EC 225 LP helicopters, all serial numbers, if equipped with an emergency flotation gear and having no antenna installed on the bottom structure, as described in Figure 1 of Alert Service Bulletin (ASB) No EC225-25A086, except helicopters modified in accordance with Airbus Helicopters modification (MOD) 0726840

N/A

Airbus Helicopters (formerly Eurocopter) ASB N° EC225-25A086, dated 11 July 2011.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Engine - Critical Parts - Identification / Replacement

EASA AD 2015-0103 (including correction)

N/A

Rolls-Royce Alert NMSB RB.211-72-AH972 Revision 2 dated 20 July 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
RR Worldwide (WW) Communication WW/11174/2, dated 22 January 2015.
RR WW/11196/1 dated 01 May 2015.

Doors - Aft Cargo Door Frame Forks - Inspection

Airbus A300F4-605R and A300F4-622R aeroplanes, all manufacturer serial numbers (MSN) on which Airbus modification (MOD) 12046 has been embodied in production.
Note: Airbus MOD 12046 has been embodied in production on MSN 0805 and above, except MSN 0836, 0837 and 0838.

N/A

Airbus AOT A52W011-15 original issue dated 23 July 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Tail Rotor - Rotor Blades - Inspection

AS 332 C, AS 332 C1, AS 332 L, and AS 332 L1 helicopters, equipped with tail rotor de-icing installation unit Part Number (P/N) 204ZP01Y01 and tail rotor blade P/N 332A12-0055-XX (where XX represents any dash number) (type A10).

N/A

Airbus Helicopters ASB AS332-05.01.02 original issue, dated 22 July 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Time Limits / Maintenance Checks - Damage Tolerant Airworthiness Limitation Items - ALS Part 2 - Amendment

Airbus A380-841 and A380-842 aeroplanes, all manufacturer serial numbers (MSN).

N/A

Airbus A380 ALS Part 2 variation 4.6 (00L050H152E/C01 Issue 01), approved on 01 July 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Equipment / Furnishings - Portable Oxygen Cylinder in Overhead Stowage - Inspection / Replacement

A300-600 and A310 passenger aeroplanes, all models, all serial numbers (except all-cargo aeroplanes), if equipped with one-frame overhead stowage compartments (OHSC).

EASA AD 2012-0245-E

N/A

Airbus AOT A25W003-12 Revision 1 dated 14 November 2012.
Airbus SB A300-25-6222 original issue dated 25 February 2015.
Airbus SB A310-25-2210 original issue dated 25 February 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Windows - Cabin Windows / Jettisoning System - Inspection

AS 332 and EC 225 LP helicopters, all manufacturer serial numbers equipped with an extraction tape fitted with press-studs on the windows.

N/A

Airbus Helicopters ASB EC225-56A008 original issue, dated 16 July 2015.
Airbus Helicopters ASB AS332-56.00.10 original issue, dated 16 July 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Fuselage - Aft Cargo Door Sill Beam Area - Inspection

Airbus A300-600 and A310 aeroplanes, all certified models, all manufacturer serial numbers on which Airbus modification (mod) 05438 has been embodied in production, except aeroplanes on which Airbus mod 12046 has also been embodied in production.

EASA AD 2014-0097-E

N/A

Airbus AOT A53W005-14 original issue dated 22 April 2014 or Revision 01 dated 29 April 2014.
Airbus SB A300-53-6179 original issue dated 12 December 2014.
Airbus SB A310-53-2139 original issue dated 12 December 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Aircraft Flight Manual - All Engine Operative Rate of Climb Performance - Revision

P.68R aeroplanes, all serial numbers (s/n) up to s/n 480 inclusive.

N/A

Vulcanair S.p.A. SB No. 244 dated 27 April 2015.
Vulcanair S.p.A. AFM NOR10.707-30, rev. 2, dated 23 April 2015.
Vulcanair S.p.A. AFM NOR10.707-30B, rev. 19, dated 23 April 2015.
Vulcanair S.p.A. AFM NOR10.707-30C, rev. 27, dated 23 April 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Wiring / Harness - Collective Lever Wiring Harness - Inspection

MBB-BK117 C-2 helicopters, all serial numbers (s/n) up to s/n 9708 inclusive.

N/A

AHD ASB MBB-BK117 C-2-88A-010 Revision 1 dated 16 April 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Flight Controls - Elevator Control System - Corrosion of the Elevator Control Rod and Elevator Actuating Lever on the Control Column

Viking Air Ltd. (formerly Bombardier Inc.) model DHC-2 Mk. I, DHC-2 Mk. II and DHC-2 Mk. III aeroplanes, all serial numbers

N/A

Viking Air Ltd. Service Bulletin (SB) V2/0005

Ice and Rain Protection - Engine Air Inlet Anti-Ice System - Aircraft Flight Manual - Amendment

Falcon 2000EX aeroplanes, all manufacturer serial numbers.

N/A

None

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FAA Air Transport Association (ATA) of America Code 35, Oxygen This AD applies to transport category airplanes, in passenger-carrying operations, as specified in paragraph (c)(1) or (c)(2) of this AD.
(1) Airplanes that complied with the requirements of AD 2011-04-09, Amendment 39-16630 (76 FR 12556, March 8, 2011).
(2) Airplanes equipped with any chemical oxygen generator installed in any lavatory and are:
(i) Operating under part 121 of the Federal Aviation Regulations (14 CFR part 121); or
(ii) U.S. registered and operating under part 129 of the Federal Aviation Regulations (14 CFR part 129), with a maximum passenger capacity of 20 or greater. N/A
N/A

None FAA Air Transport Association (ATA) of America Code 53, Fuselage This AD applies to The Boeing Company Model 747-400 and -400F series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 747-53A2860, Revision 1, dated March 18, 2014. FAA AD 2013-14-05
N/A

(3) The following service information was approved for IBR on September 1, 2015.
(i) Boeing Alert Service Bulletin 747-53A2860, Revision 1, dated March 18, 2014.
(ii) Reserved.
(4) The following service information was approved for IBR on August 26, 2013 (78 FR 43763, July 22, 2013).
(i) Boeing Alert Service Bulletin 747-53A2860, dated December 4, 2012.
(ii) Reserved. FAA Air Transport Association (ATA) of America Code 29, Hydraulic Power This AD applies to Bombardier, Inc. Model DHC-8-400, -401, and -402 airplanes, certificated in any category, serial numbers 4001 through 4424 inclusive. FAA AD 2015-10-01
N/A

(3) The following service information was approved for IBR on July 14, 2015 (80 FR 32449, June 9, 2015).
(i) Bombardier Service Bulletin 84-29-34, dated May 9, 2013.
(ii) Parker Service Bulletin 82910012-29-431, dated October 22, 2012. FAA Air Transport Association (ATA) of America Code 53, Fuselage This AD applies to The Boeing Company Model 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP series airplanes; certificated in any category, as identified in Boeing Alert Service Bulletin 747-53A2861, dated April 1, 2014. N/A
N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Boeing Alert Service Bulletin 747-53A2861, dated April 1, 2014.
(ii) Reserved. FAA Air Transport Association (ATA) of America Code 53, Fuselage. This AD applies to the airplane models identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, certificated in any category, with Live TV radomes having part number (P/N) 5063-100-XX (XX designates the color option) and a serial number in the range of 001 through 497 inclusive, and modified by supplemental type certificate (STC) ST00788SE.
(1) Airbus Model A318-111 and -112 airplanes.
(2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes.
(3) Airbus Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes. N/A
N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Live TV Service Bulletin A320-53-006, Rev 01, dated September 10, 2014.
(ii) Reserved. FAA Air Transport Association (ATA) of America Code 53, Fuselage This AD applies to the airplanes identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, certificated in any category, all manufacturer serial numbers, except those on which Airbus Modification 160055 or Airbus Modification 160056 has been embodied in production.
(1) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes.
(2) Airbus Model A320-211, -212, -214, -231, -232, and -233 airplanes.
(3) Airbus Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes. N/A
EASA AD 2014-0081

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Airbus Service Bulletin A320-53-1267, Revision 02, dated May 19, 2014.
(ii) Airbus Service Bulletin A320-53-1272, Revision 02, dated May 19, 2014. FAA Air Transport Association (ATA) of America Code 26, Fire Protection This AD applies to all BAE Systems (Operations) Limited Model ATP airplanes, certificated in any category, all manufacturer serial numbers. N/A
EASA AD 2012-0127R1

service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) BAE Systems (Operations) Limited Service Bulletin ATP-26-016, dated October 4, 2011.
(ii) Kidde Graviner Service Bulletin 26-080, Revision 1, dated July 27, 2011. FAA Air Transport Association (ATA) of America Code 57, Wings. This AD applies to The Boeing Company Model 777-200, 777-200LR, 777-300ER, and 777F series airplanes, certificated in any category, as identified in Boeing Service Bulletin 777-57A0097, Revision 1, dated May 4, 2015. N/A
N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Boeing Service Bulletin 777-57A0097, Revision 1, dated May 4, 2015.
(ii) Reserved.

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EASA Time Limits / Maintenance Checks - Engine Critical Parts - Reduction of Cyclic Life Limits

Viper Mk. 521, Mk. 522 and Mk. 601-22 engines, all serial numbers.
These engines are known to be installed on, but not limited to, Beechcraft Corporation (formerly Hawker Beechcraft, Raytheon Aircraft Company, Beech Aircraft Corporation, British Aerospace, Hawker Siddeley) BH.125 and HS.125 Series 1A and 1B, Series 3, 3A/B, 3A/R, 3B/R, 3A/RA, 3B/RA, 3B/RB and 3B/RC, Series 400, 400A, 400B, 401B, 403A(C) and 403B, and Series 600, 600A and 600B aeroplanes.

EASA AD 2012-0243

N/A

Rolls-Royce Alert SB 72-A207, original issue dated January 2015.
Rolls-Royce Alert SB 72-A408 (Circ. A), original issue dated January 2015.
Rolls-Royce Alert SB 72-A408 (Circ. B), original issue dated January 2015.
Rolls-Royce Alert SB 72-A412 (Circ. B), original issue dated January 2015.
Rolls-Royce Alert SB 72-A413 (Circ. A), original issue dated January 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Windows - Rear Hatch / Jettisoning System - Inspection

SA330 J helicopters, all manufacturer serial numbers, if equipped with an extraction tape fitted with press-studs on the emergency exit rear hatch.

N/A

Airbus Helicopters ASB SA330-56.02 original issue, dated 10 August 2015. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Windows - Cabin Windows / Jettisoning System - Inspection

EC 155 B and B1 helicopters, all manufacturer serial numbers, if equipped with an extraction tape fitted with press-studs on the emergency exit windows.

N/A

Airbus Helicopters ASB EC155-56A006 original issue, dated 10 August 2015. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Doors - Sliding / Plugging Cabin Doors - Limitation / Modification / Inspection

AS 332 C, AS 332 C1, AS 332 L, AS 332 L1, AS 332 L2 and EC 225 LP helicopters, all serial numbers, if equipped with one or two cabin lateral sliding and plugging doors incorporating a sliding lateral plug door fitting Part Number (P/N) 332A223314.00 or P/N 332A221366.06 or P/N 332A090856.02.

EASA AD 2012-0111

N/A

Eurocopter AS332 ASB No. 01.00.79 Revision 1 dated 06 June 2012 and
Airbus Helicopters AS332 ASB No. 01.00.79 Revision 2 dated 23 June 2015.
Eurocopter EC225 ASB No. 04A007 Revision 1, dated 06 June 2012, and Airbus Helicopters EC225 ASB No. 04A007 Revision 2, dated 23 June 2015.
Airbus Helicopters SB AS332-52.00.43 original issue, dated 23 June 2015.
Airbus Helicopters SB EC225-52-008 original issue, dated 23 June 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Tail Rotor - Pitch Link Spherical Bearing Accelerated Wear

Bell Helicopter Textron Canada Limited (BHTC) model 429 helicopters, serial numbers 57001 and subsequent.

N/A

BHTC Alert Service Bulletin (ASB) 429-15-16

Exhaust - Thrust Reverser Doors Attachment Lugs - Inspection / Replacement

Mystere-Falcon 50 aeroplanes, all manufacturer serial numbers.

N/A

Dassault Aviation SB F50-541 original issue dated 24 September 2014, or Revision 1 dated 12 May 2015.
Dassault Aviation Master Minimum Equipment List, DTM 824 Revision 6 dated 2 November 2011 and M&O DGT85583 Revision 2 dated 02 September 2011 Dassault Aviation Master Minimum Equipment List, DTM 824EX Revision 2 dated 25 March 2010 and M&O DTM610 Revision 2 dated 25 March 2010.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
Dassault Aviation AMM task 78-31-00-250-802, as per Mystère-Falcon 50 AMM revision 26, dated October 2014.
Dassault Aviation AMM task 78-30-00-910-809, as per Mystère-Falcon 50 AMM revision 26, dated October 2014.

