N417AW

Service difficulty reports · 217

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 = 'N417AW' 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 A6WA200540155Bushing · migratedRIGHT MAIN LANDING GEAR AFT TRUNNION BUSHING MIGRATED .012 INCH. REMOVED MIGRATED BUSHING AND INSTALLED 2ND OVERSIZE BUSHING P/N 601R5721003-2003-23, P/N 601R5721003-23 IAW BOMBARDIER INC REO 601R-57-21-003 REV B. (M)Apr 10, 2005 · N417AW · Cndair CL6002B19 · Main Landing GearSDR A6WA200540146Skin Panel · corrodedLT LOWER WING PLANK IS CORRODED UNDER PANEL 550FB, INBOARD SIDE 3 INCH LONG BY .100 WIDE BY .002 INCH DEEP, FORWARD SIDE .200 INCH LONG BY .100 INCH WIDE BY .002 INCH DEEP. S/D - REPAIRED LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT FOR PANEL 550 FB IAWApr 9, 2005 · N417AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540145Skin Panel · corrodedLEFT LOWER WING PLANK IS CORRODED UNDER PANEL 550HB AT FORWARD CENTER EDGE .600 INCH LONG BY .100 INCH WIDE BY .002 INCH DEEP, INBOARD EDGE 4 INCHES LONG BY .050 INCH WIDE BY .003 INCH DEEP, OUTBOARD SIDE 4.5 INCH LONG BY .025 INCH WIDE BY .003 INCH DEEP. S/DApr 9, 2005 · N417AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540151Skin · corrodedLEFT LOWER WING PLANK IS CORRODED UNDER PANEL 550AB, OUTBOARD EDGE 1 INCH LONG BY .100 WIDE BY .002 DEEP. (M)Apr 9, 2005 · N417AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540149Skin · corrodedLEFT LOWER WING PLANK IS CORRODED UNDER PANEL 660CB, AFT INBOARD EDGE .400 INCH LONG BY .100 INCH WIDE BY .002 INCH DEEP. (M)Apr 9, 2005 · N417AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540152Skin · corrodedLEFT LOWER WING PLANK IS CORRODED UNDER PANEL 540BB, FORWARD INBOARD EDGE 4 INCH LONG BY .100 INCH WIDE BY .002 INCH DEEP, AFT EDGE .050 INCH LONG BY .100 INCH WIDE BY .002 INCH DEEP. (M)Apr 9, 2005 · N417AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540153Skin · corrodedLEFT LOWER WING PLANK IS CORRODED AROUND ENTIRE CIRCUMFERENCE UNDER PANEL 510AB, .100 INCH S BY .002 INCH DEEP. (M)Apr 9, 2005 · N417AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540141Clip · crackedFOUND CRACK ON CLIP AT FS 280 RIGHT SIDE APPROX .5 INCH IN LENGTH AT TOP CORNER IN. REMOVED AND REPLACED RT FS 280 CLIP IAW CRJ SPM 51-42-06 FOR SOLID RIVETS AND 51-45-21 FOR HILITES. (M)Apr 6, 2005 · N417AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540142Drag Angle · crackedDOOR AFT DRAG ANGLE CRACKED .7 INCHES LONG AT SUPPORT CABLE PULLEY. (M)Apr 6, 2005 · N417AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200440147Idg · malfunctionedGEN NR 2 FAIL CASS MESSAGE FOLLOWED BY GEN 1 CASS MESSAGE. GEN NR 1 AND 2 RESET OPS NORMALLY. APU WAS RUNNING AND GEN OPS NORMALLY. SERVICED BOTH IDG IAW AMM 12-13-24. OPS CHECK GOOD. OK FOR SERVICE. NO LEAKS NOTED. NR 1 ENG 11 PUMPS AND NR 2 ENGINE 25 Oct 11, 2004 · N417AW · Cndair CL6002B19 · Alternator-Generator DriveSDR A6WA200340117Warning Light · illuminatedLEFT 14TH STAGE BLEED AIR DUCT WARNING INFLIGHT COMPLIED WITH QRH MESSAGE WENT OUT AND THEN CAME BACK 10 MINUTES. WITH ENGINE SHUTDOWN MESSAGE PERSISTED ON GROUND. REMOVED AND REPLACED LT PYLON SENSING ELEMENT A59WK IAW AMM 36-21-04. OPS CHECK GOOD. (M)Aug 4, 2003 · N417AW · Cndair CL6002B19 · Pneumatic Distribution SystemSDR A6WA200340116Warning Light · illuminatedRECEIVED LT 14TH STAGE DUCT MESSAGE, COMPLIED WITH QRH. MESSAGE CLEARED WITH THRUST LEVER RETARDED. INSPECTED LEFT 14TH STAGE DUCT BLEED AIR SYSTEM IAW MM 36-12-04. NO FAULTS FOUND. RAN ENGINES TO POWER, NO FAULTS NOTED. OK FOR SERVICE.Aug 3, 2003 · N417AW · Cndair CL6002B19 · Pneumatic Distribution SystemSDR A6WA200340105Idg · malfunctionedIDG CAUTION APPEARED ON TAKEOFF ROLL. COMPLIED WITH 'CM' ACTION PLACARDED AND PLACED ON MEL. RESET NR 2 IDG DISCONNECT MECHANISM. SERVICED IDG AS REQUIRED, OPS CHECK GOOD. REMOVED FROM MEL. (M)Jun 24, 2003 · N417AW · Cndair CL6002B19 · AC Generation SystemSDR A6WA200340037Tire · failedUPON LANDING, MKE, NR 3 MLG TIRE BLEW CAUSING DAMAGE TO RIGHT INBOARD FLAP REPLACED RIGHT INBOARD FLAP IAW AMM. RIGGED FLAP IAW AMM. OPS CHECK GOOD.Mar 12, 2003 · N417AW · Cndair CL6002B19 · TireSDR A6WA200240026Idg · lack of lubeABORTED TAKEOFF IDG NR 2 CAUTION MESSAGE. MAINTENANCE SERVICED NR 2 IDG. (M)Aug 13, 2002 · N417AW · Cndair CL6002B19 · AC Generator-AlternatorSDR A6WA200240007Control Unit · malfunctionedFLAPS FAIL ON APPROACH AT ZERO. C/W QRH, RESET FLAP CONTROL NR 1 C/B PER MECHANIC CONTROL, FLAPS NOW RUN AT HALF SPEED - NORMAL LANDING. MAINTENANCE RESET FLAPS PER AWAC SUPPLEMENT 98-18 FLAPS OPERATE AT NORMAL SPEED.Feb 14, 2002 · N417AW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR A6WA200240005Fcu · malfunctionedFLAP FAIL IN FLIGHT, FOLLOWED QRH AND MECHANIC PROCEDURES, CAS MESSAGE WENT OUT. MAINTENANCE INTERROGATED FCU, RESET FCU, RAN FLAPS OP CHECK OK C/W AWAC SUPPLEMENT 98-18, AMM 27-50.Feb 9, 2002 · N417AW · Cndair CL6002B19 · Trailing Flap Position Indicating System
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