# Service difficulty reports: N403AW, cancelled Mar 28, 2017

A list on [N403AW, cancelled Mar 28, 2017](https://openairdocs.org/deregistered/N403AW-2017-03-28.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 · 153 reports

- [SDR A6WA201643700](https://openairdocs.org/sdr/A6WA201643700.md): Coalescer Bag · odor · Mar 15, 2016 · N403AW · Cndair CL6002B19 · Humidity Control System
  > LEFT PACK SMELLS LIKE BURNT OIL. PLACARDED & PLACED ON MEL. R & R LT COALESCER IAW SUP 14-192. NO ODOR NOTED AT THIS TIME. REMOVED PLACARD & FROM MEL.
- [SDR A6WA201643548](https://openairdocs.org/sdr/A6WA201643548.md): Handle · lack of lube · Feb 7, 2016 · N403AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR WON'T OPEN FROM OUTSIDE. LUBED PAX DOOR HANDLE IAW AMM 12-12-00. OPERATIONS CHECKED GOOD AT THIS TIME.
- [SDR A6WA201643533](https://openairdocs.org/sdr/A6WA201643533.md): Shutoff Valve · malfunctioned · Feb 3, 2016 · N403AW · Cndair CL6002B19 · Fuel Transfer Valve
  > ON CLIMB OUT FUEL AT 13,000 LBS, RECEIVED RT AUTO CROSS FLOW WHITE STATUS. SYNOPTIC SHOWED RT CROSS FLOW EJECTOR CLOSED. FUEL CONTINUED TO FEED LT TANK. SELECTED GRAVITY CROSS FLOW TO RT TANK AT WHICH TIME WE RECEIVED FUEL IMBALANCE CAUTION MSG 800 - 950.
- [SDR A6WA201543315](https://openairdocs.org/sdr/A6WA201543315.md): Landing Gear · malfunctioned · Dec 1, 2015 · N403AW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, WHEN GEAR WAS RETRACTED, NOSE GEAR FAILED TO RETRACT. GEAR DISAGREE WARNING & NOSE DOOR WARNING. WOW INPUT CAUTION MSGS'S DISPLAYED. COMPLIED WITH QRH, MANUALLY DEPLOYED GEAR, LANDED NORMALLY, WEIGHT 43,000 LBS.
- [SDR A6WA201543311](https://openairdocs.org/sdr/A6WA201543311.md): Warning System · activated · Nov 30, 2015 · N403AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > AFTER TAKEOFF RECEIVED GEAR DISAGREE WARNING. NOSE GEAR NEVER SHOWED UP, CREW SELECTED GEAR DOWN & DIVERTED.
- [SDR A6WA201543087](https://openairdocs.org/sdr/A6WA201543087.md): Psu · unsecure · Sep 28, 2015 · N403AW · Cndair CL6002B19 · Passenger Compartment Equipment
  > DURING TAKEOFF PSU 1DF FELL DOWN. O2 GENERATORS DID NOT ACTIVATE. ACFT RETURNED TO FIELD.
- [SDR A6WA201542747](https://openairdocs.org/sdr/A6WA201542747.md): Pivot Assy · binding · May 15, 2015 · N403AW · Cndair CL6002B19 · Passenger/Crew Doors
  > RECEIVED PAX DOOR OUTER HANDLE CAUTION. WHILE PERFORMING QRH, PAX DOOR WARNING MSG APPEARED FOR APPROX 3 MINUTES. WARNING MSG CLEARED WITH NO CREW ACTION. EMERGENCY DECLARED & FLIGHT RETURNED. ON LANDING, OUTER HANDLE WAS FOUND OUT. COMPLIED WITH OPS C
- [SDR A6WA201542350](https://openairdocs.org/sdr/A6WA201542350.md): Fuel Control · failed · Jan 24, 2015 · N403AW · Cndair CL6002B19 · Fuel Control/Turbine Engines
  > DURING CLIMB OUT, FELT AN AIRFRAME VIBRATION. LT N1, N2, ITT & FUEL FLOW ERRATIC. LT VIBRATION 0.5. LT ENGINE PARAMETERS FLUCTUATED +/- 2% & FF 300LBS. DECLARED AN EMERGENCY & RETURNED. R & R LT FUEL CONTROL ASSEMBLY IAW AMM 73-21-00. PERFORMED OPS, LEAK,
- [SDR A6WA201542338](https://openairdocs.org/sdr/A6WA201542338.md): Smoke Detector · false activation · Jan 20, 2015 · N403AW · Cndair CL6002B19 · Smoke Detection
  > RECEIVED SMOKE IN TOILET CAUTION AFTER TAKEOFF. DECLARED EMER & COMPLIED WITH QRH. PULLED CB P2, C5, D14, D15, S2 & U2. RETURNED & DID NOT LAND OVERWEIGHT. INSPECTED LAVATORY, NO DEFECTS NOTED. NO SIGNS OF SMOKE OR FIRE FOUND. R & R LAVATORY SMOKE DETECT
- [SDR A6WA201442274](https://openairdocs.org/sdr/A6WA201442274.md): Light · damaged · Dec 23, 2014 · N403AW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS FROM ROWS 8-13 INOPERATIVE & ROW 12 - 13 FLOOR LIGHT SECTION MISSING CONNECTOR.
