# Service difficulty reports: N466AW

A list on [N466AW](https://openairdocs.org/aircraft/N466AW.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 · 169 reports

- [SDR A6WA202607278902](https://openairdocs.org/sdr/A6WA202607278902.md): Oxygen Panel · unsecure · Jul 27, 2026 · N466AW · Cndair CL6002B19 · Crew Oxygen System
  > AIRCRAFT TOOK OFF FROM MKE AND SENT AN ACARS SAYING THEY HAVE A POSSIBLE PANEL OPEN AND THAT THEY ARE RETURNING TO MKE. THEY PROCEEDED TO GO BACK TO MKE AND BUILT UP AN AIR RETURN. ON THE WAY BACK THEY ALSO RECEIVED A STALL FAIL. AIRCRAFT REMOVED FROM SERVICE
- [SDR A6WA202605028887](https://openairdocs.org/sdr/A6WA202605028887.md): Windshield · failed · May 2, 2026 · N466AW · Cndair CL6002B19 · Flight Compartment Windows
  > AT FL330 RIGHT FO WINDSHIELD SHATTERED. C/W QRH. WINDSHIELD HEAT WAS ON. NO PRESSURIZATION ISSUES. EMERGENCY DECLARED. NO MESSAGES PRESENT. AIRCRAFT REMOVED FROM SERVICE. REF WO# 347539 FOR WORK COMPLETED R & R RIGHT WINDSHIELD.
- [SDR A6WA202407238812](https://openairdocs.org/sdr/A6WA202407238812.md): Rib · chafed · Jul 23, 2024 · N466AW · Cndair CL6002B19 · Leading Edge Devices
  > CHAFING DAMAGE NOTED TO LEFT INBOARD FLAP NOSE RIB. MATERIAL LOSS RECORDED UP TO 0.015". INITIAL FLANGE THICKNESS WAS 0.06". ENGINEERING SUPPORT WAS SOUGHT FOR REPAIR PROCESS. AIRCRAFT REMOVED FROM SERVICE REPAIRED IN ACCORDANCE WITH EA AWAC-CRJ257-02062.
- [SDR A6WA202406138810](https://openairdocs.org/sdr/A6WA202406138810.md): Stiffener · corroded · Jun 13, 2024 · N466AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FRETTING CORROSION NOTED ON STIFFENER P/N: 601R32026-131 AT FS 559 BETWEEN LBL 7 AND LBL 38. CORROSION WAS REMOVED THROUGH BLENDING WITH RESULTING MATERIAL THICKNESS BEING LESS THAN PERMITTED PER SRM 53-00-00. ENGINEERING RESOLUTION WAS SOUGHT AND THE AREA RE
- [SDR A6WA202406138811](https://openairdocs.org/sdr/A6WA202406138811.md): Rib · chafed · Jun 13, 2024 · N466AW · Cndair CL6002B19 · Vertical Stabilizer, Spar/Rib
  > THREE (3) AREAS OF CHAFING DAMAGE NOTED ON RIB 9 OF VERTICAL STABILIZER UPPER SECTION. AREAS WERE BLENDED PER SUPPLEMENT 18-325 AND MEASURED OUTSIDE OF PERMISSIBLE LIMITS. AIRCRAFT REMOVED FROM SERVICE. AREAS WERE BLENDED AND REPAIRED PER EA AWAC-CRJ-255-020
- [SDR A6WA202404028728](https://openairdocs.org/sdr/A6WA202404028728.md): Sensing Element · faulted · Apr 2, 2024 · N466AW · Cndair CL6002B19 · Fire Protection System
  > ON TAKE-OFF ROLL AT APPROX. 80KNOTS; RECEIVED ANTI-ICE DUCT WARNING MESSAGE. TAKE-OFF ABORTED. ON A/ICE EICAS PAGE RT FUSELAGE STILL ILLUMINATED RED. MESSAGE REMAINS WITH NO BLEEDS ON. ALL BTMS INDICATIONS IN THE GREEN. AIRCRAFT REMOVED FROM SERVICE. R&R
