N412AW

Service difficulty reports · 200

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 = 'N412AW' 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 A6WA200940039Bulkhead · crackedPILOTS BULKHEAD FS 280 LBL 9 RBL 9 AFT ANGLE CRACKED. PILOTS BULKHEAD AT FS 280 AFT ANGLE REPAIRED IAW REO 601R-53-11-136 REV A.Jan 23, 2009 · N412AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940038Bulkhead · crackedPILOTS BULKHEAD CRACKED AT FS 280.00 RBL 9 AND LBL 9. PILOTS BULKHEAD AT FS 280.00 RBL 9 AND LBL 9 REPAIRED IAW REO 601R-53-11-171 REV D,Jan 23, 2009 · N412AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940026Skin · corroded131226-222, SURFACE CORRODED ON LT WING PLANK FUEL ACCESS HOLES AT PANEL 540AB, 540EB, 550BB, 550DB AND 550FB. REO 601R-57-21-030, REV G. (K)Jan 21, 2009 · N412AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940025Skin · corroded131266221, SURFACE CORRODED ON RT WING PLANK FUEL ACCESS HOLE AT PANEL 610AB, 640CB AND 650GB, REO 601R-57-21-030, REV G. (K)Jan 21, 2009 · N412AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940024Angle · cracked131267-57 PAX DOOR AFT SECTION FS 338.80, CRACK FOUND ON ANGLE BETWEEN STAIRS AND DOOR FRAME LINE WITH THE POWER ASSIST MOTOR. PAX DOOR AFT SECTION DRAG ANGLE AT FS 338.80. REPAIRED IAW REO 601R-52-11-513 REV A. (K)Jan 20, 2009 · N412AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200840601Bulkhead · crackedAFT PRESSURE BLKHD WEB AT FS 621.00 AT THE LINTEL INSTALLATION AREA IS CRACKED. REPAIRED IAW REO 601R53-61-1230 REV D.Oct 20, 2008 · N412AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200840228Warning Message · illuminatedAFTER TAKEOFF RECEIED ANTI-ICE DUCT WARNING MESSAGE. COMPLIED WITH QRH, MESSGE PERSISTED ON SYNOPTIC PAGE, SHOWS LT WING RED. (M)Mar 19, 2008 · N412AW · Cndair CL6002B19 · Ice/Rain Protection SystemSDR A6WA200840160Element · malfunctionedFOUND LT WING ANTI-ICE DUCT WARNING MESSAGE. REMOVED AND REPLACED HEAT SENSE ELEMENT A41WK REF AMM 36-21-04, OPS CHECK GOOD. (M)Mar 17, 2008 · N412AW · Cndair CL6002B19 · Overheat DetectionSDR A6WA200740684Cable · inoperativeLOUD WHISTLING NOISE COMING FROM MAIN CABIN DOOR, LOUDEST JUST AFTER TAKEOFF. REMOVED AND REPLACED ICE BREAK CABLE IN PRESSURE RELIEF DOOR. REF AMM 52-11-15, OPS TEST GOOD. (K)Dec 16, 2007 · N412AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740658Charger · inoperativeENTRY-WAY EMERGENCY FLOODLIGHT INOPERATIVE. REMOVED AND REPLACED CHARGER ASSY NR 2 IAW 33-51-05, OPS CHECK GOOD. (K)Dec 8, 2007 · N412AW · Cndair CL6002B19 · Emergency LightingSDR A6WA200740156Controller · malfunctionedPITOT BASE HEAT CAUTION MESSAGE CAME ON AFTER TAKEOFF. QRH COMPLIED WITH, UPON LANDING TAT PROBE HEAT, LT STATIC HEAT, LT AOA HEAT, RT STATIC HEAT, AND RT AOA HEAT CAUTION MESSAGE ALL CAME ON. REMOVED AND REPLACED ADS NR1 HEAT CONTROLLER IAW AMM 30-13-15 ANDMar 