# N974FD: 1993 Boeing 757-2Y0

- Status: Valid registration
- Airframe: [Boeing 757-2Y0](https://openairdocs.org/model/boeing-757-2y0) (registry code 138492A, 178 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: 26158
- Year built: 1993
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 31, 2013
- Certificate issued: December 12, 2012
- Expires: December 31, 2028
- Mode S code: AD9302
- 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=974FD
- Page: https://openairdocs.org/aircraft/N974FD

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 757-2Y0)

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 N974FD.

## FAA accident and incident reports

None matched to N974FD.

## Service difficulty reports (111, 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 FDEA202306281120](https://openairdocs.org/sdr/FDEA202306281120), Jun 28, 2023: HOSE. DAMAGED. LEFT HYD SYS PRESS FOLLOWED BY L HYD QTY WHEN LANDING GEAR WAS EXTENDED ON FINAL. EXECUTED GO AROUND TO RUN QRH AND CAME BACK AND LANDED UNEVENTFUL. EMERGENCY D
- [SDR FDEA202306171048](https://openairdocs.org/sdr/FDEA202306171048), Jun 17, 2023: UNKNOWN. UNKNOWN. DURING FLAP EXTENSION ON APPROACH, TRAILING EDGE FLAP DISAGREE EICAS MESSAGE WHEN FLAPS SELECTED FROM UP TO 1. COMPLIED WITH QRH, F20 LANDING, AND EMERGENCY WAS
- [SDR FDEA202304120630](https://openairdocs.org/sdr/FDEA202304120630), Apr 12, 2023: UNKNOWN. UNKNOWN. PDIS 974 27-50 9266 12APR23 MEM FACT U ON APPROACH AT FLAP EXTENSION TO FLAPS 1, RECEIVED A TE FLAP DISAGREE. DISCONTINUED APPROACH. COMPLIED WITH THE QRH, DECL
- [SDR FDEA202211302859](https://openairdocs.org/sdr/FDEA202211302859), Nov 30, 2022: UNKNOWN. ODOR. EXTREMELY STRONG ELECTRICALLY BURNING ODOR IN COCKPIT, DURING CLIMB AROUND 25,000 FT. ON ENTRY NO ODOR PRESENT.. CHECKED FOR CBS TRIPPED IN COCKPIT, ALL CLOSED.
- [SDR FDEA202206161435](https://openairdocs.org/sdr/FDEA202206161435), Jun 16, 2022: HANDLE. UNSECURE. COPILOT S WINDOW HANDLE ROTATES OPEN DURING FLIGHT. THE FRONT LATCH STAYS LATCHED, BUT THE HANDLE ROTATES OPEN (HAS TO BE HELD SECURE) AND THE ALIGNMENT ARROWS 
- [SDR FDEA202203120512](https://openairdocs.org/sdr/FDEA202203120512), Mar 12, 2022: NONE. NONE. RAMP REPORTED L1 DOOR UNABLE TO BE OPEN FROM OUTSIDE. WHEN IT IS CLOSED WITH OUTSIDE HANDLE, INSIDE HANDLE DO NOT FOLLOW TO COMPLETE CLOSED POSITION. THE INSIDE
- [SDR FDEA202110092503](https://openairdocs.org/sdr/FDEA202110092503), Oct 9, 2021: FLAP SYSTEM. FAULTED. TE FLAP DISAGREE ON APPROACH. RAN QRH. DECLARED EMERGENCY. LANDED. REPEAT WRITE UP. INTERROGATED FSEU, #1 SHOWS FAULT 305: FLAP ISOL VLV. T/S CONTINUE DURING IN
- [SDR FDEA202110092501](https://openairdocs.org/sdr/FDEA202110092501), Oct 9, 2021: UNKNOWN. FAULTED. TE FLAPS EICAS WHEN SELECTING FLAPS 1 FOR APPROACH. DUE TO QRH AND CHECKLIST DEMANDS, OPTED TO DISCONTINUE APPROACH. COORDINATED A HOLDING PATTERN AND RAN THE Q
- [SDR FDEA202102180399](https://openairdocs.org/sdr/FDEA202102180399), Feb 18, 2021: BATTERY PACK. INOPERATIVE. MDIS 974 33-50 7299 18FEB21 MUC OPEN U SEE ALSO 33-50 WRI 7298: EMRGENCY LIGHTS IN CABIN MID AND RIGHT AND RIGHT EXTERIOR DOES NOT ILLUMINATE IN ALL POSITIONS. 
