# N963FD: 1989 Boeing 757-28A

- Status: Valid registration
- Airframe: [Boeing 757-28A](https://openairdocs.org/model/boeing-757-28a) (registry code 1384976, 249 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: 24368
- Year built: 1989
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 9, 2014
- Certificate issued: October 23, 2012
- Expires: October 31, 2028
- Mode S code: AD67CC
- 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=963FD
- Page: https://openairdocs.org/aircraft/N963FD

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 757-28A)

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 N963FD.

## FAA accident and incident reports

None matched to N963FD.

## Service difficulty reports (122, 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 FDEA202608281246](https://openairdocs.org/sdr/FDEA202608281246), Aug 28, 2026: WINDOW. ARCED. AFTER INITIATING DESCENT FROM FL300, WITH PRESENCE OF ST. ELMO S FIRE, L1 WINDOW ARCING OCCURRED FOLLOWED BY SHATTERING. QRH ACTIONED AND EMERGENCY DECLARED. RE
- [SDR FDEA202606100692](https://openairdocs.org/sdr/FDEA202606100692), Jun 10, 2026: HOLDER. INOPERATIVE. L1 DOOR EMERGENCY EXIT LIGHT AND SLIDE LIGHT WILL NOT TEST. A/C HAS BEEN POWERED FOR ALMOST 3 HOURS, NO HELP. REMOVED AND REPLACED L1 DOOR EMERGENCY LIGHT POWER
- [SDR FDEA202605050558](https://openairdocs.org/sdr/FDEA202605050558), May 5, 2026: LIGHT. NO DISCREPANCY. FO SIDE SLIDE LIGHT INOP. PERFORMED OPERATIONAL TEST OF R1 GIRT BAR ENGAGED LIGHT, GIRT BAR ENGAGED WARNING LIGHT ILLUMINATES OVER SEVERAL CYCLES OF MODE SELECT
- [SDR FDEA202601050005](https://openairdocs.org/sdr/FDEA202601050005), Jan 5, 2026: SKIN. CRACKED. LEFT AFT FUSELAGE BS 1459-1461 (02EA) FASTENERS AFT OF BUTT SEAM BS 1459 ABOVE STR 20 AND DOUBLER THAT HAVE (02) POSSIBLE CRACKS INDICATION UNDER FASTENERS RUNN
- [SDR FDEA202601030003](https://openairdocs.org/sdr/FDEA202601030003), Jan 3, 2026: REPAIR. NOT REPORTED. EXISTING REPAIR FOUND AT # 2 CARGO DOOR AFT LOWER CORNER CUTOUT AREA COMPLIED WITH EA # F-5330-T0305556 B TITLE: FUSELAGE PLATES & SKINS - REPLACEMENT OF EXISTI
- [SDR FDEA202512292294](https://openairdocs.org/sdr/FDEA202512292294), Dec 29, 2025: STRINGER. CORRODED. AFT CARGO COMPARTMENT, DURING REMOVAL OF PRODUCTION STRINGER SPLICE TO GAIN ACCESS FOR STRINGER REPAIR FOUND STRINGER 21L, BS 1460 - 1465 EXFOLIATED. REPAIRED T
- [SDR FDEA202512292293](https://openairdocs.org/sdr/FDEA202512292293), Dec 29, 2025: STRINGER. CRACKED. AFTER DVI OF THE LAPPED AND OVERLAPPING SKIN UNDERNEATH OF THE EXISTING REPAIR DOUBLER BETWEEN BS 1430 TO BS 1475, STR 20L TO STR 21L FOUND STRINGER 21L CRACKED
- [SDR FDEA202512262290](https://openairdocs.org/sdr/FDEA202512262290), Dec 26, 2025: FITTING. LOOSE. NR 1 ENGINE NACELLE STRUT R/H SIDE AFTER. HINGE FITTING BOLT HEAD BROKEN OFF. REMOVED AND REPLACED BOLT AT NO 1 ENGINE NACELLE STRUT R/H SIDE AFT. HINGE FITTING
- [SDR FDEA202512232285](https://openairdocs.org/sdr/FDEA202512232285), Dec 22, 2025: FLOOR SUPPORT. DAMAGED. AFT CARGO COMPARTMENT STRINGER AT B.S. 1260 LBL 10.45 WITH SEVERAL PERFORATIONS (MISDRILLED) AFT CARGO COMPARTMENT STRINGER AT BS.1260 LBL 10.45 WAS REPAIRED IA
- [SDR FDEA202512212275](https://openairdocs.org/sdr/FDEA202512212275), Dec 21, 2025: SHEAR PLATE. CORRODED. GALLEY AREA BS 375 BTW LBL 20.00 TO LBL 26.00 SHOW PLATE CORRODED. REMOVED AND REPLACED SHEAR PLATE SEAT TRACK SUPPORT (U CHANNEL) AND (2EA) FLEXURE ANGLE IAW V
- [SDR FDEA202512202272](https://openairdocs.org/sdr/FDEA202512202272), Dec 20, 2025: STRINGER. CORRODED. AFT CARGO BAY, STRINGER 30 BTW BS 1440 TO 1460 FOUND CORRODED. REPAIRED THE STRINGER IAW SRM 53-00-03-2R, SRM 51-40-02-0G, & DWG 146N3110, REV B.
