N408AW

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 = 'N408AW' 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 A6WA200940691Handle · crackedCARGO DOOR HANDLE HOUSING CRACK. (UPPER 1.00, LOWER .500) CARGO DOOR HANDLE HSG REPLACED IAW SRM 51-42-21 AND DWG 601R35027. (K)Oct 7, 2009 · N408AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA200940694Attach Fitting · crackedAT REAR PRESSURE BULKHEAD IN AFT COMPARTMENT, INTERCOSTAL CLIP BTW FS 621 AND FS 625, ADJACENT TO STR 14R CRACK AT REAR PRESSURE BULKHEAD IN AFT COMPARTMENT, INTERCOSTAL CLIP BTW FS 621 AND 625. ADJACENT TO STR 14R REPLACED IAW SRM 51-21-42 AND REO 601R-53-61Oct 7, 2009 · N408AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940695Attach Fitting · crackedAT REAR PRESSURE BULKHEAD, IN AFT COMPARTMENT, INTERCOSTAL CLIP AT FS 621, ADJACENT TO STR 14L CRACK AT REAR PRESSURE BULKHEAD, IN AFT COMPT, INTERCOSTAL CLIP AT FS 621 ADJACENT TO STR 14L, REPLACE IAW SRM 57-42-21 AND REO 601R-53-61-422. (K)Oct 7, 2009 · N408AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940687Bulkhead · crackedFWD PRESSURE BULKHEAD FS 202.75, LBL 23.71, WL 69.7, CRACKED AT PARKING BRAKE LINE LOCATION (CRACK LENGTH 1.500") FWD PRESSURE BULKHEAD FS 202.75, LBL 23.71, WL 69.7. REPAIRED AT PARKING BRAKE IAW REO 601R-53-11-563. (K)Oct 6, 2009 · N408AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940688Floorbeam · crackedFLOORBEAM FITTING CRACKED AT FS 461.5, RBL 9.0, OTBD SIDE FLOORBEAM FITTING AT FS 461.5, RBL 9.0 OTBD SIDE REPLACED IAW SRM 51-42-06 AND SRM 51-42-21. (K)Oct 6, 2009 · N408AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940690Sill · crackedCARGO DOOR FLOOR SILL FS 574.00 LBL 45.00 CRACKED. CARGO DOOR FLOOR SILL FS 574.00, LBL 45 REPAIRED IAW REO 601R-53-61-1741. (K)Oct 5, 2009 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940689Plate · crackedCARGO DOOR FLOOR LANDING PLATE CRACKED FS 589.00, LBL 45.00. CARGO DOOR FLOOR LANDING PLATE REPAIRED IAW REO 601R-53-61-433 REV NC AND REO 601R-53-61-3403. (K)Oct 5, 2009 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940692Attach Fitting · crackedINTERCOSTAL CLIP CRACKED AT FS 484, LBL 27.0. INTERCOSTAL CLIP AT FS 484, LBL 27.0. REPLACED IAW REO 601R-53-41-059, REV B. (STEP 8 TO 14). (K)Oct 2, 2009 · N408AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200840615Control Handle · malfunctionedLOG 197305/3 AFTER TAKEOFF LANDING GEAR DID NOT COME UP WHEN SELECTED UP. LANDING GEAR LIGHT REMAINED GREEN. ALSO GOT INBD ANTI-SKID CAUTION AND PARKING BRAKE SHUT OFF VALVE CAUTION. CLEARED WHEN GEAR SELECTED DOWN. INTERROGATED PSEU AND FOUND DI 11 OFF FANov 22, 2008 · N408AW · Cndair CL6002B19 · Landing Gear SelectorSDR A6WA200740557Web · crackedPAX DOOR FORWARD WEB SKIN IS CRACKED IN RADIUS BETWEEN STEP 832CT AND FIXED STEP. MAINTENANCE CUT AWAY DAMAGED SKIN AND INSTALLED REPAIR DOUBLER AND ANGLES IAW BOMBARDIER REO 601R-52-11-702 REV A AND BSC EO 601R-52-13284. (M)Sep 28, 2007 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740568Skin · corrodedLT LOWER WING PLANK AT ACCESS PANEL 540 CB HAS MINOR PITTING DAMAGE IN NON-CRITICAL AREA, .001-.002 INCH DEEP. MAINTENANCE REPAIRED LT LOWER WING PLANK PER BOMBARDIER