# Service difficulty reports: N883FD

A list on [N883FD](https://openairdocs.org/aircraft/N883FD.md).

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

- [SDR FDEA202607140922](https://openairdocs.org/sdr/FDEA202607140922.md): Skin · damaged · Jul 14, 2026 · N883FD · Boeing 777FHT · Nacelle/Pylon, Main Frame
  > WHEN PERFORM EA G-5730-T0384072 P2 STEP 2, REPORT THE CURRENT AIRCRAFT CONFIGURATION TO FEDEX SERVICE ENGINEERING TO REQUEST AIRPLANE JACKING REQUIREMENTS FROM BOEING TO PERFORM THE PERMANENT DOUBLER/TRIPLER REPAIR AS SHOWN IN FIGURE 1. NOTED: NO.1 E
- [SDR FDEA202602260284](https://openairdocs.org/sdr/FDEA202602260284.md): Safety Wire · wrong part · Feb 26, 2026 · N883FD · Boeing 777FHT · Emergency Equipment
  > REMOVED RH DOOR SLIDE MPN 62771-128 MSN M10748 REF FEA G-2560-F0386294 REV NO. A PS P1 AND AMM 25-66-01-4 AND WRI 25-60/513. INSTALLED COPPER SAFETY WIRE (MS20995CY16). REPACKED/ LACED RH SLIDE AND INSTALLED ON AIRCRAFT PER CMM 25-61-31, FEA G-2560-
- [SDR FDEA202602260283](https://openairdocs.org/sdr/FDEA202602260283.md): Safety Wire · wrong part · Feb 26, 2026 · N883FD · Boeing 777FHT · Emergency Equipment
  > REMOVED LH SLIDE MPN 62771-127 MSN M10268 REF FEA G-2560-F0386282 REV NO. A PS P1 AND AMM 25-66-01-4 AND WRI 25-60/5712 PLACED SLIDE IN LINESHACK 380 INSTALLED COPPER SAFETY WIRE (MS20995CY16). REPACKED/ LACED LH SLIDE AND INSTALLED ON AIRCRAFT PER
- [SDR FDEA202512250013](https://openairdocs.org/sdr/FDEA202512250013.md): Modulating Valve · inoperative · Dec 25, 2025 · N883FD · Boeing 777FHT · Cabin Cooling System
  > AT FL390 WITH OAT -58C, BEGAN TO RECEIVE INTERMITTENT PACK L EICAS MESSAGE WITH CORRESPONDING CABIN TEMPERATURE DROP. COCKPIT TEMPERATURE WAS SET TO 26C AS COCKPIT TEMPERATURE DROPPED TO 10C. DECENDED TO FL350 AND RAN CABIN TEMP COLD QRH CHECKLIST THAT
- [SDR FDEA202507111178](https://openairdocs.org/sdr/FDEA202507111178.md): Skin · cracked · Jul 11, 2025 · N883FD · Boeing 777FHT · Wing, Plate/Skin
  > UT AND HFEC OPEN HOLE INSPECTION FOUND TWO CRACKS IN LH WING #5 HOLE. THE LH WING UPPER SKIN #5 HOLE TWO CRACKS REPAIRED AS PER B777 SRM51-20-07-0G REV:47.6 AND EA G-5730-T0384072 P1, TITLE:WING-PLATES AND SKINS-LH WING UPPER SKIN CRACK REPAIR IN RIB BAY
- [SDR FDEA202310041697](https://openairdocs.org/sdr/FDEA202310041697.md): Slat · dented · Oct 4, 2023 · N883FD · Boeing 777FHT · Leading Edge Devices
  > NO.7 SLAT EXTERNAL UPR SURFACE FROM IB TO OB 74 INCH CROSS TE TO LE 2 INCH FOUND ONE DENT. EVALUATED NO.7 SLAT EXTERNAL UPR SURFACE FROM IB TO OB 74INCH CROSS TE TO LE 2INCH ONE DENT DAMAGE SIZE LXWXY=8.2"X7.0"X0.098"OUT OF ALLOWABLE LIMIT AS PER B777 SRM
