# Service difficulty reports: N457AW

A list on [N457AW](https://openairdocs.org/aircraft/N457AW.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 5 · 217 reports

- [SDR A6WA202608258909](https://openairdocs.org/sdr/A6WA202608258909.md): Control Unit · unsecure · Aug 25, 2026 · N457AW · Cndair CL6002B19 · Stabilizer Position Indicating
  > ON 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 HSTCU
- [SDR A6WA202607208901](https://openairdocs.org/sdr/A6WA202607208901.md): Adc · malfunctioned · Jul 20, 2026 · N457AW · Cndair CL6002B19 · Air Data Computer
  > IN 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 REPLACE
- [SDR A6WA202605168888](https://openairdocs.org/sdr/A6WA202605168888.md): Bracket · broken · May 16, 2026 · N457AW · Cndair CL6002B19 · Engine Thrust Reverser
  > AIRCRAFT 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 REPA
- [SDR A6WA202604218886](https://openairdocs.org/sdr/A6WA202604218886.md): Ballast · failed · Apr 21, 2026 · N457AW · Cndair CL6002B19 · Passenger Compartment Lighting
  > FA 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 O
- [SDR A6WA202408098789](https://openairdocs.org/sdr/A6WA202408098789.md): Selector Valve · faulted · Aug 9, 2024 · N457AW · Cndair CL6002B19 · Landing Gear Steering System
  > RECEIVED 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.
- [SDR A6WA202407278781](https://openairdocs.org/sdr/A6WA202407278781.md): Pump · leaking · Jul 27, 2024 · N457AW · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > UPON 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 MSG
- [SDR A6WA202310068679](https://openairdocs.org/sdr/A6WA202310068679.md): Unknown · damaged · Oct 6, 2023 · N457AW · Cndair CL6002B19 · Aerodynamic Fairings
  > CRUSHED 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
- [SDR A6WA202308268651](https://openairdocs.org/sdr/A6WA202308268651.md): Unknown · unknown · Aug 26, 2023 · N457AW · Cndair CL6002B19 · Phase Adapter
  > ADG 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
- [SDR A6WA202305168606](https://openairdocs.org/sdr/A6WA202305168606.md): Proximity Sensor · unknown · May 16, 2023 · N457AW · Cndair CL6002B19 · Landing Gear System
  > IN 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.
- [SDR A6WA202212108404](https://openairdocs.org/sdr/A6WA202212108404.md): Warning Message · false activation · Dec 10, 2022 · N457AW · Cndair CL6002B19 · Engine Anti-Icing System
  > RECEIVED 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 I
- [SDR A6WA202211268389](https://openairdocs.org/sdr/A6WA202211268389.md): Smoke Detector · fault message · Nov 26, 2022 · N457AW · Cndair CL6002B19 · Smoke Detection
  > RECEIVED "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 AMM
- [SDR A6WA202207308303](https://openairdocs.org/sdr/A6WA202207308303.md): None · dented · Jul 30, 2022 · N457AW · Cndair CL2151A10 · Wing Structure
  > DENT (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 MHI
- [SDR A6WA202207308305](https://openairdocs.org/sdr/A6WA202207308305.md): None · gouged · Jul 30, 2022 · N457AW · Cndair CL2151A10 · Aileron Tabs
  > L/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 2024
- [SDR A6WA202207308307](https://openairdocs.org/sdr/A6WA202207308307.md): None · cracked · Jul 30, 2022 · N457AW · Cndair CL2151A10 · Doors
  > PASSENGER 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" L
- [SDR A6WA202207308306](https://openairdocs.org/sdr/A6WA202207308306.md): None · corroded · Jul 30, 2022 · N457AW · Cndair CL2151A10 · Fuselage Fixed Partitions
  > CORROSION 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 FS349
- [SDR A6WA202207308304](https://openairdocs.org/sdr/A6WA202207308304.md): None · corroded · Jul 30, 2022 · N457AW · Cndair CL2151A10 · Galley Doors
  > CORROSION 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 WI
- [SDR A6WA202207308302](https://openairdocs.org/sdr/A6WA202207308302.md): None · gouged · Jul 30, 2022 · N457AW · Cndair CL2151A10 · Fuselage Structure (General)
  > R/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
- [SDR A6WA202207308301](https://openairdocs.org/sdr/A6WA202207308301.md): None · gouged · Jul 30, 2022 · N457AW · Cndair CL2151A10 · Vertical Stabilizer, Spar/Rib
  > L/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*************************** BLENDE
- [SDR A6WA202207308299](https://openairdocs.org/sdr/A6WA202207308299.md): None · corroded · Jul 30, 2022 · N457AW · Cndair CL2151A10 · Fuselage Fixed Partitions
  > L/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 R
- [SDR A6WA202207308298](https://openairdocs.org/sdr/A6WA202207308298.md): None · chafed · Jul 30, 2022 · N457AW · Cndair CL2151A10 · Aileron Tabs
  > R/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*************************** V
- [SDR A6WA202207308295](https://openairdocs.org/sdr/A6WA202207308295.md): None · chafed · Jul 30, 2022 · N457AW · Cndair CL2151A10 · Aileron Tabs
  > L/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***************************
- [SDR A6WA202207308296](https://openairdocs.org/sdr/A6WA202207308296.md): None · chafed · Jul 30, 2022 · N457AW · Cndair CL2151A10 · Wing Structure
  > L/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**************************
- [SDR A6WA202207308297](https://openairdocs.org/sdr/A6WA202207308297.md): None · chafed · Jul 30, 2022 · N457AW · Cndair CL2151A10 · Aileron Tabs
  > R/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*************************** V
- [SDR A6WA202203318158](https://openairdocs.org/sdr/A6WA202203318158.md): Door · faulted · Mar 31, 2022 · N457AW · Cndair CL6002B19 · Elevator Control System
  > AT 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. OP