REO 601R-57-21-030 REV F. (M)Sep 26, 2007 · N408AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740571Skin · corrodedMINOR PITTING ON RIGHT LOWER WING PLANK WS 54.897 ACCESS PANEL 640BB IN NON-CRITICAL AREA. MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030. (M)Sep 26, 2007 · N408AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740570Skin · corrodedMINOR PITTING DAMAGE LT LOWER WING PLANK WS 188.040 FUEL ACCESS PANEL 550BB IN NON-CRITICAL AREA .001 INCH -.002 INCH DEEP. MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030. (M)Sep 26, 2007 · N408AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740572Skin · corrodedMINOR PITTING DAMAGE RT LOWER WING PLANK WAS 12.245 ACCESS PANEL 610AB, .001 INCH-.002 INCH DEEP IN CRITICAL AND NON-CRITICAL AREAS. MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV F. (M)Sep 26, 2007 · N408AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740569Skin · corrodedLT LOWER WING PLANK HAS MINOR PITTING DAMAGE IN A NON-CRITICAL AREA .001-.002 DEEP AT WING ACCESS PANEL 540BB. MAINTENANCE REPAIRED LT LOWER WING PLANK IAW BOMBARDIER REO 601R-57-21-030 REV F. (M)Sep 26, 2007 · N408AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740567Skin · crackedPAX DOOR AFT STAIRS SKIN IS CRACKED BETWEEN PANEL 832CT AND 832DT STEPS, CRACK IS .250 LONG. MAINTENANCE CUT AWAY DAMAGED SKIN AND INSTALLED REPAIR DOUBLER AND ANGLES IAW BOMBARDIER REO 601R-52-11-702 REV A. (M)Sep 23, 2007 · N408AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740527Attach Fitting · crackedFOUND FS 280 LBL 9 OUTBOARD ATTACH CLIP CRACKED. 10-24-07 MAINTENANCE REMOVED AND REPLACED CLIP P/N 601R31113-57, IAW CRJ SRM 51-42-06, 51-42-21. (M)Sep 21, 2007 · N408AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740526Attach Fitting · crackedFOUND FS 280 RBL 9 OUTBOARD ATTACH CLIP IS CRACKED. 10-24-07 MAINTENANCE REMOVED AND REPLACED LCIP P/N 601R31113-58 IAW CRJ SRM 51-42-06, 51-42-21. (M)Sep 21, 2007 · N408AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740525Attach Fitting · crackedFOUND FS 280 LBL 9 INBOARD CLIP CRACKED. 10-24-07 MAINTENANCE REMOVED AND REPLACED CLIP P/N 601R31113-57 IAW CRJ SRM 51-42-06, 51-42-21. (M)Sep 21, 2007 · N408AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740524Attach Fitting · crackedFOUNF FS 280 RBL 9 INBOARD CLIP CRACKED. 10-24-07 MAINTENANCE REMOVED AND REPLACED CLIP P/N 601R31113-58 IAW CRJ SRM 51-42-06, 51-42-21. (M)Sep 21, 2007 · N408AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740573Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED APPROX 1 INCH AT DOOR ASSIST CABLE PULLEY IN RADIUS OF ANGLE. MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER AERO SPACE REO 601R-52-11-513. (M)Sep 19, 2007 · N408AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740574Skin · crackedPAX DOOR AFT STAIR SIDE SKIN CRACKED APPROX .70 INCH BETWEEN MID UPPER STEP AND MID STEP. MAINTENANCE CUT AWAY DAMAGED SKIN AND INSTALLED REPAIR DOUBLER AND ANGLES IAW BOMBARDIER REO 601R-52-11-702 REV A. (M)Sep 19, 2007 · N408AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740523Cargo Track · crackedFOUND CARGO DOOR FORWARD TRACK LOWER AT CHANNEL CRACKED. 