# Service difficulty reports: N468AW

A list on [N468AW](https://openairdocs.org/aircraft/N468AW.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 · 177 reports

- [SDR A6WA202503198863](https://openairdocs.org/sdr/A6WA202503198863.md): Shutoff Valve · leaking · Mar 19, 2025 · N468AW · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > AFT TO IN ICING COND WITH CLIMB PWR AND WING AND CWL AICE ON REC LT WING AICE CAUT MSG, C/W QRH, 14TH STAGE ISO SELECTED AN AFTER 30 SECONDS MSG REMAINS, ON GRND WHEN SELECTING WING AICE TO STANDBY ITT DOES NOT CHANGE. AIRCRAFT REMOVED FROM SERVICE. INSPE
- [SDR A6WA202408278796](https://openairdocs.org/sdr/A6WA202408278796.md): Tire · faulted · Aug 23, 2024 · N468AW · Cndair CL6002B19 · Tire
  > RISING BTMS ON #2 TIRE AFTER LANDING. MINIMAL BRAKING. ON TAXI IN BTMS CONTINUED TO RISE. APPROACHING GATE BRAKE OVER HEAT WARNING BTMS VALUE 11 Q/W QRH. AFTER PARKING #2 TIRE OFF RIM WITH OCCASIONAL SMOKE. AIRCRAFT REMOVED FROM SERVICE. INSP #2 BREAK TIRE
- [SDR A6WA202401098691](https://openairdocs.org/sdr/A6WA202401098691.md): Fitting · gouged · Jan 9, 2024 · N468AW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > UPON REMOVAL OF THE R/H WING TO FSLG FITTING, FOUND DAMAGE ON FITTING. ******AIRCRAFT REMOVED FROM SERVICE******** REPAIRED R/H WING TO FUSELAGE FITTING AND UPPER WING SKIN AT W.S.424, RBL 45 IAW MHIRJ REO 601R-57-11-101.
- [SDR A6WA202310258664](https://openairdocs.org/sdr/A6WA202310258664.md): Unknown · unknown · Oct 25, 2023 · N468AW · Cndair CL6002B19 · Landing Gear Actuator
  > WHEN SELECTING GEAR UP ON TAKE-OFF, GOT GEAR DISAGREE WARNING. RAN QRH AND GEAR EXTENDED NORMALLY. NOSE GEAR RED SYMBOL AND NOSE DOOR OPEN RED WARNING. GEAR DISAGREE MESSAGE APPEARED WITHIN 5 SECS. *******AIRCRAFT REMOVED FROM SERVICE*********** VISUALLY
- [SDR A6WA202309308657](https://openairdocs.org/sdr/A6WA202309308657.md): Fuel Cap · corroded · Sep 30, 2023 · N468AW · Cndair CL6002B19 · Fuel Storage
  > LH AND RH OVER WING FUEL CAP RING AREAS SHOWN SIGNS OF CORROSION AND DETERMINED OUTSIDE OF SRM LIMITATIONS. ***** AC REMOVED FROM SERVICE ***** BLEND REPAIR IAW MHI TECH DATA AS PROVIDED.
- [SDR A6WA202305128604](https://openairdocs.org/sdr/A6WA202305128604.md): Floor Support · corroded · May 12, 2023 · N468AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON CARGO FLOOR SILL PN601R31132-58 AT FS605.00+5 AND RBL42. ***** AC REMOVED FROM SERVICE ***** REPLACED FLOOR SILL SUPPORT ANGLE WITH A NEW FABRICATED ANGLE 601R AT FS559 AND LBL28.00. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORME
- [SDR A6WA202305128602](https://openairdocs.org/sdr/A6WA202305128602.md): Rudder · dented · May 12, 2023 · N468AW · Cndair CL6002B19 · Rudder, Plate/Skin
  > DENT ON LH RUDDER RS 125.44-RS131.17 *******AIRCRAFT REMOVED FROM SERVICE****** REPAIRED DENT ON LH RUDDER AT RS125.44-RS131.17 AND FOUND TO BE ACCEPTABLE PER REO. DENT DIMENSION L = 1.500Ï¿½ X W = 1.150Ï¿½ X D = 0.027Ï¿½. PERFORMED HFEC WITH NO INDICATIONS.
