# Service difficulty reports: N918CA, cancelled Mar 9, 2011

A list on [N918CA, cancelled Mar 9, 2011](https://openairdocs.org/deregistered/N918CA-2011-03-09.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 3 · 114 reports

- [SDR COMA2009062950166](https://openairdocs.org/sdr/COMA2009062950166.md): Bulkhead · cracked · Jun 29, 2009 · N918CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 202.75 FWD PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE CUTOUT. REPAIRED PER REO 601R-53-11 AND EA 10-5311-02657.
- [SDR COMA0860327](https://openairdocs.org/sdr/COMA0860327.md): Stiffener · cracked · Jul 20, 2008 · N918CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING MID CK 8, INSPECTION FOUND.25 INCH CRACK ON INBOARD SIDE LOWER END, OF VERTICAL STIFFENER, AT RBL 18, FS 559. CUT OUT DAMAGE AND INSTALLED DOUBLER PER BOMBARDIER REO 601R-53-41-067. (A)
- [SDR COMA0860319](https://openairdocs.org/sdr/COMA0860319.md): Frame · cracked · Jul 8, 2008 · N918CA · Cndair CL6002B19 · Fuselage Main, Frame
  > DURING FA 640 FRAME INSPECTION FOUND 640 FRAME CRACKED ON LT SIDE AT STRINGER 9 CUTOUT. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH REO 601R-53-61-557. (A)
- [SDR COM2008F00002](https://openairdocs.org/sdr/COM2008F00002.md): Frame · cracked · Jul 8, 2008 · N918CA · Cndair CL6002B19 · Fuselage Main, Frame
  > DURING FS 640 FRAME INSPECTION FOUND 640 FRAME CRACKED ON LT SIDE AT STRINGER 9 CUTOUT. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH REO 601R-53-61-557. (S)
- [SDR COMA0860311](https://openairdocs.org/sdr/COMA0860311.md): Circuit Breaker · tripped · Jun 28, 2008 · N918CA · Cndair CL6002B19 · Hydraulic Power System Wiring
  > RECEIVED A GEAR DISAGREE AND HYDRAULIC PUMP 3B WARNING DURING CLIMBOUT OF JFK, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. RESET CIRCUIT BREAKER FOR HYDRAULIC PUMP 3B AND PERFORMED GEAR SWINGS, NO DEFECTS NOTED. (S)
- [SDR COMA0860116](https://openairdocs.org/sdr/COMA0860116.md): Connector · loose · Feb 9, 2008 · N918CA · Cndair CL6002B19 · Door System Wiring
  > FLIGHT 5311 - RECEIVED PAX DOOR OUTER HANDLE CAUTION MESSAGE. DIVERTED TO GSP, LANDED WITHOUT INCIDENT. FOUND CARGO DOOR HARNESS CONNECTOR LOOSE. REMOVED, CLEANED AND REINSTALLED HARNESS. NO FURTHER DEFECTS.
- [SDR COMA0760552](https://openairdocs.org/sdr/COMA0760552.md): Battery · discharged · Sep 1, 2007 · N918CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5348 - FORWARDS EMERGENCY LIGHTS WILL NOT COME ON. REMOVED AND REPLACED NR 1 BATTERY PACK.
- [SDR COMA0760502](https://openairdocs.org/sdr/COMA0760502.md): Valve · malfunctioned · Jul 28, 2007 · N918CA · Cndair CL6002B19 · Air Distribution System
  > FLIGHT 5540 - OVERBOARD COOL CAUTION MESSAGE ON IN FLIGHT. AIRCRAFT DID NOT PRESSURIZE NORMALLY. AIRCRAFT RETURNED BACK TO SAV AND LANDED SAFELY. TRANSFERRED TO DEFERRED LIST PER MEL 21-24-06-2.
- [SDR COMA0760490](https://openairdocs.org/sdr/COMA0760490.md): Bulkhead · damaged · Jul 19, 2007 · N918CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > PERMANENT REPAIR REQUIRED ON PREVIOUSLY APPLIED TEMP REPAIR TO FS 621.00 REAR PRESS BULKHEAD FRAME AT WEB BL 0.00 WL 111.09. APPLIED PERMANENT REPAIR ANGLE ON FS 621.00 BULKHEAD IAW BOMBARDIER REO 601R-53-61-1285.
- [SDR COMA0760332](https://openairdocs.org/sdr/COMA0760332.md): Bulkhead · cracked · Apr 19, 2007 · N918CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING FS 559 INSPECTION FOUND 2 EA CRACKS AT SEMI-PRESSURE BULKHEAD, FS 559, RBL 9-18. REMOVED DAMAGE AND INSTALLED DOUBLER PER COMAIR SR10-5341-0001.