- [SDR FDEA202512202271](https://openairdocs.org/sdr/FDEA202512202271), Dec 20, 2025: SHEAR TIE. CORRODED. AFT CARGO BAY, BS 1460 SHEAR TIE BTW STR-29L TO STR-30, FOUND CORRODED. REPLACED SHEAR TIE IAW SRM 51-40-02-0G, AND DWG 140N2002, REV C.
- [SDR FDEA202512202270](https://openairdocs.org/sdr/FDEA202512202270), Dec 20, 2025: SHEAR TIE. CORRODED. LOWER HALF OF FUSELAGE BS 1460 BETWEEN S28L AND S29L HAS POSSIBLE CORROSION. REPLACED THE SHEAR TIE IAW SRM 51-40-02-0G, AND DWG 140N2002, REV C.
- [SDR FDEA202512202269](https://openairdocs.org/sdr/FDEA202512202269), Dec 20, 2025: STRINGER SPLICE. CORRODED. AFT CARGO COMPARTMENT BS 1460 SPLICE STRINGER 30 CORRODED. REPLACED SPLICE STRINGER LOCATED BS 1460 IAW SRM 51-40-02-0G, AND DWG 146N3820, REV C.
- [SDR FDEA202512202268](https://openairdocs.org/sdr/FDEA202512202268), Dec 20, 2025: STRINGER. CORRODED. AFT CARGO BAY, STRINGER 30L BTW BS 1460 - 1480, FOUND CORRODED. REPAIRED THE STRINGER IAW SRM 51-40-02-0G, & DWG 146N3110, REV C.
- [SDR FDEA202512202267](https://openairdocs.org/sdr/FDEA202512202267), Dec 20, 2025: STRINGER SPLICE. CORRODED. AFT CARGO BAY, BS 1460 STRINGER SPLICE 29L CORRODED. REPLACED THE STRINGER SPLICE IAW SRM 51-40-02-0G, DWG 146N3820, REV C.
- [SDR FDEA202512202266](https://openairdocs.org/sdr/FDEA202512202266), Dec 20, 2025: STRINGER. CORRODED. AFT CARGO BAY STRINGER 29L BTW BS 1460 TO 1480, FOUND CORRODED. REPAIRED THE STRINGER IAW SRM 51-40-020-G, AND DWG 146N3110, REV B.