Main Rotor - Swashplate Assembly - Replacement / Inspection

MBB-BK117 A-1, MBB-BK117 A-3, MBB-BK117 A-4, MBB-BK117 B-1, MBB-BK117 B-2, MBB-BK117 C-1, MBB-BK117 C-2 and MBB-BK117 C-2e helicopters, all serial numbers (s/n), and
BO105 A, BO105 C, BO105 D, BO105 S and BO105 LS A-3 helicopters, all variants, all s/n.

EASA AD 2014-0180R1

N/A

AHD ASB MBB-BK117-40A-115 original issue dated 31 March 2014, or Revision 1 dated 04 August 2014, and Revision 2 dated 30 July 2015.
AHD ASB MBB-BK117C-2-62A-007 original issue dated 31 March 2014, revision 01 dated 04 August 2014, and Revision 2 dated 30 July 2015.
AHD ASB BO105-40A-107 original issue dated 31 March 2014, or Revision 1 dated 08 September 2014, and Revision 2 dated 30 July 2015.
AHD ASB BO105LS-40A-12 original issue dated 31 March 2014, or Revision 1 dated 08 September 2014, and Revision 2 dated 30 July 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Wing Structure and Fuselage Attachment - Revised Airworthiness Limitations

Model R 2100, R 2100 A, R 2112, R 2120 U and R 2160 D aircraft, S/N 001 through to 378.
Model R 2160 aircraft, S/N 001 though to 378 and S/N 160A-06001 onwards.
Model R 2160i aircraft, S/N 001 through to 378 and S/N 160Ai-07007 onwards

N/A

Section 3.2 - Airworthiness Limitations of Service Manuals AAA079 and AAA080

Equipment / Furnishings - Overhead Stowage Compartment Attachments - Modification

Airbus A321-211 and A321-231 aeroplanes, manufacturer serial numbers 3191, 3217, 3241, 3251, 3267, 3334, 3459, 3493, 3507, 3552, 3566, 3587, 3645, 3681, 3764, 3784, 3847, 3867, 3920, 3934, 3938, 3951, 3981, 4058, 4074, 4099, 4103, 4116, 4148, 4184, 4189, 4194, 4217, 4224, 4230, 4266, 4271, 4274, 4292, 4299, 4338, 4341, 4369, 4387, 4416, 4430, 4461 and 4500.

N/A

Airbus SB A320-25-1852 original issue dated 24 September 2012.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Oxygen - Chemical Oxygen Generators - Replacement

EASA AD 2014-0275R1

N/A

Airbus AOT A35N006-14 dated 10 December 2014, or Revision 01 dated 17 June 2015.
B/E Aerospace SB 117042-35-001 original issue dated 10 December 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
B/E Aerospace SIL D1019-01 Revision 1, dated 03 January 2000, provides instructions for the activation and the disposal of a removed generator.

Fin Forward Pickup - Inspection

Model PAL 750XL aircraft, S/N all through to 193, 195 and 197.

NZCAA AD DCA/750XL/16A

N/A

Pacific Aerospace Limited Mandatory Service Bulletin (MSB) PACSB/XL/068

Engine - Accessory Gear Box Module M01 - Inspection / Replacement

ARRIEL 2B, 2B1, 2B1A, 2B1B, 2C, 2C1, 2C2, 2D, 2E, 2N, 2S1 and 2S2 engines, all serial numbers.
These engines are known to be installed on, but not limited to, Airbus Helicopters AS350B3, EC130B4, EC130T2, AS365N3, EC155B and EC155B1, Airbus Helicopters Deutschland MBB-BK 117 D-2 (EC145T2 or H145), Avic international AC311 and Sikorsky S-76C helicopters.

N/A

Turboméca MSB 292 72 2861 version A dated 24 April 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD

Doors - Jettison System Adhesive Seal - Removal

MBB-BK 117 A-3, MBB-BK 117 A-4, MBB-BK 117 B-1, MBB-BK 117 B-2 and MBB-BK 117 C-1 helicopters, all serial numbers.

N/A

AHD ASB MBB-BK117-20A-114 Revision 1 dated 30 July 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Wings - Movable Flap Track Fairing (MFTF) #6 - Inspection / Replacement / Modification

Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers on which Airbus modification (mod) 68729 or mod 71589 has been embodied in production, or Airbus Service Bulletin (SB) A380-57-8017 or SB A380-57-8036 has been embodied in service, except aeroplanes on which Airbus mod 74424 has been embodied in production.

EASA AD 2011-0002R1

N/A

Airbus SB A380-57A8032 original issue dated 26 November 2010.
Airbus SB A380-57-8017 original issue dated 05 June 2009.
Airbus SB A380-57-8036 original issue dated 13 July 2012.
Airbus SB A380-57-8096 original issue dated 16 April 2014.
Airbus SB A380-57-8093 original issue, dated 10 December 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Stabilizers - Tailplane Lower Fitting - Inspection / Replacement

AW 189 helicopters, all serial numbers, if equipped with tailplane lower fitting Part Number (P/N) 8G5350A07051, which is part of tailplane lower fitting assembly P/N 8G5350A06731.

N/A

AgustaWestland BT 189-038 original issue, dated 05 August 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Power Plant - Engine Fan Cowl Panel Dislodgement During Flight

Bombardier Inc. model CL-600-2B19 aeroplanes.

N/A

Service Bulletin (SB) 601R-71-034

Equipment / Furnishings - Hoist - Test / Replacement

This AD applies to the following helicopters, when equipped with a Goodrich hoist having a Part Number (P/N) as listed in Table 1 of this AD:
AW109SP, AB139, AW139, AB412 and AW189 (all Models) helicopters, all serial numbers (s/n); BHTI 212, 214 and 412 helicopters, all Models, all s/n; BHTC 429 and 430 helicopters, all s/n; AH AS 365 N3, AS 332 L2, EC225 LP and EC175 B helicopters, all s/n; AHD MBB-BK117 C-2 and D-2, EC135 and EC635 (all Models) helicopters, all s/n; MDHI MD900 helicopters, all s/n; and Sikorsky S-61 (all Models), S-76A, S-76B, S-76C and S-92A helicopters, all s/n.

EASA AD 2015-0069 (including Correction)

FAA AD 2013-06-51

AHD ASB No. MBB-BK117 C-2-85A-038, Revision 4, dated 10 June 2015.
AHD ASB No. MBB-BK117 D-2-85A-004, original issue, dated 10 June 2015.
AHD ASB No. EC135-85A-058, Revision 5, dated 10 June 2015.
AH ASB No. AS365-25.01.25, Revision 5, dated 10 June 2015.
AH ASB No. AS332-25.02.70, Revision 5, dated 10 June 2015.
AH ASB No. EC225-25A133, Revision 5, dated 10 June 2015.
AgustaWestland BT 139-430, original issue, dated 11 June 2015.
AgustaWestland BT 109-095, original issue, dated 11 June 2015.
AgustaWestland BT 189-028, original issue, dated 11 June 2015.
Bell Helicopter Textron Canada Ltd.: None.
Bell Helicopter Textron, Inc.: None.
MD Helicopters, Inc.: None.
Sikorsky Aircraft Corporation: None.

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Air Transport Association (ATA) of America Code 21, Air Conditioning This AD applies to The Boeing Company airplanes, certificated in any category, as identified in paragraphs (c)(1) and (c)(2) of this AD.
(1) Model 737-100, -200, -200C, -300,-400, and -500 series airplanes, as identified in Boeing Special Attention Service Bulletin 737-21-1164, Revision 2, dated August 23, 2013.
(2) Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes, as identified in Boeing Special Attention Service Bulletin 737-21-1165, Revision 3, dated July 16, 2014. FAA AD 2012-19-11
N/A

(3) The following service information was approved for IBR on September 15, 2015.
(i) Boeing Alert Service Bulletin 737-31A1325, Revision 2, dated June 5, 2014.
(ii) Boeing Alert Service Bulletin 737-31A1332, Revision 4, dated October 31, 2013.
(iii) Boeing Special Attention Service Bulletin 737-21-1164, Revision 2, dated August 23, 2013.
(iv) Boeing Special Attention Service Bulletin 737-21-1165, Revision 3, dated July 16, 2014.
(4) The following service information was approved for IBR on November 7, 2012 (77 FR 60296, October 3, 2012).
(i) Boeing Alert Service Bulletin 737-31A1325, dated January 11, 2010.
(ii) Boeing Alert Service Bulletin 737-31A1332, Revision 1, dated June 24, 2010.
(iii) Boeing Alert Service Bulletin 737-31A1332, Revision 2, dated August 18, 2011.
(iv) Boeing Alert Service Bulletin 737-31A1332, Revision 3, dated March 28, 2012.
(v) Boeing Special Attention Service Bulletin 737-21-1164, Revision 1, dated May 17, 2012.
(vi) Boeing Special Attention Service Bulletin 737-21-1165, Revision 1, dated July 16, 2010.
(vii) Boeing Special Attention Service Bulletin 737-21-1165, Revision 2, dated April 30, 2012. Air Transport Association (ATA) of America Code 05, Time Limits/Maintenance Checks This AD applies to Airbus Model A330-201, -202, -203, -223, -243, -223F, -243F, -301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes; certificated in any category; all manufacturer serial numbers. FAA ADs listed in paragraphs (b)(1) through (b)(2)
EASA AD 2013-0268

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Airbus A330 Airworthiness Limitations Section ALS Part 4-Aging Systems Maintenance, Revision 04, dated August 27, 2013.
(ii) Airbus A330 ALS Part 4-Aging Systems Maintenance (ASM), Variation 4.1, dated July 23, 2014.
(iii) Airbus A330 ALS Part 4-Aging Systems Maintenance (ASM), Variation 4.2, dated July 23, 2014. No subject This AD applies to all Rolls-Royce plc (RR) RB211-524B-02, RB211-524B2-19, RB211-524B3-02, RB211-524B4-02, RB211-524B4-D-02, RB211-524C2-19, RB211-524D4-19, RB211-524D4-39, and RB211-524D4X-19 turbofan engines with high-pressure turbine (HPT) blades, part numbers (P/Ns) UL32958 and UL21691, installed. N/A
EASA AD 2014-0250

None Air Transport Association (ATA) of America Code 26, Fire Protection This AD applies to Kidde Graviner hand-operated fire extinguishers having part numbers 56412-001 (34H), 56411-001 (35H), and 56412-002 (38H). These fire extinguishers may be installed on, but not limited to, aircraft, certificated in any category, specified in paragraphs (c)(1), (c)(2), (c)(3), (c)(4), (c)(5), and (c)(6) of this AD.
(1) BAE Systems (Operations) Limited Model ATP airplanes.
(2) BAE Systems (Operations) Limited Model 4101 airplanes.
(3) Airbus Defense and Space S.A. (Type Certificate previously held by EADS CASA; Construcciones Aeronauticas, S.A.) Model C-212-CB, C-212-CC, C-212-CD, C-212-CE, C-212-CF, C-212-DE, and C-212-DF airplanes.
(4) Fokker Services B.V. Model F.27 Mark 050, 100, 200, 300, 400, 500, 600, and 700 airplanes.
(5) Short Brothers PLC Model SD3-60 SHERPA, SD3-SHERPA, SD3-30, and SD3-60 airplanes.
(6) SHORT BROTHERS & HARLAND LTD SC-7 Series 2 and SC-7 Series 3 airplanes. N/A
EASA AD 2012-0037

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Kidde Graviner Alert Service Bulletin A26-081, Revision 1, dated January 31, 2012. Page 2 of this document is dated August 23, 2011.
(ii) Reserved. Air Transport Association of America (ATA) Code 32: Landing Gear This AD applies to British Aerospace Regional Aircraft Jetstream Series 3101 and Jetsream Model 3201 airplanes, all serial numbers, certificated in any category. N/A
EASA AD 2015-0061

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) British Aerospace Jetstream Series 3100 & 3200 Service Bulletin 57-JA120141, REVISION 1, dated April 8, 2014.
(ii) Reserved. Air Transport Association of America (ATA) Code 57: Wings This AD applies to British Aerospace Regional Aircraft Jetstream Model 3201 airplanes, all serial numbers, that are:
(1) Certificated in any category; and
(2) Modified in service following BAE Systems (Operations) Ltd Service Bulletin (SB) 05- JM8229. N/A
EASA AD 2015-0063

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) British Aerospace Regional Aircraft British Aerospace Jetstream Series 3100 & 3200 Service Bulletin 57-JA140140, Original Issue, dated: June 26, 2014.
(ii) Reserved. Air Transport Association (ATA) of America Code 27, Flight Controls This AD applies to the airplanes, certificated in any category, identified in paragraphs (c)(1) and (c)(2) of this AD.
(1) Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700, 701, & 702) airplanes, serial numbers (S/N) 10002 through 10337 inclusive.
(2) Bombardier, Inc. Model CL-600-2D15 (Regional Jet Series 705) and CL-600-2D24 (Regional Jet Series 900) airplanes, S/Ns 15001 through 15298 inclusive. N/A
TC AD CF-2014-44

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Bombardier Service Bulletin 670BA-27-062, Revision C, dated February 13, 2015.
(ii) Reserved. Air Transport Association (ATA) of America Code 27, Flight Controls This AD applies to the Airbus airplanes, certificated in any category, identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, all manufacturer serial numbers on which Airbus modification (mod) 160500 or mod 160023 has been embodied in production, and those that have been modified in service through the Airbus Service Bulletin A320-57-1173, A320-57-1186, or A320-57-1187, except those on which Airbus mod 156108 has been embodied in production.
(1) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes.
(2) Model A320-211, -212, -214, -231, -232, and -233 airplanes.
(3) Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes. N/A
EASA AD 2014-0186

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Airbus Service Bulletin A320-27-1240, dated June 18, 2014.
(ii) Reserved. Air Transport Association (ATA) of America Code 57, Wings This AD applies to Airbus Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, and B4-622R airplanes, Model A300 F4-605R and F4-622R airplanes, and Model A300 C4-605R Variant F airplanes, certificated in any category, except those on which Airbus Modification 8608 is incorporated in production. FAA AD 98-18-02
EASA AD 2012-0194

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Airbus Service Bulletin A300-57-6027, Revision 07, dated June 6, 2011.
(ii) Airbus Service Bulletin A300-57-6033, Revision 02, dated September 19, 2011.

