N451AW

Service difficulty reports · 161

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 = 'N451AW' 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 A6WA202312198682Unknown · unknownWHEN SELECTING GEAR UP, GEAR DISAGREE. COMPLIED WITH QRH, MESSAGE CLEARED. NORMAL LANDING. NOSE STEERING NORMAL. NOSE GEAR INDICATED DOWN AFTER SELECTING UP, NOSE REMAINED GREEN. AIRCRAFT REMOVED FROM SERVICE. R&R NLG OLEO CENTERED/EXTENDED PROX SENSOR BRACKOct 19, 2023 · N451AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA202305068591Unknown · unknownRH WINDOW SHATTERED IN FLIGHT AT FL280 PRESSURIZATION IS NORMAL CW CRH REQ INSP **********AIRCRAFT REMOVED FROM SERVICE********* IN WORKMay 6, 2023 · N451AW · Cndair CL6002B19 · Window/Windshield SystemSDR A6WA202211168383Wire Harness · failedRECEIVED STEERING INOP, WOW INPUT, AND WOW OUTPUT FAIL MESSAGES DURING INITIAL CLIMB OUT. GEAR WAS UP AND LOCKED. CW QRH. STEERING SELECTED OFF VIA QRH AND WOW MESSAGES REMAINED. WOW MESSAGES CLEARED WHEN SELECTING GEAR DOWN ON APPROACH. AFTER LANDING RENEGAGNov 16, 2022 · N451AW · Cndair CL6002B19 · Landing Gear System WiringSDR A6WA202210228356Relay · failedAPU SOV STATUS PRESENT IN-FLIGHT WITH APU OFF. MESSAGE CLEARED AFTER ENGINE SHUTDOWN. AIRCRAFT REMOVED FROM SERVICE. R&R FUEL CONTROL RELAY IAW 20-22-00. OPS CHECK GOOD.Oct 22, 2022 · N451AW · Cndair CL6002B19 · APU Engine Fuel and ControlSDR A6WA202206288198Nut Plate · elongatedTEMPORARY REPAIR TO THE ELONGATED NUT PLATE HOLE IN FUSELAGE STRUCTURE AT STRINGER 19R BETWEEN FS409+80 - FS409+96. ****AIRCRAFT REMOVED FROM SERVICE *** REPAIRED FUSELAGE SKIN NUT PLATE HOLE AT STRINGER 19R BETWEEN FS409+80 TO FS409+96 REF REO 601R-53-31-128 Jun 28, 2022 · N451AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202206288199Support Angle · corrodedWIRE SUPPORT ANGLE CORRODED AT THE AFT LAV SERVICE POINT. ***AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED BRACKET.Jun 28, 2022 · N451AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202206288203Intercostal · crackedINTERCOSTAL AT FS654 TO FS672.20 FOUND CRACKED. ***AIRCRAFT REMOVED FROM SERVICE **** REPAIRED INTERCOSTAL IAW AWAC SUPPLEMENT 13-085B DATE ISSUED 2/03/2014 AND REO 601R-53-62-225 REV. DATED 2013-09-19.Jun 28, 2022 · N451AW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA202206288201Panel · dentedFS700.00+13 STRINGER 20L+5 INWARD DENT C/T EXTERIOR SIDE OF SKIN PANEL. ***AIRCRAFT REMOVED FROM SERVICE ***** DRESSED BACK DENT IAW DISPOSITION INSTRUCTIONS OUTLINED IN REO 601R-53-61-7829 REV DATED 2022-05-17.Jun 28, 2022 · N451AW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA202206288196Panel · dentedFS 654.50 TO FS 654.50 + 9 STRINGER 22R +5 2 EA. OUTWARD DENTS C/T EXTERIOR SIDE OF SKIN PANEL. ****AIRCRAFT REMOVED FROM SERVICE ***** REPAIRED FS654.50 TO FS654.50+9 STRINGER 22R DENT REF REO 601R-53-61-7835 REV. DATED 2022-05-24.Jun 28, 2022 · N451AW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA202206288202Panel · dentedFS625.30+12 STRINGER 22R+4 OUTWARD DENT C/T EXTERIOR SIDE OF SKIN PANEL. ****AIRCRAFT REMOVED FROM SERVICE **** REPAIRED DENT DAMAGE TO FUSELAGE LOWER SKIN BETWEEN FS625.00 - FS640.00 AND STR 22R - STR 23R REF REO 601R-53-61-7836 REV. DATED 2022-05-25Jun 28, 2022 · N451AW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA202206288197Panel · dentedFS605.00+1 STRINGER 23L+3 INWARD DENT C/T EXTERIOR SIDE OF SKIN PANEL. ***AIRCRAFT REMOVED FROM SERVICE **** DRESSED BACK DENT AS PER INSTRUCTIONS OUTLINED IN REO 601R-53-61-7829 REV DATED 2022-05-17.Jun 28, 2022 · N451AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202206278194Skin Panel · dentedF/S 605.00+1, STRINGER 23L+3; INWARD DENT C/T EXTERIOR SIDE OF SKIN PANEL ***AIRCRAFT REMOVED FROM SERVICE **** DRESSED BACK DENT AS PER INSTRUCTIONS OUTLINED IN REO 601R-53-61-7829, REV--, DATED 2022-05-17 AND REO 601R-51-00-309 REV. -A DATED 2017-08-23 . GEJun 27, 2022 · N451AW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA202108167856Seal · mismanufacturedREF. 