# N928FD: 1989 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: 24369
- Year built: 1989
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 12, 2011
- Certificate issued: June 16, 2010
- Expires: July 31, 2027
- Mode S code: ACDC63
- 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=928FD
- Page: https://openairdocs.org/aircraft/N928FD

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 N928FD.

## FAA accident and incident reports

None matched to N928FD.

## Service difficulty reports (102, 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 FDEA202608211220](https://openairdocs.org/sdr/FDEA202608211220), Aug 21, 2026: OXYGEN MASK. NO TEST. DURING MX PREFLIGHT; CAPTAINS O2 MASK FAILS "PRESS TO TEST." REPLACED CAPT'S FULL FACE O2 MASK IAW B757 AMM CH. REF. LISTED ABOVE. OPS AND LEAK CKS GOOD. A/C OK
- [SDR FDEA202608211213](https://openairdocs.org/sdr/FDEA202608211213), Aug 21, 2026: OXYGEN MASK. NO TEST. DURING MX PREFLIGHT, CAPTAINS O2 MASK FAILED A PRESS TO TEST. PREMATURE REMOVAL/INSTALLATION. REPLACED CAPT'S FULL FACE O2 MASK IAW AMM 35-11-51-4-99. OPS & LEA
- [SDR FDEA202604020391](https://openairdocs.org/sdr/FDEA202604020391), Apr 2, 2026: BATTERY PACK. INOPERATIVE. ON PREFLIGHT FOUND R1 DOOR SLIDE LIGHT INOPERATIVE. AMM 33-51-06-2-1, AMM 33-51-07-2, & AMM 33-51-07-862-036. REPLACED BULB IN R1 DOOR SLIDE LIGHT IAW MM 33-51-
- [SDR FDEA202511112157](https://openairdocs.org/sdr/FDEA202511112157), Nov 11, 2025: GIRT BAR. DAMAGED. L1 DOOR WILL NOT OPEN. TROUBLESHOT L1 DOOR AND DISCOVERED FWD END OF GIRT BAR JAMMED IN ARMING SLIDER. REMOVED AND REPLACED L1 DOOR GIRT BAR REMOVED IAW AMM 25-
- [SDR FDEA202503110363](https://openairdocs.org/sdr/FDEA202503110363), Mar 11, 2025: FLOOR PANEL. DAMAGED. FLOOR PANEL #252MWF HAS DAMAGE AND MISSING INSERTS, R/H AFT O/B MAIN CABIN FLOOR PANEL. FABRICATED FLOOR PANEL #252MWF ON VTMAE TRAVELER #T25/1800902 IAW STMAE 
- [SDR FDEA202503110362](https://openairdocs.org/sdr/FDEA202503110362), Mar 11, 2025: FLOOR PANEL. DAMAGED. FLOOR PANEL #251MXF AFT MAIN CABIN L/H O/B HAS DAMAGE/MISSING INSERTS. FABRICATED FLOOR PANEL #251MXF ON VTMAE TRAVELER #T25/1800901 IAW STMAE DWG. #11864182 RE
- [SDR FDEA202502280308](https://openairdocs.org/sdr/FDEA202502280308), Feb 28, 2025: SEAT TRACK. DAMAGED. SEAT TRACK AT FS 980 BL 0 HAS DAMAGE. REMOVED AND REPLACED SEAT TRACK BETWEEN STA 879 TO 1065 BL 0 IAW SRM 51-40-02 FROM MATERIAL BAC 1520-2473 BATCH # 00024258
- [SDR FDEA202501100051](https://openairdocs.org/sdr/FDEA202501100051), Jan 10, 2025: GUST LOCK. FAILED. R1 DOOR GUST LOCK INOP. R&R BROKEN GUST LOCK ON R1 DOOR. OPS CHK GOOD. OK FOR SVC.