- [SDR COMA0760122](https://openairdocs.org/sdr/COMA0760122.md): Wire Harness · faulty · Feb 2, 2007 · N918CA · Cndair CL6002B19 · Landing Gear System Wiring
  > FLIGHT 5020 - DURING TAXI-OUT TO THE RUNWAY RECEIVED AN ANTI-SKID CAUTION MESSAGE, AIRCRAFT RETURNED TO THE GATE. REPLACED THE RIGHT MLG OUTBOARD TRANSDUCER WIRING HARNESS.
- [SDR COMA0660569](https://openairdocs.org/sdr/COMA0660569.md): Caution Message · illuminated · Oct 4, 2006 · N918CA · Cndair CL6002B19 · Cabin Pressure Control System
  > FLIGHT 5217 - AFTER TAKEOFF FROM JFK RECEIVED OVERBOARD COOL CAUTION MESSAGE AT 500 FT. AIRCRAFT WAS NOT PRESSURIZING. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. TRANSFERRED TO DMI LIST PER MEL 21-24-06-2.
- [SDR COMA0660560](https://openairdocs.org/sdr/COMA0660560.md): Status Message · illuminated · Sep 25, 2006 · N918CA · Cndair CL6002B19 · Central Warning
  > FLIGHT 5001- AFTER TAKEOFF RECEIVED OVBD COOL CAUTION MESSAGE AND INBD COOL FAIL STATUS MESSAGE. RETURNED TO AIRPORT WITHOUT INCIDENT. AFTER LANDING BOTH MESSAGES WENT OUT. INSPECTED PAX DOOR WIRING AND SWITCHES, NO DEFECTS FOUND.
- [SDR COMA0660414](https://openairdocs.org/sdr/COMA0660414.md): Smoke Detector · malfunctioned · Jun 30, 2006 · N918CA · Cndair CL6002B19 · Smoke Detection
  > FLIGHT 5061- EN ROUTE TO BTR OVER TYS RECEIVED CARGO SMOKE WARNING. FOLLOWED QRH PROCEDURE, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED NR 1 SMOKE DETECTORS.
- [SDR COMA0660394](https://openairdocs.org/sdr/COMA0660394.md): Lever · out of position · Jun 19, 2006 · N918CA · Cndair CL6002B19 · AC Generator-Alternator
  > FLIGHT 5612 - AC ESSENTIAL BUS MESSAGE IN FLIGHT WITH ASSOCIATED MESSAGES. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MANUAL RELEASE LEVER FOUND PUSHED OUT SLIGHTLY DUE TO RUBBER HANDLE UNDERNEATH LEVER. PERFORMED MANUAL ADG DEPLOYMENT, NO DEFE
- [SDR COMA0660325](https://openairdocs.org/sdr/COMA0660325.md): Flap System · failed · May 2, 2006 · N918CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5306 - ON APPROACH TO BWI FLAPS FAILED AT 30 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 FURHTER FLAP CAUTION MESSAGES.
- [SDR COMA0560728](https://openairdocs.org/sdr/COMA0560728.md): Warning Light · false indication · Dec 16, 2005 · N918CA · Cndair CL6002B19 · Door Warning System
  > FLIGHT 5001- FOUND CABIN DOOR WARNING. OPERATED CABIN DOOR, NO DEFECTS FOUND.
- [SDR COMA0560656](https://openairdocs.org/sdr/COMA0560656.md): Switch · out of adjust · Nov 30, 2005 · N918CA · Cndair CL6002B19 · Tire Tube
  > FLIGHT 5672 - PARKING BRAKE CONFIG WARNING. ADJUSTED THE PARKING BRAKE MICROSWITCH.
- [SDR COMA0560651](https://openairdocs.org/sdr/COMA0560651.md): Warning Light · illuminated · Nov 27, 2005 · N918CA · Cndair CL6002B19 · Ice Detection
  > FLIGHT 5058 - EN ROUTE CMI-CVG, RECEIVED AN ANTI-ICE DUCT WARNING MESSAGE, FLIGHT DIVERTED TO EVV. PERFORMED SYSTEM CHECK OF THE WING ANTI-ICE SYSTEM, CND.
- [SDR COMA0460698](https://openairdocs.org/sdr/COMA0460698.md): Windshield · cracked · Dec 19, 2004 · N918CA · Cndair CL6002B19 · Flight Compartment Windows
  > FLIGHT 5435 CO-PILOTS WINDSHIELD CRACKED. REPLACED WINDSHIELD.
- [SDR COMA0460675](https://openairdocs.org/sdr/COMA0460675.md): Warning System · activated · Dec 10, 2004 · N918CA · Cndair CL6002B19 · Landing Gear Brake System
  > FLIGHT 5144 ANTI SKID CAUTION MESSAGE. COULD NOT DUPLICATE. INSPECTED SYSTEM AND OPERATIONAL CHECK, FOUND NO DEFECTS.
