N432AW

Service difficulty reports · 229

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 = 'N432AW' 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 A6WA200540372Skin · corrodedLT LOWER WING PLANK HOLE NR 1, WS 54.897 HAS CORROSION AT IB SIDE FORWARD EDGE 2 INCH L .005 INCH D AND AT OB SIDE AFT 4 INCH L X .005 INCH D. NOT IN CRITICAL AREA. MAINT REPAIRED LT LOWER WING PLANK ACCESS HOLE NR 1 IAW REO. (K)Dec 30, 2005 · N432AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540373Skin · corrodedLT WING LOWER PLANK HOLE NR4, WS 54.681 HAS CORROSION AT OB SIDE 5 INCH L X .002 INCH D AND AT IB SIDE 5 INCH L X .002 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 4 AT WS 54.681 IAW REO. (K)Dec 30, 2005 · N432AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540378Cover · crackedPASSENGER DOOR UPPER FORWARD CORNER CAP IS CRACKED. MAINTENANCE REPAIRED PASSENGER DOOR UPPER FWD CORNER CAP IAW REPAIR BY INSTALLING NEW COVER PN 6003190278. (K)Dec 30, 2005 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200640005Handle · out of positionCREW ESCAPE HATCH OUTER HANDLE STICKS IN THE CLOSED POSITION. CLEANED AND LUBRICATED OUTER HANDLE MECHANISM IAW AMM. (K)Dec 29, 2005 · N432AW · Cndair CL6002B19 · Emergency ExitsSDR A6WA200540380Rib · crackedLT BATT RIB ASSY AT WS 53.60, FS 523.8 CRACKED 1 INCH RADIUS MAINTENANCE REPAIRED BATT RIB ASSY IAW REO. (K)Dec 28, 2005 · N432AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200540377Angle · crackedLT FS 625 OBLIQUE ANGLE IS CRACKED. MAINTENANCE REMOVED AND REPLACED OBLIQUE ANGLE LT SIDE PH 601R-35012-51 IAW CRJ 200 SRM 51-42-06. (K)Dec 28, 2005 · N432AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540379Rib · crackedRT BAH RIB ASSY WS 53.60, FS 523.8 CRACKED 1 INCH IN RADIUS. MAINTENANCE REPAIRED RT BAH RIB ASSY IAW REO. (K)Dec 28, 2005 · N432AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200540163Windshield · crackedCAPTAINS WINDSCREEN CRACKED AT 32 FL FOLLOWED QUICK REFERENCE HANDBOOK AND DECLARED EMERGENCY. DIVERTED TO BUFFALO, NO SIGNS OF CRACKING ON INSIDE OR OUTSIDE OF WINDSCREEN. REMOVED AND REPLACED CAPTAINS WINDSCREEN. OPS AND LEAK CHECK GOOD REFERENCE CHAPTER May 3, 2005 · N432AW · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA200540042Compressor · vibrationRETURNED TO DEPARTURE, DUE TO HIGH N1 FAN VIBRATION 2.8 IN CLIMB POWER SET ITT AND N1 NORMAL. INSPECTED NR 2 ENGINE INLET FAN BLADES, EXHAUST AND CHIP DETECTORS. NO DEFECTS FOUND. GROUND RAN ENGINE VIBRATION .8 MILS WITHIN LIMITS REF CF34 ENG MANUAL 72-00-0Feb 4, 2005 · N432AW · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR A6WA200440193Fuel Bowl · contaminatedON APPROACH, RT ENG RED OIL PRESSURE WARNING MESSAGE. ENGINE FLAMED OUT C/W QRH, ENG WINDMILLED FOR 3 MINUTES. FOUND WATER IN RT ENG FUEL BOWL. ALL INSPECTION AND CHECKS GOOD EXCEPT FOR WATER IN BOWL IAW 769-10-00 AND 73-11-03.Nov 23, 2004 · N432AW · Cndair CL6002B19 · Fuel Controlling SystemSDR A6WA200440068Bushing · wornMUC 44 LT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .020. REMOVED AND REPLACED LT MAIN LANDING GEAR AFT TRUNNION BUSHING IAW MFG REO 601R5721003 REV B.May 27, 2004 · N432AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA200440065Angle · crackedCLIP ANGLE AT FS 280.0 IB SIDE OF RBL 9 IS CRACKED. REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE PN 601R31113-58 IAW CRJ SRM 51-42-06 AND 51-42-21.May 21, 2004 · N432AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440064Frame · crackedRT 718 FRAME FLANGE BETWEEN STRINGERS 11 AND 12 IS CRACKED. REPAIRED RT 718 LOWER FRAME FLANGE AT STRINGERS 11 AND 12 IAW MFG REO 601R-53-61-193 REV A.May 21, 2004 · N432AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA200440007Window · failedAT 33,000 FEET, LEFT SIDE WINDOW SHATTERED 