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

(1) This AD applies to the airplanes identified in paragraphs (c)(1)(i) and (c)(1)(ii) of this AD, certificated in any category, except as provided by paragraph (c)(2) of this AD.(i) Airbus Model A330-201, -202, -203, -223, -243, -301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes, all serial numbers, except those on which Airbus modification 55306 or 55792 has been embodied in production.(ii) Airbus Model A340-211, -212, -213, -311, -312, and -313 airplanes, all serial numbers, except those on which Airbus modification 55306 or 55792 has been embodied in production.(2) This AD does not apply to Airbus Model A340-211, -212, -213, -311, -312, and -313 airplanes on which the repair specified in Airbus Repair Drawing R57115053, R57115051, or R57115047 (installation of titanium doubler on both sides) has been accomplished. AD 2007-12-08, Amendment 39-15086 (72 FR 31171, June 6, 2007), applies to these airplanes.

FAA AD 2011-24-05EASA AD 2014-0010R1(3) The following service information was approved for IBR on February 17, 2016.(i) Airbus Service Bulletin A330-57-3081, Revision 05, dated November 13, 2012.(ii) Airbus Service Bulletin A330-57-3090, Revision 01, dated June 15, 2011.(iii) Airbus Service Bulletin A330-57-3098, dated August 30, 2007.(iv) Airbus Service Bulletin A330-57-3098, Revision 02, June 15, 2011.(v) Airbus Service Bulletin A330-57-3098, Revision 03, dated September 24, 2012.(vi) Airbus Service Bulletin A330-57-3117, dated January 25, 2013.(vii) Airbus Service Bulletin A340-57-4089, Revision 05, dated November 13, 2012.(viii) Airbus Service Bulletin A340-57-4098, Revision 01, dated June 15, 2011.(ix) Airbus Service Bulletin A340-57-4106, dated August 30, 2007.(x) Airbus Service Bulletin A340-57-4106, Revision 02, dated June 15, 2011.(xi) Airbus Service Bulletin A340-57-4106, Revision 03, dated September 24, 2012.(xii) Airbus Service Bulletin A340-57-4126, dated January 25, 2013.(4) The following service information was approved for IBR on January 3, 2012 (76 FR 73496, November 29, 2011).(i) Airbus Mandatory Service Bulletin A330-57-3081, including Appendix 01, Revision 04, dated May 31, 2011.(ii) Airbus Service Bulletin A330-57-3098, Revision 01, excluding Appendix 1, dated July 31, 2009.(iii) Airbus Mandatory Service Bulletin A340-57-4089, including Appendix 01, Revision 04, dated May 31, 2011.(iv) Airbus Service Bulletin A340-57-4106, excluding Appendix 1, Revision 01, dated July 31, 2009.(5) The following service information was approved for IBR on September 13, 2007 (72 FR 44731, August 9, 2007).(i) Airbus Service Bulletin A330-57-3081, Revision 02, including Appendix 01, dated January 24, 2006.(ii) Airbus Service Bulletin A340-57-4089, Revision 02, including Appendix 01, dated January 24, 2006.

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

This AD applies to Fokker Services B.V. Model F.28 Mark 1000, 2000, 3000, and 4000 airplanes, certificated in any category, all serial numbers

N/AEASA AD 2014-0109(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.(i) Fokker F28 Proforma Service Bulletin SBF28-28-059, Revision 1, dated July 15, 2014.(ii) Fokker F28 Appendix SB SBF28-28-059/APP01, dated July 15, 2014.

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

This AD applies to Airbus Model A320-211, -212, and -231 airplanes, certificated in any category, all manufacturer serial numbers, except those on which Airbus Modification 22418 has been embodied in production.

FAA AD 2004-14-09EASA AD 2014-0065(3) The following service information was approved for IBR on February 18, 2016.(i) Airbus Service Bulletin A320-57-1043, Revision 06, dated December 5, 2013.(ii) Airbus Service Bulletin A320-57-1082, Revision 04, dated December 5, 2013.(4) The following service information was approved for IBR on August 13, 2004 (69 FR 41398, July 9, 2004).(i) Airbus Service Bulletin A320-57-1043, Revision 05, dated April 30, 2002.(ii) Airbus Service Bulletin A320-57-1082, Revision 03, dated April 30, 2002.(5) The following service information was approved for IBR on November 27, 1998 (63 FR 56542, October 22, 1998).(i) Airbus Service Bulletin A320-57-1043, Revision 02, dated May 14, 1997. Pages 1 through 6, 8, 13, and 14 of this service bulletin are marked Revision 02, dated May 14, 1997; pages 7, 9 through 12, and 15 of this service bulletin are from the original issue, dated February 16, 1993.(ii) Airbus Service Bulletin A320-57-1082, Revision 01, dated December 10, 1997.

Air Transport Association (ATA) of America Codes 53, Fuselage; and 57, Wings.

This AD applies to all ATR-GIE Avions de Transport Regional (ATR) Model ATR42-200, -300, -320, and -500 airplanes, certificated in any category.

N/AEASA AD 2012-0193(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.(i) ATR Job Instruction Card 535100 DVI 10097, "DVI of FR26 Floor Beam Around Cut-outs for Cooling & Hydrau Ducts," dated February 9, 2012.(ii) Reserved.

No subject

This AD applies to General Electric Company (GE) GE90-76B, -77B, -85B, -90B, and -94B turbofan engines with high-pressure compressor (HPC) stage 8-10 spool, part number 1694M80G04, installed.

N/AN/ANone

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

This AD applies to Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes, certificated in any category, serial numbers 7003 and subsequent, equipped with horizontal stabilizer trim actuator (HSTA) part numbers (P/N) 601R92305-1 (vendor P/N 8396-2), 601R92305-3 (vendor P/N 8396-3), or 601R92305-5 (vendor P/N 8396-4).

N/ATC AD CF-2013-14(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 601R-27-161, Revision A, dated January 30, 2014.(ii) Supplement 23, "Horizontal Stabilizer Trim Check," of Chapter 7 "Supplements," of Bombardier CL-600-2B19 Airplane Flight Manual CSP A-012, Volume 3, Revision 61, dated April 2, 2013.(iii) Task C27-40-103-04, ''Operational Check (ground maintenance test) of the horizontal stabilizer trim control unit,'' in Bombardier CL-600-2B19 Temporary Revision 2A-56, dated June 4, 2012, to Appendix A, Certification Maintenance Requirements, of Part 2, Airworthiness Requirements, of the Bombardier CL-600-2B19 Maintenance Requirements Manual.

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

This AD applies to Airbus airplanes, certificated in any category, identified in paragraphs (c)(1) and (c)(2) of this AD.(1) Model 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 airplanes; all manufacturer serial numbers; except those on which Airbus Modification 58896 has been embodied in production or embodied through Airbus Service Bulletin A330-32-3237.(2) Model A340-211, A340-212, A340-213, A340-311, A340-312, and A340-313 airplanes; all manufacturer serial numbers; except those on which Airbus Modification 58896 has been embodied in production or embodied through Airbus Service Bulletin A340-32-4279.

