N463AW
Service difficulty reports · 190
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 = 'N463AW' 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 = 'N463AW' 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 A6WA201040054Unknown · odorON GROUND AFTER APU START AND BLEED TRANSFER FUEL ODOR FROM PACKS USING APU BLEED AIR PACKS WERE OK, O ENG. INSPECTED APU, NO OBVIOUS FUEL LEAKAGE WITH APU RUNNING, RAN PACKS OFF ENG BLEED AIR, NO ODOR NOTED, COMPLIED WITH CM ACTION, PLACED APU ON MEL.SDR A6WA200940742Pcu · malfunctionedDURING CRUISE FLT RECEIVED UNCOMMANDED FLT SPOILER DEPLOY CAUTION MSG WITH FLT SPOILER HANDLE IN STOWED POSITION. HAD A LIGHT BUFFET ASSOCIATED WITH CAUTION MSG. REF QRH NO FURTHER PILOT ACTION REQUIRED. FLT SPOILER DEPLOY CAUTION MSG APPEARED 3 TIMES. R &SDR A6WA200940735Ecu · malfunctionedDURING CRUISE FLIGHT ACFT ROLLED LT UNCOMMANDED AND A FEW SECONDS LATER RECEIVED FLIGHT SPOILER DEPLOY CAUTION MESSAGE. REF QRH. FLIGHT SPOILER HANDLE WAS FULLY STOWED. CAUTION MESSAGE APPEARED AND DISSAPPEARED SEVERAL TIMES. ALSO RECEIVED INTERMITTENT CASSDR A6WA200940339Bulkhead · gougedPILOTS BULKHEAD WEB IS GOUGED. PILOTS BULKHEAD WEB REPAIRED IAW REO 601R-53-11-1677. (K)SDR A6WA200940345Bulkhead · crackedAFT PRESSURE BULKHEAD WEB IS CRACKED AT FS 621.00, LBL 27.50, WL 130.00, ABOVE THE CARGO DOOR TRACK. AFT PRESSURE BULKHEAD WEB AT FS 621.00, LBL 27.50, WL 130.00. REPAIRED IAW REO 601R-53-61-1541, REB B. (K)SDR A6WA200940347Throttle Cable · fouledREWORK RT AND LT UPPER AND LOWER PYLON TO FUSELAGE FITTINGS IN ORDER TO ELIMINATE LOW EDGE DISTANCE AND FOULING CONDITION WITH THE THROTTLE CABLE. RT AND LT UPPER AND LOWER PYLON TO FUSELAGE FITTINGS TRIMMED IAW SB A601R-53-059, REV F PART C AND MODUSM TC 601SDR A6WA200940337Floorbeam · crackedUPPER FLOOR ANGLE IS CRACKED AT FS 28000, LBL 9.00, WL 73.00. UPPER FLOOR ANGLE AT FS280.00, LBL 9.00, WL 73.00. REPAIRED IAW REO 601R-53-11-138. (K)SDR A6WA200940343Support · crackedCARGO DOOR FWD RAIL LWR SUPPORT CRACKED. CARGO DOOR FWD RAIL LWR SUPPORT CHANNEL REPLACED IAW SRM 51-42-06. (K)SDR A6WA200940335Attach Fitting · crackedCLIP AT FS 484.00, LBL 27.00, WL 72.00 IS CRACKED. CLIP AT FS 484.00, LBL 27.00, WL 72.00. REPLACED IAW SRM 51-42-20. (K)SDR A6WA200940349Floorbeam · crackedFLIGHT COMPARTMENT BULKHEAD CROSSBEAM F/S 280, RBL 9, WL 72.00 CRACKED (CRACK LENGTH .500) FLIGHT COMPARTMENT BULKHEAD CROSSBEAM F/S 280, RBL 9, WL 72.00 REPAIR CARRIED OUT IAW REO 601R-53-11-171, REV D. (K)SDR A6WA200940409Intercostal · crackedINTERCOSTAL AT F/S 484.00, RBL 36.00, WL 72.00 IS CRACKED. (CRACK LENGTH IS .250") INTERCOSTAL AT F/S 484.00, RBL 36.00, WL 72.00 REPAIRED IAW REO 601R-53-41-059, REV A. (K)SDR A6WA200940410Intercostal · crackedINTERCOSTAL AT F/S 484.00, LBL 36.0, WL 72.0 IS CRACKED. CRACK LENGTH IS .450" INTERCOSTAL AT F/S 484.00, LBL 36.0, WL 72.0 REPAIRED IAW REO 601R-53-41-059 REV. A. (K)SDR