# N944FD: 1989 Boeing 757-2G5

- Status: Valid registration
- Airframe: [Boeing 757-2G5](https://openairdocs.org/model/boeing-757-2g5) (registry code 1384912, 239 seats)
- Engine: [Rolls-Royce RB211-535E4 series](https://openairdocs.org/engine/rolls-royce-rb211-535e4-series) (registry code 54223)
- Data sheets: [TCDS E12EU](https://openairdocs.org/tcds/E12EU) (Rolls-Royce Deutschland Ltd & Co KG) (OpenAirDocs)
- Serial number: 24497
- Year built: 1989
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 12, 2010
- Certificate issued: June 15, 2010
- Expires: July 31, 2027
- Mode S code: AD1C85
- Registered owner: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP)
- Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis)
- Owner type: Corporation
- Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=944FD
- Page: https://openairdocs.org/aircraft/N944FD

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Rolls-Royce RB211-535E4 model are included.

## ADs that may apply (OpenAirDocs): 20 in force

### Matched by airframe (Boeing 757-2G5)

None in force.

### Matched by engine (Rolls-Royce RB211-535E4 series)

- [AD 2024-10-06](https://openairdocs.org/ad/2024-10-06): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jun 27, 2024
- [AD 2020-08-03](https://openairdocs.org/ad/2020-08-03): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective May 18, 2020
- [AD 2017-24-08](https://openairdocs.org/ad/2017-24-08): Fuel control/Turbine engines · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jan 16, 2018
- [AD 2016-03-04](https://openairdocs.org/ad/2016-03-04): Life-limited rotating parts · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Mar 15, 2016
- [AD 2013-23-17](https://openairdocs.org/ad/2013-23-17): High-pressure (HP) and intermediate-pressure (IP) turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-C-37 and 3 more. Effective Dec 11, 2013
- [AD 2013-16-23](https://openairdocs.org/ad/2013-16-23): Cracked and distorted FCL metering panel · Rolls-Royce RB211-524B-02, RB211-524B2-19, RB211-524B3-02 and 13 more. Effective Oct 8, 2013
- [AD 2012-25-09](https://openairdocs.org/ad/2012-25-09): Intermediate-pressure (IP) turbine discs · Rolls-Royce RB211-524G2-19, RB211-524G2-T-19, RB211-524G3-19 and 10 more. Effective Feb 6, 2013
- [AD 2012-02-11](https://openairdocs.org/ad/2012-02-11): LP turbine stage 1, 2, and 3 discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Mar 6, 2012
- [AD 2009-20-14](https://openairdocs.org/ad/2009-20-14): Eddy current inspection (ECI) · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Nov 17, 2009
- [AD 2008-20-04](https://openairdocs.org/ad/2008-20-04): HP turbine discs · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 26 more. Effective Nov 3, 2008
- [AD 2006-11-05 R2](https://openairdocs.org/ad/2006-11-05-R2): High pressure compressor (HPC) · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 21, 2008
- [AD 2007-14-07](https://openairdocs.org/ad/2007-14-07): Fluorescent penetrant inspections (FPI) · Rolls-Royce RB211-524B-02, RB211-524B-B-02, RB211-524B2-19 and 21 more. Effective Aug 16, 2007
- [AD 2006-17-12](https://openairdocs.org/ad/2006-17-12): High pressure (HP) turbine discs · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 3 more. Effective Sep 27, 2006
- [AD 2004-19-04](https://openairdocs.org/ad/2004-19-04): Critical Life-Limited Rotating Engine Parts · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Nov 1, 2004
- [AD 2004-01-21](https://openairdocs.org/ad/2004-01-21): Frount engine mount housing · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 27, 2004
- [AD 2003-10-03 R1](https://openairdocs.org/ad/2003-10-03-R1): High pressure (HP) turbine discs · Rolls-Royce RB211-535E4-B-37 and RB211-535E4-B-75. Effective Jun 20, 2003
- [AD 2001-19-05](https://openairdocs.org/ad/2001-19-05): High Speed Gearbox Drive · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Oct 11, 2001
- [AD 2000-09-14](https://openairdocs.org/ad/2000-09-14): Radial Drive Steady Bearings · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Jul 11, 2000
- [AD 97-02-12](https://openairdocs.org/ad/97-02-12): Fuel Flow Governor (FFG) · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Apr 4, 1997
- [AD 87-25-04](https://openairdocs.org/ad/87-25-04): Fuel Quantity Indication System · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Dec 8, 1987

