# N968FD: 1995 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: 26274
- Year built: 1995
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 4, 2013
- Certificate issued: April 10, 2013
- Expires: April 30, 2029
- Mode S code: AD7A5F
- 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=968FD
- Page: https://openairdocs.org/aircraft/N968FD

From the FAA registry file of October 21, 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 N968FD.

## FAA accident and incident reports

None matched to N968FD.

## Service difficulty reports (85, newest 50)

As reported by operators and repair stations.

- [SDR FDEA202610061486](https://openairdocs.org/sdr/FDEA202610061486), Oct 6, 2026: BULB. FAILED. FOUND L1 EMERGENCY EXIT SIGN DIM DURING MX PRE-FLIGHT AMM: 33-51-01-2 REMOVED AND REPLACED 11 FAULTY BULBS AT THE L1 EMERGENCY EXIT SIGN AS PER ABOVE REF. (P/N 
- [SDR FDEA202606030667](https://openairdocs.org/sdr/FDEA202606030667), Jun 3, 2026: PRESSURE SWITCH. FAILED. JUST STARTING THE TAKEOFF ROLL GOT C HYD SYS PRESS CAUTION MESSAGE. ABORTED TAKEOFF AND RAN QRH PVD AMM: 29-11-19-4 REMOVED AND REPLACED CTR HYD SYSTEM PRESSURE
- [SDR FDEA202604160456](https://openairdocs.org/sdr/FDEA202604160456), Apr 16, 2026: CONTROL CABLE. OUT OF ADJUST. EXPERIENCED EXTREME UNCOMMANDED PITCH OSCILLATIONS ON CLIMB OUT BETWEEN 3 AND 4 THOUSAND FEET. OSCILLATIONS LASTED 10 TO 15 SECONDS. AIR CRAFT CLEAN CONFIGURATI
- [SDR FDEA202508021357](https://openairdocs.org/sdr/FDEA202508021357), Aug 2, 2025: FLOORBEAM. CORRODED. AFT CARGO COMPT. FLOORBEAM AT BS 1681 LBL 5.0 WITH CORROSION.
- [SDR FDEA202508021356](https://openairdocs.org/sdr/FDEA202508021356), Aug 2, 2025: FLOORBEAM. CORRODED. AFT CARGO COMPT. FLOOR BEAM AT BS 1681 LBL 5.0 WITH CORROSION. THIS REPAIR WAS ACCOMPLISHED FOLLOWING EA # F-5310-T0384258 REV A P1. PROCEDURES.COPY ATTACHED.TI
- [SDR FDEA202507301342](https://openairdocs.org/sdr/FDEA202507301342), Jul 30, 2025: SKIN. DENTED. RIGHT HORIZONTAL STAB. UPPER SKIN WITH DENT BETWEEN STAB STA 104.248 AND STA 152.248 AND BETWEEN FRONT . SPAR AND AUX SPAR. EVALUATED DENT ON RH HORIZONTAL STAB
- [SDR FDEA202507251319](https://openairdocs.org/sdr/FDEA202507251319), Jul 25, 2025: SKIN. BENT. L4 DOOR FWD / LWR CORNER SKIN BENT. REPAIRED L4 DOOR FWD, LWR CORNER SKIN, INSTALLED DOUBLER, FILLER IAW SRM 52-10-01-2R AND EA F - 5210-T0384238 P1. THIS IS MA
- [SDR FDEA202507181263](https://openairdocs.org/sdr/FDEA202507181263), Jul 18, 2025: SEAT TRACK. CORRODED. FLIGHT COMPT SEAT TRACK BETWEEN BS 345.0 TO 365.0 LBL 7.0 WITH CORROSION.
- [SDR FDEA202507181262](https://openairdocs.org/sdr/FDEA202507181262), Jul 18, 2025: SEAT TRACK. CORRODED. FLIGHT COMPART SEAT TRACK BETWEEN BS 345.0 TO BS 365.0 RBL 14.5 WITH CORROSION.
