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 A6WA201040140Door · crackedAPU ENCLOSURE DOOR CRACKED TOP CENTER AS MARKED. REPAIRED 3 EA CRACKS IAW REO 601R-49-11-070.Jan 8, 2010 · N432AW · Cndair CL6002B19 · APU Cowling/ContainmentSDR A6WA201040159Bracket · brokenLT JET PIPE FIRE LOOP MOUNT COVER FWD MOUNT STANDOFF BRACKET BROKEN. REMOVED BROKEN BRACKET AND REPALCED WITH FABRICATED BRACKET.Jan 8, 2010 · N432AW · Cndair CL6002B19 · Nacelle/Pylon, Attach FittingsSDR A6WA201040155Angle · crackedLT WING CTR L/E INBD ATTACH ANGLE CRACKED. REMOVED DAMAGED ANGLE, LOCATED FASTENER HOLES IN SERVICEABLE ANGLE AND INSTALLED SERVICEABLE ANGLE IAW SRM 51-41-02.Jan 6, 2010 · N432AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA201040149Angle · crackedINTERCOSTAL ATTACH ANGLE ABOVE LINTEL FITTING ON AFT SIDE OF F/S 621 IS CRACKED. R & R IAW SRM 51-40-00, 53-61-19.Jan 6, 2010 · N432AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040142Pressure Blkhd · chafed10TH STAGE BLEED AIR SHUTOFF VALVE ABOVE APU ENCLOSURE CHAFING CTR BEAM. REO 601R-53-61-1523 BLEND EDDY CURRENT INSPECT TREAT PRIME AND TOP COAT.Jan 5, 2010 · N432AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040162Seat Track · corrodedLT NR 1 FLOOR SEAT TRACK CORRODED. R & R SEAT TRACK.Jan 4, 2010 · N432AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201040160Seat Track · corrodedRT FLOOR SEAT TRACK CORRODED, R & R TRACK.Jan 4, 2010 · N432AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201040144Intercostal · crackedPAX DOOR FWD LOWER CORNER HAS A CRQCKED INTERCOSTAL. DUPLICATED ORIGINAL PART IAW SRM 51-24-21.Jan 4, 2010 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040141Angle · corrodedPAX DOOR AFT CORNER HAS CORROSION. R & R UPPER AND LOWER ANGLES.Jan 4, 2010 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040147Attach Fitting · corrodedPAX DOOR LOWER AFT SIDE AT F/S 329.50 HAS CORROSION ON CLIP. REMOVED OLD CLIP AND FABRICATED NEW CLIP IAW SRM 51-31-59.Dec 31, 2009 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040146Attach Fitting · corrodedPAX DOOR LOWER FWD AT FS 338.00 HAS CORROSION ON CLIP. REMOVED OLD CLIP AND FABRICATED NEW CLIP IAW SRM 51-31-54.Dec 31, 2009 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040143Attach Fitting · corrodedPAX DOOR LOWER FWD SIDE AT F/S 320.10 HAS CORROSION CLIP. REMOVED CORRODED CLIP, FABRICATED NEW CLIP IAW SRM 51-31-59.Dec 31, 2009 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040145Attach Fitting · corrodedPAX DOOR LOWER AFT AT F/S 338.0 JAS CORROSION ON CLIP. REMOVED OLD CLIP, FABRICATED NEW CLIP IAW SRM 51-31-59.Dec 31, 2009 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040148Attach Fitting · corrodedPAX DOOR LOWER AFT SIDE AT F/S 320.10 HAS CORROSION ON CLIP. REMOVED OLD CLIP AND FABRICATED NEW CLIP IAW SRM 51-31-59.Dec 31, 2009 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040156Bracket · crackedLT JETPIPE UPPER INBD ATTACH POINT NUTPLATE BRACKET CRACKED. REMOVED DAMAGED BRACKET, DUPLICATED SERVICEABLE BRACKET IAW CMM 