# Service difficulty reports: N786FD

A list on [N786FD](https://openairdocs.org/aircraft/N786FD.md).

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

- [SDR FDEA202610011465](https://openairdocs.org/sdr/FDEA202610011465.md): Skin · none · Oct 1, 2026 · N786FD · Boeing 757222 · Cargo/Baggage Doors
  > C2 DOOR AFT LOWER CORNER FOUND EXISTING REPAIR. ACCOMPLISHED WITH EA# F-5330-T0388754 TITLE: FUSELAGE-PLATE AND SKIN-ALTERNATIVE INSPECTION TO REPAIR AT NO 2 CARGO DOOR CUT OUT AFT LOWER CORNER, STA 1410-1450, S- 25R TO S-28R. *THIS EA DEVIATES FROM EO F-5
- [SDR FDEA202609191371](https://openairdocs.org/sdr/FDEA202609191371.md): Skin · dented · Sep 19, 2026 · N786FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > EVALUATE EXISTING REPAIR ON FUSELAGE SKIN AT SECTION 48 LH UPPER SIDE OF TAILCONE BETWEEN BS 1941 AND BS 1963.8 APPLIED PERMANENT REPAIR AT FUSELAGE SKIN SECTION 48 LT UPPER SIDE BTW BS 1941 AND 1963.8 IAW B757 SRM 53-80-01-2R, DETAIL, I, FIG 201, SHEET 1 AND
- [SDR FDEA202609191370](https://openairdocs.org/sdr/FDEA202609191370.md): Crease Beam · corroded · Sep 19, 2026 · N786FD · Boeing 757222 · Fuselage Main, Structure
  > MAIN CARGO DECK CREASE BEAM INNER CHORD AT BS 880 RBL 64 FOUND EXFOLIATED.
- [SDR FDEA202609181365](https://openairdocs.org/sdr/FDEA202609181365.md): Seat Track · corroded · Sep 18, 2026 · N786FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACKS BTWN BS 1180 - 1200, RBL 58 HAD CORROSION. REMOVED & REPLACED THE SEAT TRACK BTWN BS 1180 - 1420, RBL 58.22 IAW DWG 657N3332, REV -, AND SRM 51-40-02-0G.
- [SDR FDEA202609181364](https://openairdocs.org/sdr/FDEA202609181364.md): Seat Track · corroded · Sep 18, 2026 · N786FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACKS BTW BS 1180 - 1200, RBL 45.5 HAD CORROSION. REMOVED & REPLACED THE SEAT TRACK BTWN BS 1180 - 1320, RBL 45.2 IAW DWG 146N5133, REV -, AND SRM 51-40-02-0G.
- [SDR FDEA202609181363](https://openairdocs.org/sdr/FDEA202609181363.md): Seat Track · corroded · Sep 18, 2026 · N786FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACKS BTW BS 980 - 1180, RBL 58 HAD CORROSION. REMOVED & REPLACED THE SEAT TRACK BTWN BS 900 - 1200, RBL 58.22 IAW DWG 657N3332, REV -, P.L 657N3332, REV C, & SRM 51-40-02-0G.
- [SDR FDEA202609141336](https://openairdocs.org/sdr/FDEA202609141336.md): Elevator · no discrepancy · Sep 14, 2026 · N786FD · Boeing 757222 · Elevator, Plate/Skin
  > EVALUATE EXISTING COMPOSITE REPAIR AT LH ELEVATOR UPPER SURFACE T/E, ON INBOARD AREA THIS ITEM HAS BEEN ACCOMPLISHED ON E.A.#: F-5520-T0388684, P1, TITLE: STABILIZER- ELEVATORS-LH ELEVATOR- EXISTING REPAIR- RSC TRACKING.
- [SDR FDEA202509121697](https://openairdocs.org/sdr/FDEA202509121697.md): Lamp · failed · Sep 12, 2025 · N786FD · Boeing 757222 · Emergency Lighting
  > R1 DOOR SLIDE LIGHT INOPERATIVE. AMM: 33-51-06-2-1 RELAMPED R1 DOOR SLIDE LIGHT, OP'S CHECKS GOOD. USED P/N 767 LIGHT BULB. AMM: 33-51-06-2-1 RELAMPED R1 DOOR SLIDE LIGHT, OP'S CHECKS GOOD.
