# Service difficulty reports: N440AW

A list on [N440AW](https://openairdocs.org/aircraft/N440AW.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 · 176 reports

- [SDR A6WA202304248583](https://openairdocs.org/sdr/A6WA202304248583.md): Unknown · unknown · Apr 24, 2023 · N440AW · Cndair CL6002B19 · Engine Starting System
  > IN CRUISE FLIGHT, R ENG START STATUS MESSAGE AND NO STRTR CUTOUT CAUTION MESSAGE APPEARED INTERMITTENTLY FOR DURATION OF FLIGHT. RAN QRH AND DIVERTED. STATUS MESSAGE PERSISTS WITH ENGINES AND APU OFF. ******AIRCRAFT REMOVED FROM SERVICE********* IN WORK
- [SDR A6WA202304248580](https://openairdocs.org/sdr/A6WA202304248580.md): Unknown · unknown · Apr 24, 2023 · N440AW · Cndair CL6002B19 · Engine Starting System
  > IN CRUISE FLIGHT, R ENG START STATUS MESSAGE AND NO STRTR CUTOUT CAUTION MESSAGE APPEARED INTERMITTENTLY FOR DURATION OF FLIGHT. RAN QRH AND DIVERTED. STATUS MESSAGE PERSISTS WITH ENGINES AND APU OFF. *******AIRCRAFT REMOVED FROM SERVICE********** IN WORK
- [SDR A6WA202203308153](https://openairdocs.org/sdr/A6WA202203308153.md): None · none · Mar 30, 2022 · N440AW · Cndair CL6002B19 · Standard Practices/Structures
  > PREVIOUS BULKHEAD REPAIR, WAS NON-COMPLIANT WITH REO 601R-53-61-1240 NOTE 20 ****AIRCRAFT REMOVED FROM SERVICE **** REPAIRED AFT PRESSURE BULKHEAD IAW 601R-53-61-7793
- [SDR A6WA202203308155](https://openairdocs.org/sdr/A6WA202203308155.md): Stiffener · cracked · Mar 30, 2022 · N440AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE STIFFENER AT FS 516, ON RH BL 45.00 IS CRACKED AS MARKED ****AIRCRAFT REMOVED FROM SERVICE **** REMOVED CRACKED ANGLE STIFFENER AND INSTALLED NEW ANGLE STIFFENER AT FS 516.00 ON RH BL 45.00 IAW ED# AWAC-CRJ 253-01818
- [SDR A6WA202203308154](https://openairdocs.org/sdr/A6WA202203308154.md): None · cracked · Mar 30, 2022 · N440AW · Cndair CL6002B19 · Fuselage, Wing Attach Fittings
  > ANGLE STIFFENER AT FS 516.00, ON LH BL 45.00 IS CRACKED AS MARKED ****AIRCRAFT REMOVED FROM SERVICE*** REMOVED CRACKED STIFFENER AND INSTALLED NEW ANGLE STIFFENER AT FS 516.00 ON LH BL 45.00 IAW ED# AWAC-CRJ253-01817
- [SDR A6WA202104237752](https://openairdocs.org/sdr/A6WA202104237752.md): Line · disconnected · Apr 21, 2021 · N440AW · Cndair CL6002B19 · Humidity Control System
  > CLIMBING THROUGH FL19.5 RECEIVED CABIN ALTITUDE CAUTION. INITIATED DESCENT AND RECEIVED CABIN ALT WARNING, LITTLE TO NO AIRFLOW FELT IN COCKPIT, C/W QRH IN ITS ENTIRETY. ***AIRCRAFT REMOVED FROM SERVICE*** RE-SECURED LINE TO WATER SEPERATOR REF AMM SUP 15-1
- [SDR A6WA202103157715](https://openairdocs.org/sdr/A6WA202103157715.md): Seal · damaged · Mar 14, 2021 · N440AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSING THROUGH 8000 MSL CLIMBING, PAX DOOR HAD VERY LOUD NOISE OF AIR RUSHING OUT OF A/C. PRESSURIZATION OF A/C COULD NOT KEEP UP. BELIEVE A/C WAS PRESSURIZING. LOUD NOISE OF AIR CONTINUED THROUGHOUT ARRIVAL. RETURNED TO IAD. ***AIRCRAFT REMOVED FROM SER
- [SDR A6WA202009287297](https://openairdocs.org/sdr/A6WA202009287297.md): Bulkhead Web · cracked · Sep 26, 2020 · N440AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > PERFORMED SDI OF AFT PRESSURE BULKHEAD FWD FACE, IAW NDTM AWAC SUPPLEMENT 09-008 REV 41. PERFORMED EDDY CURRENT INSPECTION, IAW NDTM PART 1 51-20-06 REV 41. PERFORMED UT INSPECTION, IAW NDTM PART 4 53-61-153 REV 41. 5 EACH DISCREPANCIES. DISCREPANCY 1: FS
- [SDR A6WA202009287296](https://openairdocs.org/sdr/A6WA202009287296.md): Intercostal · cracked · Sep 25, 2020 · N440AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT PRESSURE BULKHEAD AT FS 621.00. RT INTERCOSTAL AT RBL 45.70 & S 14R HAS A CRACK. AIRCRAFT REMOVED FROM SERVICE. FABRICATED INTERCOSTAL P/N 601-35012-52 OUT OF.050" 7075 T6, REF SRM 53-61-17 REV 38. INSTALLED RT INTERCOSTAL, REF SRM 51-42-21 REV 38.
