# Service difficulty reports: N815CA, cancelled Dec 3, 2022

A list on [N815CA, cancelled Dec 3, 2022](https://openairdocs.org/deregistered/N815CA-2022-12-03.md).

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

- [SDR COMA2012061350042](https://openairdocs.org/sdr/COMA2012061350042.md): Downlock Sensor · failed · Jun 12, 2012 · N815CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > ON APPROACH INTO DAY DURING GEAR EXTENSION NOSE GEAR FAILED TO LOCK DOWN. RAN QRH, CYCLED GEAR OBSERVED NOSE DOOR INDICATION. EMERGENCY DECLARED, A/C LANDED SAFELY IN DAY. REMOVED AND REPLACED NLG DOWNLOCK NR 1 SENSOR. OPS CHECK GOOD.
- [SDR COMA2012032250023](https://openairdocs.org/sdr/COMA2012032250023.md): Frame · corroded · Mar 20, 2012 · N815CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME FS 589.00 IS CORRODED BELOW FLOOR. FRAME FS 589.00 WAS REPAIRED IAW BOMBARDIER REO 601R-53-61-4444.
- [SDR COMA2012032250022](https://openairdocs.org/sdr/COMA2012032250022.md): Floorbeam · corroded · Mar 20, 2012 · N815CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM FLANGE IS CORRODED BELOW FLOOR. FOORBEAM FLANGE WAS REPAIRED IAW BOMABARDIER REO 601R-53-21-2279.
- [SDR COMA2012032250021](https://openairdocs.org/sdr/COMA2012032250021.md): Frame · corroded · Mar 20, 2012 · N815CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME FS 605.00 IS CORRODED BELOW FLOOR. FRAME FS 605.00 WAS REPAIRED IAW BOMBARDIER REO 601R-53-61-4444.
- [SDR COMA2012032250020](https://openairdocs.org/sdr/COMA2012032250020.md): Angle · corroded · Mar 20, 2012 · N815CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR ANGLE FOUND TO BE CORRODED BEYOND SRM LIMITS. FLOOR ANGLE WAS REPAIRED IAW BOMBARDIER REO #601R53-41-1555.
- [SDR COMA2012032250019](https://openairdocs.org/sdr/COMA2012032250019.md): Sill · corroded · Mar 20, 2012 · N815CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE (DOOR SILL) IS CORRODED BELOW FLOOR. ANGLE WAS REPLACED IAW BOMBARDIER CRJ SRM 51-24-21, 51-24-36 AND 51-42-06.
- [SDR COMA2012032250018](https://openairdocs.org/sdr/COMA2012032250018.md): Floorbeam · corroded · Mar 20, 2012 · N815CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CAP FOUND TO BE CORRODED. R/H REPLACED FLOORBEAM CAP IAW CRJ SRM 51-42-06 AND 51-42-21.
- [SDR COMA2012032250017](https://openairdocs.org/sdr/COMA2012032250017.md): Floorbeam · corroded · Mar 20, 2012 · N815CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CAP FOUND TO BE CORRODED. LT REPLACED FLOORBEAM CAP IAW CRJ SRM 51-42-06 AND 51-42-21.
- [SDR COMA2011100550075](https://openairdocs.org/sdr/COMA2011100550075.md): Thrust Reverser · faulty · Oct 5, 2011 · N815CA · Cndair CL6002B19 · Engine Thrust Reverser
  > RECEIVED A RIGHT THRUST REVERSER UNLOCK MESSAGE DURING TAKEOFF AT MEM, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. DEFERRED THE RIGHT THRUST REVERSER PER MEL 78-30-01.
- [SDR COMA2011011050002](https://openairdocs.org/sdr/COMA2011011050002.md): Flap · failed · Jan 8, 2011 · N815CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ON LANDING IN DTW FLAPS FAILED AT 0 DEG. EMERGENCY DECLARED, A/C LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I0002, FLAPS FAIL CAUTION MESSAGE FOLLOW UP MAINTENANCE ACTION.
- [SDR COMA2010030850054](https://openairdocs.org/sdr/COMA2010030850054.md): Angle · cracked · Mar 6, 2010 · N815CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT CAP ANGLE CRACKED AT FS 559.00 RBL 18.00. REPAIRED CAP ANGLE AT FS 559.00 RBL 18.00 IAW REO 601R-53-41-260 AND DEVIATION REO 601R-53-41-609.
- [SDR COMA2010030250052](https://openairdocs.org/sdr/COMA2010030250052.md): Angle · cracked · Mar 2, 2010 · N815CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 559.00 LBL 18.00 CRACKED AT CAP ANGLE, IN BEND RADIUS. REPAIRED FS 559 CAP ANGLE AT LBL 18 IAW REO 601R-53-41-260 REV D DATED 17-SEP-2009.
