# Service difficulty reports: Boeing 777F28

A list on [Boeing 777F28](https://openairdocs.org/model/boeing-777f28.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 72 reports

- [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 FDEA202602170225](https://openairdocs.org/sdr/FDEA202602170225.md): Safety Wire · wrong part · Feb 17, 2026 · N880FD · Boeing 777F28 · Escape Slide
  > RIGHT SIDE DOOR SLIDE INSPECTION REVEALED THAT THE WRONG SAFETY WIRE WAS USED. THE WO REQUIRES REPLACING THE WIRE WITH MS20995CY16 CAD-PLATED COPPER WIRE. RH DOOR SLIDE RAFT RETURN TO NORMAL OPS, AIRCRAFT READY 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 FDEA202508021365](https://openairdocs.org/sdr/FDEA202508021365.md): Light · malfunctioned · Aug 2, 2025 · N880FD · Boeing 777F28 · Emergency Lighting
  > EMERGENCY LIGHTS ILLUMINATED DURING BEFORE START CHECKLIST. AMM 33-51-00-5 FOUND EMERGENCY LIGHT SWITCH AT THE OVERHEAD PANEL IN THE OFF POSITION. SWITCH PUT BACK TO ARM POSITION AND OPERATIONAL TEST PERFORMED IAW AMM 33-51-00-5
- [SDR FDEA202503140410](https://openairdocs.org/sdr/FDEA202503140410.md): Skin · cracked · Mar 14, 2025 · N880FD · Boeing 777F28 · Leading Edge Devices
  > RH WING NO.8 SLAT OUTER SKIN FOUND CRACKED AT 51 IN TO IB EDGE. RH WING NO.8 SLAT OUTER SKIN AT 51 INCH TO I/B EDGE CRACK AREA REPAIRED AS PER B777 SRM51-10-02-0G,51-20-01-0G,51-20-05-0G,51-40-02-0G,51-40-05-0G,51-40-08-0G,57-43-01-2R REPAIR 13 REV:47.5 AN
- [SDR FDEA202503050333](https://openairdocs.org/sdr/FDEA202503050333.md): Skin · cracked · Mar 5, 2025 · N880FD · Boeing 777F28 · Leading Edge Devices
  > RH WING NO.8 SLAT OUTER SKIN FOUND CRACKED AT 39 IN TO IB EDGE. RH WING NO.8 SLAT OUTER SKIN AT 39 IN TO IB EDGE CRACK REPAIRED AS PER B777 SRM51-10- 02-0G,51-20-01-0G,51-20-05-0G,51-40-02-0G,51-40-05-0G,51-40-08-0G,57-43-01-2R REPAIR 13 REV:47.5 AND EA G-5
- [SDR FDEA202503050332](https://openairdocs.org/sdr/FDEA202503050332.md): Skin · cracked · Mar 5, 2025 · N880FD · Boeing 777F28 · Wing, Plate/Skin
  > OPEN HOLE HFEC INSPECTION ON THE RH WING WBL 262 THEN FOUND HOLE #6 CRACK IN UPPER WING SKIN AS MARKED. RH WING WBL 262 UPPER SKIN #6 HOLE CRACK REPAIRED AS PER B777 SRM51-10-01-0G, 51-20-01- 0G, 51-20-05-0G,51-20-06-0G, 51-20-07-0G, 51-40-08-0G, 51-40-02
- [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 FDEA202410031414](https://openairdocs.org/sdr/FDEA202410031414.md): Outflow Valve · faulted · Oct 3, 2024 · N880FD · Boeing 777F28 · Pressure Regulator/Outflow Valve
  > ON DEPARTURE, ACFT WOULD NOT PRESSURIZE. THE FWD OUTFLOW VALVE ON MEL. THE REMAINING AFT OUTFLOW VALVE INDICATED CLOSED ON DEPART BUT WOULD NOT ALLOW ACFT TO PRESSURIZE. AIR RETURN OMDWB. ON ARRIVAL VERIFIED FWD OUTFLOW VALVE WAS STILL AT 7% OPEN. STATUS
- [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 FDEA202304240753](https://openairdocs.org/sdr/FDEA202304240753.md): Unknown · unknown · Apr 24, 2023 · N880FD · Boeing 777F28 · Central Warning
  > PDIS 880 31-50 3973 24APR23 MEM VMO GEAR DOWN STATUS MESSAGE. RETURNED TO MEM DUE TO UNABLE HIGHER ALTITUDE/AIRSPEED. AMM: 27-32-01-4 FIM: 31-51-00-810-957 TROUBLESHOT VMO GEAR DOWN MESSAGE PER B777 FIM 31-51-00-810-957 AND FOUND ALTERNA
- [SDR FDEA202304240752](https://openairdocs.org/sdr/FDEA202304240752.md): Unknown · unknown · Apr 24, 2023 · N880FD · Boeing 777F28 · Central Warning
  > PDIS 880 31-50 3973 24APR23 MEM FACT U VMO GEAR DOWN STATUS MESSAGE. RETURNED TO MEM DUE TO UNABLE HIGHER ALTITUDE/AIRSPEED. FACT 24APR23 08:02 MEM U AMM: 27-32-01-4 FIM: 31-51-00-810-957 TROUBLESHOT VMO GEAR DOWN MESSAGE PER B777 FIM
