N458AW
Service difficulty reports · 201
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 = 'N458AW' 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 = 'N458AW' 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 A6WA201140242Skin · chafedLT AILERON UPPER SKIN L/E CHAFED IN 4 EA PLACES. REPAIRED LT AILERON UPPER SKIN L/E IAW REO 601R-57-60-013, REV NCN.SDR A6WA201140241Skin · chafedLT FLAP VANE L/E IS CHAFED IN 3 EA LOCATIONS. REPAIRED CHAFED ON LT FLAP VANE L/E ON 3 EA LOCATION IAW 601R-57-52-004, REV C.SDR A6WA201140003Case · splitRECEIVED LT ENG OIL PRESSURE WARNING MESSAGE, OIL PRESSURE INDICATED BETWEEN 25-33 PSI, REDUCED THRUST AND OIL PRESSURE INDICATED 40 PSI, MESSAGE REAPPEARED IN 30 SECONDS, OIL PRESSURE INDICATED 25-35 PSI, SHUTDOWN ENG FOR REMAINING 15 MINUTES OF FLIGHT. DID SDR A6WA201040977Oil System · fluctuatesLT ENGINE OIL PRESSURE FLUX 28-44 PSI. CW QRH DIVERTED, OIL PRESSURE WARNING OCCURRED WHENEVER OIL PRESSURE INDICATED 28 PSI. TT FLUX 25 MINUTES. SERVICED ENGINE 5 PINTS OIL CHECKED MASTER SHIP DETECTOR IAW EMM 72-00-00, FAULT ISOLATION 15, FUZZ ON CHIP DETSDR A6WA201040460Steering Sys · malfunctionedSTEERING INOP CAUTION MSG 110 KTS ON TAKEOFF ROLL. ABORTED TAKEOFF, BRAKE TEMPS 10, 9, 9, 9. INTEROGATED NWS ECU. NO FAULTS. PERFORMED OPS TEST IAW AMM 32-51-00. OPS TEST GOOD PERFORMED TAXI TEST WITH CREW. NO DEFECTS NOTED.SDR A6WA201040277Feel Sensor · out of adjustHIGHER THAN NORMAL CONTROL FORCE REQUIRED WHEN APPLYING AND NEUTRALIZING RT ROLL INPUTS FROM CTR OS ON BOTH YOKES IN FLIGHT. INSPECTED RIGGING OF AILERON FEEL AND SENSORY MECHANISM ON BOTH SIDES. ADJUSTED IAW AMM 27-11-00. OPS CHECK GOOD.SDR A6WA200940781Engine · fluctuatesON CLIMB ABOVE 10000 FT RT ENG FLUCTUATIONS, APPROX 2 PERCENT N1 AND N2, 200 LBS F/F AND 20/30 DEG ITT FOR SEVERAL MIN, THEN ENG STABILIZED, ON DESCENT AND APPROACH MULTIPLE REPEAT EPISODE OF FLUX EXPERIENCED FDR EVENTS NOTED. EMERGENCY DECLARED, LANDED WITHOSDR A6WA200940283Floorbeam · crackedMWC 132430-61 - FLOORBEAM AND CLIPS (2EA) CRACKED AT F/S 280.00 RBL 9.0, AT F/S 280.00 RBL 9.0, REPAIR PERFORMED IAW REO 601R-53-11-171. (K)SDR A6WA200940282Stiffener · bentMWC 132430-37 - ENGINE BEAM UPPER WEB STIFFENER BENT AT RBL 9.5. ENGINE BEAM UPPER WEB STIFFENER AT RBL 9.5 FABRICATED IAW CRJ 200 51-24-36, AND INSTALLED IAW SRM 51-42-06/51-42-21 AND TREATED IAW SRM 51-21-16. (K)SDR A6WA200940221Angle · crackedMWC 132430-95 - ANGLE AT FUSELAGE STA. 484.00, RBL 27.0 CRACKED. ANGLE AT F/S 484.00, RBL 27.0 FABRICATED IAW CRJ 200, SRM 51-24-36. ANGLE AT F/S 484.00 RBL 27.00, INSTALLED IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (K)SDR A6WA200940225Sill · crackedMWC 132430-218 - CARGO BAY DOOR FLOOR SILL CRACKED AT FS 574.00 (1X.10 INCH + 0.120 INCH LENGTH) CARGO BAY FLOOR SILL CUTOUT AND PARTS FABRICATED IAW CRJ 200 REO 601R-53-61-1741. E/C PERFORMED, AMO 9-86. NO CRACK FOUND. PARTS ARE INSTALLED IAW