# Service difficulty reports: N404AW, cancelled Jan 3, 2017

A list on [N404AW, cancelled Jan 3, 2017](https://openairdocs.org/deregistered/N404AW-2017-01-03.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 · 168 reports

- [SDR A6WA201643528](https://openairdocs.org/sdr/A6WA201643528.md): Unknown · malfunctioned · Feb 2, 2016 · N404AW · Cndair CL6002B19 · Elevator Control System
  > ELEVATOR INPUT VIA YOKE SEEMS HEAVY, ALL PHASES OF FLIGHT & ON GND, CAPTAINS & FIRST OFFICERS SIDE.
- [SDR A6WA201543261](https://openairdocs.org/sdr/A6WA201543261.md): Apu · fire · Nov 18, 2015 · N404AW · Cndair CL6002B19 · APU Core Engine
  > AFTER TRANSFER OF BLEED TO APU AUTO SHUTDOWN, FUELER REPORTED LOTS OF SMOKE & FIRE COMING FROM APU EXHAUST.
- [SDR A6WA201543190](https://openairdocs.org/sdr/A6WA201543190.md): Light · inoperative · Nov 1, 2015 · N404AW · Cndair CL6002B19 · Emergency Lighting
  > ROW F & AFT EMER FLOOR TRACK LIGHTS INOPERATIVE.
- [SDR A6WA201542985](https://openairdocs.org/sdr/A6WA201542985.md): Light · inoperative · Aug 16, 2015 · N404AW · Cndair CL6002B19 · Emergency Lighting
  > REAR 1/3RD OF FLOOR LEVEL EMER LIGHTS ARE INOPERATIVE.
- [SDR A6WA201542975](https://openairdocs.org/sdr/A6WA201542975.md): Stiffener · cracked · Aug 10, 2015 · N404AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > 1012024 1000-0002 FS 409.00+128 BULKHEAD VERTICAL BEAM STIFFENER AT LBL 27.0, INBD STIFFENER CRACKED AT BOTTOM FASTENER HOLE. REPAIRED IAW GREO 601R-53-41-056.
- [SDR A6WA201542974](https://openairdocs.org/sdr/A6WA201542974.md): Stiffener · cracked · Aug 10, 2015 · N404AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS409.00+128 BULKHEAD VERTICAL BEAM AT RBL 27.0, INBD STIFFENER CRACKED AT BOTTOM FASTENER HOLE. REPAIRED IAW GREO 601R-53-41-056.
- [SDR A6WA201542976](https://openairdocs.org/sdr/A6WA201542976.md): Stiffener · cracked · Aug 10, 2015 · N404AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 409+128 BULKHEAD VERTICAL BEAM AT LBL 27.0, OTBD STIFFENER CRACKED AT BOTTOM FASTENER HOLE. REPAIRED IAW GREO 601R53-41-056.
- [SDR A6WA201542950](https://openairdocs.org/sdr/A6WA201542950.md): Light · inoperative · Jul 28, 2015 · N404AW · Cndair CL6002B19 · Emergency Lighting
  > ONE BULB BURNED OUT ONBOARD CEILING LIGHT BY LAVATORY DOOR. R & R NUMBER 4 CEILING EMERGENCY LIGHT BULB IAW AMM 33-51-16. OPERATIONS CHECKED GOOD.
- [SDR A6WA201542951](https://openairdocs.org/sdr/A6WA201542951.md): Light · inoperative · Jul 28, 2015 · N404AW · Cndair CL6002B19 · Emergency Lighting
  > THREE LIGHT BULBS BURNED OUT ON MID CABIN EMERGENCY LIGHTS ON CEILING. R & R 3 LIGHT BULBS IN MID CABIN EMERGENCY EXIT IAW AMM 33-51-14. OPERATIONS CHECKED GOOD.
- [SDR A6WA2015072942950](https://openairdocs.org/sdr/A6WA2015072942950.md): Bulb · abnormal · Jul 28, 2015 · N404AW · Cndair CL6002B19 · Passenger Compartment Lighting
  > FLIGHT 3892, ONE BULB BURNED OUT ON CEILING LIGHT BY LAVATORY DOOR. R & R THE BULB IAW AMM 33-51-16. OS CHECKED GOOD.
