# N962FD: 1988 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: 24176
- Year built: 1988
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 24, 2012
- Certificate issued: September 22, 2011
- Expires: September 30, 2027
- Mode S code: AD6415
- 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=962FD
- Page: https://openairdocs.org/aircraft/N962FD

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 N962FD.

## FAA accident and incident reports

None matched to N962FD.

## 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 FDEA202607220987](https://openairdocs.org/sdr/FDEA202607220987), Jul 22, 2026: FITTING. CRACKED. CRACK FOUND ON #2 ENGINE LOWER OUTBD MIDSPAR BULKHEAD FITTING. REPAIRED OUTBD MIDSPAR BULKHEAD FITTNG IAW EA F-5450-T0387823 PT1, NACELLS / PYLON - WING PYLON /
- [SDR FDEA202601060010](https://openairdocs.org/sdr/FDEA202601060010), Jan 6, 2026: BULB. FAILED. DURING MX PRE-FLIGHT, FOUND R1 EMERGENCY EXIT SIGN DIM. AMM: 33-51-01-2 FOUND R1 EMERGENCY EXIT SIGN HAS 9 BULBS OUT. REMOVED AND REPLACED 9 FAULTY BULBS AS PER
- [SDR FDEA202601060009](https://openairdocs.org/sdr/FDEA202601060009), Jan 6, 2026: BULB. FAILED. DURING MX PRE-FLIGHT, FOUND L1 EMERGENCY EXIT SIGN DIM. AMM 33-51-01-2 FOUND L1 EMERGENCY EXIT SIGN HAS 7 BULBS OUT. REMOVED AND REPLACED 7 FAULTY BULBS AS PER 
- [SDR FDEA202406040767](https://openairdocs.org/sdr/FDEA202406040767), Jun 4, 2024: FLOORBEAM. CORRODED. MAIN CABIN COURIER AREA, STA 346 ALONG TOP SIDE HAS SEVERAL AREAS OF BARE METAL AND CORROSION ON PREVIOSLY BLENDED AREA OF BEAM. PREVIOUS BLEND OUT ON FLOOR BEA
- [SDR FDEA202311281899](https://openairdocs.org/sdr/FDEA202311281899), Nov 28, 2023: SLIDE. DAMAGED. DOOR WAS ACCIDENTALLY ARMED, AND THEN OPENED FROM THE OUTSIDE AND THE SLIDE FELL OUT, BUT DID NOT DEPLOY. REMOVED AND REPLACED L1 DOOR ESCAPE SLIDE. OPS CHECKS 
- [SDR FDEA202210112550](https://openairdocs.org/sdr/FDEA202210112550), Oct 11, 2022: BUSS. FAILED. TURNING FINAL FOR THE RUNWAY, LOST LT GEN & LT AC BUSS, CONTINUED WITH A GO AROUND & RAN QRH & WERE ABLE ABLE TO GET A PARTIAL COCKPIT BACK. CONTINUED APPROACH 
- [SDR FDEA202209282381](https://openairdocs.org/sdr/FDEA202209282381), Sep 28, 2022: GCU. FAILED. ON FINAL TO KSBD LOST THE LEFT AC BUS. WE HAD L GEN OFF, L BUS OFF, AND L BUS TIE TO ISLN ON THE OVERHEAD PANEL. LOST ASSOCIATED EQUIPMENT ON CAPTAIN SIDE. FLAP
