# Service difficulty reports: N778FD

A list on [N778FD](https://openairdocs.org/aircraft/N778FD.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 · 82 reports

- [SDR FDEA202505220793](https://openairdocs.org/sdr/FDEA202505220793.md): Gust Lock · failed · May 22, 2025 · N778FD · Boeing 757222 · Passenger/Crew Doors
  > LEFT ENTRY DOOR GUST LOCK WILL NOT RELEASE TO ALLOW THE DOOR TO CLOSE. REPLACED SPLIT COLLAR ON L1 DOOR. OPS CHECK GOOD. OK TO CONTINUE SERVICE.
- [SDR FDEA202403280398](https://openairdocs.org/sdr/FDEA202403280398.md): Frame · cracked · Mar 28, 2024 · N778FD · Boeing 757222 · Fuselage Main, Frame
  > CRACK INDICATION NOTED ON FRAME WEB INBD OF S-26R STA 1560 AT 12 O'CLOCK ON FASTENER HOLE. CRACK MARKED IN RED. REPAIRED BY EA F-5310-T0378490 PT1 TITLE: FUSELAGE - MAINFRAME - CRACK FOUND ON FRAME STA 1560 AT S-27R. MAJOR REPAIR
- [SDR FDEA202403270382](https://openairdocs.org/sdr/FDEA202403270382.md): Floorboard · damaged · Mar 27, 2024 · N778FD · Boeing 757222 · Fuselage Floor Panel
  > ZONE 220 COURIER FLOORBOARD 222AF DAMAGED. FABRICATED ZONE 220 COURIER FLOORBOARD 222AF ON VT MAE TRAVELER T24/1738846 IAW DWG SRZ-25-005 REVISION "R" MAJOR REPAIR
- [SDR FDEA202403250369](https://openairdocs.org/sdr/FDEA202403250369.md): Floorboard · delaminated · Mar 25, 2024 · N778FD · Boeing 757222 · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 251MWF LOWER SURFACE DELAMINATED AND TORN. FABRICATED ZONE 250 FLOORBOARD PANEL 251MWF ON VT MAE TRAVELER T24/1741743 IAW DWG SRZ-25-005 REVISION "R". MAJOR REPAIR
- [SDR FDEA202403250368](https://openairdocs.org/sdr/FDEA202403250368.md): Floorboard · damaged · Mar 25, 2024 · N778FD · Boeing 757222 · Fuselage Floor Panel
  > MAIN CARGO COMPT ZONE 230 FLOORBOARD PANEL 231MFF DAMAGED. FABRICATED ZONE 230 FLOORBOARD 231MFF ON VT MAE TRAVELER T24/1740237 IAW DWG SRZ- 25-005 REVISION "R". MAJOR REPAIR
- [SDR FDEA202403250367](https://openairdocs.org/sdr/FDEA202403250367.md): Floorboard · damaged · Mar 25, 2024 · N778FD · Boeing 757222 · Fuselage Floor Panel
  > ZONE 220 COURIER FLOORBOARD 221MBF DAMAGED. FABRICATED ZONE 220 COURIER FLOORBOARD 221MBF ON VT MAE TRAVELER T24/1738845 IAW DWG SRZ-25-005 REVISION "R" MAJOR REPAIR
- [SDR FDEA202403250366](https://openairdocs.org/sdr/FDEA202403250366.md): Floorboard · damaged · Mar 25, 2024 · N778FD · Boeing 757222 · Fuselage Floor Panel
  > ZONE 220 COURIER FLOORBOARD 222BF DAMAGED. FABRICATED ZONE 220 COURIER FLOORBOARD 222BF ON VT MAE TRAVELER T24/1738847 IAW DWG SRZ-25-005 REVISION "R". MAJOR REPAIR
- [SDR FDEA202403160299](https://openairdocs.org/sdr/FDEA202403160299.md): Floor Panel · damaged · Mar 16, 2024 · N778FD · Boeing 757222 · Fuselage Floor Panel
  > ZONE 220 COURIER FLOORBOARD 221BF DAMAGED. FABRICATED ZONE 220 COURIER FLOORBOARD 221BF ON VT MAE TRAVELER T24/1738844 REVISION "R" MAJOR REPAIR.
