N442AW

Service difficulty reports · 226

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 = 'N442AW' 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.

SDR A6WA200840410Intercostal · crackedCRACK EXISTS ON INTERCOSTAL FS 484 LBL 36. DAMAGED ATTACHMENT FLANGE CUTOUT, EDDY CURRENT PERFORMED AND NEW SERVICEABLE ANGLE INSTALLED IAW REO 601R-53-41-059 REV A.May 10, 2008 · N442AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840409Sill · corrodedCORROSION EXISTS ON LOWER SILL OF CARGO DOOR FS 574 TO FS 621 LBL 45. CORROSION REMOVED IAW SRM 51-21-06.May 10, 2008 · N442AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840406Floor Support · corrodedCORROSION EXISTS UNDER FLOOR FS 576, FS 605, FS 618 LBL 40. CORROSION REMOVED UNDER FLOOR FS 576, FS 605, FS 618 LBL 40 IAW SRM 51-21-06.May 10, 2008 · N442AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840412Angle · crackedLEFT FS 280, LBL 8 & 10, ANGLE ON BEAM FOUND CRACKED. LT FS 280, LBL 8 & 10, ANGLE ON BEAM REPLACED IAW SRM 51-42-21.May 9, 2008 · N442AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840408Floorbeam · crackedRT FS 280 RBL 8 & 10 ANGLE ON BEAM FOUND CRACKED. RT FS 280 RBL 8 & 10 ANGLE ON BEAM REPLACED IAW SRM 51-42-21.May 9, 2008 · N442AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200840405Separator · wornFIREWALL SEPARATOR WORN ON ACCESS PANEL 412DB. (K) FIREWALL SEPARATOR REPLACED IAW SRM 51-42-06.May 8, 2008 · N442AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840407Support Bracket · crackedNR 2 HYDRAULIC SUPPORT MANIFOLD BRACKET CRACKED. HYDRAULIC SUPPORT BRACKET REPAIRED IAW REO 601R-53-62-031 REV A.May 6, 2008 · N442AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200640424Fire Bottle · dischargedCARGO BOTTLE LOW LIGHT ILLUMINATED, LEFT FIRE BOTTLE BLOWN. RT FIRE BOTTLE BLOWN. REMOVED AND REPLACED LEFT CARGO FIRE BOTTLE PER CRJ AMM 26-25-01, OPS CHECK GOOD. REMOVED AND REPLACED RIGHT FIRE BOTTLE PER AMM 26-25-01, OPS CHECK GOOD, P/N 34600037-1, AND Dec 26, 2006 · N442AW · Cndair CL6002B19 · Fuselage Floor PanelSDR A6WA200640242Spring · lack of lubeSERVICE DOOR MECHANISM HAS NO TENSION, WILL NOT LATCH OPEN. CLEANED AND LUBED RETURN SPRING ON SERVICE DOOR HOLD OPEN LOCK, ALL IAW CRJ AMM 52-11-00. (M)Jun 19, 2006 · N442AW · Cndair CL6002B19 · Service DoorsSDR A6WA200640228Line · leakingRT BRAKE LINE LEAKING, SMOKING. REMOVED AND REPLACED BRAKE DISCONNECT O-RING IAW AMM. OPS AND LEAK CHECK GOOD AT THIS TIME. (K)Jun 3, 2006 · N442AW · Cndair CL6002B19 · Landing Gear Brake SystemSDR A6WA200640204Skin · dentedTWO DENTS AFT OF FUSELAGE STATION 605 BETWEEN STRINGER 23L AND 24L. MAINTENANCE PERFORMED REPAIR TO FUSELAGE SKIN AFT OF FS 605 BETWEEN STRINGER 23L AND 24L IAW BSC EO 601R-53-9221. REQUIRES COMPLIANCE WITH FAR 25.571 (DTA) WITHIN 12 MONTHS FROM RETURN TO SEMay 22, 2006 · N442AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200640203Skin · dentedONE DENT FORWARD OF FS 605 BETWEEN STRINGER 19L AND 20L. MAINTENANCE PERFORMED REPAIR TO FUSELAGE SKIN FS 605.00 BETWEEN STRINGER 19L AND 20L IAW BSC EO 601R-53-9198B. REQUIRES COMPLIANCE WITH FAR 25.571 (DTA) WITHIN 12 MONTHS OF RETURN TO SERVICE. (M)May 22, 2006 · N442AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200640195Support Angle · crackedLEFT RE-ENFORCEMENT ANGLE AT FS 640 BETWEEN STRINGER 9 AND 12 IS CRACKED IN RADIUS APPROX 3 INCHED DOWN FROM TOP Y-ANGLE AND APPROX .75 INCH LONG. REF WO 95968 JOB CARD 4EOMFG10776 FOR INCORPORATION OF ENGINE BEAM MODIFICATION. (M)May 16, 2006 · N442AW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR A6WA200640194Support Angle · crackedRIGHT REINFORCEMENT ANGLE AT FS 640 BETWEEN STRINGER 9 AND 12 IS CRACKED IN RADIUS APPROX 3 INCHES DOWN FROM TOP OF ANGLE