- [SDR FDEA202208262078](https://openairdocs.org/sdr/FDEA202208262078), Aug 26, 2022: SUPPORT BRACKET. CORRODED. AUXILIARY POWER UNIT DOOR SURROUND STRUCTURE CORRODED. REMOVED & REPLACED ANGLE SUPPORT BRACKETS & APU FWD STRAP OF AUXILIARY POWER UNIT DOOR SURROUND STRUCTURE
- [SDR FDEA202208222028](https://openairdocs.org/sdr/FDEA202208222028), Aug 22, 2022: INLET. CORRODED. #1 ENGINE INLET COWL MOUNT FLANGE ON THE ENGINE SIDE IS CORRODED SPORADICALLY AROUND THE ENTIRE CIRCUMFERENCE OF THE ENGINE REMOVED AND REPLACED ENGINE PER FEDE
- [SDR FDEA202208192007](https://openairdocs.org/sdr/FDEA202208192007), Aug 19, 2022: PANEL. CRACKED. R.WING #8 SLAT I/B AUX TRACK LOWER TRAILING EDGE CLOSE OUT PANEL IS CRACKED. REMOVE AND REPLACED CLOSE OUT PANEL WITH NEW PANEL PER BAC DWG 114N4147 REV A AND B
- [SDR FDEA202208181997](https://openairdocs.org/sdr/FDEA202208181997), Aug 18, 2022: FILLER. CORRODED. NOSE LANDING GEAR WHEEL WELL, UPPER AFT ACCESS PANEL 117CL, FORWARD SIDE OF STA 377.7 LBL 10 TO LBL 25, PLATE CORRODED. REMOVED, FABRICATED AND REPLACED NEW FIL
- [SDR FDEA202208161983](https://openairdocs.org/sdr/FDEA202208161983), Aug 16, 2022: SKIN. CRACKED. R.WING O/B FIXED L/E SKIN UPPER SURFACE IS CRACKED @ #7 SLAT I/B MAIN TRACK LOCATION. APPROX. FSS 345 REPAIRED R.WING FIXED L/E SKIN PER B757 SRM 57-41-01 AND 5
- [SDR FDEA202208151979](https://openairdocs.org/sdr/FDEA202208151979), Aug 15, 2022: WEB. DAMAGED. MAIN CARGO DOOR I/B SIDE HAS 1 EA GOUGE AT THE WEB APPROX BS 519.5 BETWEEN WL210 AND 220 REMOVED, FABRICATED AND INSTALLED NEW WEB IAW B757-2 DWG 65-49309 REV D
- [SDR FDEA202208151978](https://openairdocs.org/sdr/FDEA202208151978), Aug 15, 2022: WEB. GOUGED. MAIN CARGO DOOR I/B SIDE HAS 1 EACH GOUGE AT WEB APPROX BS 602 WL220 REMOVED, FABRICATED AND INSTALLED NEW WEB IAW B757-2 DWG 65-49309 REV D
- [SDR FDEA202208111961](https://openairdocs.org/sdr/FDEA202208111961), Aug 11, 2022: PLATE. CRACKED. R. WING T/E WIGGLE PLATE IS CRACKED, O/B OF THE I/B FLAP, BELOW # 8 SPOILER REMOVE AND REPLACED WIGGLE PLATE PER BAD DWG 113N1630 REV C
- [SDR FDEA202011212942](https://openairdocs.org/sdr/FDEA202011212942), Nov 21, 2020: GIRT BAR. FAILED. L1 GIRT BAR CENTERING BLOCK EXFOLIATED. REPLACED GIRT BAR AND GIRT BAR CENTERING BLOCK, REF B757 AMM 25-66-10-2. A/C OK FOR SERVICE.
