N455AW

Service difficulty reports · 202

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 = 'N455AW' 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 A6WA201140192Panel · corrodedFUEL PANEL 510AB HAS FRETTING, CORROSION. REPAIRED FWD PANEL CUT OUT 510AB IAW REO 601R-57-21-030, REV H.Mar 9, 2011 · N455AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA201140187Seal · damagedLT THRUST REVERSER FWD GRAY SEAL DAMAGED. REMOVED UNDERSERVICEABLE GRAY SEAL AND REPLACED WITH SERVICEABLE GRAY SEAL. LT THRUST REVERSER FWD IAW REO 601R-78-30-4057, REV NC.Mar 9, 2011 · N455AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201140190Structure · gougedLT THRUST REVERSER HAS 2 GOUGES UNDER GRAY SEAL. REPAIRED 2 GOUGES IN LT THRUST REVERSER UNDER GRAY SEAL IAW REO 601R-78-30-4051, REV NC.Mar 9, 2011 · N455AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201140185Skin · erodedLT ENGINE NOSE COWL LIP SKIN PITTED & ERODED. REPAIRED LT ENGINE NOSE INLET COWL LIP SKIN IAW REO 601R-71-61-2532, REV C.Mar 8, 2011 · N455AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201140227Panel · chafedLT AILERON PANEL 599AB CHAFED. REPAIRED LT AILERON LWR L/E PANEL 599AB IAW REO 601R-57-60-020.Mar 6, 2011 · N455AW · Cndair CL6002B19 · AileronsSDR A6WA201140226Panel · chafedLT AILERON PANEL 599BB CHAFED. REPAIRED LT AILERON LWR L/E PANEL 599BB IAW REO 601R-57-60-020.Mar 6, 2011 · N455AW · Cndair CL6002B19 · AileronsSDR A6WA201140191Plate · chafedLT INBD FLAP INBD HINGE LUG PLATE CHAFED. REPAIRED IAW REO 601R-57-15-3, TYPE 1, ZONE A.Mar 4, 2011 · N455AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201140180Skin · chafedLT INBD FLAP VANE L/E CHAFED AT 3 LOCATIONS. REPAIRED 3EA LOCATIONS ON LT INBD FLAP VANE L/E IAW REO 601R-57-52-0004, REV C.Mar 3, 2011 · N455AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201140043Actuator · malfunctionedLT THRUST REVERSER UNLOCK MSG IN FLIGHT, C/W`D QRH DIVERTED TO PIT. RESET ALL 4 BALLSCREW ACTUATORS TO PROPER POSITIONS AND REZEROED ON DOG STOPS. RECONNECTED TO TRACKS AND INSTALLED FLEX DRIVES IAW AMM 78-32-01. OPS CHECKED GOOD.Jan 16, 2011 · N455AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201040627Channel · damagedLT OTBD FLAP DAMAGED AT INBD T/E. REMOVED UNSERVICEABLE T/E CHANNEL AND REPLACED FOR NEW SERVICEABLE CHANNEL.Aug 18, 2010 · N455AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040589Bulkhead Web · chafedRT PAX INLET 12 O`CLOCK INSP DOOR HOLES ELONGATED AND AREA AROUND IS CHAFED/ GOUGED. REMOVED DAMAGED WEB SECTION AND REPAIRED IAW SHORTS CMM 71-61-101.Aug 7, 2010 · N455AW · Cndair CL6002B19 · Nacelle/Pylon, Bulkhead/FirewallSDR A6WA201040588Angle · crackedLT OBLIQUE ANGLE CRACKED. R & R LT OBLIQUE ANGLE IAW SRM 51-42-06, SRM 51-42-21, AND REO 601R-53-61-422.Aug 6, 2010 · N455AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040312Engine · failedWHILE IN CRUISE AT 30,000 FT HEARD BOOM WITH RT ENG ITT CLIMBING ABOVE 900C AT SAME TIME FELT ACFT YAW AND RECEIVED "FUEL LOW PRESS" MSG. EMERGENCY DECLARED PERFORMED ENGINE SHUTDOWN OF RT ENGINE AIR DIVERSION W/NORMAL LANDING RT ENG SHUTDOWN FOR 36 MINUTES IApr 25, 2010 · N455AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA200940474Coalescer Bag · contaminatedAFTER BLEED TRANSFERE RECEIVED A STRONG BURNING RUBBER ODOR, APPEARED TO BE MORE IN COCKPIT THAN CABIN. REF WO 142295 W/C 1-5 FOR WORK COMPLETED. ODOR