- [SDR FDEA202505300825](https://openairdocs.org/sdr/FDEA202505300825.md): Warning Message · false activation · May 30, 2025 · N786FD · Boeing 757222 · Trailing Edge Flap Control System
  > TRAILING EDGE FLAP DISAGREE DURING FLAP RETRACTION FROM 1 TO UP ON TAKEOFF. RAN CHECKLIST, FLAPS RETRACTED & LIGHTS WENT OUT. CONTINUED TO DAY & LANDED AT FLAPS 20 USING ALTERNATE EXTENSION. DECLARED AN EMERGENCY. C/W HIGH ENERGY STOP/HEAT DAMAGE CONDITION
- [SDR FDEA202303010357](https://openairdocs.org/sdr/FDEA202303010357.md): Skin · corroded · Mar 1, 2023 · N786FD · Boeing 757200 · Nacelle/Pylon Structure
  > RIGHT WING PYLON UPPR FITTING #2 HOLE HAS CORROSION IN SKIN AT 3 O'CLOCK POSITION. 1) PERFORMED REPAIR OF SKIN ON R/H WING UPPER PYLON FITTING HOLE #2 IAW SRM 57-20- 01-2A REPAIR 8 & EA # F-5730-T0372934 A P1 WINGS - PLATES AND SKINS - RH WING, UPPER SKIN A
- [SDR FDEA202303010356](https://openairdocs.org/sdr/FDEA202303010356.md): Beam · cracked · Mar 1, 2023 · N786FD · Boeing 757200 · Fuselage Main, Structure
  > FORWARD PIT STA 580 AT LBL 45.5 FLOOR BEAM UPPER CAP AFT FLANGE LWR SURFACE RADIUS IS CRACKED. REPAIRED STA 580 UPPER AFT FLANGE OF FLOOR BEAM SPLICE SEGMENT 657N4313-5 PER FEDEX DRAWING SR57-53-004. MAJOR REPAIR.
- [SDR FDEA202209012135](https://openairdocs.org/sdr/FDEA202209012135.md): O-Ring · leaking · Sep 1, 2022 · N786FD · Boeing 757222 · Engine Oil System (Airframe Furnished)
  > R ENG OIL QUANTITY WENT TO 0 BY TOP OF CLIMB. PRESS WAS 180 INITIALLY. APPROXIMATELY 10 MINUTES LATER OIL PRESSURE BEGAN TO DECREASE, EVENTUALLY BEGAN TO FLUCTUATE SO WE DECLARED AN EMERGENCY AND DIVERTED TO MCI. OIL PRESSURE FURTHER DECREASED TO 90 PSI
- [SDR FDEA202103200733](https://openairdocs.org/sdr/FDEA202103200733.md): Frame Splice · cracked · Mar 20, 2021 · N786FD · Boeing 757222 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF ROTO PROBE AT BS 1640 S-14L PER EO 5310-E0344602 PT1. THE BOTTOM OUTBD FASTENER HOLE HAD A CRACK INDICATION IN THE FRAME. WORK ACCOMPLISHED ON EA F-5310-T0359979 TITLE: FUSELAGE - MAINFRAME - STA 1640 FRAME SPLICE REPAIR BETWEEN ST
- [SDR FDEA2020051870966](https://openairdocs.org/sdr/FDEA2020051870966.md): Adc · faulty · May 17, 2020 · N786FD · Boeing 757222 · Air Data Computer
  > PDIS 786 34-14 4200 17MAY20 TYS FACT U LOGPAGES:3215525 REJECTED ON RUNWAY DUE TO NO AIRSPEED ON PILOT/LEFT SIDE. REJECTED AT 78 KTS FACT 17MAY20 12:59 TYS U REPLACED LH CADC AS PER 757 MM 34-12-01-4 AIR DATA COMPUTER - REMOVAL/INSTALLATI
- [SDR FDEA202001240214](https://openairdocs.org/sdr/FDEA202001240214.md): Charger · failed · Jan 24, 2020 · N786FD · Boeing 757222 · Emergency Lighting
  > R1 DOOR EXTERIOR EMERGENCY LIGHT INOP. R1 INDOOR EMERGENCY LIGHT OPS NORMALLY. EMERGENCY BATTERY VOLTAGE GOOD, RELAMPED, NO HELP. NO POWER AT SOCKET. REF SSM 33-51-01 PG101 SH2, VERIFIED GOOD WIRING FROM BULB CONTACT AT L30 BACK TO CONNECTOR D66 AT EMERG L
- [SDR FDEA201911263107](https://openairdocs.org/sdr/FDEA201911263107.md): Warning Message · false activation · Nov 26, 2019 · N786FD · Boeing 757222 · Pneumatic Distribution System
  > PDIS 786 36-11 3853 26NOV19 GSO OPEN U LOGPAGES:3166516 REJECTED T/O BECAUSE OF "LEFT ENG BLEED AIR" AT 80 KTS. CLEARED EICAS WITH QRH AND CHECK LIST. RAN LEFT AND RIGHT ENGINES TO 80 PERCENT N2 WITH BOTH ENGI
- [SDR FDEA201804211090](https://openairdocs.org/sdr/FDEA201804211090.md): Brake · damaged · Apr 21, 2018 · N786FD · Boeing 757222 · Landing Gear Brake System
  > DURING WALKAROUND, FOUND THE NR 3 BRAKE BROKEN. REMOVED AND REPLACED THE NR 3 MAIN GEAR BRAKE ASSY IAW AMM 32-41-10-4. LEAK AND OPS CHECKED GOOD.