- [SDR FDEA202009272333](https://openairdocs.org/sdr/FDEA202009272333), Sep 27, 2020: IDG. MALFUNCTIONED. RECEIVED A LT GEN OFF EICAS ON TAKEOFF ROLL AND REJECTED THE TAKEOFF. RAN THE REJECTED TAKEOFF CHECKLIST AND THE QRH, WHICH RESET THE FAULTS. TRIED THE TAKEOFF 
- [SDR FDEA2020072761662](https://openairdocs.org/sdr/FDEA2020072761662), Jul 26, 2020: TEE FITTING. CORRODED. MAIN DECK BETWEEN STA 920-1040 RBL45.5 T CHORD CORRODED REMOVED CORR ON T CHORD STA 900-1040 RBL 45.5 IAW B757 SRM 51-10-02. ORIG MAT .090 REM O FOUND OUT OF LI
- [SDR FDEA202007241642](https://openairdocs.org/sdr/FDEA202007241642), Jul 24, 2020: TEE FITTING. CORRODED. MAIN DECK STA 1200 BETWEEN LBL 24.75- LBL 45.5 T CHORD CORRODED REMOVED CORROSION FROM BS 1200 FLOOR BEAM (T CHORD) IAW B757 SRM 51-10-02. ORIG MAT .125 REMAING
- [SDR FDEA202007201594](https://openairdocs.org/sdr/FDEA202007201594), Jul 20, 2020: SEAT TRACK. CORRODED. SEAT TRACK HAS CORROSION IN MAIN CABIN @ RBL-45.5 BETWEEN STA. 1640 AND 1660 SEAT TRACK AT STA. 1640-1660 RBL45.5 OUT OF LIMITS DUE TO EXFOILATION IAW B757 SRM 
- [SDR FDEA2020072301594](https://openairdocs.org/sdr/FDEA2020072301594), Jul 20, 2020: SEAT TRACK. CORRODED. SEAT TRACK HAS CORROSION IN MAIN CABIN AT RBL 45.5 BETWEEN BS 1640 AND 1660. FOUND OUT OF LIMITS DUE TO EXFOILATION IAW SRM 53-00-52-1A, FIG 101. REMOVED, FABRI
- [SDR FDEA202007171564](https://openairdocs.org/sdr/FDEA202007171564), Jul 17, 2020: SEAT TRACK. CORRODED. MAIN DECK BETWEEN BS 1060 - 1180 LBL 58.22, THE SEAT TRACK WAS CORRODED. REPAIRED IAW EA F-5310-T0355139 P1.
- [SDR FDEA202007171563](https://openairdocs.org/sdr/FDEA202007171563), Jul 17, 2020: FRAME. CRACKED. DURING AN NDT OPEN HOLE INSPECTION, TWO CRACK NDICATIONS NOTED IN LOWER INBOARD HOLE AT APPROX. 8 AND 4 O'CLOCK POSTIONS LOOKING AFT. BS 1640 FRAME STRINGER 14L
- [SDR FDEA202007171562](https://openairdocs.org/sdr/FDEA202007171562), Jul 17, 2020: SEAT TRACK. CORRODED. MAIN DECK BETWEEN STA 1180-1200 LBL 44.5 SEAT TRACK CORRODED. REMOVED CORR ON SEAT TRACK STA 1180-1200 LBL 44.5 IAW B757 SRM 51-10-02. ORIG MAT .070 REM 0 OUT O
- [SDR FDEA202007171561](https://openairdocs.org/sdr/FDEA202007171561), Jul 17, 2020: CREASE BEAM. CORRODED. MAIN DECK BS 1600, LEFT SIDE INBD CREASE BEAM CORRODED. REMOVED THE CORROSION IAW SRM 51-10-02. EVALUATED 100% MATERIAL LOSS, OUT OF LIMITS IAW SRM 53-60-13-1A,
- [SDR FDEA2020072351517](https://openairdocs.org/sdr/FDEA2020072351517), Jul 15, 2020: FLOORBEAM. CORRODED. MAIN DECK STA 1015 BETWEEN LBL24.75-LBL45.5 FLOOR SUPPORT CORRODED REMOVED CORR ON FLOOR SUPPORT STRAP ONLY IAW B757 SRM 51-10-02. ORIG MAT .012 REM .005 LOSS .
- [SDR FDEA2020071751517](https://openairdocs.org/sdr/FDEA2020071751517), Jul 15, 2020: STRAP. CORRODED. MAIN DECK BS 1015 BETWEEN LBL 24.75 - LBL 45.5 FLOORBEAM CORRODED. REMOVED THE CORROSION ON THE STRAP ONLY IAW SRM 51-10-02. ORIG MAT .012 REM .005 LOSS .007, F
- [SDR FDEA202007091480](https://openairdocs.org/sdr/FDEA202007091480), Jul 9, 2020: FLOORBEAM. CRACKED. MAIN DECK FLOOR BEAM CRACKED, BS 580 BELOW SEAT TRACK LBL 44.5. TRIMMED UPPER FLANGE OF THE FLOORBEAM SPLICE, FABRICATD A REPAIR ANGLE , RADIUS STRAP, AND INSTA
- [SDR FDEA2020071091480](https://openairdocs.org/sdr/FDEA2020071091480), Jul 9, 2020: FLOORBEAM. CRACKED. MAIN DECK FLOORBEAM CRACKED BS 580 BELOW SEAT TRACK LBL 44.5.
