# N967FD: 1994 Boeing 757-28A

- Status: Valid registration
- Airframe: [Boeing 757-28A](https://openairdocs.org/model/boeing-757-28a) (registry code 1384976, 249 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: 26269
- Year built: 1994
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 23, 2013
- Certificate issued: June 26, 2012
- Expires: June 30, 2028
- Mode S code: AD76A8
- 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=967FD
- Page: https://openairdocs.org/aircraft/N967FD

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 757-28A)

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 N967FD.

## FAA accident and incident reports

None matched to N967FD.

## Service difficulty reports (77, 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 FDEA202510292106](https://openairdocs.org/sdr/FDEA202510292106), Oct 29, 2025: TRANSMISSION. FAILED. TE FLAP DISAGREE ON APPROACH. ALTERNATE FLAP CHKLST DID NOT WORK. DID QRH TE FLAP ASSEMETRY & LANDED LESS THAN 1 DEGREE FLAPS IAW QRH. PERFORMED FSEU BITE & FSE
- [SDR FDEA202506060847](https://openairdocs.org/sdr/FDEA202506060847), Jun 6, 2025: BATTERY. NOT SEATED. YOW FACT COURIER AREA CENTER EMERGENCY LIGHT AND R1 DOOR EXTERIOR SLIDE LIGHT AND R1 EXIT LIGHT INOP. AMM: 33-51-07-2 TROUBLESHOT SYSTEM AND FOUND POWER SUPPLY 
- [SDR FDEA202405300750](https://openairdocs.org/sdr/FDEA202405300750), May 30, 2024: CONTROL PANEL. FAILED. EMERGENCY LIGHTS "UNARMED" LIGHT DOES NOT ILLUMINATE (EFFECTING INTERIOR EMERGENCY LIGHTS). REMOVE AND REPLACED EMERGENCY LIGHTS/PASSENGER OXYGEN CONTROL PANEL 
- [SDR FDEA202401160078](https://openairdocs.org/sdr/FDEA202401160078), Jan 16, 2024: SLIDE RAFT. INOPERATIVE. L1 DOOR WASN T DISARMED AND DOOR WAS OPENED. SLIDE DID NOT DEPLOY. L1 DOOR WAS OPEN SLIGHTLY BY FLIGHT CREW BEFORE BEING DISARMED, DOOR WAS NOT OPENED ENOUGH TO
- [SDR FDEA202311271944](https://openairdocs.org/sdr/FDEA202311271944), Nov 27, 2023: SEAT TRACK. DAMAGED. SEAT TRACK LOBE DAMAGED AT STA 582 LBL 45 MAJOR REPAIR: FABRICATED NEW SEAT TRACK BAC1520-792 7178T6511 P.O. MA6505860 , PER SAMPLE AND INSTALLED NEW SEAT TRACK
- [SDR FDEA202310241797](https://openairdocs.org/sdr/FDEA202310241797), Oct 24, 2023: SLAT. DELAMINATED. #1 SLAT UPPER SURFACE REPAIR 79" FROM INBOARD EDGE HAS AREA OF DIS-BOND CIRCLED IN BLACK. COMPLETED REPAIR OF #1 SLAT BY EDGE SEALING, PRIMING AND PAINTING REPA
- [SDR FDEA202310241796](https://openairdocs.org/sdr/FDEA202310241796), Oct 24, 2023: BRACKET. CRACKED. RH FWD WHEEL WELL BRACKET CRACKED FOR PANEL SUPPORT OF PANEL-198AR-MWT- 0000358872 : FERGUSON, STEVE M - 25-OCT-2023 03:49 REMOVED OLD CLIP-ANGLE BRACKET(149N75
- [SDR FDEA202307241282](https://openairdocs.org/sdr/FDEA202307241282), Jul 24, 2023: SWITCH. FAILED. PDIS 967 27-80 8802 24JUL23 DTW FACT U AFTER TAKEOFF, AFTER FLAP INDICATION WAS UP, PASSING APPROX 4000 MSL, AN AMBER LE SLAT ASYM POSTED. NO ROLL ASYMMETRY OBS
- [SDR FDEA202304130634](https://openairdocs.org/sdr/FDEA202304130634), Apr 13, 2023: UNKNOWN. UNKNOWN. DURING PREFLIGHT MAIN SMOKE SYSTEM TEST EICAS MESSAGE MAIN CARGO FIRE NOT DISPLAYED MEL 13APR23 00:03 BIL U RELEASED FOR SERVICE PER MEL : 26-16-02-01-B CATEGOR
- [SDR FDEA202302100245](https://openairdocs.org/sdr/FDEA202302100245), Feb 10, 2023: UNKNOWN. UNKNOWN. PDIS 967 32-30 8485 10FEB23 FLL OPEN U AFTER TAKEOFF AND RAISING THE GEAR HANDLE TO UP, RECEIVED GEAR DISAGREE EICAS MESSAGE ALONG WITH GEAR DISCRETE LIGHT. RAN
- [SDR FDEA202107151791](https://openairdocs.org/sdr/FDEA202107151791), Jul 15, 2021: TRUCK. DAMAGED. ANTISKID MSG AFTER TAKEOFF, SUSPECT DUE TO DAMAGE #3 TIRE. R/R L/H MAIN TRUCK IAW AMM 32-11-17-004-0001.