### Historical (superseded or no longer in force)

- [AD 2015-17-21](https://openairdocs.org/ad/2015-17-21) (historical): High-pressure turbine (HPT) disks · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Dec 2, 2015
- [AD 2014-24-08](https://openairdocs.org/ad/2014-24-08) (historical): Fuel leaks · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jan 6, 2015
- [AD 2013-19-18](https://openairdocs.org/ad/2013-19-18) (historical): LPT stage 2 disc failure · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Nov 7, 2013
- [AD 2013-19-17](https://openairdocs.org/ad/2013-19-17) (historical): Failure of rotating life limited parts · Rolls-Royce RB211-535E4-B-37. Effective Nov 7, 2013
- [AD 2011-11-08](https://openairdocs.org/ad/2011-11-08) (historical): LP Turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Jun 30, 2011
- [AD 2008-22-24](https://openairdocs.org/ad/2008-22-24) (historical): Low pressure compressor (LPC) fan blade · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Dec 9, 2008
- [AD 2006-11-05 R1](https://openairdocs.org/ad/2006-11-05-R1) (historical): Disc assemblies · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective May 1, 2007
- [AD 2006-11-05](https://openairdocs.org/ad/2006-11-05) (historical): High pressure compressor (HPC) stage 3 disc assemblies · Rolls-Royce RB211-22B-02, RB211-524B-02, RB211-524B-B-02 and 24 more. Effective Jun 27, 2006
- [AD 2005-02-05](https://openairdocs.org/ad/2005-02-05) (historical): Low Pressure Compressor (LPC) Fan Blade Roots · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Feb 11, 2005
- [AD 2004-26-03](https://openairdocs.org/ad/2004-26-03) (historical): High pressure (HP) turbine discs · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 3 more. Effective Jan 13, 2005
- [AD 2004-01-20](https://openairdocs.org/ad/2004-01-20) (historical): High pressure compressor (HPC) · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 24, 2004
- [AD 2003-17-15](https://openairdocs.org/ad/2003-17-15) (historical): Low pressure (LP) turbine stage 2 discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Oct 2, 2003
- [AD 2003-12-15](https://openairdocs.org/ad/2003-12-15) (historical): LPC fan blade roots · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Jul 30, 2003
- [AD 2003-10-03](https://openairdocs.org/ad/2003-10-03) (historical): High Pressure (HP) turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Jun 20, 2003
- [AD 2002-23-08](https://openairdocs.org/ad/2002-23-08) (historical): Low Pressure (LP) Turbine Stage 2 Discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Dec 30, 2002
- [AD 2001-23-02](https://openairdocs.org/ad/2001-23-02) (historical): High Pressure Turbine Disks · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 2 more. Effective Dec 24, 2001
- [AD 98-07-07](https://openairdocs.org/ad/98-07-07) (historical): Fuel System Tube Assembly · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Apr 29, 1998
- [AD 86-07-01](https://openairdocs.org/ad/86-07-01) (historical): Outer Combustion Case Inspection · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective May 16, 1986

## Information bulletins (advisory) (1 in force)

- [SAIB 2026-11](https://openairdocs.org/saib/2026-11): Theft of Turbofan Engine Parts before Mutilation. Issued Jun 8, 2026

## NTSB investigations

None matched to N944FD.

## FAA accident and incident reports

None matched to N944FD.