- [SDR A6WA202012237475](https://openairdocs.org/sdr/A6WA202012237475.md): Floorbeam · corroded · Dec 19, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR 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 AR
- [SDR A6WA202012237474](https://openairdocs.org/sdr/A6WA202012237474.md): Floorbeam · corroded · Dec 19, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR 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 AR
- [SDR A6WA202012227471](https://openairdocs.org/sdr/A6WA202012227471.md): Floor Support · corroded · Dec 15, 2020 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE 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)=0.8
- [SDR A6WA202012187463](https://openairdocs.org/sdr/A6WA202012187463.md): Skin · dented · Dec 15, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE 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 SR
- [SDR A6WA202012297497](https://openairdocs.org/sdr/A6WA202012297497.md): Floor Support · corroded · Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE 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 (
- [SDR A6WA202012237484](https://openairdocs.org/sdr/A6WA202012237484.md): Floorbeam · corroded · Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE 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
- [SDR A6WA202012237492](https://openairdocs.org/sdr/A6WA202012237492.md): Floorbeam · corroded · Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE 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-
- [SDR A6WA202012237491](https://openairdocs.org/sdr/A6WA202012237491.md): Floorbeam · corroded · Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE 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-
- [SDR A6WA202012237493](https://openairdocs.org/sdr/A6WA202012237493.md): Floorbeam · corroded · Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE 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. REWOR
- [SDR A6WA202012237490](https://openairdocs.org/sdr/A6WA202012237490.md): Floorbeam · corroded · Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE 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). PERF
- [SDR A6WA202012237473](https://openairdocs.org/sdr/A6WA202012237473.md): Floorbeam · corroded · Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE 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 DIMEN
- [SDR A6WA202012237485](https://openairdocs.org/sdr/A6WA202012237485.md): Floorbeam · corroded · Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE 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 1.15
- [SDR A6WA202012237489](https://openairdocs.org/sdr/A6WA202012237489.md): Floorbeam · corroded · Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE 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
- [SDR A6WA202012237487](https://openairdocs.org/sdr/A6WA202012237487.md): Floorbeam · corroded · Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE 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-53-4
- [SDR A6WA202012237486](https://openairdocs.org/sdr/A6WA202012237486.md): Floorbeam · corroded · Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE 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-
- [SDR A6WA202012237472](https://openairdocs.org/sdr/A6WA202012237472.md): Floorbeam · corroded · Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE 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, (P2
- [SDR A6WA202012237480](https://openairdocs.org/sdr/A6WA202012237480.md): Floorbeam · corroded · Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE 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). PERF
- [SDR A6WA202012237482](https://openairdocs.org/sdr/A6WA202012237482.md): Floorbeam · corroded · Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE 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
- [SDR A6WA202012237483](https://openairdocs.org/sdr/A6WA202012237483.md): Floorbeam · corroded · Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE 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
- [SDR A6WA202012237494](https://openairdocs.org/sdr/A6WA202012237494.md): Floorbeam · corroded · Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE 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.
- [SDR A6WA202012237478](https://openairdocs.org/sdr/A6WA202012237478.md): Floorbeam · corroded · Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE 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,
- [SDR A6WA202012237477](https://openairdocs.org/sdr/A6WA202012237477.md): Floorbeam · corroded · Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE 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). PERFORMED
- [SDR A6WA202012237479](https://openairdocs.org/sdr/A6WA202012237479.md): Floorbeam · corroded · Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE 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 REV
- [SDR A6WA202012237476](https://openairdocs.org/sdr/A6WA202012237476.md): Floorbeam · corroded · Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE 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)
- [SDR A6WA202012237488](https://openairdocs.org/sdr/A6WA202012237488.md): Floorbeam · corroded · Dec 13, 2020 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE 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
- [SDR A6WA202012297496](https://openairdocs.org/sdr/A6WA202012297496.md): Support Angle · cracked · Dec 12, 2020 · N457AW · Cndair CL6002B19 · Passenger/Crew Doors
  > SUSPECTED 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 601

Next page: https://openairdocs.org/aircraft/N457AW/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N457AW/reports

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