FAA Airworthiness Directives 06-2016

No subject

This AD applies to all Rolls-Royce plc (RR) Viper Mk. 521, Viper Mk. 522, and Viper Mk. 601-22 turbojet engines.

FAA AD 2013-11-13
EASA AD 2015-0127R1

(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 Service Bulletin (ASB) Mk. 521 Number 72-A408, Circulation A, dated January 2015.
(ii) RR ASB Mk. 521 Number 72-A408, Circulation B, dated January 2015.
(iii) RR ASB Mk. 522 Number 72-A413, Circulation A, dated January 2015.
(iv) RR ASB Mk. 522 Number 72-A412, Circulation B, dated January 2015.
(v) RR ASB Mk 601-22 Number 72-A207, dated January 2015.

See referenced SBs for affected parts; replacement; within 30 days after 14APR2016, or before any affected part exceeds its new revised life limit, WEL
Compressor shaft P/N V900766; replacement; before 20,720 CSN

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

This AD applies to the airplanes, certificated in any category, identified in paragraphs (c)(1) and (c)(2) of this AD, all manufacturer serial numbers; except those on which a gaseous system for all oxygen generators is installed.
(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, -313, -541, and -642 airplanes.

N/A
EASA AD 2015-0119

(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) A35L007-14, Revision 01, June 17, 2015; including Appendix A, Revision 01, dated June 17, 2015. The revision date is not shown on Appendix A.
(ii) B/E Aerospace Service Bulletin 117042-35-001, dated December 10, 2014.

PAX chemical oxygen generator P/N 117042-02 (15min-2 masks); replacement; within 30days to 10 yrs since mfr (per mfr date)
PAX chemical oxygen generator P/N 117042-03 (15min-3 masks); replacement; within 30days to 10 yrs since mfr (per mfr date)
PAX chemical oxygen generator P/N 117042-04 (15min-4 masks); replacement; within 30days to 10 yrs since mfr (per mfr date)
PAX chemical oxygen generator P/N 117042-22 (22min-2 masks); replacement; within 30days to 10 yrs since mfr (per mfr date)
PAX chemical oxygen generator P/N 117042-23 (22min-3 masks); replacement; within 30days to 10 yrs since mfr (per mfr date)
PAX chemical oxygen generator P/N 117042-24 (22min-4 masks); replacement; within 30days to 10 yrs since mfr (per mfr date)

No subject

This AD applies to Rolls-Royce plc (RR) RB211 Trent 768-60, 772-60, and 772B-60 turbofan engines, all serial numbers, except those engines:
(1) That have had Modification 72-H754 applied in production, or
(2) that have been modified in accordance with RR Service Bulletin (SB) No. RB.211-72-H754, including the Supplement, Revision 1, dated July 29, 2015 or initial issue dated October 1, 2014; or
(3) with sealing sleeve, part number (P/N) FW15003, with markings 102013, 112013, or 102013L.

FAA AD 2015-04-03
EASA AD 2015-0105R1

(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 No. RB.211-72-AJ035, Revision 2, dated August 10, 2015.
(ii) RR Service Bulletin No. RB.211-72-H754, including the Supplement, Revision 1, dated July 29, 2015.

Sealing sleeve P/N FW15003; replacement; within 1,600 FCs or 24 months after 19APR2016 WEF
Oil feed tube P/N FW14193; replacement (optional); within 1,600 FCs or 24 months after 19APR2016 WEF

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

This AD applies to all The Boeing Company airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category.
(1) Model DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A and KDC-10), DC-10-40, DC-10-40F airplanes.
(2) Model MD-10-10F, MD-10-30F, MD-11, and MD-11F airplanes.

FAA AD 2013-08-23
FAA ADs 2008-06-21, 2002-13-10, 2011-11-05

(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 DC10-28A253, dated June 5, 2014.
(ii) Boeing Alert Service Bulletin MD11-28A133, dated June 5, 2014.
(iii) Boeing Service Bulletin DC10-28-256, dated June 24, 2014.
(iv) Boeing Service Bulletin MD11-28-137, dated June 24, 2014.
(v) Boeing Trijet Special Compliance Item Report MDC-02K1003, Revision M, including Appendices A through D, dated July 25, 2014.

Fuel pump control and indication system wiring (various P/Ns); modification; within 48 months after 15APR2016
Fuel pump control relays (various P/Ns); replacement; within 48 months after 15APR2016

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

This AD applies to the Airbus 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) 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.

