N364FE, cancelled Feb 25, 2004
Service difficulty reports · 24
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 = 'N364FE' AND deregistration_id = 'N364FE-2004-02-25' 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 = 'N364FE' AND deregistration_id = 'N364FE-2004-02-25' 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 03FDEA02175Pressure Switch · failedRECEIVED NR 1 MANIFOLD FAIL ALERT AT FL350. COULD NOT MAINTAIN CABIN PRESSURE. RAN RED TABS AND DIVERTED TO DEN. FOUND LEFT WING PRESSURE SWITCH FAULT BALL NO LEAKS NOTED. PERFORMED DECAY CHECK PER MD-10 MM 36-00-01-5 DECAY CHECK WITHIN LIMITS. REMOVED ANSDR 03FDEA00822Bulkhead · crackedCOMPLY WITH E.A.8-5310-70387. FUSELAGE-MAINFRAME-REPAIR OF STA 1987 BULKHEAD P/N AJC7066-1. CLOSING ACTION ON 05-27-03 ON N/R C00019. COMPLIED WITH E.A.8-5310-70387.SDR 03FDEA00800Rib · crackedNR 855 NR 3 ENGINE RTCORE COWL FWD RIB CRACKED AT UPPER L/E RADIUS. CLOSING ACTION ON 05/24/03. REMOVED FASTENERS FOR ACCESS IAW SRM 51-31-01. WELLED CRACK ON MAE TRAVELER T2/336399 IAW SRM 54-31-01. REINSTALLED FASTNERS IAW SRM 51-35-01, PAINTED TEFLOSDR 03FDEA00801Control Valve · failedN 860 #2 O/B T/R FAILS TO AUTO-RESTOW CHECK. CLOSING ACTION ON 05/24/03. REMOVED AND REPLACED DIRECTI0NAL CONTROL VALVE IAW M/M 78-31-11-2, LEAK TO BE ACCOMPLISHED ON W/C 78X3501CMR.SDR 03FDEA00802Skin · crackedNR S 17 COMPLY WITH E.A.8-5710-70392.WINGS-RT-FIXED LEADING EDGE BEADED DOUBLER REPAIR ACB 1242. CLOSING ACTION ON 05/23/03. COMPLIED WITH E.A.8-5710-70392.SDR 03FDEA00803Clip · damagedAFT FUSELAGE PENTHOUSE CANTED FRAME AT Y=2029.88. HAS REPAIRS, SHOULD BE REPLACED PER E.O.8-5310-7-5000.PT 1. CLOSING ACTION ON 02/22/03. REMOVED AND REPLACED CLIP IAW E.O.8-5310-7-5000.PT1 AND SRM 51-31/01.SDR 03FDEA00804Rub Strip · crackedLT PATIO DOOR UPPER STAINLESS STRIP CRACKED AND CRUSHED. CLOSING ACTION ON 05/24/03. REMOVED CLOSEOUT STRIP IAW SRM 51-31-01.FAB NEW RUB STRIP ON TRAVLER T2/33374, LOCATED AND DRILLED NEW PART IAW SRM 51-31-01.INSTALLED RUB STRIP IAW SRM 51-31-01SDR 03FDEA00781Hinge · corrodedS 16 COMPLY WITH E.A.8-5740-70384. WINGS INBD FLAP OUTBD HINGE SUPPORT FITTING TO WING ATTACH HOLES REWORK. CLOSING ACTION ON 05/19/03. COMPLIED WITH E.A.8-5740-70384.SDR 03FDEA00760Hinge · corrodedS 14 C/W E.A.8-5740-70390. WINGS-RT INBD FLAP HINGE ASSY CORROSION REWORK. CLOSING ACTION ON 05/17/03. COMPLIED WITH E.A.8-5740-70390.WINGS R/H INBD FLAP HINGE ASSY CORROSION REWORK.SDR 03FDEA00726Door Frame · crackedNR 200 RT PATIO DOOR NR 10 FRAME CRACKED AS MARKED. STOPPED DRILL CRACK IAW MD-10 SRM 53-30-00. FAB ANGLE REPAIR IAW MAE TRAVLER T2/333232. LOCATED AND DRILLED ANGLE IAW MD-10 SRM 53-30-00, INSTALLED ANGLE REPAIR IAW SRM 51-31-01, 51-33-01.SDR 03FDEA0163Proximity Switch · inoperativeWHEN GEARS WERE LOWERED, ALL 3 GEAR INDICATED UNSAFE ON MAIN