# N969FD: 1997 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: 28164
- Year built: 1997
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 8, 2014
- Certificate issued: April 25, 2013
- Expires: April 30, 2029
- Mode S code: AD7E16
- 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=969FD
- Page: https://openairdocs.org/aircraft/N969FD

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 N969FD.

## FAA accident and incident reports

None matched to N969FD.

## Service difficulty reports (115, 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 FDEA202608291251](https://openairdocs.org/sdr/FDEA202608291251), Aug 29, 2026: TRANSMISSION. TRIPPED. DURING APPROACH, RECEIVED A TE FLAP DISAGREE. RAN QRH & DECLARED AN EMERGENCY, LANDED UNEVENTFULLY. INSPECTED OVERLOAD INDS ON LT & RT, INBD & OTBD FLAPS & FOUN
- [SDR FDEA202604080409](https://openairdocs.org/sdr/FDEA202604080409), Apr 8, 2026: TRANSMISSION. FAILED. TE FLAP DISAGREE EICAS ALONG WITH TE FLAP FAILURE DESCENT TO MEMPHIS. RAN CHECKLIST, DROVE US FROM 9.1.17 TO 9.1.14, LANDED WITH FLAPS LESS THAN TOUCHDOWN 160KT
- [SDR FDEA202510172047](https://openairdocs.org/sdr/FDEA202510172047), Oct 17, 2025: SKIN. CRACKED. NUMBER 1 PYLON, WING ATTACH INBD UPPER LINK SHOWS BOLT NR 3, & 8 NOT SEATED. COMPLIED WITH EA T F 5730-T0385064, P1. CRACKED FASTENER HOLES IN SKIN AT NR 2 AND 
- [SDR FDEA202510172043](https://openairdocs.org/sdr/FDEA202510172043), Oct 17, 2025: SKIN. CORRODED. NUMBER 1 PYLON UPPER STRUCTURE, INSIDE OF ACCESS PANEL 433JR, SHOWS CORROSION. COMPLIED WITH EA T F -5430-T0385142 P 1. REPAIRED.
- [SDR FDEA202510091936](https://openairdocs.org/sdr/FDEA202510091936), Oct 9, 2025: SEAT TRACK. DAMAGED. MAIN DECK FIRST OFFICER SEAT TRACK (AFT/LH) SHOWS GROOVE ON SURFACE AND ELONGATE REMOVED/REPLACED MAIN DECK FIRST OFFICER SEAT TRACK (AFT/LH) IAW B757 SRM 51-40
- [SDR FDEA202510091935](https://openairdocs.org/sdr/FDEA202510091935), Oct 9, 2025: SEAT TRACK. DAMAGED. MAIN DECK PILOT AFT/RH SEAT TRACK SHOWS GOUGE ON SURFACE AND HOLES ELONGATE REMOVED & REPLACED MAIN DECK PILOT AFT/RH TRACK IAW B757 SRM 51-40-02-0G AND B757 AM
- [SDR FDEA202510091934](https://openairdocs.org/sdr/FDEA202510091934), Oct 9, 2025: SKIN. GOUGED. LOWER EXT FUSELAGE, FWD E/E DOOR HAS BENT AND GOUGES AT FWD EDGE REMOVED AND REPLACED OUTER SKIN FWD E/E DOOR IAW B757 SRM 51-40-02-0G, FEDEX EA F- 5240-T038509
- [SDR FDEA202509271837](https://openairdocs.org/sdr/FDEA202509271837), Sep 27, 2025: SEAT TRACK. CORRODED. MAIN DECK FLOOR SEAT TRACK BTW STA 345-375 LBL 5 CORRODED. REMOVED AND REPLACED SEAT TRACK LOCATED ON MAIN DECK FLOOR BTW STA 345 - STA375 LBL 5 IAW SRM 53-10-5
- [SDR FDEA202509271836](https://openairdocs.org/sdr/FDEA202509271836), Sep 27, 2025: SEAT TRACK. CORRODED. MAIN DECK FLOOR SEAT TRACK CORRODED BTW STA 345- STA 375 RBL 10. REMOVED AND REPLACED SEAT TRACK LOCATED ON MAIN DECK FLOOR BTW STA 345- STA 375 RBL 10 IAW B757
- [SDR FDEA202508201515](https://openairdocs.org/sdr/FDEA202508201515), Aug 20, 2025: JACKSCREW. OUT OF ADJUST. AFTER SELECTING FLAPS 20, RECEIVED TE FLAP DISAGREE EICAS MESS. FLAPS INDICATED BETWEEN 15 & 20. RAN TE FLAP DISAGREE QRH, DIRECTED TE ALTN FLAPS SWITCH TO BE S
- [SDR FDEA202503140412](https://openairdocs.org/sdr/FDEA202503140412), Mar 14, 2025: TRANSMISSION. TRIPPED. TE FLAP DISAGREE ON EICAS, ON APPROACH WHEN SELECTING FLAPS 1. RAN QRH. LANDED FLAPS 20 PER QRH. TROUBLESHOOT IAW ABOVE REFERENCES. AFTER INSPECTING ALL 8 FLAP 
- [SDR FDEA202311081844](https://openairdocs.org/sdr/FDEA202311081844), Nov 8, 2023: DOOR. CRACKED. R2 DOOR HAS DAMAGE ABOVE THE UPPER HINGE CUTOUT REPAIRED R2 DOOR, UPPER HINGE CUTOUT IAW B757 SRM 52-10-02-2R, FIGURE 201, REPAIR 1.
