# Service difficulty reports: N949CA, cancelled Oct 19, 2007

A list on [N949CA, cancelled Oct 19, 2007](https://openairdocs.org/deregistered/N949CA-2007-10-19.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 2 · 90 reports

- [SDR COMA0660588](https://openairdocs.org/sdr/COMA0660588.md): Anti-Ice System · warning light · Oct 27, 2006 · N949CA · Cndair CL6002B19 · Ice/Rain Protection System
  > FLIGHT 5644 - ANTI-ICE DUCT MESSAGE AFTER TAKEOFF FROM CVG. AIRCRAFT RETURNED TO CVG AND LANDED WITHOUT INCIDENT. INSPECTED FORWARD FUSELAGE LOOPS AND PERFORMED OPS CHECK, CHECKS GOOD (CND).
- [SDR COMA0660490](https://openairdocs.org/sdr/COMA0660490.md): Circuit Breaker · malfunctioned · Aug 14, 2006 · N949CA · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > FLIGHT 5470 - DURING FLAP SELECTION FROM 8 DEGREES, RECEIVED 3B HYD PUMP CAUTION MESSAGE. CREW DECLARED AN EMERGENCY, LANDED WITHOUT INCIDENT. FOUND 3B CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER, PERFORMED OPS CHECK PER AMM, NO FURTHER DEFECTS NOTED.
- [SDR COMA0660370](https://openairdocs.org/sdr/COMA0660370.md): Flap · malfunctioned · Jun 1, 2006 · N949CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5480 - FLAP FAIL MESSAGE AFTER LANDING IN HSV, FAILED AT 20 DEGREES. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.
- [SDR COMA0660357](https://openairdocs.org/sdr/COMA0660357.md): Flap · malfunctioned · May 23, 2006 · N949CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 4997 - FLAP FAIL CAUTION MESSAGE WHILE IN CRUISE FLIGHT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION PARAGRAPH (B) 1, 2, 3, (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.
- [SDR COMA0660353](https://openairdocs.org/sdr/COMA0660353.md): Flap · malfunctioned · May 19, 2006 · N949CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5296 - DURING APPROACH RECEIVED FLAP FAIL MESSAGE AT 20 DEGREES, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLA
- [SDR COMA0660318](https://openairdocs.org/sdr/COMA0660318.md): Caution Message · illuminated · Apr 30, 2006 · N949CA · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLIGHT 5581 - FLAP FAIL CAUTION MESSAGE WHILE SITTING AT GATE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT, MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3, (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.
- [SDR COMA0660306](https://openairdocs.org/sdr/COMA0660306.md): Flap System · malfunctioned · Apr 17, 2006 · N949CA · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLIGHT 5199 - FLAP FAIL CAUTION MESSAGE CAME ON DURING TAXI. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3, (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.
- [SDR COMA0560685](https://openairdocs.org/sdr/COMA0560685.md): Flap System · malfunctioned · Dec 12, 2005 · N949CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5130- DURING LANDING AT MSG RECEIVED A FLAP FAIL MESSAGE AT 45 DEGREES. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A,B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES
- [SDR COMA0560544](https://openairdocs.org/sdr/COMA0560544.md): Battery · discharged · Oct 10, 2005 · N949CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5903 - EMERGENCY FLOOR LIGHTNING INOPERABLE ROWS 9 TO 13. REPLACED THE EMERGENCY BATTERY.
- [SDR COMA0560515](https://openairdocs.org/sdr/COMA0560515.md): Bulkhead · cracked · Sep 21, 2005 · N949CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > WHILE PERFORMING TASK CRJ-2-162014, DETAILED INSPECTION OF THE PRESSURE BULKHEAD WEBS AND VERTICAL BEAMS AT FS 559.0, TWO CRACKS WERE DISCOVERED IN THE BULKHEAD WEB RADIATING FROM THE HOLES FOR THE ATTACH BOLTS OF THE RIGHT AILERON CONTROL CABLE REAR QUADRANT
- [SDR COMA0560049](https://openairdocs.org/sdr/COMA0560049.md): Controller · malfunctioned · Jan 11, 2005 · N949CA · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > FLIGHT 5147 WING OVERHEAT MESSAGE. REPLACED THE CONTROLLER.