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FAA Air Transport Association (ATA) of America Code 21, Air Conditioning

This AD applies to The Boeing Company airplanes, certificated in any category, as identified in paragraphs (c)(1) and (c)(2) of this AD.
(1) Model 737-100, -200, -200C, -300,-400, and -500 series airplanes, as identified in Boeing Special Attention Service Bulletin 737-21-1164, Revision 2, dated August 23, 2013.
(2) Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes, as identified in Boeing Special Attention Service Bulletin 737-21-1165, Revision 3, dated July 16, 2014.

FAA AD 2012-19-11

N/A

Air Transport Association (ATA) of America Code 05, Time Limits/Maintenance Checks

This AD applies to Airbus Model A330-201, -202, -203, -223, -243, -223F, -243F, -301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes; certificated in any category; all manufacturer serial numbers.

FAA ADs listed in paragraphs (b)(1) through (b)(2)

EASA AD 2013-0268

No subject

This AD applies to all Rolls-Royce plc (RR) RB211-524B-02, RB211-524B2-19, RB211-524B3-02, RB211-524B4-02, RB211-524B4-D-02, RB211-524C2-19, RB211-524D4-19, RB211-524D4-39, and RB211-524D4X-19 turbofan engines with high-pressure turbine (HPT) blades, part numbers (P/Ns) UL32958 and UL21691, installed.

N/A

EASA AD 2014-0250

None

Air Transport Association (ATA) of America Code 26, Fire Protection

This AD applies to Kidde Graviner hand-operated fire extinguishers having part numbers 56412-001 (34H), 56411-001 (35H), and 56412-002 (38H). These fire extinguishers may be installed on, but not limited to, aircraft, certificated in any category, specified in paragraphs (c)(1), (c)(2), (c)(3), (c)(4), (c)(5), and (c)(6) of this AD.
(1) BAE Systems (Operations) Limited Model ATP airplanes.
(2) BAE Systems (Operations) Limited Model 4101 airplanes.
(3) Airbus Defense and Space S.A. (Type Certificate previously held by EADS CASA; Construcciones Aeronauticas, S.A.) Model C-212-CB, C-212-CC, C-212-CD, C-212-CE, C-212-CF, C-212-DE, and C-212-DF airplanes.
(4) Fokker Services B.V. Model F.27 Mark 050, 100, 200, 300, 400, 500, 600, and 700 airplanes.
(5) Short Brothers PLC Model SD3-60 SHERPA, SD3-SHERPA, SD3-30, and SD3-60 airplanes.
(6) SHORT BROTHERS & HARLAND LTD SC-7 Series 2 and SC-7 Series 3 airplanes.

N/A

EASA AD 2012-0037

Air Transport Association of America (ATA) Code 32: Landing Gear

This AD applies to British Aerospace Regional Aircraft Jetstream Series 3101 and Jetsream Model 3201 airplanes, all serial numbers, certificated in any category.

N/A

EASA AD 2015-0061

Air Transport Association of America (ATA) Code 57: Wings

This AD applies to British Aerospace Regional Aircraft Jetstream Model 3201 airplanes, all serial numbers, that are:
(1) Certificated in any category; and
(2) Modified in service following BAE Systems (Operations) Ltd Service Bulletin (SB) 05- JM8229.

N/A

EASA AD 2015-0063

Air Transport Association (ATA) of America Code 27, Flight Controls

This AD applies to the airplanes, certificated in any category, identified in paragraphs (c)(1) and (c)(2) of this AD.
(1) Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700, 701, & 702) airplanes, serial numbers (S/N) 10002 through 10337 inclusive.
(2) Bombardier, Inc. Model CL-600-2D15 (Regional Jet Series 705) and CL-600-2D24 (Regional Jet Series 900) airplanes, S/Ns 15001 through 15298 inclusive.

N/A

TC AD CF-2014-44

Air Transport Association (ATA) of America Code 27, Flight Controls

This AD applies to the Airbus airplanes, certificated in any category, identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, all manufacturer serial numbers on which Airbus modification (mod) 160500 or mod 160023 has been embodied in production, and those that have been modified in service through the Airbus Service Bulletin A320-57-1173, A320-57-1186, or A320-57-1187, except those on which Airbus mod 156108 has been embodied in production.
(1) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes.
(2) Model A320-211, -212, -214, -231, -232, and -233 airplanes.
(3) Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes.

N/A

EASA AD 2014-0186

Air Transport Association (ATA) of America Code 57, Wings

This AD applies to Airbus Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, and B4-622R airplanes, Model A300 F4-605R and F4-622R airplanes, and Model A300 C4-605R Variant F airplanes, certificated in any category, except those on which Airbus Modification 8608 is incorporated in production.

FAA AD 98-18-02

EASA AD 2012-0194

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EASA Rotor Drive - Main Gearbox Lubrication Pump - Inspection / Replacement

AS 355 E, AS 355 F, AS 355 F1, AS 355 F2 and AS 355 N helicopters, all serial numbers, equipped with lubrication pumps Part Number (P/N) 355A32-0700-01, P/N 355A32-0700-02 or P/N 355A32-0701-00, installed on the main gearbox (MGB), except those modified in accordance with Airbus Helicopters modification (mod) 077222.

EASA AD 2006-0378-E

N/A

Eurocopter AS355 ASB No. 05.00.40 Revision 2 dated 20 December 2006, or Revision 3 dated 09 July 2007.
Eurocopter AS355 ASB No. 05.00.51 original issue dated 09 July 2007, or Airbus Helicopters AS355 ASB No. 05.00.51 Revision 1 dated 29 July 2015.
Airbus Helicopters SB No. AS355-63.00.25 original issue dated 24 March 2015, or Revision 1 dated 29 July 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Engine - Low Pressure Turbine Roller Bearing - Replacement

RB211-22B-02, RB211-524B-02, RB211-524B-B-02, RB211-524B2-19, RB211-524B2-B-19, RB211-524B3-02, RB211-524B4-02, RB211-524B4-D-02, RB211-524C2-19, RB211-524C2-B-19, RB, RB211-524D4-19, RB211-524D4-B-19, RB211-524D4X-19, RB211-524D4X-B-19, RB211-524D4-39, RB211-524D4-B-39, RB211-524G2-19, RB211-524G3-19, RB211-524-G2-T-19, RB211-524G3-T-19, RB211-524H-36, RB211-524H2-19, RB211-524H-T-36 and RB211-524H2-T-19 engines, all serial numbers.
These engines are known to be installed on, but not limited to, Lockheed Martin Corporation L-1011 (TriStar), Boeing 747 and Boeing 767 aeroplanes.

N/A

Rolls-Royce NMSB RB.211-72-AG729 original issue dated 1 August 2011.
Rolls-Royce NMSB RB.211-72-AG800 original issue dated 5 March 2012.
Rolls-Royce SB RB.211-72-B540 original issue dated 28 July 1995.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Main Rotor - Swashplate and Support Assembly Nuts - Inspection / Replacement

AB412 and AB412EP helicopters, all serial numbers (S/N)

N/A

AgustaWestland BT 412-143 original issue, dated 07 September 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Oxygen - Oxygen System Flexible Hose - Incorrect Burst Pressure

Bombardier Inc. model BD-700-1A10 and BD-700-1A11 aeroplanes, serial numbers (S/Ns) 9002 through 9704 and 9998.

N/A

Bombardier SB 700-35-013
Bombardier SB 700-35-6001
Bombardier SB 700-1A11-35-012
Bombardier SB 700-35-5001

Fuel - Chaffing of the Auxiliary Power Unit Negative-G Fuel Feed Drain Line

Bombardier Inc:
Model CL-600-2A12 (601 Variant) aeroplanes, serial numbers 3001 through 3066;
Model CL-600-2B16 (601-3A/3R Variants) aeroplanes, serial numbers 5001 through 5194;
Model CL-600-2B16 (604 Variant) aeroplanes, serial numbers 5301 through 5665, and 5701 through 5970.

N/A

Bombardier SB 601-0640
Bombardier SB 604-28-021
Bombardier SB 605-28-009

Hydraulic Power - No. 3 Hydraulic System Reservoir Leak

Bombardier Inc.:
Model CL-600-2C10 aeroplanes, serial numbers 10002 through 10999;
Model CL-600-2D15 and CL-600-2D24 aeroplanes, serial numbers 15001 through 15990; and
Model CL-600-2E25 aeroplanes, serial numbers 19001 through 19990
equipped with No. 3 hydraulic system reservoir with part number (P/N) 960450-1.

N/A

Bombardier SB 670BA-29-018

Engine Controls - Engine Control Cables - Inspection / Replacement

BN2, BN2A and BN2B (piston engine) "Islander" aeroplanes, all models, all serial numbers, and BN2A MARK III "Trislander" aeroplanes, all models, all serial numbers.

EASA AD 2013-0263

N/A

Britten-Norman Aircraft Limited SB 334 Issue 1 dated 30 August 2013, and Issue 2 dated 17 July 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Landing Gear - Nose Landing Gear - Inspection / Replacement

PS-28 Cruiser aeroplanes, all manufacturer serial numbers.

EASA AD 2015-0109-E

N/A

Czech Sport Aircraft a.s. SB-CR-016 Revision 6 dated 31 August 2015.
Czech Sport Aircraft a.s. SB-CR-021 original issue dated 10 July 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Equipment / Furnishings - Passenger / Crew and Emergency Exit Door Slide and Slide Raft Attachments - Inspection

Airbus A330-201, A330-202, A330-203, A330-223, A330-223F, A330-243, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes, all manufacturer serial numbers (MSN), and
Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340-642 and A340-643 aeroplanes, all MSN,
except those aeroplanes where all escape slides and slide rafts installations have passed an inspection in accordance with the instructions of the applicable Airbus Maintenance Planning Document Task 25-62-41-02-1 or Airbus Maintenance Review Board Report Maintenance Schedule Item 25.62.00.

N/A

Airbus AOT A25L004-15 original issue, dated 24 August 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Landing Gear - Main Landing Gear Bogie Beam - Inspection / Repair

Airbus A330-201, A330-202, A330-203, A330-223, A330-223F, A330-243, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342, and A330-343 aeroplanes, all manufacturer serial numbers (MSN) except those that have embodied Airbus modification (mod) 204421 in production, and
Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340-642, and A340-643 aeroplanes, all MSN except those that have embodied Airbus mod 204421 in production.

EASA AD 2011-0211

N/A

Airbus SB A330-32-3220 at original issue dated 10 October 2008, or Revision 01 dated 05 October 2011, or Revision 02 dated 13 December 2012.
Airbus SB A330-32-3248 at original issue dated 05 October 2011, or Revision 01 dated 13 December 2012.
Airbus SB A340-32-4264 at original issue dated 10 October 2008.
Airbus SB A340-32-4286 at original issue dated 05 October 2011.
Airbus SB A340-32-5087 at original issue dated 10 October 2008.
Airbus SB A340-32-5112 at original issue dated 24 October 2013.
Airbus SB A330-32-3268 at original issue dated 20 April 2015.
Airbus SB A340-32-4300 at original issue dated 20 April 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Fire Protection - Engine Fire Extinguisher System - Modification

AS 355 NP helicopters, all serial numbers, if equipped with the ARRIUS 1A1 engine fire extinguishing system through production modification (mod) OP- 3931, except those incorporating Airbus Helicopters (AH) mod 07-3990.