- [SDR FDEA202310021685](https://openairdocs.org/sdr/FDEA202310021685.md): Flap · dented · Oct 2, 2023 · N883FD · Boeing 777FHT · Trailing Edge Flaps
  > LH WING OB FLAP LOWER SURFACE FROM OB TO IB 210 INCH CROSS TE TO LE 13 INCH FOUND ONE DENT. EVALUATED LH WING OB FLAP LOWER SURFACE FROM OB TO IB 210 INCH CROSS TE TO LE 13 INCH ONE DENT DAMAGE SIZE LXW=1.5"X1.5" OUT OF ALLOWABLE LIMIT AS PER B777 SRM 57-5
- [SDR FDEA202310021684](https://openairdocs.org/sdr/FDEA202310021684.md): Floor Panel · cracked · Oct 2, 2023 · N883FD · Boeing 777FHT · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N:152W8601-31 FOUND CRACKED,AT STA1710 RBL1. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8601-31 CRACKED AT STA1710 RBL1, DAMAGE SIZE L=2.5" OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1 REV 45.0. RE
- [SDR FDEA202310021683](https://openairdocs.org/sdr/FDEA202310021683.md): Floor Panel · cracked · Oct 2, 2023 · N883FD · Boeing 777FHT · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N:152W8601-19 FOUND CRACKED,AT STA1660 RBL1. EVALUATED AND MEASURE MAIN DECK CARGO FLOOR PANEL P/N:152W8601-19 CRACKED AT STA1660 RBL1, DAMAGE SIZE L=2.3" DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00- 50-1A ALLOWABLE DA
- [SDR FDEA202105281416](https://openairdocs.org/sdr/FDEA202105281416.md): Skin · damaged · May 28, 2021 · N883FD · Boeing 777FHT · Elevator Structure
  > RH ELEVATOR FWD EDGE FOUND FASTENER SINK AT ELEV STA 232.2857. REPAIRED DAMAGE ON RH ELEVATOR FWD EDGE AT ELEV STA 232.2857 AS PER B777 SRM 55-20- 01-2R REPAIR 1 AND SRM 51-70-05 REV.38. COMPLIED WITH EA G-5520-T0361976 P1.TITLE STABILIZERS-RH ELEVATORS-
- [SDR FDEA202105281415](https://openairdocs.org/sdr/FDEA202105281415.md): Floor Support · cracked · May 28, 2021 · N883FD · Boeing 777FHT · Fuselage Miscellaneous Structure
  > FOUND BULK CARGO COMPARTMENT STRINGER CRACK AT STA1958.00 LBL8.2 BULK CARGO COMPARTMENT AT STA1958 LBL 8.2 CRACKED STRINGER REPAIRED AS PER B777 SRM 53-70-53-2R REPAIR 2 REV 38. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100
- [SDR FDEA202105241376](https://openairdocs.org/sdr/FDEA202105241376.md): Floor Panel · cracked · May 24, 2021 · N883FD · Boeing 777FHT · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PNL 241QF FOUND CRACKED. REPAIRED DAMAGE ON MAIN DECK CARGO PNL 241QF AS PER B777 SRM 53-00-50-2R, REPAIR 1, REV.38. REPAIR CLASSIFIED AS MAJOR PER GMM 06-2-100.
- [SDR FDEA202105241370](https://openairdocs.org/sdr/FDEA202105241370.md): Floor Panel · damaged · May 24, 2021 · N883FD · Boeing 777FHT · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 242PF FOUND CRACKED. REPAIRED DAMAGE ON MAIN DECK CARGO FLOOR PNL 242PF AS PER B777 SRM 53-00-50-2R, REPAIR 1,REV.38. REPAIR CLASSIFIED AS MAJOR PER GMM 06-2-100.
