# Service difficulty reports: N406AW, cancelled Jun 25, 2019

A list on [N406AW, cancelled Jun 25, 2019](https://openairdocs.org/deregistered/N406AW-2019-06-25.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 · 161 reports

- [SDR A6WA201543414](https://openairdocs.org/sdr/A6WA201543414.md): Wire Harness · defective · Dec 28, 2015 · N406AW · Cndair CL6002B19 · Landing Gear System Wiring
  > STEERING INOPERATIVE CAUTION IN FLIGHT. COMPLIED WITH QRH, MSG PERSISTED. R & R NLG HARNESS & LT ROTARY VOLTAGE DIFFERENTIAL TRANSDUCER. OPERATIONS CHECKED GOOD.
- [SDR A6WA201543368](https://openairdocs.org/sdr/A6WA201543368.md): Warning System · activated · Dec 16, 2015 · N406AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > RECEIVED GEAR DISAGREE WARNING ALONG WITH WOW INPUT CAUTION ON CLIMB OUT. TRIED TO RECYCLE GEAR WITH NO CHANGE. LEFT THE GEAR IN DOWN POSITION. GEAR SHOWED DOWN & 3 GREEN. RAN QRH FOR GEAR DISAGREE WARNING. PERFORMED MANUAL EXTENSION AS PRECAUTION & LANDE
- [SDR A6WA201543149](https://openairdocs.org/sdr/A6WA201543149.md): Handle · lack of lube · Oct 19, 2015 · N406AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR WILL NOT OPEN FROM OUTSIDE. INSPECTED PAX DOOR OUTER HANDLE & CLEARANCES IAW AMM 52-11-03, NO VISUAL DEFECTS NOTED. DOOR WILL NOT OPEN FROM OUTSIDE. HANDLE EXTENDS, BUT WILL NOT ROTATE. LUBED PAX DOOR HANDLE, PIN & BELL CRANK ASSEMBLIES IAW A
- [SDR A6WA201543048](https://openairdocs.org/sdr/A6WA201543048.md): Light · inoperative · Sep 10, 2015 · N406AW · Cndair CL6002B19 · Emergency Lighting
  > FORWARD FACING EMER EXIT SIGN AT ROW 8, LIGHTS BURNED OUT.
- [SDR A6WA201543042](https://openairdocs.org/sdr/A6WA201543042.md): Apu · unknown · Sep 7, 2015 · N406AW · Cndair CL6002B19 · APU Core Engine
  > FLIGHT 3945, APU WILL NOT START IN THE AIR. HEAVY FUEL ODOR OCCURS AFTER START ON THE GND WITH BOTH PACKS ON. COMPLIED WITH CM ACTION PLACARDED & PLACED ON MEL.
- [SDR A6WA201542620](https://openairdocs.org/sdr/A6WA201542620.md): Seal · failed · Apr 11, 2015 · N406AW · Cndair CL6002B19 · Service Doors
  > AT 30,000 FT RECEIVED LOUD NOISE COMING FROM SERVICE DOOR. PRESSURIZATION WAS NORMAL, NO DOOR WARNING INDICATIONS. NOISE COMES FROM LOWER RT SIDE. FLIGHT ATTENDANT REPORTS VIBRATION & FELT LIKE AIR WAS COMING FROM DOOR. DECLARED AN EMER & DIVERTED. R & R
- [SDR A6WA201341324](https://openairdocs.org/sdr/A6WA201341324.md): Unknown · odor · Feb 8, 2015 · N406AW · Cndair CL6002B19 · Air Distribution System
  > WITH PACKS ON THERE IS A STRONG FUEL SMELL IN THE AIRPLANE WITH APU ON.
- [SDR A6WA201442091](https://openairdocs.org/sdr/A6WA201442091.md): Light · inoperative · Oct 27, 2014 · N406AW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY FLOOR TRACK LIGHTS ROW 8 - 12 INOPERATIVE.
- [SDR A6WA201442048](https://openairdocs.org/sdr/A6WA201442048.md): Warning System · activated · Oct 12, 2014 · N406AW · Cndair CL6002B19 · Central Computers
  > DESCENDING THROUGH 20,000' ALL CRTS EXCEPT ED1 & 2 WENT BLANK. FMS WENT BLANK. FMS, FD MAP CAUTION, FMS NOT AVAILABLE. G/S WARNING APPEARED. THROUGH 10,000' APU BATTERY CHARGER STATUS MSG APPEARED.
