# Service difficulty reports: N924FD

A list on [N924FD](https://openairdocs.org/aircraft/N924FD.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 136 reports

- [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 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 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 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 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 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 FDEA202312071922](https://openairdocs.org/sdr/FDEA202312071922.md): Proximity Sensor · failed · Dec 7, 2023 · N924FD · Boeing 757200 · Door Warning System
  > ON CLIMB OUT THRU 18,000 L EMER DOOR EICAS MESSAGE. PRESSURIZATION REMAINED NORMAL CONTINUED TO DESTINATION. DESCENDING BELOW 10,000 EICS MESSAGE EXTINGUISHED. REMOVED AND REPLACED L3 DOOR LOCK PROX SENSOR REF 52-71-00-4. TESTS PASS.
- [SDR FDEA202312071920](https://openairdocs.org/sdr/FDEA202312071920.md): Unknown · unknown · Dec 7, 2023 · N924FD · Boeing 757200 · Emergency Exits
  > CLIMBING THRU 12,000 FEET OUT OF BFM EICAS L EMER DOOR LIGHT. LEVELED AT 15,000 AND RAN QRH. DECLARED EMERGENCY AND DESCENDED TO 10,000 FEET. PRESSURIZATION OPERATED NORMAL AND AFTER A FEW MINUTES AT 10,000 AND EICAS MESSAGE DISAPPEARED. GAINED ACESS
- [SDR FDEA202312011902](https://openairdocs.org/sdr/FDEA202312011902.md): Fitting · damaged · Dec 1, 2023 · N924FD · Boeing 757200 · Wing, Attach Fittings
  > REMOVE # 2 ENG PYLON I/B DRAG FITTING REQUIEST PER EA # F-5730-TO376999 REPAIR PERFORMED I.A.W EA # F-5730-TO376999 WING - OUTER WING-UPPER SKIN, DRAG FITTING AND DIAGONAL BRACE FASTENER AND SHIM INSPECTION RB 757- 57A0073. CAT "B" MAJOR REPAIR.
- [SDR FDEA202112073043](https://openairdocs.org/sdr/FDEA202112073043.md): None · cracked · Dec 7, 2021 · N924FD · Boeing 757200 · Wing, Plate/Skin
  > RIGHT WING #7 SLAT AFT SKIN HAS CRACK AROUND THE RIVET HOLE LOCATED AT INBD AUXILLARY TRACK AREA. REMOVED AND REPLACED DAMAGED SKIN ON #7 SLAT R/H WING IAW SRM 51-40-02. MAJOR REPAIR
- [SDR FDEA202112052989](https://openairdocs.org/sdr/FDEA202112052989.md): None · damaged · Dec 5, 2021 · N924FD · Boeing 757200 · Standard Practices/Structures
  > ZONE 220 FLOOR BOARD 222AF IS DAMAGED. FABRICATED ZONE 220 FLOORBOARD 222AF ON VT MAE TRAVELER T21/1586160 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIR
- [SDR FDEA202112022979](https://openairdocs.org/sdr/FDEA202112022979.md): None · damaged · Dec 2, 2021 · N924FD · Boeing 757200 · Standard Practices/Structures
  > ZONE 220 FLOOR BOARD 221AF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221AF ON VT MAE TRAVELER T21/1586162 IAW SRZ-25- 005 REVISION R. MAJOR REPAIR
- [SDR FDEA202112022980](https://openairdocs.org/sdr/FDEA202112022980.md): None · damaged · Dec 2, 2021 · N924FD · Boeing 757200 · Standard Practices/Structures
  > ZONE 220 FLOOR BOARD 222MAF IS DAMGED. FABRICATED ZONE 220 FLOOR BOARD 222MAF ON VT MAE TRAVELER T21/1586164 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIR
- [SDR FDEA202112022978](https://openairdocs.org/sdr/FDEA202112022978.md): None · damaged · Dec 2, 2021 · N924FD · Boeing 757200 · Standard Practices/Structures
  > ZONE 220 FLOOR BOARD 221MBF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221MBF ON MAE TRAVELER T21/1586166 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIR
- [SDR FDEA202105181285](https://openairdocs.org/sdr/FDEA202105181285.md): Warning Message · false activation · May 18, 2021 · N924FD · Boeing 757204 · Trailing Edge Flap Control System
  > TE FLAP DISAGREE EICAS MESSAGE ON APPROACH. COMPLIED WITH QRH PROCEDURES, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. T/ S PER 757 F.I.M. 27-51 TREE 808. ALSO PERFORMED FSEU BITE TEST PER AMM 27-51-01-2. NO CURRENT FAULTS. OPERATED FLAPS FULL TRAVEL
- [SDR FDEA202101270207](https://openairdocs.org/sdr/FDEA202101270207.md): Transmitter · failed · Jan 27, 2021 · N924FD · Boeing 757204 · Trailing Flap Position Indicating System
  > DURING ARRIVAL GOT TE FLAP ASYM WHEN FLAPS SELECTED TO 5. FLAP INDICATION SHOWS BETWEEN 1 AND 5. COMPLIED WITH QRH, LANDED UNEVENTFULLY. TRAILING EDGE FLAP INDICATION SHOWING APPROXIMATELY HALF A NEEDLE WIDTH SPLIT AFTER BLOCK-IN. LEFT AND RIGHT TRAILING E
- [SDR FDEA2019122313278](https://openairdocs.org/sdr/FDEA2019122313278.md): Frame · corroded · Dec 21, 2019 · N924FD · Boeing 757204 · Elevator, Spar/Rib
  > LT ELEVATOR OUTBOARD UPPER AND LOWER CONDUCTIVE FRAME ARE CORRODED. REPLACED LT ELEVATOR UPPER AND LOWER CONDUCTIVE FRAMES IAW SRM 55-20-01 AND 55-20-01-2R WITH EA F-2730-T0351345 STATIC BASE AND WICK REMOVED AND INSTALLED IAW AMM 23-61-01-2. FINISH RESTOR
- [SDR FDEA201912173250](https://openairdocs.org/sdr/FDEA201912173250.md): Floor Panel · damaged · Dec 17, 2019 · N924FD · Boeing 757204 · Fuselage Floor Panel
  > AFT PIT FLOOR PANEL 161AF HAS 1EA A PUNCTURE FABRICATED NEW FLOOR PANEL 161AF IAW BOEING PL 453N1270 BN-REV
- [SDR FDEA201912173249](https://openairdocs.org/sdr/FDEA201912173249.md): Floor Panel · damaged · Dec 17, 2019 · N924FD · Boeing 757204 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 161BF HAS 1EA PUNCTURE FABRICATED AFT CARGO FLOOR PANEL 161BF IAW B757 SRM 53-60-53 AND BOEING PL 453N1270 REV BN PARTMARKED IAW BAC5307
- [SDR FDEA2019121753246](https://openairdocs.org/sdr/FDEA2019121753246.md): Guide · cracked · Dec 15, 2019 · N924FD · Boeing 757204 · Trailing Edge Flaps
  > LEFT WING,OUTBOARD FLAP,AFTFLAP,INBOARD TRACK,GUIDE CRACKED. REPAIRED LEFT WING,OUTBOARD FLAP,AFT FLAP,INBOARD TRACK,GUIDE CRACKED BY REMOVING DAMAGE AND APPLYING HOT BOND FIBERGLASS OVERLAY REPAIRS IN 2 EACH AREAS,CURING,SHAPING AND RESTORING FINISH IA
- [SDR FDEA2019121303219](https://openairdocs.org/sdr/FDEA2019121303219.md): Floorboard · damaged · Dec 10, 2019 · N924FD · Boeing 757204 · Fuselage Floor Panel
  > AFT MAIN CARGO FLOORBOARD P.NO 11864182-40 DAMAGED. REPAIRED FLOOR BOARD IAW B757-2 SRM 53-00-50-2R
- [SDR FDEA2019121303218](https://openairdocs.org/sdr/FDEA2019121303218.md): Floorboard · damaged · Dec 10, 2019 · N924FD · Boeing 757204 · Fuselage Floor Panel
  > AFT MAIN CABIN FLOORBOARD P.NO 11864182-42 DAMAGED. REPAIRED FLOOR BOARD IAW B757-2 SRM 53-00-50-2R
- [SDR FDEA201912043178](https://openairdocs.org/sdr/FDEA201912043178.md): Panel · cracked · Dec 4, 2019 · N924FD · Boeing 757204 · Wing Miscellaneous Structure
  > RT WING T/E WIGGLE PANEL IS CRACKED AT APPROX WSTA 335. REMOVED AND REPLACED WIGGLE PANEL AT RT WING T/E AT APPROX WSTA335 PER SRM 51-40-02-0G APPLIED PROTECTIVE FINISH PER SRM 51-20-01-0G.
