Boeing 777F28

Service difficulty reports · 72

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duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA202610051477Hose · disconnectedON 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.Oct 5, 2026 · N882FD · Boeing 777F28 · Landing Gear Brake SystemSDR FDEA202602170225Safety Wire · wrong partRIGHT 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 SERVICEFeb 17, 2026 · N880FD · Boeing 777F28 · Escape SlideSDR FDEA202602150202Slide · not reportedLH SLIDE ELECTRONIC CLOSURE FROM TRANSACTION MCFCTMOD, CLOSED DUE TO REMOVAL OF AFFECTED PART.Feb 15, 2026 · N882FD · Boeing 777F28 · Escape SlideSDR FDEA202510222070Skin · dentedREWORK: 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 Oct 22, 2025 · N882FD · Boeing 777F28 · Trailing Edge FlapsSDR FDEA202510162033Skin · dentedRH 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 6Oct 16, 2025 · N882FD · Boeing 777F28 · Trailing Edge FlapsSDR FDEA202510152010Skin · crackedDURING 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,Oct 15, 2025 · N882FD · Boeing 777F28 · Fuselage Main, Plate/SkinSDR FDEA202510152009Skin · crackedDURING 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, SROct 15, 2025 · N882FD · Boeing 777F28 · Fuselage Main, Plate/SkinSDR FDEA202508021365Light · malfunctionedEMERGENCY 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 33-51-00-5Aug 2, 2025 · N880FD · Boeing 777F28 · Emergency LightingSDR FDEA202503140410Skin · crackedRH 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 ANMar 14, 2025 · N880FD · Boeing 777F28 · Leading Edge DevicesSDR FDEA202503050333Skin · crackedRH 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-5Mar 5, 2025 · N880FD · Boeing 777F28 · Leading Edge DevicesSDR FDEA202503050332Skin · crackedOPEN 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, 51-40-02Mar 5, 2025 · N880FD · Boeing 777F28 · Wing, Plate/SkinSDR FDEA202501150071Controller · failedANTI 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. TJan 15, 2025 · N882FD · Boeing 777F28 · Engine Anti-Icing SystemSDR FDEA202410031414Outflow Valve · faultedON 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 Oct 3, 2024 · N880FD · Boeing 777F28 · Pressure Regulator/Outflow ValveSDR FDEA202405190689Tire · leakingON 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 May 19, 2024 · N882FD · Boeing 777F28 · TireSDR FDEA202312231955Switch · failedDURING 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.Dec 23, 2023 · N882FD · Boeing 777F28 · Emergency LightingSDR FDEA202312231954Module · failedDURING 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.Dec 23, 2023 · N882FD · Boeing 777F28 · Emergency LightingSDR FDEA202304240753Unknown · unknownPDIS 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 ALTERNAApr 24, 2023 · N880FD · Boeing 777F28 · Central WarningSDR FDEA202304240752Unknown · unknownPDIS 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 Apr 24, 2023 · N880FD · Boeing 777F28 · Central WarningSDR FDEA202304210731Floor Panel · crackedMAIN 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,REPAIRApr 21, 2023 · N882FD · Boeing 777F28 · Fuselage Floor PanelSDR FDEA202304210730Floor Panel · crackedMAIN 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. REPAApr 21, 2023 · N882FD · Boeing 777F28 · Fuselage Floor PanelSDR FDEA202304210729Floor Panel · crackedMAIN 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,REPAIRApr 21, 2023 · N882FD · Boeing 777F28 · Fuselage Structure (General)SDR FDEA202209222354Lamp · inoperativeMDIS 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. Sep 22, 2022 · N880FD · Boeing 777F28 · Emergency LightingSDR FDEA202207291819Floor Panel · crackedMAIN 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.Jul 29, 2022 · N880FD · Boeing 777F28 · Fuselage Floor PanelSDR FDEA202207291818Floor Panel · crackedMAIN 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.Jul 29, 2022 · N880FD · Boeing 777F28 · Fuselage Floor PanelSDR FDEA202207291817Floor Panel · crackedMAIN 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.Jul 29, 2022 · N880FD · Boeing 777F28 · Fuselage Floor PanelSDR FDEA202206261566Tire · delaminatedPDIS 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 COJun 26, 2022 · N880FD · Boeing 777F28 · Brake Anti-Skid SectionSDR FDEA202201270753Lamp · failedPDIS 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 SERVICEJan 27, 2022 · N882FD · Boeing 777F28 · Emergency LightingSDR FDEA202106021435Brake Assy · fireAFTER 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 AJun 2, 2021 · N880FD · Boeing 777F28 · Landing Gear Brake SystemSDR FDEA202009302365Battery · corrodedMDIS 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 DOSep 30, 2020 · N880FD · Boeing 777F28 · Emergency EquipmentSDR FDEA202008071783Floor Support · crackedBULK 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 MAJOAug 7, 2020 · N882FD · Boeing 777F28 · Fuselage Miscellaneous StructureSDR FDEA2020081821747Skin · cracked02 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 Aug 2, 2020 · N882FD · Boeing 777F28 · Fuselage Main, Plate/SkinSDR FDEA2020081402747Skin · cracked02 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: FUAug 2, 2020 · N882FD · Boeing 777F28 · Fuselage Main, Plate/SkinSDR FDEA2020081421746Skin · crackedCRACK 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 - INSPAug 2, 2020 · N882FD · Boeing 777F28 · Fuselage Main, Plate/SkinSDR FDEA2020080321747Skin · crackedTWO 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.Aug 2, 2020 · N882FD · Boeing 777F28 · Fuselage Main, Plate/SkinSDR FDEA2020080321746Skin · crackedCRACK FOUND APPROXIMATE 0.7" IN LENGTH, DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON THE FUSELAGE SKIN AT BS 1030, STRINGER 37L.Aug 2, 2020 · N882FD · Boeing 777F28 · Fuselage Main, Plate/SkinSDR FDEA2020080321745Skin · damagedWHILE ACCOMPLISHING EO G-5310-E0332629 G P6, FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT BS 998, STRINGER 35R NEAR MILLED EDGE.Aug 2, 2020 · N882FD · Boeing 777F28 · Fuselage Main, Plate/SkinSDR FDEA2020080321744Skin · damagedWHILE ACCOMPLISHING EO G-5310-E0332629 G P5 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT BS 998, STRINGER 35L NEAR MILLED EDGE.Aug 2, 2020 · N882FD · Boeing 777F28 · Fuselage Main, Plate/SkinSDR FDEA202007301725Floor Support · crackedLOWER 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 6-2-100Jul 30, 2020 · N882FD · Boeing 777F28 · Fuselage Miscellaneous StructureSDR FDEA2020081421648Longeron · crackedDURING 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 - INSPEJul 25, 2020 · N882FD · Boeing 777F28 · Fuselage Main, Longeron/StringerSDR FDEA2020081451647Longeron · crackedDURING 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 - INSPECTIOJul 25, 2020 · N882FD · Boeing 777F28 · Fuselage Main, Longeron/StringerSDR FDEA2020072751648Stringer · crackedDURING 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.Jul 25, 2020 · N882FD · Boeing 777F28 · Fuselage Main, Longeron/StringerSDR FDEA2020072751647Stringer · crackedDURING 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.Jul 25, 2020 · N882FD · Boeing 777F28 · Fuselage Main, Longeron/StringerSDR FDEA202005291078Battery · dischargedPOST 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.May 29, 2020 · N880FD · Boeing 777F28 · Passenger/Crew DoorsSDR FDEA202002200358Skin · damagedWHILE 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-T0352363Feb 20, 2020 · N880FD · Boeing 777F28 · Fuselage Main, Plate/SkinSDR FDEA202002200357Skin · crackedDURING 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 LFeb 20, 2020 · N880FD · Boeing 777F28 · Fuselage Main, Plate/SkinSDR FDEA202002140333Skin · crackedDURING 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 RIGHFeb 13, 2020 · N880FD · Boeing 777F28 · Fuselage Main, Plate/SkinSDR FDEA202002140332Spar · crackedDURING 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 LFeb 13, 2020 · N880FD · Boeing 777F28 · Wing SparSDR FDEA2020020650268Longeron · crackedDURING 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 UNDERWINGFeb 5, 2020 · N880FD · Boeing 777F28 · Fuselage Main, Longeron/StringerSDR FDEA202002060267Longeron · crackedDURING 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 Feb 5, 2020 · N880FD · Boeing 777F28 · Fuselage Main, Longeron/StringerSDR FDEA2019101082496Battery Pack · inoperativeEMERGENCY LIGHT TEST FAIL. FOUND LH SIDE EMERGENCY LIGHT BATTERY PACK UNSERVICEABLE. REPLACED BATTERY PACK ACC. AMM. 33-51-06. OPS CHECK FOUND SATISFACTORY.Oct 8, 2019 · N880FD · Boeing 777F28 · Emergency Lighting
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