Boeing 757-223 airworthiness directives FAA ADs that may apply, with the official text
- In effect
- 35
- Recurring
- 12
- Superseded or removed12
- Latest2005-18-03
Boeing 757-223: price, specs and every tail number · Look up ADs by N-number · AD burden by model, ranked
IN EFFECT
35 Boeing 757-223 ADs in effect, newest first
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.
- AD 2005-18-03 One-time Engine
Pratt & Whitney PW2000 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) PW2037, PW2040, PW2043, PW2143, PW2643, PW2037D, PW2037M, and PW2040D series turbofan engines. These engines are installed on, but not limited to Boeing 757 series and Ilyushin IL-96T series airplanes.
- AD 2005-12-18 Recurring
Boeing Model 757 Series Airplanes
To prevent grease contamination on the primary horizontal stabilizer trim actuator (HSTA) brake and consequent loss of the primary brake function, which, in combination with the loss of the secondary HSTA brake function, could result in loss of control of the airplane.
Applicability, as the AD words it
All Model 757-200, -200PF, -200CB, and -300 series airplanes, certificated in any category.
- AD 2005-05-01 One-time
Boeing Model 757 Series Airplanes
This AD was prompted by a report of damage caused by an electrical arc in a connector on the cable assembly for the lower anti-collision light.
Applicability, as the AD words it
This AD applies to Boeing Model 757-200, -200CB, and -200PF series airplanes identified in Boeing Alert Service Bulletin 757- 33A0048, dated March 28, 2002; and Boeing Model 757-300 series airplanes identified in Boeing Alert Service Bulletin 757-33A0049, dated March 28, 2002; certificated in any category.
- AD 2005-02-10 Recurring Engine
Boeing Model 757 Series Airplanes Equipped With Rolls Royce Model RB211 Engines
To prevent flammable fluids from leaking into the interior compartment of the nacelle struts where ignition sources exist, which could result in the ignition of flammable fluids and an uncontained fire.
Applicability, as the AD words it
Model 757 series airplanes; certificated in any category; line numbers 1 through 1018 inclusive; equipped with Rolls Royce Model RB211 engines.
- AD 2002-24-51 One-time
Boeing Model 737-600, -700, -700C, -800, and -900 Series Airplanes; Model 747 Series Airplanes; and Model 757 Series Airplanes
Applicability, as the AD words it
Model 737-600, -700, -700C, -800, and -900 series airplanes; Model 747 series airplanes; and Model 757 series airplanes; certificated in any category.
- AD 2002-19-52 One-time
Boeing Model 737-600, -700, -700C, -800, and -900 Series Airplanes; Model 747 Series Airplanes; and Model 757 Series Airplanes
To prevent fuel vapors from coming into contact with an ignition source in the center wing fuel tank, horizontal stabilizer fuel tank, center auxiliary fuel tank, or auxiliary fuel tanks 1 and 4, which could result in fire/explosion.
Applicability, as the AD words it
All Model 737-600, -700, -700C, "800, and -900; 747; and 757 series airplanes; certificated in any category.
- AD 2002-10-02 One-time
Boeing Model 757 Series Airplanes
To prevent contact between the compensator for the Simmonds fuel quantity indication system (FQIS) and a flapper check valve on a baffle rib in the main fuel tanks, which--in conjunction with another wiring failure outside the fuel tank--could result in an electrical arc and a consequent potential source of ignition in the fuel tank.
Applicability, as the AD words it
Model 757 series airplanes listed in Boeing Service Bulletin 757-28-0057 or 757-28-0059, both Revision 1, both dated February 28, 2002, certificated in any category.
- AD 2002-02-04 One-time
Boeing Model 757 Series Airplanes
To prevent chafing between the wire bundle and the left wing front spar, which could result in electrical arcing and subsequent ignition of flammable vapors and possible uncontrollable fire.
Applicability, as the AD words it
Model 757 series airplanes, certificated in any category, as listed in Boeing Service Bulletins 757-29-0058 and 757- 29-0059, both dated November 9, 2000.
- AD 2001-23-14 One-time
Boeing Model 757 Series Airplanes
To prevent a fractured spring washer in a geared rotary actuator (GRA) for the leading edge slats, which could lead to a disconnect in the GRA, and result in a slat skew condition and consequent reduced controllability of the airplane.
