# Service difficulty reports: N454AW

A list on [N454AW](https://openairdocs.org/aircraft/N454AW.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 · 156 reports

- [SDR A6WA202610098919](https://openairdocs.org/sdr/A6WA202610098919.md): Landing Gear · malfunctioned · Oct 10, 2026 · N454AW · Cndair CL6002B19 · Nose/Tail Landing Gear
  > AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT. AFTER LANDING FOUND NOSE STRUT FULLY COMPRESSED. AIRCRAFT REMOVED FROM SERVICE. SERVICED NLG SHOCK STRUT REFR MCTM 000.12-710-003 AND PERFORMED NLG EXTENSION AND RETRACTION TEST IAW AMM 32-33-00. OPS CHECK GOOD
- [SDR A6WA202512038872](https://openairdocs.org/sdr/A6WA202512038872.md): Wire Harness · false activation · Dec 3, 2025 · N454AW · Cndair CL6002B19 · Landing Gear System Wiring
  > EAR DISAGREE AFTER SELECTING GEAR UP. ALSO RECEIVED PROX SYSTEM FAULT STATUS FOR SEVERAL SECONDS THEN CLEARED. NOSE GEAR RETRACTED SLOWLY. AIRCRAFT REMOVED FROM SERVICE. DOWNLOADED PSEU CODES AND RECEIVED "INSP 523" AND A02 FAIL" FOR BOTH LEGS. CODES POINT TO
- [SDR A6WA202511138870](https://openairdocs.org/sdr/A6WA202511138870.md): Priority Valve · faulted · Nov 13, 2025 · N454AW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE MSG DURING RETRACTION. AFTER 28 SECONDS, NOSE DOOR MESSAGE AFTER EMERGENCY EXTENSION HANDLE. HYD PUMPS IN AUTO DURING INITIAL MSGS, THEN SELECTED TO "ON" DURING QRH, NO ICE OR TURBULENCE DURING EVENT. JUST NLG BOX SHOWED RED. AIRCRAFT REMOVED FR
- [SDR A6WA202405158750](https://openairdocs.org/sdr/A6WA202405158750.md): Button · engaged · May 15, 2024 · N454AW · Cndair CL6002B19 · Fire Detection
  > REVEIVED APU FIRE INDICATION AFTER APU START, C/W QRH MSG CLEARED IN 5 SECONDS. ALSO HAD APU FIRE FAIL AND APU ECU FAULT CAUTION MSG'S -ALL MSG'S CAME ON AT THE SAME TIME APU FIRE BOTTLE NOT BLOWN. AIRCRAFT REMOVED FROM SERVICE. FOUND APU FIRE PUSHBUTTON EN
- [SDR A6WA202404018727](https://openairdocs.org/sdr/A6WA202404018727.md): Control Unit · faulted · Apr 1, 2024 · N454AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL AT 20 ON APPROACH WHILE SELECTING FLAPS 30 PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE. R&R FECU IAW AMM 27-51-05-04. OPS CHECK GOOD AT THIS TIME. REMO
- [SDR A6WA202301268706](https://openairdocs.org/sdr/A6WA202301268706.md): Apu · smoke · Jan 26, 2024 · N454AW · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) System
  > SMOKE TOILET CAUTION MSG SHORTLY AFTER TAKE OFF. MSG DISAPPEARED 3 MINUTES LATER. C/W QRH. ********AIRCRAFT REMOVED FROM SERVICE********* REF LP 338553-4 FOR CORRECTIVE ACTION. SMOKE DETECTOR OPS CHECK NORMAL IAW AMM 26-16-00. REF WO 335707, APU R&R F
- [SDR A6WA202301268705](https://openairdocs.org/sdr/A6WA202301268705.md): Apu · smoke · Jan 26, 2024 · N454AW · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) System
  > APU SHUTDOWN ON GND AND CAUSED SMOKE IN CABIN *****AIRCRAFT REMOVED FROM SERVICE********** PREFORMED PAC BURN OUT PROCEDURE IAW AWAC SUP 09-037E, NO UNUSUAL SMELLS OR SMOKE IN CABIN AFTER PROCEDURE. REF 338553-4 FOR MEL OF APU. AIRCRAFT OK FOR RTS. REF
