# Service difficulty reports: N853FD

A list on [N853FD](https://openairdocs.org/aircraft/N853FD.md).

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

- [SDR FDEA202508201514](https://openairdocs.org/sdr/FDEA202508201514.md): Skin · cracked · Aug 20, 2025 · N853FD · Boeing 777FS2 · Wing, Plate/Skin
  > UT&OPEN HOLE HFEC INSPECTION ON THE RIGHT WING UPPER WING SKIN COMMON TO FASTENERS 0-6 AND FOUND 02EA CRACK ON THE HOLE #5. RIGHT WING UPPER WING SKIN #5 HOLE CRACK REPAIRED AS PER B777 SRM51-50-02- 0G,SRM51-40-02-0G,SRM51-20-05-0G,SRM51-10-01-0G,SRM51-20-0
- [SDR FDEA202508171484](https://openairdocs.org/sdr/FDEA202508171484.md): Skin · dented · Aug 17, 2025 · N853FD · Boeing 777FS2 · Trailing Edge Flaps
  > LEFT OTBD FLAP LWR SURFACE FROM IB TO OB 40 INCHES CORSS TE TO LE 12 INCHES FOUND ONE DENT. REPAIRED LH OB FLAP LWR SURFACE DENT AT OTEF STA 73 AS PER B777 SRM 57-53-01-2R REPAIR 2 AND SRM 51-70-04-2R REPAIR 1 REV 47.6 AND EA: G-5750-T0384564 PI, TITLE: WI
- [SDR FDEA202508171483](https://openairdocs.org/sdr/FDEA202508171483.md): Skin · dented · Aug 17, 2025 · N853FD · Boeing 777FS2 · Trailing Edge Flaps
  > LEFT OTBD FLAP LWR SURFACE FROM OB TO IB 93 INCHES CORSS TE TO LE 4 INCHES FOUND ONE DENT. REPAIRED LH OB FLAP LWR SURFACE DENT AT OTEF STA 434 AS PER B777 SRM 57-53-01-2R REPAIR 2 AND SRM 51-70-04-2R REPAIR 1 REV 47.6 AND EA: G-5750-T0384564 PI, TITLE: WI
- [SDR FDEA202508171482](https://openairdocs.org/sdr/FDEA202508171482.md): Skin · dented · Aug 17, 2025 · N853FD · Boeing 777FS2 · Trailing Edge Flaps
  > FOUND RHW T/E O/B FLAP LOWER SURFACE 01 EA DENT AT THE CROSS OTEF 428 AND T/E 4 INCHES. REPAIRED RHW T/E O/B FLAP LOWER SURFACE 01 EA DENT AT OTEF STA 428 AS PER B777 SRM 57-53-01-2R REPAIR 2 AND SRM 51-70-04-2R REPAIR 1 REV 47.6 AND EA:G-5750-T0384565 P1
- [SDR FDEA202508171481](https://openairdocs.org/sdr/FDEA202508171481.md): Skin · dented · Aug 17, 2025 · N853FD · Boeing 777FS2 · Trailing Edge Flaps
  > FOUND RHW T/E O/B FLAP LOWER SURFACE 01EA DENT AT THE CROSS OTEF 127 AND T/E 01 INCHES. REPAIRED RHW T/E O/B FLAP LOWER SURFACE 01EA DENT AT OTEF STA 127 AS PER B777 SRM 57- 53-01-2R REPAIR 2 AND SRM 51-70-04-2R REPAIR 1 REV 47.6 AND EA: G-5750-T0384565 P1,
- [SDR FDEA202508171480](https://openairdocs.org/sdr/FDEA202508171480.md): Floor Panel · cracked · Aug 17, 2025 · N853FD · Boeing 777FS2 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N: 152W8302-33 FOUND CRACKED AT STA 1010 LBL 85 - LBL 113. MAIN DECK CARGO FLOOR PANEL P/N:152W8302-33 CRACKED AT STA 1010 LBL 85 -LBL 113. DAMAGE SIZE:(1) L=3.4"; (2) L=2.8"; (3) L=2.2" DAMAGE OUT OF ALLOWABLE LIMIT AS PER B7
- [SDR FDEA202508171479](https://openairdocs.org/sdr/FDEA202508171479.md): Floor Panel · cracked · Aug 17, 2025 · N853FD · Boeing 777FS2 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N: 152W8302-34 FOUND CRACKED AT STA 1010 RBL 85. MAIN DECK CARGO FLOOR PANEL P/N:152W8302-34 CRACKED AT STA 1010 RBL 85. DAMAGE SIZE: L=2.8", DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1 FIGURE
