# Service difficulty reports: N785FD

A list on [N785FD](https://openairdocs.org/aircraft/N785FD.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 2 · 78 reports

- [SDR FDEA202608221217](https://openairdocs.org/sdr/FDEA202608221217.md): Seat Track · corroded · Aug 22, 2026 · N785FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > GALLEY AREA STA 360-370 RBL 50, SEAT TRACK HAS CORROSION COMPLIED WITH EA# F-5310-T0388291. MAJOR REPAIR.
- [SDR FDEA202608201194](https://openairdocs.org/sdr/FDEA202608201194.md): Crease Beam · corroded · Aug 20, 2026 · N785FD · Boeing 757222 · Fuselage Main, Structure
  > MAIN DECK FLOOR STRUCTURE CREASE BEAM PROFILE AT LBL 64 HAS CORROSION BETWEEN BODY STA 1040 AND BODY STA 1080. REPAIRED CREASE BEAM INBOARD CHRORD AT LBL 64 BETWEEN STA 1040 TO STA 1080 MAIN DECK FLOOR STRUCTURE IAW B757 SRM 53-00-13-2R FIG 201 SHEET 1 TO
- [SDR FDEA202608181144](https://openairdocs.org/sdr/FDEA202608181144.md): Skin · dented · Aug 18, 2026 · N785FD · Boeing 757222 · Leading Edge Devices
  > DENT AT R/H WING SLAT #9 UPPER TRAILING EDGE AT OSS 669. REPAIRED DENT ON RH WING SLAT #9 UPPER EDGE AT OSS 669 IAW B757 SRM 51-70-10-2R. MAJOR REPAIR
- [SDR FDEA202608181143](https://openairdocs.org/sdr/FDEA202608181143.md): Skin · dented · Aug 18, 2026 · N785FD · Boeing 757222 · Trailing Edge Flaps
  > LEFT WING INBD FLAP HAS TWO DENTS AT WS 177.50 ZONE 553. REPAIRED LT WING INBD FLAP PANEL IAW SRM 51-70-10-2R. MAJOR REPAIR.
- [SDR FDEA202601210079](https://openairdocs.org/sdr/FDEA202601210079.md): Bulb · dim · Jan 21, 2026 · N785FD · Boeing 757222 · Emergency Lighting
  > L1 OVERHEAD EMERGENCY EXIT SIGN DIM. AMM: 33-51-01-2 REMOVED AND REPLACED 17 FAULTY BULBS AT THE L1 OVERHEAD EXIT SIGN AS PER ABOVE REF. OPS CHECK GOOD. (P/N OL3071BPEGPL) A/C OK FOR SERVICE.
- [SDR FDEA202408241170](https://openairdocs.org/sdr/FDEA202408241170.md): Skin · ground damage · Aug 24, 2024 · N785FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > DURING TOWING OF THE AIRCRAFT INTO THE HANGAR 8.2, TAIL LH SIDE OF FUSELAGE STA 1768.80 TO STA 1787.45 STRINGER 20L MADE CONTACT WITH THE TAIL STAND. ACCMPLISHED REPAIR IAW EA 757-5380-16-A3665 SECTION 48 - FUSELAGE STA 1768 TO STA 1787.5 S-19L TO S-20L LA
- [SDR FDEA202311221884](https://openairdocs.org/sdr/FDEA202311221884.md): Collar · sheared · Nov 22, 2023 · N785FD · Boeing 757200 · Passenger/Crew Doors
  > GUST LOCK BROKEN ON R1 ENTRY DOOR. VERIFIED HOLD-OPEN COLLAR NEEDS REPLACED BUT NIS AT GSO. R1 ENTRY OPEN & CLOSED SEVERAL TIMES REF FDX RELEASED FOR SERVICE PER MEL: 52-11-01-A. REMOVED AND REPLACED R1 DOOR GUST LOCK REF B757 AMM 52-11-08-4. OP CHECK G
- [SDR FDEA202311161867](https://openairdocs.org/sdr/FDEA202311161867.md): Adapter · loose · Nov 16, 2023 · N785FD · Boeing 757200 · Aileron Control System
  > PDIS 785 27-10 7609 16NOV23 IND FACT U IN THE FLARE BELOW APPROXIMATELY 50 IT TOOK SIGNIFICANTLY MORE EFFORT THAN NORMAL TO MOVE THE CONTROL WHEEL LEFT OR RIGHT. THE RESISTANCE INCREASES SIGNIFICANTLY AFTER A SHORT AMOUNT OF CONTROL WHEEL TR
- [SDR FDEA202301300179](https://openairdocs.org/sdr/FDEA202301300179.md): Battery · discharged · Jan 30, 2023 · N785FD · Boeing 757222 · Emergency Lighting
  > ONE EMERGENCY LIGHT WILL NOT ILLUMINATE EXTERIOR OF L1 DOOR. DUE TO EXTENDED LAYOVER BATTERIES NEEDED TO BE CHARGED FOR OPS CHECK. PERFORMED ADJUSTMENT/TEST PER B757 AMM 33-51-00-5 WITH NO DEFECTS NOTED. AC OK FOR SERVICE.