A6WA200940411Handle · crackedPAX DOOR HANDLE FOUND CRACKED AT 4 PLACES. PAX DOOR HANDLE REPLACED IAW AMM 52-11-03-400-802. (K)SDR A6WA200940336Structure · crackedAPU ENCLOSURE IS CRACKED. APU ENCLOSURE REPAIRED IAW REO 601R-49-11-071. (K)SDR A6WA200940341Panel · crackedPASSENGER DOOR STAIRS FWD STAIRS FWD SIDE PANEL CRACKED IN ZONE NR 2 (REF REO 601R-52-11-702, REV A). PAX DOOR STAIR ASSY FWD PANEL REPAIRED IAW REO 601R-52-11-702, REV A. (K)SDR A6WA200940340Structure · crackedPASSENGER DOOR EDGE MEMBER FOUND CRACKED ON AFT SECTION. PAX DOOR EDGE MEMBER REPAIRED IAW REO 601R-52-11-279. (K)SDR A6WA200940334Attach Fitting · crackedCLIP AT FS 484.00, RBL 27.00, WL 72.00 IS CRACKED. CLIP AT FS 484.00, RBL 27.00, WL 72.00. REPLACED IAW SRM 51-42-06 AND 51-42-20. (K)SDR A6WA200940346Bulkhead · crackedCRACK FOUND ON FWD PRESSURE BULKHEAD FS 202.75, LBL 23.71, CRACK LENGTH IS .500. FWD PRESSURE BULKHEAD REPAIRED IAW REO 601R-53-11-563. (K)SDR A6WA200940342Panel · crackedPASSENGER DOOR STAIRS AFT SIDE PANEL FOUND CRACKED IN ZONE 2 AND ZONE 3 (REF: REO 601R-52-11-702, REV A) PAX DOOR STAIR ASSY AFT SIDE PANEL REPAIRED IAW REO 601R-52-11-702, REV A. (K)SDR A6WA200940338Drag Angle · crackedPASSENGER DOOR STAIR AFT DRAG ANGLE FOUND CRACKED AT PULLEY BRACKET LOCATION. PAX DOOR STAIR ASSY AFT DRAG ANGLE REPAIRED IAW REO 601R-52-11-513 REV A. (K)SDR A6WA200940344Bulkhead · crackedAFT PRESSURE BULKHEAD WEB AT FS 621.00, LBL 45.00, WL 110.00, IS CRACKED AT THE LINTEL INSTALLATION. AFT PRESSURE BULKHEAD AT FS 621.00, LBL 45.00, WL 110.00. REPAIRED IAW REO 601R-53-61-1230, REV D. (K)SDR A6WA200940301Handle · corrodedCREW EMERGENCY HATCH OUT HANDLE CAN`T EJECT. CORROSION FOUND ON OUTER HANDLE SHAFT. CREW EMERGENCY HATCH OUTER HANDLE REPLACED IAW AMM TASK 52-22-03-400-801. (K)SDR A6WA200940123Element · malfunctioned14TH DUCT O/H, C/W QRH RED LENG TO IDLET MSG WENT AWAY AND REAPPEARED 5 MINUTES LATER. LANDING WEIGHT 49,000, BTMS 6-5-5-6. REMOVED AND REPLACED LT PYLON 14TH STAGE LENS ELEMENT A59WK IAW AMM 36-21-04. OPS AND LEAK CHECK NORMAL. (K)SDR A6WA200940121Cooling Fan · failedDISPLAY COOL CAUTION MSG IN FLIGHT, C/W`D QRH, AT FLT LEVEL 270. REMOVED AND REPLACED FAN NR 1 IAW AMM 21-24-19, OPS CHECK GOOD. (K)SDR A6WA200840599Light · malfunctionedSMOKE IN COCKPIT WHEN FO TURNED FLOODLIGHT ON. TURNED OFF FLOODLIGHT AND SMOKE WENT AWAY.SDR A6WA200740638Connector · dirtyINFLIGHT, RT N2 GAUGE READS ZERO APPROXIMATELY 30 MINUTES INTO FLIGHT. CLEANED BLUE HARNESS CONNECTOR W8P2 AT RT ALTERNATOR IAW 73-21-13 AND AWAC SUPP 06-003, OPS CHECK GOOD. (K)SDR A6WA200740356Angle · cracked(2) EA CRACKED ANGLES AT FS 280.0, RBL 9.0. MAINTENANCE REMOVED AND REPLACED ANGLES AT FS 280.00, RBL 9 IAW SRM AND BSC SR 601R-53-0057A. (K)SDR A6WA200740355Angle · cracked2 EA, CRACKED ANGLES AT FS 280, LBL 9.0. MAINTENANCE REMOVED AND REPLACED ANGLES AT FS280, LBL 9 CRJ 200, SRM 51-42-21 AND BSC SR 