# Service difficulty reports: N445AW

A list on [N445AW](https://openairdocs.org/aircraft/N445AW.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 · 154 reports

- [SDR A6WA202203258141](https://openairdocs.org/sdr/A6WA202203258141.md): None · none · Mar 25, 2022 · N445AW · Cndair CL6002B19 · Engine Oil System (Airframe Furnished)
  > ****SUPPLEMENTAL INFORMATION****AT FL 280 RH OIL PRESSURE INDICATION DROPPED TO ZERO. RECEIVED OIL LOW PRES WARN AND AURAL WARN. ENGINE ROLLED BACK AND STOPPED RUNNING. CW QRH SHUT DOWN THE ENGINE. ***AIRCRAFT REMOVED FROM SERVICE*** REF WO#314605 JOB CARD 4
- [SDR A6WA202012237481](https://openairdocs.org/sdr/A6WA202012237481.md): Detector Loop · shorted · Dec 22, 2020 · N445AW · Cndair CL6002B19 · Detection System
  > WHILE ON CLIMB OUT RECEIVED RT 10TH ST DUCT MESSAGE. C/W QRH. MESSAGE REMAINED AND THEN EXTINGUISHED A FEW MINS LATER. ONCE ON GROUND, BRIEFLY APPEARED TWICE ON TAXI. ECS SYNOPTIC SHOWED RED FROM RT SOV UP TO PACK PRESSURE. AIRCRAFT REMOVED FROM SERVICE.
- [SDR A6WA202012227470](https://openairdocs.org/sdr/A6WA202012227470.md): Element · shorted · Dec 20, 2020 · N445AW · Cndair CL6002B19 · Detection System
  > RECEIVED RT 10TH DUCT WARNING ON INITIAL CLIMB OUT OF ORD, RAN QRH, MESSAGE PERSISTED. SYNOPTIC PAGE SHOWED RED FROM ISOL TO THE PYLON, MESSAGE REMAINED EVEN AFTER ENGINE AND APU SHUTDOWN. AIRCRAFT REMOVED FROM SERVICE. TROUBLESHOT AND FOUND SENSE ELEMENT A
- [SDR A6WA202011067395](https://openairdocs.org/sdr/A6WA202011067395.md): Seat Track · corroded · Oct 17, 2020 · N445AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 FS 421 TO 559+80 SEAT TRACK CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK SEGMENT LBL 9 FS 421 TO 559+80, IAW REO 601R-53-00-764 & SRM 51-41-02.
- [SDR A6WA202010217345](https://openairdocs.org/sdr/A6WA202010217345.md): Tee Fitting · corroded · Oct 16, 2020 · N445AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RBL 9 AT FS 559+80 HAS CORROSION ON T CAP. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED T CAP AT RBL 9 AT FS 559+80 TO FS 559, IAW BOMBARDIER DWG 601R3501 AND CRJ200 SRM 51-42-21.
- [SDR A6WA202010197341](https://openairdocs.org/sdr/A6WA202010197341.md): Seat Track · corroded · Oct 16, 2020 · N445AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 AT FS 421-559+80 SEAT TRACK HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK SEGMENT RBL 9 AT FS 421-559+80, IAW REO 601R-53-00-764 AND CRJ 200 SRM 51-41-02.
- [SDR A6WA202010197342](https://openairdocs.org/sdr/A6WA202010197342.md): Seat Track · corroded · Oct 16, 2020 · N445AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDEWALL SEAT TRACK AT FS 421 TO FS 559+80 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED DAMAGED SEAT TRACK SECTION LT SIDEWALL, IAW REO 601-53-00-764.
- [SDR A6WA202010197340](https://openairdocs.org/sdr/A6WA202010197340.md): Seat Track · corroded · Oct 16, 2020 · N445AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9, FS 558+88 HAS CORROSION ON SEAT TRACK. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK SEGMENT AT LB L9 FS 559+88, IAW REO 601R-53-00-764 AND CRJ200 51-40-02.