- [SDR A6WA202305118599](https://openairdocs.org/sdr/A6WA202305118599.md): Vane · chafed · May 11, 2023 · N468AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LH WING INBOARD FLAP IB FLAP HAS CHAFFING PN 601R14303-41 LH WING LEADING EDGE SKIN MID IB FLAP PN 601R14303-39 ****AIRCRAFT REMOVED FROM SERVICE********* LH WING INBOARD FLAP IB FLAP HAS CHAFFING PN 601R14303-41 LH WING LEADING EDGE SKIN MID IB FLAP PN 601R14
- [SDR A6WA202305118600](https://openairdocs.org/sdr/A6WA202305118600.md): Stiffener · dented · May 11, 2023 · N468AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DENT ON V STIFFENER ON AFT ACCESS PANEL PN#15A150-1 OF APU ENCLOSURE ASSY PN#15A104-103) *****AIRCRAFT REMOVED FROM SERVICE********* DENT ON V STIFFENER ON AFT ACCESS PANEL PN#15A150-1 OF APU ENCLOSURE ASSY PN#15A104-103) EVALUATED DENTED AREA AT V STIFFENER O
- [SDR A6WA202305118601](https://openairdocs.org/sdr/A6WA202305118601.md): Floor Support · corroded · May 11, 2023 · N468AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON RH FLOOR SILL STRAP PN# 601R31133-1225 AND LIPPED PLATE PN#601R31133-101 AT FS559.00+12-559-80 FS559.00+112-559.00+80 AND RBL28.00 *******AIRCRAFT REMOVED FROM SERVICE******** REPLACED FLOOR SILL WITH A NEW FABRICATED P/N 601R31133-1225 AT FS5
- [SDR A6WA202305108598](https://openairdocs.org/sdr/A6WA202305108598.md): Rudder · dented · May 10, 2023 · N468AW · Cndair CL6002B19 · Rudder Structure
  > DENT ON SKIN RUDDER AT RS121.80 *******AIRCRAFT REMOVED FROM SERVICE****** DENT ON SKIN RUDDER AT RS121.80 EVALUATED DENT ON RUDDER AT RS 121.80 AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION L = 1.90Ï¿½ X W = 0.400 X D = 0.012Ï¿½. PERFORMED HFEC WITH
- [SDR A6WA202305108597](https://openairdocs.org/sdr/A6WA202305108597.md): Floor Support · corroded · May 10, 2023 · N468AW · Cndair CL6002B19 · Fuselage Structure (General)
  > BLENDED CORROSION ON RH FLOOR SUPPORT STRUCTURE BETWEEN FS621.00 AT RBL 9 AND RBL 27 ******AIRCRAFT REMOVED FROM SERVICE******* CORROSION 2 AREAS ON RH FLOOR SUPPORT STRUCTURE BETWEEN FS621.00 AT RBL 27 BLENDED CORROSION ON RH FLOOR SUPPORT STRUCTURE BETWEE
- [SDR A6WA202305098593](https://openairdocs.org/sdr/A6WA202305098593.md): Bracket · corroded · May 9, 2023 · N468AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON PASSENGER DOOR LOWER SILL AT BETWEEN FS310.00 AND FS349.00. ***** AC HAS BEEN REMOVED FROM SERVICE ***** BLENDED CORROSION ON PASSENGER DOOR LOWER SILL AT BETWEEN FS310.00 AND FS349.00. BRACKET P/N 601R31527-217. MEASUREMENTS P1-L=5.900Ï¿½ X W=1.
- [SDR A6WA202305058596](https://openairdocs.org/sdr/A6WA202305058596.md): Seat Track · corroded · May 5, 2023 · N468AW · Cndair CL6002B19 · Fuselage Structure (General)
  > CORROSION ON SEAT RAIL AT FS589.00+8 TO FS605.00 & LBL27. P1-L=1.800Ï¿½X W=0.900Ï¿½X D=.050 AIRCRAFT REMOVED FROM SERVICE. CORROSION ON SEAT RAIL BLENDED CORROSION ON SEAT RAIL FS589.00+8 & RBL27.ORIGINAL MATERIAL THICKNESS 0.050Ï¿½ & REMAINING THICKNESS 0.