- [SDR FDEA202102180398](https://openairdocs.org/sdr/FDEA202102180398), Feb 18, 2021: BATTERY PACK. MISINSTALLED. MDIS 974 33-50 7298 18FEB21 MUC OPEN U AFTER AIRCRAFT POWER OFF FOUND EMERGENCY LIGHT IN COCKPIT LEFT SIDE ABOVE DOOR AND LEFT EXTERIOR LIGHT ILLUMINATED. WITH 
- [SDR FDEA2020031210534](https://openairdocs.org/sdr/FDEA2020031210534), Mar 11, 2020: COLLAR. BROKEN. L1 DOOR HOLD OPEN LOCK COLLAR BROKEN. REMOVED PANEL 221AL TO GET ACCESS TO COLLAR AS PER MM 52-11-08-4. INSTALLED COLLAR AND CATCH ASSY AS PER AMM 52-11-08-8. O
- [SDR FDEA201912063197](https://openairdocs.org/sdr/FDEA201912063197), Dec 6, 2019: POWER SUPPLY. INOPERATIVE. LT PASSENGER DOOR EXTERNAL EMERGENCY LIGHT L25 INOP. POWER SUPPLY M731 REPLACED.
- [SDR FDEA201909102200](https://openairdocs.org/sdr/FDEA201909102200), Sep 10, 2019: SHUTOFF VALVE. INOPERATIVE. PDIS 974 36-10 5902 10SEP19 CDG OPEN U LOGPAGES:3010680 REJECTED TAKEOFF FOR " L ENG BLEED OFF " AFTER ENGINE REDUCED IDLE EICAS MESSAGE REMOVED. GOT EICAS MESS
- [SDR FDEA2019083092040](https://openairdocs.org/sdr/FDEA2019083092040), Aug 29, 2019: SKIN. DELAMINATED. RH I/B FLAP, LOWER SURFACE REPAIR 52" FORM O/B EDGE AND 13" FORM T/E. REPAIR FOUND TO BE UNSERVICABLE PLEASE PERFORM REPAIR IAW SRM 57-53-01-0I IDENT 1, SRM 57-
- [SDR FDEA2019082191948](https://openairdocs.org/sdr/FDEA2019082191948), Aug 19, 2019: PANEL. CORRODED. NR 2 ENG I/B C-DUCT UPPER BIFURICATION PANEL DAMAGE UPPER BIFURICATION UPPER TRACK BEAM SUPPORT PANEL EVALUATED AND FOUND TO BE CORROSION. CORROSION OUT OF LIMI
- [SDR FDEA2019082191940](https://openairdocs.org/sdr/FDEA2019082191940), Aug 19, 2019: SKIN. DAMAGED. UPON EVALUATION OF AGING AIRCRAFT INSPECTION OF EXISTING DOUBLER AND TRIPLER REPAIR @ BSTA 620-624, STR21R - STR24R DAMAGED FASTENER HOLE FOUND ON INTERNAL SKIN
- [SDR FDEA2019082181930](https://openairdocs.org/sdr/FDEA2019082181930), Aug 18, 2019: NOZZLE. CRACKED. NR 1 ENGINE CNA HAS CRACKS AT THE 3 O'CLOCK AND 9 O'CLOCK POSITIONS. CRACKS REMOVED IAW EM 78-11-04 AND CRACKS REPAIR IAW E.A. F-7810-T0348465.