- [SDR FDEA202501080038](https://openairdocs.org/sdr/FDEA202501080038), Jan 8, 2025: FLAP SYSTEM. MALFUNCTIONED. TE FLAP DISAGREE, EMERGENCY DECLARED. ON INITIAL TROUBLESHOOTING NO EICAS MSG NOTED FOR TE FLAP DISAGREE. PUT FLAPS BACK TO NORMAL CONFIG FROM ALT MODE. BITE CH
- [SDR FDEA202409231342](https://openairdocs.org/sdr/FDEA202409231342), Sep 23, 2024: BOTTLE. LOW PRESSURE. ON SERVICE CHECK FOUND R1 DOOR EMERGENCY RESEVOIR BELOW MINIMUM REQUIRED PRESSURE. AMM: 52-11-30-4 REMOVED AND REPLACED RI DOOR ASSIST BOTTLE PER ABOVE B757 REF
- [SDR FDEA202405310754](https://openairdocs.org/sdr/FDEA202405310754), May 31, 2024: FERRULE. DAMAGED. R1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. AMM: 33-51-06-2-1 RELAMPED, NO HELP. FOUND LIGHT WOULD INTERMITTENTLY COME ON WHEN MANIPULATING LIGHT ASSY. REMOVE
- [SDR FDEA202401250111](https://openairdocs.org/sdr/FDEA202401250111), Jan 25, 2024: ENGINE. INOPERATIVE. PDIS 928 73-22 1096 25JAN24 MEM OPEN U AT CRUISE, FL360, #1 ENG EPR DID NOT INDICATE PROPERLY. THE WHITE EPR NEEDLE WAS FULL POWER ABOVE THE DIAL, THE POWER STR
- [SDR FDEA202212012864](https://openairdocs.org/sdr/FDEA202212012864), Dec 1, 2022: CONTROL PANEL. FAILED. OVERHEAD COCKPIT EMERGENCY LIGHTS PANEL WON'T TEST IAW AMM 33-51-08-4. REMOVED AND REPLACED P5 EMEGENCY LIGHTS PANEL IAW AMM 33-51-08-4. OPS CHECKED NORMAL. ACF
- [SDR FDEA202110162545](https://openairdocs.org/sdr/FDEA202110162545), Oct 16, 2021: WARNING MESSAGE. FALSE ACTIVATION. TRAILING EDGE FLAP DISAGREE. HANDLE AT 20. INDICATOR SAID BOTH FLAPS AT 15. RAN QRH. RECONFIGURED FLAPS FROM ALT TO REGULAR AND RAISED FLAPS. OPERATED FLAPS THR
- [SDR FDEA202105231364](https://openairdocs.org/sdr/FDEA202105231364), May 23, 2021: FAIRING. CRACKED. #2 ENG PYLON O/B LOWER FLEXABLE FAIRING CLOSEOUT PANEL IS CRACKED ABOVE EXHAUST NOZZLE REMOVED AND REPLACED PANEL PER DWG # 311N5137
- [SDR FDEA202105201323](https://openairdocs.org/sdr/FDEA202105201323), May 20, 2021: STOP FITTING. CRACKED. R2 DOOR, 3RD FROM BOTTOM DOOR STOP IS CRACKED REMOVED AND REPLACED R-2 DOOR PER FEDEX B757 AMM 52-11-01-4
- [SDR FDEA202105181289](https://openairdocs.org/sdr/FDEA202105181289), May 18, 2021: WEB. DENTED. MCD AFT PRESSURE RELIEF DOOR INTERNAL CLOSE OUT WEB HAS SEVERAL INTERNALLY PROTRUDING DENTS AT THE UPPER EDGE OF THE WEB BETWEEN WL 210 AND 220, BETWEEN STA 580
- [SDR FDEA202105181288](https://openairdocs.org/sdr/FDEA202105181288), May 18, 2021: WEB. DENTED. MCD FWD PRESSURE RELIEF DOOR INTERNAL CLOSE OUT WEB HAS SEVERAL INTERNALLY PROTRUDING DENTS AT THE UPPER EDGE OF THE WEB BETWEEN WL 210 AND 220, BETWEEN STA 500
- [SDR FDEA202105121204](https://openairdocs.org/sdr/FDEA202105121204), May 12, 2021: ATTACH ANGLE. CRACKED. LMLG WHEEL WELL FWD EDGE WING TO BODY PANEL ATTACH CLIP IS CRACKED 32" OUTBOARD OF KEEL BEAM. REMOVED AND REPLACED CRACKED CLIP WITH NEW CLIP PER BAC DWG 149N75
- [SDR FDEA2020043090838](https://openairdocs.org/sdr/FDEA2020043090838), Apr 29, 2020: FIRE WARNING. FALSE ACTIVATION. UPON DESCENT INTO DESTINATION APPROXMATELY FL 180 IN IMC/RAIN RT ENG FIRE WARNING AND LIGHT CAME ON. RAN PHASE ONES AND QRH FOR RT ENG FIRE. UPON RT ENGINE SHUT
- [SDR FDEA201909272357](https://openairdocs.org/sdr/FDEA201909272357), Sep 27, 2019: LANYARD. OUT OF POSITION. RT CABIN ENTRY DOOR WILL NOT ARM FOUND LANYARD CORD STUCK IN GIRT BAR, PROPERLY STOWED LANYARD CORD . DOOR ARM LIGHT OPS CHECKED NORMAL PER AMM 52-71-00-5
- [SDR FDEA2019042290862](https://openairdocs.org/sdr/FDEA2019042290862), Apr 19, 2019: BRACKET. CORRODED. BS 1410, AFT CARGO DOOR, LOWER FRAME SUPPORT BRACKET HAS EXFOILIATING CORROSION, 1 INCH BY 1 INCH SIZE. BOTH SIDES OF BRACKET ARE CORRODED.