- [SDR FDEA202503110355](https://openairdocs.org/sdr/FDEA202503110355), Mar 11, 2025: BATTERY PACK. FAILED. DURING PREFLIGHT CENTER GALLEY EXIT LIGHT AND L1 DOOR SLIDE LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS POWER SUPPLY BATTERY REF757MM 
- [SDR FDEA202410031419](https://openairdocs.org/sdr/FDEA202410031419), Oct 3, 2024: BOLT. BROKEN. PDIS 968 52-10-0118 03OCT24 13:43 MIA L1 DOOR HINGE S BROKEN RELEASED FOR SERVICE PER MEL : 52-11-01-A CATEGORY : B EXPIRATION : 06OCT24 "MEL 52-11-01-A: L1 DOO
- [SDR FDEA202410031418](https://openairdocs.org/sdr/FDEA202410031418), Oct 3, 2024: HINGE. FAILED. L1 DOOR HINGE S BROKEN INITIAL INSPECTION APPEARS THAT LOWER ARM ASSY - GUIDE-HINGE MECH" DETACHED FROM THE DOOR, THE 4 BOLTS THAT HELD THE SERRADED PLATE ATTAC
- [SDR FDEA202409261375](https://openairdocs.org/sdr/FDEA202409261375), Sep 26, 2024: BOTTLE. EMPTY. R1 DOOR EMERGENCY POWER RESERVOIR DEFLATED. RELEASED FOR SERVICE PER MEL : 52-11-01-A CATEGORY : B EXPIRATION : 29SEP24 "MEL 52-11-01-A: _R1____ (IDENTIFY L1 OR
- [SDR FDEA202307181241](https://openairdocs.org/sdr/FDEA202307181241), Jul 18, 2023: FAN. FAILED. AT CRUISE FL370 WE EXPERIENCED AN ACRID ODOR ELECTRICAL IN NATURE. WE DONNED THE O2 MASKS INITIATED AN EMERGENCY DESCENT AND RAN QRH 8.1.14. WE STOPPED THE CHEC
- [SDR FDEA202206281614](https://openairdocs.org/sdr/FDEA202206281614), Jun 28, 2022: LAMP. INOPERATIVE. ON POSTFLIGHT NOTICED LH SIDE EXTERNAL EMERGENCY LIGHT INOP. RELAMPED 917 AS PER AMM TASK 33-51-06-962-001-001 REV 129.22 OPS CHECK GOOD.
- [SDR FDEA202205181256](https://openairdocs.org/sdr/FDEA202205181256), May 18, 2022: SPACER. CRACKED. MDIS 968 32-41 8125 18MAY22 OPO FACT U DURING DAILY CHECK FOUND THE NLG WHEEL LH SPACER WITH A CRACK WITH 2 INCH. SPACER OF NOSE LANDING GEAR WHEEL LH REPLACED 
- [SDR FDEA202203020401](https://openairdocs.org/sdr/FDEA202203020401), Mar 2, 2022: NONE. NONE. PDIS 968 27-50 7913 02MAR22 HEL FACT U DURING FINAL LANDING CONFIGURATION, UPON SELECTING FLAPS 25, WE RECEIVED A TE FLAPS DISAGREE. THE FLAP HANDLE WAS 25 (CHE
- [SDR FDEA202201190103](https://openairdocs.org/sdr/FDEA202201190103), Jan 19, 2022: TRANSMISSION. TRIPPED. TRAILING EDGE FLAP DISAGREE LIGHT AT FLAPS 20 SELECTING 25. RAN QRH & LANDED. TROUBLEHOT IAW FIM 27-51 FAULT TREE 805, NO FAULT FOUND ON FSEU 1, 2 OR 3. FOUND I
- [SDR FDEA202110182646](https://openairdocs.org/sdr/FDEA202110182646), Oct 18, 2021: CREASE BEAM. CORRODED. MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CREASE BEAM INBD CHORD CORRODED, BETWEEN STA1400 AND STA1620, RBL64.4 COMPLIED WITH FEDEX EA: F-5321-T0364905 PT1,
