N450AW

Service difficulty reports · 232

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 = 'N450AW' 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 A6WA202212228422Actuator · faultedFLAP FAIL AT 42 DEG. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RH IB OB FLAP ACTUATOR DUE TO HIGH TORQUE.Dec 22, 2022 · N450AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA202211298393Fan · odorA/C WAS PUSHED BACK FROM THE GATE FOR ENGINE START WITH PACKS OFF ELECT SMELL IN COCKPIT, NO SMELL NOTED IN CABIN NO SMOKE NOTED. NO SMELL NOTED IN CABIN NO SMOKE NOTED. ****AIRCRAFT REMOVED FROM SERVICE ***** INSPECTED AND FOUND THE SMELL COMING FROM THE GRNov 29, 2022 · N450AW · Cndair CL6002B19 · Navigation SystemSDR A6WA202205188184Actuator · failedIN APPROACH PHASE, GEAR SELECTED DOWN, WE REC'VD TWO GREEN AND ONE RED AND A SINGLE WARNING MESSAGE "GEAR DISAGREE". THE RED INDICATION WAS FOR THE RIGHT MAIN LANDING GEAR. WARNING MESSAGE OCCURRED ABOUT 7 SECS AFTER SELECTING GEAR DOWN. HY TEMPS AND PSI WEREMay 18, 2022 · N450AW · Cndair CL6002B19 · Landing Gear Door ActuatorSDR A6WA202202188109None · noneON APPROACH, RECEIVED SPOILERONS CAUTION MESSAGE AND. IB AND OB GROUND SPOILER FAULTS STATUS MESSAGES ***AIRCRAFT REMOVED FROM SERVICE*** C/W FIM RESET MESSAGES CLEARED. SPOILERS OPERATED NORMALFeb 17, 2022 · N450AW · Cndair CL6002B19 · Flight Control SystemSDR A6WA202103027674Bpsu · malfunctioned"FLAP FAIL" CAUTION MESSAGE AT FL 290. FAILED AT 0 WITH NO FLAP HANDLE MOVEMENT. PERFOMRED FLAP RESET PROCEDURE IAW AWAC SUPP 98-018I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED RT BPSU AS PER INFeb 28, 2021 · N450AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA202012097451Uplock · malfunctionedGEAR DISAGREE WARNING MESSAGE AFTER GEAR RETRACTION ON TAKE-OFF. AFTER SELECTING THE GEAR LEVER TO UP POSITION WE HEARD A GRINDING NOISE FROM THE NOSE GEAR BAY. APPROXIMATELY 20 SECONDS LATER, THE GEAR DISAGREE WARNING OCCURRED. WE FOLLOWED THE QRH WHICH DIDec 6, 2020 · N450AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA202012047450Sensor · malfunctionedAIRCRAFT 450 OPERATING 3771 FROM ORD TO TYS RECIEVED A GEAR DISAGREE. THEY HAD 18 PASSENGERS ON BOARD. C/W QRH AND DECLARED AN EMERGENCY. GEAR WAS COMMANDED DOWN. GEAR EXTENDED AND ALL LIGHTS SHOWED GREEN FOR DOWN AND LOCKED. AIRCRAFT REMOVED FROM SERVICEDec 2, 2020 · N450AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA202011187423Priority Valve · malfunctionedUPON T/O RECEIVED GEAR DISAGREE WARNING MESSAGE AFTER SELECTING GEAR UP, AIR SPEED GEAR UP SELECTION WAS 170 KNOTS, MAIN LANDING GEAR SHOWED UP NO NLG SHOWED YELLOW HASH MARKS 20 SECONDS AFTER GEAR UP SELECTION NOSE GEAR HASH MARKS TURNED RED THEN RECEIVED GEANov 15, 2020 · N450AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA202011137413Landing Gear · malfunctionedRECEIVED GEAR DISAGREE WARNING AFTER 6 SECOND S AFTER GEAR SELECTION ON T/O. NOSE GEAR INDICATED RED HASHES AT 160 KNOTS C/W QRH GEAR CAME DOWN WITH EMERGENCY HANDLE SELECTION. (BLK 3) LANDING WT 46,000. AIRCRAFT REMOVED FROM SERVICE. INTERROGATED PSEU ANDNov 10, 2020 · N450AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA202011137419Control Unit · malfunctionedENROUTE TO FNT, THE CREW RECEIVED A FLAP FAIL MESSAGE AT ZERO DEGREES AND FL190. THE FLIGHT WILL CONTINUE TO FNT AND AN EMERGENCY HAS BEEN DECLARED. C/W QRH. LANDED AT FLAPS ZERO. LANDING WEIGHT LESS THAN 42,000 LBS. BRAKE TEMPS INDICATE 1, 8, 4 , 4. NO Nov 9, 2020 · N450AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA202011067399Bulkhead Web · crackedAFT PRESSURE BULKHEAD FWD SURFACE CRACKED AT FS 621.00 LBL 27.5 AND WL 130.0 0.85'' IN LENGTH. AIRCRAFT REMOVED FROM SERVICE. PERFORMED CUTOUT OF AFT PRESSURE BULKHEAD CRACKED AREA