N466AW
Service difficulty reports · 169
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 = 'N466AW' 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 = 'N466AW' 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 A6WA201309034M151Floor Support · crackedCARGO FLOOR LANDING PLATE ATTACH ANGLE IS CRACKED. R & R ANGLE.SDR A6WA201309034147Threshold · corrodedSERVICE DOOR THRESHOLD IS CORRODED. REMOVED CORROSION ON SERVICE DOOR THRESHOLD DAMAGE FOUND TO BE OUT OF LIMITS AND LOCATED AND DRILLED SERVICEABLE SERVICE DOOR THRESHOLD IAW SRM 51-21-06, TR 53-27, 51-40-11, 51-42-06 AND 51-25-16.SDR A6WA201309024159Trunnion · damagedDURING COLD WORKING PROCESS, FOUND FOUR OVERSIZED HOLES, TWO ON LT & TWO ON RT LOWER MLG TRUNNION FLANGES. REPAIRED OVERSIZED HOLES IAW REO 601R-57-21-1993, REV.SDR A6WA201309024M153Angle · crackedRT OTBD FS 484 ANGLE CRACKED. REMOVED CRACKED ANGLE AND REPLACED WITH SERVICEABLE.SDR A6WA201309024152Angle · crackedLEFT INBD FS 484 ANGLE HAD .2500" CRACK. REPLACED LEFT INBD FS 484 ANGLE.SDR A6WA201309014144Skin · crackedLOW PRESSURE ACFT DOOR CUT OUT STRUCTURE IS SEPARATED AND CRACKED ON FWD AND AFT EDGES. RETURNED FWD LAND TO ORIGINAL CONTOUR IAW SRM 51-24-16 AND R & R AFT LAND IAW SRM 51-42-06, 51-42-16.SDR A6WA201307084023Ballast · failedSTRONG BURNING ODOR IN CABIN NEAR ROW 3. R & R LIGHT BALLAST ABOVE BIN 5/6 FD IAW AMM 33-10. RESEALED ALL BIN ACCESS DOORS PER AMM SUP 13-018A.SDR A6WA201303224017Heater · inoperativeSTRONG ELECTRICAL ODOR DURING FLIGHT NO SMOKE OR OTHER ABNORMALITIES NOTED WITHIN COCKPIT-SMELL ISOLATED TO COCKPIT. T/S AND FOUND GALLEY HTR SYS CAUSING BURNING SMELL. REMOVED AND REPLACED NR 1 GALLEY HEATER BLOWER IAW AMM 21-23-05, OPS CHECK GOOD.SDR A6WA201140879Lug · crackedRT OTBD FLAP HINGE ARM (WS220) AFT LUG IS GOUGED AND MARRED. REPAIRED RT OTBD FLAP HINGE ARM IAW REO 601R-57-53-896 WORKED PERFORMED.SDR A6WA201140881Retainer · corrodedCORRODED MAIN AVIONICS BAY DOOR SEAL RETAINERS. R & R 4EC DOOR SEAL RETAINERS PN CC670-38662-5, CC670-38675-3, CC670-38663-5, CC670-38674-3.SDR A6WA201140871Angle · damagedFS 559 LOWER CAP ANGLE LEFT HAS SEVERAL DOUBLE AND ELONGATED HOLES THRU SKIN AND ANGLE. REPAIRED IAW REO 601R-53-41-1475.SDR A6WA201140875Skin · bentRIGHT ENGINE TAIL PIPE FAIRING CUT OUT FOR ACCESS PANEL 446BB IS BENT AND GOUGED. REPAIRED RT ENGINE TAIL PIPE IAW CMM 78-11-00, REPAIR SRS 062.SDR A6WA201140873Fitting · crackedPILOT SIDE WINDOW POST AFT LOWER FITTING CRACKED IN