CRJ200 REO 6SDR A6WA200940281Stiffener · crackedMWC 132430-36 - ENGINE SUPPORT BEAM UPPER STIFFENER AT RBL 6 CRACKED (.200 FT LENGTH). ENGINE SUPPORT BEAM UPPER STIFFENER AT RBL 6 REPLACED IAW CRJ200 51-42-06 AND 51-24-36. (K)SDR A6WA200940286Shim · corrodedSERVICE DOOR CUTOUT LOWER PROTECTIVE PLATE SHIM CORRODED. REPLACED SHIM ON IAW SRM 51-40-11. (K)SDR A6WA200940287Support Bracket · crackedMWC 132430-199 - CRACK EXISTS ON SKIN BEHIND AC GROUND POWER RECEPTACLE (ACCESS 122BR) AC GROUND POWER RECEPTACLE SUPPORT BRACKET REPLACED IAW SRM 51-42-06 AND 51-42-13. (K)SDR A6WA200940284Drag Angle · crackedMWC 132430-170- PASSENGER DOOR STAIRS AFT DRAG ANGLE FOUND CRACKED. PASSENGER DOOR STAIRS AFT DRAG ANGLE REPLACED IAW REO 601R-52-11-513. (K)SDR A6WA200940285Stiffener · crackedMWC 132430-173 - PASSENGER DOOR ASSIST MOTOR STIFFENER FOUND CRACKED. PASSENGER DOOR ASSIST MOTOR STIFFENER REPLACED IAW SRM 51-42-13. (K)SDR A6WA200940224Angle · crackedMWC 132430-180- ANGLE AT F/S 484.00, RBL 36 CRACKED. ANGLE AT F/S 484.00 CUTOUT IAW CRJ 200, REO 601R-53-41-059, EDDY CURRENT PERFORMED ON CUTOUT AND FABRICATED PARTS - PARTS FABRICATED AND INSTALL IAW REO 601R-53-41-059, REV A. (K)SDR A6WA200940222Fitting · crackedMWC 132430-162-BEAM AND CLIPS (2X) CRACKED AT F/S 280.00 LBL 9.0. REPAIR PERFORMED AT F/S 280.00, LBL 9.0 IAW CRJ 200 REO 601R-53-11-171, REV "SCHEME B". (K)SDR A6WA200940223Angle · crackedMWC 132430-164- UPPER AFT FLOOR ANGLE CRACKED AT F/S 280.0, LBL 9.0 UPPER AFT FLOOR ANGLE AT F/S 280.0, LBL 9.0, REPAIR PERFORMED IAW CRJ 200 REO 601R-53-11-138. (K)SDR A6WA200940322Pressure Blkhd · crackedMWC 132431-25 - F/S 621.00 LHS, REAR PRESSSSUE BULKHEAD FOUND CRACKED AT LINTEL LOCATION (CRACK LENGTH .250) REPAIR PERFORMED ON FS 621.0 LT PRESSURE BULKHEAD AT LINTEL LOCATION IAW REO 601R-53-61-1230. (K)SDR A6WA200940280Structure · crackedMWC 132430-24 - APU ENCLOSURE CRACKED AT 2 LOCATIONS. REPAIRED PERFORMED IAW REO 601R-49-11-017. (K)SDR A6WA200940051Bulkhead · crackedMWC 132430-18- FWD PRESSURE BULKHEAD CRACKED ON LT SIDE AT F/S 202.75, W/L 66.275 AT PARKING BRAKE LOCATION. FWD PRESSURE BULKHEAD ON LT SIDE AT F/S 202.75, W/L 66.275, REPAIR IAW REO 601R-53-11-563. (K)SDR A6WA200940020Flap System · failedFLAPS FAIL AT ZERO DEGREES ON APPROACH DURING SELECTION TO 8 DEGREES. INFLIGHT AIR TEMP -28 DEGREES. C/W RESET PROCEDURE IAW SUP 98-018B, STEPS 1.3 AND 1.4 FLAP RESET, OK. (K)SDR A6WA200840608Windshield · crackedFIRST OFFICERS WINDSHIELD CRACKED DURING DESCENT. REF 186497/2 R&R RT WINDSHIELD. APPLIED AERODYNAMIC FILLER TO RT WINDOW STRAP. APPLIED SPEED TAPE. TAPE MUST BE REMOVED AFTER 48 HRS. IAW AMM 56-11-01 PLACED ON DIL.SDR A6WA200840176Skin · delaminatedREQUEST INSPECTION RIGHT WINGLET TRAILING EDGE DELAMINATED/PILOT FOUND ON WALK AROUND. (M)SDR A6WA200840016Bpsu · failedREF 183967/2 DUE TO RECENT FLAP HISTORY AND CRJ AMM TEMP REVISION 05-035, AIRCRAFT REQUIRES FURTHER FLAP