# N921FD: 1991 Boeing 757-23A

- Status: Valid registration
- Airframe: [Boeing 757-23A](https://openairdocs.org/model/boeing-757-23a) (registry code 1384967, 178 seats)
- Engine: [Rolls-Royce RB211-535E437](https://openairdocs.org/engine/rolls-royce-rb211-535e437) (registry code 54053)
- Data sheets: [TCDS A2NM](https://openairdocs.org/tcds/A2NM) (The Boeing Company), [TCDS E12EU](https://openairdocs.org/tcds/E12EU) (Rolls-Royce Deutschland Ltd & Co KG) (OpenAirDocs)
- Serial number: 24924
- Year built: 1991
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 24, 2009
- Certificate issued: July 15, 2009
- Expires: November 30, 2027
- Mode S code: ACC262
- 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=921FD
- Page: https://openairdocs.org/aircraft/N921FD

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.

## ADs that may apply (OpenAirDocs): 19 in force

### Matched by airframe (Boeing 757-23A)

None in force.

### Matched by engine (Rolls-Royce RB211-535E437)

- [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 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 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 N921FD.

## FAA accident and incident reports

None matched to N921FD.

## Service difficulty reports (121, 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 FDEA202507221293](https://openairdocs.org/sdr/FDEA202507221293), Jul 22, 2025: SOCKET. LOOSE. PARKING BRAKE DISCRETE LIGHT DOES NOT ILLUMINATE WHEN PARKING BRAKE SET FOUND PARKING BRAKE LIGHT BASE ASSY LOOSE, TIGHTEN BASE. LIGHT OPS CKED GOOD. A/C OK FOR
- [SDR FDEA202507191267](https://openairdocs.org/sdr/FDEA202507191267), Jul 19, 2025: SKIN. DAMAGED. WHILE PERFORMING INSPECTION ON THE #2 CARGO DOOR LWR CORNERS SKIN CUTOUT FWD AND AFT, FOUND A REPAIR ON THE AFT LOWER CORNER OF THE #2 CARGO DOOR AREA. AD2006-1
- [SDR FDEA202507141192](https://openairdocs.org/sdr/FDEA202507141192), Jul 14, 2025: FLOORBEAM. CORRODED. MCD STA 1640 SUPPORT BEAM BL 0.00 TO LBL 45.50 HAS CORROSION. REMOVED CORROSION AT STA 1640 SUPPORT BEAM BL 0.00 - LBL 45050 IAW SRM 51-10-02. FOUND OUT OF LIMI
- [SDR FDEA202507141191](https://openairdocs.org/sdr/FDEA202507141191), Jul 14, 2025: CREASE BEAM. CORRODED. CORROSION NOTED ON THE ATTACHMENT FRAME OF MAIN DECK FLOORBOARD # 252 MKF (RH MOST O/B) AT STA 1540 - 1620. REPAIRED FRAME ATTACHMENT (CREASE BEAM) AT MAIN CABI
- [SDR FDEA202507111182](https://openairdocs.org/sdr/FDEA202507111182), Jul 11, 2025: SEAT TRACK. CORRODED. CORROSION NOTED ON THE SEAT TRACK BASE AT LH STA 1200-1240 I/B OF FLOOR PNL 251 MCF. REMOVED AND REPLACED SEAT TRACK AT L/H STA 1180 TO 1240 LBL 45.50 IAW SRM 5
- [SDR FDEA202504040573](https://openairdocs.org/sdr/FDEA202504040573), Apr 4, 2025: MODULE. FAULTED. DURING FIRE/OVHT TEST MASTER WARNING, MASTER CAUTION LIGHTS DID NOT ILLUMINATE. REMOVED AND REPLACED MASTER WARNING MODULE (M618) REF AMM 31-51-04-4 OPS TEST GO
