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 A6WA201240157Structure · chafedRT WING AILERON HAS MINOR CHAFING TOP LEADING EDGE. BLENDED CHAFE ON RT WING AILERON L/E IAW REO 601R-57-60-013.Dec 31, 2011 · N410AW · Cndair CL6002B19 · AileronsSDR A6WA201240150Seat Track · corrodedFIRST SECTION OF SEAT TRACK HEAVILY CORRODED. R & R SEAT TRACK IAW SRM 51-40-11, AMM 53-01-11.Dec 31, 2011 · N410AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201240154Structure · chafedLT AILERON LOWER L/E CHAFED. REMOVED CHAFING IAW REO 601R-57-60-020.Dec 30, 2011 · N410AW · Cndair CL6002B19 · AileronsSDR A6WA201240155Skin · chafedLEFT AILERON UPPER SKIN IS CHAFED ENTIRE LENGTH OF AILERON. REMOVED CHAFING IAW REO 601R-57-60-013.Dec 30, 2011 · N410AW · Cndair CL6002B19 · AileronsSDR A6WA201240148Lug · chafedLEFT MLG DOOR LUG CHAFED. REMOVED CHAFING IAW REO 601R-52-82-143.Dec 30, 2011 · N410AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201240149Structure · chafedRT MLG DOOR CHAFED ON FWD AND AFT EDGES. C/W REO`S 601R-52-82-034 & 601R-52-82-102. BLENDED, ALODINED, PRIMED & TOP COATED AFT LOCATION CHAFING.Dec 30, 2011 · N410AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201240156Panel · chafedPANEL 599BB CHAFED. BLENDED PANEL 599BB DAMAGED AREA, FOUND REMAINING MATERIAL TO BE WITHIN SERVICEABLE LIMITS IAW REO 601R-57-60-020.Dec 30, 2011 · N410AW · Cndair CL6002B19 · AileronsSDR A6WA201240147Rod · chafedRT MLG DOOR ROD LUG CHAFED. C/W REO 601R52-82-143. MEASURED CHAFING AFTER BLENDING IAW REO STEP 1, ORIG MATERIAL 0.329, IN LIMITS IAW REO. C/W NDT, NO DEFECTS NOTED. RETURNED FINISH TO A023 IAW REO 601R-52-82-143.Dec 30, 2011 · N410AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201240146Door · chafedLT MLG DOOR CHAFED IN 2 PLACES, BOTTOM L/E. REMOVED CHAFING IAW REO 601R-52-82-034.Dec 30, 2011 · N410AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201240145Skin · dentedLT INBD FLAP LOWER SKIN HAS DENT TOWARDS T/E AFT OF OTBD MLG TIRE. DENT ON LT INBD FLAP LOWER SKIN FOUND TO BE OUT OF LIMITS. REPAIRED DAMAGED AREA IAW SRM 57-52-00, REPAIR NR 3.Dec 29, 2011 · N410AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201240144Guide · chafedLT OTBD ROLLER GUIDE CHAFED. BLENDED LT OTBD FLAP ROLLER GUIDE, REMAINING MATERIAL IS WITHIN SERVICEABLE LIMITS IAW REO 601R57-51-143, TOTAL AMOUNT REMOVED 0.008, MAX ALLOWED 0.005.Dec 3, 2011 · N410AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201140980Landing Gear · malfunctionedGEAR WAS SELECTED DOWN AT 150 KTS, FLAPS AT 30. A BANGING NOISE WAS HEARD COMING FROM THE NOSE AREA. IT TOOK APPROX 10-15 SECS BEFORE NOSE GEAR INDICATED GREEN WHICH OCCURRED AFTER THE MAIN GEAR SHOWED GREEN. NO GEAR UNSAFE INDICATION. OPENNov 17, 2011 · N410AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA201040199Skin · damagedFUSELAGE SKIN DENTED AND CRACK ON RT SIDE JUST FWD OF VERTICAL STABILIZER 67.5. REPAIRED DAMAGE TO FUSELAGE SKIN AND OTHER DAMAGE AT RT SIDE AT 67.5 IAW REO 601R-53-71-110, O SPLICED SECTION OF UPPER SKIN, SPLICED SECTIO OF AFT WEB STIFFENER. REPLACED 