# Service difficulty reports: N882FD

A list on [N882FD](https://openairdocs.org/aircraft/N882FD.md).

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

- [SDR FDEA202610051477](https://openairdocs.org/sdr/FDEA202610051477.md): Hose · disconnected · Oct 5, 2026 · N882FD · Boeing 777F28 · Landing Gear Brake System
  > ON POSTFLIGHT WALKAROUND FOUND NR 10 BRAKE HOSE DISCONNECTED AND HANGING. AMM: 32-45-07-4 RECONNECTED NR 10 BRAKE HOSE. REF AMM 32-45-07-4. OP'S CHECK GOOD, LEAK CHECK GOOD. A/C OK FOR SERVICE.
- [SDR FDEA202602150202](https://openairdocs.org/sdr/FDEA202602150202.md): Slide · not reported · Feb 15, 2026 · N882FD · Boeing 777F28 · Escape Slide
  > LH SLIDE ELECTRONIC CLOSURE FROM TRANSACTION MCFCTMOD, CLOSED DUE TO REMOVAL OF AFFECTED PART.
- [SDR FDEA202510222070](https://openairdocs.org/sdr/FDEA202510222070.md): Skin · dented · Oct 22, 2025 · N882FD · Boeing 777F28 · Trailing Edge Flaps
  > REWORK: RH WING IB AFT FLAP LWR SURFACE FOUND DENT AT 58 INCHES TO OB EDGE AND 3 INCHES TO FWD EDGE. REPAIRED RH WING IB AFT FLAP LWR SURFACE DENT AT ITEF BS 279 IAW SRM 57-53-01- 2R-1, & SRM 51-70-04-2R-1, REV 51.0, EA:G-5750-T0385411 P1. MAJOR REPAIR
- [SDR FDEA202510162033](https://openairdocs.org/sdr/FDEA202510162033.md): Skin · dented · Oct 16, 2025 · N882FD · Boeing 777F28 · Trailing Edge Flaps
  > RH WING OB FLAP LWR SURFACE FOUND DENT AT 99.5 INCHES TO IB EDGE AND 11.5 INCHES TO AFT EDGE. REPAIRED RT WING OTBD FLAP LWR SURFACE DENT AT OTEF STA 99.5 IAW SRM 57-53-01-2R-2, & SRM 51-70-04-2R-1, REV 51.0 AND EA:G-5750-T0385311 P1. MAJOR REPAIR PER GMM 6
- [SDR FDEA202510152010](https://openairdocs.org/sdr/FDEA202510152010.md): Skin · cracked · Oct 15, 2025 · N882FD · Boeing 777F28 · Fuselage Main, Plate/Skin
  > DURING PERFORMANCE OF WORK CARD: E G-5710-E0376285E, P12, STEP 3.B.(1), STEP 5.A.(2), & FOUND TWO CRACKS AT HOLE NR 5 OF RT UPPER WING SKIN COMMON TO FASTENERS 0-5. RT WING UPPER WING SKIN REPAIRED IAW SRM 51-40-05-0G, SRM 51-40-02-0G, SRM 51-40-04-0G, REV 51,
- [SDR FDEA202510152009](https://openairdocs.org/sdr/FDEA202510152009.md): Skin · cracked · Oct 15, 2025 · N882FD · Boeing 777F28 · Fuselage Main, Plate/Skin
  > DURING PERFORM WORK CARD:EG-5710-E0376285E P11 STEP 3.B.(1)&STEP 5.A.(2) AND FOUND TWO CRACKS AT HOLE #5 OF LH UPPER WING SKIN COMMON TO FASTENERS 0-5. LH WING UPPER SKIN TRAILING EDGE #5 HOLE CRACK REPAIRED AS PER B777 SRM 51-50-02-0G, SRM 51-40-02-0G, SR
- [SDR FDEA202501150071](https://openairdocs.org/sdr/FDEA202501150071.md): Controller · failed · Jan 15, 2025 · N882FD · Boeing 777F28 · Engine Anti-Icing System
  > ANTI ICE ENG L EICAS DISPLAYED IN FLIGHT. EMERGENCY DECLARED, T/S ACTIVE MX MSG 30-10291, FOUND SOLENOID ON LH ENG ANTI ICE CONTROLLER BAD, REMOVED AND REPLACED ANTI-ICE VALVE CONTROLLER IN REF. ABOVE, ALL CHECKS GOOD, NO ACTIVE MSG OR EICAS, ALSO REF. T