FAA ADs AD 2011-13-11 and 2013-16-09
EASA AD 2014-0221R1

(3) The following service information was approved for IBR on April 13, 2016.
(i) Airbus A318/A319/A320/A321 Temporary Revision TR437, L/G-GEAR NOT DOWNLOCKED, Issue 1.0, dated May 23, 2014, to the Airbus A318/A319/A320/A321 Airplane Flight Manual.
(ii) Airbus Service Bulletin A320-32-1390, Revision 03, dated July 3, 2014.
(iii) Airbus Service Bulletin A320-32-1407, Revision 01, dated July 3, 2014.
(iv) General Electric Service Bulletin 114122-32-105, Revision 2, dated June 24, 2014.
(4) The following service information was approved for IBR on August 23, 2013 (78 FR 48286, August 8, 2013).
(i) Airbus Alert Operators Transmission A32N001-13, dated June 24, 2013.
(ii) Reserved.
(5) The following service information was approved for IBR on July 12, 2011 (76 FR 37241, June 27, 2011).
(i) Airbus All Operators Telex A320-32A1390, dated February 10, 2011.
(ii) Reserved.
(6) The following service information was approved for IBR on April 27, 2007 (72 FR 13681, March 23, 2007).
(i) Airbus Service Bulletin A320-32-1309, Revision 01, dated June 19, 2006.
(ii) Reserved.

MLG door actuator 114122012; replacement/modification; within 12 months after 13APR2016
MLG door actuators 114122006, 114122007, 114122009, 114122010 and 114122011; replacement/modification; within 24 months after 13APR2016

Flight Warning Computer (various P/Ns); replacement (inst prohibition); after MLG door actuator replacement/modification

No subject

This AD applies to Dowty Propellers R352/6-123-F/1, R352/6-123-F/2, and R410/6-123-F/35 model propellers, part numbers (P/Ns) 660715001, 660715004, and 660715005 with hub P/Ns 660715201, 660715255, 660720217, 660720241, 660720252, 660720260, and 660720288, installed.

N/A
EASA AD 2015-0158

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Dowty Propellers Alert Service Bulletin No. F50-61-A165, Revision 2, dated July 28, 2015.
(ii) Reserved.

Liners (see SB for P/Ns); installation; at next prop removal from the aircraft after 15APR2016

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

This AD applies to the Airbus airplanes specified in paragraphs (c)(1) through (c)(6) of this AD, certificated in any category, all manufacturer 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.
(6) Airbus Model A310-203, -204, -221, -222, -304, -322, -324, and -325 airplanes.

N/A
EASA AD 2014-0164

(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 A300-53-0394, dated February 14, 2014.
(ii) Airbus Service Bulletin A300-53-0395, dated February 14, 2014.
(iii) Airbus Service Bulletin A300-53-6172, dated February 14, 2014.
(iv) Airbus Service Bulletin A300-53-6174, dated February 14, 2014.
(v) Airbus Service Bulletin A310-53-2136, dated February 14, 2014.
(vi) Airbus Service Bulletin A310-53-2137, dated February 14, 2014.

Aluminum support struts P/Ns R21449, R21449D, R21449G and R21449H; inspection/repair/replacement; earliest compliance within 12 months after 13APR2016

No subject

This AD applies to Engine Alliance (EA) GP7270 turbofan engines with one or both of the following installed:
(1) A high-pressure compressor (HPC) rotor stage 2 to 5 spool, part number (P/N) 382-104-807-0, with a serial number (S/N) listed in EA Service Bulletin (SB) EAGP7-72-327, dated July 21, 2015; or
(2) An HPC rotor stage 7 to 9 spool, P/N 2031M90G04, 2031M90G05, or 2031M90G07, with an S/N listed in EA SB EAGP7-72-328, dated July 21, 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) Engine Alliance Service Bulletin (SB) EAGP7-72-327, dated July 21, 2015.
(ii) Engine Alliance SB EAGP7-72-328, dated July 21, 2015.

