N453AW

Service difficulty reports · 152

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 = 'N453AW' 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 A6WA201040862Fitting · chafedLT OTBD FLAP ALIGNMENT GUIDE ROLLER FITTING HAS CHAFING DAMAGE BLENDED OUT CHAFED DAMAGE IAW B/A REO 601R-57-53-835 AND SRM 51-12-00.Oct 23, 2010 · N453AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040855Shaft · dentedLT INBD VANE ACTUATOR SHAFT DENTED FROM ROLLERS. EXCESSIVELY BLENDED ACTUATOR SHAFT FOUND TO BE WITHIN LIMITS IAW BA REO 601R-57-52-1640.Oct 23, 2010 · N453AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA201040798Angle · crackedFOUND INBD CAP ANGLE AY FS559 & RBL 9 CRACKED. REPAIRED CRACKED CAP ANGLE AT FS 559 & RBL 9 BY FULL INCORPORATION OF REO 601R-53-41-260, REV E. INCLUDING DEVIATION REO 601R-53-41-609, REV B DEVIATION E TO THE FS 559 PRESSURE BULKHEAD LT & RT SIDES FROM LBL 27Oct 23, 2010 · N453AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040797Floorbeam · crackedINBD FLOORBEAM CLIP ON LBL 9 AT FS 280 IS CRACKED. R & R PN 601R31113-57 AT OTBD LBL FS 280 IAW SRM 51-42-21.Oct 22, 2010 · N453AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201040796Pressure Panel · gougedRT FUSELAGE PRESSURE PANEL CUT OUT HAS TOOLING MARKS AROUND A HOLE LOCATED AT THE 3 O`CLOCK POSITION. BLENDED OUT TOOL MARKS AROUND A HOLE LOCATED AT THE 3 O`CLOCK POSITION ON RT PRESSURE PANEL (132AL) OPENING IAW REO 601R-53-11-2002.Oct 22, 2010 · N453AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040859Fitting · crackedBATHTUB FITTING AT RBL9, FS 461 CRACKED PN 600-31068-19. REPLACED BATHTUB FITTING WITH SERVICEABLE FITTING IAW SRM 51-42-21, 51-42-06.Oct 21, 2010 · N453AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201040790Skin · chafedLT MLG LOWER L/E CHAFING DAMAGE. REPAIRED LT MLG LOWER L/E IAW REO 601R-52-82-034 NC.Oct 21, 2010 · N453AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201040791Angle · crackedRT FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED UNSERVICEABLE OBLIQUE ANGLE FROM RT FS 625 AND INSTALLED SERVICEABLE ANGLE IAW SRM 51-42-21 AND REO 601R-53-61-985.Oct 21, 2010 · N453AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040860Attach Fitting · crackedLT OTBD 484.00 CLIP CRACKED. FATRICATED CLIP AND INSTALLED SERVICEABLE CLIP IAW REO 601R-53-41-059, REV B.Oct 20, 2010 · N453AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201040793Skin · chafedSKIN ON FUSELAGE AT RT STUB FAIRING IS CHAFED. REPAIRED DAMAGE AREA IAW REO 601R-53-41-341, REV C.Oct 20, 2010 · N453AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA201040792Angle · crackedLT FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED UNSERVICEABLE OBLIQUE ANGLE FROM LT FS 625 AND INSTALLED SERVICEABLE ANGLE IAW SRM 51-42-21 AND REO 601R-53-61-985.Oct 20, 2010 · N453AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040854Intercostal · crackedUPPER AFT INTERCOSTAL ON PAX DOOR IS CRACKED. REPLACED CRACKED INTERCOSTAL DOUBLER WITH NEW SERVICEABLE PN 601R318094-2, IAW SRM 51-40-11, 51-42-06.Oct 19, 2010 · N453AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040794Skin · chafedENTIRE TOP SIDE OF LT AILERON L/E IS CHAFED. REPAIRED THE CHAFED ON ENTIRE TOP SIDE OF LT AILERON L/E IAW MFG 601R-57-60-013 REV NC.Oct 19, 2010 · N453AW · Cndair CL6002B19 · AileronsSDR A6WA201040021Connector · contaminatedON ARRIVAL THE FLAPS FAILED AT 20 DEGREES WHEN ATTEMPTED TO SELECT 30 DEGREES. INITIATED A GO-AROUND AND COMPLIED WITH THE QRH THEN MADE A 20 DEGREE FLAP