- [SDR FDEA201806151498](https://openairdocs.org/sdr/FDEA201806151498.md): Idg · failed · Jun 15, 2018 · N924FD · Boeing 757204 · AC Generator-Alternator
  > ACFT ELECTRICAL SYSTEM WENT IRRADIC, COCKPIT LIGHTS BEGAN FLICKERING, LOWER EICAS WENT BLACK. NUMEROUS EICAS MESSAGES ENSUED BUT MAIN ONES REMAINED. EVERYTHING CAME BACK ON WHEN THE RIGHT ENGINE WAS SHUTDOWN. REMOVED AND REPLACED THE RIGHT ENGINE IDG IAW
- [SDR FDEA201805181257](https://openairdocs.org/sdr/FDEA201805181257.md): Cylinder · leaking · May 18, 2018 · N924FD · Boeing 757204 · Passenger/Crew Doors
  > UPON ARRIVAL, THE L1 ENTRY DOOR EMERGENCY POWER RESERVOIR INDICATION WAS ZERO PSI. REMOVED AND REPLACED L1 ENTRY DOOR EMERGENCY POWER RESERVOIR IAW MM 52-11-30-4. OK FOR SERVICE
- [SDR FDEA201711213290](https://openairdocs.org/sdr/FDEA201711213290.md): Floorbeam · cracked · Nov 21, 2017 · N924FD · Boeing 757204 · Fuselage Main, Floor Beam
  > STA 580 LBL 45.5 FLOORBEAM IS CRACKED. SEEN FROM FORWARD CARGO. COMPLIED WITH EA # F-5310-T0336514 P1,FUSELAGE-MAINFRAME-STA 580 FLOOR BEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR.
- [SDR FDEA201711183275](https://openairdocs.org/sdr/FDEA201711183275.md): Seat Track · corroded · Nov 18, 2017 · N924FD · Boeing 757204 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK BETWEEN STA 1620 - 1640 LBL 45.5 SEAT TRACK FLANGE CORRODED. REMOVED CORROSION ON SEAT TRACK IAW B 757 SRM 51-10-02-0G,EVALUATED AREA,ORIGINAL MAT. 0.070",MAT. REMAINING 0.015",MAT. LOSS 0.055" FOUND TO BE OUT OF LIMITS IAW B 757 SRM 53-00-52
- [SDR FDEA201711183274](https://openairdocs.org/sdr/FDEA201711183274.md): Cusp Web · corroded · Nov 18, 2017 · N924FD · Boeing 757204 · Fuselage Miscellaneous Structure
  > MAIN DECK BETWEEN STA 980 - 1000 RT SIDE CUSP WEB CORRODED. REMOVED CORROSION AND EVALUATED CUSP WEB AT STA 980 - 1000 RT, ORIGINAL MAT.056", MAT REM.048" FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13-1A DET III FIG 101. FORMED, LOCATED, DRILLED AND TRIMMED NEW
- [SDR FDEA201711183273](https://openairdocs.org/sdr/FDEA201711183273.md): Cusp Web · corroded · Nov 18, 2017 · N924FD · Boeing 757204 · Fuselage Miscellaneous Structure
  > MAIN DECK STA 978 LT SIDE CUSP WEB CORRODED. REMOVED CORROSION AND EVALUATED CUSP WEB MAIN DECK AT STA 978 LT, ORIGINAL MAT.056", MAT REM.044" FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13-1A DET II FIG 101. FORMED, LOCATED, DRILLED AND TRIMMED SHEAR WEB (CUSP
- [SDR FDEA201711173261](https://openairdocs.org/sdr/FDEA201711173261.md): Seat Track · corroded · Nov 17, 2017 · N924FD · Boeing 757204 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK BETWEEN BS 1360 - 1383, LBL 58.22 SEAT TRACK FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-10-02-0G, EVALUATED THE AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, DETAIL VII, FIG 101. REMOVED THE DAMAGED SEAT TRACK, TRIMMED, AND DRILLED
- [SDR FDEA201711173258](https://openairdocs.org/sdr/FDEA201711173258.md): Floorbeam · corroded · Nov 17, 2017 · N924FD · Boeing 757204 · Fuselage Main, Floor Beam
  > MAIN DECK BS 1640 BETWEEN BL 0 - LBL 58.22 FLOORBEAM TEE CORRODED. REMOVED CORROSION IAW SRM 51-10-02-0G, LBL 38 TO LBL 58.22, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A, FIG 101, DETAL VI. CUT-OUT THE DAMAGED FLOORBEAM UPPER TEE, FABRICATED ANGLES,
- [SDR FDEA201711173260](https://openairdocs.org/sdr/FDEA201711173260.md): Crease Beam · corroded · Nov 17, 2017 · N924FD · Boeing 757204 · Fuselage Main, Structure