## Service difficulty reports (130, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR FDEA202409041238](https://openairdocs.org/sdr/FDEA202409041238), Sep 4, 2024: LIGHT. INOPERATIVE. L1 DOOR EMERGENCY EXIT LIGHT INOP. RELEASED FOR SERVICE PER MEL 33-51-01-01. ACFT OK FOR SERVICE.
- [SDR FDEA202407251050](https://openairdocs.org/sdr/FDEA202407251050), Jul 25, 2024: TACH GENERATOR. FAILED. AFTER TAKEOFF, RECEIVED L ENG BLEED OFF EICAS RAN QRH 2.1.14 LEVELED AT FL360. NOTICED CABIN ALT AT 8000 WHILE 5 MIN CABIN ALT AT 9500 DESCENDED DOWN TO LOWER A
- [SDR FDEA202302220332](https://openairdocs.org/sdr/FDEA202302220332), Feb 22, 2023: ENGINE. FAILED. PDIS 944 79-01 0275 22FEB23 RSW OPEN U IN FLIGHT AT FL390 NOTICED R ENG OIL PRESS DISCREET LIGHT FLICKERING. ON EICAS NOTICED OIL QUANTITY 0, ALL OTHER ENGINE I
- [SDR FDEA202211042728](https://openairdocs.org/sdr/FDEA202211042728), Nov 4, 2022: PAN. GOUGED. R1 DOOR EXTERIOR HANDLE PAN WORN REMOVED AND REPLACED R1 DOOR HANDLE PAN IAW DWG 141N6200 REV T AND AMM 52-11-13-02.
- [SDR FDEA202211032725](https://openairdocs.org/sdr/FDEA202211032725), Nov 3, 2022: WEDGE. DELAMINATED. #6 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 81-01-4
- [SDR FDEA202211032724](https://openairdocs.org/sdr/FDEA202211032724), Nov 3, 2022: WEDGE. DELAMINATED. #4 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 27-81-02-4
- [SDR FDEA202211032723](https://openairdocs.org/sdr/FDEA202211032723), Nov 3, 2022: WEDGE. DELAMINATED. #3 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 27-81-02-4
- [SDR FDEA202211032722](https://openairdocs.org/sdr/FDEA202211032722), Nov 3, 2022: WEDGE. DELAMINATED. #5 SLAT T/E WEDGE IS DISBONDED REMOVED AND REPLACED PER B757 AMM 27-81-01-4
- [SDR FDEA202211022713](https://openairdocs.org/sdr/FDEA202211022713), Nov 2, 2022: FLOORBEAM. CORRODED. MAIN CABIN FLOOR BEAM STA 1681 IS CORRODED ON THE AFT FACE AND LOWER SURFACE OF THE UPPER CAP AT APPROX RBL 48 ACCOMPLISHED FEDEX EA # F-5310-T0371106 FUSELAGE 
- [SDR FDEA202211022714](https://openairdocs.org/sdr/FDEA202211022714), Nov 2, 2022: FLOORBEAM. CORRODED. MAIN CABIN FLOOR BEAM IS CORRODED AT FASTENER HOLE BS 310 LBL 20 ACCOMPLISHED FEDEX EA # F-5310-T0371036 FUSELAGE - MAINFRAME - FLOOR BEAM TEE CAP, STA 310, LBL
- [SDR FDEA202211022712](https://openairdocs.org/sdr/FDEA202211022712), Nov 2, 2022: PANEL. CRACKED. #1 PYLON PANEL 434DR HAS A CORNER CRACKED REPAIRED #1 PYLON PANEL 434DR CRACKED CORNER WITH 350 DEGREE REPAIR IAW B757 SRM 54-50-70-2R FIG 201 REPAIR 1 SHEET 3,
