# Service difficulty reports: Boeing 757-204

A list on [Boeing 757-204](https://openairdocs.org/model/boeing-757-204.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 14 · 675 reports

- [SDR FDEA202610201625](https://openairdocs.org/sdr/FDEA202610201625.md): Stringer · abnormal · Oct 20, 2026 · N923FD · Boeing 757204 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY LOWER FRAME AT BS 1560, FOUND PREVIOUS REPAIR ON STR 26R.
- [SDR FDEA202610201624](https://openairdocs.org/sdr/FDEA202610201624.md): Structure · corroded · Oct 20, 2026 · N923FD · Boeing 757204 · Nacelle/Pylon, Main Frame
  > NR 2 ENGINE PYLON STRUT, OTBD LOWER STRUCTURE NAC S 146.675 FOUND CORRODED.
- [SDR FDEA202610191606](https://openairdocs.org/sdr/FDEA202610191606.md): Skin · corroded · Oct 19, 2026 · N923FD · Boeing 757204 · Nacelle/Pylon, Plate/Skin
  > NR 1ENGINE PYLON OUTB SIDE INTERNAL STRUCTURE SIDE SKIN CORRODED (PP STA 144.55 APROX.)
- [SDR FDEA202610151595](https://openairdocs.org/sdr/FDEA202610151595.md): Strut · corroded · Oct 15, 2026 · N923FD · Boeing 757204 · Nacelle/Pylon, Main Frame
  > ENG #2 PYLON STRUT INBD LOWER CHORD STA 144.425 CORROSION. THIS DISCREPANCY WAS ACCOMPLISHED ON EA # F-5430-T0389069 P1 TITLE: NACELLES / PYLONS-SKIN / PLATES / PANELS - CORROSION BLENDOUT #2 PYLON, LHS (INBD) SIDE SKIN DOUBLER INNER SURFACE, PP STA 153-16
- [SDR FDEA202610121558](https://openairdocs.org/sdr/FDEA202610121558.md): Frame · corroded · Oct 12, 2026 · N923FD · Boeing 757204 · Horizontal Stabilizer, Spar/Rib
  > RH ELEVATOR CONDUCTIVE FRAME MULTIPLE ZONES WITH CORROSION (UPPER AND LOWER) EVALUATED CONDUCTIVE FRAME RH ELEVATOR UPPER/LOWER HORIZONTAL STABILIZER AND REPLACED CONDUCTIVE SPLICE PLATE (02EA) AND SHIMS (02EA) UPPER/LOWER IAW B757 SRM 51-40-02-0G, SRM 55-
- [SDR FDEA202610121557](https://openairdocs.org/sdr/FDEA202610121557.md): Frame · corroded · Oct 12, 2026 · N923FD · Boeing 757204 · Elevator, Spar/Rib
  > LEFT ELEVATOR CONDUCTIVE FRAME MULTIPLE ZONES WITH CORROSION (UPPER AND LOWER) EVALUATED CONDUCTIVE FRAME LH ELEVATOR UPPER/LOWER HORIZONTAL STABILIZER AND REPLACED CONDUCTIVE SPLICE PLATE (02EA) AND SHIMS (02EA) UPPER/LOWER IAW B757 SRM 51-40-02-0G, SRM 5
- [SDR FDEA202610071490](https://openairdocs.org/sdr/FDEA202610071490.md): Seat Track · damaged · Oct 7, 2026 · N923FD · Boeing 757204 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK BETWEEN BS 1080-1180, LBL 45.5. REMOVED AND REPLACED THE SEAT TRACK SECTION IAW SRM 51-40-02-OG, & DWG 144N5021, REV C.
- [SDR FDEA202610071489](https://openairdocs.org/sdr/FDEA202610071489.md): Seat Track · corroded · Oct 7, 2026 · N923FD · Boeing 757204 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK BETWEEN STA 1140 TO STA 1160 RBL 45.50 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK SECTION ON MAIN CABIN FROM BS 1080 - 1180, RBL 45.5 IAW SRM 51-40-02-OG, & DWG 144N5021, REV C.
