# N935FD: Boeing 757-2T7

- Status: Valid registration
- Airframe: [Boeing 757-2T7](https://openairdocs.org/model/boeing-757-2t7) (registry code 138491A, 239 seats)
- Engine: [Rolls-Royce RB211-535E4 series](https://openairdocs.org/engine/rolls-royce-rb211-535e4-series) (registry code 54223)
- Data sheets: [TCDS E12EU](https://openairdocs.org/tcds/E12EU) (Rolls-Royce Deutschland Ltd & Co KG) (OpenAirDocs)
- Serial number: 22780
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Certificate issued: February 24, 2009
- Expires: August 31, 2029
- Mode S code: ACF8BD
- 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=935FD
- Page: https://openairdocs.org/aircraft/N935FD

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 757-2T7)

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 N935FD.

## FAA accident and incident reports

None matched to N935FD.

## Service difficulty reports (298, 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 FDEA202610131587](https://openairdocs.org/sdr/FDEA202610131587), Oct 13, 2026: INDICATION SYS. MALFUNCTIONED. DURING CLIMB OUT, GOT RT HYD SYS PRESSURE EICAS & ASSOCIATED LIGHT ON OVERHEAD. LOWER EICAS STATUS PAGE SHOWED NORMAL PRESSURE & NORMAL QUANTITY. EMERGENCY DECL
- [SDR FDEA202610131564](https://openairdocs.org/sdr/FDEA202610131564), Oct 13, 2026: WIRE. SHORTED. DURING CLIMB OUT GOT R HYD SYS PRESS EICAS AND ASSOCIATED LIGHT ON OVERHEAD. LOWER EICAS STATUS PAGE SHOWED NORMAL PRESSURE AND NORMAL QUANTITY. EMERGENCY DECLA
- [SDR FDEA202609181374](https://openairdocs.org/sdr/FDEA202609181374), Sep 18, 2026: EEC. FAILED. L EEC EICAS DURING TAKEOFF ROLL AND 4X IN FLIGHT ALL WITH ASSOCIATED AUTOTHROTTLES EICAS. NOTABLE YAW IN FLIGHT WHEN IT WOULD OCCUR. COMPLIED WITH QRH. FIM: 73-
- [SDR FDEA202607231013](https://openairdocs.org/sdr/FDEA202607231013), Jul 23, 2026: BEAM. CORRODED. NOSE WHEEL WELL STRUCTURE BS 310.5 LOWER AREA INTERNAL BEAM WITH CORROSION REMOVED VERTICAL BEAM OUT OF LIMITS AT NOSE WEEL STRUCTURE BS 310.5 LBL 20.05 LOWER A
- [SDR FDEA202607200955](https://openairdocs.org/sdr/FDEA202607200955), Jul 20, 2026: STRAP. CORRODED. APU INLET DUCT ATTACHMENTS AT THE AFT FRAME WITH CORROSION CORRSION OUT OF LIMITS AT APU INLET DUCT ATTACHMENTS ON THE AFT FRAME (MIDDLE STRAP) IAW B-757 SRM 53
- [SDR FDEA202607200954](https://openairdocs.org/sdr/FDEA202607200954), Jul 20, 2026: CREASE BEAM. CORRODED. MCC CREASE BEAM SIDE LH BSTA 1620 TO BSTA 1370 IT HAS CORROSION SPOTS MCC L/H CREASE BEAM SECTION WITH CORROSION OUT OF LIMITS FROM STA 1430 TO 1530 LBL 64.40 I
- [SDR FDEA202607200953](https://openairdocs.org/sdr/FDEA202607200953), Jul 20, 2026: CREASE BEAM. CORRODED. MCC SIDE LH BETWEEN BS 1080 TO BS 1100 CREASE BEAM WITH CORROSION MCC L/H CREASE BEAM SECTION WITH CORROSION OUT OF LIMITS FROM STA 1040 TO STA 1100 IAW B-757 S