- [SDR FDEA202405250726](https://openairdocs.org/sdr/FDEA202405250726), May 25, 2024: CONTROLLER. FAILED. AT FL400 CABIN ALT HIGH WARNING DONNED MASKS. RAN QRH. INITIATED EMERGENCY DESCENT. CABIN ALTITUDE RATE REACHED 2000 FT PER MIN DOWN AND HIGHEST ALTITUDE REACHE
- [SDR FDEA202304240748](https://openairdocs.org/sdr/FDEA202304240748), Apr 24, 2023: CAM. FAILED. ON APPROACH, GOT LT FWD ENTRY DOOR EICAS. AFTER SHUTDOWN, DOOR HANDLE HAD RAISED APPROX 4 INCHES, SLIGHTLY ABOVE DOOR ARMED KNUCKLE BUSTER. DOOR HANDLE CONFIRME
- [SDR FDEA202304200725](https://openairdocs.org/sdr/FDEA202304200725), Apr 20, 2023: ROLLER. MISALIGNED. PDIS 921 52-10 0900 20APR23 FAT FACT U L FWD ENTRY DOOR EICAS CAME ON DURING DEPARTURE PASSING APPROX 3000 . RAN QRH AND CONTINUED NORMAL OPS AS PRESSURIZATION 
- [SDR FDEA202210212637](https://openairdocs.org/sdr/FDEA202210212637), Oct 21, 2022: LAMP. BURNED OUT. L1 DOOR INTERIOR EXIT LIGHTS 3/4 OF LIGHTS BURNED OUT. REMOVED AND REPLACED L1 DOOR INTERIOR EXIT LIGHT SIGN IAW AMM 33-51-01-2. LIGHT OPS CHECKS NORMAL. ACFT O
- [SDR FDEA202206251551](https://openairdocs.org/sdr/FDEA202206251551), Jun 25, 2022: OIL SYSTEM. LOW PRESSURE. LEFT ENGINE OIL QUANTITY DECREASED TO 0 ON TAKEOFF, PRESSURE DECREASED TO 0 AS WELL. L ENG OIL PRESS EICAS MESSAGE ILLUMINATED. RAN QRH AND SHUT DOWN LEFT ENGIN
- [SDR FDEA202108262107](https://openairdocs.org/sdr/FDEA202108262107), Aug 26, 2021: HANDLE. UNSECURE. DURING A TEST FLIGHT, LT ENTRU DOOR EICAS MSG, IMMEDIATELY AFTER TAKEOFF. HANDLE HAD POPPED UP APPROX 6 INCHES AND WOULD NOT LOCK BACK DOWN. NO ABNORMAL PRESSUR
- [SDR FDEA202108232075](https://openairdocs.org/sdr/FDEA202108232075), Aug 23, 2021: HANDLE. UNSECURE. TEST FLIGHT- L FWD ENT DOOR EICAS OCCURRED IN THE APPROACH PATTERN. THE DOOR HANDLE HAD POPPED UP APPROX 6 IN. FROM FULL LOCKED POSITION. COULD MOVE HANDLE DOWN
- [SDR FDEA202108232074](https://openairdocs.org/sdr/FDEA202108232074), Aug 23, 2021: RAM AIR TURB. FAILED. TEST FLIGHT- RAT WOULD NOT DEPLOY WITH BOTH SPEED CAD C/B PULLED. REMOVED AND REPLACED LEFT AND RIGHT ENG SPEED CARDS IAW AMM 77-12-03-4, PERFORMED RAT AUTO DRO
- [SDR FDEA202108192042](https://openairdocs.org/sdr/FDEA202108192042), Aug 19, 2021: FRAME. CRACKED. L/H SIDE FR 1640 S-14 WEB FRAME. BOTH BOTTOM INBD AND OUTBD HOLES HAVE CRACK INDICATIONS. CLOCK POSITION FOR BOTH HOLES ARE 9 AND 3:00 O'CLOCK. ACCOMPLISHED FIN
- [SDR FDEA202108102000](https://openairdocs.org/sdr/FDEA202108102000), Aug 10, 2021: FLOOR PANEL. CRACKED. MAIN DECK FLOOR PANEL 251MWF HAS CRACK (ADAJACENT L4 DOOR) DOT 136-51 FABRICATED MAIN DECK PANEL 251MWF ON VTMAE TRAVELER # T21/1565104 IAW DWG SRZ-25- 005 REVI
- [SDR FDEA202108101999](https://openairdocs.org/sdr/FDEA202108101999), Aug 10, 2021: FLOOR PANEL. CRACKED. MAIN DECK FLOOR PANEL 251MVF HAS CRACK (ADJACENT R4 DOOR). DOT 136-58 FABRICATED MAIN DECK FLOOR PANEL 251MVF ON VTMAE TRAVELER # T21/1565102 IAW DWG SRZ-25-005