- [SDR A6WA202401088690](https://openairdocs.org/sdr/A6WA202401088690.md): Unknown · unknown · Jan 8, 2024 · N466AW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > AFTER TAKE-OFF WHEN PUTTING GEAR UP RECEIVED GEAR DISAGREE CAUTION AND NOSE DOOR CAUTION MESSAGES. MAIN GEAR INDICATED UP AND LOCKED. NOSE GEAR NOT RETRACTED. C/W QRH. RECEIVED THREE DOWN AND GREEN INDICATIONS. GEAR DISAGREE CAUTION OCCURS 150 KNOTS. HIGHES
- [SDR A6WA202305168605](https://openairdocs.org/sdr/A6WA202305168605.md): Unknown · unknown · May 16, 2023 · N466AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGE AFTER SELECTING GEAR UP. NOSE GEAR SHOWED DOWN/LOCKED WITH MAINS UP/LOCKED. UPON LANDING RECEIVED NWS INOP CAUTION. AFTER TURNING OFF RUNWAY RECEIVED HYD 3 HI TEMP CAUTION WITH 3A, AND 3B PUMPS ON. PRESSURE IND
- [SDR A6WA202303088527](https://openairdocs.org/sdr/A6WA202303088527.md): Unknown · dented · Mar 8, 2023 · N466AW · Cndair CL6002B19 · Wing Structure
  > RH WING LEADING EDGE PANEL P/N 601R12016-6 HAS DENTS MEASURES P1 L= 2.100 X W= 1.300Ï¿½ P2 L= 2.500 X W= 1.500Ï¿½ P3 L= 2.400 X W= 1.650Ï¿½ P4 L= 2.100 X W= 0.500Ï¿½ ON LE INBOARD SECTION BETWEEN WS96.134-WS131.800. *******AIRCRAFT REMOVED FROM SERVICE*****
- [SDR A6WA202301168526](https://openairdocs.org/sdr/A6WA202301168526.md): Bracket · corroded · Jan 16, 2023 · N466AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT STRUCTURE BRACKET PN 601R31527-217 AT FS319.70 AND LBL44. DIMENSIONS P1 - L= 3.900Ï¿½ X W= 3.100Ï¿½ X D= 0.003Ï¿½, ORIGINAL THICKNESS 0.063Ï¿½ REMAINING THICKNESS 0.060Ï¿½. CORROSION ON FLOOR SUPPORT STRUCTURE BRACKET PN 601R31527-2
- [SDR A6WA202301168525](https://openairdocs.org/sdr/A6WA202301168525.md): Support · corroded · Jan 16, 2023 · N466AW · Cndair CL6002B19 · Fuselage Structure (General)
  > CABIN RH FLOOR SILL SUPPORT PN 601R31133-102 AND PLATE PN 601R31133-101 AT FS559.00 + 85 TO FS559.00 + 116 AND RBL42 TO RBL44 HAS EXFOLIATION CORROSION. ********AIRCRAFT REMOVED FROM SERVICE******** REMOVED AND REPLACED CABIN RH FLOOR SILL SUPPORT PN 601R311
- [SDR A6WA202301168524](https://openairdocs.org/sdr/A6WA202301168524.md): Splice · dented · Jan 16, 2023 · N466AW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > HORIZONTAL STABILIZER LEADING EDGE SHROUD DENTED BETWEEN FSS 31.999 AND FSS 59.221, RHS. ******AIRCRAFT REMOVED FROM SERVICE******** REPAIRED HORIZONTAL STABILIZER LEADING EDGE SHROUD DENT BETWEEN FSS 31.999 AND FSS 59.221, RHS. REMOVED DAMAGED SECTION OF SH
- [SDR A6WA202301168522](https://openairdocs.org/sdr/A6WA202301168522.md): Fitting · corroded · Jan 16, 2023 · N466AW · Cndair CL6002B19 · Fuselage Fixed Partitions
  > CORROSION ON FLOOR SUPPORT PN 601R38673-43 AT FS349.00 AND LBL38 TO LBL44. **********AIRCRAFT REMOVED FROM SERVICE****** REPLACED FLOOR SUPPORT PN 601R38673-43 AT FS349.00 AND LBL38 TO LBL44. ALL WORK WITHIN LIMITS WAS PERFORMED IAW AIR WISCONSIN CRJ200 SRM 53
- [SDR A6WA202301168513](https://openairdocs.org/sdr/A6WA202301168513.md): Vane · chafed · Jan 16, 2023 · N466AW · Cndair CL6002B19 · Wing Structure
