# Service difficulty reports: N783FD

A list on [N783FD](https://openairdocs.org/aircraft/N783FD.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 · 54 reports

- [SDR FDEA202608221216](https://openairdocs.org/sdr/FDEA202608221216.md): Rub Strip · gouged · Aug 22, 2026 · N783FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > AFT LOWER CARGO DOOR CONTROL PANEL LOWER CUT OUT HAS A GOUGE ACCOMPHLISHED REPAIR 18 - CARGO DOOR PANEL ACCESS DOOR CUTOUT SKIN REPAIR IAW B757 SRM 53-00-01-2R
- [SDR FDEA202608201192](https://openairdocs.org/sdr/FDEA202608201192.md): Skin · damaged · Aug 20, 2026 · N783FD · Boeing 757222 · Horizontal Stabilizer, Plate/Skin
  > DURING AGING AIRCRAFT INSPECTION FOUND PREVIOUS EXISTING REPAIR ON RH HORIZONTAL STAB LOWER SKIN, INBD AREA, NOT INCLUDED ON THE MCMRT/CCMRP COMPLIED WITH EA F -5510-T0324519 A P3 TITLE: STABILIZER -HORIZONTAL STABILIZER-RIGHT HORIZONTAL STAB LOWER SKIN DAMA
- [SDR FDEA202601120026](https://openairdocs.org/sdr/FDEA202601120026.md): Battery Pack · failed · Jan 12, 2026 · N783FD · Boeing 757222 · Emergency Lighting
  > AFTER WEEKEND LAYOVER, DURING MX PRE-FLIGHT CHECKS, FOUND EMERGENCY EXIT LIGHTS POWERED BY M730 INOP. AMM: 33-51-07-2 GMM: 12-7-600 REMOVED AND REPLACED BATTERY HOLDER ASSY. M730, MFR: RADIANT POWER CORP, MPN 2013-1A, S/N 118058, OPS CHECKS GOOD. A/C
- [SDR FDEA202505090743](https://openairdocs.org/sdr/FDEA202505090743.md): Gust Lock · damaged · May 9, 2025 · N783FD · Boeing 757222 · Passenger/Crew Doors
  > L1 DOOR GUST LOCK COLLAR BROKEN. INSTALLED A NEW L1 DOOR GUST LOCK COLLAR, OPS CHECKS GOOD, OK FOR SERVICE.
- [SDR FDEA202504040563](https://openairdocs.org/sdr/FDEA202504040563.md): Gust Lock · broken · Apr 4, 2025 · N783FD · Boeing 757222 · Passenger/Crew Doors
  > L1 DOOR GUST LOCK IS BROKEN (LOCK IS REMOVED). INSTALLED NEW GUST LOCK. OPS CHECK OK.
- [SDR FDEA202411171683](https://openairdocs.org/sdr/FDEA202411171683.md): Lamp · failed · Nov 17, 2024 · N783FD · Boeing 757222 · Emergency Lighting
  > L1 DOOR EXTERIOR SLIDE LIGHT INOP FACT 17NOV24 17:47 BNA AMM: 33-51-06-2-1 RELAMPED L1 DOOR EXTERIOR SLIDE LIGHT, OP'S CHECKS GOOD REF AMM 33-51-06-2-1. BULB PART NUMBER 767 REPLACED.
- [SDR FDEA202411121668](https://openairdocs.org/sdr/FDEA202411121668.md): Clamp · leaking · Nov 12, 2024 · N783FD · Boeing 757222 · Cabin Cooling System
  > LOSS OF CABIN PRESSURE AT FL340. CABIN CLIMBED TO @ 14,000 DURING THE DESCENT WITH THE CABIN CONTINUING TO CLIMB @700 FPM. COMPLIED WITH QRH NO OBVIOUS FUSELAGE LEAKS NOTED ON WALK AROUND. AUTOMATIC CABIN PRESSURE CONTROLLER 1 AND 2 BITE CHECK GOOD.