Applicability, as the AD words it
All Model 757 series airplanes, certificated in any category.
- AD 2001-20-11 Recurring
Boeing Model 757 Series Airplanes
To prevent unacceptable airframe vibration during flight, which could lead to excessive wear of elevator bearings and result in reduced controllability of the airplane.
Applicability, as the AD words it
All Model 757 series airplanes, certificated in any category.
- AD 2001-13-15 One-time Engine
Boeing Model 757 Series Airplanes Equipped with Rolls Royce Engines
To prevent a short circuit that could result in either the possible ignition of fuel vapors in a flammable leakage zone or in the inability to stop the flow of fuel in the event of an engine fire.
Applicability, as the AD words it
Model 757 series airplanes, certificated in any category, equipped with Rolls Royce engines.
- 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.
- AD 2000-09-14 One-time Engine
Rolls-Royce plc RB211-535 Series Turbofan Engines
To prevent radial drive steady bearing failure, which could result in an in-flight engine shutdown and smoke and fumes in the cabin.
Applicability, as the AD words it
Rolls-Royce plc RB211-535 series turbofan engines, with radial drive steady bearings with outer race serial number (S/N) prefixes: DLJO, DLJP, DLOQ, DLSK, and DMBA, installed. Affected engines are those that have had a new bearing fitted at overhaul, were new production engines, or had a bearing changed in service between July 26, 1998, and September 30, 1999. These engines are installed on but not limited to Boeing 757 series aircraft and Tupolev Tu204 series aircraft.
- AD 2000-04-18 One-time
Boeing Model 757 Series Airplanes
Applicability, as the AD words it
Model 757 series airplanes, as listed in Boeing Service Bulletin 757-27A0127, Revision 1, dated September 2, 1999; certificated in any category.
- AD 99-23-21 One-time
Boeing Model 757 Series Airplanes
To prevent operation with an energized sync lock or malfunctioning sleeve locking devices, which could result in deployment of a thrust reverser in flight and subsequent reduced controllability of the airplane.
Applicability, as the AD words it
Model 757 series airplanes, as listed in Boeing Service Bulletin 757-76-0009, Revision 1, dated December 3, 1998, or Boeing Service Bulletin 757-78-0012, dated August 31, 1989; certificated in any category.
- AD 99-08-14 One-time Engine
Pratt & Whitney PW2000 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) PW2037, PW2040, PW2037M, PW2240, PW2337, PW2043, PW2643, and PW2143, series turbofan engines, installed on but not limited to Boeing 757 series and Ilyushin IL- 96T series airplanes.
- AD 99-05-10 One-time
Boeing Model 757 Series Airplanes
To prevent the failure of the actuators used to deploy the RAT.
Applicability, as the AD words it
Model 757 airplanes; equipped with ram air turbine (RAT) deployment actuators having Boeing part number (P/N) S271N102-4 (Arkwin P/N 1211233-004) or Boeing P/N S271N102-5 (Arkwin P/N 1211233-005), and having a serial number of 00001 and subsequent; certificated in any category.
- AD 98-26-04 Recurring
Boeing Model 757 Series Airplanes
To prevent uncommanded fuel flow from the fuel tanks to the engine nacelle in the event of a leak in the engine fuel line or a fire in the engine nacelle.
Applicability, as the AD words it
Model 757 series airplanes, as listed in Boeing Alert Service Bulletin 757-28A0045, Revision 1, dated November 19, 1998; certificated in any category.
- AD 96-18-08 Recurring Engine
Pratt & Whitney PW2000 Series Turbofan Engines
To prevent high pressure turbine (HPT) or low pressure turbine (LPT) failure, which may result in an uncontained engine failure and possible damage to the aircraft.
Applicability, as the AD words it
Pratt & Whitney Models PW2037, PW2037(M), PW2040, PW2240, and PW2337 turbofan engines, installed on but not limited to, Boeing 757 series and Ilyushin IL96 series aircraft.
- AD 98-03-20 One-time
Boeing Model 757 Series Airplanes
To prevent chafing of wire bundles, which could result in smoke and fire at the E1-1 rack of the electrical equipment bay.