TROUBLESHOOTING AND RECTIFICATION CW CRJ AMM TR 05-035. REMOVED AND REPLACED LT BPSU, OPS TEST GOOD IAW AMM 27-51-10. (K)SDR A6WA200740683Pitch Control · inoperativeCONTROL COLUMN BINDS IN PITCH WHEN MOVED FORWARD AND AFT OF NEUTRAL AND FEELS HEAVIER THAN NORMAL THRU WHOLE RANGE OF MOVEMENT IN-FLIGHT AND ON GROUND AT ALL FLAP ANGLES. REMOVED AND REPLACED PITCH FEEL SIMULATOR. (K)SDR A6WA200740657Drive Unit · malfunctionedFLAP FAIL CAUTION MESSAGE INFLIGHT. LANDED WITH FLAPS AT 8 DEGREES. LANDING WEIGHT 40,300 LBS. SPEED 150 KNOTS VERTICAL SPEED LESS THAN 400 FT MINUTE MAX BTMS READING =3. REMOVED AND REPLACED FLAPS POWER DRIVE UNIT IAW AMM 27-52-01. PERFORMED OPS CHECK IASDR A6WA200740647Actuator · malfunctionedDURING MISSED APPROACH WHEN FLAP HANDLE MOVED TO 8 DEGREES, FLAP FAIL CAS MESSAGE ILLUMINATED AND FLAP STAYED AT 45 DEGREES. ALL 8 FLAPS ACTUATORS REPLACED ALSO RIGHT BPSU UNIT. REPLACED UE TO FLUCTUATION CAUSING JAMMING. FLAP SYSTEM. OPS CHECK GOOD.SDR A6WA200740646Drive Assy · unknownWHEN FLAP HANDLE SELECTED FROM 20 DEGREES TO 8 DEGREES IN FLIGHT, FLAP FAIL CAS MESSAGE STAYED AT 20 DEGREES. REMOVED AND REPLACED FLEX DRIVE NR 5 PER CRJ AMM 27-50-00, OPS CHECK GOOD. (M)SDR A6WA200740636Flap System · failedAFTER TAKEOFF FLAPS FAILED AT 13 DEGREES OAT +6 DEGREES CELCIUS, WHEN FLAPS BEING RETRACTED FROM 20 DEGREES TO 8 DEGREES. RESET FLAPS IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4 FLAPS RESET, AIRCRAFT RELEASED FOR SERVICE. (K)SDR A6WA200740612Smoke Detector · malfunctionedRECEIVED SMOKE CARGO WARNING MESSAGE FOR 5-10 SECONDS. INSPECTED CARGO COMPARTMENT AND FOUND NO EVIDENCE OF SMOKE OR FIRE. REMOVED AND REPLACED BOTH CARGO SMOKE DETECTORS IAW 26-15-01, OPS CHECK GOOD.SDR A6WA200740446Control Unit · malfunctionedHIGH SPEED ABORT DUE TO RED WARNING STAB CONFIGURATION. AIRCRAFT WEIGHT 47200 SPEED 120 KNOTS BRAKE TEMPS AFT 5 MINUTES 10, 8, 8, 8 (STAB CHANNEL 1 INOP). REMOVED AND REPLACED MOTOR CONTROL UNIT, HORIZONTAL STAB TRIM ACTUATOR, AND HORIZONTAL STAB TRIM CONTROSDR A6WA200740257Skin · corrodedLT WING LOWER PLANK ACCESS HOLE NR 9 FOR PANEL 550AB HAS FRETTING/ CORROSION DAMAGE 1 INCH AREAS AT IB END NOT IN CRITICAL AREA. (K) [07-17-07] MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 9 PANEL 550AB IAW BOMBARDIER REO 601R-57-21-030 REV A. (SDR A6WA200740256Skin · corrodedLT WING LOWER PLANK ACCESS HOLE NR 1 FOR PANEL 540BR HAS FRETTING/ CORROSION DAMAGE AREA ABOUT 2 INCHES LONG AT FWD/ OB QUADRANT, NO IN CRITICAL AREA. S/D MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 1 PANEL 540BB IAW BOMBARDIER REO 601R-57-21-030SDR A6WA200740255Skin · corrodedLT WING LOWER PLANK ACCESS HOLE NR 3 FOR PANEL 510BR HAS FRETTING/ CORROSION DAMAGE AT IB END 1 INCH LONG NOT IN CRITICAL AREA. S/D MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 3 PANEL 510BB IAW BOMBARDIER REO 601R-57-21-030 REV A. (K)SDR A6WA200740254Skin · corrodedLT WING