- [SDR A6WA202009227292](https://openairdocs.org/sdr/A6WA202009227292.md): Shroud · cracked · Aug 29, 2020 · N440AW · Cndair CL6002B19 · Wing Main, Frame Structure
  > TWO CRACKS FOUND ON RT LEADING EDGE PANEL 630KL AT AROUND W/S 314.50. THE FIRST CRACK WAS 8.44" FROM THE INBOARD EDGE THAT MEASURED.7" AND THE SECOND CRACK WAS 6.75" FROM THE OUTBOARD EDGE THAT MEASURED 1.3". AIRCRAFT REMOVED FROM SERVICE. REMOVED SHROUD (
- [SDR A6WA202009237294](https://openairdocs.org/sdr/A6WA202009237294.md): Skin · dented · Aug 28, 2020 · N440AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT AT FS 679.8 & S22R-1 THAT MEASURES.8" L X.8" W X.006" D WITH A W/D=133 AND IS LESS THAN 1" FROM S22R. DENT IS NOT WITHIN ALLOWABLE LIMITS, REF CRJ 200 SRM 53-00-31 FIG 103 SH 3 AND SH 4. AIRCRAFT REMOVED FROM SERVICE. CUT DAMAGE AREA OUT 1.5" X 1.2"
- [SDR A6WA202009217291](https://openairdocs.org/sdr/A6WA202009217291.md): Skin · dented · Aug 28, 2020 · N440AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT AT FS 660.9 & S22R-2", DENT MEASURED AT.5" L X.5" W X.005" D WITH A W/D=100 ADDITIONAL DENT IDENTIFIED ON AERSALE W/O 002862 CARD NO 453-900-501-N0002 FOUND AT FS 657.80 & S22R+2" THAT MEASURES.7"L X.7"W X.009"D WITH A W/D=77. BOTH DENTS ARE NOT WI
- [SDR A6WA2020021847185](https://openairdocs.org/sdr/A6WA2020021847185.md): Controller · failed · Feb 16, 2020 · N440AW · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
  > EN ROUTE TO SAV, THE FLIGHT EXPERIENCED A RH WINDSHEILD HEAT CAUTION MESSAGE. AFTER FOLLOWING THE QRH, THE MESSAGE PERSISTED. THE FLIGHT COULD NOT CONTINUE TO SAV DUE TO ICING CONDITIONS, DIVERTED TO DAY FOR REPAIR. AIRCRAFT REMOVED FROM SERVICE TROUBLESHO
- [SDR A6WA201904126549](https://openairdocs.org/sdr/A6WA201904126549.md): Elevator System · abnormal · Apr 10, 2019 · N440AW · Cndair CL6002B19 · Rudder Actuator
  > ON TAKE OFF AC REQUIRED EXCESSIVE BACK PRESSURE TO ROTATE. ELEVATOR CONTROLS FEEL HEAVY AND SLOW TO REACT TO CONTROL WHEEL INPUTS. AC CAN BE TRIMMED FOR FLT. DID NOT ENGAGE AUTOPILOT. THERE IS SLACK IN THE CONTROLS (EXCESSIVE HYSTERESIS) COORDINATED WITH DISP
- [SDR A6WA2018052545846](https://openairdocs.org/sdr/A6WA2018052545846.md): Landing · cracked · May 25, 2018 · N440AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT TRU DOOR AFT LATCH CUTOUT ON PNL LANDING CRACKED.