- [SDR FDEA202508161478](https://openairdocs.org/sdr/FDEA202508161478.md): Skin · cracked · Aug 16, 2025 · N853FD · Boeing 777F · Wing, Plate/Skin
  > UT & OPEN HOLE HFEC INSPECTION ON THE LEFT WING UPPER WING SKIN COMMON TO FASTENERS 0-6 AND FOUND 01EA CRACK ON THE HOLE #5. THE LEFT WING UPPER SKIN #5 FASTENER HOLE CRACKED AREA REPAIRED AS PER B777 SRM 51-40-05-0G, SRM 51-40-02-0G, SRM 51-40-04-0G REV47
- [SDR FDEA202508151453](https://openairdocs.org/sdr/FDEA202508151453.md): Skin · worn · Aug 15, 2025 · N853FD · Boeing 777F · Leading Edge Devices
  > #7 SLAT OUTER SKIN TRAILING EDGE FASTENER HOLE AT ISS 184 FOUND WORN. LH WING #7 SLAT OUTER SKIN TRAILING EDGE AT ISS 184 WORN FASTENER HOLE REPAIRED AS PER B777 SRM 57-43-01-2R REPAIR 6 FIG 203 REV 47.6 AND EA G-5750-T0384537 A P1, TITLE: WING - FLIGHT
- [SDR FDEA202505200769](https://openairdocs.org/sdr/FDEA202505200769.md): Power Supply · no test · May 20, 2025 · N853FD · Boeing 777FS2 · Emergency Lighting
  > EMERGENCY LIGHTS OF SUPERNUMERARY LEFT AREA SIDE DID NOT WORK WHEN EMER LIGHT ON MODE. AMM: 33-51-06-2 REMOVED AND REPLACED LEFT DOOR EMER PWR SUPPLY (M33093) (MANUFACTURE;GOODRICH,PARTS NAME;EMERGENCY POWER SUPPLY)PER ABOVE AMM.TEST NORMAL.A/C OK FO
- [SDR FDEA202203070436](https://openairdocs.org/sdr/FDEA202203070436.md): None · none · Mar 7, 2022 · N853FD · Boeing 777FS2 · Standard Practices/Structures
  > 1859Z AT FL 290 ENCOUNTERED SEVERE TURBULENCE. TWO OVER SPEEDS WERE NOTED DURING THE EVENT OVER SPEED WAS APPROXIMATELY 40 KNOTS. OVERALL AIRSPEED LOSS AND GAIN APPROXIMATELY 50 KTS. ALTITUDE LOSS AND GAIN WAS 1000. FINALLY GOT CONTROL OF THE AIRCRAFT
- [SDR FDEA2020062571140](https://openairdocs.org/sdr/FDEA2020062571140.md): Skin · cracked · Jun 7, 2020 · N853FD · Boeing 777FS2 · Fuselage Main, Plate/Skin
  > DURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE RIGHT HAND UNDERWING LONGERON AND FUSELAGE SKIN, FOUND 03 EACH CRACKS ON THE SKIN APPROXIMATELY 1.5Ï¿½ AT STATION 10
- [SDR FDEA2020062571139](https://openairdocs.org/sdr/FDEA2020062571139.md): Skin · cracked · Jun 7, 2020 · N853FD · Boeing 777FS2 · Fuselage Main, Plate/Skin
  > DURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE LEFT HAND UNDERWING LONGERON AND FUSELAGE SKIN, FOUND 03 EACH CRACKS ON THE SKIN APPROXIMATELY 0.5Ï¿½ AT STATION 1
- [SDR FDEA2020060871140](https://openairdocs.org/sdr/FDEA2020060871140.md): Skin · cracked · Jun 7, 2020 · N853FD · Boeing 777FS2 · Fuselage Main, Plate/Skin
  > DURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE RIGHT HAND UNDERWING LONGERON AND FUSELAGE SKIN, FOUND 03 EACH CRACKS ON THE SKIN APPROXIMATELY 1.5 AT STATION 1027 STRI
- [SDR FDEA2020060871139](https://openairdocs.org/sdr/FDEA2020060871139.md): Skin · cracked · Jun 7, 2020 · N853FD · Boeing 777FS2 · Fuselage Main, Plate/Skin
  > DURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE LEFT HAND UNDERWING LONGERON AND FUSELAGE SKIN. FOUND 03 EACH CRACKS ON THE SKIN APPROXIMATELY 0.5 AT STATION 1027 STRIN
- [SDR FDEA2020062641124](https://openairdocs.org/sdr/FDEA2020062641124.md): Spar · cracked · Jun 4, 2020 · N853FD · Boeing 777FS2 · Wing Spar
  > DURING ULTRASONIC INSPECTION ON THE VERTICAL FLANGE OF THE SPAR CHORD AND HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON REMOVED FASTENER HOLES AT RIGHT HAND SIDE UNDERWING LONGERON LOWER WING BODY STATION 1035. VERTICAL FLANGE OF THE SPAR CH
- [SDR FDEA2020060541124](https://openairdocs.org/sdr/FDEA2020060541124.md): Longeron · cracked · Jun 4, 2020 · N853FD · Boeing 777FS2 · Fuselage Main, Longeron/Stringer
  > HIGH FREQUENCY EDDY CURRENT, OPEN HOLE INSPECTION CARRIED OUT ON. REMOVED FASTENER HOLES AT RIGHT HAND SIDE UNDERWING LONGERON LOWER WING BASE STATION 1035. VERTICAL FLANGE OF THE SPAR CHORD AND FOUND 01 EA LOWEST OUTBOARD HOLE WITH CRACK INDICATION.
- [SDR FDEA202005291077](https://openairdocs.org/sdr/FDEA202005291077.md): Longeron · cracked · May 29, 2020 · N853FD · Boeing 777FS2 · Fuselage Main, Longeron/Stringer
  > ULTRASONIC INSPECTION OF THE RIGHT HAND UNDERWING LONGERON FOUND CRACK AT BASE STATION 1035. COMPLIANCE WITH E.O. # G-5310-E0332629 E P6. TITEL: FUSELAGE Ï¿½ MAINFRAME INSPECTION AND MODIFICATION OF THE UNDERWING LONGERON AT BODY STATION 1035. SERVICE B
- [SDR FDEA202005291076](https://openairdocs.org/sdr/FDEA202005291076.md): Longeron · cracked · May 29, 2020 · N853FD · Boeing 777FS2 · Fuselage Main, Longeron/Stringer
  > ULTRASONIC INSPECTION OF THE LEFT HAND UNDERWING LONGERON FOUND CRACKED AT BS 1035. COMPLIANCE WITH E.O. # G-5310-E0332629 E P5. TITEL: FUSELAGE Ï¿½ MAINFRAME Ï¿½ INSPECTION AND MODIFICATION OF THE UNDERWING LONGERON AT BODY STATION 1035, SERVICE BULLETI
- [SDR FDEA201807191787](https://openairdocs.org/sdr/FDEA201807191787.md): Light · inoperative · Jul 19, 2018 · N853FD · Boeing 777FS2 · Emergency Lighting
  > SUPERNUMERARY EMERGENCY LIGHT TEST PERFORMED. CEILING LIGHT CLOSEST TO GALLEY INOP. RELAMPED SUPERNUMERARY EMERGENCY AREA LIGHT AS PER AMM 33-51-03-2 AND TEST OK AS PER SAME AMM.
- [SDR FDEA201807101665](https://openairdocs.org/sdr/FDEA201807101665.md): Charger · inoperative · Jul 10, 2018 · N853FD · Boeing 777FS2 · Emergency Lighting
  > DURING CABIN PREFLIGHT, FOUND THAT EMERGENCY LIGHTS ON LEFT SIDE OF CABIN WOULD NOT ILLUMINATE DURING EMERGENCY LIGHT TEST. P/N INSTALLED/REMOVED MPN D717-02-0001. SERIAL NUMBER REMOVED 48407. REMOVAL INSTALLATION C/W AMM 33-51-06-2. OPS TEST SATISFACTORY. A/C
- [SDR FDEA201705031347](https://openairdocs.org/sdr/FDEA201705031347.md): Handle · out of position · May 3, 2017 · N853FD · Boeing 777FS2 · Emergency Equipment
  > UNABLE TO ARM L1 OUTER DOOR HANDLE, NOT IN STOW POSITION. POSITIONED HANDLE IAW AMM 52-11-00-2.