N/AEASA AD 2014-0222(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 A32L004-14, dated July 28, 2014, including Appendixes 1, 2, 3, and 4, which are not dated.(ii) Messier-Dowty Service Bulletin A33/34-32-272, dated November 16, 2007, including Appendixes A, B, C, and D, dated November 16, 2007.(iii) Messier-Dowty Service Bulletin A33/34-32-272, Revision 1, dated September 22, 2008, including Appendixes A, B, C, and D, dated September 22, 2008.

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

This AD applies to The Boeing Company Model 747-100, -100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, and 747SR series airplanes; certificated in any category; as identified in Boeing Alert Service Bulletin 747-53A2494, Revision 1, dated January 9, 2015.

FAA AD AD 2005-01-09N/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 747-53A2494, Revision 1, dated January 9, 2015.(ii) Reserved.

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

This AD applies to The Boeing Company Model 737-400 series airplanes, certificated in any category, having serial numbers 23865, 24231, 24706, 24474, 25417, 27003, 27149, 25375, 26281, 28661, and 28881, as modified by Supplemental Type Certificate ST01114WI

N/AN/A(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.(i) Advanced Aircraft Extinguishers Service Bulletin TFA10-26-0020, Revision IR, dated January 12, 2015.(ii) Reserved.

Air Transport Association (ATA) of America Code 71, Power Plant

This AD applies to the airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category.(1) Airbus Model A319-113 and A319-114 airplanes, all manufacturer serial numbers.(2) Airbus Model A320-211 and A320-212 airplanes, all manufacturer serial numbers.

N/AEASA AD 2015-0229(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 (AOT) A71N010-15, dated September 30, 2015.(ii) Reserved.

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

This AD applies to Airbus Model A318-111, -112, -121, and -122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes; certificated in any category; all manufacturer serial numbers.

FAA AD 2013-13-04EASA AD 2013-0202(3) The following service information was approved for IBR on February 17, 2016.(i) Airbus Service Bulletin A320-32-1346, Revision 07, dated February 10, 2015, including Appendices 01 and 02, dated February 10, 2015.(ii) Task 32.30.00.17, "Functional Check of LGCIU Power Supply Relays," of Section C-32 of Section C, Systems and Powerplant, of the Airbus A318/A319/A320/A321 Maintenance Review Board Report, Revision 18, dated March 2013.(4) The following service information was approved for IBR on August 14, 2013 (78 FR 41286, July 10, 2013).(i) Airbus Service Bulletin A320-32-1346, Revision 04, including Appendices 01 and 02, dated April 22, 2011.(ii) Airbus Service Bulletin A320-32-1349, Revision 03, including Appendix 1, dated October 5, 2011.

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 and subsequent

N/ATC AD CF-2013-20R1(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 84-52-77, Revision C, dated June 5, 2014, including Appendix A, which is undated, and attached Short Brothers Service Bulletin D8400-52-0011, Revision C, dated February 26, 2014.(ii) Reserved.

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

This AD applies to Airbus Model A320-211, -212, and -231 airplanes, certificated in any category, manufacturer serial numbers (MSN) 0001 through 0155 inclusive

FAA AD 98-18-26EASA AD 2014-0069(3) The following service information was approved for IBR on February 25, 2016.(i) Airbus Service Bulletin A320-57-1178, Revision 01, dated May 28, 2014, including Appendix 01, dated May 28, 2014.(ii) Reserved.

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

This AD applies to Bombardier, Inc. Model BD-700-1A10 and BD-700-1A11 airplanes, certificated in any category, serial numbers 9001 through 9476 inclusive and 9998.

N/ATC AD CF-2014-25(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 700-1A11-52-019, dated March 29, 2012.(ii) Bombardier Service Bulletin 700-52-042, dated March 29, 2012.(iii) Bombardier Service Bulletin 700-52-5007, dated March 29, 2012.(iv) Bombardier Service Bulletin 700-52-6007, dated March 29, 2012.

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

This AD applies to all Airbus Model A310-203, -204, -221, -222, -304, -322, -324, and -325 airplanes; Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes; Model A300 B4-605R and B4-622R airplanes; and Model A300 F4-605R, F4-622R, and A300 C4-605R Variant F airplanes; certificated in any category.

N/AEASA AD 2014-0026(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.(i) Airbus Service Bulletin A300-55-6050, Revision 01, dated August 20, 2014.(ii) Airbus Service Bulletin A310-55-2051, Revision 01, dated August 20, 2014.

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

This AD applies to all DASSAULT AVIATION Model MYSTERE-FALCON 900 airplanes, certificated in any category.

FAA AD 2002-23-20FAA AD 2010-26-05 and EASA AD 2013-0053(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.(i) Chapter 5-40, Airworthiness Limitations, Revision 20, dated October 2012, of the Dassault Aviation Falcon 900 Maintenance Manual.(ii) Reserved.

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

This AD applies to Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700, 701, & 702) airplanes, certificated in any category, serial numbers 10002 and subsequent, as identified in Bombardier Service Bulletin 670BA-32-042, Revision A, dated July 2, 2014, including Appendixes A and B, both dated November 5, 2013.

N/ATC AD CF-2014-42(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.(i) Bombardier Modification Summary Package IS670528200033, Revision A-2, dated October 11, 2005.(ii) Bombardier Service Bulletin 670BA-32-040, Revision D, dated July 2, 2014, including Appendix A, Revision A, dated July 2, 2014, and Appendix B, Revision B, dated July 2, 2014.(iii) Bombardier Service Bulletin 670BA-32-040, Revision E, dated November 13, 2014, including Appendix A, Revision A, dated July 2, 2014, and Appendix B, Revision B, dated July 2, 2014.(iv) Bombardier Service Bulletin 670BA-32-042, Revision A, dated July 2, 2014, including Appendixes A and B, both dated November 5, 2013.(v) Bombardier Service Bulletin 670BA-32-043, dated July 2, 2014.(vi) Bombardier Service Bulletin 670BA-32-043, Revision A, dated November 13, 2014.

ATA 57 - Prohibition of all flights / Restoration of Airworthiness Wings - Wing Main Spar - Inspection / Operational Limitation / Operational Records Check

L-13 and L-13 A Blaník sailplanes, all serial numbers

EASA Emergency AD 2010-0185-E
N/A

AI IB No L13/107b, dated 18 July 2011.
AI MB No L13/108a, dated 14 July 2011.
AI MB No L13/112a, dated 16 May 2011.
AI MB No L13/117a, dated 20 January 2016.
Aircraft Design and Certification Ltd. modification ADxC-DC-39-001, approved by EASA through STC 10035295, which includes associated documentation:
- ADxC-39-EO-013, Issue A, dated 01 April 11 (Template for installation of structural modification),
- ADxC-39-001-AFM dated 30 March 11 (AFM supplement), and
- ADxC-39-001-AMM dated 11 June 11 (MM supplement).
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

ATA 72 - Engine - Power Turbine Disc - Inspection / Replacement

M601D, M601D-1, M601D-2, M601E, M601E-11, M601E-21, and M601Z engines, having a serial number (s/n) as listed in Table 1 of this AD.