- [SDR FDEA202409061250](https://openairdocs.org/sdr/FDEA202409061250.md): Web · cracked · Sep 6, 2024 · N783FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > AFTER INSPECTION PER ED F-5310-E0329085DP5 STEP 3, A CRACK WAS FOUND AT FR-1640 LH, S- 14. COMPLIED WITH FEDEX E.A. # F -5310-T0380418 P1 TITLE: FUSELAGE- MAINFRAME - LH STA 1640 - TYPICAL FRAME SPLICE REPAIR BETWEEN STRINGER S-9L AND S-20L.
- [SDR FDEA202405150671](https://openairdocs.org/sdr/FDEA202405150671.md): Wire · broken · May 15, 2024 · N783FD · Boeing 757222 · Light System Wiring
  > WHEN SELECTING EMERGENCY LTS SWITCH ON OVERHEAD TO ON, COCKPIT OVERHEAD LT DOES NOT ILLUMINATE. ALL OTHERS OPERATE NORMALLY. PER WDM 33-51-21 FOUND GOOD GROUND BITWEEN GD602 AND G TERMINAL OF RESISTER R10381 AND DISCOVERED THAT WIRE WAS BROKEN FROM RESISTE
- [SDR FDEA202212072887](https://openairdocs.org/sdr/FDEA202212072887.md): Drag Fitting · corroded · Dec 7, 2022 · N783FD · Boeing 757200 · Wing, Attach Fittings
  > HOLE #2 AND 5 ON UPPER SKIN AND DRAG FITTINGS PRESENT CORROSION RH WING. WORKS STEPS ACCOMPLISHED ON EA #: F5730-T0371761 MAJOR REPAIR.
- [SDR FDEA202212072886](https://openairdocs.org/sdr/FDEA202212072886.md): Drag Fitting · corroded · Dec 7, 2022 · N783FD · Boeing 757200 · Wing, Attach Fittings
  > HOLES 4 & 5 ON LT WING UPPER SKIN DRAG FITTINGS PRESENT CORROSION. WORKS STEPS ACCOMPLISHED ON EA F5730-T0371760 EA TITLE: WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, CORROSION FINDINGS* THIS EA DEVIATES FROM EO F-5730-E0340076. MAJOR
- [SDR FDEA202212072883](https://openairdocs.org/sdr/FDEA202212072883.md): Floorboard · delaminated · Dec 7, 2022 · N783FD · Boeing 757222 · Fuselage Floor Panel
  > ZONE 220 FLOORBOARD 221MBF IS DELAMINATED. FABRICATED ZONE 220 FLOORBOARD 221MBF ON TRAVELER T22/1649009 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIR
- [SDR FDEA202211282850](https://openairdocs.org/sdr/FDEA202211282850.md): Floorbeam · cracked · Nov 28, 2022 · N783FD · Boeing 757222 · Fuselage Main, Floor Beam
  > FWD PIT CEILING AREA STA 580 FLOOR BEAM UPPER CAP AFT SIDE FLANGE RADIUS HAS SUSPECTED CRACK, APPROX LBL 45. FLOOR BEAM WAS REPAIRED AND NEW ANGLE & RADIUS STRAP INSTALLED ON FWD PIT CEILING AREA STA 580 AT LBL 45 IAW DRAWING SR57-53-004 & SRM 51-40-02. MA
- [SDR FDEA202209122309](https://openairdocs.org/sdr/FDEA202209122309.md): Battery · no test · Sep 12, 2022 · N783FD · Boeing 757222 · Emergency Lighting
  > R1 EMERGENCY EXIT SIGN, R1 SLIDE LIGHT AND EMERGENCY EXIT LOCATOR SIGN INOP DURING EMERGENCY LIGHT TEST. FOUND THAT AFTER AIRCRAFT HAD BEEN POWERED FOR OVER AN HOUR, ALL LIGHTS WOULD TEST, HOWEVER THE TEST ONLY LASTED APPROX 5-10 SECONDS, ALL OTHERS STA
- [SDR FDEA202204130945](https://openairdocs.org/sdr/FDEA202204130945.md): Fmc · failed · Apr 13, 2022 · N783FD · Boeing 757222 · Flight Management Computing Software System
  > L AND R FMC FAIL -EMERGENCY DECLARED ***EMERGENCY DECLARED*** R&R'D BOTH FMC COMPUTERS. UPDATED ALL SOFTWARE. BOTH FMCS OPS CKS NORMALLY. REF B757 MM SEC 34-61-01-4-1. ALL SOFTWARE UPDATED TO CURRENT REQUIREMENTS.