  > MAIN DECK BETWEEN STA 900 - 1040 LBL 64 CREASE BEAM CORRODED. REMOVED CORROSION AND EVALUATED CREASE BEAM AT MAIN CABIN STA 900-1040 LBL 64 ORIGINAL MAT.070" MAT REMAINING.046" FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13-1A DET III FIG 101. REMOVED AND REPLAC
- [SDR FDEA201711173259](https://openairdocs.org/sdr/FDEA201711173259.md): Crease Beam · corroded · Nov 17, 2017 · N924FD · Boeing 757204 · Fuselage Main, Structure
  > MAIN DECK BETWEEN STA 900-1040 RBL 64 CREASE BEAM CORRODED. REMOVED CORROSION AT MAIN CABIN CREASE BEAM STA 900 AT 1040 RBL 64 AND FOUND TO BE OUT OF LIMITS ORIGINAL MAT.070" MATERIAL REM. 050" IAW SRM 53-40-13-1A DET III FIG 101. REMOVED AND REPLACED CREAS
- [SDR FDEA201711173257](https://openairdocs.org/sdr/FDEA201711173257.md): Cusp Web · corroded · Nov 17, 2017 · N924FD · Boeing 757204 · Fuselage Miscellaneous Structure
  > MAIN DECK STA 1110 LBL 70 CUSP WEB CORRODED. REMOVED CORROSION AT CUSP WEB MAIN DECK STA 1110 LBL 70 AND EVALUATED ORIGINAL MAT.063" MAT REM.030" FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13-1A DET III FIG 101. FORMED, LOCATED, DRILLED AND TRIMMED NEW SHEAR WE
- [SDR FDEA201711153244](https://openairdocs.org/sdr/FDEA201711153244.md): Web · corroded · Nov 15, 2017 · N924FD · Boeing 757204 · Fuselage Miscellaneous Structure
  > MAIN DECK WEB BETWEEN BS 1640 - 1680, LBL 54 CORRODED. REMOVED THE CORROSION IAW SRM 51-10-02-0G, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A, DETAIL VIII, FIG 101. REMOVED THE WEB, FABRICATED AND INSTALLED A NEW WEB IAW DWG 657N4304, REV - AND SRM
- [SDR FDEA201711153243](https://openairdocs.org/sdr/FDEA201711153243.md): Crease Beam · corroded · Nov 15, 2017 · N924FD · Boeing 757204 · Fuselage Main, Structure
  > MAIN DECK CREASE BEAM BETWEEN BS 1610 - 1620, LBL 64 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13-1A, DET II. CUT OUT THE DAMAGE AREA BS 1570 TO 1630 IAW SRM 53-00-13-2R, LOCATED, DRILLED, AND TRIMMED A NEW CREASE BEAM SECTION,
- [SDR FDEA201711153242](https://openairdocs.org/sdr/FDEA201711153242.md): Crease Beam · corroded · Nov 15, 2017 · N924FD · Boeing 757204 · Fuselage Main, Structure
  > MAIN DECK BETWEEN BS 1370 - 1415, LBL 64 CREASE BEAM CORRODED. D. REMOVED THE CORROSION. FOUND OUT OF LIMITS IAW SRM 53-60-13-1A, DET II AND III, CUT OUT DAMAGE SECTION FROM BS 1480 TO 1360 IAW SRM 53-00-13-2R. LOCATED AND DRILLED A NEW CREASE BEAM, CHANNE
- [SDR FDEA201711103319](https://openairdocs.org/sdr/FDEA201711103319.md): Stringer · corroded · Nov 10, 2017 · N924FD · Boeing 757204 · Fuselage Main, Longeron/Stringer
  > CORROSION BS 1434 STR 26L STRINGER AT AFT CARGO PIT. REMOVED DAMAGED ON STRINGER 26L STA 1434,EVAL ORINAL MAT. 0.080",MAT. LOSS 0.080",MAT. REMAINING 0.000",FOUND TO BE OUT OF LIMITS IAW B 757 SRM 53-00-03-1A FIG 101,DETAIL II AND B DWG. # 140N1530 REV.
- [SDR FDEA201710213021](https://openairdocs.org/sdr/FDEA201710213021.md): Door · lack of lube · Oct 21, 2017 · N924FD · Boeing 757204 · Passenger/Crew Doors
  > L1 DOOR IS HARD TO OPEN AND CLOSE. LUBRICATED THE DOOR IAW MM 12-21-18-3. OPERATED THE DOOR IAW MM 52-11-00-2. OPS CHECKED NORMAL. OK FOR SERVICE.

Next page: https://openairdocs.org/aircraft/N924FD/reports.md?page=2

## 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 n_number = 'N924FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N924FD/reports

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