- [SDR FDEA201511213750](https://openairdocs.org/sdr/FDEA201511213750.md): Container · smoke · Nov 21, 2015 · N853FD · Boeing 777FS2 · Cargo Compartments
  > DURING CRUISE AT FL 310 RECEIVED FIRE CARGO AFT WARNING. RAN CHECKLIST, DISCHARGED FIRE BOTTLES. FIRE WARNING CONTINUED TO DISPLAY FOR OVER 30 MINUTES. FIRE WARNING EXT PRIOR TO TOUCHDOWN. AFTER BLOCK IN RECEIVED FIRE CARGO AFT WARNING AGAIN. SHUT DOWN AL
- [SDR FDEA201506031682](https://openairdocs.org/sdr/FDEA201506031682.md): Arming Lever · unknown · Jun 3, 2015 · N853FD · Boeing 777FS2 · Passenger/Crew Doors
  > LEFT MAIN CABIN ENTRY DOOR ARMING LEVER MOVED TO THE, GREEN BAND, DISARMED POSITION ON LANDING. PERFORMED MODE SELECT MECHANISM TEST ND CHECK IAW AMM 52-11-15-2. ALL GOOD, ACFT OK FOR SERVICE.
- [SDR FDEA201505191536](https://openairdocs.org/sdr/FDEA201505191536.md): Light · inoperative · May 19, 2015 · N853FD · Boeing 777FS2 · Emergency Lighting
  > EMERGENCY LIGHT OVER THE LT ENTRY DOOR IS OUT. R & R EMER LIGHT LAMP IAW MM 33-50-00-2. OPERATIONS CHECKED NORMAL. OK TO CONTINUE.
- [SDR FDEA201504201266](https://openairdocs.org/sdr/FDEA201504201266.md): Lens · missing · Apr 20, 2015 · N853FD · Boeing 777FS2 · Escape Slide
  > FOUND EPAS PRESS GAUGE VIEWPORT LENS ON LT ENTRY DOOR MISSING. REPLACED LENS. IAW S.M.P.
- [SDR FDEA201412174136](https://openairdocs.org/sdr/FDEA201412174136.md): Blade · damaged · Dec 17, 2014 · N853FD · Boeing 777FS2 · Turbine Engine Compressor Section
  > RIGHT ENG VIBRATION DURING CLIMB PASSING 1000` AGL. ENG SECONDARY VIBRATION MONITOR DISPLAYED 5.0 N1 ON RT ENG. VIBRATION FELT IN YOKE, RUDDER PEDALS & FLOOR. NO OTHER ABNORMAL INDICATIONS. DUMPED FUEL & RETURNED. FOUND NR 2 FAN BLADE TE TIP CAP & TE GUAR
- [SDR FDEA201304080745](https://openairdocs.org/sdr/FDEA201304080745.md): Spring · fouled · Apr 8, 2013 · N853FD · Boeing 777FS2 · Emergency Lighting
  > SPRING ON THE EMERGENCY LIGHTS APPEARS TO BE FOULED UP. ADJUSTED SPRING IAW SMP FUNCTIONED GOOD.
- [SDR FDEA201207062508](https://openairdocs.org/sdr/FDEA201207062508.md): Lamp · inoperative · Jul 6, 2012 · N853FD · Boeing 777FS2 · Emergency Lighting
  > LEFT SIDE EXTERIOR EMERENCY LIGHT INOPERATIVE. RELAMPED LT EMERGENCY LIGHT AND OPS CHECK NORMAL IAW AMM 33-51-04-2.
- [SDR FDEA201201030008](https://openairdocs.org/sdr/FDEA201201030008.md): Skin · damaged · Jan 3, 2012 · N853FD · Boeing 777FS2 · Passenger/Crew Doors
  > FOUND LEFT PASSENGER ENTRY DOOR FWD LOWER SKIN NICK DAMAGED, 25/32" X 14/32" X 19/32". REPAIRED IAW EA G-5210-157508 PT1 AND PT2.
- [SDR FDEA201108063125](https://openairdocs.org/sdr/FDEA201108063125.md): Spring · inoperative · Aug 6, 2011 · N853FD · Boeing 777FS2 · Emergency Lighting
  > EMERGENCY LIGHT SWITCH ARM/DISARM SPRING INOP. REINSTALLED SPRING. SWITCH GUARD OPERATES NORMALLY.

## 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 = 'N853FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N853FD/reports

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