- [SDR COMA0560026](https://openairdocs.org/sdr/COMA0560026.md): Connector · defective · Jan 3, 2005 · N949CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5198, EMERGENCY FLOOR PATH LIGHTING INOP AT ROW 2 THRU 5. REPLACED WIRE CONNECTOR.
- [SDR COMA0460568](https://openairdocs.org/sdr/COMA0460568.md): Selector Valve · unreliable · Oct 3, 2004 · N949CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > FLIGHT 5994 GEAR DISAGREE WARNING. REPLACED THE NLG SELECTOR VALVE.
- [SDR COMA0460528](https://openairdocs.org/sdr/COMA0460528.md): Reservoir · inoperative · Sep 11, 2004 · N949CA · Cndair CL6002B19 · Hydraulic Reservoir, Main
  > FLIGHT 5492 GEAR DISAGREE WARNING. REPLACED THE SYSTEM 3 HYDRAULIC RESERVOIR.
- [SDR COMA0460392](https://openairdocs.org/sdr/COMA0460392.md): Computer · malfunctioned · Jun 28, 2004 · N949CA · Cndair CL6002B19 · Drag Control System
  > FLIGHT 5546 STAB TRIM AND MACH TRIM CAUTION. RESET HSTCU, COULD NOT DUPLICATE, OPERATIONAL CHECK NORMAL.
- [SDR COMA0460011](https://openairdocs.org/sdr/COMA0460011.md): Warning Light · illuminated · Jan 2, 2004 · N949CA · Cndair CL6002B19 · Engine Thrust Reverser
  > FLIGHT 5682 RIGHT THRUST REVERSER UNLOCK INFLIGHT. SECURED AND DEFERRED MAINT PER MEL.
- [SDR COMA0360564](https://openairdocs.org/sdr/COMA0360564.md): Windshield · cracked · Dec 18, 2003 · N949CA · Cndair CL6002B19 · Flight Compartment Windows
  > FLIGHT 5815 CO-PILOTS WINDSHIELD CRACKED. REPLACED WINDSHIELD.
- [SDR COMA0360537](https://openairdocs.org/sdr/COMA0360537.md): Wire · loose · Dec 6, 2003 · N949CA · Cndair CL6002B19 · Emergency Lighting
  > THE AFT SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOP. SECURED LOOSE WIRING CONNECTION.
- [SDR COMA0360504](https://openairdocs.org/sdr/COMA0360504.md): Frame · cracked · Nov 13, 2003 · N949CA · Cndair CL6002B19 · Fuselage Main, Frame
  > RT 718 FRAME FLANGE CRACKED BELOW STRINGER 10. REPAIRED FRAME IN ACCORDANCE WITH REO 601R-53-61-193.
- [SDR COMA0460314](https://openairdocs.org/sdr/COMA0460314.md): Skin Panel · cracked · Nov 6, 2003 · N949CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > PRESSURE FLOOR SKIN HAS CRACK AT FS 461.00. REPAIRED IN ACCORDANCE WITH REO 601R-53-41-102.
- [SDR COMA0360502](https://openairdocs.org/sdr/COMA0360502.md): Floor Panel · cracked · Nov 6, 2003 · N949CA · Cndair CL6002B19 · Fuselage Floor Panel
  > PRESSURE FLOOR SKIN HAS CRACK AT FS 461.00. REPAIRED IN ACCORDANCE WITH REO 601R-53-41-102.
- [SDR COMA0360289](https://openairdocs.org/sdr/COMA0360289.md): Idg · malfunctioned · Jun 24, 2003 · N949CA · Cndair CL6002B19 · Alternator-Generator Drive
  > FLIGHT 5304 LEFT IDG CAUTION MESSAGE DURING T/O. DEFERRED MAINT PER MEL.
- [SDR COMA0260711](https://openairdocs.org/sdr/COMA0260711.md): Power Cable · inoperative · Dec 12, 2002 · N949CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5893 EMERGENCY FLOOR PATH LIGHTING IS INOP.REPLACED TRACK LIGHTING POWER STRIPS.