- [SDR FDEA201504031147](https://openairdocs.org/sdr/FDEA201504031147.md): Inverter · failed · Apr 3, 2015 · N786FD · Boeing 757222 · DC Generating System
  > DURING INITIAL PREFLIGHT, STANDBY INVERTER INDICATION SHOWED ON EICAS & WOULD NOT CLEAR. RAN FIM REF 24-33 FAULT TREE 802 FOUND STANDBY INVERTER SMOKING. INSPECTED IAW FIM 24-51-21-00 NO OTHER DAMAGE TO ANY COMPONENTS BESIDES INVERTER. R & R STANDBY INVERTE
- [SDR FDEA201412044062](https://openairdocs.org/sdr/FDEA201412044062.md): Slide · unserviceable · Dec 4, 2014 · N786FD · Boeing 757222 · Escape Slide
  > R1 DOOR SLIDE PRESS BELOW LIMIT. RELEASED FOR SERVICE IAW MEL 52-11-01-B CATEGORY B. IDENTIFY L1 & R1 DOOR SLIDES INOPERATIVE OR MISSING. NO JUMP SEATERS ACM'S ARE TO OCCUPY COURIER AREA IN FLIGHT. R & R R1 DOOR SLIDE IAW 75 MM 25-66-01-4. OK TO CONTINUE
- [SDR FDEA201412024028](https://openairdocs.org/sdr/FDEA201412024028.md): Sensor · tripped · Dec 2, 2014 · N786FD · Boeing 757222 · Door Warning System
  > RIGHT WING SLIDE DISPLAYED ON EICAS DURING APPROACH. DISAPPEARED AFTER LANDING. PRESSURIZATION WAS NORMAL. SMP CHECK TARGET ON RT WING SLIDE DOOR S10374 NO DEFECTS NOTED. CLEANED SAME, CHECKED PSEU FOUND SENSOR S10374 TRIPPED, RESET SAME. OPERATIONAL CHE
- [SDR FDEA201406061323](https://openairdocs.org/sdr/FDEA201406061323.md): Skin · damaged · Jun 6, 2014 · N786FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > EXTERNAL LOWER SKIN BETWEEN BS 1306 - 1310, STRINGERS 29 - 30R HAD THREE NICKS WITH PREVIOUS BLEND. BLENDED IAW EA F-5330-T0308052.
- [SDR FDEA201406041307](https://openairdocs.org/sdr/FDEA201406041307.md): Frame · punctured · Jun 4, 2014 · N786FD · Boeing 757222 · Fuselage Main, Frame
  > MDC LT FRAME WEB AT STATION 395, BETWEEN STRINGER 11L TO 12L, HAS 2 AREAS WITH PUNCTURED HOLES. REPAIRED FRAME WEB AT STATION 395, BETWEEN STRINGER 11L TO 12L IAW EA F-5310-T0308591 PT 1. FUSELAGE MAINFRAME, FUSELAGE FRAME REPAIR STATION 395 BETWEEN STRINGER
- [SDR FDEA201405231149](https://openairdocs.org/sdr/FDEA201405231149.md): Door Frame · cracked · May 23, 2014 · N786FD · Boeing 757222 · Fuselage Main, Structure
  > R2 DOOR FWD FRAME, UPPER HINGE CUT OUT EDGE NICKED. CRACK WAS FOUND OUT OF LIMITS IAW SRM 52-10-02, DETAIL IX, FIG. 101. LOCATED AND DRILLED AND INSTALLED REPAIR IAW SRM 52-10-02, FIG. 201, REPAIR 1. COMPLIED WITH EA F-5210-T0308334, PT. 1. MAJOR REPAI
- [SDR FDEA201405130993](https://openairdocs.org/sdr/FDEA201405130993.md): Spar · corroded · May 13, 2014 · N786FD · Boeing 757222 · Wing Main, Frame Structure
  > RT REAR SPAR AT IRSS 183 CORROSION NOTED. REPAIRED IAW EA F-5710-T0307459 P1.