- [SDR FDEA202105241369](https://openairdocs.org/sdr/FDEA202105241369.md): Floor Panel · damaged · May 24, 2021 · N883FD · Boeing 777FHT · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PNL 242LF FOUND CRACKED. REPAIRED DAMAGE ON MAIN DECK CARGO FLOOR PNL 242LF AS PER B777 SRM 53-00-50-2R, REPAIR 1,REV.38. REPAIR CLASSIFIED AS MAJOR PER GMM 06-2-100.
- [SDR FDEA202105241377](https://openairdocs.org/sdr/FDEA202105241377.md): Floor Panel · cracked · May 24, 2021 · N883FD · Boeing 777FHT · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PNL 242QF FOUND CRACKED. REPAIRED DAMAGE ON MAIN DECK CARGO FLOOR PNL 242QF AS PER B777 SRM 53-00-50-2R, REPAIR 1,REV.38. REPAIR CLASSIFIED AS MAJOR PER GMM 06-2-100.
- [SDR FDEA202105151227](https://openairdocs.org/sdr/FDEA202105151227.md): Floor Support · cracked · May 15, 2021 · N883FD · Boeing 777FHT · Fuselage Miscellaneous Structure
  > FOUND BULK CARGO FLOOR SUPPORT CRACKED AT STA1958.00 LBL 8.2. BULK CARGO AT STA1958 LBL8.2 CRACKED STRINGER REPAIRED AS PER B777 SRM 53-70-53- 2R REPAIR 2 REV38. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.
- [SDR FDEA202105121197](https://openairdocs.org/sdr/FDEA202105121197.md): Fitting · damaged · May 12, 2021 · N883FD · Boeing 777FHT · Engine Mount Section
  > RHW ENG STRUT AFT FAIRING I/B AFT INSTALLATION BOLT HOLE FOUND ELONGATED RHW ENG STRUT AFT FAIRING I/B AFT SUPPORT FITTING HOLE ELONGATED REPAIRED AS PER B777 SRM 57-20-90-2R REPAIR 4 REV:38. REPAIR CLASSIFIED MINOR AS PER GMM6-2-100.
- [SDR FDEA202105121198](https://openairdocs.org/sdr/FDEA202105121198.md): Fitting · worn · May 12, 2021 · N883FD · Boeing 777FHT · Engine Mount Section
  > RHW ENG STRUT AFT FAIRING O/B FWD INSTALLATION BOLT HOLE FOUND ELONGATED RHW ENG STRUT AFT FAIRING O/B FWD SUPPORT FITTING HOLE ELONGATED REPAIRED AS PER B777 SRM 57-20-90-2R REPAIR 4 REV:38. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100
- [SDR FDEA202105111173](https://openairdocs.org/sdr/FDEA202105111173.md): Skin · cracked · May 11, 2021 · N883FD · Boeing 777FHT · Fuselage Main, Plate/Skin
  > SURFACE HFEC INSPECTION FOUND 02EA CRACKS (FWD CRACK APPROX.0.700 INCH IN LENGTH AND AFT CRACK APPROX.0.650 INCH IN LENGTH) ON THE EXTERNAL SUR FACE OF THE FUSELAGE SKIN AROUND THE 2 HOLES COMMON TO THE LEFT SIDE UNDERWING LONGERON AND FUSELAGE SKIN AS
- [SDR FDEA202105111172](https://openairdocs.org/sdr/FDEA202105111172.md): Skin · cracked · May 11, 2021 · N883FD · Boeing 777FHT · Fuselage Main, Plate/Skin