- [SDR A6WA2018052545843](https://openairdocs.org/sdr/A6WA2018052545843.md): Skin · dented · May 23, 2018 · N440AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > REPAIR FS193-FS202.75 STGR16L COCKPIT LT SIDE SKIN BETWEEN FS193.00 - FS210.0 AND STGR16L-STGR20L (RVSM AREA).
- [SDR A6WA2018052545844](https://openairdocs.org/sdr/A6WA2018052545844.md): Intercostal · cracked · May 23, 2018 · N440AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > STR 15L FS 621-625 INTERCOSTAL MEMBER AT FS 621 BULKHEAD AFT FACE IS CRACKED. REPLACED.
- [SDR A6WA2018052545845](https://openairdocs.org/sdr/A6WA2018052545845.md): Guide · damaged · May 22, 2018 · N440AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > LT WING OUTBD FLAP, INBD FLAP ROLLER GUIDE HAS ABRASION/WEAR. REPLACED
- [SDR A6WA2018052145832](https://openairdocs.org/sdr/A6WA2018052145832.md): Door Sill · corroded · May 19, 2018 · N440AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS313 RT FLOOR SILL SPOT OF CORROSION FWD OF SERVICE DOOR.
- [SDR A6WA2018052145835](https://openairdocs.org/sdr/A6WA2018052145835.md): Skin · chafed · May 19, 2018 · N440AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT I/B FLAP VANE HAS THREE L/E CHAFES.
- [SDR A6WA2018052145837](https://openairdocs.org/sdr/A6WA2018052145837.md): Guide Plate · dented · May 19, 2018 · N440AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > RIGHT I/B FLAP I/B HINGE ARM I/B FAIRING GUIDE PLATE IS DENTED.
- [SDR A6WA2018052345842](https://openairdocs.org/sdr/A6WA2018052345842.md): Skin · chafed · May 17, 2018 · N440AW · Cndair CL6002B19 · Ailerons
  > RIGHT AILERON UPPER CLOSEOUT SKIN CHAFED. REPLACED SKIN IAW SRM 51-42-21.
- [SDR A6WA2018052145841](https://openairdocs.org/sdr/A6WA2018052145841.md): Fitting · cracked · May 17, 2018 · N440AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLIGHT DECK WINDSHIELD CENTER POST LOWER LT FITTING IS CRACKED. REPLACED WINDSHIELD CENTER POST LOWER LT FITTING IAW SRM 51-42-21.
- [SDR A6WA2018052145834](https://openairdocs.org/sdr/A6WA2018052145834.md): Intercostal · cracked · May 17, 2018 · N440AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > STG 15L CLIP INTERCOSTAL AT FS621 BULKHEAD AFT FACE IS CRACKED.
- [SDR A6WA2018052145836](https://openairdocs.org/sdr/A6WA2018052145836.md): Frame · cracked · May 16, 2018 · N440AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS280 RBL9 FRAME HAS A CRACK.
- [SDR A6WA2018052145831](https://openairdocs.org/sdr/A6WA2018052145831.md): Support Angle · cracked · May 16, 2018 · N440AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS280 LBL9 FWD FLOOR SUPPORT ANGLE CORRODED.
- [SDR A6WA2018052145833](https://openairdocs.org/sdr/A6WA2018052145833.md): Fitting · cracked · May 16, 2018 · N440AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AT FS 280 AND LBL 9 CRACKED CLIP.
- [SDR A6WA2018052145839](https://openairdocs.org/sdr/A6WA2018052145839.md): Strap · damaged · May 15, 2018 · N440AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ELONGATED HOLE IN FLOOR STRAP AT FS559.00, LBL38. REPLACED STRAP IAW SRM 51-45-00, 51-42-06.
- [SDR A6WA2018052145838](https://openairdocs.org/sdr/A6WA2018052145838.md): Seat Track · corroded · May 15, 2018 · N440AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDEWALL SEAT TRACK NR 4 CORRODED. REPLACED SEAT TRACK NR 4 IAW SUPP 13-074 AND AMM 53-01-11.
