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 A6WA2016122244680Skin · chafedRIGHT INBD FLAP VANE LEADING EDGE IS CHAFED.Dec 20, 2016 · N412AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2016122244676Attach Angle · crackedATTACH ANGLE AT BS 625 STRINGER 14L IS CRACKED.Dec 17, 2016 · N412AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2016122244675Attach Angle · crackedATTACH ANGLE AT BS 625 STRINGER 13L IS CRACKED.Dec 17, 2016 · N412AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2016122244670Support Fitting · crackedWINDSHIELD CENTER POST INTERNAL SIDE LOWER STRAP LT SUPPORT FITTING CRACKED. REMOVED AND REPLACED THE SUPPORT FITTING IAW SRM 51-42-21.Dec 16, 2016 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2016122244669Floor Support · corrodedMAIN CABIN FLOOR SUPPORT ANGLE CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06, 51-42-21, AND 51-42-10.Dec 16, 2016 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2016122244672Floorbeam · crackedFWD FLOORBEAM ANGLE AT BS 280 IS CRACKED NEAR RBL 9.Dec 16, 2016 · N412AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA2016122244665Support Fitting · crackedWINDSHIELD CENTER POST INTERNAL SIDE LOWER STRAP RT SUPPORT FITTING CRACKED. REMOVED AND REPLACED THE SUPPORT FITTING IAW SRM 51-42-21.Dec 16, 2016 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201644668Attach Angle · corrodedSERVICE DOOR SILL FWD ATTACH ANGLE CORRODED. REMOVED AND REPLACED ANGLE IAW SRM 51-42-06.Dec 16, 2016 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2016122244673Floorbeam · corrodedFLOORBEAM BS 280 HAS CORROSION ON THE TOP SIDE BETWEEN LBL 9 AND RBL 9.Dec 16, 2016 · N412AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA2016122844667Seat Track · corrodedRIGHT MAIN CABIN SEAT TRACK CORRODED OUT OF LIMITS, BS 364 - 409, RBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.Dec 16, 2016 · N412AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2016122244662Skin · dentedRIGHT INBD FLAP LOWER SKIN HAS A DENT 1 1/2 INCHES FROM THE TRAILING EDGE AND 6 INCHES FROM THE INBD EDGE.Dec 12, 2016 · N412AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2016121244659Bracket · corrodedPAX DOOR LOWER SILL AFT CLEAT BRACKET IS CORRODED.Dec 9, 2016 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2016121244658Bracket · corrodedPAX DOOR SILL FWD CLEAT BRACKET IS CORRODED.Dec 9, 2016 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2016121244660Floorbeam · crackedLBL 9, INBD ANGLE ON BS 280 FLOORBEAM IS CRACKED.Dec 9, 2016 · N412AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201644433Connector · out of adjustEMERGENCY ROW LIGHTING BETWEEN ROW 5 AND 8 INOP. INSPECTED FLOOR TRACK LIGHTING AT ROW 5 TO 8 AND ADJUSTED CONNECTOR P39LY, AND OPS CHECK GOOD IAW AMM 33-51-01.Oct 16, 2016 · N412AW · Cndair CL6002B19 · Light System WiringSDR A6WA201644369Light · inoperativeCREW REPORTED EMERGENCY FLOOR TRACK LIGHTS NOT WORKING FROM ROWS 5-8.Sep 25, 2016 · N412AW · Cndair CL6002B19 · Emergency LightingSDR A6WA201643733Switch · out of rigWHILE EN-ROUTE RECEIVED LT REVERSER UNLOCKED CAUTION. COMPLIED WITH QRH & DIVERTED. REVERSER APPEARS STOWED ON WALK AROUND. DEACTIVATED LT THRUST REVERSER IAW SUPP 15-046. COMPLIED WITH M ACTION. TROUBLE SHOT & FOUND LT THRUST REVERSER STOW SWITCH TO BE EMar 28, 2016 · N412AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201643502Trim System · bindingWITH CAPTAIN FLYING PILOT , AUTOPILOT OFF DESCENDING THRU 1500 FT EXPERIENCED BINDING OF ELEVATOR DOWN PITCH. FREED MOVEMENT BY EXTENDING