- [SDR FDEA202106251590](https://openairdocs.org/sdr/FDEA202106251590), Jun 25, 2021: ATTACH FITTING. CRACKED. CHECK FOUND RH WING OUTBOARD DRAG FITTING NO. 4# FASTENER HOLE CRACKED REPLACED THE RH WING OUTBOARD DRAG FITTING PER EA:F-5740-T0361981 P1, EA TITLE: WINGS - A
- [SDR FDEA202106151543](https://openairdocs.org/sdr/FDEA202106151543), Jun 15, 2021: SKIN. DENTED. FUSELAGE SKIN EXTERNAL SURFACE FOUND 1EA DENT AT STA1480 - STA1500, S23R - S24R REPAIRED THE DENT AT FUSELAGE SKIN EXTERNAL SURFACE STA1480 - STA1500, S23R - S2
- [SDR FDEA202106141536](https://openairdocs.org/sdr/FDEA202106141536), Jun 14, 2021: CARGO TRACK. CRACKED. MAIN CARGO COMPARTMENT TRACK BEAM CRACKED AT STA1460 - STA1480, RBL45.5 REPAIRED THE CRACKED TRACK BEAM AT MAIN CARGO COMPT. STA1460 - STA1480, RBL45.5 PER B757
- [SDR FDEA2020081071800](https://openairdocs.org/sdr/FDEA2020081071800), Aug 7, 2020: BATTERY PACK. FAILED. R1 DOOR SLIDE EMERGENCY LIGHT AND RIGHT SIDE EMERGENCY LIGHTS IN COURIER COMPARTMENT INOPERATIVE. REPLACED THE BATTERY PACK. INSTALLED AND TESTED OK IAW AMM: 33
- [SDR FDEA2020061981282](https://openairdocs.org/sdr/FDEA2020061981282), Jun 18, 2020: CHARGER. INOPERATIVE. L1 EXTERIOR SLIDE EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY HOLDER ASSY (BATTERY) AND CHARGER ASSY FOR THE LT EXTERIOR SLIDE EMERGENCY LIGHT. OPS CHECK
- [SDR FDEA2020032300601](https://openairdocs.org/sdr/FDEA2020032300601), Mar 20, 2020: GUIDE ARM. DAMAGED. UPON TOUCHDOWN "L FWD ENTRY DOOR" EICAS MESSAGE. DOOR HANDLE ALSO APPEARED TP MOVE AFTER TOUCHDOWN. REPEAT WRITE UP. REMOVED L/H #1 DOOR GUIDE ARM IN REF TO 757
- [SDR FDEA201903140643](https://openairdocs.org/sdr/FDEA201903140643), Mar 14, 2019: RELAY. FAULTY. PDIS 967 36-11 5155 14MAR19 TLH FACT U LOGPAGES:3073947 RIGHT ENGINE BLEED OFF. ACCOMPLISHED QRH PERFORMED AIR SUPPLY BACK PRESSURE CHECK ON RT ENGINE PNEUMATIC
- [SDR FDEA201812203567](https://openairdocs.org/sdr/FDEA201812203567), Dec 20, 2018: LAMP. INOPERATIVE. "SLIDE" LIGHT ON RT ENTRY DOOR DOES NOT COME ON WHEN DOOR IS ARMED. RELAMPED R1 DOOR "SLIDE" LT PER SMP AND B757 WDM 25-66-1. OPENED/CLOSED DOOR SEVERAL TIMES, 
