Airworthiness Directive Lookup Free FAA AD search by N-number, make or model
Find the FAA airworthiness directives that may apply to an aircraft: 12,857 ADs from the Federal Register since 1995, through Oct 1, 2026, each with its applicability text and the official document. Free, no account.
N536LA is a 2001 Boeing 767-316F in the FAA registry (aircraft page). Matched on type certificate model 767-316F.
RESULTS
84 ADs in effect may apply to N536LA
- In effect84
- Recurring31
- Superseded or removed39
Informational only. These are FAA airworthiness directives whose published applicability names this make and model. Whether an AD applies to a particular aircraft depends on its serial number, installed engines, propellers, parts and modifications, and some ADs listed here will not apply. This list is not the official AD record and not a compliance determination: confirm applicability and compliance against the FAA’s Dynamic Regulatory System and the aircraft’s records with a certificated mechanic or inspector. Covers ADs published in the Federal Register since 1995, through Oct 1, 2026; older ADs, and engine, propeller and appliance ADs that do not name the aircraft, are not included.
Show only ADs in effect N536LA’s registration record
- AD 2011-22-07 Recurring Engine
Rolls-Royce plc RB211-524 Series, RB211-Trent 700 Series, and RB211-Trent 800 Series Turbofan Engines
We are issuing this AD to detect cracks in the front combustion liner, which could result in hot section distress, multiple blade release, and possible damage to the airplane.
Applicability, as the AD words it
This AD applies to Rolls-Royce (RR) turbofan engine models RB211-524G2-T-19, RB211-524G3-T-19, RB211-524H2-T-19, RB211-524H-T- 36, RB211-Trent 768-60, RB211-Trent 772-60, RB211-Trent 772B-60, RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17, RB211- Trent 884B-17, RB211-Trent 892-17, RB211-Trent 892B-17 and RB211- Trent 895-17 that incorporate RR Service Bulletin (SB) RB.211-72- D133 or RB.211-72-E902. These engines are installed on, but not limited to, Airbus A330 series airplanes; Boeing 747-400 series, 767 series, and 777 series airplanes.
- AD 2011-13-01 Superseded by AD 2013-04-01 Engine
Rolls-Royce plc (RR) RB211-524 Series Turbofan Engines
We are issuing this AD to prevent failure of the attachment rivets resulting in loss of engine structural integrity, which may result in release of the thrust reverser unit from the engine.
Applicability, as the AD words it
This AD applies to RB211-524D4-19, -524D4-B-19, -524D4-39, - 524D4-B-39, -524D4X-19, -524D4X-B-19, -524H-36, -524H2-19, -524H-T- 36, -524H2-T-19, -524G2-19, -524G3-19, -524G2-T-19, and -524G3-T-19 engines with thrust reverser units (TRUs) that have a part number (P/N) specified in paragraph 1.A. of RR Alert Service Bulletin (ASB) RB.211-78-AG084, Revision 5, dated February 4, 2011, installed. These engines are installed on, but not limited to, Boeing 747 series and 767 series airplanes.
- AD 2009-07-10 One-time Engine
General Electric Company CF6-80A Series Turbofan Engines
We are issuing this AD to prevent the HPTR stage 1 disk from exceeding its part life, which could cause fatigue cracks to start and grow.
Applicability, as the AD words it
This AD applies to General Electric Co. (GE) CF6-80A, CF6- 80A1, CF6-80A2, and CF6-80A3 turbofan engines with a high-pressure turbine rotor (HPTR) stage 1 disk, part number (P/N) 9367M45G06, installed. These engines are installed on, but not limited to, Airbus A310 series and Boeing 767 series airplanes.
- AD 2009-04-10 One-time Engine
General Electric Company CF6-80A, CF6-80C2, and CF6-80E1 Series Turbofan Engines
We are issuing this AD to prevent critical life-limited rotating engine part failure, which could result in an uncontained engine failure and damage to the airplane.
Applicability, as the AD words it
This AD applies to General Electric Company CF6-80A, CF6- 80C2, and CF6-80E1 series turbofan engines. These engines are installed on, but not limited to, Airbus A300, A310, and A330 series, Boeing 747 and 767 series, and McDonnell Douglas MD-11 series airplanes.
- AD 2008-21-11 One-time Engine
General Electric Company CF6-80C2 Series and CF6-80E1 Series Turbofan Engines
We are issuing this AD to prevent an uncontained release of engine debris and loss of the structural integrity of the mount system that supports the engine.
Applicability, as the AD words it
This AD applies to the General Electric Company (GE) CF6- 80C2 and CF6-80E1 engines specified in the following Table 1 of this AD. These engines are installed on, but not limited to, Airbus A300, A310, and A330 series airplanes, Boeing 747 and 767 series airplanes, and McDonnell Douglas MD11 series airplanes. Table 1--Applicable Engines by Engine Model With Low-Pressure Turbine (LPT) Engine model Case Part No. (P/N) Installed CF6-80C2A1, -80C2A2, -80C2A3, -80C2A5, - 1336M99G01, 1336M99G02, 80C2A5F, -80C2A8, -80C2B1, -80C2B1F, - 1336M99G03, 1336M99G04, 80C2B1F1, -80C2B1F2, -80C2B2, - 1336M99G06, 1336M99G07, 80C2B2F, -80C2B3F, -80C2B4, -80C2B4F, - 1336M99G08, 1336M99G09, 80C2B5F, -80C2B6, -80C2B6F, -80C2B6FA, 1336M99G10, 1336M99G12, -80C2B7F, -80C2B8F, -80C2D1F, and - 1336M99G13, or 1336M99G15. 80C2L1F. 1647M68G05, 1647M68G08, 1647M68G09, or 1647M68G15. 1713M73G01, 1713M73G02, or 1713M73G05. 9367M99G11or 9367M99G17. CF6-80E1A1, -80E1A2, -80E1A3, -80E1A4, - 1647M68G02, 1647M68G04, 80E1A4/B. 1647M68G07, 1647M68G12, or 1647M68G13.
- AD 2008-16-18 One-time Engine
Rolls-Royce plc RB211-524 Series Turbofan Engines
We are issuing this AD to detect cracks that could cause the HP turbine disc to fail and result in uncontained failure of the engine.
Applicability, as the AD words it
This AD applies to Rolls-Royce (RR) RB211-524 series turbofan engines with certain high pressure (HP) turbine discs installed. These engines are installed on, but not limited to, Boeing 747 series and 767 series airplanes and Lockheed L1011 series airplanes.
- AD 2007-14-07 Recurring Engine
Rolls-Royce plc RB211-524 and -535 Series Turbofan Engines
We are issuing this AD to prevent uncontained engine failure and damage to the airplane.
Applicability, as the AD words it
This AD applies to the following Rolls-Royce plc (RR) RB211- 524 and -535 series turbofan engines: -524B2-19 -524C2-B-19 -524B-02 -524D4X-19 -524B3-02 -524D4X-B-19 -524C2-19 -524G2-19 -524B4-02 -524G3-19 -524B4-D-02 -524H-36 -524D4-19 -524H2-19 -524D4-39 -535E4-37 -524B-B-02 -535E4-B-37 -524B2-B-19 -535E4-C-37 -524D4-B-19 -535E4-B-75 -524D4-B-39 -535C-37 These engines are installed on, but not limited to, Boeing 747, 757, 767 series, Lockheed L-1011 series, and Tupolev Tu204 airplanes.
- AD 2007-12-07 Superseded by AD 2012-04-05 Engine
General Electric Company (GE) CF6-80C2B Series Turbofan Engines
Applicability, as the AD words it
This AD applies to General Electric Company (GE) CF6- 80C2B1F, -80C2B2F, -80C2B4F, -80C2B5F, -80C2B6F, -80C2B6FA, - 80C2B7F, and -80C2B8F turbofan engines with electronic control units (ECUs), installed on Boeing 747 and 767 series airplanes.
- AD 2007-05-17 Superseded by AD 2012-04-15 Engine
Pratt & Whitney JT9D Series Turbofan Engines
We are issuing this AD to prevent critical life-limited rotating engine part failure, which could result in an uncontained engine failure and damage to the airplane.
Applicability, as the AD words it
This AD applies to Pratt & Whitney (PW) JT9D-3A, -7, -7A, - 7H, -7AH, -7F, -7J, -20J, -59A, -70A, -7Q, -7Q3, -7R4D, -7R4D1, - 7R4E, -7R4E1, -7R4E4, -7R4G2, and -7R4H1 series turbofan engines. These engines are installed on, but not limited to, Boeing 747 and 767 series, McDonnell Douglas DC-10 series, and Airbus Industrie A300 and A310 series airplanes.
- AD 2005-18-09 One-time
Boeing Model 757-200 and -300 Series Airplanes and Model 767 Series Airplanes
This AD was prompted by reports of "old" or expired air traffic control (ATC) clearance messages being displayed on the control display unit (CDU) of the FMC system during subsequent flights.
Applicability, as the AD words it
This AD applies to Boeing Model 757-200 and -300 series airplanes and Model 767-200, -300, -300F, and -400ER series airplanes; certificated in any category; equipped with a Pegasus flight management computer (FMC) system.