- [SDR FDEA201904160811](https://openairdocs.org/sdr/FDEA201904160811), Apr 16, 2019: CREASE BEAM. CORRODED. MAIN CABIN CREASE BEAM STA. 860-880 RBL64.20 HAS CORROSION REMOVED CORR. ON CREASE BEAM STA 860-880 RBL 64.20 IAW B757 SRM 51-10-02. ORIG MAT .071 REM .051 LOSS
- [SDR FDEA201904160810](https://openairdocs.org/sdr/FDEA201904160810), Apr 16, 2019: SEAT TRACK. CORRODED. CORROSION SEAT TRACK FLANGE MAIN CABIN STA. 1540 RBL 45.50 PERFORMED SEAT TRACK REPAIR AT RBL 45.50 BETWEEN BS 1500-1540 IAW B757 SRM 53-00-52- 2R FIG 201 REPAI
- [SDR FDEA201804241109](https://openairdocs.org/sdr/FDEA201804241109), Apr 24, 2018: TUBE. DAMAGED. PDIS 928 76-00 6718 24APR18 BNA OPEN U LOGPAGES:2252904 AT CRUISE NOTICED L EPR PEGGED. FUEL FLOW AT 1.5. LOTS OF RIGHT RUDDER. A/S STARTED TO DECREASE. NO EICA
- [SDR FDEA2018042601109](https://openairdocs.org/sdr/FDEA2018042601109), Apr 24, 2018: TUBE. DAMAGED. DURING CRUISE, NOTICED THE LT EPR PEGGED. FUEL FLOW AT 1.5. A LOT OF RIGHT RUDDER. A/S STARTED TO DECREASE. NO EICAS. LT ENG DID NOT RESPOND TO THROTTLE MOVEMEN
- [SDR FDEA201804090955](https://openairdocs.org/sdr/FDEA201804090955), Apr 9, 2018: SEAT TRACK. GOUGED. MAIN CABIN SEAT TRACK LBL 45.5, BS 580 CROWN AREA DAMAGED. INSTALLED A NEW SECTION OF SEAT TRACK IAW DWG 143N5090, REV-, SRM 51-40-05-0G, SRM 51-40-02-0G, SRM 5
- [SDR FDEA201804090954](https://openairdocs.org/sdr/FDEA201804090954), Apr 9, 2018: FLOORBEAM. CRACKED. MAIN CABIN STA 580 FLOORBEAM STUB FITTING HAS A CRACK ON AFT FLANGE AT LBL 45. COMPLIED WITH EA F-5310-T0339360 P1.