- [SDR FDEA202202090257](https://openairdocs.org/sdr/FDEA202202090257.md): None · failed · Feb 9, 2022 · N783FD · Boeing 757200 · Fuel Controlling System
  > PDIS 783 73-20 6104 09FEB22 TPA OPEN U CLIMBING THROUGH FL300 LEFT ENGINE BEGAN SPOOLING DOWN. AUTOTHROTTLES DISCONNECTED WITH THE MASTER CAUTION. EMERGENCY WAS DECLARED AND DIVERTED TO TPA. ENGINE THRUST CAME BACK AFTER APPROXIMATELY 10 S
- [SDR FDEA202202030203](https://openairdocs.org/sdr/FDEA202202030203.md): None · leaking · Feb 3, 2022 · N783FD · Boeing 757200 · Engine Oil Quantity
  > PDIS 783 79-32 6083 03FEB22 TPA OPEN U EMERGENCY DECLARED. DURING CLIMB OUT FROM TAMPA TO MEMPHIS, HAD INDICATION OF HIGH OIL TEMP ON LEFT ENGINE. SOON AFTER, NOTICED OIL QUANTITY WAS ZERO. OIL PRESSURE WAS NORMAL. RETARDED LEFT THRUST LEVER
- [SDR FDEA202201300164](https://openairdocs.org/sdr/FDEA202201300164.md): None · failed · Jan 30, 2022 · N783FD · Boeing 757200 · Pneumatic Distribution System
  > AFTER ENGINE START GOT EICAS MSG: L PACK OFF. AFTER ADVANCING THROTTLE TO TAXI, MSG EXTINGUISHED. TAKEOFF POWER WAS COMPUTED FOR DTO 50 WITH TEMPERATURE MINUS 6 CELSIUS. ON RUNWAY AFTER THRUST LEVERS WERE ADVANCED TO TAKEOFF POWER AT APPROXIMATELY 100 KNOT
- [SDR FDEA202107031662](https://openairdocs.org/sdr/FDEA202107031662.md): Collar · cracked · Jul 3, 2021 · N783FD · Boeing 757222 · Service Doors
  > DURING SERVICE CHK FOUND 1R DOOR HOLD OPEN LOCK BROKEN. RMVD AND RPLD R1 DOOR HOLD-OPEN LOCK- DOOR HOLD OPEN LOCK CHKS GOOD- REF: B757 M/M 52-11-08-8
- [SDR FDEA202101210166](https://openairdocs.org/sdr/FDEA202101210166.md): Skin · cracked · Jan 21, 2021 · N783FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > R2 DOOR CUTOUT FWD FRAME UPPER HINGE CUTOUT IS CRACKED ACCOMPLISHED FEDEX EA F-5210-T0312598-B. DOORS-PASSENGER/CREW R2 DOOR EXISTING REPAIR.
- [SDR FDEA202101210165](https://openairdocs.org/sdr/FDEA202101210165.md): Guard · debonded · Jan 21, 2021 · N783FD · Boeing 757222 · Passenger/Crew Doors
  > L1 DOOR EXTERIOR HANDLE SCUFF GUARD AROUND CENTER CUTOUT IS DISBONDED. FOUND OUT OF LIMITS GOUGE UNDER SCUFF GUARD. REMOVED AND REPLACED L1 DOOR ASSEMBLY, PER FEDEX B757-2 AMM 52-11-01-4.
