# Service difficulty reports: N465AW

A list on [N465AW](https://openairdocs.org/aircraft/N465AW.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 4 · 170 reports

- [SDR A6WA202605268890](https://openairdocs.org/sdr/A6WA202605268890.md): Proximity Sensor · malfunctioned · May 26, 2026 · N465AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > RECEIVED GEAR DISAGREE WARNING MSG AFTER T/OFF CLIMBING THRU 5000'. MSG CLEARED AFTER A COUPLE SECONDS. GEAR WAS ALREADY UP/LOCKED WHEN MSG CAME ON. GEAR AND FLAP INDICATORS CAME ON BRIEFLY FOR APPROX 5 MINS AFTER GEAR DISAGREE MSG WARNING MSG MESSAGE. RECEIVE
- [SDR A6WA202502118860](https://openairdocs.org/sdr/A6WA202502118860.md): Anti-Ice Valve · faulted · Feb 11, 2025 · N465AW · Cndair CL6002B19 · Engine Anti-Icing System
  > INFIGHTING REC'D "R COWL A/I" CAUTION WITH SWITCH SELECTED OFF. FOUND R COWL PRV POPPED ON POST FLIGHT. AIRCRAFT REMOVED FROM SERVICE R&R RH COWL PRESSURE RELIEF VALVE REF 30-2204. OPS CHECK GOOD
- [SDR A6WA202405258754](https://openairdocs.org/sdr/A6WA202405258754.md): Sensor · faulted · May 25, 2024 · N465AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > UPON DEPARTURE AND CLIMB OUT OF KDAY FLAP FAILED WITH INDICATION OF 0. CREW HAS ELECTED TO FLY ONTO KORD. CREW HAS DECLARED AN EMERGENCY FOR FLAP FAILURE. CREW IS SCHEDULED TO ARRIVE AT KORD AT 0838 CENTRAL TIME. AIRCRAFT REMOVED FROM SERVICE. R&R L BPSU IA
- [SDR A6WA202405248753](https://openairdocs.org/sdr/A6WA202405248753.md): Fcu · faulted · May 24, 2024 · N465AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > RECEIVED FLAP FAIL MESSAGE BEFORE DESCENT. AIRCRAFT REMOVED FROM SERVICE. T/S PER FIM 27-50 FIG 108, FECU #1 MOST PROBABLE FAULT #12 PRESENT. REPLACED THE FECU PER AMM 27-51-05, OPS CHECK GOOD. REMOVED PLACARD/MEL.
- [SDR A6WA202312318686](https://openairdocs.org/sdr/A6WA202312318686.md): Unknown · unknown · Dec 31, 2023 · N465AW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE ON TAKE-OFF. WARNING MESSAGE APPEARED WITHIN 5 SECS OF SELECTION. NLG DID NOT MOVE. MLG RETRACTED NORMALLY. NOSE DOOR OPEN MESSAGE ALSO APPEARED. C/W QRH. RECEIVED THREE GREEN DOWN AND LOCKED. LANDING AT 46,500 LBS. BELOW LANDING WEIGHT. AIRCR
- [SDR A6WA202301608430](https://openairdocs.org/sdr/A6WA202301608430.md): Stiffener · missing · Jan 6, 2023 · N465AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD FS621 IS MISSING ALL REINFORCEMENT ANGLES, AIRCRAFT REMOVED FROM SERVICE. INSTALLED REINFORCEMENT ANGLES TO AFT PRESSURE BULKHEAD FS621. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORM
- [SDR A6WA2023011688428](https://openairdocs.org/sdr/A6WA2023011688428.md): Drag Angle · cracked · Dec 28, 2022 · N465AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT PANEL DRAG ANGLE IS CRACKED AT PULLEY BRACKET AREA. AIRCRAFT REMOVED FROM SERVICE. REPAIRED DRAG ANGLE. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW REO 601R-52-11-513 REV C.