LANDING. AN EMERGENCY WAS DECLARED. AS PART OF FLAP FAIL TROUBLESHOOTING: MEGOHM CKD TRANSDUCER CIRCUITJan 11, 2010 · N453AW · Cndair CL6002B19 · Flight Control System WiringSDR A6WA200940333Ecu · malfunctionedTROUBLESHOT APU ECU. FAULT CODES INDICATED INTERNAL ECU FAULT. REMOVED AND REPLACED ECU IAW AMM 49-61-01. OPS CHECKS GOOD. FUEL ODOR DISSIPATED AFTER APU AND PACKS WERE OPERATED. (K)Jun 24, 2009 · N453AW · Cndair CL6002B19 · APU ControlsSDR A6WA200940214Ground Wire · damagedGENERATOR 2 AND IDG CAUTION MESSAGE ON CLIMB-OUT, COMPLIED WITH QRH. SERVICED NR IDG IAW 12-12-24, REPAIRED RT ENGINE IDG TEMP BULB GROUND WIRE (P22EZ) IAW ESPM 20. CONNECTED IDG NR 2 IAW AMM 24-11-01. OPS CHECK GOOD AT THIS TIME. IDG NR 2 TOOK 13 PUMPS. Apr 15, 2009 · N453AW · Cndair CL6002B19 · Electrical Power System WiringSDR A6WA200940203Controller · malfunctioned190224/2 - LT WINDSHIELD HEAT CAUTION LIGHT ON EICAS AND WILL NOT RESET. RETURNED TO DEPARTURE. REMOVED AND REPLACED LT WINDSHIELD TEMP CONTROLLER IAW AMM 30-41 & PLACED LT WINDSHIELD ON BACKUP SENSOR IAW AMM 30-41. OPS CHECK GOOD. (K)Apr 6, 2009 · N453AW · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR A6WA200940158Engine · seized190219/1 - (AT GATE) DETECTED STRONG ACRID ELECTRICAL BURNING ODOR FOLLOWED BY APU AUTO SHUTDOWN, GRND SUPERVISOR EXCESS SMOKE FROM APU EXHAUST AFTER APU SHUTDOWN. FA REPORTED POP PRIOR TO APU. FOUND APU SEIZED, APU DOOR IS CLOSED NO SMELL OF ANY KIND EVIDENMar 23, 2009 · N453AW · Cndair CL6002B19 · APU Core EngineSDR A6WA200940177Apu · seizedDETECTED STRONG ACRID ELECTRICAL BURNING SMELL FOLLOWED APU AUTO SHUTDOWN, GROUND SUPERVISOR EXCESS SMOKE FROM APU EXHAUST AFTER APU SHUTDOWN. F/A REPORTED POP PRIOR TO APU SHUTDOWN. FOUND APU SEIZED APU DOOR IS CLOSED, NO SMELL OF ANY KIND EVIDENT WITH APU.Mar 23, 2009 · N453AW · Cndair CL6002B19 · APU Core EngineSDR A6WA200940210Bulkhead · crackedMWC 133218-23 FWD PRESSURE BULKHEAD AT FS202.75 FOUND CRACKED AT PARKING BRAKE LOCATION. CUTOUT PERFORMED ON CRACKED PORTION OF FWD BULKHEAD, EDDY CURRENT PERFORMED ON CUTOUT IAW REO 601R-53-11-563. REPAIR PERFORMED IAW REO601R-53-11-563. (K)Mar 16, 2009 · N453AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940211Support Bracket · crackedHYD SUPPORT BRACKET IN LT SIDE MLG BAY FOUND CRACKED. HYD SUPPORT BRACKET IN LT MLG BAY REPLACED IAW SRM 51-42-06. (K)Mar 13, 2009 · N453AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940212Attach Fitting · crackedMWC 133218 - ATTACH FITTING CRACKED AT INTERCOSTAL F/S 484.0 RBL 27.0 UNDER FLOOR STRUCTURE. FITTING REPLACED AT INTERCOSTAL FS 484.0, RBL 27.0 IAW CRJ 200 SRM 51-42-10, 51-42-21. (K)Mar 13, 2009 · N453AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940130Panel · crackedPAX DOOR AFT SIDE PANEL CRACKED IN ZONE Z (CRACK LENGTH .500) REF REO 601R-52-11-702, REV A. REPAIR ON AFT SIDE PANEL OF PAX DOOR PERFORMED IAW REO 601R-52-11-702, REV A. (K)Mar 11, 2009 · N453AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200940135Sill · crackedCRACK FOUND ON CARGO DOOR LOWER SILL, FS 574 (CRACK LENGTH .400 INCH). REPAIRED ON CARGO DOOR LOWER SILL PERFORMED IAW REO 601R-53-61-1741. (K)Mar 11, 2009 · N453AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940152Bulkhead · crackedCRACK FOUND ON AFT ANGLE OF PILOT BULKHEAD FS 280, LBL 9 CRACK LENGTH IS .500. REPAIR ON ANGLE OF PILOT BULKHEAD FS 28000, LBL 9 C/O IAW REO 601R-53-11-138. (K)Mar 10, 2009 · N453AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940151Floorbeam · crackedCRACK FOUND ON CLIPS FS 280, LBL 