- [SDR FDEA2019082181931](https://openairdocs.org/sdr/FDEA2019082181931), Aug 18, 2019: PANEL. CRACKED. SLAT #6 IN/B T/E SKIRT (FLEX PANEL) IS CRACKED. REPAIRED CRACK IAW SRM 51-70-17 GENERAL & E.A. F-5750-T0348677
- [SDR FDEA2019081541877](https://openairdocs.org/sdr/FDEA2019081541877), Aug 14, 2019: SKIN. DENTED. DENT OUTSIDE PERMITTED LIMITS IAW SRM 53-00-01 ALLOWABLE DAMAGE FIG101 DETAIL III @ B/S 580-597 STR 25L REAPIRED DENT IAW FEDEX EA# F-5300-T0348400 (P1) AND SRM
- [SDR FDEA2019081531854](https://openairdocs.org/sdr/FDEA2019081531854), Aug 13, 2019: STRINGER CLIP. CRACKED. STRINGER CLIP ' B/S 1500 STR2 WAS FOUND DAMAGED AND CRACKED . REPLACED STRINGER CLIP IAW SRM 51-40-02
- [SDR FDEA201908121843](https://openairdocs.org/sdr/FDEA201908121843), Aug 12, 2019: SEAT TRACK. CORRODED. SEAT TRACK B/S 364 RBL 47-51 CORRODED BEYOND PERMITTED LIMITS. REPAIRED IAW FEDEX EA F-5310-T0348507(P1).
- [SDR FDEA201908071844](https://openairdocs.org/sdr/FDEA201908071844), Aug 7, 2019: FLOOR SUPPORT. NONE. EXISTING REPAIR FOUND ON FLOOR SUPPORT STRUCTURE BS 570 APPROX. LBL 10. REPAIR REQUIRES EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE
- [SDR FDEA2019080211788](https://openairdocs.org/sdr/FDEA2019080211788), Aug 1, 2019: STRAP. CRACKED. STRAP CRACKED FWD GALLEY FLOOR BS 367 ,LBL 24 FABRICATED NEW STRAP AND REPLACED OLD PART IAW EA F-5310-T034848 PART 1, SRM 53-00-5-2R, REPAIR 13, AND GMM. 7-0-1
- [SDR FDEA2019080211787](https://openairdocs.org/sdr/FDEA2019080211787), Aug 1, 2019: FLOOR PANEL. DELAMINATED. FLOOR PANEL DAMAGED @ DOORWAY #1R OUTSIDE PERMITTED LIMITS IAW SRM53-00-50-1A REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R
- [SDR FDEA2019080211786](https://openairdocs.org/sdr/FDEA2019080211786), Aug 1, 2019: FLOOR PANEL. DELAMINATED. FLOORBOARD @ 1L DOORWAY DAMAGED OUTSIDE PERMITTED LIMITS IAW SRM 53-00-50-1A. REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R
- [SDR FDEA201907281732](https://openairdocs.org/sdr/FDEA201907281732), Jul 28, 2019: SEAT TRACK. CORRODED. SEAT TRACK HAS EVIDENCE OF CORROSION @ B/S-344-356 AND 367-374. REMOVED SEAT TRACK SECTION IAW SRM 51-40-02. REMOVED CORROSION FROM SEAT TRACK SECTION AND FOUND
- [SDR FDEA201907081504](https://openairdocs.org/sdr/FDEA201907081504), Jul 8, 2019: WARNING SYSTEM. FALSE ACTIVATION. PDIS 974 27-50 5786 08JUL19 TLV OPEN U LOGPAGES:3010096 TE FLAP ASYM INDICATED WHEN FLAPS SELECTED TO "1". FOLLOWED QRH PROCEDURES TO LANDING. TOUCHDOWN SPEED W
- [SDR FDEA201902030253](https://openairdocs.org/sdr/FDEA201902030253), Feb 3, 2019: BULB. INOPERATIVE. EMERGENCY SLIDE LIGHT L1 NO LIGHT FACT 03FEB19 11:23 CPH EMERGENCY SLIDE LIGHT L1 BULP REPLACED AMM 33-51-06-2-1 REV 123.4 BULP P/N 767 LIGHT TEST PERFORMED NO 
- [SDR FDEA201707242026](https://openairdocs.org/sdr/FDEA201707242026), Jul 24, 2017: SKIN. DELAMINATED. COMPOSITE DISBOND TOP OF LEFT OUTBOARD AFT FLAP. REPAIRED AREA AT TOP OF LEFT OTBD AFT FLAP IAW SRM 57-53-01-2R, FIG 201, TABLE II, AND SRM 51-70-04, PAR 5.A.1.
