# N901FD: 1993 Boeing 757-2B7

- Status: Valid registration
- Airframe: [Boeing 757-2B7](https://openairdocs.org/model/boeing-757-2b7) (registry code 1384964, 178 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: 27122
- Year built: 1993
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 28, 2008
- Certificate issued: March 13, 2007
- Expires: December 31, 2029
- Mode S code: AC7364
- 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=901FD
- Page: https://openairdocs.org/aircraft/N901FD

From the FAA registry file of October 22, 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 757-2B7)

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 N901FD.

## FAA accident and incident reports

None matched to N901FD.

## Service difficulty reports (172, 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 FDEA202607110913](https://openairdocs.org/sdr/FDEA202607110913), Jul 11, 2026: CONTROL VALVE. ODOR. FUME EVENT DESCEND THROUGH 20-25K. IT WAS A DIRTY OILY SOCK SMELL. PERFORMED INSPECTION OF HIGH PRESSURE DUCT & INTERMEDIATE PRESSURE DUCT ON BOTH ENGINES. REMO
- [SDR FDEA202511212196](https://openairdocs.org/sdr/FDEA202511212196), Nov 21, 2025: BULB. FAILED. R1 DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOP. RELAMPED R1 DOOR EXTERIOR SLIDE LIGHT IAW AMM 33-51-06-2. OPS CHKD SERVICEABLE.
- [SDR FDEA202509261839](https://openairdocs.org/sdr/FDEA202509261839), Sep 26, 2025: ACTUATOR. FAILED. ON TAKE OFF OUT OF MEM, LANDING GEAR WOULD NOT RETRACT. RAN QRH, LANDING GEAR RETRACTED WITH LOCK OVERRIDE. LANDING GEAR EXTENDED NORMALLY ON APPROACH INTO FSD.
- [SDR FDEA202509261838](https://openairdocs.org/sdr/FDEA202509261838), Sep 26, 2025: PACKING. FAILED. TAKEOFF ROTATION ON DEPARTURE IN MEM DID NOT FEEL NORMAL. IT FELT LIKE THE GEAR TRUCKS DID NOT TILT. AMM: 32-32-15-4 ON INSPECTION OF LEFT TRUCK TILT ACTUATOR, 
- [SDR FDEA202506261062](https://openairdocs.org/sdr/FDEA202506261062), Jun 26, 2025: BATTERY PACK. INOPERATIVE. CENTER AND RIGHT EMERGENCY EXIT SIGNS IN GALLEY FAIL TO LIGHT WHEN TESTED FOR SERVICE CHECK. AMM: 33-51-07-2 REMOVED AND REPLACED FOWARD GALLEY EMERGENCY LIGHTI
- [SDR FDEA202505030711](https://openairdocs.org/sdr/FDEA202505030711), May 3, 2025: LAMP. INOPERATIVE. R1 DOOR EXTERIOR SLIDE LIGHT INOP DURING TEST. AMM: 33-51-06-2-1 RELAMPED IAW ABOVE REF, OPS CHECK GOOD. OK FOR SERVICE. AMM: 33-51-06-2-1 RELAMPED IAW ABOVE RE
- [SDR FDEA202411261744](https://openairdocs.org/sdr/FDEA202411261744), Nov 26, 2024: PROXIMITY SENSOR. LOOSE. R REV ISLN VAL STATUS MESSAGE DURING CLIMB. REVERSER SECURED IN FORWARD THRUST POSITION." MEL: 78-31-01-01 R/H T/R DEACTIVATED PER MEL PROCEDURE. REVERSED MEL D
- [SDR FDEA202409241381](https://openairdocs.org/sdr/FDEA202409241381), Sep 24, 2024: CAM. FAILED. FLIGHT CREW REPORT, L1 DOOR IS DIFFICULT TO CLOSE. REMOVED L1 DOOR LINING IAW AMM 52-11-02-4. FOUND COCKING PUSHROD MISADJUSTED. ADJUSTED COCKING PUSHROD IAW AM