- [SDR FDEA202101190153](https://openairdocs.org/sdr/FDEA202101190153.md): Attach Bracket · gouged · Jan 19, 2021 · N783FD · Boeing 757222 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE STARTER DUCT SUPPORT LINK ATTACH BRACKET ON THE ENGINE SIDE IS GOUGED AT THE 3 O'CLOCK POS (OUTBOARD SIDE). REMOVED AND REPLACED NR 2 ENGINE LINK ATTACH BRACKET ON THE ENGINE SIDE AT THE 3 O'CLOCK POSITION, IAW B757 SRM 51-40-02 AND AMM 70-50-00,
- [SDR FDEA202101160131](https://openairdocs.org/sdr/FDEA202101160131.md): Skin · delaminated · Jan 16, 2021 · N783FD · Boeing 757222 · Leading Edge Devices
  > LT WING INBOARD AFT FLAP OUTBOARD EDGE DELAM. REPAIRED LT WING INBOARD AFT FLAP OUTBOARD EDGE DELAM, IAW FEDEX EA F-5750-T0359087, B757 SRM 57-53-01-2R REPAIR 1 AND 51-70-17-0G. REPAIR ACCOMPLISHED, IAW FEDEX EA F-5750-T0359087-P1 WING-FLIGHT SURFACES-LT INB
- [SDR FDEA202101140100](https://openairdocs.org/sdr/FDEA202101140100.md): Channel · cracked · Jan 14, 2021 · N783FD · Boeing 757222 · Nacelle/Pylon Miscellaneous Structure
  > NR 2 PYLON PNL 445BL IS CRACKED REMOVED AND REPLACED CHANNEL, PER B757 SRM 51-40-02 AND DWG 313N3022.
- [SDR FDEA202101140093](https://openairdocs.org/sdr/FDEA202101140093.md): Skin · damaged · Jan 14, 2021 · N783FD · Boeing 757222 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL STABILIZER WING TIP FORWARD END PAINT AND COMPOSITE DETERIORATED. REPAIRED RIGHT HORIZONTAL STABILIZER WING TIP FORWARD END PAINT AND COMPOSITE DETERIORATED, IAW B757 SRM 55-10-2R, 51-70-05-OG, 51-70-14, B757 AMM 51-21-00-7. REMOVED THEN R
- [SDR FDEA202101140091](https://openairdocs.org/sdr/FDEA202101140091.md): Web · cracked · Jan 14, 2021 · N783FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > PREVIOUS WEB REPAIR AT STA 400-420 AT APPROXIMATELY RBL 25 HAS FASTENERS WHICH ARE TOO LONG, HAVE EXCESSIVE WASHERS AND THE WEB IS DAMAGED. REMOVED DAMAGE WEB AT STA 400-420 RBL 25, IAW B757 SRM 51-40-02. RECEIVED NEW PART P/N 141N5150U54, PO NR 989969.1, IA
- [SDR FDEA202101130085](https://openairdocs.org/sdr/FDEA202101130085.md): Deck Plate · gouged · Jan 13, 2021 · N783FD · Boeing 757222 · Fuselage Main, Structure
  > PREVIOUS REPAIR ON AFT DECK PLATE AT STA 1681 RBL 12 HAS A GOUGE ON THE UPPER SURFACE. REMOVED, FABBED AND REPLACED DOUBLER, IAW B767 SRM 53-60-51-2R FIG 201 REPAIR 2.
- [SDR FDEA202101100033](https://openairdocs.org/sdr/FDEA202101100033.md): Angle · cracked · Jan 10, 2021 · N783FD · Boeing 757222 · Nacelle/Pylon Miscellaneous Structure
  > ENGINE NR 1 AFT PYLON RT SIDE FWD LOWER CORNER CLIP CRACKED UNDER PANEL 435AR. REMOVED AND REPLACED -24 CLIP AT NR 1 PYLON RT SIDE FWD LOWER CORNER, IAW B757 FEDEX DWG 313N3053 REV P AND SRM 51-40-02.