- [SDR FDEA202610071488](https://openairdocs.org/sdr/FDEA202610071488.md): Seat Track · corroded · Oct 7, 2026 · N923FD · Boeing 757204 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK BETWEEN BS 1180 - 1200, RBL 45.50 WAS CORRODED. REMOVED AND REPLACED SEAT TRACK SECTION ON MAIN CABIN FROM BS 1180 - 1280, RBL 45.50 IAW SRM 51-40-02-OG, & DWG 146N5130 REV C.
- [SDR FDEA202606170770](https://openairdocs.org/sdr/FDEA202606170770.md): Sequence Valve · inoperative · Jun 17, 2026 · N924FD · Boeing 757204 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE MESSAGE. NLG INDICATION WAS NOT ILLUMINATED. NLG DID NOT EXTEND. COMPLETED QRH 14.1.12. AFTER CHKLST COMPLETION NLG EXTENSION SUCCESSFUL. EMERGENCY DECLARED. AFTER SHUTDOWN STATUS MESSAGE LDG GEAR MONITOR. EMERGENCY DECLARED. LANDING G
- [SDR FDEA202605290650](https://openairdocs.org/sdr/FDEA202605290650.md): Collar · broken · May 29, 2026 · N927FD · Boeing 757204 · Passenger/Crew Doors
  > POST FLIGHT FOUND L1 DOOR GUST LOCK COLLAR BROKEN. REMOVED AND REPLACED L1 HOLD OPEN DOOR GUST COLLAR. OPS CHK GOOD. THIS CLEARS MEL 7460636
- [SDR FDEA202605220627](https://openairdocs.org/sdr/FDEA202605220627.md): Girt Bar · out of adjust · May 22, 2026 · N923FD · Boeing 757204 · Emergency Equipment
  > LH ENTRY DOOR WILL NOT ARM. PERFORMED ADJUSTMENT OF L1 DOOR GIRT BAR. ARMED AND DISARMED L1 SLIDE MULTIPLE TIMES WITH GOOD INDICATION. DOOR ARMS AND DISARMS SMOOTHLY WITH NO BINDS. MEL CLEARED AND PLACARD REMOVED. A/C OK FOR SERVICE.
- [SDR FDEA202604240494](https://openairdocs.org/sdr/FDEA202604240494.md): Lamp · no test · Apr 24, 2026 · N925FD · Boeing 757204 · Emergency Lighting
  > ON SERVICE CHECK FOUND LH EMERGENCY SLIDE LIGHT INOP. AMM 33-51-06-2-1 RELAMPED LH EMERGENCY SLIDE LIGHT AS PER 757 AMM 33-51-06-2-1. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. FACT 24APR26 03:02 GSO AMM 33-51-06-2-1 RELAMPED LH EMERGENCY SLIDE LIGHT
- [SDR FDEA202604040400](https://openairdocs.org/sdr/FDEA202604040400.md): Bottle · empty · Apr 4, 2026 · N923FD · Boeing 757204 · Passenger/Crew Doors
  > DURING MX PRE-FLIGHT, NOTICED THAT R1 DOOR EMERGENCY POWER RESEVOIR BOTTLE IS DEPLETED, READS 0 PSI. REMOVED AND REPLACED EMERGENCY POWER RESERVOIR FOR THE R1 DOOR W/REF TO B757 MM 52-11-30-4. ACFT OK TO CONTINUE.
- [SDR FDEA202604040399](https://openairdocs.org/sdr/FDEA202604040399.md): Sequence Valve · failed · Apr 4, 2026 · N924FD · Boeing 757204 · Landing Gear Retraction/Extension System
  > NOSE GEAR FAILED TO EXTEND NORMALLY WHEN GEAR HANDLE WAS MOVED INTO THE DOWN POSITION. NOSE GEAR EXTENDED USING THE ALTN GEAR EXTEND SWITCH. LDG GEAR MONITOR STATUS MESSAGE DISPLAYED. AMM: 32-34-05-4 COMPLETED INSTALL OF NOSE GEAR DOOR OPERATED SEQUENC
- [SDR FDEA202603020305](https://openairdocs.org/sdr/FDEA202603020305.md): Battery Pack · inoperative · Mar 2, 2026 · N923FD · Boeing 757204 · Emergency Lighting
  > EMERGENCY LIGHTS AT DOOR L1 INOPERATIVE. REPLACED DOOR L1 EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-51-07-2. OPS CHECKED GOOD.