- [SDR A6WA202312198683](https://openairdocs.org/sdr/A6WA202312198683.md): Unknown · unknown · Dec 19, 2023 · N454AW · Cndair CL6002B19 · Air Distribution System
  > 364734-1 FO REPORTS SMOKE SMELL SIMILAR TO MARIJUANA COMING FROM THE GASPER, NO AIRCRAFT SYSTEM ABNORMALITY NOTED. C/W AWAC SUP 09-037D FOR USUAL ODORS, NO SMOKE SMELL NOTED AC OK FOR SERVICE
- [SDR A6WA202304028540](https://openairdocs.org/sdr/A6WA202304028540.md): Fuel Control · unknown · Apr 2, 2023 · N454AW · Cndair CL6002B19 · Fuel Control/Turbine Engines
  > DURRING OUR DECENT WE NOTICED N1 WILL NOT REDUCE BELOW 67% ON LH ENGINE. THROTTLE LEVER DID MOVE TO FLIGHT IDLE POSITION. NO CHANGE IN N1. WAS ABLE TO INCREASE N1 WHEN COMMANDED. ********AIRCRAFT REMOVED FROM SERVICE******** R&R LH FUEL CONTROL IAW AMM 73-
- [SDR A6WA2023012318438](https://openairdocs.org/sdr/A6WA2023012318438.md): Indicator · inoperative · Jan 21, 2023 · N454AW · Cndair CL6002B19 · Altimeter, Barometric/Encoder
  > ABORTED TAKE-OFF AT APPROX. 100 KNOTS DUE TO STANDBY ASI NOT COMING ALIVE. STANDBY ASI REMAINED AT ZERO. BRACKET TEMPS SHOWED 5,6,5,4. NO BRAKE OVERHEAT WARNING DISPLAYED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED STBY ALT /IND ASI (SA/IAS) IAW
- [SDR A6WA202212138418](https://openairdocs.org/sdr/A6WA202212138418.md): Plate · corroded · Dec 13, 2022 · N454AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR THRESHOLD PROTECTOR (P/N; 601R38957-31) CORRODED INBD LOWER SURFACE. AIRCRAFT REMOVED FROM SERVICE. REPLACED SERVICE DOOR THRESHOLD PROTECTOR PER SRM 51-41-02 PAR 7
- [SDR A6WA202212138407](https://openairdocs.org/sdr/A6WA202212138407.md): Angle · cracked · Dec 13, 2022 · N454AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACKED MLG WHEEL BAY WEB, FWD OF OUTBOARD SIDE AT BS 409+128 ON THE AFT SPAR. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE ANGLE IAW EA AWAC-CRJ253-01913, REV IR.
- [SDR A6WA202212128406](https://openairdocs.org/sdr/A6WA202212128406.md): Seat Track · corroded · Dec 12, 2022 · N454AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT CABIN SEAT TRACK, BS 349 - 409 HAD EVIDENCE OF SURFACE CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK BS 349 - 409 IAW AMM 53-01-11.
- [SDR A6WA202212118421](https://openairdocs.org/sdr/A6WA202212118421.md): Skin · corroded · Dec 11, 2022 · N454AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERIOR SKIN UNDER FORWARD DRAIN MAST CORRODED. AIRCRAFT REMOVED FROM SERVICE. BLENDED & CUT OUT CORROSION AND INSTALLED EXTERNAL DOUBLER IAW EA AWAC-CRJ253-01922.
- [SDR A6WA202212088399](https://openairdocs.org/sdr/A6WA202212088399.md): Angle · cracked · Dec 8, 2022 · N454AW · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > LEFT STRUCTURE CRACKED AT MLG WHEEL WELL BAY WEB FWD OF OUTBOARD SIDE AT FS 409+128 ON AFT SPAR. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LT MLG WHEEL BAY ANGLE IAW AWAC-CRJ253-1914 REV IR.
- [SDR A6WA202211168414](https://openairdocs.org/sdr/A6WA202211168414.md): Seat Track · corroded · Nov 16, 2022 · N454AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > L/H CABIN SIDE SEAT TRACK BS 349 - 409 WAS CORRODED. R & R THE SEAT TRACK.