- [SDR FDEA201405130995](https://openairdocs.org/sdr/FDEA201405130995.md): Fitting · gouged · May 13, 2014 · N786FD · Boeing 757222 · Wing, Nacelle/Pylon Attach Fittings
  > IAW NR N00032 DURING OK TO INSTALL NR 1 PYLON FOUND MID SPAR FITTING INBD LUG BUSHING INNER BORE HAS DEEP SCORED MARKS, WING SIDE. REPAIRED IAW EA F-5740-T0307296 DATED APR 30,2014. TITLE, WINGS & ATTACH FITTINGS NR 1 ENG PYLON INBD WING MOUNTED SIDE LOAD
- [SDR FDEA201405130994](https://openairdocs.org/sdr/FDEA201405130994.md): Frame Splice · corroded · May 13, 2014 · N786FD · Boeing 757222 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT STATION 1540 STRINGER 24L FRAME SPLICE HAS CORROSION. REMOVED FRAME SPLICE STATION 1540 DUE TO ELONGATED HOLES, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DET I. R & R FRAME SPLICE IAW SRM 51-40-05 & DWG 146N1042. REMOVED CORRO
- [SDR FDEA201405030932](https://openairdocs.org/sdr/FDEA201405030932.md): Frame Splice · corroded · May 3, 2014 · N786FD · Boeing 757222 · Fuselage Main, Frame
  > HIDDEN DAMAGE FRAME SPLICE STA 1480 STRINGER 24L CORRODED. EVALUATED CORROSION IAW SRM 53-00-07 FIG 101 DETAIL 2, FOUND TO BE OUT OF LIMITS. ORIGINAL MATERIAL IS.071 INCHES, MATERIAL REMOVED IS.021 INCHES & MATERIAL REMAINING IS.050 INCHES. FABRICATED SP
- [SDR FDEA201405030931](https://openairdocs.org/sdr/FDEA201405030931.md): Frame Splice · corroded · May 3, 2014 · N786FD · Boeing 757222 · Fuselage Main, Frame
  > HIDDEN DAMAGE FRAME SPLICE STA 1420, STRINGER 24L CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DET 1. R & R FRAME SPLICE PN FX146N1012-3 IAW SRM 51-40-02 & DWG 146N1012 STA 1420, STRINGER 24L. MAJOR REPAIR.
- [SDR FDEA201404230797](https://openairdocs.org/sdr/FDEA201404230797.md): Sill · corroded · Apr 23, 2014 · N786FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR CUT OUT LOWER SILL CORRODED BS 1360 - 1460, STRINGER 27R.
- [SDR FDEA201404140729](https://openairdocs.org/sdr/FDEA201404140729.md): Crease Beam · corroded · Apr 14, 2014 · N786FD · Boeing 757222 · Fuselage Main, Structure
  > MAIN DECK CARGO LT CREASE BEAM OTBD ANGLE SPLICE HAS EDGE CORROSION AT BS 1462. SPLICE WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13 DETAIL III PG 103. REMOVED AND REPLACED SPLICE IAW SRM 51-40-02 AND DRAWING 146N5590. MAJOR REPAIR.
- [SDR FDEA201404120718](https://openairdocs.org/sdr/FDEA201404120718.md): Floorbeam · corroded · Apr 12, 2014 · N786FD · Boeing 757222 · Fuselage Main, Floor Beam
  > FLOORBEAM AT FS 1661 BL 0 HAS CORROSION ON TOP CHORD. R & R CORRODED FLOORBEAM IAW SRM 51-40-02 & DWG 146N5110.