- [SDR FDEA202512202265](https://openairdocs.org/sdr/FDEA202512202265), Dec 20, 2025: SKIN PANEL. CRACKED. RIGHT WING OTBD LEADING EDGE SLAT NR 10 INTERNAL LOWER MAIN TRACK SLAT HAS POSSIBLE CRACKED. REMOVED DAMAGED COVE SKIN AT RT WING OTBD LEADING EDGE SLAT 10 IAW 
- [SDR FDEA202512182261](https://openairdocs.org/sdr/FDEA202512182261), Dec 18, 2025: STRINGER. CORRODED. BULK AREA BETWEEN STA 1700 TO 1720 STR 23L CORRODED ACCOMPLISHED REPAIR ON STRINGER BTW STA 1685 TO STR 1720 IAW B757 SRM 53-00-03-2R, 51- 40-02-0G
- [SDR FDEA202512112236](https://openairdocs.org/sdr/FDEA202512112236), Dec 11, 2025: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK BETWEEN BS 900 TO BS 1180.0 LBL 58.22 HAS MULTIPLE SPOTS WITH CORROSION. REMOVED AND EVALUATED MAIN CABIN SEAT TRACK BTW BS 900-1180, LBL 
- [SDR FDEA202510172049](https://openairdocs.org/sdr/FDEA202510172049), Oct 17, 2025: PITOT TUBE. FAILED. STARTED TAKEOFF. POWER WAS SET. SHORTLY THEREAFTER BETWEEN 30 AND 40 KNOTS, RECEIVED ABOUT 3 TO 5 CAS MESSAGES. AUTOTHROTTLE DISCONNECT, SOME PROBE WARNING AND 
- [SDR FDEA202505100745](https://openairdocs.org/sdr/FDEA202505100745), May 10, 2025: SLIDE. FAILED. RAMP PERSONNEL OPENED L1 AFTER DOORS WERE ARMED AND THE SLIDE FELL OUT OF THE DOOR WITHOUT INFLATING. L1 DOOR ASSIST BOTTLE BLOWN, SLIDE DID NOT DEPLOY. REPLACE
- [SDR FDEA202503210469](https://openairdocs.org/sdr/FDEA202503210469), Mar 21, 2025: COMPUTER. FAULTED. MADE 2 TAKEOFF ATTEMPTS , MAX POWER FOR WIND SHEAR, EACH TIME REJECTED TAKEOFF DUE TO AIRCRAFT VEERING TO THE RIGHT OF CENTERLINE. NO EICAS MESSAGES OR WARNINGS
- [SDR FDEA202307071182](https://openairdocs.org/sdr/FDEA202307071182), Jul 7, 2023: UNKNOWN. UNKNOWN. WITH OUR BEACON ON, A MECHANIC OPENED L FWD ENT DOOR FROM OUTSIDE THE AIRCRAFT WHEN THE SLIDE WAS ARMED. THE SLIDE FELL OUT OF THE DOOR WITHOUT INFLATING. OLD S
- [SDR FDEA202206171458](https://openairdocs.org/sdr/FDEA202206171458), Jun 17, 2022: HOSE. MALFUNCTIONED. RIGHT ENGINE PROBLEM AT CRUISE. RIGHT EPR SHOWED MAX ON SCALE. FUEL FLOW APPRX 1/2 OF LEFT ENGINE. ALL RIGHT INSTRUMENTS WERE SIGNIFICANT THEN LEFT. HAD TO DESC
- [SDR FDEA202204120932](https://openairdocs.org/sdr/FDEA202204120932), Apr 12, 2022: GIRT BAR. MISALIGNED. MDIS 963 52-10 7334 12APR22 PDX FACT U L-1 DOOR WILL NOT ARM FACT 12APR22 21:02 AFW U INSPECTED AND VERIFIED GIRT BAR ALLIGNMENT IN REF TO AMM 25-66-10-2. PERFO
- [SDR FDEA202202160422](https://openairdocs.org/sdr/FDEA202202160422), Feb 16, 2022: FLOORBEAM. CRACKED. MAIN DECK CARGO COMPARTMENT FLOOR BEAM - UPPER CAP AFT FLANGE CRACKED, AT STA580, LBL45.5 COMPLIED WITH FEDEX EA: F-5310-T0367280 PT1, EA TITLE: FUSELAGE - MAIN
- [SDR FDEA202201260143](https://openairdocs.org/sdr/FDEA202201260143), Jan 26, 2022: LIFE RAFT. DAMAGED. R1 DOOR WAS OPENED FROM THE OUTSIDE WHILE STILL ARMED, SLIDE FELL OFF OF DOOR RAR R1 SLIDE/RAFT, REF B757 AMM 25-66-01-4. NO DEFECTS NOTED AT THIS TIME. MEL ITE
- [SDR FDEA202110272644](https://openairdocs.org/sdr/FDEA202110272644), Oct 27, 2021: NONE. NONE. FOUND LIGHTING STRIKE DAMAGE TO SKIN 1.5" AFT OF STA 520 2.75" IB OF STR S29L WRITTEN ON WRI 53-00-6918 WORKED ON SEQ 5 UNDER W/O 81650 CARD WRITTEN FOR RDR/SDR
- [SDR FDEA202110272643](https://openairdocs.org/sdr/FDEA202110272643), Oct 27, 2021: NONE. NONE. FOUND LIGHTING STRIKE DAMAGE ON SECTION 43, ON STA 580, 4.5" IB OF STR 29R DAMAGE WRITTEN UP ON WRI 53-00-6925 REPAIR WORKED ON SEQ 6 W/O 81650. CARD WRITTEN FO
- [SDR FDEA202107071697](https://openairdocs.org/sdr/FDEA202107071697), Jul 7, 2021: BATTERY PACK. INOPERATIVE. RIGHT SIDE EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK AND TESTED OK IAW AMM: 33-51-07-2-2.