- [SDR A6WA201542351](https://openairdocs.org/sdr/A6WA201542351.md): Warning System · activated · Jan 28, 2015 · N404AW · Cndair CL6002B19 · Landing Gear Steering System
  > RECEIVED NWS INOPERATIVE MSG ENROUTE. COMPLIED WITH QRH, MSG REMAINED.
- [SDR A6WA201442136](https://openairdocs.org/sdr/A6WA201442136.md): Light · inoperative · Nov 6, 2014 · N404AW · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT ATTENDANT REPORTED EMERGENCY LIGHTS ROW 6 - 8 AND LOWER EMER EXIT SIGN RT SIDE INOPERATIVE.
- [SDR A6WA201441535](https://openairdocs.org/sdr/A6WA201441535.md): Ballast · defective · May 1, 2014 · N404AW · Cndair CL6002B19 · Passenger Compartment Lighting
  > BURNING WIRE SMELL FROM OVERHEAD BIN ROW 10 RT SIDE. INSPECTED OVERHEAD BIN & FOUND BALLAST AT OVERHEAD BIN ROW 10 D/F INOPERATIVE WITH BURNT SMELL. R & R BALLAST AT OVERHEAD BIN ROW 10 D/F IAW SUPP 13-096, OPERATIONS CHECKED GOOD.
- [SDR A6WA201441340](https://openairdocs.org/sdr/A6WA201441340.md): Heater · shorted · Mar 31, 2014 · N404AW · Cndair CL6002B19 · Water/Waste System Wiring
  > STRONG BURNING RUBBER ODOR INFLIGHT, LOCALIZED TO GALLEY & FIRST COUPLE ROWS OF CABIN. NO SMOKE NOTED & NO ELECTRICAL ISSUES NOTED. GALLEY HEAT & POTABLE WATER SYS ON. PULLED BREAKERS FOR POTABLE WATER & GALLEY HEAT & ODOR DISPERSED. FOUND GALLEY LINE HEAT
- [SDR A6WA201441319](https://openairdocs.org/sdr/A6WA201441319.md): Angle · corroded · Mar 18, 2014 · N404AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ANGLE AT PAX DOOR THRESHOLD CORRODED AT FS 310 TO 349. R & R FLOOR SUPPORT ANGLE AT PAX DOOR SILL F 310 - 349 WITH SERVICEABLE PN 601R31527-221 IAW CRJ200 SRM 51-40-11 & 51-42-21.
- [SDR A6WA201441291](https://openairdocs.org/sdr/A6WA201441291.md): Handle · cracked · Mar 18, 2014 · N404AW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR OUTER HANDLE CRACKED. R & R CARGO DOOR HANDLE ASSEMBLY IAW CRJ200 SRM 51-21-11, 51-42-21 & 51-40-11.
- [SDR A6WA201441290](https://openairdocs.org/sdr/A6WA201441290.md): Panel · corroded · Mar 18, 2014 · N404AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LOWER ATTACH POINT ON CARGO BAY PANEL 282AR CORRODED. R & R WITH NEW SERVICEABLE PANEL.
- [SDR A6WA201441303](https://openairdocs.org/sdr/A6WA201441303.md): Step · corroded · Mar 17, 2014 · N404AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR STEP PANEL 832 FT IS DELAMINATED FROM CORROSION. R & R PAX DOOR STEP PANEL 832 FT WITH SERVICEABLE PN 601R31980-59 IAW CRJ200 SRM 51-41-02.
- [SDR A6WA201441302](https://openairdocs.org/sdr/A6WA201441302.md): Hinge · corroded · Mar 17, 2014 · N404AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR UPPER FOLDING STEP HINGE CORRODED THROUGH. R & R PAX DOOR UPPER FOLDING STOP HINGE IAW CRJ 200 AMM 52-11-14, PN 601R-31980-41.
- [SDR A6WA201441293](https://openairdocs.org/sdr/A6WA201441293.md): Skin · cracked · Mar 17, 2014 · N404AW · Cndair CL6002B19 · Engine Drains
  > RIGHT JET PIPE HAS 3 CRACKS IN SKIN AROUND COMBUSTOR DRAIN. REPAIRED CRACKS IAW STS EA 15-2014-050.
