N420AW

Service difficulty reports · 222

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 = 'N420AW' 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 A6WA200640208Stator · damagedSHORTLY AFTER TAKEOFF, ENGINE NR 2 FAN VIBE WENT TO 3.3 TWO, YELLOW RANGE. COMPLIED WITH QRH, ENGINE WAS SHUTDOWN AND AIRCRAFT RETURNED TO ELM. CLEANED INLET AREA, REPLACED BLADES 1, 2, 4, 5, 6, 14, 16, 18, 19, 29 AND REPLACED SPACER ON STATOR ASCEND AT 10 OMay 27, 2006 · N420AW · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR A6WA200640161Control Unit · malfunctionedANTI-ICE DUCT WARNING CASS IN FLIGHT RIGHT WING INDICATED RED ON SYNOPTIC PAGE. COMPLIED QRH, WARNING EXTINGUISHED. REMOVED AND REPLACED RIGHT BLEED LEAK CONTROL UNIT IAW 36-31-10. PERFORMED OPS CHECK OF ANTI-ICE CONTROL AND INDICATION, OPS CHECK GOOD IAW 3Apr 25, 2006 · N420AW · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR A6WA200640048Wheel · inoperative(TIRE BLOWN OUT ON LANDING) LT IB TIRE NEEDS TO BE REPLACED. THRUST REVERSER USED IAW FOM BRAKE TEMPS AND GATE WAS 4,1,4,4. REMOVED AND REPLACED MLG NR2 WHEEL ASSEMBLY IAW AMM. (K)Jan 30, 2006 · N420AW · Cndair CL6002B19 · TireSDR A6WA200540329Control Unit · malfunctionedSTAB TRIM AND MACH TRIM MESSAGE APPEARED DURING CLIMB. COMPLIED WITH QRH, MESSAGE PERSISTED. REMOVED AND REPLACED HSTCU PN 7060-9, IAW AMM. OPS CHECK GOOD.Nov 18, 2005 · N420AW · Cndair CL6002B19 · Stabilizer Control SystemSDR A6WA200540272Spoiler · out of adjustCONFIG SPOILER MESSAGE ON TAKEOFF. ABORTED TAKEOFF AT 120 KNOTS. BRAKE TEMPS 5, 6 AND 7. AIRCRAFT WEIGHT 50,900 LBS. ADJUSTED GAP ON LEFT INBOARD GROUND SPOILER NR 4 TO WITHIN LIMITS IAW AMM 27-60-00-220-801. (M)Aug 8, 2005 · N420AW · Cndair CL6002B19 · Drag Control SystemSDR A6WA200540279Idg · lack of lubeDURING TAKEOFF ROLL 70 KNOTS IDG NR FAIL, GEN NR 2 OFF APPEARED MODERATE BREAKING BTMS READOUT 4, 5,6,7 FOUND NR 2 IDG OIL LEVEL LOW SERVICED NR 2 IDG RAN ENGINE NO LEAKS NOTED OPS CHECK GOOD IAW MM. PERFORMED RTO INSPECTION. (K)Aug 5, 2005 · N420AW · Cndair CL6002B19 · Alternator-Generator DriveSDR A6WA200540267Drag Angle · crackedPASSENGER DOOR STAIR AFT DRAG ANGLE IS CRACKED, .5 INCH LONG IN RADIUS (ADJACENT TO MOUNT FOR PASSENGER DOR ASSIST CABLE PULLEY). REMOVED DAMAGED SECTION OF ANGLE, FABRICATED REPAIR ANGLE AND INSTALLED ANGLE IAW REO. (K)Jul 24, 2005 · N420AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200540266Fitting · looseHORIZONTAL STABILIZER FORWARD STEADY FITTING HAS 3 LOOSE MOUNT BOLTS ON LT SIDE OF FITTING. REMOVED BOLTS, VISUALLY INSPECTED HARDWARE AND HOLES, REINSTALLED BOLTS AND TORQUED IAW AMM. (K)Jul 24, 2005 · N420AW · Cndair CL6002B19 · Horizontal Stabilizer StructureSDR A6WA200540258Beam · dentedNESTED ANGLE ON FWD WEB OF ENGINE BEAM HAS A DEEP GOUGE IN RADIUS APPROX .300 INCH LONG X .075 INCH WIDE AND .050 DEEP. REMOVED DAMAGED SECTION OF NESTING ANGLE. FABRICATED AND INSTALLED REPAIR PARTS IAW EO. (K)Jul 21, 2005 · N420AW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR A6WA200540248Door · damagedRT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT FOR PANEL 640BB HAS FRETTING DAMAGE. 