Applicability, as the AD words it
Model 757 series airplanes, on which Boeing Alert Service Bulletin 757-24A0025, dated May 10, 1985, and/or Boeing Service Bulletin 757-24A0025, Revision 1, dated December 17, 1987, has been accomplished; excluding variable numbers NA003, NA004, NA007, NA009, NA010, NA012 through NA016 inclusive, and NA021; certificated in any category.
- AD 97-18-05 Recurring Engine
Boeing Model 757 Series Airplanes Equipped With Pratt & Whitney Engines
To detect and correct fatigue cracking of the midspar fuse pins, which could lead to separation of the strut and engine from the wing of the airplane.
Applicability, as the AD words it
Model 757 series airplanes equipped with Pratt & Whitney engines, certificated in any category.
- AD 97-18-04 Recurring Engine
Boeing Model 757 Series Airplanes Equipped With Rolls Royce Engines
To detect and correct fatigue cracking of the midspar fuse pins, which could lead to separation of the strut and engine from the wing of the airplane.
Applicability, as the AD words it
Model 757 series airplanes equipped with Rolls Royce engines, certificated in any category.
- AD 97-11-51 One-time Engine
Pratt & Whitney PW2000 Series Turbofan Engines
To prevent fracture of the first stage HPT disk, resulting in a possible uncontained engine failure and damage to the aircraft.
Applicability, as the AD words it
Pratt & Whitney (PW) PW2000 series turbofan engines, with first stage high press turbine (HPT) disk assembly, Part Numbers (P/N) 1A5921, 1B2671, and 1B3621, installed. These engines are installed on but not limited to Boeing 757 series and Ilyushin IL-96 series aircraft.
- AD 97-09-06 Recurring
Boeing Model 757 Series Airplanes
To detect and correct chafing of the tubes of the fire extinguishing and smoke detection systems, which could prevent the proper distribution of the fire extinguishing agent within the aft cargo compartment in the event of a fire, or could result in the delay of detection of a fire in the aft cargo compartment.
Applicability, as the AD words it
All Model 757 series airplanes, certificated in any category.
- AD 97-09-01 One-time Engine
Pratt & Whitney PW2000 Series Turbofan Engines
To prevent fracture of the first stage high pressure turbine (HPT) disk, resulting in a possible uncontained engine failure and damage to the aircraft.
Applicability, as the AD words it
Pratt & Whitney (PW) PW2000 series turbofan engines, installed on but not limited to Boeing 757 series, Ilyushin IL-96 series, and McDonnell Douglas Model C-17 (military) aircraft.
- AD 97-03-17 Recurring
Boeing Model 747 and 757 Series Airplanes
To prevent fuel leakage at the fuel boost and override/jettison pumps, which could result in a fire at the location of the affected fuel pump.
Applicability, as the AD words it
All Model 747 and 757 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 96-19-17 One-time
Boeing Model 757 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 757 series airplanes, as listed in Boeing Alert Service Bulletin 757-24A0079, dated August 8, 1996; certificated in any category.
- AD 96-09-07 One-time
Boeing Model 757 Series Airplanes Equipped With Moog Spoiler Actuators
To prevent a significant control upset of the airplane due to problems associated with incorrectly assembled Abex electro- hydraulic servo valves (EHSV) on certain Moog spoiler actuators.