10-24-07 MAINTENANCE REPLACED C-CHANNEL IAW CRJ SRM 51-42-06. (M)Sep 19, 2007 · N408AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA200740558Handle · failedWO 114147, MWC 144, CREW ESCAPE HATCH OUTER HANDLE WILL NOT OPEN. REMOVED AND REPLACED CREW ESCAPE HATCH OUTSIDE HANDLE IAW CMM 52-22-03, FUNCTIONAL TEST OF OUTSIDE HANDLE GOOD IAW CMM 52-22-03. (K)Sep 18, 2007 · N408AW · Cndair CL6002B19 · Emergency ExitsSDR A6WA200740112Wire · damagedPROXIMITY SYSTEM FAULT WHITE STATUS MESSAGE. INSTALLED NEW WIRES FROM P4MB TO PROXIMITY SWITCH S38. WIRES INSTALLED WERE RED AND BLUE IAW WDM 20-12-00. OPS CHECK GOOD. (K)Mar 12, 2007 · N408AW · Cndair CL6002B19 · Landing Gear System WiringSDR A6WA200640267Skin · dentedTEMPORARY DISPOSITION FOR THE DENTS TO RUDDER SKIN BETWEEN RS 108.25 AND RS 113.98. MAINTENANCE REPAIRED RUDDER BY CUTTING AWAY DAMAGE AND INSTALLING NON FLUSH DOUBLER IAW CRJ200 SRM 55-40-00. (M)Jun 26, 2006 · N408AW · Cndair CL6002B19 · Rudder, Plate/SkinSDR A6WA200540328Radome · noneREQUEST BIRD STRIKE INSPECTION. REMOVED AND REPLACED RADOME DUE TO BIRD STRIKE IAW AMM 53-81-01. PERFORMED BIRDSTRIKE AMM 05-51-25. NO FURTHER DAMAGE AND NO ENGINE INGESTION FOUND. (K)Nov 14, 2005 · N408AW · Cndair CL6002B19 · Aerodynamic FairingsSDR A6WA200540234A/C Pack · leakingCABIN FILLED WITH SMOKE WHILE AT GATE WITH ENGINES OFF, APU AND BOTH PACKS RUNNING. INSPECTED AFT EQUIPMENT BAY AND FOUND AIR LEAK RT PACK WATER SEPARATOR PIPE. NO EVIDENCE OF SMOKE WITH APU AND BOTH PACK ON. (K)Jul 13, 2005 · N408AW · Cndair CL6002B19 · APU Oil SystemSDR A6WA200440234Dcu · malfunctionedAFTER ROTATION AND GEAR UP RECEIVED SEVERAL M/C'S AND WINDSHEAR NOSE GEAR DOOR, DISAGREE AND STEERING INOPERATIVE FOLLOWED QRH RETURNED TO CKB WITHOUT INCIDENT. POWERED DOWN AC REMOVED AND RERACKED NR 2 DCU, OPS IAW CRJ AMM 31-41-04. OPS GOOD, NOTE GROSS AT Dec 22, 2004 · N408AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA200440233Strut · dischargedAFTER ROTATION AND GEAR UP RECEIVED SEVERAL MESSAGES NOSE DOOR, GEAR DISAGREE, WOW INPUT AND STEERING INOP. FOLLOWED QRH PROCEDURES LANDED WITH NOSE STEERING INOPERATIVE. SERVICED NLG STRUT IAW CRJ AMM 12-12-32B REFERENCE AWAC W/O NR 77064 FOR DETAILS OF WORDec 22, 2004 · N408AW · Cndair CL6002B19 · Main Landing Gear Strut/Axle/TruckSDR A6WA200440226Skin · dentedFLAP LOWER SKIN DENTED AT WS NEAR T/E. DENT MEASURES 2 INCHES ROUND BY .085 INCH DEEP. INSTALLED EXTERNAL REPAIR TO LT IB FLAP LOWER SKIN AT WS 106, 5 INCHES FROM T/E IAW REO.Dec 17, 2004 · N408AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6W2005F00002Floor Support · crackedRT FS 621.00, FLOOR SUPPORT ANGLE CRACKED. REMOVED DAMAGED PORTION OF ANGLE AND INSTALLED REPAIR ANGLE IAW REO.Dec 14, 2004 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440218Angle · crackedFOUND LEFT FS 625 OBLIQUE ANGLE CRACKED. REPLACED ANGLE P/N 601-35012-51 IAW CRJ SRM 51-42-06. (M)Dec 14, 2004 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440216Angle · crackedFOUND RIGHT FS 484 AT RBL 36 ANGLE CRACKED. REPAIRED RIGHT FS 484 AT RBL 36 ANGLE IAW BOMBARDIER REO 601R-53-41-059 REV A. (M)Dec 14, 2004 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440217Angle · crackedFOUND LEFT FS 484 AT LBL 36 