# Service difficulty reports: N453AW

A list on [N453AW](https://openairdocs.org/aircraft/N453AW.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 · 152 reports

- [SDR A6WA202109147876](https://openairdocs.org/sdr/A6WA202109147876.md): Warning Message · false activation · Sep 10, 2021 · N453AW · Cndair CL6002B19 · Door Warning System
  > RECEIVED SERVICE DOOR CAUTION AFTER ROTATION. MESSAGE CLEARED ON ITS OWN. BOTH HANDLES VERIFIED STOWED, AND GREEN WITNESS MARKS WERE ALIGNED. AIRCRAFT REMOVED FROM SERVICE. VERIFIED SWITCHES IN CORRECT RIG, NO PSEU CODES. COULD NOT DUPILCATE. OPS CHECK GOOD.
- [SDR A6WA202010067306](https://openairdocs.org/sdr/A6WA202010067306.md): Adg · unwanted deploy · Oct 3, 2020 · N453AW · Cndair CL6002B19 · AC Generation System
  > ADG DEPLOYED IN FLIGHT AT APPROX 280 KTS. ADG WAS DEPLOYED FOR 72 MINS. AC ESSENTIAL BUS WAS NEVER DE-POWERED. AIRCRAFT REMOVED FROM SERVICE. COMPLIED WITH SUP 16-172, TROUBLESHOT, PER FIM 24-23-00, NO FAULT FOUND. PERFORMED SPECIAL VISUAL INSPECTION OF A
- [SDR A6WA202010077317](https://openairdocs.org/sdr/A6WA202010077317.md): Timer · corroded · Oct 1, 2020 · N453AW · Cndair CL6002B19 · Waste Disposal System
  > TOILET TIMER HAS CORROSION ON HOUSING AT ATTACH POINTS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED TIMER, IAW AMM25-41-00-04.
- [SDR A6WA202010067303](https://openairdocs.org/sdr/A6WA202010067303.md): Seat Track · corroded · Oct 1, 2020 · N453AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 AT FS 559+80 SEAT TRACK AFT SECTION 6" STRIP HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK AT FS 559 AT LBL 9, IAW REO 601R-53-00-764.
- [SDR A6WA202010067302](https://openairdocs.org/sdr/A6WA202010067302.md): Seat Track · corroded · Oct 1, 2020 · N453AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > NR-N RBL 9 SEAT TRACK AT FS 429 THROUGH FS 570 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK AT FS 429-FS 570 AT RBL 9, IAW REO 601R-53-00-764.
- [SDR A6WA202010067304](https://openairdocs.org/sdr/A6WA202010067304.md): Spar · cracked · Oct 1, 2020 · N453AW · Cndair CL6002B19 · Wing Spar
  > RIGHT WING LOWER EDGE OF REAR SPAR AT WS 62.5 SUSPECTED CRACK/CORROSION INDICATION DETECTED DURING NDT INSPECTION. AIRCRAFT REMOVED FROM SERVICE. DAMAGE WAS REMOVED BY BLENDING WITH A MINIMUM REMAINING THICKNESS OF.235" NDT EVALUATION SHOW NO CRACK EXIST.
- [SDR A6WA2019022546419](https://openairdocs.org/sdr/A6WA2019022546419.md): Unknown · unknown · Feb 24, 2019 · N453AW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > DURING CLIMB AFTER DEPARTURE, THE FLIGHT CREW NOTED THE LANDING GEAR TOOK AN ABNORMALLY LONG TIME TO RETRACT. THE CREW EVALUATED THE SITUATION AND ELECTED TO RETURN TO KIAD. THE CREW DECLARED AN EMERGENCY AND COORDINATED WITH DISPATCH. THE FLIGHT HELD TO BURN
- [SDR A6WA2018100146095](https://openairdocs.org/sdr/A6WA2018100146095.md): Door Seal · defective · Sep 28, 2018 · N453AW · Cndair CL6002B19 · Service Doors
  > FOLLOWING HEAVY CHECK MAINTENANCE DURING CLIMB OUT CREW HEARD A LOUD POP THEN CABIN BEGAN TO DEPRESSURIZE. CREW COMPLIED WITH QRH AND REDUCED ALTITUDE AND DIVERTED BACK TO OKC FOR INSPECTION. FOUND SERVICE DOOR SEAL WITH NO VENT HOLES, CUT HOLES IN SEAL IAW A
- [SDR A6WA2018092846089](https://openairdocs.org/sdr/A6WA2018092846089.md): Landing · cracked · Sep 25, 2018 · N453AW · Cndair CL6002B19 · Fuselage Main, Structure
  > LEFT TRU DOOR LANDING AFT LATCH AREA HAS CRACK. REPLACED LH TRU DOOR LANDING IAW AWAC SUPPLEMENT 17-280
- [SDR A6WA2018092446084](https://openairdocs.org/sdr/A6WA2018092446084.md): Skin · cracked · Sep 21, 2018 · N453AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT NLG DOOR CUT OUT, AFT RIGHT CORNER FUSELAGE SKIN IS CRACKED. REPAIRED NLG AFT DOOR CUT OUT FUSELAGE SKIN IAW REO 601R-53-11-0048 REV-D.
