N312FL
Service difficulty reports not matched to an aircraft · 35
They name N312FL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N312FL' AND registry_match IS NULL 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 = 'N312FL' AND registry_match IS NULL 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 DU4R108Pan · corrodedRT FLOOR PAN AT BS 1016 WL208.1 CORRODED. S/O 109001, N/R 22825SDR DU4R107Angle · corrodedFWD ENTRY DOOR THRESHOLD HAS CORRODED ANGLE (OB OF INNER CHORD). S/O 109001, N/R 23118.SDR DU4R106Bushing · corrodedLT HORIZONTAL STAB AFT SPAR, UPPER ATTACH LUG, CENTER SECTION, AFT FACE HAS CORROSION AROUND BUSHING. S/O 109001, N/R 22994SDR DU4R05105Bushing · corrodedLT HORIZONTAL STAB FRONT SPAR, UPPER ATTACH BOLT BORE, BUSHINGS HAVE PITTING CORROSION. S/O 109001, N/R 22971.SDR DU4R104Floor Support · corrodedCORROSION AT FLOORBOARD SUPPORT ANGLE FROM BS 949 TO 1000 RBL 68.0. S/O 109001, N/R 22787SDR 103Seat Track · gougedCABIN RT OB SEAT TRACK HAS NUMEROUS GOUGES STA. 540 TO 727E. S/O 109001, N/R 22858SDR 102Seat Track · gougedCABIN LT IB SEAT TRACK HAS NUMEROUS GOUGES STA. 540 TO 727E. S/O 109001, N/R 22850SDR 85Floorbeam · corrodedCORRODED AFT CABIN FLOORBEAM UPPER SKIN FROM BS 987 LBL 48.0.SDR 84Frame · crackedCRACKED FRAME AT BS 294.5, WL 208.1 FWD GALLEY DOOR.SDR 83Crease Beam · corrodedR-1 SERVICE DOOR INNER CHORD CREASE BEAM HAS CORROSION THRU OUT THE BEAM.SDR 82Shear Tie · crackedCABIN UPPER LOBE SHEAR TIE CRACKED AT BS 639 S-4L.SDR 81Frame · crackedLOWER FWD SIDE OF FRAME AT STA 616 S-16R CRACKED AT LOWER FASTENER.SDR 80Skin · gougedAIRCRAFT DAMAGE BELOW AFT PIT FROM BELT LOADER BS 755-790, S-25R. LOG PAGE ITEM NR1 PG. 158526,S/O 109001, N/R 22583.SDR DU4R20050428Floor Support · corrodedCORROSION AT FLOORBOARD ANGLE SUPPORT FROM BS 947 - 1000 LBL 68.SDR 78Skin · dentedDENTS AND GOUGES STA 770 - 827 STR 26 - 27 RT BELOW AFT PIT DOOR.SDR F3LA200400117Proximity Sensor · faultyFLIGHT CREW REPORTED LANDING GEAR WARNING HORN STUCK ON WHEN FULLY CONFIGURED ON FINAL AND WOULD NOT SILENCE UNTIL FLAPS RETURNED TO UP POSITION AFTER LANDING. REPLACED PROXIMITY SENSOR 5853. OPS CHECKED GOOD.SDR F3LA200400066Fire Loop · faultyAIR RETURN, NR 2 ENG OVERHEAT CAUTION LIGHT ILLUM TWICE. DECLARED EMERGENCY, LANDED W/O INCIDENT. ON DESCENT, MASTER CAUTION SYS ILLUM 4 TIMES, NO SIX PACK INDICATION. MX TESTED CAUTION SYS THRU SIMULATION OF CONDITIONS CAUSING ILLUMIN ANNUNCIATORS, ALL SYSSDR F3LA200400064Panel · damagedDURING C-6 CHECK, INSPECTION REPORTED SCREW BROKEN ON NR 1 PYLON TOP AFT FAIRING PANEL ATTACHED TO THE WING AND A CRACK FROM THE HOLE. REPLACED PANEL PER SRM 51-40-02, SRM 51-40-08 AND MM 28-11-00. PERFORMED LEAK CHECK. NO LEAKS NOTED.SDR F3LA200400063Panel · crackedDURING C-6 CHECK, INSPECTION REPORTED RT WING UPPER SURFACE AFT PYLON PANEL CRACKED AT AFT I/B CORNER AT FASTENER COMMON TO FUEL CELL. REPLACED PANEL PER SRM 51-40-02 AND 51-40-65.SDR F3LA200300156Support · brokenDURING WALK-AROUND, FLIGHT CREW REPORTED NR 7 FLAP TRANSMISSION FLAP TRACK FAIRING A-FRAME ATTACH POINTS BROKEN. REPLACED NR 7 FLAP TRACK FAIRING A-FRAME AND SUPPORT STRUTS, ADJUSTED AND TESTED NR 7 FLAP, AND OPS CHECKED GOOD PER MM 27-51-52 AND OHM 57-53-35.SDR F3LA200200198Fmc · faultyAIR TURNBACK. ON CLIMBOUT, THE FLIGHT CREW REPORTED