- [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 FDEA202209222354](https://openairdocs.org/sdr/FDEA202209222354.md): Lamp · inoperative · Sep 22, 2022 · N880FD · Boeing 777F28 · Emergency Lighting
  > MDIS 880 33-50 3430 21SEP22 ANC OPEN U DURING PREFLIGHT FOUND CENTER OVERHEAD EMERGENCY LIGHT OUT DURING EMERGENCY LIGHT TEST. ALL OTHER LIGHTS OPERATE NORMALLY. RELAMPED CENTER SUPERNUMERARY AREA LIGHT I..W. B777 M.M. TASK 33-51-03-960-801.
- [SDR FDEA202207291819](https://openairdocs.org/sdr/FDEA202207291819.md): Floor Panel · cracked · Jul 29, 2022 · N880FD · Boeing 777F28 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N:152W8701-11 FOUND CRACKED AT STA1970 LBL40. REPAIRED MAIN DECK CARGO FLOOR PANEL P/N:152W8701-11 CRACKED AT STA 1970 LBL40 AS PER B777 SRM 53-00-50-2R REPAIR 1 REV 41.0.REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202207291818](https://openairdocs.org/sdr/FDEA202207291818.md): Floor Panel · cracked · Jul 29, 2022 · N880FD · Boeing 777F28 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N:152W8601-31 FOUND CRACKED AT STA1748 BL0. MAIN DECK CARGO FLOOR PANEL P/N: 152W8601-31 CRACKED AT STA1748 BL0 AS PER B777 SRM 53-00-50-2R REPAIR 1 REV 41.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202207291817](https://openairdocs.org/sdr/FDEA202207291817.md): Floor Panel · cracked · Jul 29, 2022 · N880FD · Boeing 777F28 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N:152W8601-17 FOUND CRACKED AT STA1660 BL0. REPAIRED MAIN DECK CARGO FLOOR PANEL P/N:152W8601-19 CRACKED AT STA1660 BL0 AS PER B777 SRM 53-00-50-2R REPAIR 1 REV41.0.REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202206261566](https://openairdocs.org/sdr/FDEA202206261566.md): Tire · delaminated · Jun 26, 2022 · N880FD · Boeing 777F28 · Brake Anti-Skid Section
  > PDIS 880 32-41 3226 26JUN22 MEM FACT U SUSPECTED TIRE FAILURE ON TAKEOFF IN OSAKA. LANDED WITHOUT INCIDENT. TIRE DID INCUR FURTHER DAMAGE. NEED CHANGE RH NOSE WHEEL ***EMERGENCY DECLARED*** RH NOSE TIRE FOUND TO HAVE A COUPLE STRANDS OF CO
- [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 FDEA202106021435](https://openairdocs.org/sdr/FDEA202106021435.md): Brake Assy · fire · Jun 2, 2021 · N880FD · Boeing 777F28 · Landing Gear Brake System
  > AFTER BLOCK IN, #8 BRAKE CAUGHT FIRE. FIRE EXTINGUISHED BY RAMP CREW, THEN BY FIRE DEPARTMENT. REMOVED #8 BRAKE & WHEEL & PERFORMED HIGH ENERGY STOP/ HEAT DAMAGE INSPECTION ON ALL WHEELS & BRAKES IAW AMM: 05-51-14-2. NO DEFECT FOUND. REPLACED # 8 BRAKE A
- [SDR FDEA202009302365](https://openairdocs.org/sdr/FDEA202009302365.md): Battery · corroded · Sep 30, 2020 · N880FD · Boeing 777F28 · Emergency Equipment
  > MDIS 880 52-20 1013 30SEP20 MEM. L1 EPAS BATTERY UNIT TERMINALS ARE CORRODED. FACT 30SEP20 21:38 MEM 0000086819 STEVENSON, BRIAN A-30-SEP-2020 14:10. REPLACED L1 DOOR EPAS BATTERY PACK, REF B777 AMM 52-11-20-4-2. OPS CHECK GOOD. REMOVAL AND INSTALATION DO
- [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 FDEA202005291078](https://openairdocs.org/sdr/FDEA202005291078.md): Battery · discharged · May 29, 2020 · N880FD · Boeing 777F28 · Passenger/Crew Doors
  > POST FLIGHT INSPECTION. L-1 DOOR EPAS BATTERY PACK STATUS LIGHT NOT FLASHING. REMOVED AND REPLACED THE 2 9V BATTERIES FOR THE L-1 EPAS BATTERY PACK IAW AMM 52-11-20-4-2. RE-ARMED L-1 EPAS SYS AND GREEN STATUS LT RESTORED. NORMAL ITEM OK FOR SERVICE.