3 EA SMar 11, 2010 · N410AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA201040197Skin · damagedACFT SKIN WAS SCRATCHED AND DENTED AT FS 736, STR 26L AND STR 25R, DAMAGE IS ON BELLY, REF LOGBOOK PG 180013, BLOCK 2. COLD WORKED DENTS AND BLENDED MINOR SCRATCHES AND INSTALLED SERVICEABLE STR26L, IAW REO 601R-53-61-355.Mar 10, 2010 · N410AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA201040202Skin · damagedREMOVED DAMAGED RT LOWER SKIN BETWEEN FS 755.0 AND 67.5 (VERTICAL STABILIZER REAR SPAR). R & R WITH SERVICEABLE SKIN.Mar 9, 2010 · N410AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA201040201Angle · damagedREMOVED DAMAGED RT CTR SECTION OF CORNER CAP ANGLE (VERTICAL STABILIZER REAR SPAR). REMOVED DAMAGED RT CTR SECTION OF CORNER CAP ANGLE AND INSTALLED SERVICEABLE CORNER CAP ANGLE.Mar 8, 2010 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040200Finger Doubler · damagedREMOVED DAMAGED LOWER RT OTBD FINGER DOUBLER FROM FS 67.5 FROM STR 13R TO STR 26R IAW SRM 51-42-06. INSTALLED SERVICEABLE RT LWR DOUBLER AT 67.5 FROM STR 13R TO STR 26R IAW SRM 51-42-06.Mar 2, 2010 · N410AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA201040198Stringer · damagedMWC 51589-3000-0004- AIRCRAFT DAMAGE FOUND ON STRINGERS JUST FWD OF AFT BULKHEAD. FWD STRINGER 12R,13R, & 14R (REF LOGBOOK 180012, BLOCK) FROM FS 755 TO VERTICAL STABILIZER REAR SPAR. R & R STR 12R, & STR 14R IAW SRM 51-42-06.Mar 2, 2010 · N410AW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA201040110Bracket · crackedBRACKET ON TOP OF LT MLG WW IS CRACKED. R & R BRACKET IAW REO 601R53-42-007.Jan 24, 2010 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040044Retainer · gougedRT PYLON PANEL 422AB SUPPORT ANGLE IS GOUGED. REMOVED DAMAGED SEAL RETAINER AND INSTALLED SERVICEBLE RETAINER.Jan 21, 2010 · N410AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA201040046Seat Track · corrodedNR 1 SEAT RAIL RT INBD CORRODED. REMOVED UNSERVICEABLE NR 1 RT INBD SEAT RAIL AND INSTALLED SERVICEABLE NR 1 RT INBD SEAT RAIL.Jan 21, 2010 · N410AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201040115Stiffener · crackedFOUND (VISUAL) RBL 18 STIFFENER ON FS 559 BULKHEAD CRACKED AT LOWEST OTBD RIVET. COMPLIED WITH REPAIR OF RBL 18 STIFFENER ON FS 559 BULKHEAD BY INCORPORATION OF REO`S 601R-53-41-260, AND 601R-53-41-609.Jan 19, 2010 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040042Hinge Fitting · gougedRT ENGINE LWR TRANS COWL INNER INBD CTR HINGE FITTING IS GOUGED. REPAIRED GOUGE IAW REO NR 601R-78-33-3922.Jan 19, 2010 · N410AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201040041Hinge Fitting · gougedRT ENGINE UPR TRANS COWL INNER INBD HINGE FITTING IS GOUGED. REPAIRED GOUGE IAW REO 601R-78-33-3923.Jan 19, 2010 · N410AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201040039Web · crackedHYD SYS NR 1 FWD ACCUMULATOR MOUNT WEB CRACKED UNDER MOUNT INSTALLED NEW WEB PN 600-75221-109.Jan 18, 2010 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040040Duct · crackedAPU UPPER INTAKE DUCT CRACKED, REMOVED