- [SDR FDEA202210312701](https://openairdocs.org/sdr/FDEA202210312701), Oct 31, 2022: FITTING. CORRODED. MAIN CABIN - STA 324-345 RBL2 INTERCOSTAL IS CORRODED AT FLOOR PANEL HOLES REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL IAW B757 DWG 141N5160 REV CD AND 14
- [SDR FDEA202210282687](https://openairdocs.org/sdr/FDEA202210282687), Oct 28, 2022: STRINGER. CRACKED. AFT CARGO COMPARTMENT STA 1680-1701 STR29R HAS CRACKED STINGER REMOVED CRACKED STINGER SECTION ON STA 1680 - 1701 STR29 R/H FABRICATED -1 HAT SECTION AND -2 FIL
- [SDR FDEA202210282685](https://openairdocs.org/sdr/FDEA202210282685), Oct 28, 2022: FLOORBEAM. CORRODED. MAIN CABIN - ZONE 250 - STA 1681 FLOOR BEAM IS CORRODED ON LOWER SURFACE - LBL5 ACCOMPLISHED FEDEX EA #: F-5310-T0371106 FUSELAGE - MAINFRAME - FLOOR BEAM, STA 
- [SDR FDEA202210252660](https://openairdocs.org/sdr/FDEA202210252660), Oct 25, 2022: WEB. CORRODED. MAIN CABIN FLOOR SUPPORT PLATE IS CORRODED AFT OF CABLES BS 340, LBL 27 REMOVED, FABRICATED AND INSTALLED NEW FLOOR WEB IAW B757 DWG 141N5170 REV C
- [SDR FDEA202210242651](https://openairdocs.org/sdr/FDEA202210242651), Oct 24, 2022: INTERCOSTAL. CORRODED. MAIN CABIN INTERCOSTAL IS CORRODED UPPER AND LOWER SIDE AT NUTPLATES HOLES BS 327 RBL 25 - RBL 39 REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW BAC DWG 141N5
- [SDR FDEA202210242650](https://openairdocs.org/sdr/FDEA202210242650), Oct 24, 2022: INTERCOSTAL. CORRODED. MAIN CABIN INTERCOSTAL IS CORRODED UPPER AND LOWER SIDE AT NUTPLATES HOLES BS 327 RBL 4- RBL 23 REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW B757-2 DWG 141N
- [SDR FDEA202210242652](https://openairdocs.org/sdr/FDEA202210242652), Oct 24, 2022: FLOORBEAM. CORRODED. MAIN CABIN FLOOR SUPPORT BEAM IS CORRODED UPPER SIDE AT NUTPLATE HOLE BS 344 LBL20 - LBL22 REMOVED, FABRICATED AND REPLACED FLOOR SUPPORT BEAM ISW B757-2 DWG 14
- [SDR FDEA202210242649](https://openairdocs.org/sdr/FDEA202210242649), Oct 24, 2022: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL AT STA 480-500 LBL 45 IS DAMAGED REPAIRED FLOOR PANEL IAW B757SRM 53-00-50-2R REPAIR 1
- [SDR FDEA202210242648](https://openairdocs.org/sdr/FDEA202210242648), Oct 24, 2022: FLOORBEAM. CORRODED. MAIN CABIN FLOOR BEAM IS CORRODED UPPER AND LOWER SIDE AT NUTPLATES HOLES AND FWD EDGE IS GOUGED AND CORRODED BS 344 LBL0-LBL20 REPAIRED FLOOR BEAM IAW B757-2 S
- [SDR FDEA202210242647](https://openairdocs.org/sdr/FDEA202210242647), Oct 24, 2022: FLOOR PANEL. DELAMINATED. MAIN CABIN ZONE 240 - FLOOR PANEL 242MCF IS DELAMINATED REPAIRED FLOOR PANEL 242 MCF IAW B757 SRM 53-00-50-2R, REMOVED AND INSTALLED INSERTS IAW B757 SRM 53-00-