EASA AD 2011-0192-E

N/A

Eurocopter AS355NP Emergency ASB No 26.00.09 original issue, dated 15 September 2011.
Airbus Helicopters ASB No. AS355-26.00.10 original issue, dated 02 July 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Flight Controls - Control Stick - Inspection / Replacement

MDM-1 "Fox" and MDM-1P "Fox-P" sailplanes, all serial numbers.

EASA AD 2011-0210-E

N/A

Zaklady Lotnicze Marganski & Myslowski SB No. BO-17/2011 MDM-1 FOX Revision 1 dated 05 August 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

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FAA No subject

This AD applies to all Rolls-Royce plc (RR) RB211 Trent 768-60, 772-60, and 772B-60 turbofan engines, if fitted with fuel tube, part number (P/N) FW53576, which was incorporated through RR production modification 73-F343 or which were modified in service in accordance with RR Service Bulletin (SB) No. RB.211-73-F343, Revision 4, dated May 26, 2011.

N/A

EASA AD 2014-0243R1

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Rolls-Royce plc (RR) Alert Non-Modification Service Bulletin (NMSB) No. RB.211-73-AH522, Revision 2, dated July 18, 2014.
(ii) RR NMSB No. RB.211-73-AH837, dated September 9, 2014.

No subject

This AD applies to CFM International S.A. (CFM) CFM56-7B and CFM56-3 engines with a 73-tooth or 41-tooth gearshaft installed in the accessory gearbox (AGB), that has a gearshaft serial number in Appendix A or Appendix B of CFM Service Bulletin (SB) No. CFM56-7B S/B 72-0964, Revision 1, dated December 15, 2014

N/A

(3) The following service information was approved for IBR on October 20, 2015.
(i) CFM International Service Bulletin No. CFM56-7B S/B 72-0964, Revision 1, dated December 15, 2014.
(ii) Reserved.

Air Transport Association (ATA) of America Code 57, Wings

This AD applies to Airbus Model A320-211 and -231 airplanes, certificated in any category, all manufacturer serial numbers (MSN) up to MSN 0084 inclusive.

FAA AD 97-07-14

EASA AD 2014-0053

(i) Airbus Service Bulletin A320-57-1175, Revision 01, including Appendix 01, dated May 28, 2014.
(ii) Reserved.
(4) The following service information was approved for IBR on May 12, 1997 (62 FR 16473, April 7, 1997).
(i) Airbus Service Bulletin A320-57-1013, Revision 1, dated September 29, 1992.
Note 1 to paragraph (n)(4)(i): Airbus Service Bulletin A320-57-1013, Revision 1, dated September 29, 1992, contains the following list of effective pages: Pages 1 through 3 show revision level 1, dated September 29, 1992; pages 4 through 11 are from the original issue, dated April 12, 1989.
(ii) Reserved

Air Transport Association (ATA) of America Code 28, Fuel.

This AD applies to The Boeing Company Model 777-200, -200LR, -300, -300ER, and 777F series airplanes, certificated in any category, line numbers 1 through 1164 inclusive.

N/A

None

Joint Aircraft System Component (JASC) Code 28, Fuel.

This AD applies to all The Boeing Company Model 767-200, -300, -300F, and -400ER series airplanes, certificated in any category.

N/A

None

Joint Aircraft System Component (JASC) Code 2823, Fuel Selector/Shutoff Valve.

This AD applies to all The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes, certificated in any category.

N/A

None

Air Transport Association (ATA) of America Code 28, Fuel.

This AD applies to all The Boeing Company Model 757-200, -200PF, -200CB, and -300 series airplanes, certificated in any category

N/A

None

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EASA Airplane Flight Manual - Section Normal Procedures / After Start - Amendmen

N/A

Airbus AFM TR 572 Issue 1, approved 19 August 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Equipment / Furnishings - External Life Raft Jettison System / Inflation Cylinder Percussion System / Bellcrank - Inspection

EC 225 LP helicopters, all manufacturer serial numbers delivered before 16 August 2015, if equipped with life rafts installed in the multi-purpose sponsons, except helicopters that successfully passed Aircrfat Maintenance Manual (MMA) Task 25-66-01-0821 (adjustment - ground testing of the life raft percussion control POST MOD 0726590) on both left hand (LH) and right hand (RH) sides.

N/A

Airbus Helicopters EC225 Emergency ASB 25A181 Original issue dated 25 September 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Landing Gear - Nose Landing Gear (NLG) Retraction Actuator - Overhaul

Airbus A330-201, A330-202, A330-203, A330-223, A330-223F, A330-243, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes, all manufacturer serial numbers (MSN), and
Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all MSN.

N/A

Airbus SB A330-32-3255 original issue, dated 13 October 2011.
Airbus SB A340-32-4291 original issue, dated 13 October 2011.
Airbus A330 MRBR at Revision 14, published in June 2013.
Airbus A340 MRBR at Revision 14, published in June 2013.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Tail Rotor Drive - Drive Shaft Bearings - Inspection / Replacement

AS 350 B, BA, BB, B1, B2, B3 and D helicopters, and AS 355 E, F, F1, F2, N and NP helicopters, all serial numbers, if equipped with tail rotor (TR) drive shaft bearings as indicated in Table 1 of this AD.

DGAC France ADs 98-173-073(A) and 82-078-005(A)R5

N/A

Eurocopter AS350 SB 05.00.08 Revision 5 dated 02 February 1998.
Eurocopter AS355 SB 05.00.02 Revision 5 dated 02 February 1998.
Airbus Helicopters ASB AS350-01.00.70 original issue dated 06 July 2015, or Revision 1 dated 21 September 2015.
Airbus Helicopters ASB AS355-01.00-57 original issue dated 06 July 2015, or Revision 1 dated 21 September 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Fuel - Fuel Pumps - Inspection / Modification

Airbus A330-201, A330-202, A330-203, A330-223, A330-243, A330-223F, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes, all manufacturer serial numbers (MSN), and
Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340-642 and A340-643 aeroplanes, all MSN.

N/A

Airbus SB A330-28-3127 original issue dated 14 July 2015.
Airbus SB A340-28-4138 original issue dated 14 July 2015.
Airbus SB A340-28-5060 original issue dated 14 July 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Propeller - Fastening Bolts and Nuts - Inspection / Replacement

L 13 SW Vivat and L 13 SE Vivat powered sailplanes, all manufacturer serial numbers.

N/A

Evektor s.r.o. MSB No SW13-065a Revision 1 dated 24 August 2015,
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
Parma – Technik s.r.o. BB No. MIII SAB-002/2015 dated 20 August 2015.

Doors - Forward and Aft Cargo Compartment Doors - Inspection

Airbus A330-201, A330-202, A330-203, A330-223, A330-223F, A330-243, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes, all manufacturer serial numbers (MSN), and
Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340-642 and A340-643 aeroplanes, all MSN,
except those that have embodied Airbus modification (mod) 202702 and mod 202790 in production

EASAs ADs 2011-0007R1 and 2012-0274

N/A

Airbus SB A330-52-3087 original issue dated 29 August 2013, or Revision 01 dated 09 July 2014.
Airbus SB A340-52-4095 original issue dated 29 August 2013, or Revision 01 dated 09 July 2014.
Airbus SB A340-52-5020 original issue dated 29 August 2013, or Revision 01 dated 09 July 2014.
Airbus SB A330-52-3095 original issue dated 29 August 2013, or Revision 01 dated 28 July 2014.
Airbus SB A340-52-4101 original issue dated 29 August 2013, or Revision 01 dated 03 October 2014.
Airbus SB A340-52-5023 original issue dated 29 August 2013, or Revision 01 dated 28 July 2014.
Airbus AOT A330-52A3084 original issue dated 19 December 2010.
Airbus AOT A330-52A3085 original issue dated 20 December 2010.
Airbus AOT A330-A52L001-12 original issue dated 20 December 2010.
Airbus AOT A330-A52L003-12 original issue dated 03 December 2012.
Airbus AOT A340-52A4091 original issue dated 20 December 2010.
Airbus AOT A340-52A4092 original issue dated 20 December 2010.
Airbus AOT A340-A52L002-12 original issue dated 03 December 2012.
Airbus AOT A340-A52L004-12 original issue dated 03 December 2012.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Time Limits / Maintenance Checks - Airworthiness Limitation Section - Amendment

TAE 125-02-99 (commercial designation CD-135, formerly Centurion 2.0) and
TAE 125-02-114 (commercial designation CD-155, formerly Centurion 2.0S) engines, all serial numbers.
These engines are known to be installed on, but not limited to, the following aeroplane types, mostly through application of a Supplemental Type Certificate (STC):
- Cessna 172 and (Reims-built) F172 series (STC EASA.A.S.01527 or EASA 10014287).
- Piper PA-28 series (STC EASA.A.S.01632 or STC EASA 10014364).
- CEAPR (APEX, Robin) DR 400 series (STC EASA.A.S.01380 or STC EASA 10014219).
- Diamond DA 40 and DA 42 series.

N/A

Operation & Maintenance Manual OM-02-02, Chapter 5, Issue 4, Revision 4, dated 02 September 2015
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Main Rotor - Blades - Inspection

A109A and A109AII helicopters, all serial numbers.

N/A

AgustaWestland BT 109-150 original issue dated 17 September 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Air Conditioning - Electronic Centralized Aircraft Monitoring / Flight Warning System - Software Update / Aircraft Flight Manual Changes

Airbus A380-841, A380-842, and A380-861 aeroplanes, all manufacturer serial numbers, except aeroplanes on which Airbus modification (mod.) 76212 or Airbus mod. 76214 has been embodied in production.

N/A

Airbus SB A380-31-8082 original issue dated 31 July 2015.
Airbus SB A380-31-8083 original issue dated 31 July 2015.
AFM TR 173 Issue 1 dated 17 July 2015.
AFM TR 174 Issue 1 dated 17 July 2015.
AFM TR 179 Issue 1 dated 17 July 2015.
AFM TR 180 Issue 1 dated 17 July 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
FOT 999.0082/15 original issue dated 27 July 2015

Stabilizers - Inboard and Outboard Elevators Hinge Lines - Inspection

Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers (MSN).

N/A

Airbus SB A380-55-8002 original issue, dated 13 May 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
Airbus TD_G1_S4_05612_2013 issue A dated 26 November 2013.
Airbus TD_G15_S4_00195_2014 issue A dated 12 December 2014.
Airbus TD_G15_S4_00237_2015 issue A dated 16 January 2015.
Airbus TD_G15_S4_00225_2015 issue A dated 08 January 2015.
Airbus TD_G15_S4_00213_2014 issue A dated 12 December 2014.
Airbus TD_G15_S4_00207_2014 issue A dated 07 January 2015.
Airbus TD_G1_S4_06050_2014 issue B dated 10 February 2014.
Airbus TD_G1_S4_05613_2013 issue A dated 11 December 2013.
Airbus TD_G1_S4_06829_2014 issue A dated 14 May 2014.
Airbus TD_G1_S4_04696_2013 issue A dated 16 July 2013.
Airbus TD_G1_S4_04619_2013 issue A dated 16 July 2013.
Airbus TD_G15_S4_00214_2014 issue A dated 12 December 2014.
Airbus TD_G15_S4_00297_2015 issue A dated 30 March 2015.

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FAA Air Transport Association (ATA) of America Code 21, Air Conditioning; 31, Instruments

This AD applies to The Boeing Company Model 747-400 and -400F series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 747-21A2523, Revision 2, dated June 7, 2013.

FAA AD 2012-24-10

N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Boeing Alert Service Bulletin 747-21A2523, Revision 2, dated June 7, 2013.
(ii) Boeing Special Attention Service Bulletin 747-21-2532, dated February 13, 2014.
(iii) Boeing Special Attention Service Bulletin 747-21-2533, dated February 13, 2014.

Air Transport Association (ATA) of America Code 27, Flight Controls

This AD applies to the airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers.
(1) Airbus Model A318-111, -112, -121, and -122 airplanes.
(2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes.
(3) Airbus Model A320-211, -212, -214, -231, -232, and -233 airplanes.
(4) Airbus Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes.

FAA AD 2011-19-04

EASA AD 2014-0137

(3) The following service information was approved for IBR on October 27, 2015.
(i) Airbus Service Bulletin A320-27-1223, dated September 3, 2013.
(ii) UTC Aerospace Systems Service Bulletin 31075-27-22, dated July 2, 2013.
(4) The following service information was approved for IBR on October 21, 2011 (76 FR 57630, September 16, 2011).
(i) Airbus Service Bulletin A320-27A1186, Revision 07, including Appendices 1, 2, 3, 4, 5, and 6, dated March 2, 2011.
(ii) Reserved.
(5) The following service information was approved for IBR on September 22, 2009 (74 FR 41611, August 18, 2009).
(i) Airbus All Operators Telex A320-27A1186, Revision 04, dated April 3, 2009. The document number and issue date of Airbus AOT A320-27A1186, Revision 04, dated April 3, 2009, are specified only on the first page of the AOT.
(ii) Reserved.

