# N957FD: 1990 Boeing 757-21B

- Status: Valid registration
- Airframe: [Boeing 757-21B](https://openairdocs.org/model/boeing-757-21b) (registry code 1384917, 239 seats)
- Engine: [Rolls-Royce RB211-535E437](https://openairdocs.org/engine/rolls-royce-rb211-535e437) (registry code 54053)
- Data sheets: [TCDS E12EU](https://openairdocs.org/tcds/E12EU) (Rolls-Royce Deutschland Ltd & Co KG) (OpenAirDocs)
- Serial number: 24774
- Year built: 1990
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 17, 2007
- Certificate issued: November 5, 2010
- Expires: November 30, 2029
- Mode S code: AD4F29
- 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=957FD
- Page: https://openairdocs.org/aircraft/N957FD

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 757-21B)

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 N957FD.

## FAA accident and incident reports

None matched to N957FD.

## Service difficulty reports (118, 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 FDEA201805251317](https://openairdocs.org/sdr/FDEA201805251317), May 25, 2018: ENGINE. FAILED. DURING A TEST FLIGHT, 2 HOURS 39 MINUTES INTO FLIGHT, THE RIGHT ENGINE OIL QUANTITY WENT TO ZERO & OIL PRESSURE DECREASED TO 4 PSI IN THE RED BAND. SHUT THE RT 
- [SDR FDEA2018051861247](https://openairdocs.org/sdr/FDEA2018051861247), May 16, 2018: SHEAR TIE. CORRODED. FWD CARGO BILGE, BS 680 SHEAR TIE CORRODED BETWEEN STRINGERS 27L - 28L. EVALUATED AREA OF CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A, FIG 101, 
- [SDR FDEA201805121211](https://openairdocs.org/sdr/FDEA201805121211), May 12, 2018: KEELBEAM. CORRODED. EVIDENCE OF CORROSION, STRINGER 28L-FORWARD LOWER CARGO BAY BETWEEN BS 660 - 680. COMPLIED WITH EA T F-5310-T0339895 .
- [SDR FDEA2018051831162](https://openairdocs.org/sdr/FDEA2018051831162), May 3, 2018: SKIN. DENTED. LOWER LOBE EXTERNAL SKIN HAS TWO PROTRUDING DENTS AT APPROX BS 524, BETWEEN STRINGERS 26L & 27L. COMPLIED WITH EA F-5330-T0339825, P1.
- [SDR FDEA201511183701](https://openairdocs.org/sdr/FDEA201511183701), Nov 18, 2015: ADC. FAILED. ON TAKEOFF ROLL, CAPTAIN ADC FAILED. DUPLICATED DADC FAIL ON GND. R & R LT DADC IAW AMM 34-12-01-4. OPERATIONS CHECKED NORMAL. OK FOR SERVICE.
- [SDR FDEA201511143605](https://openairdocs.org/sdr/FDEA201511143605), Nov 14, 2015: GIRT BAR. BENT. RIGHT ESCAPE SLIDE CAME LOOSE. R & R RT 1 DOOR GIRT BAR ASSEMBLY IAW AMM 25-66-10-2-0. OPERATIONS CHECKED GOOD. OK FOR SERVICE.
- [SDR FDEA201506021677](https://openairdocs.org/sdr/FDEA201506021677), Jun 2, 2015: CHARGER. INOPERATIVE. DURING PREFLIGHT L1 DOOR EMER & SLIDE LIGHTS INOPERATIVE. INSTALLED NEW BATTERY PACK, NO HELP. R & R L1 EMER LIGHTS BATTERY CHARGER & BATTERY PACK IAW AMM 33-51
- [SDR FDEA201503180968](https://openairdocs.org/sdr/FDEA201503180968), Mar 18, 2015: LIGHT. INOPERATIVE. RIGHT SLIDE ARM LIGHT INOPERATIVE. RELAMPED DOOR SLIDE ARM LIGHT IAW SMP. OPERATIONS CHECKED GOOD.
