# Service difficulty reports: N897FD

A list on [N897FD](https://openairdocs.org/aircraft/N897FD.md).

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

- [SDR FDEA202603200361](https://openairdocs.org/sdr/FDEA202603200361.md): None · none · Mar 20, 2026 · N897FD · Boeing 777F · Standard Practices/Structures
  > REF WRI 56-11 /8255, C/OUT RTO / HIGH ENERGY STOP INSP. RTO / HIGH ENERGY INSPECTION C/OUT IAW B777 AMM 05-51-14-2-0, FOUND SATIS. A/C OK TO SVC ALL BRAKE TEMPS WITHIN DISPATCHABLE LIMITS.A/C OK FOR SVC
- [SDR FDEA202603200360](https://openairdocs.org/sdr/FDEA202603200360.md): Warning Message · false activation · Mar 20, 2026 · N897FD · Boeing 777F · Flight Compartment Windows
  > RTO AT 102KTS DUE TO WINDOW FLIGHT DECK L EICAS MESSAGE DEBRIEFED CREW, ONLY THE MOVEMENT OF THE WINDOW HANDLE MOVED JUST A BIT, FOLLOWED BY INDICATION. MAT INTEROGATED., FOUND NO FAULTS LOGGED IN. CHECKED THE WINDOW OPERATION PER AMM 56-11-03-5. NI
- [SDR FDEA202602280289](https://openairdocs.org/sdr/FDEA202602280289.md): Safety Wire · wrong part · Feb 28, 2026 · N897FD · Boeing 777F · Emergency Equipment
  > LEFT DOOR SLIDE, NEEDS TO REPLACE WIRE WITH MS20995CY16 CAD-PLATTED COPER WIRE AS PER AMM 25-66-01-4 (REFERENCE EA 9-2560-T0386431). AMM: 25-66-01-4 LEFT DOOR EMRCY ESCAPE SLIDE REPLACED WIRE WITH MS20995CY16 CAD-PLATED COPPER WIRE AS PER AMM 25-66-01-4
- [SDR FDEA202602180234](https://openairdocs.org/sdr/FDEA202602180234.md): Slide · inoperative · Feb 18, 2026 · N897FD · Boeing 777F · Escape Slide
  > FOLLOWING WRI 25-60/8141, ON THE LEFT DOOR SLIDE, NEED TO REPLACE WIRE WITH MS20995CY16 CAD-PLATTED COPER WIRE AS PER AMM 25-66-01-4. LEFT DOOR EMRCY ESCAPE SLIDE REPLACED WIRE WITH MS20995CY16 CAD-PLATED COPPER WIRE AS PER AMM 25-66-01-4.
- [SDR FDEA202509161711](https://openairdocs.org/sdr/FDEA202509161711.md): Skin · cracked · Sep 16, 2025 · N897FD · Boeing 777F · Leading Edge Devices
  > MFEC INSPECTION FOUND 01 EA CRACK ON NO.5 SLAT EXTERNAL SKIN FROM O/B TO I/B 3.5 INCHES OF OSCS 732 ON UPPER ROW FASTENERS. 01 EA CRACK ON NO.5 SLAT EXTERNAL SKIN FROM O/B TO I/B 3.5 " OF OSCS 732 ON UPPER ROW FASTENERS REPAIRED AS PER B777 SRM 57-43-01
- [SDR FDEA202509161710](https://openairdocs.org/sdr/FDEA202509161710.md): Skin · cracked · Sep 16, 2025 · N897FD · Boeing 777F · Leading Edge Devices
  > MFEC INSPECTION FOUND 01 EA CRACK ON NO.5 SLAT EXTERNAL SKIN FROM O/B TO I/B 2.5 INCHES OF OSCS 732 ON UPPER ROW FASTENERS. 01 EA CRACK ON NO.5 SLAT EXTERNAL SKIN FROM O/B TO I/B 2.5 " OF OSCS 732 ON UPPER ROW FASTENERS REPAIRED AS PER B777 SRM 57-43-01-2R
- [SDR FDEA202509121695](https://openairdocs.org/sdr/FDEA202509121695.md): Skin · punctured · Sep 12, 2025 · N897FD · Boeing 777F · Elevator, Plate/Skin
  > LEFT ELEVATOR UPPER SURFACE HAS A SMALL HOLE AT PROXIMATELY 150" FROM THE INBOARD SIDE OF ELEVATOR, 37" FWD OF TRAILING EDGE AND 20" AFT OF LEADING EDGE. REPAIRED LH ELEVATOR UPPER SURFACE A SMALL HOLE AS PER B777 SRM 55-20-01-2R-1 AND SRM 51-70-04-2R-1 A
- [SDR FDEA202509121694](https://openairdocs.org/sdr/FDEA202509121694.md): Skin · cracked · Sep 12, 2025 · N897FD · Boeing 777F · Leading Edge Devices
  > NUMBER 5 SLAT EXTERNAL SKIN FROM OB TO IB 50 INCHES CROSS TE TO LE 19 INCHES FOUND CRACKED. NR 5 SLAT EXTERNAL SKIN FROM OB TO IB 50 INCHES CROSS TE TO LE 19 INCHES REPAIRED IAW SRM 57-43-01-2R-9 FIGURE 202 REV 47.6 AND EA G-5750-T0384896 P1,TITLE:WING - FLI
- [SDR FDEA202509121693](https://openairdocs.org/sdr/FDEA202509121693.md): Skin · cracked · Sep 12, 2025 · N897FD · Boeing 777F · Leading Edge Devices