  > CHAFE DAMAGE TO THE LH INBOARD FLAP VANE LEADING EDGE SKIN PN 601R14303-43. WEAR DIMENSIONS FOR P3 ARE - L = 1.600Ï¿½ X W = 0.600Ï¿½ X D = 0.015Ï¿½, WS137.012+4. ********AIRCRAFT REMOVED FROM SERVICE************ BLENDED DAMAGE OF LH INBOARD FLAP VANE CHAFE
- [SDR A6WA202301168512](https://openairdocs.org/sdr/A6WA202301168512.md): Vane · chafed · Jan 16, 2023 · N466AW · Cndair CL6002B19 · Aileron Tabs
  > CHAFE DAMAGE TO THE LH INBOARD FLAP VANE LEADING EDGE SKIN PN 601R14303-51. WEAR DIMENSIONS FOR P2 ARE - L = 1.400Ï¿½ X W = 0.700Ï¿½ X D = 0.007Ï¿½, WS98.509+7. *****AIRCRAFT REMOVED FROM SERVICE******** BLENDED DAMAGE OF LH INBOARD FLAP VANE CHAFE DAMAGE A
- [SDR A6WA202301168511](https://openairdocs.org/sdr/A6WA202301168511.md): Vane · chafed · Jan 16, 2023 · N466AW · Cndair CL6002B19 · Wing Structure
  > CHAFE DAMAGE TO THE LH INBOARD FLAP VANE LEADING EDGE SKIN PN 601R14303-53. WEAR DIMENSIONS FOR P1 ARE - L = 1.600Ï¿½ X W = 0.700Ï¿½ X D = 0.014Ï¿½, WS50.498+7. *****AIRCRAFT REMOVED FROM SERVICE******** BLENDED DAMAGE OF LH INBOARD FLAP VANE CHAFE DAMAGE A
- [SDR A6WA202210148342](https://openairdocs.org/sdr/A6WA202210148342.md): None · none · Oct 14, 2022 · N466AW · Cndair CL2151A10 · Tire
  > A-SKID INOP CAUTION MSG OBSERVED AT 120KIAS, T/O ABORTED, BTMS 5,5,7,3 MAX ***AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED A-SKID CONTROL UNIT IAW AMM 32-42-06 PERFORMED A-SKID ADJUSTMENT TEST. OPS CHECK GOOD P
- [SDR A6WA202202148099](https://openairdocs.org/sdr/A6WA202202148099.md): None · none · Feb 12, 2022 · N466AW · Cndair CL6002B19 · Landing Gear Door Retract Section
  > ON TAKEOFF RECEIVED NOSE DOOR OPEN AND GEAR DISAGREE WARNING MSG C/W QRH RETURNED TO LAND WITH GEAR DOWN AND THREE GREEN. CW M ACTION IN PREPARATION FOR MEL 32-30-01 REF 347921-2 FOR MEL PER FIM PER FIM32-60-08 NOSE DOOR OPEN INDICATION IS NORMAL
- [SDR A6WA202108097852](https://openairdocs.org/sdr/A6WA202108097852.md): Skin · corroded · Jul 29, 2021 · N466AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CORROSION AND SCRIBE MARKS AT VHF #1 ANTENNA LOCATION FS295.00 Ï¿½ FS310.00 S1L Ï¿½ S1R. AIRCRAFT REMOVED FROM SERVICE. BLENDED FUSELAGE SKIN CORROSION AND SCRIBE MARKS AT VHF #1 ANTENNA LOCATION FS295.00 Ï¿½ FS310.00 S1L Ï¿½ S1R. PERFORMED
- [SDR A6WA202108107854](https://openairdocs.org/sdr/A6WA202108107854.md): Angle · cracked · Jul 27, 2021 · N466AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR SUPPORT STRUCTURE 1.500Ï¿½ CRACK AT FS280 LBL9.0 Ï¿½ RBL9.0 AND WL73.0. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED REPAIR ON THE FLOOR STRUCTURE AT FS280 LBL9.0 - RBL9.0 AND WL73.0. FABRICATED FILLER ANGLE P/N 601R-53-11-3720-1 DIM. L= 28.40Ï¿½ X W
- [SDR A6WA202108107853](https://openairdocs.org/sdr/A6WA202108107853.md): Fitting · corroded · Jul 27, 2021 · N466AW · Cndair CL6002B19 · Fuselage Main, Structure