- [SDR FDEA202607150928](https://openairdocs.org/sdr/FDEA202607150928), Jul 15, 2026: FLOORBEAM. CORRODED. MCC BL 0 TO LBL 24.75 BS 1200 FLOOR BEAM WITH CORROSION AREA WITH CORROSION OUT OF LIMITS AT FLOOR BEAM BS 1200 LBL 8 TO LBL 14 WAS REPAIRED IAW B757 SRM 53-00-
- [SDR FDEA202607100893](https://openairdocs.org/sdr/FDEA202607100893), Jul 10, 2026: SKIN PANEL. DENTED. UPPER FUSELAGE TAIL AREA BETWEEN B.S. 1918 TO B.S. 1941 TOP SECTION WITH 01 EA DENT. APPLIED PERMANENT REPAIR AT UPPER FUSELAGE TAIL AREA BS 1918 TO B.S. 1941 I
- [SDR FDEA202607100892](https://openairdocs.org/sdr/FDEA202607100892), Jul 10, 2026: ACCESS PANEL. CRACKED. LH WING #3 SLAT LOWER SKIN ACCESS PANEL 523GB AREA WITH 02 EA CRACK. 2EA CRACK AT LH WING #3 SLAT LOWER COVE SKIN ACCESS PANEL 523GB AREA WERE REPAIRED IAW B-75
- [SDR FDEA202607100890](https://openairdocs.org/sdr/FDEA202607100890), Jul 10, 2026: ACCESS PANEL. CRACKED. LH WING #3 SLAT LOWER SKIN ACCESS PANEL 523FB AREA WITH 01EA CRACK. CRACK AT LH WING #3 SLAT LOWER COVE SKIN ACCESS PANEL 523FB AREA WAS REPAIRED IAW B-757 SRM 
- [SDR FDEA202506060850](https://openairdocs.org/sdr/FDEA202506060850), Jun 6, 2025: GUST LOCK. INOPERATIVE. L1 DOOR GUST LOCK FOUND DAMAGED/BROKEN ON WALKAROUND. AMM: 52-11-08-8 INSTALLED NEW SPLIT COLLAR IRW AMM 52-11-08-8.
- [SDR FDEA202408171144](https://openairdocs.org/sdr/FDEA202408171144), Aug 17, 2024: STRINGER. CORRODED. FORWARD CARGO LSTR 19-22 STA 760 FRAME HAS AREAS OF CORROSION AT SKIN ATTACHMENT POINTS AND STR EVALUATED CORROSION AT SKIN ATTACHMENT POINTS S-19L, 21L, AND 22
- [SDR FDEA202403300423](https://openairdocs.org/sdr/FDEA202403300423), Mar 30, 2024: BATTERY PACK. INOPERATIVE. THROUGHOUT MAINTANENCE DAILY CHECK FOUND L1 EMER EXIT SIGN DOOR 1 LT, FLT DECK DOME EMER LT MODULE, SLIDE LT DR 1 EMER INOP. SHGN 30MAR24 05:49 BNA WDM: CH 33-5
- [SDR FDEA202403160300](https://openairdocs.org/sdr/FDEA202403160300), Mar 16, 2024: GIRT BAR. OUT OF ALIGNMENT. L1 DOOR ESCAPE SLIDE BEGAN TO FALL OUT WHEN DOOR WAS OPENED FOR CREW STAIR MATING. DURING TROUBLESHOOTING FOUND LH DOOR AFT FLOOR FITTING MISALIGNED. RE-ALIGNED
- [SDR FDEA202212062878](https://openairdocs.org/sdr/FDEA202212062878), Dec 6, 2022: SHUTOFF VALVE. OUT OF ALIGNMENT. ON TAKEOFF ROLL HAD ODOR IN COCKPIT. AFTER LIFTOFF GOT LEFT ENGINE OVERHEAT MESSAGE. THEN FOLLOWED BY FIRE BELL. RAN QRH AN LANDED. EMERGENCY DECLARED. R&R'D LH
- [SDR FDEA202208081928](https://openairdocs.org/sdr/FDEA202208081928), Aug 8, 2022: SKIN. CORRODED. #2 PYLON INTERNAL SKIN THRU ACCESS PANEL 443HL IS CORRODED AT FWD LOWER SIDE. REPAIRED #2 PYLON I/B SKIN PER FEDEX EA F-5450-T0369607 TITLE: NACELLES/PYLON - WI
- [SDR FDEA202208071908](https://openairdocs.org/sdr/FDEA202208071908), Aug 7, 2022: FRAME. DELAMINATED. LEFT ELEVATOR O/B UPPER SURFACE CONDUCTIVE FRAME IS DELAMINATED. REMOVED & REPLACED -7 ADAPTER PLATE IAW DWG 183N2003 REV G, -5 SPLICE PLATE & CONDUCTIVE FRAME 
