N14534
Service difficulty reports not matched to an aircraft · 71
They name N14534, 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 = 'N14534' 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 = 'N14534' 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 L1GA200000315Retainer · missingNR 2 MLG BOLT RETAINER MISSING .25 INCH X 1 INCH PIECE.SDR L1GA20000313Jackscrew · nickedDURING INSPECTION OF THE HORZ STAB ACTUATOR JACKSCREW FOUND NICKS AND SCRATCHES IN THE GROOVES. REMOVED AND REPLACED JACKSCREW.SDR L1GA200000310Doubler · corrodedLEFT WING MAIN LANDING GEAR DOUBLER ON THE UPPER SURFACE OF THE WING HAD EXFOLIATION AND DELAMINATION NOTED.SDR L1GA200000246Web · crackedA 6 INCH CRACK AT FS 218 BL 55RT-CUSP MEMBRANE. FABRICATED AND INSTALLED REPAIR WEB AND DOUBLERS.SDR L1GA200000181Altimeter · stuckON FLIGHT 4, CAPT ALTIMETER STUCK AT 100 FT AND BOTH MODE C NOT ENCODING. R2 CAPT ADC, RETURNED TO SERVICE.SDR L1GA200000064Skin · corrodedLEVEL 2 CORROSION LWR SKIN OF RT WING T/E WEDGE.SDR L1GA200000063Web · crackedCRACK CTR WEB OF TOP RT PYLON.SDR L1GA200000062Attach Fitting · corrodedLEVEL 2 CORROSION RT MLG FITTING AFT FACE OF FIXED BRACE BOLT HOLE.SDR L1GA200000061Attach Fitting · corrodedLEVEL 2 CORROSION LT MLG FIXED BRACE BUSHING ATTACH LUG AT THE MLG ATTACH FITTING.SDR LG1A200000126Helicoil · strippedFLT NR 1 DEP FROM IAD & DIVERTED TO MEM (OIL LOSS NR 1 ENG/DOWN 7 QUARTS ON LANDING) ENGINE WAS STILL OPERATING/NORMAL LANDING. HELICOILS BACKING OUT OF GEARBOX FOR MAIN OIL SUPPLY LINE.SDR L1GA200000060Intercostal · crackedCRACKED INTERCOSTAL FS 580 BETWEEN L27L AND L28L.SDR L1GA200000058Floorbeam · corrodedLEVEL 2 CORROSION FLOORBEAM UPPER SURFACE FS 980 BL 40L.SDR L1GA200000057Floorbeam · corrodedLEVEL 2 CORROSION LWR FLOORBEAM FLANGE FS 980 BL 45L.SDR L1GA200000056Cargo Track · corrodedLEVEL 2 CORROSION LT FWD CARGO FLOOR TRACK.SDR L1GA200000055Seat Track · corrodedLEVEL 2 CORROSION RT FWD CARGO FLOOR TRACK.SDR L1GA200000054Seat Track · crackedFWD PIT FLOOR RAIL CRACKED AND CORRODED.SDR L1GA200000053Floorbeam · corrodedLEVEL 2 CORROSION FLOORBEAM FS 980 UNDER LT LAV.SDR L1GA200000052Frame · crackedCRACK - L5L FS 522.SDR L1GA200000051Structure · crackedCRACK - FWD EDGE OF AFT CARGO DOOR.SDR L1GA200000050Floorboard · corrodedLEVEL 2 CORROSION RT OUTBD CO-PILOT SEAT FLOOR PANEL.SDR L1GA200000049Longeron · crackedCRACK L2R FS 427.SDR L1GA200000048Fuel Heater · crackedFUEL HTR S/O VLV EXTERIOR FIBERGLASS COATING CRACKED.SDR L1GA200000047Support Bracket · corrodedLEVEL 2 CORROSION AND CRACK CEILING SUPPORT UNDER LT LAV.SDR L1GA200000046Floorbeam · corrodedLEVEL 2 CORROSION FLOORBEAM UPPER SURFACE FS 980 BL 30L - BL 40L.SDR L1GA200000045Attach Fitting · corrodedLEVEL 2 CORROSION ATTACH FITTING FS 980 AND L18L.SDR L1GA200000044Longeron · elongatedLONGERON 22R ATTACH HOLE DAMAGED AT FS 980.SDR L1GA200000043Nut Plate · brokenFOWARD ENTRY DOOR SLIDE GIRT DOOR BAR LATCH ANCHOR NUT WAS FOUND SPINNING.SDR L1GA200000065Skin · dentedAFT EDGE OF REAR CARGO DOOR DENTED BEYOND LIMITS.SDR L1GA200000059Door · dentedFWD EDGE OF AFT BAGGAGE BIN DOOR DENTED BEYOND LIMITS.SDR L1GA200000304Skin · corrodedRIGHT WING T/E WEDGE CORRODED INSIDE 4 X 6 INCHES.SDR L1GA200000308Brace · corrodedRIGHT MLG SIDE BRACE CORRODED 3 X 5 INCHES AND BOLT HOLE ELONGATED.SDR L1GA200000306Door Frame · corrodedFWD CARGO DOOR FWD DOOR JAMB CORRODED 3 X 4 INCHES.SDR L1GA200000307Floor Support · corrodedFWD CARGO COMPARTMENT FLOOR RAIL CORRODED.SDR L1GA200000309Floor Support · corrodedAFT CARGO COMPARTMENT SHORT RAIL CORRODED 1 X 12 INCHES.SDR L1GA200000305Cargo Track · corrodedAFT CARGO COMPARTMENT RT FLOOR TRACK CORRODED 1 X 24 INCHES.SDR L1GA200000303Floor Support · corrodedAFT CARGO COMPARTMENT LT FLOOR RAIL CORRODED 1 X 12 INCHES.SDR CALA9802004Megaphone · inopINSPECTION FOUND FORWARD MEGAPHONE INOPERATIVE. THE MEGAPHONE WAS REPLACED.SDR CALA9801600Position Switch · inoperativeTHE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED ON APPROACH TO IAH. QRH PROCEDURE WAS FOLLOWED, BUT GREEN LIGHT STILL DID NOT ILLUMINATE. THE NOSE GEAR WAS VISUALLY CONFIRMED DOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE NLG DOWNLOCSDR CALA9801415Cables · out of adjustTHE FORCE REQUIRED TO DROP TAILCONE USING INTERIOR HANDLE WAS EXCESSIVE AT 45 POUNDS. THE FORCE REQUIRED USING EXTERIOR HANDLE WAS LOW AT 15 POUNDS. THE TAILCONE CABLES WERE ADJUSTED IAW MM 53-50-3.SDR CALA9801385Skin · crackedINSPECTION FOUND A .75 INCH CRACK IN FUSELAGE SKIN AT STA 1087, LONGERON 2L. REPAIRED IAW SRM 53-04, FIGURE 27.SDR CALA9801375Angle · crackedINSPECTION FOUND A .75 INCH CRACK IN FUSELAGE ATTACH ANGLE AT STA 1059, LONGERON 15R. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-01, FIGURE 2.SDR CALA9801374Skin · crackedINSPECTION FOUND TWO .5 INCH CRACKS AT FASTENERS IN LEFT FUSELAGE SKIN AT STA 1019 ABOVE PYLON. THE AREA WAS REPAIRED IAW SRM 53-04, FIGURE 27.SDR CALA9801373Longeron · crackedINSPECTION FOUND A .5 INCH CRACK IN LONGERON 2R AT STA 1068. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIGURE 8.SDR CALA9801372Skin · wornINSPECTION FOUND FUSELAGE SKIN HAD ELONGATED HOLES AT LT VERTICAL FIN ATTACH ANGLE AREA. ALL HOLES WERE REAMED, FILLER WAS FABRICATED AND INSTALLED, AND EDDY CURRENT WAS PERFORMED IAW ECRA 5330-02692.SDR CALA9801371Torsion Bar · corrodedINSPECTION FOUND RT WING INBOARD TORSION BAR CORRODED. THE TORSION BAR WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 27-61-6.SDR CALA9801368Floorbeam · corrodedINSPECTION FOUND CORROSION AROUND FLOORBEAM NUT PLATES AT RT AFT LAV, STA 980, APPROXIMATELY 18 INCHES FROM RT SIDE OF FUSELAGE. THE FLOORBEAM WAS REPAIRED IAW SRM 53-05, FIGURE 20A.SDR CALA9801360Clip · crackedINSPECTION FOUND A 2 INCH CRACK IN CLIP AT STA 1109, LONGERON 2R. THE CLIP WAS REPLACED IAW SRM 51-60-0.SDR CALA9801351Bulkhead Tee · crackedINSPECTION FOUND A .5 INCH CRACK IN AFT PRESSURE BULKHEAD TEE CAP AT RT LAV BETWEEN LONGERON 15R AND 16R, STA 996. THE TEE CAP WAS REPLACED IAW SRM 53-03, FIGURE 37A.SDR CALA9801350Pan · crackedINSPECTION FOUND A .5 INCH CRACK AT UPPER RADIUS OF MAIN CABIN DOOR PAN UPPER HINGE CUTOUT. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 52-05, FIGURE 33.SDR CALA9801349Bulkhead Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN RT LAV ANGLE, LOWER SIDE OF Z-63 FROM END FASTENER AT AFT PRESSURE BULKHEAD. THE ANGLE WAS REPAIRED IAW SRM 51-30-5.
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