AT FS 621.00 LBL 27.5 AND WL 130.0 CUTOUT MEASURES L=2.100'' W=1.00", REF REONov 5, 2020 · N450AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA202011067394Floor Support · corrodedPRESSURE FLOOR SILL ANGLE AT FS 449 AND RBL 42 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR SILL ANGLE AT FS 449 AND RBL 42 BLEND MEASURED L=1.5'' AND W=1.2'', REF BOMBARDIER REO NO: 601R-53-41-666 REV C DATED 2012-11-0Nov 5, 2020 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202011067396Floor Support · corrodedPRESSURE FLOOR SILL ANGLE AT FS 431 AND RBL 42 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR SILL ANGLE AT FS 431 AND RBL 42 BLEND MEASURED L=2.0'' AND W=2.7'', REF BOMBARDIER REO NO: 601R-53-41-666 REV C DATED 2012-11-0Nov 5, 2020 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202011067391Floor Support · corrodedPRESSURE FLOOR SILL ANGLE AT FS 484 AND LBL 42 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR SILL ANGLE AT FS 484 AND LBL 42 BLEND MEASURED L=1.5'' AND W=1.0'', REF BOMBARDIER REO NO: 601R-53-41-666 REV C DATED 2012-11-0Nov 5, 2020 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202011067392Floor Support · corrodedPRESSURE FLOOR SILL ANGLE AT FS 450 AND LBL 42 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR SILL ANGLE AT FS 450 AND LBL 42 BLEND MEASURED L=1.8'' AND W=1.3'', REF BOMBARDIER REO NO: 601R-53-41-666 REV C DATED 2012-11-0Nov 5, 2020 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202011067402Skin · dentedFUSELAGE SKIN AT FS 559 TO FS 559+16 AND BETWEEN STR 9R AND STR 10R DENTED. DENT DIMENSIONS L=3.75'' W=0.50'' AND D=0.046''. AIRCRAFT REMOVED FROM SERVICE. CUT-OUT DAMAGED SKIN AT FS 559 TO FS 559+16 AND BETWEEN STR 9R AND STR 10R, REF EA AWAC-CRJ253-01521 Nov 5, 2020 · N450AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202011067400Skin · dentedOUTWARD DENT IN SKIN AT FS 677 AND STR 23R + 2. AIRCRAFT REMOVED FROM SERVICE. EVALUATED DENT AT FS 677 AND STR 23R + 2. DENT MEASURES L=0.700'' W=0.600 D=0.015 FOUND TO BE OUT OF LIMITS, PER CRJ-200 SRM 53-00-31 REV 38 DIAL DEPTH GAUGE S/N X102407 CAL DUE Nov 5, 2020 · N450AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202011067397Floor Support · corrodedPRESSURE FLOOR SILL ANGLE AT FS 508 TO FS 517 AND LBL 36 TO LBL 40 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR SILL ANGLE AT FS 508 TO FS 517 AND LBL 36 TO LBL 40. BLEND MEASURED L=1.8'' AND W=1.5'', REF BOMBARDIER RENov 5, 2020 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202011067398Skin · dentedFUSELAGE SKIN DENT AT FS 583 BETWEEN STR 25L AND STR 26L. AIRCRAFT REMOVED FROM SERVICE. PERFORMED HAND DRESS OF DENT BACK TO ORIGINAL CONTOUR OF FUSELAGE SKIN AT FS 583 BETWEEN STR 25L AND STR 26L, REF EA AWAC-CRJ253-01522 REV IR DATED 10/29/2020. PERFORMNov 5, 2020 · N450AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202011057390Floor Support · corrodedPRESSURE FLOOR SILL ANGLE AT FS 426 AND LBL 36 TO LBL 38 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR SILL ANGLE AT FS 426 AND LBL 36 TO LBL 38 BLEND MEASURED L=0.98'' AND W=0.5''. REMOVED CORROSION FROM PRESSURE FLOORNov 4, 2020 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202011057388Floor Support · corrodedPRESSURE FLOOR SILL ANGLE AT FS 439 AND RBL 42 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR SILL ANGLE AT FS 439 AND RBL 42 BLEND MEASURED L=1.5'' AND W=1.0'', REF BOMBARDIER REO NO: 601R-53-41-666 REV C DATED 2012-11-0Nov 4, 2020 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202011057386Floor Support · corrodedPRESSURE FLOOR SILL ANGLE AT FS 499 TO FS 501 AND RBL 42 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR SILL ANGLE AT FS 499 TO FS 501 AND RBL 42 BLEND MEASURED L=2.0'' AND W=1.7'', REF