78-11-00, AND INSTALLED SERVICEABLE BRACKET IAW CMM 20-42-06.Dec 30, 2009 · N432AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA201040138Bracket · crackedNUT BRACKET UNDER PANEL 326CL, LT SIDE OF VERTICAL STAB, CRACKED. REMOVED DAMAGED BRACKET AND INSTALLED SERVICEABLE PN 600-21137-5 BRACKET.Dec 7, 2009 · N432AW · Cndair CL6002B19 · Vertical StabilizerSDR A6WA200940303Drag Angle · damagedMWC 137953-7 - FOUR FWD MISALIGNED BOLT HOLES ON LT AND RT TAILCONE DRAG ANGLES. TRIMMED DRAG ANGLES, FABRICATED AND INSTALLED FILLERS AND REPAIR ANGLES IAW EO 601R-53-16986. (K)Jun 8, 2009 · N432AW · Cndair CL6002B19 · Aerodynamic FairingsSDR A6WA200940202Wheel · cracked191210/3 - MAIN TIRE NR 1 FLAT, TIRE WAS NORMAL ON POST FLIGHT WALKAROUND, AGENT FOUND TIRE FLAT PRIOR TO PUSHBACK. WHEEL RIM NR 1 FOUND CRACKED. REMOVED AND REPLACED MAIN TIRE ASSEMBLIES NR 1 AND NR 2. MLG WHEEL ASSY, NR 1 PN 5010571-1, SN DEC03-6173, TSN=Apr 5, 2009 · N432AW · Cndair CL6002B19 · Wheel/Ski/FloatSDR A6WA200940010Duct · leakingLOG 188027/2- AFTER CLIMBOUT RT PACK OVERPRESSURE. COMPLIED WITH QRH. PERFORMED AIR RETURN TO DEPARTURE. REMOVED AND REPLACED LT DUCT ASSY IAW AMM 21-51-15. OPS AND LEAK CHECK GOOD AT THIS TIME. REMOVED PLACARD, REMOVED FROM MEL. (K)Jan 9, 2009 · N432AW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA200840648Unknown · odorLOG 188020/1 STRONG ODOR IN CABIN AND COCKPIT WITH APU AND ENGINE AIR SELECTED ON. DOES NOT DISSIPATE.Dec 20, 2008 · N432AW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA200840639Screen · cokedRT ENGINE OIL PRESSURE WARNING MSG AT CRUISE. WARNING PERSISTED AT POWER SETTINGS ABOVE IDLE. CW QRH DIVERTED TO PHL. ENGINE REMAINED AT IDLE DURING THE 40 MINUTE FLIGHT TO PHL. LOWEST OIL PRESSURE SHOWN WAS 24 PSI. REMOVED RT LUBE SCAVENGE PUMP AND FOUNDDec 10, 2008 · N432AW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA200840555Carbon Seal · leakingIN FLIGHT RT ENG OIL PRESSURE FLUCTUATED BETWEEN 30-45 PSI. ON SHORT FINAL RECEIVED "RT ENG OIL PRESSURE" WARNING MESSAGE, PRESSURE FLUCTUATED BETWEEN 23-33 PSI. ALSO, RECEIVED AURAL "ENG OIL" WARNING. REMOVED AND REPLACED RT ENG INTEGRATED DRIVE GENERATOR Aug 3, 2008 · N432AW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA200740701Plate · corrodedSERVICE DOOR PLATE FIND CORRODED, OUT OF LIMITS IAW SRM 53-00-00, FIG 101. SERVICE DOOR PLATE REPLACED IAW SRM 51-42-00, 51-41-02, 51-41-04. (K)Dec 18, 2007 · N432AW · Cndair CL6002B19 · Service DoorsSDR A6WA200740700Bracket · crackedCARGO DOOR CONNECTOR BRACKET CRACKED. (K) CARGO DOOR CONNECTOR BRACKET FABRICATED AND INSTALLED IAW SRM 51-24-15 AND 51-42-06.Dec 15, 2007 · N432AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA200740693Nut Clip · crackedFS 484.0 RT SIDE, CLIP FOUND CRACKED ON FLOOR SUPPORT STRUCTURE AT RBL 27.0, FS 484.00, RBL 27.00, FLOOR SUPPORT CLIP REPLACED IAW SRM 51-42-16, 51-21-16 AND SRM 51-42-06. (K)Dec 13, 2007 · N432AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740692Bulkhead · crackedCRACK ON FWD PRESSURE BULKHEAD AROUND PARKING BRAKE AT FS 