ANGLE CRACKED. REPAIRED LEFT FS 484 AT LBL 36 IAW BOMBARDIER REO 601R-53-41-059 REV A. (M)Dec 14, 2004 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440206Angle · crackedLT FS 621 FLOOR SUPPORT ANGLE CRACKED.Dec 14, 2004 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440205Angle · crackedRT FS 625.00 OBLIQUE ANGLE CRACKED. REPLACED ANGLE P/N 601-35012-12 IAW CRJ SRM 51-42-06. (M)Dec 14, 2004 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440210Angle · crackedLT FS 621.00 FLOOR SUPPORT ANGLE CRACKED.Dec 14, 2004 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440219Angle · crackedRT FS 625.00 OBLIQUE ANGLE CRACKED. REMOVED CRACKED OBLIQUE ANGLE AT FS 625 RT SIDE AND REPLACED WITH NEW SERVICEABLE ANGLE PN 601-35012-52 IAW SRM.Dec 14, 2004 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440214Angle · crackedRT FS 625.00 OBLIQUE ANGLE CRACKED.Dec 14, 2004 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440212Angle · crackedLT FS 484.00 AT LBL 36 ANGLE CRACKED.Dec 14, 2004 · N408AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200440207Floor Support · crackedRT FS 621 FLOOR SUPPORT ANGLE CRACKED.Dec 14, 2004 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440211Floor Support · crackedRT FS 621 FLOOR SUPPORT ANGLE CRACKED.Dec 14, 2004 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA20041213Rib · crackedFOUND RIGHT MLG WHEEL WELL BATT RIB IS CRACKED 1.5 INCHES LONG IN UPPER AFT RADIUS. REPAIRED RIGHT MLG BATTERY RIB IAW CRJ BOMBARDIER REO 601R-57-51-046 REV B. (M)Dec 13, 2004 · N408AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200440208Skin · corrodedLT WING LOWER PANEL FUEL TANK ACCESS DOOR CUT-OUT AT WS 12.245 HAS NUMEROUS AREAS OF PITTING/ FRETTING LOCATED ON FAYING SURFACE AND RADIUS AREAS. DEPTH LESS THAN .015 INCH. REPAIRED ACCESS DOOR CUTOUT AT WS 12/245 IAW BOMBARDIER REO 601R-57-21-030 REV C. (MDec 13, 2004 · N408AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200440203Handle · lack of lubeCREW ESCAPE HATCH, OUTER HANDLE FROZE IN POSITION, WILL NOT DEPLOY. LUBRICATED OUTER HANDLE ASSEMBLY ON CREW ESCAPE HATCH. FOUND TO BE IN GOOD WORKING ORDER IAW CRJ AMM 12-20-52-640-803. (M)Dec 11, 2004 · N408AW · Cndair CL6002B19 · Emergency ExitsSDR A6WA200440209Vane · wornLT OB FLAP - VANE FITTING AT WS 296.073 IS WORN BEYOND LIMITS. COMPLY WITH MFG REO.Dec 10, 2004 · N408AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200440215Angle · crackedLT FS 625.00 OBLIQUE ANGLE CRACKED.Nov 14, 2004 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440025Apu · smokeSMOKE FROM APU, SHUTDOWN APU AND BLEW BOTTLE. REMOVED AND REPLACED APU FIRE EXTINGUSHER IAW AMM 26-22-07. OPS CHECK GOOD. PERFORMED OPS CHECK OF APU, NO DEFECTS NOTED. (M)Feb 21, 2004 · N408AW · Cndair CL6002B19 · APU Core EngineSDR A6WA200340100Wire · out of positionBLEED AIR DUCT MASTER WARNING WOULD COME ON INTERMITTENTLY AND REPEATEDLY IN FILGHT 31,000 FEET. COMPLIED WITH QRH MSS EXTINGUISHING 55 PERCENT N1 LEFT ENGINE. STRAIGHTENED WIRE AT 14TH STAGE BLEED AIR DUCT AND TIGHTENED CLAMP AT AIR SWITCH. RAN ENGINE, OPERJul 3, 2003 · N408AW · Cndair CL6002B19 · Overheat Detection
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