N410AW

Service difficulty reports · 297

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 = 'N410AW' 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 A6WA201643527Seat Track · corrodedSEAT RAIL BEAM AT FS 589 - 574, LBL 9, CORRODED, REPLACED.Feb 2, 2016 · N410AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201643524Bracket · crackedCENTER WINDSHIELD RT LOWER BRACKET CRACKED. R & R CTR WINDSHIELD POST BRACKET IAW SRM 51-42-21.Feb 2, 2016 · N410AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201643522Floorbeam · crackedFLOORBEAM AT STATION 280, RBL 13 CRACKED, REPLACED.Jan 31, 2016 · N410AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201643519Bracket · crackedCENTER WINDSHIELD, LOWER LT POST BRACKET CRACKED, REPLACED.Jan 30, 2016 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201643515Fitting · crackedFLOOR ANGLE CLIPS, 4 CRACKED AT FS 280.00 & LBL 12. REPAIRED FLOORBEAM ANGLE CLIPS, 4 AT FS 280.00 & LBL 12 IAW REO 601R-53-11-136.Jan 29, 2016 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201643513Fitting · crackedCLIP AT STRINGER 14L, INTERCOSTAL AFT SIDE OF FS 621.00, BULKHEAD IS CRACKED. R & R CLIP INTERCOSTAL AT FS 621.00, BULKHEAD & STRINGER 14L IAW SRM 51-42-21.Jan 29, 2016 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201643516Angle · crackedVERTICAL FLOORBEAM ANGLE CRACKED AT FASTENER HOLES, FS 280.00 & LBL 8. R & R VERTICAL FLOORBEAM ANGLE AT FS 280.00 & LBL 8 IAW REO 601R-53-11-171.Jan 29, 2016 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201643517Web · crackedFORWARD E & E BAY, RT SIDE WEB CRACKED AT FS 193. REPAIRED FWD E & E BAY RT SIDE FLOOR IAW REO 601R-53-11-245 REV B.Jan 29, 2016 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201643514Angle · crackedVERTICAL FLOORBEAM ANGLES, 2 CRACKED FS 280.00, RBL 8. R & R VERTICAL FLOORBEAM ANGLES 2 AT FS 280.00, RBL 8, IAW REO 601R-53-11-171 REV D.Jan 29, 2016 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201643510Fitting · crackedANGLE CLIP IS CRACKED ON THE OTBD SIDE OF LBL 9 AT FS 484, IN CABIN BELOW FLOOR. INSTALLED NEW ANGLE CLIP AT LBL 9 & FS 484 IAW SRM 51-42-06 & 51-42-21.Jan 28, 2016 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201643509Intercostal · crackedCLIP AT STRINGER 13L, INTERCOSTAL AFT SIDE OF FS 621.00, BULKHEAD IS CRACKED. R & R CLIP INTERCOSTAL AT STRINGER 13L, ON AFT SIDE OF FS 621.00 BULKHEAD IAW SRM 51-42-21.Jan 27, 2016 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201643505Fitting · crackedANGLE CLIP ON THE INBD SIDE OF RBL 36 AT FS 484 CRACKED, REPLACED.Jan 26, 2016 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201643507Fitting · crackedWINDSHIELD POST ON FIRST OFFICERS SIDE, AFT LOWER FITTING CRACKED.Jan 26, 2016 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201643508Strap · gougedSEAL SURROUND AT FWD UPPER PIN FITTING ON L1 DOOR CUT OUT IS GOUGED.Jan 26, 2016 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201643506Fitting · crackedWINDSHIELD POST ON CAPTAINS SIDE, AFT LOWER FITTING CRACKED.Jan 26, 2016 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201643499Strap · corrodedFLOOR STRAP HAS CORROSION, BETWEEN RBL 36 & RT FLOOR SILL AT FS 559.00 IN THE CABIN. R & R FLOOR STRAP RBL 36 & FS 559.00 IAW SRM 51-42-06.Jan 24, 2016 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201643488Cleat · corrodedPASSENGER DOOR SILL AFT CLEAT CORRODED. REPAIRED PAX DOOR SILL AFT CLEAT IAW SRM 53-21-23, 53-00-00 & 51-40-11.Jan 22, 2016 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201643489Seat Track · corrodedRIGHT FLOOR SEAT TRACK STICK 2 HAS CORROSION. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS. INSTALLED NEW SEAT TRACK IAW REO 601R-53-00-485.Jan 22, 2016 · N410AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201543386Fuel Sys · leakingAFTER START OF APU ON THE GND, STRONG FUEL ODOR FILLED THE CABIN, ODOR DISSIPATE UPON APU SHUTDOWN. INSPECTED AFT EQUIPMENT BAY & APU ENCLOSURE DRAINS, FOUND FUEL LEAKING FROM RT ENCLOSURE DRAIN WHILE APU PUMP IS ON. APU LEAK NOTED LEFT OF COMBUSTOR DRAIN ONDec 18, 2015 · N410AW · Cndair CL6002B19 · APU Engine Fuel and ControlSDR A6WA201543256Warning System · activatedABORTED TO AT 55 KTS, DUE TO IDG 1 CAUTION. FOLLOWED BY GEN 1 CAUTION MSG.Nov 16, 2015 · N410AW · Cndair CL6002B19 · AC Indicating SystemSDR A6WA201543049Hydraulic System · fluctuatesFLIGHT 3987, HYD PUMP 2B PRESS FLUX 0-3000 PSI, UNUSUAL RUBBER & SMOKE ODOR. NO EVIDENCE OF RUBBER & SMOKE ODOR FROM THIS ACFT AT THIS TIME. HYD PRESS SYS NR 1 FLUX 0-3000 PSI, APPROX 1 TIME EACH 10 MIN.Sep 11, 2015 · N410AW · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA201543039Engine · surgesLEFT ENG ITT AT IDLE IS 590 DEGREES C & RT ENG ITT AT IDLE IS 480 DEGREES C. AT TAKEOFF POWER 91%, LT ENG WAS SLOW TO SPOOL UP, ITT IMMEDIATELY WENT TO 900 DEGREES C & AN AUDIBLE SURGE WAS HEARD FROM LT ENG. PERFORMED ENG POWER ASSURANCE CHECK IAW AMM 71-00-Sep 5, 2015 · N410AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA201543014Light · defectiveFLIGHT 3768, FLOOR TRACK LIGHTING AFT OF ROW 8 IS MISSING ARROWS. PLACARDED & PLACED ON MEL. R & R FLOOR TRACK LIGHTS AFT OF ROW 8 IAW AMM 33-51-01. OPERATIONS CHECKED GOOD. REMOVED PLACARD & REMOVED FROM MEL.Aug 29, 2015 · N410AW · Cndair CL6002B19 · Emergency LightingSDR A6WA201542832Bulkhead · damagedAFT PRESS BULKHEAD DAMAGED.Jun 6, 2015 · N410AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201542649Wire Harness · inoperativeEMERGENCY LIGHTS ON RT SIDE WILL NOT ILLUMINATE. R & R AFT EMERGENCY LIGHT HARNESS IAW AMM 33-50. OPS CHECKED GOOD.Apr 19, 2015 · N410AW · Cndair CL6002B19 · Light System WiringSDR A6WA201542507Inverter · inoperativeEMERGENCY LIGHTS ROW 2 - 5, INOPERATIVE. R & R NR 2 INVERTER IAW AMM 33-51-07. OPS CHECKED GOOD.Mar 13, 2015 · N410AW · Cndair CL6002B19 · Emergency LightingSDR A6WA201542508Inverter · inoperativeLT WING EMERGENCY EXIT