- [SDR A6WA202110277940](https://openairdocs.org/sdr/A6WA202110277940.md): None · none · Oct 27, 2021 · N454AW · Cndair CL6002B19 · Steering Unit
  > AFTER TAKEOFF RECEIVED STEERING INOP. C/W QRH, MESSAGE PERSIST. WORKED AFTER LANDING. R&R STEERING ELECTRO HYD SERVO VALVE AND PERF OP CK IAW AMM 32-51-15. NO DEFECTS AT THIS TIME. P/N: 16736-105, S/N OFF; DUO
- [SDR A6WA202102147630](https://openairdocs.org/sdr/A6WA202102147630.md): Pressure Blkhd · cracked · Nov 13, 2020 · N454AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACK DETECTED ON FWD FACE OF AFT PRESSURE BULKHEAD AT RBL 18.00 36 INCHES ABOVE FLOOR AND ON LBL 36.20 6 INCHES ABOVE FLOOR LEVEL ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED DAMAGE AREAS ON AFT PRESSURE BULKHEAD AT RBL 18.00, 36 INCHES ABOVE FLOOR LEVEL A
- [SDR A6WA202011167421](https://openairdocs.org/sdr/A6WA202011167421.md): Skin · dented · Nov 13, 2020 · N454AW · Cndair CL6002B19 · Leading Edge Devices
  > RIGHT INBOARD FLAP HAS A DENT 9" X 6.4" X.087". DENT OUT OF LIMITS DUE TO DENT ON FASTENER ROW, IAW CRJ200-SRM57-52-00. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT INBOARD FLAP, IAW CRJ 200 AMM 27-54-01.
- [SDR A6WA202011167420](https://openairdocs.org/sdr/A6WA202011167420.md): Bulkhead Web · cracked · Nov 13, 2020 · N454AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACK DETECTED ON FWD FACE OF AFT PRESSURE BULKHEAD AT FS 621 LBL 36.2, 6" ABOVE THE FLOOR LINE. AIRCRAFT REMOVED FROM SERVICE. CRACK REPAIRED AT FS 621 LBL 36.2, 6" ABOVE THE FLOOR LINE, IAW REO 601R-53-61-1285.
- [SDR A6WA202011167422](https://openairdocs.org/sdr/A6WA202011167422.md): Angle · cracked · Nov 13, 2020 · N454AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR STAIR TO DOOR SKIN ANGLE CRACKED AFT OF DOOR ASSIST CABLE PULLEY BRACKET. AIRCRAFT REMOVED FROM SERVICE. REMOVED CRACKED DOOR SKIN ANGLE AFT SIDE PASSENGER DOOR AND INSTALLED NEW SKIN ANGLE, IAW PL 601R-52-11-513.
- [SDR A6WA202011137418](https://openairdocs.org/sdr/A6WA202011137418.md): Skin · cracked · Nov 13, 2020 · N454AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > TRANSFORMER RECTIFIER SUPPORT SKIN CRACKED BETWEEN FS 193.00 AND HYDRAULIC SYSTEM 2 & 3 ACCUMULATOR SUPPORT BRACKET. AIRCRAFT REMOVED FROM SERVICE. REPAIRED RECTIFIER SUPPORT SKIN AT FS 193, IAW REO 601R-53-11-111.
- [SDR A6WA202011137417](https://openairdocs.org/sdr/A6WA202011137417.md): Bulkhead Web · cracked · Nov 12, 2020 · N454AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACK DETECTED ON FWD FACE OF AFT PRESSURE BULKHEAD AT RBL 18 36" ABOVE FLOOR LEVEL FS 621. AIRCRAFT REMOVED FROM SERVICE. REPAIRED DAMAGE ON AFT PRESSURE BULKHEAD AT RBL 18 FS 621 36" ABOVE FLOOR LEVEL, IAW BOMBARDIER REO 601R-53-61-1285 REV D.
- [SDR A6WA202011137416](https://openairdocs.org/sdr/A6WA202011137416.md): Structure · corroded · Nov 12, 2020 · N454AW · Cndair CL6002B19 · Fuselage Main, Structure
  > T-CAP EXTRUSION AT FS 574 T0 FS 605+10 CORRODED. AIRCRAFT REMOVED FROM SERVICE. REPLACE CORRODED T-CAP EXTRUSION AT FS 574 T0 FS 605+10 LBL 27, IAW BOMBARDIER DRWG 601R35031 REV P.
- [SDR A6WA202011137415](https://openairdocs.org/sdr/A6WA202011137415.md): Seat Track · corroded · Nov 12, 2020 · N454AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 AT FS 559+88 SEAT TRACK HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK SECTION, IAW BOMBARDIER REO 601R-53-00-764.