- AD 2004-22-01 One-time
Various Transport Category Airplanes on Which Cargo Restraint Strap Assemblies Have Been Installed per Supplemental Type Certificate (STC) ST01004NY
To prevent shifting or unrestrained cargo in the cargo compartment, which could cause an unexpected change in the airplane's center of gravity, damage to the airplane structure and/ or flight control system, a hazard to the flightcrew, and/or possible loss of controllability of the airplane.
Applicability, as the AD words it
The following transport category airplanes, certificated in any category, on which cargo restraint strap assemblies part number (P/N) 1519-MCIDS have been installed per Supplemental Type Certificate (STC) ST01004NY: Table 1.--Manufacturers/Airplane Models Manufacturer Airplane model Aerospatiale: ATR42 and ATR72 series airplanes. Airbus: A300 B2 and A300 B4 series airplanes; A300 B4-600, A300 B4-600R, and A300 F4- 600R (collectively called A300-600) series airplanes; A310, A320, A321, A330, and A340 series airplanes. Boeing: 707-100, 707-200, 707-100B, and 707-100B series airplanes; 727, 737, 747, 757, and 767 series airplanes. British Aerospace: BAe 146 series airplanes and Avro 146-RJ series airplanes. Fokker: F27 and F.28 series airplanes. Lockheed: 188A and 188C airplanes, and L-1011 series airplanes. Maryland Air Industries, Inc. F-27 series airplanes and FH-227 series airplanes. McDonnell Douglas: DC-7, DC-7B, and DC-7C airplanes; DC-8- 11, DC-8-12, DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, and DC-8-43 airplanes; DC-8-51, DC-8-52, DC-8-53, and DC-8-55 airplanes; DC-8F-54 and DC- 8F-55 airplanes; DC-8-61, DC-8-62, and DC-8-63 airplanes; DC-8-61F, DC-8-62F, and DC-8-63F airplanes; DC-8-71, DC-8- 72, and DC-8-73 airplanes; DC-8-71F, DC- 8-72F, and DC-8-73F airplanes; DC-9-11, DC-9-12, DC-9-13, DC-9-14, DC-9-15, and DC-9-15F airplanes; DC-9-21 airplanes; DC-9-31, DC-9-32, DC-9-32 (VC-9C), DC-9- 32F, DC-9-33F, DC-9-34, DC-9-34F, DC-9- 41, DC-9-51, DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87 (MD-87) airplanes; MD-88 airplanes; MD- 90-30 airplanes; 717-200 airplanes; DC- 10-10 and DC-10-10F airplanes; DC-10-15 airplanes; DC-10-30 and DC-10-30F (KDC- 10) airplanes; DC-10-40 and DC-10-40F airplanes; MD-10-10F and MD-10-30F airplanes; and MD-11 and MD-11F airplanes.
- AD 2004-16-11 One-time
Boeing Model 757 and 767 Series Airplanes
Applicability, as the AD words it
Model 757-200, -200CB, -200PF, and -300 series airplanes, line numbers 1 through 998 inclusive; and Model 767-200, -300, -300F, and -400ER series airplanes, line numbers 1 through 869 inclusive; certificated in any category.
- AD 2004-14-19 Recurring
Boeing Model 767 Series Airplanes
To detect and correct the propagation of fatigue cracks in the vicinity of "oil cans" on the web of the aft pressure bulkhead, which could result in rapid decompression of the passenger cabin, possible damage or interference with the airplane control systems that pass through the bulkhead, and consequent loss of control of the airplane.
Applicability, as the AD words it
All Model 767 series airplanes, certificated in any category.
- AD 2004-09-14 Superseded by AD 2005-19-23 Engine
Boeing Model 767 Series Airplanes Powered by General Electric or Pratt & Whitney Engines
To prevent fatigue cracking in the primary strut structure and reduced structural integrity of the strut, which could result in separation of the strut and engine.
Applicability, as the AD words it
Model 767 series airplanes, as listed in Boeing Service Bulletin 767-54A0101, Revision 3, dated September 5, 2002; certificated in any category.
- AD 2004-07-13 One-time Engine
General Electric Company CF6-80C2 Series Turbofan Engines
Applicability, as the AD words it
This AD applies to General Electric Company (GE) CF6- 80C2A5F, CF6-80C2B5F, CF6-80C2B7F, and CF6-80C2D1F turbofan engines with high pressure turbine (HPT) stage 1 disks, part numbers (P/Ns) 1531M84G10 or 1531M84G12 installed. These engines are installed on, but not limited to, Airbus Industrie A300 and A330 series, Boeing 747 and 767 series, and McDonnell Douglas MD-11 airplanes.
- AD 2004-05-10 Recurring
Boeing Model 767 Series Airplanes
Applicability, as the AD words it
Model 767 series airplanes, line number 001 through 175 inclusive; certificated in any category.
- AD 2004-05-07 One-time
Boeing Model 767 Series Airplanes
To detect and prevent abrasion damage and correct installation discrepancies of the wire bundles located below the P37 panel, which could result in arcing to structure and consequent fire or loss of function of affected systems.
Applicability, as the AD words it
Model 767 airplanes, certificated in any category, line numbers (L/Ns) 1 through 853 inclusive.
- AD 2003-22-04 One-time Engine
Rolls-Royce plc RB211-524 Series Turbofan Engines
This AD was prompted by the discovery of damaged LP compressor blade roots resulting from entrapment of ceramic polishing media between the blade roots and the masking boot during blade root repair.
Applicability, as the AD words it
This AD applies to Rolls-Royce plc (RR) RB211-524G2-19,- 524G2-T-19, -524G3-19, -524G3-T-19, -524H2-19, -524H2-T-19, -524H- 36, and "524-H-T-36 turbofan engines with low pressure (LP) compressor fan blades part numbers (PNs) and serial numbers (SNs) as listed in Table 1 of RR Mandatory Service Bulletin (MSB) No. RB.211- 72-D184, Revision 3, dated December 20, 2002, installed. These engines are installed on, but not limited to, Boeing 747 and 767 series airplanes.
- AD 2003-21-11 One-time Engine
Rolls-Royce plc RB211-524 Series Turbofan Engines
We are issuing this AD to prevent possible uncommanded engine acceleration with no reaction to throttle movement, which could result in uncontrollable asymmetric engine thrust levels during takeoff or climb.
Applicability, as the AD words it
This AD applies to the Rolls-Royce plc (RR) engines in the following Table 1, with the dedicated generator rotor assembly, part number (P/N) UL39102, adaptor casing P/N UL26756 or UL26729, on the high speed gearbox (HSGB), and bearings P/N UL21029 installed. Table 1.--Affected Engines and Compliance Times Comply after the effective date of this Engine model Engine serial numbers AD RB211-524G2-19: Before SN 13793: Within 62 months. RB211-524G2-T-19: All SNs: Within 62 months. RB211-524G3-19: Before SN 13793: Within 62 months. RB211-524G3-T-19: All SNs: Within 62 months. RB211-524H2-19: Before SN 13793: Within 62 months. RB211-524H2-T-19: All SNs: Within 62 months. RB211-524H-36: Before SN 13472: Within 16 months. RB211-524H-T-36: All SNs: Within 16 months. These engines are installed on, but not limited to, Boeing 747 and 767 series airplanes.
- AD 2003-19-09 Recurring
Boeing Model 767 Series Airplanes
Applicability, as the AD words it
All Model 767 series airplanes, certificated in any category.
- AD 2003-14-09 Recurring
Boeing Model 767 Series Airplanes
To prevent failure of the collar fittings on the inboard trailing edge flaps, which could result in separation of the flap and consequent reduced controllability of the airplane.
Applicability, as the AD words it
Model 767 series airplanes, line numbers 1 through 749 inclusive, certificated in any category.
- AD 2003-14-08 One-time
Boeing Model 737-600, 737-700, 737-700C, 737-800, 737-900, 757, and 767 Series Airplanes
To prevent incapacitation of the flightcrew due to lack of oxygen, which could result in loss of control of the airplane.
Applicability, as the AD words it
All Model 737-600, 737-700, 737-700C, 737-800, 737-900, 757, and 767 series airplanes; certificated in any category.
- AD 2003-13-01 Superseded by AD 2015-15-06
Boeing Model 767 Series Airplanes
To prevent the inboard aft flap from separating from the wing and potentially striking the airplane, which could result in damage to the surrounding structure and potential personal injury.
Applicability, as the AD words it
Model 767 series airplanes, certificated in any category; line numbers 1 through 826 inclusive, 830, 842, 855, 856, 859, 862, 864 through 866 inclusive, 868, 869, 871 through 874 inclusive, and 876.
- AD 2003-11-16 One-time
Boeing Model 767 Series Airplanes
To detect missing, loose, or cracked bolts on the inboard and outboard support of the inboard main flap and prevent loss of the inboard main flap, which could result in loss of control of the airplane.
Applicability, as the AD words it
Model 767 series airplanes, including Model 767- 400ER series airplanes, line numbers 1 through 879 inclusive, certificated in any category.
- AD 2003-03-02 Superseded by AD 2010-03-08
Boeing Model 767 Series Airplanes
To prevent loss of the strut and engine due to corrosion damage and cracking of both fuse pins on the same strut.
Applicability, as the AD words it
Model 767-200, -300, and -300F series airplanes, as listed in Boeing Alert Service Bulletin 767-54A0062, Revision 5, dated November 11, 2002; certificated in any category.