  > FORWARD GALLEY INBOARD AFT MOUNT FITTING IS CORRODED AT FS310.00 RBL10 AND WL73.5. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED FORWARD GALLEY INBOARD AFT MOUNT FITTING P/N 4602319-5 AT FS310.00 RBL10 AND WL73.5. RESTORED SURFACE FINISH. ALL WORK
- [SDR A6WA202108047849](https://openairdocs.org/sdr/A6WA202108047849.md): Skin · corroded · Jul 23, 2021 · N466AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SKIN SURFACE CORROSION AT ADF ANTENNA SKIN SURFACE FS409.00 + 63 TO FS409.00 + 73 AND AROUND 3 BOLT HOLES AT FS409.00 + 73 AND FS409.00 + 82. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION AT ADF SKIN SURFACE FS409.00 + 63 TO FS409.00 + 73 AND AROUND
- [SDR A6WA202108067851](https://openairdocs.org/sdr/A6WA202108067851.md): Window Frame · gouged · Jul 22, 2021 · N466AW · Cndair CL6002B19 · Fuselage Main, Structure
  > CO- PILOTS SIDE WINDOW POST SPLICE STRAP PN 601R33224-4 HAS NUMEROUS SCRATCHES AND GOUGES ON UPPER AND LOWER AREAS. AIRCRAFT REMOVED FROM SERVICE, BLENDED 11 TOOLING MARKS ON RH WINDSHIELD SIDE POST SPLICE STRAP. MEASUREMENTS: P1=L=3.00Ï¿½XW=1.500Ï¿½XD=0.008
- [SDR A6WA202108047848](https://openairdocs.org/sdr/A6WA202108047848.md): Skin · dented · Jul 22, 2021 · N466AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE DENT AT FS590.00 + 3Ï¿½ STR23L + 1Ï¿½ AND FS590.00 + 2Ï¿½ STR22L + 5Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SKIN DENTS AT FS590.00 + 3Ï¿½ STR23L + 1Ï¿½ AND FS590.00 + 2Ï¿½ STR22L + 5Ï¿½. PART NUMBER 601R35005 SKIN THICKNESS 0.063Ï¿½. D
- [SDR A6WA202108037844](https://openairdocs.org/sdr/A6WA202108037844.md): Skin · dented · Jul 22, 2021 · N466AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE HAS 3 SKIN DENTS AT FS654.50 THROUGH FS672.00 AND S21R Ï¿½ S23R. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED AFT FUSELAGE SKIN AT FS654.50 THROUGH FS672.00 AND S21R Ï¿½ S23R TO ORIGINAL CONTOUR. DIMENSIONS DENT #1 - L = 1.600Ï¿½ X W = 0.600Ï¿½
- [SDR A6WA202108037846](https://openairdocs.org/sdr/A6WA202108037846.md): Access Panel · damaged · Jul 22, 2021 · N466AW · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT HAND WING PCU ACCESS PANEL 650KB HAS DAMAGE ON LOWER SURFACE NEXT TO SCREW HOLE. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DRILL MARKS DAMAGED AREA OF PANEL 650KB. MEASUREMENTS L = 1.500Ï¿½ X W = 1.200Ï¿½ D = 0.008Ï¿½. PART NUMBER 601R10049 AND PAN
- [SDR A6WA202108037847](https://openairdocs.org/sdr/A6WA202108037847.md): Drag Angle · cracked · Jul 22, 2021 · N466AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT DRAG ANGLE CRACKED, LOCATED ON AFT SIDE OF DOOR AT MOTOR ASSIST PULLEY AT FS344.00. ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED PASSENGER DOOR STAIRS AFT DRAG ANGLE AT FS344.00. MEASUREMENT OF CRACK 0.300Ï¿½ IN LENGTH. INSTALLED REPAIR