- [SDR FDEA202101070018](https://openairdocs.org/sdr/FDEA202101070018.md): Panel · cracked · Jan 7, 2021 · N783FD · Boeing 757222 · Wing, Plate/Skin
  > RT WING LEADING EDGE PANEL 611EB IS CRACKED. REPAIRED RT WING LEADING EDGE PANEL 611EB BY BONDING REPAIRPLIES, IAW B757 SRM 57-41-01-0I AND 57-41-01-2R REPAIR 1 FIG 201 AND 51-70-08 REPAIR GENERAL AND PARA 5G FIG 9. APPLIED FINISH, IAW B757 SRM 51-70-08 AND
- [SDR FDEA202101070016](https://openairdocs.org/sdr/FDEA202101070016.md): Panel · cracked · Jan 7, 2021 · N783FD · Boeing 757222 · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL STABILIZER TRAILING EDGE PANEL 335AB IS CRACKED. REPAIRED PANEL 335AB, IAW B757 SRM 55-10-01-2R FIG 201 TABLE 2 AND B757 SRM 51-70-05-0G PARA 5G.
- [SDR FDEA202010162534](https://openairdocs.org/sdr/FDEA202010162534.md): Idg · failed · Oct 16, 2020 · N783FD · Boeing 757222 · AC Generator-Alternator
  > RT GEN OFF IN FLIGHT. CREW RAN QRH AS REQUIRED. CHECKED ELEC/HYD DISPLAY SELECT SWITCH ON THE EICAS PANEL AT P61 HAD RT GEN DRIVE PUSH THE BIT SWITCH ON THE BUS POWER CONTROL UNIT MESSAGES WAS RT LOW OIL AND DELTA TEMP OPENED COWL AND FOUND DELTA P POP ON RI
- [SDR FDEA202004100728](https://openairdocs.org/sdr/FDEA202004100728.md): Linkage · broken · Apr 10, 2020 · N783FD · Boeing 757222 · Cargo/Baggage Doors
  > THE MAIN CARGO DOOR IS DENTED AND GOUGED ON SKIN AT UPPER FWD CORNER OF DOOR FROM FWD LIFT ACT. LINKAGE BREAKING. COMPLETED REPAIR OF MAIN DECK CARGO DOOR REF B757 SRM 52-30-01-2R.
- [SDR FDEA201812173530](https://openairdocs.org/sdr/FDEA201812173530.md): Deck Plate · corroded · Dec 17, 2018 · N783FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > CORROSION AROUND FASTENER HOLES IN MAIN CARGO FLOOR STRUCTURE SHEAR WEB UPPER CHORD UPPER SURFACE B.S. 1681 RBL.48 REMOVED CORROSION AT STA.1681 RBL48. ORIG. MAT..071", REM.MAT..055, MATERIAL LOSS OF.016" IS OUT OF LIMITS PER B757 SRM 53-00-51-1A. FABRIC
- [SDR FDEA201812173529](https://openairdocs.org/sdr/FDEA201812173529.md): Deck Plate · corroded · Dec 17, 2018 · N783FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > CORROSION AROUND FASTENER HOLES IN THE MAIN CARGO FLOOR STRUCTURE SHEAR WEB UPPER CHORD UPPER SURFACE B.S.1681 RBL.12. REMOVED CORROSION, MATERIAL LOSS.027", REMAINING MAT..044" OUT OF LIMITS IAW B757 SRM 53-00-51-1A DETAIL II, CUT-OUT DAMAGE, FABRICATED
- [SDR FDEA201612024305](https://openairdocs.org/sdr/FDEA201612024305.md): Skin · dented · Dec 2, 2016 · N783FD · Boeing 757222 · Vertical Stabilizer, Plate/Skin
  > SIX INCH HORIZONTAL DENT ON THE RIGHT SIDE FOR THE VERTICAL STAB VSS 125. REPAIRED THE VERTICAL STAB IAW SRM 51-70-10-2R. PRIMED AND TOP COATED IAW SRM 51-70-10-2R AND AMM 51-21-10-7.