- [SDR A6WA202212278431](https://openairdocs.org/sdr/A6WA202212278431.md): Angle · corroded · Dec 27, 2022 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON SERVICE DOOR LOWER SILL ANGLE P/N 601R38303-253 AT FS 310.0 AND RBL 43. AIRCRAFT REMOVED FROM SERVICE. REMOVED DAMAGE BY BLENDING SERVICE DOOR LOWER SILL ANGLE AT FS310.0 AND RBL 43. ORIGINAL MATERIAL THICKNESS 0.063. REMAINING THICKNESS 0.050
- [SDR A6WA202212168426](https://openairdocs.org/sdr/A6WA202212168426.md): Skin · corroded · Dec 16, 2022 · N465AW · Cndair CL6002B19 · Aileron Tabs
  > RIGHT HAND WING INBOARD FLAP INBOARD SIDE LOWER SKIN PN 601R4008 HAS CORROSION AND 5 GOUGES AT INBOARD WING STATION 50.498 - 79.062. ***********AIRCRAFT REMOVED FROM SERVICE**************** BLENDED OUT CORROSION IAW CRJ200 SRM 51-12-00 REV 39 AND SRM 51-21-06
- [SDR A6WA2023016258429](https://openairdocs.org/sdr/A6WA2023016258429.md): Floorbeam · cracked · Dec 15, 2022 · N465AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION AND CRACK ON CABIN FLOORBEAM AT BS 621, LBL 27-43. AIRCRAFT REMOVED FROM SERVICE. BLENDED CORROSION, REMOVED AND REPLACED THE SECTION OF ANGLE. HFEC PERFORMED WITH NO INDICATIONS IAW NDT 51-20-06 REV 44 PART 1. RESTORED SURFACE FINISH. WORK WI
- [SDR A6WA2023012638445](https://openairdocs.org/sdr/A6WA2023012638445.md): Rib · damaged · Nov 30, 2022 · N465AW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > RIGHT WINGLET ATTACH STRUCTURE HAS ONE ELONGATED HOLE ON RIB AND STRAP AT WS404.08. REPAIRED THE RT WINGLET ATTACH STRUCTURE BY REPLACING STRAP, INSTALLED FREEZE PLUG AND COUNTERBORED FREEZE PLUG. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE FINISH.
- [SDR A6WA2023012638448](https://openairdocs.org/sdr/A6WA2023012638448.md): Strap · corroded · Nov 30, 2022 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR STRUCTURE RH STRAP, BS 559, RBL 27 - 42. REMOVED AND INSTALLED FLOOR STRUCTURE RT STRAP WITH FABRICATED STRAP. RESTORED SURFACE FINISH. PERFORMED IAW SRM 53-00-00, REV 39, SRM 53-41-43 REV 39, SRM 51-40-11 REV 39, SRM 51-42-06 REV 39,
- [SDR A6WA2023012638444](https://openairdocs.org/sdr/A6WA2023012638444.md): Floorbeam · corroded · Nov 30, 2022 · N465AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON CABIN FLOOR STRUCTURE SUPPORT P/N 601R38672-1 AT FS349.0 AND RBL19.0 TO RBL21. REMOVED CORROSION BY BLENDING CABIN FLOOR STRUCTURE SUPPORT. PERFORMED HFEC WITH NO INDICATIONS. RESTORED SURFACE PROTECTIVE FINISH. ALL WORK WITHIN LIMITS PERFORMED I
- [SDR A6WA2023012638446](https://openairdocs.org/sdr/A6WA2023012638446.md): Rib · damaged · Nov 30, 2022 · N465AW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > LH WINGLET ATTACH STRUCTURE HAS ONE ELONGATED HOLE ON RIB AT WS404.08. REPAIRED LH WINGLET ATTACH STRUCTURE BY REPLACING RIB P AT WS404.08 AND WGLT3.25. INSTALLED FREEZE PLUG AND COUNTERBORED FREEZE PLUG. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE
- [SDR A6WA2023012638443](https://openairdocs.org/sdr/A6WA2023012638443.md): Floorbeam · corroded · Nov 30, 2022 · N465AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON CABIN FLOOR STRUCTURE CROSSBEAM AT FS349.0 AND RBL19.0 TO RBL24. REMOVED CORROSION BY BLENDING CABIN FLOOR STRUCTURE CROSSBEAM P/N 601R32005-149 AT FS349.0 AND RBL19.0 TO RBL24. FABRICATED STRAP FROM 0.050Ï¿½ ALUM. SHEET MATERIAL HEAT TREATED TO
- [SDR A6WA2023012308440](https://openairdocs.org/sdr/A6WA2023012308440.md): Seat Track · corroded · Nov 30, 2022 · N465AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RT SEAT TRACK FROM BS 559 - 559+84, RBL 9. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION, PERFORMED HFEC WITH NO INDICATIONS IAW NDTM 51-20-06 PART 1, REV 44. RESTORED PROTECTIVE FINISH. WORK WITHIN LIMITS IAW AMM 53-01-11 REV 66, REPLACED TH
- [SDR A6WA2023012308441](https://openairdocs.org/sdr/A6WA2023012308441.md): Floorbeam · corroded · Nov 30, 2022 · N465AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON CABIN FLOOR STRUCTURE SUPPORT ANGLE AT SERVICE DOOR FS349 AND RBL28 TO RBL42. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ANGLE SUPPORT ANGLE AT SERVICE DOOR FS349 AND RBL28 TO RBL42. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS
- [SDR A6WA2023012308442](https://openairdocs.org/sdr/A6WA2023012308442.md): Skin · corroded · Nov 30, 2022 · N465AW · Cndair CL6002B19 · Trailing Edge Flaps
  > CORROSION ON LEFT WING INBOARD FLAP LOWER SKIN FROM WS50.498- WS100.009. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED DAMAGED SECTION ON LEFT WING INBOARD FLAP LOWER SKIN FROM WS50.498 WS100.009. CUTOUT DIMENSIONS L= 29.700X W= 21.250. RESTORED SURF
- [SDR A6WA202301208436](https://openairdocs.org/sdr/A6WA202301208436.md): Fitting · corroded · Nov 30, 2022 · N465AW · Cndair CL6002B19 · Passenger/Crew Doors
  > CORROSION ON PAX DOOR FWD ANCHOR FITTING AT BS 310, WL 75. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ON PAX DOOR FWD ANCHOR FITTING. RESTORED PROTECTIVE FINISH. WORK WITHIN LIMITS, PERFORMED IAW AMM 52-11-17-400-804, REV 66, ADJUSTMENT IAW A
- [SDR A6WA202301208437](https://openairdocs.org/sdr/A6WA202301208437.md): Anchor Fitting · corroded · Nov 30, 2022 · N465AW · Cndair CL6002B19 · Passenger/Crew Doors
  > CORROSION ON PAX DOOR AFT ANCHOR FITTING, PLATE AND COVER AT BS 349, WL 75. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED PAX DOOR AFT ANCHOR FITTING, PLATE, AND COVER. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW AMM 52-11-1
- [SDR A6WA202106227805](https://openairdocs.org/sdr/A6WA202106227805.md): Housing · leaking · Jun 19, 2021 · N465AW · Cndair CL6002B19 · Turbine Engine Oil System
  > AT 3,000-3,500 FEET RH ENGINE OIL (PSI) FLUXUATION FROM 15 PSI TO 51 PSI, EVEN AT CRUISING POWER, C/W QRH, AIR RETURN. AIRCRAFT REMOVED FROM SERVICE. UPON FURTHER INSPECTION FOUND OIL TO BE LEAKING FROM SCAVENGER OIL FILTER HOUSING. FOUND OIL FILTER HOUS
- [SDR A6WA202105287789](https://openairdocs.org/sdr/A6WA202105287789.md): Angle · cracked · May 22, 2021 · N465AW · Cndair CL6002B19 · Passenger/Crew Doors