- [SDR A6WA201441978](https://openairdocs.org/sdr/A6WA201441978.md): Light · inoperative · Sep 17, 2014 · N406AW · Cndair CL6002B19 · Emergency Lighting
  > FLOOR TRACK EMER LIGHTS 2 - 5 WILL NOT ILLUMINATE.
- [SDR A6WA201441902](https://openairdocs.org/sdr/A6WA201441902.md): Trim System · out of adjust · Aug 27, 2014 · N406AW · Cndair CL6002B19 · Rudder Tab Control System
  > ON DEPARTURE LEVELING OFF AT 8,000 FT UNCOMMANDED FULL RT RUDDER TRIM. AUTO PILOT HAD BEEN ENGAGED FOR 2 MINUTES. COMPLIED WITH QRH DISCONNECTED AUTO PILOT & YAW DAMP. DISCOVERED RUDDER TRIM WAS AT FULL RT WITH NO INPUT FROM THE KNOB. KNOB WAS CENTERED. A
- [SDR A6WA201441592](https://openairdocs.org/sdr/A6WA201441592.md): Mount Bracket · cracked · May 26, 2014 · N406AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FWD LT NOSE HYD COMPARTMENT BRAKE ACCUMULATOR FWD OTBD MOUNT BRACKET CRACKED. R & R WITH SERVICEABLE PART, PN 601R75250-55 IAW SRM 51-40-11 & 51-42-21.
- [SDR A6WA201441590](https://openairdocs.org/sdr/A6WA201441590.md): Floor Support · corroded · May 25, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 27 FLOORBEAM CAP CORRODED AROUND NUTPLATE HOLES, FS 574 TO 621. R & R FLOORBEAM CAP WITH SERVICEABLE SECTION IAW SRM 51-40-11 & 51-42-21.
- [SDR A6WA201441571](https://openairdocs.org/sdr/A6WA201441571.md): Door Sill · corroded · May 23, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR LWR SILL IS CORRODED BETWEEN FS 315 TO FS 344. R & R WITH NEW SERVICEABLE SILL ANGLE IAW SRM 51-41-02, 51-42-06 & 51-42-13.
- [SDR A6WA201441572](https://openairdocs.org/sdr/A6WA201441572.md): Skin · chafed · May 23, 2014 · N406AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE LE SKIN IS CHAFED AT 3 LOCATIONS. REMOVED & REPLACED INBD & CTR FLAP VANE LE SKIN IAW SRM 51-42-13 & 51-40-11.
- [SDR A6WA201441573](https://openairdocs.org/sdr/A6WA201441573.md): Door Frame · cracked · May 22, 2014 · N406AW · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR AFT FRAME AT FS 338 IS CRACKED UNDER PREVIOUS REPAIR. REMOVED CRACKED FRAME & REPLACED WITH NEW SERVICEABLE FRAME IAW REO 601R-52-11-402 REV H.
- [SDR A6WA201441588](https://openairdocs.org/sdr/A6WA201441588.md): Mount Bracket · cracked · May 20, 2014 · N406AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > EXTERNAL SERVICES PANEL ASSEMBLY UPPER MOUNT BRACKET CRACKED. R & R EXTERNAL SERVICES PANEL UPPER MOUNT BRACKET WITH SERVICEABLE PART, PN 601R51590-13 IAW SRM 51-40-11 & 51-42-06.
- [SDR A6WA201441560](https://openairdocs.org/sdr/A6WA201441560.md): Fitting · corroded · May 18, 2014 · N406AW · Cndair CL6002B19 · Passenger Compartment Equipment
  > RIGHT WINDSCREEN LWR FITTINGS HAVE CORROSION ON LWR SIDE. R & R UNSERVICEABLE FITTINGS & INSTALLED NEW SERVICEABLE FITTINGS IAW SRM 51-41-02.
- [SDR A6WA201441587](https://openairdocs.org/sdr/A6WA201441587.md): Skin · damaged · May 17, 2014 · N406AW · Cndair CL6002B19 · Elevator, Plate/Skin
  > COMPLIED WITH CARD 4DMI16358 REPAIR LT ELEVATOR DAMAGE NR 12 & 13 601R-51-00-293. PERFORMED PERMANENT REPAIR IAW SRM 55-20-00 FIG 204.
