N890FD
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 = 'N890FD' 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 = 'N890FD' 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 FDEA202604240496Bulb · inoperativeR1 DOOR AFT EMERGENCY EXIT SIGN LIGHT INOP (1EA BULB). REPLACED THE BULB EMERGENCY EXIT LIGHT AT R1 DOOR IAW AMM 33-51-01-2.SDR FDEA202602150211Safety Wire · wrong partWRI TO REPLACE THE R1 DOOR SLIDE WIRE WITH MS20995CY16 WIRE. AMM: 25-66-01-4 REPLACED R1 DOOR SLIDE SHEAR WIRE WITH MS20995CY16 WIRE PER REF ABOVESDR FDEA202505010702Skin · chafedFWD CARGO DOOR SURROUND FWD EDGE AT 10.5" FROM BOTTOM FOUND CHAFFED. FWD CARGO DOOR SURROUND FWD EDGE AT 10.5" FROM BOTTOM CHAFFED AREA REPAIRED AS PER B777 SRM 51-40-02-0G, SRM 51-10-02-0G, SRM53-10-01-2R REPAIR 1, SRM 51-40-05-0G, SRM 51- 40-08-0G, SRM 51SDR FDEA202505010701Skin · dentedFOUND RHW T/E O/B FLAP LOWER SURFACE DENT 01 EA AT THE CROSS OTEF 263 AND T/E 4 INCHES. REPAIRED RHW T/E O/B FLAP LOWER SURFACE DENT 01 EA AT THE CROSS OTEF 263 AND T/E 4 INCHES AS PER B777 SRM 57-53-01-2R-2 AND SRM 51-70-04-2R-1 REV 47.5 AND EA:G-5750-T0SDR FDEA202505010700Skin · dentedFOUND RHW T/E I/B FLAP LOWER SURFACE DENT (LENGTH 15.5 INCHES AND WIDE 13.5 INCHES) AT THE CROSS ITEF 260 AND T/E 21 INCHES. REPAIRED RHW T/E I/B FLAP LOWER SURFACE DENT(LENGTH 15.5 INCHES AND WIDE 13.5 INCHES) AT THE CROSS ITEF 260 AND T/E 21 INCHES AS PSDR FDEA202505010698Skin · crackedOPEN HOLE HFEC INSPECTION OF #5 HOLE AT RH WING UPPER SKIN WBL 262 AND FOUND 01EA CRACK AS MARKED. RH WING UPPER SKIN WBL 262 #5 HOLE CRACKED AREA REPAIRED AS PER B777 SRM 51-40-05-0G, SRM51-40-02-0G, SRM51-40-04-0G AND EA G-5730-T0383252 P1 TITLE:WING-PLASDR FDEA202505010697Skin · crackedOPEN HOLE HFEC INSPECTION OF #5 HOLE AT LH WING UPPER SKIN WBL262 AND FOUND 01EA CRACK AS MARKED. LH WING UPPER SKIN WBL 262 #5 HOLE CRACKED AREA REPAIRED AS PER B777 SRM 51-40-05-0G, SRM51-40-02-0G, SRM51-40-04-0G AND EA G-5730-T0383251 P1, TITLE:WING - PSDR FDEA202412041774None · noneCREW WAS NOTIFIED ENROUTE THAT PER MEL RESTRICTION THE AFT BELLY POSITION A3L WAS LOADED 736 POUNDS OVER THE MEL RESTRICTION. LOWER DECK CARGO RESTRAINING SYSTEM INSPECTION. ACCOMPLISHED IAW AMM 25-58-00-6 REV 101.5. THE CARGO GUIDES AND RESTRAINTS ARE INSSDR FDEA202210072506Doubler · misrepairedDURING PERFORMING EO G-5710-E0365655 B P8 STEP8.C.(5), FOUND 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 RHS TOO CLOSE TO EDGE OF MACHINED STEP OF DOUBLER P/N : 143W2314Y406, AND WILL RESULT IN KNIFE EDGE WITH MACHINED STEP ON AFT EDGE SDR FDEA2022101172505Doubler · misrepairedDURING PERFORMING EO G-5710-E0365655 B P7 STEP8.C.