- [SDR A6WA202010197339](https://openairdocs.org/sdr/A6WA202010197339.md): Seat Track · corroded · Oct 16, 2020 · N445AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9, FS 559+88, SEAT TRACK CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK SEGMENT AT RBL 9, FS 559+88.
- [SDR A6WA2019090946848](https://openairdocs.org/sdr/A6WA2019090946848.md): Warning System · false activation · Sep 5, 2019 · N445AW · Cndair CL6002B19 · Door Warning System
  > ON CLIMBOUT RECEIVED PAX DOOR LATCH CAUTION MESSAGE INTERMITTANTLY FOR 10 MINUTES, THEN MESSAGE ON STEADY FOR 10 MINUTES, THEN MESSAGE CLEARED. AFTER CONFERRING WITH MAINTENANCE CONTROL THE DECISION WAS MADE TO RETURN TO CKB.
- [SDR A6WA2019090546842](https://openairdocs.org/sdr/A6WA2019090546842.md): Hinge · damaged · Sep 4, 2019 · N445AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > FOUND PAX DOOR HINGE HALF ON FUSELAGE SIDE TO BE WORN BEYOND LIMITS.
- [SDR A6WA2018120946219](https://openairdocs.org/sdr/A6WA2018120946219.md): Fairing · damaged · Dec 7, 2018 · N445AW · Cndair CL6002B19 · Engine Thrust Reverser
  > DURING WALK AROUND INSPECTION OF AIRCRAFT AFTER ARRIVAL AT HANGAR, MECHANIC NOTED RT ENGINE LOWER STANG FAIRING DAMAGED AND PARTIALLY MISSING FROM AIRCRAFT. MECHANIC REMOVED AND REPLACED THE RT ENGINE LOWER STANG FAIRING PER AMM 78-34-15. NO DAMAGE NOTED TO SU
- [SDR A6WA2018082345999](https://openairdocs.org/sdr/A6WA2018082345999.md): Floor Support · corroded · Aug 21, 2018 · N445AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPORT CORRODED IN THE AFT CARGO BAY, BS 574 TO 621. REPAIRED THE FLOOR SUPPORT IAW EA CRJ253-01021, REV-IR.
- [SDR A6WA2018082045992](https://openairdocs.org/sdr/A6WA2018082045992.md): Flange · cracked · Aug 16, 2018 · N445AW · Cndair CL6002B19 · Engine Thrust Reverser
  > LEFT ENGINE THRUST REVERSER TORQUE BOX CRACKED ON THE AFT FLANGE, 6 O'CLOCK POSITION. REPAIRED THE FLANGE IAW REO 601R-78-34-2527, REV-B.
- [SDR A6WA2018082045991](https://openairdocs.org/sdr/A6WA2018082045991.md): Flange · cracked · Aug 16, 2018 · N445AW · Cndair CL6002B19 · Engine Thrust Reverser
  > LEFT THRUST REVERSER TORQUE BOX FLANGE CRACKED. REPAIRED THE FLANGE IAW REO 601R-78-30-2553, REV-A.
- [SDR A6WA2018082045990](https://openairdocs.org/sdr/A6WA2018082045990.md): Frame · cracked · Aug 15, 2018 · N445AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT BS 605 OUTER FLANGE WAS CRACKED AT 2 LOCATIONS, STRINGER 9L. REPAIRED THE FRAME IAW REO 601R-53-61-5214, REV-A.
- [SDR A6WA2018082045989](https://openairdocs.org/sdr/A6WA2018082045989.md): Beam · damaged · Aug 15, 2018 · N445AW · Cndair CL6002B19 · Fuselage Main, Structure
  > CARGO DOOR ASSIST CABLE HAS CUT INTO HORIZONTAL SUPPORT BEAM. REPLACED THE BEAM IAW SRM 51-42-21, 51-40-11, AND 51-42-06.
