N457AW

Service difficulty reports · 217

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 = 'N457AW' 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 A6WA202608258909Control Unit · unsecureON TAKE OFF, RECEIVED A CONFIG WARNING, ABORTED TAKE OFF JUST AFTER TAKEOFF ROLL, BELOW 80 KTS. RETRIED TAKE OFF AFTER TAXI BACK AROUND. DID STANDING TAKEOFF, RECEIVED CONFIG TRIM WARNING, DID NOT MOVE FOR TAKEOFF. AIRCRAFT REMOVED FROM SERVICE. SECURED HSTCUAug 25, 2026 · N457AW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR A6WA202607208901Adc · malfunctionedIN FLT A/P DISENGAGED, YAW 1 INOPERATIVE, ALT , VERT SPEED AND IAS INOP/FLAGGED, C/W QRH FLAGS CLEARED( SWITCHED TO #2 ADC), ALL INDICATIONS NORMAL. AIRCRAFT REMOVED FROM SERVICE. REF W/O 348209 W/C NUMBER 9 FOR THE REPLACEMENT OF ADC1 AND W/C #8 FOR REPLACEJul 20, 2026 · N457AW · Cndair CL6002B19 · Air Data ComputerSDR A6WA202605168888Bracket · brokenAIRCRAFT REMOVED FROM SERVICE. FOD WAS FOUND OBSTRUCTING THE RH TORQUE BOX DRAIN HOLE, UPON FURTHER INSP WITH A BORE SCOPE THROUGH THE DRAIN HOLE IT WAS FOUND THAT A BRACKET HAD BROKEN OFF AIRCRAFT IS IN THE PROCESS OF BEING FERRIED FOR FURTHER INSP AND REPAMay 16, 2026 · N457AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA202604218886Ballast · failedFA REPORTED HOT ELECTRICAL SMELL DURING AIRCRAFT WALK THROUGH POST FLIGHT. FIRE DEPARTMENT NOTED WARM SPOTS IN OVERHEAD BINS 3-6 BOTH SIDES AND SOME BROWN SPOTS ON WIRES. ***AIRCRAFT REMOVED FROM SERVICE ***** R&R LIGHT BALLAST OVER ROW 8AB IAW AMM 25-28-01 OApr 21, 2026 · N457AW · Cndair CL6002B19 · Passenger Compartment LightingSDR A6WA202408098789Selector Valve · faultedRECEIVED STEERING INOP CAUTION ON LANDING ROLL OUT. QRH CW, MESSAGE REMAINS. COMPLIED WITH FIM RESET, MESSAGE REMAINS. ****AIRCRAFT REMOVED FROM SERVICE **** REMOVED AND REPLACED NLG SELECTOR VALVE OPS AND LEAK CHECK GOOD REF AMM 32-32-10.Aug 9, 2024 · N457AW · Cndair CL6002B19 · Landing Gear Steering SystemSDR A6WA202407278781Pump · leakingUPON SELECTING GEAR LEVER TO THE DOWN POSITION, RECEIVED GEAR DISAGREE MASTER WARNING, MAIN GEARS NOT LOCKED IN POSITION. PULLED EMERGENCY EXTENSION TO CW QRH, ALL GEAR DOWN AND LOCKED. AIRCRAFT REMOVED FROM SERVICE. 6028 - RECEIVED HYD 3 LO PRESS CAUTION MSGJul 27, 2024 · N457AW · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR A6WA202310068679Unknown · damagedCRUSHED RADOME, WEATHER RADAR UNIT, AND BULKHEAD DAMAGE AT FS 169, FUSELAGE SKIN, STRINGERS & FRAME DAMAGE FROM FS169 TO FS193 ON RH AND LH SIDES OF FUSELAGE *******AIRCRAFT REMOVED FROM SERVICE********* FORWARD FUSELAGE AT FS169 TO FS193 REPAIR COMPLETED BY Oct 6, 2023 · N457AW · Cndair CL6002B19 · Aerodynamic FairingsSDR A6WA202308268651Unknown · unknownADG INADVERNTANT DEPLOYMENT AT FL 320, C/W QRH. ADG DEPLOYED AT MACH .67/260 KIAS FOR 20 MINUTES. NO EICAS INDICATIONS. (MOC NOTE, CREW STATED THEY DID NOT ACCIDENTLY DEPLOY THE ADG) AIRCRAFT REMOVED FROM SERVICE. INSPECTED ADG PER AMM 05-51-19, AWAC SUP Aug 26, 2023 · N457AW · Cndair CL6002B19 · Phase AdapterSDR A6WA202305168606Proximity Sensor · unknownIN CRUISE GOT PROX SYS CHAN CAUTION MSG, RAN QRH MSG REMAINED. R & R PSEU IAW AMM 32-61-01 AND PREFORMED OPERATIONAL TEST IAW AMM 32-61-00. OPS CHECK GOOD. AIRCRAFT OK FOR RTS.May 16, 2023 · N457AW · Cndair CL6002B19 · Landing Gear SystemSDR A6WA202212108404Warning Message · false activationRECEIVED A RT COWL ANTI-ICE WARNING AFTER TAKE OFF. C/W QRH AND