- [SDR FDEA202110082601](https://openairdocs.org/sdr/FDEA202110082601), Oct 8, 2021: NONE. NONE. FUSELAGE - MAINFRAME - STATION 1640 FUSELAGE FRAME WEB OPEN HOLE HFEC INSPECTION FOUND INBD 2EA HOLES WITH CRACK SIGNAL, AT STGR14RH COMPLIED WITH FEDEX EA: F-5
- [SDR FDEA202109172322](https://openairdocs.org/sdr/FDEA202109172322), Sep 17, 2021: DRIVE ASSY. TRIPPED. ON APPROACH SELECTED FLAPS 25 AND GOT TE FLAP DISAGREE. QRH AND LANDED FLAPS 20. FIM 27-51 FT 808 REV 127.2 APPLIED, FOUND RH INB FLAPDRIVE OVERLOAD POPOUT ACTU
- [SDR FDEA202011262978](https://openairdocs.org/sdr/FDEA202011262978), Nov 26, 2020: LAMP. INOPERATIVE. FLIGHT COMPARTMENT EMERGENCY LIGHT IS NOT WORKING. ENT BY: 624027 RPT BY: 624027 FACT 26NOV20 08:22 MUC U 944, S/N NONE. ACC AMM: 33-51-09-3 COCKPIT EMERGENCY L
- [SDR FDEA202011262977](https://openairdocs.org/sdr/FDEA202011262977), Nov 26, 2020: LIGHT. INOPERATIVE. EMERGENCY SLIDE LIGHT AT DOOR 1 LT IS INOPERABLE. ACC AMM: 33-51-06-2-1 L1 SLIDE EMERGENCY LIGHT LAMP REMOVED AND REPLACED, FUNCTION OK.
- [SDR FDEA202011262975](https://openairdocs.org/sdr/FDEA202011262975), Nov 26, 2020: LAMP. BURNED OUT. MDIS 968 33-50 6639 26NOV20 MUC FACT U. FLIGHT COMPARTMENT EMERGENCY LIGHT IS NOT WORKING. FACT 26NOV20 08:22 MUC U ACC AMM: 33-51-09-3. COCKPIT EMERGENCY LIGHT
- [SDR FDEA202011262974](https://openairdocs.org/sdr/FDEA202011262974), Nov 26, 2020: LAMP. BURNED OUT. MDIS 968 33-50 6638 26NOV20 MUC FACT U. EMERGENCY SLIDE LIGHT AT DOOR 1 L IS INOPERABLE. FACT 26NOV20 08:12 MUC U. ACC AMM: 33-51-06-2-1 L1 SLIDE EMERGENCY LIGH
- [SDR FDEA202009252329](https://openairdocs.org/sdr/FDEA202009252329), Sep 25, 2020: TRANSMISSION. TRIPPED. TRAILING EDGE FLAP DISAGREE EICAS MESSAGE WHEN SELECTING FLAP 20 TO 25. BITE DONE ON ESCU NR 1. FOUND ON EXT FAULTS MSG 221 RIGHT FLAP XNT. TRAILING EDGE FLAP T
- [SDR FDEA2020081861918](https://openairdocs.org/sdr/FDEA2020081861918), Aug 16, 2020: BATTERY PACK. INOPERATIVE. EXTERIOR EMERGENCY LIGHTING AT L1 DOOR NOT WORKING. BATTERY PACK M731 REPLACED AND TESTED IAW AMM 33-51-07-2,
- [SDR FDEA2020081861917](https://openairdocs.org/sdr/FDEA2020081861917), Aug 16, 2020: BATTERY. INOPERATIVE. INTERIOR EMERGENCY LIGHT ABOVE L1 DOOR NOT WORKING. BATTERY PACK M731 REPLACED AND TESTED IAW AMM 33-51-07-2.
- [SDR FDEA201911263098](https://openairdocs.org/sdr/FDEA201911263098), Nov 26, 2019: TEE FITTING. CORRODED. FORWARD CARGO DOOR LOWER INTERCOSTAL OUTER TEE #4 FROM FWD SIDE IS CORRODED EVALUATED CORROSION ON FWD CARGO DOOR LWR. INTERCOSTAL OUTER TEE #4 FROM FWD SIDE FO
- [SDR FDEA201911263097](https://openairdocs.org/sdr/FDEA201911263097), Nov 26, 2019: TEE FITTING. CORRODED. FWD CARGO DOOR LOWER INTERCOSTAL OUTER TEE #2 FROM THE FWD SIDE IS CORRODED EVALUATED CORROSION ON FWD CARGO DOOR LWR. INTERCOSTAL OUTER TEE #2 FROM THE FWD SID