- AD 2002-25-08 Engine
General Electric Company (GE) CF6-45, -50, -80A, -80C2, and -80E1 Turbofan Engines
Applicability, as the AD words it
This airworthiness directive (AD) is applicable to GE CF6-45, -50, -80A, -80C2, and -80E1 turbofan engines with high pressure compressor rotor (HPCR) stage 3-9 spools with part numbers (P/N's) listed in the following Table 1 installed: Table 1 Engine model HPCR stage 3-9 spool P/N CF6-45/50 Series Engines: 9136M89G02, 9136M89G03, 9136M89G06, 9136M89G07, 9136M89G08, 9136M89G09, 9136M89G17, 9136M89G18, 9136M89G19, 9136M89G21, 9136M89G22, 9136M89G27, 9136M89G29, 9253M85G01, 9253M85G02, 9273M14G01, 9331M29G01. CF6-80A Series Engines: 9136M89G10, 9136M89G11, 9136M89G20, 9136M89G21, 9136M89G22, 9136M89G27, 9136M89G28 CF6-80C2 Series Engines: 1333M66G01, 1333M66G03, 1333M66G07, 1333M66G09, 1333M66G10, 1781M52P01, 1781M52P02, 1781M53G01, 1781M53G02 1781M53G03, 1781M53G04, 1781M53G05, 1781M53G06, 1781M53G07, 1781M53G08, 1781M53G09, 1781M53G10, 1854M95P01, 1854M95P02, 1854M95P03, 1854M95P04, 1854M95P05, 1854M95P06, 1854M95P07, 1854M95P08, 9380M28P05. CF6-80E1 Series Engines: 1669M22G01, 1669M22G03, 1782M22G01, 1782M22G02, 1782M22G04. These engines are installed on, but not limited to, Airbus A300, A310, and A330 series, Boeing 747 and 767 series, and McDonnell Douglas DC-10 and MD-11 series airplanes.
- AD 2002-22-07 Superseded by AD 2003-11-16
Boeing Model 767 Series Airplanes
To detect missing, loose, or cracked bolts on the inboard and outboard support of the inboard main flap and prevent loss of the inboard main flap, which could result in loss of control of the airplane.
Applicability, as the AD words it
Model 767 series airplanes, including Model 767- 400ER series airplanes, line numbers 1 through 879 inclusive, certificated in any category.
- AD 2002-16-05 Superseded by AD 2002-22-07
Boeing Model 767 Series Airplanes
To detect missing, loose, or cracked bolts on the outboard support of the inboard main flap and prevent loss of the inboard main flap, which could result in loss of control of the airplane.
Applicability, as the AD words it
Model 767 series airplanes, including Model 767- 400ER series airplanes, line numbers 1 through 879 inclusive, certificated in any category.
- AD 2002-12-05 Recurring
Boeing Model 767-200 Series Airplanes
To detect and correct broken rivets in the nose wheel well side panels and top panel, which could impair the function of the nose landing gear and cause fatigue cracks in the nose wheel well side panel and top panel webs, which could result in rapid cabin depressurization during flight.
Applicability, as the AD words it
Model 767 series airplanes, line numbers 1 through 62; certificated in any category.
- AD 2002-08-15 One-time
Boeing Model 767 Series Airplanes
To prevent damage to the tripod strut assembly due to a preload condition, which could result in loss of control of the inboard leading edge slat or separation of the slat from the airplane, and consequent reduced controllability of the airplane.
Applicability, as the AD words it
Model 767 series airplanes, line numbers 160 through 541 inclusive, certificated in any category.
- AD 2002-08-11 Superseded by AD 2007-05-17 Engine
Pratt & Whitney JT9D Series Turbofan Engines
To prevent critical life-limited rotating engine part failure, which could result in an uncontained engine failure and damage to the airplane.
Applicability, as the AD words it
This airworthiness directive (AD) is applicable to Pratt & Whitney (PW) JT9D-3A, -7, -7A, -7H, -7AH, -7F, -7J, -20, -20J, -59A, -70A, -7Q, -7Q3, -7R4D, -7R4D1, -7R4E, -7R4E1, -7R4E4, - 7R4G2, and -7R4H1 series turbofan engines, installed on but not limited to Boeing 747 and 767 series, McDonnell Douglas DC-10 series, and Airbus Industrie A300 and A310 series airplanes.
- AD 2002-07-12 Superseded by AD 2009-04-10 Engine
General Electric Company CF6-80A, CF6-80C2, and CF6-80E1 Series Turbofan Engines
To prevent critical life-limited rotating engine part failure, which could result in an uncontained engine failure and damage to the airplane.
Applicability, as the AD words it
This airworthiness directive (AD) is applicable to General Electric Company (GE) CF6-80A, CF6-80C2, and CF6-80E1 series turbofan engines, installed on but not limited to Airbus Industrie A300, A310, and A330 series, Boeing 747 and 767 series, and McDonnell Douglas MD-11 series airplanes.
- AD 2002-07-04 One-time Engine
Pratt & Whitney JT9D-7R4 Series Turbofan Engines
To prevent uncontained failure of the low pressure turbine (LPT) 5th stage disk due to incomplete blend repairs, resulting in in- flight shutdown and damage to the airplane.
Applicability, as the AD words it
This airworthiness directive (AD) is applicable to Pratt & Whitney (PW) JT9D-7R4D, -7R4D1, -7R4E, -7R4E1, -7R4E4, -7R4G2, and 7R4H1 series turbofan engines with LPT 5th stage disks, part numbers (P/N's) 787905, 787905-001, and 798305 installed. These engines are installed on, but not limited to Airbus Industrie A300 and A310 series, and Boeing 747 and 767 series airplanes.
- AD 2002-02-12 Recurring Engine
Rolls-Royce plc RB211-524G and -524H Series Turbofan Engines
To detect cracked fan blades, which could result in an uncontained engine failure and damage to the airplane.
Applicability, as the AD words it
This airworthiness directive (AD) is applicable to Rolls-Royce plc (RR) models RB211-524G2-19, RB211-524G2-T-19, RB211-524G3-19, RB211-524G3-T-19, RB211-524H2-19, RB211-524H2-T-19, RB211-524H-36, and RB211-524H-T-36 turbofan engines, with fan blades part numbers (P/N's) UL23061, UL25772, UL27253, UL29561, UL29573, UL30533, UL36245, UL38009, UL38052, or UL38628, installed. These engines are installed on, but not limited to Boeing 747-400 series and 767 series airplanes.
- AD 2002-01-13 Recurring
Boeing Model 767 Series Airplanes
To prevent collapse of the main landing gear (MLG) due to stress corrosion cracking of the aft trunnion of the outer cylinder.
Applicability, as the AD words it
Model 767 series airplanes having line numbers 001 through 605 inclusive, on which the terminating action required by paragraph (e) of this AD has not been accomplished; certificated in any category.
- AD 2001-26-19 Superseded by AD 2009-04-12
Boeing Model 767 Series Airplanes
To prevent failure of an entry or service door to open fully in the event of an emergency evacuation, which could impede exit from the airplane and result in injury to passengers or crewmembers.
Applicability, as the AD words it
Model 767 series airplanes, line numbers 1 through 854 inclusive, certificated in any category.
- AD 2001-24-01 One-time Engine
Boeing Model 767 Series Airplanes Powered by Pratt & Whitney Model PW4000 Series Engines
To prevent the potential for dual wire faults from grounded, separated, or shorted wires, which could result in inadvertent takeoff thrust overboost, in-flight loss of thrust, or engine shutdown.
Applicability, as the AD words it
Model 767 series airplanes, line numbers 1 through 821, equipped with Pratt & Whitney PW4000 series engines; certificated in any category.
- AD 2001-17-28 Superseded by AD 2004-05-07
Boeing Model 767 Series Airplanes
To detect and correct abrasion damage and installation discrepancies of the wire bundles located below the P37 panel, which could result in arcing to structure and consequent fire or loss of function of affected systems.
Applicability, as the AD words it
Model 767 airplanes, certificated in any category, line numbers 1 through 815 inclusive.
- AD 2001-17-30 Recurring Engine
Pratt & Whitney JT9D-7R4 Series Turbofan Engines
To prevent high pressure turbine (HPT) disk firtree fracture, which could result in an uncontained engine failure, and damage to the airplane.
Applicability, as the AD words it
This airworthiness directive (AD) is applicable to Pratt & Whitney (PW) JT9D-7R4 series turbofan engines. These engines are installed on, but not limited to, Boeing 747 and 767 series and Airbus A300 and A310 series airplanes.
- AD 2001-16-07 One-time Engine
Boeing Model 747-400 and 767 Series Airplanes Equipped With General Electric CF6-80C2 Series Engines
To prevent failure of the core cowl latches during an engine fire, and consequent in-flight separation of an engine core cowl and its strut fire barrier from the airplane.
Applicability, as the AD words it
Model 747-400 and 767 series airplanes, certificated in any category, equipped with General Electric CF6- 80C2 series engines; as listed in Boeing Service Bulletin 747-71- 2285 or 767-71-0088, both dated October 8, 1998.
- AD 2001-14-19 Superseded by AD 2011-12-11
Boeing Model 767 Series Airplanes
Applicability, as the AD words it
Model 767 series airplanes, line numbers 1 through 757 inclusive, certificated in any category.