- [SDR FDEA202211012705](https://openairdocs.org/sdr/FDEA202211012705.md): Sensor · failed · Nov 1, 2022 · N785FD · Boeing 757222 · Leading Edge Slat Position Indicating System
  > LE SLAT ASYM MESSAGE ON DEPARTURE BETWEEN FLAPS 1 AND UP. RAN QRH AND COMPLIED WITH CHECKLIST. DECLARED EMERGENCY AND RETURNED TO MCI. REST OF FLIGHT WAS UNEVENTFUL. EMERGENCY DECLARED AMM: 27-81-41-4 REMOVED AND REPLACED LOSS SENSING SWITCH FOR THE I
- [SDR FDEA202210222643](https://openairdocs.org/sdr/FDEA202210222643.md): Fitting · corroded · Oct 22, 2022 · N785FD · Boeing 757222 · Nacelle/Pylon, Attach Fittings
  > LT WING PYLON DRAG LINK FITTING HAS CORROSION IN 5EA HOLES IN FITTING LAYER ONLY. HOLE NUMBERS 1,3,8,10, AND 15. COMPLIED WITH EA F-5730-T0370901 PT1 WINGS - PLATES AND SKIN AT PYLON DRAG FITTING, CORROSION FINDINGS. THIS EA DEVIATES FROM EO F-5730-E034007
- [SDR FDEA202210212636](https://openairdocs.org/sdr/FDEA202210212636.md): Floorbeam · cracked · Oct 21, 2022 · N785FD · Boeing 757222 · Fuselage Main, Floor Beam
  > VIEW FROM FWD CARGO COMPT. MAIN CARGO FLOOR BEAM AT BS 580 LBL 45 HAS CRACK. REPAIRED FLOOR BEAM AT STA 580 LBL 45 IAW EA TF-5310-T0370825 PT1. FUSELAGE - MAINFRAME- FLOOR BEAM AT STA 580 AND LBL 45 CRACKED - REPAIR PER DRAWING SR57-53- 004. MAJOR REPAIR
- [SDR FDEA202210212634](https://openairdocs.org/sdr/FDEA202210212634.md): Floor Support · corroded · Oct 21, 2022 · N785FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR FS1681. FS 1681 FLOOR BEAM UPPER CHORD, UPPER SECTION EXFILIATED BETWEEN WEB AND FLOOR BEAM APPROX LBL12. REPAIRED MAIN DECK FLORO FS 1681 FLOOR BEAM UPPER CHORD, UPPER SECTION FROM LBL 3 TO LBL 20 IAW SRM 53-60-51-2R. CORROSION FOUND OUT O
- [SDR FDEA202210212633](https://openairdocs.org/sdr/FDEA202210212633.md): Attach Fitting · corroded · Oct 21, 2022 · N785FD · Boeing 757222 · Nacelle/Pylon, Attach Fittings
  > #2 ENGINE PYLON DRAG LINK ATTACHMENT FITTING HAS 8 HOLES WITH CORROSION. HOLES 2,3,5,7,10,14. AND 15 IN FITTING LAYER. HOLE 8 HAS CORROSION IN SKIN LAYER. COMPLIED WITH EA F-5730-T03700894 PT1 R/H WING UPPER SKIN AT DRAG FITTING CORROSION FINDINGS. THIS
- [SDR FDEA202210192623](https://openairdocs.org/sdr/FDEA202210192623.md): Floorboard · delaminated · Oct 19, 2022 · N785FD · Boeing 757222 · Fuselage Floor Panel
  > ZONE 20 FLOOR BOARD 222MAF IS DELAMINATED. FABRICATED ZONE 220 FLOOR BOARD 222MAF ON VT MAE TRAVELER T22/1638358 IAW DWG SRZ- 25-005 REV R. MAJOR REPAIR