TRAVEL FARTHER FORCING YOKE FWD. BINDING CLEARED WITH A POP SOUND FROM THE FIRST OFFICERS SIDE YOKE AREA. ACFT WAS NOTJan 24, 2016 · N412AW · Cndair CL6002B19 · Elevator Tab Control SystemSDR A6WA201543018Ballast · defectiveFLIGHT 3725, ELEC SMELL IN CABIN, MIDDLE TO FWD SECTION OF CABIN. R & R BALLAST BH4 IAW AMM 33-21. OPERATIONS CHECKED GOOD AT THIS TIME.Sep 1, 2015 · N412AW · Cndair CL6002B19 · Passenger Compartment LightingSDR A6WA201542979Wire · brokenFLIGHT 3901, 3992X2 XLD EMER FLOOR TRACK LIGHTING ROW 8 & AFT WN ILLUMINATE. REPAIRED BROKEN WIRES TO AFT SECTION OF EMER FLOOR TRACK LIGHTING IAW AMM 33-51-01 & ESPM 20-11-00. OPERATIONS CHECKED GOOD.Aug 11, 2015 · N412AW · Cndair CL6002B19 · Light System WiringSDR A6WA201542423Display · malfunctionedDURING TAKEOFF ROLL, LOST ED1, ED2, FMS, RTU1, & RTU2 DISPLAY. CONTINUED DEPARTURE & AT APPROX FL 15000 ADJUSTING DISPLAY KNOB, DISPLAYS RETURNED. DECLARED AN EMERGENCY & RETURNED, LANDED APPROX 45,000 LBS.Feb 19, 2015 · N412AW · Cndair CL6002B19 · Central DisplaySDR A6WA201542333Channel · damagedLOWER CHANNEL ON RT MLG APRON STRUCTURE IS DAMAGED. DENTED & TORN BETWEEN FS 529 & 533.Jan 17, 2015 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201542321Stiffener · crackedFS 409+128 LBL 18 VERTICAL STIFFENER HAS CRACK ON LOWER AFT OTBD CORNER.Jan 17, 2015 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201542323Skin · chafedRIGHT AILERON UPPER LE SKIN HAS CHAFING BETWEEN CTR OTBD HINGE.Jan 17, 2015 · N412AW · Cndair CL6002B19 · AileronsSDR A6WA201542322Stiffener · crackedFS 409+128 LBL 27 STIFFENER HAS CRACK AT LOWER AFT INBD & OTBD CORNERS.Jan 17, 2015 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201542332Channel · damagedLOWER CHANNEL ON LT MLG APRON STRUCTURE DAMAGED. DENTED & TORN BETWEEN FS 529 & 533.Jan 16, 2015 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201542316Seat Track · corrodedLBL 27 SEAT TRACK CORRODED AT APPROX FS 559+80.Jan 11, 2015 · N412AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201542314Seal · crackedRIGHT THRUST REVERSER SPRING SEAL CRACKED, NEAR 5 O'CLOCK POSITION.Jan 9, 2015 · N412AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201542313Drag Angle · crackedRIGHT MLG WW BATTERY RIB DRAG ANGLE IS CRACKED.Jan 8, 2015 · N412AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA201542318Drag Angle · crackedLEFT MLG WW BATTERY RIB DRAG ANGLE IS CRACKED.Jan 8, 2015 · N412AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA201542315Fitting · crackedCLIPS AT STRINGER 4L & FS 280 ARE CRACKED.Jan 8, 2015 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201542294Fitting · crackedLBL 36 FS 484 CLIP IS CRACKED ON UPPER END, OTBD CLIP.Jan 8, 2015 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201542295Seat Track · corrodedLBL 9 BAGGAGE TIE DOWNS AT FS 583.00 ARE CORRODED & SEAT TRACK AT LBL 9 AT FS 615.00 IS CORRODED.Jan 8, 2015 · N412AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201542312Cargo Track · corrodedBAGGAGE COMPARTMENT SEAT TRACKS AT LBL 9 & RBL 9 AT FS 559+90 & FS 563 CORRODED.Jan 7, 2015 · N412AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201542329Structure · crackedCRACK IN AFT LT CORNER ON NLG WW CUT OUT.Jan 5, 2015 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201442228Connector · disconnectedRECEIVED SMOKE CAUTION MSG IN FLIGHT WHILE PAX WAS IN LAVATORY. INSPECTED LAVATORY & FOUND NO EVIDENCE OF SMOKE IN LAVATORY. AFTER THOROUGH INSPECTION OF SINK & TOILET ELECTRICAL COMPONENTS. GAINED ACCESS TO LAVATORY SMOKE DETECTOR & FOUND CONNECTOR