- [SDR FDEA202311011819](https://openairdocs.org/sdr/FDEA202311011819), Nov 1, 2023: SLAT. DENTED. LH WING UPPER SURFACE OF SLAT #3 T/E WEDGE HAS 1 DENT LOCATED 83" FROM I/B EDGE AND 4.5" FROM T/E REPAIRED 1EA DENT ON LH WING #3 SLAT T/E WEDGE UPPER SURFACE B
- [SDR FDEA202310311818](https://openairdocs.org/sdr/FDEA202310311818), Oct 31, 2023: CHANNEL. CRACKED. LMLG W/W CUTOUT AROUND THE BODY DOOR TANG SUB STRUCTUREAL CLIP IS CRACKED AT APPROX STA 1100 REMOVED AND REPLACED LMLG W/W CUTOUT, FWD STA 1100 CHANNEL IAW BAC 
- [SDR FDEA202306211068](https://openairdocs.org/sdr/FDEA202306211068), Jun 21, 2023: COLLAR. FAILED. MDIS 969 52-10 7499 21JUN23 MEM FACT U L1 DOOR HOLD OPEN LOCK BROKEN. REF 757 AMM 52-11-08-8, REMOVED AND REPLACED L1 DOOR HOLD OPEN LOCK COLLAR (P/N 10N6008-1)
- [SDR FDEA202306030988](https://openairdocs.org/sdr/FDEA202306030988), Jun 3, 2023: UNKNOWN. UNKNOWN. PDIS 969 25-60 7463 03JUN23 TYS OPEN U WHILE CLOSING R1 , ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT DID NOT ILLUMINATE. WITH SLIDE ARMING LEVER IN THE ARMED POSITI
- [SDR FDEA202305160872](https://openairdocs.org/sdr/FDEA202305160872), May 16, 2023: MODULE. FAILED. PASSING 8000 FEET, GOT R HYD QTY LOW WHICH TURNED INTO R HYD SYS PRESS. CONSULTED QRH, FOLLOWED PROCEDURE, DECLARED EMERGENCY AND LANDED SAFELY. ***EMERGENCY DE
- [SDR FDEA202201220277](https://openairdocs.org/sdr/FDEA202201220277), Jan 22, 2022: FLAP. CRACKED. RH WING INBD FLAP OUTBD SIDE UPPER SURFACE FOUND 1EA CRACKED REPAIRED RH WING INBD FLAP OUTBD SIDE UPPER SURFACE PER B757 SRM57-53-01-2R REPAIR 1 & SRM51-70-10-
- [SDR FDEA202201080267](https://openairdocs.org/sdr/FDEA202201080267), Jan 8, 2022: FLOORBEAM. CORRODED. MAIN DECK SECTION 41 CROSS BEAM FOUND CORROSION AT STA345 BL0.0-LBL9.0 REPAIRED THE MAIN DECK SECTION 41 STA345 BL0.0-LBL9.0 CORRODED CROSS BEAM PER B757 SRM53-
- [SDR FDEA202201050278](https://openairdocs.org/sdr/FDEA202201050278), Jan 5, 2022: FLAP. DELAMINATED. RH WING INBD FLAP TRAILING EDGE MID DELAMINATION REPAIRED RH WING INBD FLAP TRAILING EDGE MID SKIN PER B757 SRM57-53-01-2R REPAIR 1 & SRM51-70-10-2R REPAIR 4. T
- [SDR FDEA202002210369](https://openairdocs.org/sdr/FDEA202002210369), Feb 21, 2020: TEST SWITCH. INOPERATIVE. ALL EMERGENCY LIGHTS INOP ON PREFLIGHT R&R'D EMERGENCY LIGHT TEST SW. ( S10292) I.A.W. SWP MANUAL. OPS CHECK GOOD PER MM 33-51-00-5. CLEARED MEL.