- [SDR FDEA202602110174](https://openairdocs.org/sdr/FDEA202602110174.md): Bulb · dim · Feb 11, 2026 · N923FD · Boeing 757204 · Emergency Lighting
  > DURING MX PRE-FLIGHT FOUND R1 EMERGENCY EXIT SIGN DIM. REMOVED AND REPLACED 5 FAULTY BULBS AT THE R1 EMERGENCY EXIT SIGN IAW AMM 33-51-01-2. OPS CHECK GOOD. ACFT OK FOR SERVICE.
- [SDR FDEA202602110173](https://openairdocs.org/sdr/FDEA202602110173.md): Bulb · inoperative · Feb 11, 2026 · N923FD · Boeing 757204 · Emergency Lighting
  > DURING PRE-FLIGHT CHECK, FOUND CENTER OVERHEAD EMERGENCY EXIT IDENTIFIER SIGN DIM. AMM 33-51-01-2 FOUND CENTER OVERHEAD EMERGENCY EXIT SIGN HAS 14 FAULTY BULBS. REMOVED AND REPLACED 14 FAULTY BULBS AS PER ABOVE REF. OPS CHECK GOOD.
- [SDR FDEA202602110172](https://openairdocs.org/sdr/FDEA202602110172.md): Bulb · inoperative · Feb 11, 2026 · N923FD · Boeing 757204 · Emergency Lighting
  > DURING PRE-FLIGHT FOUND L1 OVERHEAD EMERGENCY EXIT SIGN SLIGHTLY DIM. AMM 33-51-01-2 FOUND L1 OVERHEAD EMERGENCY EXIT SIGN HAS 5 FAULTY BULBS. REMOVED AND REPLACED 5 FAULTY BULBS AS PER ABOVE REF. OPS CHECKED GOOD.
- [SDR FDEA202511262209](https://openairdocs.org/sdr/FDEA202511262209.md): Wire · broken · Nov 26, 2025 · N924FD · Boeing 757204 · Light System Wiring
  > COCKPIT EMERGENCY DOME LIGHT INOPERATIVE. RELAMPED NO HELP. DURING TROUBLESHOOTING, FOUND WIRE W0200-0009-22, BROKEN FROM RELAY R10381. RESOLDER SAME, LIGHT OPS CHECK NORMAL. DOME LIGHT ASSEMBLIES REQUIRE MOUNTING AND RE-OPS CHECK.
- [SDR FDEA202511192190](https://openairdocs.org/sdr/FDEA202511192190.md): Lamp · inoperative · Nov 19, 2025 · N927FD · Boeing 757204 · Passenger Compartment Lighting
  > R1 DOOR SLIDE LIGHT INOPERATIVE. RELAMPED R1 DOOR SLIDE LIGHT IAW AMM 33-51-06-2. OPS CHKD SERVICEABLE.
- [SDR FDEA202511172186](https://openairdocs.org/sdr/FDEA202511172186.md): Floorbeam · corroded · Nov 17, 2025 · N924FD · Boeing 757204 · Fuselage Main, Floor Beam
  > AFT CARGO COMPARTMENT BS 1560 LBL 45.50 UPPER FLOOR BEAM LOWER CHORD WITH CORROSION. COMPLIED WITH FEDEX EA # F-5310-T0385569 P1 TILE: FUSELAGE -MAINFRAME CORROSION REPAIR -STA 1560 FLOOR BEAM LOWER FLANGE DAMAGE
- [SDR FDEA202511172185](https://openairdocs.org/sdr/FDEA202511172185.md): Stringer · worn · Nov 17, 2025 · N924FD · Boeing 757204 · Fuselage Main, Structure
  > AFT CARGO COMPARTMENT BETWEEN BS 1440 AND 1460 LOWER SECTION BL 0.0 PROTECTIVE TREATMENT DAMAGED BARE METAL AND CORROSION EVALUATED STRINGER AT AFT CARGO BETWEEN BS 1440-1460 BL 0 FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-03-1A. REMOVED STRINGER AND S
- [SDR FDEA202511172184](https://openairdocs.org/sdr/FDEA202511172184.md): Cover Panel · cracked · Nov 17, 2025 · N924FD · Boeing 757204 · Fuselage Main, Structure
  > R1 DOOR FRAME BETWEEN BS 324 AND BS 333.45 TORQUE TUBE CAVITY SKIN WITH CRACK COMPLIED WITH FEDEX EA # F-5310-T0385531 P1 TITTLE: FUSELAGE - MAINFRAME - SECTION 41: STUB FRAME INSTALLATION, R1 DOOR CUTOUT, STA 335, COVER PANEL, CRACK REPAIR.