MSG CLEARED. RT COWL ANTI-ICE WAS OFF IAW QRH, PILOT DECLARED AN EMERGENCY, NO PLACE TO GET OUT OF ICING CONDITIONS. AIRCRAFT REMOVED FROM SERVICE. COMPLIED WITH OPS CHECK OF COWL ANTI-ICE IDec 10, 2022 · N457AW · Cndair CL6002B19 · Engine Anti-Icing SystemSDR A6WA202211268389Smoke Detector · fault messageRECEIVED "SMOKE TOILET" MASTER CAUTION THROUGH 5K. MESSAGE CLEARED AFTER 2 MIN. RETURNED TO ORD. NO EVIDENCE OF SMOKE OR ODOR DETECTED IN THE CABIN OR COCKPIT. O2 MASKS NOT USED. ***AIRCRAFT REMOVED FROM SERVICE***** R&R LAV SMOKE DETECTOR PER CRJ 200 AMMNov 26, 2022 · N457AW · Cndair CL6002B19 · Smoke DetectionSDR A6WA202207308303None · dentedDENT (3.5"L X 5"W X 0.031"D ON RHS FWD LWR PLANK (DWG 601R10044 REF) BETWEEN RBL 20 & WING STA 29.421. DENT RUNS OVER MACHINED STRINGERS S18R & S19R. ****************AIRCRAFT REMOVED FROM SERVICE*********************** COMPLIED WITH ALL STEPS (#1 - #5) OF MHIJul 30, 2022 · N457AW · Cndair CL2151A10 · Wing StructureSDR A6WA202207308305None · gougedL/H INBOARD FLAP P/N: 601R14002-1 S/N:SB/RJ/884 LOWER SURFACE HAS A GOUGE BETWEEN WS 113.582 AND WS 120.803 WITH DIMENSIONS OF .900"L X .900"W X .047"D *******************AIRCRAFT REMOVED FROM SERVICE********************* FABRICATED REPAIR DOUBLER OUT OF 2024Jul 30, 2022 · N457AW · Cndair CL2151A10 · Aileron TabsSDR A6WA202207308307None · crackedPASSENGER DOOR HAS CRACKED REPAIR ANGLE P/N: 601R31907-301 FROM PREVIOUS REPAIR AT FS 349 AND CRACKED STAIR RISER AFT WEB P/N: 601R31701-1. ****************AIRCRAFT REMOVED FROM SERVICE************************ REMOVED REPAIR ANGLE P/N: 601R31907-301 (16.0" LJul 30, 2022 · N457AW · Cndair CL2151A10 · DoorsSDR A6WA202207308306None · corrodedCORROSION ON EDGE OF CABIN FLOOR FRAME AT FS 349 AND RBL42 AND CORROSION ON FRAME SUPPORT ANGLE P/N: 601R38783-13 AT FS 349 AND RBL 32 TO RBL 42. *******************AIRCRAFT REMOVED FROM SERVICE********************* BLENDED AREA ON CABIN FLOOR FRAME AT FS349Jul 30, 2022 · N457AW · Cndair CL2151A10 · Fuselage Fixed PartitionsSDR A6WA202207308304None · corrodedCORROSION ON SERVICE DOOR FLOOR ANGLE P/N: 601R38303-253 BENEATH FITTINGS AT FS 329 AND FS 342 AND RBL 42 - RBL 45. *******************AIRCRAFT REMOVED FROM SERVICE********************* BLENDED TWO EACH AREAS ON SERVICE DOOR FLOOR ANGLE P/N: 601R38303-253 WIJul 30, 2022 · N457AW · Cndair CL2151A10 · Galley DoorsSDR A6WA202207308302None · gougedR/H EXTERNAL SKIN HAS 5 EACH GOUGES BENEATH APU EXHAUST SHIELD AT FS 640+12 TO FS 672+6 & S15R. EVALUATED DAMAGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 53-00-31 REV 39. *********AIRCRAFT REMOVED FROM SERVICE*************************** BLENDED DAMAGE Jul 30, 2022 · N457AW · Cndair CL2151A10 · Fuselage Structure (General)SDR A6WA202207308301None · gougedL/H HSTAB Z BRACKET AT CANTED RIB 158.71 HAS TOOLING MARK DAMAGE MEASURING .600"L X .300"W X .030"D. EVALUATED DAMAGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-31-27 REV 39. *********AIRCRAFT REMOVED FROM SERVICE*************************** BLENDEJul 30, 2022 · N457AW · Cndair CL2151A10 · Vertical Stabilizer, Spar/RibSDR A6WA202207308299None · corrodedL/H FLOOR SEAT TRACK FROM FS 364 TO FS 409+8 RBL 9.5 HAS SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON L/H FLOOR SEAT TRACK AT FS 364 TO FS 409+8 AND RBL 9.5 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-41-49 REV 39. *********AIRCRAFT RJul 30, 2022 · N457AW · Cndair CL2151A10 · Fuselage Fixed