- [SDR FDEA202001300243](https://openairdocs.org/sdr/FDEA202001300243), Jan 30, 2020: SKIN. DENTED. NUMEROUS DENTS LOCATED ON LEFT WING INBD MAIN FLAP UPPER SURFACE. REMOVED AND INSTALLED A NEW INBD MAIN FLAP LT SIDE IAW AMM 27-51-02-4, ACCOMPLISHED OPERATIONA
- [SDR FDEA2020013090235](https://openairdocs.org/sdr/FDEA2020013090235), Jan 29, 2020: SKIN. GOUGED. FUSELAGE SKIN AT STATION 215 LBL14. EXISTING REPAIR FOUND TO BE DAMAGED, AND WAS REMOVED AND REPLACED IAW E.A. F-5330-T0352079.
- [SDR FDEA2020012320199](https://openairdocs.org/sdr/FDEA2020012320199), Jan 22, 2020: SKIN. DENTED. FUSELAGE SKIN HAS A DENT B.S. 1560 BETWEEN S5R AND S6R ACCOMPLISHED FEDEX EA# F-5330-T0351978-P1 FUSELAGE - PLATES AND SKINS - STA 1558-1 1559, S5R 1559, S5R-6R
- [SDR FDEA2020012320197](https://openairdocs.org/sdr/FDEA2020012320197), Jan 22, 2020: BRACKET. CRACKED. NR 1 ENGINE PYLON SUB-STRUCTURE IS CRACKED ON THE OTBD SIDE AT THE TOP OF THE PYLON JUST FWD OF THE WING FWD SPAR. REMOVED AND REPLACED CRACKED BRACKET IAW DWG 
- [SDR FDEA2020010640020](https://openairdocs.org/sdr/FDEA2020010640020), Jan 4, 2020: LANYARD. TANGLED. RIGHT ENTRY DOOR (R1) ARM LIGHT (SLIDE LIGHT) DOES NOT ILLUMINATE WHEN DOOR ARMED. FOUND SLIDE LANYARD TANGLED UNTANGLED LANYARD AND STOWED OPS NORMAL REF MM 25
- [SDR FDEA201908211997](https://openairdocs.org/sdr/FDEA201908211997), Aug 21, 2019: RESERVOIR. LEAKING. EMERGENCY POWER RESERVO READING 0 PSI . REMOVED AND REPLACED R-1 EMERGENCY POWER RESERVOIR IAW 52-11-30-4
- [SDR FDE202011270001](https://openairdocs.org/sdr/FDE202011270001), Aug 20, 2019: SLIDE. INOPERATIVE. AFTER BLOCK-IN, R1 DOOR WAS POWER ASSISTED OPEN AND SLIDE FELL OUT, DID NOT DEPLOY. REMOVED & REPLACED R1 DOOR SLIDE/RAFT ASSEMBLY, PER B757 AMM 25-66-01-4 UP T
- [SDR FDEA201908201960](https://openairdocs.org/sdr/FDEA201908201960), Aug 20, 2019: SLIDE. DISLODGED. AFTER BLOCK-IN, R1 DOOR WAS POWER ASSISTED OPEN AND SLIDE FELL OUT, DID NOT DEPLOY REMOVED & REPLACED R1 DOOR SLIDE/RAFT ASSEMBLY PER B757 AMM 25-66-01-4 UP TO 
- [SDR FDEA201801230179](https://openairdocs.org/sdr/FDEA201801230179), Jan 23, 2018: SHEAR PLATE. CORRODED. MAIN UPPER CABIN, SEC 46 AT BS 1681 HAS AFT SHEAR DECK WITH SPOTS OF SURFACE CORROSION AND BARE METAL ON ENTIRE LENGTH OF UPPER STRUCTURE FROM LEFT TO RIGHT SID
- [SDR FDEA201801180115](https://openairdocs.org/sdr/FDEA201801180115), Jan 18, 2018: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, RIGHT AFT WING TO BODY BS 1240, STRINGER 25R. FABRICATED AND INSTALLED A NEW SUPPORT ANGLE IAW AMS2770, AND DWG 149N7740, SHT 2, REV A.
