# Service difficulty reports: N430AW

A list on [N430AW](https://openairdocs.org/aircraft/N430AW.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 5 · 211 reports

- [SDR A6WA202203098125](https://openairdocs.org/sdr/A6WA202203098125.md): Controller · inoperative · Mar 9, 2022 · N430AW · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > IN CLIMB WITH WING ANTIICE SELECTED ON RECEIVED WING OVERHEAT WARNING. SYNOPTIC PAGE SHOWS RH WING ONLY RED. CW QRH SELECTED WING ANTIICE OFF. MSG PERSISTED FOR MORE THAN 40 SECONDS. LEFT ICING AT THAT TIME. MSG CLEARED.WITHIN 2 MINUTES. AT THIS POINT RECEIVE
- [SDR A6WA202111047952](https://openairdocs.org/sdr/A6WA202111047952.md): None · corroded · Nov 3, 2021 · N430AW · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > FOUND PITTING AND EXFOLIATION CORROSION ON ALL 4 SEAL RETAINERS P/N CC670-38663-5, CC670-38675 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED ALL4 SEAL RETAINERS-3,CC670-38675-3,CC38662-5 FOR THE MAIN AVIONICS DOOR P/N 601R38346-83
- [SDR A6WA202110217923](https://openairdocs.org/sdr/A6WA202110217923.md): Seat Track · corroded · Oct 20, 2021 · N430AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > RH SIDE SEAT RAIL-SEAT TRACK AT FS 529-FS 559 HAS MULTIPLE AREAS CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM RH SIDE SEAT RAIL SEAT TRACK IAW CRJ-200 SRM 51-21-06 AND 51-21-49, REPAIR WITHIN LIMITS
- [SDR A6WA202105287791](https://openairdocs.org/sdr/A6WA202105287791.md): Switch · malfunctioned · May 28, 2021 · N430AW · Cndair CL6002B19 · Stabilizer Position Indicating
  > MACH TRIM STAB TRIM CASS MESSAGES IN FLT. C/W QRH, MESSAGES REMAINED. OCCURRED DURING CRUISE AFTER NORMAL TAKE OFF. C/W QRH AND SET FLAPS TO 20. CONTROLS DIFFICULT TO MOVE BUT FELT SAFE TO PROCEED. LANDED WITHOUT ISSUES, SMOOTH LANDING BUT DID DECLARE AN EM
- [SDR A6WA2020032447236](https://openairdocs.org/sdr/A6WA2020032447236.md): Bulkhead · cracked · Mar 23, 2020 · N430AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD IS CRACKED AT THE LINTEL FITTING. "AIRCRAFT REMOVED FROM SERVICE" REPAIRED AFT PRESSURE BULKHEAD AT LINTEL FITTING IAW REO 601R-53-61-1230 REV-F.
- [SDR A6WA2020032447233](https://openairdocs.org/sdr/A6WA2020032447233.md): Bulkhead · cracked · Mar 21, 2020 · N430AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD IS CRACKED AT THE TOP END OF THE CARGO DOOR TRACK. "AIRCRAFT REMOVED FROM SERVICE" REPAIRED AFT PRESSURE BULKHEAD IAW BOMBARDIER REO 601R-53-61-1541 REV. F.
- [SDR A6WA2020032447235](https://openairdocs.org/sdr/A6WA2020032447235.md): Bulkhead · cracked · Mar 19, 2020 · N430AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESURE BULKHEAD IS CRACKED AT BL O IN THE SPLICE WEB AT APPROXIMATELY WL 140. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED SPLICE WEB IAW CRJ-200 SRM 51-42-06
- [SDR A6WA2020032447234](https://openairdocs.org/sdr/A6WA2020032447234.md): Bulkhead · cracked · Mar 19, 2020 · N430AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD IS CRACKED AT THE RBL 27.5 APPROX WL112 "AIRCRAFT REMOVED FROM SERVICE" REPAIRED CRACKED BULKHEAD IAW BOMBARDIER REO 601R53-61-1285 REV E
- [SDR A6WA2020031647228](https://openairdocs.org/sdr/A6WA2020031647228.md): Angle · cracked · Mar 13, 2020 · N430AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR POWER ASSIST MOTOR MOUNT ANGLE IS CRACKED. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED MOUNT ANGLE IAW CRJ200 SRM 51-42-06 & 51-42-13.