- AD 2001-12-08 One-time
Boeing Model 767 Series Airplanes
To ensure that flight crew members safely reach the ground from a flight compartment window in the event of an emergency evacuation.
Applicability, as the AD words it
Model 767 series airplanes, as listed in Boeing Alert Service Bulletin 767-25A0265, dated May 27, 1999; certificated in any category.
- AD 2001-11-07 Recurring
Boeing Model 737, 757, and 767 Series Airplanes
To prevent failure of the motor operated hydraulic shutoff valves, which could result in leakage of hydraulic fluid to the engine fire zone, reduced ability to retract the landing gear, loss of backup electrical power or other combinations of failures, and consequent reduced controllability of the airplane.
Applicability, as the AD words it
Model 737, 757, and 767 series airplanes, certificated in any category, as listed in the following Boeing Service Bulletins: Table 1.--Effectivity Affected models/ Boeing Service Bulletin Date series 737-29A1073, Revision 3: December 2, 1999. Model 737-100, -200, 300, -400, and -500. 737-29A1081: December 2, 1999. Model 737-600, -700, and -800. 757-29A0048, Revision 3: December 2, 1999. Model 757-200. 757-29A0051: December 2, 1999. Model 757-300. 767-29A0083, Revision 4: September 28, Model 767. 2000.
- AD 2001-10-07 Superseded by AD 2004-04-07 Engine
General Electric Co. CF6-80C2 Turbofan Engines
Applicability, as the AD words it
This airworthiness directive (AD) is applicable to General Electric Company (GE) CF6-80C2 series turbofan engines with stage 1 high pressure turbine (HPT) rotor disks, part numbers (P/N's) 1531M84G02, 1531M84G06, 1531M84G08, 1531M84G10, 9392M23G10, 9392M23G12, 9392M23G21, and 1862M23G01 installed. These engines are installed on, but not limited to Airbus Industrie A300 and A310 series, Boeing 747 and 767 series, and McDonnell Douglas MD-11 series airplanes.
- AD 2001-08-28 Superseded by AD 2003-18-10
Boeing Model 767 Series Airplanes
To ensure continued structural integrity of these airplanes.
Applicability, as the AD words it
Model 767-200 and -300 series airplanes having line numbers 1 through 669 inclusive, certificated in any category.
- AD 2001-07-05 Superseded by AD 2004-09-14 Engine
Boeing Model 767 Series Airplanes Powered by General Electric or Pratt & Whitney Engines
To prevent fatigue cracking in primary strut structure and reduced structural integrity of the strut, which could result in separation of the strut and engine.
Applicability, as the AD words it
Model 767 series airplanes, certificated in any category, as listed in Boeing Service Bulletin 767-54A0101, Revision 1, dated February 3, 2000.
- AD 2001-06-12 One-time Engine
Boeing Model 767 Series Airplanes Powered by General Electric Engines
To prevent fatigue cracking in the primary strut structure and consequent reduced structural integrity of the strut.
Applicability, as the AD words it
Model 767 series airplanes powered by General Electric engines, line numbers 1 through 663 inclusive, certificated in any category.
- AD 2001-04-11 Engine
Pratt & Whitney JT9D Series Turbofan Engines
Applicability, as the AD words it
Pratt & Whitney (PW) JT9D-7R4D, -7R4D1, -7R4E, - 7R4E1 (AI-500), -7, -7A, -7AH, -7H, -7F, and -20 series turbofan engines, installed on but not limited to Boeing 747 and 767 series, McDonnell Douglas DC-10 series, and Airbus Industrie A310 series aircraft.
- AD 2001-04-09 Recurring
Boeing Model 767 Series Airplanes
To prevent continued operation with yielded or failed shear rivets on a bellcrank assembly for the elevator power control actuator (PCA), which could result in reduced controllability of the airplane.
Applicability, as the AD words it
All Model 767 series airplanes, certificated in any category.
- AD 2001-02-07 Superseded by AD 2004-16-12 Engine
Boeing Model 767 Series Airplanes Powered by Pratt & Whitney Engines
To prevent fatigue cracking in primary strut structure and consequent reduced structural integrity of the strut.
Applicability, as the AD words it
Model 767 series airplanes powered by Pratt & Whitney engines, line numbers 1 through 663 inclusive, certificated in any category.
- AD 2000-26-05 One-time
Boeing Model 737, 747, 757, and 767 Series Airplanes
To prevent potential ignition of fiberglass insulation in the environmental control system (ECS) ducts, which could propagate a small fire and lead to a larger fire.
Applicability, as the AD words it
Model 737-300, 737-400, 737-500, 747, 757-200, 757-300, 767-200, 767-300, and 767-300F sries airplanes, certificated in any category, having the line numbers listed in the following table: Applicability Model Affected line numbers (L/N) Except L/N 737-300, -400, -500,: 2591, 2601, 2720, 2723, 2730, N/A 2733, 2734, 2736 through 2850 inclusive, 2852 through 3126 inclusive. 747: 1011 through 1233 inclusive.. 1012, 1174, 1216 757-200, -300: 580 through 895 inclusive: 581, 583 through 586 inclusive, 589, 595, 609, 613, 615, 622, 624, 626, 669, 674 767-200, -300, -300F: 521 through 767 inclusive,... 522, 525, 718, 758 770
- AD 2000-22-11 One-time
Boeing Model 767 Series Airplanes
To prevent ice accumulation on the aileron control cables and/or main landing gear (MLG) door and door seal during flight, which could render one of the aileron control systems and/or the MLG doors inoperative, resulting in reduced controllability of the airplane.
Applicability, as the AD words it
Model 767 series airplanes, line numbers 1 through 723 inclusive, certificated in any category.
- AD 2000-21-04 One-time
Boeing Model 767 Series Airplanes
To prevent damage to the 90-minute auxiliary power unit (APU) standby power feeder cable, which could result in arcing between the standby power feeder cable and the shroud of the APU fuel line, penetration of the fuel line shroud, and a consequent fire in the main deck floor above the aft cargo compartment.
Applicability, as the AD words it
Model 767 series airplanes; as listed in Boeing Alert Service Bulletin 767-24A0126, dated February 24, 2000; certificated in any category.
- AD 2000-19-09 One-time Engine
Boeing Model 767 Series Airplanes Powered by Rolls-Royce RB211 Series Engines
To prevent fatigue cracking in primary strut structure and consequent reduced structural integrity of the strut.
Applicability, as the AD words it
Model 767 series airplanes powered by Rolls-Royce RB211 series engines, line numbers 1 through 663 inclusive, certificated in any category.
- AD 2000-17-06 Recurring Engine
Boeing Model 747 and 767 Series Airplanes Equipped With General Electric CF6-80C2 Series Engines
To ensure the integrity of the fail-safe features of the thrust reverser system by preventing possible failure modes, which could result in inadvertent deployment of a thrust reverser during flight, and consequent reduced controllability of the airplane.
Applicability, as the AD words it
Model 747 and 767 series airplanes equipped with General Electric CF6-80C2 series engines, certificated in any category.
- AD 2000-16-12 One-time Engine
General Electric Company CF6-45, -50, -80A, -80C2, and -80E1 Turbofan Engines
To detect cracks which can cause separation of the HPCR stage 3- 9 spool and result in an uncontained engine failure, perform the following inspections: CF6-45/50 Series Engines (a) For HPCR stages 3-9 spools installed in CF6-45/50 series engines that have not been inspected in accordance with AD 99-24-15.
Applicability, as the AD words it
This airworthiness directive is applicable to General Electric Company (GE) CF6-45, -50, -80A, -80C2, and -80E1 turbofan engines with high pressure compressor rotor stage 3-9 spools with the following part numbers (P/N's). These engines are installed on, but not limited to, Airbus A300, A310, and A330 series, Boeing 747 and 767 series, and McDonnell Douglas DC-10 and MD-11 series airplanes. Engine model HPCR 3-9 spool P/N CF6-45/50 Series Engines: 9136M89G02, 9136M89G03, 9136M89G06, 9136M89G07, 9136M89G08, 9136M89G09, 9136M89G17, 9136M89G18, 9136M89G19, 9136M89G21, 9136M89G22, 9136M89G27, 9273M14G01, 9331M29G01, 9253M85G01, 9253M85G02 CF6-80A Series Engines: 99136M89G10, 9136M89G11, 9136M89G20, 9136M89G21, 9136M89G22, 9136M89G27 CF6-80C2 Series Engines: 1333M66G01, 1333M66G03, 1333M66G07, 1333M66G09, 1781M52P01, 1781M53G01, 1854M95P01, 1854M95P02, 1854M95P03, 1854M95P04, 1854M95P05, 1854M95P06, 1854M95P07, 9380M28P05 CF6-80E1 Series Engines: 1669M22G01, 1669M22G03, 1782M22G01, 1782M22G02
- AD 2000-15-16 One-time
Boeing Model 737, 757, 767, and 777 Series Airplanes
To prevent failure of the supplemental oxygen system to deliver oxygen to the passengers and flight attendants in the event of decompression, which could result in injury to passengers and flight attendants.