- [SDR FDEA202409051239](https://openairdocs.org/sdr/FDEA202409051239), Sep 5, 2024: AOA. FAILED. ON ARRIVAL, FOUND WHEN STANDBY POWER SWITCH IS PLACED TO BATTERY, LOST ALTITUDE, SPEED & VERTICAL SPEED INFO & SCALE ON CAPT PFD & TAS ON CAPT ND. 1ST OFFICER W
- [SDR FDEA202408121118](https://openairdocs.org/sdr/FDEA202408121118), Aug 12, 2024: DOOR. BINDING. THE L1 DOOR IS DIFFICULT TO OPEN. FACT 12AUG24 23:13 CDG AMM: 52-11-00-6 PERFORMED FAST CHECK FOR THE CORRECT OPERATION OF THE DOOR ,TORQUE WITHIN LIMITS. AC/OK
- [SDR FDEA202408091117](https://openairdocs.org/sdr/FDEA202408091117), Aug 9, 2024: GUIDE ARM. FAILED. MDIS 901 52-10 7107 09AUG24 01:28 CDG FACT DURING POSTFLIGHT FOUND L1 DOOR HARD TO CLOSE FROM INSIDE (INTERIOR HANDLE) SHGN 09AUG24 02:20 CDG AMM: 52-11-04-2 AM
- [SDR FDEA202406010760](https://openairdocs.org/sdr/FDEA202406010760), Jun 1, 2024: SKIN. DELAMINATED. APU COMPARTMENT RH INSIDE WALL SKIN REPAIR DELAMINATED DOET 42-024. REPAIRED IAW SRM 51-70-10-2R AND EA F-5330-T0801330 FUSELAGE PLATES AND SKINS APU COMPARTMEN
- [SDR FDEA202406010759](https://openairdocs.org/sdr/FDEA202406010759), Jun 1, 2024: SKIN. DELAMINATED. AFTER ACCOMPLISHING DELAMINATION REPAIR ON R/H SIDE APU INSIDE WALL SKIN A NEW AREA OF DELAMINATION WAS FOUND DURING POST REPAIR TAP TEST ON THE OUTER SKIN ON T
- [SDR FDEA202405220715](https://openairdocs.org/sdr/FDEA202405220715), May 22, 2024: FLOORBOARD. DAMAGED. MAIN DECK CARGO COMPT FLOORBOARD PANEL 251MWF DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 251MWF ON VTMAE TRAVELER #T24/1755537 IAW DWG SRZ-25-005 REVISION R,
- [SDR FDEA202405220714](https://openairdocs.org/sdr/FDEA202405220714), May 22, 2024: FLOORBOARD. DAMAGED. MAIN DECK CARGO COMPT FLOORBOARD PANEL 251MVF BROKEN. FABRICATED ZONE 250 FLOORBOARD PANEL 251MVF ON VTMAE TRAVELER #T24/1755536 IAW DWG SRZ-25-005 REVISION R, 
- [SDR FDEA202405210710](https://openairdocs.org/sdr/FDEA202405210710), May 21, 2024: STRAP. CRACKED. FLOOR BEAM STABILIZATION STRAP AT STA 377.7 LEFT SIDE OF NOSE WHEEL WELL CRACKED AT FASTENERS IN FLOOR BEAM. REMOVED DAMAGED STRAP IAW SRM 51-40-02 FABRICATED S
- [SDR FDEA202405180686](https://openairdocs.org/sdr/FDEA202405180686), May 18, 2024: SKIN. DENTED. FOR TRACKING PURPOSE, REPAIR ASSOCIATED WITH EA F-5210-T0371765 PT3. ACCOMPLISHED REPAIR ON EA F-5210-T0371765 PT 3. THIS N/R IS FOR TRACKING PURPOSE ONLY. EA F
- [SDR FDEA202401190087](https://openairdocs.org/sdr/FDEA202401190087), Jan 19, 2024: GIRT BAR. OUT OF POSITION. LEFT CREW ENTRANCE DOOR WOULD NOT FULLY CLOSE AND ARM. AMM: 25-66-01-4 REINSTALLED GIRT BAR PER MM 25-66-01-4.
- [SDR FDEA202308171454](https://openairdocs.org/sdr/FDEA202308171454), Aug 17, 2023: CYLINDER. FAILED. L1 MAIN CABIN EXIT DOOR INOP REPLACED NO 1 PASSENGER DOOR EMERGENCY POWER RESERVOIR IAW AMM 52-11-30-4. ITEM REMOVED FROM MEL.