- [SDR FDEA2019111542955](https://openairdocs.org/sdr/FDEA2019111542955), Nov 14, 2019: ACOUSTIC PANEL. PUNCTURED. APU LH SIDE ABOVE OIL COOLING DUCT HAS A PUCTURE HOLE ON ACCUSTIC PANEL. ACCOMPLISHED REPAIR ON APU L/H SIDE ABOVE OIL COOLING DUCT ON ACCUSTIC PANEL (INTERNAL 
- [SDR FDEA201908201954](https://openairdocs.org/sdr/FDEA201908201954), Aug 20, 2019: FLAP SYSTEM. MALFUNCTIONED. ON APPROACH (ABOUT 1500') CALLED FOR FLAPS 25 DEGREES AND THE TRAILING EDGE FLAPS DISAGREE LGT ILLUMINATED. BROKE OFF THE APPROACH, RAN THE QRH AND LANDED FLAPS
- [SDR FDEA2019061751308](https://openairdocs.org/sdr/FDEA2019061751308), Jun 15, 2019: CONTROL ROD. OUT OF ADJUST. THE SLIDE PLACARD DOES NOT COME INTO VIEW WHEN THE LEFT FORWARD DOOR IS ARMED, ADJUSTED AND LUBRICATED L1 DOOR EMERGENCY MECHANISM RETRACTABLE DOOR CONTROL ROD 
- [SDR FDEA2019060391194](https://openairdocs.org/sdr/FDEA2019060391194), May 29, 2019: BALLSCREW. DAMAGED. WHILE COMPLYING WITH TSI 27-50/5006 FOUND OVERLOAD INDICATOR POPPED ON R/H INBOARD TRANSMISSION ASSY ON INBD FLAP INPECTED BALLSCREW WITH A CHEESECLOTH FOR SHAR
- [SDR FDEA201905291180](https://openairdocs.org/sdr/FDEA201905291180), May 29, 2019: WARNING SYSTEM. FALSE ACTIVATION. ON FINAL APP. ATH. EICAS DISPLAYED TE FLAP DISAGREE (WITH FLAPS 20). RAN QRH. PERFORMED FIM 27-51 FAULT 811. UNABLE TO DUPLICATE THE FAULT FLAP SLAT ELEX UNIT 1
- [SDR FDEA201903150644](https://openairdocs.org/sdr/FDEA201903150644), Mar 15, 2019: TRANSDUCER. OUT OF ADJUST. A/P ON IN VNAV, BELOW PATH, THROTTLES IDLE AIRCRAFT NOSE PITCHES DOWN RESULTING IN 6000' FPM DESCENT WITH AIRSPEED INCREASING AND SPEED BRAKES OUT. AIRCRAFT DOE
- [SDR FDEA201902150417](https://openairdocs.org/sdr/FDEA201902150417), Feb 15, 2019: COMPUTER. MALFUNCTIONED. WITH R A/P ON, A/C WENT FROM A 2000 FPM TO A 4500 FPM RATE OF DESCENT. APPROACHING LEVEL OFF ALT PF CLCK IS OFF A/P AND HAND FLEW REMAINDER OF ARRIVAL AND APPRO
- [SDR FDEA201902150416](https://openairdocs.org/sdr/FDEA201902150416), Feb 15, 2019: AUTOLAND SYS. MALFUNCTIONED. PDIS 968 22-20 4737 14FEB19 TLV FACT U LOGPAGES:3011346 3011350 REPEAT EVENT: IN VNAV PATH @ 350, DECENDING TO 210, ACT WENT FROM VNAV PATH TO VNAV SPEED AND PI
- [SDR FDEA2018092102640](https://openairdocs.org/sdr/FDEA2018092102640), Sep 20, 2018: PUMP. MALFUNCTIONED. RT HYD ENG PUMP EICAS DURING FLIGHT AUTO EVENT RECORDED IN FLIGHT SHOWING RIGHT SYSTEM HYDRAULIC PRESSURE AT 1070 PSI, WHILE LEFT SYSTEM WAS AT 2980 PSI, AND CE
- [SDR FDEA2018090502338](https://openairdocs.org/sdr/FDEA2018090502338), Aug 30, 2018: SENSOR. DIRTY. R1 CREW DOOR SLIDE ARMED LIGHT INOP. CLEANED SENSOR AND PERFORMED INSPECTION AND TEST IAW AMM 52-11-25-5-0 SYSTEM OK ACFT RELEASED FOR FLIGHT.