- [SDR A6WA2018092446085](https://openairdocs.org/sdr/A6WA2018092446085.md): Floorbeam · corroded · Sep 21, 2018 · N453AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED AT FS 559+86, RBL9. REPAIRED FLOORBEAM IAW SRM 53-00-43.
- [SDR A6WA2018092146083](https://openairdocs.org/sdr/A6WA2018092146083.md): Skin · cracked · Sep 21, 2018 · N453AW · Cndair CL6002B19 · Wing, Plate/Skin
  > RT OB WING LE HAS 2 CRACKED EDGING BY RIVETS. REPLACED RT OB WING LE EDGING IAW SRM 51-42-13.
- [SDR A6WA2018092146080](https://openairdocs.org/sdr/A6WA2018092146080.md): Skin · chafed · Sep 20, 2018 · N453AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT FLAP VANE SKIN CHAFED AT I/B BUMPER. REPLACED FLAP VANE SKIN IAW SRM 51-42-13.
- [SDR A6WA2018092146078](https://openairdocs.org/sdr/A6WA2018092146078.md): Torque Box · cracked · Sep 19, 2018 · N453AW · Cndair CL6002B19 · Engine Thrust Reverser
  > NR 1 T/R AFT TORQUE BOX CRACKED AT THE 7 O'CLOCK POSITION. REPAIRED T/R TORQUE BOX AT THE 7O'CLOCK POSITION IAW REO 601R-78-30-2616 REV-NC.
- [SDR A6WA2018092146079](https://openairdocs.org/sdr/A6WA2018092146079.md): Attach Angle · cracked · Sep 19, 2018 · N453AW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > ENGINE SUPPORT BEAM LT LOWER FUSELAGE ATTACH ANGLE CRACKED. REPLACED ANGLE IAW SRM 51-42-21.
- [SDR A6WA2018091946063](https://openairdocs.org/sdr/A6WA2018091946063.md): Drag Angle · cracked · Sep 19, 2018 · N453AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE CRACKED AT PULLEY BRACKET. REPAIRED.
- [SDR A6WA2018092146076](https://openairdocs.org/sdr/A6WA2018092146076.md): Fitting · cracked · Sep 18, 2018 · N453AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CLIP CRACKED AT FS 625.00, STR 15L. REPLACED CLIP IAW SRM TR51-42, 51-42-21.
- [SDR A6WA2018092146061](https://openairdocs.org/sdr/A6WA2018092146061.md): Seat Track · corroded · Sep 18, 2018 · N453AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT FLOOR SEAT TRACK NR 1 CORRODED. REPLACED SEAT TRACK IAW AMM 53-01-11.
- [SDR A6WA2018092146075](https://openairdocs.org/sdr/A6WA2018092146075.md): Fitting · cracked · Sep 18, 2018 · N453AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CLIP CRACKED AT FS 625.00, STR 15R. REPLACED CLIP IAW SRM TR51-42, 51-42-21.
- [SDR A6WA2018091846057](https://openairdocs.org/sdr/A6WA2018091846057.md): Bulkhead · cracked · Sep 18, 2018 · N453AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD HAS 2 CRACKS AT BL 0.0, WL 110. REPAIRED BULKHEAD IAW REO 601R-53-61-1285 REV-E.
- [SDR A6WA2018091846059](https://openairdocs.org/sdr/A6WA2018091846059.md): Bulkhead · cracked · Sep 18, 2018 · N453AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD HAS 2 CRACKS AT FS621.00, BL0.0, WL 132.0. REPAIRED BULKHEAD IAW REO601R-53-61-1285 REV-E.
- [SDR A6WA2018092146077](https://openairdocs.org/sdr/A6WA2018092146077.md): Torque Box · cracked · Sep 17, 2018 · N453AW · Cndair CL6002B19 · Engine Thrust Reverser
  > NR 1 THRUST REVERSER TORQUE BOX IS CRACKED AT THE 5 O'CLOCK POSITION. REPAIRED NR 1 T/R TORQUE BOX IAW REO601R-78-30-2616 REV-NC.