- [SDR FDEA201503040652](https://openairdocs.org/sdr/FDEA201503040652), Mar 4, 2015: COVER. DAMAGED. DURING LT ENTRY DOOR CLOSING, SLIDE COVER DISLODGED ON L1. REPAIRED SLIDE COVER PER SRM 51-70-03-G. REINSTALLED L1 SLIDE COVER PER AMM 25-66-01-4. ACFT OKAY FOR
- [SDR FDEA201403240568](https://openairdocs.org/sdr/FDEA201403240568), Mar 24, 2014: FRAME. PUNCTURED. PUNCTURE TO FRAME AT FWD ACCESSORY EQUIPMENT BAY BS 239 LOWER LOBE DOOR CUT OUT. REPAIRED IAW EA F-5310-T0306819 REV A P1.
- [SDR FDEA201401310225](https://openairdocs.org/sdr/FDEA201401310225), Jan 31, 2014: COVER. DELAMINATED. L1 DOOR ESCAPE SLIDE COVER HAS ONE EACH LATCH BROKEN. RELEASED FOR SERVICE IAW MEL 52-11-01-A. L1 DOOR SLIDE INOPERABLE, IDENTIFY INOPERABLE OR MISSING. REPAIRE
- [SDR FDEA201310302646](https://openairdocs.org/sdr/FDEA201310302646), Oct 30, 2013: PRESSURE SWITCH. FAILED. AT LEVEL OFF, FL 380, RUDDER RATIO, EICAS FOLLOWED IMMEDIATLLY BY LT HYD SYS PRESSURE. CHECKED SYS, PRESSURE ON STATUS PAGE, IT SHOWED DECREASING. LT YAW DAMPER
- [SDR FDEA201305211062](https://openairdocs.org/sdr/FDEA201305211062), May 21, 2013: LIGHT. INOPERATIVE. RT EMERGENCY SLIDE LIGHT INOPERATIVE. LIGHT SOCKET CORRODED. FUSE BLOWN IN EMERGENCY POWER SUPPLY. REPLACED LAMP AND R & R EMERGENCY LIGHT POWER SUPPLY AND BATT
- [SDR FDEA201211204102](https://openairdocs.org/sdr/FDEA201211204102), Nov 20, 2012: SLIDE. DISLODGED. F/O DISARMED DOOR & CHECKED. RAMP OPEN DOOR AND SLIDE DEPLOYED. FOUND SLIDE HAD DEPARTED FROM DOOR AND WAS NOT INFLATED. R & R L1 SLIDE USING AMM 25-66-01-4.
- [SDR FDEA201210313794](https://openairdocs.org/sdr/FDEA201210313794), Oct 31, 2012: BATTERY PACK. MISINSTALLED. EMERGENCY EXIT LIGHT OVER R1 DOOR INOPERATIVE WHEN SWITCHED TO ON IN COCKPIT. FOUND EXIT LIGHT BATTERY PACK IMPROPERLY INSTALLED. INSTALLED CORRECTLY IAW AMM 33
- [SDR FDEA201210273759](https://openairdocs.org/sdr/FDEA201210273759), Oct 27, 2012: LIGHT. UNKNOWN. INTERIOR EMERGENCY EXIT SIGN ABOVE DOOR 1R INOPERATIVE. CHECKED OPERATION OF EMERGENCY LIGHTS IAW AMM 33-51-00-5, ALL OPS CHECK GOOD FOR CONTINUED SERVICE AT TH
- [SDR FDEA201210033543](https://openairdocs.org/sdr/FDEA201210033543), Oct 3, 2012: LIGHT. INOPERATIVE. THE RT CABIN DOOR EXIT EMERGENCY LIGHT WAS NOT ILLUMINATED DURING TEST. THE CABIN OVERHEAD EXIT LIGHT ALSO WAS NOT ILLUMINATED. EMERGENCY EXIT LIGHT SYS IAW MM 
- [SDR FDEA201205221921](https://openairdocs.org/sdr/FDEA201205221921), May 22, 2012: SAFETY WIRE. WRONG PART. DURING FLIGHT DECK INSPECTION, FOUND WRONG SAFETY WIRE ON THE LEFT GUARDED GEN DISC SWITCH. DURING FLIGHT DECK INSP FOUND RT GUARDED GEN DISC SWITCH WITH THE WR