- [SDR A6WA202212228423](https://openairdocs.org/sdr/A6WA202212228423.md): Controller · failed · Dec 31, 2022 · N468AW · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
  > R WINDOW HEAT CAUTION MESSAGE IN FLIGHT. INFLIGHT SMELT ELECTRICAL SMELL. C/W QRH MESSAGE CLEARED. AIRCRAFT REMOVED FROM SERVICE. FOUND RT WINDSHIELD HEAT CONTROLLER HAS BURNED SMELL, R&R RT WINDSHIELD HEAT CONTROLLER IAW AMM 30-41-01 PERFORMED RT WINDOW A
- [SDR A6WA202212098401](https://openairdocs.org/sdr/A6WA202212098401.md): Relief Valve · faulted · Dec 9, 2022 · N468AW · Cndair CL6002B19 · Air Intake Anti/De-Ice System
  > LH COWL ANTI ICE CAU IN FLT WITH COWL SWITCH SELECTED OFF. C/W QRH RETURNED TO DAY, AIRCRAFT REMOVED FROM SERVICE. R & R THE RELIEF VALAVE OF LT ENG IAW AMM 30-22-04, OPS CHECKED GOOD.
- [SDR A6WA202110157934](https://openairdocs.org/sdr/A6WA202110157934.md): Skin · dented · Oct 15, 2021 · N468AW · Cndair CL6002B19 · Fuselage Structure (General)
  > MULTIPLE DENTS AND GOUGES ON AFT FUSELAGE SKIN BTW FS589.00 Ï¿½ FS605.00 AND STR24R Ï¿½ STR26R. DRESSED 4 DENTS AND BLENDED 22 GOUGES ON AFT FUSELAGE SKIN BTW FS589.00 Ï¿½ FS605.00 AND STR24R Ï¿½ STR26R. SKIN PN 601R35005. POST DRESS DENT DIMENSIONS P1 - L=
- [SDR A6WA202110147933](https://openairdocs.org/sdr/A6WA202110147933.md): Skin · dented · Oct 14, 2021 · N468AW · Cndair CL6002B19 · Fuselage Structure (General)
  > DENT ON AFT FUSELAGE SKIN AT FS605.00 Ï¿½ FS621.00 AND S21L TO S23L. EVALUATED DENT ON AFT FUSELAGE SKIN AT FS682.00 Ï¿½ FS700.00 AND S23R TO S24R. AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION L = 4.200Ï¿½ X W = 0.800Ï¿½ X D = 0.008Ï¿½. PERFORMED HFEC W
- [SDR A6WA202110147931](https://openairdocs.org/sdr/A6WA202110147931.md): Skin · dented · Oct 14, 2021 · N468AW · Cndair CL6002B19 · Fuselage Structure (General)
  > DENT ON AFT FUSELAGE SKIN AT FS672.00 Ï¿½ FS682.00 AND S22-L TO S23L. EVALUATED DENT ON AFT FUSELAGE SKIN AT FS672.00 Ï¿½ FS682.00 AND S22-L TO S23L. AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION L = 0.150Ï¿½ X W = 0.100Ï¿½ X D = 0.004Ï¿½. PERFORMED HFEC
- [SDR A6WA202110147932](https://openairdocs.org/sdr/A6WA202110147932.md): Skin · dented · Oct 14, 2021 · N468AW · Cndair CL6002B19 · Fuselage Structure (General)
  > DENT ON AFT FUSELAGE SKIN AT FS682.00 Ï¿½ FS700.00 AND S23R TO S24R. EVALUATED DENT ON AFT FUSELAGE SKIN AT FS682.00 Ï¿½ FS700.00 AND S23R TO S24R. AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION L = 0.600Ï¿½ X W = 0.250Ï¿½ X D = 0.006Ï¿½. PERFORMED HFEC W
- [SDR A6WA202101157545](https://openairdocs.org/sdr/A6WA202101157545.md): Warning Message · false activation · Jan 14, 2021 · N468AW · Cndair CL6002B19 · Engine Thrust Reverser
  > LT REVERSER UNLOCKED CAUTION IN FLIGHT. CW WITH IAPS AND QRH. A/C PERFORMANCE NORMAL THROUGHOUT. AIRCRAFT REMOVED FROM SERVICE. PERFORMED OPERATIONAL TEST OF THRUST REVERSER SYSTEM, REFERENCE AMM 71-00-00-710-806. OPERATIONAL TEST NORMAL, AIRCRAFT OK FOR