- [SDR FDEA202403160298](https://openairdocs.org/sdr/FDEA202403160298.md): Floor Panel · damaged · Mar 16, 2024 · N778FD · Boeing 757222 · Fuselage Floor Panel
  > ZONE 220 COURIER FLOORBOARD 221AF DAMAGED. FABRICATED ZONE 220 FLOORBOARD 221AF ON VT MAE TRAVELER T24/1738843 IAW DWG SRZ-25-005 REVISION "R" MAJOR REPAIR.
- [SDR FDEA202403160297](https://openairdocs.org/sdr/FDEA202403160297.md): Floor Panel · damaged · Mar 16, 2024 · N778FD · Boeing 757222 · Fuselage Floor Panel
  > ZONE 220 CURIER FLOORBOARD 222MDF DAMAGED. FABRICATED ZONE 220 COURIER FLOORBOARD 222MDF ON VT MAE TRAVELER T24/1738850 IAW DWG SRZ-25-005 REVISION "R" MAJOR REPAIR.
- [SDR FDEA202403160296](https://openairdocs.org/sdr/FDEA202403160296.md): Floor Panel · damaged · Mar 16, 2024 · N778FD · Boeing 757222 · Fuselage Floor Panel
  > ZONE 220 COURIER FLOORBOARD 222MAF DAMAGED. FABRICATED ZONE 220 COURIER FLOORBOARD 222MAF ON VT MAE TRAVELER T24/1738849 REVISION "R" IAW DWG SRZ-25-005. MAJOR REPAIR
- [SDR FDEA202307121206](https://openairdocs.org/sdr/FDEA202307121206.md): Ball Screw · failed · Jul 12, 2023 · N778FD · Boeing 757200 · Trailing Edge Flap Actuator
  > TE FLAP DISAGREE WHEN GOING TO FLAPS 25. COMPLETED QRH 9.1.17 LANDED FLAPS 20 ***EMERGENCY DECLARED*** ENT BY:5190314 RPT BY:5190314 R/I 12JUL23 22:37 MEM U REASON CODE: PREMATURE REMOVAL/INSTALLATION OFF MPN: 7820924 CPN: 2717624 POS
- [SDR FDEA202305050813](https://openairdocs.org/sdr/FDEA202305050813.md): Transmission · unknown · May 5, 2023 · N778FD · Boeing 757200 · Trailing Edge Flap Control System
  > TE FLAP DISAGREE EICAS WHEN FLAPS 20 SELECTED AT APPROX 170 KIAS, FLAP INDICATION SHOWED BETWEEN 15 AND 20. COMPLETED QRH 9.1.17 AND LANDED USING FLAPS 20.EMERGENCY DECLARED. ***EMERGENCY DECLARED***. TROUBLESHOT IN REF TO FIM 27-51 FAULT TREE 808 WITH N
- [SDR FDEA202304250759](https://openairdocs.org/sdr/FDEA202304250759.md): Gust Lock · damaged · Apr 25, 2023 · N778FD · Boeing 757200 · Passenger/Crew Doors
  > MDIS 778 52-10 6283 23APR23 MEM FACT U L1 GUST LOCK BROKEN. FACT 25APR23 17:35 GSO U AMM: 52-11-08-8 REPLACED L1 DOOR HOLD OPEN LOCK COLLAR IAW B757 AMM. INSTALLED PART: ALLIANCE AEROSPACE ENGINEERING SPLIT LOCK COLLAR P/N 10-N6008-1 S/N
- [SDR FDEA202304200726](https://openairdocs.org/sdr/FDEA202304200726.md): Unknown · unknown · Apr 20, 2023 · N778FD · Boeing 757200 · Trailing Edge Flap Control System
  > EMERGENCY DECLARED FOR TE FLAP DISAGREE. FLAP EXTENSION NORMAL TO 15 DEGREES. AT APPROX 175 KNOTS WE SELECTED FLAPS 20. THE FLAP INDICATOR MOVED TO APPROX 17 DEGREES AND STOPPED. TE FLAP DISAG EICAS MESSAGE WAS DISPLAYED. RAN QRH PROCEDURE AND LANDED WI
- [SDR FDEA202203280722](https://openairdocs.org/sdr/FDEA202203280722.md): Flap · unknown · Mar 28, 2022 · N778FD · Boeing 757200 · Wing, Control Surfaces