- [SDR FDEA202511152183](https://openairdocs.org/sdr/FDEA202511152183.md): Floorbeam · corroded · Nov 15, 2025 · N924FD · Boeing 757204 · Fuselage Main, Floor Beam
  > MAIN CARGO STA 1200 BETW BL 0 TO LBL 58 FLOOR BEAM UPPER T CHORD HAS CORROSION 7 SPOTS CUT OUT UPPER FLOOR BEAM FOUND AREA OUT OF LIMITS STA 1200 BL 0 TO LBL 58 IAW B757 SRM 53-00-51-2R FIG 201 REP 8 AND B757 SRM 53-0051-1A DET II MANUFACTURE (FORMED) REP
- [SDR FDEA202511142181](https://openairdocs.org/sdr/FDEA202511142181.md): Cover Panel · cracked · Nov 14, 2025 · N924FD · Boeing 757204 · Fuselage Miscellaneous Structure
  > SKIN CRACK FOUND AT L1 OPERATING MECHANSIM CAVITY STA 327 STR 14-15 COMPLIED WITH FEDEX EA # F-5310-T0385532 P1 TITLE: FUSELAGE-MAINFRAME-SECTION 41: STUB FRAME INSTALLATION, L1 DOOR CUT OUT, STA 355, CONER PANEL, CRACK REPAIR
- [SDR FDEA202511132173](https://openairdocs.org/sdr/FDEA202511132173.md): Skin · dented · Nov 13, 2025 · N924FD · Boeing 757204 · Leading Edge Devices
  > SLAT NR 3 UPPER SURFACE T/E HAS A SKIN DEFORMATION REPAIRED SLAT NR 3 UPPER SURFACE IAW SRM 57-43-02-1A REMOVED AND REINSTALLED SLAT NR 3 AND OPS CHECK IAW AMM 27-81-02-4, OPS CHECK SATISTFACTORY AND PERFORMED O/B SLAT LOSS SENSING TEST IAW AMM 27-81-00-5,
- [SDR FDEA202511132171](https://openairdocs.org/sdr/FDEA202511132171.md): Seat Track · corroded · Nov 13, 2025 · N924FD · Boeing 757204 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO STA 1200 BETW BL 0 TO LBL 58 FLOOR BEAM UPPER T CHORD HAS CORROSION 7 SPOTS CUT OUT UPPER FLOOR BEAM FOUND AREA OUT OF LIMITS STA 1200 BL 0 TO LBL 58 IAW B757 SRM 53-00-51-2R FIG 201 REP 8 AND B757 SRM 53-00-51-1A DET II MANUFACTURE (FORMED)
- [SDR FDEA202511112162](https://openairdocs.org/sdr/FDEA202511112162.md): Seat Track · corroded · Nov 11, 2025 · N924FD · Boeing 757204 · Fuselage Main, Floor Beam
  > MAIN CARGO FLOORBEAM UPPER FLANGE FOUND WITH CORROSION AT BS 1620, LBL 50. CUT OUT FLOOR BEAM SECTION FOUND AREA OUT OF LIMITS MAIN CARGO CABIN FLOORBEAM BS 1200 LBL 50 IAW SRM 53-00-21-1A DET II AND SRM 53-00-51-2R REP 8. MANAFACTURED PARTS TRIMMED, LOCATED
- [SDR FDEA202511102155](https://openairdocs.org/sdr/FDEA202511102155.md): Door · out of sequence · Nov 10, 2025 · N927FD · Boeing 757204 · Passenger/Crew Doors
  > L1 DOOR HARD TO OPEN & CLOSE. UPPER & LOWER DOOR GATES WILL NOT CLOSE. OUTER HANDLE ROTATES APPROX 3 INCHES PAST THE CLOSE POSITION WHEN ATTEMPTING TO CLOSE. INNER DOOR HANDLE WILL NOT ROTATE TO THE FULL CLOSE POSITION. & AS PREV STATED UPPER & LOWER GATE