PartitionsSDR A6WA202207308298None · chafedR/H IB FLAP VANE L/E PN:601R14303-44 AT WS 50.498+5" HAS CHAFE DAMAGE MEASURING 1.50"L X .600"W X .025"D. EVALUATED DAMAGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 57-52-00 REV 39. *********AIRCRAFT REMOVED FROM SERVICE*************************** VJul 30, 2022 · N457AW · Cndair CL2151A10 · Aileron TabsSDR A6WA202207308295None · chafedL/H IB FLAP VANE L/E PN:601R14303-51AT WS 98.509+6.7" HAS CHAFE DAMAGE MEASURING 1.10"L X .600"W X .013"D. EVALUATED DAMAGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 57-52-00 REV 39. *********AIRCRAFT REMOVED FROM SERVICE*************************** Jul 30, 2022 · N457AW · Cndair CL2151A10 · Aileron TabsSDR A6WA202207308296None · chafedL/H IB FLAP VANE L/E PN:601R14303-53 AT WS 50.498+6.0"" HAS CHAFE DAMAGE MEASURING 1.30"L X .650"W X .020"D. EVALUATED DAMAGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 57-52-00 REV 39. *********AIRCRAFT REMOVED FROM SERVICE**************************Jul 30, 2022 · N457AW · Cndair CL2151A10 · Wing StructureSDR A6WA202207308297None · chafedR/H IB FLAP VANE L/E PN:601R14303-10 AT WS 98.509+7" HAS CHAFE DAMAGE MEASURING 1.90"L X .650"W X .016"D. EVALUATED DAMAGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 57-52-00 REV 39. *********AIRCRAFT REMOVED FROM SERVICE*************************** VJul 30, 2022 · N457AW · Cndair CL2151A10 · Aileron TabsSDR A6WA202203318158Door · faultedAT ROTATION ON TAKEOFF, RECEIVED IS FLAG ON PFD AND EFIS COMP MON MSG LSO RECEIVED STALL FAIL CAUTION MESSAGE. RAN QRH. ON GROUND F/O FOUND OXYGEN SERVICE PANEL OPEN. REQ INSP. ***AIRCRAFT REMOVED FROM SERVICE**** PERFORMED STALL OPS CHECK IAW AMM 27-35-01. OPMar 31, 2022 · N457AW · Cndair CL6002B19 · Elevator Control SystemSDR A6WA202012237475Floorbeam · corrodedFLOOR SUPPORT STRUCTURE AT FS 559, RBL 28 TO RBL 42 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM FLOOR SUPPORT STRUCTURE AT FS 559, RBL 28 TO RBL 42, REF CRJ 200 REV (38) SRM 51-21-06. PERFORMED UT THICKNESS MEASUREMENT ON BLENDED ARDec 19, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202012237474Floorbeam · corrodedFLOOR SUPPORT STRUCTURE AT FS 559, LBL 28 TO LBL 42 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM FLOOR SUPPORT STRUCTURE AT FS 559, LBL 28 TO LBL 42, REF CRJ 200 REV (38) SRM 51-21-06. PERFORMED UT THICKNESS MEASUREMENT ON BLENDED ARDec 19, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202012227471Floor Support · corrodedPRESSURE FLOOR ANGLE AT FS 436+6 TO FS 437.15+5, LBL 36 TO LBL 43 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM FLOOR ANGLE (3 EA) POSITIONS AT FS 436+6 TO FS 437.15+15, LBL 36 TO LBL 43 REWORKED DIMENSIONS (P1)=4.5 W X 1.7 L, (P2)=0.8Dec 15, 2020 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202012187463Skin · dentedFUSELAGE STATION 654.20+11 AND STR 21L+26 HAS SMALL OUTWARD DENT C/T SKIN PANEL. AIRCRAFT REMOVED FROM SERVICE. EVALUATED DENT AT FS 654.20+11 STR 21L+6 ORIGINAL MATERIALS .063" DENT DIMENSION .300"L, .200"W, .001"D, FOUND TO BE OUT OF LIMITS, REF CRJ 200 SRDec 15, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202012297497Floor Support · corrodedPRESSURE FLOOR ANGLE AND PANEL AT FS 449.875 TO FS 461, RBL 42, STR 17, W/L 73.50, STR 17 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM (2 EA) POSITIONS AT FS 449.875 TO FS 461, RBL 42, STR 17, W/L 73.50, STR 17. REWORKED DIMENSIONS (Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202012237484Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 436, LBL 42, STR 17, W/L 73.50 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE (2 EA) POSITIONS AT FS 436, LBL 42, STR. 17, W/L 73.50. REWORKED DIMENSIONS (P1)=2.6 L X 0.5 W, (P2)=0.7 L X Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202012237492Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 513+4, LBL 35 TO LBL 43, W/L 73.59, STR 17 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 513+4, LBL 35 TO LBL 43, W/L 73.59, STR 17. REWORKED DIMENSION=1.6 L X 1.2 W, REF REO 601R-Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202012237491Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 499+1, LBL 41 TO LBL 43, W/L 73.50, STR 17 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 499+1, LBL 41 TO LBL 43, W/L 73.50, STR 17. REWORKED DIMENSION=5.5 L X 0.8 W, REF REO 601R-Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202012237493Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 409+128+10 TO FS 424+4, LBL 36 TO LBL 43, STR 17, W/L 73.50 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM FLOOR ANGLE (4 EA) POSITIONS AT FS 409+128+10 TO FS 424+4, LBL 36 TO LBL 43, STR 17, W/L 73.50. REWORDec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202012237490Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 484, LBL 42, W/L 73.50, STR 17 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 484, LBL 42, W/L 73.50, STR 17. REWORKED DIMENSION=2.3 L X 1.5 W, REF REO 601R-53-41-666 REV (C). PERFDec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202012237473Floorbeam · corrodedPRESSURE FLOOR ANGLE AND SUPPORT AT FS 544 TO FS 559, RBL 43, STR 17, W/L 73.50, STR 17 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM FLOOR ANGLE (2 EA) POSITIONS AT FS 544 TO FS 559, RBL 43, STR. 17, W/L 73.50, STR 17. REWORKED DIMENDec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202012237485Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 529+13, RBL 40, STR 17, W/L 73.50 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM FLOOR ANGLE (3 EA) POSITIONS AT FS 529+13, RBL 40, STR 17, W/L 73.50. REWORKED DIMENSIONS (P1)=1.2 L X 0.8 W, (P2)=1.6 L X 1.15Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202012237489Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 529+11, LBL 40 TO LBL 43, STR 17, W/L 73.50 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE (2 EA) POSITIONS AT FS 529+11, LBL 40 TO LBL 43, STR 17, W/L 73.50 REWORKED DIMENSIONS (P1)=0.25 Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202012237487Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 544, LBL 41 TO LBL 43, W/L 73.50, STR 17 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 544, LBL 41 TO LBL 43, W/L 73.50, STR 17. REWORKED DIMENSION=1.0 L X 1.0 W, REF REO 601R-53-4Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202012237486Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 513+6, RBL 40 TO RBL 43, W/L 73.50, STR 17 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 513+6, RBL 40 TO RBL 43, W/L 73.50, STR 17. REWORKED DIMENSION=1.8 L X 1.8 W, REF REO 601R-Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202012237472Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 559, LBL 33 TO LBL 43, STR 17, W/L 73.50 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM FLOOR ANGLE (2 EA) POSITIONS AT FS 559, LBL 33 TO LBL 43, STR 17, W/L 73.50. REWORKED DIMENSIONS (P1)=1.2 W X 1.6 L, (P2Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202012237480Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 409+128, RBL 36, W/L 73.50, STR 17 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM FLOOR ANGLE AT FS 409+128, RBL 36, W/L 73.50, STR 17. REWORKED DIMENSION=1.2 W X 1.6 L, REF REO 601R-53-41-666 REV (C). PERFDec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202012237482Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 439, LBL 41 TO LBL 43, STR 17, W/L 73.50 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE (2 EA) POSITIONS AT FS.439, LBL 41 TO LBL 43, STR. 17, W/L 73.50. REWORKED DIMENSIONS (P1) = 2.0 L Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202012237483Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 449.85, LBL 43, STR 17, W/L 73.50 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM FLOOR ANGLE (3 EA) POSITIONS AT FS 449.85, LBL 43, STR 17, W/L 73.50. REWORKED DIMENSIONS (P1)=1.1 L X 0.7 W, (P2)=0.9 L X 0.5 Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202012237494Floorbeam · corrodedPRESSURE FLOOR PANEL AT FS 513+5, LBL 42, STR 17, W/L 73.50 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE (3 EA) POSITIONS AT FS 513+5, LBL 42, STR 17, W/L 73.50. REWORKED DIMENSIONS (P1) = 0.6 L X 0.92 W, (P2)=1.Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202012237478Floorbeam · corrodedPRESSURE FLOOR PANEL AT FS 439+9, RBL 42, STR 17, W/L 73.50 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM FLOOR PANEL (2 EA) POSITIONS AT FS 439+9, RBL 42, STR 17, W/L 73.50. REWORKED DIMENSIONS (P1)=0.8 W X 1.1 L, (P2)=1.1 W X 1.8 L,Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202012237477Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 424+3, RBL 38, W/L 73.50, STR 17 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM FLOOR ANGLE AT FS 424+3, RBL 38, W/L 73.50, STR 17. REWORKED DIMENSION=0.80 W X 2 L, REF REO 601R-53-41-666 REV (C). PERFORMEDDec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202012237479Floorbeam · corrodedPRESSURE FLOOR PANEL AT FS 499, RBL 35 TO RBL 43, W/L 73.50, STR 17 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM FLOOR PANEL AT FS 499, RBL 35 TO RBL 43, W/L 73.50, STR 17. REWORKED DIMENSION=0.9 W X 8.1 L, REF REO 601R-53-41-666 REVDec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202012237476Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 461 TO FS 484, RBL 35 TO RBL 43, W/L 73.50, STR. 17 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM FLOOR ANGLE (3 EA) POSITIONS AT FS 461 TO FS 484, RBL 35 TO RBL 43, W/L 73.50, STR 17 REWORKED DIMENSIONS (P1)Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202012237488Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 513+14, LBL 40 TO LBL 43, STR 17, W/L 73.50 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM FLOOR ANGLE (3 EA) POSITIONS AT FS 513+14, LBL 40 TO LBL 43, STR 17, W/L 73.50. REWORKED DIMENSIONS (P1)=0.9 L X 0.8 Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA202012297496Support Angle · crackedSUSPECTED CRACK ON PASSENGER DOOR STEP 832CT FORWARD LOWER CORNER. AIRCRAFT REMOVED FROM SERVICE. REMOVED CHANNEL SUPPORT, SUPPORT BRACKET, PREVIOUS REPAIR DOUBLER AND ANGLE, REF BOMBARDIER REO 601R-52-11-702 REV (D). REPAIR ANGLE FOUND CRACKED, REF REO 601Dec 12, 2020 · N457AW · Cndair CL6002B19 · Passenger/Crew Doors
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