- [SDR FDEA202307011144](https://openairdocs.org/sdr/FDEA202307011144), Jul 1, 2023: BATTERY. UNKNOWN. MDIS 901 33-50 6224 01JUL23 BSL FACT U SVC CHECK, NO EMERGENCY LIGHT ON DOOR 1L (EXTRERIOR AND INTERIOR) R/I 01JUL23 11:36 BSL U REASON CODE : PREMATURE REMOVAL
- [SDR FDEA202307011143](https://openairdocs.org/sdr/FDEA202307011143), Jul 1, 2023: UNKNOWN. UNKNOWN. DOOR 1L, EMERGENCY "EXIT" SIGN, X6 BULB U/S "EXIT" SIGN STILL VISIBLE AND CLEAR (INFO: PLZ SEE MDIS 33-40-6224 FOR BSL/01JUL/R&R BATTERY PACK POWER SUPPLY M0073
- [SDR FDEA202306271119](https://openairdocs.org/sdr/FDEA202306271119), Jun 27, 2023: UNKNOWN. UNKNOWN. LEFT CREW ENTRANCE DOOR IS VERY HARD TO CLOSE AND ARM THE SLIDE. SOMETIMES THE ARMING HANDLE GETS STUCK HALFWAY. PERFORMED SOME TESTS/INSPECTIONS AS PER AMM 52-
- [SDR FDEA202305110871](https://openairdocs.org/sdr/FDEA202305110871), May 11, 2023: BATTERY. FAILED. AED SHOW RED CROSS (LOW BATTERIE) MEL 11MAY23 22:51 VIE U RELEASED FOR SERVICE PER MEL : 25-64-01-03-B CATEGORY : D EXPIRATION : 08SEP23 "MEL 25-64-01-03-B: AUT
- [SDR FDEA202302010197](https://openairdocs.org/sdr/FDEA202302010197), Feb 1, 2023: NOT ENTERED. NOT ENTERED. PDIS 901 52-10 5844 01FEB23 CDG FACT U LEFT ENTRY DOOR SLIDE ARMING HANDLE REQUIRES EXCESSIVE FORCE TO MOVE. FACT 02FEB23 00:21 CDG U AMM: 12-21-18-3 INSPECTION
- [SDR FDEA202210262675](https://openairdocs.org/sdr/FDEA202210262675), Oct 26, 2022: LAMP. BURNED. MDIS 901 33-50 5555 26OCT22 BER FACT U DOOR 1R SLIDE LIGHT U/S FACT 26OCT22 10:09 BER U DOOR 1R SLIDE LIGHR RELAMPED. FUNCTION OK. AMM 33-51-06-2-2 REV 129 DOOR
- [SDR FDEA202207051704](https://openairdocs.org/sdr/FDEA202207051704), Jul 5, 2022: PANEL. DAMAGED. ENG NO 2 INBORD C-DUCT THERE ARE SEPARATIONS ON THE AFT SIDE OF PANEL NO 425BL PERFORMED WET LAYUP REPAIR PER AMM 78-31-10-8-1, PARAGRAPH 3,FIG. 803 (SHEET 3). 
- [SDR FDEA202206191913](https://openairdocs.org/sdr/FDEA202206191913), Jun 19, 2022: FLOOR SUPPORT. CORRODED. MULTIPLE CORROSIONS WERE FOUND ON FWD CARGO FLOOR STRUCTURE UPPER LOCATED AT STA 510 STA 840 RBL 19 PERFORMED TYPICAL FORMED SECTION REPAIR PER SRM 51-70-11, GE
- [SDR FDEA202206151943](https://openairdocs.org/sdr/FDEA202206151943), Jun 15, 2022: SKIN. CORRODED. L/H WING UPPER SKIN DRAG FITTING BOLTS HOLES HAVE CORROSION HOLES #1, #2 , #4 , #7 , #9 , #10 #12, #14, #15 , #16 , #17, AND #18 ACCOMPLISHED PER E.A :F-5730-T0
- [SDR FDEA202206151931](https://openairdocs.org/sdr/FDEA202206151931), Jun 15, 2022: SEAT TRACK. CORRODED. CABIN BETWEEN STA 1080-1180 FOUND CORROSION ON SEAT TRACK BETWEEN RBL 45 DAMAGED PART REMOVED AND NEW PART P/N FX-144N5021-1 INSTALLED PER SRM 51-40-02
- [SDR FDEA202206151912](https://openairdocs.org/sdr/FDEA202206151912), Jun 15, 2022: SEAT TRACK. CORRODED. CABIN BETWEEN STA 1180-1200 FOUND CORROSION ON SEAT TRACK UPPER FLANGE BETWEEN RBL 45 DAMAGED PART REMOVED AND NEW PART P/N FX-146N5130-2 (SEAT TRACK) INSTALLED