RADIUS. R & R WITH SERVICEABLE FITTING.SDR A6WA201140878Shroud · crackedRIGHT OTBD L/E INNER SHROUD IS CRACKED. REMOVED DAMAGED AREA AND REPAIRED IAW REO 601R-57-41-773 AND SRM 51-24-36.SDR A6WA201140876Lug · chafedLEFT THRUST REVERSER OTBD LOWER TRACK LUG CHAFED, BLENDED DISCREPANT AREA IAW SRM 51-21-06 AND COMPLIED WITH REO 601R-78-34-2435.SDR A6WA201140874Floorbeam · crackedFS280, RBL 9, OTBD CLIP CRACKED. REMOVED UNSERVICEABLE CLIP AT FS 280, LBL 9 OTBD IAW SRM 51-42-21. FABRICATED CLIP IAW SRM.SDR A6WA201140882Plate · wornPAX DOOR FWD AND AFT CENTERING PLATES ARE WORN. REPAIRED PAX DOOR FWD AND AFT CENTERING PLATES IAW REO 601R-52-11-296.SDR A6WA201140883Drag Angle · crackedPAX DOOR FIXED STAIRS AFT DRAG ANGLE IS CRACKED. REPAIRED PAX DOOR FIXED STAIRS AFT DRAG ANGLE IAW REO 601R-52-11-513.SDR A6WA201140872Floor Support · crackedFS484 FLOOR SUPPORT CLIP CRACKED AT RBL36. REMOVED DAMAGED 484 CLIP AND INSTALLED SERVICEABLE 484 FLOOR SUPPORT CLIP IAW REO 601R-53-11-059.SDR A6WA201140877Bracket · chafedLEFT STUB FAIRING BRACKET CHAFED/ PN 601R10371-1. REMOVED UNSERVICEABLE LT STUB FAIRING BRACKET AND INSTALLED SERVICEABLE STUB FAIRING BRACKET IAW SRM 51-47-21.SDR A6WA201140880Bracket · crackedBRACKET FOR HYDRAULIC LINES CRACKED IN RT WHEEL WELL, REMOVED AND REPLACED.SDR A6WA201140870Bracket · crackedCARGO DOOR FWD TRACK LOWER MOUNT BRACKET CRACKED. REMOVED CHANNEL IAW SRM 51-42-06. FAB CHANNEL IAW SRM 53-61-23, INSTALLED IAW SRM 51-42-06, 51-41-04.SDR A6WA201140783Bracket · crackedBRACKET FOR HYD LINES (PRESSURE NR 2) CRACKED IN LT WHEEL WELL. REMOVED UNSERVICEABLE BRACKET 601R75262-159 IAW SRM 51-42-06. REPLACED 601R75262-159 SERVICEABLE BRACKET IAW 51-41-11 SRM.SDR A6WA201140782Angle · crackedOBLIQUE ANGLES CRACKED ON APB AFT SIDE. COMPLIED WITH REO 601R-53-61-100 AND REO 601R-53-61-422 TO REMOVE UNSERVICEABLE LT AND RT OBLIQUE ANGLES AND REPLACE WITH SERVICEABLE LT AND RT OBLIQUE ANGLES PN 601-35012-51/52.SDR A6WA201140063Gcu · malfunctionedAC1 AUTOTRANSFER AND AC2 AUTOTRANSFER CAUTION MSG`S ON GROUND. WILL NOT ACCEPT EXT AC PWR. WILL NOT ACCEPT GEN PWR. MAIN GEN`S WON`T SUPPLY OPPOSITE SIDE. R & R GCU NR 3 IAW AMM 24-11-07. PERFORMED OPS CHECK IAW 24-22-01. OPS CK GOOD AT THIS TIME.SDR A6WA201040311Rudder Pedal · stiffRUDDER PEDALS WERE STIFF AND EXTRA SENSITIVE ON TAKEOFF ROLL ON F/O`S SIDE. C/W VISUAL INSP OF VISIBLE CABLES AND PULLEYS C/W OP CK OF RUDDER CONTROL SYS REF AMM 27-21-00, OPS CK GOOD AT THIS TIME. C/W HI