- [SDR FDEA202210192622](https://openairdocs.org/sdr/FDEA202210192622.md): Floorboard · delaminated · Oct 19, 2022 · N785FD · Boeing 757222 · Fuselage Floor Panel
  > ZONE 220 FLOOR BOARD 221MBF IS DELAMINATED FABRICATED ZONE 220 FLOOR BOARD 221MBF ON VT MAE TRAVELER T22/1638356 IAW DWG SRZ-25-005 REV R. MAJOR REPAIR
- [SDR FDEA202210192621](https://openairdocs.org/sdr/FDEA202210192621.md): Floorboard · delaminated · Oct 19, 2022 · N785FD · Boeing 757222 · Fuselage Floor Panel
  > ZONE 220 FLOOR BOARD 222AF IS DELIAMINATED FABRICATED ZONE 220 FLOOR BOARD 222AF ON VT MAE TRAVELER T22/1638359 IAW DWG SRZ- 25- 005 REV R. MAJOR REPAIR
- [SDR FDEA202210192619](https://openairdocs.org/sdr/FDEA202210192619.md): Floorboard · delaminated · Oct 19, 2022 · N785FD · Boeing 757222 · Fuselage Floor Panel
  > ZONE 220 FLOOR BOARD 221AF IS DELAMINATED. FABRICATED ZONE 220 FLOOR BOARD 221AF ON VT MAE TRAVELER T22/1638355 IAW DWG SRZ- 25- 005 REVISION R. MAJOR REPAIR
- [SDR FDEA202207291807](https://openairdocs.org/sdr/FDEA202207291807.md): Slide · dislodged · Jul 29, 2022 · N785FD · Boeing 757200 · Escape Slide
  > DOOR WAS DISARMED AND NEW CALLOUT WAS MADE BUT SLIDE FELL OUT OF DOOR. SLIDE DID NOT DEPLOY. REMOVED AND INSTALLED NEDW R-1 DOOR SLIDE RFEF B757 AMM 25-66-01-4 GIRT BAR OPERATES
- [SDR FDEA202205171225](https://openairdocs.org/sdr/FDEA202205171225.md): Gust Lock · damaged · May 17, 2022 · N785FD · Boeing 757200 · Passenger/Crew Doors
  > L1 DOOR GUST LOCK FOUND BROKEN ON POST FLIGHT. (REMOVED BROKEN COLLAR) INSTALLED NEW GUST LOCK TO L1 DOOR REFERENCE TO AMM 52-11-08-8. DOOR OPS CHECK GOOD TO AMM 52-11-08-8.
- [SDR FDEA202203040417](https://openairdocs.org/sdr/FDEA202203040417.md): Bulb · failed · Mar 4, 2022 · N785FD · Boeing 757200 · Emergency Lighting
  > MDIS 785 33-50 6302 04MAR22 EWR FACT U ON SERVICE CHECK FOUND LH EMERGENCY SLIDE LIGHT INOP. FACT 04MAR22 18:42 EWR U RELAMPED LH EMERGENCY SLIDE LIGHT AS PER 757 AMM 33-51-06-2-1. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.
- [SDR FDEA202202220348](https://openairdocs.org/sdr/FDEA202202220348.md): Door · gouged · Feb 22, 2022 · N785FD · Boeing 757200 · Cargo/Baggage Doors
  > MAIN CARGO DOOR IS GOUGED AND DENTED ON SKIN AT STA 599 REPAIRED REF 757 SRM 52-30-01-2R REPAIR 4 AND EA F-5230-T0367049
- [SDR FDEA202012183189](https://openairdocs.org/sdr/FDEA202012183189.md): Cylinder · discharged · Dec 18, 2020 · N785FD · Boeing 757222 · Emergency Equipment
  > R1 DOOR EMERGENCY POWER RESERVOIR CYLINDER DISCHARGED. REMOVED AND REPLACED EMERGENCY POWER RESERVOIR, REF B757 AMM 52-11-32-4.