Air Transport Association (ATA) of America Code 28, Fuel

This AD applies to all The Boeing Company Model 787-8 airplanes, certificated in any category

N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Boeing Service Bulletin B787-81205-SB280015-00, Issue 002, dated June 19, 2014.
(ii) Reserved.

Air Transport Association (ATA) of America Code 53, Fuselage

(1) This AD applies to The Boeing Company Model 767-200, -300, -300F, and -400ER series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 767-53A0251, dated August 7, 2013. (2) Installation of Supplemental Type Certificate (STC) ST01920SE does not affect the ability to accomplish the actions required by this AD. Therefore, for airplanes on which STC ST01920SE is installed, a "change in product" alternative method of compliance (AMOC) approval request is not necessary to comply with the requirements of 14 CFR 39.17.

N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Boeing Alert Service Bulletin 767-53A0251, dated August 7, 2013.
(ii) Reserved.

Air Transport Association (ATA) of America Code 27, Flight Controls.

This AD applies to Bombardier, Inc. Model DHC-8-400, -401, and -402 airplanes, certificated in any category, serial numbers 4001 and 4003 through 4453 inclusive with an outboard spoiler power control unit (PCU) having part number 390700-1007 installed in the outboard position.

N/A

TC AD CF-2014-22

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Bombardier Service Bulletin 84-27-63, dated October 17, 2013.
(ii) Reserved

Air Transport Association (ATA) of America Code 78, Engine Exhaust

This AD applies to The Boeing Company Model 777-200, -200LR, -300,-300ER, and 777F series airplanes; certificated in any category; equipped with Rolls-Royce Trent 800 series engines.

N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Boeing Special Attention Service Bulletin 777-78-0051, Revision 4, dated February 7, 2014.
(ii) Reserved.

Air Transport Association (ATA) of America Code 53, Fuselage.

This AD applies to all airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category.
(1) Airbus Model A330-201, -202, -203, -223, -223F, -243, -243F, -301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes.
(2) Airbus Model A340-211, -212, -213, -311, -312, and -313 airplanes.

FAA AD 2013-02-10

EASA AD 2012-0005

(3) The following service information was approved for IBR on March 8, 2013 (78 FR 7257, February 1, 2013).
(i) Airbus Service Bulletin A330-53-3186, Revision 01, dated April 7, 2011.
(ii) Airbus Service Bulletin A340-53-4185, Revision 01, dated April 7, 2011

Air Transport Association (ATA) of America Code 57, Wings

This AD applies to Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model 188A and 188C airplanes, certificated in any category, serial numbers 1001 and subsequent

N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Lockheed Martin Electra Service Bulletin 88/SB-721, dated April 30, 2014.
(ii) Reserved.

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EASA Navigation - Airspeed Pitot Probes - Replacement

EASA AD 2014-0237R1

N/A

Airbus SB A320-34-1127 original issue dated 24 April 1997, or Revision (Rev.) 01 dated 04 December 2001.
Airbus SB A320-34-1456 original issue dated 02 December 2009, or Rev. 01 dated 15 May 2012.
Airbus SB A320-34-1463 original issue dated 09 March 2010, or Rev. 01 dated 15 May 2012.
Airbus SB A320-34-1170 original issue dated 18 December 1998, or Rev. 01 dated 14 May 1999, or Rev. 02 dated 07 December 1999, or Rev. 03 dated 17 February 2000, or Rev. 04 dated 24 May 2000, or Rev. 05 dated 11 September 2000, or Rev. 06 dated 18 October 2001, or Rev. 07 dated 04 December 2001, or Rev. 08 dated 15 January 2003, or Rev. 09 dated 17 February 2003, or Rev. 10 dated 21 November 2003, or Rev. 11 dated 18 August 2004, or Rev. 12 dated 02 December 2004, or Rev. 13 dated 18 January 2005, or Rev. 14 dated 21 April 2005, or Rev. 15 dated 19 July 2005, or Rev. 16 dated 23 November 2006, or Rev. 17 dated 14 February 2007, or Rev. 18 dated 09 October 2009, or Rev. 19 dated 09 November 2009, or Rev. 20 dated 01 December 2010, or Rev. 21 dated 24 March 2011, or Rev. 22 dated 19 July 2011, or Rev. 23 dated 03 February 2012, or Rev. 24 dated 12 April 2012, or Rev. 25 dated 04 September 2012, or Rev. 26 dated 16 September 2013, or Rev. 27 dated 18 March 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Fuselage - Lateral Engine Pylons - Stiffener Attachments to Pylon Spar 41 Assembly - Inspection / Repair

Falcon 7X aeroplanes serial numbers (S/N) 1 to 221 inclusive, except S/N 182 and S/N 220.

N/A

Dassault Aviation SB 7X-346 original issue dated 24 April 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Landing Gear - Nose Wheel Axle and Attachment Screws - Inspection / Replacement

Societe de Construction d'Avions de Tourisme et d'Affaires "S.O.C.A.T.A." - Groupe AEROSPATIALE, Société d'Exploitation des Etablissements MORANE-SAULNIER, Societe MORANE-SAULNIER)

DGAC France AD 91-163(A)R2

N/A

SOCATA SB 150-32 Revision 2 dated January 1994, or Revision 3 dated September 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Navigation - Pitot / Static Pressure Head - Inspection / Test

BN2, BN2A, BN2B and BN2T (Islander) aeroplanes, all models, all serial numbers (s/n), and BN2A Mark III (Trislander) aeroplanes, all models, all s/n.

EASA AD 2006-0143R1

N/A

Britten Norman Aircraft Ltd SB 310 issue 4 dated 25 September 2015.
Britten Norman Aircraft Ltd Mod NB-M-1728 original issue (A) dated 20 May 2009, or issue 1 dated 04 August 2011, or issue 2 dated 14 August 2013.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Nacelles/Pylons - Pylon Side Panels at Rib 8 - Inspection

Airbus A300B4-203, A300B4-2C, A300C4-203 and A300F4-203 aeroplanes, manufacturer serial numbers (MSN) 210, 212, 218, 220, 227, 234, 235, 236, 239, 247, 255, 256, 259, 261, 274, 277, 292, 299, and 302.

N/A

Airbus SB A300-54-0075 original issue dated 11 August 1993, or Revision 01 dated 01 November 2007, or Revision 02 dated 26 June 2008, or Revision 03 dated 27 March 2013, or Revision 04 dated 26 May 2015.
Airbus SB A300-54-0081 original issue dated 23 May 1995.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Fuel - FUELTRON Flowmeter - Removal

AS 355 E, AS 355 F, AS 355 F1 and AS 355 F2 helicopters, all serial numbers.

EASA AD 2013-0205

N/A

Eurocopter ASB AS355-28.00.20 original issue dated 06 June 2013, or Airbus Helicopters ASB AS355-28.00.20 Revision 1 dated 24 June 2015.
Airbus Helicopters SB AS355-28.00.21 original issue dated 24 June 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Exhaust - Exhaust Duct / End-pipe - Inspection / Modification

Scheibe SF 25 C powered sailplanes, all manufacturer serial numbers equipped with a Rotax 914 F3 engine.

N/A

Scheibe TM/SB 653-94 original issue, dated 24 September 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Power Plant - Engine Mount Bushings - Inspection

MBB-BK 117 D-2 helicopters, all serial numbers.

N/A

AHD ASB MBB-BK117 D-2-71A-002 original issue, dated 28 September 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Fuselage - Frame 74 to 90 / Shim Sheet on Section 18.1 - Inspection / Repair

Airbus A380-841, A380-842 and A380-861 aeroplanes, manufacturer serial numbers (MSN) 0003, MSN from 0005 to 0017 inclusive, MSN from 0019 to 0023 inclusive, MSN from 0025 to 0031inclusive, MSN from 0033 to 0036 inclusive, MSN from 0038 to 0052 inclusive, MSN from 0054 to 0059 inclusive, MSN from 0061 to 0090 inclusive, MSN from 0092 to 0096 inclusive, MSN from 0098 to 0101 inclusive, MSN 0103, MSN from 0105 to 0112 inclusive, MSN 0114, MSN from 0120 to 0122 inclusive and MSN 0126.

N/A

Airbus SB A380-53-8095 original issue dated 22 July 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Flight Controls - Rudder Control System - Cracking of the Pilot-Side Rudder Pedal Tubes

Bombardier Inc.:
Model CL-600-2C10 aeroplanes, serial numbers 10002 through 10340;
Model CL-600-2D15 & CL-600-2D24 aeroplanes, serial numbers 15001 through 15318;
Model CL-600-2E25 aeroplanes, serial numbers 19001 through 19039.

N/A

Bombardier Service Bulletin 670BA-27-065

Equipment / Furnishings - Passenger / Crew and Emergency Exit Door Slide and Slide Raft Attachments - Inspection

Airbus A330-201, A330-202, A330-203, A330-223, A330-223F, A330-243, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes, all manufacturer serial numbers (MSN), except MSN 1543, 1592, 1607, 1608, 1619, 1624, 1628, 1634, 1635, 1641, 1642, 1645 through 1648 inclusive, 1650 and all higher MSN, and
Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340-642 and A340-643 aeroplanes, all MSN,
except those aeroplanes where all escape slides and slide rafts installations have passed an inspection in accordance with the instructions of the applicable Airbus Maintenance Planning Document (MPD) Task 256241-01-1, or Task 256241-02-1 or Task 256241-03-1, or Task 256241-04-1, as applicable, or Airbus Maintenance Review Board Report (MRBR) Maintenance Schedule Item (MSI) 25.62.00 section 01 or 02 or 03.

N/A

Airbus AOT A25L004-15 original issue, dated 24 August 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

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FAA Air Transport Association (ATA) of America Code 57, Wings

(1) This AD applies to The Boeing Company airplanes, certificated in any category, identified in paragraphs (c)(1)(i) and (c)(1)(ii) of this AD.
(i) Model 767-200, -300, and -300F series airplanes, as specified in Boeing Alert Service Bulletin 767-57A0076, Revision 3, dated April 4, 2012.
(ii) Model 767-400ER series airplanes, as specified in Boeing Alert Service Bulletin 767-57A0079, Revision 2, dated March 23, 2012.
(2) Installation of Supplemental Type Certificate (STC) ST01920SE does not affect the ability to accomplish the actions required by this AD. Therefore, for airplanes on which STC ST01920SE is installed, a ''change in product'' alternative method of compliance (AMOC) approval request is not necessary to comply with the requirements of 14 CFR 39.17.

FAA AD 2003-13-01

N/A

(3) The following service information was approved for IBR on November 13, 2015.
(i) Boeing Alert Service Bulletin 767-57A0079, Revision 2, dated March 23, 2012.
(ii) Boeing Alert Service Bulletin 767-57A0076, Revision 3, dated April 4, 2012.
(4) The following service information was approved for IBR on July 29, 2003 (68 FR 37402, June 24, 2003).
(i) Boeing Alert Service Bulletin 767-57A0079, dated June 20, 2002.
(ii) Boeing Service Bulletin 767-57A0076, Revision 1, dated March 29, 2001.

Air Transport Association (ATA) of America Code 57, Wings

This AD applies to Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model 188A and 188C airplanes, certificated in any category, serial numbers 1001 and subsequent.

FAA AD 81-03-53R1

N/A

No subject

This AD applies to Pratt & Whitney Canada Corp. (P&WC) PW120, PW121, and PW121A turboprop engines with post SB 21610 configuration; PW124B, PW127, PW127E, and PW127F turboprop engines with post SB 21607 configuration; PW127E and PW127F turboprop engines with serial numbers (S/Ns) PCE-EB0366 and earlier; PW127G turboprop engines with S/Ns PCE-AX0275 and earlier; and PW127M turboprop engines with S/Ns PCE-ED0810 and earlier.

FAA AD 2014-14-02

TC AD CF-2014-41

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Pratt & Whitney Canada Corp. Service Bulletin (SB) No. PW100-72-21861, dated November 21, 2014.
(ii) Reserved.

Air Transport Association (ATA) of America Code 54, Nacelles/Pylons.

This AD applies to all Viking Air Limited (Type Certificate previously held by Bombardier, Inc.) Model DHC-7-1 and DHC-7-100 airplanes, certificated in any category.

N/A

TC CF-2014-34

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Viking Air Limited Service Bulletin V7-54-02, Revision NC, dated December 14, 2012.
(ii) Reserved

Air Transport Association (ATA) of America Code 32, Landing Gear

This AD applies to the airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category. (1) Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700, 701, & 702) airplanes, serial number (S/N) 10002 and subsequent. (2) Bombardier, Inc. Model CL-600-2D15 (Regional Jet Series 705), and CL-600-2D24 (Regional Jet Series 900) airplanes, S/N 15001 and subsequent.