- [SDR A6WA2020020547153](https://openairdocs.org/sdr/A6WA2020020547153.md): Transducer · malfunctioned · Feb 4, 2020 · N468AW · Cndair CL6002B19 · Hydraulic Indicating System
  > 3926 AT ALTITUDE OBSERVED THAT HYD SYS WAS AT APPROX 2400 PSI AND 60% QTY, DECREASING PRESSURE AND FLUCTUATION. WHEN PRESSURE WAS AT 1800 PSI, RAN APPROPIATE QRH PROCEDURE. DIVERTING TO SDF. DURING DESCENT NOTICED LARGE FLUCTUATIONS IN HYD 1 PRESSURE FR
- [SDR A6WA2019101746929](https://openairdocs.org/sdr/A6WA2019101746929.md): Track · gouged · Oct 13, 2019 · N468AW · Cndair CL6002B19 · Cargo/Baggage Doors
  > PERMANENT REPAIR CARGO DOOR BEAM TRACK. REPLACED CARGO DOOR BEAM MEMBER IAW SRM 51-42-06 AND 51-42-21
- [SDR A6WA2019101546924](https://openairdocs.org/sdr/A6WA2019101546924.md): Support Angle · cracked · Oct 13, 2019 · N468AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR LOWER CLOSING PLATE SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED LOWER CLOSING PLATE SUPPORT ANGLE IAW SRM 51-41-02.
- [SDR A6WA2019101546927](https://openairdocs.org/sdr/A6WA2019101546927.md): Post · cracked · Oct 13, 2019 · N468AW · Cndair CL6002B19 · Fuselage Main, Structure
  > FS 409+128 RBL 18 POST OUTBOARD IS CRACKED IN THE RADIUS AT THE BOTTOM PASSED ONE RIVET. REPAIRED FS 409+128 RBL 18 OUTBOARD POST IAW REO 601R-53-41-056 REV F
- [SDR A6WA2019101546925](https://openairdocs.org/sdr/A6WA2019101546925.md): Step · corroded · Oct 13, 2019 · N468AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR LOWER STEP CORRODED (832AT). REMOVED AND REPLACED PAX DOOR LOWER STEP IAW AMM 52-11-04
- [SDR A6WA2019101546926](https://openairdocs.org/sdr/A6WA2019101546926.md): Vane · chafed · Oct 12, 2019 · N468AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT WING INBOARD FLAP VANE SKIN CHAFFED ON I/B SIDE. REMOVED AND REPLACED L/H INBOARD FLAP VANE, INBOARD VANE SKIN IAW SRM 51-42-10
- [SDR A6WA2019101546928](https://openairdocs.org/sdr/A6WA2019101546928.md): Vane · chafed · Oct 12, 2019 · N468AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT WING INBOARD FLAP VANE SKIN CHAFFED IN MIDDLE OF VANE. REMOVED AND REPLACED L/H WING INBOARD FLAP VANE SKIN MIDDLE OF VANE IAW SRM 51-42-13
- [SDR A6WA2019101546917](https://openairdocs.org/sdr/A6WA2019101546917.md): Intercostal · cracked · Oct 12, 2019 · N468AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR LOWER AFT INTERCOSTAL HAS POSSIBLE CRACK INDICATION. REMOVED AND REPLACED PAX DOOR LWR AFT INTERCOSTAL IAW CRJ-200 SRM 51-42-066 AND 51-42-21
- [SDR A6WA2019101546921](https://openairdocs.org/sdr/A6WA2019101546921.md): Bracket · corroded · Oct 10, 2019 · N468AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > PAX DOOR LWR SILL ANGLE BOTH CONNECTOR PLUG BRACKETS HAVE CORROSION. REMOVED AND REPLACED PAX DOOR LWR SILL CONNECTOR PLUG BRACKETS IAW CRJ-200 SRM 51-42-06.