25, 2007 · N412AW · Cndair CL6002B19 · Pitot/Static Anti-Ice SystemSDR A6WA200740028Bulkhead · crackedFOUND LEFT SIDE FORWARD FACE OF FORWARD PRESSURE BULKHEAD FS 202.75 CRACKED APPROX .2 INCH LONG AT HYDRAULIC SYSTEM NR 3 RT INBOARD BRAKE FITTING. MAINTENANCE REPAIRED CRACKED AREA IAW BOMBARDIER SERVICES CORP EO 601R-53-10650. (M)Jan 11, 2007 · N412AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200740027Floor Support · crackedFOUND LEFT FS 280 FLOOR SUPPORT CLIP P/N 601R31113-57 CRACKED APPROX .2 INCH LONG INBOARD SIDE LBL 9.0. MAINTENANCE REMOVED AND CRACKED ANGLE, FITTED AND INSTALLED NEW ANGLE P/N 601R31113-57 IAW CRJ SRM 51-42-06, 51-42-21, 51-42-13, 51-40-11 AND BSC STANDARD Jan 10, 2007 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740022Floor Support · crackedFOUND FS 460 FLOOR SUPPORT FITTING CRACKED OUTBOARD SIDE OF RBL 9, APPROX 1 INCH LONG. MAINTENANCE REMOVED AND REPLACED FITTING P/N 600-31068-19 AT FS 460.0 RBL 9,0 IAW CRJ SRM 51-40-11, 51-42-06 AND 51-42-21. (M)Jan 10, 2007 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740021Angle · crackedFOUND LEFT ANGLE AT FS 484 LBL 27 CRACKED APPROXIMATELY .2 INCHES LONG. MAINTENANCE REMOVED AND REPLACED CLIP IAW CRJ SRM 51-42-06, 51-40-11 AND 51-42-21. (M)Jan 10, 2007 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740020Intercostal · crackedFOUND LEFT INTERCOSTAL AT FS 484 LBL 36 CRACKED APPROXIMATELY .2 INCHES LONG. MAINTENANCE CUT AWAY DAMAGED SECTION OF INTERCOSTAL FLANGE, PERFORM EDDY CURRENT, FABRICATED REPAIR PARTS AND INSTALLED IAW BOMBARDIER REO 601R-53-41-059 REV A AND BSC STANDARD REPAJan 10, 2007 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740019Intercostal · crackedRIGHT INTERCOSTAL AT FS 484 RBL 36 CRACKED APPROXIMATELY .3 INCHES LONG MAINTENANCE CUT AWAY DAMAGED SECTION OF INTERCOSTAL FLANGE, PERFORMED EDDY CURRENT, FABRICATED REPAIR PARTS AND INSTALLED IAW BOMBARDIER REO 601R-53-41-059 REV A AND BSC STANDARD REPAIR 60Jan 10, 2007 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740018Angle · crackedFOUND RIGHT ANGLE AT FS 484 RBL 27 CRACKED APPROXIMATELY .25 INCHES LONG. MAINTENANCE REMOVED AND REPLACED CLIP IAW CRJ SRM 51-42-06 AND 51-42-21. (M)Jan 10, 2007 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740017Floor Support · crackedFOUND LEFT FS 621 FLOOR SUPPORT ANGLE IS CRACKED .5 INCH LONG IN OUTBOARD RADIUS. MAINTENANCE REPAIRED FS 621 FLOOR SUPPORT ANGLE IAW BOMARDIER REO 601R-53-61-117. (M)Jan 10, 2007 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740016Floor Support · crackedRIGHT FS 621 FLOOR SUPPORT ANGLE IS CRACKED .5 INCH LONG IN OUTBOARD RADIUS. MAINTENANCE REPAIRED FLOOR SUPPORT IAW BOMBARDIER REO 601R-53-61-117 REV C. (M)Jan 10, 2007 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740015Nut Clip · crackedRIGHT FS 280 FLOOR SUPPORT CLIP P/N 601R31113-58 CRACKED APPROX .3 