- [SDR A6WA2018091746056](https://openairdocs.org/sdr/A6WA2018091746056.md): Angle · cracked · Sep 15, 2018 · N453AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VERTICAL POST AT FS409+128 AND BL 0.0, WL 69.0 IS CRACKED IN THE RIGHT AFT RADIUS. VERTICAL POST FOUND TO NOT BE CRACKED, REINFORCEMENT ANGLE WAS CRACKED. REPLACED REINFORCEMENT ANGLE IAW SRM TR51-42, 51-42-06, REO 601R-53-41889 REV-C.
- [SDR A6WA2018091746055](https://openairdocs.org/sdr/A6WA2018091746055.md): Retainer · cracked · Sep 14, 2018 · N453AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > PYLON PANEL 422BT SEAL RETAINER CRACKED. REPLACED SEAL RETAINER IAW SRM 51-42-06.
- [SDR A6WA2018091746054](https://openairdocs.org/sdr/A6WA2018091746054.md): Retainer · cracked · Sep 14, 2018 · N453AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > PYLON PANEL 412BT SEAL RETAINER CRACKED. REPLACED SEAL RETAINER IAW SRM 51-42-06.
- [SDR A6WA2018091446052](https://openairdocs.org/sdr/A6WA2018091446052.md): Fitting · cracked · Sep 13, 2018 · N453AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 484.00 OUTBOARD CLIP CRACKED AT LBL27. REPLACED CLIP IAW CRJ200 SRM 51-42-06, 51-42-21, 51-24-36, TR 51-42.
- [SDR A6WA2018092446087](https://openairdocs.org/sdr/A6WA2018092446087.md): Strap · corroded · Sep 12, 2018 · N453AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT STRAP CORRODED AT FS559.00, RBL29 TO RBL43. REPAIRED STRAP IAW EA AWAC-CRJ253-01045 REV-IR.
- [SDR A6WA2018040645752](https://openairdocs.org/sdr/A6WA2018040645752.md): Unknown · unknown · Apr 5, 2018 · N453AW · Cndair CL6002B19 · Flight Control System
  > DURING DESCENT, AN UNCOMMANDED YAW AND ROLL OCCURED AT 16000 FT. RAN QRH FOR THE UNCOMMANDED YAW MOTION AND DISCONNECTED YAW DAMPERS. YAW CONTINUED ALL THE WAY TO TOUCH DOWN. INTERMITTENT LEFT AND RIGHT DUTCH ROLL.
- [SDR A6WA2017091345273](https://openairdocs.org/sdr/A6WA2017091345273.md): Light · contaminated · Sep 12, 2017 · N453AW · Cndair CL6002B19 · Emergency Lighting
  > DURING PRE-FLIGHT ACCEPTANCE CHECK, CREW FOUND THAT THE EMERGENCY LIGHTS FROM ROWS 2-5 WERE INOPERATIVE INSPECTED AND FOUND WATER IN THE LIGHT. REMOVED WATER AND INSTALLED. SYSTEM OPS CHECKED GOOD IAW 16-374A.
- [SDR A6WA201745019](https://openairdocs.org/sdr/A6WA201745019.md): Inverter · inoperative · May 16, 2017 · N453AW · Bombdr CL6002D15 · Emergency Lighting
  > EMERGENCY FLOOR LIGHTING ROW 9 AND AFT NOT ILLUMINATING. R&R NR 4 EMERGENCY LIGHT INVERTER IAW AMM 33-51. OPS CHECK GOOD AT THIS TIME.
- [SDR A6WA2017051645007](https://openairdocs.org/sdr/A6WA2017051645007.md): Battery Pack · inoperative · May 14, 2017 · N453AW · Cndair CL6002B19 · Emergency Lighting
  > FLOOR EMERGENCY LIGHTS FROM ROW 9 TO AFT NOT WORKING. R & R THE BATTERY PACK AT POSITION 4 IAW AMM 33-51-04. OPS CHECKED GOOD.
- [SDR A6WA2016122844684](https://openairdocs.org/sdr/A6WA2016122844684.md): Unknown · odor · Dec 22, 2016 · N453AW · Cndair CL6002B19 · Air Distribution System
  > CREW REPORTED THAT AT FLIGHT LEVEL 16,000 A STRONG ODOR OF EXHAUST FUMES, CABIN PRESSURE WAS NORMAL, APU WAS OFF, PACKS WERE RUNNING ON ENGINES AND SET TO AUTO, ODOR WAS PRESENT IN COCKPIT ONLY, FA COULD NOT ODOR ANYTHING ABNORMAL IN THE CABIN.
- [SDR A6WA201644436](https://openairdocs.org/sdr/A6WA201644436.md): Plug · migrated · Oct 16, 2016 · N453AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING CUSTOMER WALK, FOUND 3 FREEZE PLUGS PUSHING IN ON FWD PRESSURE PNL 132AL.
- [SDR A6WA201644428](https://openairdocs.org/sdr/A6WA201644428.md): Frame · cracked · Oct 14, 2016 · N453AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 333 IS CRACKED JUST I/B OF STR 1L.