- [SDR A6WA2018052545847](https://openairdocs.org/sdr/A6WA2018052545847.md): Skin · gouged · May 11, 2018 · N440AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT WING AT WS264, O/B FLAP FIXED VANE L/E SKIN GOUGED. REPLACED SKIN IAW SRM 51-42-13.
- [SDR A6WA2018052545848](https://openairdocs.org/sdr/A6WA2018052545848.md): Skin · dented · May 11, 2018 · N440AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT O/B FLAP LOWER SKIN IS DENTED. REPAIRED FLAP IAW REO 601R-57-53-1125 REV-B.
- [SDR A6WA2018052145840](https://openairdocs.org/sdr/A6WA2018052145840.md): Skin · chafed · May 7, 2018 · N440AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RT I/B FLAP VANE, I/B AND O/B LEADING EDGE CHAFED. REPLACED I/B SKIN AND REPAIRED O/B SKIN IAW REO M601R-57-52-004 AND SRM 51-42-13.
- [SDR A6WA2018022145630](https://openairdocs.org/sdr/A6WA2018022145630.md): Proximity Sensor · out of adjust · Feb 15, 2018 · N440AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > DEPARTING TYS GEAR DISAGREE WARNING. NOSE DOOR OPEN. NOSE GEAR DOWN. DID NOT RETRACT. FOLLOWED QRH & MANUAL GEAR EXTENSION. GEAR HANDLE DOWN. GEAR EXTENDED. 3 GREEN. EMERGENCY EXTENSION HANDLE STOWED. LANDED AT 46,500 SMOOTHLY. BTMS READS 3-2-1-2. ADJUSTED N
- [SDR A6WA201744897](https://openairdocs.org/sdr/A6WA201744897.md): Connector · unsecure · Mar 28, 2017 · N440AW · Cndair CL6002B19 · Light System Wiring
  > FLOOR EMERGENCY LIGHTS WILL NOT REMAIN ILLUMINATED FROM ROWS 8-12. IT COMES ON THEN FADES OUT. SECURED THE CONNECTOR P40LY IAW 16-371A, OPS CHECKED GOOD.
- [SDR A6WA201744845](https://openairdocs.org/sdr/A6WA201744845.md): Connector · defective · Mar 10, 2017 · N440AW · Cndair CL6002B19 · Light System Wiring
  > 4031 EMERGENCY LIGHTS NO ILLUMINATING PAST ROW 8 TO THE BACK OF AIRCRAFT ON FLOOR. FOUND CONNECTORS P40LY AND P39LY BAD. REMOVED AND REPLACED BOTH CONNECTORS IAW AMM 16-371A, OPS CHECKED GOOD,
- [SDR A6WA2016120544619](https://openairdocs.org/sdr/A6WA2016120544619.md): Control Handle · failed · Dec 2, 2016 · N440AW · Cndair CL6002B19 · Landing Gear Selector
  > FLT.4127, NO GEAR MOVEMENT AFTER LANDING GEAR LEVER BROUGHT UP. NO GEAR DISAGREE MESSAGE. ALL LANDING GEAR INDICATION LIGHTS STAYED GREEN. PARKING BRAKE SOV CAUTION MESSAGE APPEARED WHEN GEAR LEVER SELECTED UP, CLEARED WHEN GEAR LEVER SELECTED DOWN. ANTISKID I
- [SDR A6WA201644005](https://openairdocs.org/sdr/A6WA201644005.md): Door · stuck · Jun 15, 2016 · N440AW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR WILL NOT OPEN FROM THE OUTSIDE.
- [SDR A6WA201643923](https://openairdocs.org/sdr/A6WA201643923.md): Pin · out of adjust · May 23, 2016 · N440AW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR OUTER HANDLE PUSH TO RELEASE BUTTON STUCK. ADJUSTED SERVICE DOOR OUTER HANDLE RETENTION PIN AS REQUIRED. OPERATIONS CHECKED GOOD IAW AMM 52-41-03.
- [SDR A6WA201643913](https://openairdocs.org/sdr/A6WA201643913.md): Shaft · cracked · May 20, 2016 · N440AW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR OUTER HANDLE WILL NOT OPEN FROM OUTSIDE USING PUSHBUTTON. INSPECTED SERVICE DOOR OUTER HANDLE & LUBRICATED IAW SUPP 11-029B, NO FIX. FOUND CRACK IN OUTER SERVICE DOOR OUTER HANDLE SHAFT. DOOR CLOSES, LATCHES & LOCKS NORMALLY.