- [SDR COMA0460669](https://openairdocs.org/sdr/COMA0460669.md): Oil System · overserviced · Dec 8, 2004 · N918CA · Cndair CL6002B19 · Turbine Engine Oil System
  > FLIGHT 5729 HIGH OIL TEMP CAUTION MESSAGE. FOUND ENGINE OIL SYSTEM OVERFILLED. DRAINED SYSTEM AND SERVICED TO PROPER LEVEL.
- [SDR COMA0460656](https://openairdocs.org/sdr/COMA0460656.md): Control System · malfunctioned · Dec 1, 2004 · N918CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5173 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
- [SDR COMA0460505](https://openairdocs.org/sdr/COMA0460505.md): Torque Link · disconnected · Sep 5, 2004 · N918CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > FLIGHT 5666 AFTER TAKEOFF RECEIVED A NOSE GEAR UP DISAGREE CAUTION. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. RECONNECTED THE NLG TORQUE LINKS AND REPLACED BOTH TIRES.
- [SDR COMA0460060](https://openairdocs.org/sdr/COMA0460060.md): Interphone · noisy · Jan 15, 2004 · N918CA · Cndair CL6002B19 · Interphone/Passenger Announcement (PA) System
  > FLIGHT 5718 LOUD TICKING NOISE IN HEADSET DURING T/O. REPLACED THE APU BAY INTERPHONE UNIT.
- [SDR COMA0360565](https://openairdocs.org/sdr/COMA0360565.md): Door · open · Dec 18, 2003 · N918CA · Cndair CL6002B19 · Service Doors
  > FLIGHT 5400 STALL FAIL WARNING AFTER T/O. LOUD BUZZ FROM NOSE AREA. FOUND 02 SERVICE DOOR OPEN. CLOSED SERVICE DOOR.
- [SDR COMA0360488](https://openairdocs.org/sdr/COMA0360488.md): Pulley · defective · Nov 6, 2003 · N918CA · Cndair CL6002B19 · Aileron Control System
  > FLIGHT 5369 DURING CRUISE FLIGHT THE AILERON CONTROLS SEEMED TO REQUIRE MORE THAN NORMAL FORCE TO OPERATE. CREW ELECTED TO PERFORM AN EMERGENCY DESCENT TO LOWER ALTITUDE WHERE THE AILERONS RETURNED BACK TO NORMAL OPERATION. REPLACED AILERON CONTROL PATH PULL
- [SDR COMA0360324](https://openairdocs.org/sdr/COMA0360324.md): Skin Panel · cracked · Jul 18, 2003 · N918CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING COMPLIANCE OF TASK NR 002-53-160-610, 2 CRACKS WERE FOUND IN THE PRESSURE FLOOR SKIN NEAR FS 461.0, BETWEEN LBL 9.0 AND RBL 9.0. THE CRACKS RANGE FROM 2.875 INCHES TO 3.125 INCHES IN LENGTH. THE PRESSURE FLOOR SKIN WAS REPAIRED IAW BOMBARDIER REO #610
- [SDR COMA0360149](https://openairdocs.org/sdr/COMA0360149.md): Flap · Mar 13, 2003 · N918CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5885 FLAPS FAIL CAUTION DURING TAXI.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
- [SDR COMA0360073](https://openairdocs.org/sdr/COMA0360073.md): Wire Harness · defective · Jan 31, 2003 · N918CA · Cndair CL6002B19 · Landing Gear Brake System
  > FLIGHT 5767 INBD ANTI SKID INOP CAUTION MESSAGE.REPLACED ANTI-SKID WIRE HARNESS.
- [SDR COMA0360031](https://openairdocs.org/sdr/COMA0360031.md): Actuator · unreliable · Jan 14, 2003 · N918CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5575 FLAPS FAIL MESSAGE DURING APPROACH.REPLACED THE L/H #1 FLAP ACTUATOR.
- [SDR COMA0360027](https://openairdocs.org/sdr/COMA0360027.md): Flap · out of rig · Jan 13, 2003 · N918CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5133 FLAPS FAIL MESSAGE DURING TAXI. FOUND THE FLAPS TO BE OUT OF RIG 130TH MECHANICALLY AND ELECTRICALLY. RIGGED FLAPS TO M/M SPECIFICATIONS.
- [SDR COMA0360022](https://openairdocs.org/sdr/COMA0360022.md): Pdu · malfunctioned · Jan 11, 2003 · N918CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5621 FLAPS FAILED WHEN SELECTED TO 30 DEGREES.REPLACED THE PDU
- [SDR COMA0260727](https://openairdocs.org/sdr/COMA0260727.md): Flap · Dec 19, 2002 · N918CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED DURING TAXI.INSPECTED FLAP SYSTEM IAW AD 98-20-01.