SPEED TAXI CHECK, NO FAULTS DEFECTS NOTED.SDR A6WA201040313Trim Panel · malfunctionedACFT ROLLED TO RT ON APPROACH AND FELT SPRING LIKE, FLAPS AT 45 DEGREES, GOT AILERON TRIM WITH AUTOPILOT ON. DURING OPS CK OF AILERON TRIM, CAN`T TRIM ACFT LEFT WING DOWN. R & R AILERON TRIM PANEL IAW 21-12-10, OPS CK GOOD. C/W OPS CK OF AUTO PILOT AILERON SDR A6WA200940483Bulkhead · crackedAFT PRESSURE BULKHEAD WEB IS CRACKED ABOVE THE CARGO DOOR TRACK AT FS 621.00, LBL 27.50, WL 130.00, CRACK LENGTH IS .250 INCH REO 601R-53-61-1541 PERFORMED. (K)SDR A6WA200940482Bushing · corrodedON LT WING, FLAP HINGE BOX LOCATED AT WS 220.00 FOUND CORRODED INBD OA FLAP ATTACHMENT FITTING, ON THE SIDE OF THE STAINLESS BUSHING. REO 601R-57-21-1144 PERFORMED. (K)SDR A6WA200940478Floorbeam · crackedUNDER FLOOR AT FS 484.00, LBL 36 CLIP CRACKED. CLIP UNDER FLOOR AT FS 484.00, LBL 36 REPLACED IAW SRM 51-42-21. (K)SDR A6WA200940491Skin · dentedSKIN DENTED ON LT INNER FLAP AS REQUIRED. UNDERSIDE SKIN OF LT INNER FLAP REPAIRED IAW REO 601R-57-52-1483. (K)SDR A6WA200940476Attach Fitting · crackedUNDER FLOOR AT FS 484.00, RBL 27 CLIP CRACKED. UNDER FLOOR AT FS 484.00, RBL 27 CLIP REPLACED IAW SRM 51-42-06 AND SRM 51-42-20, ALODINED, PRIMED AND PAINTED IAW SRM 51-21-16. (K)SDR A6WA200940510Bulkhead · crackedAFT PRESSURE BULKHEAD (FS 621) CRACK AT LINTEL FITTING LOCATION, CRACK LENGTH .500 INCH. AFT PRESSURE BULKHEAD AT FS 621 REPAIRED IAW REO 601R-53-61-1230, REV D.SDR A6WA200940490Bracket · crackedLINTEL BRACKET (AFT FS 621 BULKHEAD), UPPER BRACKET CRACKED. LINTEL BRACKET REPLACED IAW SRM 51-42-06. (K)SDR A6WA200940479Support Bracket · crackedLT ENGINE UPPER PYLON TRACK SUPPORT BRACKET IS CRACKED. LT ENG T/R UPPER PYLON TRACK SUPPORT BRACKET REPLACED IAW SRM 51-42-06. (K)SDR A6WA200940485Angle · crackedUPPER AFT ANGLE AT FS 280. LBL 11.00, WL 72.00 IS CRACKED. CRACK LENGTH IS .500 INCH. UPPER AFT ANGLE AT FS 280, LBL 11, WL 72.00 REPAIRED IAW REO 601R-53-11-138-NC.SDR A6WA200940487Pressure Blkhd · crackedCRACK FOUND ON PRESSURE BULKHEAD AT FS 202.75, LBL 23.71 AT PARKING BRAKE LOCATION. CRACK LENGTH .50 INCH CRACK ON PRESSURE BULKHEAD AT FS 202.75, LBL 23.71 AT PARKING BRAKE LOCATION, REPAIRED IAW REO 601R-53-11-563. (K)SDR A6WA200940488Attach Fitting · crackedCLIPS AT FS 280.00, LBL 9.0, WL 72.00 IS CRACKED. CRACKED LENGTH IS .500 INCHES. CLIP REPLACED AT FS 280, LBL 9, WL 72, IAW SRM 51-42-06 AND 51-42-21. (K)SDR A6WA200940481Sill · crackedCARGO DOOR FLOOR SILL