# Service difficulty reports: N401AW, cancelled Mar 28, 2017

A list on [N401AW, cancelled Mar 28, 2017](https://openairdocs.org/deregistered/N401AW-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 · 175 reports

- [SDR A6WA201644339](https://openairdocs.org/sdr/A6WA201644339.md): Fitting · cracked · Sep 15, 2016 · N401AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BATH TUB FITTING AT FS 461 AND RBL 9 IS CRACKED, REPLACED.
- [SDR A6WA201643523](https://openairdocs.org/sdr/A6WA201643523.md): Flap · malfunctioned · Feb 1, 2016 · N401AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL CAUTION MSG WITH FLAPS AT 35 DEGREES ON APPROACH. COMPLIED WITH FIM RESET, RESET FAILED IAW SUPP 97-018G.
- [SDR A6WA201543133](https://openairdocs.org/sdr/A6WA201543133.md): Sign · missing · Oct 13, 2015 · N401AW · Cndair CL6002B19 · Emergency Lighting
  > PASSENGER DOOR EMER EXIT SIGN MISSING.
- [SDR A6WA201542936](https://openairdocs.org/sdr/A6WA201542936.md): Skin · chafed · Jul 17, 2015 · N401AW · Cndair CL6002B19 · Trailing Edge Flaps
  > THE RT INBD FLAP VANE LE CHAFED BEYOND LIMITS AT CTR STOP.
- [SDR A6WA201542934](https://openairdocs.org/sdr/A6WA201542934.md): Bushing · scored · Jul 17, 2015 · N401AW · Cndair CL6002B19 · Main Landing Gear Attach Section
  > RIGHT MLG FWD FACE OF MAIN FITTING BUSHING SCORED.
- [SDR A6WA201542652](https://openairdocs.org/sdr/A6WA201542652.md): Autopilot Sys · malfunctioned · Apr 20, 2015 · N401AW · Cndair CL6002B19 · Autopilot System
  > FLIGHT NUMBER 3753. AUTOPILOT ENGAGED RECEIVED A LT WING DOWN CAUTION, DISCONNECTED AUTOPILOT. AILERON CONTROL WAS HEAVY IN BOTH DIRECTIONS. COMPLIED WITH AUTO PILOT TRIM QRH & AILERON JAMBED QRH SUSPECTED ICE & FREED JAMB. INSPECTED TED VISIBLE CONTROL CA
- [SDR A6WA201442217](https://openairdocs.org/sdr/A6WA201442217.md): Warning System · activated · Dec 3, 2014 · N401AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > AFTER TAKEOFF, SELECTED GEAR UP RECEIVED GEAR DISAGREE WARNING MSG WITHIN 6 SECONDS. AFTER MSG PERSISTED FOR ONE MINUTE, BEGAN GEAR DISAGREE QRH.
- [SDR A6WA201441090](https://openairdocs.org/sdr/A6WA201441090.md): Housing · cracked · Jan 30, 2014 · N401AW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR HANDLE HOUSING CRACKED. R & R WITH SERVICEABLE HANDLE HOUSING IAW CRJ 200 SRM 51-40-11 & 51-42-21.
- [SDR A6WA201441083](https://openairdocs.org/sdr/A6WA201441083.md): Fitting · worn · Jan 30, 2014 · N401AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT WING TE, OTBD FLAP ALIGNMENT FITTING WORN BEYOND LIMITS. R & R FITTING PN 601R10156-4 IAW CRJ 200 SRM 51-40-11 & 51-42-06.
- [SDR A6WA201441087](https://openairdocs.org/sdr/A6WA201441087.md): Seal Depressor · corroded · Jan 29, 2014 · N401AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL AREA, FWD & AFT SPIGOT STOP BOLT FITTINGS & LOWER SILL AREA, SEAL DEPRESSOR CORRODED. R & R LOWER SILL SUPPORT ANGLE & DEPRESSOR WITH SERVICEABLE PARTS IAW CRJ 200 SRM 51-24-21,51-40-11, 51-42-06 & 51-42-21 & REO 601R-53-21-2502.