  > SURFACE HFEC INSPECTION FOUND 01EA CRACK APPROX.0.650 INCH IN LENGTH ON THE EXTERNAL SURFACE OF THE FUSELAGE SKIN AROUND THE 01EA HOLE COMMON TO THE RIGHT SIDE UNDERWING LONGERON AND FUSELAGE SKIN AS MARK AS PER W/C EO G-5310- E0332629 K P6 STEP 9. C. CO
- [SDR FDEA202105071149](https://openairdocs.org/sdr/FDEA202105071149.md): Doubler · damaged · May 7, 2021 · N883FD · Boeing 777FHT · Fuselage Main, Plate/Skin
  > ELONGATE HOLE FOUND ON THE DOUBLER AT STA993 STGR34LH-35LH DURING PERFORMING EO EG-5310-E0332629 K P5 STEP 11.P. REPAIR CARRIED OUT TO THE ENLONGATED HOLE ON THE DOUBLER AT STA993 STGR34LH- 35LH, AS PER EA: G-5310-T0361432 PART1 STEP3,4, TITLE: FUSELAGE-M
- [SDR FDEA202105071148](https://openairdocs.org/sdr/FDEA202105071148.md): Longeron · damaged · May 7, 2021 · N883FD · Boeing 777FHT · Fuselage Main, Longeron/Stringer
  > DURING PERFORMING EO EG-5310-E0332629K P6 STEP 13.H, 11EA YYT-10 FASTENER HOLES WERE 1ST OVERSIZED AT STA993-1003 STGR35RH-36RH, 3EA YLK-16 FASTENER HOLES WERE OVERSIZED TO 0.562" AT STA 1024 STGR36RH-37RH. REPAIR CARRIED OUT TO 11EA YYT-10 FASTENER HOLES
- [SDR FDEA202105071147](https://openairdocs.org/sdr/FDEA202105071147.md): Skin · damaged · May 7, 2021 · N883FD · Boeing 777FHT · Fuselage Main, Plate/Skin
  > DURING PERFORMING EO EG-5310-EO332629K P6 STEP 11.P,FOUND 01EA ZLJ-8 (BACB30NY8K*) COUNTERSUNK FASTENER AT STA 998 STGR 35R NEAR THE EDGE OF MACHINED STEP OF DOUBLER (P/N:143W2314Y406),AND RESULT IN KNIFE EDGE WITH MACHINED STEP ON AFT EDGE OF COUNTERSUN
- [SDR FDEA202105071145](https://openairdocs.org/sdr/FDEA202105071145.md): Fitting · damaged · May 7, 2021 · N883FD · Boeing 777FHT · Fuselage Main, Structure
  > DURING PERFORMING EO EG-5310-EO332629K P5 STEP 11.P,FOUND 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA 998 STGR35L NEAR THE EDGE OF MACHINED STEP OF DOUBLER P/N 143W2314Y405,AND WILL RESULT IN KNIFE EDGE WITH MACHINED STEP ON AFT EDGE OF COUNTERSU
- [SDR FDEA202105071143](https://openairdocs.org/sdr/FDEA202105071143.md): Fitting · damaged · May 7, 2021 · N883FD · Boeing 777FHT · Fuselage Main, Structure
  > DURING PERFORMING EO EG-5310-EO332629K P6 STEP 13.H, 11 EA YYT-10 FASTENER HOLES WERE 1ST OVERSIDED AT STA 993-1003 STGR35RH-36RH, 3EA YLK-16 FASTENER HOLES WERE OVERSIZED TO 0.562" AT STA1024 STGR36RH-37RH. REPAIR CARRIED OUT TO 11EA YYT-10 FASTENER HOLES
- [SDR FDEA202105071150](https://openairdocs.org/sdr/FDEA202105071150.md): Skin · gouged · May 7, 2021 · N883FD · Boeing 777FHT · Fuselage Main, Plate/Skin