- [SDR A6WA2020010247086](https://openairdocs.org/sdr/A6WA2020010247086.md): Wire Harness · defective · Dec 31, 2019 · N430AW · Cndair CL6002B19 · Landing Gear System Wiring
  > STEERING INOP CAUTION IN FLIGHT. QRH HAS US TURN NWS SWITCH OFF. MSG EXTINGUISHED. NO NWS ON GROUND REGARDLESS OF NWS SWITCH POSITION. AIRCRAFT REMOVED FROM SERVICE R&R NLG STEERING HARNESS IAW CMM 32-60-01-R3, OPS TEST GOOD IAW 32-51. REF MX WORK C
- [SDR A6WA2019020246356](https://openairdocs.org/sdr/A6WA2019020246356.md): Warning System · activated · Jan 30, 2019 · N430AW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > DURING FERRY FLIGHT FROM ORD TO MKE, CREW REPORTED: AFTER TAKEOFF FLAPS FAIL AND STAB AND MACH TRIM CAUTION MSGS. FLAPS FAIL AT 8 DEGREES. CW QRH. STAB AND MACH TRIM RESET OK. LANDING WEIGHT 36000, MAX BTMS 2112. CREW PERFORMED AND AIR RETURN TO ORD FOR FURTH
- [SDR A6WA2018062945910](https://openairdocs.org/sdr/A6WA2018062945910.md): Angle · cracked · Jun 28, 2018 · N430AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CRACKED AT BS 280, LBL9, AFT OF THE BEAM. REPLACED THE ANGLE IAW SRM 51-42-06, AND 51-42-21.
- [SDR A6WA201845732](https://openairdocs.org/sdr/A6WA201845732.md): Intercostal · cracked · Mar 26, 2018 · N430AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT PRESSURE BULKHEAD AFT FACE HAS A CRACKED INTERCOSTAL AT STRINGER 14L. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-21, AND SRM 51-42-06.
- [SDR A6WA2018032645724](https://openairdocs.org/sdr/A6WA2018032645724.md): Riser · cracked · Mar 25, 2018 · N430AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT RISER IS CRACKED BY LOWER FIXED STEP.
- [SDR A6WA2018032645730](https://openairdocs.org/sdr/A6WA2018032645730.md): Plate · cracked · Mar 25, 2018 · N430AW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO STEP PLATE IS CRACKED AND HAS BROKEN HINGE TANGS.
- [SDR A6WA2018032645727](https://openairdocs.org/sdr/A6WA2018032645727.md): Step · cracked · Mar 22, 2018 · N430AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR UPPER STAIR AFT WEB REPAIR ANGLE IS CRACKED. REPLACED THE REPAIR ANGLE IAW REO 601R-52-11-279 REV-NC.
- [SDR A6WA2018032645726](https://openairdocs.org/sdr/A6WA2018032645726.md): Step · cracked · Mar 22, 2018 · N430AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR UPPER STAIR WEB, FWD REPAIR ANGLE IS CRACKED. REPLACED THE REPAIR ANGLE IAW REO 601R-52-11-279 REV-NC.
- [SDR A6WA2018032645723](https://openairdocs.org/sdr/A6WA2018032645723.md): Intercostal · cracked · Mar 21, 2018 · N430AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT PRESSURE BULKHEAD AFT FACE HAS A CRACKED INTERCOSTAL AT STRINGER 13L. REPLACED THE INTERCOSTAL IAW SRM 51-42-00, AND 51-42-21.