- [SDR FDEA201804261126](https://openairdocs.org/sdr/FDEA201804261126), Apr 26, 2018: TILLER. MALFUNCTIONED. DURING TAXI IN, NOSE WHEEL STEERING TILLER FAILED. IAW JRH, PERFORMED A TAXI CHECK OF THE TILLER, OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR FDEA201803290803](https://openairdocs.org/sdr/FDEA201803290803), Mar 29, 2018: ROPE. UNSECURE. A ROPE IS HANGING OUT OF THE SLIDE AREA ON THE LT FWD ENTRY DOOR. STOWED EXTRA LENGTH OF THE STATIC LINE INTO STOWAGE POCKET IAW AMM 25-66-10-2.
- [SDR FDEA201803030571](https://openairdocs.org/sdr/FDEA201803030571), Mar 3, 2018: STATIC LINE. UNSECURE. L1 DOOR ESCAPE SLIDE HAS LARGE AMOUNT OF SLIDE HARNESS ROPE HANGING BELOW INSIDE INSTALLATION. RESTOWED GIRT BAR STATIC LINE, PERFORMED OPS CHECK OF THE DOOR SL
- [SDR FDEA201801170102](https://openairdocs.org/sdr/FDEA201801170102), Jan 17, 2018: GIRT BAR. DIRTY. L1 ENTRY DOOR WILL NOT ARM. REMOVED GIRT BAR FROM FLOOR FITTINGS. WITH GIRT BAR REMOVED, DOOR ARMING & DISARMIG LEVER OPS SMOOTH AND NO BINDING. MANUALLY SLID F
- [SDR FDEA201801120094](https://openairdocs.org/sdr/FDEA201801120094), Jan 12, 2018: GIRT BAR. DIRTY. L1 DOOR WILL NOT ARM WITH SLIDE ARMED. CLEANED AND LUBRICATED GIRT BAR PER MM 12-21-18-3. OPS CHECK GOOD.
- [SDR FDEA201710293097](https://openairdocs.org/sdr/FDEA201710293097), Oct 29, 2017: CONTROL LEVER. MALFUNCTIONED. GEAR LEVER WOULD NOT MOVE PAST OFF POSITION WHILE ATTEMPTING TO RETRACT THE GEAR. GEAR LEVER MOVED TO THE UP POSITION AFTER SECOND ATTEMPT. GEAR RETRACTION WAS 
- [SDR FDEA201709192614](https://openairdocs.org/sdr/FDEA201709192614), Sep 19, 2017: STRIKER. FAILED. COCKPIT DOOR CAME OPEN DURING TAKEOFF. ON ARRIVAL, APPEARED IT CAN BE FORCED OPEN. REMOVED AND REPLACED COCKPIT DOOR ELECTRIC STRIKER IAW AMM 52-51-03-2-2, CHEC
- [SDR FDEA201706141643](https://openairdocs.org/sdr/FDEA201706141643), Jun 14, 2017: ATTACH FITTING. CRACKED. MAIN CARGO FLOORBEAM ATTACH FITTING AT BS 580, LBL 45.5 IS CRACKED. REMOVED & REPLACED THE FLOORBEAM ATTACH FITTING IAW SRM 51-40-02-0G, & DWG 657N4311, REV - .