- [SDR FDEA201203160962](https://openairdocs.org/sdr/FDEA201203160962), Mar 16, 2012: STRINGER SPLICE. CORRODED. STRINGER SPLICE 28R, BS 660, FOUND WITH CORRODED. STRINGER SPLICE R & R WITH FABRICATED STRINGER SPLICE IAW SRM 51-40-05, REV 105. REPAIR IS CLASSIFIED AS MAJOR
- [SDR FDEA201202280696](https://openairdocs.org/sdr/FDEA201202280696), Feb 28, 2012: STRINGER. CORRODED. RT SIDE INTERIOR, CORROSION ON STRINGER 6R WHERE IT IS ATTACHED TO THE BS 1787 BULKHEAD ON THE AFT SIDE OF THE BULKHEAD. REPAIRED IAW EA F-5310-157138 PART 1. R
- [SDR FDEA201202280695](https://openairdocs.org/sdr/FDEA201202280695), Feb 28, 2012: FRAME. CORRODED. BS 1787 AT S3R, CORROSION ON THE AFT SIDE OF THE FRAME WHERE IT ATTACHES TO THE STRINGER. REPAIRED IAW EA F-5310-157138, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201202280694](https://openairdocs.org/sdr/FDEA201202280694), Feb 28, 2012: FRAME. CORRODED. BS 1787 S3R, CORROSION ON THE AFT SIDE OF THE FRAME WHERE IT ATTACHES TO THE SKIN. REPAIR CARRIED OUT IAW EA F-5310-157138, PART 1. REPAIR IS CLASSIFIED AS MAJO
- [SDR FDEA201202100540](https://openairdocs.org/sdr/FDEA201202100540), Feb 10, 2012: DOOR FRAME. MISINSTALLED. NR 2 CARGO DOOR FRAME FOUND SHORT EDGE MARGIN ON LOWER CHORD OF AFT SIDE FRAME. R & R WITH FABRICATED CHORD IAW SRM 51-40-02, REV 105. REPAIR IS CLASSIFIED AS M
- [SDR FDEA201202080518](https://openairdocs.org/sdr/FDEA201202080518), Feb 8, 2012: FRAME. CORRODED. AFT LWR CARGO BAY FRAME AT BS 1300 HAS CORROSION ON UPPER FLANGE BETWEEN STRINGERS 26 -27R. REPAIRED IAW EA F-5310-158002. REPAIR IS CLASSIFIED AS MINOR.
- [SDR FDEA201202060492](https://openairdocs.org/sdr/FDEA201202060492), Feb 6, 2012: TIE DOWN. CORRODED. FWD LWR CARGO BAY, RIGHT TIE DOWN FITTING HAS CORROSION AT BS 540. REPAIRED IAW EA F-5340-154493. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201202060491](https://openairdocs.org/sdr/FDEA201202060491), Feb 6, 2012: TIE DOWN. CORRODED. FWD LWR CARGO BAY, RIGHT TIE DOWN FITTING HAS CORROSION AT BS 520. REPAIRED IAW EA F-5340-154493. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201202060490](https://openairdocs.org/sdr/FDEA201202060490), Feb 6, 2012: TIE DOWN. CORRODED. FWD LWR CARGO BAY, LEFT TIE DOWN FITTING HAS CORROSION AT BS 740. REPAIRED IAW EA F 5340-154493. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201202060489](https://openairdocs.org/sdr/FDEA201202060489), Feb 6, 2012: TIE DOWN. CORRODED. FWD LWR CARGO BAY, LEFT TIE DOWN FITTING HAS CORROSION AT BS 839. REPAIR CARRIED OUT IAW EA F-5340-154493. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201202060488](https://openairdocs.org/sdr/FDEA201202060488), Feb 6, 2012: TIE DOWN. CORRODED. FWD LWR CARGO BAY, LEFT TIE DOWN FITTING HAS CORROSION AT BS 820. REPAIRED IAW EA F-5340-154493. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201202060487](https://openairdocs.org/sdr/FDEA201202060487), Feb 6, 2012: TIE DOWN. CORRODED. FWD LWR CARGO BAY, LEFT TIE DOWN FITTING HAS CORROSION AT BS 800. REPAIR CARRIED OUT IAW EA F-5340-154493. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201202060486](https://openairdocs.org/sdr/FDEA201202060486), Feb 6, 2012: TIE DOWN. CORRODED. AFT LWR CARGO BAY, LEFT TIE DOWN FITTING HAS CORROSION AT BS 760. REPAIR CARRIED OUT IAW EA F-5340-154493 . REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201202060485](https://openairdocs.org/sdr/FDEA201202060485), Feb 6, 2012: TIE DOWN. CORRODED. AFT LWR CARGO BAY, LEFT TIE DOWN FITTING HAS CORROSION AT BS 520. REPAIRED IAW EA F-5340-154493. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201202060484](https://openairdocs.org/sdr/FDEA201202060484), Feb 6, 2012: TIE DOWN. CORRODED. AFT LWR CARGO BAY, RIGHT TIE DOWN FITTING HAS CORROSION AT BS 1620. REPAIRED IAW EA F-5340-154494. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201202060483](https://openairdocs.org/sdr/FDEA201202060483), Feb 6, 2012: TIE DOWN. CORRODED. AFT LWR CARGO BAY, RIGHT TIE DOWN FITTING HAS CORROSION AT BS 1600. REPAIR CARRIED OUT IAW EA F-5340-154494. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201202060482](https://openairdocs.org/sdr/FDEA201202060482), Feb 6, 2012: TIE DOWN. CORRODED. AFT LWR CARGO BAY, RIGHT TIE DOWN FITTING HAS CORROSION AT BS 1480. REPAIR CARRIED OUT IAW EA F-5340-154494. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201202060481](https://openairdocs.org/sdr/FDEA201202060481), Feb 6, 2012: TIE DOWN. CORRODED. AFT LWR CARGO BAY, RIGHT TIE DOWN FITTING HAS CORROSION AT BS 1340. REPAIR CARRIED OUT IAW EA F-5340-154494. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201202060480](https://openairdocs.org/sdr/FDEA201202060480), Feb 6, 2012: TIE DOWN. CORRODED. AFT LWR CARGO BAY, RIGHT TIE DOWN FITTING HAS CORROSION AT BS 1220. REPAIR CARRIED OUT IAW EA F-5340-154494. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201202060479](https://openairdocs.org/sdr/FDEA201202060479), Feb 6, 2012: TIE DOWN. CORRODED. AFT LWR CARGO BAY, LEFT TIE DOWN FITTING HAS CORROSION AT BS 1480. REPAIR CARRIED OUT IAW EA F-5340-154494. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201202060478](https://openairdocs.org/sdr/FDEA201202060478), Feb 6, 2012: TIE DOWN. CORRODED. AFT LWR CARGO BAY, LEFT TIE DOWN FITTING HAS CORROSION AT BS 1260. REPAIR CARRIED OUT IAW EA F-5340-154494. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201202060477](https://openairdocs.org/sdr/FDEA201202060477), Feb 6, 2012: TIE DOWN. CORRODED. AFT LWR CARGO BAY LEFT TIE DOWN FITTING HAS CORROSION BS 1240. REPAIR CARRIED OUT IAW EA F-5340-154494. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201202060476](https://openairdocs.org/sdr/FDEA201202060476), Feb 6, 2012: TIE DOWN. CORRODED. AFT LWR CARGO BAY TIE DOWN FITTING HAS CORROSION AT BS 1220. REPAIRED IAW EA F-5340-154494. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201202010409](https://openairdocs.org/sdr/FDEA201202010409), Feb 1, 2012: FRAME. DENTED. FORWARD LOWER CARGO BAY, AFTER REMOVAL OF RT TRANSITION PANEL FRAME AT STA 700 UPPER SURFACE HAS DENT BETWEEN STRINGERS S24R - S25R. REPAIR CARRIED OUT IAW EA F