- [SDR COMA0260591](https://openairdocs.org/sdr/COMA0260591.md): Lamp · Oct 15, 2002 · N949CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5480 EMERGENCY FLOOR LIGHT AT ROW 3 IS INOP.DEFERRED MAINT PER MEL
- [SDR COMA0260538](https://openairdocs.org/sdr/COMA0260538.md): Lamp · Sep 18, 2002 · N949CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5284 1 SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOP.DEFERRED MAINT PER MEL.
- [SDR COMA0260501](https://openairdocs.org/sdr/COMA0260501.md): Cart · Aug 29, 2002 · N949CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > A/C FUSELAGE STRUCK BY BAGGAGE CART AND SUSTAINED MAJOR DAMAGE BETWEEN F.S. 654 AND 672, AND STRINGERS 21L TO 23L.C/W REPAIR TO SKIN AND STRINGERS I/A/W SRM 53-00-31 AND 53-00-03 AND REO 601R 53-61-577 AND 579.
- [SDR COMA0260393](https://openairdocs.org/sdr/COMA0260393.md): Seal · leaking · Jun 28, 2002 · N949CA · Cndair CL6002B19 · Engine Oil System (Airframe Furnished)
  > FLIGHT 5298 LEFT ENGINE OIL PRESSURE WARNING AFTER T/O, AIRCRAFT RETURNED TO MSP. (IFSD)REPLACED ACCESSORY GEAR BOX OIL SEALS AT AXIS D&F.
- [SDR COMA0260220](https://openairdocs.org/sdr/COMA0260220.md): Door · Mar 31, 2002 · N949CA · Cndair CL6002B19 · Passenger/Crew Doors
  > FLIGHT 5472 CABIN DOOR WARNING.COULD NOT DUPLICATE OPERATIONAL CHECK OF DOOR NORMAL. NO FAULT CODES IN COMPUTER.
- [SDR COMA0160825](https://openairdocs.org/sdr/COMA0160825.md): Window · fractured · Oct 16, 2001 · N949CA · Cndair CL6002B19 · Flight Compartment Windows
  > FLIGHT 5903. PILOT'S SIDE WINDOW SHATTERED AT 29,000 FT.REPLACED THE PILOT'S SIDE WINDOW.
- [SDR COMA0160729](https://openairdocs.org/sdr/COMA0160729.md): Angle · cracked · Sep 14, 2001 · N949CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LEFT SIDE INBOARD ANGLE AT F.S. 484.0 LBL 9 UNDER FLOOR PANEL 261CLF IS CRACKED.REPAIRED THE ANGLE AT FS 484.0 LBL9 I/A/W WVAC EO 601R-53-2711A.
- [SDR COMA0160728](https://openairdocs.org/sdr/COMA0160728.md): Angle · cracked · Sep 14, 2001 · N949CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LEFT SIDE INBOARD ANGLE AT F.S. 484.0 LBL 27 UNDER FLOOR PANEL 261DLF IS CRACKED.REPAIRED THE ANGLE AT F.S. 484.0 LBL27 I/A/W WVAC EO 601R-53-2711A.
- [SDR COMA0160727](https://openairdocs.org/sdr/COMA0160727.md): Angle · cracked · Sep 14, 2001 · N949CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RIGHT SIDE ELEVATER AND RUDDER PULLEY SUPPORT BRACKET AT F.S. 484.0 UNDER FLOOR PANEL 262DRF IS CRACKED.REPAIRED THE RIGHT SIDE ELEVATER AND RUDDER SUPPORT BRACKET AT F.S. 484.0 I/A/W WVAC EO 601R-53-2711A.
- [SDR COMA0160708](https://openairdocs.org/sdr/COMA0160708.md): Cap · chafed · Sep 11, 2001 · N949CA · Cndair CL6002B19 · Leading Edge Slat Control System
  > THE L/H AND R/H INBOARD FLAP LEADING EDGE INBOARD VANE CAPS ARE CHAFED WHERE THEY CONTACT THE TEFLON BUMPER PADS.REMOVED THE CHAFED INBOARD VANE CAPS. INSTALLED NEW VANE CAPS L/H (601R14303-53S) AND R/H (601R14303-54) IAW WVAC EO 601R-57-2706.