- [SDR A6WA201644425](https://openairdocs.org/sdr/A6WA201644425.md): Door Sill · corroded · Oct 14, 2016 · N453AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL CORRODED BETWEEN FS 559+48 AND 559+112 RBL 43.
- [SDR A6WA201644429](https://openairdocs.org/sdr/A6WA201644429.md): Skin · damaged · Oct 14, 2016 · N453AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN HAS LIGHTNING STRIKE DAMAGE ON SKIN AND STRINGER AT FS 248-265 S14L.
- [SDR A6WA201644426](https://openairdocs.org/sdr/A6WA201644426.md): Support Angle · corroded · Oct 14, 2016 · N453AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR SILL FLOOR SUPPORT ANGLE CORRODED AROUND NUTPLATES.
- [SDR A6WA201644423](https://openairdocs.org/sdr/A6WA201644423.md): Skin · dented · Oct 12, 2016 · N453AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT I/B FLAP HAS DENT ON LOWER SURFACE AT WS 56.30. REPLACED DAMAGED SECTION OF LOWER LT I/B FLAP SKIN FROM WS 64.00 TO I/B CORNER IAW REO 601R-57-52-1544.
- [SDR A6WA201644416](https://openairdocs.org/sdr/A6WA201644416.md): Angle · cracked · Oct 9, 2016 · N453AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 621 BULKHEAD INTERCOSTAL ANGLE STRINGER 15L IS CRACKED
- [SDR A6WA201644418](https://openairdocs.org/sdr/A6WA201644418.md): Intercostal · cracked · Oct 9, 2016 · N453AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 621 BULKHEAD INTERCOSTAL ANGLE STRINGER 13L IS CRACKED
- [SDR A6WA201644417](https://openairdocs.org/sdr/A6WA201644417.md): Intercostal · cracked · Oct 9, 2016 · N453AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 621 BULKHEAD INTERCOSTAL ANGLE STRINGER 14L IS CRACKED
- [SDR A6WA201644415](https://openairdocs.org/sdr/A6WA201644415.md): Bracket · cracked · Oct 9, 2016 · N453AW · Cndair CL6002B19 · Fuselage Main, Frame
  > PILOT WINDSHIELD LWR INBD BRACKET AT CENTER POST IS CRACKED.
- [SDR A6WA201644412](https://openairdocs.org/sdr/A6WA201644412.md): Door Sill · cracked · Oct 7, 2016 · N453AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR SILL PLATE CRACKED AT FS 589 FROM I/B FASTENER TO EDGE OF PART.
- [SDR A6WA201644408](https://openairdocs.org/sdr/A6WA201644408.md): Angle · cracked · Oct 6, 2016 · N453AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RIGHT WINDSHIELD SIDE POST OTBD ATTACH ANGLE CRACKED.
- [SDR A6WA201644406](https://openairdocs.org/sdr/A6WA201644406.md): Floorbeam · cracked · Oct 6, 2016 · N453AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM RBL 27, OTBB ANGLE IS CRACKED AT BS 484.
- [SDR A6WA201644407](https://openairdocs.org/sdr/A6WA201644407.md): Attach Angle · cracked · Oct 6, 2016 · N453AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LEFT WINDSHIELD SIDE POST OTBD ATTACH ANGLE CRACKED.
- [SDR A6WA2016081844241](https://openairdocs.org/sdr/A6WA2016081844241.md): Inverter · inoperative · Aug 17, 2016 · N453AW · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 4069, LAST SECTION OF EMERGENCY LIGHTS INOPERATIVE. ROWS 9-12. R & R INVERTER IAW AMM, OP CHECKED GOOD.
- [SDR A6WA201644175](https://openairdocs.org/sdr/A6WA201644175.md): Light · inoperative · Aug 2, 2016 · N453AW · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 4018. FLOOR EMERGENCY LIGHTS INOPERATIVE BEHIND ROW 8.
- [SDR A6WA201644145](https://openairdocs.org/sdr/A6WA201644145.md): Connector · detached · Jul 25, 2016 · N453AW · Cndair CL600* · Light System Wiring
  > FLIGHT 3822. EMERGENCY LIGHTS AFT OF ROW 8 INOPERATIVE. RECONNECTED EMERGENCY LIGHT STRIP FROM STRIP AT ROW 8F.
- [SDR A6WA201643933](https://openairdocs.org/sdr/A6WA201643933.md): Bulkhead · cracked · May 24, 2016 · N453AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > COMPLIED WITH PERMANENT REPAIR TO FS 621 PRESS BULKHEAD AT LBL 27.5, WL 131, REPAIRED.

Next page: https://openairdocs.org/aircraft/N453AW/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 = 'N453AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N453AW/reports

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