- [SDR A6WA201441565](https://openairdocs.org/sdr/A6WA201441565.md): Cleat · corroded · May 17, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR LWR SILL FWD & AFT CLEATS ARE CORRODED. REMOVED FWD & AFT CLEATS ON LWR PAX DOOR SILL & INSTALLED NEW SERVICEABLE CLEATS IAW SRM 51-42-06.
- [SDR A6WA201441574](https://openairdocs.org/sdr/A6WA201441574.md): Skin · gouged · May 16, 2014 · N406AW · Cndair CL6002B19 · Wing, Plate/Skin
  > UPPER SURFACE OF LWR WING PLANK IS GOUGED AT WS 88.5. REPAIRED GOUGED UPPER SURFACE OF LWR WING PLANK IAW REO 601R--57-21-2192 DATED 5-21-14.
- [SDR A6WA201441589](https://openairdocs.org/sdr/A6WA201441589.md): Frame · corroded · May 16, 2014 · N406AW · Cndair CL6002B19 · Fuselage Main, Frame
  > LOWER SECTION OF FS 605 FRAME HAS CORROSION. REPAIRED FRAME FS 605 IAW EA 15-2014-122 REV C DATED 5/24/2014.
- [SDR A6WA201441561](https://openairdocs.org/sdr/A6WA201441561.md): Cleat · corroded · May 16, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR CUT OUT THRESHOLD CLEATS HAVE CORROSION ATTACHED FASTENERS. REMOVED CORRODED FASTENERS & INSTALLED NEW SERVICEABLE FASTENERS IAW AMM 20-24-00.
- [SDR A6WA201441558](https://openairdocs.org/sdr/A6WA201441558.md): Rib · cracked · May 16, 2014 · N406AW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > LEFT BATTERY RIB CRACKED ON FWD END. REMOVED CRACKED RIB & INSTALLED SERVICEABLE BATTERY RIB IAW REO 601R-57-51-046 REV B.
- [SDR A6WA201441591](https://openairdocs.org/sdr/A6WA201441591.md): Housing · chafed · May 15, 2014 · N406AW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR HANDLE HOUSING CHAFED. R & R HANDLE HOUSING WITH SERVICEABLE PART, PN 119935-1 IAW SRM 51-40-11 & 51-42-21.
- [SDR A6WA201441562](https://openairdocs.org/sdr/A6WA201441562.md): Fitting · cracked · May 15, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIPS AT FS 280 & STRINGER 3L CRACKED. REMOVED UNSERVICEABLE CLIP & INSTALLED SERVICEABLE CLIP IAW SRM 51-42-06, 51-41-02, 51-42-06 & 51-42-21.
- [SDR A6WA201441559](https://openairdocs.org/sdr/A6WA201441559.md): Fitting · cracked · May 15, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP AT FS 280 & STRINGER 3L CRACKED. REMOVED CRACKED CLIP & INSTALLED SERVICEABLE CLIP IAW SRM51-41-11 & 51-41-02.
- [SDR A6WA201441553](https://openairdocs.org/sdr/A6WA201441553.md): Angle · cracked · May 14, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT & RIGHT OBLIQUE ANGLES IN AEB ARE CRACKED. R & R CRACKED RT OBLIQUE ANGLE WITH NEW SERVICEABLE ANGLE IAW SRM 51-40-11 & 51-42-21. SEE W C 54596-3000-0004 FOR REMOVAL & REPLACEMENT OF LT OBLIQUE ANGLE.
- [SDR A6WA201441549](https://openairdocs.org/sdr/A6WA201441549.md): Drag Angle · cracked · May 14, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT DRAG ANGLE COMMON TO BATTERY RIB CRACKED AT AFT END. R & R CRACKED LT DRAG ANGLE WITH NEW SERVICEABLE DRAG ANGLE IAW SRM 51-42-21, 51-40-11 & 51-25-16.
- [SDR A6WA201441548](https://openairdocs.org/sdr/A6WA201441548.md): Drag Angle · cracked · May 14, 2014 · N406AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR DRAG ANGLE FWD OF POWER ASSIST PULLEY BRACKET IS CRACKED. REPAIRED PAX DOOR DRAG ANGLE IAW REO 601R-52-11-513 REV A.