2 INCH LONG X .125 INCH WIDE. REPAIRED BY BLENDING AND TREATING DAMAGED AREA IAW REO. (K)Jul 17, 2005 · N420AW · Cndair CL6002B19 · Fluid Service DoorsSDR A6WA200540274Angle · crackedFS 280, LBL 9, IB ATTACH CLIP CRACKED. REPLACED ANGLE IAW SRM AND EO. (K)Jul 16, 2005 · N420AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540255Clip · crackedFS700, LBL 9 IB ATTACH CLIP CRACKED. REPLACED ANGLE IAW CRM AND EO. (K)Jul 16, 2005 · N420AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540253Clip · crackedFS 280, LBL 9, OB ATTACH CLIP CRACKED. (K) REPLACED ANGLE P/N 601R31113-58 IAW CRJ CRM 51-42-06 AND BRAS EO 601R-53-6888. (M)Jul 16, 2005 · N420AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540252Clip · crackedFS 280, RBL 9, IB ATTACH CLIP CRACKED. REPLACED ANGLE IAW SRM AND EO. (K)Jul 16, 2005 · N420AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540249Access Panel · damagedRT LOWER WING PLANK AT WS 45, FUEL ACCESS PANEL 640BB CUT OUT, RAS FRETTING DAMAGE 2 INCH LONG X .175 INCH WIDE. (K)Jul 16, 2005 · N420AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540251Clip · crackedFS 280, RBL 9, OB ATTACH CLIP CRACKED. (K) REPLACED ANGLE P/N 601R31113-58 IAW CRJ SRM 51-42-06 AND BRAS EO 601R-53-6888. (M)Jul 16, 2005 · N420AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540244Angle · crackedRT FS 625, OBLIQUE ANGLE IS CRACKED. REMOVED CRACKED OBLIQUE ANGLE AND REPLACED WITH NOW IAW SRM. (K)Jul 15, 2005 · N420AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540254Support · crackedWO 84084, MWC 131, RT SIDE UNDERFLOOR SUPPORT STRUCTURE IS CRACKED 1.0 INCH AT FS 621, RBL 40, WL 73. REPAIRED BY REMOVING DAMAGED SECTION OF ANGLE, FABRICATING AND INSTALLING REPAIR ANGLES IAW REO. (K)Jul 15, 2005 · N420AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540250Skin · dentedPROTRUDING DENT AT FS 679, BETWEEN STR 23 AND STR 24, RT MEASURES .5 INCH X .020 INCH DEEP. PERFORMED REPAIR TO FUSELAGE SKIN FROM FS 672 TO 682 BETWEEN STRING STR 23 AND 24 BY CUTTING OUT DAMAGED AREA, PERFORMED NDT OF CUT LINE FAB AND DOUBLER AND INSTALLED Jul 15, 2005 · N420AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200440239Control Panel · malfunctionedABORTED TAKEOFF DUE TO CONFIG TRIM WARNING. ABORTED AT 60 KNOTS, RUDDER IN GREEN BAND, WILL TRAVEL TO LEFT BUT NOT TO THE RIGHT. REMOVED AND REPLACED RUDDER TRIM CONTROL PANEL, IAW AMM 27-10-01, OPS CHECK GOOD. (M)Dec 29, 2004 · N420AW · Cndair CL6002B19 · Rudder Tab Control SystemSDR A6WA200340204Angle · crackedFLOOR ANGLE AT FS 621, LEFT SIDE, NEXT TO CARGO DOOR IS CRACKED. REPAIR IAW BOMBARDIER REO 601R-53-61-117. SEALED AND PAINTED IAW BOMBARDIER REO 601-53-61-117. PRESSURIZED AIRCRAFT IAW AMM 21-32-00-863-801. NO LEAKS NOTED. (M)Jan 3, 2004 · N420AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200340109Apu · seizedAFTER ROTATION SMELLED SOMETHING HOT, APU EGT ABOVE RED LINE, APU SHUTDOWN AND TRANSFERRED BLEEDS TO ENGINE. SMOKEY ODOR DISAPPEARED. REMOVED APU SEIZED. REMOVED AND REPLACED APU. NO FURTHER INCIDENT. (M)Jul 18, 2003 · N420AW · Cndair CL6002B19 · APU Cowling/Containment
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