- [SDR A6WA201441292](https://openairdocs.org/sdr/A6WA201441292.md): Fitting · corroded · Mar 15, 2014 · N404AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIVETS CORRODED AT FS 349, LBL 9 - LBL 27. REMOVED CORROSION IAW CRJ 200 SRM 51-21-06, 53-00-00 & 51-21-11. R & R WINDSCREEN FITTING.
- [SDR A6WA201441289](https://openairdocs.org/sdr/A6WA201441289.md): Bracket · corroded · Mar 14, 2014 · N404AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT HANDRAIL SUPPORT STOW CUP BRACKET CORRODED. R & R AFT HANDRAIL SUPPORT BRACKET IAW CRJ SRM 51-40-11, 51-42-10.
- [SDR A6WA201441297](https://openairdocs.org/sdr/A6WA201441297.md): Rib · corroded · Mar 13, 2014 · N404AW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > LT OTBD LE, INBD RIB IS CORRODED. R & R INBD RIB ON LT OTBD LE PN 601R12063-21 IAW CRJ 200 SRM 51-40-11 & 51-42-13.
- [SDR A6WA201441288](https://openairdocs.org/sdr/A6WA201441288.md): Floor Support · corroded · Mar 11, 2014 · N404AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT BEAM AT 349.00 CORRODED. R & R FLOOR SUPPORT BEAM IAW CRJ200 51-42-13 & 51-42-06.
- [SDR A6WA201441301](https://openairdocs.org/sdr/A6WA201441301.md): Hinge · gouged · Mar 10, 2014 · N404AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR UPPER FOLDING STEP HINGE HAS NUMEROUS GOUGES AT EACH STEP, SIDE HINGE HALF PIN LOBE & UPPER STEP CLOSING PLATE CORRODED BEYOND LIMITS. R & R TWO EACH HINGES ON PAX DOOR UPPER FOLDING STEP WITH NEW SERVICEABLE HINGES PN 601R31980-41 & 600-31980-103S &
- [SDR A6WA201441300](https://openairdocs.org/sdr/A6WA201441300.md): Rib · cracked · Mar 10, 2014 · N404AW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > RIGHT MLG BATTERY RIB IS CRACKED. REPAIRED RT MLG BATTERY RIB IAW REO 601R 57-51-046 REV B DATED 2002-02-28 REPAIR NR 2.
- [SDR A6WA201441299](https://openairdocs.org/sdr/A6WA201441299.md): Drag Angle · cracked · Mar 10, 2014 · N404AW · Cndair CL6002B19 · Landing Gear Doors
  > RT MLG DRAG ANGLE COMMON TO BATTERY RIB IS CRACKED. REMOVED & INSTALLED RT MLG DOOR DRAG ANGLE, STIFFENER PN 600-10389-2 IAW CRJ 200 SRM 51-42-21.
- [SDR A6WA201441298](https://openairdocs.org/sdr/A6WA201441298.md): Drag Angle · cracked · Mar 10, 2014 · N404AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BATTERY RIB DRAG ANGLE CRACKED IN LT MLG WW. R & R WITH SERVICEABLE PART, PN 600-10389-1 IAW CRJ 200 SRM 51-40-11 & 51-42-21.
- [SDR A6WA201441287](https://openairdocs.org/sdr/A6WA201441287.md): Structure · cracked · Mar 9, 2014 · N404AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > NLG CUTOUT AFT RT CORNER CRACKED. REPAIRED NLG CUTOUT RT CORNER IAW REO 601R-53-11-048.
- [SDR A6WA201441239](https://openairdocs.org/sdr/A6WA201441239.md): Angle · cracked · Mar 7, 2014 · N404AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT OBLIQUE ANGLE AT FS 621 - 625 & STRINGER 14L IS CRACKED. R & R WITH SERVICEABLE PART, PN 601-35012-51 IAW SRM 51-40-11 & 51-42-21.
