N410AW

Service difficulty reports · 295

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 A6WA202607128899Warning Light · illuminatedDURING CLIMB RECEIVED FLAPS FAIL CAUTION OCCURRED AT FL220. FLAPS WERE NOT SELECTED FLAPS FAILED AT 0. NO IMPROPER FLAP HANDLE MOVEMENT SUSPECTED. AIRCRAFT REMOVED FROM SERVICE.Jul 12, 2026 · N410AW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR A6WA202502128862Smoke Detector · false activationSMOKE TOILET CAUTION MESSAGE DISPLAYED WHILE PARKED AT GATE. C/W QRH MESSAGE REMAINED. C/B 2C5 2D14 2D15 2S2 2U2 PULLED. AIRCRAFT REMOVED FROM SERVICE. R&R LAV SMOKE DETECTOR IAW AMM 26-16-01. OPS CHECK GOOD AT THIS TIME. CLOSED C/B 2C5, 2D14, 2D15, 2S2, Feb 12, 2025 · N410AW · Cndair CL6002B19 · Smoke DetectionSDR A6WA202405288755Winglet · damagedREPAIR TO RIGHT WINGLET TIP STRUCTURE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FOLLOWING ITEMS REF CRJ200 SRM 51-42-13, 51-40-11, 51-41-00, 51-42-06, 51-42-20, 51-42-13 REV.39. TIP FAIRING PN 600-15110-4; LEADING EDGE PN 600-15111-4; AFT FMay 28, 2024 · N410AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA202405138748Support Bracket · crackedCRACK FOUND ON POWER RECEPTACLE SUPPORT. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED BRACKET SUPPORT MEMBER P/N 600-33-83-33 ON POWER RECEPTACLE IAW SRM 51-42-06 REV. 39. ALL WORK PERFORMED UNDER WORK ORDER 004309, CARD 20031, TT: 47,227:03 TC: 4May 13, 2024 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202405118746Fitting · crackedCRACKED FITTING ON UPPER TRANSLATING COWLING DOOR. ACFT REMOVED FROM SERVICE. REMOVED & REPLACED FITTING INTERLOCK RH ON UPPER TRANSLATING COWLING DOOR, IAW SRM 51-42-28 REV. 39 DATE 2024-05-08. ALL WORK PERFORMED UNDER WORK ORDER 004309. NO. 20124,May 11, 2024 · N410AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA202405108744Seat Track · damagedAIRCRAFT REMOVED FROM SERVICE. REPAIR CAPTAINS I/B SEAT TRACK 601R-53-11-1093C. REPAIR CAPTAINS I/B SEAT TRACK 601R-53-11-1093C.May 10, 2024 · N410AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA202405108745Seat Track · damagedREPAIR CAPTAINS I/B SEAT TRACK 601R-53-11-1093C. AIRCRAFT REMOVED FROM SERVICE. PERFORMED PERMANENT REPAIR ON FLOOR PANEL & ANGLE AT LBL 12 BETWEEN BS 250 TO 265 IAW MHI RJ REO 601R-53-11-3927 REV. -. ALL WORK PERFORMED UNDER WORK ORDER 004309, CARD 50008May 10, 2024 · N410AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA202405048740Channel · corrodedFWD GALLEY COMPARTMENT 112 LOWER STRIP HAS SIGNS OF CORROSION. ***** AIRCRAFT REMOVED FROM SERVICE ***** REPLACED LOWER STRIP ON FWD GALLEY COMPARTMENT 112 REF. C&D ZODIAC CMM 25-33-39 REV. 2May 4, 2024 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202405028739Doubler · corrodedRIGHT FWD GALLEY HARD POINT MOUNT CORROSION. ***** AIRCRAFT REMOVED FROM SERVICE ***** REPLACED RIGHT FORWARD GALLEY HARD MOUNT POINT REF. C&D ZODIAC CMM 25-31-56 REV. 8May 2, 2024 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202404308737Bracket · corrodedCORROSION FOUND ON SERVICE DOOR BASE STRUCTURE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BRACKET LOWER FRAM ON SERVICE DOOR BASE STRUCTURE IAW CRJ200SRM 51-42-20 REV39Apr 29, 2024 · N410AW · Cndair CL6002B19 · Service DoorsSDR A6WA202404268738Bracket · corrodedCORROSION FOUND ON PASSENGER DOOR CUTOUT STRUCTURE IN 4 PLACES. FS319.7 TO FS349. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED 2 EA BRACKET ASSYS P/N 601R31527-217 ON PASSENGER DOOR SURROUND STRUCTURE AT FS310+5 AND FS 333+10 LBL 42 AND REMOVED AND Apr 26, 2024 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202404306732Blanking Plate · crackedBLANKING PLATE IN LEFT AND RIGHT WHEEL WELL FOUND CRACKED ***** AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED LH AND RH BRACKETS FROM WHEEL WELLS IAW CRJ200 SRM 51-42-06 REV 39.Apr 26, 2024 · N410AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA202404298735Line · crackedRH MLG HYDRAULIC LINE ANGLE SUPPORT BRACKET CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED 1EA BRACKET ASSY P/N 601R75262-153 ON RH MLG PANEL RACK AT FS 523.67 BETWEEN RBL18 AND RBL27 IAW CRJ200SRM 51-42-06 REV 39.Apr 25, 2024 · N410AW · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA202404308731Support · crackedCARGO DOOR CROSSBEAM SUPPORT CRACKED ***** AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED ANGLE P/N 601R35050-109 AT BAGGAGE DOOR ON AFT CARGO SURROUND STRUCTURE IAW CRJ200 SRM 51-42-21 REV 39.Apr 23, 2024 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202202218116None · noneAFTER T/O RECEIVED STEERING INOP CAUTION MSG. WT OFF WHEEL INOP CAUTION MSG. WT OFF WHEEL OUTPUT FAIL STATUS MSG. C/W QRH MSG PERSISTED. ***AIRCRAFT REMOVED FROM SERVICE*** R&R NLG RH WOW HARNESS PER CRJ 200 AMM 32-61-05 OPOS CK AND NLG STEERING GOOD Feb 18, 2022 · N410AW · Cndair CL6002B19 · Landing Gear SystemSDR A6WA202110087896None · noneBOTH RIGHT MAIN LANDING GEAR TIRES WERE FLAT TAXING INTO GATE. ***AIRCRAFT REMOVED FROM SERVICE*** REF 343164/3, 343164/4, 343165/1, 343165/2, FOR THE CORRECTIVE ACTIONS, REPLACING #3 AND 4 MAIN TIRESOct 7, 2021 · N410AW · Cndair CL6002B19 · Brake Anti-Skid SectionSDR A6WA202102087621Pdu · malfunctionedFLAPS FAIL CAUTION AFTER TAKE-OFF, FLAPS REMAINED AT 8 DEGREES WHEN SELECTING ZERO DEGREES (FLAPS FAILED AT 8 DEGREES), BRAKE TEMPS NORMAL ON LANDING. COMPLIED WITH FLAP RESET PROCEDURE IAW AWAC SUP. 98-18I, BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. AFeb 6, 2021 · N410AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA2020031347227Nut · looseHYD 1 LO PRESS ON CLIMB-OUT, COMPLIED WITH QRH, RECEIVED HYD EDP 1A CAUTION. HYD 1B SELECTED ON APPROX. 1 MIN. SELECTED OFF PER QRH, HYD 1 LO PRESS RETURNED. NO OBSERVED TEMPERATURE CHANGE IN SYSTEM. "AIRCRAFT REMOVED FROM SERVICE" INSPECTED AND FOUND LOOSEMar 12, 2020 · N410AW · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA2020031247224Pseu · malfunctionedSHORTLY AFTER DEPARTURE OUT OF OKC, THE CREW RECEIVED A NOSE WHEELS STEERING INOP MESSAGE. THERE WAS A STEERING AND WOW INPUT CAUTION AT THE SAME TIME. THE FLIGHT AIR RETURNED TO OKC. NO OVERWEIGHT LANDING AND NO EMERGENCY WAS DECLARED "AIRCRAFT REMOVED FROM Mar 10, 2020 · N410AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA2020031047222Stringer · corrodedSUPPLEMENTAL, STRINGER 26R CORRODED BETWEEN FS333 AND FS349. AIRCRAFT REMOVED FROM SERVICE: BLENDED TO REMOVE CORROSION. ORIGINAL MATERIAL THICKNESS - .080 MATERIAL LOSS - .080 REMAINING THICKNESS - 0.00 ALLOWABLE LIMITS - .008 REPAIRED STRINGER 26R IAW EA AWMar 10, 2020 · N410AW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA2020030947219Intercostal · corrodedSUPPLEMENTAL, INTERCOSTAL JUST TO THE LEFT OF STRINGER 27 HAS CORROSION BETWEEN FS349 AND FS364. AIRCRAFT REMOVED FROM SERVICE. BLENDED TO REMOVE CORROSION ORIGINAL THICKNESS - .080 MATERIAL LOSS - .010 REMAINING MATERIAL - .070 ALLOWABLE LIMITS - .008 REMOVMar 7, 2020 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2020030947218Stringer · corrodedSUPPLEMENTAL, STRINGER 26L HAS CORROSION BETWEEN FS333 AND FS349. AIRCRAFT REMOVED FROM SERVICE. BLENDED TO REMOVE CORROSION ORIGINAL THICKNESS - .063 MATERIAL LOSS - .030 REMAINING THICKNESS - .033 REMOVED AND REPLACED STRINGER SECTION IAW SRM 51-42-06 AND Mar 7, 2020 · N410AW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA2020030647217Stringer · crackedSTRINGER 3 IS CRACKED AT FS379.00. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED STRINGER IAW CRJ200 SRM 51-42-06 & 51-42-21.Mar 6, 2020 · N410AW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA2020030347215Attach Angle · crackedPAX DOOR LATCH COVER FWD ATTACH ANGLE IS CRACKED. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED ANGLE IAW CRJ200 SRM 51-41-02.Mar 3, 2020 · N410AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA2020030247213Angle · corrodedSERVICE DOOR LOWER SILL ANGLE CORRODED "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED SERVICE DOOR LOWER SILL ANGLE IAW CRJ 200 SRM 51-42-21Feb 29, 2020 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2020030247212Angle · corrodedSERVICE DOOR LOWER SILL ANGLE CORRODED "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED SERVICE DOOR LOWER SILL ANGLE IAW CRJ 200 SRM 51-42-21Feb 29, 2020 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2020030247211Seat Track · corrodedRH #2 SEAT TRACK IS CORRODED. "AIRCRAFT REMOVED FROM SERVICE" BLENDED TO REMOVE CORROSION ORIGINAL THICKNESS - .110 MATERIAL LOSS - .025 REMAINING THICKNESS .085 ALLOWABLE LOSS .020 REMOVED AND REPLACED SEAT TRACK IAW CRJ200 53-01-11.Feb 29, 2020 · N410AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2020030247214Splice Angle · crackedFRAME SPLICE ANGLE AT FS 409+96 STRINGER 20 RIGHT IS CRACKED "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED CRACKED REINFORCING SPLICE ANGLE IAW CRJ 200 SRM 51-42-06 AND REO 601R-53-31-1092Feb 29, 2020 · N410AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA2020022847209Seat Track · corrodedLEFT HAND #4 FLOOR SEAT TRACK CORRODED. "AIRCRAFT REMOVED FROM SERVICE" BLENDED TO REMOVE CORROSION ORIGINAL THICKNESS - .110 MATERIAL REMOVED - .022 REMAINING MATERIAL - .088 ALLOWABLE LOSS - .011 REMOVED AND REPLACED SEAT TRACK IAW CRJ200 AMM 53-01-11Feb 28, 2020 · N410AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2020022747206Seat Track · corrodedLH #3 FLOOR SEAT TRACK IS CORRODED. "AIRCRAFT REMOVED FROM SERVICE" BLENDED TO REMOVE CORROSION ORIGINAL THICKNESS - .110 MATERIAL LOSS - .022 REMAINING THICKNESS - .088 ALLOWABLE MATERIAL LOSS - .011 REMOVED AND REPLACED SEAT TRACK IAW CRJ200 AMM 53-01-11.Feb 27, 2020 · N410AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2020022547200Bulkhead Web · crackedCOMPLY WITH AWAC JOB CARD 4EOAWA21045-E17/003/453 MODIFICATION OF THE REAR PRESSURE BULKHEAD WEB FS621.00 USING GREO 601R-53-61-1240 REV. D. "AIRCRAFT REMOVED FROM SERVICE" MODIFIED REAR PRESSURE BULKHEAD FS621 IAW GREO 601R-53-61-1240 REV. D.Feb 25, 2020 · N410AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA202002247197Support · crackedLEFT INBOARD FLAP VANE, INBOARD END LEADING EDGE PANEL 584DT SUPPORT IS CRACKED. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED SUPPORT IAW CRJ200 SRM 51-42-13Feb 23, 2020 · N410AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA202002247195Attach Angle · crackedLOWER ATTACH ANGLE ON AFT END OF BEAM IS CRACKED. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED ANGLE IAW CRJ200 SRM 51-42-21.Feb 23, 2020 · N410AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA202002247196Skin · chafedRH AILERON UPPER LEADING EDGE SKIN IS CHAFFED. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED LEADING EDGE SKIN IAW CRJ200 SRM 51-42-06 AND AWAC SUPPLEMENT 13-055B.Feb 23, 2020 · N410AW · Cndair CL6002B19 · AileronsSDR A6WA202002247198Floor Support · corrodedFLOOR BEAM IS CORRODED AT FS559+48 TO 559+80, RBL 9. "AIRCRAFT REMOVED FROM SERVICE" REPAIRED FLOOR BEAM IAW CRJ200 SRM 53-00-43, FIG. 203. BLENDED TO REMOVE CORROSION ORIGINAL MATERIAL - .050 MATERIAL LOSS - .024 REMAINING MATERIAL - .026 ALLOWABLE LOSS - .Feb 23, 2020 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202002247191Support Angle · crackedPAX DOOR UPPER LATCH CLOSE PLATE HAS A CRACKED SUPPORT ANGLE. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED ANGLE IAW CRJ200 SRM 51-41-02.Feb 21, 2020 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202022147190Angle · crackedFS625 TO INTERCOSTAL CLIP CRACKED AT STRINGER 14L. Ï¿½AIRCRAFT REMOVED FROM SERVICEÏ¿½ REMOVED AND REPLACED CLIP IAW CRJ200 SRM 51-42-21.Feb 21, 2020 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2020022047189Support Bracket · crackedRIGHT WING AILERON CENTER PANEL SUPPORT BRACKET IS CRACKED. Ï¿½AIRCRAFT REMOVED FROM SERVICEÏ¿½ REMOVED AND REPLACED SUPPORT BRACKET IAW CRJ200 SRM 51-42-06.Feb 19, 2020 · N410AW · Cndair CL6002B19 · AileronsSDR A6WA2020021947188Bulkhead Web · crackedAFT PRESSURE BULKHEAD WEB IS CRACKED AT BL 0 AND WL 111.00. Ï¿½AIRCRAFT REMOVED FROM SERVICEÏ¿½ WORK TRANSFERRED TO AAR W.O. 1018176/2000/0019, S/N 7601432, C/W AWAC JOB CARD 4EOAWA21045-E17/003/453 - MODIFICATION OF THE REAR PRESSURE BULKHEAD WEB FS621.00 UFeb 19, 2020 · N410AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2020021847183Door Sill · corrodedPAX DOOR LOWER SILL ANGLE IS CORRODED. FULL LENGTH OF PART. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED LOWER SILL ANGLE I/A/W CRJ-200 SRM 51-42-06, 51-42-10, 51-42-21Feb 14, 2020 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2020021447181Skin · chafedLEFT INBOARD FLAP VANE LEADING EDGE SKIN IS CHAFFED IN TWO PLACES. AIRCRAFT REMOVED FROM SERVICE BLENDED TO SMOOTH CONTOUR FLAP STATION 56.50 MATERIAL LOSS .014 FLAP STATION 105.00 MATERIAL LOSS .026 ORIGINAL THICKNESS .050 REMOVED AND REPLACED LEADING EDGEFeb 14, 2020 · N410AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA202002147175Floor Support · corrodedPAX DOOR FLOOR SUPPORT CLEATS ARE CORRODED, FWD AND AFT. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE CORROSION ORIGINAL MATERIAL .063 MATERIAL LOSS .018 REMAINING THICKNESS .045 ALLOWABLE LOSS .006 REMOVED AND REPLACED CLEAT AND BRACKET IAW CRJ200 SRM 51Feb 13, 2020 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202002147178Skin · chafedRIGHT WING IB FLAP VANE SKIN LE CHAFFED IN 3 PLACES. AIRCRAFT REMOVED FROM SERVICE BLENDED MID AND INBD AREAS IAW BOMBARDIER REO 601R-57-52-004 REMOVED AND REPLACED LE PANEL AT STA. 141 IAW CRJ200 SRM 51-42-13Feb 13, 2020 · N410AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA202002147177Cargo Track · corrodedCARGO SEAT TRACK AT RBL9, FS559.00+87 TO FS559.00+96 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE DAMAGE ORIGINAL THICKNESS .160 MATERIAL LOSS .080 REMAINING THICKNESS .080 ALLOWABLE LOSS .060 REMOVED AND REPLACED TRACK IAW CRJ200 AMM 53-00-Feb 13, 2020 · N410AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA202002147176Cargo Track · corrodedCARGO SEAT TRACK AT LBL9, FS559.00+87 TO FS559.00+96 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE DAMAGE ORIGINAL THICKNESS .160 MATERIAL REMOVED .070 REMAINING MATERIAL .090 ALLOWABLE LOSS .060 REMOVED AND REPLACED TRACK IAW CRJ200 AMM 53-00Feb 13, 2020 · N410AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA202021247169Bulkhead Web · crackedAFT PRESSURE BULKHEAD IS CRACKED AT CARGO DOOR AFT TRACK, APPROX. LBL27.5 AND WL 130. AIRCRAFT REMOVED FROM SERVICE REPAIR TRANSFERRED TO AAR W.O. 1018176/2000/0019 C/W AWAC JOB CARD 4EOAWA21045-E17/003/453 MODIFICATION OF THE REAR PRESSURE BULKHEAD WEB FS6Feb 12, 2020 · N410AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2019052346633Skin · dentedEXTERNAL FUSELAGE SKIN IS DENTED BETWEEN FS 700.00 AND 736.00 AND BETWEEN STRINGER 16R AND 17R.May 22, 2019 · N410AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA2019051546600Warning System · activatedAT 600 FT AGL RECEIVED NLG UNSAFE (YELLOW CROSSHATCHED) ACCOMPLISHED G O AROUND AND CW QRH PROCEDURE. CYCLED GEAR AND RECEIVED 3 GREEN (INTER MITTENT) MC THIS INDICATION IS WITH GEAR DOWN ONLY AND INTERMITTENT. *FROM PLOT* - THE PILOT WAS ON APPROACH AND SELEMay 13, 2019 · N410AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA2018022645659Frame · chafedREPAIR RT FRAME FS718.Feb 25, 2018 · N410AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA2018022645657Bracket · crackedPAX DOOR ASSIST MOTOR BRACKET CRACKED.Feb 25, 2018 · N410AW · Cndair CL6002B19 · Passenger/Crew Doors
Back to N410AW