N/A
N/A

GE Aviation Czech SB-2016-72-50-00-1, original issue, dated 21 january 2016.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

ATA 26 - Fire Protection - Optical and Ambient Smoke Detectors - Identification / Replacement

Part Number (P/N) PMC1102-02, P/N PMC3100-00 and P/N GMC1102-02 smoke detectors, having a date of manufacture (DMF, in digits as 'MMYYYY', e.g. 072010, see Appendix 2 of this AD) between November 2010 to January 2013 inclusive, and certain repaired units, as identified by P/N and serial number (s/n) in Appendix 1 of this AD.
These smoke detectors are known to be installed on, but not limited to: Airbus A330, A330 Freighter and A380 aeroplanes by the aeroplane manufacturer on the production line; and in service by Supplemental Type Certificate (STC) modification on certain Airbus A319 and A320, Bombardier CL-600-2B19 (Challenger 850), Boeing (formerly McDonnell Douglas) DC-9 series 80, and Boeing 737-400(BDSF), 767 and 747-8 aeroplanes.

N/A
N/A

Siemens SIL PMC-26-002 original issue dated December 2015, and Revision 1 dated January 2016.
Siemens SIL PMC-26-003 original issue and Revision 1, both dated December 2015.

ATA 73 - Engine Fuel & Control - High Pressure / Low Pressure Fuel Pump Metering Unit - Inspection / Replacement

ARRIEL 2B, 2B1 and 2B1A engines, as defined in Turboméca Mandatory Service Bulletin (MSB) A292 73 2836 version A, and Turbomeca MSB A292 73 2830 version B, except engines on which Turbomeca Modification (Mod) TU178 has been embodied in production, or on which Turbomeca Service Bulletin (SB) 292 73 2178 has been embodied in-service.
These engines are known to be installed on, but not limited to, Airbus Helicopters (formerly Eurocopter) AS 350 B3 and EC 130 B4 helicopters, and Changhe Z11 helicopters.

N/A
N/A

Turbomeca MSB A292 73 2830 version B dated 10 July 2009.
Turbomeca MSB A292 73 2836 version A dated 17 August 2010.
Turbomeca SB 292 73 2178 Version A dated 01 April 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

ATA 63 - Rotor Drive - Main Gearbox Bottom Casing - Inspection / Replacement

AS 350 B1, B2 and AS 355 E, F, F1, F2, N helicopters, all serial numbers, if equipped with main gearbox (MGB) bottom Casing (sump) P/N 350A32-3119-03 or P/N 350A32-3119-05.

N/A
N/A

AH ASB AS355-01.00.56 Revision 3 dated 07 January 2016
AH ASB AS350-01.00.69 Revision 3 dated 07 January 2016
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Flight Controls - Flap and Slat Torque Tube Corrosion

Bombardier Inc. models: CL-600-2C10 - serial numbers 10002 through 10342 CL-600-2D15 and CL-600-2D24 - serial numbers 15001 through 15361; and CL-600-2E25 - serial numbers 19001 through 19041.

N/A
N/A

Bombardier Service Bulletin (SB) 670BA-27-067

ATA 63 - Rotor Drive - Main Gearbox Main and Bottom Casings - Inspection / Replacement

EC 130 B4 helicopters, all serial numbers, if equipped with main gearbox (MGB) main casing Part Number (P/N) 350A32-3156-21 (Fitted on assembly 350A32-3156-01) or P/N 350A32-3156-22 (Fitted on assembly 350A32-3156-02) or equipped with MGB bottom casing (sump) P/N 350A32- 3119-05.

N/A
N/A

AH ASB EC130-04A005 Revision 2 dated 22 December 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

ATA 63 - Rotor Drive - Main Gearbox Main and Bottom Casings - Inspection / Replacement

AS 355 NP helicopters, all serial numbers, if equipped with main gearbox (MGB) main casing Part Number (P/N) 350A32-3121-07, or equipped with MGB bottom casing (sump) P/N 350A32-3119-03 or P/N 350A32-3119-05.

N/A
N/A

AH ASB AS355-01.00.55 Revision 4 dated 07 January 2016.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

ATA 63 - Rotor Drive - Main Gearbox Main and Bottom Casings - Inspection / Replacement

AS 350 B3 helicopters, all serial numbers, if equipped with main gearbox (MGB) main casing Part Number (P/N) 350A32-3156-21 (Fitted on assembly 350A32-3156-01), or P/N 350A32-3156-22 (Fitted on assembly 350A32-3156-02) or P/N 350A32-3121-04 or P/N 350A32-3121-06 or equipped with MGB bottom Casing (sump) P/N 350A32-3119-05.

N/A
N/A

AH ASB AS350-01.00.68 Revision 2 dated 22 December 2015
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

ATA 32 - Landing Gear - Main Landing Gear Side Stay Assemblies - Replacement / Modification

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.

N/A
N/A

Airbus SB A320-32-1429 original issue dated 10 September 2015.
Messier-Bugatti-Dowty SB 200-32-315 dated 24 April 2015.
Messier-Bugatti-Dowty SB 201-32-63 dated 24 April 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

ATA 25 - Equipment / Furnishings - Life Raft / Banjo Bolt - Inspection

AS 332 L2 and EC 225 LP helicopters, all manufacturer serial numbers, equipped with life raft type RFD Heliraft 18R MK3 Manufacurer Part Number (MPN) 00051054 or MP/N 00051055, having a serial number up to and including 4197100100635, except life raft inspected and depending on finding corrected in accordance with SurvitecGroup WI560 procedure or Equipment Manufacturer Service Bulletin No. 25-122.

N/A
N/A

Airbus Helicopters ASB 332-25.03.23 original issue, dated 14 January 2016.
Airbus Helicopters ASB EC225-25A189 original issue, dated 14 January 2016.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Ice and Rain Protection - Pitot and Static System - Pitot Probe Heater Circuit Breaker Tripping During Adverse Environmental Conditions

Bombardier Inc. DHC-8 aeroplanes, models -102, -103, -106, -201, -202, -301, -311, -314 and -315, serial numbers 003 through 672.

N/A
N/A

Bombardier Service Bulletin (SB) 8-30-39
Bombardier Service Bulletin (SB) 8-30-40

ATA 72 - Engine - Propeller Fastening Bolts and Nuts - Replacement

Mikron IIIAE1, Mikron IIIAE2, Mikron IIIA3, Mikron IIIAS and Mikron IIIB engines, all manufacturer serial numbers.

EASA AD 2015-0193-E
N/A

Evektor s.r.o. MSB No SW13-065a Revision 1, dated 24 August 2015.
Parma-Technik s.r.o. BB No. MIII SAB-002/2015, dated 20 August 2015.
Parma-Technik s.r.o. BB No MIII SAB-003/2015 original issue, dated 16 October 2015 or Revision 1, dated 12 November 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Auto Flight - Uncommanded Reference Airspeed Changes

Bombardier Inc. model CL-600-2B19, CL-600-2C10, CL-600-2D15, CL-600-2D24 and CL-600-2E25 aeroplanes, equipped with Flight Control Computer (FCC), as indicated below.