- [SDR FDEA202206151881](https://openairdocs.org/sdr/FDEA202206151881), Jun 15, 2022: FLOORBEAM. CORRODED. CABIN STA 1200 FOUND CORROSION ON FLOOR BEAM UPPER FLANGE BETWEEN LBL 24-45 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX EA# F-5300-T0369445, FLOOR BEAM STA 1200,
- [SDR FDEA202206151875](https://openairdocs.org/sdr/FDEA202206151875), Jun 15, 2022: CREASE BEAM. CORRODED. FOUND CORROSION ON CREASE BEAM INBOARD CHORD BETWEEN STA 800-820 LBL 24 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0369731, SEC 43, FLOOR BEAM STR
- [SDR FDEA202206151874](https://openairdocs.org/sdr/FDEA202206151874), Jun 15, 2022: SEAT TRACK. CORRODED. FOUND CORROSION ON SEAT TRACK BETWEEN STA 1020 TO 1080 AT LBL 58 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5320-T0369373 SEAT TRACK BETWEEN STA 1080 AN
- [SDR FDEA202206151872](https://openairdocs.org/sdr/FDEA202206151872), Jun 15, 2022: CREASE BEAM. CORRODED. CABIN STA 1360-1400 FOUND CORROSION ON CREASE BEAM RBL 64 WORK ACCOMPLISHMENT IN ACCORDANCE WITH FEDEX E.A # F-5310-T0369769, CREASE BEAM INNER CHORD, STA 1370-
- [SDR FDEA202206151868](https://openairdocs.org/sdr/FDEA202206151868), Jun 15, 2022: SEAT TRACK. CORRODED. FOUND CORROSION ON SEAT TRACK BETWEEN STA 1020-1040 RBL 24 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0369328 A, HEAVY CORROSION AT RBL 24.75 FLOO
- [SDR FDEA202206151867](https://openairdocs.org/sdr/FDEA202206151867), Jun 15, 2022: SEAT TRACK. CORRODED. FOUND CORROSION ON UPPER FLANGE OF SEAT TRACK BETWEEN STA 920-1020 AT LBL 45 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5340-T0369647, SEC 44, FLOOR BEA
- [SDR FDEA202206141930](https://openairdocs.org/sdr/FDEA202206141930), Jun 14, 2022: SEAT TRACK. CORRODED. FOUND CORROSION ON SEAT TRACK AT STA 1320 TO 1540 RBL 25 DAMAGED SEAT TRACK REMOVED AND PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52-2R, FIG. 201, REPAIR OPTION
- [SDR FDEA202206141929](https://openairdocs.org/sdr/FDEA202206141929), Jun 14, 2022: SEAT TRACK. CORRODED. FOUND CORROSION ON SEAT TRACK AT STA 1420-1620 RBL 58 DAMAGED SECTION REMOVED AND SET TRACK REPAIR PERFORMED PER SRM 53-00-52-2R, FIG. 201, OPTION 1 MAJOR REPAI
- [SDR FDEA202206141927](https://openairdocs.org/sdr/FDEA202206141927), Jun 14, 2022: SEAT TRACK. CORRODED. FOUND CORRODED SEAT TRACK BETWEEN STA 1280-1320 LBL 45 DAMAGED SEAT TRACK REMOVED AND NEW REPAIR SETA TRACK INSTALLED PER SRM 53-00-52-2R, FIG. 201, OPTION 1 MA
- [SDR FDEA202206141911](https://openairdocs.org/sdr/FDEA202206141911), Jun 14, 2022: SEAT TRACK. CORRODED. FOUND CORROSION ON SEAT TRACK UPPER FLANGE BETWEEN STA 530-660 AT RBL 58 PERFORMED SETA TRACK REPAIR PER SRM 53-00-52-2R, FIG 201, REPAIR OPTION 2 MAJOR REPAIR