- [SDR FDEA202004300862](https://openairdocs.org/sdr/FDEA202004300862), Apr 30, 2020: TRANSITION PANEL. CRACKED. BULK PIT AT BS 1550 & L/H TRANSITION PANEL PUNCHED (CRACKED). TRANSITION PANEL REPAIR ACCOMPLISHED IAW B757-200 SRM 53-00-53-2R REPAIR 2.
- [SDR FDEA202004300860](https://openairdocs.org/sdr/FDEA202004300860), Apr 30, 2020: ACCESS PANEL. CRACKED. #2 PYLON, OUTBOARD, HINGED PANEL 443AR, INNER SURFACE CRACKED. REPAIRED INNER SURFACE OF #2 PYLON, OUTBOARD, HINGED PANEL 443AR IAW B757 SRM 51- 70-17-0G RESTOR
- [SDR FDEA2020043080815](https://openairdocs.org/sdr/FDEA2020043080815), Apr 28, 2020: SEAT TRACK. CORRODED. R/H SUPERNUMERARY SEAT TRACK CORRODED REMOVED AND REPLACED SEAT TRACK IAW VENTURA AEROSPACE DWG 3470 REV G
- [SDR FDEA2020043080814](https://openairdocs.org/sdr/FDEA2020043080814), Apr 28, 2020: SEAT TRACK. CORRODED. L/H SUPERNUMERARY SEAT TRACK CORRODED REMOVED AND REPLACED SEAT TRACK IAW VENTURA AEROSPACE DWG 3470 REV G
- [SDR FDEA202004260795](https://openairdocs.org/sdr/FDEA202004260795), Apr 26, 2020: STRAP. GOUGED. FUSELAGE EXTERIOR AFT CAGO DOOR CONTROL ANEL CUT OUT LOWER EDGE IS GOUGED ACCOMPLISHED BLEND REPAIR PER FEDEX EA F-5330-T0305556-P2
- [SDR FDEA2020042760795](https://openairdocs.org/sdr/FDEA2020042760795), Apr 26, 2020: STRAP. GOUGED. FUSELAGE EXTERIOR AFT CAGO DOOR CONTROL ANEL CUT OUT LOWER EDGE IS GOUGED ACCOMPLISHED BLEND REPAIR PER FEDEX EA F-5330-T0305556-P2
- [SDR FDEA2020042760792](https://openairdocs.org/sdr/FDEA2020042760792), Apr 26, 2020: SEAL. CRACKED. #2 EXHAUST NOZZLE 6 OCLOCK POSITION CASE DRAIN SUPPORT PLATE CRACKED REMOVED AND REPLACED SEAL PER B757 SRM 51-40-02-OG AND RR EIPC 78-11-04-03
- [SDR FDEA2020042750785](https://openairdocs.org/sdr/FDEA2020042750785), Apr 25, 2020: FILLER. WORN. DURING AGING AIRCRAFT INSPECTION OF EXISTING REPAIR ON RIGHT WING OUTBOARD FLAP INBOARD LEADING EDGE SKIN FOUND FLUSH SKIN FILLER TO BE WORN REMOVED WORN FILLER
- [SDR FDEA2020042740782](https://openairdocs.org/sdr/FDEA2020042740782), Apr 24, 2020: MOUNT BRACKET. CRACKED. AILERON A2B CABLE PULLEY MOUNT BRACKET CRACKED AT STA 358 RBL25. STREAMER ATTACHED REMOVED, FABRICATED AND INSTALLED NEW STIFFENER, P/N 251N6133 IAW DWG 251N613
- [SDR FDEA2020042310767](https://openairdocs.org/sdr/FDEA2020042310767), Apr 21, 2020: SKIN. DENTED. LOWER FUSELAGE EXTERNAL SKIN ,STA 1592.7 BETWEEN S22R-S23R DENTED REPAIRED PER B757 SRM 53-00-01-2R REPAIR 29
- [SDR FDEA2018081402006](https://openairdocs.org/sdr/FDEA2018081402006), Aug 10, 2018: COVER. DAMAGED. L1 DOOR SLIDE COVER DAMAGED. REPAIRED L1 DOOR SLIDE COVER IAW AMM 25-00-00-8. ACFT OK FOR SERVICE.