N/A
N/A

Bombardier Aerospace SB 601R-22-018
Bombardier Aerospace SB 670BA-22-009

AAR has signed its first power-by-the-hour (PBH) contract in Asia with Japanese carrier Ibex Airlines in support of its Bombardier CRJ family aircraft.

Under the terms of the agreement, AAR will manage the supply chain from its CRJ components inventory through its global warehouse network, including the management of the component repair cycle at a fixed price.

Tokyo-based Ibrex will also have access to AAR’s inventory pool through exchanges and procurement.

The programme will initially cover two CRJ200 aircraft before expanding to nine in the coming months with the inclusion of seven CRJ700 aircraft.

Ken Hein, AAR’s senior vice-president of supply chain, said: “Given the rapid growth of Asia’s aviation market, PBH programmes allow airlines to outsource capital costs and parts management so they can focus on operations and passengers.”

GA Telesis Engine Services (GATES) has been granted certification from Saudi Arabia’s General Authority of Civil Aviation (GACA).

GATES said the approval opens up an MRO market opportunity for servicing CFM56 and CF6 engines.

The Helsinki-based firm said it also hopes the GACA certification will allow it to develop and expand its customer base in the region.

Tommi Valtonen, managing director of GATES, said: “We look forward to broadening our engine maintenance solutions to customers in Saudi Arabia and the GCC, while also demonstrating our commitment to being a partner in their success.”

Air France KLM Engineering & Maintenance (AFI KLM E&M) has signed an agreement with Emirates to develop a certified cockpit mount installation for the electronic flight bags (EFB) on its fleet of 777 and A380 aircraft.

Under the terms of the contract, which will cover more than 200 aircraft, AFI KLM E&M will engineer the cockpit integration of the EFB tablet including installation design, ergonomic and certification of the mounts and cradle system.

Jean-Michel Picard, vice-president of sales for the Middle East and Africa at AFI KLM E&M, said the firm’s avionics expertise was essential in winning the retrofit contract.

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

This AD applies to all The Boeing Company Model 777-200, -200LR, -300, -300ER, and 777F series airplanes, certificated in any category.

N/A
N/A

(3) The following service information was approved for IBR on January 28, 2016 (80 FR 80234, December 24, 2015).
(i) Boeing Alert Service Bulletin 777-53A0078, dated December 5, 2014.
(ii) Reserved.

No subject

This AD applies to Engine Alliance (EA) GP7270 turbofan engines with a high-pressure compressor (HPC) cone shaft, part number 382-100-907-0, installed

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) Engine Alliance (EA) Service Bulletin (SB) No. EAGP7-72-329, dated July 21, 2015.
(ii) EA SB No. EAGP7-72-330, dated July 21, 2015.

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

This AD applies to the Airbus airplanes identified in paragraphs (c)(1) through (c)(5) of this AD, certificated in any category, all manufacturer serial numbers.
(1) Airbus Model A300 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 2004-20-14
EASA AD 2013-0184R1

(3) The following service information was approved for IBR on March 10, 2016.
(i) Airbus Service Bulletin A300-53-0350, Revision 03, dated July 26, 2007.
(ii) Airbus Service Bulletin A300-53-6123, Revision 06, dated September 28, 2011

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

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

FAA AD AD 98-20-27
EASA AD 2013-0232R1

(3) The following service information was approved for IBR on March 3, 2016.
(i) Airbus Service Bulletin A300-57-6045, Revision 10, dated November 13, 2013.
(ii) Reserved.

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

This AD applies to Airbus Model A320-211, -212, and -231 airplanes, certificated in any category, manufacturer serial numbers 0002 through 0104 inclusive.

FAA AD 96-18-06
EASA AD 2013-0226

(3) The following service information was approved for IBR on March 3, 2016.
(i) Airbus Service Bulletin A320-57-1028, Revision 02, dated June 3, 2013.
(ii) Airbus Service Bulletin A320-57-1029, Revision 02, dated June 16, 1999.

Air Transport Association (ATA) of America Code 71, Powerplant

This AD applies to the airplanes, certificated in any category, identified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD, all manufacturer serial numbers.
(1) Airbus Model A318-111 and -112 airplanes.
(2) Airbus Model A319-111, -112, and -115 airplanes.
(3) Airbus Model A320-214 airplanes.
(4) Airbus Model A321-111, -112, -211, -212, and -213 airplanes.

N/A
EASA AD 2014-0276

(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 A320-71-1062, dated July 28, 2014.
(ii) Goodrich Aerostructures Service Bulletin RA32071-151, dated June 11, 2014.

Air Transport Association (ATA) of America Code 71, Powerplant

This AD applies to the airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category, all manufacturer serial numbers.
(1) Airbus Model A319-113 and -114 airplanes.
(2) Airbus Model A320-211 and -212 airplanes.

N/A
EASA AD 2014-0258

(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 A320-71-1063, including Appendix 01, dated August 13, 2014.
(ii) Reserved

No subject

This AD applies to CFM International S.A. (CFM) CFM56-5B engines with turbine rear frame (TRF), part number (P/N) 338-102-907-0 or P/N 338-102-908-0, installed.

N/A
N/A

(3) The following service information was approved for IBR on March 1, 2016.
(i) CFM International S. A. (CFM) Service Bulletin No. CFM56-5B S/B 72-0850, dated December 19, 2012.
(ii) Reserved.

Air Transport Association (ATA) of America Code 34, Navigation.

This AD applies to Bombardier, Inc. Model BD-100-1A10 (Challenger 300) airplanes, certificated in any category, serial numbers 20003 through 20500 inclusive.

N/A
TC AD CF-2015-04

(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 100-34-38, dated January 9, 2014.
(ii) Reserved.

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

(1) This AD applies to all The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series airplanes, certificated in any category.
(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 ST01219SE 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
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 737-57A1323, dated December 5, 2014.
(ii) Reserved.

US-based conversion specialist PacAvi and component MRO Guangzhou Aircraft Maintenance Engineering (GAMECO) have completed the preliminary design review of their joint A320 and A321 passenger-to-freighter (PTF) conversion programme and remain on track to bring it to market in 2017.

The PTF conversion work on the A320 freighter aircraft will take place at GAMECO’s Guangzhou facility, where it will also develop PacAvi’s A321 LITE prototype.

PacAvi CEO Stephan Hollmann said: “We are going to advance the industry’s traditional approach with a groundbreaking one stop shop-concept, offering tailored turnkey packages of airframe sourcing, purchase, customised conversion, and leasing or sale to airline customers of all tiers, worldwide.” 

Safran has opened a new 10,000m² facility in Querétaro, Mexico dedicated to the repair of CFM56 engine components.

The centre will operate as Snecma America Engine Service and becomes Safran’s tenth Mexican facility.

The firm said the facility will provide repairs for engine parts which were previously replaced while helping it maintain competitiveness in the component repair segment.

Paris-headquartered Safran also confirmed it plans to use Mexico as the location for a third composites plant alongside material specialist Albany, citing demand for the forthcoming LEAP engine and the rise in 737 MAX production.

The plant will start producing 3D composite fan blades from Q4 2017 with a targeted production rate of more than 20,000 blades annually by 2021. 