9 (2 CRACKS, LENGTH IS .500) CLIP CHANGED ON FS 280.00, LBL 9 IAW SRM 51-42-06 AND 51-42-21. (K)Mar 10, 2009 · N453AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940131Structure · crackedPASSENGER DOOR EDGE MEMBER AFT SIDE FOUND CRACKED. (CRACK LENGTH .500) REPAIR PAX DOOR EDGE MEMBER IAW REO 601R-52-11-279. (K)Mar 10, 2009 · N453AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200940129Panel · crackedPAX DOOR FWD SIDE PANEL CRACKED IN ZONE 2 (CRACK LENGTH .460) REF REO 601R-52-702, REV A. REPAIR ON FWD FWD SIDE OF PAX DOOR PANEL PERFORMED IAW REO 601R-52-11-702, REV A. (K)Mar 10, 2009 · N453AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200940134Floorbeam · crackedCRACK FOUND ON CLIP FS 280, RBL 9 (CRACK LENGTH IS .500) CLIP FS 280.00 RBL 9 FABRICATED IAW SRM 52-24-16 AND INSTALLED IAW SRM 51-42-06 AND 51-42-21. (K)Mar 10, 2009 · N453AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940132Bulkhead · crackedCRACK FOUND ON PILOT BULKHEAD FS 280, RBL 9 (CRACK LENGTHIS .500). REPAIR TO PILOTS BULKHEAD FS 280, RBL 9 DONE IAW REO 601R-53-11-171, REV D. (K)Mar 10, 2009 · N453AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940133Bulkhead · crackedAFT PRESSURE BULKHEAD AT F/S 621.00 FOUND CRACKED AT LINTEL FITTING LOCATION. REPAIR TO AFT PRESSURE BULKHEAD AT FS 621.00 CARRIED OUT IAW REO 601R-53-61-1230, REV D. (K)Mar 9, 2009 · N453AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940111Priority Valve · failedAFTER T/O GEAR DISAGREE WITH NOSE GEAR SHOWING NOT STOWED C/W QRH RETURN TO DEPARTURE (APPROX 15 SECONDS AFTER SELECTING GEAR UP WARNING CAME ON.) FOUND PRIORITY VALVE FAILING TEST REF 32-30-00, REMOVED AND REPLACED NLG PRIORITY VALVE IAW AMM 32-33-15, OPS CHMar 4, 2009 · N453AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA200940109Strut · failedAFTER T/O GEAR DISAGREE AND NLG DOOR OPER WARNING MSG APPEARED AT ACCELLERATION ALTITUDE MSGS CLEARED AND NOSE GEAR RETRACTED NORMALLY. BOTH MAINS UP AND LOCKED. INTERROGATED PSCU FOUND CODES SHOWING NLG DIDN`T EXTEND. REPACKED NLG SHOCK STRUT REF AMM 32-21Mar 3, 2009 · N453AW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR A6WA200940073Blocker Door · missingLT THRUST REVERSER BLOCKER DOOR NR 8 MISSING. REMOVED AND REPLACED LT ENGINE THRUST REVERSER BLOCKER DOOR NR 8, SPRING BOX SUPPORT AND LOCK ASSY AND LT DIVERTER FAIRING ASSY IAW AMM REF 78-33-21 AND CMM 78-30-00, THRUST REVERSER CK OK IAW AMM 71-00-00-710-806Feb 19, 2009 · N453AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA200840224Control System · malfunctionedON TAKEOFF ROLL, FULL RUDDER DEFLECTION UNABLE TO MAINTAIN CENTERLINE. ABORTED TAKEOFF AT APPROXIMATELY 60 KNOTS, MAX BTMS READING = 2. CROSSWING ABOUT 10 KNOTS. OPS CHECK OF NWS IAW 32-51-00. OP CHECK GOOD. PERFORMED OPS CHECK OF RUDDER CONTROL SYSTEM IAMar 20, 2008 · N453AW · Cndair CL6002B19 · Rudder Control SystemSDR AA6WA200840150Strut · underservicedON TAKEOFF RECEIVED NWS INOP AND GEAR DISAGREE, COMPLIED WITH QRH. GEAR DISAGREE ILLUMINATED APPROX 30 SECS. AFTER GEAR UP SELECTION. RETURNED FOR LANDING, LANDING WEIGHT= 41,000 LBS., MAX BTMS=2,2,2,2. SERVICE NOSE GEAR STRUT IAW 12-12-32 OPS CHECK GOOD, Mar 4, 2008 · N453AW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR A6WA200740682Filter · inoperativeRT PACK HIGH PRESS CAUTION MESSAGE ON TAKEOFF ROLL, ABORTED TAKEOFF AT APPROXIMATELY 20 KNOTS, BTMS READINGS=2,2,1,2. REMOVED AND REPLACED RT ENGINE PRESSURE REGULATING SHUTOFF VALVE FILTER, REF AMM 21-51-43 AND AWAC SUPPLEMENT 06-039. (K)Dec 16, 2007 · N453AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA200740599Control Unit · malfunctionedSTAB CHANNEL 1 DIS-ENGAGED NUMEROUS TIMES IN FLIGHT. REMOVED AND REPLACED MCU IAW 27-42-05, OPS CHECK GOOD. (M)Nov 5, 2007 · N453AW · Cndair CL6002B19 · Stabilizer Control SystemSDR A6WA200740442Element · malfunctionedLT 14TH DUCT MESSAGE INTERMITTENT, INFLIGHT. COMPLIED WITH QRH. REMOVED AND REPLACED LEFT PYLON SENSING ELEMENT IAW AMM 36-21-04. TEST GOOD AT THIS TIME. (M)Aug 9, 2007 · N453AW · Cndair CL6002B19 · Overheat DetectionSDR A6WA200740287Flap System · unknownON APPROACH INTO LGA, FLAP FAIL CAUTION ILLUMINATED FLAPS AT 30 DEGREES, COMPLIED WITH Q2RH. TOUCHDOWN AT 138 KNOTS, LANDING WEIGHT = 45,020 MAX BTMS READING = 6, 5, 6, 6. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4, FLAPS REJun 8, 2007 · N453AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200740286Shutoff Valve · malfunctionedLT PACK OVERPRESSURE ON CLIMB-OUT OF 5000 FT, RESET PACK UPON CLIMBING LT PACK OVERTEMP MESSAGE. AIR RETURN TO ORF. LANDING WEIGHT = 41,300. MAX BTMS = 4. REMOVED AND REPLACED LT PRSOV IAW 21-51-43, OPS AND LEAK CHECK GOOD. AIRCRAFT LANDING WEIGHT WITHIN Jun 6, 2007 · N453AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA200740123Skin · corrodedRT WING PLANK ACCESS HOLE NR6 HAS MINOR PITTING IN CRITICAL AND NOT CRITICAL AREAS. MAINTENANCE REPAIRED RT WING PLANK ACCESS HOLE NR6 UNDER FUEL ACCESS PANEL 640 DB IAW REO 601R-57-21-030 REV D AND AWAC E06/021-457. (K)Mar 10, 2007 · N453AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740122Drag Angle · crackedPAX DOOR AFT DRAG ANGLE IS CRACKED. REPAIRED IAW REO 601R-52-11-513, REV A. (K)Mar 8, 2007 · N453AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740102Intercostal · crackedINTERCOSTAL CRACKED AT FS484.0, LBL 36.0. MAINTENANCE CUT AWAY DAMAGED FLANGE AND INSTALLED REPAIR ANGLE IAW BSC SR 601R-53-0030A AND REO 601R-53-41-059, REV A. (K)Mar 2, 2007 · N453AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740101Intercostal · crackedINTERCOSTAL CRACKED AT FS484.0, RBL 36.0. MAINTENANCE CUT AWAY DAMAGED FLANGE AND INSTALLED REPAIR ANGLE IAW BSC SR 601-53-0030A AND REO 601R-53-41-059, REV A. (K)Mar 2, 2007 · N453AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740100Floor Support · crackedFLOOR SUPPORT ANGLE AT FS 621 IS CRACKED (RT). MAINTENANCE REPAIRED RT FLOOR SUPPORT ANGLE IAW REO 601R-53-61-117, REV C. (K)Mar 2, 2007 · N453AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740099Floorbeam · crackedFLOOR SUPPORT ANGLE AT FS621.0 IS CRACKED (LT) MAINTENANCE REPAIRED LT FS621 FLOOR SUPPORT ANGLE IAW REO 601R-53-61-117, REV C. (K)Mar 2, 2007 · N453AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740089Intercostal · crackedLT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.2 INCH LONG. MAINTENANCE REMOVED AND REPLACED LT INTERCOSTAL PN 601-35012-51 IAW SRM 51-42-06. (K)Feb 28, 2007 · N453AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740088Intercostal · crackedRT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX 1.2 INCH LONG. MAINTENANCE REPLACED INTERCOSTAL PN 601-35012-52 IAW SRM 51-42-06. (K)Feb 28, 2007 · N453AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640415Flap System · unknownFLAPS FAILED AT 30 DEGREES, FOLLOWED QRH, COMPLIED WITH LANDING REQUIREMENT FOR LANDING FLAPS 30. RESET FLAPS C-B PER AMM SUPP 98-018A, PLACED ON 72 HOURS FLAP WATCH. (M)Dec 18, 2006 · N453AW · Cndair CL6002B19 · Trailing Edge Flap Control System
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