LOWER SIGN DOES NOT LIGHT UP. R & R NR 2 EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD.Mar 13, 2015 · N410AW · Cndair CL6002B19 · Emergency LightingSDR A6WA201542504Connector · unsecure3841 FLOOR EMER LIGHTS INOPERATIVE AT ROW 2 - 5. SECURED ELEC CONNECTOR AT ROW 3 IAW AMM 33-51-01 & SUPP 13-022. OPERATIONS CHECKED GOOD AT THIS TIME.Mar 12, 2015 · N410AW · Cndair CL6002B19 · Light System WiringSDR A6WA201542498Connector · unsecureEMERGENCY LIGHTS INOPERATIVE AT ROW 2 - 5. SECURED RED ELECTRICAL CONNECTOR AT ROW 3 IAW AMM 33-51-01 & SUPP 13-022. OPS CHECKED GOOD.Mar 11, 2015 · N410AW · Cndair CL6002B19 · Light System WiringSDR A6WA201542468Light · inoperativeSEVERAL SECTIONS OF FLOOR TRACK LIGHTING INOPERATIVE.Mar 3, 2015 · N410AW · Cndair CL6002B19 · Emergency LightingSDR A6WA201542439Landing Gear · malfunctionedDURING GEAR RETRACTION ON TAKEOFF RECEIVED GEAR DISAGREE WARNING WITH NOSE GEAR INDICATING DOWN & BOTH MAINS UP. COMPLIED WITH QRH ALL 3 LANDING GEAR SHOWED DOWN. APPROX WT AT LANDING 47200. NOSE GEAR & NOSE DOOR MSGS. IN ADDITION, THE GEAR LEVER WAS LEFT Feb 25, 2015 · N410AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA201542414Warning System · activatedON DEPARTURE AFTER GEAR RETRACTION RECEIVED TRIPLE CHIME & NOSE GEAR DOOR WARNING MSG & GEAR DISAGREE MSG. RAN QRH & RETURNED. MSG POSTED IMMEDIATELY AFTER HANDLE MOVEMENT. HYD PUMPS WERE IN AUTO, NO OVERWEIGHT LANDING. MAINS SHOWED UP & LOCKED, NOSE GEAR Feb 16, 2015 · N410AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA201442212Connector · out of adjust3728 FLOOR LEVEL EMER LIGHTING INOPERATIVE BETWEEN ROWS 2 - 5. SIDEWALL EMER LIGHTS AT ROW 8AC INOPERATIVE. ADJUSTED EMER FLOOR LIGHT CONNECTION AT ROW 5. OPERATIONS CHECKED GOOD AT THIS TIME.Dec 1, 2014 · N410AW · Cndair CL6002B19 · Light System WiringSDR A6WA201442176Warning System · activatedAFTER DEPARTURE AT 3000 FT RECEIVED WING OVERHEAT WARNING MSG. COMPLIED WITH QRH MSG CLEARED WITH WING ANTI-ICE OFF, AIR RETURN TO CVG.Nov 16, 2014 · N410AW · Cndair CL6002B19 · Overheat DetectionSDR A6WA201442160Warning System · false activationWING OVERHEAT WARNING MSG DURING CLIMB BETWEEN 5K & 8K FEET. IAW QRH TURNED OFF ANTI-ICE MSG EXT, USED STBY MODE FOR REMAINDER OF THE FLIGHT. MSG DID NOT RETURN.Nov 13, 2014 · N410AW · Cndair CL6002B19 · Overheat DetectionSDR A6WA201441129Hinge · corrodedPASSENGER DOOR TOP STEP HINGE CORRODED. REPLACED HINGE IAW CRJ200 SRM 51-41-02.Jan 25, 2014 · N410AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201401254528Support · crackedRIGHT TR NOSE COWL SUPPORT RING, SPRING SEAL, CRACKED OTBD LOWER POS 1. R & R WITH NEW SERVICEABLE SEAL IAW CMM 78-30-00.Jan 25, 2014 · N410AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201401244514Skin · crackedFUSELAGE SKIN CRACKED IN AFT RT WW CUT OUT. REPAIRED IAW REO 601R-53-11-2614 REV.Jan 24, 2014 · N410AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA201441094Skin · gougedLEFT