- [SDR A6WA201441085](https://openairdocs.org/sdr/A6WA201441085.md): Plate · cracked · Jan 29, 2014 · N401AW · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > LEFT EXHAUST FAIRING INBD NUTPLATE MOUNT PLATE CRACKED. R & R PN 228-50181-833 IAW CMM 20-42-06.
- [SDR A6WA201441084](https://openairdocs.org/sdr/A6WA201441084.md): Skin · dented · Jan 29, 2014 · N401AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > COMPLIED WITH JOB CARD 4DMI16050 PERFORM PERMANENT REPAIR OF FUSELAGE AT FS 265 IAW REO 601R-53-11-2301. COMPLIED WITH PERMANENT REPAIR OF FUSELAGE SKIN AT FS 265 & STRINGER 25R-26R IAW REO 601R-53-11-2615 REV.
- [SDR A6WA201441091](https://openairdocs.org/sdr/A6WA201441091.md): Bracket · corroded · Jan 27, 2014 · N401AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR LOWER SILL HAND RAIL RELIEF BRACKETS CORRODED. R & R TWO EACH BRACKETS PN 601R31527-149 IAW CRJ 200 SRM 51-40-11 & 51-42-06.
- [SDR A6WA201441086](https://openairdocs.org/sdr/A6WA201441086.md): Angle · corroded · Jan 27, 2014 · N401AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR LOWER SILL ANGLE CORRODED. R & R WITH SERVICEABLE PART IAW CRJ 200 SRM 51-40-11, 51-42-21 & 51-24-21.
- [SDR A6WA201441092](https://openairdocs.org/sdr/A6WA201441092.md): Stiffener · cracked · Jan 25, 2014 · N401AW · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > LEFT EXHAUST FAIRING STIFFENER IS CRACKED, 2ND FROM FRONT. REPAIRED STIFFENER IAW CMM 78-11-00-300-810-A01.
- [SDR A6WA201441074](https://openairdocs.org/sdr/A6WA201441074.md): Frame · corroded · Jan 24, 2014 · N401AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT FS 319 CORRODED ON AFT SIDE BETWEEN STRINGER 26L & 26R. R & R LOWER FRAME SECTOR PN 601R32003-61 IAW CRJ 200 SRM 51-42-06, 51-42-21 & 51-40-11.
- [SDR A6WA201441082](https://openairdocs.org/sdr/A6WA201441082.md): Mount Bracket · cracked · Jan 23, 2014 · N401AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > EXTERNAL SERVICE PANEL LOWER MOUNT BRACKET CRACKED. R & R WITH SERVICEABLE PN 601R33003-19 IAW CRJ 200 SRM 51-40-11 & 51-42-06.
- [SDR A6WA201441078](https://openairdocs.org/sdr/A6WA201441078.md): Drag Angle · cracked · Jan 23, 2014 · N401AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DRAG ANGLE IN RT MLG WW UPPER APRON CRACKED. R & R ANGLE PN 600-10389-2 IAW CRJ 200 SRM 51-40-11 & 51-42-21.
- [SDR A6WA201441077](https://openairdocs.org/sdr/A6WA201441077.md): Stringer Clip · cracked · Jan 23, 2014 · N401AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > STRINGER ATTACH CLIP AFT OF FS 280 AT STRINGER 3L CRACKED. R & R WITH SERVICEABLE CLIP IAW CRJ 200 SRM 51-24-21,51-40-11, 51-42-06 & 51-42-21.
- [SDR A6WA201441076](https://openairdocs.org/sdr/A6WA201441076.md): Attach Angle · cracked · Jan 23, 2014 · N401AW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > RIGHT WING INBD LE, OTBD ATTACH ANGLE CRACKED. R & R WITH SERVICEABLE ANGLE PN 600-12025-8 IAW CRJ 200 SRM 51-40-11 & 51-41-02.
- [SDR A6WA201441075](https://openairdocs.org/sdr/A6WA201441075.md): Support Angle · cracked · Jan 23, 2014 · N401AW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FWD SUPPORT UPPER ANGLE CRACKED. R & R WITH SERVICEABLE ANGLE IAW CRJ 200 SRM 51-24-16, 51-40-11 & 51-42-21.