- [SDR A6WA2018032845720](https://openairdocs.org/sdr/A6WA2018032845720.md): Landing · cracked · Mar 20, 2018 · N430AW · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > PANEL 446BL LANDING IS CRACKED. REPLACED LANDING IAW CMM 20-42-06.
- [SDR A6WA2018032645719](https://openairdocs.org/sdr/A6WA2018032645719.md): Angle · cracked · Mar 19, 2018 · N430AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 621 TO 624, OBLIQUE ANGLE AT STRINGER 15R IS CRACKED. REPLACED THE OBLIQUE ANGLE IAW SRM 51-42-21.
- [SDR A6WA2018032245711](https://openairdocs.org/sdr/A6WA2018032245711.md): Floorbeam · corroded · Mar 19, 2018 · N430AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM LBL 9 BETWEEN FS 589 AND FS 605 CORRODED.
- [SDR A6WA2018032245704](https://openairdocs.org/sdr/A6WA2018032245704.md): Bracket · cracked · Mar 18, 2018 · N430AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RT MLG WW BRAKE PRESSURE TRANSDUCER HYD LINES BRACKET IS CRACKED. REPLACED.
- [SDR A6WA2018032245703](https://openairdocs.org/sdr/A6WA2018032245703.md): Bracket · cracked · Mar 18, 2018 · N430AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LT MLG WW BRAKE PRESSURE TRANSDUCER BRACKET CRACKED. REPLACED.
- [SDR A6WA2018032645718](https://openairdocs.org/sdr/A6WA2018032645718.md): Gusset · cracked · Mar 17, 2018 · N430AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT BS 719, GUSSET FOR THE NR 2 HYDRAULIC SYSTEM RACK IS CRACKED. REPLACED THE GUSSET IAW SRM 51-42-06.
- [SDR A6WA2018032245700](https://openairdocs.org/sdr/A6WA2018032245700.md): Fitting · cracked · Mar 17, 2018 · N430AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CLIP AT FS 484 AND RBL 36 CRACKED. REPLACED.
- [SDR A6WA2018032245701](https://openairdocs.org/sdr/A6WA2018032245701.md): Fitting · cracked · Mar 17, 2018 · N430AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CLIP AT FS 484 AND RBL 27 CRACKED. REPLACED.
- [SDR A6WA2018032645722](https://openairdocs.org/sdr/A6WA2018032645722.md): Drag Angle · cracked · Mar 16, 2018 · N430AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT RISER DRAG ANGLE IS CRACKED. REPAIRED THE DRAG ANGLE IAW REO601R-52-11-513 REV-B.
- [SDR A6WA2018032245707](https://openairdocs.org/sdr/A6WA2018032245707.md): Seat Track · corroded · Mar 16, 2018 · N430AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT NR 4 FLOOR SEAT TRACK CORRODED. REPLACED.
- [SDR A6WA2018032245706](https://openairdocs.org/sdr/A6WA2018032245706.md): Bracket · cracked · Mar 16, 2018 · N430AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RT MLG WW BRAKE PRESSURE TRANSDUCER BRACKET IS CRACKED. REPLACED.
- [SDR A6WA2018032245709](https://openairdocs.org/sdr/A6WA2018032245709.md): Seat Track · corroded · Mar 15, 2018 · N430AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT NR 1 FLOOR SEAT TRACK CORRODED. REPLACED.
- [SDR A6WA2018032245708](https://openairdocs.org/sdr/A6WA2018032245708.md): Seat Track · corroded · Mar 15, 2018 · N430AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT FLOOR NR 2 SEAT TRACK CORRODED. REPLACED.
- [SDR A6WA2018032645717](https://openairdocs.org/sdr/A6WA2018032645717.md): Gusset · cracked · Mar 14, 2018 · N430AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT SIDE HYDRAULIC SYSTEM, NR 2 EQUIPMENT RACK GUSSET IS CRACKED. REPLACED GUSSET AT BS 736, IAW SRM 51-42-06.