  > PREVIOUS COMPSITE MAJOR REPAIR RW O/B FLAP, UPPER SURFACE, APPROX. 52" FROM THE I/B END AND 5.5" FROM T/E. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS ACCORDANCE WITH APPROVED DATA. REMOVED PREVIOUS REPAIR AND PERDORMED PERMANENT REPAIR IAW B757 S
- [SDR FDEA202203280720](https://openairdocs.org/sdr/FDEA202203280720.md): None · none · Mar 28, 2022 · N778FD · Boeing 757200 · Fuselage Main, Structure
  > MAIN CABIN SEAT TRACK SCALLOP IS GOUGED LBL0 AT APPROX STA 1013 ACCOMPLISHED FEDEX EA# F-5310-T0367542: FUSELAGE - MAINFRAME - SEAT TRACK STA 1013, BL 0, SPLICE REPAIR
- [SDR FDEA202203280719](https://openairdocs.org/sdr/FDEA202203280719.md): None · none · Mar 28, 2022 · N778FD · Boeing 757200 · Fuselage Structure (General)
  > FLOOR PANEL REQ REWORK IAW FEDEX EA F-5310-T0367574 REWORKED FLOOR PANEL IAW FEDWX EA F-5310-T0367574 FUSELAGE - MAIN FRAME- DECK PLATE, STA 1708, BL 0, CORROSION
- [SDR FDEA202203280718](https://openairdocs.org/sdr/FDEA202203280718.md): None · none · Mar 28, 2022 · N778FD · Boeing 757200 · Fuselage Miscellaneous Structure
  > AFT CABIN SHEAR WEB CORRODED AT FASTENER HOLES BS 1684 - BS 1720 BL 0 ACCOMPLISHED FEDEX EA # F-5310-T036757P1: FUSELAGE- MAINFRAME - DECK PLATE STA 1708 BL 0 CORROSION
- [SDR FDEA202203260698](https://openairdocs.org/sdr/FDEA202203260698.md): Skin Panel · unknown · Mar 26, 2022 · N778FD · Boeing 757200 · Horizontal Stabilizer Structure
  > DURING AGING A/C INSPECTION, PERFORMED TAP TEST AND FOUND EXISTING REPAIR TO BE DISBANDED ON LEFT HORIZONTAL STAB LOWER SURFACE AT APPROX. STAB STA 214 AND 4' FROM FRONT SPAR. REMOVED PREVIOUS REPAIR AND PERFORMED PERMANENT REPAIR ON L/H HORIZONTAL STAB LOW
- [SDR FDEA202203250694](https://openairdocs.org/sdr/FDEA202203250694.md): Flap · unknown · Mar 25, 2022 · N778FD · Boeing 757200 · Wing, Control Surfaces
  > PREVIOUS COMPOSITE MAJOR REPAIR RW O/B FLAP UPPER SURFACE APPROX 53" FROM I/B END AND 9.5" FROM T/E. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS IN ACCORDANCE WITH APPROVED DATA. REMOVED PREVIOUS REPAIR AND PERFOMED PERMANENT REPAIR IAW B757 SRM:
- [SDR FDEA202203250693](https://openairdocs.org/sdr/FDEA202203250693.md): Flap · unknown · Mar 25, 2022 · N778FD · Boeing 757200 · Wing, Control Surfaces
  > PREVIOUS COMPOSITE MAJOR REPAIR R/W O/B FLAP UPPER SURFACE APPROX 95" FROM I/B END AND 7.5" FROM T/E. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS IN ACCORDANCE WITH APPROVED DATA. REMOVED PREVIOUS REPAIR AND PERFORMED PERMANENT REPAIR IAW B757 SRM
- [SDR FDEA202203250690](https://openairdocs.org/sdr/FDEA202203250690.md): Rudder · unknown · Mar 25, 2022 · N778FD · Boeing 757200 · Rudder Structure