Applicability, as the AD words it
Model 737 series airplanes, line numbers 1 through 2984 inclusive; Model 757 series airplanes, line numbers 1 through 798 inclusive; Model 767 series airplanes, line numbers 1 through 682 inclusive; and Model 777 series airplanes, line numbers 1 through 083 inclusive; certificated in any category; and equipped with Puritan-Bennett passenger and flight attendant oxygen masks, as listed in Boeing Service Bulletin 737-35-1049, dated September 17, 1998; 757-35-0014, dated September 10, 1998; 767-35-0033, dated September 10, 1998; or 777-35-0005, dated September 3, 1998; as applicable.
-
Boeing Model 767 Series Airplanes
Applicability, as the AD words it
Model 767 series airplanes, line numbers 1 through 663 inclusive, certificated in any category.
- AD 2000-10-51 Recurring
Boeing Model 767 Series Airplanes
To detect and correct cracking or fracturing of the tension bolts on the side load underwing fittings on the strut, which would eventually result in loss of the strut.
Applicability, as the AD words it
Model 767 series airplanes, line numbers (L/N) 1 through 230 inclusive, certificated in any category.
- AD 2000-11-10 One-time Engine
Rolls-Royce plc RB211 Series Turbofan Engines
To prevent an uncontained engine failure due to rupture of an IP compressor stage 6-7 rotor shaft.
Applicability, as the AD words it
Rolls-Royce plc (R-R) Model RB211-22B and -524 series turbofan engines, not incorporating new intermediate pressure (IP) compressor stage 6-7 rotor shafts assemblies with redesigned stage 6 disks in accordance with R-R Service Bulletin (SB) No. RB.211-72-9993, dated August 26, 1994. These engines are installed on but not limited to Boeing 747 series and 767 series, and Lockheed L-1011 series aircraft.
- AD 2000-11-08 One-time Engine
Boeing Model 747 and 767 Series Airplanes Powered by General Electric Model CF6-80C2 Series Engines
To prevent engine flameouts due to the use of JP-4 or Jet B fuel on certain engines with dribble flow fuel nozzles (DFFN) installed, and consequent engine shutdown.
Applicability, as the AD words it
Model 747 and 767 series airplanes, powered by General Electric Model CF6-80C2 series engines, certificated in any category.
- AD 2000-11-06 Superseded by AD 2013-25-02
Boeing Model 767 Series Airplanes
To prevent exposure of electrical conductor, which could permit arcing from the wire to the conduit and create a potential for a fuel tank fire or explosion.
Applicability, as the AD words it
All Model 767 series airplanes, certificated in any category.
- AD 2000-09-04 Recurring Engine
Boeing Model 767 Series Airplanes Equipped with General Electric Model CF6-80C2 Series Engines
To ensure the integrity of the fail safe features of the thrust reverser system by preventing possible failure modes in the thrust reverser control system that can result in inadvertent deployment of a thrust reverser during flight.
Applicability, as the AD words it
Model 767 series airplanes equipped with General Electric Model CF6-80C2 series engines, certificated in any category.
- AD 2000-08-12 Superseded by AD 2002-07-12 Engine
General Electric Company CF6-80A, CF6-80C2, and CF6-80E1 Series Turbofan Engines
To prevent critical life-limited rotating engine part failure, which could result in an uncontained engine failure and damage to the airplane.
Applicability, as the AD words it
General Electric Company (GE) CF6-80A, CF6-80C2, and CF6-80E1 series turbofan engines, installed on but not limited to Airbus Industrie A300, A310, and A330 series, Boeing 747 and 767 series, and McDonnell Douglas MD-11 series airplanes.
- AD 2000-07-05 Recurring
Boeing Model 767 Series Airplanes
To prevent cracking of the diagonal brace of the nacelle strut, which could result in failure of the diagonal brace, and consequent fatigue failure of a strut secondary load path and separation of the engine and strut.
Applicability, as the AD words it
Model 767 series airplanes; as listed in Boeing Alert Service Bulletin 767-54A0094, dated May 22, 1998; certificated in any category.
- AD 2000-05-12 Superseded by AD 2002-02-12 Engine
Rolls-Royce plc RB211-524 Series Turbofan Engines
To prevent possible multiple fan blade failures, which could result in an uncontained engine failure and damage to the aircraft.
Applicability, as the AD words it
Rolls-Royce plc (R-R) Models RB211-524G2-19, RB211-524G3-19, RB211-524H2-19, RB211-524G2-T-19, RB211-524G3-T-19, RB211-524H2-T-19, and RB211-524H-36 turbofan engines, with fan blades, part numbers (P/Ns) UL36245, UL38009, UL38052, or UL38628, installed. These engines are installed on but not limited to Boeing 747-400 series and 767 series airplanes.
- AD 2000-03-21 One-time
Boeing Model 767 Series Airplanes
To prevent interference between the landing gear control lever and wire bundles adjacent to the landing gear control lever module, and to prevent wire chafing and arcing between the landing gear control cable and adjacent wire bundles, which could result in the inability to extend the landing gear prior to landing.
Applicability, as the AD words it
Model 767 airplanes, as listed in Boeing Service Bulletin 767-32A0163, Revision 1, dated October 1, 1998; certificated in any category.
- AD 2000-03-07 One-time Engine
Rolls-Royce plc RB211-524H-36 Series Turbofan Engines
To prevent burn through of the combustor case due to combustor liner cracking, which can result in an engine fire and damage to the aircraft.
Applicability, as the AD words it
Rolls-Royce plc (R-R) RB211-524H-36 series turbofan engines installed on but not limited to Boeing 767 series airplanes.
- AD 2000-03-04 One-time Engine
General Electric Company CF6-80C2 Series Turbofan Engines
To prevent fan mid shaft failure, which could result in an uncontained engine failure and damage to the aircraft.
Applicability, as the AD words it
General Electric Company (GE) CF6-80C2 series turbofan engines, with fan mid shafts, part number (P/N) 9326M74P04 or P/N 9326M74P05, installed. These engines are installed on but not limited to Airbus Industrie A300 and A310 series, Boeing 747 and 767 series, and McDonnell Douglas MD-11 series aircraft.
- AD 2000-02-20 Superseded by AD 2000-09-04 Engine
Boeing Model 767 Series Airplanes Equipped With General Electric Model CF6-80C2 Series Engines
To ensure the integrity of the fail safe features of the thrust reverser system by preventing possible failure modes in the thrust reverser control system that can result in inadvertent deployment of a thrust reverser during flight.
Applicability, as the AD words it
Model 767 series airplanes equipped with General Electric Model CF6-80C2 series engines, certificated in any category.
- AD 2000-01-13 Superseded by AD 2002-08-11 Engine
Pratt & Whitney JT9D Series Turbofan Engines
To prevent critical life-limited rotating engine part failure, which could result in an uncontained engine failure and damage to the airplane.
Applicability, as the AD words it
Pratt & Whitney (PW) JT9D-7, -7A, -7H, -7AH, -7F, -7J, -20, - 20J, -59A, -70A, -7Q, -7Q3, -7R4D, -7R4D1, -7R4E, -7R4E1, -7R4E4, - 7R4G2, and -7R4H1 series turbofan engines, installed on but not limited to Boeing 747 and 767 series, McDonnell Douglas DC-10 series, and Airbus Industrie A300 and A310 airplanes.
- AD 99-26-09 Recurring
Boeing Model 767 Series Airplanes
To prevent possible separation of the engine from the airplane in the event of a primary thrust linkage failure.
Applicability, as the AD words it
Model 767 series airplanes, powered by Pratt & Whitney Model JT9D or Model PW4000 series engines, as listed in Boeing Alert Service Bulletin 767-71A0087, dated October 10, 1996; certificated in any category.
- AD 99-26-02 One-time Engine
Boeing Model 747-400 and 767 Series Airplanes Powered by Pratt & Whitney PW4000 Series Engines
To prevent failure of the thrust reverser deactivation pins, which could result in deployment of the thrust reverser in flight and consequent reduced controllability of the airplane.
Applicability, as the AD words it
Model 747-400 series airplanes powered by Pratt & Whitney PW4000 series engines, as listed in Boeing Service Bulletin 747-78A2165, Revision 1, dated May 13, 1999; and Model 767 series airplanes powered by Pratt & Whitney PW4000 series engines, as listed in Boeing Alert Service Bulletin 767-78A0080, dated February 25, 1999; certificated in any category.
- AD 99-24-15 Recurring Engine
General Electric Company CF6 Series Turbofan Engines
To prevent HPCR stage 3-9 spool cracking and separation, which can result in an uncontained engine failure and aircraft damage.
Applicability, as the AD words it
General Electric Company (GE) CF6-45, -50, -80A, -80C2 and -80E1 series turbofan engines, with High Pressure Compressor Rotor (HPCR) stage 3-9 spools, part numbers (P/Ns) 1333M66G01, 1333M66G03, 1333M66G07, 1333M66G09, 1333M66G10, 1669M22G01, 1669M22G03, 1781M52P01, 1781M53G01, 1782M22G01, 1782M22G02, 1782M22G04, 1854M95P01, 1854M95P02, 1854M95P03, 1854M95P04, 1854M95P05, 1854M95P06, 1854M95P07, 1854M95P08, 9136M89G02, 9136M89G03, 9136M89G06, 9136M89G07, 9136M89G08, 9136M89G09, 9136M89G10, 9136M89G11, 9136M89G17, 9136M89G18, 9136M89G19, 9136M89G20, 9136M89G21, 9136M89G22, 9136M89G27, 9136M89G28, 9136M89G29, 9253M85G01, 9253M85G02, 9273M14G01, 9331M29G01, and 9380M28P05 installed. These engines are installed on but not limited to Airbus A300, A310, and A330 series, Boeing 747 and 767 series, and McDonnell Douglas DC-10 and MD-11 series aircraft.