- [SDR A6WA201441238](https://openairdocs.org/sdr/A6WA201441238.md): Angle · cracked · Mar 7, 2014 · N404AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT OBLIQUE ANGLE FS 621 - 625 AT STRINGER 14R IS CRACKED. R & R RT OBLIQUE ANGLE WITH SERVICEABLE PART PN 601-35012-52 IAW CRJ 200 SRM 51-40-11 & 51-42-21.
- [SDR A6WA201441242](https://openairdocs.org/sdr/A6WA201441242.md): Seat Track · corroded · Mar 6, 2014 · N404AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT FLOOR SEAT TRACK AT RBL 9 HAS CORROSION AT FS 364. R & R WITH SERVICEABLE PART IAW SRM 51-40-11 & AMM 53-01-11.
- [SDR A6WA201441241](https://openairdocs.org/sdr/A6WA201441241.md): Seat Track · corroded · Mar 6, 2014 · N404AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT FLOOR SEAT TRACK CORRODED AT FS 364 & LBL 9. R & R WITH SERVICEABLE PART IAW SRM 51-40-11 & AMM 53-01-11.
- [SDR A6WA201441243](https://openairdocs.org/sdr/A6WA201441243.md): Cargo Track · corroded · Mar 5, 2014 · N404AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO COMPARTMENT SEAT TRACKS CORRODED AT LBL & RBL 9, FS 559+112, LBL & RBL 27 AT FS 559+85. R & R THREE TRACKS AT RBL 9, FS 559+112, LBL & RBL 27 AT FS 559+85 WITH SERVICEABLE PARTS IAW SRM 51-40-11.
- [SDR A6WA201441240](https://openairdocs.org/sdr/A6WA201441240.md): Fitting · cracked · Mar 5, 2014 · N404AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOORBEAM LBL 9 OTBD CLIP AT FS 280 IS CRACKED. R & R CLIP WITH SERVICEABLE PART IAW 601R-53-11-171 REV D DATED 13-FEB-07.
- [SDR A6WA201441244](https://openairdocs.org/sdr/A6WA201441244.md): Strap · corroded · Mar 4, 2014 · N404AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT STRAP AT FS 559 & LBL 38 CORRODED. R & R WITH SERVICEABLE PART IAW SRM 51-40-11 & 51-42-06.
- [SDR A6WA201312024043](https://openairdocs.org/sdr/A6WA201312024043.md): Autopilot Sys · malfunctioned · Nov 27, 2013 · N404AW · Cndair CL6002B19 · Autopilot System
  > 3925DLY NON COMMANDED YAW MOTION TO THE RT AT FL290 SAT 46C ON FLIGHT DIRECTOR NR 2 FOR APPROXIMATELY 2 SECONDS. YAW DAMPER REMAINED ENGAGED, NO FURTHER OCCURRENCES. INTEGRATED FCC & REPORTS CUT R OCCURRENCE, IAW FIM 22-22, ACTION REQUIRED IS NONE. PERFORMED
- [SDR A6WA201310084033](https://openairdocs.org/sdr/A6WA201310084033.md): Adg · malfunctioned · Oct 7, 2013 · N404AW · Cndair CL6002B19 · AC Generator-Alternator
  > DURING TAKEOFF, WOW, ADG DEPLOYED. DEACTIVATED ADG AUTO DEPLOY IAW AMM 24-23-22, RESTOWED ADG IAW AMM 24-23-22.
- [SDR A6WA201240773](https://openairdocs.org/sdr/A6WA201240773.md): Unknown · odor · Aug 15, 2012 · N404AW · Cndair CL6002B19 · Air Distribution System
  > STRONG ELECTRICAL BURNING ODOR DETECTED IN COCKPIT AND GALLEY AREA. SEEMS STRONGER WITH COCKPIT DOOR CLOSED. TROUBLESHOT PACK SYSTEM TO FULL HOT, FULL COLD FOR 30 MIN, RAN ALL INTERIOR LIGHTS ON BRIGHT FOR 30 MIN WITH PAX DOOR AND COCKPIT DOOR CLOSED, NO EL
- [SDR A6WA201240386](https://openairdocs.org/sdr/A6WA201240386.md): Bracket · cracked · Mar 2, 2012 · N404AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FWD UPPER CARGO DOOR TRACK ROLLER BRACKET CRACKED. R & R WITH SERVICEABLE IAW REO 601R-52-31-179.