North American MRO Flying Colours has completed the expansion of its Canadian headquarters in Peterborough, Ontario which includes increasing its technical workshop space.

The firm said it has added a further 600m² of space to increase workflow capacity resulting from a rise in customer demand for refurbishment and completion projects.

It said the expanded site will provide room to house two new downdraft tables as well as a new down draft spray booth.

Sean Gillespie, executive vice-president of Flying Colours, said: “The increased demand for work on larger type aircraft and our Global ASF status means we need to match customer expectation in terms of their experience when visiting us.” 

ATA 32 - Landing Gear - Main Landing Gear Door Actuator - Monitoring / Inspection / Replacement / Modification

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.

EASA AD 2013-0288
N/A

Airbus AFM TR 437 dated 06 June 2014.
Airbus AOT A320-32A1390 original issue dated 10 February 2011.
Airbus SB A320-32-1390 Revision 01 dated 21 September 2011, or Revision 02 dated 23 October 2013, or Revision 03 dated 13 July 2014.
Airbus AOT A32N001-13 original issue dated 24 June 2013.
Airbus SB A320-32-1409 original issue dated 19 March 2013.
Airbus SB A320-32-1407 original issue dated 14 May 2013, or Revision 01 dated 03 July 2014.
Airbus SB A320-31-1414 original issue dated 19 December 2012, or Revision 01 dated 21 March 2013, or Revision 02 dated 30 July 2013.
GE SB 114122-32-105 original issue dated 17 January 2013.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

ATA 27 - Flight Controls - Airbrake Panels - Inspection

Discus-2a, Discus-2b, Discus-2c sailplanes, Ventus-2a, Ventus-2b and Ventus-2c sailplanes, and Discus-2T, Discus-2cT, Ventus-2cT and Ventus-2cM powered sailplanes, serial numbers as listed in Schempp-Hirth Flugzeugbau GmbH issued Technische Mitteilung / Technical Note (TN) 349-39, 360-29, 825-55 and 863-22 (published as a single document).

N/A
N/A

Schempp-Hirth Flugzeugbau GmbH TN 349-39, 360-29, 825-55, 863-22 (single document) and the associated Arbeitsanweisung (Working Instructions) to the TN, both dated 22 January 2016.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

ATA 62 - Main Rotor System - Main Rotor Hub - Inspection / Replacement

EC 135 P1(CDS), EC 135 P1(CPDS), EC 135 P2(CPDS), EC 135 P2+, EC 135 T1(CDS), EC 135 T1(CPDS), EC 135 T2(CPDS), EC 135 T2+, EC 635 T1(CPDS), EC 635 P2+ and EC 635 T2+ helicopters, all serial numbers.

EASA AD 2012-0041R1
N/A

ECD/AHD ASB No. EC135-62A-029 Rev. 1, dated 16 May 2012, or Rev. 2 dated 17 May 2012, or Rev.
3 dated 09 August 2012, or Rev. 4 dated 23 August 2012, or Rev. 5 dated 10 September 2012, or Rev. 6 dated 02 October 2012, or Rev. 7 dated 22 October 2012, or Rev. 8 dated 22 April 2015.
ECD SB No. EC135-62-030 original issue dated 16 August 2012, or Rev. 1 dated 31 August 2012, or Rev. 2 dated 15 October 2012.
ECD SB No. EC135-62-032 original issue dated 04 September 2012, or Rev. 1 dated 15 October 2012.
AHD SB No. EC 135-62-036 original issue dated 29 July 2015.
The use of later approved revisions of these documents (that may be published by AHD, the current design approval holder) is acceptable for compliance with the requirements of this AD.

ATA 73 - Engine Fuel & Control - Hydro-Mechanical Metering Unit - Inspection

ARRIEL 2D engines, all serial numbers.
These engines are known to be installed on, but not limited to, Airbus Helicopters (formerly Eurocopter) AS 350 B3 and EC 130 T2 helicopters.

EASA AD 2013-0079R1
N/A

Turbomeca MSB A292 73 2847 version A dated 29 May 2012, or version B dated 06 March 2013, or version C dated 03 December 2013.
Turbomeca MSB A292 73 2851 version A dated 03 December 2013, or version B dated 22 October 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

ATA 57 - Wings - Leading Edge Shear Cleats - Inspection / Replacement

Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers (MSN), except aeroplanes on which Airbus modification (mod) 73979, mod 73981 and mod 73983 have been embodied in production.

EASA AD 2012-0052R1
N/A

Airbus SB A380-57-8035 original issue dated 16 September 2011, or Revision 01 dated 30 August 2013, or Revision 02 dated 09 June 2015.
Airbus SB A380-57-8089 original issue dated 01 October 2014.
Airbus SB A380-57-8108 original issue dated 05 October 2015.
Airbus SB A380-57-8110 original issue dated 01 October 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

ATA 57 - Wings - Wing Inboard Leading Edge Droop Nose Gooseneck - Inspection / Repair / Replacement

Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers (MSN), except aeroplanes that have embodied Airbus modification (mod) 73979, mod 73981 and mod 73983 in production.

EASA AD 2012-0153
N/A

Airbus AOT A57R001-12 original issue dated 14 May 2012.
Airbus SB A380-57-8071 original issue dated 18 June 2013.
Airbus SB A380-57-8087 original issue dated 28 November 2013.
Airbus SB A380-57-8089 original issue dated 01 October 2014.
Airbus SB A380-57-8108 original issue dated 05 October 2015.
Airbus SB A380-57-8110 original issue dated 01 October 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

ATA 25 - Equipment / Furnishings - Emergency Parachute Rubber Bands - Replacement

Type 10-30/24, 12-61/24 and 12-82/23 Emergency Parachutes, all variants, serial number (s/n) 13-227154 to s/n 14-227292 inclusive.

N/A
N/A

Heinrich Mertens TM 002-03-16, dated 02 February 2016.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

ATA 27 - Flight Controls - Flight Control Primary Computer - Modification / 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), 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
N/A

Airbus SB A330-27-3205 original issue dated 09 March 2015.
Airbus SB A330-27-3207 original issue dated 30 June 2015.
Airbus SB A330-27-3208 [expected to be issued in April 2017].
Airbus SB A340-27-4195 original issue dated 24 November 2015.
Airbus SB A340-27-4196 original issue dated 24 November 2015.
Airbus SB A340-27-5064 [expected to be issued in July 2016].
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

ATA 27 - Flight Controls - Trimmable Horizontal Stabilizer Actuator Ballscrew Lower Splines - Inspection / Replacement

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.

N/A
N/A

Airbus SB A320-27-1214 original issue dated 23 February 2012.
Airbus SB A320-27-1222 original issue dated 17 July 2015.
Goodrich SB 47145-27-16 original issue dated 07 November 2011.
UTAS SB 47145-27-18 original issue dated 31 March 2015.
UTAS SB 47145-27-20 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.

Time Limits and Maintenance Checks - Changes to Component Retirement Lives

Bell Helicopter Textron Canada Ltd. (BHTC) model 407 helicopters, serial numbers 53000 and subsequent.