  > NUMBER 5 SLAT EXTERNAL SKIN FROM OB TO IB 49 INCHES CROSS TE TO LE 12.5 INCHES FOUND CRACK. NO.5 SLAT EXTERNAL SKIN FROM OB TO IB 49" CROSS TE TO LE 12.5" REPAIRED AS PER B777 SRM 57-43-01-2R-9 FIGURE 202 REV 47.6 AND EA G-5750-T0384896 P1,TITLE:WING -
- [SDR FDEA202509121691](https://openairdocs.org/sdr/FDEA202509121691.md): Skin · cracked · Sep 12, 2025 · N897FD · Boeing 777F · Leading Edge Devices
  > NUMBER 5 SLAT EXTERNAL SKIN FROM OB TO IB 54 INCHES CROSS TE TO LE 19 INCHES FOUND CRACK. NO.5 SLAT EXTERNAL SKIN FROM OB TO IB 54" CROSS TE TO LE 19" REPAIRED AS PER B777 SRM 57- 43-01-2R-9 FIGURE 202 REV 47.6 AND EA G-5750-T0384896 P1,TITLE:WING - FLI
- [SDR FDEA202412201822](https://openairdocs.org/sdr/FDEA202412201822.md): Tire · worn · Dec 20, 2024 · N897FD · Boeing 777F · Tire
  > ON TAKE OFF RECEIVED #3 TIRE LOW PRESSURE ALERT. ACCOMPLISHED LOW TIRE CHECKLIST AND DID A 30 FLAP NO AUTO BRAKES LANDING FOUND #3 TIRE PUNCTURE IN TREAD WITH NO FINDINGS. NO VISIBLE DAMAGE EITHER ON TIRES. CARRIED OUT INSPECTION OF MAIN & AFT INBOARD RIG
- [SDR FDEA202404020431](https://openairdocs.org/sdr/FDEA202404020431.md): Skin · damaged · Apr 2, 2024 · N897FD · Boeing 777FS2 · Fuselage Main, Plate/Skin
  > TO REPAIR SKIN & STRINGERS AT LH F.STA 508-STA529, BETWEEN S-39L AND S-41L. SKIN & STRINGERS AT LH F.STA508-STA529, BETWEEN S-39L AND S-41L REPAIRED AS PER B777 SRM 51-40-02-0G, SRM 51-10-02-0G, SRM 53-10-03-2R REPAIR 1, SRM 51-40-05-0G, SRM 51-20-01-0G, S
- [SDR FDEA202402050138](https://openairdocs.org/sdr/FDEA202402050138.md): Gearbox · damaged · Feb 5, 2024 · N897FD · Boeing 777F · Turbine Engine Oil System
  > PERFORMED PRECAUTIONARY ENGINE SHUTDOWN WON RT ENGINE IN CRUISE FL280. IN TITAN INDICATION WAS SECONDARY ENG DISPLAY APPEARING ON MFD & OIL QUANTITY 3. OIL TEMP & PRESSURE INDICATED NORMAL. AFTER APPROX 5 MINS, OIL PRESSURE SLOWLY BEGAN DECREASING OVER 30-40
- [SDR FDEA202303300524](https://openairdocs.org/sdr/FDEA202303300524.md): Floor Panel · cracked · Mar 30, 2023 · N897FD · Boeing 777FS2 · Fuselage Floor Panel
  > REWORK:MAIN DECK CARGO FLOOR PANEL P/N:152W8750-2 FOUND CRACKED AT STA2020 BL0. EVALUATED MAIN DECK CARGO FLOOR.P/N:152W8750-2 AT STA 2020 BL0 AS.PER B777 SRM 53-00- 50-1A. ALLOWABLE DAMAGE 1, REV.43.1 FOUND UPPER TEAR L X W=2.1" X 0.5", OUT OF ALLOWABLE LI
- [SDR FDEA202303230496](https://openairdocs.org/sdr/FDEA202303230496.md): Flap · dented · Mar 23, 2023 · N897FD · Boeing 777FS2 · Wing, Control Surfaces
  > LH OB FLAP LWR SURFACE FROM OB TO IB 162INCH CROSS TE TO LE 6INCH FOUND ONE DENT LH OB FLAP LWR SURFACE FROM OB TO IB 162INCH CROSS TE TO LE 6INCH DENT WITH DELAMINATION L X W=3.4" X 2.3", OUT OF ALLOWABLE LIMIT PER B777 SRM 57-53-01-1A ALLOWABLE DAMAGE 2,
- [SDR FDEA202303230495](https://openairdocs.org/sdr/FDEA202303230495.md): Flap · dented · Mar 23, 2023 · N897FD · Boeing 777FS2 · Wing, Control Surfaces
  > LH OB FLAP LWR SURFACE FROM IB TO OB 177INCH CROSS TE TO LE 15.8INCH FOUND ONE DENT LH OB FLAP LWR SURFACE FROM IB TO OB 177INCH CROSS TE TO LE 15.8INCH DENT WITH DELAMINATION L X W=3.1" X 2.5", OUT OF ALLOWABLE LIMIT PER B777 SRM 57-53-01-1A ALLOWABLE DAM
- [SDR FDEA202202170313](https://openairdocs.org/sdr/FDEA202202170313.md): None · none · Feb 17, 2022 · N897FD · Boeing 777FS2 · Door Warning System
  > AC DID NOT PRESSURIZE, GOT ALTITUDE WARNING AT 10,000. MAIN CARGO DOOR INDICATED NOT CLOSED PROPERLY. DUMPED FUEL & RETURNED TO CDG. LANDED AT 568,000# AT ARRIVAL FOUND VENT MAIN CARGO DOOR PARTIALLY CLOSED AND LATCH LIGHT NOT ILLUMINATED. MAIN CARGO TEST

## 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 = 'N897FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N897FD/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.