- [SDR FDEA202208061906](https://openairdocs.org/sdr/FDEA202208061906), Aug 6, 2022: FLOOR PANEL. DENTED. MAIN DECK FLOOR PANEL AT STA 1100-1200 BL0 TO LBL24.75 HAS DENT REMOVED, FABRICATED AND INSTALLED NEW PANEL IAW FEDEX REPAIR DWG SRZ-25-005 AND AMM 25-55-04-4
- [SDR FDEA202208061905](https://openairdocs.org/sdr/FDEA202208061905), Aug 6, 2022: FLOOR PANEL. DENTED. MAIN DECK FLOOR PANEL AT STA 1100-1200 BL0 TO RBL24.75 HAS DENT REMOVED, FABRICATED AND INSTALLED NEW PANEL IAW FEDEX REPAIR DWG SRZ-25-005 AND AMM 25-55-04-4
- [SDR FDEA202208061904](https://openairdocs.org/sdr/FDEA202208061904), Aug 6, 2022: SKIN. WORN. #1 PYLON PANEL 433LR LANDING CENTER AFT IS WORN FROM PANEL LATCH. REPAIRED WORN LATCH LANDING PER FEDEX EA F-5450-T0369581 TITLE: NACELLES/PYLONS - SKIN - NO. 1
- [SDR FDEA202208051901](https://openairdocs.org/sdr/FDEA202208051901), Aug 5, 2022: SKIN. CORRODED. #1 PYLON CORROSION ON INNER SKIN BETWEEN PANEL 433BL AND 433CL REPAIR DAMAGE PER FEDEX EA F-5450-T0369650 TITLE: NACELLES/PYLONS - WING PYLON - NO. 1 PYLON, OUT
- [SDR FDEA202208051900](https://openairdocs.org/sdr/FDEA202208051900), Aug 5, 2022: SKIN. DAMAGED. L. SIDE FUSELAGE SKIN AT STATION 213.5 HAS LIGHTENING STRIKE DAMAGE. REPAIR LIGHTENING STRIKE DAMAGE PER FEDEX EA F-5330-T0369622 TITLE: FUSELAGE - SKIN - LIGHT
- [SDR FDEA202208051899](https://openairdocs.org/sdr/FDEA202208051899), Aug 5, 2022: SKIN. DAMAGED. L. SIDE FUSELAGE SKIN AT STATION 221.5 HAS LIGHTENING STRIKE DAMAGE. REPAIR LIGHTENING STRIKE DAMAGE PER FEDEX EA F-5330-T0369622 TITLE: FUSELAGE - SKIN - LIGHT
- [SDR FDEA202208051898](https://openairdocs.org/sdr/FDEA202208051898), Aug 5, 2022: SKIN. DAMAGED. L. SIDE FUSELAGE SKIN @ BS 211, S21L HAS A LIGHTENING STRIKE DAMAGE. REPAIR LIGHTENING STRIKE DAMAGE PER FEDEX EA F-5330-T0369622 TITLE: FUSELAGE - SKIN - LIGHT
- [SDR FDEA202208051897](https://openairdocs.org/sdr/FDEA202208051897), Aug 5, 2022: WEB. CORRODED. AREA BELOW MAIN CABIN FLOOR SUPPORT STRUCTURE, WEB STA 1440 TO 1460 RBL 65, UPPER SURFACE IS CORRODED REMOVED AND REPLACED CORRODED WEB IAW BAC DWG 146N8521 REV
- [SDR FDEA202208041883](https://openairdocs.org/sdr/FDEA202208041883), Aug 4, 2022: WEB. CORRODED. AREA BELOW MAIN CABIN FLOOR ,SUPPORT STRUCTURE, UPPER DOOR SILL WEB IS CORRODED ON THE UPPER SURFACE AT STA 1440, APPROX RBL 65 CUT-OUT CORRODED SECTION OF WEB 
- [SDR FDEA202208041873](https://openairdocs.org/sdr/FDEA202208041873), Aug 4, 2022: BEAM. CORRODED. L.WING I/B FIXED L/E NOSE BEAM IS CORRODED REPLACED NOSE BEAM ASSY. PER BAC DWG 114N1606 AND FEDEX EA F-5720-T0369810 TITLE WING - SECONDARY WING STRCT - LH WIN
- [SDR FDEA202208031857](https://openairdocs.org/sdr/FDEA202208031857), Aug 3, 2022: FRAME. DELAMINATED. AFT CARGO COMPARTMENT STA 1300 INBD OF STR 26R HAS EXISTING FRAME REPAIR, REF: OPS CARD 8508. REPAIRED AFT CARGO COMPARTMENT FRAME @ STA 1300 R/H PER EA F-5310-