N/A

TC CF-2013-24R1

N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Task 320100-225, Restoration of the NLG Manual Release Actuator, of Subject 1-32, Landing Gear, of Section 1, Systems and Powerplant Program, Volume 1 of Part 1, Maintenance Review Board Report, Revision 14, dated July 10, 2013, of the CRJ 700/900/1000 Maintenance Requirements Manual, CSP-B-053.
(ii) Reserved.

Air Transport Association (ATA) of America Code 26, Fire protection.

This AD applies to Dassault Aviation Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes; Model MYSTERE-FALCON 200 airplanes; and Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5 airplanes, certificated in any category, all manufacturer serial numbers.

N/A

EASA AD 2013-0299

None

Air Transport Association (ATA) of America Code 36, Pneumatic

This AD applies to all Gulfstream Aerospace Corporation Model GVI airplanes, certificated in any category

N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Section 04-08-20, Normal Airstart-Automatic, of Chapter 04, Emergency Procedures, of the Gulfstream GVI (G650) Airplane Flight Manual, Document Number GAC-AC-G650-OPS-0001, Revision 5, dated August 12, 2013.
(ii) Section 04-08-30, Manual Airstart-Starter Assist, of Chapter 04, Emergency Procedures, of the Gulfstream GVI (G650) Airplane Flight Manual, Document Number GAC-AC-G650-OPS-0001, Revision 5, dated August 12, 2013.
(iii) Section 04-08-40, Manual Airstart-Windmilling, of Chapter 04, Emergency Procedures, of the Gulfstream GVI (G650) Airplane Flight Manual, Document Number GAC-AC-G650-OPS-0001, Revision 5, dated August 12, 2013.
(iv) Section 05-10-10, Airworthiness Limitations, of Chapter 05, Time Limits/Maintenance Checks, of the Gulfstream GVI (G650) Maintenance Manual, Revision 4, dated September 30, 2013.

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EASA ATA 53 - Fuselage - Horizontal Tail Plane Pivot Fittings - Inspection

Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers, except those on which Airbus modification (mod) 75897 has been embodied in production.

N/A

Airbus AOT A53R008-14 original issue dated 25 November 2014.
Airbus SB A380-53-8089 original issue dated 21 October 2015.

ATA 62 - Main Rotor - Blades - Inspection

A109A and A109AII helicopters, all serial numbers.

N/A

AgustaWestland BT 109-150 original issue dated 17 September 2015, or revision A dated 22 October 2015

Equipment/Furnishings - Damaged Decompression Window Louver Panel Assemblies and Detached Blowout Panels

Bombardier Inc.:
Model CL-600-2B19 aeroplanes, serial number 7003 and subsequent;
Model CL-600-2C10 aeroplanes, serial numbers 10002 and subsequent;
Model CL-600-2D15 and CL-600-2D24 aeroplanes, serial numbers 15001 and subsequent; and Model CL-600-2E25 aeroplanes, serial numbers 19001 and subsequent,
configured with Class C Cargo Compartment.

N/A

Bombardier Service Bulletin SB 601R-25-201
Bombardier Service Bulletin SB 670BA-25-100

ATA 71 - Power Plant - Forward Engine Mounts Bolts - Torque Check / Replacement

Airbus A330-223, A330-223F, A330-321, A330-322 and A330-323 aeroplanes, all manufacturer serial numbers (MSN)

EASA AD 2012-0094

N/A

Airbus SB A330-71-3028 original issue, dated 24 December 2011, or Revision 01, dated 20 February 2012, or Revision 02, dated 31 August 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
PW ASB PW4G-100-A71-32 original issue, dated 15 April 2005, or Revision 1, dated 08 November 2011, or Revision 2, dated 03 June 2015.

Engine Fuel & Control - Hydro-Mechanical Metering Unit - Additional Check Valve and Constant Delta Pressure Valve Diaphragm - Replacement

ARRIEL 2E and 2N engines, all serial numbers.
These engines are known to be installed on, but not limited to, Airbus Helicopters AS 365 N3 and Airbus Helicopters Deutschland MBB-BK 117 D-2 helicopters

N/A

urbomeca MSB 292 73 2193 version A dated 16 July 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Engine - Centrifugal Diffuser Ferrule - Inspection

MAKILA 2A and MAKILA 2A1 engines, all serial numbers, if Turbomeca modification (Mod) TU 52 is embodied in production or incorporated in service with Turbomeca Sevice Bulletin (SB) 298 72 2052.
These engines are known to be installed on, but not limited to, Airbus Helicopters (formerly Eurocopter) EC 225 LP helicopters.

N/A

Turbomeca MSB 298 72 2832 Version A dated 03 September 2015, or Version B dated 12 October 2015. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

Engine - Third Stage Turbine Wheel - Inspection

ASTAZOU XIV B and XIV H engines, all serial numbers, if fitted with a third stage turbine wheel that incorporates modification AB 173 or modification AB 208, except those engines that have been reworked in accordance with the instructions of Turbomeca Service Bulletin (SB) 283 72 0805.
These engines are known to be installed on, but not limited to, Airbus Helicopters (formerly Aerospatiale, Sud Aviation) Alouette III SA 319 B and GAZELLE SA 342 J helicopters.

EASA AD 2010-0004

N/A

Turbomeca MSB 283 72 0804 Version C dated 23 October 2009, or Version D dated 24 July 2015.
Turbomeca SB 283 72 0805 Version B dated 15 December 2010.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Hydraulic Power - Plate Assembly Attachment Points - Inspection / Check

MBB-BK117 C-2, MBB-BK117 C-2e, MBB-BK117 D-2 and MBB-BK117 D-2m helicopters, all serial numbers

N/A

AHD ASB MBB-BK117 C-2-29A-003 original issue dated 12 October 2015.
AHD ASB MBB-BK117 D-2-29A-001 original issue dated 12 October 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Doors - Body Landing Gear Centre Door Hinge Fitting - Inspection

Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers.

EASA AD 2014-0171R1

N/A

Airbus SB A380-52-8076 original issue, dated 03 July 2014, or Revision 01, dated 30 June 2015.
Airbus SB A380-52-8070 original issue, dated 05 November 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
Airbus Technical Disposition TD TD_G1_S4_05971_2014 Issue A, dated 20 January 2014.

Doors - Forward Avionics Door Cross-Members - Inspection

Airbus A330-201, A330-202, A330-203, A330-223, A330-243, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes, all manufacturer serial number (MSN), except those on which Airbus modification (mod) 49194 has been embodied in production.
Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313, all MSN, except those on which Airbus mod 49194 has been embodied in production.
Airbus A340-541 and A340-642 all MSN, except those on which Airbus mod 51172 has been embodied in production.

N/A

Airbus SB A330-52-3109 original issue dated 16 June 2015.
Airbus SB A340-52-4112 original issue dated 16 June 2015.
Airbus SB A340-52-5033 original issue dated 16 June 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Flight Controls - Spoiler Actuators - Life Limitation

A300-600 aeroplanes, all certified models, all serial numbers, and A300F4-608ST aeroplanes, all serial numbers, if Smiths Part Number (P/N) P376A0002-05, P/N P376A0002-06, P/N P376A0002-07, P/N P376A0002-09 or P/N P725A0001-00 spoiler actuators are installed.

N/A

EASA AD 2007-0245

Airbus Service Bulletin (SB) A300-27A6062 original issue dated 06 July 2007.
Airbus SB A300-27A9015 original issue dated 06 July 2007.
Airbus SB A300-27-6060 original issue dated 18 February 2008.
Airbus SB A300-27-9014 original issue dated 18 February 2008.
The use of later approved revisions of these do

Fuselage - Cabin and Cargo Compartments Parts - Inspection / Replacement

Airbus A330-201, A330-202, A330-203, A330-223, A330-243, A330-223F, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes, manufacturer serial numbers (MSN) as identified in Airbus Service Bulletin (SB) A330-53-3261 and/or SB A330-53-3262, as applicable.
Airbus A340-541, A340-542, A340-642 and A340-643 aeroplanes, MSN 1030, 1040, 1079, 1091, 1102 and 1122.

N/A

Airbus SB A330-53-3261 original issue dated 23 June 2015.
Airbus SB A330-53-3262 original issue dated 23 June 2015.
Airbus SB A340-53-5072 original issue dated 23 June 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

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FAA No subject

This AD applies to all Rolls-Royce plc (RR), RB211-535E4-37, RB211-535E4-B-37, and RB211-535E4-C-37 turbofan engines

N/A

EASA AD 2014-0249R1

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Task 05-00-01-800-000, "Recording and Control of the Lives of Parts", dated July 1, 2015, of the Rolls-Royce (RR) RB211-535E4-37/23 Time Limits Manual (TLM), publication reference T-211(535)-6RR, Revision 49, dated July 1, 2015.
(ii) Task 05-10-01-800-000, "Group A Parts Lives–CONFIG-1", dated July 1, 2014, of the RR RB211-535E4-37/23 TLM, publication reference T-211(535)-6RR, Revision 49, dated July 1, 2015.

No subject

N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(3) The following service information was approved for IBR on October 20, 2015.
(i) CFM International Service Bulletin No. CFM56-7B S/B 72-0964, Revision 1, dated December 15, 2014.
(ii) Reserved.

Air Transport Association (ATA) of America Code 24, Electrical Power

This AD applies to Bombardier, Inc. Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 airplanes, certificated in any category, serial numbers 003 through 672 inclusive

N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Bombardier Service Bulletin 8-24-84, Revision D, dated April 10, 2014.
(ii) Bombardier Service Bulletin 8-24-89, Revision C, dated November 4, 2014.

No subject

This AD applies to the airplanes specified in paragraphs (c)(1) and (c)(2) of this AD.
(1) Airbus Model A330-243, -341, -342, and -343 airplanes, certificated in any category, all manufacturer serial numbers equipped with Rolls-Royce Trent 700 engines, on which Airbus Modification 56966MP16199 has been embodied in production or Airbus Service Bulletin A330-28-3105 has been embodied in service.
(2) Airbus Model A330-243F airplanes, certificated in any category, all manufacturer serial numbers on which Airbus Modification 56966H16199 has been embodied in production or Airbus Service Bulletin A330-28-3105 has been embodied in service.

N/A

FAA ADs 2010-08-08 and 2011-06-04

None

Air Transport Association (ATA) of America Code 28, Fuel

This AD applies to Fokker Services B.V. Model F.27 Mark 200, 300, 400, 500, 600, and 700 airplanes, certificated in any category, all serial numbers.

N/A

EASA AD 2014-0099

None

Air Transport Association (ATA) of America Code 25, Equipment/furnishings

This AD applies to the Airbus airplanes, certificated in any category, as specified in paragraphs (c)(1) and (c)(2) of this AD.
(1) This AD applies to the airplanes identified in paragraphs (c)(1)(i) through (c)(1)(vii) of this AD.
(i) Model A330-201, -202, -203, -223, and -243 airplanes.
(ii) Model A330-223F and -243F airplanes.
(iii) Model A330-301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes.
(iv) Model A340-211, -212, and -213 airplanes.
(v) Model A340-311, -312, and -313 airplanes.
(vi) Model A340-541 airplanes.
(vii) Model A340-642 airplanes.
(2) This AD does not apply to airplanes on which the installations of all escape slides and slide rafts have passed an inspection as specified in any task/item identified in paragraphs (c)(2)(i) through (c)(2)(v) of this AD.
(i) Task 25-62-41-01-1 Cabin Escape Facilities, of the applicable Airbus Maintenance Planning Document.
(ii) Task 25-62-41-02-1 Cabin Escape Facilities, of the applicable Airbus Maintenance Planning Document.
(iii) Task 25-62-41-03-1 Cabin Escape Facilities, of the applicable Airbus Maintenance Planning Document.
(iv) Task 25-62-41-04-1 Cabin Escape Facilities, of the applicable Airbus Maintenance Planning Document.
(v) Maintenance Schedule Item 25.62.00 section 01, 02, or 03, of the Cabin Escape Facilities, of the applicable Airbus Maintenance Review Board Report.

N/A

EASA AD 2015-0183R1

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Airbus Alert Operators Transmission A25L004-15, Rev 00, dated August 24, 2015.
(ii) Reserved

Air Transport Association (ATA) of America Code 57, Wings

This AD applies to The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 737-57A1326, dated September 22, 2015; except for Group 1, configuration 1, airplanes identified in Boeing Alert Service Bulletin 737-57A1326, dated September 22, 2015.