- [SDR FDEA202105281418](https://openairdocs.org/sdr/FDEA202105281418), May 28, 2021: CONTROLLER. MALFUNCTIONED. DURING CLIMB COCKPIT TEMP BECAME EXCESSIVELY HOT. RAN QRH AND AFTER TRIM AIR SWITCH TURNED OFF REGAINED TEMP CONTROL. PERFORMED BITE TEST ON CABIN ZONE TEMP CON
- [SDR FDEA202012163169](https://openairdocs.org/sdr/FDEA202012163169), Dec 16, 2020: HANDLE. MALFUNCTIONED. LEFT MAIN DOOR ARM HANDLE WILL NOT MOVE, REF FIM 52-11 TREE 802. INSPECTED DOOR LATCHING MECHANISMS FOR DEFECTS OR OBSTRUCTIONS WITH NONE FOUND. ALSO, OPERATED 
- [SDR FDEA202009232318](https://openairdocs.org/sdr/FDEA202009232318), Sep 23, 2020: LANDING GEAR. FAILED. PDIS 921 32-51 8989 23SEP20 IND OPEN U. AIRCRAFT STILL PULLS HARD TO THE RIGHT. IT TAKES ALMOST 1/2 RUDDER DEFLECTION TO TRACK STRAIGHT. ALSO IT TAKES CONSIDERA
- [SDR FDEA2019120973208](https://openairdocs.org/sdr/FDEA2019120973208), Dec 7, 2019: BULB. INOPERATIVE. SVC CK R-1 DOOR EMERGENCY ESCAPE SLIDE LIGHT INOP. RELAMPED R ESCAPE SLIDE LIGHT REF AMM 33-51-06-2-1, BULB GE767. OP'S NORMAL OK FOR SERVICE
- [SDR FDEA2019112202998](https://openairdocs.org/sdr/FDEA2019112202998), Nov 20, 2019: OUTFLOW VALVE. INOPERATIVE. PDIS 921 21-30 8717 20NOV19 MEM FACT U LOGPAGES:3170064 SAME PROBLEM AS YESTERDAY WITH PRESSURIZATION EXCEPT AUTO 1, AUTO 2 AND MANUAL CONTROL WORKED. HOWEVER T
- [SDR FDEA201911192993](https://openairdocs.org/sdr/FDEA201911192993), Nov 19, 2019: OUTFLOW VALVE. FAILED. PDIS 921 21-30 8714 19NOV19 MCI OPEN U LOGPAGES:3170061 CABIN AUTOMATIC INOP. UNABLE TO MAINTAIN CABIN ALT IN MANUAL WITH VALVE FULLY CLOSED. REPLACED CABIN PRE
- [SDR FDEA201911192997](https://openairdocs.org/sdr/FDEA201911192997), Nov 19, 2019: CONTROLLER. FAILED. CABIN AUTOMATIC INOP. UNABLE TO MAINTAIN CABIN ALT IN MANUAL WITH VALVE FULLY CLOSED. REPLACED CABIN PRESSURE OUTFLOW VALVE AND TESTED PER AMM 21-31-03-2, OPS C
- [SDR FDEA2019111522934](https://openairdocs.org/sdr/FDEA2019111522934), Nov 12, 2019: BATTERY. SMOKE. STRONG BURNING ELECTRICAL SMELL MAIN CARGO COMPARTMENT T/S FOUND APU BATTERY SMOKING WITH A HEAVY BURNT SMELL. R&R APU BATTERY REF AMM 24-31-03-4. ALSO R&R APU 
- [SDR FDEA201902280547](https://openairdocs.org/sdr/FDEA201902280547), Feb 28, 2019: TRANSMITTER. FAILED. AT FLAP CONFIGURATION WE RECEIVED A TE FLAP ASYM EICAS WITH NO LE SLAT OR LE SLAT DISAGREE INDICATED. RAN QRH, DECLARED EMERGENCY AND LANDED IAW QRH GUIDANCE, F
- [SDR FDEA201812133499](https://openairdocs.org/sdr/FDEA201812133499), Dec 13, 2018: SOCKET. DAMAGED. RIGHT FORWARD ENTRY DOOR SLIDE WILL NOT ARM. R1 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS INOP. REMOVED AND REPLACED SLIDE ANNUNCIATOR ASSY IAW SMP AND 757 WDM CH
- [SDR FDEA201708062125](https://openairdocs.org/sdr/FDEA201708062125), Aug 6, 2017: SPAR. CORRODED. LT WING O/B FLAP MID AREA INTERIOR FRONT SPAR LOWER CHORD FOUND HEAVY CORROSION. COMPLIED WITH EA F-5750-T0334766 P1, REPAIRED LT WING O/B FLAP MID AREA INTERIO