- [SDR A6WA201441547](https://openairdocs.org/sdr/A6WA201441547.md): Skin · cracked · May 14, 2014 · N406AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERNAL LWR FUSELAGE SKIN AT AFT NLG CUT OUT ON BOTH LT & RT CORNERS ARE CRACKED. REPAIRED NLG WW CUT OUT IAW REO 601R-53-11-048 REV C 10-1-08.
- [SDR A6WA201441554](https://openairdocs.org/sdr/A6WA201441554.md): Attach Fitting · corroded · May 13, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR FWD SILL ATTACH AT FRAME IS CORRODED. R & R WITH NEW SERVICEABLE PART IAW SRM 51-42-21.
- [SDR A6WA201441552](https://openairdocs.org/sdr/A6WA201441552.md): Angle · cracked · May 13, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT LWR OBLIQUE ANGLE CRACKED ON AFT SIDE OF 621 BULKHEAD. R & R LWR OBLIQUE ANGLE WITH NEW SERVICEABLE ANGLE IAW SRM 51-42-21.
- [SDR A6WA201441551](https://openairdocs.org/sdr/A6WA201441551.md): Drag Angle · cracked · May 13, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT DRAG ANGLE COMMON TO BATTERY RIB IS CRACKED. R & R RT DRAG ANGLE IAW SRM 51-42-21.
- [SDR A6WA201441550](https://openairdocs.org/sdr/A6WA201441550.md): Mount Bracket · cracked · May 13, 2014 · N406AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > EXTERNAL SERVICE PANEL 122CR CUT OUT LWR MOUNT BRACKET FOR SERVICE BOX CRACKED. REMOVED CRACKED MOUNT BRACKET & INSTALLED NEW BRACKET IAW SRM 51-42-13 & 51-40-11.
- [SDR A6WA201441600](https://openairdocs.org/sdr/A6WA201441600.md): Post · cracked · May 11, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VERTICAL POST AT RBL 18 ON FS 409+128 BULKHEAD IS CRACKED AT LOWER END, OTBD AFT FLANGE. REPAIRED RBL 18 OTBD POST AT FS 409+128 IAW REO 601R-53-41-056 REV F DATED 2011/09/02.
- [SDR A6WA201441586](https://openairdocs.org/sdr/A6WA201441586.md): Skin · dented · May 11, 2014 · N406AW · Cndair CL6002B19 · Elevator, Plate/Skin
  > LEFT ELEVATOR HAS 4 DENTS ON LOWER SURFACE. REPAIRED 2 DENTS IAW SRM 55-20-00 FIG 204 & FOUND 2 DENTS TO BE IN LIMITS IAW SRM 55-20-00 FIG 101.
- [SDR A6WA201441543](https://openairdocs.org/sdr/A6WA201441543.md): Seat Track · corroded · May 11, 2014 · N406AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN NR 1 FLOOR SEAT TRACK CORRODED AT FWD END OF LBL 9 FS 364.00. REMOVED CORRODED SEAT TRACK & REPLACED WITH NEW SERVICEABLE SEAT TRACK IAW AMM 53-01-11.
- [SDR A6WA201441542](https://openairdocs.org/sdr/A6WA201441542.md): Seat Track · corroded · May 11, 2014 · N406AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN NR 1 FLOOR SEAT TRACK CORRODED AT FWD END RBL 9 AT FS 364.00. REMOVED CORRODED FLOOR SEAT TRACK & REPLACED WITH NEW SERVICEABLE FLOOR SEAT TRACK IAW SRM 53-01-11.
- [SDR A6WA201441544](https://openairdocs.org/sdr/A6WA201441544.md): Seat Track · corroded · May 10, 2014 · N406AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AFT OF 9G TIE DOWN AT FS 559+112 HAS CORROSION AROUND FASTENERS HOLES. REMOVED UNSERVICEABLE SEAT TRACK & INSTALLED A NEW SERVICEABLE TRACK IAW SRM 53-01-11.
- [SDR A6WA201441541](https://openairdocs.org/sdr/A6WA201441541.md): Angle · corroded · May 10, 2014 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280.00 FLOOR ANGLES CORRODED & RBL 9 OTBD CLIP CRACKED. REPAIRED FWD 7 AFT FLOOR ANGLES AT FS 280 RBL 9 - LBL9. R & R OTBD CLIP AT FS 280 & RBL 9 IAW SRM 51-21-06, 53-00-00 & REO 601R-53-11-171 REV D.