AND REPLACED.Jan 18, 2010 · N410AW · Cndair CL6002B19 · APU Core EngineSDR A6WA201040038Intercostal · crackedINTERCOASTAL FUSELAGE IS CRACKED ON FWD END (AT APU DOOR ACTUATOR). REMOVED AND REPLACED INTERCOSTAL.Jan 18, 2010 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040037Structure · damagedRT PYLON PANEL 422DB DIVIDER ARE BOTH CRACKED. REMOVED DAMAGED RT PYLON PNL 422DB DIVIDERS AND INSTALLED 2 EA SERVICEABLE DIVIDERS IAW SRM 51-42-10, 51-42-10.Jan 15, 2010 · N410AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA201040034Seal · damagedMETAL SEAL UNDER LT FLIGHT SPOILER BETWEEN CENTER HINGES IS CRACKED. REMOVED DAMAGED SEAL AND INSTALLED SERVICEABLE SEAL.Jan 14, 2010 · N410AW · Cndair CL6002B19 · SpoilersSDR A6WA201040196Bracket · corrodedCORROSION ON PAX DOOR C/O SILL, AFT HANDRAIL CLEAT AND BRACKET. REMOVED AND REPLACED PAX DOOR C/O AFT HANDRAIL CLEAT AND BRACKET WITH SERVICEABLE P/N 601R31527-217, PRACKET & PN 601R31527-137 CLEAT, IAW SRM 51-42-06 & 51-42-13.Jan 13, 2010 · N410AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040116Bracket · corrodedCORROSION ON PAX DOOR CUT-OUT SILL, AFT HANDRAIL CLEAT AND BRACKET. R & R PAX DOOR CUT-OUT AFT HANDRAIL CLEAT BRACKET WITH SERVICEABLE PN 601R31527-217 BRACKET AND PN 601R31527-137 CLEAT, IAW SRM 51-42-06 AND 51-42-13.Jan 13, 2010 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040112Skin · crackedPAX DOOR FWD SIDE SKIN CRACKED AT HANDRAIL. REMOVED DAMAGED AREA AND REPLACED WITH 2 EACH REPAIR ANGLES AND EXTERNAL DOUBLER IAW REO 601R-52-11-702.Jan 13, 2010 · N410AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040035Structure · crackedAPU ENCLOSURE CRACKED ON AFT SIDE ON DOOR MATING SURFACE REPAIRED CRACKS IAW REO 601R-49-11-070.Jan 13, 2010 · N410AW · Cndair CL6002B19 · APU Cowling/ContainmentSDR A6WA201040036Stiffener · crackedAPU ENCLOSURE DOOR AFT STIFFENERS CRACKED ON UPPER END REPAIRED CRACKS IAW REO 601R-49-11-070.Jan 13, 2010 · N410AW · Cndair CL6002B19 · Auxiliary Power Unit (APU) DoorsSDR A6WA201040111Door Frame · crackedFRAME ANGLE BELOW PAX DOOR PANEL 832AR CRACKED. REMOVED CRACKED FRAME ANGLE AND INSTALLED NEW SERVICEABLE PN 601R-318094-2.Jan 12, 2010 · N410AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA201040114Attach Angle · crackedPAX DOOR VENT FLAP AFT ATTACH ANGLE APPEARS TO BE CRACKED. REMOVED CRACKED ATTACH ANGLE AND DUPLICATED IAW SRM 51-24-24.Jan 12, 2010 · N410AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040113Attach Angle · crackedLT OTBD FLAP OTBD HINGE ARM HAS CRACKED FAIRING ATTACH ANGLE ON INBD SIDE. R & R ANGLE AT LT OTBD FLAP OTBD HINGE INBD SIDE IAW SRM 57-54-00, 51-40-00, 51-40-11, 51-42-13.Jan 11, 2010 · N410AW · Cndair CL6002B19 · Wing, Attach FittingsSDR A6WA201040045Channel · crackedU-CHANNEL CRACKED ON FWD SIDE OF CARGO DOOR CUTOUT (LOWER DOOR TRACK ATTACHMENT) REMOVED DAMAGED BRACKET AND DUPLICATED AND INSTALLED NEW BRACKET.Jan 11, 2010 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940752O-Ring · cutRT ENG OIL PSI WARNING MSG DISPLAYED IN FLIGHT C/W QRH. REDUCED