# Service difficulty reports: N830AY

A list on [N830AY](https://openairdocs.org/aircraft/N830AY.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR REXA2013121102297](https://openairdocs.org/sdr/REXA2013121102297.md): Flap · failed · Dec 11, 2013 · N830AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT 2 DEG ON APPROACH. PERFORMED RESET & OPERATIONS CHECKED IAW AD 2009-06-12 PARA H-6 SEE DISC NR 2 FOR MEL DEFERRAL.
- [SDR REXA2013061401186](https://openairdocs.org/sdr/REXA2013061401186.md): Coalescer Bag · odor · Jun 14, 2013 · N830AY · Cndair CL6002B19 · Humidity Control System
  > FUEL ODOR IN CABIN. R & R LT & RT WATER SEPARATOR COALESCER SOCKS, IAW AMM 21-10-00, 21-51-13, & 71-00-00.
- [SDR REXA2013060201046](https://openairdocs.org/sdr/REXA2013060201046.md): Bpsu · failed · Jun 2, 2013 · N830AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION MESSAGE WHEN SELECTING FLAPS FROM 0 TO 20 AFTER ENGINE START PERFORMED TROUBLESHOOTING IAW FIM REV 44 IAW AD 2009-06-12 PARA (H)(6)(I) AMOC DATED DECEMBER 07,2012,AND PA AD27-05 2L. R & R LT BPSU IAW AMM 27-51-10. OPC GOOD, COULD NOT DUPLICA
- [SDR REXA2013060201038](https://openairdocs.org/sdr/REXA2013060201038.md): Bpsu · failed · Jun 2, 2013 · N830AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > "FLAPS FAIL" CAUTION MESSAGE WHEN SELECTING FLAPS FROM 0 TO 20 AFTER ENGINE START. PERFORMED TROUBLESHOOTING IAW FIM REV 44 IAW AD 2009-06-12, PARA H.6.I AMOC DATED DECEMBER 07,2012, AND AD27-05 2L. R & R LT BPSU IAW AMM 27-51-10. OPS CHECK GOOD, COULD NOT D
- [SDR REXA2013033000412](https://openairdocs.org/sdr/REXA2013033000412.md): Structure · damaged · Mar 28, 2013 · N830AY · Cndair CL6002B19 · Vertical Stabilizer Miscellaneous Structure
  > VERTICAL STABILIZER HAS TOOL DAMAGE ON THE UPPER LEFT AROUND LEADING EDGE NUT PLATES BETWEEN SPAR STATION 110 AND 117.75 BETWEEN 0.003" AND 0.007". REPAIRED IAW BOMBARDIER REO 601R-55-31-231.
- [SDR REXA201303300041](https://openairdocs.org/sdr/REXA201303300041.md): Fitting · cracked · Mar 27, 2013 · N830AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 CLIPS INBOARD AND OUTBOARD CRACKED ON RBL 9, ALSO LOWER WEB CRACKED AT RBL 9 AND LBL 9 AND UPPER ANGLE CRACKED OUTBOARD OR RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-137 AND 601R-53-11-171.
- [SDR REXA2013032600407](https://openairdocs.org/sdr/REXA2013032600407.md): Stiffener · chafed · Mar 25, 2013 · N830AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD AEB VERTICAL STIFFENER AT BL 00 AND WL 126.43 HAS CHAFE DAMAGE THAT MESURES 0.275" X 0.090" X 0.015" DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-1523 AND 601R-53-61-4851.
- [SDR REXA2013032500406](https://openairdocs.org/sdr/REXA2013032500406.md): Bulkhead · damaged · Mar 24, 2013 · N830AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > ELEVEN SCREW/TOOL MARKS ON FWD FACE ABOVE FLOOR OF AFT PRESSURE BULKHEAD AT FS 621. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.
- [SDR REXA2013032500405](https://openairdocs.org/sdr/REXA2013032500405.md): Fitting · cracked · Mar 22, 2013 · N830AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT OUTBOARD FS 484 CLIP CRACKED. REPAIRED IAW SRM 51-42-21.
- [SDR REXA2013010500114](https://openairdocs.org/sdr/REXA2013010500114.md): Cover · cracked · Jan 5, 2013 · N830AY · Cndair CL6002B19 · Emergency Lighting
  > EXIT SIGN CRACKED AT ROW 1. REMOVED AND REPLACED EXIT SIGN COVER IAW AMM 33-20-00.
- [SDR REXA2012101501403](https://openairdocs.org/sdr/REXA2012101501403.md): Light · inoperative · Oct 15, 2012 · N830AY · Cndair CL6002B19 · Emergency Lighting