- AD 98-21-22 Recurring Engine
Pratt & Whitney JT9D Series Turbofan Engines
To prevent 14th and 15th stage HPC disk rupture, which could result in an uncontained engine failure and damage to the airplane.
Applicability, as the AD words it
Pratt & Whitney (PW) Model JT9D-59A, -70A, -7Q, - 7Q3, and JT9D-7R4 series turbofan engines, with the following 14th and 15th stage high pressure compressor (HPC) disks installed: Part Numbers (P/Ns) 5000814-01, 790014, 789914, 790114, 5000815-01, 5000815-021, 704315, 704315-001, 786215, 786215-001, 704314, 789814, and 790214. These engines are installed on but not limited to Airbus A300 and A310 series aircraft, Boeing 747 and 767 series aircraft, and McDonnell Douglas DC- 10 series aircraft.
- AD 99-21-18 Recurring Engine
Boeing Model 767 Series Airplanes Powered by Pratt & Whitney JT9D-7R4 Series Turbofan Engines or General Electric CF6-80A Series Turbofan Engines
To prevent engine thrust control cable failure, which could result in a severe asymmetric thrust condition during landing, and consequent reduced controllability of the airplane.
Applicability, as the AD words it
Model 767 series airplanes powered by Pratt & Whitney JT9D-7R4 series turbofan engines or General Electric CF6-80A series turbofan engines, certificated in any category.
- AD 99-19-29 Recurring
Boeing Model 767 Series Airplanes
To prevent cracking of the H-11 tension bolts on the side-of- body kick-load fitting due to stress corrosion, which could result in reduced structural integrity of the wing-to-body joint structure.
Applicability, as the AD words it
Model 767 series airplanes, line positions 1 through 177 inclusive, certificated in any category.
- AD 99-11-14 Recurring
Boeing Model 767 Series Airplanes
To detect and correct corrosion and cracking of the fuse pins in the outboard support of the MLG beam, which could result in the failure of a fuse pin and, consequently, lead to collapse of the MLG.
Applicability, as the AD words it
Model 767 series airplanes, line numbers 1 through 609 inclusive; certificated in any category; having 4330M steel fuse pins installed in the outboard support of the main landing gear (MLG) beam.
- AD 99-10-08 Recurring
Boeing Model 767 Series Airplanes
To prevent corrosion of the forward trunnion joint of the main landing gear (MLG), which could lead to a stress corrosion fracture of the forward trunnion and possible consequent collapse of the MLG.
Applicability, as the AD words it
Model 767 series airplanes, manufacturer's line positions 001 through 455 inclusive, certificated in any category.
- AD 99-08-13 Superseded by AD 2000-08-12 Engine
General Electric Company CF6-80A, CF6- 80C2, and CF6-80E1 Series Turbofan Engines
To prevent critical life-limited rotating engine part failure, which could result in an uncontained engine failure and damage to the airplane.
Applicability, as the AD words it
General Electric Company CF6-80A, CF6-80C2 and CF6-80E1 series turbofan engines, installed on but not limited to Airbus A300, A310, and A330 series, Boeing 747 and 767 series, and McDonnell Douglas MD-11 series airplanes.
- AD 99-08-12 Superseded by AD 2000-01-13 Engine
Pratt & Whitney JT9D Series Turbofan Engines
To prevent critical life-limited rotating engine part failure, which could result in an uncontained engine failure and damage to the airplane.
Applicability, as the AD words it
Applicability: Pratt & Whitney (PW) JT9D-3A, -7, -7H, -7A, -7AH, -7F, -7J, -20J, -59A, -70A, -7Q, -7Q3, -7R4D, - 7R4D1, -7R4E, -7R4E1, -7R4G2, -7R4H1, and 7R4E4 series turbofan engines, installed on but not limited to Boeing 747 and 767 series, McDonnell Douglas DC-10 series, and Airbus A300 and A310 series airplanes.
- AD 99-07-06 Superseded by AD 2000-07-05
Boeing Model 767 Series Airplanes
To detect and correct cracking of the diagonal brace of the nacelle strut, which could result in failure of the diagonal brace, and consequent fatigue failure of a strut secondary load path and separation of the engine and strut.
Applicability, as the AD words it
Model 767 series airplanes; as listed in Boeing Alert Service Bulletin 767-54A0094, dated May 22, 1998; certificated in any category.
- AD 98-23-07 Removed 1999-07-30 Engine
Pratt & Whitney JT9D Series Turbofan Engines
To prevent turbine exhaust case (TEC) structural failure under abnormal operating conditions, which could result in reduced main mount load capability, engine separation from the wing and subsequent loss of aircraft control.
Applicability, as the AD words it
Pratt & Whitney (PW) Models JT9D-7, -7A, -7H, - 7AH, -7F, -7J, -20, -20J, -7Q, -7Q3, -59A, -70A, and -7R4D turbofan engines. These engines are installed on but not limited to Boeing 747 and 767 series, McDonnell Douglas DC-10 series, and Airbus A300 and A310 series aircraft.
- AD 98-23-05 One-time
Boeing Model 767 Series Airplanes
To prevent wire chafing and subsequent electrical arcing in the vicinity of the stowage box for the captain's oxygen mask, which could result in a fire in the flight compartment.
Applicability, as the AD words it
Model 767 series airplanes, as listed in Boeing Alert Service Bulletin 767-35A0029, dated January 30, 1997; certificated in any category.
- AD 98-22-12 Superseded by AD 2003-14-09
Boeing Model 767 Series Airplanes
To prevent separation of the inboard trailing edge flap from the airplane due to fractured collar fittings.
Applicability, as the AD words it
Model 767 series airplanes, line numbers 1 through 721 inclusive, certificated in any category.
- AD 98-19-03 One-time Engine
Pratt & Whitney PW4000 Series Turbofan Engines
To prevent 2nd stage HPT rotating airseal cracking, which could result in an uncontained engine failure and damage to the aircraft.
Applicability, as the AD words it
Pratt & Whitney Models PW4052, PW4056, PW4060, PW4060A, PW4062, PW4152, PW4156A, PW4158, PW4460, PW4462, PW4164, and PW4168 turbofan engines, with 2nd stage high pressure turbine (HPT) rotating airseals, Part Numbers (P/N) 50L156 or 50L195, installed. These engines are installed on but not limited to Boeing 747 and 767 series, McDonnell Douglas MD-11 series, and Airbus Industrie A300, A310, and A330 series aircraft.
- AD 98-17-13 One-time Engine
Boeing Model 747 and 767 Series Airplanes Equipped with Rolls-Royce Model RB211-524G/H Engines
To prevent failure of the engine fire detection system to annunciate a fire warning message to the flight crew following a severe engine failure, which could lead to delayed or improper flight crew response to the engine failure.
Applicability, as the AD words it
Model 747 and 767 series airplanes, equipped with Rolls-Royce Model RB211-524G/H engines; certificated in any category.
- AD 98-16-07 Recurring
Boeing Model 767 Series Airplanes
To detect and correct corrosion or plating cracks of the pin assemblies in the front trunnion support of the main landing gear (MLG), which could cause these assemblies to break and result in collapse of the MLG.
Applicability, as the AD words it
Model 767 series airplanes having line positions 1 through 562 inclusive, certificated in any category.
- AD 98-10-10 One-time
Boeing Model 747 and 767 Series Airplanes
To prevent chafing of the wire insulation inside conduits installed in the fuel tanks, which could eventually expose the electrical conductor creating the potential for arcing from the wire to the conduit, and consequent fuel tank fire/explosion.
Applicability, as the AD words it
Model 747 series airplanes, line positions 0001 through 1145 inclusive, that have not been inspected in accordance with AD 96-26-06, amendment 39-9870 (reference Boeing Alert Service Bulletin 747-28A2204, dated December 19, 1996), or AD 97-26-07, amendment 39-10250 (reference Boeing Alert Service Bulletin 747- 28A2204, Revision 1, dated October 30, 1997); and Model 767 series airplanes, line positions 001 through 689 inclusive, and 691; certificated in any category.
- AD 98-08-23 Superseded by AD 2000-11-08 Engine
Boeing Model 747 and 767 Series Airplanes Equipped With General Electric (GE) CF6-80C2 Engines
To prevent engine flameouts due to the use of JP-4 or Jet B fuel on certain engines with dribble flow fuel nozzles (DFFN's) installed and consequent shutdown.
Applicability, as the AD words it
All Model 747 and 767 series airplanes having General Electric CF6-80C2 engines, certificated in any category.
- AD 98-07-26 Recurring
Boeing Model 767 Series Airplanes
To prevent arcing between exposed conductors, which could result in burning of the adjacent electrical bundles, failure of essential electrical systems, and consequent fire hazard for passengers and crewmembers.
Applicability, as the AD words it
Model 767 series airplanes, line numbers 1 through 683 inclusive, equipped with forward galley air chillers; certificated in any category.
- AD 98-03-10 One-time
Boeing Model 737, 747, 757, and 767 Series Airplanes
To prevent uncommanded movement of the pilots' seats during acceleration and take-off of the airplane, and consequent reduced controllability of the airplane.