  > DURING PERFORMING EO G-5310-EO332629 K P6 STEP 9A FOUND SOME GOUGES ON THE EXTERNAL SURFACE OF THE FUSELAGE SKIN COMMON TO LONGERON FITTING AFTER REMOVAL OF THE LONGERON FITTING. REPAIR CARRIED OUT TO GOUGES ON THE EXTERNAL SURFACE OF THE FUSELAGE SKIN C
- [SDR FDEA202105071146](https://openairdocs.org/sdr/FDEA202105071146.md): Fitting · damaged · May 7, 2021 · N883FD · Boeing 777FHT · Fuselage Main, Structure
  > DURING PERFORMING EO EG-5310-EO332629K P6 STEP 11.M, FOUND 01 EA EXISTING HOLES OVERSIZED (DIAMETER:0.434") ON THE SKIN AT STA 993 - STA1035,STGR 35R - 37R. THE BOEING DRAWING 675W0002 SH 7 VIEW 1B6 CALL OUT THE DIAMETER 0.371". COMPLIED WITH EO: G-5310-E0
- [SDR FDEA202105071144](https://openairdocs.org/sdr/FDEA202105071144.md): Fitting · damaged · May 7, 2021 · N883FD · Boeing 777FHT · Fuselage Main, Structure
  > DURING PERFORMING EO EG-5310-EO332629K P5 STEP 11.M,FOUND 01EA EXISTING HOLES OVERSIZED (DIAMETER:0.434") ON THE SKIN AT STA 993-STA 1035 STGR 35L-37L. THE BOEING DRAWING 675W0002 SH 7 VIEW 1B6 CALL OUT THE DIAMETER 0.371". COMPLIED WITH EO: G-5310-E033262
- [SDR FDEA202012033018](https://openairdocs.org/sdr/FDEA202012033018.md): None · none · Dec 3, 2020 · N883FD · Boeing 777FHT · Standard Practices/Structures
  > R/H HORIZONTAIL STAB TIP T/E DAMAGED BY A/C STRIKE ALL WORK COMPLETED ON R/H HORIZONTAL STAB FAIRING. PART INSTALLED MADE SERVICABLE BY COMPLETION OF EA G-5510-T0358408. O/K FOR SERVICE.
- [SDR FDEA2020062311304](https://openairdocs.org/sdr/FDEA2020062311304.md): Bracket · cracked · Jun 21, 2020 · N883FD · Boeing 777FHT · Nacelle/Pylon Miscellaneous Structure
  > WHEN OPENING NR 2 ENGINE T/R FOUND BIFURICATION BRACKET ON PYLON CRACKED. REMOVED AND REPLACED NR 2 ENG T/R BIFURICATION BEACKET IN REF TO 777 SRM 51-40-02, JOB COMPLETE.
- [SDR FDEA201807111662](https://openairdocs.org/sdr/FDEA201807111662.md): Skin · damaged · Jul 11, 2018 · N883FD · Boeing 777FHT · Leading Edge Devices
  > LT WING SLAT NR 7 L/E FOUND WRINKLE AT FROM O/B TO I/B 23IN POS. COMPLIED WITH EA G-5750-T0340942 P1, REPAIRED THE LT WING NR 7 SLAT L/E WRINKLE. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA201710213019](https://openairdocs.org/sdr/FDEA201710213019.md): Lamp · failed · Oct 21, 2017 · N883FD · Boeing 777FHT · Emergency Lighting
  > RIGHT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-04-2.
- [SDR FDEA201411193807](https://openairdocs.org/sdr/FDEA201411193807.md): Light · inoperative · Nov 19, 2014 · N883FD · Boeing 777FHT · Emergency Lighting
  > ONE EMER LIGHT INOPERATIVE. RELAMPED EMER LIGHT AT 1R. EMER LIGHTS CHECKED GOOD IAW AMM SMP.