- [SDR FDEA201708032102](https://openairdocs.org/sdr/FDEA201708032102), Aug 3, 2017: FLOOR SUPPORT. CORRODED. MDCC BS 920 - 1040, LBL 45.5 FLOOR SUPPORT CORRODED. REPAIRED THE FLOOR SUPPORT IAW EA:F-5310-T0334767 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201708032100](https://openairdocs.org/sdr/FDEA201708032100), Aug 3, 2017: SEAT TRACK. CORRODED. MDCC BS 1180 - 1200, LBL 24.75 SEAT TRACK CORRODED. FABRICATED A NEW SEAT TRACK IAW DWG 146N5130. REPLACED THE SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR IAW GMM
- [SDR FDEA201708032103](https://openairdocs.org/sdr/FDEA201708032103), Aug 3, 2017: SEAT TRACK. CORRODED. MDCC BS 1180 - 1200, RBL 45.5 SEAT TRACK CORRODED. FABRICATED A NEW SEAT TRACK IAW DWG 146N5130. REPLACED THE SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR IAW GMM 
- [SDR FDEA201708032101](https://openairdocs.org/sdr/FDEA201708032101), Aug 3, 2017: SEAT TRACK. CORRODED. MDCC BS 1080 - 1180, LBL 45.5 SEAT TRACK CORRODED. FABRICATED A NEW SEAT TRACK IAW DWG 144N5021. REPLACED THE SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR IAW GMM 
- [SDR FDEA201706301788](https://openairdocs.org/sdr/FDEA201706301788), Jun 30, 2017: HYDRAULIC SYSTEM. LEAKING. INFLIGHT EICAS LT HYD QTY INDICATED 0.45. QUANTITY CONTINUED DECREASING AND LOST ENTIRE L HYDRAULIC SYSTEM AFTER LANDING ROLLOUT, NO NLG STEERING AVAILABLE. OPE
- [SDR FDEA201704111131](https://openairdocs.org/sdr/FDEA201704111131), Apr 11, 2017: FLAP SYSTEM. MALFUNCTIONED. DURING FINAL APPROACH, EXTENDED FLAPS 15 TO 20, FLAPS STUCK AT 17 DEGREES. RECEIVED A TE FLAP DISAGREE EICAS MESSAGE. DECLARED AN EMERGENCY PERFORMED QRH. UNEVE
- [SDR FDEA201603291099](https://openairdocs.org/sdr/FDEA201603291099), Mar 29, 2016: FSEU. INOPERATIVE. AT LEVEL OFF FLIGHT 360, EICAS MSG LE SLAT ASYM MSG CAME ON. COMPLIED WITH QRH. ACFT ARRIVED WITH NO LOWER EICAS MSG OR MX MSG. LE LIGHT WAS ON ABOVE POSITION G
- [SDR FDEA201603291098](https://openairdocs.org/sdr/FDEA201603291098), Mar 29, 2016: COMPUTER. INOPERATIVE. AT LEVEL OFF FLIGHT 360, EICAS MSG LE SLAT ASYM MSG CAME ON. COMPLIED WITH QRH. ACFT ARRIVED WITH NO LOWER EICAS MSG OR MX MSG. LE LIGHT WAS ON ABOVE POSITION G
- [SDR FDEA201511293815](https://openairdocs.org/sdr/FDEA201511293815), Nov 29, 2015: SLIDE. UNSECURE. AFTER LANDING, FIRST OFFICER FAILED TO DISARM RT ENTRY DOOR. SLIDE & RAFT CAME OUT OF CONTAINER BUT DID NOT INFLATE, WHEN MX OPENED DOOR. REMOVED AND REPLACED R
- [SDR FDEA201508122540](https://openairdocs.org/sdr/FDEA201508122540), Aug 12, 2015: SKIN. DELAMINATED. LEFT WING INBD FLAP, CHIPPED PAINT, POSSIBLE DELAMINATION UPPER SURFACE. REPAIRED IAW SRM 51-70-07-00-0 PARAGRAPHS 4 D4 & 4.6.