POWER TO IDLE FOR REMAINDER OF FLIGHT. AT IDLE OIL PSI INDICATED 36 PSI AND OIL TEMP AT 80 DEG. LANDED ACFT BELOW 47,000 LBS. FOUND O-RING AT EDP CARBON SEAL CUT REPLACED IAW AMM 72-60-00. PENov 8, 2009 · N410AW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA200940416A/C Pack · odorLEFT AC PACK HAS FUEL ODOR AT HIGHER DUCT TAPS. RAN BOTH PACK OFF ENGINE BLEED AIR NO FUEL SMELL. (K)Jul 20, 2009 · N410AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA200940375Connector · damagedON CLIMBOUT, HAD A MASTER CAUTION ON IDG 1. REMOVED AND REPLACED NR 1 ENG IDG TEMP BULB AND TEMP BULB CONNECTOR IAW 24-13-05. OPS CHECK GOOD. (K)Jul 6, 2009 · N410AW · Cndair CL6002B19 · Electrical Power System WiringSDR A6WA200940213Light · damagedAT 11,000 FT SMOKE IN COCKPIT AFTER ADJUSTING F/O FLOODLIGHT, FOLLOWED 1AC AND QRH SMOKE SUBSIDED, DECLARED EMERGENCY, LANDED, FOUND CBP4C1 POPPED. INSPECTED AND FOUND F/O FLOODLIGHT DAMAGED, INSPECTED AREA, NO FURTHER DAMAGE TO SURROUNDING AREA REF 198190/2 Apr 13, 2009 · N410AW · Cndair CL6002B19 · Flight Compartment LightingSDR A6WA200940017Actuator · malfunctionedLOG 186985/3 - FLAPS FAIL INFLT DURING EXTENSION AT ZERO DEGREES PERFORMED FLAP RESET IAW SUPP 98-018B STEPS 1.3 AND 1.4, FLAP RESET. COMPLIED WITH FIM 27-50-00 AND FOUND THE INPUT TORQUE OUT OF LIMITS ON LT FLAP DRIVE SYS. FOUND LT INBD FLAP INBD ACTUATOR TJan 15, 2009 · N410AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840334Target · looseON DEPARTURE, AFTER LANDING GEAR RETRACTION RECEIVED GEAR DISAGREE MASTER WARNING RT MAIN GEAR C/W QRH DIVERTED IAD GEAR INDICATED 3 GREEN. FOUND RT MLG UPLOCK TARGET LOOSE. RETORQUED AND PERFORMED GEAR SWINGS PER AMM 32-30-00. REMOVED FROM MEL.Apr 12, 2008 · N410AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA200840165Diaphragm · missingRUDDER UPPER CLOSURE RIB IS MISSING DIAPHRAGM CLOTH. REPAIRED IAW CRJ 200 REO 601R-55-41-037. (M)Mar 8, 2008 · N410AW · Cndair CL6002B19 · Rudder StructureSDR A6WA200840168Bulkhead · crackedFORWARD PRESSURE BULKHEAD AT FS 202.75 LBL 23.71, WL 69 IS CRACKED. REPAIRED IAW REO 601R-53-11-563. (M)Mar 7, 2008 · N410AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200840163Fairing · damagedABRASION FOUND ON RT FLAP STUB FAIRING EXTERNAL SURFACE. (M) REPLACED IAW SRM 51-42-06, 51-41-02, 51-42-11. (K)Mar 7, 2008 · N410AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200840162Fairing · damagedABRASION FOUND ON LEFT FLAP STUB FAIRING EXTERNAL SURFACE. (M) REPLACED IAW SRM 51-42-06. (K)Mar 7, 2008 · N410AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200840184Hinge · crackedPAX DOOR FOLDING STEP UPPER HINGE, REF P/N 601R31980-41, AND LOWER HINGE , REF P/N 601R31980-63 FOUND CRACKED. (M)Mar 6, 2008 · N410AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200840183Angle · crackedTWO ANGLES CRACKED ON THE REAR PRESSURE BULKHEAD AT RBL AND LBL 46 FS 621 AND WL 93.50. TWO ANGLES ON THE REAR PRESSURE BULKHEAD REPLACED IAW REO 601R-53-61-100 REV A. (M)Mar 6, 2008 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
Back to N410AW