  > PREVIOUS COMPOSITE MAJOR REPAIR ON THE L/H SIDE OF RUDDER APPROX 20" FROM T/E AND 36" FROM BOTTOM. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS IN ACCORDANCE WITH APPROVED DATA. REMOVED PREVIOUS REPAIR AND ACCOMPLISHED PERMANENT REPAIR TO L.H LOWER
- [SDR FDEA202203250689](https://openairdocs.org/sdr/FDEA202203250689.md): Flap · unknown · Mar 25, 2022 · N778FD · Boeing 757200 · Wing, Control Surfaces
  > PREVIOUS COMPOSITE MAJOR REPAIR. L/W O/B FLAP UPPER SURFACE APPROX 36" FROM I/B END AND 10" FROM T/E. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIRS IS IN ACCORDANCE WITH APPROVED DATA. REMOVED PREVIOUS REPAIR AND APPLIED NEW REPAIR IAW B757 SRM 57-53-
- [SDR FDEA202203250688](https://openairdocs.org/sdr/FDEA202203250688.md): Flap · unknown · Mar 25, 2022 · N778FD · Boeing 757200 · Wing, Control Surfaces
  > PREVIOUS COMPOSITE MAJOR REPAIR. L/W O/B FLAP UPPER SURFACE APPROX 83" FROM I/B END AND 8" FROM T/E. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIRS IS IN ACCORDANCE WITH APPROVED DATA REMOVED PREVIOUS REPAIR AND APPLIED NEW REPAIR IAW B757 SRM 57-53-01
- [SDR FDEA202203250687](https://openairdocs.org/sdr/FDEA202203250687.md): Flap · unknown · Mar 25, 2022 · N778FD · Boeing 757200 · Wing, Control Surfaces
  > PREVIOUS COMPOSITE MAJOR REPAIR. L/W O/B FLAP UPPER SURFACE APPROX 98" FROM I/B END AND 6.5" FROM T/E. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIRS IS IN ACCORDANCE WITH APPROVED DATA. REMOVED PREVIOUS REPAIR AND APPLIED NEW REPAIR IAW B757 SRM 57-53
- [SDR FDEA202203250686](https://openairdocs.org/sdr/FDEA202203250686.md): Flap · unknown · Mar 25, 2022 · N778FD · Boeing 757200 · Wing, Control Surfaces
  > PREVIOUS COMPOSITE MAJOR REPAIR, L/W O/B FLAP UPPER SURFACE APPROX 42" FROM I/B END AND 5.5" FROM T/E; REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS IN ACCORDANCE WITH APPROVED DATA. REMOVED PREVIOUS REPAIR AND APPLIED NEW REPAIR IAW B757 SRM 57-53-
- [SDR FDEA202203250685](https://openairdocs.org/sdr/FDEA202203250685.md): Web · damaged · Mar 25, 2022 · N778FD · Boeing 757200 · Cargo/Baggage Doors
  > MAIN CARGO DOOR LOWER INNER WEB HAS DAMAGE FROM STA 580-590 REMOVED, FABRICATED AND INSTALLED NEW WEB IAW BOEING DWG 65-49309 REV D
- [SDR FDEA202203250684](https://openairdocs.org/sdr/FDEA202203250684.md): Web · damaged · Mar 25, 2022 · N778FD · Boeing 757200 · Cargo/Baggage Doors
  > MAIN CARGO DOOR INNER WEB HAS DAMAGE FRO STA 500-520 REMOVED FABRICATED AND INSTALLED NEW WEB IAW BOEING DWG 65-49309 REV D
- [SDR FDEA202203240681](https://openairdocs.org/sdr/FDEA202203240681.md): Support · cracked · Mar 24, 2022 · N778FD · Boeing 757200 · Fuselage Main, Structure