- [SDR COMA2010022450046](https://openairdocs.org/sdr/COMA2010022450046.md): Bulkhead · cracked · Feb 24, 2010 · N815CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD WEB CRACKED AT CARGO DOOR TRACK ATTACH, LBL 27, FS 621. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1541, REV B.
- [SDR COMA2009030850098](https://openairdocs.org/sdr/COMA2009030850098.md): Adc · faulty · Mar 8, 2009 · N815CA · Cndair CL6002B19 · Air Data Computer
  > DURING TAKEOFF ROLL A 20 KNOTS SPLIT BETWEEN AIRSPEED INDICATORS. CREW DECLARED AN EMERGENCY AND ABORTED TAKEOFF. AIRCRAFT RETURNED TO THE GATE. REPLACED NR 2 AIR DATA COMPUTER.
- [SDR COMA2009010550056](https://openairdocs.org/sdr/COMA2009010550056.md): Transmitter · fluctuates · Jan 4, 2009 · N815CA · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > ON APPROACH, LT FLAP INDICATION FLUCTUATES. EMERGENCY DECLARED, ACFT LANDED SAFELY. REMOVED AND REPLACED LT FLAP POSITION TRANSMITTER.
- [SDR COMA2008112450008](https://openairdocs.org/sdr/COMA2008112450008.md): Flap System · failed · Nov 21, 2008 · N815CA · Cndair CL6002B16 · Trailing Edge Flap Control System
  > FLAPS FAILED AT 20 DEG WHEN SELECTED TO 30 DEG. ACFT LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I0002, FLAPS FAIL CAUTION MESSAGE FOLLOW UP MAINTENANCE ACTION.
- [SDR COMA0860151](https://openairdocs.org/sdr/COMA0860151.md): Flap · failed · Mar 1, 2008 · N815CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5104 - FLAPS FAIL CAUTION MESSAGE WHEN SELECTING FLAPS TO 8 DEGREES. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I0002, FLAPS FAIL CAUTION MESSAGE FOLLOW-UP MAINTENANCE ACTION.
- [SDR COMA0860150](https://openairdocs.org/sdr/COMA0860150.md): Pdu · faulty · Feb 28, 2008 · N815CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5669 - RECEIVED FLAP FAIL CAUTION. ABORTED APPROACH, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED SI-2-27I0002. REPLACED FLAP PDU. NO FURTHER DEFECTS.
- [SDR COMA0860054](https://openairdocs.org/sdr/COMA0860054.md): Priority Valve · faulty · Jan 7, 2008 · N815CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > FLIGHT 4982 - NOSE GEAR DISAGREE ON APPROACH INTO CVG. PERFORMED QRH, EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED NLG PRIORITY VALVE.
- [SDR COMA0760635](https://openairdocs.org/sdr/COMA0760635.md): Flap System · malfunctioned · Nov 9, 2007 · N815CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5006 - FLAPS FAILED AT 0 DEGREES ON APPROACH INTO LGA. AIRCRAFT LANDED SAFELY. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C) FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES.
- [SDR COMA0760309](https://openairdocs.org/sdr/COMA0760309.md): Flap · malfunctioned · Apr 10, 2007 · N815CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED A ZERO DEGREES DURING APPROACH. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.
- [SDR COMA0760251](https://openairdocs.org/sdr/COMA0760251.md): Unknown · unknown · Mar 13, 2007 · N815CA · Cndair CL6002B19 · Drag Control System
  > FLIGHT 5429 - CONFIG SPOILER MESSAGE ON TAKEOFF ROLL. ABORTED TAKEOFF AT 20 KTS, RETURNED TO GATE. PERFORMED FIM RESET AND PERFORMED SPOILER TEST AND GROUND FUNCTIONAL CHECK. NO FURTHER DEFECTS.
- [SDR COMA0760244](https://openairdocs.org/sdr/COMA0760244.md): Thermocouple · faulty · Mar 9, 2007 · N815CA · Cndair CL6002B19 · Engine Indicating System
  > FLIGHT 5693 - DURING TAKEOFF ROLL THE NR 1 ITT INDICATION FLUCTUATED, ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE LEFT ENGINE OUTBOARD THERMOCOUPLE ASSEMBLY.
- [SDR COMA0760087](https://openairdocs.org/sdr/COMA0760087.md): Idg · faulty · Jan 28, 2007 · N815CA · Cndair CL6002B19 · AC Generation System
  > FLIGHT 5117 - RECEIVED IDG NR 1 CAUTION DURING 2 TAKEOFF ATTEMPTS AT 85 PERCENT N1. REPLACED NR 1 IDG, NO FURTHER DEFECTS.