- [SDR FDEA201706071587](https://openairdocs.org/sdr/FDEA201706071587), Jun 7, 2017: FRAME. CHAFED. FORWARD LOWER NOSE COMPARTMENT INSIDE DOOR 113AL, BS 231.25 FRAME AND UPPER SURFACE GUSSET PLATE GOUGED AT EDGE OF EXISTING REPAIR. DAMAGE CUT OUT. BL 0 IAW EA 
- [SDR FDEA201706061581](https://openairdocs.org/sdr/FDEA201706061581), Jun 6, 2017: SKIN. GOUGED. GOUGED DENT IN SKIN BS 1540 - 1560, 3 INCHES BELOW STRINGER 3L TO 5 INCHES ABOVE STRINGER 4L. FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGE, FABRICATED REPAIR DOUBL
- [SDR FDEA201606142001](https://openairdocs.org/sdr/FDEA201606142001), Jun 14, 2016: SKIN. DAMAGED. NR 2 ENGINE LT FAN COWL LAND HAS WEAR ON SKIN AT 6 O'CLOCK POSITION, 2016-06-14. R & R DAMAGED SKIN IAW SRM 54-10-00, FIG 20, SHT 4.
- [SDR FDEA201601120131](https://openairdocs.org/sdr/FDEA201601120131), Jan 12, 2016: GIRT BAR. DIRTY. L1 DOOR LIGHT INOPERATIVE WITH DOOR ARMED & GIRT BAR ENGAGED. INSPECTED GIRT BAR AND FOUND DEBRIS ON AFT END OF GIRT BAR PREVENTING ENGAGEMENT. CLEANED GIRT BAR
- [SDR FDEA201507252394](https://openairdocs.org/sdr/FDEA201507252394), Jul 25, 2015: BOTTLE. LOW PRESSURE. L1 DOOR ASSIST BOTTLE LOW. R & R L1 DOOR EMER POWER RESERVOIR IAW AMM 52-11-30-4.
- [SDR FDEA201507212291](https://openairdocs.org/sdr/FDEA201507212291), Jul 21, 2015: COVER. DETACHED. LIFE VEST COVER LT WALL DETACHED. SECURED COVER.
- [SDR FDEA201505131496](https://openairdocs.org/sdr/FDEA201505131496), May 13, 2015: DOOR FRAME. DENTED. FORWARD E & E BAY DOOR FRAME AT BS 231.25 BL0 IS DENTED. COMPILED WITH EA F-5310-T0317555 REV
- [SDR FDEA201407021600](https://openairdocs.org/sdr/FDEA201407021600), Jul 2, 2014: BATTERY. ODOR. AT 38000 FT WE WERE DIVERTING AROUND WX NEAR. WE HAD LARGE LIGHTNING FLASH & SHORTLY AFTER C APTAIN SMELLED ACRID SMELL & THEN THE COCKPIT STARTED TO GET SOME S
- [SDR FDEA201305161009](https://openairdocs.org/sdr/FDEA201305161009), May 16, 2013: FLOORBEAM. CORRODED. FLOORBEAM TEE BS 1641 AND RBL 48-54 CORRODED. . FLOORBEAM WAS R & R IAW DWG 146N5109, SHT1, REV A AND 146N5089 SHT1 REV B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-
- [SDR FDEA201305161008](https://openairdocs.org/sdr/FDEA201305161008), May 16, 2013: FLOORBEAM. CORRODED. FLOORBEAM TEE CORRODED BS 378.5, LBL 26-31. FLOORBEAM WAS REMOVED AND REPLACED AS PER DWG 141N5123 SHT 1 REV A AND 141N5113 SHT 1 REV F. REPAIR CLASSIFIED AS MA
- [SDR FDEA201305130976](https://openairdocs.org/sdr/FDEA201305130976), May 13, 2013: RIB. CRACKED. RIGHT WING SLAT NR 10 OTBD RIB AT OSS 838 FOUND CRACKED. REPAIRED IAW EA F-5720-166070. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201305100961](https://openairdocs.org/sdr/FDEA201305100961), May 10, 2013: FLOORBEAM. CORRODED. MAIN DECK FLOORBEAM BS 377 CORRODED ON UPPER TEE LBL 45.5 - 24.75. FLOORBEAM REMOVED IAW SRM 51-40-02, REV 108 AND NEW FLOORBEAM INSTALLED IAW DWG 141N5113, SHT
- [SDR FDEA201305100960](https://openairdocs.org/sdr/FDEA201305100960), May 10, 2013: FLOORBEAM. CORRODED. MAIN DECK FLOORBEAM BS 377 HAS CORROSION ON UPPER TEE, LBL 12 -BL 0. FLOORBEAM REMOVED IAW SRM 51-40-02, REV 108 AND NEW FLOORBEAM INSTALLED IAW DWG 141N5113, S
- [SDR FDEA201305100959](https://openairdocs.org/sdr/FDEA201305100959), May 10, 2013: FLOORBEAM. CORRODED. MAIN DECK FLOORBEAM BS 395 HAS CORROSION ON UPPER TEE, RBL 6 - 17. REPAIRED IAW EA 757-5315-08-E2135, REV. CLASSIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201305100958](https://openairdocs.org/sdr/FDEA201305100958), May 10, 2013: FLOORBEAM. CORRODED. FLOORBEAM BS 345 UPPER TEE BL 0-LBL 25. WITH CORRODED. REPAIRED IAW EA 757-5315-08-E2133 REV.