TC AD CF-99-04
N/A

Bell 407 Maintenance Manual, BHT-407-MM, ALS, Chapter 4

AAR has confirmed the expansion of its hydraulic repair and overhaul facility in Amsterdam.

The plant, operated by the firm’s Aircraft Component Services (ACS) division, has seen upgrades to testing equipment and staff.

AAR also said it has more than doubled the capacity of the facility to accommodate work on an expanded list of parts and systems, including hydraulic pumps; flap, thrust-reverser and landing-gear actuators; and flow control and shutoff valves for Airbus, Boeing, Embraer and Bombardier aircraft types.

Salvatore Cristofori, director of sales and commercial operations, Aircraft Component Services – Amsterdam, said: “This refresh propels ACS – Amsterdam to the leading edge of hydraulic component repair and overhaul for commercial aircraft.”  

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 2015-0148

(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 (RR) Alert Non-Modification Service Bulletin No. RB.211-72-AH972, Revision 3, including Appendices 1 through 6, dated August 28, 2015.
(ii) Reserved.

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

This AD applies to The Boeing Company airplanes, certificated in any category, that are identified in paragraphs (c)(6) through (c)(8) of this AD and equipped with center wing fuel tanks; and those identified in paragraphs (c)(1) through (c)(8) of this AD that are equipped with Boeing original equipment manufacturer-installed auxiliary fuel tanks. For airplanes on which the auxiliary fuel tanks are removed, the actions specified for the auxiliary fuel tanks are not required.
(1) Model DC-9-11, DC-9-12, DC-9-13, DC-9-14, DC-9-15, and DC-9-15F airplanes.
(2) Model DC-9-21 airplanes.
(3) Model DC-9-31, DC-9-32, DC-9-32 (VC-9C), DC-9-32F, DC-9-33F, DC-9-34, DC 9 34F, and DC 9 32F (C-9A, C 9B) airplanes.
(4) Model DC-9-41 airplanes.
(5) Model DC-9-51 airplanes.
(6) Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87 (MD-87) airplanes.
(7) Model MD-88 airplanes.
(8) Model MD-90-30 airplanes.

FAA AD 2012-18-05
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 Service Bulletin MD80-28-228, Revision 1, dated August 27, 2015.
(ii) Boeing Service Bulletin MD90-28-013, Revision 1, dated August 27, 2015.
(iii) Boeing Twinjet Special Compliance Item Report MDC-92K9145, Revision N, dated June 13, 2014, including Appendices A through D.
(iv) McDonnell Douglas MD-80 Service Bulletin 28-53, Revision 1, dated April 16, 1992.
(v) McDonnell Douglas MD-80 Service Bulletin 28-63, Revision 2, dated April 8, 1992.

Air Transport Association (ATA) of America Code 29, Hydraulic Power.

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

FAA AD 2015-26-02
FAA AD 2012-21-19 and EASA AD 2013-0274

(3) The following service information was approved for IBR on February 2, 2016 (80 FR 81174, December 29, 2015).
(i) Airbus Service Bulletin A330-29-3122, dated October 25, 2012.
(ii) Airbus Service Bulletin A330-29-3126, dated June 12, 2014.
(iii) Airbus Service Bulletin A340-29-4093, dated October 25, 2012.
(iv) Airbus Service Bulletin A340-29-4097, dated June 12, 2014.
(v) Airbus Service Bulletin A340-29-5021, dated October 2, 2012.
(vi) Airbus Service Bulletin A340-29-5025, dated June 16, 2014.
(vii) Hamilton Sundstrand Service Bulletin ERPS06M-29-19, dated August 6, 2012.

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

This AD applies to The Boeing Company Model 747-200C, -200F, -400, -400D, and -400F series airplanes; certificated in any category; as identified in Boeing Alert Service Bulletin 747-53A2499, Revision 3, dated July 15, 2014.

FAA AD 2010-26-10
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 747-53A2499, Revision 3, dated July 15, 2014.
(ii) Reserved.

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

This AD applies to all The Boeing Company Model 747-400F series airplanes, certificated in any category, as identified in paragraph 1.A., "Effectivity," of Boeing Alert Service Bulletin 747-53A2880, dated December 3, 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 747-53A2880, dated December 3, 2014.
(ii) Reserved.

Messier-Bugatti-Dowty (Safran) has won a contract with Singapore Airlines to provide landing gear services on its upcoming fleet of A350-900 aircraft.

The agreement for the aircraft, the first of which is due to enter service this year, expands on existing landing gear services between the parties covering the A380.

The contract gives Singapore Airlines access to component spares needed for the braking, steering, monitoring, gear extension and retraction systems on the aircraft.

Messier-Bugatti-Dowty CEO Vincent Mascré said: "Our comprehensive service package, which includes not only repairs, but also quick access to state-of-the-art spare parts, clearly reflects our total commitment to customer service."

GA Telesis has confirmed it will disassemble six PW6000 engines in Q1 2016 with the materials used for its airline and MRO customers currently operating A300/A310/A330, 747-400/767/777 and MD-11 aircraft.

The firm said the PW6000 work is part of its aim to increase aftermarket support programmes and adds to existing commitments to disassemble more than fifty commercial engines.

Jason Reed, president of GA Telesis’s component solutions group, said: “As we continue to expand our operations, adding this inventory puts us in an even better position to provide the highest level replacement parts support that our customers need.”

Spanish carrier Swiftair has extended its agreement with Sabena technics for component support on its fleet of 27 ATR aircraft.

Under the terms of the contract, Madrid-based Swiftair will continue to have access to Sabena’s rotable components pool, while also utilising component testing, repair and overhaul coverage.

Work on the aircraft will continue to be carried out at the French MRO’s facility in Dinard.

The extended agreement extends the cooperation between the parties which began in 2003. 

ATA 57 - Wings - Wing-To-Fuselage Attachment Torlon Plates - Inspection

PC-12, PC-12/45, PC-12/47 and PC-12/47E aeroplanes, all manufacturer serial numbers, delivered before 01 January 2015 (see Note 1 of this AD).
Note 1: For the purpose of this AD, the date of delivery is the issue date of the EASA Form 52.

N/A
N/A

Pilatus Aircraft Ltd. SB No. 57-007 original issue, dated 29 September 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

MCTOW Limitation and Wing Modification

Model 750XL aircraft, S/N 101 through to 131

N/A
N/A

Flight Manual

ATA 72 - Engine - Low Pressure Turbine Fuel Shut-Off Pawl Carrier Pivot Pin - Replacement

BR700-710A1-10 engines, manufacturer serial number (MSN) up to and including 11505 and equipped with low pressure turbine (LPT) module Part Number (P/N) M51-104 or P/N M51-111.
BR700-710A2-20 engines, MSN up to and including 12492 and equipped with LPT module P/N M51-108 or P/N M51-111.
BR700-710C4-11 engines, MSN up to and including 15277, having configuration standard 710C4-11 engraved on the engine data plate and equipped with LPT module P/N M51-112.
BR700-710C4-11 engines, MSN up to and including 15329, having configuration standard 710C4-11/10 engraved on the engine data plate and equipped with LPT module P/N M51-112.
These engines are known to be installed on, but not limited to, Gulfstream GV and GV-SP (G500, G550) and Bombardier BD-700-1A10 and BD-700-1A11 series aeroplanes.