- [SDR A6WA202108037845](https://openairdocs.org/sdr/A6WA202108037845.md): Skin · dented · Jul 22, 2021 · N466AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE SKIN DENT AT FS636.5, S27R-3.5Ï¿½. *AIRCRAFT REMOVED FROM SERVICE*** BLENDED SKIN DENT AT FS636.5 S27R-3.5Ï¿½ TO ORIGINAL SKIN CONTOUR. DIMENSIONS L = 1.700Ï¿½ X W = 1.00Ï¿½ D = 0.023Ï¿½. PART NUMBER 601R35005 AND SKIN THICKNESS 0.063Ï¿½. HFEC
- [SDR A6WA2020031747231](https://openairdocs.org/sdr/A6WA2020031747231.md): Unknown · malfunctioned · Mar 16, 2020 · N466AW · Cndair CL6002B19 · Cabin Cooling System
  > UPON INITIAL CLIMB OUT OF KMCO THE CREW WAS NOT ABLE TO TRANSFER TO THE LEFT PACK, THE RIGHT PACK WAS ON MEL. THE CREW RETURNED TO KMCO FOR MAINTENANCE "AIRCRAFT REMOVED FROM SERVICE" ACCOMPLISHED VISUAL INSPECTION OF AIR CONDITIONING COOLING DUCTS, FOUND NO
- [SDR A6WA2019122347080](https://openairdocs.org/sdr/A6WA2019122347080.md): Wire Harness · faulty · Dec 22, 2019 · N466AW · Cndair CL6002B19 · Landing Gear System Wiring
  > SUPPLIMENTAL INFORMATION, THE CREW REPORTED THAT THE ANTISKID FAILED AND WERE DIVERTING TO MLI DUE TO THE AVAILABLE RUNWAY LENGTH FOR CID. ANTI SKID OB CAUTION MESSAGE OCCURED 3 TIMES AFTER SELECTING GEAR DOWN FOR LANDING. AIRCRAFT REMOVED FROM SERVICE. REM
- [SDR A6WA2019080946768](https://openairdocs.org/sdr/A6WA2019080946768.md): Frame · corroded · Aug 2, 2019 · N466AW · Cndair CL6002B19 · Fuselage Main, Frame
  > AFT FUSELAGE FS 605 FRANE HAS SEVERAL AREAS OF CORROSION FROM STGR 25R TO 23L.
- [SDR A6WA2019073146762](https://openairdocs.org/sdr/A6WA2019073146762.md): Beam · gouged · Jul 31, 2019 · N466AW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR BEAM MEMBER CHAFFED AT FWD AND AFT COUNTER BALANCE CABLE PULLEY LOCATIONS.
- [SDR A6WA2019073146761](https://openairdocs.org/sdr/A6WA2019073146761.md): Seat Track · gouged · Jul 31, 2019 · N466AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SEAT SIDE TRACK AT THE #2 LOCATION FROM FWD SIDE OF A/C IS GOUGED APPROX 0.375 LONG, 0.250 WIDE AND 0.025 DEEP. FS 409+16 - 409+112.
- [SDR A6WA2019073046755](https://openairdocs.org/sdr/A6WA2019073046755.md): Seat Track · corroded · Jul 30, 2019 · N466AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT #3 SIDE SEAT TRACK FROM FWD SIDE OF A/C IS CORRODED, MARKED WITH TAPE. FS 409+112 - 449.85.
- [SDR A6WA2019073046757](https://openairdocs.org/sdr/A6WA2019073046757.md): Seat Track · corroded · Jul 30, 2019 · N466AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDE #4 SEAT RAIL IS CORRODED, MARKED WITH TAPE. FS 449+85 - 529.
- [SDR A6WA2019073046756](https://openairdocs.org/sdr/A6WA2019073046756.md): Seat Track · corroded · Jul 30, 2019 · N466AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDE SEAT TRACK #3 IS CORRODED, MARKED WITH TAPE. 409+112 - 449.85.
