N419AW
Service difficulty reports · 178
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 = 'N419AW' 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 = 'N419AW' 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 A6WA200740165Control Unit · malfunctionedSTAB TRIM RUNAWAY AFTER TAKEOFF, QRH COMPLIED WITH, RETURNED TO DEPARTURE. REMOVED AND REPLACED HORIZONTAL STAB TRIM CONTROL UNIT IAW AMM REF 27-41-01 AND FOUND SERVICEABLE. (K)SDR A6WA200740051Priority Valve · malfunctionedGEAR DISAGREE AFTER TAKEOFF. NOSE GEAR DID NOT COME OUT OF DOWN AND LOCKED. AIRSPEED MAINTAINED LESS THAN 190 KNOTS COMPLIED WITH QRH ALL GEAR WENT DOWN AND LOCKED AS NORMAL. REMOVED AND REPLACED NLG PRIORITY VALVE P/N 4622 IAW CRJ AMM 32-33-51. (M)SDR A6WA200740050Check Valve · malfunctionedAFTER TAKEOFF, HAD RIGHT PACK OVERTEMP MESSAGE AND SMOKE FROM AIR CONDITIONING VENTS. TURNED RIGHT PACK OFF AND SMOKE CLEARED. REMOVED AND REPLACED RAM AIR CHECK VALVE. INSPECTED RIGHT PACK, FOUND BLOWN GASKET ON PLATE ABOVE OIL SIGHT GAUGE, REF 148439/4. SDR A6WA200640353Actuator · malfunctionedFLAPS FAIL MESSAGE ILLUMINATED IN FLIGHT. ON APPROACH, FLAPS INDICATED 38 DEGREES. COMPLIED WITH QUICK REFERENCE HANDBOOK. REMOVED AND REPLACED LEFT OUTER OUTBOARD FLAP ACTUATOR S/N OFF 1686, LT OUTER INBOARD FLAP ACTUATOR S/N OFF 1851, RT INBOARD OUTER FLASDR A6WA200640103Idg · inoperativeIDG1 CAUTION ILLUMINATED ON T/O ROLL. ABORTED TAKEOFF AT 60 KNOTS. BTMS ALL GREEN. RESET GEN 1 OK. ACTION TAKEN: REMOVED AND REPLACED IDG NR 1. OPS AND LEAK CHECK GOOD. (K)SDR A6WA200540362Dcu · malfunctionedAFTER DEPARTURE, UPON FLAP RETRACTION, FLAP FAIL CAUTION MESSAGE APPEARED ON ED1 FLAP POSITION INDICATION ON ED1 READS ZERO DEGREES, FLIGHT CONTROL PAGE ALSO READS ZERO ON ED2. RETURN TO DEPARTURE FOR (FLAP ZERO LANDING). FOUND GROUND PROXIMITY MESSAGE ON MDSDR A6WA200540223Drag Angle · damagedPAX DOOR AFT DRAG ANGLE CRACKED NEAR UPPER SUPPORT PULLEY. REPAIRED AFT DRAG ANGLE BY REMOVING DAMAGE, PERFORMED EDDY CURRENT INSPECTION, FABRICATED AND INSTALLED REPAIR PIECES IAW REO. (K)SDR A6WA200540245Angle · crackedRT OBLIQUE ANGLE AT FS 625 CRACKED ON AFT EDGE APPROX 1 INCH LONG. REMOVED OBLIQUE ANGLE RT FS 625, INSTALLED NEW SERVICEABLE ANGLE IAW SRM. (K)SDR A6WA200540214Angle · crackedLT OBLIQUE ANGLE AT FS 625, CRACKED ON AFT SIDE .5 INCHES LONG. REMOVED OBLIQUE ANGLE LT FS 625, INSTALLED NEW SERVICEABLE ANGLE IAW SRM. (K)SDR A6WA200540202Floorbeam · crackedRIGHT SIDE FLOOR SUPPORT ANGLE AT FS 621 CRACKED APPROX 1.1 INCH LONG, RBL 41.5 WL 73. REPAIRED RIGHT SIDE FLOOR SUPPORT ANGLE AT FS 621 BY CUTTING AWAY DAMAGED AREA AND INSTALLED MG REPAIR PARTS IAW BOMBARDIER REO 601R-53-61-117 REV C. (M)SDR A6WA200540204Floorbeam · crackedLT SIDE FLOOR SUPPORT ANGLE AT FS 621 CRACKED APPROX 1.1 INCH LONG LBL 41.5, WL 73. CUT AWAY DAMAGED SECTION OF ANGLE AND INSTALLED REPAIR ANGLE IAW BOMBARDIER, INC REO 601R-53-61-117 REV C. (M)SDR A6WA200540200Intercostal · crackedLEFT INTERCOSTAL AT FS 484, LBL 27, IS CRACKED IN RADIUS APPROX .30 INCH LONG. REMOVED CRACKED ANGLE, P/N 601R31171-17. FABRICATED NEW ANGLE USING PERFORMED ANGLE P/N S6444-14 ETCHED, PRIMED, TOP COATED FABRICATED ANGLE. INSTALLED FABRICATED ANGLE ON LEFT SSDR A6WA200540196Intercostal · crackedLEFT SIDE INTERCOSTAL AT FS 484, LBL 36 IS CRACKED IN RADIUS APPROX .20 INCH LONG. REPAIRED LEFT SIDE INTERCOSTAL AT FS 484 LBL 36 IAW BOMBARDIER REO 601R-53-41-059 REV A AND BRAS STANDARD REPAIR 601R-53-0030. (M)SDR A6WA200540195Intercostal · crackedRIGHT SIDE INTERCOSTAL AT FS 484, RBL 36, IS CRACKED IN FLANGE FROM TOP RIVET HOLE TO EDGE, APPROX .35 INCH LONG. REPAIRED RIGHT SIDE INTERCOSTAL AT FS 484 RBL 36 IAW BOMBARDIER REO 601R-53-41-059 REV A AND BRAS STANDARD REPAIR 601R-53-0030. (M)SDR A6WA200540198Clip · crackedCLIP AT FS 280, RBL 9, OUTBOARD SIDE IS CRACKED IN RADIUS APPROX .70 INCH LONG. (M)SDR A6WA200540199Clip · crackedCLIP AT FS 280, RBL 9, INBOARD SIDE IS CRACKED IN RADIUS APPROX .40 INCH LONG. REMOVED CRACKED CLIP AT FS 280 RBL 9 LEFT SIDE AND INSTALLED NEW CLIP IAW CRJ 200 SRM 51-40-11, 51-23-00, 51-42-06 AND 51-42-21. (M)SDR A6WA200540201Intercostal · crackedLEFT SIDE INTERCOSTAL AT FS 484, LBL S7, IS CRACKED IN RADIUS APPROX .30 INCH LONG. (M) REMOVED CRACKED ANGLE FABED NEW ANGLE USING PREFORMED ANGLE. ETCHED, ALODINED, PRIMED, AND TOP COATED FABED ANGLE. INSTALLED FABED ANGLE ON LT SIDE INTERCOSTAL FS 484, SDR A6WA200540203Clip · crackedCLIP AT FS 280, LBL 9, OUTBOARD SIDE, IS CRACKED IN RADIUS APPROX .50 INCH LONG. REMOVED CRACKED CLIP AT FS 280 LBL 9 OUTBOARD SIDE AND REPLACED WITH NEW CLIP P/N 601R31113-57 IAW CRJ200 SRM 51-42-06 AND 51-42-21. (M)SDR A6WA200540197Hinge · crackedCREW ESCAPE HATCH HINGES ARE CRACKED AROUND BASE. REPLACED BOTH HINGE ARMS WITH NEW HINGE ARMS IAW REO SRM. (K)SDR A6WA200540113Apu · making metalAPU FAULT CONDITION IN FLIGHT. SMOKE APPEARED IN