- [SDR FDEA202206141910](https://openairdocs.org/sdr/FDEA202206141910), Jun 14, 2022: SEAT TRACK. CORRODED. FOUND CORROSION ON SEAT TRACK UPPER FLANGE BETWEEN STA 510-570 AT RBL 45 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52-2R, FIG 201, REPAIR OPTION 2 MAJOR REPAIR
- [SDR FDEA202206141879](https://openairdocs.org/sdr/FDEA202206141879), Jun 14, 2022: SEAT TRACK. CORRODED. FOUND CORRODED CROWN AREA OF SEAT TRACK AT STA 1600 TO 1640 RBL 25 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52-2R FIG 201 REPAIR 1 MAJOR REPAIR
- [SDR FDEA202206141871](https://openairdocs.org/sdr/FDEA202206141871), Jun 14, 2022: SEAT TRACK. CORRODED. FOUND CORRODED SEAT TRACK BETWEEN STA 1280-1320 RBL 45 DAMAGED SETA TRACK REMOVED AND NEW FAB. SEAT TRACK PER SRM 53-00-53-2R( REF. SRM 53-60-52, I.D 1) INSTALL
- [SDR FDEA202206141870](https://openairdocs.org/sdr/FDEA202206141870), Jun 14, 2022: SEAT TRACK. CORRODED. FOUND CORRODED CROWN AREA AND SEAT TRACK LOWER FLANGE BETWEEN STA 1540-1640 LBL 25 PERFORMED SEAT TRACK REPAIR, USING 1 EA SEAT TRACK SECTION , 2 EA ANGLES AND 
- [SDR FDEA202206141869](https://openairdocs.org/sdr/FDEA202206141869), Jun 14, 2022: SEAT TRACK. CORRODED. FOUND CORROSION ON SEAT TRACK AT STA 1320 TO 1540 RBL 45 PERFORMED SEAT TRACK REPAIR , USING 1 EA SETA TRACK SECTION , 2 EA ANGLES, 1 EA STRAP PER SRM 53-00-52-
- [SDR FDEA202206121656](https://openairdocs.org/sdr/FDEA202206121656), Jun 12, 2022: FLOOR PANEL. DENTED. DENT ON MAIN DECK FLOOR PANEL P/N 11864182-26 STA 1540-1620 RBL 48 PERFORMED REPAIR PER SRM 53-00-50-2R, PARAGRAPH 3.B, FIG. 201, DETAIL I AND II. SRM REV. 135.
- [SDR FDEA202206121655](https://openairdocs.org/sdr/FDEA202206121655), Jun 12, 2022: FLOOR PANEL. DENTED. DENT ON MAIN DECK FLOOR PANEL P/N 11862182-16 STA 740-780 LBL 24 PERFORMED REPAIR PER SRM 53-00-50-2R,PARAGREPH 3.B, FIG. 201, DETAIL I AND II. SRM REV. 135.0. 
- [SDR FDEA202206121654](https://openairdocs.org/sdr/FDEA202206121654), Jun 12, 2022: FLOOR PANEL. DENTED. DENT ON MAIN DECK FLOOR PANEL P/N 11862182-2 STA 440-560 RBL 48 PERFORMED REPAIRS PER SRM 53-00-50-2R, PARAGRAPH 3.B, FIG. 201, DETAIL I AND II. SRM REV. 135.0.
- [SDR FDEA202206071607](https://openairdocs.org/sdr/FDEA202206071607), Jun 7, 2022: FLOOR PANEL. WORN. FLOOR PANEL PN 141N5370-38 MAF 222 FOUND WORN REPLACED FLOOR PANEL PER DWG SRZ-25-005. P/N:FX141N5370-38 222MAF. MAJOR REPAIR.
- [SDR FDEA202206071606](https://openairdocs.org/sdr/FDEA202206071606), Jun 7, 2022: FLOOR PANEL. WORN. FLOOR PANEL PN 11861182-3 MBF 222 FOUND WORN REPLACED FLOOR PANEL PER DWG SRZ-25-005. P/N:FX11861182-3 222MBF. MAJOR REPAIR.

All 172: https://openairdocs.org/aircraft/N901FD/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 757-2B7 aircraft: https://openairdocs.org/model/boeing-757-2b7/aircraft.md
- The Rolls-Royce RB211-535E437 engine: https://openairdocs.org/engine/rolls-royce-rb211-535e437.md

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