- [SDR FDEA201802010285](https://openairdocs.org/sdr/FDEA201802010285), Feb 1, 2018: TUBE. LEAKING. DURING CLIMB THROUGH FL 270, THE LEFT ENGINE INDICATED N1 OF 82% VS N1 95%, FOR THE RIGHT ENGINE. LEFT EGT WAS 120DEG. LOWER, N2 WAS 10% LOWER. RUDDER TRIM OF 4
- [SDR FDEA201707292081](https://openairdocs.org/sdr/FDEA201707292081), Jul 29, 2017: ENGINE. FLAMED OUT. RT ENGINE FLAMED OUT ON ARRIVAL AT 15000 FT. AT BLOCK IN, THE RT ENG LP PUMP STATUS MESSAGE INDICATED. REMOVED AND REPLACED THE HIGH PRESSURE FUEL PUMP, ENGINE 
- [SDR FDEA201706161686](https://openairdocs.org/sdr/FDEA201706161686), Jun 16, 2017: GOVERNOR. MALFUNCTIONED. RIGHT ENGINE FAILED AT APPROXIMATELY 7000' MSL DURING DESCENT. INITIALLY NOTED RIGHT GENERATOR OFF, THEN UTILITY BUSSES, AUTOTHROTTLES, AND AUTOPILOT. ENGINE WA
- [SDR FDEA201704211249](https://openairdocs.org/sdr/FDEA201704211249), Apr 21, 2017: TERMINAL. LOOSE. EMERGENCY LIGHTS FAIL TO TEST WITH SWITCH ABOVE L1 DOOR IN COURIER COMPT. FOUND TERMINAL END OF WIRE W3532-0036-20 LOOSE AT GROUND STUD GD1420-DC. TIGHTENED TER
- [SDR FDEA201704111132](https://openairdocs.org/sdr/FDEA201704111132), Apr 11, 2017: SKIN. DAMAGED. DURING REMOVAL OF INBOARD MAIN FLAP OUTBOARD FLAP FAIRING FWD INBOARD ATTACH BRACKET. FOUND THE SKIN MOUNT BOLT HOLES WORN AND ELONGATED. COMPLIED WITH EA 5750-
- [SDR FDEA201704061099](https://openairdocs.org/sdr/FDEA201704061099), Apr 6, 2017: BRACE. CRACKED. TWO CRACK INDICATIONS AT THE INSIDE HOLES ON AFT SIDE OF NR 1 PYLON DIAGONAL BRACE FITTING LOWER SURFACE IN ALUMINUM ONLY. COMPLIED WITH EA F-5450-T0332370 B P1
- [SDR FDEA201703301014](https://openairdocs.org/sdr/FDEA201703301014), Mar 30, 2017: FITTING. CRACKED. MAIN CABIN FLOORBEAM BS 580, STUB BEAM FITTING AT LBL 44.5 HAS A CRACK IN UPPER RADIUS OF TOP FLANGE. REMOVED AND REPLACED THE STUB BEAM FITTING IAW DWG 657N431
- [SDR FDEA201701110122](https://openairdocs.org/sdr/FDEA201701110122), Jan 11, 2017: COVER. LOOSE. CAN NOT ARM LEFT MAIN ENTRY DOOR SLIDE. FOUND LOWER SLIDE COVER LOOSE, REMOVED SLIDE COVER AND FOUND THE HOOK AND LOOP STRAPS LOOSE THAT STOW THE MATERAL TO THE
- [SDR FDEA201612064328](https://openairdocs.org/sdr/FDEA201612064328), Dec 6, 2016: CONTROL CABLE. OUT OF ADJUST. ON EXITING RUNWAY TILLER STUCK HARD AT 45' POSITION DURING 90' LT TURN. UPON GETTING BACK ON CENTER LINE, TILLER REQUIRED .5 TO 1 INSIDE RT TO REMAIN IN POSITSI
- [SDR FDEA201607212593](https://openairdocs.org/sdr/FDEA201607212593), Jul 21, 2016: HYDRAULIC LINE. LEAKING. DURING CLIMBOUT, RECEIVED LT HYD SYS LOW QUANTITY MESSAGE. SHORTLY, RECEIVED LT HYD SYS PRESSURE MESSAGE. COMPLIED WITH QRH EXTEND FLAPS ALTERNATELY AND ALTERNA
- [SDR FDEA201412194152](https://openairdocs.org/sdr/FDEA201412194152), Dec 19, 2014: LINE. OUT OF POSITION. LEFT COURIER SEAT O2 MASK DOES NOT TEST. AMM SMP UPON INSPECTION OF NR 1 COURIER MASK, FOUND OXYGEN LINES IMPROPERLY STOWED. STOWED MASK & LINES IAW AMM 35-11-0