- [SDR FDEA202511072142](https://openairdocs.org/sdr/FDEA202511072142.md): Seat Track · corroded · Nov 7, 2025 · N924FD · Boeing 757204 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO BETW STA 1180 TO 1420 RBL 58 SEAT TRACK HAS CORROSION REMOVED DAMAGE SEAT TRACK. NO ALLOWABLE DAMAGE LIMITS MAIN CABIN BETWEEN STA 1180 TO 1420 RBL 58 IAW B757 SRM 51-40-02-0G AND B757 SRM 51-10-02-0G TRIMMED, LOCATED AND DRILLED NEW SEAT TRACK
- [SDR FDEA202511052130](https://openairdocs.org/sdr/FDEA202511052130.md): Seat Track · corroded · Nov 5, 2025 · N924FD · Boeing 757204 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LBL 45.50 BETWEEN BS 1130 TO BS 1540 HAS MULTIPLE AREAS WITH CORROSION REMOVED SEAT TRACK SECTION LBL 45.5 BETWEEN STA 1320 TO 1540 IAW B757 SRM 51-40-02-0G TRIMMED, LOCATED AND DRILLED, NEW SEAT TRACK SECTIOM IAW B757 SRM 51-40-05-0G, SRM 51-4
- [SDR FDEA202511052129](https://openairdocs.org/sdr/FDEA202511052129.md): Seat Track · corroded · Nov 5, 2025 · N924FD · Boeing 757204 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO CABIN SEAT TRACK FOUND CORRODED AT LEVEL STA 1560 TO STA 1600 LBL 58 REMOVED AND EVALUATED MAIN CARGO CABIN SEAT TRACK BETWEEN STA 1420-1600 LBL 58 NO ALLOWABLE DAMAGE IAW B757 SRM 53-00-52-1A FIG 101, SRM51-40-02-0G. TRIMMED, LOCATED, DRILLED
- [SDR FDEA202511052128](https://openairdocs.org/sdr/FDEA202511052128.md): Seat Track · corroded · Nov 5, 2025 · N924FD · Boeing 757204 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO BETW STA 1180-1200 LBL 45 SEAT TRACK HAS CORROSION. REMOVED SEAT TRACK SECTION BETWEEN STA 1180 TO 1240 LBL 45 FOUND SEAT TRACK OUT OF LIMITS IAW B757 SRM 51-40-02-0G AND B757 SRM 53-00-52-1A FIG 101. TRIMMED, LOCATED AND DRILLED NEW SEAT TRACK
- [SDR FDEA202511052127](https://openairdocs.org/sdr/FDEA202511052127.md): Seat Track · corroded · Nov 5, 2025 · N924FD · Boeing 757204 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO BETW STA 1000-1019 LBL 24 SEAT TRACK CROWN SUPPORT HAS CORROSION. COMPILED WITH EA # F-5310-T0385669.
- [SDR FDEA202509251832](https://openairdocs.org/sdr/FDEA202509251832.md): Floorbeam · corroded · Sep 25, 2025 · N925FD · Boeing 757204 · Fuselage Main, Structure
  > AFTER GVI ON DECK PLATE BS 1681.8 BETWEEN LBL 24.75 TO LBL 45.50 FOUND CORROSION COMPLIED WITH FEDEX EA # F-5310-T0384883 P1 TITLE: FUSELAGE - MAINFRAME-FLOOR BEAM AND DECK PLATE STA 1681 LBL24-LBL45 CORROSION REPAIR.
