N855FD
Service difficulty reports · 32
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
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 n_number = 'N855FD' AND registry_match = 'registration' 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.
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 = 'N855FD' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA202605140595Skin · debondedLEFT OTBD FLAP LWR SURFACE FROM OTBD TO INBD 268 INCHES CROSS TE TO LE 10 INCHES FOUND DEBONDED. REPAIRED LH OB FLAP LWR SURFACE DISBOND AT OTEF STA 260 AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 AND SRM 51-70-04-2R-0 PARA 4N FIGURE SDR FDEA202605110581Skin · bulgedFOUND RT WING LE NR 11 SLAT EXTERNAL SURFACE A BULGE AT STA 873. BULGE REPAIRED AS PER B777 SRM57- 43-01-2R REPAIR 9 FIGURE 202 REV:51.0 AND EA G-5750-T0387321 P1. TITLE: WING-FLIGHT SURFACES-RH WING #11 SLAT OUTER SKIN BULGES AT NOSE BEAM AREA BETWEEN OSBSDR FDEA202605110580Skin · bulgedFOUND RT WING LE NR 9 SLAT EXTERNAL SURFACE A BULGE AT STA 564. BULGE REPAIRED AS PER B777 SRM57-43- 01-2R REPAIR 16 FIGURE 202 REV:53.0. AND EA G-5750-T0387322 P1. TITLE: WING - FLIGHT SURFACES-RH WING #9 SLAT OUTER SKIN BULGE AT NOSE RIB AT OSCS 564 - SRSDR FDEA202605100579Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285 G P12 STEP3.B & STEP5.A.(2) THEN FOUND 01EA CRACK ON THE RH UPPER WING SKIN FASTENER #5. RH UPPER WING SKIN RIB BAY 10 TRAILING EDGE #5 HOLE REPAIRED AS PER B777 SRM 51-40-05- 0G FIGURE 4 TABLE C,51-40-02-0G,51-40-SDR FDEA202605100578Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285 G P11 STEP3.B & STEP5.A.(2) FOUND TWO CRACKS ON THE LT UPPER WING SKIN FASTENER #5. H WING UPPER SKIN IN RIB BAY 10 TRAILING EDGE #5 HOLE REPAIRED AS PER B777 SRM 51-50- 02-0G FINGURE 1,51-40-02-0G,51-10-01-0G,51-20SDR FDEA202508181496Power Supply · no test2 EMERGENCY LIGHTS IN COURIER AREA ABOVE R1 ARE INOP. ONE INOPERATIVE LIGHT LOCATED ABOVE GALLEY AREA, SECOND INOPERATIVE LIGHT LOCATED NEAR R1 DOOR. AMM: 33-51-06-2, AMM: 33-51-00-5. REPLACED RIGHT POWER SUPPLY PER AMM 33-51-06-2, ACCOMPLISHED EMERGENCY SDR FDEA202410091453Throttle Control · malfunctionedDURING LEFT ENGINE START, WITH THE RIGHT ENGINE SHUTDOWN, BOTH THROTTLES ADVANCED UNCOMMANDED TOWARDS MAX POWER. CREW PULLED BOTH THROTTLES TO FLIGHT IDLE AND APPLIED MAX WHEEL BRAKING. NO STATUS OR MAINTENANCE MSGS RELATED TO THIS OBSERVED FAULT. RAN ALLSDR FDEA202308151433Flap · dentedLH OB FLAP LWR SURFACE FROM IB TO OB 330 INCH CROSS LE TO TE 43 INCH FOUND ONE DENT. EVALUATED LH OB FLAP LWR SURFACE FROM IB TO OB 330 INCH CROSS LE TO TE 43 INCH ONE DENT WITH DAMAGE SIZE L*W=3"*2.75" WITHIN REPAIR LIMIT AS PER B777 SRM 57-53-01-1A ALLOWSDR FDEA202308101393Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241MF(P/N:152W8402-17) AT STA1290/LBL105.5-107.5 FOUND CRACK(OFF WING). EVALUATED MAIN DECK CARGO FLOOR PANEL 241MF(P/N:152W8402-17) CRACK, THE DAMAGE SIZE : L=2.2", OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DSDR