601R-53-0057A. (K)SDR A6WA200740349Angle · crackedFS 484.0 LT LBL 27.0, WL 71.0 TO 73.5 ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED CRACKED ANGLE AT FS 484.00, LBL 27.0 IAW REO 601R53-41-059. (K)SDR A6WA200740354Floorbeam · crackedLT FLOOR SUPPORT STRUCTURE IS CRACKED AT FS 621.00. MAINTENANCE REPAIRED FLOOR SUPPORT BY CUTTING OUT DAMAGED ANGLE, FABBING REPAIR PARTS AND INSTALLING IAW REO 601R53-61-717, REV C AND BSC EO 601R-53-12256. (K)SDR A6WA200740353Floorbeam · crackedRT FLOOR SUPPORT STRUCTURE IS CRACKED AT FS 621.00. MAINTENANCE REPAIRED RT FS 621 IAW REO 601R53-61-117 REV C. (K)SDR A6WA200740352Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED APROX .7 INCH LONG IN AREA OF PULLEY BRACKET. MAINTENANCE CUT AWAY CRACKED SECTION OF DRAG ANGLE AND INSTALLED REPAIR ANGLE IAW REO 601R52-11-513, REV A. (K)SDR A6WA200740351Intercostal · crackedLT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. MAINTENANCE REMOVED AND REPLACED LT SIDE FS 621.00 TO 625.00 INTERCOSTAL AT STR 14L IAW CRJ 200, SRM 51-42-06. (K)SDR A6WA200740350Intercostal · crackedRT SIDE FS 621.00 TO 625.30 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. MAINTENANCE REMOVED AND REPLACED RT SIDE FS621.00 TO 625..00 INTERCOSTAL AT STR 14 R IAW CRJ 200 SRM 51-42-06. (K)SDR A6WA200720222Warning Message · illuminatedDURING APPROACH SPOILERONS CAUTION AND OUTBOARD GROUND SPOILERS CAUTION MESSAGE ILLUMINATED, COMPLIED WITH QRH, PREFORMED FLAP 20 DEGREES LANDING. PERFORMED FUNCTION TEST OF SPOILER IAW AMM 27-61-00. OPS CHECK GOOD AT THIS TIME. (M)SDR A6WA200540009Skin · dentedDENT ON LT SKIN FROM FS 193, 00 TP FS 202.75 BETWEEN STR 18L AND STR 20L. REPAIRED DENT IN FUSELAGE SKIN FROM FS 193.00 TO FS 202.75 BETWEEN STR 18L AND 20L IAW BRAS EO. (K)SDR A6WA200540010Skin · dentedFOUND DENT IN LEFT SKIN FROM FS 235 TO FS 265 BETWEEN STRINGER 17L AND STRINGER 19L. REPAIRED DENT IN FUSELAGE SKIN FROM FS 235 TO FS 265 BETWEEN STRINGER 17L AND STRINGER 19L IAW BRAS EO 601R-53-5788A. (M)SDR A6WA200440049Skin · damagedTHE RIGHT FUSELAGE SKIN WAS DAMAGED WHEN THE SERVICE DOOR WAS OPENED WHILE PRESSURIZED. FUSELAGE SKIN WAS DENTED BETWEEN STRINGERS 13/14 APPROX 3.5 INCHES AFT OF FS 295 AND DENTED WITH A CREASE BETWEEN STRINGERS 16/17 AT FS 295. TRIMMED OUT SKIN PANEL AND FRSDR A6WA200440050Skin · damagedTHE RIGHT FUSELAGE SKIN WAS DAMAGED WHEN THE SERVICE DOOR WAS OPENED WHILE PRESSURIZED. PERFORMED A MAJOR REPAIR TO RIGHT SIDE OF FUSELAGE SKIN AT FS 298.5 BETWEEN STRINGERS 13R AND 14R USING STANDARD SHOP PRACTICES. FABRICATED STIFFENER FROM 2024-T3 .063 INSDR A6WA200440045Skin · dentedFORWARD SERVICE DOOR JAMMED. TWO DENTS FORWARD OF RT FORWARD SERVICE DOOR. DENTS OUT OF LIMITS. COMPLIED WITH REPAIR BRAS EO 601R-53-4835 STEPS 1, 2, 3, 4 AND 5. PERFORMED REPAIR OF SERVICE DOOR STRINGER 16/17 OF FIG 245 AND STRINGER 13/14 FIG 295. (M)
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