- [SDR FDEA202405190689](https://openairdocs.org/sdr/FDEA202405190689.md): Tire · leaking · May 19, 2024 · N882FD · Boeing 777F28 · Tire
  > ON CLIMB OUT GOT TIRE PRESS ALERT. RAN ECL AND TIRE PRESSURE SLOWLY DECREASED TO BELOW 50 PSI AND BEFORE DESCENT TO 7 PSI. LANDED UNEVENTFULLY 36C MEM. AIRPORT MOBILE INSPECTED TIRE AFTER RUNWAY TURNOFF. NO DAMAGE NOTED. TAXIED TO GATE. AMM: 32_45_01_4
- [SDR FDEA202312231955](https://openairdocs.org/sdr/FDEA202312231955.md): Switch · failed · Dec 23, 2023 · N882FD · Boeing 777F28 · Emergency Lighting
  > DURING POSTFLIGHT FOUND EMERGENCY LIGHT SWITCH IN THE FLIGHT DECK INTERMITTENT. AMM: 30-41-02-4 FIM: 33-51-00-2 PER ABOVE 777 FIM, REMOVED AND REPLACED WINDOW HEAT/EMERGENCY LIGHTS MODULE PER ABOVE 777 AMM. OPS CHECK GOOD. A/C OK FOR SERVICE.
- [SDR FDEA202312231954](https://openairdocs.org/sdr/FDEA202312231954.md): Module · failed · Dec 23, 2023 · N882FD · Boeing 777F28 · Emergency Lighting
  > DURING POSTFLIGHT FOUND EMERGENCY LIGHT SWITCH IN THE FLIGHT DECK INTERMITTENT. REMOVED AND REPLACED WINDOW HEAT/EMERGENCY LIGHTS MODULE PER ABOVE 777 AMM. OPS CHECK GOOD. A/C OK FOR SERVICE.
- [SDR FDEA202304210731](https://openairdocs.org/sdr/FDEA202304210731.md): Floor Panel · cracked · Apr 21, 2023 · N882FD · Boeing 777F28 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N:152W8601-31 FOUND CRACKED AT STA1780 RBL1. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8601-31 CRACK AT STA1780 RBL1. CRACK SIZE L=3.1" OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-53-1A ALLOWABLE DAMAGE 1 REV 43.1,REPAIR
- [SDR FDEA202304210730](https://openairdocs.org/sdr/FDEA202304210730.md): Floor Panel · cracked · Apr 21, 2023 · N882FD · Boeing 777F28 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N:152W8407-34 FOUND CRACKED AT STA1245 RBL55. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8407-34 CRACKED AT STA1245 RBL55.CRACK SIZE L=3.3" OUT OF ALLOWABLE LIMIT AS PER B777SRM 53-00-53-1A ALLOWABLE DAMAGE 1,REV43.1. REPA
- [SDR FDEA202304210729](https://openairdocs.org/sdr/FDEA202304210729.md): Floor Panel · cracked · Apr 21, 2023 · N882FD · Boeing 777F28 · Fuselage Structure (General)
  > MAIN DECK CARGO FLOOR PANEL P/N:152W8601-9 FOUND CRACKED AT STA1555 RBL1. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8601-9 CRACKED AT STA1555 RBL1.CRACK SIZE L=2.3" OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-53-1A ALLOWABLE DAMAGE 1 REV 43.1,REPAIR
- [SDR FDEA202201270753](https://openairdocs.org/sdr/FDEA202201270753.md): Lamp · failed · Jan 27, 2022 · N882FD · Boeing 777F28 · Emergency Lighting