N/A
N/A

RRD SB-BR700-72-A101523 original issue dated 05 September 2005, or Revision 1 dated 14 December 2005, or Revision 2 dated 19 December 2013, or Revision 3 dated 10 December 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

ATA 71 - Powerplant - Engine Cooling Fan - Replacement / Inspection

Cabri G2 helicopters, all manufacturer serial numbers.

EASA AD 2014-0196
N/A

Helicopteres Guimbal SB 13-022 issue B, dated 10 September 2013.
Helicopteres Guimbal SB 14-018 issue D, dated 05 November 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

ATA 05 - Time Limits / Maintenance Checks - Airworthiness Limitation Section - Amendment / Implementation

Cabri G2 helicopters, all manufacturer serial numbers.

N/A
N/A

Helicopteres Guimbal Cabri G2 MM No J70-002 issue 05.1 dated 30 October 2015, Section C, Airworthiness Limitations, approved under reference EASA.10055313.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

ATA 53 - Fuselage - Structure Frames and Joints - Modification / Reinforcement

Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all manufacturer serial numbers (MSN).

N/A
N/A

Airbus SB A340-53-4065 original issue dated 15 May 1996, or Revision 01 dated 27 May 1998, or Revision 02 dated 22 February 1999, or Revision 03 dated 15 November 1999, or Revision 04 dated 01 June 2012.
Airbus SB A340-53-4135 original issue dated 12 July 2002, or Revision 01 dated 19 March 2003, or Revision 02 dated 21 June 2010, or Revision 03 dated 17 July 2012.
Airbus SB A340-53-4191 original issue dated 25 June 2012.
Airbus SB A340-53-4194 original issue dated 04 October 2012.
Airbus SB A340-53-4196 original issue dated 16 May 2013.
Airbus SB A340-53-4197 original issue dated 16 May 2013.
Airbus SB A340-53-4198 original issue dated 24 May 2013.
Airbus SB A340-53-4234 original issue dated 30 November 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
Airbus OIT 999-0133/14 Revision 02, dated 27 August 2015, provides additional information on the subject addressed by this AD.

ATA 53 - Fuselage - Upper Fuselage Skin External Doublers at TCAS Antenna Position - Inspection

F28 Mark 0100 aeroplanes, serial number (s/n) 11244 to s/n 11407 inclusive.

N/A
N/A

Fokker Services SBF100-53-130 original issue dated 01 December 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

ATA 54 - Nacelles / Pylons - Engine Nacelle Stringers - Inspection

F27 Mark 050, Mark 0502 and Mark 0604 aeroplanes, all serial numbers.

N/A
N/A

Fokker Services SBF50-54-012 original issue dated 01 December 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

ATA 72 - Engine / Critical parts - Engine Health Check and Revised Operating Procedures / Critical Part Identification and Replacement

RB211-535C-37 engines, all serial numbers. These engines are known to be installed on, but not limited to, Boeing 757 series aeroplanes.

CAA UK ADs 009-02-87 and AD 002-05-87
N/A

Rolls-Royce NMSB RB.211-72-A8251 Revision 7, dated 21 December 2015.
Rolls-Royce Alert NMSB RB.211-72-AJ067 original issue, dated 11 December 2015.
Rolls-Royce RB211-535C TLM 05-10-01-800-000, Group A Parts Lives.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

ATA 71 - Powerplant - Aft Engine Mount Retainers - Inspection / Replacement

Airbus A318-111, A318-112, A319-111, A319-112, A319-113, A319-114, A319-115, A320-211, A320-212, A320-214, A320-215, A320-216, A321-111, A321-112, A321-211, A321-212, and A321-213 aeroplanes, all manufacturer serial numbers

EASA AD 2015-0021
N/A

Airbus AOT A71N001-12, Revision 01 dated 09 August 2012, or Revision 02 dated 27 February 2013.
Airbus AOT A71N011-15 original issue, dated 16 September 2015, or Revision 1, dated 1 February 2016.
Airbus SB A320-71-1060 original issue, dated 09 October 2014.
Airbus SB A320-71-1070 original issue, dated 23 November 2015.
Goodrich Aerostructures SB RA32071-146, Revision 2 dated 26 July 2012.
Goodrich Aerostructures SB RA32071-160, original issue dated 18 September 2014.
Goodrich Aerostructures SB RA32071-165 dated 9 October 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

ATA 64 - CANCELLED: Tail Rotor - Tail Rotor Hub Pitch Horn - Inspection / Replacement

AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS 350 B2, AS 350 B3, AS 350 D, AS 355 E, AS 355 F, AS 355 F1, AS 355 F2, AS 355 N and AS 355 NP helicopters, all serial numbers, equipped with Tail Rotor Hub (TRH) pitch horn assemblies (hereafter called 'assembly') Part Number (P/N) 350A121368.01, P/N 350A121368.02, P/N 350A121368.03, or P/N 350A121368.04, incorporating TRH pitch horn (hereafter called 'part') P/N 350A121368.XX (where XX stands for two digit dash number excluding 01, 02, 03, and 04 which are reserved for assemblies).
Note: Either the assembly P/N or the part P/N can be marked on the affected TRH pitch horns.

N/A
N/A

Airbus Helicopters AS350 Emergency ASB No. 05.00.74 Revision 2 dated 17 December 2015.
Airbus Helicopters AS355 Emergency ASB No. 05.00.65 Revision 2 dated 17 December 2015.

Tail Rotor - Pitch Link Corrosion

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

N/A
N/A

BHTC Alert Service Bulletin (ASB) 429-15-26

Flight Controls - Flap and Slat Torque Tube Corrosion

Bombardier Inc. models:
CL-600-2C10 - serial numbers 10002 through 10342
CL-600-2D15 and CL-600-2D24 - serial numbers 15001 through 15361; and
CL-600-2E25 - serial numbers 19001 through 19041.

N/A
N/A

Bombardier Aerospace SB 670BA-27-067

ATA 25 - Equipment / Furnishing - Internal Life Rafts - Inspection

SA 365 N, SA 365 N1, AS 365 N2 and AS 365 N3 helicopters, all serial numbers, if equipped with an internal life raft installation.

EASA AD 2015-0242
N/A

Airbus Helicopters ASB AS365-25.01.63 original issue, dated 15 December 2015 or Revision 01, dated 05 February 2016.
Zodiac Aerospace SB No. 025-64-13 original issue, dated 23 November 2015, or Revision 01, dated 20 January 2016.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Independent aircraft leasing and components provider Jet Midwest has confirmed the purchase of an additional six 757-200 aircraft from American Airlines.

The transaction follows on from the Kansas City-based firm buying 13 aircraft from the same carrier in June 2015, an order comprised of five 757-200s, three 767s and five MD 80 aircraft.

Jet Midwest vice-president Kevin Lee, said: “The six 757-200 aircraft equipped with twelve RB211 engines are in excellent condition and will be available for sale and freighter conversions, or dismantled for parts sales.”