BOMBARDIER REO NO: 601R-53-41-666 RNov 4, 2020 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202011047385Floor Support · corrodedPRESSURE FLOOR SILL ANGLE AT FS 484 AND RBL 42 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR SILL ANGLE AT FS 484 AND RBL 42 BLEND MEASURED L=2.0'' AND W=1.5'', REF BOMBARDIER REO NR 601R-53-41-666 REV C DATED 2012-11-06Nov 4, 2020 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202011057387Floor Support · corrodedPRESSURE FLOOR SILL ANGLE AT FS 506 TO FS 517 AND RBL 42 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR SILL ANGLE AT FS 506 TO FS 517 AND RBL 42 BLEND MEASURED L=1.0'' AND W=0.9'', REF BOMBARDIER REO NO: 601R-53-41-666 RNov 4, 2020 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202011047382Floor Support · corrodedRT HAND FLOOR SILL ANGLE AT FS 409 TO FS 501, RBL 42 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL ANGLE AT FS 499 TO FS 501 RBL 42, REF REO 601R-53-41-666 REV-C DATED 2012-11-06 AND CRJ 200 SRM 51-21-06 REV 38. REWONov 4, 2020 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202011047384Floor Support · corrodedPRESSURE FLOOR SILL ANGLE AT FS 468 AND RBL 42 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR SILL ANGLE AT FS 468 AND RBL 42 BLEND MEASURED L=1.8'' AND W=1.0'', REF BOMBARDIER REO NO: 601R-53-41-666 REV C DATED 2012-11-0Nov 4, 2020 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202011047381Floor Support · corrodedPRESSURE FLOOR SILL ANGLE AT FS 426 AND RBL 37 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR SILL ANGLE AT FS 426 AND RBL 37 BLEND MEASURED L=1.8'' AND W=1.0'' REF BOMBARDIER REO NO: 601R-53-41-666 REV C DATED 2012-11-06Nov 4, 2020 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202011047383Floor Support · corrodedPRESSURE FLOOR SILL ANGLE AT FS 439 AND RBL 42 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR SILL ANGLE AT FS 439 AND RBL 42 BLEND MEASURED L=2.1'' AND W=1.1'', REF BOMBARDIER REO NO: 601R-53-41-666 REV C DATED 2012-11-0Nov 4, 2020 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202011067401Skin · corrodedTCAS ANTENNA SKIN HAS CORROSION AT FS 295+4. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FUSELAGE SKIN UNDER TCAS ANTENNA IN 4 EA LOCATIONS (P1) FS 295 +4 STR 0+1.165 (P2) FS 295+4 STR 0-1.765 (P3) FS 295+10.394 AND STR 0+1.394 438?L X .08?W (P4) FS Nov 2, 2020 · N450AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202010297373Bulkhead Web · crackedAFT PRESSURE BULKHEAD FWD SURFACE CRACKED AT FS 621.00 BL 0.0 AND WL 130.0 0.75'' IN LENGTH. AIRCRAFT REMOVED FROM SERVICE. PERFORMED CUTOUT OF AFT PRESSURE BULKHEAD CRACKED AREA AT FS 621.00 BL 0.0 AND WL 130.0 CUTOUT MEASURES L=1.992'' W=1.262, REF REO 601Oct 28, 2020 · N450AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA202010297371Bulkhead Web · crackedAFT PRESSURE BULKHEAD FWD SURFACE CRACKED AT FS 621.00 LBL 36 AND WL 79.25 1.00'' IN LENGTH. AIRCRAFT REMOVED FROM SERVICE. PERFORMED CUTOUT OF AFT PRESSURE BULKHEAD CRACKED AREA AT FS 621.00 LBL 36 AND WL 79.25 CUTOUT MEASURES L=1.190'' W=1.130, REF REO 601Oct 28, 2020 · N450AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA202010297372Bulkhead Web · crackedAFT PRESSURE BULKHEAD FWD SURFACE CRACKED AT FS 621.00 LBL 18 AND WL 104.5 1.25'' IN LENGTH. AIRCRAFT REMOVED FROM SERVICE. PERFORMED CUTOUT OF AFT PRESSURE BULKHEAD CRACKED AREA AT FS 621.00 LBL 18 AND WL 104.5 CUTOUT MEASURES L=2.925'' W=1.242, REF REO 601Oct 28, 2020 · N450AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA202011067393Floorbeam · corrodedRT HAND FLOOR SILL ANGLE AT FS 426 RBL 37 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL ANGLE AT FS 426 RBL 37, REF REO 601R-53-41-666 REV-C DATED: 2012-11-06 AND CRJ 200 SRM 