- [SDR A6WA201442257](https://openairdocs.org/sdr/A6WA201442257.md): Light · inoperative · Dec 18, 2014 · N403AW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTING FROM ROW 8 - 12 FOUND INOPERATIVE.
- [SDR A6WA201442157](https://openairdocs.org/sdr/A6WA201442157.md): Light · inoperative · Nov 13, 2014 · N403AW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE ROWS 9 & 10.
- [SDR A6WA201441504](https://openairdocs.org/sdr/A6WA201441504.md): Floor Skin · cracked · May 6, 2014 · N403AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FORWARD EQUIPMENT BAY FLOOR SKIN CRACKED ON LT SIDE OTBD OF GAUGES. REPAIRED IAW REO 601R-53-11-081 REV NC.
- [SDR A6WA201441500](https://openairdocs.org/sdr/A6WA201441500.md): Rib · cracked · May 2, 2014 · N403AW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > LEFT MLG WW BATTERY RIB CRACKED AFT RADIUS. R & R EXISTING REPAIR DOUBLER IAW REO 601R-57-51-046 REV B DATED 2002-02-28.
- [SDR A6WA201441497](https://openairdocs.org/sdr/A6WA201441497.md): Drag Angle · cracked · May 2, 2014 · N403AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR STAIR AFT DRAG ANGLE IS CRACKED AT PULLEY BRACKET. R & R EXISTING REPAIR ANGLE FROM PN 601R31907-301 IAW REO 601R-52-11-513 REV A DATED 09 MAR 05.
- [SDR A6WA201441499](https://openairdocs.org/sdr/A6WA201441499.md): Mount Bracket · corroded · May 1, 2014 · N403AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD FWD SIDE CRACKED ISOLATOR MOUNT BRACKET. R & R WITH SERVICEABLE PN 601R45156-75 IAW SRM 51-40-11 & 51-42-06.
- [SDR A6WA201441492](https://openairdocs.org/sdr/A6WA201441492.md): Angle · cracked · Apr 29, 2014 · N403AW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > UPPER ANGLE BEHIND RT WING LE TRANSITION PANEL 620ML IS CRACKED ON OTBD CORNER. R & R WITH SERVICEABLE PART IAW SRM 51-40-11, 51-24-16 & 51-42-13.
- [SDR A6WA201441479](https://openairdocs.org/sdr/A6WA201441479.md): Drag Angle · cracked · Apr 29, 2014 · N403AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT MLG WW DRAG ANGLE CRACKED. R & R ANGLE PN 600-10389-1 IAW SRM 51-40-11 & 51-42-21.
- [SDR A6WA201441502](https://openairdocs.org/sdr/A6WA201441502.md): Retainer · cracked · Apr 27, 2014 · N403AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > SEAL RETAINER CRACKED ON PANEL 412AT. R & R WITH SERVICEABLE PN 601-37003-39 IAW SRM 51-40-11 & 51-42-06.
- [SDR A6WA201441503](https://openairdocs.org/sdr/A6WA201441503.md): Skin · cracked · Apr 26, 2014 · N403AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > NLG CUT OUT LT & RT AFT RADIUS CRACKS AT FS 235. REPAIRED NLG CUT OUT AFT RADIUS SURROUND SKIN ON LT & RT SIDES IAW REO 601R-53-121-048 REV C DATED 2008-10-01.
- [SDR A6WA201441491](https://openairdocs.org/sdr/A6WA201441491.md): Fitting · corroded · Apr 25, 2014 · N403AW · Cndair CL6002B19 · Passenger Compartment Equipment
  > WARDROBE AFT FEET CORRODED. R & R AFT WARDROBE FEET WITH SERVICEABLE PARTS IAW SRM 51-40-11 & 51-41-02.