(5), FOUND 01EA ZLJ-8 COUNTERSUNK FASTENER AT STA 998 S35L TOO CLOSE TO EDGE OF MACHINED STEP OF DOUBLER P/N 143W2314Y405, AND WILL RESULT IN KNIFE EDGE WITH MACHINED STEP ON AFT EDGE OF COUNTERSUNK HOLE.SDR FDEA202210032455Skin · dentedRHW T/E O/B FLAP MIDDLE LOWER SURFACE FOUND 1EA DENT AT 310" TO O/B CROSS 10" TO T/E. RHW T/E O/B FLAP MIDDLE LOWER SURFACE AT 310" TO O/B CROSS 10" TO T/E REPAIRED AS PER B777 SRM 57-53-01-2R REPAIR 2 AND SRM 51-70-04-2R REPAIR 1,REV 41.0. THE B777 SRM 5SDR FDEA202210032454Skin · dentedLH WING O/B FLAP LOWER SURFACE FROM O/B TO I/B 39" CROSS AFT TO FWD 6" AREA FOUND DENTED. LH WING O/B FLAP LOWER SURFACE FROM O/B TO I/B 39" CROSS AFT TO FWD 6"AREA REPAIRED AS PER B777 SRM 57-53-01-2R REPAIR 2 AND SRM 51-70-04-2R REPAIR1,REV 41.0. THE B777SDR FDEA202210022450Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242LF(P/N:152W8452-20) AT STA1413/RBL38.5-40 FOUND CRACK. REPAIRED MAIN DECK CARGO FLOOR PANEL 242LF(P/N:152W8452-20) AT STA1413/RBL38.5-40 CRACK AS PER B777 SRM 53-00-50-2R REPAIR 1, REV41.0. REPAIR CLASSIFIED AS MAJOR PER GMSDR FDEA202210022449Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242PF(P/N:152W8652-6) AT STA1439.5/RBL22-25.5 FOUND CRACK. REPAIRED MAIN DECK CARGO FLOOR PANEL 242PF (P/N:152W8652-6)AT STA 1439.5/RBL22-25.5 CRACK AS PER B777 SRM 53-00-50-2R REPAIR 1, REV41.0. REPAIR CLASSIFIED AS MAJOR PER GMSDR FDEA202210022448Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242QF(P/N:152W8652-4) AT STA1445.5/RBL73-75 FOUND CRACK. REPAIRED MAIN DECK CARGO FLOOR PANEL 242QF(P/N:152W8652-4) AT STA1445.5/RBL73-75 CRACK AS PER B777 SRM 53-00-50-2R REPAIR 1, REV41.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6SDR FDEA202210022447Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241PF(P/N:152W8452-19) AT STA1388.75/LBL38.5-40 FOUND CRACK. REPAIRED MAIN DECK CARGO FLOOR PANEL 241PF(P/N:152W8452-19) AT STA1388.75/LBL38.5-40 CRACK AS PER B777 SRM 53-00-50-2R REPAIR 1, REV41.0. REPAIR CLASSIFIED AS MAJOR PERSDR FDEA202210022446Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241QF(P/N:152W8452-21) AT STA1383.5/LBL43.75-45.5 FOUND CRACK. REPAIRED MAIN DECK CARGO FLOOR PANEL 241QF(P/N:152W8452-21) AT STA1383.5/LBL43.75-45.5 CRACK AS PER B777 SRM 53-00-50-2R REPAIR 1, REV41.0. REPAIR CLASSIFIED AS MAJOR SDR FDEA202210022445Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8452-18) AT STA1255-1256.25/RBL87.5 FOUND CRACK. REPAIRED MAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8452-18) AT STA1255 -1256.25/RBL87.5 CRACK AS PER B777 SRM 53-00-50-2R REPAIR 1, REV41.0. REPAIR CLASSIFIED AS MAJOSDR FDEA202210022444Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241UF(P/N:152W8652-3) AT STA1446/LBL57-57.5 FOUND CRACK. REPAIRED MAIN DECK CARGO FLOOR PANEL 241UF(P/N:152W8652-3) AT STA1446/LBL57-57.5 CRACK AS PER B777 SRM 53-00-50-2R REPAIR 1, REV41.