342366/4 AND 342667/1- LOUD SQUEAL AT 4,000 FT 250 KNOTS. ABNORMAL CLIMB RATE AT CABIN ALT. AT 10,000 FT, CABIN ALT REMAINED AT 5,000 FT. CABIN ALT INCREASED WITH DECREASED POWER. ON FINAL APPROACH ABNORMALLY HIGH RATE OF DECENT OF CABIN ALT. LANDING WAug 15, 2021 · N451AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA202108177857Seal · leaking3930 DURING CLIMBOUT AROUND 13K FEET HEARD LOUD HISSING SOUND COMING FROM BEHIND THE FLIGHT DECK. FA CALLED AND SAID IT WAS FROM THE MAIN CABIN DOOR. AROUND 19K FEET HISSING GOT LOUDER AND CABIN RATE RAPIDLY INCREASED. CABIN ALTITUDE NEVER EXCEEDED 6K FEET. Aug 14, 2021 · N451AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA202010267364Windshield · crackedCAPTAIN OUTER SINDSCREEN (WINDSHIELD) CRACKED WHILE ASCENDING THROUGH 19,000FT. C/W QRH AND RETURNED TO DAY. AIRCRAFT REMOVED FROM SERVICE. R & R LT WINDSHIELD, IAW AMM 56-11-01 REF WO 300890 MX WORK CARD NR 3 FOR OPERATIONS AND LEAK CHECK.Oct 26, 2020 · N451AW · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA202010067312Skin · damagedNUT PLATE HOLE IN FUSELAGE SKIN AND UNDERLINING DOUBLER AT STR 19R AND FS 409+93 OBLONG/ELONGATED TO 0.297W X 0.294. AIRCRAFT REMOVED FROM SERVICE. OPENED HOLE IN STR 19R TO 0.2055, REF REO 601R-53-31-1145 DATED 2020-10-05. OPENED ELONGATED HOLE IN FUSELAGEOct 6, 2020 · N451AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202010067311Former · crackedPAX DOOR AFT FORMER CRACKED. P/N 601R318034-3 AT FS 347.25 THAT MEASURES 2.9'' L. AIRCRAFT REMOVED FROM SERVICE. CUT OUT DAMAGED AREA OF FORMER 3.0" L, REF REO NR: 601R-52-11-2834 DATED 2020-10-05. PERFORMED HFEC INSPECTION OF CUT OUT AREA AND INNER SKIN, IOct 6, 2020 · N451AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA202010057310Access Panel · gougedLT FLAP LOWER INBOARD ACCESS PANEL 584AB GOUGED AT UPPER CENTER LEADING EDGE. GOUGE ON LT FLAP LOWER INBOARD ACCESS PANEL 584AB MEASURES 0.6125''L X 0.30''W X0.011''D. BLENDED GOUGE TO A SMOOTH CONTOUR. DEPTH NOT TO EXCEED ORIGINAL DEPTH OF 0.011'', IAW EAOct 5, 2020 · N451AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA202010057309Skin · gouged2 EACH MISS-DRILLED SCREWS LT FWD WING TO BODY FAIRING ATTACHED POINT (ON FUSELAGE). HOLE NR 1 LOCATED AT FS 409+71.6 AND STR 21L THAT MEASURES 0.307'' W AND 0.25'' L. HOLE NR2 LOCATED AT FS 409+70.45 AND STR 22L THAT MEASURES 0.249'' W AND 0.208'' L. AIRCROct 4, 2020 · N451AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202010057305Skin · crackedPASSENGER DOOR INTERNAL STRUCTURE ENTRY DOOR/STAIRS AFT SIDE FOUND CRACK IN SKIN AT 2ND TO TOP STEP. AIRCRAFT REMOVED FROM SERVICE. REPAIRED PASSENGER DOOR STAIRS AFT SIDE AT 2ND STEP, REF AIR WISCONSIN SUPPLEMENT NO: 14-162 DATE OF ISSUE JULY 21, 2014. REMOct 3, 2020 · N451AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA2020031147223Landing Gear · malfunctionedAFTER T/OFF ON CLIMB, RECEIVED GEAR DISAGREE AFTER 6 SECS FROM SELECTION. NLG SHOWS DOWN AND NLG DOOR OPEN. BOTH MLG SHOW UP AND LOCKED. ALSO