- [SDR A6WA201441490](https://openairdocs.org/sdr/A6WA201441490.md): Fitting · corroded · Apr 25, 2014 · N403AW · Cndair CL6002B19 · Buffet/Galleys
  > GALLEY INBD AFT FOOT CORRODED. R & R INBD AFT GALLEY FOOT WITH SERVICEABLE PART IAW SRM 51-40-11 & 51-41-02.
- [SDR A6WA201441480](https://openairdocs.org/sdr/A6WA201441480.md): Mount Fitting · cracked · Apr 24, 2014 · N403AW · Cndair CL6002B19 · Wing, Attach Fittings
  > PRESS REFUEL PORT MOUNT ANGLE IS CRACKED. R & R MOUNT ANGLE PN 600-62441-13 IAW SRM 51-40-11 & 51-42-06.
- [SDR A6WA201441478](https://openairdocs.org/sdr/A6WA201441478.md): Angle · cracked · Apr 24, 2014 · N403AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT OBLIQUE ANGLE CRACKED AT FS 621 - 625 NEAR STRINGER 13L. R & R WITH SERVICEABLE ANGLE IAW REO 601R-53-61-100 REV A DATED 2008-01-23 & SRM 51-40-11 & 51-42-21.
- [SDR A6WA201441506](https://openairdocs.org/sdr/A6WA201441506.md): Doubler · corroded · Apr 23, 2014 · N403AW · Cndair CL6002B19 · Passenger Compartment Equipment
  > LEFT WINDSCREEN KICK PLATE DOUBLERS CORRODED, FWD & AFT. R & R WITH SERVICEABLE DOUBLERS IAW CMM 25-22-89.
- [SDR A6WA201441477](https://openairdocs.org/sdr/A6WA201441477.md): Post · cracked · Apr 23, 2014 · N403AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 18 OTBD VERTICAL POST AT FS 409+128 IS CRACKED AT BOTTOM. REPAIRED IAW REO 601R-53-41-056 REV F DATED 2011-09-02.
- [SDR A6WA201441458](https://openairdocs.org/sdr/A6WA201441458.md): Fitting · cracked · Apr 23, 2014 · N403AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INBD & OTBD CLIPS ARE CRACKED AT LBL 9 FS 280. R & R INBD & OTBD CLIPS AT FS 280, LBL 9.
- [SDR A6WA201441457](https://openairdocs.org/sdr/A6WA201441457.md): Fitting · cracked · Apr 23, 2014 · N403AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INBD CLIP CRACKED AT FS 280 RBL 9. R & R CRACKED CLIP AT FS 280 RBL 9 IAW REO 601R-53-11-171 REV D.
- [SDR A6WA201441505](https://openairdocs.org/sdr/A6WA201441505.md): Mount Bracket · corroded · Apr 22, 2014 · N403AW · Cndair CL6002B19 · Passenger Compartment Equipment
  > LEFT & RIGHT WINDSCREEN CORROSION ON MOUNT FEET. R & R FEET ON LT & RT WINDSCREENS IAW CMM 25-22-89.
- [SDR A6WA201441498](https://openairdocs.org/sdr/A6WA201441498.md): Angle · corroded · Apr 22, 2014 · N403AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL FLOOR SUPPORT LOWER ANGLE CORRODED. R & R ANGLE WITH SERVICEABLE PART IAW SRM 51-40-11, 51-42-13 & 51-42-21.
- [SDR A6WA201441481](https://openairdocs.org/sdr/A6WA201441481.md): Angle · corroded · Apr 21, 2014 · N403AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CROSSBEAM AT FS 349 HAS CORROSION FROM RBL 36 TO RBL 45. CLEANED CORROSION & REPLACED AFT FLOOR SUPPORT ANGLE ON FS 349 CROSSBEAM RT SIDE IAW SRM 51-40-11 & 51-40-06.
- [SDR A6WA201441463](https://openairdocs.org/sdr/A6WA201441463.md): Fitting · corroded · Apr 21, 2014 · N403AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR SILL FWD & AFT CLEAT FITTINGS, FS 316 & 343 CORRODED. R & R WITH SERVICEABLE PARTS PN 601R31527-217 IAW SRM 51-40-11 & 51-42-06.