N/A

(3) The following service information was approved for IBR on November 12, 2015.
(i) Boeing Alert Service Bulletin 737-57A1326, dated September 22, 2015.
(ii) Reserved.
(4) The following service information was approved for IBR on April 9, 2014 (79 FR 12368, March 5, 2014).
(i) Boeing Special Attention Service Bulletin 737-57-1318, dated May 15, 2013.
(ii) Reserved.

Air Transport Association (ATA) of America Code 28, Fuel

This AD applies to all The Boeing Company Model 767-200, -300, -300F, and -400ER series airplanes, certificated in any category

FAA AD 2015-19-02

N/A

None

Air Transport Association (ATA) of America Code 2823, Fuel Selector/Shutoff Valve

This AD applies to all The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes, certificated in any category.

N/A

None

Air Transport Association (ATA) of America Code 21, Air Conditioning

This AD applies to The Boeing Company airplanes, certificated in any category, as identified in paragraphs (c)(1) and (c)(2) of this AD.
(1) Model 737-100, -200, -200C, -300,-400, and -500 series airplanes, as identified in Boeing Special Attention Service Bulletin 737-21-1164, Revision 2, dated August 23, 2013.
(2) Model 737-600, -700, -700C, -800,-900, and -900ER series airplanes, as identified in Boeing Special Attention Service Bulletin 737-21-1165, Revision 3, dated July 16, 2014.

FAA AD 2015-16-01

N/A

(3) The following service information was approved for IBR on September 15, 2015 (80 FR 48013, August 11, 2015).
(i) Boeing Alert Service Bulletin 737-31A1325, Revision 2, dated June 5, 2014.
(ii) Boeing Alert Service Bulletin 737-31A1332, Revision 4, dated October 31, 2013.
(iii) Boeing Special Attention Service Bulletin 737-21-1164, Revision 2, dated August 23, 2013.
(iv) Boeing Special Attention Service Bulletin 737-21-1165, Revision 3, dated July 16, 2014.
(4) The following service information was approved for IBR on November 7, 2012 (77 FR 60296, October 3, 2012).
(i) Boeing Alert Service Bulletin 737-31A1325, dated January 11, 2010.
(ii) Boeing Alert Service Bulletin 737-31A1332, Revision 1, dated June 24, 2010.
(iii) Boeing Alert Service Bulletin 737-31A1332, Revision 2, dated August 18, 2011.
(iv) Boeing Alert Service Bulletin 737-31A1332, Revision 3, dated March 28, 2012.
(v) Boeing Special Attention Service Bulletin 737-21-1164, Revision 1, dated May 17, 2012.
(vi) Boeing Special Attention Service Bulletin 737-21-1165, Revision 1, dated July 16, 2010.
(vii) Boeing Special Attention Service Bulletin 737-21-1165, Revision 2, dated April 30, 2012

Air Transport Association (ATA) of America Code 53, Fuselage

This AD applies to all The Boeing Company Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-300, 747-400, 747-400D, and 747SR series airplanes, certificated in any category.

N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Boeing Alert Service Bulletin 747-53A2451, Revision 2, dated June 13, 2014.
(ii) Reserved.

No subject

This AD applies to:
(1) All Pratt & Whitney Division PW4164, PW4168, PW4168A, PW4164C, PW4164C/B, PW4164-1D, PW4168-1D, PW4168A-1D, PW4170, PW4164C-1D, and PW4164C/B-1D turbofan engines with a low-pressure turbine (LPT) 4th stage inner air seal (IAS), part number (P/N) 51N038, installed.
(2) All PW4050, PW4052, PW4056, PW4060, PW4060A, PW4060C, PW4062, PW4062A, PW4152, PW4156, PW4156A, PW4158, PW4160, PW4460, PW4462, and PW4650 turbofan engines including models with a ''-3'' suffix with an LPT 4th stage IAS, P/N 51N038, installed.

N/A

None

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EASA ATA 53 - Fuselage - Cabin and Cargo Compartments Structural Parts - Inspection

N/A

Airbus SB A330-53-3227 original issue dated 18 August 2015.
Airbus SB A330-53-3228 original issue dated 18 August 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

ATA 53 - Fuselage - Cabin / Cargo Compartment Parts - Inspection / Replacement [Improper Heat Treatment]

Airbus A318-112, A319-111, A319-112, A319-115, A319-132, A319-133, A320-214, A320-216, A320-232, A320-233, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, manufacturer serial numbers (MSN) 4895, 4903, 4911, 4919, 4929, 4938, 4942, 4944, 4946, 4948 and 4951, MSN 4956 to 5541 inclusive, MSN 5544, 5547, 5550, 5551, 5553, 5556, 5559, 5561, 5562, 5563, 5565, 5566, 5570, 5572, 5576 and 5578

N/A

Airbus SB A320-53-1292 original issue dated 23 July 2015.
Airbus SB A320-53-1293 original issue dated 30 July 2015.
Airbus SB A320-53-1294 original issue dated 23 July 2015.
The use of later approved revisions of these documents are acceptable for compliance with the requirements of this AD.

ATA 53 - Fuselage - Cabin / Cargo Compartment Parts - Inspection / Replacement [Wrong Material]

Airbus A318-112, A319-111, A319-112, A319-115, A319-132, A319-133, A320-214, A320-216, A320-232, A320-233, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, manufacturer serial numbers (MSN) 3586, 3588, 3589, 3590, 3595, 3604, 3608, 3614, 3615, 3620, 3632, 3634, 3638, 3647, 3651, 3657, 3660, 3661, 3663, 3671, 3675, 3680, 3683 to 3687 inclusive, 3689, 3691, 3694, 3700, 3702, 3704, 3705, 3710, 3720, 3727, 3728, 3733, 3735, 3742, 3744, 3746, 3754, 3757, 3759, 3763, 3768, 3770, 3772, 3774, 3775, 3779, 3788, 3790, 3794, 3797, 3799, 3801, 3803, 3808, 3810, 3818, 3822, 3824, 3826 to 4329 inclusive, 4331 to 6051 inclusive, 6053 to 6061 inclusive, 6063 to 6072 inclusive, 6074 to 6100 inclusive, 6102 to 6115 inclusive, 6117 to 6126 inclusive, 6128 to 6136 inclusive, 6138 to 6143 inclusive, 6145 to 6150 inclusive, 6152 to 6159 inclusive, 6161 and 6162.

N/A

Airbus SB A320-53-1298 original issue dated 16 February 2015.
Airbus SB A320-53-1299 original issue dated 16 February 2015.
The use of later approved revisions of these documents are acceptable for compliance with the requirements of this AD.

ATA 53 - Fuselage - Frame Base Fitting between Frames 41 and 46 - Inspection / Repair

Airbus A300 B4-603, A300 B4-605R, A300 B4-620, A300 B4-622, A300 B4-622R, A300 C4-605R variant F, A300 C4-620, A300 F4-605R, and A300 F4-622R aeroplanes, all manufacturer serial numbers

EASA AD 2012-0103

N/A

Airbus A300 B4-603, A300 B4-605R, A300 B4-620, A300 B4-622, A300 B4-622R, A300 C4-605R variant F, A300 C4-620, A300 F4-605R, and A300 F4-622R aeroplanes, all manufacturer serial numbers

ATA 53 - Fuselage - Horizontal Tail Plane Pivot Fittings - Inspection

Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers, except those on which Airbus modification (mod) 75897 has been embodied in production

N/A

Airbus AOT A53R008-14 original issue dated 25 November 2014.
Airbus SB A380-53-8089 original issue dated 21 October 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

ATA 29 - Hydraulic Power - Plate Assembly Attachment Points - Inspection / Check

MBB-BK117 C-2, MBB-BK117 C-2e, MBB-BK117 D-2 and MBB-BK117 D-2m helicopters, all serial numbers.

N/A

ATA 39 - Lightning - Fuel Tank Wall Panels - Inspection / Repair

Falcon 7X aeroplanes, serial numbers (S/N) 17 to 21 inclusive, S/N 86 to 90 inclusive, S/N 115 to 119 inclusive, S/N 129 to 138 inclusive and S/N 155.

N/A

Dassault Aviation F7X SB 7X-245 original issue dated 08 June 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

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EASA ATA 25 - Equipment / Furnishings - Hoist - Test / Replacement

This AD applies to the following helicopters, when equipped with a Goodrich hoist having a Part Number (P/N) as listed in Table 1 of this AD: AW109SP, AB139, AW139 and AB412 (all Models) helicopters, all serial numbers (s/n); BHTI 212, 214 and 412 helicopters (all Models), all s/n; BHTC 429 and 430 helicopters, all s/n; AH AS 365 N3, AS 332 L2 and EC225 LP helicopters, all s/n; AHD MBB-BK117 C-2, EC135 and EC635 (all Models) helicopters, all s/n; MDHI MD900 helicopters, all s/n; and Sikorsky S-61 (all Models), S-76A, S-76B, S-76C and S-92A helicopters, all s/n.

EASA AD 2015-0160

FAA AD 2013-06-51

Airbus Helicopters Deutschland ASB MBB-BK117 C-2-85A-038, Revision 5, dated 18 November 2015.
Airbus Helicopters Deutschland ASB MBB-BK117 C-2-85A-045, original issue, dated 18 November 2015.
Airbus Helicopters Deutschland ASB EC135-85A-058, Revision 6, dated 19 November 2015.
Airbus Helicopters Deutschland ASB EC135-85A-064, original issue, dated 19 November 2015.
Airbus Helicopters ASB AS365-25.01.25, Revision 6, dated 19 November 2015.
Airbus Helicopters ASB AS365-25.01.65, original issue, dated 19 November 2015.
Airbus Helicopters ASB AS332-25.02.70, Revision 6, dated 19 November 2015.
Airbus Helicopters ASB AS332-25.03.19, original issue, dated 19 November 2015.
Airbus Helicopters ASB EC225-25A133, Revision 6, dated 19 November 2015.
Airbus Helicopters ASB EC225-25A187, original issue, dated 19 November 2015.
AgustaWestland Bolletino Tecnico (BT) 139-443 dated 19 November 2015.
AgustaWestland BT 109SP-100 dated 19 September 2015.
Bell Helicopter Textron Canada Ltd.: None.
Bell Helicopter Textron, Inc.: None.
MD Helicopters, Inc.: None.
Sikorsky Aircraft Corporation: None.

Rotorcraft Flight Manual - Limitations Section - Amendment

A109S helicopters, all serial numbers.

N/A

AgustaWestland RFM 109G0040A013 Issue 2 Revision 3, dated 23 April 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

ATA 21 - Air Conditioning - Electronic Centralized Aircraft Monitoring / Flight Warning System - Software Update / Aircraft Flight Manual Changes

Airbus A380-841, A380-842, and A380-861 aeroplanes, all manufacturer serial numbers, except aeroplanes on which Airbus modification (mod) 76212, or mod 76214, or mod 76715 has been embodied in production.

N/A

ATA 72 - Engine - Operating Restriction

Solo Model 2350 C engines, all manufacturer serial numbers, equipped with a non-foldable propeller, except engines modified in accordance with Solo Kleinmotoren GmbH drawing nb. 2031211-V2 and, for engines installed on DG-Flugzeugbau Model DG-1000T powered sailplanes, concurrently modified in accordance with DG-Flugzeugbau drawing nb. 10 M 067.
These engines are known to be installed on, but not limited to, DG-Flugzeugbau Model DG-1000T powered sailplanes.

EASA AD 2013-0217R1

N/A

Solo Kleinmotoren GmbH Inspection Instruction SB 4603-1, dated 26 March 2015.
Solo Kleinmotoren GmbH SB 4603-17, dated 15 July 2015.
DG Flugzeugbau TN 1000/26, dated 23 September 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

ATA 52 - Doors - Main Landing Gear Doors - Modification

CN-235, CN-235-200, and CN-235-300 aeroplanes, all manufacturer serial numbers.

N/A

EADS CASA SB-235-52-0068 original issue 15 July 2002 or Revision 1 dated 24 October 2014 or Revision 2 dated 09 January 2015.
EADS CASA SB-235-52-0061 original issue 31 dated October 1996 or Revision 1 dated 24 October 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

ATA 05 - Fuel - Fuel Tanks Safety - Inspection / Modification

Airbus A330-201, A330-202, A330-203, A330-223, A330-243, A330-223F, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes, all Manufacturer Serial Numbers (MSN).
Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340-642 and A340-643 aeroplanes, all MSN.