RECEIVED NWS INOP, WOW INPUT CAUTION, WOW OUTPUT FAIL MESSAGES. RAN QRH AND STEERING MESSAGE CLEAREDMar 9, 2020 · N451AW · Cndair CL6002B19 · Nose/Tail Landing GearSDR A6WA2020012247121Wire Harness · not reportedAFTER TAKE OFF, RECEIVED A GEAR DISAGREE, NOSE GEAR REMAINED DOWN. COMPLIED WITH QRH. MANUAL GEAR EXTENSION ACCOMPLISHED, RECEIVED 3 GREEN. ON TAXI IN, RECEIVED A HYD 3 HIGH TEMP AND NWS INOPERATIVE CAUTION. COMPLIED WITH QRH. MESSAGES CLEARED. AIRCRAJan 20, 2020 · N451AW · Cndair CL6002B19 · Landing Gear System WiringSDR A6WA2019092346882Warning System · activatedNOSE DOOR OPEN (W) MSG RECEIVED WHEN PUTTING GEAR UP ON DEPARTURE GEAR DISAGREE(W) ALSO RECEIVED. RAN QRH FOR NOSE DOOR OPEN. MSG APPEARED IMMEDIATELY AFTER HANDLE MOVEMENT.Sep 20, 2019 · N451AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA201904106548Warning Message · illuminatedDURING CLIMB, AT APPROXIMATELY 15,000 FEET, THE FLIGHT CREW RECEIVED A RIGHT THRUST REVERSER UNLOCKED CAUTION MESSAGE. THE CREW COMPLETED THE APPROPRIATE CHECKLISTS, DECLARED AN EMERGENCY. THE FLIGHT RETURNED TO ORD AND LANDED WITHOUT FURTHER INCIDENT.Apr 6, 2019 · N451AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA2019022546417Adc · malfunctionedDURING APPROACH, THE FLIGHT CREW IDENTIFIED A AIR DATA COMPUTER 2 ISSUE (INDICATED AIRSPEED AND ALTITUDE) AND ABANDONED THE APPROACH. THE CREW COMPLETED THE APPROPRIATE CHECKLISTS, DECLARED AN EMERGENCY AND ATTEMPTED AN APPROACH FOR THE SECOND TIME. AFTER RECEFeb 24, 2019 · N451AW · Cndair CL6002B19 · Air Data ComputerSDR A6WA2018080945968Bulkhead Web · crackedAFT PRESSURE BULKHEAD ABOVE AFT CARGO DOOR, AFT OF THE TRACK WAS CRACKED. REPAIRED THE BULKHEAD WEB.Aug 6, 2018 · N451AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2018080645967Skin · dentedLEFT INBD FLAP, LOWER OTBD SKIN PANEL HAD TWO DENTS. REPLACED THE FLAP SKIN PANEL IAW SRM 51-42-13Aug 5, 2018 · N451AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2018080645966Skin · dentedRIGHT INBD FLAP, LOWER INBD SKIN PANEL HAD MULTIPLE AREAS OF DENTS, DINGS, AND PITS. REPLACED THE FLAP SKIN IAW SRM 51-42-13.Aug 5, 2018 · N451AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2018080645960Beam · crackedCARGO DOOR BEAM CUT BY BOTH DOOR ASSIST CABLE, LOWER OTBD FLANGE, AT TWO PLACES. REPLACED THE CARGO DOOR BEAM LOWER OTBD FLANGE IAW SRM 51-42-21, AND SRM 51-42-06.Aug 2, 2018 · N451AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA2018080645962Angle · crackedBS 280 FLOORBEAM OTBD ANGLE AT LBL 9 WAS CRACKED. REPLACED THE FLOORBEAM ANGLE.Aug 2, 2018 · N451AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA2018080645959Strap · corrodedFLOORBEAM STRAP AT BS 559 HAD CORROSION BETWEEN RBL 27 AND THE RT FLOOR SUPPORT, IN THE CABIN. REMOVED AND REPLACED THE FLOORBEAM STRAP IAW SRM 51-42-06, 51-40-11, 53-41-43, AND 53-00-00Aug 1, 2018 · N451AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA2018080645958Web · crackedON REMOVAL OF A CRACKED DRAG ANGLE REPAIR, AFT RISER WEB FOUND TO BE CRACKED BY THE ASSIST MOTOR YOKE. REPAIRED PAX DOOR AFT WEB RISER IAW SUPP 15-310Aug 1, 2018 · N451AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA2018080645956Skin · dentedRIGHT INBOARD FLAP LOWER OTBD SKIN PANEL WAS DENTED. REMOVED AND REPLACED THE SKIN IAW SRM 51-42-13.Aug 1, 2018 · N451AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2018080645957Skin · crackedON REMOVAL OF THE PAX DOOR AFT RISER DRAG ANGLE, THE INNER SKIN HAD A CRACK UNDER THE DRAG ANGLE SLPICE. REPAIRED PAX DOOR INNER