51-21-06 REV 38. PERFORMED HFEC INSPECTIOOct 24, 2020 · N450AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202011057389Floor Support · corrodedLT HAND FLOOR SILL ANGLE AT FS 468 TO FS 477, LBL 36 TO LBL 38 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL ANGLE AT FS 468 TO FS 477, LBL 38, REF REO 601R-53-41-666 REV-C DATED 2012-11-06 AND CRJ 200 SRM 51-21-06 ROct 24, 2020 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2020010647087Bpsu · malfunctioned3818 FLAPS FAILED AT ZERO DURING FLIGHT. CW FLAP FAIL SUPP 98-018G FLAPS FAIL MSG REMAINS AIRCRAFT REMOVED FROM SERVICE REF 312519/4 FOR R&R OF RH BPSU R&R RH BPSU IAW AMM 27-51-10, SAFTIED AND PERFORMED RIGGING. OPS CHECK GOOD AT THIS TIMEJan 2, 2020 · N450AW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR A6WA2018090446040Web · crackedFS 280 WEB AT RBL9 CRACKED. REPAIRED.Sep 4, 2018 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018090446036Door Sill · corrodedSERVICE DOOR LOWER SILL CORRODED. REPLACED SILL IAW SRM 51-77-11, 53-00-00, 51-42-06.Sep 1, 2018 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018090446033Nozzle · crackedEXHAUST NOZZLE 446AL INBOARD LONGITUDINAL JOINT HAS A CRACKED STRAP. REPLACEMENT EXHAUST NOZZLE, 446AL.Aug 31, 2018 · N450AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA2018090446035Seat Track · corrodedRIGHT SIDEWALL SEAT TRACK NR 2 CORRODED. REPLACED RIGHT SIDEWALL SEAT TRACK NR 2 IAW AMM 53-01-11.Aug 31, 2018 · N450AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2018090446031Seat Track · corrodedRIGHT SIDEWALL SEAT TRACK NR 1 CORRODED. REPLACED RIGHT SIDEWALL SEAT TRACK NR 1 IAW AMM 53-01-11.Aug 31, 2018 · N450AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2018090446034Seat Track · corrodedLEFT SIDEWALL SEAT TRACK NR 3 CORRODED. REPLACED LEFT SIDEWALL SEAT TRACK NR 3 IAW AMM 53-01-11.Aug 31, 2018 · N450AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2018090446025Seat Track · corrodedLEFT SIDEWALL SEAT TRACK NR 4 CORRODED. REPLACED LEFT SIDEWALL SEAT TRACK NR 4 IAW AMM 53-01-11.Aug 30, 2018 · N450AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2018090446029Skin · dentedRIGHT I/B FLAP LOWER SKIN HAS 2 DENTS. REPAIRED RIGHT I/B FLAP LOWER SKIN IAW REO 601R-57-52-1544 REV-.Aug 30, 2018 · N450AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2018090446030Intercostal · crackedINTERCOSTAL CRACKED AT FS 621.00, STR14L. REPLACED INTERCOSTAL IAW SRM 51-40-11, 51-42-06, 51-42-21.Aug 30, 2018 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018090446024Seat Track · corrodedLEFT SIDEWALL SEAT TRACK NR 6 CORRODED. REPLACED LEFT SIDEWALL SEAT TRACK IAW AMM 53-01-11.Aug 30, 2018 · N450AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2018090446027Seat Track · corrodedRIGHT SIDEWALL SEAT TRACK NR 4 CORRODED. REPLACED RIGHT SIDEWALL SEAT TRACK NR 4 IAW AMM 53-01-11.Aug 30, 2018 · N450AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2018090446026Seat Track · corrodedRIGHT SIDEWALL SEAT TRACK NR 5 CORRODED. REPLACED RIGHT SIDEWALL SEAT TRACK NR 5 IAW AMM 53-01-11-400-802.Aug 30, 2018 · N450AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2018090446028Seat Track · corrodedRIGHT SIDEWALL SEAT TRACK NR 3 CORRODED. REPLACED RIGHT SIDEWALL SEAT TRACK NR 3 IAW AMM 53-01-11.Aug 30, 2018 · N450AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2018090446022Seat Track · corrodedRIGHT SIDEWALL SEAT TRACK NR 6 CORRODED. REPLACED RIGHT SIDEWALL SEAT TRACK NR 6 IAW AMM 53-01-11.Aug 29, 2018 · N450AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2018090446020Fitting · crackedRIGHT LOWER WINDSHIELD CENTER POST FITTING IS CRACKED. REPLACED FITTING IAW SRM 51-12-21.Aug 29, 2018 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
Back to N450AW