  > TWO CRACKED ANGLES ON PASSENGER DOOR AFT SIDE WALL PANEL AT 2ND STEP. FS340. PAX DOOR P/N 601R31701-1 S/N 7896 ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED PASSENGER DOOR FORWARD SIDE PANEL ANGLES P/N 601R-52-11-702-7 AND 601R-52-11-702-9 WITH FABRICATED A
- [SDR A6WA202105287788](https://openairdocs.org/sdr/A6WA202105287788.md): Angle · cracked · May 22, 2021 · N465AW · Cndair CL6002B19 · Passenger/Crew Doors
  > CRACKED ANGLE ON PASSENGER DOOR FORWARD SIDE WALL PANEL AT 2ND STEP. FS318 PAX DOOR P/N 601R31701-1 S/N 7896 ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED PASSENGER DOOR FORWARD SIDE PANEL ANGLE P/N 601R-52-11-702-10 WITH FABRICATED ANGLE, FS318. RESTORED S
- [SDR A6WA202106017792](https://openairdocs.org/sdr/A6WA202106017792.md): Strap · gouged · May 21, 2021 · N465AW · Cndair CL6002B19 · Wing Main, Frame Structure
  > LH WINGLET HAS 3 GOUGES AT INBOARD AND OUTBOARD LOWER FORWARD STRAPS, WS389. P/N 600-15108-7 AND P/N 600-15108-18. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED 2 GOUGES AT LH LOWER FORWARD WINGLET OUTBOARD STRAP P/N 600-15108-7. DIMENSIONS 3.200Ï¿½L X 2.00Ï¿½
- [SDR A6WA202105287790](https://openairdocs.org/sdr/A6WA202105287790.md): Angle · cracked · May 20, 2021 · N465AW · Cndair CL6002B19 · Passenger/Crew Doors
  > CRACKED ANGLE ON PASSENGER DOOR FORWARD LOWER SIDE WALL PANEL AT LOWER STEP. FS318 PAX DOOR P/N 601R31701-1 S/N 7896 ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED PASSENGER DOOR FORWARD LOWER SIDE WALL PANEL AT LOWER STEP, ANGLE P/N 601R-52-11-702-44, SHIM
- [SDR A6WA202106077797](https://openairdocs.org/sdr/A6WA202106077797.md): Skin · dented · May 19, 2021 · N465AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE SKIN DENT FS 640.00 - 1Ï¿½ LH STR 26 + 2Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SKIN DENT AT AFT FUSELAGE FS640.00 - 1Ï¿½ LH STR 26 +2Ï¿½. DAMAGE MEASURES 1.200Ï¿½L X 0.600Ï¿½W X 0.023Ï¿½D. PERFORMED HFEC WITH NO INDICATIONS. RESTORED P
- [SDR A6WA202106077795](https://openairdocs.org/sdr/A6WA202106077795.md): Skin · gouged · May 19, 2021 · N465AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE SKIN GOUGE FS 589.00 + 1Ï¿½ RH STR 25 + 2Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SKIN GOUGE FS 589.00 + 1 RH STR 25 + 2Ï¿½. DAMAGE MEASURES 1.10Ï¿½ L X 0.007Ï¿½ W X 0.006Ï¿½ D. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FI
- [SDR A6WA202106077796](https://openairdocs.org/sdr/A6WA202106077796.md): Skin · dented · May 19, 2021 · N465AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE SKIN DENT FS 640.00 - 2Ï¿½ LH STR 26 + 2Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SKIN DENT AT AFT FUSELAGE FS640.00 - 2Ï¿½ LH STR 26 +2Ï¿½.DAMAGE MEASURES 0.550Ï¿½L X 0.500Ï¿½W X 0.008Ï¿½D. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PR
- [SDR A6WA202105277787](https://openairdocs.org/sdr/A6WA202105277787.md): Skin · dented · May 19, 2021 · N465AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE SKIN DENT FS682.0 + 9Ï¿½ RIGHT HAND STRINGER 24 + 2Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** HAND FORMED DENT AT FS682.0 + 9Ï¿½ RIGHT HAND STRINGER 24 + 2Ï¿½, DIMENSION0.700Ï¿½L X 0.500Ï¿½W X 0.050Ï¿½W. DENT FOUND TO BE OUT OF LIMITS REF CRJ200