INCHES LONG INBOARD SIDE RBL 9.0. MAINTENANCE REMOVED CRACKED ANGLE. FITTED AND INSTALLED NEW ANGLE P/N 601R31113-58 IAW CRJ SRM 51-42-06, 51-42-21, 51-42-13, 51-40-11 AND BSC STANDARD REPAIRJan 10, 2007 · N412AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA200740014Floorbeam · crackedFOUND LEFT FS 280 FLOOR SUPPORT CLIP, P/N 601R31113-57 CRACKED APPROX .1 INCH LONG OUTBOARD SIDE LBL 9.0. REMOVED CRACKED ANGLE. FITTED AND INSTALLED NEW ANGLE P/N 601R31113-57 IAW CRJ SRM 51-42-06, 51-42-13-51-40-11, 51-42-21 AND BSC STANDARD REPAIR 601R-53Jan 10, 2007 · N412AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740012Bracket · crackedHYDRAULIC TRANSDUCER HOT CHANNEL IN LEFT MLG BAY CEILING CRACKED APPROXIMATELY .2 INCHES LONG, BRACKET P/N 601R75262-159. MAINTENANCE DRILLED OFF REMOVED CRACKED BRACKET, DRILLED UP AND INSTALLED NEW BRACKET P/N 601R75262-159 WET USING PR1422B SEALANT AND MS Jan 9, 2007 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740011Bracket · crackedHYDRAULIC TRANSDUCER HOT CHANNEL IN RIGHT MLG BAY CEILING CRACKED APPROXIMATELY .2 INCHES LONG, BRACKET P/N 601R75262-157. MAINTENANCE DRILLED OFF, REMOVED CRACKED BRACKET. DRILLED UP AND INSTALLED NEW BRACKET P/N 601R-75262-15T WET USING PR1422B SEALANT AN Jan 9, 2007 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640318Idg · failedIDG CAUTION MESSAGE AT APPROXIMATELY 30 KNOTS ON TAKEOFF ROLL, ABORTED TAKEOFF. REMOVD AND REPLACED IDG NR 2. (M)Aug 17, 2006 · N412AW · Cndair CL6002B19 · AC Generator-AlternatorSDR A6WA200640182Door · damagedMAIN PAX DOOR DROPS 1 FOOT PRIOR TO GROUND. SOME STRUCTURAL DAMAGE INCURRED ON PAX DOOR AS A RESULT OF COMPONENT FAILURE. MAINTENANCE REPAIRED PAX DOOR IAW AMM 52-11-17-400-802, BOMBARDIER REO 601R-52-11-702, BSC EO 601R-52-9149, BSC EO 601R-52-91-46A, SRM 5May 11, 2006 · N412AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200540178Apu · flamed outAPU AUTOSHUT AND GRD CREW ADVISED FLAME COME OUT OF INTAKE. LOUD BANG WHEN SHUTDOWN. DISCHARGED BOTTLES. INSP APU AREA, NO EVIDENCE OF FIRE, C/W (M) ACTION IAW MEL. (K)May 18, 2005 · N412AW · Cndair CL6002B19 · APU Engine Fuel and ControlSDR A6WA200540243Aileron · out of rigWITH AILERON TRIM CENTERED, AIRCRAFT HAS A STRONG ROLL TO THE RT. WITH LARGE AMOUNT OF LT WING DOWN TRIM, THE AIRCRAFT CAN BE MADE TO FLY LEVEL. AUTO-PILOT WAS OFF. FOUND RT AILERON SLIGHTLY OUT OF RIG. RE-RIGGED RT AILERON IAW AMM. (K)Mar 18, 2005 · N412AW · Cndair CL6002B19 · Aileron Tab Control SystemSDR A6WA200540044Doubler · mismanufacturedWHILE PERFORMING SB 601R57037 (WING SPAR MOD) IT WAS DISCOVERED THAT THE JOINT STRAP ON THE RT WING LACKS PROPER LENGTH FOR EDGE DISTANCE. COMPLIED WITH BRAS EO 601R575944A, BY FABRICATING DOUBLER FROM 2024T3, .050 INCH AND USING TO EXTEND CUTLINES TO OBTAIN Feb 5, 2005 · N412AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA200540074Drag