202.00 LT LBL 23.00. CRACK ON FWD PRESSURE BULKHEAD AROUND PARKING BRAKE REPAIRED IAW REO 601R53-11-563. (K)Dec 13, 2007 · N432AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200740698Diaphragm · crackedDIAPHRAGM CRACK UNDER FWD UPPER PAX DOOR CORNER COVER. (K) BRACKET CRACKED UNDER FWD UPPER PAX DOOR CORNER COVER REPLACED IAW SRM 51-42-06.Dec 12, 2007 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740689Bracket · crackedBRACKET CRACK ON LOWER PAX DOOR EDGE (LOCK MECHANISM AREA) AFT STA 334.00. CRACKED BRACKET ON PAX DOOR BTW FS 329.5 TO FS 338.0 IS REPLACED IAW SRM 51-41-04. (K)Dec 11, 2007 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740705Intercostal · crackedCRACK SUSPECTED ON AC CONNECTOR BOX. CRACK CONFIRMED BY EDDY CURRENT INSPECTION. INTERCOSTAL AND RECEPTACLE SUPPORT REPLACED IAW SRM 51-42-06. (K)Dec 10, 2007 · N432AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740688Cover · crackedAFT UPPER CORNER COVER CRACK ON PAX DOOR. (K) AFT UPPER CORNER COVER REPLACED IAW SRM 51-42-13. (K)Dec 10, 2007 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740687Structure · crackedFWD UPPER CORNER COVER CRACK ON PAX DOOR. (K) FWD UPPER CORNER COVER OF PAX DOOR REPLACED IAW SRM 51-42-13.Dec 10, 2007 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740686Structure · gougedFWD PAX DOOR PULL IN LEVEL GOUGED PULL IN LEVEL GOUGED .070 INCH AND ALLOWABLE MAXIMUM .050 INCH IAW REO 601R-52-11-524. (K) FWD PAX DOOR PULL IN LEVER REPAIRED IAW REO 601R-52-11-524.Dec 10, 2007 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740685Structure · crackedEDGE MEMBER CRACK ON PAX DOOR AT FOLDING STEP HINGE. (K) PAX DOOR EDGE MEMBER FABRICATED IAW SRM 51-24-26 AND INSTALL IAW SRM 51-42-13.Dec 10, 2007 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740699Floor Panel · corrodedCORROSION EXIST ON FLOOR STRUCTURE FS 280, LBL 9 TO RBL 9. PERFORMED ON FLOOR STRUCTURE FS 280, LBL 9 TO RBL 9 IAW REO 601R-53-11-926. (K)Dec 10, 2007 · N432AW · Cndair CL6002B19 · Fuselage Floor PanelSDR A6WA200740697Support Bracket · crackedRT HYDRAULIC SUPPORT BRACKET AT FS 718 IS CRACKED. RT HYDRAULIC SUPPORT BRACKET AF FS 718 IS CRACKED. (K)Dec 10, 2007 · N432AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740696Intercostal · crackedLT INTERCOSTAL CLIP AT FS 621.0 TO FS 625.0 IS CRACKED. INTERCOSTAL CLIP AT FS 621.0 TO FS 625.0 LT REPLACED IAW SRM 51-42-20. (K)Dec 10, 2007 · N432AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740695Drag Angle · crackedCRACK FOUND ON AFT ATTACH ANGLE OF PAX DOOR (DRAG ANGLE). AFT ATTACH ANGLE OF PAX DOOR REPAIRED IAW REO 61R-52-11-513 REV A. (K)Dec 10, 2007 · N432AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740694Intercostal · crackedCRACK FOUND ON INTERCOSTAL FS 484, LBL 27 AND LBL 36, WL 72.00. INTERCOSTAL AT FS 484, LBL 27 AND LBL 36 AT WL 72.00. REPAIRED IAW REO 601R-53-41-059 REV A AND SRM 51-24-16, 51-21-16 AND SRM 51-42-06. (K)Dec 10, 2007 · N432AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740691Skin · damagedON MLG DOOR RIGHT INNER