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-SDR FDEA202209032157Pump · failedHYDRAULIC QUANTITY CENTER LOW NNC FOLLOWED BY RESERVE BRAKES STRG NNC. BOTH ECL CHECKLISTS RUN, SLOW LOSS OF CENTER HYDRAULIC QUANTITY UNTIL TOUCHDOWN. NORMAL EXTENSION OF GEAR AND FLAPS. LANDED STRAIGHT AHEAD AND AIRCRAFT TOWED IN. CENTER HYDRAULIC QUANTSDR FDEA202209022146Pump · leakingPDIS 890 29-02 0368 02SEP22 KIX HYDRAULIC QUANTITY CENTER LOW NNC FOLLOWED BY RESERVE BRAKES STRG NNC. BOTH ECL CHECKLISTS RUN, SLOW LOSS OF CENTER HYDRAULIC QUANTITY UNTIL TOUCHDOWN. NORMAL EXTENSION OF GEAR AND FLAPS. LANDED STRAIGHT AHEAD ANSDR FDEA2020061091156Skin · puncturedLT WING NR 5 SPOILER UPPER SURFACE FOUND PUNCTURE DAMAGE AT WS722. LEFT HAND WING NR 5 SPOILER UPPER SURFACE PUNCTURE DAMAGE AT WING STATION 717 TO WING STATION 722. REPAIRED AND SMOOTHENED AS PER SRM 51-70-04 AND EA G-5750-T0354457 PART1. TITLE : WINGS- FLIGHSDR FDEA202006051132Skin · puncturedLT WING NR 5 SPOILER UPPER SURFACE FOUND PUNCTURE DAMAGE AT WS 717. LEFT HAND WING NR 5 SPOILER UPPER SURFACE AT WING STATION 717 TO WING STATION 722. REPAIRED AND SMOOTHENED AS PER SRM 51-70-04 AND EA G-5750-T0354457 PART1. TITLE : WING - FLIGHT SURFACES LT WSDR FDEA202006051131Skin · puncturedLT WING NR 3 SPOILER UPPER SURFACE FOUND PUNCTURE DAMAGE AT WS907. LEFT HAND WING NR 3 SPOILER UPPER SURFACE PUNCTURE DAMAGE AT WING STATION 907. REPAIRED AND SMOOTHENED AS PER SRM 51-70-04 AND EA G-5750-T0354459 PART 1 TITLE : WINGS - FLIGHT SURFACES - LT WINSDR FDEA202005221030Skin · crackedDURING ACCOMPLISHMENT OF MEDIUM FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND WING SLAT NR 5 OUTER SKIN FOUND 01 EACH CRACK. INDICATION AT FASTENER HOLE AT STATION OSCS 713 APPROXIMATELY 0.2" IN LENGTH. LEFT HAND WING SLAT NR 5 OUTER SKIN REPAIRED AS PER SRM SDR FDEA201907041482Cooling Fan · jammedFUMES IN COCKPIT NO CAUTION OR WARNING DISPLAYED FUMES DETECTED BY SMELL-DISIPATED AFTER RIGHT EQUIP COOLING FAN WAS DEACTIVATED. FLIGHT SAFETY REPORT FILED. DEBRIEFED WITH CREW WHEN RIGHT FAN C'B OPENED NO FUMES IN CABIN. CHECK MAT FOUND MX MESSAGE21-14024, SDR FDEA201804281140Slide · low pressureL1 SLIDE RAFT PRESSURE LOW. R/RD L1 SLIDE RAFT PER AMM 25-66-01-4. REMOVED SLIDE RAFT.SDR FDEA201702090493Cover · missingCOVER FOR EXIT LIGHT ON LEFT SIDE OF L1 DOOR IS MISSING, INSTALLED A NEW EMERGENCY EXIT LIGHT COVER.SDR FDEA201702090492Cover · missingCOVER FOR THE EXIT LIGHT ON THE LT SIDE OF THE L1 DOOR IS MISSING. INSTALLED THE EXIT SIGN ASSY AND COVER SMP. LIGHT CHECKED OK.SDR FDEA201503050686Handle · out of positionHAD TO OPEN LT WINDOW TO MAKE TURN INTO GATE. WINDOW WILL NOT LOCK CLOSED. FOUND LT WINDOW LOCKING HANDLE IN THE INCORRECT POSITION. OPENED & CLOSED LT WINDOW SEVERAL TIMES ON GND, LT WINDOW CHECKS GOOD IAW MM CH 56-11-04-4-0. OK FOR SERVICE.SDR FDEA201410042965Girt Bar · out of adjustL1 DOOR WILL NOT ARM. ADJUSTED GIRT BAR, OPS CHECKED GOOD IAW MM 52-11-00-5.SDR FDEA201409122603Spring · missingEMERGENCY LIGHTS SWITCH IS MISSING INTERNAL SPRING CLIP, DOES NOT DISARM OR ARM EMER LIGHTS WHEN COVER IS POSITIONED DOWN OR WHEN SELECTED TO OFF. R & R EMER LIGHTS SWITCH GUARD COVER WITH SPRING CLIP PN 402-122 IAW SMP. PERFORMED EMER LIGHT OPERATIONAL TEST
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