- [SDR FDEA201704181229](https://openairdocs.org/sdr/FDEA201704181229), Apr 18, 2017: BATTERY PACK. DISCHARGED. FOUND ON PREDEPARTURE CHECK, 2 EA EMERGENCY EXIT SIGNS AND RT EXTERIOR LIGHT NOT TESTING. REMOVED AND REPLACED M730 POWER SUPPLY BATTERY PACK PER AMM 33-51-07-2
- [SDR FDEA201704101135](https://openairdocs.org/sdr/FDEA201704101135), Apr 10, 2017: PIN. MISSING. R1 DOOR SLIDE SAFTEY PIN MISSING. REPLACED MISSING SAFETY PIN AT R1 DOOR ESCAPE SLIDE POUCH IAW MM 52-11-02-4.
- [SDR FDEA201704101134](https://openairdocs.org/sdr/FDEA201704101134), Apr 10, 2017: PIN. MISSING. L1 DOOR SLIDE SAFTEY PIN MISSING. REPLACED MISSING SAFETY PIN AT L1 DOOR ESCAPE SLIDE POUCH REF: 757 M.M. 52-11-02-4
- [SDR FDEA201608313087](https://openairdocs.org/sdr/FDEA201608313087), Aug 31, 2016: SKIN. DAMAGED. RUDDER HAS HAIL DAMAGE. ACCOMPLISHED 3 EA REPAIRS ON RUDDER LT SIDE IAW SRM 55-40-01-2R, 51-70-04-0G AND EA F05540-T0328008, P1 TRACKING REPAIRS.
- [SDR FDEA201608303070](https://openairdocs.org/sdr/FDEA201608303070), Aug 30, 2016: SKIN. DENTED. DENTS IN MAIN CARGO DOOR SKIN. EVALUATED AND MEASURED DENTS, 224, MAIN CARGO DOOR SKIN, HFEC AND DVI INPSECTIONS CW, NO ADDITIONAL DEFECTS NOTED. DENTS, 195, FO
- [SDR FDEA201601210274](https://openairdocs.org/sdr/FDEA201601210274), Jan 21, 2016: PROXIMITY SENSOR. FAILED. SLIDE LIGHT IN DOOR R1 FAILS TO ILLUMINATE WITH DOOR ARMED. R1 ESCAPE SLIDE ARMED INDICATOR LIGHTS INOPERATIVE. REMOVED AND REPLACED R1 DOOR AFT SLIDE PROXIMITY
- [SDR FDEA201507252390](https://openairdocs.org/sdr/FDEA201507252390), Jul 25, 2015: DECK PLATE. CORRODED. BS 415, LBL 54 DECK PLATE HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. FABRICATED DOUBLER REPAIR & INSTALLATION IAW SRM 757-200 RIGID CARGO BARRIER SECTIO
- [SDR FDEA201505311668](https://openairdocs.org/sdr/FDEA201505311668), May 31, 2015: LANYARD. OUT OF POSITION. RIGHT SIDE ENTRY DOOR WOULD NOT ARM. FOUND GIRT BAR ARMING LANYARD WRAPPED AROUND GIRT BAR. R1 DOOR SLIDES INOPERATIVE OR MISSING. NO JUMP SEATERS OR ACM'S ARE 
- [SDR FDEA201501150184](https://openairdocs.org/sdr/FDEA201501150184), Jan 15, 2015: GIRT BAR. OBSTRUCTED. UPON LANDING, DOOR ARM LIGHT DOOR 1R WAS NOT ILLUMINATED. RELAMPED, NO HELP. FOUND SOME DEBRIS AT GIRT BAR AFT HOOK. REMOVED DEBRIS, LIGHT NOW OPERATES WHEN DOO
- [SDR FDEA201501060025](https://openairdocs.org/sdr/FDEA201501060025), Jan 6, 2015: GIRT BAR. OUT OF POSITION. ON BLOCK OUT R2 DOOR WOULD NOT ARM & ARM LIGHT WOULD NOT LIGHT. FOUND ESCAPE SLIDE GIRT BAR FELL OUT OF PLACE & WAS ABLE TO PLACE BACK IN PLACE. TESTED IAW MM 5
- [SDR FDEA201408142176](https://openairdocs.org/sdr/FDEA201408142176), Aug 14, 2014: LANYARD. OUT OF POSITION. RIGHT FWD ENTRY DOOR WILL NOT ARM DOOR SLIDES INOPERATIVE. NO JUMPSEATERS OR ACM'S ARE TO OCCUPY COURIER AREA IN FLIGHT. FOUND CORD OF SLIDE TANGLED IN BAR. NO 
- [SDR FDEA201312102952](https://openairdocs.org/sdr/FDEA201312102952), Dec 10, 2013: SLIDE RAFT. DEPLOYED. L1 MAIN CABIN EXIT SLIDE DEPLOYED. RELEASED FOR SERVICE IAW MEL 52-11-01-A CATEGORY B EXPIRATION 10DEC13 MEL 52-11-01-A L1 DOOR SLIDE MISSING IDENTIFY INOPERATI
- [SDR FDEA201308161926](https://openairdocs.org/sdr/FDEA201308161926), Aug 16, 2013: LAMP. BURNED OUT. EMERGENCY LIGHTS R1 DOOR EXTERIOR SLIDE INOPERATIVE. REPLACED LAMPS, OPS NORMAL, IAW AMM 33-51-06-2-1. OK FOR SERVICE.