- [SDR FDEA202509181740](https://openairdocs.org/sdr/FDEA202509181740.md): Seat Track · corroded · Sep 18, 2025 · N925FD · Boeing 757204 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK FLANGES WITH CORROSION BETWEEN BS 1620 TO 1420 LBL 58.22 REMOVED MAIN CABIN SEAT TRACK BETWEEN BS 1420-1620 LBL 58.22 IAW B757 SRM 51-40-02-0G TRIMMED, LOCATED AND DRILLED NEW SEAT TRACK IAW B757 SRM 51-40-05-0G, 51-40-08-0G BOEING D
- [SDR FDEA202509091678](https://openairdocs.org/sdr/FDEA202509091678.md): Seat Track · corroded · Sep 9, 2025 · N925FD · Boeing 757204 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK RT FLANGE AT BS 1540, RBL 45.5 CORRODED. REMOVED THE SEAT TRACK FROM BS 1320-1540, RBL 45.5 IAW SRM 51-40-02-0G. TRIMMED, LOCATED, AND DRILLED A NEW SEAT TRACK IAW SRM 51-40-05-0G, 51-40-08-0G, & DWG 146N5130, REV A. INSTALLED THE SEAT
- [SDR FDEA202509091677](https://openairdocs.org/sdr/FDEA202509091677.md): Seat Track · corroded · Sep 9, 2025 · N925FD · Boeing 757204 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK RT & LT FLANGES AT BS 1640, LBL 45.5 CORRODED. REMOVED THE SEAT TRACK BS 1540-1640 LBL 45.5 IAW SRM 51-40-02-0G. TRIMMED, LOCATED, AND DRILLED A NEW SEAT TRACK IAW SRM 51-40-05-0G, 51-40-08-0G, & DWG 146N5130, REV A. INSTALLED THE SEA
- [SDR FDEA202509091676](https://openairdocs.org/sdr/FDEA202509091676.md): Seat Track · corroded · Sep 9, 2025 · N925FD · Boeing 757204 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK LT FLANGE AT BS 1620 CRACKED RBL 45.5. REMOVED THE SEAT TRACK BS 1540-1640 RBL 45.5 IAW SRM 51-40-02-0G, TRIMMED, LOCATED, AND DRILLED A NEW SEAT TRACK IAW SRM 51-40-05-0G, 51-40-08-0G, AND DWG 146N5130, REV A. INSTALLED THE SEAT
- [SDR FDEA202509091675](https://openairdocs.org/sdr/FDEA202509091675.md): Seat Track · corroded · Sep 9, 2025 · N925FD · Boeing 757204 · Fuselage Structure (General)
  > CABIN SEAT TRACK AT B.S 770 RBL 58.22 WITH CORROSION. TRIMMED, LOCATED AND DRILLED NEW SEAT TRACK MAIN CABIN STA 660-880 RBL 58.22 IAW B757 SRM 51-40-05-0G, 51-40-08-0G BOEING DWG # 657N3332 REV A. INSTALLED MAIN CABIN NEW SEAT TRACK FROM STA 660-880 RBL
- [SDR FDEA202509081644](https://openairdocs.org/sdr/FDEA202509081644.md): Skin · corroded · Sep 8, 2025 · N925FD · Boeing 757204 · Trailing Edge Flaps
  > LEFT WING INBOARD MAIN FLAP LOWER SKIN HAS CORROSION, (OUTBOARD FLAP TRACK AREA) UPON FURTHER EVALUATION ON LT WING INBD MAIN FLAP LOWER SKIN CORROSION FOUND OUT OF LIMITS IAW SRM 57-53-01-1A DETAIL I, FIG 101, SHEET 1, NOTE F AND APPLIED PERMANENT REPAIR IN S
- [SDR FDEA202508281564](https://openairdocs.org/sdr/FDEA202508281564.md): Outflow Valve · failed · Aug 28, 2025 · N923FD · Boeing 757204 · Pressure Regulator/Outflow Valve
  > DECLARED EMERGENCY DIVERTED TO IND. MECHS PERFORMED GVI OF PACK BAYS AND COMPONENTS. OUTFLOW VALVE CLEAR OF ANY DEBRIS, RAN LT PACK FOR LEAKS AND NO LEAKS DETECTED. WILL PROCEED WITH 757 AMM 21-51-00-5, PARG.10. SINGLE PACK PRESSURIZATION CONFIDENCE CHK
- [SDR FDEA202508271550](https://openairdocs.org/sdr/FDEA202508271550.md): Controller · inoperative · Aug 27, 2025 · N923FD · Boeing 757204 · Central Warning
  > AT FL350 RIGHT ENG BLEED EICAS FLICKERED THEN CABIN ALT HI DISCRETE LIGHT & EICAS ILLUM. CABIN RATE SHOWED A CLIMB OF 500-750 FT PER MIN & A CABIN ALT OF 12,000. DONNED O2 MASK. DESCENDED TO 10,000 FT. CABIN ALT INOP LIGHT ALSO ILLUM. DECLARED AN EMERGENCY.