- [SDR A6WA2020022847205](https://openairdocs.org/sdr/A6WA2020022847205.md): Shutoff Valve · malfunctioned · Feb 26, 2020 · N454AW · Cndair CL6002B19 · Cabin Cooling System
  > RECEIVED R PACK HIGH PRESS CAUTION AFTER TAKEOFF IN CLIMB,PER QRH PER MEL MESSAGE DID NOT CLEAR RAN APENDIX B PER MEL. "AIRCRAFT REMOVED FROM SERVICE" R/R RH PRSOV IAW CRJ 200 AMM 21-51-43 OPS CHECK GOOD NO MSG ON EICAS SN OFF 1845 S
- [SDR A6WA2019080246766](https://openairdocs.org/sdr/A6WA2019080246766.md): Warning Message · illuminated · Jul 28, 2019 · N454AW · Cndair CL6002B19 · Door Warning System
  > SHORTLY AFTER TAKEOFF CREW RECEIVED A SERVICE DOOR CAUTION MESSAGE. THEY CIRCLED BACK AROUND TO LAND AT IAD. CREW SPOKE WITH MAINTENANCE UPON LANDING AND THE SERVICE DOOR INDICATION SYSTEM WAS PLACED ON MEL. AIRCRAFT DEPARTED WITH NO FURTHER ISSUES. SERVICE D
- [SDR A6WA2018111246146](https://openairdocs.org/sdr/A6WA2018111246146.md): Stringer · corroded · Nov 10, 2018 · N454AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STR 27 HAS PITTING BETWEEN THE APB AND FS 605 FRAME. REPAIRED STR 27 IAW REO 601R-53-61-6766 AND SRM 53-00-03.
- [SDR A6WA2018111246145](https://openairdocs.org/sdr/A6WA2018111246145.md): Skin · cracked · Nov 10, 2018 · N454AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LT TRU DOOR LANDING SKIN IS CRACKED AT AFT LATCH CUTOUT. REPLACED LT TRU DOOR LANDING IAW SRM 51-42-13, 51-42-06 AND SUPP 17-280.
- [SDR A6WA2018111246143](https://openairdocs.org/sdr/A6WA2018111246143.md): Plug · pulled · Nov 7, 2018 · N454AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FWD LT PRESSURE PANEL 131AL CUT OUT PREVIOUS FREEZE PLUG PULLED OUT OF SURROUND DOUBLER. REPAIRED.
- [SDR A6WA2018110546132](https://openairdocs.org/sdr/A6WA2018110546132.md): Support Channel · cracked · Nov 3, 2018 · N454AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR FOWARD TRACK SUPPORT CHANNEL WAS CRACKED. REMOVED AND REPLACED THE SUPPORT CHANNEL IAW SRM 51-42-02, AND 51-42-06.
- [SDR A6WA2018110546133](https://openairdocs.org/sdr/A6WA2018110546133.md): Bracket · cracked · Nov 3, 2018 · N454AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LEFT FWD ZEE BRACKET WAS CRACKED ON THE OTBD SIDE FOR HYDRAULIC VOLUMETRIC FUSE. REMOVED AND REPLACED THE BRACKET IN THE LT WHEEL WELL IAW SRM 51-42-06.
- [SDR A6WA2018110546131](https://openairdocs.org/sdr/A6WA2018110546131.md): Support Bracket · cracked · Nov 3, 2018 · N454AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > OTBD FWD AND INDB AFT SCREW HOLES FOR EXTERNAL RECEPTACLE CRACKED. REMOVED AND REPLACED THE EXTERNAL POWER RECEPTACLE SUPPORT BRACKET IAW SRM 51-42-21, AND SRM 51-42-06
- [SDR A6WA2018110546135](https://openairdocs.org/sdr/A6WA2018110546135.md): Bracket · corroded · Nov 1, 2018 · N454AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR AFT BRACKET CORRODED. REPLACED THE PAX DOOR BRACKET IAW SRM 51-42-13, AND 51-42-06.
- [SDR A6WA2018110546130](https://openairdocs.org/sdr/A6WA2018110546130.md): Bracket · cracked · Oct 30, 2018 · N454AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LEFT TRANSDUCER BRACKET WAS CRACKED. REPLACED THE BRACKET.
- [SDR A6WA2018103146129](https://openairdocs.org/sdr/A6WA2018103146129.md): Seal Depressor · bent · Oct 30, 2018 · N454AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT UPPER SEAL DEPRESSOR BENT. REPAIRED.
- [SDR A6WA2018102946128](https://openairdocs.org/sdr/A6WA2018102946128.md): Seat Track · corroded · Oct 27, 2018 · N454AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SEAT TRACK NR 1 WAS CORRODED. REPLACED THE SEAT TRACK IAW AMM 53-01-11.