- [SDR COMA0760077](https://openairdocs.org/sdr/COMA0760077.md): Drive Shaft · damaged · Jan 26, 2007 · N815CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5620 - RECEIVED FLAP FAIL MESSAGE AT 8 DEGREES. DECLARED EMERGENCY, FOLLOWED QRH AND LANDED WITHOUT INCIDENT. REPLACED LEFT WING NR 1 FLEX DRIVE SHAFT.
- [SDR COMA0760076](https://openairdocs.org/sdr/COMA0760076.md): Shaft · damaged · Jan 26, 2007 · N815CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5620 - RECEIVED FLAP FAIL MESSAGE AT 8 DEGREES. DECLARED EMERGENCY, FOLLOWED QRH AND LANDED WITHOUT INCIDENT. REPLACED LEFT WING NR 3 FLEX DRIVE SHAFT.
- [SDR COMA0660626](https://openairdocs.org/sdr/COMA0660626.md): Actuator · failed · Nov 9, 2006 · N815CA · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLIGHT 5609 - FLAPS FAILED AT 11 DEGREES AT GATE. REMOVED AND REPLACED LEFT OUTER FLAP INBOARD ACTUATOR.
- [SDR COMA0660507](https://openairdocs.org/sdr/COMA0660507.md): Connector · failed · Aug 23, 2006 · N815CA · Cndair CL6002B19 · Light System Wiring
  > FLIGHT 5157 - THE EMERGENCY FLOOR LEVEL EXIT PATH LIGHTING FAILED TEST. REPAIRED FLOOR LEVEL LIGHT STRIP CONNECTORS NEAR CENTER CABIN.
- [SDR COMA0660432](https://openairdocs.org/sdr/COMA0660432.md): Bpsu · faulty · Jul 15, 2006 · N815CA · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLIGHT 5591 - EN ROUTE JFK-BOS RECEIVED A FLAP CAUTION MESSAGE AT ZERO DEGREES, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LEFT BPSU.
- [SDR COMA0560175](https://openairdocs.org/sdr/COMA0560175.md): Outflow Valve · malfunctioned · Mar 12, 2005 · N815CA · Cndair CL6002B19 · Pressure Regulator/Outflow Valve
  > FLIGHT 5152 AIRCRAFT FAILED TO PRESSURIZE DURING CLIMBOUT OF CVG, AIRCRAFT RETURNED TO THE FIELD. REPLACED THE PRIMARY OUTFLOW VALVE.
- [SDR COMA0460046](https://openairdocs.org/sdr/COMA0460046.md): Angle · cracked · Jan 9, 2004 · N815CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE INTERCOSTAL FLANGES AT BL 36 LT AND RT AND ATTACH ANGLE AT LBL 27 AT FS 484.0, WL 70 TO WL 73 ARE CRACKED. REMOVED THE CRACKED ANGLE AND CUT OFF THE CRACKED FLANGED, FABRICATED AND INSTALLED REPAIR ANGLES IAW WVAC EO 601R-53-4532.
- [SDR COMA0460027](https://openairdocs.org/sdr/COMA0460027.md): Skin · corroded · Jan 8, 2004 · N815CA · Cndair CL6002B19 · Wing, Plate/Skin
  > THE LEFT WING LOWER PLANK ACCESS HOLE CUTOUTS HAVE CORROSION AT 540CB AND 550 AB. REMOVED THE CORROSION AND RESTORED SURFACE FINISH IAW REO 601R-57-21-030 REV C.
- [SDR COMA0460026](https://openairdocs.org/sdr/COMA0460026.md): Floor Support · cracked · Jan 7, 2004 · N815CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE UNDER FLOOR SUPPORT ANGLE P/N 601R35031-239 IS CRACKED AT FS 621.9 WL 73, LBL 41.5 AND RBL 41.5. REMOVED THE CRACKED AREAS AND INSTALLED REPAIR PARTS IAW REO 601R-53-61.117 REV.B.
- [SDR COMA0460006](https://openairdocs.org/sdr/COMA0460006.md): Warning Light · illuminated · Dec 31, 2003 · N815CA · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLIGHT 5937 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
- [SDR COMA0360578](https://openairdocs.org/sdr/COMA0360578.md): Pump · malfunctioned · Dec 26, 2003 · N815CA · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > FLIGHT 5039 HYDRAULIC NR 2 LOW PRESSURE CAUTION. REPLACED THE RT ENGINE HYDRAULIC PUMP.