Applicability, as the AD words it
Models 737, 747, 757, and 767 series airplanes, certificated in any category; equipped with non-powered IPECO pilots' seats; and having the following line position numbers: Airplane model Line position Nos. 737: 1 through 2836 inclusive. 747: 1 through 1104 inclusive. 757: 1 through 731 inclusive. 767: 1 through 642 inclusive.
- AD 97-22-04 Superseded by AD 98-08-23 Engine
Boeing Model 747 and 767 Series Airplanes Equipped With General Electric (GE) CF6-80C2 Engines
To prevent engine flameout and consequent shutdown due to the use of JP-4 or Jet B fuel.
Applicability, as the AD words it
Model 747 series airplanes having line positions 679 through 1117 inclusive, and Model 767 series airplanes having line positions 158 through 661 inclusive; equipped with General Electric (GE) CF6-80C2 engines, on which dribble flow fuel nozzles (DFFN's) having General Electric part number 9331M72P33, 9331M72P34, or 9331M72P41, have been installed; certificated in any category.
- AD 97-19-15 Superseded by AD 2001-15-08
Boeing Model 767 Series Airplanes
To prevent the generation of sparks and a potential ignition source inside the fuel tank caused by metal-to-metal contact during dry fuel pump operation.
Applicability, as the AD words it
All Model 767 series airplanes, certificated in any category.
- AD 97-16-03 One-time
Boeing Model 767 Series Airplanes
To prevent aft-acting landing gear trunnion loads from being transferred to the main landing gear (MLG) beam, and consequent fracture and collapse of the MLG and loss of control of the airplane on the ground.
Applicability, as the AD words it
Model 767 series airplanes, line positions 1 through 600 inclusive, except line positions 579 and 586; certificated in any category.
- AD 97-15-09 Recurring
Boeing Model 757 and 767 Series Airplanes
To detect and correct improperly installed/maintained auxiliary power unit (APU) battery grounds, which could result in heat damage and consequent smoke/fire on the airplane.
Applicability, as the AD words it
All Model 757 and 767 series airplanes, certificated in any category.
- AD 97-15-06 Superseded by AD 98-03-10
Boeing Model 737, 747, 757, and 767 Series Airplanes
Applicability, as the AD words it
Model 737, 747, 757, and 767 series airplanes equipped with IPECO pilots' seats; as listed in Boeing Service Bulletins 737-25-1334, 747-25-3132, 757-25-0183, and 767-25-0244; all dated December 19, 1996; certificated in any category.
- AD 97-08-51 Superseded by AD 2003-09-08
Boeing Model 767 Series Airplanes
To prevent separation of the outboard trailing edge flap from the airplane due to failed bolts of the attach fitting.
Applicability, as the AD words it
Model 767 series airplanes, certificated in any category.
- AD 97-02-19 One-time
Boeing Model 757 and 767 Series Airplanes
To prevent runaway of the autothrottle during flight or ground operations, which could distract the crew from normal operation of the airplane or lead to an unintended speed or altitude change.
Applicability, as the AD words it
Model 757 series airplanes, having line positions 001 through 716, inclusive; and Model 767 series airplanes having line positions 001 through 556 inclusive, 558 through 587 inclusive, and 589 through 615 inclusive; certificated in any category.
- AD 96-25-18 Recurring
Boeing Model 767 Series Airplanes
To prevent reduced controllability of the airplane and damage to or cracking of the leading edge slats or the fixed leading edge of the wing.
Applicability, as the AD words it
All Model 767 series airplanes, certificated in any category.
- AD 96-25-10 One-time Engine
Pratt & Whitney JT9D Series Turbofan Engines
To prevent release of uncontained debris from the turbine exhaust case (TEC) following an internal engine failure, which can result in damage to the aircraft.
Applicability, as the AD words it
Pratt & Whitney (PW) JT9D-3, -7, -20, -59A, -70A, -7Q, and -7R4 series turbofan engines, installed on but not limited to Airbus A300 and A310 series; Boeing 747 and 767 series; and McDonnell Douglas DC-10 series aircraft.
- AD 96-21-06 Superseded by AD 2002-01-13
Boeing Model 767 Series Airplanes
To prevent the collapse of the main landing gear (MLG) due to stress corrosion cracking of the aft trunnion of the outer cylinder.
Applicability, as the AD words it
Model 767 series airplanes having line numbers 001 through 605 inclusive, on which the terminating action required by paragraph (e) of this AD has not been accomplished; certificated in any category.
- AD 96-20-05 Recurring
Boeing Model 767 Series Airplanes
To ensure that the RAT actuator motor is not corroded to the point where it may result in the failure of the RAT to deploy and subsequently result in loss of emergency hydraulic power to the flight controls in the event that power is lost in both engines.
Applicability, as the AD words it
All Model 767 series airplanes, certificated in any category.
- AD 96-19-10 One-time
Boeing Model 767 Series Airplanes
To prevent interruptions of electrical power during flight, which could result in loss of battery power to the source of standby power for the airplane.
Applicability, as the AD words it
Model 767 series airplanes, as listed in Boeing Alert Service Bulletin 767-24A0112, Revision 1, dated August 8, 1996; certificated in any category.
- AD 96-17-11 One-time Engine
Pratt & Whitney JT9D-7R4 Series Turbofan Engines
To prevent low pressure turbine (LPT) vane failures, which can result in uncontained engine failure, fire, and possible damage to the aircraft.
Applicability, as the AD words it
Pratt & Whitney (PW) JT9D-7R4 series turbofan engines, installed on but not limited to Airbus A300 and A310 series, and Boeing 747 and 767 series aircraft. Note: This airworthiness directive (AD) applies to each engine identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For engines that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (e) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and, if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it.
- AD 96-14-51 One-time
Boeing Model 767 Series Airplanes
To prevent reduced controllability of the airplane due to failure of the aileron control cable.
Applicability, as the AD words it
Model 767 series airplanes; line numbers 1 through 618 inclusive, except for line numbers 580, 590, 594, 598, and 600; certificated in any category.
- AD 96-14-05 Recurring
Boeing Model 767 Series Airplanes
To prevent loss of the pilot's ability to control the affected slat, which could adversely affect the controllability of the airplane.
Applicability, as the AD words it
Model 767 series airplanes; as listed in Boeing Service Bulletin 767-57-0021, Revision 1, dated September 14, 1989, or Revision 5, dated June 15, 1995; certificated in any category.
- AD 96-14-02 One-time Engine
Boeing Model 767 Series Airplanes Equipped With Pratt & Whitney Model JT9D-7R4 Engines
To prevent chafing of the number 18 fuel nozzle secondary transfer fuel tube of the engine, and subsequent fuel leakage and possible engine fire.
Applicability, as the AD words it
Model 767 series airplanes having line position 1 through 329, inclusive; equipped with Pratt & Whitney Model JT9D-7R4 engines; certificated in any category.
- AD 96-07-09 One-time
Boeing Model 747-400, 757, and 767 Series Airplanes
To ensure that the flight crew is appropriately aware of conditions involving a severely contaminated airplane fuel system and the associated increased potential for engine power loss.
Applicability, as the AD words it
All Model 747-400, 757, and 767 series airplanes; certificated in any category.
- AD 96-06-09 One-time
Boeing Model 767 Series Airplanes
To prevent loss of shutdown protection for the trailing edge flap drive, which could result in reduced controllability of the airplane in the event of uncommanded or asymmetrical flap motion.
Applicability, as the AD words it
Model 767 series airplanes, having serial number 26847, 27048, or 27049, certificated in any category.
- AD 95-25-08 One-time Appliance
Royal Inventum Company DR1 and DR6 Series Galley Water Heaters
To prevent possible explosion of water heaters that could cause personal injury and aircraft damage.
Applicability, as the AD words it
Royal Inventum Company DR1 and DR6 series galley water heaters, installed on but not limited to Boeing 727, 737, 747, 757 and 767 series, McDonnell Douglas DC-9 series; and Fokker F.28 series (except Mk. 0100) aircraft. Note: This AD applies to each water heater identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For water heaters that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must use the authority provided in paragraph (b) to request approval from the FAA. This approval may address either no action, if the current configuration eliminates the unsafe condition, or different actions necessary to address the unsafe condition described in this AD. Such a request should include an assessment of the effect of the changed configuration on the unsafe condition addressed by this AD. In no case does the presence of any modification, alteration, or repair remove any water heater from the applicability of this AD.
- AD 96-03-02 Superseded by AD 96-21-06
Boeing Model 767 Series Airplanes
To prevent the collapse of the main landing gear (MLG) due to stress corrosion cracking of the aft trunnion of the outer cylinder.
Applicability, as the AD words it
Model 767 series airplanes having line numbers 001 through 609, on which the terminating action described in paragraph (e) of this AD has not been accomplished; certificated in any category.
- AD 95-23-03 Superseded by AD 99-24-15 Engine
General Electric Company CF6 Series Turbofan Engines
To prevent high pressure compressor rotor (HPCR) stage 3-9 spool cracking and separation, which can result in an uncontained engine failure and aircraft damage.