- [SDR A6WA202106117801](https://openairdocs.org/sdr/A6WA202106117801.md): Bulkhead · cracked · Apr 21, 2021 · N465AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACK INDICATIONS (7 TOTAL) AT FS621.00 AFT PRESSURE WEB. CRACKS AT THE FOLLOWING LOCATIONS, WL 128.5 - 131.2, LBL 18.0, CRACK LENGTH 2.7"L, WL 113.5 - 114.2, LBL 9.50, CRACK LENGTH 0.7"L, 109.5 - 112.0, BL 0.0, CRACK LENGTH 2.5"L, WL 110.5 - 111.2, RBL 9.50,
- [SDR A6WA2020072097275](https://openairdocs.org/sdr/A6WA2020072097275.md): Rvdt · failed · Jul 19, 2020 · N465AW · Cndair CL6002B19 · Landing Gear Steering System
  > RECIEVED A STEERING INOPERATIVE CAUTION MESSAGE AFTER RETRACTING GEAR, COMPLIED WITH QRH, MESSAGE REMAINED, RETURNED TO DEPARTURE, LANDED NORMAL USING DIFFERENTIAL BREAKING. NO HYD SYST 3 MESSAGE, NO OTHER EICAS MESSAGES, NO STEERING ON TAXI AFTER LANDING.
- [SDR A6WA2019091846876](https://openairdocs.org/sdr/A6WA2019091846876.md): Unknown · malfunctioned · Sep 17, 2019 · N465AW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > NOSE GEAR WOULD NOT RETRACT AFTER T/O. EICASE SHOWED NOSE GEAR DOWN AND NOSE GEAR OPEN INDICATIONS. RAN QRH. SELECTED GEAR DOWN. GEAR EXTENDED AND NORMAL LANDING.
- [SDR A6WA2019053046642](https://openairdocs.org/sdr/A6WA2019053046642.md): Stiffener · cracked · May 30, 2019 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND INDICATION AT FS 409.00+128 OTBD RBL 18 POST AFT FLANGE RADIUS APPROX.250" LONG FSH FAILS NDT.
- [SDR A6WA2019053046641](https://openairdocs.org/sdr/A6WA2019053046641.md): Bracket · cracked · May 30, 2019 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AC GROUND POWER RECEPTACLE STRUCTURE CRACKED @ MOUNT FASTENERS.
- [SDR A6WA2019052046621](https://openairdocs.org/sdr/A6WA2019052046621.md): Seat Track · corroded · May 18, 2019 · N465AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT WALL SEAT TRACK IS CORRODED AT FS 409+128.
- [SDR A6WA2019052046620](https://openairdocs.org/sdr/A6WA2019052046620.md): Bulkhead · cracked · May 18, 2019 · N465AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > INDICATION NOTED AT FS621 REAR PRESSURE BULKHEAD FWD FACE AT BL0.00, WL 131 APROX 7.5" LONG AND 53% FULL SCREEN HEIGHT FAILING NDT.
- [SDR A6WA2019061446610](https://openairdocs.org/sdr/A6WA2019061446610.md): Intercostal · corroded · May 17, 2019 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CORRODED BETWEEN F.S.349.00 AND F.S.364.00, STRG 26L AND 27.
- [SDR A6WA2019052046613](https://openairdocs.org/sdr/A6WA2019052046613.md): Seat Track · corroded · May 17, 2019 · N465AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT WALL SEAT TRACK IS CORRODED AT VF.S.409+128.
- [SDR A6WA2019052046609](https://openairdocs.org/sdr/A6WA2019052046609.md): Fitting · cracked · May 17, 2019 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT F.S.484 CLIP IS CRACKED AT RBL27.