- [SDR A6WA201441462](https://openairdocs.org/sdr/A6WA201441462.md): Sill · corroded · Apr 21, 2014 · N403AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SILL FROM FS 349 TO 356 CORRODED. REPAIRED IAW EA 15-2014-094 DATED 4-24-2014 & REO 601R-53-00-530 DATED 06-JUN-2013.
- [SDR A6WA201441514](https://openairdocs.org/sdr/A6WA201441514.md): Floorbeam · corroded · Apr 19, 2014 · N403AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LBL 27 FLOORBEAM CAP CORRODED AROUND NUTPLATE LOCATIONS BETWEEN FS 561 & 564. REPAIRED FLOORBEAM CAP LBL 27 AT FS 561 - 564 IAW SRM 53-00-43 REPAIR NR 2 FLOORBEAM SPLICE REPAIR.
- [SDR A6WA201441459](https://openairdocs.org/sdr/A6WA201441459.md): Cowling · cracked · Apr 19, 2014 · N403AW · Cndair CL6002B19 · Engine Cowling System
  > LEFT ENG LOWER CORE COWL FWD CORNER CRACKED. REPAIRED LT ENG LOWER CORE COWL FWD CORNER IAW CMM TASK 71-12-01-300-826-A01.
- [SDR A6WA201308194201](https://openairdocs.org/sdr/A6WA201308194201.md): Packing · leaking · Aug 16, 2013 · N403AW · Cndair CL6002B19 · Hydraulic System, Main
  > ON FINAL, RECEIVED HYD 2 LOW PRESS CAUTION HYD 2 QTY READS 5 PERCENT. MESSAGE APPEARED APROX 30 SECONDS AFTER GEAR SELECTD DOWN, COMPLIED WITH QRH TURNED ACMP2 OFF, EDP 2 WAS RUNNING FOR APROX 20 MIN WITH LOW PRESSURE MESSAGE (INCLUDING TAXI TIME). REPLACED
- [SDR A6WA201240595](https://openairdocs.org/sdr/A6WA201240595.md): Computer · failed · Jun 21, 2012 · N403AW · Cndair CL6002B19 · Flight Management Computing Hardware System
  > ON TAKEOFF ROLL, F/O RECEIVED RED FLT DIRECTOR FLAG ON PFD AND AIRSPEED INDICATION WAS ERRATIC. ABORTED TAKEOFF AT 117 KNOTS, BTMS 7786, TROUBLESHOT SYS AND FOUND FCC 2 FAILING. REPLACED FCC2 IAW AMM 22-12-04. PERFORMED OPS CHECKS. NO DEFECTS AT THIS TIME.
- [SDR AA6WA201240595](https://openairdocs.org/sdr/AA6WA201240595.md): Computer · failed · Jun 21, 2012 · N403AW · Cndair CL6002B19 · Flight Management Computing Hardware System
  > ON TAKEOFF ROLL, F/O RECEIVED RED FLT DIRECTOR FLAG ON PFD AND AIRSPEED INDICATION WAS ERRATIC. ABORTED TAKEOFF AT 117 KNOTS, BTMS 7786. TROUBLESHOT SYSTEM AND FOUND FCC2 FAILING. REPLACED FCC 2 IAW AMM 22-12-04. PERFORMED OPS CHECKS. NO DEFECTS AT THIS T
- [SDR A6WA201240572](https://openairdocs.org/sdr/A6WA201240572.md): Angle · cracked · May 29, 2012 · N403AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL 9 OTBD CLIP AT FS 280.00 CRACKED. REMOVED UNSERVICEABLE CLIP ON RBL 9 AT FS 280.00 IAW SRM 51-42-21 AND REPLACED WITH SERVICEABLE CLIP IAW REO 601R-53-11-171, REV D.
- [SDR A6WA201240578](https://openairdocs.org/sdr/A6WA201240578.md): Floor Support · corroded · May 12, 2012 · N403AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 9 FLOOR SUPPORT CAP FS 529-610 HAS CORROSION ON OTBD SIDE. REPAIR BY SPLICING IN NEW MEMBER IAW SRM 53-00-43.
- [SDR A6WA201240564](https://openairdocs.org/sdr/A6WA201240564.md): Skin · chafed · May 12, 2012 · N403AW · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK CHAFED FROM FAIRING AT WS 45 WING REAR FACE RT SIDE BLENDED AREA AT WS 45 MEASURED DEPTH.045 WITHIN LIMITS IAW REO 601R-57-21-1673.