Applicability, as the AD words it
General Electric Company (GE) CF6-45/-50/-80A/- 80C2 series turbofan engines installed with High Pressure Compressor Stage 3-9 Spools, Part Numbers (P/Ns) 1333M66G01, 1333M66G03; 1333M66G07, 1333M66G09, 1781M52P01, 1781M53G01,1854M95P01, 1854M95P02, 1854M95P03, 1854M95P04, 1854M95P05, 1854M95P06; 9136M89G02, 9136M89G03, 9136M89G06, 9136M89G07, 9136M89G08, 9136M89G09, 9136M89G10, 9136M89G11, 9136M89G17, 9136M89G18, 9136M89G19, 9136M89G20, 9136M89G21, 9136M89G22, 9136M89G27, 9253M85G01, 9253M85G02, 9273M14G01, 9331M29G01, and 9380M28P05 installed on, but not limited to, Airbus A300 and A310 series, Boeing 747 and 767 series, and McDonnell Douglas DC-10 and MD-11 series aircraft. Note: This airworthiness directive (AD) applies to each engine identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For engines that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must use the authority provided in paragraph (o) to request approval from the Federal Aviation Administration (FAA). This approval may address either no action, if the current configuration eliminates the unsafe condition, or different actions necessary to address the unsafe condition described in this AD. Such a request should include an assessment of the effect of the changed configuration on the unsafe condition addressed by this AD. In no case does the presence of any modification, alteration, or repair remove any engine from the applicability of this AD.
- AD 95-21-05 Superseded by AD 98-23-05
Boeing Model 767 Series Airplanes
To prevent wire chafing and subsequent electrical arcing in the vicinity of the stowage box for the captain's oxygen mask, which could result in a fire in the flight compartment.
Applicability, as the AD words it
Model 767 series airplanes; line positions 2 through 589 inclusive except VA801 through VA810 inclusive, VN684 through VN691 inclusive, and VW701; certificated in any category.
- AD 95-19-10 Recurring
Boeing Model 767 Series Airplanes
To prevent stress corrosion cracking, which could result in fractures of the outer cylinder aft trunnion and the subsequent loss of the main landing gear (MLG).
Applicability, as the AD words it
All Model 767 series airplanes, certificated in any category.
- AD 95-18-03 One-time
Boeing Model 767 Series Airplanes Equipped With BFGoodrich Off-Wing Ramp/Slide Evacuation Systems
To prevent tube puncture of the ramp/slide evacuation system, which could delay or impede the evacuation of passengers during an emergency.
Applicability, as the AD words it
Model 767 series airplanes, equipped with BFGoodrich off-wing ramp/slide evacuation systems having part number (P/N) 101630, 101655, or 101656; certificated in any category.
- AD 95-18-02 One-time
Boeing Model 757 and 767 Series Airplanes Equipped With Sundstrand Ram Air Turbine (RAT)/Hydraulic Pumps
To prevent overload of the hydraulic pressure transfer tube, which could result in cracking of the tube of the ram air turbine (RAT), and subsequently could lead to the loss of all center systems hydraulic fluid and the inability of the RAT to pressurize the center hydraulic system.
Applicability, as the AD words it
Model 757 series airplanes having line positions 1 through 650 inclusive, and equipped with Sundstrand ram air turbine (RAT)/hydraulic pumps having part number (P/N) 730814 series, serial numbers 0001 through 0735 inclusive; and Model 767 series airplanes having line positions 1 through 564 inclusive, and equipped with Sundstrand RAT/hydraulic pumps having P/N 729548 series, serial numbers 0001 through 0620 inclusive; certificated in any category.
- AD 95-17-16 One-time Engine
General Electric Company CF6 Series Turbofan Engines
To prevent a compressor rear frame (CRF) separation, which could result in a rejected takeoff and damage to the aircraft.
Applicability, as the AD words it
General Electric Company (GE) CF6-80A series turbofan engines installed on, but not limited to, Airbus A310 series and Boeing 767 series aircraft. Note: This airworthiness directive (AD) applies to each engine identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For engines that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must use the authority provided in paragraph (d) to request approval from the Federal Aviation Administration (FAA). This approval may address either no action, if the current configuration eliminates the unsafe condition, or different actions necessary to address the unsafe condition described in this AD. Such a request should include an assessment of the effect of the changed configuration on the unsafe condition addressed by this AD. In no case does the presence of any modification, alteration, or repair remove any engine from the applicability of this AD.
- AD 95-18-14 Superseded by AD 2002-25-08 Engine
General Electric Company CF6 Series Turbofan Engines
To prevent an uncontained high pressure compressor rotor (HPCR) engine failure, which can result in damage to the aircraft.
Applicability, as the AD words it
General Electric Company (GE) CF6 series engines. These engines are installed on but not limited to Airbus Industries A300, A310, and A330 series; Boeing 747 and 767 series; and McDonnell Douglas DC10 and MD11 series aircraft. Note: This AD applies to each engine identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For engines that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must use the authority provided in paragraph (b) to request approval from the FAA. This approval may address either no action, if the current configuration eliminates the unsafe condition, or different actions necessary to address the unsafe condition described in this AD. Such a request should include an assessment of the effect of the changed configuration on the unsafe condition addressed by this AD. In no case does the presence of any modification, alteration, or repair remove any engine from the applicability of this AD.
- AD 95-15-01 One-time
Boeing Model 767 Series Airplanes Equipped with Over-Wing Escape Slides
To prevent damage to the over-wing escape slide, which could hinder inflation of the slide to a usable configuration during an emergency evacuation.
Applicability, as the AD words it
Model 767 series airplanes, having line positions 1 through 542 inclusive, and equipped with over-wing escape slides; certificated in any category.
- AD 95-13-12 Superseded by AD 2000-02-20 Engine
Boeing Model 767 Series Airplanes Equipped With General Electric CF6-80C2 Series Engines
To ensure the integrity of the fail-safe features of the thrust reverser system.
Applicability, as the AD words it
Model 767 series airplanes equipped with General Electric CF6-80C2 series engines, certificated in any category.
- AD 95-08-11 Recurring
Boeing Model 767 Series Airplanes Equipped With Off-Wing Escape Slides
To prevent failure of the escape slide to deploy, which could delay and possibly jeopardize successful emergency evacuation of an airplane.
Applicability, as the AD words it
Model 767 series airplanes equipped with off-wing escape slides, certificated in any category.
- AD 95-03-01 Superseded by AD 95-23-03 Engine
General Electric Company CF6 Series Turbofan Engines
To prevent an uncontained high pressure compressor rotor (HPCR) stage 3-9 spool failure, which could result in damage to the aircraft.
Applicability, as the AD words it
General Electric Company (GE) CF6-45/-50/-80A series turbofan engines installed on, but not limited to, Airbus A300 and A310 series, Boeing 747 and 767 series, and McDonnell Douglas DC-10 series aircraft.
Radar reads the logbooks and ties each AD to the entries that show how and when it was complied with, with recurring ADs due by date and hours.
QUESTIONS
AD lookup questions
Sources: FAA final rules under 14 CFR part 39, from the Federal Register; make and model from the FAA aircraft registry. The FAA’s Dynamic Regulatory System holds the official AD list.
What is an airworthiness directive (AD)?
An airworthiness directive is a legally enforceable rule the FAA issues under 14 CFR part 39 when it finds an unsafe condition in an aircraft, engine, propeller or appliance that is likely to exist in others of the same design. It says which products it applies to and what must be done, and by when: an inspection, a part replacement, a modification or a limitation. No one may operate a product to which an AD applies except in accordance with it.
How do I look up the ADs for my aircraft?
Type the N-number, or the make and model, into the box above. Radar finds the aircraft's make and model in the FAA registry and lists every AD published in the Federal Register whose applicability names it, newest first, with the AD's own applicability text and a link to the official document. The FAA's Dynamic Regulatory System (drs.faa.gov) holds the official list.
Does every AD in the results apply to my aircraft?
Not necessarily. An AD can be limited to serial number ranges, to aircraft with certain parts or modifications installed, or to a configuration. The results are ADs that may apply because they name the make and model. A certificated mechanic or inspector determines applicability against the aircraft's serial number and records, and records how each applicable AD was complied with.
What is the difference between a recurring and a one-time AD?
A one-time AD is complied with once, for example by replacing a part. A recurring (repetitive) AD requires an action again at an interval, such as an inspection every 100 hours or every 12 months, until a terminating action ends it. Radar marks an AD Recurring when its text requires repetitive actions; always read the AD for the intervals.
What does superseded mean?
When the FAA replaces an AD with a new one, the old AD is superseded: its requirements are carried into, or replaced by, the new AD. Results show the ADs in effect by default; superseded and removed ADs can be shown for the history.
Where does this data come from?
The Federal Register, where the FAA publishes every AD as a final rule. Radar reads each one from the Federal Register API (12,857 ADs since 1995) and refreshes the list every weekday. Make and model come from the FAA aircraft registry. ADs issued before 1995 are not in the Federal Register's online edition and are not included.
Are engine and propeller ADs included?
Only when their applicability names the aircraft. Most engine and propeller ADs name the engine or propeller model, so check those by the installed engine and propeller models. Appliance ADs that list the aircraft among those the appliance can be installed on are included and marked Appliance.
Know which ADs apply, and where each one was signed off.
Radar reads every logbook page, typed or handwritten, and builds one searchable record per tail: times, inspections, ADs and components, each tied to the page it came from.