Rolls-Royce has extended its contract with Austrian component specialist FACC for the supply of composite components for its civil aircraft engines.

The extended deal, which will run up to 2025, includes deliveries of both production and aftermarket parts to the British engine OEM.

FACC has supplied Rolls-Royce since 2000 with engine components including fan case linings, sound-absorbing fairings, nose spinners, and bypass ducts.

Walter Stephan, chairman of FACC, said the new contract consolidates the firm’s position as a Rolls-Royce supplier and “recognises our technological leadership in the sector of high-strength lightweight components for civil aircraft”. 

Bolivian carrier Amaszonas Linea Aerea has contracted Fokker Technologies to provide its Bombardier CRJ200 fleet with component support.

As part of its Abacus programme, Fokker will exchange and repair all rotable components on Amaszonas’ fleet of eight aircraft for the next five years.

In 2015, Fokker added the CRJ family to the Abacus programme and signed Spanish airline Air Nostrum as a launch customer.

Sergio de Urioste, executive president at Amaszonas, said: “The customised approach Fokker employs within the Abacus programme offered Amaszonas a long-term solution which we are confident will produce the desired results in terms of cost as well as fleet reliability.”

Air Transport Association (ATA) of America Code 2120, Air Distribution System

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
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 737-26A1137, dated May 22, 2014.
(ii) Boeing Special Attention Service Bulletin 737-26-1122, Revision 1, dated August 13, 2009.

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

(1) This AD applies to all The Boeing Company Model 767-200, -300, -300F, and -400ER series airplanes, certificated in any category.
(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
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 767-53A0263, dated January 12, 2015.
(ii) Reserved.

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

The Boeing Company Model 787-8 airplanes, certificated in any category, having line numbers 78 and 82.

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 787 Airworthiness Limitations-Line Number Specific, D011Z009-03-02, dated February 2015.
(ii) Reserved.

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

This AD applies to Dassault Aviation airplanes specified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category.
(1) Dassault Aviation Model FALCON 900EX airplanes, all serial numbers on which Dassault Aviation Modification M5281 has been embodied, except those on which Dassault Aviation Modification M5870 has been embodied in production.
(2) Dassault Aviation Model FALCON 2000EX airplanes, all serial numbers on which Dassault Aviation Modification M2846 has been embodied, excep

N/A
EASA AD 2014-0115

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Dassault Erratum Service Bulletin F900EX-450, dated July 16, 2014. (All pages of this revised service bulletin are marked "Initial issuance" and dated July 16, 2014.)
(ii) Dassault Erratum Service Bulletin F2000EX-344, dated July 16, 2014. (All pages of this revised service bulletin are marked "Initial issuance" and dated July 16, 2014.)

Air Transport Association (ATA) of America Code 92, Electrical Routing.

This AD applies to the ATR-GIE Avions de Transport Régional airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category.
(1) Model ATR42-500 airplanes, serial numbers 443 through 1006 inclusive, and 1014; except serial numbers 811, 1002, and 1005.
(2) Model ATR72-102, -202, -212, and -212A airplanes, serial numbers 475 through 969 inclusive, 971 through 988 inclusive, 1025, 1028 through 1069 inclusive, 1072, and 1089 through 1175 inclusive; except serial numbers 872, 887, 893, 956, 1042, and 1162.

N/A
EASA AD 2015-0171

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Avions de Transport Régional Service Bulletin ATR42-92-0024, Revision 03, dated January 21, 2015.
(ii) Avions de Transport Régional Service Bulletin ATR72-92-1032, Revision 03, dated January 21, 2015.

No subject

This AD applies to all General Electric Company (GE) GEnx-1B54, -1B58, -1B64, -1B67, and -1B70 turbofan engine models with high-pressure turbine (HPT) rotor stage 1 blade, part number 2305M26P06, installed.

N/A
N/A

GE GEnx-1B Service Bulletin No. 72-0267 R01

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

This AD applies to The Boeing Company Model 777-200 series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 777-53A0052, dated October 10, 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 777-53A0052, dated October 10, 2014.
(ii) Reserved.

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

This AD applies to The Boeing Company Model 747-100, -200B, -200C, -200F, -300, -400, -400D, and -400F series airplanes; certificated in any category, as identified in Boeing Alert Service Bulletin 747-53A2876, dated October 22, 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 747-53A2876, dated October 22, 2014.
(ii) Reserved.

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

This AD applies to Airbus Defense and Space S.A. (Formerly known as Construcciones Aeronauticas, S.A.) Model CN-235, CN-235-100, CN-235-200, CN-235-300, and C-295 airplanes, certificated in any category, all manufacturer serial numbers.

N/A
EASA AD 2016-0012

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Airbus Defence and Space Alert Operators Transmission AOT-C295-27-0001, Revision 1, dated September 29, 2015.
(ii) Airbus Defence and Space Alert Operators Transmission AOT-CN235-27-0002, Revision 1, dated September 22, 2015.

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

This AD applies to all The Boeing Company airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category.
(1) Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes.
(2) Model 757-200, -200PF, -200CB, and -300 series airplanes.
(3) Model 767-200, -300, -300F, and -400ER series airplanes.
(4) Model 777-200, -200LR, -300, -300ER, and -777F series airplanes.

N/A
N/A

None

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

This AD applies to all The Boeing Company Model DC-8-11, DC-8-12, DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, DC-8-43, DC-8-51, DC-8-52, DC-8-53, DC-8-55, DC-8F-54, DC-8F-55, DC-8-61, DC-8-62, DC-8-63, DC-8-61F, DC-8-62F, DC-8-63F, DC-8-71, DC-8-72, DC-8-73, DC-8-71F, DC-8-72F, and DC-8-73F airplanes; certificated in any category.

N/A
N/A

(3) The following service information was approved for IBR on April 5, 2016.
(i) Boeing Service Bulletin DC8-57-104, dated August 18, 2014.
(ii) Reserved.

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 2014-0100

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Fokker F27 Proforma Service Bulletin SBF27-28-072, Revision 1, dated March 6, 2014, including Fokker F27 Service Bulletin Appendix SBF27-28-072/APP01, dated July 17, 2014, including List of Drawings/Part Lists, dated July 17, 2014.
(ii) Fokker Manual Change Notification-Maintenance Documentation MCNM-F27-027, dated September 9, 2014.

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

This AD applies to The Boeing Company Model 787-8 airplanes, certificated in any category, as identified in Boeing Service Bulletin B787-81205-SB250081-00, Issue 001, dated December 9, 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 Service Bulletin B787-81205-SB250081-00, Issue 001, dated December 9, 2014.
(ii) Reserved.

Air Transport Association (ATA) of America Code 11, Placards and Markings

This AD applies to The Boeing Company Model 757-200 series airplanes, certificated in any category, modified by the applicable supplemental type certificate identified in paragraphs (c)(1) and (c)(2) of this AD.
(1) ST01529SE.
(2) ST02278SE.

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) Precision Conversions Service Bulletin PC-757-11-0023, dated August 1, 2014.
(ii) Reserved.