CRACKED AT FS 589.00. AT CARGO DOOR FLOOR SILL (FS 589.00) CUTOUT PERFORMED IAW REO 601R-61-433. (K)SDR A6WA200940480Sill · corrodedCARGO DOOR FLOOR SILL CORRODED AROUND NUTPLATES. CORROSION REMOVED ON CARGO FLOOR SILL AROUND NUTPLATES IAW SRM 51-21-00. PROTECTION RESTORED ON CARGO DOOR FLOOR SILL AROUND NUTPLATES IAW SRM 51-21-16.SDR A6WA200940486Attach Fitting · crackedCLIP AT FS 280.00, RBL 9.0, WL 72.00 IS CRACKED. CRACK LENGTH IS .200 INCH. CLIP AT FS 280, RBL 9.0 REPLACED IAW SRM 57-42-06 AND 57-42-21 AT FS 280, WL 72.0, RBL 9.0. (K)SDR A6WA200940489Floorbeam · crackedLOWER ANGLE RADIUS OF CROSSBEAM AT FS 280.00, RBL 9.00, WL 72.00 FOUND CRACKED. REPAIRED IAW REO 601R-11-171, REV D. (K)SDR A6WA200940484Floorbeam · crackedLOWER RADIUS OF CROSSBEAM AT FS 280, LBL 9.00, WL 72.00 CRACKED LOWER RADIUS OF CROSSBEAM AT FS 280.00, LBL 9.00, WL 72.00 REPAIRED IAW REO 601R-53-11-171, REV D. (K)SDR A6WA200940477Attach Fitting · crackedUNDER FLOOR AT FS 484 AND LBL 27 CLIP CRACKED. CLIP AT FS 484, LBL 27. REPLACED IAW SRM 51-42-21. (K)SDR A6WA200940105Carbon Seal · leakingLT OIL PRESS FLUX BETWEEN 28 AND 53 PSI. LT OIL TEMP RUNNING 15 DEG WARMER THAT RT ENG. THEN LT OIL PRESS WARNING MESSAGE ON SHORT FINAL. FOUND LT IDG CARBON SEAL LEAKING. REPLACED LT ENG IDG CARBON SEAL AND MOUNTING RING IAW AMM 72-60-00 AND 05-018A. PERSDR A6WA200940069A/C Pack · smokeAFTER BLEEDS TRANSFERRED TO APU, SMELLED SMOKE IN COCKPIT, TURNED PACKS OFF, SMOKE CLEARED. T/S TO LT PACK PRODUCING SMOKE REF LP 187703/3 FOR MEL. (K)SDR A6WA200840153Door · stiffSERVICE DOOR HARD TO OPEN. LUBED AND OPS CHECKED IAW 52-40-00, OPS CHECK GOOD. (K)SDR A6WA200840012Cooler · vibrationAIRFRAME VIBRATION FELT AF VIBES FELT FROM T/O, TO DESCENT , WENT AWAY ON FINAL APPROACH. FELT IN REAR ON LT SIDE OF THE AC EVIDENT AT ROW 13 BUT NOT EVIDENT IN LAV. REMOVE AND REPLACED HYDRAULIC COOLER REF AMM 29-11-42, OPS CHECK GOOD. (K)SDR A6WA200740708Engine · leakingSMOKE TOILET CAS MESSAGE INFLIGHT, SMOKE VISIBLE COMPLIED WITH QRH. SMOKE SOURCE APPEARED TO BE FROM ACROSS LAV ROW 13, AREA LOWER AREA. (K) AIRCRAFT WAS TROUBLESHOT TO RT ENGINE INTERNAL LEAK. REMOVED AND REPLACED. (VENDOR FINDINGS: CARBON SEAL PRESSURIZATSDR A6WA200740706Unknown · smokeTOILET SMOKE CAS MESSAGE IN FLIGHT, COMPIED WITH QRH SMOKE VISIBLE IN COCKPIT, ELECTRICAL SMOKE ODOR IN LAV, SMOKE SUBSIDED WHEN QRH COMPLIED WITH. CORRECTIVE ACTION IN PROGRESS. (K)
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