CABIN. CLOSED PACKS AND SHUTDOWN APU. INSPECTED APU COMPARTMENT, NO FUEL OR OIL LEAKS NOTED CHECKED BOTH ACM`S IAW AMM. OIL LEVEL CHECK GOOD. CHECKED APU OIL LEVEL IAW AMM. OIL LEVEL GOOD. FOUND METAL INSSDR A6WA200540093Skin · damagedDURING POST FLIGHT WALK AROUND, RIGHT ENGINE COWLING DISCOVERED POSSIBLY OPENED IN FLIGHT. DAMAGED NOTED. (M) REMOVED AND REPLACED DOOR INSTALL LOWER CORE COWL. OPS CHECK GOOD. (K)SDR A6WA200540080Odor · detectedSTRONG ODOR OF EXHAUST NOTED WHEN THRUST LEVERS ADVANCED. OPERATED PACKS AND COULD SMELL FAINT ODOR OF DIESEL. OPERATED PACKS ON APU FOR SEVERAL MINUTES, ODOR FADED. BELIEVE AIRSTART CART INGESTED ITS OWN EXHAUST. OPERATED PACKS ON BOTH ENGINES, ODOR DID NSDR A6WA200440074Handle · failedLANDING GEAR DID NOT RETRACT AFTER TAKEOFF. PARKING BRAKE SHUT-OFF VALVE MESSAGE AND ANTI-SKID IB MESSAGE. COMPLIED WITH QRH, RETURNED TO COS WITH UNEVENTFUL LANDING. REMOVED AND REPLACED GEAR SELECTOR HANDLE IAW MM FUNCTION AND OPS CHECK GOOD.SDR A6WA200340174Skin · damagedTEMPORARY REPAIR ON RT FORWARD FUSELAGE SKIN JUST FORWARD OF FS 202.75 BULKHEAD, DENT 4 INCH LOG BY .062 INCH DEEP, TEMP REPAIR WS PERFORMED PER REO 601R-53-11-327. COMPLIED WITH STEPS 1 THROUGH 3 OF WVAC EO NR 601R-53-4413. PERFORMED EDDY CURRENT INSPECTIONSDR A6WA200340180Vane · chafedLEFT OUTBOARD FLAP FIXED VANE LEADING EDGE CAP, P/N 601R-14574-7 IS CHAFED AT WS 297 APPROXIMATELY .25 INCH BY .5 INCH AND .001 DEEP. PERFORMED MAJOR REPAIR TO THE LEFT OUTBOARD FLAP LEADING EDGE FIXED VANE BY REMOVING AND REPLACING LEADING EDGE CAP P/N 601R-SDR A6WA200340179Vane · chafedRIGHT INBOARD FLAP LEADING EDGE MOVEABLE VANE LEADING EDGE HAS THREE MINOR CHAFES AT WS 56.177, WAS 104.429 AND WS 140.364. ALL THREE CHAFES ARE LESS THAN .001 INCHE DEEP. PERFORMED A MAJOR REPAIR TO RIGHT INBOARD FLAP LEADING EDGE MOVEABLE VANE LEADING EDGESDR A6WA200340181Skin · dentedTEMPORARY REPAIR ON RT FORWARD FUSELAGE SKIN JUST FORWARD OF FS 202.75 BULKHEAD, DENT 4 INCHES BY .062 INCH DEEP. TEMP REPAIR WAS PERFORMED IAW REO 601R-53-11-327. PERFORMED A MAJOR REPAIR TO FUSELAGE SKIN AT FS 202.75 TO FS 204, BETWEEN STRINGERS 12R AND 13RSDR A6WA200340182Vane · chafedLT INBOARD FLAP LEADING EDGE MOVEABLE VANE LEADING EDGE HAS 2 MINOR CHAFF AREAS AT WS 56.177 AND WS 104.429. BOTH CHAFES ARE LESS THAN .001 INCH DEEP. PERFORMED A MAJOR REPAIR TO LEFT INBOARD FLAP LEADING EDGE MOVEABLE VANE LEADING EDGE AT WS 56.177 AND WSL
Back to N419AW