- [SDR A6WA2019073046751](https://openairdocs.org/sdr/A6WA2019073046751.md): Seat Track · corroded · Jul 29, 2019 · N466AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK CORRODED FS 364 - FS 400 LBL9.
- [SDR A6WA2019073046747](https://openairdocs.org/sdr/A6WA2019073046747.md): Seat Track · corroded · Jul 29, 2019 · N466AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SEAT TRACK #6 IS CORRODED, MARKED WITH TAPE. FS 529.00 - 559+16.
- [SDR A6WA2019073046744](https://openairdocs.org/sdr/A6WA2019073046744.md): Seat Track · corroded · Jul 29, 2019 · N466AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDE SEAT TRACK AT THE #5 LOCATION FROM FWD OF A/C IS CORRODED, MARKED WITH TAPE. FS 499.00 - 529.
- [SDR A6WA2019073046748](https://openairdocs.org/sdr/A6WA2019073046748.md): Fitting · cracked · Jul 29, 2019 · N466AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR SUPPORT BEAM CLIP AT FS 484, LBL36 IS CRACKED.
- [SDR A6WA2019073046746](https://openairdocs.org/sdr/A6WA2019073046746.md): Seat Track · corroded · Jul 29, 2019 · N466AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT #2 SIDE SEAT TRACK IS CORRODED MARKED WITH TAPE. FS 409+112 - 409+116.
- [SDR A6WA2019073046750](https://openairdocs.org/sdr/A6WA2019073046750.md): Seat Track · corroded · Jul 29, 2019 · N466AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK CORRODED FS 364 - F.S.400 RBL9.
- [SDR A6WA2019073046745](https://openairdocs.org/sdr/A6WA2019073046745.md): Seat Track · corroded · Jul 29, 2019 · N466AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDE SEAT TRACK AT THE #4 LOCATION IS CORRODED, MARKED WITH TAPE. FS 449.85 - 499.00.
- [SDR A6WA2019073046749](https://openairdocs.org/sdr/A6WA2019073046749.md): Bracket · cracked · Jul 29, 2019 · N466AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RIGHT MAIN LANDING GEAR WHEEL WELL HYDRAULIC TRANSDUCER BRACKET CRACKED.
- [SDR A6WA2019073046752](https://openairdocs.org/sdr/A6WA2019073046752.md): Post · cracked · Jul 29, 2019 · N466AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND INDICATIONS BL0 409+128 VERTICAL POSTS L AND R AFT FLANGE RADIUS APPROX.25" LONG 55% FSH BOTH FAILS NDT.
- [SDR A6WA2019073046738](https://openairdocs.org/sdr/A6WA2019073046738.md): Strap · corroded · Jul 28, 2019 · N466AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOORBOARD SUPPORT STRAP AT FS 559 BETWEEN LBL27 AND LBL36 IS CORRODED.
- [SDR A6WA2019073046739](https://openairdocs.org/sdr/A6WA2019073046739.md): Fitting · cracked · Jul 28, 2019 · N466AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR SUPPORT BEAM CLIP AT FS 484, LBL27 IS CRACKED.
- [SDR A6WA2019073046740](https://openairdocs.org/sdr/A6WA2019073046740.md): Bracket · cracked · Jul 28, 2019 · N466AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LEFT MAIN LANDING GEAR WHEEL WELL HYD. TRANSDUCER BRACKET CRACKED.
- [SDR A6WA2019080146764](https://openairdocs.org/sdr/A6WA2019080146764.md): Angle · cracked · Jul 23, 2019 · N466AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE FLOOR SUPPORT BEAM CLIP AT F.S.484, RBL27 IS CRACKED.
- [SDR A6WA2019080146763](https://openairdocs.org/sdr/A6WA2019080146763.md): Seat Track · corroded · Jul 22, 2019 · N466AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > R/H SEAT TRACK #6 IS CORRODED, MARKED WITH TAPE, F.S.529.00 - 559+16.

Next page: https://openairdocs.org/aircraft/N466AW/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 = 'N466AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N466AW/reports

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