- [SDR A6WA2018081645982](https://openairdocs.org/sdr/A6WA2018081645982.md): Floorbeam · cracked · Aug 15, 2018 · N445AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM ANGLE AT BS 280, AFT SIDE, LBL 9 WAS CRACKED. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-21.
- [SDR A6WA2018081645985](https://openairdocs.org/sdr/A6WA2018081645985.md): Skin · dented · Aug 15, 2018 · N445AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN HAD A PROTRUDING DENT AT BS 654 TO 672, STRINGERS 22L TO 23L. REPAIRED THE SKIN IAW EACRJ253-01011, REV-IR.
- [SDR A6WA2018081645984](https://openairdocs.org/sdr/A6WA2018081645984.md): Skin · dented · Aug 15, 2018 · N445AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN HAD A PROTRUDING DENT BETWEEN BS 654 AND 672, STRINGERS 21L TO 22L. REPAIRED THE SKIN IAW EA CRJ253-01011REV-IR
- [SDR A6WA2018081645979](https://openairdocs.org/sdr/A6WA2018081645979.md): Skin · dented · Aug 14, 2018 · N445AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBOARD FLAP LOWER SKIN HAS AREAS OF DENTS FROM WS 75.0 TO 50.5. REPAIRED RIGHT INBOARD FLAP LOWER SKIN IAW SRM 57-52-00.
- [SDR A6WA2018081445977](https://openairdocs.org/sdr/A6WA2018081445977.md): Housing · cracked · Aug 13, 2018 · N445AW · Cndair CL6002B19 · Fuselage Main, Structure
  > FOUND CRACKS ON THE POWER RECEPTACLE ATTACH HOUSING. REPLACED THE HOUSING IAW REO 601R-53-11-569 REV-B.
- [SDR A6WA2018081445978](https://openairdocs.org/sdr/A6WA2018081445978.md): Skin · chafed · Aug 12, 2018 · N445AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP VANE LEADING EDGE CHAFED AT WS 57.0. REPLACED THE FLAP VANE L/E SKIN IAW IAW SRM 51-42-13.
- [SDR A6WA2018082045993](https://openairdocs.org/sdr/A6WA2018082045993.md): Frame · corroded · Aug 11, 2018 · N445AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 605 WAS FOUND CORRODED BETWEEN STRINGERS 22L AND 22R. REPLACED THE FRAME SECTION IAW SRM 51-21-06, 51-42-06, AND 53-61-15.
- [SDR A6WA2018081345974](https://openairdocs.org/sdr/A6WA2018081345974.md): Skin · chafed · Aug 8, 2018 · N445AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE L/E SKIN WAS CHAFED. REPLACED FLAP VANE IAW SRM 51-42-13.
- [SDR A6WA2018081345975](https://openairdocs.org/sdr/A6WA2018081345975.md): Skin · chafed · Aug 8, 2018 · N445AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE SKIN WAS CHAFED. REPLACED THE FLAP VANE SKIN IAW SRM 51-42-13.
- [SDR A6WA2018081345972](https://openairdocs.org/sdr/A6WA2018081345972.md): Bracket · cracked · Aug 8, 2018 · N445AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > A/C EXTERNAL SERVICE PANEL LOWER ATTACH ANGLE BRACKET IS CRACKED. REPLACED BRACKET IAW SRM 51-42-06.
- [SDR A6WA2018081345973](https://openairdocs.org/sdr/A6WA2018081345973.md): Flap · damaged · Aug 7, 2018 · N445AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT WING TE FLAP DAMAGED. REPAIRED IAW SRM 57-52-00.
- [SDR A6WA2018081345971](https://openairdocs.org/sdr/A6WA2018081345971.md): Bracket · cracked · Aug 5, 2018 · N445AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RIGHT MLG WW TRANSDUCER BRACKET CRACKED. REPLACED THE BRACKET IAW SRM 51-42-06.