AND APPROX .75 INCH LONG. REF WO 95968 JOB CARD 4EOMFG10776 FOR INCORPORATION OF ENGINE SUPPORT BEAM MODIFICATION. (M)May 16, 2006 · N442AW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR A6WA200640191Support Beam · unknownRIGHT ENGINE SUPPORT BEAM LOWER.May 16, 2006 · N442AW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR A6WA200640190Skin · corrodedTHE LOWER WING PLANK ACCESS HOLE FOR PANEL 410AB HAS SOME MINOR CORROSION AND PITTING AROUND OUTER PANEL SURFACE. BLENDED MINOR PITTING AND CORROSION ON LOWER LEFT WING PLANK ACCESS HOLE FOR PANEL 510AB IAW BOMBARDIER REO 601R-57-21-030. (M)May 15, 2006 · N442AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200640189Floorbeam · crackedRIGHT FS 621 FLOORBEAM ANGLE HAS A 1 INCH CRACK ON OUTBOARD RADIUS. REPAIRED FLOORBEAM ANGLE AT RT FS 621 IAW BOMBARDIER REO 601R-53-61-117 REV C. (M)May 14, 2006 · N442AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200640188Floorbeam · crackedFOUND LEFT FS 621 FLOORBEAM ANGLE HAS 1 INCH CRACK IN OUTBOARD RADIUS. REPAIRED ANGLE AT LT FS 621 IAW BOMBARDIER REO 601R-53-61-117 REV C. (M)May 14, 2006 · N442AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200640187Intercostal · crackedLT INTERCOSTAL AT FS 484 LBL 36 HAS A .25 INCH CRACK IN UPPER RADIUS. REPAIRED LEFT INTERCOSTAL AT FS 484 LBL 36 IAW BOMBARDIER REO 601R-53-41-059 AND BSC SR 601R-53-0030A. (M)May 14, 2006 · N442AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640186Rib · crackedFOUND RIGHT MLG WHEEL WELL BATTERY RIB HAS A .5 INCH LONG CRACK IN TOP RADIUS. REPAIRED RT MLG WHEEL WELL BATTERY RIB BY TRIMMING OUT DAMAGED AREA, CUT DOUBLER, FABRICATED REPAIR PARTS AND WET INSTALLED IAW BOMBARDIER REO 601R-57-51-046 REV B REPAIR NR 1. (MMay 14, 2006 · N442AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA200640185Angle · crackedFOUND LEFT FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED AND REPLACED LEFT OBLIQUE INTERCOSTAL P/N 601-35012-51 IAW CRJ 200 SRM 51-42-06. (M)May 12, 2006 · N442AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640184Intercostal · crackedFOUND RIGHT FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED AND REPLACED RT 625 OBLIQUE INTERCOSTAL P/N 601-35012-52 IAW CRJ 200 SRM 51-42-06. (M)May 12, 2006 · N442AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640192Support Beam · crackedLT ENGINE SUPPORT BEAM LOWER WEB IS CRACKED 1 INCH LONG IN FORWARD INBOARD CORNER OF ACCESS DOOR CUTOUT, REF WO 95968 JOB CARD 4EOMFG10776 FOR INCORPORATION OF ENGINE SUPPORT BEAM MODIFICATION. (M)May 9, 2006 · N442AW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR A6WA200640070Idg · unknownIDG NR 2 CAUTION MESSAGE ILLUMINATED ON TAKEOFF ROLL. AC WEIGHT=43000, MAX BTMS= 5. 344. ALL IN GREEN SPEED AT ABORTED TAKEOFF = 45 KNOTS INITIAL LEAK CHECK NO LEAKS NOTED. SERVICED IDG NR 2 GROUND RAN ENGINE IDG/GEN OPERATES NORMAL, POST RUN NO LEAKS NOTEDFeb 10, 2006 · N442AW · Cndair CL6002B19 · Alternator-Generator DriveSDR A6WA200540357Landing Gear · malfunctionedAFTER GEAR RETRACTION, NOSE GEAR WOULD NOT RETRACT, GEAR RETRACTION HORN SOUNDED. C/W QRH LANDED IN MSP AT 42000. MEL`D GEAR RET SYS FUNCTION TESTED GEAR SYS. PERFORMED GEAR DISAGREE TEST, FULLY SERVICED NLG STRUT.. PERFORMED LANDING GEAR EXT/RETRACT FUNCTDec 20, 2005 · N442AW · Cndair CL6002B19 · Nose/Tail Landing GearSDR A6WA200440185Doubler · damagedAFTER REMOVING ACCESS PANEL 132AL, FOUND 4 HOLES IN FORWARD FUSELAGE ACCESS PANEL DOOR SURROUND DOUBLER FS 228, STR19R-20R. PERFORMED A MAJOR REPAIR BY OPENING UP HOLES TO REMOVE DAMAGE, FABRICATED AND INSTALLING FREEZE PLUGS. OPENED HOLES IN FREEZE PLUGS USNov 17, 2004 · N442AW · Cndair CL6002B19 · Fuselage Main, Structure
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