- [SDR A6WA201441089](https://openairdocs.org/sdr/A6WA201441089.md): Seat Track · corroded · Jan 21, 2014 · N401AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SUPPORT SEAT RAIL AT LBL 9 FROM FS 409 TO 409+128 IS CORRODED. R & R SEAT TRACK AT LBL 9 WITH SERVICEABLE PART IAW CRJ 200 SRM 51-40-11 & AMM 53-01-11.
- [SDR A6WA201441088](https://openairdocs.org/sdr/A6WA201441088.md): Seat Track · corroded · Jan 21, 2014 · N401AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SUPPORT SEAT RAIL AT RBL 9 FROM FS 409 TO 409+128 HAS CORROSION & GOUGES. R & R FLOOR SEAT TRACK WITH SERVICEABLE TRACK IAW CRJ 200 SRM 51-40-11 & AMM 53-01-11.
- [SDR A6WA201441081](https://openairdocs.org/sdr/A6WA201441081.md): Cargo Track · corroded · Jan 21, 2014 · N401AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO FLOOR TIE DOWN TRACK AT RBL 27 & FS 559+80 IS CORRODED. R & R WITH SERVICEABLE TRACK IAW CRJ 200 SRM 51-40-11 & AMM 53-01-11.
- [SDR A6WA201441080](https://openairdocs.org/sdr/A6WA201441080.md): Cargo Track · corroded · Jan 21, 2014 · N401AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO FLOOR TIE DOWN TRACK AT LBL 27 & FS 559+96 IS CORRODED. R & R WITH SERVICEABLE TRACK IAW CRJ 200 SRM 51-40-11 & AMM 53-01-11.
- [SDR A6WA201441079](https://openairdocs.org/sdr/A6WA201441079.md): Cargo Track · corroded · Jan 21, 2014 · N401AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO FLOOR, TIE DOWN TRACK AT LBL 9 & FS 559+112 CORRODED. R & R WITH SERVICEABLE TRACK IAW CRJ 200SRM 51-40-11 & 53-01-11.
- [SDR A6WA201441063](https://openairdocs.org/sdr/A6WA201441063.md): Attach Fitting · cracked · Jan 16, 2014 · N401AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE INTERCOSTAL REPAIR ATTACH CLIP AT 484 & RBL 36 ABOVE THE PRESS FLOOR IS CRACKED. R & R REPAIR ATTACH CLIP IAW 601R-53-41-059 REV B DATED 2009-09-16.
- [SDR A6WA201441062](https://openairdocs.org/sdr/A6WA201441062.md): Attach Fitting · cracked · Jan 16, 2014 · N401AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE INTERCOSTAL ATTACH CLIP AT FS 484 & LBL 27 ABOVE THE PRESS FLOOR IS CRACKED. R & R ATTACH CLIP IAW CRJ 200 SRM 51-40-11, 51-42-06 & 601R-53-41-059 REV B DATED 2009-09-16.
- [SDR A6WA201441061](https://openairdocs.org/sdr/A6WA201441061.md): Attach Angle · cracked · Jan 16, 2014 · N401AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > THE RBL 9 FLOOR BEAM OTBD ATTACH ANGLE AT FS 280 IS CRACKED. R & R ANGLE IAW 601R-53-11-171 REV D.