GEAR INDICATORS AND CONFIGURATION PAGE. NO ABNORMAL YAW OR NOISE. RECYCLED GEAR AND GOT 3 GOOD DOWN INDICATIONS. REMOVED AND REPLACED PROXIMITY SWITCH ELECTRONICS UNIT IN REF TO MD1 0-10 M/M 31-71SDR 02FDEA00210Detector · inoperativeON CLIMBOUT NR 2 MANIFOLD FAIL ILLUM'D. NR 2 MANIFOLD FAIL DET LOOP INOP, DO NOT PRESS PNEU SYS NR 2 EXCEPT FOR ENG START.SDR 01FDEA00954Skin · crackedLEFT HAND INBOARD FLAP OUTER SKIN HAS .5 INCH CRACK. REMOVED AND REPLACED SKIN PER SRM 57-00-01.SDR 01FDEA00953Vane · gougedLEFT HAND OUTBOARD FLAP VANE HAS GOUGE. REMOVED AND REPLACED FLAP PER SRM 51-71-00.SDR 01FDEA00887Attach Angle · crackedIN CTR CARGO AT BS 1521 BILGE AREA BETWEEN LONGERONS R44 & R46 CRACK IN BULKHEAD ATTACH ANGLE. REMOVED AND REPLACED TEE CHORD PER SRM & AEA0453-1 & SRM 51-39-01.SDR 01FDEA00884Splice · crackedCTR CARGO BILGE AREA LEFT LONGERON 46 BETWEEN BS 1744 & 1761 LONGERON SPLICE CRACKED. REMOVED AND REPLACED SPLICE PER SRM 51-21-01, 51-35-01.SDR 01FDEA00885Splice · crackedCTR CARGO BILGE AREA L47 BETWEEN BS 1741 & 1761 LONGERON SPLICE CRACKED. REMOVED AND REPLACED SPLICE PER SRM 51-23-01, 51-00-00.SDR 01FDEA00886Splice · crackedIN CTR CARGO BILGE AREA BETWEEN BS 1701 & 1721 CRACK ON LONGERON SPLICE 51L. REMOVED AND REPLACED LONGERON SPLICE PER SRM 51-23-01 & 51-00-00.SDR 01FDEA00871Aileron · corrodedSIX SEPARATE AREAS ON RT OUTBOARD AILERON LWR CORRODED. REMOVED AND REPLACED AILERON PER IAW AMM 27-10-02-4.SDR 2000ZZZX652Web · crackedDURING MAINTENANCE, 3.0 INCH CRACK WAS FOUND ON RIGHT/CENTER WHEELWELL WEB. CRACK AFFECTED UPPER SPLICE WEB, P/N AEA0161-1, RT SIDE, AND AEA0501-1. (X)SDR 99FDEA00304Bolt · corrodedN2764, DURING A/C P-F CONV AT AERONAVALI, A SUSPECTED BOLT FAILURE WAS FOUND AT STA Y=275 FOR ATTACH P/N ABA7003-2, ABA7023-1, NBA6044-15 AND ABA7171. REPAIR WAS ACCOMPLISHED IAW EA NR 8-5311-44057 AND IT WAS APPROVED PER FEDEX 8110-3 DATED 29 APR 99. THE APSDR 99FDEA00305Spar · crackedN2420 - DURING A/C PF CONVERSION AT AERONAVALI AND ACCOMPLISHMENT OF DAC SB 55-17, R3, AD 88-03-08, A CRACK WAS FOUND ON THE HORIZONTAL STAB. REPAIR ATTEMPS TO REMOVE CRACK DAMAGE BY LOCAL BLENDING AND PERF HFEC TO QUAN DAMAGE. B/P EQUIVALENT BOLT IS REINSTASDR 99FDEA00307Web · crackedN0527 - DURING AC P-F CONV AT AERONAVALI, A CRACK 0.87 IN LONG WAS FOUND ON WEB OF UPPER TORQUE BOX PLANE AT Y=2017 AND RBL = 20. SRM 53-00-01, FIG 4 SHEET 2 WEB REPAIR COULD NOT BE ACCOMPLISHED. REPAIR TO STOP DRILL CRACK AND VERIFY CONTAINMENT. THEN INSTSDR 99FDEA00306Doubler · corrodedN0235 - DURING A/C P-F CONV AT AERONAVALI, CORROSION WAS FOUND ON LT UPPER WING AND MLG DOUBLER, TYPICAL PER DC10 SRM 57-00-01, FIG 8. THE AMOUNT OF DAMAGE FOUND ON PN ARB0866-1 IS NOT COVERED BY SRM. REPAIR REMOVES ALL CORROSION BY CUTTING OUT DAMAGE AND TH
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