Angle · crackedPAX DOOR AFT DRAG ANGLE IS CRACKED 3 INCHES LONG JUST FORWARD OF PAX DOOR ASSIST PULLEY MOUNT BRACKET. REPAIRED ANGLE IAW BRAS EO 601R-52-5929 AND BOMBARDIER, INC REO 601R-52-11-513. (M)Feb 2, 2005 · N412AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200540075Handle · lack of lubeCREW ESCAPE HATCH OUTER HANDLE WILL NOT RELEASE. LUBRICATED HANDLE IAW CRJ 200 AMM 12-20-52-640-803. PERFORMED CHECK IAW CRJ 200 AMM 52-22-00-710-801. (M)Jan 31, 2005 · N412AW · Cndair CL6002B19 · Emergency ExitsSDR A6WA200540039Panel · corrodedRT WING PLANK HAS CORROSION UNDER THE FOLLOWING FUEL PANELS 640BB AND 650HB. REMOVED MINOR CORROSION FROM RIGHT WING LOWER PLANK AT FUEL TANK ACCESS PANELS 340BB AND 650 HB IAW BOMBARDIER, INC REO 601R-57-21-030 REV C. (M)Jan 31, 2005 · N412AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540037Access Panel · corrodedLT WING PLANK HAS CORROSION UNDER THE FOLLOWING FUEL TANK PANELS 550BB, 540ED, 540BB, 510AB. REMOVED MINOR CORROSION FROM LT WING LOWER PLANK AT FUEL ACCESS PANELS 550BB, 540FB, 540EB, 540BB AND 510AB IAW MFG REO 601R-57-21-030 REV C. (M)Jan 31, 2005 · N412AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA20050033Rib · crackedLT WING STATION 53.6 BUTT RIB IS CRACKED, 1 INCH LONG IN UPPER AFT RADIUS. REPAIRED LT WING STATION 53.60, BATT RIB IAW MFG REPAIR EO 601R-57-51-046, REV B.Jan 25, 2005 · N412AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200540034Rib · crackedMWC 60. RT WING STATION 53.6 BUTT RIB IS CRACKED .5000 INCH LONG IN UPPER AFT RADIUS. REPAIRED RT WING STATION 53.60 BATT RIB IAW MFG EO 601R-57-51-046, REV B.Jan 25, 2005 · N412AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200540036Intercostal · crackedRT SIDE FS621 THROUGH 625.3 INTERCOSTAL AT STR 14R IS CRACKED IN RADIUS APPROXIMATELY 1.0 INCH. FABRICATED INTERCOSTAL FROM S6144-3 7075 T62-050 INSTALLED IAW CRJ-200 SRM 51-42-06. (M) (K)Jan 25, 2005 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540035Intercostal · crackedLT SIDE FS621 THROUGH 625.3 INTERCOSTAL AT STR 14L IS CRACKED IN RADIUS APPROXIMATELY 1.0 INCH. (K) REMOVED AND REPLACED INTERCOSTAL IAW CRJ 200 SRM 51-42-06. (M)Jan 25, 2005 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540017Fire Bottle · lowLT ENGINE SQUIB LIGHT WILL NOT ILLUMINATE. FOUND LT ENGINE FIRE BOTTLE LOW PRESSURE. REMOVED AND REPLACED BOTTLE. (K)Jan 8, 2005 · N412AW · Cndair CL6002B19 · Fire Bottle, FixedSDR A6WA200440114Indicator · inoperativeABORTED TAKEOFF AT 110 KNOTS DUE TO STANDBY AIRSPEED INDICATOR READING ZERO KNOTS. TAKEOFF WEIGHT AT 49380 LBS. NO OVERHEAT. FOUND P3 DRAIN TUBE FULL OF WATER. PURGED P3 SYSTEM IAW 34 P3 AND S3 SYSTEM LEAK CHECK GOOD. STANDBY AIRSPEED ALTITUDE. OPS CHECKAug 16, 2004 · N412AW · Cndair CL6002B19 · Airspeed/Mach IndicatorSDR A6WA200440054Control Panel · burnedFMS PAGE STUCK ON PERFORMANCE