- [SDR FDEA202002200358](https://openairdocs.org/sdr/FDEA202002200358.md): Skin · damaged · Feb 20, 2020 · N880FD · Boeing 777F28 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING E.O. #G-5310-EO332629 D P5 FOUND EXISTING UNDERWING LONGERON FASTENER HOLE AT LEFT HAND STATION 1014 AND STRINGER 36 LEFT OVERSIZED TO 0.403" INSTEAD OF 0.371" AS PER DRAWING 675W0002 SHEET 8. WORK ACCOMPLISHED AS PER EA G-5310-T0352363
- [SDR FDEA202002200357](https://openairdocs.org/sdr/FDEA202002200357.md): Skin · cracked · Feb 20, 2020 · N880FD · Boeing 777F28 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND SIDE FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND 02 CRACK INDICATION AROUND FASTENER HOLES AT STATION 1024 AND STATION 1032, STRINGER 37 LEFT, APPROXIMATE 0.8" AND 1" IN L
- [SDR FDEA202002140333](https://openairdocs.org/sdr/FDEA202002140333.md): Skin · cracked · Feb 13, 2020 · N880FD · Boeing 777F28 · 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 UNDERWING LONGERON AND FUSELAGE SKIN FOUND 02 EACH CRACKS WHICH APPROXIMATE 0.3" AT STATION 1032. STRINGER 37 RIGH
- [SDR FDEA202002140332](https://openairdocs.org/sdr/FDEA202002140332.md): Spar · cracked · Feb 13, 2020 · N880FD · Boeing 777F28 · Wing Spar
  > DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON RIGHT HAND SIDE UNDERWING LONGERON LOWER WING FRONT SPAR CHORD AND FOUND 01 EACH HOLE WITH CRACK INDICATION AS MARKED. (STATION 1035 RBL 82) CRACKED RIGHT HAND SIDE UNDERWING LONGERON L
- [SDR FDEA2020020650268](https://openairdocs.org/sdr/FDEA2020020650268.md): Longeron · cracked · Feb 5, 2020 · N880FD · Boeing 777F28 · Fuselage Main, Longeron/Stringer
  > DURING ULTRASONIC INSPECTION CARRIED OUT AT LEFT SIDE UNDERWING LONGERON AT BODY STATION 1035, FOUND CRACK INDICATIONS ON 02 EACH FASTENER AT VERTICAL FLANGE AND 01 EACH FASTENER AT HORIZONTAL FLANGE AS MARKED. WORK ACCOMPLISHED ON LEFT HAND SIDE UNDERWING
- [SDR FDEA202002060267](https://openairdocs.org/sdr/FDEA202002060267.md): Longeron · cracked · Feb 5, 2020 · N880FD · Boeing 777F28 · Fuselage Main, Longeron/Stringer
  > DURING ULTRASONIC INSPECTION CARRIED OUT AT RIGHT SIDE UNDERWING LONGERON AT BODY STATION 1035, FOUND CRACK INDICATIONS ON 02 EACH FASTENER AT VERTICAL FLANGE AS MARKED. WORK ACCOMPLISHED ON RIGHT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 AS PER
- [SDR FDEA2019101082496](https://openairdocs.org/sdr/FDEA2019101082496.md): Battery Pack · inoperative · Oct 8, 2019 · N880FD · Boeing 777F28 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAIL. FOUND LH SIDE EMERGENCY LIGHT BATTERY PACK UNSERVICEABLE. REPLACED BATTERY PACK ACC. AMM. 33-51-06. OPS CHECK FOUND SATISFACTORY.

Next page: https://openairdocs.org/model/boeing-777f28/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 aircraft_model_key = '777F28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-777f28/reports

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