- [SDR FDEA202210222642](https://openairdocs.org/sdr/FDEA202210222642), Oct 22, 2022: SKIN. DAMAGED. RIGHT WING #8 SLAT UPPER TRAILING EDGE LOWER SURFACE HAS AREA OF BARE METAL REPAIRED #8 SLAT UPPER TRAILING EDGE LOWER SURFACE ARE OF BARE METAL IAW FEDEX EA# F
- [SDR FDEA202210222641](https://openairdocs.org/sdr/FDEA202210222641), Oct 22, 2022: WEDGE. DELAMINATED. #8 SLAT T/E WEDGE IS DISBONDED REPAIRED #8 SLAT T/E WEDGE DISBOND ON 3EA. AREA IAW FEDEX EA# F-5750-T0370952.
- [SDR FDEA202210052470](https://openairdocs.org/sdr/FDEA202210052470), Oct 5, 2022: PANEL. CRACKED. RW LEADING EDGE PANEL BEHIND #7 SLAT IS CRACKED AT OB SPLICE AREA. REPAIRED RW LEADING EDGE PANEL BEHIND #7 SLAT IAW B757-200 SRM 57-41-02-2RFIG 201 SHEET 8 AND
- [SDR FDEA202210052469](https://openairdocs.org/sdr/FDEA202210052469), Oct 5, 2022: PANEL. DAMAGED. LH VERTICAL PANEL 322CL DAMAGED REPAIRED L/H VERTICAL STAB PANEL 322CL SKIN IAW B757-200 SRM 55-30-01-2R FIG 201 REPAIR 4 SHEET1 AND SRM 51-70-07-0G.
- [SDR FDEA202011202924](https://openairdocs.org/sdr/FDEA202011202924), Nov 20, 2020: DRAG FITTING. CRACKED. THE RT WING OUTBOARD DRAG FITTING HAS INDICATIONS OF DEFECTS ON THE NR 4 & NR 13 HOLE. THE NR 4 HOLE HAS INDICATION AT THE 3 O`CLOCK LOCKING AFT AND NR 13 HAS I
- [SDR FDEA202011202923](https://openairdocs.org/sdr/FDEA202011202923), Nov 20, 2020: DRAG FITTING. CORRODED. THE RT INBOARD DRAG FITTING UPPER SURFACE HAS CORROSION AT NR 3 AND NR 8 HOLES. COMPLIED WITH FEDEX EA NR F-5740-T0343112 C P3. REPLACED INBOARD FITTING.
- [SDR FDEA202011202922](https://openairdocs.org/sdr/FDEA202011202922), Nov 20, 2020: DRAG FITTING. CRACKED. THE RT WING INBOARD DRAG FITTING HAS INDICATIONS ON THE NR 3, NR 8 HOLE AND THE 3RD HOLE FROM THE BOTTOM THAT ATTACHES TO THE SPAR. THE 2 HOLES THAT ATTACH TO T
- [SDR FDEA202011202921](https://openairdocs.org/sdr/FDEA202011202921), Nov 20, 2020: DRAG FITTING. CRACKED. THE RT UPPER SKIN DRAG FITTING NR 3 AND NR 5 HOLES HAVE INDICATIONS OF DEFECTS NOTED. THE NR 3 HOLE HAS INDICATION AT THE 1 O`CLOCK LOOKING AFT. THE NR 5 HOLE H
- [SDR FDEA202011202918](https://openairdocs.org/sdr/FDEA202011202918), Nov 20, 2020: DRAG FITTING. CORRODED. THE RT WING OUTBOARD DRAG FITTING UPPER SURFACE HAS CORROSION ON NR 4 AND NR 13 HOLES. COMPLIED WITH FEDEX EA NR F-5740-T0343112 C P3. WINGS-ATTACH FITTINGS-RT 
- [SDR FDEA202011192911](https://openairdocs.org/sdr/FDEA202011192911), Nov 19, 2020: SKIN. DENTED. LH ENGINE PYLON IB SIDE ABOUT MID SECTION ON LWR FACE HAS DENT. COMPLIED WITH FEDEX EA. F - 5430-T0358210 P1 NACELLS / PYLON - SKIN /PLATES/ PANELS - LH ENGINE 
- [SDR FDEA202011072791](https://openairdocs.org/sdr/FDEA202011072791), Nov 7, 2020: FRAME. CRACKED. THE RT 1640 FRAME BY STR 14R LOWER INBOARD OPEN HOLE HAS AN INDICATION OF DEFECT NOTED. INDICATION IS AT THE 9 O`CLOCK POSITION LOOKING AFT (GOING OUTBOARD). RE