- [SDR FDEA2019110762899](https://openairdocs.org/sdr/FDEA2019110762899), Nov 6, 2019: CIRCUIT CARD. MALFUNCTIONED. DURING CLIMBOUT GOT STATUS MESSAGE L ENG OH LP2 PER CREW REPORT , STATUS MESSAGE WENT OUT ON LANDING. NO STATUS MESSAGE SHOWN. TROUBLESHOT PER 757 FIM 26-11/802
- [SDR FDEA201803010538](https://openairdocs.org/sdr/FDEA201803010538), Mar 1, 2018: FSEU. MALFUNCTIONED. DURING CRUISE, HAD A TE FLAP ASYMETERY EICAS MESSAGE. PERFORMED QRH PROCEDURE AND LANDED FLAPS UP. HAPPENED AFTER ABOUT 1.5 HOURS IN MODERATE TO LIGHT TURBULANC
- [SDR FDEA201801300276](https://openairdocs.org/sdr/FDEA201801300276), Jan 30, 2018: SENSOR. MALFUNCTIONED. DURING CRUISE, NOTICED THE SLIDE LIGHT FOR THE L1 DOOR WAS EXTINGUISHED. REPLACED THE SENSOR IAW AMM 25-66-11-4. OPS CHECKED GOOD.
- [SDR FDEA201708112188](https://openairdocs.org/sdr/FDEA201708112188), Aug 11, 2017: COVER. DISLODGED. LEFT FWD ENTRY DOOR SLIDE COVER DISLODGED. IAW MM 25-66-01-4, REINSTALLED THE SLIDE COVER. OK FOR SERVICE.
- [SDR FDEA201607292656](https://openairdocs.org/sdr/FDEA201607292656), Jul 29, 2016: HINGE. DIRTY. LEFT CABIN DOOR HARD TO CLOSE. FOUND DEBRIS IN DOOR HINGE. CLEANED AND OPERATED THE DOOR SEVERAL TIMES IAW AMM 52-11-00-2, NO DEFECTS NOTED.
- [SDR FDEA201607012222](https://openairdocs.org/sdr/FDEA201607012222), Jul 1, 2016: SHEAR PLATE. CORRODED. MAIN CABIN SHEAR PLATE BS 380 - 440 BL 0 TO RBL 24.75 HAS LIGHT CORROSION. BLENDED SHEAR PLATE IAW SRM 51-10-02, ORIGINAL .125 REM .057 LOSS .068. FOUND OUT OF 
- [SDR FDEA201510223332](https://openairdocs.org/sdr/FDEA201510223332), Oct 22, 2015: COLLAR. BROKEN. L1 DOOR WOULD NOT OPEN FULL TRAVEL. REPLACED PREVIOUSLY REMOVED BROKEN HOLD & OPEN COLLAR IAW AMM 52-11-08-8. ACFT OK FOR SERVICE.
- [SDR FDEA201504231288](https://openairdocs.org/sdr/FDEA201504231288), Apr 23, 2015: VALVE. MALFUNCTIONED. AT SLOW TAXI SPEEDS WITH PRESS ON BRAKES, THE BRAKES WILL SLOWLY RELEASE, RESULTING IN, PULSATING BRAKES DURING TAXI. IAW MM 12-15-05, CHECKED BRAKE CONTROL ACC
- [SDR FDEA201504041151](https://openairdocs.org/sdr/FDEA201504041151), Apr 4, 2015: DOOR. LACK OF LUBE. L1 DOOR WILL NOT OPEN ALL THE WAY FWD TO LOCKED OPEN POSITION. LUBED DOOR HINGE TORQUE TUBE. DOOR OPENS & CLOSES NORMALLY.
- [SDR FDEA201502200556](https://openairdocs.org/sdr/FDEA201502200556), Feb 20, 2015: DOOR. UNKNOWN. DOOR 1L WILL ONLY OPEN 1/2 WAY & IS TIGHT.