- [SDR FDEA201202010408](https://openairdocs.org/sdr/FDEA201202010408), Feb 1, 2012: FRAME. DENTED. FWD LOWER CARGO BAY, AFTER REMOVAL OF RT TRANSITION PANEL FRAME AT BS 680. UPPER SURFACE HAS DENT BETWEEN STRINGERS 23- 24 RIGHT. REPAIR CARRIED OUT IAW EA F-53
- [SDR FDEA201202010407](https://openairdocs.org/sdr/FDEA201202010407), Feb 1, 2012: FRAME. DENTED. AFT LOWER CARGO BAY, FRAME UPPER SURFACE AT BS 1380 HAS DENT BETWEEN STRINGERS 25 -26L. DENT REPAIR CARRIED OUT IAW EA F-5310-158005, PART 1. REPAIR IS CLASSIFI
- [SDR FDEA201202010406](https://openairdocs.org/sdr/FDEA201202010406), Feb 1, 2012: SKIN. CORRODED. RIGHT WING UPPER SURFACE FIXED T/E SKIN PANEL (SRM 57-51-01) L/E ROW OF RIVETS FOUND SUNKEN IN AT WBL 79.02 OTBD 28" TO 38". REPAIRED IAW EA F-5730-15300, PART 
- [SDR FDEA201201310388](https://openairdocs.org/sdr/FDEA201201310388), Jan 31, 2012: ATTACH ANGLE. CORRODED. THE APU INLET DOOR ASSY ATTACH ANGLE AT RT STRINGER 3 HAS CORROSION BETWEEN BS 1787-1806. CORRODED ATTACHMENT ANGLE R & R WITH FABRICATED ANGLE IAW SRM 51-40-02
- [SDR FDEA201201290375](https://openairdocs.org/sdr/FDEA201201290375), Jan 29, 2012: STIFFENER. CORRODED. KEEL BEAM STRUCTURE CENTER STIFFENER FOUND CORROSIONS AT BS 1022 TO 1027. REPAIRED IAW EA F-5310-157127, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201201290374](https://openairdocs.org/sdr/FDEA201201290374), Jan 29, 2012: STIFFENER. CORRODED. KEEL BEAM STRUCTURE CENTER STIFFENER FOUND CORROSIONS AT BS 989 TO 1006. REPAIRED IAW EA F-5310-157127, PART 1. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201201290373](https://openairdocs.org/sdr/FDEA201201290373), Jan 29, 2012: STIFFENER. CORRODED. KEEL BEAM STRUCTURE CENTER STIFFENER FOUND CORROSIONS AT BS 974 TO 984. REPAIRED IAW E.A. F-5310-157127 PART 1. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201201290370](https://openairdocs.org/sdr/FDEA201201290370), Jan 29, 2012: STIFFENER. CORRODED. KEEL BEAM STRUCTURE CENTER STIFFENER FOUND CORROSION AT BS 955 TO 959. REPAIRED IAW EA F-5310-15727, PART 1. REPAIR IS CLASSIFIED AS MAJOR.

All 118: https://openairdocs.org/aircraft/N957FD/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 RB211-535E437)

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

## Related

- Other Boeing 757-21B aircraft: https://openairdocs.org/model/boeing-757-21b/aircraft.md
- The Rolls-Royce RB211-535E437 engine: https://openairdocs.org/engine/rolls-royce-rb211-535e437.md

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