- [SDR A6WA2018032245634](https://openairdocs.org/sdr/A6WA2018032245634.md): Warning System · false activation · Feb 16, 2018 · N445AW · Cndair CL6002B19 · Pneumatic Indicating System
  > CLIMBING THROUGH FL210 RECEIVED ANTI ICE WARNING WITH OVERHEAT INDICATION, C/W QRH MESSAGE PERSISTED. AIR RETURNED TO ROC PER QRH, FLAPS 20 REF 45+30 KNOTS (SPEED WAS 169) NO THRUST REVERSERS AVAILABLE/FULL BRAKING. TEMPS AT GATE 8-10-5-5 LANDING WEIGHT 46,000
- [SDR A6WA201745413](https://openairdocs.org/sdr/A6WA201745413.md): Handle · dirty · Nov 13, 2017 · N445AW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR OUTER HANDLE WILL NOT POP OUT AND ALLOW DOOR TO OPEN. CLEANED AND LUBED OUTER HANDLE OPS CHECK GOOD AT THIS TIME REF AMM 52-41-00.
- [SDR A6WA201745093](https://openairdocs.org/sdr/A6WA201745093.md): Unknown · leaking · Jul 11, 2017 · N445AW · Cndair CL6002B19 · APU Engine Fuel and Control
  > STRONG FUEL EXHAUST SMELL INSIDE OF ACFT REF 276650/3 APU FUEL LEAK. MAINTENANCE IS INVESTIGATING SOURCE OF SUSPECTED APU FUEL LEAK.
- [SDR A6WA2017050144957](https://openairdocs.org/sdr/A6WA2017050144957.md): Warning Message · activated · Apr 30, 2017 · N445AW · Cndair CL6002B19 · Drag Control System
  > SPOILERON CAUTION MESSAGE IN CRUISE FLT. COMPLIED WITH QRH. LANDED AT FLAPS 20.
- [SDR A6WA201644348](https://openairdocs.org/sdr/A6WA201644348.md): Engine · fluctuates · Sep 20, 2016 · N445AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > DURING CLIMB, WITH CLIMB POWER SET, N1 & N2 WILL NOT STABILIZE. N1 FLUCTUATES 88 PERCENT TO 92 PERCENT RAPIDLY ON RT ENGINE. DIVERTED AND LANDED AT APPROXIMATELY 40,000 LBS GROSS.
- [SDR A6WA201644167](https://openairdocs.org/sdr/A6WA201644167.md): Angle · corroded · Jul 30, 2016 · N445AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FRAME 319.70 FWD LOWER ANGLE STRIP HAS CORROSION BETWEEN STR 22R AND 20R IN THE FWD ELECTRICAL EQUIPMENT BAY. REPAIRED CORROSION ON ANGLE AT FS 319.70 BETWEEN STR 20R AND 22R.
- [SDR A6WA2016080144167](https://openairdocs.org/sdr/A6WA2016080144167.md): Angle · corroded · Jul 30, 2016 · N445AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 319.70 FWD LOWER ANGLE STRIP HAS CORROSION BETWEEN STRINGERS 20 AND 22R IN THE FWD E&E BAY. REPAIRED THE ANGLE.
- [SDR A6WA2016080144166](https://openairdocs.org/sdr/A6WA2016080144166.md): Angle · chafed · Jul 30, 2016 · N445AW · Cndair CL6002B19 · Passenger/Crew Doors
  > WHILE PERFORMING NDT ON L1 DOOR, FOUND FRAME CHAFED UNDER FWD PULL IN LEVER. REPLACED THE L1 DOOR FRAME ANGLE IAW SRM 51-42-06, 51-42-21, EA CRJ252-00464 AND SUPPLEMENT 16-229.
- [SDR A6WA2016080144165](https://openairdocs.org/sdr/A6WA2016080144165.md): Seat Track · corroded · Jul 30, 2016 · N445AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SEAT TRACK NR 4, BS 559+04 TO FS 559+80 HAS CORROSION. REPLACED THE SEAT TRACK IAW AMM 53-01-11 AND REO 601R-53-00-485 REV-B.