- [SDR FDEA202011072790](https://openairdocs.org/sdr/FDEA202011072790), Nov 7, 2020: FRAME. CRACKED. THE LT 1640 FRAME BY STR 14L LOWER INBOARD OPEN HOLE HAS AN INDICATION OF DEFECT NOTED. INDICATION IS AT THE 9 O`CLOCK POSITION LOOKING AFT (GOING INBOARD). REP
- [SDR FDEA2020040620689](https://openairdocs.org/sdr/FDEA2020040620689), Apr 2, 2020: RESERVOIR. FAILED. R1 DOOR EMERGENCY POWER RESERVOIR HAS NO PRESSURE. REMOVED AND REPLACED EMERGENCY POWER RESERVOIR REF B757 AMM 52-11-30-4. OPS CHECK SATIS. A/C OK TO CONT SERVI
- [SDR FDEA2019122313275](https://openairdocs.org/sdr/FDEA2019122313275), Dec 21, 2019: COLLAR. INOPERATIVE. GUST LOCK ON L FWD ENTRY DOOR WILL NOT MOVE TO ALLOW DOOR TO CLOSE. REF MM 52-11-08-08, INSTALLED NEW HOLD OPEN LOCK COLLAR ON L1 DOOR. L1 DOOR HOLD OPEN LOCK C
- [SDR FDEA2019061741301](https://openairdocs.org/sdr/FDEA2019061741301), Jun 14, 2019: BOTTLE. EMPTY. FOUND POWER ASSIST RESIVOUR FOR L1 DOOR BLOWN. REMOVED AND REPLACED L1 DOOR ASSIST BOTTLE PER AMM 52-11-30-4-0 NOMENCLATURE-CYLINDER, EMERGENCY POWER RESERVOIR,
- [SDR FDEA2019022860509](https://openairdocs.org/sdr/FDEA2019022860509), Feb 26, 2019: HOSE. DEFECTIVE. L HYD SYS PRESS LIGHT ILLUMINATED ON FINAL AFTER LANDING GEAR DOWN AND LOCKED AND FLAPS AT FINAL CONFIGURATION. FOLLOWED BY L HYD SYS PRESS AND L YAW DAMPER. CL
- [SDR FDEA201811123187](https://openairdocs.org/sdr/FDEA201811123187), Nov 12, 2018: SHIM. MIGRATED. RT PYLON UPPER AFT DRAG LINK SPAR FITTING SHOWS SIGNS OF SHIM MIGRATION. COMPLIED WITH EA F-5740-T0343112 PART 1. RT WING DRAG FITTING TO WING UPPER SKIN SHIM M
- [SDR FDEA201810303054](https://openairdocs.org/sdr/FDEA201810303054), Oct 30, 2018: SKIN. CRACKED. CRACK LIKE INDICATION WAS NOTED AROUND AND BELOW FASTENER DURING NDT INSPECTION OF REPAIR AREA AT BS 1360 APPROX 4 INCHES ABOVE STR 5L. STRIP/REMOVED PAINT AT M
- [SDR FDEA201810283036](https://openairdocs.org/sdr/FDEA201810283036), Oct 28, 2018: FLOORBEAM. CRACKED. SUB BEAM AT STA 580 IS CRACKED. TRIMMED ENTIRE UPPER FLANGE OF THE BS 580 FLOOR BEAM SPLICE. FABRICATED REPAIR ANGLE AND RADIUS STRAP AND INSTALLED IAW EA F-531
- [SDR FDEA201810263017](https://openairdocs.org/sdr/FDEA201810263017), Oct 26, 2018: SKIN. CORRODED. CORROSION FOUND AFT LOWER SKIN, APPROX @ WSTA-681.50 RIGHT WING AFT OF FUEL VENT PANEL. ALL WORK ACCOMPLISHED IAW FEDEX EA F-5730-T0343147 P1 WINGS - PLATES AND
- [SDR FDEA20181113017](https://openairdocs.org/sdr/FDEA20181113017), Oct 26, 2018: SKIN. CORRODED. CORROSION FOUND AFT LOWER SKIN, APPROX @ WSTA-681.50 RIGHT WING AFT OF FUEL VENT PANEL. ALL WORK ACCOMPLISHED IAW FEDEX EA F-5730-T0343147 P1 WINGS - PLATES AND