LOWER PLANK ACCESS HOLE NR 2 FOR PANEL 510AB HAS FRETTING/ CORROSION DAMAGE AT IB END, ALL ALONG FWD SIDE AND OB END, IN AND OUT OF CRITICAL AREA. S/D MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 2 PANEL 510AB IAW BOMBARDER REO 601R-57-21-SDR A6WA200740253Intercostal · crackedINTERCOSTAL AT FS 484.00 HAS CRACKED FLANGE AT LBL 36.0 CRACK MEASURES APPROX .20 INCH LONG. S/D MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-53-41-059. (K)SDR A6WA200740252Intercostal · crackedINTERCOSTAL AT FS 484.00 HAS CRACKED FLANGE AT LBL 27.0 CRACK MEASURES APPROX .50 INCH LONG. S/D MAINTENANCE REPLACED CLIP IAW BSC SR 601R-53-0029B. (K)SDR A6WA200740251Intercostal · crackedINTERCOSTAL AT FS 484.00 HAS CRACKED FLANGE AT RBL 27.0 CRACK MEASURES APPROX .20 INCH LONG. S/D MAINTENANCE REPLACED CLIP IAW BSC SR 601R-53-0029B. (K)SDR A6WA200740250Floorbeam · crackedFS 280 FLOORBEAM CLIP AT OB SIDE OF LBL 9.0 IS CRACKED IN RADIUS APPROX .20 INCH LONG. (K) [07-17-07] MAINTENANCE REPLACED CLIP IAW BSC EO 601R-53-0057A. (M)SDR A6WA200740249Floorbeam · crackedFS280, FLOORBEAM CLIP AT IB SIDE OF LBL 9.0 IS CRACKED IN RADIUS APPROX. .20 INCH LONG. S/D - MAINTENANCE REPLACED CLIP IAW BSC EO 601R-53-0057A. (K)SDR A6WA200740248Floorbeam · crackedFS 280, FLOORBEAM CLIP AT IB SIDE OF RBL 9.0 IS CRACKED IN RADIUS APPROX .30 INCH LONG. S/D MAINTENANCE REPLACED CLIP IAW BSC EO 601R-57-0057A. (K)SDR A6WA200740247Floorbeam · crackedFS 280 FLOORBEAM CLIP AT OB SIDE OF RBL 9.0 IS CRACKED IN RADIUS APPROX .60 INCH LONG. (K) [07-17-07] MAINTENANCE REPLACED CLIP IAW BSC EO 601R-53-0057A. (M)SDR A6WA200740246Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE IS CRACKED. (K) [07-17-07] MAINTENANCE REMOVED DAMAGED SECTION OF DRAG ANGLE AND INSTALLED REPAIR PARTS IAW REO 601R-52-11-513 REV A. (M)SDR A6WA200740245Channel · crackedLT MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER HAT CHANNEL, PN 601R75262159, IS CRACKED AT OB LEGS LONGEST CRACK IS APPROX. .25 INCH LONG. (K) [07-17-07] MAINTENANCE REPLACED CHANNEL IAW CRJ SRM 51-42-06. (M)SDR A6WA200740244Channel · crackedRT MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER HAT CHANNEL PN 601R75262157, IS CRACKED THRU ON IB LEGS. (K) [07-17-07] MAINTENANCE REPLACED CHANNEL IAW SRM 51-42-06. (M)SDR A6WA200740243Structure · crackedRT MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER PLUMBING (Z) MEMBER ASSY PN 601R75262-153, IS CRACKED THRU ON OB LEG. (K) [07-17-07] MAINTENANCE REPLACED ZEE MEMBER IAW CRJ SRM 51-42-06. (M)SDR A6WA200740024Target · out of adjustGEAR DISAGREE WARNING MESSAGE AFTER DEPARTING PHL. COMPLIED WITH QRH. GEAR DOWN 3 GREEN. (M) ADJUSTED RT MLG UPLOCK TARGET REF CMM 32-30-15, OPS CHECK GOOD. (K)SDR A6WA200540358Flap System · failedFLAPS FAIL AT 8 DEGREES UPON FLAP RETRACTION. COMPLIED WITH SUPPLEMENT 98-18, FLAPS RESET, NO HISTORY IN PAST 72 HOURS. (K)
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