- [SDR COMA0360272](https://openairdocs.org/sdr/COMA0360272.md): Warning System · activated · Jun 11, 2003 · N815CA · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLIGHT 5142 FLAP FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
- [SDR COMA0360129](https://openairdocs.org/sdr/COMA0360129.md): Sensing Element · malfunctioned · Mar 1, 2003 · N815CA · Cndair CL6002B19 · Pitot/Static Anti-Ice System
  > FLIGHT 5578 ANTI-ICE DUCT WARNING MESSAGE.REPLACED FUSELAGE SECTION OF BLEED LEAK SENSING ELEMENTS.
- [SDR COMA0360117](https://openairdocs.org/sdr/COMA0360117.md): Element · Feb 22, 2003 · N815CA · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > FLIGHT 9959 ANTI ICE DUCT WARNING MESSAGE.FOUND DUCT LEAK SENSING ELEMENT POSITIONED TO CLOSE TO BLEED AIR DUCT. REPOSITIONED ELEMENT.
- [SDR COMA0260160](https://openairdocs.org/sdr/COMA0260160.md): Power Unit · malfunctioned · Mar 5, 2002 · N815CA · Cndair CL6002B19 · Engine Thrust Reverser
  > FLIGHT 5786 R/H ENGINE REVERSE UNLOCKED DURING FLIGHT.REPLACED THE R/H ENGINE PDU
- [SDR COMA0160981](https://openairdocs.org/sdr/COMA0160981.md): Bpsu · malfunctioned · Dec 23, 2001 · N815CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5296 - FLAPS FAILED AT 30 DEGREES.REPALCED THE R/H BPSU.
- [SDR COMA0160982](https://openairdocs.org/sdr/COMA0160982.md): Pcu · malfunctioned · Dec 22, 2001 · N815CA · Cndair CL6002B19 · Drag Control System
  > FLIGHT 5280 - DURING TAXI THE LEFT SPOILERON DEPLOYED UNCOMMANDED AND WOULD NOT RETRACT.REPLACED THE L/H SPOILERON OUTBD PCU.
- [SDR COMA0160868](https://openairdocs.org/sdr/COMA0160868.md): Flap · Nov 4, 2001 · N815CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT #5515. FLAPS FAILED AT 30 DEGREES DURING APPROACH.RESET THE FLAP SYSTEM PER AD 98-20-01 AND DEFERRED FURTHER MAINTENANCE.
- [SDR COMA0160788](https://openairdocs.org/sdr/COMA0160788.md): Flap · failed · Oct 7, 2001 · N815CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5671, FLAPS FAILED AT 30 DEGREES DURING LANDING APPROACH. RESET THE FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. A/C CONTINUED SERVICE.
- [SDR COMA0160740](https://openairdocs.org/sdr/COMA0160740.md): Computer · faulty · Sep 20, 2001 · N815CA · Cndair CL6002B19 · Drag Control System
  > FLIGHT #5449. DURING TAXI OUT RECEIVED A SPOILERON FAULT MESSAGE, AIRCRAFT RETURNED TO THE GATE.REPLACED THE SPOILERON ELECTRONIC CONTROL UNIT.
- [SDR COMA0160719](https://openairdocs.org/sdr/COMA0160719.md): Idg · faulty · Sep 13, 2001 · N815CA · Cndair CL6002B19 · Alternator-Generator Drive
  > FLIGHT #5098. ABORTED TAKE OFF AT 50KTS DUE TO #1 IDG CAUTION MESSAGE, AIRCRAFT RETURNED TO THE GATE.REPLACED THE #1 ITEGRATED DRIVE GENERATOR.
- [SDR COMA0160239](https://openairdocs.org/sdr/COMA0160239.md): Fcu · malfunctioned · Feb 11, 2001 · N815CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU.
- [SDR COMA0061062](https://openairdocs.org/sdr/COMA0061062.md): Computer · malfunctioned · Dec 17, 2000 · N815CA · Cndair CL6002B19 · Stall Warning System
  > STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER.
- [SDR COMA0060945](https://openairdocs.org/sdr/COMA0060945.md): Computer · malfunctioned · Nov 20, 2000 · N815CA · Cndair CL6002B19 · Stall Warning System
  > STALL FAIL MESSAGE DURING T/O. RESET STALL COMPUTER.
- [SDR COMA0060750](https://openairdocs.org/sdr/COMA0060750.md): Computer · failed · Sep 17, 2000 · N815CA · Cndair CL6002B19 · Stall Warning System
  > STALL FAIL CAUTION MESSAGE DURING TAKEOFF ROLL, AIRCRAFT RETURNED TO THE GATE. RESET THE STALL COMPUTER.

## 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 = 'N815CA' AND deregistration_id = 'N815CA-2022-12-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N815CA-2022-12-03/reports

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