  > EMPENNAGE INTERIOR CROWN AREA APU INLET DUCT SUPPORT BRACKET CRACKED AT BS 1862 LOCATED & DRILLED NEW -1 SUPPORT BRACKET IAW BAC DWG 353N1043 REV A, ALODINED NEW -1 SUPPORT BRACKET IAW B757 SRM 51-20-01, PRIMED NEW -1 SUPPORT BRACKET IAW B757 SRM 51-20-01,
- [SDR FDEA202203240680](https://openairdocs.org/sdr/FDEA202203240680.md): Stiffener · misaligned · Mar 24, 2022 · N778FD · Boeing 757200 · Fuselage Main, Structure
  > MAIN CABIN STIFFENER P/N 146N5376-7 REQUIRES TO BE FABRICATED PER PROD DWGS. FABRICATED MAIN CABIN STIFFENER, P/N 146N5376-7 IAW BAC DWG 146N5376 REV-
- [SDR FDEA202203240679](https://openairdocs.org/sdr/FDEA202203240679.md): None · none · Mar 24, 2022 · N778FD · Boeing 757200 · Cargo/Baggage Doors
  > MAIN CARGO DOOR INNER ACCESS PANEL HAS SCRATCHES AT APPROX STA 592 REMOVED, FABRICATED AND INSTALLED NEW ACCESS PANEL IAW BOEING DWG 65-49309 REV D
- [SDR FDEA202203230662](https://openairdocs.org/sdr/FDEA202203230662.md): None · unknown · Mar 23, 2022 · N778FD · Boeing 757200 · Horizontal Stabilizer Structure
  > EXISTING COMPOSITE REPAIR ON L HORIZONTAL STAB. LWR SURFACE AT APPROX. STAB STA 214 AND 4" FROM FRONT SPAR EXISTING COMPOSITE REPAIR ON L HORIZONTAL STAB. LWR SURFACE AT APPROX. STAB STA 214 AND 4" FROM FRONT SPAR IS LOCATED ON A PRIMARY STRUCTURE PER B757
- [SDR FDEA202203230661](https://openairdocs.org/sdr/FDEA202203230661.md): Flap · unknown · Mar 23, 2022 · N778FD · Boeing 757200 · Wing, Control Surfaces
  > EXISTING COMPOSITE REPAIR ON R/WING OTBD FLAP, UPPER SURFACE, APPROX. 30" FROM INBD END AND 2.5" FROM T/E EXISTING COMPOSITE REPAIR ON R/WING OTBD FLAP, UPPER SURFACE, APPROX. 30" FROM INBD END AND 2.5" FROM T/E IS LOCATED ON A PRIMARY STRUCTURE PER B757-2
- [SDR FDEA202203230659](https://openairdocs.org/sdr/FDEA202203230659.md): Flap · unknown · Mar 23, 2022 · N778FD · Boeing 757200 · Rudder Structure
  > EXISTING COMPOSITE REPAIR ON R/WING OTBD FLAP, LWR SURFACE T/E, APPROX 12" FROM INBD END AND 5" FROM T/E. EXISTING COMPOSITE REPAIR, R/WING OTBD FLAP, LWR SURFACE T/E, APPROX 12" FROM INBD END AND 5" FROM T/E., IS LOCATED ON A PRIMARY STRUCTURE PER B757-20
- [SDR FDEA202203230656](https://openairdocs.org/sdr/FDEA202203230656.md): Doubler · chafed · Mar 23, 2022 · N778FD · Boeing 757200 · Wing, Control Surfaces
  > R/W O/B FLAP L/E HAS A WORN AREA ON REPAIR DOUBLER 11IN I/B FROM O/B EDGE REPAIRED PER FEDEX EA # F-5750-T0322968 A
- [SDR FDEA202203220645](https://openairdocs.org/sdr/FDEA202203220645.md): Floorboard · delaminated · Mar 22, 2022 · N778FD · Boeing 757200 · Fuselage Floor Panel
  > MAIN CABIN STA 640/680 RBL 35 FLOOR PANEL TOP SURFACE DAMAGED. FABRICATED NEW PANEL 11862181-92 MAIN CABIN FLOOR PANEL IAW FED B757 SRZ 25-005 AND SRM 53-00-50-1A FIG 101 TABLE 1.