- [SDR FDEA201611294288](https://openairdocs.org/sdr/FDEA201611294288.md): Skin · debonded · Nov 29, 2016 · N783FD · Boeing 757222 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STAB HSS 81.0 FOUND DEBONDED. REPAIRED IAW SRM 51-70-17-0G PRIMED AND TOP COATED IAW SRM 51-70-17-0G AND AMM 51-21-10-7.
- [SDR FDEA201611294287](https://openairdocs.org/sdr/FDEA201611294287.md): Frame · chafed · Nov 29, 2016 · N783FD · Boeing 757222 · Fuselage Main, Frame
  > PUNCTURE ON FRAME BS 231 FORWARD ACCESSORY ACCESS DOOR CUTOUT. REMOVED DAMAGE AND INSTALLED REPAIR IAW EA F-5310-T0330045 P1.
- [SDR FDEA201501190228](https://openairdocs.org/sdr/FDEA201501190228.md): Skin · dented · Jan 19, 2015 · N783FD · Boeing 757222 · Horizontal Stabilizer, Plate/Skin
  > A 2 INCH X 2 INCH X.094 INCH DENT ON TOP OF THE RT HORIZONTAL STAB. REPAIRED IAW SRM 55-10-01 FIG 201 REPAIR 4. CATEGORY A MAJOR REPAIR.
- [SDR FDEA201412024031](https://openairdocs.org/sdr/FDEA201412024031.md): Skin · delaminated · Dec 2, 2014 · N783FD · Boeing 757222 · Trailing Edge Flaps
  > RIGHT INBD FLAP, OTBD LOWER END, INNER SKIN DISBONDED. REPAIRED RT INBD FLAP, OTBD LOWER END SKIN IAW SRM 51-70-10. IAW EA F-5710-T0313603 FOR RSC TRACKING. MAJOR REPAIR.
- [SDR FDEA201412024030](https://openairdocs.org/sdr/FDEA201412024030.md): Skin · damaged · Dec 2, 2014 · N783FD · Boeing 757222 · Cargo/Baggage Doors
  > AFT CARGO DOOR SKIN AT LOWER AFT CORNER, NOTED EDGE WITH PREVIOUS BLEND. PREVIOUS BLEND FOUND TO BE OUT OF LIMITS IAW SRM 52-30-01 PG 104 DETAIL 4. MATERIAL LOSS.017 INCHES OF ORIGINAL.063 INCHES. REPAIR DOUBLER, INSTALLED TO REPAIR DAMAGE IAW SRM 52-30-
- [SDR FDEA201411183796](https://openairdocs.org/sdr/FDEA201411183796.md): Frame · mechanic error · Nov 18, 2014 · N783FD · Boeing 757222 · Fuselage Main, Frame
  > MAIN CABIN, LT AT BS 960 FWD EMER WINDOW CUT OUT JUST BELOW STRINGER 9L DOUBLE DRILLED HOLE IN FRAME. FUSELAGE FRAME REPAIR AT STATION 960 BELOW STRINGER 9L WAS ACCOMPLISHED DUE TO EFFECTING THE PTF CONVERSION ON EA 757-5342-16-F4770 REV DATED NOV 7 2014 & NR
- [SDR FDEA201411043504](https://openairdocs.org/sdr/FDEA201411043504.md): Skin · delaminated · Nov 4, 2014 · N783FD · Boeing 757222 · Leading Edge Devices
  > NR 1 SLAT TE WEDGE UPPER SURFACE DELAMINATED AT INBD END. REPAIRED IAW SRM 51-70-10 REPAIR 4.
- [SDR FDEA201410293416](https://openairdocs.org/sdr/FDEA201410293416.md): Frame · corroded · Oct 29, 2014 · N783FD · Boeing 757222 · Fuselage Main, Frame
  > FRAME BS 1661 STRINGER 25L TO 25R CORRODED ON AFT LOWER FLANGE. R & R FRAME IAW DWG 146N1032 & SRM 51-40-02 DUE TO CORROSION FOUND WITH MATERIAL LOSS CLEANUP OF.047 OF ORIGINAL.063 OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DETAIL II. MAJOR REPAIR.