- [SDR FDEA201707282079](https://openairdocs.org/sdr/FDEA201707282079), Jul 28, 2017: ADC. MALFUNCTIONED. AFTER TAKEOFF, LOST MULTIPLE AVIONICS, PILOTS ALTITUDE, AIRSPEED, RADIO ALTIMETER, AUTOTHROTTLES. FIRST OFFICER`S FLT DISPLAY WAS SIMILAR BUT REGAINED AIRSPEED,
- [SDR FDEA201707282078](https://openairdocs.org/sdr/FDEA201707282078), Jul 28, 2017: LANDING GEAR. MALFUNCTIONED. AFTER TAKE OFF, PUT GEAR UP. GEAR RETRACTED. WHEN GEAR HANDLE WAS PUT TO OFF, GEAR CAME DOWN. PUT GEAR DOWN FOR LANDING AND RECEIVED GOOD DOWN INDICATION. PERFO
- [SDR FDEA201610013404](https://openairdocs.org/sdr/FDEA201610013404), Oct 1, 2016: FLOORBEAM. CRACKED. STUB FRAME BS 580 LBL 44-46 CRACKED. REMOVED AND REPLACED FLOORBEAM SECTION REINFORCEMENT STUB FRAME IAW DWG 657N4311 REV - AND SRM 51-40-05-0G, 51-40-02-0G. MA
- [SDR FDEA201410173289](https://openairdocs.org/sdr/FDEA201410173289), Oct 17, 2014: SKIN. DELAMINATED. LEFT OTBD AFT FLAP UPSIDE OTBD END DELAMINATED. REPAIRED IAW EA F-5750-T0312494.
- [SDR FDEA201409032431](https://openairdocs.org/sdr/FDEA201409032431), Sep 3, 2014: WINDSHIELD. CRACKED. ON CLIMB OUT FIRST OFFICERS R1 WINDOW BEGAN TO ARC. COMPLIED WITH QRH & WINDOW CRACKED AFTER COMPLETING CHECKLIST. LANDED AT NEAREST SUITABLE AIRPORT. R&R FIRST
- [SDR FDEA201212214349](https://openairdocs.org/sdr/FDEA201212214349), Dec 21, 2012: SLIDE. DISLODGED. L1 DOOR ESCAPE SLIDE FELL OFF OF DOOR. REMOVED AND REPLACED L1 DOOR ESCAPE SLIDE IAW AMM 25-66-01-4. OPS CHECKED NORMAL. ACFT OK TO CONTINUE.
- [SDR FDEA201210293773](https://openairdocs.org/sdr/FDEA201210293773), Oct 29, 2012: CARRIAGE. GOUGED. NR 3 FLAP TRACK CARRIAGE OTBD LOWER FITTING GOUGED. COMPLIED WITH EA F-2750-154109 WINGS-LT INBD FLAP CARRIAGE ASSY-GOUGE ON ROLLER SUPPORT ASSY.
- [SDR FDEA201209233412](https://openairdocs.org/sdr/FDEA201209233412), Sep 23, 2012: SENSOR. DIRTY. TAXIING INTO POSITION FOR TAKE OFF, RECEIVED LEFT FWD ENTRY DOOR EICAS MESSAGE CAME ON INTERMITTENTLY DURING TAXI BACK TO GATE. INSPECTED ENTRY DOOR, FOUND GREA

All 130: https://openairdocs.org/aircraft/N944FD/reports.md

## STCs that may be installed (OpenAirDocs) (1)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (Rolls-Royce RB211-535E4 series)

- [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc. Lists RB211-535E4-37

## Related

- Other Boeing 757-2G5 aircraft: https://openairdocs.org/model/boeing-757-2g5/aircraft.md
- The Rolls-Royce RB211-535E4 series engine: https://openairdocs.org/engine/rolls-royce-rb211-535e4-series.md

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