FDEA202308101392Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8402-18) AT STA1269.5/RBL81-83.25 FOUND CRACK(OFF WING). EVALUATED MAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8402-18) CRACK ,THE DAMAGE SIZE :L=2.3" , OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DSDR FDEA202308081373Skin · corrodedFOUND THE LOWER FUSELAGE SKIN CORROSION INSIDE BODY FAIRING 192JR AT BS 930 TO BS 940 AND S-49L TO S-49R. THE LOWER FUSELGE SKIN CORRODED AREA AT BS 930 TO BS 940 AND S-49L TO S-49R REMOVED & THE REWORKED AREA MEASURED THE ORIGINAL THICKNESS IS T=0.100", SDR FDEA202101280212Skin · crackedDURING ACCOMPLISHMENT OF HFEC INSPECTION ON RH FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATIONS AROUND 01 EA FASTENER HOLE AT STA 1033 STR 37R, APPROX 1.5" IN LENGTH. COMPLIED WITH E.O.#:G-5310-E0332629 I P6 TITLE:FUSELAGE-MAINFRAME-INSPSDR FDEA202101150117Doubler · misinstalledWHILE ACCOMPLISHING LH E.O.#G-5310-E0332629 I P5 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STA 998 STR. S-35L NEAR MILLED EDGE COMPLIED WITH E.A.#:G-5310-T0359410 P1 TITLE : FUSELAGE-MAINFRAME-DEVIATIONS TO SB- 777-53-0087 R1 - LHS AND RHS UNDERWING SDR FDEA202101150116Doubler · misinstalledWHILE ACCOMPLISHING RH E.O.#G-5310-E0332629 I P6 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STA 998 STR. S-35R NEAR MILLED EDGE. COMPLIED WITH E.A.#:G-5310-T0359410 P2 TITLE : FUSELAGE-MAINFRAME-DEVIATIONS TO SB- 777-53-0087 R1 - LHS AND RHS UNDERWINGSDR FDEA202101150115Skin · crackedDURING ACCOMPLISHMENT OF HFEC INSPECTION ON RH FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATIONS AROUND 01 EA FASTENER HOLE STA 1028 STR 37R, APPROX 1.5" IN LENGTH. COMPLIED WITH E.O.#:G-5310-E0332629 I P6. TITLE: FUSELAGE-MAINFRAME-INSPESDR FDEA202101150109Spar · crackedDURING HFEC OPEN HOLE INSPECTION CARRIED OUT AS PER EO NO:E G-5310-E0332629 I P6 ON OVERSIZED FASTENER HOLES AND FOUND (01 EA) CRACK INDICATION ON RHS VERTICAL FLANGE OF THE FRONT LOWER SPAR CHORD AT BS 1035 APPROX. RBL 81.30 LOWER O/B HOLE. WING CENTER SDR FDEA202101150114Skin · crackedDURING ACCOMPLISHMENT OF HFEC INSPECTION ON LH FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATION AROUND FASTENER HOLE AT STA 1033 STR 37L, APPROX 1.5" IN LENGTH, AS MARKED. COMPLIED WITH E.O.#G-5310-E0332629 I P5. TITLE:FUSELAGE- MAINFRAMSDR FDEA202101110038Floor Support · crackedLOWER BULK CARGO COMPARTMENT STATION 1937, RIGHT BUTT LINE 41 FLOOR STRINGER FOUND WITH CRACK AS MARK. LOWER BULK CARGO COMPARTMENT STATION 1937 RIGHT BUTT LINE 41 FLOOR STRINGER CRACKED REPAIRED AS PER B777 SRM 53-70-53-2R FIGURE 202 REPAIR 2 FROM STATIONSDR FDEA202101100032Floor Support · crackedLOWER BULK CARGO COMPARTMENT STATION 1980, RIGHT BUTT LINE 33 FLOOR STRINGER FOUND WITH CRACK AS MARK. LOWER BULK CARGO COMPARTMENT STATION 1980 RIGHT BUTT LINE 33. FLOOR STRINGER CRACKED REPAIRED AS PER B777 SRM 53-70-53-2R FIGURE 202 REPAIR 2 FROM EXISTISDR FDEA202101100031Floor Support · crackedLOWER BULK CARGO COMPARTMENT STATION 1980, RIGHT BUTT LINE 41 