- [SDR FDEA2018051871251](https://openairdocs.org/sdr/FDEA2018051871251), May 17, 2018: HEATER. FAILED. APPOACHING THE BEGINNING OF THE HITHR 2 RNAV, ARRIVAL AT 340 LIGHT SMOKE AND AN ELECRICAL BURNING ODOR WAS IMMEDIATELY NOTICED IN THE COCKPIT. THE SOURCE SEEMED
- [SDR FDEA201804050858](https://openairdocs.org/sdr/FDEA201804050858), Apr 5, 2018: STRINGER. DAMAGED. FOUND STRINGER 16L AT BS 1710 DAMAGED. CUT-OUT THE DAMAGED SECTION OF THE STRINGER, DRILLED A NEW STRINGER AND SPLICE. A REPAIR WAS INSTALLED IAW SRM 53-00-03-2
- [SDR FDEA201802220467](https://openairdocs.org/sdr/FDEA201802220467), Feb 22, 2018: ADC. FAILED. AT APPROXIMATELY 7000 FT, LOST THE LT AIR DATA COMPUTER. SPEED TAPE, ALTITUDE, ALL INDICATIONS ON CAPTAIN`S SIDE, ROLLING ERRATICLY UP AND DOWN. DURING TROUBLES
- [SDR FDEA201706061571](https://openairdocs.org/sdr/FDEA201706061571), Jun 6, 2017: CONNECTOR. DAMAGED. DURING DESCENT, LT ENGINE HYD PUMP EICAS MESSAGE DISPLAYED. TURNED OFF PUMP IAW QRH. PINNED THE NR 2 WIRE ON THE CONNECTOR IAW SWPM. DRY MOTORED THE NR 1 ENGINE
- [SDR FDEA201705021325](https://openairdocs.org/sdr/FDEA201705021325), May 2, 2017: GIRT BAR. LACK OF LUBE. R1 DOOR WOULD NOT OPEN AT BLOCK IN. R1 DOOR GIRT BAR LOCK PLATES DIRTY AND DRY. LUBED GIRT BAR. OPS NORMAL.
- [SDR FDEA201702170580](https://openairdocs.org/sdr/FDEA201702170580), Feb 17, 2017: LINER. OUT OF POSITION. WHILE ARMING THE RIGHT CREW ENTRY DOOR THE KNUCKLEBUSTER FAILED TO ARM IN THE CORRECT POSITION. REMAINED FLUSH WITH THE DOOR AND THE RED ARM WAS NOT VISIBLE. AD
- [SDR FDEA201609103187](https://openairdocs.org/sdr/FDEA201609103187), Sep 10, 2016: LIGHT. INTERMITTENT. BOTTOM ONE THIRD OF OVERHEAD PANEL LIGHTS WERE INTERMITTENT. REF WDM 23-71-11, 33-13-31 & CMM 23-70-43 CVR MPN 980-6116-002 DOES NOT CONTAIN CONTACTS FOR INTEGR
- [SDR FDEA201604211334](https://openairdocs.org/sdr/FDEA201604211334), Apr 21, 2016: LOCK SENSOR. FAILED. AFTER TAKEOFF, RECEIVED GEAR DISAGREE EICAS ALERT. FOLLOWED CHECKLIST & PERFORMANCE TABLES & CONTINUED. DURING APPROACH WE EXTENDED GEAR EARLY AT APPROX 210 KTS

All 122: https://openairdocs.org/aircraft/N963FD/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 757-28A aircraft: https://openairdocs.org/model/boeing-757-28a/aircraft.md
- The Rolls-Royce RB211-535E4 series engine: https://openairdocs.org/engine/rolls-royce-rb211-535e4-series.md

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