SKIN, ABRASION EXIST ON FORWARD SIDE OF DOOR, LOWER AND UPPER. (M) REPAIRED IAW REO 601R-52-82-016 AND REO 601R-52-82-102. (K)Dec 10, 2007 · N432AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA200740690Skin · damagedON LT MLG DOOR INNER SKIN, FOUND ABRASION ON FORWARD SIDE OF DOOR, LOWER AND UPPER. (M) REPAIRED IAW REO 601R-52-82-016 AND REO 601R-52-82-102. (K)Dec 10, 2007 · N432AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA200740337Intercostal · crackedRT FS 625 OBLIQUE ANGLE IS CRACKED APPROX 1 INCH L. MAINTENANCE REMOVED AND REPLACED ANGLE IAW SRM 51-42-21 AND REO 601R-53-61-422. (K)Jun 23, 2007 · N432AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740152Skin · ground damageLAV TRUCK HIT AC - 4 INCH HOLE IN FUSELAGE FS 615, WL 73. MAINTENANCE PERFORMED A MAJOR REPAIR BY CUTTING AWAY DAMAGED SKIN AND INSTALLING A 14 INCH X 8 INCH EXTERNAL REPAIR DOUBLER IAW EO 601R-11202. (K)Mar 19, 2007 · N432AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200540381Clip · crackedFS 280 FRAME CLIP AT LBL 9 IB IS CRACKED. MAINTENANCE REPLACED CLIP PN 601R3111357 IAW SRM. (K)Dec 30, 2005 · N432AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540376Clip · crackedFS 280 FRAME CLIP AT LBL 9 OB IS CRACKED. MAINTENANCE REPLACED CLIP (PN 601R3111357) IAW SRM. (K)Dec 30, 2005 · N432AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540375Clip · crackedFS280 FRAME CLIP AT RBL 9 ON OB SIDE IS CRACKED. MAINTENANCE REPLACED CLIP (PN 601R3111358) IAW SRM. (K)Dec 30, 2005 · N432AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540374Skin · corrodedLT LOWER WING PLANK HOLE NR 7, WS 166.366 HAS CORROSION ON IB SIDE 4 INCH L X .002 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED LT WING PLANK ACCESS HOLE NR 7 IAW REO. (K)Dec 30, 2005 · N432AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540370Skin · corrodedRT WING LOWER PLANK HOLE NR 16, WS 303.861 HAS CORROSION AT IB SIDE 1 INCH L X .005 INCH D. NOT CRITICAL. MAINTENANCE REPAIRED RT LWR WING PLANK ACCESS HOLE NR 16 IAW REO. (K)Dec 30, 2005 · N432AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540369Skin · corrodedRT WING LWR PLANK HOLE NR 7, WS 116.366 HAS CORROSION AT IB SIDE 2 INCHES L X .005 INCH DEEP AND FWD SIDE .5 INCH L X .005 INCH D, NOT IN CRITICAL AREA. MAINTENANCE REPAIRED RT LWR WING PLANK ACCESS HOLE NR 7 IAW REO. (K)Dec 30, 2005 · N432AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540368Skin · corrodedRT WING LOWER PLANK HOLE NR 5 WS 76.161 HAS CORROSION AT IB FORWARD SIDE 4 INCHES L X .002 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED RT WING LOWER WING PLANK ACCESS HOLE NR 5 IAW REO. (K)Dec 30, 2005 · N432AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540371Skin · corrodedLT LWR WING PLANK HOLE NR 2, WS 12.245 HAS CORROSION AT OB SIDE AFT 2 INCH L X .005 INCH D AND AT IB SIDE 8 INCHES L X .005 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 2 IAW REO. (K)Dec 30, 2005 · N432AW · Cndair CL6002B19 · Wing, Plate/Skin
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