- [SDR A6WA2018032645716](https://openairdocs.org/sdr/A6WA2018032645716.md): Channel · cracked · Mar 14, 2018 · N430AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT HYDRAULIC SYSTEM, NR 2 EQUIPMENT RACK, C-CHANNEL CRACKED. REPAIRED CHANNEL IAW REO 601R-53-62-031 REV-A.
- [SDR A6WA2018032245702](https://openairdocs.org/sdr/A6WA2018032245702.md): Support Fitting · cracked · Mar 14, 2018 · N430AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BATHTUB FLOOR SUPPORT FITTING AT FS 431 AND LBL 9 CRACKED. REPLACED BATHTUB FITTING AT FS 431 AND LBL 9 IAW SRM 51-42-06 AND 51-42-21.
- [SDR A6WA2018032845733](https://openairdocs.org/sdr/A6WA2018032845733.md): Beam · cracked · Mar 13, 2018 · N430AW · Cndair CL6002B19 · Fuselage Main, Structure
  > BS 409+128 VERTICAL BEAM AT RBL 27 HAS A VISUAL INDICATION OF A CRACK ON LOWER INBD SIDE. REPAIRED THE VERTICAL BEAM IAW REO 601R-53-41-056, REV-F.
- [SDR A6WA2018032645721](https://openairdocs.org/sdr/A6WA2018032645721.md): Beam · cracked · Mar 13, 2018 · N430AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 409+128 FWD BULKHEAD VERTICAL BEAM AT RBL18 IS CRACKED. REPAIRED VERTICAL BEAM IAW REO601R-53-41-056 REV-F.
- [SDR A6WA2018032245705](https://openairdocs.org/sdr/A6WA2018032245705.md): Channel · cracked · Mar 12, 2018 · N430AW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR CAM TRACK SUPPORT LOWER CHANNEL AT FS 574 CRACKED. REPLACED.
- [SDR A6WA2018032645715](https://openairdocs.org/sdr/A6WA2018032645715.md): Skin · dented · Mar 11, 2018 · N430AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP LOWER SKIN HAS MULTIPLE DENTS. REPLACES THE FLAP LOWER SKIN IAW SRM 51-42-13.
- [SDR A6WA2018032645725](https://openairdocs.org/sdr/A6WA2018032645725.md): Frame · cracked · Mar 11, 2018 · N430AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 605 FLANGE IS CRACKED AT STRINGER 9L. REPLACED THE FRAME SECTION IAW SRM 51-42-06, 51-42-21, AND REO 601R-53-61-6504, REV-.
- [SDR A6WA2018032245710](https://openairdocs.org/sdr/A6WA2018032245710.md): Frame · chafed · Mar 6, 2018 · N430AW · Cndair CL6002B19 · Fuselage Main, Frame
  > PERFORM PERMANENT REPAIR FS718, STR17R & STR 16R. PERFORMED PERMANENT REPAIR IAW EA CRJ253-00905 REV-IR.
- [SDR A6WA2017111745429](https://openairdocs.org/sdr/A6WA2017111745429.md): Inverter · inoperative · Nov 16, 2017 · N430AW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT WILL NOT ILLUMINATE PAST ROW 8. FOUND LOW VOLTAGE AT SFT CABLE. R & R THE NR 4 INVERTER IAW AMM 33-51-07, OPS CHECKED GOOD.
- [SDR A6WA2017092945313](https://openairdocs.org/sdr/A6WA2017092945313.md): Connector · unsecure · Sep 29, 2017 · N430AW · Cndair CL6002B19 · Light System Wiring
  > DURING PRE-FLIGHT ACCEPTANCE, CREW REPORTED THAT THE FLOOR EMERGENCY LIGHTING WILL NOT ILLUMINATE FROM ROW 9 AFT. SECURED THE CONNECTOR AT ROW 12 IAW AMM 33-51-00, OPS CHECKED GOOD.