- [SDR FDEA201406301595](https://openairdocs.org/sdr/FDEA201406301595), Jun 30, 2014: SKIN. DENTED. LEFT SIDE OF FUSELAGE HAS A DENT AT BS 502 JUST BELOW STRINGER 26L. COMPLIED WITH EA F-5330-T0309215 REV NR PS P1 FUSELAGE PLATES & SKINS STATION 502-5-266-SKIN
- [SDR FDEA201406301594](https://openairdocs.org/sdr/FDEA201406301594), Jun 30, 2014: SKIN. DENTED. LEFT SIDE OF FUSELAGE HAS A DENT AT BS 1701 BETWEEN STRINGERS 19L & 20L. COMPLIED WITH F-5330-T0309246 REV NR PS P1 FUSELAGE PLATES & SKINS STATION 1701 SKIN DE
- [SDR FDEA201406251548](https://openairdocs.org/sdr/FDEA201406251548), Jun 25, 2014: SKIN. DENTED. LEFT SIDE OF FUSELAGE HAS A DENT AT BS 763 JUST BELOW STRINGER 14L. COMPLIED WITH FX EA F-5330-TO309193 PT 1 FUSELAGE SKIN DENT BELOW STRINGER 14L AND AFT OF ST
- [SDR FDEA201406231533](https://openairdocs.org/sdr/FDEA201406231533), Jun 23, 2014: SEAT TRACK. CORRODED. LT COURIER SEAT TRACK HAS CORROSION AT BS 345, LBL 4. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK AT BS 345 LBL 4 IAW B757 DWG 3504-NC-2, B757 SRM 51-40-0
- [SDR FDEA201406231532](https://openairdocs.org/sdr/FDEA201406231532), Jun 23, 2014: SEAT TRACK. CORRODED. RIGHT COURIER SEAT TRACK HAS CORROSION AT BS 345. REMOVED, FABRICATED & INSTALLED NEW SEAT TRACK IN COURIER AREA AT BS 345 IAW SRM 51-40-02, 51-40-5, 51-20-61, 
- [SDR FDEA201403110478](https://openairdocs.org/sdr/FDEA201403110478), Mar 11, 2014: LIGHT. INOPERATIVE. R1 SLIDE ILLUMINATION LIGHT INOPERATIVE. RE LAMPED IAW AMM 33-51-06, OPERATIONS CHECKED GOOD.
- [SDR FDEA201303270674](https://openairdocs.org/sdr/FDEA201303270674), Mar 27, 2013: HANDLE. DETACHED. CAPTAIN`S WINDOW CRANK HANDLE DETACHED. REPLACED WINDOW CRANK HARDWARE. OPS CHECKED GOOD IAW AMM 56-11-04-4.
- [SDR FDEA201212294398](https://openairdocs.org/sdr/FDEA201212294398), Dec 29, 2012: CONNECTOR. DAMAGED. WHILE INSTALLING PANEL ON LT SIDE OF PEDESTAL REF WRI 27-60/0753. FOUND CAPT'S STICK SHAKER WIRES ARCING. CONNECTOR MSN 1299126. REMOVED SPORTS TAPE AND FOUND W
- [SDR FDEA201211023816](https://openairdocs.org/sdr/FDEA201211023816), Nov 2, 2012: LAMP. INOPERATIVE. RT ENTRY DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED LAMP IAW MM 33-51-06-2-1. OPS CHECKED NORMAL.
- [SDR FDEA201211013806](https://openairdocs.org/sdr/FDEA201211013806), Nov 1, 2012: LAMP. INOPERATIVE. RIGHT ENTRY DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE. LAMPED IAW MM 33-51-06-2-1. OPS CHECKED NORMAL.
- [SDR FDEA201211013805](https://openairdocs.org/sdr/FDEA201211013805), Nov 1, 2012: LAMP. INOPERATIVE. RIGHT ENTRY DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE. LAMPED PER MM 33-51-06-2-1 OPS CHECKED NORMAL

All 130: https://openairdocs.org/aircraft/N962FD/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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