- [SDR FDEA201307221620](https://openairdocs.org/sdr/FDEA201307221620), Jul 22, 2013: FLOORBEAM. CORRODED. CABIN FLOORBEAM BS 1640 RBL 24 CORRODED. R & R WITH FLOORBEAM FABRICATED IAW DWG 146N5136, SHT 1 REV - AND INSTALLED IAW DWG 146N5089, SHT 6, REV. MAJOR REPAIR.
- [SDR FDEA201307221613](https://openairdocs.org/sdr/FDEA201307221613), Jul 22, 2013: TEE FITTING. CRACKED. LOWER FUSELAGE BS 900 - 1037, LBL 60 WING TO BODY FAIRING SUPPORT TEE CRACKED AT AFT INBD CORNER. REPAIRED IAW EA F-5310-167523 PART 1.
- [SDR FDEA201307191587](https://openairdocs.org/sdr/FDEA201307191587), Jul 19, 2013: PANEL. CORRODED. RIGHT WING INBD T/E MAIN FLAP UPPER PANEL FOUND CORRODED AT MAIN FLAP STA 92.5, FRONT SPAR UPPER AREA. REPAIRED IAW EA F-5750-167524, PART 1. REPAIR IS MAJOR.
- [SDR FDEA201307191586](https://openairdocs.org/sdr/FDEA201307191586), Jul 19, 2013: PANEL. CORRODED. RT WING INBD T/E MAIN FLAP UPPER PANEL FOUND CORRODED AT MAIN FLAP STA 81.0 FRONT SPAR UPPER AREA. REPAIRED IAW EA F-5750-167524, PART 1. MAJOR REPAIR.
- [SDR FDEA201307071489](https://openairdocs.org/sdr/FDEA201307071489), Jul 7, 2013: WEB. CORRODED. R4 DOOR INTERNAL DOOR HANDLE MECHANISM CUTOUT FWD INTERCOSTAL FWD SIDE FOUND CORRODED. REMOVED AND REPLACED, FABRICATED AND INSTALLED IAW DWG 146N6100 SHT.3, RE
- [SDR FDEA201307071487](https://openairdocs.org/sdr/FDEA201307071487), Jul 7, 2013: WEB. CORRODED. R4 DOOR INTERNAL DOOR-MOUNTED WINDOW CUTOUT FWD WEB FWD SIDE HAD MINOR CORROSION. REMOVED AND REPLACED FABRICATED AND INSTALLED IAW DWG 146N6100 SHT.3, REV.H. R
- [SDR FDEA201307011434](https://openairdocs.org/sdr/FDEA201307011434), Jul 1, 2013: CREASE BEAM. CORRODED. BS 1000 -1010 RT CREASE BEAM INBD ANGLE FOUND CORRODED AROUND FASTENER HOLES. REPAIRED.
- [SDR FDEA201307011433](https://openairdocs.org/sdr/FDEA201307011433), Jul 1, 2013: CREASE BEAM. CORRODED. BS 960-980 RT CREASE BEAM INBD ANGLE FOUND CORRODED AROUND THREE FASTENERS HOLES. REPAIRED IAW REPAIR DWG LOR5L53017 SHT 3, REV A. REPAIR IS MAJOR.

All 111: https://openairdocs.org/aircraft/N974FD/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 757-2Y0 aircraft: https://openairdocs.org/model/boeing-757-2y0/aircraft.md
- The Rolls-Royce RB211-535E4 series engine: https://openairdocs.org/engine/rolls-royce-rb211-535e4-series.md

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