- [SDR A6WA2018102946126](https://openairdocs.org/sdr/A6WA2018102946126.md): Bracket · cracked · Oct 25, 2018 · N454AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RT TRANSDUCER BRACKET CRACKED. REPLACED RT TRANSDUCER BRACKET IAW SRM 51-41-02, 51-42-06.
- [SDR A6WA2018102946127](https://openairdocs.org/sdr/A6WA2018102946127.md): Angle · cracked · Oct 25, 2018 · N454AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > Z ANGLE FWD OF RT TRANSDUCER BRACKET IS CRACKED. REPLACED Z ANGLE IAW SRM 51-41-02, 51-42-06.
- [SDR A6WA2018061845881](https://openairdocs.org/sdr/A6WA2018061845881.md): Bpsu · malfunctioned · Jun 11, 2018 · N454AW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAP FAIL CAUTION WHEN MOVING FLAPS 8-20. FLAPS STUCK IN 8 DEG POSITION. R&R LT BPSU IAW AMM 27-51-10 RIG AND FUNCTION CHECK GOOD IAW AMM 27-54-00 OPS CHECK GOOD.
- [SDR A6WA201745483](https://openairdocs.org/sdr/A6WA201745483.md): Wire · broken · Dec 14, 2017 · N454AW · Cndair CL6002B19 · Light System Wiring
  > 4214 EMERGENCY FLOOR LIGHTS ROW 9-12 INOP. WHEN TURNED ON REMOVED AND REPLACED BROKEN HARNESS AND ROW 12 IAW AWAC SUPP 16-371A, ALSO INSTALLED NEW QUICK DISCONNECTOR TO AIRCRAFT WIRING IAW ESPM, OPS CHECK GOOD,
- [SDR A6WA201644399](https://openairdocs.org/sdr/A6WA201644399.md): Fitting · corroded · Oct 4, 2016 · N454AW · Cndair CL6002B19 · Landing Gear Doors
  > UPON REMOVAL OF THE NLG SPADE DOOR FOUND EVIDENCE OF CORROSION UNDER THE LH HINGE FITTING
- [SDR A6WA201644398](https://openairdocs.org/sdr/A6WA201644398.md): Frame · cracked · Oct 4, 2016 · N454AW · Cndair CL6002B19 · Fuselage Floor Panel
  > FRAME BS 333 IS CRACKED BETWEEN STRINGERS 1 AND 2L.
- [SDR A6WA201644397](https://openairdocs.org/sdr/A6WA201644397.md): Floor Support · corroded · Oct 3, 2016 · N454AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT IS CORRODED AT FASTENER HOLES LBL 28 BS 559+80 - 621.
- [SDR A6WA201644396](https://openairdocs.org/sdr/A6WA201644396.md): Cargo Track · corroded · Oct 3, 2016 · N454AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > THE CARGOTRACK WAS CORRODED AT BS 621-559+112 LBL 9 IN AFT CARGO
- [SDR A6WA201644393](https://openairdocs.org/sdr/A6WA201644393.md): Frame · corroded · Oct 1, 2016 · N454AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME FS333 HAS CORROSION ON AFT SIDE BETWEEN STR 26L AND 24R.
- [SDR A6WA201644391](https://openairdocs.org/sdr/A6WA201644391.md): Intercostal · corroded · Oct 1, 2016 · N454AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL THAT SITS ON TOP OF STR 25R HAS CORROSION ON BOTH SIDES BETWEEN FRAMES 349 AND 333.
- [SDR A6WA201644392](https://openairdocs.org/sdr/A6WA201644392.md): Frame · corroded · Oct 1, 2016 · N454AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 333 HAS CORROSION ON THE FWD SIDE BETWEEN STR 23R AND 22R.
- [SDR A6WA201644390](https://openairdocs.org/sdr/A6WA201644390.md): Attach Angle · cracked · Sep 30, 2016 · N454AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RT WING TO FUSELAGE PNL ATTACH STRUCTURE FS 469.65 IS CRACKED.
- [SDR A6WA201644387](https://openairdocs.org/sdr/A6WA201644387.md): Attach Fitting · corroded · Sep 30, 2016 · N454AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL ANGLE ATTACH FITTING AT FS 319.70 HAS CORROSION.

Next page: https://openairdocs.org/aircraft/N454AW/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 = 'N454AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N454AW/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.