- [SDR A6WA201240339](https://openairdocs.org/sdr/A6WA201240339.md): Roller · cracked · Mar 2, 2012 · N404AW · Cndair CL6002B19 · Cargo/Baggage Doors
  > FWD UPPER CARGO DOOR TRACK ROLLER BRACKET CRACKED. R & R WITH SERVICEABLE PN CC670-38706-3 IAW REO 601R-52-31-179.
- [SDR A6WA201240332](https://openairdocs.org/sdr/A6WA201240332.md): Sill · corroded · Mar 1, 2012 · N404AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR SILL CORRODED AROUND NUT PLATE HOLES FS 574-621. R & R CARGO DOOR SILL FS 574-621 IAW SRM 51-40-11, 51-42-06, & REO 601R-53-690, REV D.
- [SDR A6WA210240334](https://openairdocs.org/sdr/A6WA210240334.md): Trunnion · damaged · Mar 1, 2012 · N404AW · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > DURING COLD WORKING OF THE MLG TRUNNION LOWER FLANGED, FOUND FOUR PREVIOUSLY OVERSIZED HOLES RT REPAIRED IAW REO 601R-57-21-1607.
- [SDR A6WA201240333](https://openairdocs.org/sdr/A6WA201240333.md): Hinge Fitting · cracked · Mar 1, 2012 · N404AW · Cndair CL6002B19 · Wing, Control Surface Attach Fittings
  > NDT INDICATED A CRACK AT THE AFT HOLE OF THE AFT HINGE FITTING LOCATION. REPAIRED IAW REO 601R-57-21-1608.
- [SDR A6WA201240331](https://openairdocs.org/sdr/A6WA201240331.md): Sill · corroded · Feb 29, 2012 · N404AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL AREA HAS CORROSION. R & R SERVICE DOOR SILL ANGLE IAW SRM 51-42-06, 51-42-21. R & R SERVICE DOOR STEP PLATE IAW AMM 25-33-01.
- [SDR A6WA201240275](https://openairdocs.org/sdr/A6WA201240275.md): Floorbeam · cracked · Feb 29, 2012 · N404AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LEFT FS 484, BL27 INBD CLIP IS CRACKED. R & R CLIP IAW REO 601R-53-41-059, REV B.
- [SDR A6WA201240328](https://openairdocs.org/sdr/A6WA201240328.md): Frame · corroded · Feb 29, 2012 · N404AW · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON RIB AT STA 349 IN AVIONICS BAY BILGE AREA ( FWD SIDE) R & R LOWER FRAME SECTION AT FS 349, STR 34L-24 PN 601R32005-69 IAW SRM 51-42-06, 51-42-21 & 51-40-11.
- [SDR A6WA20124329](https://openairdocs.org/sdr/A6WA20124329.md): Frame · corroded · Feb 29, 2012 · N404AW · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON RIB AT STA 333 IN AVIONICS BAY BILGE AREA (FWD AND AFT SIDE) R 7 R FRAME SECTION PN 601R32004-55 IAW SRM 51-42-06, 51-42-21, 51-40-11.
- [SDR A6WA201240330](https://openairdocs.org/sdr/A6WA201240330.md): Frame · corroded · Feb 29, 2012 · N404AW · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON RIB AT STA 319 IN AVIONICS BAY BILGE AREA (FWD & AFT SIDE). R & R LOWER FRAME SECTION AT BS 319 S24L-24R IAW SRM 51-42-06, 51-42-21, 51-40-11.
- [SDR A6WA201240384](https://openairdocs.org/sdr/A6WA201240384.md): Floorbeam · cracked · Feb 28, 2012 · N404AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM BS 621 CRACKED. REPAIRED FLOORBEAM IAW REO 601R-53-61-117, REV C.

Next page: https://openairdocs.org/deregistered/N404AW-2017-01-03/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 = 'N404AW' AND deregistration_id = 'N404AW-2017-01-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N404AW-2017-01-03/reports

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