DISCONNDec 9, 2014 · N412AW · Cndair CL6002B19 · Fire Protection System WiringSDR A6WA201442037Lens · missingEMERGENCY LIGHT FLOOR TRACK AT BULKHEAD ROW 1 MISSING ORANGE OVERLAY.Oct 8, 2014 · N412AW · Cndair CL6002B19 · Emergency LightingSDR A6WA201441633Unknown · odorREQUEST INSP OF BURNING RUBBER SMELL MORE NOTICEABLE NEAR PAX DOOR. PERFORMED OPERATIONS TEST OF GALLEY HEATER SYS IAW AMM 21-23-05, INSPECTED TIRES FOR ABNORMAL WEAR IAW AWAC SUP 08-005C. PERFORMED OPERATIONS CHECK OF AIR CONDITIONING SYS IAW AMM 21-51-00, Jun 11, 2014 · N412AW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA201308194029Aileron Sys · malfunctionedON APROACH, UNCOMMANDED AILERON MOVEMENT AND ROLL. AILERON MOVEMENT OBSERVED ON FLT CONTROL SYNOPTIC SAW LT MOVE NOT SURE ABOUT RIGHT AUTOPILOT OFF AT THE TIME. APROX 2 MIN PRIOR TO LDG. OPENAug 18, 2013 · N412AW · Cndair CL6002B19 · Aileron Control SystemSDR A6WA201302124013Yaw Damper · faultyDURING CRUISE FLT WITH A/P ON A/C YAWED SUDDENLY BOTH RT & LT YAWING MOVEMENTS LESSENED AT SPEEDS 250 KIAS OR LESS. YAWING MOVEMENTS WOULD LAST APPROXIMATELY 1-2 MINUTES THAN SUBSIDE FOR 10 MINUTES AND THAN BEGIN AGAIN. REMOVED AND REPLACED LEFT & RIGHT YAW Feb 11, 2013 · N412AW · Cndair CL6002B19 · Autopilot SystemSDR A6WA20134676Bracket · crackedSUPPORT BRACKET ON RIGHT MLG AFT TRUNNION I/B SIDE IS CRACKED. REPLACED WITH NEW SERVICEABLE SUPPORT BRACKET P/N 601R10205-30 IAW CRJ SRM 51-42-21.Jan 30, 2013 · N412AW · Cndair CL6002B19 · Main Landing Gear Attach SectionSDR A6WA201302050665Structure · chafedCHAFE ON LEFT ENGINE UPPER CORE COWL FWD AT 11 O`CLOCK POSITION. REMOVED & REPLACED REBATE DISH WITH SERVICEABLE IAW SRM 51-22-00.Jan 30, 2013 · N412AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA2013020504669Skin · chafedLEFT I/B FLAP VANE LEADING EDGE CHAFED BY I/B & O/B PADS. REMOVED AND REPLACED I/B SKIN IAW SRM 51-40-11 & 51-42-13. O/B POSITION LIMITS PER GREO 601R-57-52-004 REV D.Jan 29, 2013 · N412AW · Cndair CL6002B19 · Leading Edge DevicesSDR A6WA0134660Frame · corrodedCORROSION ON FRAME 333 STR 26L TO 25R & AROUND GROUND LOCATIONS. REMOVED AND REPLACED FRAME SECTION (601R32004-55) IAW REO 601R-53-21-2400.Jan 29, 2013 · N412AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA2013020500670Beam · gougedLEFT I/B FLAP VANE SLIDING BEAMS ARE GOUGED UNDER UPPER AD LOWER ROLLERS. REPAIRED PER REO 601R-57-52-1979.Jan 28, 2013 · N412AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2013020504668Bracket · chafedLEFT WING TE FLAP VANE MOUNTING BRACKET IS CHAFED AND ON IN FRONT THE I/B EDGE. REMOVED CHAFED DAMAGE BY EDGE BLENDING.Jan 28, 2013 · N412AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA20134663Threshold · corrodedSERVICE DOOR THRESHOLD CORRODED. REMOVED AND REPLACED THRESHOLD P/N: 601R38957-31.Jan 28, 2013 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201340000663Sill · corrodedCARGO DOOR LOWER SILL HAS NUT PLATES CORRODED WITH CORROSION. REPAIR CORROSION ON CARGO DOOR LOWER SILL IAW REO 601R-53-61-690 REV D AND SRMS 51-21-06, 51-24-21, 51-40-11.Jan 26, 2013 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201302204804Skin · gougedGOUGE ON I/B LOWER SKIN ON RIGHT I/B FLAP. REMOVED & REPLACED SKIN IAW CRJ 200 SRM 57-52-00 REPAIR 3 FIG 202 SHEET 2.Jan 25, 2013 · N412AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201340219803Trunnion · damagedLEFT AND RIGHT MLG TRUNNION FOUND WEB TO HAVE TOOL MARKS. REPAIRED TRUNNION PER REO 601R-57-21-1855.Jan 25, 2013 · N412AW · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
Back to N412AW