Applicability, as the AD words it
Model 757 airplanes, certificated in any category, that are equipped with Moog spoiler actuators having Abex electro-hydraulic servo valves (EHSV), part number 72196, with the serial numbers listed in Table 1 of this AD: Table 1 Abex order EHSV serial No. No.*- Shipment Date * AH-0001: C716657- 8 November 1991. AH-0002-: C716657- 8 November 1991. AH-0003-: C727995- 25 August 1994. AH-0004: C727995- 25 August 1994. AH-0005-: C727995- 25 August 1995. AH-0006-: C727995- 25 August 1995. AH-0007-: C727995- 25 August 1995. 13-: C731181- 12 June 1995. 49-: C730878- 01 June 1995. 61-: C727955- 13 September 1994. 131-: C708905- 13 November 89. 233-: C727730- 17 June 1994. 241-: C731540- 13 September 1995. 260-: C727955- 13 September 1994. 279-: C728298- 02 September 1994. 275-: C727880- 24 June 1994. 308-: C725421- 01 December 1993. 329-: C727711- 17 June 1994. 347-: C727518- 14 June 1994. 401-: C728298- 05 September 1994. 407-: C727730- 17 June 1994. 427-: C731181- 03 July 1995. 450-: C731181- 03 July 1995. 445-: C706627- 22 February 89. 457-: C731663- 12 September 1995. 456-: C728887- 28 November 1994. 463-: C731435- 21 August 1995. 484-: C727748- 22 June 1994. 515-: C727745- 24 June 1994. 559-: C728290- 05 September 1994. 563-: C724224- 14 September 1993. 579-: C724176- 14 September 1993. 595-: C727735- 24 January 1994. 611-: C727955- 14 September 1994. 607-: C727997- 20 July 1994. 647-: C728459- 10 October 1994. 726-: C731096- 04 September 1995. 725-: C729525- 19 December 1994. 819-: C728135- 03 August 1994. 890-: C726803- 06 April 1994. 874-: C730890- 26 April 1995. 909-: C724877- 29 November 1993. 912-: C727977- 04 August 1994. 991-: C713602- 10 December 1990. 998-: C731477- 4 September 1995. 1022: C708905- 13 November 1989. 1023: C708905- 13 November 1989. 1072: C709166- 14 November 1989. 1148: C730192- 13 March 1995. 1175: C723278- 05 August 1993. 1227: C728303- 31 August 1994. 1283: C731833- 04 September 1995. 1487: C728549- 04 October 1994. 1655: C728442- 28 November 1994. 1780: C726757- 06 April 1994. 1807: C728669 29 September 1994. 1862: C727625- 17 June 1994. 1929: C727977- 04 August 1994. 1986Z: C727730- 17 June 1994. 2017Z: C725411- 24 November 1993. 2034: C727730- 17 June 1994. 2073: C731272- 12 September 1995. 2125: C725713- 12 January 1994. 2220: C729735 29 March 1995. 2334: C727730- 17 June 1994. 2348: C727730- 17 June 1994. 2426: C731623 12 July 1995. * The Abex Order Number and Shipment Date are included in this listing to enable operators to review their records in order to determine if a suspect EHSV has been ordered, and if, or where, it has been installed on an airplane.
- AD 95-25-01 Recurring
Boeing Model 757 Series Airplanes
To ensure proper operation of the door opening system during an emergency evacuation.
Applicability, as the AD words it
This AD applies to each airplane 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 airplanes 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 (f) of this AD 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 airplane from the applicability of this AD. -
- AD 95-21-08 One-time
Boeing Model 757 Series Airplanes
Applicability, as the AD words it
Model 757 series airplanes equipped with Pratt & Whitney PW2000 engines, as listed in Boeing Service Bulletin 757-76- 0010, dated August 12, 1993; and Model 757 series airplanes equipped with Rolls-Royce RB211-535 engines, as listed in Boeing Service Bulletin 757-76-0011, dated December 2, 1993; 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 95-10-13 Recurring Engine
Boeing Model 757 Series Airplanes Equipped With Rolls Royce Engines
To prevent fuel or hydraulic fluid leakage into the interior of the engine strut, which could cause a fire.
Applicability, as the AD words it
Model 757 series airplanes equipped with Rolls Royce engines; as listed in Boeing Alert Service Bulletin 757- 54A0030, Revision 1, dated December 20, 1993; certificated in any category.
- AD 95-02-10 One-time
Boeing Model 757 Series Airplanes
To prevent these airplanes from taking off with broken bolts that attach the transmission bracket to the flap track structure, which could result in the airplane rolling at liftoff.
Applicability, as the AD words it
Model 757 series airplanes having line numbers 181 through 647 inclusive, certificated in any category.
- AD 95-01-05 Recurring Engine
Boeing Model 757 Equipped With Pratt & Whitney Model PW2000 Series Engines
To prevent damage to these engines due to ice ingestion into the compressor, which may result in the loss of power from the affected engine.
Applicability, as the AD words it
Model 757 series airplanes equipped with Pratt & Whitney Model PW2000 series engines, certificated in any category.
12 superseded or removed ADs
- AD 2004-12-07 Superseded by AD 2014-05-13 Engine
Boeing Model 757 Series Airplanes Equipped With Rolls Royce RB211 Engines
To prevent fatigue cracking in primary strut structure and consequent reduced structural integrity of the strut.
Applicability, as the AD words it
Model 757 series airplanes equipped with Rolls Royce RB211 engines, line numbers 1 through 735 inclusive; certificated in any category.