  > PDIS 882 33-50 2851 27JAN22 DXB STARBOARD CEILING EMERGENCY LIGHT IN SUPERNUMERARY INOP. RELAMPED STARBOARD SIDE AREA LIGHT & OPS CHK SATISFACTORY IAW AMM REF 33-51-03-2.A/C OK FOR SERVICE
- [SDR FDEA202008071783](https://openairdocs.org/sdr/FDEA202008071783.md): Floor Support · cracked · Aug 7, 2020 · N882FD · Boeing 777F28 · Fuselage Miscellaneous Structure
  > BULK CARGO COMPARTMENT BS 1937, RBL 49.8 ON REMOVAL OF FLOOR SUPPORT FOUND EDGE CRACKED. STRINGER REPAIRED AS PER B777 SRM 53-70-53-2R FIGURE 202 REPAIR 2 FROM EXISTING SPLICE STATION 1927 TO STATION 1980.5 RIGHT BUTT LINE 49.8. REPAIR CLASSIFIED AS MAJO
- [SDR FDEA2020081821747](https://openairdocs.org/sdr/FDEA2020081821747.md): Skin · cracked · Aug 2, 2020 · N882FD · Boeing 777F28 · Fuselage Main, Plate/Skin
  > 02 EACH CRACK FOUND APPROXIMATE 0.6" IN LENGTH FOR BOTH CRACK DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND SIDE FUSELAGE SKIN BETWEEN STATION 1030 AND STATION 1035, STRINGER 37R AS MARKED. COMPLIED WITH E.O.#: G-5310-E0332629G P6. REPAIR
- [SDR FDEA2020081402747](https://openairdocs.org/sdr/FDEA2020081402747.md): Skin · cracked · Aug 2, 2020 · N882FD · Boeing 777F28 · Fuselage Main, Plate/Skin
  > 02 EACH CRACK FOUND APPROXIMATE 0.6" IN LENGTH FOR BOTH CRACK DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND SIDE FUSELAGE SKIN BETWEEN STATION 1030 AND STATION 1035, STRINGER 37R AS MARKED. COMPLIED WITH E.O.#: G-5310-E0332629G P6.TITLE: FU
- [SDR FDEA2020081421746](https://openairdocs.org/sdr/FDEA2020081421746.md): Skin · cracked · Aug 2, 2020 · N882FD · Boeing 777F28 · Fuselage Main, Plate/Skin
  > CRACK FOUND APPROXIMATE 0.7" IN LENGTH DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND SIDE FUSELAGE SKIN AT APPROXIMATELY STATION 1030, STRINGER STRINGER 37L AS MARKED. COMPLIED WITH E.O.#: G-5310-E0332629G P5. TITLE: FUSELAGE - MAINFRAM - INSP
- [SDR FDEA2020080321747](https://openairdocs.org/sdr/FDEA2020080321747.md): Skin · cracked · Aug 2, 2020 · N882FD · Boeing 777F28 · Fuselage Main, Plate/Skin
  > TWO CRACKS FOUND APPROXIMATE 0.6" IN LENGTH FOR BOTH CRACKS FOUND DURING HIGH FREQUENCY EDDY CURRENT INSPECTION FUSELAGE SKIN BETWEEN BS 1030 AND 1035, STRINGER 37R.
- [SDR FDEA2020080321746](https://openairdocs.org/sdr/FDEA2020080321746.md): Skin · cracked · Aug 2, 2020 · N882FD · Boeing 777F28 · Fuselage Main, Plate/Skin
  > CRACK FOUND APPROXIMATE 0.7" IN LENGTH, DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON THE FUSELAGE SKIN AT BS 1030, STRINGER 37L.
- [SDR FDEA2020080321745](https://openairdocs.org/sdr/FDEA2020080321745.md): Skin · damaged · Aug 2, 2020 · N882FD · Boeing 777F28 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING EO G-5310-E0332629 G P6, FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT BS 998, STRINGER 35R NEAR MILLED EDGE.