- [SDR FDEA2018082312151](https://openairdocs.org/sdr/FDEA2018082312151), Aug 21, 2018: CONTROL PANEL. MALFUNCTIONED. WITH VERTICAL SPEED SELECTED, RIGHT AUTO PILOT, AND -500FT/MIN SELECTED AT 10,000FT, ACTUAL VERTICAL SPEED WENT TO -2500FT/MIN UNTIL AUTOPILOT WAS DESESECTED IS
- [SDR FDEA2018081752046](https://openairdocs.org/sdr/FDEA2018081752046), Aug 15, 2018: SERVO VALVE. FAILED. DURING DESCENT FROM 15,000 TO 11,000 IN VERT SPEED WITH -1 300 FPM SELECTED, ON THE LEFT AUTOPILOT, THE AIRCRAFT PUSHED OVER TO -3 000FPM. DISCONNECTED THE AUTO
- [SDR FDEA201806151499](https://openairdocs.org/sdr/FDEA201806151499), Jun 15, 2018: WHEEL. LOOSE. NOSEWHEEL STEERING HAD TO BE STEERED TO THE LEFT TO MAINTAIN STRAIGHT COURSE. R&R RT NOSE WHEEL PER MM 32-45-02-4.
- [SDR FDEA201711123237](https://openairdocs.org/sdr/FDEA201711123237), Nov 12, 2017: BEAM. CRACKED. STUB BEAM AT STA 580 IS CRACKED CUTOUT & REMOVED DAMAGE AREA FROM FLOOR SUPPORT BEAM STA 580 LBL 45 UPPER FLANGE AFT IAW SRM 51-10-02 & EA F5310-T0336463 P1. FA
- [SDR FDEA201711023131](https://openairdocs.org/sdr/FDEA201711023131), Nov 2, 2017: FRAME. CRACKED. MAIN CABIN, FRAME BS 1640 CRACKED APROXIMATELY 5/16 INCH LONG, BELOW STRINGER 14L. REPAIRED THE FRAME IAW EA F-5310-T0336394, P1.
- [SDR FDEA201707212016](https://openairdocs.org/sdr/FDEA201707212016), Jul 21, 2017: STRAP. OUT OF POSITION. R1 DOOR WOULD NOT ARM FOUND SLIDE STRAP IN THE WAY OF THE GIRT BAR, STOWED STRAP, OPS CHECKED GOOD IAW MM 25-66-11-2.
- [SDR FDEA201707191994](https://openairdocs.org/sdr/FDEA201707191994), Jul 19, 2017: LAMP. INOPERATIVE. R1 SLIDE LIGHT INOPERATIVE. REPLACED THE LAMPS IAW SMP, OPS CHECKED GOOD.
- [SDR FDEA201610283756](https://openairdocs.org/sdr/FDEA201610283756), Oct 28, 2016: RESERVOIR. LOW PRESSURE. FOUND L1 EMERGENCY POWER DOOR RESERVOIR PSI BELOW LIMITS. R & R THE RESERVOIR IAW MM 52-11-30-4, ACFT OK FOR SERVICE.
- [SDR FDEA201610273704](https://openairdocs.org/sdr/FDEA201610273704), Oct 27, 2016: COVER. MISSING. DURING POST FLIGHT, FOUND EMERGENCY ESCAPE ROPE COVER MISSING ONE LATCH . INSTALLED NEW COVER IAW 25-61-00-4-0. OK FOR SERVICE
- [SDR FDEA201607312695](https://openairdocs.org/sdr/FDEA201607312695), Jul 31, 2016: PROXIMITY SENSOR. DIRTY. L1 DOOR SLIDE LIGHT INOPERATIVE WITH DOOR CLOSED AND SLIDE ARMED. CLEANED SMALL AMOUNT OF DEBRIS FROM GIRT BAR PROXIMITY SWITCHES, CYCLED DOOR ARMING LEVER MANY

All 85: https://openairdocs.org/aircraft/N968FD/reports.md

## Related

- Other Boeing 757-28A aircraft: https://openairdocs.org/model/boeing-757-28a/aircraft.md
- STCs for the Boeing 757-28A: https://openairdocs.org/model/boeing-757-28a/stcs.md
- The Rolls-Royce RB211-535E4 series engine: https://openairdocs.org/engine/rolls-royce-rb211-535e4-series.md

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