- [SDR FDEA201404110717](https://openairdocs.org/sdr/FDEA201404110717.md): Shear Tie · cracked · Apr 11, 2014 · N786FD · Boeing 757222 · Fuselage Internal Mounting Structure
  > MDC RT FRAME SHEAR TIE INNER RADIUS, UPPER AREA AT STATION 1160 BETWEEN STRINGER 10R - 11R HAS A CRACK. REMOVED CRACKED SHEAR TIE IAW SRM 51-40-02. FABRICATED NEW SHEAR TIE PN FX144N1126-10 & INSTALLED NEW SHEAR TIE IAW SRM 51-40-02. SHEAR TIE FABRICATED O
- [SDR FDEA201404100704](https://openairdocs.org/sdr/FDEA201404100704.md): Web · corroded · Apr 10, 2014 · N786FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > MAIN DECK, BS 1380 - 1400 STRINGER 17R UPPER SURFACE WEB CORRODED. R & R WEB IAW SRM 51-40-02 & DWG 146N5590.
- [SDR FDEA201404100705](https://openairdocs.org/sdr/FDEA201404100705.md): Rib · cracked · Apr 10, 2014 · N786FD · Boeing 757222 · Trailing Edge Flaps
  > RIGHT WING INBD FLAP INBD EDGE RIB IS CRACKED. FOUND TO BE OUT OF LIMITS IAW SRM 57-53-01. REPAIRED IAW SRM 51-70-04 PAR 4G. MAJOR REPAIR.
- [SDR FDEA201404020640](https://openairdocs.org/sdr/FDEA201404020640.md): Frame · misrepaired · Apr 2, 2014 · N786FD · Boeing 757222 · Fuselage Main, Frame
  > AFT CARGO, FRAME REPAIR AT BS 1440 S24L-27RFRAME MISINSTALLED. R & R FRAME IAW SRM 51-40-02 & DWG 146N1013.
- [SDR FDEA201403290599](https://openairdocs.org/sdr/FDEA201403290599.md): Crease Beam · corroded · Mar 29, 2014 · N786FD · Boeing 757222 · Fuselage Main, Structure
  > MAIN CARGO DECK BETWEEN BS 940 - 960, RT CREASE BEAM CORRODED. R & R IAW SRM 53-40-13, SRM 51-40-02, & DWG 144N5150.
- [SDR FDEA201403220545](https://openairdocs.org/sdr/FDEA201403220545.md): Floor Support · damaged · Mar 22, 2014 · N786FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > BS 377.7 - 395 RBL 24.75 FLOOR SUPPORT DOUBLE DRILLED. R & R FLOOR SUPPORT IAW DWG 141N5130 & SRM 51-40-02.
- [SDR FDEA201403220544](https://openairdocs.org/sdr/FDEA201403220544.md): Floorbeam · corroded · Mar 22, 2014 · N786FD · Boeing 757222 · Fuselage Main, Floor Beam
  > FWD CABIN FLOORBEAM AT STATION 365 BL 0 - RBL 62 UPPER TEE HAS CORROSION. REPAIRED FLOORBEAM RBL 70 TO LBL 16 IAW SRM 53-00-51 REPAIR 8.
- [SDR FDEA201403180520](https://openairdocs.org/sdr/FDEA201403180520.md): Floorbeam · corroded · Mar 18, 2014 · N786FD · Boeing 757222 · Fuselage Main, Floor Beam
  > MAIN DECK CARGO FLOORBEAM AT BS 377 HAS AREAS WITH NICKS, SCRATCHES & CORROSION. REPAIRED FLOORBEAM AT STATION 377 LBL 35 - 70 IAW SRM 53-00-51, FIG 201, DET II, SHEET NR 4, REPAIR NR 8. BLENDED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, D
- [SDR FDEA201403110489](https://openairdocs.org/sdr/FDEA201403110489.md): Floorbeam · corroded · Mar 11, 2014 · N786FD · Boeing 757222 · Fuselage Main, Floor Beam
  > FLOORBEAM AT FS 1640 RBL-LBL 65, HAS AREAS OF CORROSION ON TOP TEE. REMOVED CORROSION ON FLOORBEAM. FOUND OUT OF LIMITS, REMOVED FLOORBEAM, FABRICATED NEW FLOORBEAM. INSTALLED FLOORBEAM IAW DWG 146N5136 & SRM 51-40-02. MAJOR REPAIR.
- [SDR FDEA201403040443](https://openairdocs.org/sdr/FDEA201403040443.md): Floorbeam · corroded · Mar 4, 2014 · N786FD · Boeing 757222 · Fuselage Main, Floor Beam
  > MAIN DECK CARGO FLOORBEAM BS 333.45, BETWEEN LBL 45-58, UPPER TEE CORRODED. REMOVED CORROSION IAW SRM51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DET6. R & R FLOORBEAM IAW SRM 51-40-02.

## 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 = 'N786FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N786FD/reports

---
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.