- [SDR FDEA2020062321650](https://openairdocs.org/sdr/FDEA2020062321650.md): Vane · damaged · Jul 22, 2019 · N785FD · Boeing 757222 · Engine Thrust Reverser
  > DURING POST STORM WALKAROUND FOUND RT ENGINE RT THRUST REVERSER HALF AT 2 O'CLOCK POSITION L.E. DAMAGE APPX 16 INCHES X 9 INCHES. TEMP REPAIR PER EA F-7830-T0348334. COMPLIED WITH EA F-7830-T0348334 PT 1 INSTALLED RT ENGINE O/B SLEEVE IAW AMM 78-31-07-4,
- [SDR FDEA2020061621650](https://openairdocs.org/sdr/FDEA2020061621650.md): Cascade · damaged · Jul 22, 2019 · N785FD · Boeing 757222 · Engine Thrust Reverser
  > DURING POST STORM WALKAROUND FOUND RT ENGINE RT T/R HALF AT 2 O'CLOCK POSITION L.E. DAMAGE APPX 16 INCHES X 9 INCHES.
- [SDR FDEA201609203316](https://openairdocs.org/sdr/FDEA201609203316.md): Frame · punctured · Sep 20, 2016 · N785FD · Boeing 757222 · Fuselage Main, Frame
  > FRAME AT BS 231, BL 0 IS PUNCTURED. REPAIRED IAW EA F-5310-T0328373 P1.
- [SDR FDEA201605251733](https://openairdocs.org/sdr/FDEA201605251733.md): Unknown · odor · May 25, 2016 · N785FD · Boeing 757222 · Air Distribution System
  > THREE TIMES DURING FLIGHT WE SMELLED AN ACRID ELEC BURNING SMELL. NO SMOKE NOTED & UNABLE TO ISOLATE. FIRST OFFICER ALWAYS SMELLED IT FIRST. ALWAYS WENT AWAY IN 1 MIN. NO SMELL IN COURIER AREA. IAW FIM 21-00 PROC 4, SINCE FAULT CAN'T BE DUPLICATED & ALL E
- [SDR FDEA201511253776](https://openairdocs.org/sdr/FDEA201511253776.md): Light · inoperative · Nov 25, 2015 · N785FD · Boeing 757222 · Emergency Lighting
  > R1 DOOR EXTERNAL SLIDE LIGHT INOPERATIVE. R & R R1 DOOR SLIDE LIGHT ASSEMBLY IAW MM 33-51-06-2-1. OPERATIONS CHECKED NORMAL.
- [SDR FDEA201505011355](https://openairdocs.org/sdr/FDEA201505011355.md): Lamp · inoperative · May 1, 2015 · N785FD · Boeing 757222 · Emergency Lighting
  > DURING SERVICE CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE, REPLACED THE LAMP. ALL OPS CHECKED NORMAL IAW AMM 33-51-06-2-1.