- [SDR COMA0160707](https://openairdocs.org/sdr/COMA0160707.md): Cap · chafed · Sep 11, 2001 · N949CA · Cndair CL6002B19 · Leading Edge Slat Control System
  > THE R/H INBOARD FLAP LEADING EDGE VANE CAP MIDDLE SKIN IS CHAFED WHERE THE FLAP CONTACTS THE TEFLON BUMPER PAD.REMOVED THE CHAFED MIDDLE VANE CAP. INSTALLED A NEW CAP (P/N 601R14303-10) IAW AERODESIGN ENGINEERING REPORT NO. 1286-1.
- [SDR COMA0160706](https://openairdocs.org/sdr/COMA0160706.md): Bushing · worn · Sep 10, 2001 · N949CA · Cndair CL6002B19 · Vertical Stabilizer, Attach Fittings
  > HORIZONTAL STABILIZER RHS VERTICLE BUSHING WORN.REMOVED R/H VERTICAL STAB BUSHING P/N 600-21061 INSTALLED NEW BUSHING ALT P/N 600-21061-7/SB I/A/W CRJ MM 20-26-00-910-803 FINAL REAMED BUSHING 1.50 I/A/W CANADAIR REO 601R-55-11-022 MACHINED BUSHING HAT I/A/W WV
- [SDR COMA0160552](https://openairdocs.org/sdr/COMA0160552.md): Web · cracked · Aug 5, 2001 · N949CA · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > ENGINE SUPPORT BEAM LOWER WEB CRACKED ON LEFT SIDE.PERFORMED A MAJOR REPAIR TO ENGINE SUPPORT BEAM LOWER NIB I/A/W CANADAIR REO 601R-53-61-366 REV C.
- [SDR COMA0160554](https://openairdocs.org/sdr/COMA0160554.md): Web · cracked · Aug 5, 2001 · N949CA · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > ENGINE SUPPORT BEAM LOWER WEB CRACKED ON RIGHT SIDE.PERFORMED A MAJOR REPAIR TO ENGINE SUPPORT BEAM LOWER WEB I/A/W CANADAIR REO 601R-53-61-366 REV C.
- [SDR COMA0160553](https://openairdocs.org/sdr/COMA0160553.md): Web · cracked · Aug 5, 2001 · N949CA · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > ENGINE SUPPORT BEAM IS CRACKED ON CENTER OF TOP WEB.PERFORMED A TEMPORARY MAJOR REPAIR TO CRACKED ENGINE SUPPORT BEAM I/A/W CANADAIR REO 601R-53-61-315 REV B.
- [SDR COMA0160210](https://openairdocs.org/sdr/COMA0160210.md): Warning Light · illuminated · Feb 6, 2001 · N949CA · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAP FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE IAW AD 98-20-01.
- [SDR COMA0160128](https://openairdocs.org/sdr/COMA0160128.md): Carbon Seal · leaking · Jan 17, 2001 · N949CA · Cndair CL6002B19 · Turbine Engine Oil System
  > LEFT ENGINE OIL PRESSURE FLUCTUATING BETWEEN 30 AND 48 PSI. REPLACED THE ACCESSORY DRIVES CARBON SEALS.
- [SDR COMA0160092](https://openairdocs.org/sdr/COMA0160092.md): Bulb · burned out · Jan 8, 2001 · N949CA · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT AT ROW 5 IS INOP. REPLACED LIGHT BULB.
- [SDR COMA0061023](https://openairdocs.org/sdr/COMA0061023.md): Warning System · malfunctioned · Dec 7, 2000 · N949CA · Cndair CL6002B19 · Pitot/Static Anti-Ice System
  > STANDBY PITOT HEAT CAUTION MESSAGE. REPLACED THE NR 3 ADSHC.