THE ONLY MODE CONTROL WAS N1. NO AUTO-PILOT, NO AUTO THROTTLE OR MODE CONTROL. MAINTENANCE REMOVED AND REPLACED AIR DATA COMPUTER, FMCS AND OPERATIONS CHECK WAS NORMAL.SDR F3LA200200139Channel · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON Z-CHANNEL AFT GALLEY SUPPORTS, STA 1028, BBL 10L AND BBL 10R. REPLACED CORRODED Z-CHANNEL PER EA 53-737-165, SRM 51-20-01, MM 51-21-99, SOPM 20-41-02 AND EA 53-737-171.SDR F3LA200200138Pan · corrodedDURING C-4 CHECK, INSPECTION REPORTED AFT LAV PAN BETWEEN STA 1016 AND THE AFT PRESSURE BULKHEAD HAD THREE CORRODED FASTENERS ON RT SIDE, 16 INCHES FROM CENTER LINE. REMOVED CORRODED AREA ON CABIN FLOOR PAN AND INSTALLED A FILLER AND REPAIR DOUBLER PER EA 57-SDR F3LA200200137Frame · crackedDURING C-4 CHECK, INSPECTION REPORTED FRAME CRACKED AT BS 663.75, STR 1R AND 2R. REMOVED DAMAGE IN FRAME PER SRM 53-00-07 FIG 209. FABRICATED FILLERS AND REPAIRED AND INSTALLED FRAME PER SRM 53-00-07 FIG 209.SDR F3LA200200134Sill · corrodedDURING C-4 CHECK, INSPECTION REPORTED FLOOR ANGLE CORRODED AT L1 ENTRY THRESHOLD, STA 312 TO 344. REMOVED L1 MOP SILL PER SRM 53-10-15. INSTALLED NEW MOP SILL PER SRM 51-40-02 AND 51-10-02.SDR F3LA200200130Panel · corrodedDURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT RT TRANSITION PANEL CORRODED FROM STA 767 TO STA 787. REPLACED TRANSITION PANEL PER SRM 51-40-02 AND 51-30-01.SDR F3LA200200126Strap · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT DOOR FRAME UNDER UPPER FLANGE AT NUT PLATES AT STA 794, STR 25-R. REPLACED CORRODED RADIUS STRAP FROM STR 17R TO 27R PER SRM 51-40-02 AND 51-10-02.SDR F3LA200200125Door Frame · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT DOOR FRAME WEB FROM STR 23-R TO 25-R. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 51-40-02 AND 51-10-02.SDR F3LA200200128Nut Plate · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON NUT PLATES OF FLOORBEAM AT STA 344, LBL 10. REPAIRED DAMAGE PER SRM 53-00-51.SDR F3LA200200129Strap · corrodedDURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOORBOARD TIE DOWN STRAP CORRODED AROUND SCREW HOLES. REPAIRED DAMAGE PER SRM 51-10-2, 51-40-02 AND SOPM 20-41-02.SDR F3LA200200127Panel · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT RT TRANSITION PANEL FROM STA 767 TO 727. FABRICATED AND INSTALLED REPLACEMENT PANEL PER SRM 51-10-02 AND 51-40-02.SDR F3LA200200123Intercostal · crackedDURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL AT STA 344-360, BL 0, CRACKED ON TOP FLANGE FWD END AND HAS DAMAGE ON BOTTOM FLANGE. FABRICATED REPAIR PARTS PER SRM 51-70-11 AND INSTALLED REPAIR PER SRM 51-40-02.SDR F3LA200200124Crossbeam · crackedDURING C-4 CHECK, INSPECTION REPORTED C-1 DOOR LOWER CROSSBEAM WEB CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 51-70-13.SDR F3LA200200121Skin · crackedMAINTENANCE REPORTED SKIN CRACKED AT OUTBOARD END OF NR 6 SLAT. REMOVED DAMAGED AREA AND INSTALLED REPAIR PER SRM 57-43-01 FIG 206 AND SRM 51-40-02.SDR F3LA99122Tire · failedDEN - UPON ARRIVAL IN BOS, FLIGHT CREW REPORTED NR 4 MAIN TIRE RECAP MISSING. TIRE REMAINED INFLATED. MAINTENANCE IN BOS REPLACED NR 4 MAIN TIRE AND WHEEL ASSY AND PERFORMED TEMPORARY REPAIRS NECESSARY TO FERRY AIRCRAFT TO DEN. UPON ARRIVAL IN DEN, MAINTENA
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