  > MAIN CABIN DOOR EMERGENCY LIGHT (WHITE) BY FLOOR HAS A COUPLE OF BULBS INOPERABLE. INSTALLED NEW BULBS.
- [SDR REXA2012009281371](https://openairdocs.org/sdr/REXA2012009281371.md): Engine · malfunctioned · Sep 28, 2012 · N830AY · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > ON FLIGHT 4021 DURING CLIMBOUT OF CLT AT 4000FT LOUD POP WAS HEARD, NR 1 ENGINE N1 AND N2 ROWED BACK WITH ITT SPIKE TO AROUND 960. THE CREW THEN PROCEEDED TO SHUTDOWN THE ENGINE WITHIN 1.5 MINUTES. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT.
- [SDR REXA2012071301156](https://openairdocs.org/sdr/REXA2012071301156.md): B-Nut · loose · Jul 13, 2012 · N830AY · Cndair CL6002B19 · Hydraulic System, Main
  > AIRCRAFT DIVERTED DUE TO NR 1 HYD QUANTITY LOSS. CREW REPORTED INTERMITTENT 1A AND 1B CAUTION MESSAGES WITH ERRATIC PRESSURE INDICATION AND THE NR 1 HYD QTY INDICATION. PRELIMINARY INVESTIGATION BY MAINTENANCE, FOUND THE NR 1 RESERVOIR QTY AT ZERO AND THE R
- [SDR REXA2012052600777](https://openairdocs.org/sdr/REXA2012052600777.md): Battery · unknown · May 26, 2012 · N830AY · Cndair CL6002B19 · Emergency Lighting
  > NR 2 EMERGENCY LIGHT BATTERY RS. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY IAW AMM 33-51-04.
- [SDR REXA201200149](https://openairdocs.org/sdr/REXA201200149.md): Wire · damaged · Jan 28, 2012 · N830AY · Cndair CL6002B19 · Ice/Rain Protection System Wiring
  > DIVERTED FOR RT WING ANTI-ICE CAUTION WOULD NOT EXTINGUISH WITH WING ANTI-ICE IN THE NORM OR STBY POSITION. T/S RT WING CAUTION IAW FIM 30-10-00. FOUND BAD WIRING ON RT MODULATION SOV CONNECTOR 2P3HA. RE-PIN WIRE IAW ESPM 20-17-10. OPS CHECK GOOD. A/C OK
- [SDR REXA201200142](https://openairdocs.org/sdr/REXA201200142.md): Wire · defective · Jan 28, 2012 · N830AY · Cndair CL6002B19 · Ice/Rain Protection System Wiring
  > FLIGHT DIVERTED FOR RT WING ANTI-ICE CAUTION WOULD NOT EXTINGUISH WITH WING ANTI-ICE IN THE NORM OR STBY POSITION. T/S RT WING CAUTION IAW FIM 30-10-00. FOUND BAD WIRING ON RT MODULATION SOV CONNECTOR 2P3HA. RE-PIN WIRE IAW ESPM 20-17-10. OPS CHECK GOOD.
- [SDR REXA201100224](https://openairdocs.org/sdr/REXA201100224.md): Seal · damaged · Apr 8, 2011 · N830AY · Cndair CL6002B19 · Passenger/Crew Doors
  > AIR RETURN FOR NOT PRESSURIZING, REPAIRED PAX DOOR SEAL IAW AMM 52-10-11. PRESSURE CHECKS GOOD, OK FOR SERVICE.
- [SDR REXA201000042](https://openairdocs.org/sdr/REXA201000042.md): Priority Valve · malfunctioned · Apr 5, 2010 · N830AY · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE ON APPROACH, INITIALLY NOSE DID NOT COME DOWN GEAR THEN DOWN AND 3 GREEN, UNEVENTFUL LANDING. FLT 4024 STA--MEM EMP--53431. REMOVED AND REPLACED NLG PRIORITY VALVE IAW AMM OPS CHECK GOOD DM CLEARED.
- [SDR REXA201000001](https://openairdocs.org/sdr/REXA201000001.md): Bpsu · failed · Jan 2, 2010 · N830AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION MESSAGE, FLAPS FAIL AT 20 DEGS. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I). PER AMOC DATED MARCH 27 2009 AND PA AD27-052F. REMOVED AND REPLACED LT BPSU IAW CRJ AMM 27-51-10. RIGGED LT BPSU I
- [SDR REXA200900144](https://openairdocs.org/sdr/REXA200900144.md): Amplifier · defective · Dec 29, 2009 · N830AY · Cndair CL6002B19 · Engine Controls
  > ON CLIMBOUT OF KDTW THE FLIGHT CREW NOTICED THE LT N1 INDICATION ACCELERATE TO 96.7 PERCENT. THE THRUST LEVER WAS REDUCED AND THE LT N1 DECREASED, BUT FLUCTUATED 20-25 PERCENT. ALL OTHER ENGINE PARAMETERS WERE NORMAL. THE FLIGHT CREW CONTACTED ATC, REQUESTE

## 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 = 'N830AY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N830AY/reports

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