- [SDR FDEA201411153722](https://openairdocs.org/sdr/FDEA201411153722.md): Unknown · malfunctioned · Nov 15, 2014 · N883FD · Boeing 777FHT · Flight Management Computing Software System
  > UNCOMMANDED TURN, DURING CRUISE PHASE OF FLIGHT WITH LNAV & VNAV SELECTED, THE ACFT STARTED A RANDOM TURN TO THE LEFT. SWITCHED TO HEADING SELECT TO TURN BACK TOWARDS PROPER COURSE THEN RE-ENGAGED LNAV WHERE UPON THE ACFT NAVIGATED NORMALLY. THE ONLY PILOT
- [SDR FDEA201408092126](https://openairdocs.org/sdr/FDEA201408092126.md): Module · malfunctioned · Aug 9, 2014 · N883FD · Boeing 777FHT · Flight Environment Data
  > LOSS OF MULTIPLE SYS DURING CLIMB OUT. ACFT WAS LOADED DURING HEAVY RAIN, DURING LAST PART OF LOADING SECONDARY EXTERNAL POWER CYCLED OFF & ON RAPIDLY SEVERAL TIMES CAUSING TIMING OUT OF SEVERAL SYS. DURING CLIMB LOST VSPD GUIDANCE ON FLIGHT DIRECTOR FOLLOWI
- [SDR FDEA201311062694](https://openairdocs.org/sdr/FDEA201311062694.md): Circuit Card · failed · Nov 6, 2013 · N883FD · Boeing 777FHT · Fire Detection
  > "DET FIRE ENG RT" EICAS MESSAGE 230 INTO FLIGHT. INTERROGATED MATERIAL, FOUND MAINT MESSAGE 26-10012 NOT ACTIVE. TROUBLESHOT IAW FIM 26-11 TASK 805, R & R ENGINE FIRE DETECTION CARD IAW AMM 26-11-03-4. PERFORMED ENGINE FIRE DETECTION TEST IAW AMM 26-11-00-
- [SDR FDEA201306171317](https://openairdocs.org/sdr/FDEA201306171317.md): Scavenge Pump · failed · Jun 17, 2013 · N883FD · Boeing 777FHT · Turbine Engine Oil System
  > RT ENGINE APPEARED TO BE LOOSING OIL BEFORE START, LEFT 24 QTS, RIGHT 23 QTS. AFTER 3 HOURS OF FLIGHT RT ENG SLOWLY DECREASED TO 14 QTS WHILE LT ENG REMAINED AT 19 QTS. JUST PRIOR TO ENTERING ETOPS, RT ENG REDUCED TO 13 QTS LT AT 19 QTS. DIVERTED. OIL WENT
- [SDR FDEA201305291119](https://openairdocs.org/sdr/FDEA201305291119.md): Circuit Breaker · tripped · May 29, 2013 · N883FD · Boeing 777FHT · AC Power Distribution System
  > DURING ACFT POWER UP, FOUND P320 PANEL, RELAY K24050, CTRL (F1) CIRCUIT BREAKER TRIPPED. RELAY, CONNECTOR, AND WIRES REMOVED AND REPLACED AS PER SWPM 20-10-11 REVISION 53 AND WDM 24-51-41 REVISION 15. PERFORMED AS PER AMM 49-11-00-2 REVISION 67.1 AND BOTH
- [SDR FDEA201212184316](https://openairdocs.org/sdr/FDEA201212184316.md): Lamp · burned out · Dec 18, 2012 · N883FD · Boeing 777FHT · Emergency Lighting
  > EMERGENCY LIGHT LAMP BURNED OUT. REPLACED LAMP IAW AMM 33-51-03-2. EMERGENCY LIGHT TESTED SATISFACTORY.
- [SDR FDEA201108313594](https://openairdocs.org/sdr/FDEA201108313594.md): Ballast · failed · Aug 31, 2011 · N883FD · Boeing 777FHT · Passenger Compartment Lighting
  > LIGHT OVER LEFT ENTRY DOOR COMES ON IF YOU CYCLE EMERGENCY LIGHT SWITCH IT GOES OFF. AFTER A PERIOD OF TIME COMES BCACK ON. TROUBLESHOT TO A BAD ENTRY DOOR LIGHT BALLAST. R & R ENTRY DOOR LEFT BALLAST IAW MM 33-32-01-2 AND SYS OPS. CHECKED NORMAL, ACFT OK

## 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 = 'N883FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N883FD/reports

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