- [SDR A6WA201745274](https://openairdocs.org/sdr/A6WA201745274.md): None · none · Sep 12, 2017 · N430AW · Cndair CL6002B19 · Lighting System
  > 4261 FLOOR PATH EMERGENCY LIGHTS WILL NOT ILLUMINATE FROM ROW 8 TO 13 CW OP TEST OF EMERG LIGHTS IAW AMM SUPP 16-374A AND VISUAL INSP IAW AMM 33-51-01 ACFT GOOD FOR SERVICE
- [SDR A6WA2017083045245](https://openairdocs.org/sdr/A6WA2017083045245.md): Connector · unsecure · Aug 30, 2017 · N430AW · Cndair CL6002B19 · Light System Wiring
  > FLOOR EMERGENCY LIGHTS PAST ROW 8 WILL NOT ILLUMINATE. INSPECTED EMERGENCY LIGHTING AND FOUND CONNECTOR LOOSE AT ROW 12. SECURED THE CONNECTOR IAW AMM 33-51-00, OPS CHECKED GOOD.
- [SDR A6WA2017082445222](https://openairdocs.org/sdr/A6WA2017082445222.md): Wire Harness · loose · Aug 23, 2017 · N430AW · Cndair CL6002B19 · Light System Wiring
  > AFT HALF OF EMERERGENCY FLOOR LIGHTING DOES NOT ILLUMINATE. INSPECTED AND FOUND ROW 12 WIRE HARNESS ASSY LOOSE. ADJUSTED THE WIRE HARNESS, OPS CHECKED GOOD IAW AMM 33-51-00
- [SDR A6WA201745202](https://openairdocs.org/sdr/A6WA201745202.md): Wire Harness · defective · Aug 15, 2017 · N430AW · Cndair CL6002B19 · Light System Wiring
  > AFT FLOOR EMERGENCY LIGHT DO NOT TEST (ROW 8 AND AFT). REMOVED AND REPLACED AFT HARNESS AND CONNECTIONS IAW AMM 33-50-00. OPS CHECK GOOD.
- [SDR A6WA2017062645072](https://openairdocs.org/sdr/A6WA2017062645072.md): Connector · loose · Jun 23, 2017 · N430AW · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY LIGHT INOPERATIVE AFT OF ROW 9. INSPECTED THE EMERGENCY LIGHT AND FOUND A LOOSE CONNECTION. CONNECTED AND PERFORMED AN OPS CHECK IAW AMM 33-51-00, OPS CHECKED GOOD.
- [SDR A6WA201644241](https://openairdocs.org/sdr/A6WA201644241.md): Light · inoperative · Aug 17, 2016 · N430AW · Cndair CL6002B19 · Emergency Lighting
  > LAST SECTION OF EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE, ROW 9-12 REPORTED.
- [SDR A6WA201644119](https://openairdocs.org/sdr/A6WA201644119.md): Light · inoperative · Jul 17, 2016 · N430AW · Cndair CL6002B19 · Emergency Lighting
  > LOWER LEVEL EMERGENCY EXIT LIGHTS OUT, FROM ROW 9 & AFT.
- [SDR A6WA2016071944119](https://openairdocs.org/sdr/A6WA2016071944119.md): Connector · disconnected · Jul 17, 2016 · N430AW · Cndair CL600* · Light System Wiring
  > FLIGHT 3860. LOWER LEVEL EMERGENCY EXIT LIGHTS OUT, FROM ROW 9 & AFT. CONNECTED CONNECTOR ROW 12 & OPS CHECK IAW 12-032 & AMM 33-51-00.

Next page: https://openairdocs.org/aircraft/N430AW/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 = 'N430AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N430AW/reports

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