- [SDR FDEA201712273449](https://openairdocs.org/sdr/FDEA201712273449), Dec 27, 2017: ADC. FAILED. REJECTED TAKE-OFF AT 80KTS. NORMAL ACCELERATION TO 80 KNOTS, THEN CAPTAIN`S AIRSPEED INCREASED TO 450 KNOTS AND ALTITUDE INCREASED TO 50,000 FT. REMOVED AND REP
- [SDR FDEA201601060058](https://openairdocs.org/sdr/FDEA201601060058), Jan 6, 2016: SHEAR PLATE. CORRODED. MAIN CABIN FLOOR SHEAR PLATE HAS CORROSION AT STATION 395, LBL 50. REMOVED CORROSION AT FLOOR SHEAR PLATE ON STA 395 LBL 50 IAW B757 SRM 51-10-02-0G, FABRICATED
- [SDR FDEA201601060057](https://openairdocs.org/sdr/FDEA201601060057), Jan 6, 2016: SHEAR PLATE. CORRODED. MAIN CARGO FLOOR SHEAR PLATE HAS CORROSION AT STATION 403, LBL 16. REMOVED CORROSION AT FLOOR SHEAR PLATE ON STA 403 LBL IAW B757 SRM 51-10-02-0G, FABRICATE DOU
- [SDR FDEA201601060061](https://openairdocs.org/sdr/FDEA201601060061), Jan 6, 2016: SHEAR PLATE. CORRODED. MAIN CABIN FLOOR SHEAR PLATE HAS CORROSION AT BS 398, RBL 9. REPAIRED IAW EA F-5310- T0322562 P1.
- [SDR FDEA201601060060](https://openairdocs.org/sdr/FDEA201601060060), Jan 6, 2016: SHEAR PLATE. CORRODED. MAIN CABIN FLOOR, SHEAR PLATE HAS CORROSION AT BS 398, RBL 32. REPAIRED IAW EA F-5310-T0322563 P1.
- [SDR FDEA201601060059](https://openairdocs.org/sdr/FDEA201601060059), Jan 6, 2016: SHEAR PLATE. CORRODED. MAIN CABIN FLOOR, SHEAR PLATE HAS CORROSION, BS 423, LBL 50. REPAIRED IAW EA F-53-T032259 P1.
- [SDR FDEA201502140531](https://openairdocs.org/sdr/FDEA201502140531), Feb 14, 2015: COVER. LOOSE. L1 ENTRY DOOR HARD TO CLOSE. HANDLE DIFFICULT TO MOVE TO FULL CLOSED POSITION. FOUND L1 DOOR SLIDE RAFT COVER LOOSE. FOUND LOWER ATTACH POINT TO COVER DISCONNEC
- [SDR FDEA201407241935](https://openairdocs.org/sdr/FDEA201407241935), Jul 24, 2014: LIGHT. INOPERATIVE. R1 DOOR SLIDE LIGHT DOES NOT ILLUMINATE WHEN ARMED. RELAMPED SLIDE INDICATOR LIGHT ABOVE R1 DOOR IAW SMP. SLIDE LIGHT NOW ILLUMINATES WHEN R1 DOOR IS ARMED.