- [SDR FDEA202507311346](https://openairdocs.org/sdr/FDEA202507311346.md): Transmission · faulted · Jul 31, 2025 · N925FD · Boeing 757204 · Trailing Edge Flap Control System
  > TE FLAP DISAGREE CAUTION. COMPLIED WITH QRH. WITH FLAPS SELECTED TO 25, FLAPS WOULD NOT MOVE PAST 20. ALTN FLAPS SELECTOR USED TO SET FLAPS TO 25. EMERGENCY DECLARED. AMM: 27-51-06-4 WORKED IN CONJUNCTION WITH TSI 27-50-2326, REMOVED AND REPLACED #5 FLAP T
- [SDR FDEA202504300694](https://openairdocs.org/sdr/FDEA202504300694.md): Ballscrew · lack of lube · Apr 30, 2025 · N925FD · Boeing 757204 · Trailing Edge Flap Control System
  > ON CONFIGURING AND SELECTING FLAPS 25 WE RECEIVED A TRAILING EDGE FLAP DISAGREE WARNING AND ASSOCIATED CAUTION LIGHT. WE DISCONTINUED THE APPROACH AND LANDED FLAPS 20. EMERGENCY DECLARED. FIM: 27-51, FT 808 AMM: 12-13-06-3 AMM: 12-21-09-3 AMM: 27-51-00
- [SDR FDEA202502140231](https://openairdocs.org/sdr/FDEA202502140231.md): Skin · dented · Feb 14, 2025 · N927FD · Boeing 757204 · Leading Edge Devices
  > L/H WING #4 SLAT UPPER SURFACE, T/E WEDGE HAS DENT 39 INCHES FROM OTBD EDGE REPAIRED #4 LH WING SLAT IAW AMM 27-81-02-4 & SRM 57-43-02-2R F.201, OPS CHECK GOOD IAW AMM 27-81-02-4, THIS IS A MAJOR REPAIR
- [SDR FDEA202502110211](https://openairdocs.org/sdr/FDEA202502110211.md): Strap · cracked · Feb 11, 2025 · N927FD · Boeing 757204 · Fuselage Miscellaneous Structure
  > FWD LOWER FUSELAGE INT SEAT TRACK STABILIZER AT STA 377.7 UNDER FLOORBOARD LH SIDE CRACKED. DOT #54-33 REMOVED AND REPLACED SECTION OF SEAT TRACK STABILIZER REPAIR AT STA 377.7 L/H SIDE IAW SRM 51-40-02 AND SRM 53-00-51-2R REPAIR 12, MAJOR REPAIR.
- [SDR FDEA202502100208](https://openairdocs.org/sdr/FDEA202502100208.md): Lamp · failed · Feb 10, 2025 · N924FD · Boeing 757204 · Emergency Lighting
  > MDIS 924 33-50 2328 10FEB25 13:47 YOW FACT R1 DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOP. FACT 10FEB25 14:04 YOW AMM: 33-51-06-2-1 RELAMPED R1 DOOR EXTERIOR SLIDE LIGHT IAW ABOVE REF. OPS CHK SERVICEABLE. OK TO CONTINUE.
- [SDR FDEA202502060189](https://openairdocs.org/sdr/FDEA202502060189.md): Floor Panel · damaged · Feb 6, 2025 · N927FD · Boeing 757204 · Fuselage Floor Panel
  > FLOOR PANEL 222MEF HAS FRAYED DAMAGE FABRICATED FLOOR PANEL 222MEF ZONE 220 ON VTMAE TRAVELER #T24/1796467 IAW MAE DWG PL11861182-1 REV G. MAJOR REPAIR

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## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = '757204'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-757-204/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.