- [SDR A6WA201643828](https://openairdocs.org/sdr/A6WA201643828.md): Strap · corroded · Apr 30, 2016 · N440AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL T STRAP FS 349.00 HAS CORROSION.
- [SDR A6WA201643824](https://openairdocs.org/sdr/A6WA201643824.md): Frame · cracked · Apr 30, 2016 · N440AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS FRAME 333.00, BETWEEN STRINGER 0 & 1L IS CRACKED. REPLACED FRAME 333.00 IAW SRM 51-40-11, 51-42-06, 51-42-21 & 53-21-15.
- [SDR A6WA201643826](https://openairdocs.org/sdr/A6WA201643826.md): Attach Fitting · corroded · Apr 30, 2016 · N440AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ATTACHMENT FITTING FS 349.00 AT RT SILL HAS CORROSION. REPLACED FLOOR SUPPORT ATTACHMENT FITTING AT FS 349.00 AT RT SILL IAW SRM 51-42-21.
- [SDR A6WA201643825](https://openairdocs.org/sdr/A6WA201643825.md): Frame · corroded · Apr 30, 2016 · N440AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 310.00 HAS CORROSION ON THE FWD & AFT SIDES, BETWEEN STRINGER 23R & 22R, IN THE FWD E & E BAY. REPLACED FRAME 310.00 IAW SRM 51-42-21, 51-42-06, 51-42-13, 51-21-11, 51-25-06 & 51-25-16.
- [SDR A6WA201643821](https://openairdocs.org/sdr/A6WA201643821.md): Frame · corroded · Apr 29, 2016 · N440AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 333.00 HAS CORROSION ON THE FWD SIDE, BETWEEN STRINGER 23R & 22R, IN THE FWD E & E BAY. REPLACED FRAME 333.00 SECTION, BETWEEN STRINGER 23R & 18R IAW SRM 51-42-06 & 51-42-21.
- [SDR A6WA201643817](https://openairdocs.org/sdr/A6WA201643817.md): Fitting · cracked · Apr 28, 2016 · N440AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > AFT ACCESSORY COMPARTMENT STATION 621.0, BULKHEAD AFT SIDE LT INTERCOSTAL STRINGER 14L, CLIP IS CRACKED. REPAIRED IAW SRM 51-42-01.
- [SDR A6WA201643816](https://openairdocs.org/sdr/A6WA201643816.md): Intercostal · cracked · Apr 28, 2016 · N440AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT ACCESSORY COMPARTMENT STATION 621, BULKHEAD AFT SIDE LT INTERCOSTAL STRINGER 13L, CLIP IS CRACKED. REPLACED IAW SRM 51-42-21.
- [SDR A6WA201643809](https://openairdocs.org/sdr/A6WA201643809.md): Skin · dented · Apr 27, 2016 · N440AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT LOWER FUSELAGE SKIN, BETWEEN FS 654.0 & 672.20, STRINGER 26R - 27 HAS A DENT. REPAIRED AFT LOWER FUSELAGE SKIN IAW EA AWAC CRJ253 00359 REV IR DATED 04 16 2016.
- [SDR A6WA201643812](https://openairdocs.org/sdr/A6WA201643812.md): Plate · cracked · Apr 27, 2016 · N440AW · Cndair CL6002B19 · Engine Thrust Reverser
  > RIGHT THRUST REVERSER PDU CONNECTOR PLUG MOUNTING PLATE IS CRACKED. REPLACED RT THRUST REVERSER PDU MOUNT PLATE IAW SRM 51-42-06.
- [SDR A6WA201643813](https://openairdocs.org/sdr/A6WA201643813.md): Retainer · cracked · Apr 27, 2016 · N440AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > LEFT PYLON PANEL 412DB HAS A CRACKED SEAL RETAINER. REPLACED SEAL RETAINER ON LT PYLON PANEL 412DB IAW SRM 51-42-06.
- [SDR A6WA201643806](https://openairdocs.org/sdr/A6WA201643806.md): Attach Bracket · cracked · Apr 26, 2016 · N440AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT OTBD FLAP CTR HINGE ARM, OTBD FAIRING ATTACH BRACKET IS CRACKED. R & R ATTACH BRACKET IAW SRM 51-40-11, 51-42-06 & 51-25-16.

Next page: https://openairdocs.org/aircraft/N440AW/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 = 'N440AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N440AW/reports

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