- [SDR FDEA202203220644](https://openairdocs.org/sdr/FDEA202203220644.md): Floorboard · delaminated · Mar 22, 2022 · N778FD · Boeing 757200 · Fuselage Floor Panel
  > MAIN CABIN STA 680/720 RBL 35 FLOOR PANEL TOP SURFACE DAMAGED. FABRICATED NEW PANEL 11862182-5 FLOOR PANEL IAW FED EX B757 SRZ-25-005 AND B757 SRM 53-00-50-1A FIG 101 TABLE 1.
- [SDR FDEA202203220638](https://openairdocs.org/sdr/FDEA202203220638.md): None · none · Mar 22, 2022 · N778FD · Boeing 757200 · Fuselage Main, Plate/Skin
  > EXTERIOR FUSELAGE SKIN HAS AN OUTWARDLY PROTUDING DENT AT STA 1602 BETWEEN S16R AND S17R ACCOMPLISHED B757-2 SRM 53-00-51-2R REPAIR 29 - FIG 201 - SHEET 129 - CATEGORY B REPAIR
- [SDR FDEA202203190596](https://openairdocs.org/sdr/FDEA202203190596.md): Spoiler · dented · Mar 19, 2022 · N778FD · Boeing 757200 · Wing Structure
  > LEFT WING #4 SPOILER I/B SIDE UPPER SURFACE IS DENTED REPAIRED LEFT WING #4 SPOILER UPPER SKIN DENT IAW B757 SRM: 57-70-01-2R REP 1 AND SRM 51-70-05.
- [SDR FDEA202203170563](https://openairdocs.org/sdr/FDEA202203170563.md): Seal · cracked · Mar 17, 2022 · N778FD · Boeing 757200 · Powerplant System
  > #2 ENGINE O/B CORE COWL PYLON SKIRT SPRING SEAL IS CRACKED. REMOVE AND REPLACED CRACKED SPRING SEAL PER BAC DWG 311N3570 REV G
- [SDR FDEA202202090266](https://openairdocs.org/sdr/FDEA202202090266.md): Hose · ruptured · Feb 9, 2022 · N778FD · Boeing 757222 · Hydraulic System, Main
  > UPON LOWERING THE LANDING GEAR WE RECEIVED "L HYD PRESS" FOLLOWED BY "L HYD QTY" EICAS MESSAGES. HYD QTY WAS "0.00" ALONG WITH HYD PRESS "0". WE HAD ASSOCIATED "L YAW DAMPER" AND "RUDDER RATIO" MESSAGES. PERFORMED A GO AROUND, LEFT GEAR DOWN AND FLAPS 20.