HPC rotor stage 2 to 5 spool P/N 382-104-807-0; replacement; within 30 days after 19APR2016 or before accumulating 2,100 EFCs since the last disassembly of the compressor module, WEL
HPC rotor stage 7 to 9 spool P/Ns 2031M90G04, 2031M90G05 and 2031M90G07; replacement; within 30 days after 19APR2016 or before accumulating 2,100 EFCs since the last disassembly of the compressor module, WEL

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

This AD applies to The Boeing Company Model 747-100B SUD, 747-300, 747-400, and 747-400D series airplanes; and Model 747-200B series airplanes having a stretched upper deck; certificated in any category; excluding airplanes that have been converted to a large cargo freighter configuration.

FAA AD 2012-15-13
N/A

(3) The following service information was approved for IBR on April 22, 2016.
(i) Boeing Alert Service Bulletin 747-53A2559, Revision 2, dated May 13, 2014.
(ii) Reserved.
(4) The following service information was approved for IBR on September 12, 2012 (77 FR 47267, August 8, 2012).
(i) Boeing Alert Service Bulletin 747-53A2507, Revision 1, dated January 14, 2010.
(ii) Boeing Service Bulletin 747-53A2559, Revision 1, dated August 4, 2011.
(5) The following service information was approved for IBR on November 28, 2007 (72 FR 65655, November 23, 2007).
(i) Boeing Alert Service Bulletin 747-53A2507, dated April 21, 2005.
(ii) Reserved.

None

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

This AD applies to all The Boeing Company Model 737-300, -400, and -500 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 737-55A1100, dated January 26, 2016.
(ii) Reserved.

None

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

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.
(1) Model A319-131, -132, and -133 airplanes.
(2) Model A320-232 and -233 airplanes.
(3) Model A321-131, -231, and -232 airplanes.

N/A
EASA AD 2015-0004

(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 A320-71-1064, Revision 01, dated April 1, 2015.
(ii) Goodrich Aerostructures Service Bulletin V2500-NAC-71-0323, Revision 01, dated January 28, 2015.

FWD engine mount attachment pin P/N 740-2022-501 (with mount 745-2010-503 and specific S/N); replacement; 24months/7,500FHs/5,000FCs after 22APR2016 or next engine removal WEF

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

(1) This AD applies to The Boeing Company Model 737-300, -400, and -500 series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 737-53A1328, dated July 22, 2014.
(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 737-53A1328, dated July 22, 2014.
(ii) Reserved.

None

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

This AD applies to The Boeing Company Model 777-200, -200LR, -300, -300ER, and -777F series airplanes, certificated in any category, as identified in Boeing Special Attention Service Bulletin 777-54-0035, dated October 30, 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 Special Attention Service Bulletin 777-54-0035, dated October 30, 2014.
(ii) Reserved.

None

Joint Aircraft System Component (JASC)/Air Transport Association (ATA) of America Code 2730; Elevator Control System.

This AD applies to Quest Aircraft Design, LLC Model KODIAK 100 airplanes, all serial numbers 100-0001 through 100-0149, that are 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) Quest Aircraft Company KODIAK 100 Mandatory Service Bulletin SB14-07, Revision 01, dated November 23, 2015.
(ii) Quest Aircraft KODIAK Mandatory Service Bulletin SB14-07, dated August 26, 2014.
(iii) Quest Aircraft Company Field Service Instruction, Elevator Control System-Cushion Edging Inspection, Report No. FSI-105, Revision 00, not dated.
(iv) Quest Aircraft KODIAK 100 Recommended Service Bulletin SB15-01, dated March 26, 2015.
(v) Quest Aircraft Field Service Instruction, Yoke Anti-Rotation Guide Wear Pad Upgrade, Report No. FSI-108, Revision 00, not dated.

Cushion edging P/N M22529/2-3R-25; inspection/replacement; before further flight after 22APR2016
Wear pad P/N 100-619-0037; installation (term aciton); within 1 year fater 22APR2016

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, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP series airplanes, certificated in any category

FAA AD AD 2006-22-15
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 747-53A2808, dated November 30, 2012.
(ii) Boeing Service Bulletin 747-53A2465, Revision 5, dated July 11, 2013.
(iii) Boeing Service Bulletin 747-53A2562, Revision 3, dated July 11, 2013.

None

Air Transport Association (ATA) of America Code 72, Engines

This AD applies to The Boeing Company Model 787-8 and 787-9 airplanes, certificated in any category, powered by General Electric (GE) GEnx engines

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) GE GEnx-1B Service Bulletin 72-0309 R00, dated March 11, 2016.
(ii) Reserved

None

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