- [SDR FDEA201305090951](https://openairdocs.org/sdr/FDEA201305090951), May 9, 2013: FLOORBEAM. CORRODED. FLOORBEAM BS 377 HAS CORROSION ON UPPER TEE LBL 45.5 - 58.22. FLOORBEAM REMOVED IAW SRM 51-40-02 REV 108 AND NEW FLOORBEAM INSTALLED IAW DWG 141N5113 SHT 1 REV 
- [SDR FDEA201305090950](https://openairdocs.org/sdr/FDEA201305090950), May 9, 2013: FLOORBEAM. DAMAGED. FLOORBEAM UPPER TEE AT BS 1300 LBL 24.75 FOUND WITH SCRATCHES AND GOUGED. REPAIRED IAW EA 757-5365-08-E2134.
- [SDR FDEA201305090947](https://openairdocs.org/sdr/FDEA201305090947), May 9, 2013: FRAME. DAMAGED. BS 395, S1-2R FRAME FOUND TWO DOUBLE HOLES. REPAIRED IAW EA 757-5312-08-E2419
- [SDR FDEA201305040907](https://openairdocs.org/sdr/FDEA201305040907), May 4, 2013: FRAME. CHAFED. FRAME AT BS 1280 FOUND DAMAGED BETWEEN S14-15R. COMPLIED WITH EA F-5310-166066. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100. 
- [SDR FDEA201304290887](https://openairdocs.org/sdr/FDEA201304290887), Apr 29, 2013: STRINGER. DAMAGED. STRINGER 3R AT BS 377 FOUND WITH A HOLE ELONGATED DURING PART INSPECTION. COMPLIED WITH EA F-5310-166058. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201304290883](https://openairdocs.org/sdr/FDEA201304290883), Apr 29, 2013: STRINGER. GOUGED. STRINGER 6R BS 418 FOUND GOUGED NEAR FASTENER HOLE. DAMAGED STRINGER 6R REPLACED WITH FABRICATED STRINGER AS PER EA 757-5311-08-E2148. 
- [SDR FDEA201304260859](https://openairdocs.org/sdr/FDEA201304260859), Apr 26, 2013: SKIN. DAMAGED. FUSELAGE SKIN RT SIDE HAS A LIGHTING STRIKE AT BS 395, STR 7R. REPAIRED IAW EA F-5330-168308, PART 1. MAJOR REPAIR.
- [SDR FDEA201304240847](https://openairdocs.org/sdr/FDEA201304240847), Apr 24, 2013: SKIN. DAMAGED. FUSELAGE EXTERIOR SKIN THERE ARE NUMEROUS NICKS AND SCRATCHES AT STA 1681.8 TO 1701 BETWEEN STR 14L AND STR 20L. REPAIRED IAW EA F-5330-166061, PART 1. REPAIR M

All 77: https://openairdocs.org/aircraft/N967FD/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 757-28A aircraft: https://openairdocs.org/model/boeing-757-28a/aircraft.md
- The Rolls-Royce RB211-535E4 series engine: https://openairdocs.org/engine/rolls-royce-rb211-535e4-series.md

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