- [SDR A6WA2019052046611](https://openairdocs.org/sdr/A6WA2019052046611.md): Seat Track · corroded · May 17, 2019 · N465AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT WALL SEAT TRACK IS CORRODED AT F.S.513.
- [SDR A6WA2019052046612](https://openairdocs.org/sdr/A6WA2019052046612.md): Seat Track · corroded · May 17, 2019 · N465AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT WALL SEAT TRACK IS CORRODED AT F.S.513.
- [SDR A6WA2019052046608](https://openairdocs.org/sdr/A6WA2019052046608.md): Vane · chafed · May 17, 2019 · N465AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT WING OUTBOARD FLAP FIXED VANE IS CHAFED AT W.S.274.
- [SDR A6WA2019051746607](https://openairdocs.org/sdr/A6WA2019051746607.md): Seat Track · corroded · May 17, 2019 · N465AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDEWALL SEAT TRACK IS CORRODED AT FS 529.00.
- [SDR A6WA2019051646606](https://openairdocs.org/sdr/A6WA2019051646606.md): Post · cracked · May 16, 2019 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND INDICATIONS AT FS409+128 BL 0 LT AND RT POSTS AFT FLANGE RADIUS APPROX..500" LONG 100% FSH BOTH FAILS NDT.
- [SDR A6WA2019051646605](https://openairdocs.org/sdr/A6WA2019051646605.md): Angle · cracked · May 16, 2019 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND INDICATIONS AT FS 409+128 B.L.0.00 LT AND RT POSTS AFT FLANGE RADIUS APPROX..500" LONG 100% FSH BOTH FAIL NDT.
- [SDR A6WA2018053145855](https://openairdocs.org/sdr/A6WA2018053145855.md): Flap System · malfunctioned · May 30, 2018 · N465AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > DURING TAKEOFF, THE FLAPS FAILED AT 3 DEGREES WHEN SELECTING FLAPS FROM 0 TO 8. RAN QRH, RETURNED TO DEPARTURE, EMERGENCY WAS DECLARED. AFTER LANDING FLAPS SYSTEM WAS SUCCESSFULLY RESET IAW 98-018G.
- [SDR A6WA2018040645751](https://openairdocs.org/sdr/A6WA2018040645751.md): Stiffener · cracked · Apr 5, 2018 · N465AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR MOTOR FOUND CRACKED IN THE LOWER VERTICAL STIFFENER. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-42-06, AND 51-42-13.
- [SDR A6WA201745473](https://openairdocs.org/sdr/A6WA201745473.md): Pin · pulled · Dec 11, 2017 · N465AW · Cndair CL6002B19 · Light System Wiring
  > 4182 EMERGENCY PATH LIGHTING FROM ROW 5 TO 8 INOP. FOUND PIN PULLED OUT OF ENVIRONMENTAL SPLICE AT ROW 7. R&R'D PIN IAW ESPM 20-17, FUNCTION CHECK GOOD.
- [SDR A6WA2017120745456](https://openairdocs.org/sdr/A6WA2017120745456.md): Light · inoperative · Dec 6, 2017 · N465AW · Cndair CL6002B19 · Emergency Lighting
  > 4231 EMERGENCY LIGHTS ROW 5 INOP ON FLOOR. PLACARDED & PLACED ON MEL. REMOVED & REPLACED EMERGENCY LIGHT STRIP ROW 5 IAW 33-51 & AWAC SUPP 16-371A. OPS CHECK GOOD.
- [SDR A6WA2017061445057](https://openairdocs.org/sdr/A6WA2017061445057.md): Frame · corroded · Jun 13, 2017 · N465AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 409+16 HAS CORROSION ON THE FWD AND AFT SIDE BETWEEN STRINGERS 26R AND 26L

Next page: https://openairdocs.org/aircraft/N465AW/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 = 'N465AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N465AW/reports

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