FUSELAGE 3 INCH GOUGE DAMAGE AT FS 409.00 + 16 & WL 73.50. CUT OUT DAMAGE, FABRICATED & REPAIRED DOUBLER & FILLER, NDT CUT OUT, APPLIED CORROSION PREVENTION TREATMENT, PRIMER SURFACE TREATMENT, FAY & FILLET SEALED, INSTALLED REPAIR DOUBLER, FILLER & RESTJan 22, 2014 · N410AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA201401204538Handle · unserviceableCARGO DOOR HANDLE HAS EXCESSIVE PLAY. REMOVED UNSERVICEABLE HANDLE ASSEMBLY & REPLACED WITH A NEW SERVICEABLE ASSEMBLY IAW CRJ 200 SRM 51-42-21 & SRM 51-40-11.Jan 20, 2014 · N410AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA201401204521Tie Down · corrodedCARGO FLOOR TIE DOWNS CLEATS AT FS 589 & 605 LBL 9 CORRODED. R & R IAW SRM 51-41-02.Jan 20, 2014 · N410AW · Cndair CL6002B19 · Cargo CompartmentsSDR A6WA201401194524Housing · chafedSERVICE DOOR OUTER HANDLE HOUSING IS CHAFED & GOUGED. REPLACED HOUSING IAW CRJ 200 SRM & AMM SRM 51-40-11 & SRM 51-42-21.Jan 19, 2014 · N410AW · Cndair CL6002B19 · Service DoorsSDR A6WA201401254529Skin Panel · damagedLIGHTNING BURN DAMAGE TO RT OTBD FLAP UPPER SKIN PANEL & TE. PERFORMED CHANNEL SPLICER & DOUBLER REPAIR IAW CRJ 200 SRM 57-53-00 REPAIR NR 3.Jan 15, 2014 · N410AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201401144535Mount Bracket · crackedSERVICE DOOR INDICATOR SWITCH MOUNT IS CRACKED. R & R SWITCH MOUNT BRACKET WITH SERVICEABLE PART PN 601R38723-17 IAW CRJ SRM 51-40-11 & 51-42-21.Jan 14, 2014 · N410AW · Cndair CL6002B19 · Service DoorsSDR A6WA201401144534Bracket · crackedRIGHT BRAKE PRESS TRANSDUCER BRACKET IS CRACKED. R & R ONE EACH RT BRAKE PRESS TRANSDUCER BRACKET.Jan 14, 2014 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201401114539Mount Bracket · crackedPASSENGER DOOR PRESS DOOR AFT MOUNT BRACKET CRACKED. REMOVED UNSERVICEABLE BRACKET, INNER ANGLE. FABRICATED & INSTALLED SERVICEABLE BRACKET, INNER ANGLE.Jan 11, 2014 · N410AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201401114531Vane · chafedRIGHT INBD FLAP VANE IS CHAFED TWO SPOTS, INBD & MIDDLE LE SECTIONS, AT FLAP STATIONS 58 & 110. R & R UNSERVICEABLE SECTIONS OF RT INBD FLAP VANE LE WITH NEW SERVICEABLE LE SECTIONS.Jan 11, 2014 · N410AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201401114523Plate · crackedCARGO THRESHOLD STEP PLATE CRACKED. STOP DRILLED & REMOVED CRACK DAMAGE IAW CRJ 200 SRM 51-12-00.Jan 11, 2014 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201401104530Attach Angle · crackedRIGHT WING INBD LE PANEL OTBD ATTACH ANGLE CRACKED AT LOWER RADIUS. R & R ATTACH ANGLE.Jan 10, 2014 · N410AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA201401104527Acoustic Panel · damagedRIGHT LOWER TRANS COWL ACOUSTIC PANEL HAS FIVE EACH DENTS WITH GOUGING & CRACKED SKIN. REPLACED FIVE DENTS IAW CRJ 200 SRM 51-12-00. REPAIRED WITHIN STRUCTURAL LIMITS, NO CRACKS NOTED IN SKIN.Jan 10, 2014 · N410AW · Cndair CL6002B19 · Engine Thrust Reverser
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