- [SDR A6WA201240561](https://openairdocs.org/sdr/A6WA201240561.md): Attach Bracket · cracked · May 12, 2012 · N403AW · Cndair CL6002B19 · Wing, Attach Fittings
  > RT WING INBD L/E OTBD ATTACH BRACKET CRACKED. REMOVED UNSERVICEABLE BRACKET AND INSTALLED SERVICEABLE BRACKET IAW SRM 51-41-02/ 51-40-11.
- [SDR A6WA201240559](https://openairdocs.org/sdr/A6WA201240559.md): Pulley Bracket · chafed · May 11, 2012 · N403AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR MOTOR PULLEY BRACKET CHAFED AREA ON PAX DOOR MOTOR PULLEY BRACKET. BLENDED CHAFE ON PAX DOOR MOTOR PULLEY BRACKET WITHIN LIMITS ORIG.165. REMOVED.015 REMAINING.090 NDT, ALODINED, PRIMED AND TOP COATED IAW REO 601R-52-11-2077.
- [SDR A6WA201240562](https://openairdocs.org/sdr/A6WA201240562.md): Cover · chafed · May 11, 2012 · N403AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT MLG BATTERY RIB COVER CHAFED FROM LT MLG HARNESS. BLENDED CHAFED AREA ON TL MLG BATTERY RIB COVER ORIG THICKNESS.080, REMOVED.023 REMAINING.057 IAW SRM 51-12-00 USING THICKNESS GAUGE. ALODINED, PRIMED AND TOP COATED IAW SRM 51-21-11, 51-25-06, 51-25-16
- [SDR A6WA201240548](https://openairdocs.org/sdr/A6WA201240548.md): Panel · cracked · May 10, 2012 · N403AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/Skin
  > PANEL 412AT CRACKED. REMOVED UNSERVICEABLE RETAINER & SEAL. REPLACED WITH SERVICEABLE RETAINER AND SEAL IAW SRM 51-40-11, 51-42-06, AMM 54-63-01.
- [SDR A6WA201240569](https://openairdocs.org/sdr/A6WA201240569.md): Housing · cracked · May 10, 2012 · N403AW · Cndair CL6002B19 · Cargo/Baggage Doors
  > FOUND CARGO BAY DOOR HANDLE HOUSING CRACKED ABOVE CENTER OF HANDLE. REMOVED UNSERVICEABLE CARGO DOOR HANDLE AND REPLACED WITH SERVICEABLE HANDLE IAW AMM CMM 52-31-03 AND SRM 51-40-03, AND SRM 51-40-11, 51-42-06.
- [SDR A6WA201240568](https://openairdocs.org/sdr/A6WA201240568.md): Bulkhead · gouged · May 9, 2012 · N403AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > RT AFT SIDE OF 280 BULKHEAD HAS 2 GOUGES ON THE INBD SIDE FROM MAKING CONTACT WITH GALLEY STORAGE COMPARTMENT DOOR.
- [SDR A6WA201240566](https://openairdocs.org/sdr/A6WA201240566.md): Cargo Track · corroded · May 8, 2012 · N403AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON CARGO TRACK. R & R CARGO TRACK WITH SERVICEABLE IAW 51-40-11, SRM 51-21-11, AMM 53-01-11.
- [SDR A6WA201240567](https://openairdocs.org/sdr/A6WA201240567.md): Floor Support · corroded · May 7, 2012 · N403AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT SIDE FLOOR SILL CORRODED AROUND NUTPLATES FS 559+112, FS 621. REMOVED AND INSTALLED NEW SERVICEABLE FLOOR SILL AT FS 559+112 TO FS 621 IAW REO 601R-53-61-4497.
- [SDR A6WA201240563](https://openairdocs.org/sdr/A6WA201240563.md): Panel · chafed · May 5, 2012 · N403AW · Cndair CL6002B19 · Wing, Plate/Skin
  > PANEL 684BB & 684AB IS CHAFED. BLENDED PANEL 684BB MAT LOSS.003. REMAINING MAT.077 WITHIN LIMITS IAW SRM 57-52-00. BLENDED PANEL 684AB MAT LOSS.017 REMAINING MAT.063 WITHIN LIMITS IAW REO 601R-57-52-1910.

Next page: https://openairdocs.org/deregistered/N403AW-2017-03-28/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 = 'N403AW' AND deregistration_id = 'N403AW-2017-03-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N403AW-2017-03-28/reports

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