- [SDR FDEA2020080321744](https://openairdocs.org/sdr/FDEA2020080321744.md): Skin · damaged · Aug 2, 2020 · N882FD · Boeing 777F28 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING EO G-5310-E0332629 G P5 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT BS 998, STRINGER 35L NEAR MILLED EDGE.
- [SDR FDEA202007301725](https://openairdocs.org/sdr/FDEA202007301725.md): Floor Support · cracked · Jul 30, 2020 · N882FD · Boeing 777F28 · Fuselage Miscellaneous Structure
  > LOWER BULK CARGO COMPARTMENT BS 1916, RBL 49.8 FLOOR SUPPORT FOUND CRACKED. REPAIRED AS PER B777 SRM 53-70-53-2R FIGURE 202 REPAIR 2 FROM EXISTING SPLICE STATION 1927 TO STATION 1886.6. RIGHT BUTT LINE 49.8. REPAIR CLASSIFIED AS MAJOR MAJOR PER GMM 6-2-100
- [SDR FDEA2020081421648](https://openairdocs.org/sdr/FDEA2020081421648.md): Longeron · cracked · Jul 25, 2020 · N882FD · Boeing 777F28 · Fuselage Main, Longeron/Stringer
  > DURING ULTRASONIC INSPECTION CARRIED OUT AT LEFT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 AND STRINGER 36 FOUND 02 EA FASTENER HOLES WITH CRACK INDICATIONS AS MARKED. COMPLIED WITH EO. #: G-5310-E0332629G P5. TITLE: FUSELAGE - MAINFRAME - INSPE
- [SDR FDEA2020081451647](https://openairdocs.org/sdr/FDEA2020081451647.md): Longeron · cracked · Jul 25, 2020 · N882FD · Boeing 777F28 · Fuselage Main, Longeron/Stringer
  > DURING ULTRASONIC INSPECTION CARRIED OUT AT RIGHT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 AND STRINGER 36 FOUND 01EA FASTENER HOLES WITH CRACK INDICATIONS AS MARKED. COMPLIED WITH EO. #:G-5310-E0332629G P6. TITLE:FUSELAGE- MAINFRAME - INSPECTIO
- [SDR FDEA2020072751648](https://openairdocs.org/sdr/FDEA2020072751648.md): Stringer · cracked · Jul 25, 2020 · N882FD · Boeing 777F28 · Fuselage Main, Longeron/Stringer
  > DURING ULTRASONIC INSPECTION CARRIED OUT AT LEFT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 AND STRINGER 36 FOUND 04EA FASTENER HOLES WITH CRACK INDICATION AS MARKED.
- [SDR FDEA2020072751647](https://openairdocs.org/sdr/FDEA2020072751647.md): Stringer · cracked · Jul 25, 2020 · N882FD · Boeing 777F28 · Fuselage Main, Longeron/Stringer
  > DURING ULTRASONIC INSPECTION CARRIED OUT AT RIGHT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 AND STRINGER 36 FOUND 03EA FASTENER HOLES WITH CRACK INDICATIONS AS MARKED.
- [SDR FDEA201901110098](https://openairdocs.org/sdr/FDEA201901110098.md): Sleeve · missing · Jan 11, 2019 · N882FD · Boeing 777F28 · Landing Gear Brake System
  > FOUND DURING REMOVAL OF MAIN WHEEL NR 10 BRAKE SLEEVE ASSY MISSING. ADDITIONALLY FOUND CHARFING DAMAGE ON MAIN WHEEL ASSY AND BRAKE ASSY. C/W E.A. G-3242-T0344587. NO FURTHER DAMAGE NOTICED. INSTALLED NEW BRAKE SLEEVE IAW AMM 32-45-07-4. A/C OK FOR SERVICE.