- [SDR FDEA201406241540](https://openairdocs.org/sdr/FDEA201406241540), Jun 24, 2014: LIGHT. INOPERATIVE. RIGHT FWD ENTRY DOOR ESCAPE SLIDE ARMED LIGHT INOPERATIVE AT BLOCK IN. RELAMPED RT FWD ENTRY DOOR LIGHT INDICATOR IAW SMP. OPERATIONS CHECKED GOOD. ACFT OK FOR 
- [SDR FDEA201402060280](https://openairdocs.org/sdr/FDEA201402060280), Feb 6, 2014: MECHANISM. DIRTY. R1 DOOR SLIDE WOULD NOT ARM. IDENTIFY L1 & R1 DOOR SLIDES INOPERABLE OR MISSING. NO JUMP SEATER`S OR ACM'S ARE TO OCCUPY COURIER AREA IN FLIGHT. TROUBLESHOT R1 
- [SDR FDEA201402060273](https://openairdocs.org/sdr/FDEA201402060273), Feb 6, 2014: MECHANISM. DIRTY. R1 DOOR SLIDE WOULD NOT ARM. IDENTIFY L1 & R1 DOOR SLIDES INOPERATIVE OR MISSING. NO JUMP SEATER`S OR ACM'S ARE TO OCCUPY COURIER AREA IN FLIGHT. TROUBLESHOT R1
- [SDR FDEA201312283058](https://openairdocs.org/sdr/FDEA201312283058), Dec 28, 2013: STRUCTURE. CORRODED. BS 962 - 978, RBL 50 - 65 CENTER FUEL TANK UPPER SKIN FOUND CORRODED. REPAIRED IAW EA F-5730 T0 303250A PART 1.
- [SDR FDEA201312283061](https://openairdocs.org/sdr/FDEA201312283061), Dec 28, 2013: SKIN PANEL. CORRODED. CABIN STATION 980 - STATION 998, LBL 50 - LBL 65, CTR FUEL TANK TOP PANEL UPPER SURFACE FOUND CORROSION. REPAIRED IAW EA F-5730 T0 303250A PART 1. CORROSION FOU
- [SDR FDEA201312283060](https://openairdocs.org/sdr/FDEA201312283060), Dec 28, 2013: SKIN PANEL. CORRODED. CABIN STATION 1000, LBL 55, CTR FUEL TANK TOP PANEL UPPER SURFACE FOUND CORROSION. REPAIRED IAW EA F-5730 T0 303250A PART 1. CORROSION FOUND ON LT & RT SIDE CTR
- [SDR FDEA201312283059](https://openairdocs.org/sdr/FDEA201312283059), Dec 28, 2013: SKIN PANEL. CORRODED. CABIN STATION 1006, LBL 60, CTR FUEL TANK TOP PANEL UPPER SURFACE FOUND CORROSION. REPAIRED EA F-5730 T0 303250A PART 1. CORROSION FOUND ON LT & RT SIDE CTR WIN
- [SDR FDEA201312283057](https://openairdocs.org/sdr/FDEA201312283057), Dec 28, 2013: SKIN PANEL. CORRODED. CABIN STATION 1022 - STATION 1040, LBL 50 - LBL 60, CTR FUEL TANK TOP PANEL UPPER SURFACE FOUND CORROSION. REPAIRED IAW EA F-5730 T0 303250A PART 1. CORROSION F
- [SDR FDEA201312283056](https://openairdocs.org/sdr/FDEA201312283056), Dec 28, 2013: SKIN PANEL. CORRODED. CABIN STATION 980, RBL 60 CTR FUEL TANK UPPER SKIN PANEL FOUND CORROSION. REPAIRED IAW EA F-5730 T0 303250A PART 1. CORROSION FOUND ON LT & RT SIDE CTR WING TAN
- [SDR FDEA201312283055](https://openairdocs.org/sdr/FDEA201312283055), Dec 28, 2013: SKIN PANEL. CORRODED. CABIN STATION 990 - STATION 998, RBL 54, CTR FUEL TANK UPPER SKIN PANEL FOUND CORROSION. REPAIR CARRIED OUT IAW EA F-5730 T0 303250A PART 1. CORROSION FOUND ON 
- [SDR FDEA201312283054](https://openairdocs.org/sdr/FDEA201312283054), Dec 28, 2013: SKIN PANEL. CORRODED. CABIN STATION 1020 - 1040, RBL 53 - 60 CTR FUEL TANK UPPER SKIN PANEL FOUND CORROSION. REPAIR CARRIED OUT IAW EA F-5730 T0 303250A PART 1. CORROSION FOUND ON LT

All 115: https://openairdocs.org/aircraft/N969FD/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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