- [SDR FDEA201508102527](https://openairdocs.org/sdr/FDEA201508102527), Aug 10, 2015: SHEAR PLATE. CORRODED. MAIN CABIN SHEAR PLATE HAS CORROSION BS 395 - 440, BETWEEN LBL 24.75 & 45.50. REPAIRED IAW EA F-5310-T0319429 REV NR PS P1.
- [SDR FDEA201508102526](https://openairdocs.org/sdr/FDEA201508102526), Aug 10, 2015: SHEAR PLATE. CORRODED. MAIN CABIN SHEAR PLATE HAS CORROSION BS 395 - 440, BETWEEN LBL 0 & 24.75. REPAIRED IAW EA F-5310-T0319384 REV NR PS P1
- [SDR FDEA201312193024](https://openairdocs.org/sdr/FDEA201312193024), Dec 19, 2013: CONTROLLER. FAILED. DURING CRUISE FL380, IN CLEAR AIR WITH ANTI-ICE OFF, RECEIVED EICAS MESSAGES FOR RT ENGINE BLEED OFF, RT PACK OFF, & RT PACK TEMP, IAW QRH TURNED RT ENGINE BLEE
- [SDR FDEA201307311708](https://openairdocs.org/sdr/FDEA201307311708), Jul 31, 2013: ATTACH FITTING. CRACKED. FWD ENTRY AREA, FRAME BS 350, ATTACH FITTING TO L1 DOOR UPPER SILL IS CRACKED. REMOVED DAMAGED ATTACH FITTING, FABRICATED AND INSTALLED NEW ATTACH FITTING IAW D
- [SDR FDEA201307261670](https://openairdocs.org/sdr/FDEA201307261670), Jul 26, 2013: SKIN. DENTED. LOWER FUSELAGE DENTED BS 510 BETWEEN STRINGERS 27-28L. FABRICATED, AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-00 AND SRM 53-00-01, REPAIR 16 FIG 201.
- [SDR FDEA201306271408](https://openairdocs.org/sdr/FDEA201306271408), Jun 27, 2013: LINE. LEAKING. AFTER TAKE OFF PASSING 10K FT, LEFT HYD QTY LT ILLUMINATED, SHORTLY FOLLOWING THE LEFT HYD SYS PRESSURE LIGHT ILLUMINATED SYS QTY & SYS PRESSURE BOTH WENT TO ZE
- [SDR FDEA201306131272](https://openairdocs.org/sdr/FDEA201306131272), Jun 13, 2013: UNKNOWN. UNKNOWN. LEFT FWD ENTRY DOOR, WHEN SAFETIED AFTER SHUTDOWN "KNUCKLE KNUCKER" DID NOT RELEASE. HANDLE WENT TO GREEN AREA AND SLIDE LIGHT WENT OUT. DOOR ARMING SLIDE/ GIRT
- [SDR FDEA201305151001](https://openairdocs.org/sdr/FDEA201305151001), May 15, 2013: INDICATOR. FAILED. LEFT ENGINE EPR WAS SURGING OR - 0.10 EPR DURING T/O ROLL WITH AUTOTHROTTLES ENGAGED. REJECTED T/O AT 80 KNOTS. R & R FFG CONTINUED AND ENGINE WAS REMOVED FOR T
- [SDR FDEA201305100956](https://openairdocs.org/sdr/FDEA201305100956), May 10, 2013: ENGINE. SURGES. LEFT ENGINE EPR SURGED. .10 EPR DURING TAKE OFF ROLL WITH AUTOTHROTTLES ENGAGED. REJECTED TAKE OFF AT 80 KNOTS. PERFORMED IP/HP COMPRESSOR AIRFLOW CONTROL TEST 
- [SDR FDEA201305090952](https://openairdocs.org/sdr/FDEA201305090952), May 9, 2013: COMPRESSOR. STALLED. AFTER TAKEOFF LT ENGINE BEGAN SURGING AND HAD A NOTICABLE THUMP LIKE A COMPRESSOR STALL. ALT 2000' AGL. POWER AT CLIMB, RETARDED THROTTLE RETURNED TO DEPARTURE.
- [SDR FDEA201212174313](https://openairdocs.org/sdr/FDEA201212174313), Dec 17, 2012: LIGHT. INOPERATIVE. RT EMERGENCY SLIDE LIGHT INOPERATIVE. R & R RT EMERGENCY SLIDE LIGHT IAW SMP, OPS NORMAL.
- [SDR FDEA201212164311](https://openairdocs.org/sdr/FDEA201212164311), Dec 16, 2012: LIGHT. INOPERATIVE. RT SIDE EMERGENCY EXTERIOR LIGHT INOPERATIVE. R & R RT EMERGENCY SLIDE LIGHT IAW SMP, OPS NORMAL.