SKIN IAW 18-225.Aug 1, 2018 · N451AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA2018080645964Strap · damagedPAX DOOR FWD SEAL STRIKER REPAIR STRAP DAMAGED. REPLACED PAX DOOR FWD SEAL STRIKER REPAIR STRAP IAW SUPP 17-009.Jul 30, 2018 · N451AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018073045955Skin Panel · damagedLT INBD FLAP LOWER INBD SKIN PANEL HAS MULTIPLE AREAS WITH DAMAGE. REPLACED LT INBD FLAP LOWER INBD SKIN PANEL IAW SRM 51-42-13.Jul 29, 2018 · N451AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2018073045954Fitting · crackedFLIGHT DECK WINDSHIELD CENTER POST LOWER LEFT FITTING CRACKED. REPLACED FITTING IAW SRM 51-42-21.Jul 28, 2018 · N451AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018073045953Web · crackedPAX DOOR UPPER STEP WEB BELOW TOP FOLDING STEP IS CRACKED. REPAIRED IAW REO 601R-52-11-279 REV-NC.Jul 26, 2018 · N451AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA2018080645963Drag Angle · crackedPAX DOOR AFT DRAG ANGLE WAS CRACKED. REPAIRED THE AFT DRAG ANGLE IAW REO 601R-52-11-513 REV B.Jul 23, 2018 · N451AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA2018072445949Bracket · crackedAFT CARGO DOOR TRACK, LOWER AFT BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-42-06.Jul 22, 2018 · N451AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201745241Connector · unsecureFLOOR EMERGENCY LIGHTS DO NOT ILLUMINATE FROM ROWS 9 AFT. SECURED THE EMERGENCY LIGHT CONNECTOR AT ROW 12, OPS CHECKED GOOD IAW AMM 33-51-01.Aug 29, 2017 · N451AW · Cndair CL6002B19 · Light System WiringSDR A6WA201745084Sign · inoperativeEXIT SIGN INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT SIGN IAW AMM 33-51-10, OPS CHECKED GOOD.Jul 4, 2017 · N451AW · Cndair CL6002B19 · Emergency LightingSDR A6WA201644072Bracket · brokenLEFT NOSE COWL PDU WIRE HARNESS BRACKET BROKEN. REPLACED BRACKET IAW CMM 20-42-06.Jul 6, 2016 · N451AW · Cndair CL6002B19 · Nacelle/Pylon, Attach FittingsSDR A6WA201644071Stringer Clip · crackedSTRINGER CLIP BS 621 STRINGER 13L AFT SIDE IS CRACKEDJul 6, 2016 · N451AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201644067Frame · corrodedFRAME BS 333 HAS CORROSION ON THE FWD SIDE BETWEEN STRINGERS 22 - 23R IN THE FWD E&E BAY. REMOVED CORROSION AND INSTALLED DOUBLERS AS REQUIRED IAW REO 601R-53-21-2733 REV-A.Jul 5, 2016 · N451AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA201644059Skin · crackedRT I/B L/E INNER SKIN IS CRACKED 24 INCHES FROM I/B EDGE. REPAIRED DAMAGE IAW EA AWAC-CRJ257-00423 REV-IR AND AWAC SUPPLEMENT 16-188.Jul 1, 2016 · N451AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA201644061Lug · chafedRIGHT O/B FLAP, CENTER HINGE ARM FWD ATTACH POINT, O/B LUG IS CHAFED. REPAIRED IAW REO 601R-57-53-1048 REV.Jul 1, 2016 · N451AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201644058Fitting · crackedBS 621 SEAT TRACK ATTACHMENT LBL 27 HAS CORROSION. REPAIRED ATTACH FITTING IAW EA AWAC-CRJ 253-00421 REV-IR.Jul 1, 2016 · N451AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201644052Floor Support · gougedRIGHT FLOOR SUPPORT BETWEEN BS 559+48 AND 559+64 IS GOUGED BY THE TOILET DUMP FITTING. REPAIRED THE FLOOR SUPPORT IAW EA AWAC-CRJ253-00422 REV- IR.Jun 29, 2016 · N451AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201644050Rib · crackedJET PIPE FAIRING 446AL FWD RIB IS CRACKED. REPAIRED THE RIB IAW CMM 78-11-00-300-810-A01.Jun 28, 2016 · N451AW · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
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