'PRESSURIZATION SPIKED DOWN 500 FEET THEN STABILIZED. AIRCRAFT EN ROUTE FROM ICT TO ATL. REMOVED AND REPLACED LEFT SIDE WINDOW PER AMM 56-12-01. (M)Jan 13, 2004 · N432AW · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA200340171Warning Light · false activationRIGHT PACK HI PRESSURE CAUTION MESSAGE. PERFORMED PACK OPS CHECK WITH ENGINES IAW AMM 21-50-863-805 AND PERFORMED OPS CHECK IAW AMM 21-50-863-801. OPS CHECK GOOD. OK FOR SERVICE. (M)Nov 16, 2003 · N432AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA200340159Warning Light · false indicationABORTED TAKEOFF AT 100 KNOTS DUE TO APU WARNING (HI-TEMP) TEMP 999 DEGREES FOLLOWED BY AMBER CAS MESSAGE APU OIL PRESSURE. NORMAL BRAKING APPLIED. INSPECTED APU, NO VISUAL SIGNS ON APU FIRE. INSPECTED TAILPIPE, NO EVIDENCE OF APU DAMAGE, COMPLIED WITH RTO INov 7, 2003 · N432AW · Cndair CL6002B19 · Overheat DetectionSDR A6WA200340138Odor · detectedSTRONG BURNING SULFUR ODOR IN FLIGHT. COMPLIED WITH PACK BURN OUT PROCEDURE. NO SMELLS OR DEFECTS NOTED AT THIS TIME. INSPECTED AVIONICS AND APU BAY, NO DEFECTS NOTED. AIRCRAFT OK FOR CONTINUED SERVICE. (M)Sep 10, 2003 · N432AW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA200340134Smoke Detector · malfunctionedCARGO SMOKE MESSAGE INTERMITTENT DURING FLIGHT AT 20,000 FT COMPLIED WITH EMERGENCY ACTION CHECKLIST. REMOVED AND REPLACED NR 2 FIRE BOTTLE (REF BLK 2) SEE 116092/2 FOR MEL. FIRE DEPARTMENT FOUND NO EVIDENCE OF SMOKE OR FUMES. SMOKE DETECTION SYSTEM, OPS TESep 9, 2003 · N432AW · Cndair CL6002B19 · Smoke DetectionSDR A6WA200340003Strut · lowRECEIVED NOSE GEAR OPEN WARNING IN FLIGHT AND GEAR DISAGREE MESSAGE IN FLIGHT. SERVICED STRUT. (M)Dec 18, 2002 · N432AW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR A6WA200340001Uplock Sensor · malfunctionedAFTER TAKEOFF WITH GEAR HANDLE UP, GEAR UP DISAGREE AND NOSE DOOR OPEN MESSAGES ILLUMINATED. REMOVED AND REPLACED NOSE LANDING GEAR UPLOCK SENSOR. (M)Dec 14, 2002 · N432AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR MDR02030Frame · crackedLEFT FS 718.0 FRAME IS CRACKED AT STRINGER 11L, CRACK IS .5 INCH LONG.Oct 9, 2002 · N432AW · Cndair CL6002B19 · Fuselage Main, FrameSDR MDR02028Floor Support · crackedDURING BRIDGING INSPECTION, FOUND RIGHT HAND SIDE CARGO FLOOR SUPPORT ANGLE IS CRACKED AT FS 621.00.Oct 9, 2002 · N432AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR MDR02027Floor Support · crackedDURING BRIDGING INSPECTION FOUND LEFT HAND SIDE CARGO FLOOR SUPPORT ANGLE IS CRACKED AT FS621.00.Oct 9, 2002 · N432AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR MDR02026Skin · dentedDURING BRIDGING INSPECTION, FOUND DENT IN FUSELAGE AT FS 605.00, WL 86, .010 DEEP BY 1 INCH LONG.Oct 9, 2002 · N432AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR MDR02025Skin · nickedDURING BRIDGING INSPECTION, FOUND NICK IN SKIN BELOW CARGO DOOR, FS 605.00 WL 89.00.Oct 9, 2002 · N432AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR MDR02024Floor Support · crackedDURING BRIDGING INSPECTION DISCOVERED FLOOR SUPPORT ANGLE AT FS484, LBL34, WL73.1 CRACKED.Oct 9, 2002 · N432AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR MDR02023Floor Support · crackedDURING BRIDGING INSPECTION DISCOVERED FLOOR SUPPORT ANGLE AT FS 484, LBL27, WL73.1 CRACKED.Oct 9, 2002 · N432AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR MDR02022Frame · crackedDURING BRIDGING INSPECTION DISCOVERED LEFT FS 718 FRAME CRACKED AT STRINGER 11L, .5 INCHES LONG.Oct 9, 2002 · N432AW · Cndair CL6002B19 · Fuselage Main, FrameSDR MDR02021Angle · crackedDURING BRIDGING INSPECTION DISCOVERED RIGHT UPPER OBLIQUE ANGLE CRACKED IN RADIUS 1.0 INCH AT FS 621-625.3.Oct 9, 2002 · N432AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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