- AD 2003-18-05 Superseded by AD 2013-10-02 Engine
Boeing Model 757 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 757 series airplanes powered by Pratt & Whitney engines, line numbers 1 through 735 inclusive, certificated in any category.
- AD 2002-12-06 Superseded by AD 2005-18-03 Engine
Pratt & Whitney (PW) PW2000 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) PW2037, PW2040, PW2037M, PW2240, PW2337, PW2043, PW2643, and PW2143, series turbofan engines. These engines are installed on, but not limited to Boeing 757 series and Ilyushin IL- 96T series airplanes.
- AD 2001-20-12 Superseded by AD 2006-11-11
Boeing Model 757 Series Airplanes
To ensure continued structural integrity of these airplanes.
Applicability, as the AD words it
Model 757 series airplanes having line numbers 1 through 764 inclusive, certificated in any category.
- AD 2000-20-09 Superseded by AD 2003-18-05 Engine
Boeing Model 757 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 757 series airplanes powered by Pratt & Whitney engines, line numbers 1 through 735 inclusive, certificated in any category.
- AD 99-24-07 Superseded by AD 2004-12-07 Engine
Boeing Model 757 Series Airplanes Equipped With Rolls Royce Engines
To prevent fatigue cracking in primary strut structure and consequent reduced structural integrity of the strut.
Applicability, as the AD words it
Model 757 series airplanes equipped with Rolls Royce engines, line numbers 1 through 735 inclusive; certificated in any category.
- AD 98-07-07 Superseded by AD 2014-24-08 Engine
Rolls-Royce, plc RB211 Series Turbofan Engines
To prevent high volume fuel leaks and reported fuel collection inside the engine nacelle, which could result in an uncontrolled engine fire.
Applicability, as the AD words it
Rolls-Royce, plc. (R-R) Models RB211-535E4 and - 535E4-B turbofan engines installed on but not limited to Boeing 757 series and Tupolev 204 series aircraft.
- AD 96-17-02 Superseded by AD 98-26-04
Boeing Model 757 Series Airplanes
To prevent uncommanded fuel flow from the fuel tanks to the engine nacelle in the event of a leak in the engine fuel line or a fire in the engine nacelle.
Applicability, as the AD words it
Model 757 series airplanes, line positions 478 through 699 inclusive; certificated in any category.
- AD 96-13-04 Superseded by AD 98-07-07 Engine
Rolls-Royce, plc RB211 Series Turbofan Engines
To prevent a fuel system leak, which could result in rapid atomization of fuel and an engine fire.
Applicability, as the AD words it
Rolls-Royce, plc. (R-R) Models RB211-535E4 series and -535E4-B series turbofan engines, prior to engine Serial Number (S/N) 31292, installed on but not limited to Boeing 757 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 (b) 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 96-06-01 Superseded by AD 96-09-07
Boeing Model 757 Series Airplanes Equipped With Abex Spoiler Actuators
To prevent a significant control upset of the airplane due to problems associated with incorrectly assembled Abex electro- hydraulic servo valves (EHSV) on certain Abex spoiler actuators.