- [SDR A6WA2013090740025](https://openairdocs.org/sdr/A6WA2013090740025.md): Clamp · damaged · Sep 7, 2013 · N401AW · Cndair CL6002B19 · Pneumatic Distribution System
  > WHILE CLIMBING, RECEIVED LT 10TH DUCT WARNING MESSAGE. PERFORMED QRH, MESSAGE CAME BACK SEVERAL TIMES WHILE PERFORMING QRH. ONCE LT ENGINE AT IDLE POWER, MESSAGE DID NOT COME BACK. FOUND LT 10TH PRSOV CLAMP LEAKING AND DAMAGED, R & R CLAMP IAW AMM SUP 10-00
- [SDR A6WA20130114009](https://openairdocs.org/sdr/A6WA20130114009.md): Proximity Switch · out of adjust · Jan 14, 2013 · N401AW · Cndair CL6002B19 · Door Warning System
  > DURING CLIMB THRU 30,000FT RECEIVED PAX DOOR OUTER HANDLE CAUTION MESSAGE. RAN QRH, MESSAGE PERSISTED. CREW DECLARED AN EMERGENCY AND DIVERTED TO CVG IAW QRH. CAUTION MESSAGE CLEARED DURING DESCENT AT APPROX 13,000FT. FLIGHT LANDED UNEVENTFULLY. ADJUSTED
- [SDR A6WA201212114000](https://openairdocs.org/sdr/A6WA201212114000.md): Anti-Ice Valve · faulty · Dec 7, 2012 · N401AW · Cndair CL6002B19 · Air Intake Anti/De-Ice System
  > LEFT COWL ANTI-ICE CAUTION IN FLT, WOULD NOT EXTINGUISH. COMPLIED WITH QRH. WITH SWITCH OFF MSG CLEARED. AIR RETURN DCA. REMOVED AND REPLACED LEFT COWL ANTI-ICE VALVE IAW AMM 30-22-01, OP CHECK/LEAK GOOD AT THIS TIME.
- [SDR A6WA201240316](https://openairdocs.org/sdr/A6WA201240316.md): Doubler · cracked · Feb 7, 2012 · N401AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FWD PRESSURE BULKHEAD STRIP, DOUBLER, 2ND RT OTBD FROM BL0.00 IS CRACKED, UPPERFWD INBD RADIUS BY WIPER MOTOR BRACKET. REPAIRED IAW REO 601R-53-11-2271, REV A.
- [SDR A6WA201240309](https://openairdocs.org/sdr/A6WA201240309.md): Stringer · cracked · Feb 5, 2012 · N401AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 6R IS CRACKED AFT SIDE OF FS 439.
- [SDR A6WA201240284](https://openairdocs.org/sdr/A6WA201240284.md): Skin · cracked · Feb 3, 2012 · N401AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERIOR SKIN CRACKED ON AFT FRAME AT FS 338.00 AND INTERCOSTAL. REPAIRED INNER SKIN CRACK AT FS 338.00 IAW REO 601R-52-11-2009.
- [SDR A6WA201240285](https://openairdocs.org/sdr/A6WA201240285.md): Intercostal · cracked · Feb 3, 2012 · N401AW · Cndair CL6002B19 · Passenger/Crew Doors
  > INTERCOSTAL UNDER PAX DOOR PANEL 832BR CRACKED. REMOVED CRACKED INTERCOSTAL THEN INSTALLED NEW SERVICEABLE INTERCOSTAL.
- [SDR A6WA201240326](https://openairdocs.org/sdr/A6WA201240326.md): Seat Track · corroded · Feb 3, 2012 · N401AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED AT LBL9, FS 364. R & R SEAT TRACK.
- [SDR A6WA201240283](https://openairdocs.org/sdr/A6WA201240283.md): Door Frame · cracked · Feb 3, 2012 · N401AW · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR FRAME AT FS 338.00 IS CRACKED 4" FROM BOTTOM OF FRAME. REMOVED CRACKED SECTION WHEN INSTALLED NEW SECTION IAW REO 601R-52-11-402, REV H.
- [SDR A6WA201240198](https://openairdocs.org/sdr/A6WA201240198.md): Skin · worn · Feb 2, 2012 · N401AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LEFT EXTERIOR FUSELAGE SKIN WHERE STUB FAIRING MAKES CONTACT IS GOUGED AND WORN, APPROX FS 544. CUT AWAY DAMAGED PORTION OF SKIN PANEL AND INSTALLED NEW SKIN SECTION AND STRAP ON LT EXTERIOR FUSELAGE SKIN IAW REO 601R-53-41-610, REV.
- [SDR A6WA201240297](https://openairdocs.org/sdr/A6WA201240297.md): Skin · gouged · Feb 2, 2012 · N401AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LEFT EXTERIOR FUSELAGE SKIN & WHERE STUB FAIRING MAKES CONTACT IS GOUGED AND WORN. APPROXIMATELY FS 544.0 - 559.0. C UT AWAY DAMAGED PORTION OF SKIN PANEL AND INSTALLED NEW SKIN SECTION AND STRAP ON LT EXTERIOR FUSELAGE SKIN IAW REO 601R-53-41-610, REV.