All 121: https://openairdocs.org/aircraft/N921FD/reports.md

## STCs that may be installed (OpenAirDocs) (6)

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 airframe (Boeing 757-23A)

- [STC ST01162NY](https://openairdocs.org/stc/ST01162NY): Installation of Literature Pockets. Magee Plastics Company. Lists 757 Series
- [STC ST01675CH](https://openairdocs.org/stc/ST01675CH): Installation of Butterfly Valve Ring AIR23028 in starter control valves, part number 775538 or 799700. Cook Airtomic. Lists 757 Series
- [STC ST02296AT](https://openairdocs.org/stc/ST02296AT): Upgrade existing HF Voice Communication System to provide HF datalink capability. ARINC, Inc. Lists 757 Series
- [STC SA01916AT](https://openairdocs.org/stc/SA01916AT): Manufacture of Tray Carrier P/N 1839-501. BFE Services. Lists 757 Series
- [STC SA1258EA](https://openairdocs.org/stc/SA1258EA): Installation of Cosco model78-( ) child restraint system. (172M S/N 17263459 - 17267584). Miller Stuart R. Lists 757 Series

### Approved for the engine (Rolls-Royce RB211-535E437)

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

## Related

- Other Boeing 757-23A aircraft: https://openairdocs.org/model/boeing-757-23a/aircraft.md
- The Rolls-Royce RB211-535E437 engine: https://openairdocs.org/engine/rolls-royce-rb211-535e437.md

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