- [SDR A6WA201441113](https://openairdocs.org/sdr/A6WA201441113.md): Apu · shutdown · Feb 6, 2014 · N406AW · Cndair CL6002B19 · APU Core Engine
  > TURNED APU GENERATOR ON, APU AUTO SHUTDOWN. HEAVY SMELL OF JET FUEL & SMOKE FROM EXHAUST. ACTION TAKEN IN PROGRESS.
- [SDR A6WA201312104046](https://openairdocs.org/sdr/A6WA201312104046.md): Fuel Sys · leaking · Dec 8, 2013 · N406AW · Cndair CL6002B19 · APU Engine Fuel and Control
  > 3847 WITH PACKS ON THERE IS A STRONG FUEL SMELL IN THE AIRPLANE WITH APU ON. FOUND FUEL LEAK BY FUEL CONTROL. R, OPERATIONS & LEAK CHECKED GOOD AT THIS TIME NO FUEL SMELL NOTED IN CABIN.
- [SDR A6WA201303014018](https://openairdocs.org/sdr/A6WA201303014018.md): Warning System · activated · Mar 1, 2013 · N406AW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAPS FAIL CAUTION MSG DURING RETRACTION AFTER LANDING. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-18E BOX 12. FLAPS RESET. PLACARD AND PLACED ON MEL.
- [SDR A6WA201301234011](https://openairdocs.org/sdr/A6WA201301234011.md): Windshield · damaged · Jan 23, 2013 · N406AW · Cndair CL6002B19 · Flight Compartment Windows
  > IN FLIGHT SAW SPARKING AND MELTING ON LEFT WINDSHIELD. COMPLIED WITH QRH. TURNED WINDSHIELD HEAT OFF, SPARKS STOPPED. COORDINATED WITH DISPATCH AND ATC, RETURNED TO LAND AT DCA. LANDING WEIGHT 39,000. NO FURTHER INCIDENT. REPLACED LEFT WINDSHIELD.
- [SDR A6WA201240805](https://openairdocs.org/sdr/A6WA201240805.md): Bpsu · failed · Aug 15, 2012 · N406AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED WHEN SELECTED 20-30. FLAPS STAYED AT 20 DEGREES. REPLACED RT BPSU PER 27 51 OPS CK GOOD.
- [SDR A6WA201240772](https://openairdocs.org/sdr/A6WA201240772.md): Bpsu · failed · Aug 14, 2012 · N406AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED IN FLT AT 20 DEGREES WHEN 30 DEGREES WAS SELECTED. PERFORMED FLAP RESET PROCEDURE IAW SUPPLEMENT 98-18E BOX 12, FLAPS RESET. FOUND REPEAT BPSU FAULT CODES IN FECU, REPLACED LT BPSU IAW AMM 27-51. OPS CK GOOD.
- [SDR A6WA201240645](https://openairdocs.org/sdr/A6WA201240645.md): Warning Message · false activation · Jun 30, 2012 · N406AW · Cndair CL6002B19 · Fire Protection System
  > CARGO BOTTLE LOW CAUTION MESSAGE IN FLIGHT, NO INDICATION OF FIRE/SMOKE. INSPECTED CARGO BAY, NO EVIDENCE OF FIRE/SMOKE. NO BOTTLE DISCHARGE.
- [SDR A6WA201240535](https://openairdocs.org/sdr/A6WA201240535.md): Panel · cracked · May 11, 2012 · N406AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/Skin
  > RT ENGINE PYLON PANEL 422AB HAS CRACKED SEAL RETAINER. REMOVED UNSERVICEABLE RT ENG PYLON PANEL 422AB SEAL RETAINER AND INSTALLED SERVICEABLE SEAT RETAINER IAW SRM 51-42-06.
- [SDR A6WA201240534](https://openairdocs.org/sdr/A6WA201240534.md): Bracket · broken · May 4, 2012 · N406AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > T2 SENSE LINE BRACKET BROKEN, SUPPORT BRACKET FOR THE T2 SENSE LINE ON TOP OF THE ENGINE. REMOVED ENG INLET AND INSTALLED A NEW SERVICEABLE BRACKET.

Next page: https://openairdocs.org/deregistered/N406AW-2019-06-25/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 = 'N406AW' AND deregistration_id = 'N406AW-2019-06-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N406AW-2019-06-25/reports

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