SCREEN, AFTER DETECTING ELECTRICAL BURNING ODOR IN COCKPIT AND IN FROM CABIN. PULLED CIRCUIT BREAKER H12. REMOVED AND REPLACED FMS CONTROL PANEL FOR BURNING ODOR AFTER FROZEN SCREEN. NO FURTHER ODOR NOTED WITH REPLACEMENT. OPSApr 30, 2004 · N412AW · Cndair CL6002B19 · Flight Management Computing Hardware SystemSDR A6WA200340127Bpsu · failedFLAP FAIL WARNING INFLIGHT WITH NO MOVEMENT AFTER FLAP SELECTION. INTERROGATED FECU, RIGHT BRAKE AND POSITION SENSORING UNIT (BPSU) FAIL. REMOVED AND REPLACED RIGHT BPSU.Aug 26, 2003 · N412AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200340082Skin · dentedRIGHT INBOARD GROUND SPOILER HAS A DENT ON TOP SKIN INSPECTED AND NOTED DENT IAW WVAC EO 601R-57-4039A. (M)May 20, 2003 · N412AW · Cndair CL6002B19 · SpoilersSDR A6WA200340081Skin · damagedFUSELAGE SKIN IS DAMAGED AT PAX DOOR CUTOUT FS 310. REPAIRED DAMGE AT PAX DOOR CUTOUT FS 310 IAW BOMBARDIER INC REO 601R-53-21-160A. (M)May 20, 2003 · N412AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200340080Skin · damagedFUSELAGE SKIN IS DAMAGED AT PAX DOOR CUTOUT FS 349. REPAIRED FUSELAGE SKIN AT PAX DOOR CUTOUT FS 349 IAW BOMBARDIER INC REO 601R-53-21-078. (M)May 20, 2003 · N412AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200340068Skin · damagedFUSELAGE SKIN IS DAMAGED AT PASSENGER DOOR CUTOUT FS 349. REPAIRED FUSELAGE SKIN AT PASSENGER DOOR CUTOUT FS 349 IAW BOMBARDIER INC REO 601R-53-21-078. (M)May 20, 2003 · N412AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200340069Skin · damagedFUSELAGE SKIN IS DAMAGED AT PASSENGER DOOR CUTOUT FS 310. REPAIRED DAMAGE AT PASSENGER DOOR CUTOUT FS 310 IAW BOMBARDIER INC REO 601R-53-21-160A. (M)May 20, 2003 · N412AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200340070Skin · dentedRIGHT INBOARD GROUND SPOILER HAS A DENT ON TOP SKIN INSPECTED AND NDT'ED DENT IAW WVAC EO 601R-57-4039A. (M)May 20, 2003 · N412AW · Cndair CL6002B19 · SpoilersSDR A6WA200340083Structure · damagedLEFT INBOARD FLAP HAS WORN RIVET HEADS ON INBOARD RIB OUTER FACE. REPLACED DISCREPANT RIVETS IAW CRJ SRM CHAP 51 AND WVAC EO 601R-57-4038. (M)May 19, 2003 · N412AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200240031A/C Pack · malfunctionedRIGHT PACK HIGH PRESSURE 80 PSI RUNNING QRH GOT LEFT PACK HIGH PRESSURE. RETURNED TO AIRPORT. DEPOWERED AND REPOWERED AIRCRAFT. RESET PACKS CIRCUIT BREAKERS. OPS CHECK GOOD. (M)Dec 20, 2002 · N412AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA200240027Odor · detectedFLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN, SMELLED LIKE ELECTRICAL OR MECHANICAL SOURCE. SMOKE CLEARED AFTER FOLLOWING QRH PROCEDURES. MAINTENANCE GROUND RAN BOTH ENGINES, OPERATED PACKS AND INSPECTED GALLEY HEATER AND FAN FOR CORRECT OPERATION. NO DEFECSep 29, 2002 · N412AW · Cndair CL6002B19 · Air Distribution System
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