- [SDR A6WA201240321](https://openairdocs.org/sdr/A6WA201240321.md): Skin · misinstalled · Feb 2, 2012 · N401AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SKIN MISREPAIRED. REPAIRED IAW REO 601R-53-41-1535, REV A.
- [SDR A6WA201240289](https://openairdocs.org/sdr/A6WA201240289.md): Fitting · chafed · Jan 31, 2012 · N401AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RT OTBD FLAP ROLLER FITTING CHAFED, COMPIED WITH REO 601R-57-53-915.
- [SDR A6WA201240302](https://openairdocs.org/sdr/A6WA201240302.md): Skin · cracked · Jan 31, 2012 · N401AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/Skin
  > A CRACK IN RT (FWD) CORE COWL DOOR OUTER SKIN. REMOVED DAMAGE FROM OUTER SKIN. FABRICATED DOUBLER AND SPIGOT IAW REO 601R-71-12-4095 AND CMM 71-12-01. REPAIR SRS118.
- [SDR A6WA201240320](https://openairdocs.org/sdr/A6WA201240320.md): Structure · cracked · Jan 28, 2012 · N401AW · Cndair CL6002B19 · Fuselage Main, Structure
  > BOTH CORNERS ON MLG WW CUT CRACKED. REPAIRED CRACKS IAW REO 601R-53-11-048.
- [SDR A6WA201240286](https://openairdocs.org/sdr/A6WA201240286.md): Structure · chafed · Jan 27, 2012 · N401AW · Cndair CL6002B19 · Landing Gear Doors
  > LEFT MLG DOOR CHAFED NEAR BRUSH, COMPLIED WITH REO 601R-52-82-330.
- [SDR A6WA201240306](https://openairdocs.org/sdr/A6WA201240306.md): Floor Support · corroded · Jan 27, 2012 · N401AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FS 349 CORRODED AND SILL IS SEPARATING. REMOVED UNSERVICEABLE ANGLE SUPPORT ANGLE AND UNSERVICEABLE SILL AND INSTALLED SERVICEABLE ANGLE SUPPORT AND SILL IAW SRM 51-42-06 AND REO 601R-53-21-326.
- [SDR A6WA201240322](https://openairdocs.org/sdr/A6WA201240322.md): Skin · damaged · Jan 27, 2012 · N401AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT FS 295.00 AND S26L. ONE LIGHTNING STRIKE 0.018" DEEP X 0.125" WIDE ON THE FUSELAGE SKIN LOCATED 3/00" AFT OF FS 295.00 + 0.156" FROM STRINGER 26L RIVET LINES REPAIRED LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN AT FS 295.0, STR 26L IAW REO 601R-5
- [SDR A6WA201240317](https://openairdocs.org/sdr/A6WA201240317.md): Striker · gouged · Jan 26, 2012 · N401AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT SEAL STRIKER GOUGED. REPAIRED IAW REO 601R53-22-033, REV C.
- [SDR A6WA201240299](https://openairdocs.org/sdr/A6WA201240299.md): Fitting · chafed · Jan 26, 2012 · N401AW · Cndair CL6002B19 · Trailing Edge Flaps
  > CHAFING AT LEFT OTBD FLAP ROLLER FITTING. OPEN
- [SDR A6WA201240305](https://openairdocs.org/sdr/A6WA201240305.md): Fitting · corroded · Jan 26, 2012 · N401AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FITTING CORRODED AT FS 349, JUST AFT OF THE SERVICE DOOR. BLENDED CORROSION IAW SRM 53-00-00 AND SRM 51-21-06. REMAINING MATERIAL IS WITHIN SERVICEABLE LIMITS IAW SRM 53-00-00.

Next page: https://openairdocs.org/deregistered/N401AW-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 = 'N401AW' AND deregistration_id = 'N401AW-2017-03-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N401AW-2017-03-28/reports

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