- [SDR FDEA202003170581](https://openairdocs.org/sdr/FDEA202003170581.md): Beam · cracked · Mar 17, 2020 · N778FD · Boeing 757222 · Fuselage Main, Structure
  > FWD CARGO STA 580 STUB BEAM IS CRACKED. LBL45.5 CUT OUT DAMAGED FLANGE ON FLOOR STUB BEAM STA 580 IAW FEDEX DWG SR57-53-004 REV -. FABRICATED, LOCATED, DRILLED AND INSTALLED ANGLE AND FILLER IAW FEDEX DWG SR57-53- 004 REV -. REF FEDEX EA F-5310-T0352978 P1
- [SDR FDEA202002140337](https://openairdocs.org/sdr/FDEA202002140337.md): Filter · defective · Feb 14, 2020 · N778FD · Boeing 757222 · Air Distribution System
  > AFTER LANDING TOWARD END OF ROLLOUT, GOT FIRE EICAS MESSAGE AND FIRE MASTER WARNING INDICACTIONS. NO OTHER FIRE INDICATIONS. AS WE PULLED OFF RWY COCKPIT FILLED UP WITH SMOKE. FIRE INDICATION CLEARED. SHUT DOWN JET, RAN QRH FOR EMERG EVAC, AND EXITED LT SIDE V
- [SDR FDEA2018081762048](https://openairdocs.org/sdr/FDEA2018081762048.md): Warning Message · false activation · Aug 16, 2018 · N778FD · Boeing 757222 · Pneumatic Distribution System
  > REJECTED TAKEOFF, DUE TO A LT ENG BLEED OFF MESSAGE. DURING TAXI BACK, CREW PERFORMED SYSTEM TESTED IAW MM 36-11-00-5. COULD NOT DUPLICATE. OPS CHECKED OKAY. NO HISTORY IN PAST 30 DAYS.
- [SDR FDEA201804020829](https://openairdocs.org/sdr/FDEA201804020829.md): Frame · punctured · Apr 2, 2018 · N778FD · Boeing 757222 · Fuselage Main, Frame
  > BS 231 FRAME IS PUNCTURED. CUT OUT DAMAGED SECTION OF THE FRAME IAW SRM 53-00-07-2R, REP 7. REPAIRED IAW SRM 53-00-07-2R, REP 7, FIG 202.
- [SDR FDEA201704261271](https://openairdocs.org/sdr/FDEA201704261271.md): Slide · low pressure · Apr 26, 2017 · N778FD · Boeing 757222 · Escape Slide
  > L1 DOOR ESCAPE SLIDE PRESSURE BELOW GREEN BAND. REMOVED AND REPLACED THE L1 DOOR SLIDE IAW AMM 25-66-01-6, SLIDE AND ARMING SYSTEM OPS CHECKED NORMAL IAW AMM 25-66-01-4
- [SDR FDEA201704251257](https://openairdocs.org/sdr/FDEA201704251257.md): Reservoir · low pressure · Apr 25, 2017 · N778FD · Boeing 757222 · Escape Slide
  > L1 DOOR ESCAPE SLIDE PRESSURE BELOW GREEN BAND. REMOVED AND REPLACED THE SLIDE, SLIDE AND ARMING SYSTEM OPS CHECKED NORMAL IAW AMM 25-66-01-4.
- [SDR FDEA201603130912](https://openairdocs.org/sdr/FDEA201603130912.md): Repair · debonded · Mar 13, 2016 · N778FD · Boeing 757222 · Wing, Plate/Skin
  > EXISTING REPAIR WING, THERE IS A REPAIR AT LT SIDE OUTER WING, UPPER INTER SPAR SKIN AT WS 790. THIS REPAIR REQUIRES EVALUATION IAW EO F-5100-7-5001 A4 PT 1 ATTACHMENT B, NO HISTORY. EXISTING REPAIR WAS EVALUATED IAW ATTACHMENT B OF EO F-5100-7-5001 A5 PT 1
- [SDR FDEA201603090874](https://openairdocs.org/sdr/FDEA201603090874.md): Skin · delaminated · Mar 9, 2016 · N778FD · Boeing 757222 · Trailing Edge Flaps
  > RIGHT INBD TE MAIN FLAP, UPPER OTBD ACCESS PANEL, UPPER SURFACE FOUND WITH MULTIPLE DENT MARKS & MULTIPLE DELAMINATED AREA. DAMAGED AREAS REMOVED, CLEANED & DRIED USING 150 DEG F PROCESS IAW SRM 57-53-01-2R DETAIL 1 REV 116 & SRM 57-70-10-2R REV 116. REPAIR

Next page: https://openairdocs.org/aircraft/N778FD/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 = 'N778FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N778FD/reports

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