- [SDR FDEA202207281806](https://openairdocs.org/sdr/FDEA202207281806), Jul 28, 2022: BUTTSTRAP. CORRODED. EXTERIOR FUSELAGE IS CORRODED IN THE BUTT SEAM AT STA 900 BETWEEN S12R AND S17R (4 PLACES EXPOSED) ACCOMPLISHED FEDEX EA# F-5330-T0369294 - FUSELAGE - PLATES AN
- [SDR FDEA202207261801](https://openairdocs.org/sdr/FDEA202207261801), Jul 26, 2022: FLOOR SUPPORT. CORRODED. STATION 1715 MAIN CARGO FLOOR STRUCTURE RIGHT SIDE PAN HAS CORROSION UNDER NUT PLATE ON L-BRACKET REMOVED, FABRICATED AND REPLACED L-BRACKET IAW B757 SRM 51-40-
- [SDR FDEA202207261800](https://openairdocs.org/sdr/FDEA202207261800), Jul 26, 2022: FLOOR SUPPORT. CORRODED. STATION 1710 MAIN CARGO FLOOR STRUCTURE LEFT SIDE PAN HAS CORROSION UNDER NUTPL;ATE ON L-BRACKET REMOVED, FABRICATED AND REPLACED L-BRACKET IAW B757 SRM 51-40-0
- [SDR FDEA202207261799](https://openairdocs.org/sdr/FDEA202207261799), Jul 26, 2022: FLOOR SUPPORT. CORRODED. STATION 1710 MAIN CARGO FLOOR STRUCTURE CENTER OF PAN HAS CORROSION UNDER NUT PLATE ON L-BRACKET REMOVED, FABRICATED AND REPLACED L-BRACKET IAW B757 SRM 51-40-0
- [SDR FDEA202207251795](https://openairdocs.org/sdr/FDEA202207251795), Jul 25, 2022: NONE. UNKNOWN. EXISTING MAJOR REPAIR FOUND ON FLOOR BEAM, UPPER CHORD AT STA 345, 40 RBL TO 52 LBL. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS IN ACCORDANCE WITH APP
- [SDR FDEA202207221790](https://openairdocs.org/sdr/FDEA202207221790), Jul 22, 2022: INTERCOSTAL. CORRODED. AFT CARGO COMPARTMENT INTERCOSTAL @ STA 1520 LBL 2.90 HAS CORRODED CLIP. FABRICATED NEW ATTACHMENT ANGLE IAW BAC DWG 146N5450-7 REV A & INSTALLED IAW B757 SRM 5
- [SDR FDEA202207221789](https://openairdocs.org/sdr/FDEA202207221789), Jul 22, 2022: INTERCOSTAL. CORRODED. INTERCOSTAL FROM STATION 1500 TO 1520 IN BILGE AREA HAS CORROSION IN 3 AREAS FABRICATED NEW INTERCOSTAL IAW BAC DWG 146N5451-11 REV C & INSTALLED IAW B757 SRM 5
- [SDR FDEA202207211788](https://openairdocs.org/sdr/FDEA202207211788), Jul 21, 2022: SKIN. DELAMINATED. LEFT HORIZONTAL STABILIZER UPPER SKIN PANEL HAS DELAMINATED REPAIR DOUBLER REPAIRED BY REMOVING AND REPLACING REPAIR DOUBLER IAW B757 SRM 55-10-01-1A TABLE 1 AN
- [SDR FDEA202207191770](https://openairdocs.org/sdr/FDEA202207191770), Jul 19, 2022: SKIN. CORRODED. #2 PYLON INTERNAL SKIN IS CORRODED ON THE O/B SIDE APPROX 9IN AFT OF ACCESS PANEL 443AR REPAIRED PER FEDEX EA # F-5450-T0369337 - TITLE: NACELLES/PYLON - WING P
- [SDR FDEA202207191772](https://openairdocs.org/sdr/FDEA202207191772), Jul 19, 2022: SUPPORT BRACKET. BENT. RADOME BULKHEAD BRACKET BENT FOR HOLD OPEN RODS FABRICATED SUPPORT BRACKET IAW BAC DWG 141N7835-2 REV F & INSTALLED IAW B757 SRM 51-40-02
- [SDR FDEA202207191769](https://openairdocs.org/sdr/FDEA202207191769), Jul 19, 2022: SKIN. CORRODED. #2 PYLON APPROX. 9IN AFT OF DOOR CUTOUT INTERNAL PYLON SIDE SKIN THRU ACCESS PANEL 443GL IS EXFOILATED REPAIRED PER FEDEX EA # F-5430-T0369607