- [SDR COMA0060897](https://openairdocs.org/sdr/COMA0060897.md): Seal · damaged · Nov 8, 2000 · N949CA · Cndair CL6002B19 · Passenger/Crew Doors
  > LOUD SQUEAL FROM CABIN DOOR AREA. REPAIRED DOOR SEAL NIB DAMAGE I/A/W REO 601R-5211-108.
- [SDR COMA0060868](https://openairdocs.org/sdr/COMA0060868.md): Frame · damaged · Nov 1, 2000 · N949CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME WEB DAMAGED AT FS 654.5 BETWEEN STRINGER 21B AND 22B LEFT HAND. CAUSED BY ELECTRICAL ARCING AT APU GROUND CABLE (N1232). REMOVED DAMAGED FRAME SECTION AND SPLICED IN A NEW SECTION IAW REO 601R-53-61-301.
- [SDR COMA0060874](https://openairdocs.org/sdr/COMA0060874.md): Battery · discharged · Oct 28, 2000 · N949CA · Cndair CL6002B19 · Battery/Charger System
  > APU BATTERY AT ZERO VOLTS, APU BATTERY CHARGER IS INTERMITTENT. APU GROUND CABLE ARCHING AT GROUND STUD N1232, WHICH CAUSED SUBSTANTIAL DAMAGE AT FRAME 654.5. REPAIRED DAMAGED FRAME AND RELOCATED GROUND STUD IAW S/B 601R-49-014.
- [SDR COMA0060792](https://openairdocs.org/sdr/COMA0060792.md): Connector · loose · Oct 2, 2000 · N949CA · Cndair CL6002B19 · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS AND SIGNS ARE INOP, FWD CABIN AREA. SECURED LOOSE CONNECTION AT FLOOR TRACK LIGHTING.
- [SDR COMA0060754](https://openairdocs.org/sdr/COMA0060754.md): Transducer · failed · Sep 15, 2000 · N949CA · Cndair CL6002B19 · Stall Warning System
  > STALL FAIL CAUTION MESSAGE DURING TAKEOFF, AIRCRAFT RETURNED TO THE GATE. REPLACED THE NR 1 AOA TRANSDUCER.
- [SDR COMA0060720](https://openairdocs.org/sdr/COMA0060720.md): Angle · corroded · Sep 10, 2000 · N949CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE FWD J ANGLE AT FS 280 BETWEEN LBL 9.0 AND RBL 9.0 IS CORRODED. PERFORMED A MAJOR REPAIR BY REPLACING CORRODED FWD J ANGLE AT FS 280 BETWEEN LBL 9.0 AND RBL 9.0 IAW WVAC EO 601R-53-1681.
- [SDR COMA0060719](https://openairdocs.org/sdr/COMA0060719.md): Floorbeam · damaged · Sep 10, 2000 · N949CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > THE OUTBOARD FLANGE OF THE BEAM AT RBL 9.0 AND FS 409 + 8 WAS PREVIOUSLY REPAIRED. THIS EO PROVIDES FOR MODIFYING THE SPLICE ANGLE TO ACCOMODATE THE REPAIR. PERFORMED A MAJOR REPAIR TO THE OUTBOARD FLANGE OF THE BEAM AT RBL 9.0 AND FS 409 + 8 IAW WVAC EO 601
- [SDR COMA0060718](https://openairdocs.org/sdr/COMA0060718.md): Floorbeam · damaged · Sep 10, 2000 · N949CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > DURING ACCOMPLISHMENT OF SB 601R-53-037 REV A, THE I/B FLANGE OF THE FLOORBEAM AT RBL 27.0 FS 409 + 8 WAS FOUND TO HAVE A PREVIOUS REPAIR. PERFORMED A MAJOR REPAIR BY REMOVING EXISTING REPAIR AND INSTALLING A SPLICE ANGLE ON FLOORBEAM RBL 27.0 FS 409 + 8 IAW

Next page: https://openairdocs.org/deregistered/N949CA-2007-10-19/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 = 'N949CA' AND deregistration_id = 'N949CA-2007-10-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N949CA-2007-10-19/reports

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