- [SDR FDEA201410133133](https://openairdocs.org/sdr/FDEA201410133133.md): Doubler · scratched · Oct 13, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN, WHILE PERFORMING EA F-5330-T0308700PT1 FOUND DOUBLER HAS SCRATCHES AT STATION 1350 STRINGER 1 - 2R. SCRATCH ON DOUBLER CLEARED & TREATED IAW SRM 51-10-02 REV 112 & SRM 51-20-01 REV 112. FOUND NO SIGNIFICANT MATERIAL LOST. PART 1 OF E
- [SDR FDEA201410103075](https://openairdocs.org/sdr/FDEA201410103075.md): Skin · dented · Oct 10, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A DENT BS 1701 - 1720 STRINGER 28 - 30R. REPAIRED IAW EA F5330-T0310832. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201410083010](https://openairdocs.org/sdr/FDEA201410083010.md): Floorbeam · corroded · Oct 8, 2014 · N785FD · Boeing 757222 · Fuselage Main, Floor Beam
  > BS 377.7 LBL 55 - 60 FLOORBEAM UPPER TEE FOUND CORROED ON LOWER SURFACE. FLOORBEAM TEE REMOVED AND REPLACED IAW DWG 141N5113 SHT 1 REV F. DWG 141N5123 SHT 1 REV A AND EA F-5310-T0311051 PART 1. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201410072997](https://openairdocs.org/sdr/FDEA201410072997.md): Skin · damaged · Oct 7, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAD NUMEROUS NICKS & SCRATCHES BETWEEN STRINGER 26L & 26R BETWEEN BS 1701 - 1720. DAMAGE REMOVED AND TREATED IAW SRM 51-10-02 REV 112. FOUND ONE SPOT OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE 1 REV 112, REPAIRED OUT OF LI
- [SDR FDEA201410022892](https://openairdocs.org/sdr/FDEA201410022892.md): Skin · damaged · Oct 2, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN HAD A LIGHTNING STRIKE AT BS 1654 STRINGER 28 - 29L. THE DAMAGE WAS REMOVED AND TREATED IAW SRM 53-00-01 REPAIR 6 AND SRM 51-20-01 REV 112, FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE I REV 112. REPAIR CAR
- [SDR FDEA201410022891](https://openairdocs.org/sdr/FDEA201410022891.md): Skin · damaged · Oct 2, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN HAD A LIGHTNING STRIKE AT BS 1622 STRINGER 27 - 28L. THE DAMAGE WAS REMOVED AND TREATED IAW SRM 53-00-01 REPAIR 6 REV 112 AND 51-20-01 REV 112 AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE 1 REV 112. PART 1
- [SDR FDEA201410022890](https://openairdocs.org/sdr/FDEA201410022890.md): Skin · damaged · Oct 2, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN HAS A LIGHTNING STRIKE AT BS 1627 STRINGER 27 - 28L. DAMAGE WAS REMOVED AND TREATED IAW SRM 53-00-01 REPAIR 6 REV 112 AND 51-20-01 REV 112 AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 11 DETAIL II ALLOWABLE DAMAGE 1 REV 112. REPAIR CA
- [SDR FDEA201410022889](https://openairdocs.org/sdr/FDEA201410022889.md): Skin · damaged · Oct 2, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN HAS A LIGHTNING STRIKE AT BS 1630 STRINGER 27 - 28L. DAMAGE WAS REMOVED AND TREATED IAW SRM 53-00- 01 REPAIR 6 REV 112 AND 51-20-01 REV 112 AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE I REV 112. REPAIR
- [SDR FDEA201410022888](https://openairdocs.org/sdr/FDEA201410022888.md): Skin · damaged · Oct 2, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN HAS A LIGHTNING STRIKE AT BS 1653 STRINGER 28 - 29L. DAMAGE REMOVED IAW SRM 53-00- 01 REPAIR 6 REV 112 AND 51-20-01 REV 112 AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE I REV 112. REPAIR CARRIED OUT IAW E
- [SDR FDEA201410022913](https://openairdocs.org/sdr/FDEA201410022913.md): Skin · damaged · Oct 2, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN HAD A LIGHTNING STRIKE AT BS 1581 STRINGER 27 - 28L. DAMAGE BLENDED AND FOUND OUT OF LIMITS IAW SRM 53- 00-01 FIG 101 DETAIL II ALLOWANCE DAMAGE 1 REV 112. REPAIR CARRIED OUT IAW EA F-5330-T0311361. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201410022912](https://openairdocs.org/sdr/FDEA201410022912.md): Skin · damaged · Oct 2, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN HAD A LIGHTNING STRIKE AT BS 1576 STRINGER 27 - 28L. BLENDED THE DAMAGE AND FOUND OUT OF LIMITS IAW SRM 53- 00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE 1 REV 112. REPAIR CARRIED OUT IAW EA F-5330-T0311361. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201410022914](https://openairdocs.org/sdr/FDEA201410022914.md): Skin · damaged · Oct 2, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN HAD A LIGHTNING STRIKE AT BS 1571 STRINGERS 27 - 28L. DAMAGE BLENDED AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWANCE DAMAGE 1 REV 112. REPAIR CARRIED OUT IAW EA F-5330-T0311361. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201410012879](https://openairdocs.org/sdr/FDEA201410012879.md): Frame Splice · gouged · Oct 1, 2014 · N785FD · Boeing 757222 · Fuselage Main, Frame
  > AFT CARGO BAY BS 1520 STRINGER 24 - 25R, FRAME SPLICE FOUND DAMAGED. REMOVED AND REPLACED IAW SNRM N04012. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201409282844](https://openairdocs.org/sdr/FDEA201409282844.md): Skin · damaged · Sep 28, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > MULTIPLE TOOL DAMAGE ON THE INTERIOR SKIN AT BS 1420 - 1423, STRINGER 25L - 26L. REPAIRED IAW EA F-5330-T0311215 PART 1. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201409262791](https://openairdocs.org/sdr/FDEA201409262791.md): Frame · gouged · Sep 26, 2014 · N785FD · Boeing 757222 · Fuselage Main, Frame
  > AFT CARGO BAY FRAME BS 1360 STRINGER 23 - 24L OUTER FLANGE GOUGED. REPAIRED IAW EA F5310-T0311806 P1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201409262793](https://openairdocs.org/sdr/FDEA201409262793.md): Skin · cracked · Sep 26, 2014 · N785FD · Boeing 757222 · Cargo/Baggage Doors
  > THERE IS A CRACK AT FWD CARGO DOOR EXTERIOR SKIN AT LOWER AFT CORNER BS 600 - 620 STRINGER 25 - 26R. REPAIRED IAW EA F-5230-T0311723. REPAIR CLASSIFED AS MAJOR.
- [SDR FDEA201409252761](https://openairdocs.org/sdr/FDEA201409252761.md): Skin · cracked · Sep 25, 2014 · N785FD · Boeing 757222 · Passenger/Crew Doors
  > L4 DOOR INTERNAL HANDLE BOX CUT OUT AFT EDGE INNER SKIN FOUND CRACKED AT EDGE. REPAIRD IAW EA F-5210-T0311310 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201409232722](https://openairdocs.org/sdr/FDEA201409232722.md): Skin · gouged · Sep 23, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > EXISTING REPAIR FINDING FUSELAGE THERE IS GOUGE ON THE INTERIOR SURFACE OF THE DOUBLER OF THE EXISTING REPAIR AT STATION 1350 STRINGER 29L - 28R. REMOVED BY HAND CLEAN & TREATED PER SRM 51-10-01 REV 112 AND SRM 51-20-01 REV 112. NEW REPAIR CARRIED OUT PER F
- [SDR FDEA201409232711](https://openairdocs.org/sdr/FDEA201409232711.md): Frame · corroded · Sep 23, 2014 · N785FD · Boeing 757222 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT STATION 1380 RBL 10 FRAME UPPER CHORD FOUND CORROSION DURING REMOVING CORROSION AT FRAME FLANGE IAW SNRM N03563. COMPLIED AS PER EA F-5310-T0311624 P1 TITLE: FUSELAGE - MAINFRAME - REPAIR FOR OUT OF LIMIT BLEND OUT CORROSION AT FREE F
- [SDR FDEA201409232709](https://openairdocs.org/sdr/FDEA201409232709.md): Frame · corroded · Sep 23, 2014 · N785FD · Boeing 757222 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT STATION 1380 BL0 - RBL 15 FRAME FLANGE HAS CORROSION. COMPLIED AS PER EA F-5310 - T0311624 PT 1. TITLE: FUSELAGE - MAINFRAME - REPAIR FOR OUT OF LIMIT BLEND OUT CORROSION AT FREE FLANGE OF STA 1380 146N1028-88 BOTTOM FRAME AND 146N8511
- [SDR FDEA201409182654](https://openairdocs.org/sdr/FDEA201409182654.md): Skin · gouged · Sep 18, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > GOUGES ON EXTERIOR SURFACE OF THE REPAIR DOUBLER BS 1701 - 1720 STRINGERS 28 - 30R. REPAIRED IAW EA F-5330-T0310832. REPAIR CLASSIFIED AS MAJOR.

Next page: https://openairdocs.org/aircraft/N785FD/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 = 'N785FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N785FD/reports

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