CAUSED BY COMP WASH FLUID THAT WAS NOT PROPERLY BURNED OFF. ALSO CHANGED COALESCER SOCKS. OPS CHECK GOOD.Aug 15, 2009 · N455AW · Cndair CL6002B19 · Humidity Control SystemSDR A6WA200940258Pump · inoperativeHYD SYS NR1 QUANTITY DROPPED TO 25 PERCENT IN FLIGHT. REMOVED AND REPLACED ENG DRIVEN HYD PUMP NR 1 IAW AMM 29-11-01. OPS AND LEAK CHECKS GOOD. (K)May 13, 2009 · N455AW · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR A6WA200940186Structure · crackedCLIP OF FS 280.00, LBL 9.0 INBD AND OTBD FOUND CRACKED IAW SRM 51-42-21. NEW CLIP OF FS 280.00 LBL 9.0 INBD AND OTBD INSTALLED. (K)Apr 7, 2009 · N455AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA200940184Floorbeam · crackedLT PILOT - BULKHEAD FLOOR SUPPORT AT FS 280, LBL 9.0 FOUND CRACKED. REPAIR TO LT PILOT BULKHEAD FLOOR SUPPORT AT FS 280.00 LBL 9.0 CARRIED OUT IAW REO 601R-53-11-171. (K)Apr 7, 2009 · N455AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940183Bracket · crackedMWC 132379-184- PASSENGER DOOR FWD SIDE PANEL, RETAINING BRACKET (REF: PN 601R317727-1) FOUND CRACKED. PASSENGER DOOR FWD SIDE PANEL, RETAINING BRACKET (REF:PN 601R31727-1) REPLACED IAW SRM 51-42-21. (K)Apr 6, 2009 · N455AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200940182Support · crackedCARGO DOOR FWD RAIL LOWER CHANNEL SUPPORT FOUND CRACKED 2 PLACES. CARGO DOOR FWD RAIL LWR SUPPORT REPLACED IAW SRM 51-42-06. (K)Apr 6, 2009 · N455AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940180Panel · crackedMWC 132379-33 - PASSENGER DOOR AFT SIDE PANEL FOUND CRACK (REO 601R-52-11-702, ZONE2) CRACK LENGTH .150. REPAIR TO PASSENGER DOOR AFT SIDE PANEL CARRIED OUT IAW REO 601R -52-11-702, REV A.Apr 3, 2009 · N455AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200940237Sill · corrodedSERVICE DOOR LOWER SILL, SCUFF PLATE FOUND CORRODED. SERVICE DOOR LOWER SILL PLATE REPLACED IAW SRM 51-42-02. (K)Apr 1, 2009 · N455AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940187Support · crackedMWC 132380-46 - RT PILOT BULK SUPPORT AT FS 280.00, RBL 9.0 FOUND CRACKED (.800 LONG). TR PILOT BULK SUPPORT AT FS 280.00, RBL 9.0, REPAIR PERFORMED IAW REO 601R-53-11-171 SCHEME B REV D. (K)Apr 1, 2009 · N455AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940181Panel · crackedMWC 132379-34 - PASSENGER DOOR FWD SIDE PANEL FOUND CRACKED (REF: REO601R-52-11-702, ZONE 2) CRACK LENGTH .180. REPAIR ON PASSENGER DOOR FWD SIDE PANEL PERFORMED IAW REO 601R-52-11-702, REV A. (K)Apr 1, 2009 · N455AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200940185Pressure Blkhd · crackedPRESSURE BULKHEAD CRACK AT FS 202.75 (PARKING BRAKE CUTOUT AND LBL 23.71) FWD PRESSURE BULKHEAD AT FS 202.75, LBL 23.71. REPAIR PERFORMED IAW REO 601R-53-11-563. (K)Apr 1, 2009 · N455AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940179Support Bracket · crackedHYD SUPPORT BRACKET IN RT WHEEL WELL FOUND CRACKED. HYD SUPPORT BRACKET IN RT WHEEL WELL REPLACED IAW SRM 51-42-06. (K)Apr 1, 2009 · N455AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940178Support Bracket · crackedHYD SUPPORT BRACKET IN LT MLG WHEEL WELL FOUND CRACKED. HYD SUPPORT BRACKET IN LT MLG WHEEL WELL REPLACED IAW SRM 51-42-06. (K)Apr 1, 2009 · N455AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940036Latch · dirtyFLIGHT ATTENDANT JUMPSEAT LATCH HARD TO RELEASE. CLEANED AND ADJUSTED FAA JUMPSEAT LATCH AS PER AMM 25-22. OPS CHECK GOOD AT THIS TIME. REMOVED PLACARD AND REMOVED FROM MEL.Jan 26, 2009 · N455AW · Cndair CL6002B19 · Flight Compartment EquipmentSDR A6WA200940022Flap System · failedFLAPS FAILED AT ZERO DEGREES ON ARRIVAL INTO YOW. PERFORMED ZERO FLAP LANDING. BRAKE TEMP NOT OVER 4. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B, STEPS 1.3 AND 1.4. FLAP SYSTEM RESET OK.Jan 20, 2009 · N455AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840621Fire Loop · malfunctionedANTI ICE DUCT WARNING MSG ON TAKEOFF. TAKEOFF ABORTED AT 80 KNOTS, BRAKE TEMPS WERE 5,6,3,3 SYNOPTIC PAGE SHOWS LT FUSELAGE RED. R&R LT FUSELAGE FIRE DETECTION LOOP AS PER AMM 36-21-04, OPS CHECK GOOD AT THIS TIME.Nov 30, 2008 · N455AW · Cndair CL6002B19 · Fire DetectionSDR A6WA200840597Control Unit · failedAT FL280 LANDING CONFIGURATION INDICATION APPEARED AND ACFT NOSED OVER AND BACKUP. FLAP DEGRADE STATUS MSG APPEARED. PERFORMED FLAP FAULT ISOLATION PER AMM 27-50-00 WHICH INDICATED A FAULT WITH SKEW DETECTION SYS. PERFORMED TEST OF SDS SYS PER FIM. NO FAULOct 20, 2008 · N455AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840236Sensor · failedFLAPS FAIL CAUTION MESSAGE ON APPROACH AT ZERO DEGREES, COMPLIED WITH QRH AND NORMAL LANDING. FOUND REPEAT RT BRAKE AND POSITION SENSOR UNIT FAILURES. REMOVED AND REPLACED RT BPSU PER AMM 27. OPS CHECK GOOD. (M)Mar 24, 2008 · N455AW · Cndair CL6002B19 · Landing Gear Brake SystemSDR A6WA200840200Flap System · malfunctionedFLAPS FAIL CAUTION MESSAGE FLAPS FAILED AT 0 DURING EXTENSION. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4 FLAP SYSTEM RESET, OK. (M)Mar 17, 2008 · N455AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840062Flap · failedFLAP FAIL CAS MESSAGE IN FLIGHT, FLAP FAILED AT ZERO DEGREES. LDNG WT= 44,300. APPROX 150 KNTS. MAT BTMS = 5,4,2,2 AND VERTICAL DESCENT RATE LESS THAN 10 FT PM. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPP 98-018B. STEPS 13 AND 1.4, FLAP SYS OK. (K)Feb 10, 2008 · N455AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200740242Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED. (K) [07-17-07] MAINTENANCE REMOVED DAMAGED SECTION OF DRAG ANGLE AND INSTALLED SERVICEABLE SECTION IAW BOMBARDIER REO 601R-52-11-513. (M)May 10, 2007 · N455AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740241Angle · crackedFS 484.0 ANGLE AT LBL 27 IS CRACKED APPROX 1.0 INCH. (K) [07-17-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW BOMBARDIER SRM 601R-53-0029B AND CRJ 200 SRM 51-42-06. (M)May 10, 2007 · N455AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740240Angle · crackedFS 484.0 ANGLE AT RBL 27 IS CRACKED APPROX 1.0 INCH. (K) [07-17-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW BOMBARDIER SR 601R-53-0029B AND CRJ 200 SRM 51-42-06. (M)May 10, 2007 · N455AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740239Angle · crackedFS 484.0 ANGLE AT LBL36 IS CRACKED APPROX 1.0. CORRECTIVE ACTION IN PROGRESS. (K) [07-17-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW BOMBARDIER REO 601R-53-41-059. (M)May 10, 2007 · N455AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740238Angle · crackedFS484.0 ANGLE AT RBL 36 IS CRACKED APPROX 1.0 INCH. (K) [07-17-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW BOMBARDIER REO 601R-53-41-059 AND BSC SR 601R-53-0030A. (M)May 10, 2007 · N455AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740237Floorbeam · crackedFOUND LEFT FS 621 FLOOR SUPPORT ANGLE IS CRACKED 1.25 INCH LONG IN OUTBOARD RADIUS. MAINTENANCE CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW BOMBARDIER REO 601R-53-61-117. (M)May 3, 2007 · N455AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WQA200740237Floorbeam · crackedLT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED 1.2500 INCH LONG IN OB RADIUS. (K)May 3, 2007 · N455AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740236Floorbeam · crackedRT FS 621..00 FLOOR SUPPORT ANGLE IS CRACKED 1.2500 INCH LONG IN OB RADIUS. (K) [07-17-07] MAINTENANCE CUT AWAY DAMAGED AREA AND INSTALLED SERVICEABLE REPAIR IAW BOMBARDIER REO 601R-53-61-117. (M)May 3, 2007 · N455AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740235Angle · crackedLT FS 621.00 AND 625.00 OBLIQUE ANGLE HAS A 1.5 INCH LONG CRACK IN AFT RADIUS. (K) [07-17-07] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE IAW CRJ200 SRM 51-42-06. (M)May 1, 2007 · N455AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740234Angle · crackedRT FS 621.00 TO 625.00 OBLIQUE ANGLE HAS A 1.2500 INCH LONG CRACK IN AFT RADIUS. (K) [07-17-07] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALL NEW ANGLE IAW CRJ200 SRM 51-42-06. (M)May 1, 2007 · N455AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640346Shutoff Valve · malfunctionedIN THE AIR AND ON THE GROUND WITH THRUST LEVERS AT IDLE, BOTH PACKS OFF LINE AND UNABLE TO MAINTAIN PRESSURIZATION. REMOVED AND REPLACED LEFT AND RIGHT PRESSURE REGULATING SHUTOFF VALVE FILTERS IAW AMM SUP 0639, OPS CHECK GOOD. (M)Sep 11, 2006 · N455AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA200640345Actuator · unknownAFTER DISCONNECTION AUTOPILOT ON APPROACH UNABLE TO MOVE CONTROL COLUMN FORWARD AND AFT, EVENTUALLY FIXED ITSELF. REMOVED AND REPLACED ELEVATOR SERVO SERV N/R OFF 13VYD. (M)Sep 11, 2006 · N455AW · Cndair CL6002B19 · Flight ControllerSDR A6WA200640241Bulb · inoperativeGENERATOR NR 1 OFF MESSAGE IN FLIGHT. COMPLIED WITH QRH, COULD NOT RESET. REMOVED AND REPLACED IDG TEMP BULB IAW CRJ AMM 24-13-05, OPS AND LEAK CHECK GOOD AT THIS TIME. (M)Jun 18, 2006 · N455AW · Cndair CL6002B19 · Electrical Power SystemSDR A6WA200540312Control Panel · inoperativeADG INADVERDENTLY DEPLOYED DURING CLIMBOUT, PERFORMED QRH AMBER CAS MESSAGE FOR L WINDOW HEAT, L AOA HEAT, PITOT BASE HEAT ILLUMINATED. ADG POWERED AC ESS BUS. EMERGENCY LIGHTS ILLUMINATED BEFORE ADG DEPLOYMENT. REMOVED AND REPLACED AUTO DEPLOY CONTROL PANESep 30, 2005 · N455AW · Cndair CL6002B19 · Alternator-Generator DriveSDR A6WA200540181Skin · dentedLT IB FLAP HAS A DENT 22 INCHES FROM IB EDGE AND 14 INCHES FROM THE DENT IS 2 INCH X 2 INCH X 0.55 INCH. LOWER SKIN. PERFORMED A MAJOR REPAIR B4 INSTALLING A 8 INCH X 16 INCH NON-FLUSH REPAIR. (K)May 24, 2005 · N455AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200540180Bushing · migratedLT AFT MLG TRUNNION BUSHING MIGRATED .053 INCH. REMOVED LT AFT MLG TRUNNION BUSHING AND INSTALLED NEW SERVICEABLE BUSHING IAW MFG REO. (K)May 19, 2005 · N455AW · Cndair CL6002B19 · Main Landing GearSDR A6WA200540179Bushing · migratedRT AFT MAIN LANDING GEAR TRUNNION BUSHING MIGRATED .058 INCH. REMOVED RT AFT MLG TRUNNION BUSHING AND INSTALLED NEW SERVICEABLE BUSHING IAW MFG REO. (K)May 19, 2005 · N455AW · Cndair CL6002B19 · Main Landing Gear Attach Section
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