- [SDR A6WA201644168](https://openairdocs.org/sdr/A6WA201644168.md): Stiffener · broken · Jul 30, 2016 · N445AW · Cndair CL6002B19 · APU Cowling/Containment
  > APU ENCLOSURE HAS 3 EA BROKEN STIFFENERS FROM WEB. REPAIRED DAMAGED AREAS ON APU ENCLOSURE IAW SUP: NR 16-168, 16-233 AND EA AWAC-CRJ249-00467.
- [SDR A6WA2016080144162](https://openairdocs.org/sdr/A6WA2016080144162.md): Fitting · corroded · Jul 29, 2016 · N445AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LBL 9, BS 621 ATTACH FITTING IS CORRODED. REPAIRED THE FITTING IAW EA AWAC-CRJ253-00452.
- [SDR A6WA2016080144161](https://openairdocs.org/sdr/A6WA2016080144161.md): Panel · cracked · Jul 29, 2016 · N445AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT RISER PANEL IS CRACKED AT FIRST STEP. REPAIRED THE RISER PANEL IAW REO 601R-52-11-702.
- [SDR A6WA2016080144163](https://openairdocs.org/sdr/A6WA2016080144163.md): Angle · cracked · Jul 29, 2016 · N445AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LEFT WING TO FUSELAGE PANEL ATTACHING STRUCTURE BS 473.15 IS CRACKED. REPLACED ATTACH FITTING IAW SRM 51-42-10, 51-42-02.
- [SDR A6WA201644164](https://openairdocs.org/sdr/A6WA201644164.md): Panel · cracked · Jul 29, 2016 · N445AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD RISER PANEL IS CRACKED AT THIRD STEP. REPAIRED THE RISER PANEL IAW REO 601R-52-11-702 REV-D AND SUPPLEMENT 16-223.
- [SDR A6WA2016080144158](https://openairdocs.org/sdr/A6WA2016080144158.md): Fitting · corroded · Jul 27, 2016 · N445AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LBL 27, BS 621ATTACH FITTING HAS CORROSION. REPAIRED THE FITTING IAW EA AWAC-CRJ253-00453.
- [SDR A6WA2016080144155](https://openairdocs.org/sdr/A6WA2016080144155.md): Floor Support · corroded · Jul 27, 2016 · N445AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL 27 FLOOR SUPPORT HAS CORROSION AT BS 597 AND 609. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-21, 51-42-22, SUPPLEMENT 15-279.
- [SDR A6WA2016080144159](https://openairdocs.org/sdr/A6WA2016080144159.md): Skin · damaged · Jul 27, 2016 · N445AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP LOWER SKIN CORNER HAS NNUMEROUS NICKS, SCRATCHES AND GOUGES. REPLACED THE FLAP SKIN IAW SRM 51-42-13.
- [SDR A6WA2016080144152](https://openairdocs.org/sdr/A6WA2016080144152.md): Panel · cracked · Jul 26, 2016 · N445AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT RISER PANEL IS CRACKED AT 3RD STEP.
- [SDR A6WA2016080144149](https://openairdocs.org/sdr/A6WA2016080144149.md): Floorbeam · corroded · Jul 26, 2016 · N445AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RBL 9 FLOORBEAM CAP HAS CORROSION AT FS 559+82.
- [SDR A6WA2016080144151](https://openairdocs.org/sdr/A6WA2016080144151.md): Panel · cracked · Jul 26, 2016 · N445AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT RISER PANEL IS CRACKED AT 4TH STEP
- [SDR A6WA2016080144153](https://openairdocs.org/sdr/A6WA2016080144153.md): Skin · chafed · Jul 26, 2016 · N445AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE LE IS CHAFED AT THREE LOCATIONS WERE STOPS HIT THE VANE

Next page: https://openairdocs.org/aircraft/N445AW/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 = 'N445AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N445AW/reports

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