- [SDR FDEA201410223331](https://openairdocs.org/sdr/FDEA201410223331), Oct 22, 2014: PANEL. NOT SEATED. L1 DOOR SLIDE WOULD NOT ARM PROPERLY BEFORE PUSHBACK. THE POP OUT ARMED PANEL STAYS FLUSH AGAINST THE DOOR WHEN THE EVACUATION SLIDE LEVER IS MOVED TO THE ARMED
- [SDR FDEA201410213327](https://openairdocs.org/sdr/FDEA201410213327), Oct 21, 2014: BRACKET. BROKEN. SLIDE COVER LOOSE & NOT ATTACHED PROPERLY AT THE BOTTOM OF THE L1 DOOR. FOUND TOP LT BRACKET BROKEN ON SLIDE RAFT COVER. INSTALLED SERVICEABLE SLIDE COVER
- [SDR FDEA201406071327](https://openairdocs.org/sdr/FDEA201406071327), Jun 7, 2014: BOLT. SHEARED. DURING TAXI OUT, CAPTAIN'S RT RUDDER PEDAL BROKE AS THE PARKING BRAKE WAS BEING SET. RT PEDAL MOVES FREELY WITH NO EFFECT ON FLIGHT CONTROLS. FOUND THE BOLT WHE
- [SDR FDEA201307091510](https://openairdocs.org/sdr/FDEA201307091510), Jul 9, 2013: COVER. LOOSE. LEFT ENTRY DOOR SLIDE COVER IS LOOSE. TIGHTENED LOWER STRAP. OPS CHECKED NORMAL.
- [SDR FDEA201303170589](https://openairdocs.org/sdr/FDEA201303170589), Mar 17, 2013: SHEAR TIE. CRACKED. AFT CARGO BS 1300 FRAME HAS A CRACKED SHEAR TIE BETWEEN S20-21L. REMOVED DAMAGED SHEAR TIE, FABRICATED NEW SHEAR TIE AND INSTALLED NEW SHEAR TIE IAW DRAWING 140
- [SDR FDEA201303120553](https://openairdocs.org/sdr/FDEA201303120553), Mar 12, 2013: SKIN. DENTED. FUSELAGE SKIN DENTED LEFT SIDE BS 637, STR 20L. CUT OUT DAMAGED AREA, FABRICATED REPAIR AND INSTALLED IAW SRM 53-00-01 REPAIR 15 AND SRM 53-00-00.
- [SDR FDEA201208112954](https://openairdocs.org/sdr/FDEA201208112954), Aug 11, 2012: COVER. LOOSE. L-1 DOOR SLIDE HOUSING IS LOOSE. RETIGHTENED SLIDE COVER IAW 25-66-01-414-101, FIG 402. OK FOR SERVICE.
- [SDR FDEA201204031237](https://openairdocs.org/sdr/FDEA201204031237), Apr 3, 2012: BRACKET. BACKED OUT. L1 ENTRY DOOR IS VERY DIFFICULT TO CLOSE. LOWER RT SIDE OF DOOR IS NOT ALIGNING PROPERLY AND IT TAKES SEVERAL ATTEMPTS TO CLOSE. REF PRIOR WRITE UPS. QTY 2 FITT
- [SDR FDEA201109213997](https://openairdocs.org/sdr/FDEA201109213997), Sep 21, 2011: ACM. FAILED. AFTER ENGINES STARTED, AN ACRID ODOR SEEMED TO ORIGINATE FROM THE LT PACK. WE ALSO HEARD A WHINNING NOISE AS THE THRUST LEVERS WERE ADVANCED. BOTH THE SMELL AND
- [SDR FDEA201108203390](https://openairdocs.org/sdr/FDEA201108203390), Aug 20, 2011: SENSOR. OUT OF ADJUST. EICAS RT EMERGENCY DOOR AND OVERHEAD EMERGENCY DOOR LIGHT ON MOST OF FLIGHT. OFF DURING DESCENT. ADJUSTED DOOR PROX SENSOR GAP. OPS CHECKS GOOD.
- [SDR FDEA201108053104](https://openairdocs.org/sdr/FDEA201108053104), Aug 5, 2011: DUCT. DISCONNECTED. ON DEPARTURE WITH LT PACK MEL'D, RECEIVED "RT PACK TRIP". COULD NOT PRESSURIZE ACFT. FOUND DUCT DISCONNECTED FROM TOP OF R/H HEAT EXCHANGER AND FROM THE ACM COM

All 102: https://openairdocs.org/aircraft/N928FD/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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