- [SDR A6WA2019101546918](https://openairdocs.org/sdr/A6WA2019101546918.md): Angle · cracked · Oct 10, 2019 · N468AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 621 APB FWD SIDE MACHINED ANGLE AT WL 73 LBL 42 HAS A CRACK. REMOVED AND REPLACED FWD SIDE MACHINED ANGLE FS 621 AT WL 73 LBL 42 IAW BOMB. REO 601R-53-61-117.
- [SDR A6WA2019101546922](https://openairdocs.org/sdr/A6WA2019101546922.md): Bracket · corroded · Oct 10, 2019 · N468AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > PAX DOOR LWR SILL ANGLE BOTH CONNECTOR PLUG BRACKETS HAVE CORROSION. REMOVED AND REPLACED PAX DOOR LWR SILL CONNECTOR PLUG BRACKETS IAW SRM 51-42-06.
- [SDR A6WA2019101546920](https://openairdocs.org/sdr/A6WA2019101546920.md): Rib · cracked · Oct 9, 2019 · N468AW · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > PANEL 436AL EXHAUST FAIRING #2 RIB CRACKED AT TOOLING HOLE. REPAIRED CRACKED STIFFENER IAW 78-11-11 SRS042
- [SDR A6WA2019101546923](https://openairdocs.org/sdr/A6WA2019101546923.md): Floor Support · corroded · Oct 9, 2019 · N468AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SILL AT FS 310 BY PAX DOOR HAS CORROSION. REMOVED AND REPLACED DOUBLER IAW CRJ-200 SRM 51-42-10
- [SDR A6WA2019101146912](https://openairdocs.org/sdr/A6WA2019101146912.md): Skin · cracked · Oct 8, 2019 · N468AW · Cndair CL6002B19 · Landing Gear Doors
  > NLG DOOR CUT-OUT HAS A CRACK ON R/H AFT SIDE. REPAIRED CRACKED AREA ON NOSE LANDING GEAR DOOR CUT-OUT. R/H AFT SIDE IAW B/A REO 601R-53-11-048 REV. D
- [SDR A6WA2019101546919](https://openairdocs.org/sdr/A6WA2019101546919.md): Post · cracked · Oct 7, 2019 · N468AW · Cndair CL6002B19 · Fuselage Main, Structure
  > FS 409+128 VERTICAL POST AT BL 0 IS CRACKED AT AFT ANGLE, 6TH FASTENER DOWN FROM TOP, IN RADIUS ON BOTH LEFT AND RIGHT SIDES. REMOVED AND REPLACED VERTICAL POST AT BL 0 IAW SRM 51-42-06 AND REO 601R-53-41-889.
- [SDR A6WA2019101146914](https://openairdocs.org/sdr/A6WA2019101146914.md): Angle · cracked · Oct 7, 2019 · N468AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CLIP AT LBL 9 AND FS 280 IS CRACKED REMOVED AND REPLACED CLIP IAW CRJ-200 SRM 51-42-21.
- [SDR A6WA2019100846905](https://openairdocs.org/sdr/A6WA2019100846905.md): Bracket · cracked · Oct 3, 2019 · N468AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RIGHT MLG WHEEL WELL VOLUMETRIC FUSE LINE BRACKET IS CRACKED. REPLACED BRACKET IAW SRM 51-41-02, 51-42-06.
- [SDR A6WA2019100846906](https://openairdocs.org/sdr/A6WA2019100846906.md): Bracket · cracked · Oct 3, 2019 · N468AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RIGHT WHEEL WELL AREA VOLUMETRIC FUSE BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-41-02, 51-42-06.
- [SDR A6WA2019100846904](https://openairdocs.org/sdr/A6WA2019100846904.md): Skin · cracked · Oct 3, 2019 · N468AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LEFT TRU DOOR CUT OUT CRACKED AT AFT LATCH. REPAIRED IAW 19-016B.