- [SDR FDEA201410283410](https://openairdocs.org/sdr/FDEA201410283410.md): Frame · corroded · Oct 28, 2014 · N783FD · Boeing 757222 · Fuselage Main, Frame
  > BS 1620 STRINGER 22R - 23R, FRAME FOUND TO BE CORRODED. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02 AND DWG 146N1030, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG. 101, DETAIL II. MAJOR REPAIR.
- [SDR FDEA201410183300](https://openairdocs.org/sdr/FDEA201410183300.md): Frame · corroded · Oct 18, 2014 · N783FD · Boeing 757222 · Fuselage Main, Frame
  > CORROSION FOUND ON AFT FUSELAGE FRAME WEB AT BS 1681 BETWEEN STRINGERS 28 - 29R. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02 AND DWG 146N1032, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG. 101, DETAIL II. MAJOR REPAIR.
- [SDR FDEA201410183299](https://openairdocs.org/sdr/FDEA201410183299.md): Frame · corroded · Oct 18, 2014 · N783FD · Boeing 757222 · Fuselage Main, Frame
  > HIDDEN DAMAGE AFT FUSELAGE AT STATION 1710 BETWEEN STRINGER 28R & 29R FRAME WEB AFT FACE HAS CORROSION.
- [SDR FDEA201410173234](https://openairdocs.org/sdr/FDEA201410173234.md): Stringer · corroded · Oct 17, 2014 · N783FD · Boeing 757222 · Fuselage Main, Longeron/Stringer
  > HIDDEN DAMAGE STRINGER 27L STATION 1661 - 1720 CORRODED BETWEEN STRINGER & SKIN. R & R STRINGER STATION 1661 - 1720, STRINGER 27L IAW SRM 51-40-02. CORROSION WAS OUT OF LIMITS IAW SRM 53-00-03 FIG 101 DETAIL I. MAJOR REPAIR.
- [SDR FDEA201410163228](https://openairdocs.org/sdr/FDEA201410163228.md): Frame · corroded · Oct 16, 2014 · N783FD · Boeing 757222 · Fuselage Main, Frame
  > AFT PIT BS 1580 STRINGER 28L - 30 FRAME & SHEAR TIE CORRODED. REMOVED AND REPLACED FRAME AT STA 1580, FOUND TO BE OUT OF LIMITS WITH MATERIAL LOSS OF.011" OF ORIGINAL 0.63", IAW SRM 53-00-07, FIG 101, DETAIL I, AND IAW SRM 51-40-02 AND DWG 140N2002. MAJOR
- [SDR FDEA201410163229](https://openairdocs.org/sdr/FDEA201410163229.md): Frame · corroded · Oct 16, 2014 · N783FD · Boeing 757222 · Fuselage Main, Frame
  > AFT CARGO BAY BS 1640, STRINGER 26 - 28L FRAME CORRODED. REMOVED COROSION IAW SRM 51-10-02 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG. 101, DEATIAL II. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02 AND DWG 146N1032. MAJOR REPAIR.
- [SDR FDEA201410163227](https://openairdocs.org/sdr/FDEA201410163227.md): Floorbeam · corroded · Oct 16, 2014 · N783FD · Boeing 757222 · Fuselage Main, Structure
  > BS 365, LBL 7, WL 208, FLOORBEAM UPPER ANGLE CORRODED. FOUND OUT OF LIMITS PER SRM 53-00-51, FIG. 101, DETAIL III. REPAIRED THE FLOORBEAM ANGLE BETWEEN LBL 15 - RBL 69, IAW SRM 53-00-51, FIG. 201, REPAIR 8. MAJOR REPAIR.

Next page: https://openairdocs.org/aircraft/N783FD/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 = 'N783FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N783FD/reports

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