- [SDR FDEA202207181763](https://openairdocs.org/sdr/FDEA202207181763), Jul 18, 2022: WEB. CORRODED. AFT CABIN FLOOR SUPPORT AT L4 DOOR CORRODED AT FASTENER HOLE BS 1661 BL 54L ACCOMPLISHED FEDEX EA # F-5310-T0369397-P1 : FUSELAGE, MAINFRAME - FLOOR WEB. STA 16
- [SDR FDEA202207181762](https://openairdocs.org/sdr/FDEA202207181762), Jul 18, 2022: PANEL. CRACKED. #1 PYLON PANEL 433LR IS CRACKED IN CENTER AT LATCH. REPAIRED #1 PYLON PANEL 433LR BY REMOVING DAMAGED AREA AT LATCH AND BONDING FIBERGLASS PREPREG REPAIR IAW B7
- [SDR FDEA202207151737](https://openairdocs.org/sdr/FDEA202207151737), Jul 15, 2022: TRANSITION PANEL. CRACKED. LBL 14 TRANSITION PANEL CRACKED AT STATION APPROXIMATELY 1530. REPAIRED TRANSITION PANEL @ STA 1530 IAW B757 SRM 51-70-13-OG SHEET 1 & 2, & B757 SRM 53-60- 53-2
- [SDR FDEA202207151735](https://openairdocs.org/sdr/FDEA202207151735), Jul 15, 2022: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 251MVF IS DAMAGED REPAIRED MAIN CABIN FLOOR PANEL IAW B757 SRM 53-00-50-2R FIG. 201 REPAIR 1.
- [SDR FDEA202207141729](https://openairdocs.org/sdr/FDEA202207141729), Jul 14, 2022: SKIN. GOUGED. L/W AILERON LOWER SURFACE IS GOUGED 13 IN FROM I/B L/E REPAIRED PER B757 SRM 57-60-01-2R FIG 201 REPAIR # 2 SHEET 3
- [SDR FDEA202207111710](https://openairdocs.org/sdr/FDEA202207111710), Jul 11, 2022: NUT PLATE. CORRODED. AFT CABIN NUTPLATE STRAP IS CORRODED AT BS 1682 RBL 32 REMOVED, FABRICATED AND REPLACED NEW NUTPLATE STRAP IAW B757 DWG 146N5300 REV E - DWG 146N5393 REV C , B7
- [SDR FDEA202207101705](https://openairdocs.org/sdr/FDEA202207101705), Jul 10, 2022: SKIN. CRACKED. LW INB LEADING EDGE SKIN BEHIND #5 SLAT AT INB MAIN TRACK CUTOUT IS CRACKED REPAIRED LEFT WING INBOARD LEADING EDGE SKIN BEHIND #5 SLAT AT INBOARD MAIN TRACK CU
- [SDR FDEA202107221842](https://openairdocs.org/sdr/FDEA202107221842), Jul 22, 2021: SLIDE. DAMAGED. UPON ARRIVAL. DOOR OPEN ASSIST BOTTLE DEPLOYED LEFT SIDE. SLIDE LOCK DETACHED FROM GIRT BAR. SLIDE DID NOT DEPLOY. NOTE: F/O DID NOT DIS ARM SLIDE PRIOR TO UN-L
- [SDR FDEA2020090312078](https://openairdocs.org/sdr/FDEA2020090312078), Sep 1, 2020: SWITCH. FAILED. REJECTED T/O FOR CONFIG SPOILERS EICAS WARNING. RAN QRH, TRIED TO T/O AGAIN, SAME ISSUE. RAN QRH AND RETURNED TO GATE. REMOVED SPEED BRAKE HANDLE POSITION SWITC
- [SDR FDEA202007161520](https://openairdocs.org/sdr/FDEA202007161520), Jul 16, 2020: ACTUATOR. INOPERATIVE. GEAR DISAGREE EICAS MESSAGE W/AMBER GEAR CAUTION LIGHT ON TAKEOFF. NO LIGHT IN GEAR HANDLE AND 3 GREEN GEAR LIGHTS EXTINGUISHED. REMOVED NOSE GEAR LOCK ACTUATOR

All 298: https://openairdocs.org/aircraft/N935FD/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 757-2T7 aircraft: https://openairdocs.org/model/boeing-757-2t7/aircraft.md
- The Rolls-Royce RB211-535E4 series engine: https://openairdocs.org/engine/rolls-royce-rb211-535e4-series.md

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