- [SDR FDEA201710263059](https://openairdocs.org/sdr/FDEA201710263059.md): Floor Support · cracked · Oct 26, 2017 · N882FD · Boeing 777F28 · Fuselage Miscellaneous Structure
  > BULK CARGO FLOOR SUPPORT AT BS 1915 - 1920, RBL 42 FOUND CRACKED. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 53-70-53-2R, FIG 202, REPAIR 2. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201703220970](https://openairdocs.org/sdr/FDEA201703220970.md): Switch · bent · Mar 22, 2017 · N882FD · Boeing 777F28 · Emergency Lighting
  > ON ARRIVAL, DURING CONNECT FLT INTERPHONE FOUND EMER EXIT LIGHT TEST SWITCH BENT ON NLG. REPLACED THE TEST SWITCH.
- [SDR FDEA201605271742](https://openairdocs.org/sdr/FDEA201605271742.md): Fms · out of date · May 27, 2016 · N882FD · Boeing 777F28 · Flight Management Computing Hardware System
  > REJECTED ON TAKEOFF DUE TO A FMC RNWY DISAGREE, CAUTION MSG ON EICAS. REJECT WAS AT 30 KT, ON RNWY 04 WINDS WERE 050 - 10 KTS. THE FMC IS AN MEL 34-61-01-03, REGARDING THE NAV DATA BASE IN THE FMC BEING OUT OF DATE, BUT IT DOES NOT SAY ANYTHING ABOUT GETTIN
- [SDR FDEA201501030014](https://openairdocs.org/sdr/FDEA201501030014.md): Light · inoperative · Jan 3, 2015 · N882FD · Boeing 777F28 · Emergency Lighting
  > EMERGENCY CEILING LIGHT AT L1 DOOR IS INOPERATIVE. RELAMPED L1 DOOR AREA EMER LIGHT IAW AMM 33-50-00-2. OPERATIONS CHECKED NORMAL.
- [SDR FDEA201307221671](https://openairdocs.org/sdr/FDEA201307221671.md): Slide · low pressure · Jul 22, 2013 · N882FD · Boeing 777F28 · Escape Slide
  > R1 DOOR EMERGENCY SLIDE OUT OF GREEN BAND. R & R R1 DOOR EMERGENCY SLIDE IAW AMM 25-66-01-4. ACFT OK FOR SERVICE.
- [SDR FDEA201303120551](https://openairdocs.org/sdr/FDEA201303120551.md): Bottle · low pressure · Mar 12, 2013 · N882FD · Boeing 777F28 · Escape Slide
  > FOUND R1 DOOR SLIDE INDICATOR NEEDLE IN RED. R & R R1 DOOR SLIDE RAFT ASSY PER MM 25-66-01-4.
- [SDR FDEA201302210389](https://openairdocs.org/sdr/FDEA201302210389.md): Line · leaking · Feb 21, 2013 · N882FD · Boeing 777F28 · Crew Oxygen System
  > F/O O2 MASK DOES NOT INFLATE CORRECTLY WHEN DONNING. F/O OXYGEN MASK HARNESS PIPE WAS LEAKING. R & R F/O OXYGEN MASK IAW MM 35-11-18-2.
- [SDR FDEA201109013627](https://openairdocs.org/sdr/FDEA201109013627.md): Spring · out of adjust · Sep 1, 2011 · N882FD · Boeing 777F28 · Emergency Lighting
  > GUARD ON EMERGENCY LIGHTS SWITCH HAS MALFUNCTIONED; DOES NOT ARM SOMETIMES WHEN CLOSED. ADJUSTED SPRING ON SWITCH GUARD; SWITCH CHECKS GOOD REF AMM 33-51-00-5-0. FINAL CLOSED.
- [SDR FDEA201105231930](https://openairdocs.org/sdr/FDEA201105231930.md): Warning Light · illuminated · May 23, 2011 · N882FD · Boeing 777F28 · Auto Throttle System
  > AFTER LANDING DURING RUNWAY TURNOFF AT LESS THAN 10 KNOTS F/O SELECTED SPEED BRAKES UP ENGINES WENT TO MAX POWER ON GROUND. WITH ALERTS CONFIG GEAR/CONFIG FLAPS/GEAR STEERING AD ORAL ALERT - HAD TO SLAM BRAKES HARD. AD DISCONNECT A/T MANUALLY. INTERROGATED

## 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 = 'N882FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N882FD/reports

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