Applicability, as the AD words it
Model 757 airplanes, certificated in any category, that are equipped with Abex spoiler actuators having Abex electro-hydraulic servo valves (EHSV), part number 72196, with the serial numbers listed in Table 1 of this AD: Table 1 Boeing order EHSV serial No. No.*- Shipment date* AH-0001: C716657: 8 November 1991. AH-0002: C716657: 8 November 1991. AH-0003: C727995: 25 August 1994. AH-0004: C727995: 25 August 1994. AH-0005: C727995: 25 August 1995. AH-0006: C727995: 25 August 1995. AH-0007: C727995: 25 August 1995. 13: C731181: 12 June 1995. 49: C730878: 01 June 1995. 61: C727955: 13 September 1994. 131: C708905: 13 November 89. 233: C727730: 17 June 1994. 241: C731540: 13 September 1995. 260: C727955: 13 September 1994. 279: C728298: 02 September 1994. 275: C727880: 24 June 1994. 308: C725421: 01 December 1993. 329: C727711: 17 June 1994. 347: C727518: 14 June 1994. 401: C728298: 05 September 1994. 407: C727730: 17 June 1994. 427: C731181: 03 July 1995. 450: C731181: 03 July 1995. 445: C706627: 22 February 89. 457: C731663: 12 September 1995. 456: C728887: 28 November 1994. 463: C731435: 21 August 1995. 484: C727748: 22 June 1994. 515: C727745: 24 June 1994. 569: C728290: 05 September 1994. 579: C724176: 14 September 1993. 611: C727955: 14 September 1994. 607: C727997: 20 July 1994. 647: C728459: 10 October 1994. 726: C731096: 04 September 1995. 725: C729525: 19 December 1994. 819: C728135: 03 August 1994. 890: C726803: 06 April 1994. 874: C730890: 26 April 1995. 912: C727977: 04 August 1994. 991: C713602: 10 December 90. 998: C731477: 4 September 1995. 1022: C708905: 13 November 89. 1023: C708905: 13 November 89. 1072: C709166: 14 November 89. 1148: C730192: 13 March 1995. 1175: C723278: 05 August 1993. 1227: C728303: 31 August 1994. 1283: C731833: 04 September 1995. 1487: C728549: 04 October 1994. 1655: C728442: 28 November 1994. 1780: C726757: 06 April 1994. 1807: C728669: 29 September 1994. 1862: C727625: 17 June 1994. 1929: C727977: 04 August 1994. 1986Z: C727730: 17 June 1994. 2017Z: C725411: 24 November 1993. 2034: C727730: 17 June 1994. 2073: C731272: 12 September 1995. 2125: C725713: 12 January 1994. 2220: C729735: 29 March 1995. 2334: C727730: 17 June 1994. 2348: C727730: 17 June 1994. 2426: C731623: 12 July 1995. *The Boeing Order Number and Shipment Date are included in this listing to enable operators to review their records in order to determine if a suspect EHSV has been ordered, and if, or where, it has been installed on an airplane.
- AD 96-05-08 Superseded by AD 97-18-04 Engine
Boeing Model 757 Series Airplanes Equipped With Rolls Royce Engines
To prevent cracking of the midspar fuse pins, which may lead to separation of the strut and engine from the wing of the airplane.
Applicability, as the AD words it
Model 757 series airplanes equipped with Rolls Royce engines, certificated in any category.
- AD 96-05-07 Superseded by AD 97-18-05 Engine
Boeing Model 757 Series Airplanes Equipped with Pratt & Whitney Engines
To prevent cracking of the midspar fuse pins, which may lead to separation of the strut and engine from the wing of the airplane.
Applicability, as the AD words it
Model 757 series airplanes equipped with Pratt & Whitney engines, certificated in any category.
Radar reads the aircraft’s 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
Boeing 757-223 AD questions
Source: FAA final rules under 14 CFR part 39, from the Federal Register. The FAA’s Dynamic Regulatory System holds the official list.
How many airworthiness directives apply to the Boeing 757-223?
47 FAA ADs published since 1995 name the Boeing 757-223's type certificate model (757-223) in their applicability. 35 are still in effect as far as the Federal Register shows; the others were superseded by a later AD or removed. How many apply to one aircraft depends on its serial number, equipment and modifications.
Which Boeing 757-223 ADs are recurring?
12 of the ADs in effect require actions that repeat, such as inspections at set intervals, until a terminating action is done. They are marked Recurring above. One-time ADs are complied with once, but the compliance record stays with the aircraft.
What is the latest Boeing 757-223 airworthiness directive?
AD 2005-18-03, effective Feb 28, 2006: Pratt & Whitney PW2000 Series Turbofan Engines. The list is refreshed from the Federal Register every weekday.
How do I know whether an AD applies to my Boeing 757-223?
Read the AD's applicability paragraph, shown with each AD on this page, against the aircraft's serial number and its installed engines, propellers, parts and modifications. A certificated mechanic or inspector makes the determination and records the method of compliance in the maintenance records. The FAA's Dynamic Regulatory System holds the official list of ADs.
Why are engine and propeller ADs missing?
This page lists ADs whose applicability names the Boeing 757-223 airframe, plus appliance ADs that list it among the aircraft they can be installed on. Engine and propeller ADs name the engine or propeller model rather than the aircraft, so check them by the installed engine and propeller models.
Every AD on your Boeing 757-223, tied to the logbook entry that closed it.
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.