N/A

Airbus SB A330-21-3096 Revision 01 dated 10 October 2005.
Airbus SB A330-21-3148 original issue dated 30 January 2009.
Airbus SB A330-28-3092 Revision 01 dated 14 December 2005.
Airbus SB A330-28-3044 Revision 01 dated 25 November 1997.
Airbus SB A330-28-3053 original issue dated 25 November 1997.
Airbus SB A330-28-3101 Revision 01 dated 11 October 2006.
Airbus SB A330-28-3082 original issue dated 14 June 2004, Revision 01 dated 2 March 2005, Revision 02 dated 11 August 2006, Revision 03 dated 15 November 2006 and Revision 04 dated 3 August 2007.
Airbus SB A330-28-3113 original issue dated 19 July 2011.
Airbus SB A330-31-3146 original issue dated 2 February 2010.
Airbus SB A330-55-3016 Revision 01 dated 12 February 1997.
Airbus SB A340-21-4107 Revision 01 dated 10 October 2005.
Airbus SB A340-21-4147 original issue dated 30 January 2009.
Airbus SB A340-28-4107 Revision 01 dated 14 December 2005.
Airbus SB A340-28-4054 Revision 01 dated 25 November 1997.
Airbus SB A340-28-4118 Revision 02 dated 10 July 2007.
Airbus SB A340-28-4097 original issue dated 14 June 2004, Revision 01 dated 3 March 2005, Revision 02 dated 16 August 2006, Revision 03 dated 03 July 2007, Revision 04 dated 15 September 2008 and Revision 05 dated 3 June 2010.
Airbus SB A340-28-4129 original issue dated 19 July 2011.
Airbus SB A340-28-4078 original issue dated 17 March 2000.
Airbus SB A340-28-4073 original issue dated 14 May 1998.
Airbus SB A340-31-4125 original issue dated 27 October 2008.
Airbus SB A340-55-4017 Revision 01 dated 12 February 1997.
Airbus SB A340-57-5007 original issue dated 20 July 2005.
Airbus SB A340-92-5010 original issue dated 31 March 2004.
Airbus SB A340-28-5051 original issue, dated 01 September 2011.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

ATA 72 - Engine - Third Stage Turbine Wheel - Inspection

ASTAZOU XIV B and XIV H engines, all serial numbers, if fitted with a third stage turbine wheel part number (P/N) 0 265 25 700 0 or 0 265 25 706 0, and incorporate Turbomeca modification (mod) AB 173 or mod AB 208.
These engines are known to be installed on, but not limited to, Airbus Helicopters (formerly Aerospatiale, Sud Aviation) SA 319 B (Alouette III) and SA 342 J (Gazelle) helicopters.

N/A

Turbomeca SB 283 72 0811 Version A dated 25 August 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

ATA 72 - Engine - Intermediate Pressure Turbine Blade Rear Seal Fins - Inspection

Trent 1000-A, Trent 1000-C, Trent 1000-D, Trent 1000-E, Trent 1000-G, Trent 1000-H, Trent 1000-AE and Trent 1000-CE engines, serial numbers 10062, 10081, 10146, 10154, 10166, 10172 and 10186.
These engines are known to be installed on, but not limited to, Boeing 787 aeroplanes.

N/A

Rolls-Royce NMSB Trent 1000 72-J125, original issue, dated 06 November 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

ATA 64 - Tail Rotor - Rotor Blades - Inspection

AS 332 C, AS 332 L, and AS 332 L1 helicopters, equipped with tail rotor (TR) de-icing installation unit Part Number (P/N) 204ZP01Y01 and tail rotor blade P/N 332A12-0055-XX (where XX represents any dash number) (type A10).

N/A

Airbus Helicopters ASB AS332-05.01.02 original issue, dated 22 July 2015, or Revision 1 dated 05 November 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

ATA 90 - Electrical Power - Ground Reference Connection - Inspection / Modification

BO105 A, BO105 C, BO105 D and BO105 S helicopters (all variants, except CB-5 and CBS-5), all serial numbers (S/N), if equipped with voltage regulator part number (P/N) 51565-000, or P/N 51565-000R, or P/N 51509-002R, except helicopters modified in service in accordance with ECD Alert Service Bulletin (ASB) BO105-80-118, or Service Bulletin (SB) BO105-80-119, or SB BO105-90-104.

N/A

ECD ASB BO105-90-103 Revision 2, dated 06 May 2009, or Revision 3, dated 08 March 2010, or Revision 4, dated 21 June 2010.
ECD SB BO105-90-104 original issue, dated 08 March 2010, or Revision 1, dated 21 June 2010.
The use of later approved revisions (that may be published by Airbus Helicopters Deutschland GmbH, the current design approval holder) of these documents is acceptable for compliance with the requirements of this AD.

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Air Transport Association (ATA) of America Code 57, Wings

This AD applies to all Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model 382, 382B, 382E, 382F, and 382G airplanes, certificated in any category.

FAA AD 2011-09-04

N/A

(3) The following service information was approved for IBR on December 28, 2015.
(i) Lockheed Service Bulletin 382-57-85 (82-790), Revision 3, dated July 8, 2013, including Appendix A, Revision 3, dated July 8, 2013, and Appendixes B, C, D, E, F, and G, all Revision 1, all dated March 8, 2007.
(ii) Reserved.
(4) The following service information was approved for IBR on June 22, 2011 (76 FR 28626, May 18, 2011).
(i) Lockheed Service Bulletin 382-57-85 (82-790), Revision 2, dated August 23, 2007, including Appendixes A, B, C, D, E, F, and G, all Revision 1, all dated March 8, 2007.
(ii) Reserved.

Air Transport Association (ATA) of America Code 53, Fuselage

This AD applies to the airplanes identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, certificated in any category, all manufacturer serial numbers.
(1) Airbus Model A330-201, -202, -203, -223, -223F, -243, and -243F airplanes.
(2) Airbus Model A330-301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes.
(3) Airbus Model A340-211, -212, -213, -311, -312, and -313 airplanes

N/A

EASA AD 2014-0068

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Airbus Service Bulletin A330-53-3206, Revision 03, dated February 28, 2014.
(ii) Airbus Service Bulletin A340-53-4208, Revision 03, dated February 28, 2014.

Air Transport Association (ATA) of America Code 53, Fuselage

This AD applies to Airbus Model A330-201, -202, -203, -223, -243, -301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes; and Model A340-311, -312, and -313 airplanes; certificated in any category; all manufacturer serial numbers on which Airbus Modification 44205 has been embodied in production, except those on which Airbus Modification 52974 or 53223 has been embodied in production.

FAA AD 2008-22-20

EASA AD 2014-0012R1

(3) The following service information was approved for IBR on December 29, 2015.
(i) Airbus Service Bulletin A330-53-3159, Revision 02, dated March 29, 2010.
(ii) Airbus Service Bulletin A330-53-3160, Revision 03, dated January 6, 2012.
(iii) Airbus Service Bulletin A330-53-3168, Revision 02, dated December 21, 2011.
(iv) Airbus Service Bulletin A340-53-4165, Revision 02, dated March 29, 2010.
(v) Airbus Service Bulletin A340-53-4172, Revision 01, dated July 8, 2009.
(vi) Airbus Service Bulletin A340-53-4174, Revision 02, dated December 21, 2011.
(4) The following service information was approved for IBR on December 17, 2008 (73 FR 66747, November 12, 2008).
(i) Airbus Service Bulletin A330-53-3168, Revision 01, dated February 15, 2008.
(ii) Airbus Service Bulletin A340-53-4174, Revision 01, dated February 15, 2008.

Air Transport Association (ATA) of America Code 24, Electrical Power

This AD applies to Bombardier, Inc. Model BD-100-1A10 (Challenger 300) airplanes, certificated in any category, having serial numbers 20003 through 20382 inclusive, 20384, and 20386.

N/A

TC AD CF-2014-32

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Bombardier, Inc. Service Bulletin 100-24-24, dated June 6, 2014.
(ii) Reserved.

Air Transport Association (ATA) of America Code 53, Fuselage

(1) This AD applies to The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 737-53A1323, dated December 6, 2013.
(2) Installation of Supplemental Type Certificate (STC) ST01219SE does not affect the ability to accomplish the actions required by this AD. Therefore, for airplanes on which STC ST01920SE is installed, a "change in product" alternative method of compliance (AMOC) approval request is not necessary to comply with the requirements of 14 CFR 39.17.

N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Boeing Alert Service Bulletin 737-53A1323, dated December 6, 2013.
(ii) Reserved.

Air Transport Association (ATA) of America Code 35, Oxygen

This AD applies to Zodiac Aerotechnics (formerly Intertechnique Aircraft Systems) flightcrew oxygen mask regulators having part number MC10, MF10, and MF20 series, with serial numbers listed in Appendix 1 of Zodiac Services Service Bulletin MCF-SBU-35-001, Revision 1, dated December 3, 2012. These oxygen mask regulators are installed on various transport and small airplanes, certificated in any category, including, but not limited to, the airplanes of the manufacturers specified in paragraphs (c)(1), (c)(2), (c)(3), (c)(4), (c)(5), (c)(6), and (c)(7) of this AD. An oxygen mask regulator having part number MC10-04-127 with serial number 48573 is affected only if it is part of part number MSE101-27 with serial number 7521.
(1) Airbus.
(2) ATR-GIE Avions de Transport Régional.
(3) The Boeing Company.
(4) Bombardier, Inc.
(5) Cessna Aircraft Company.
(6) Gulfstream Aerospace Corporation.
(7) Gulfstream Aerospace LP.

N/A

EASA AD 2012-0254R1

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Zodiac Aerospace Service Bulletin MCF-SBU-35-001, Revision 1, dated December 3, 2012.
(ii) Reserved.

Air Transport Association (ATA) of America Code 25, Equipment/Furnishings

This AD applies to The Boeing Company Model 747-8 series airplanes, certificated in any category, as identified in Boeing Special Attention Service Bulletin 747-25-3649, dated July 24, 2014.

N/A

Air Transport Association (ATA) of America Code 53, Fuselage

This AD applies to The Boeing Company Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-300, 747SR, and 747SP series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 747-53A2367, Revision 5, dated July 8, 2014.

N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Boeing Alert Service Bulletin 747-53A2367, Revision 5, dated July 8, 2014.
(ii) Reserved

Air Transport Association (ATA) of America Code 32, Landing Gear

This AD applies to ATR-GIE Avions de Transport Regional Model ATR42-200, -300, -320, and -500 airplanes; and Model ATR72-101, -201, -102, -202, -211, -212, and -212A airplanes; certificated in any category; all certified models; all manufacturer serial numbers

N/A

EASA AD 2014-0074

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Messier-Bugatti-Dowty Service Bulletin 631-32-213, dated December 16, 2013.
(ii) Messier-Bugatti-Dowty Service Bulletin 631-32-214, dated January 13, 2014.
(iii) Messier-Bugatti-Dowty Service Bulletin 631-32-215, dated January 13, 2014.
(iv) Messier-Bugatti-Dowty Service Bulletin 631-32-216, Revision 1, dated December 17, 2013. Pages 4, 5, and 8 of this service bulletin are the original issue and are dated October 30, 2013.
(v) Messier-Bugatti-Dowty Service Bulletin 631-32-219, dated March 3, 2014.
(vi) Messier-Bugatti-Dowty Service Bulletin 631-32-220, dated March 3, 2014.

Air Transport Association (ATA) of America Code 22, Auto Flight; 31, Instruments

N/A

EASA AD 2014-0217R1

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Airbus Service Bulletin A320-22-1375, dated January 15, 2014.
(ii) Airbus Service Bulletin A320-22-1427, Revision 05, including Appendix 01, dated November 24, 2014.
(iii) Airbus Service Bulletin A320-22-1447, Revision 03, dated April 21, 2015.
(iv) Airbus Service Bulletin A320-22-1454, dated February 12, 2014.
(v) Airbus Service Bulletin A320-22-1461, Revision 07, including Appendix 01, dated March 23, 2015.
(vi) Airbus Service Bulletin A320-22-1480, Revision 02, dated March 30, 2015.
(vii) Airbus Service Bulletin A320-22-1502, dated November 14, 2014.
(viii) Airbus Service Bulletin A320-31-1414, Revision 03, dated September 15, 2014.

Air Transport Association (ATA) of America Code 53, Fuselage

This AD applies to Fokker Services B.V. Model F.28 Mark 0070 and 0100 airplanes, certificated in any category, all serial numbers

N/A

EASA AD 2014-0039

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Fokker Service Bulletin SBF100-53-124, dated January 23, 2014.
(ii) Fokker Service Bulletin SBF100-53-125, Revision 1, dated February 13, 2014.

Air Transport Association (ATA) of America Code 55, Stabilizers

This AD applies to all airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category.
(1) Airbus Model A330-201, -202, -203, -223, -223F,-243, -243F, -301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes, all manufacturer serial numbers.
(2) Airbus Model A340-211, -212, -213, -311, -312, -313, -541, and -642 airplanes, all manufacturer serial numbers.

N/A

EASA AD 2014-0033

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Airbus Service Bulletin A330-55-3043, Revision 1, dated August 20, 2014.
(ii) Airbus Service Bulletin A340-55-4039, Revision 1, dated August 20, 2014.
(iii) Airbus Service Bulletin A340-55-5007, Revision 1, dated August 20, 2014.

AD revises MRO programme for MD aircraft

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Read the latest EASA report

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