- [SDR A6WA2019070346687](https://openairdocs.org/sdr/A6WA2019070346687.md): Warning System · activated · Jul 1, 2019 · N468AW · Cndair CL6002B19 · Landing Gear Steering System
  > WHILE ENROUTE FROM KCAK TO KORD, THE FLIGHT CREW RECEIVED A NOSE WHEEL STEERING INOP CAUTION MESSAGE. THE FLIGHT CREW FOLLOWED THE QRH, COORDINATED WITH ATC AND DISPATCH, BRIEFED THE FLIGHT ATTENDANT AND PASSENGERS AND CONTINUED TO KORD FOR AN OTHERWISE NORMAL
- [SDR A6WA2019061946669](https://openairdocs.org/sdr/A6WA2019061946669.md): Wire Harness · crushed · Jun 18, 2019 · N468AW · Cndair CL6002B19 · Landing Gear System Wiring
  > AFTER GEAR RETRACTION (6 TO 10 SECONDS) RECIEVED GEAR DISAGREE WARNING WITH NOSE DOOR WARNING WITH GEAR LEVER IN UP POSITION. RAN QRH,MESSAGE WENT AWAY, GEAR DOWN AND LOCKED. CREW PERFORMED AN AIR RETURN TO ORD. ON POST FLIGHT, FO FOUND HYD FLUID IN NOSE GEAR
- [SDR A6WA2019012846330](https://openairdocs.org/sdr/A6WA2019012846330.md): Escape Rope · short · Jan 25, 2019 · N468AW · Cndair CL6002B19 · Emergency Equipment
  > FLIGHT ATTENDANT REPORTS LT OVER WING ESCAPE ROPE TOO SHORT WHEN USED FOR TRAINING.
- [SDR A6WA2018031345690](https://openairdocs.org/sdr/A6WA2018031345690.md): Windshield · failed · Mar 11, 2018 · N468AW · Cndair CL6002B19 · Flight Compartment Windows
  > DURING CLIMB OUT, AT 15,000 FT, THE RIGHT WINDSHIELD SHATTERED INFLIGHT, APPEARS TO BE INNER OR OUTER PANE. COMPLIED WITH QRH. DECLARED EMERGENCY.
- [SDR A6WA201745400](https://openairdocs.org/sdr/A6WA201745400.md): Intercostal · cracked · Nov 5, 2017 · N468AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 621 TO 625.3 INTERCOSTAL CRACKED AT STRINGER 13L.
- [SDR A6WA2017110645394](https://openairdocs.org/sdr/A6WA2017110645394.md): Support Angle · cracked · Nov 2, 2017 · N468AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR POWER ASSIST MOTOR LWR SUPPORT ANGLE IS CRACKED
- [SDR A6WA2017110645390](https://openairdocs.org/sdr/A6WA2017110645390.md): Rib · cracked · Oct 31, 2017 · N468AW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > LEFT WING BATTERU RIB CRACKED.
- [SDR A6WA2017103045387](https://openairdocs.org/sdr/A6WA2017103045387.md): Stringer · cracked · Oct 27, 2017 · N468AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L CRACKED AT BS 379. REPAIRED THE STRINGER IAW SRM 53-00-03.
- [SDR A6WA2017103045379](https://openairdocs.org/sdr/A6WA2017103045379.md): Bracket · cracked · Oct 26, 2017 · N468AW · Cndair CL6002B19 · Fuselage Main, Structure
  > CENTER POST, RT SIDE LOWER BRACKET CRACKED. REPLACED THE BRACKET IAW SRM 51-42-21.
- [SDR A6WA2017103045380](https://openairdocs.org/sdr/A6WA2017103045380.md): Intercostal · cracked · Oct 24, 2017 · N468AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED AT BS 621 TO 625, STRINGER 14L. REPLACED THE INTERCOSTAL IAW SRM 51-42-21, AND 51-42-22.

Next page: https://openairdocs.org/aircraft/N468AW/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 = 'N468AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N468AW/reports

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