FLOOR STRINGER FOUND WITH CRACK AS MARK. LOWER BULK CARGO COMPARTMENT STATION 1980 RIGHT BUTT LINE 41 FLOOR STRINGER CRACKED REPAIRED AS PER B777 SRM 53-70-53-2R FIGURE 202 REPAIR 2 FROM STATIONSDR FDEA201710152964Frame · crackedNR 2 ENGINE PYLON HAS AN INTERNAL FRAME CRACKED. CRACK LOCATED INBOARD SIDE NAC STA 325.3, JUST ABOVE AFT ACCESS DOOR FOR AFT ENGINE MOUNT BOLTS. CRACK CONFIRMED WITH HFEC AND MEASURES APPROXIMATELY 2.5 INCH. FABRICATED A DOUBLER. CLEANED PART , PRIMED, SDR FDEA201703270995Duct · rupturedCARGO FIRE WARNING DURING TAXI, BOTTLES DISCHARGED, STATUS MESSAGE FOR BOTTLE 1B AND BOTTLE 1A. REPLACED A RUPTURED DUCT.SDR FDEA201610063476Switch · out of positionEICAS MESSAGE FOR EMERGENCY LIGHTS. ACFT RETURNED TO BLOCKS. FOUND EMERGENCY SWITCH GUIDE RING OUT OF RANK. REPOSITION AND PERFORMED RTS PASSED IAW MM 33-50-00. ACFT OK FOR SERVICESDR FDEA201507112197Link · brokenON ARRIVAL, FOUND LT MAIN GEAR DOOR & MLG DRAG STRUT DOOR DAMAGED DUE TO LINK BROKEN ON MLG DRAG STRUT DOOR. REINSTALLED LT MAIN LANDING GEAR SHOCK STRUT DOOR IAW AMM 32-12-06-4, REINSTALLED LT MAIN LANDING GEAR DRAG STRUT DOOR AND LINKAGE IAW AMM 32-12-08-4SDR FDEA201504171254Eec · inoperativeDURING CRUISE THE LT ENGINE FLAMED OUT, WOULD NOT RESTART. LEFT FUEL CONTROL VALVE ILUMINATED SHUTTING DOWN LEFT ENGINE. INFLIGHT START CHECKLIST ACCOMPLISHED LEFT ENGINE WOULD NOT RESTART. INTERROGATED MAT AND FOUND ENG EEC C1 L FAULT LATCHED (FAULT CODE )SDR FDEA201406081361Tire · leakingABOUT 90 MINUTES INTO THE FLIGHT, RECEIVED AN EICAS, TIRE PRESSURE NR 10. TIRE SHOWED AMBER AT 184 PSI. NR 10 TIRE PRESSURE CONTINUED TO SLOWLY DECREASE DURING FLIGHT. LOWEST PRESSURE OBSERVED 128 PSI. R & R NR 9 & 10 MLG WHEEL & TIRE ASSEMBLY IAW AMM 32-45SDR FDEA201307101519Lamp · inoperativeEXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP. OPS CHECK GOOD IAW MM 33-51-00-5.SDR FDEA201303300690Skin · damagedRIGHT NOSE SKIN BEHIND F/O WINDOW FOUND 2 LIGHTNING STRIKES DAMAGED AT BS 246 AND 228. REPAIRED IAW EA G 5330-161299A PART 3.SDR FDEA201205151811Handle · out of adjustL1 DOOR WAS HARD TO MOVE SLIDE HANDLE FROM DISARM TO ARMED POSITION ON BLOCKOUT. PERFORMED ADJUSTMENT AND TEST IAW MM 52-11-00-5. OPS CHECKED NORMAL. OK FOR SERVICE.SDR FDEA201203070865Skin · delaminatedLEFT WING FLAP DELAMINATED T/E BETWEEN NR 1 AND NR 2 CANOE APPROX 10" X 10" AREA . REMOVED LT OTBD T/E FLAP REF MM 27-51-21-4. T/E FLAP SYS MAINT PRACTICES COMPLIED WITH IAW MM 27-51-00-2. REMOVAL/INSTALLATION COMPLIED WITH IAW MM 27-51-21-4 AND OTBD T/E FLASDR FDEA201202150580Bracket · looseL1 DOOR SLIDE CONTAINER LOWER BRACKET LOOSE. AFFIXED COMESTIC TRIM PIECE TO L1 DOOR BUSTLE IAW MM 25-66-06 AND SMP CH 20.SDR FDEA201107082614Autothrottle Sys · malfunctionedON TAXI OUT, HAD AN UNCOMMANDED AUTO THROTTLE ENGAGEMENT TO TAKEOFF POWER. THROTTLES HAS JUST BEEN MOVED TO IDLE FROM ABOUT 30 PERCENT, AT WHICH TIME THE ATS ENGAGED. POWER CAME UP TO ABOUT 45 PERCENT BEFORE THROTTLES WERE OVER-RIDEN & THE A/T SWITCHES WERE
Back to N855FD