- [SDR COMA0260615](https://openairdocs.org/sdr/COMA0260615.md): Coalescer Bag · dirty · Oct 27, 2002 · N918CA · Cndair CL6002B19 · Cabin Cooling System
  > FLIGHT 5906 BURNING SMELL FILLED COCKPIT.REPLACED THE COALESCER SOCKS ON THE L/H AND R/H ACM WATER SEPERATORS.
- [SDR COMA0260604](https://openairdocs.org/sdr/COMA0260604.md): Oil System · Oct 24, 2002 · N918CA · Cndair CL6002B19 · APU Oil System
  > FLIGHT 5796 APU LOW OIL PRESSURE CAUTION MESSAGE.SERVICED APU OIL - G OPERATONAL CHECKS NORMAL.
- [SDR COMA0260597](https://openairdocs.org/sdr/COMA0260597.md): Apu · Oct 20, 2002 · N918CA · Cndair CL6002B19 · APU Oil System
  > FLIGHT 5502 APU OIL PRESSURE CAUTION MESSAGE.COULD NOT DUPLICATE. OPERATIONAL CHECK OF APU WAS NORMAL.
- [SDR COMA0260542](https://openairdocs.org/sdr/COMA0260542.md): Landing Gear · Sep 25, 2002 · N918CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > FLIGHT 5968 GEAR DISAGREE MESSAGE - NLG DID NOT RETRACT.SERVICED THE NLG SHOCK STRUT WITH OIL AND N2 PER AMM.
- [SDR COMA0260544](https://openairdocs.org/sdr/COMA0260544.md): Flap · Sep 23, 2002 · N918CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5258 FLAPS FAILED WHEN SELECTED UP AFTER T/O.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01.
- [SDR COMA0260540](https://openairdocs.org/sdr/COMA0260540.md): Element · false activation · Sep 18, 2002 · N918CA · Cndair CL6002B19 · Pneumatic Indicating System
  > FLIGHT 5064 R/H ANTI ICE DUCT WARNINGREPLACED FUSELAGE SECTION OF BLEED LEAK SENSING ELEMENT.
- [SDR COMA0260203](https://openairdocs.org/sdr/COMA0260203.md): Trim Switch · Mar 19, 2002 · N918CA · Cndair CL6002B19 · Rudder Control System
  > FLIGHT 5407 T/O CONFIG TRIM WARNING.FOUND AILERON TRIM OUT OF T/O RANGE - OPERATIONAL CHECK OF TRIM SYSTEM WAS NORMAL.
- [SDR COMA0260087](https://openairdocs.org/sdr/COMA0260087.md): Fuel Tank · damaged · Jan 28, 2002 · N918CA · Cndair CL6002B19 · Fuel System Wiring
  > WHEN L/H BOOST PUMP CANISTER WAS REMOVED FOR REPAIR, FOUND THE WIRING INSULATION PULLED BACK AND WIRE CONDUCTORS EXPOSED.REPLACED CANISTER.
- [SDR COMA0260067](https://openairdocs.org/sdr/COMA0260067.md): Skin · cracked · Jan 27, 2002 · N918CA · Cndair CL6002B19 · Wing, Plate/Skin
  > LT FUEL BOOST PUMP ACCESS HOLES ARE CRACKED NR 1 (APPROX.125 INCH LONG BY.020 INCHDEEP), NR 9 (APPROX.200 INCH LONG BY.040 INCH DEEP) AND NR 11 (APPROX.200 INCH LONG BY.040 INCH DEEP). PERFORMED A MAJOR REPAIR TO LT BOOST PUMP ACCESS HOLE NR 1, 9 AND 11 IA
- [SDR COMA0260046](https://openairdocs.org/sdr/COMA0260046.md): Element · malfunctioned · Jan 13, 2002 · N918CA · Cndair CL6002B19 · Overheat Detection
  > FLIGHT 5991 L/H 14TH STAGE BLEED DUCT WARNING.REPLACED THE L/H PYLON LEAK DETECTOR ELEMENT.
- [SDR COMA0160930](https://openairdocs.org/sdr/COMA0160930.md): Beam · cracked · Nov 28, 2001 · N918CA · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > ENGINE SUPPORT BEAM CRACKED.REPAIRED DAMAGE I/A/W REO 601-53-345.
- [SDR COMA0160769](https://openairdocs.org/sdr/COMA0160769.md): Light · Sep 30, 2001 · N918CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5362. DURING INSPECTION FOUND THE FLOOR EMERGENCY EXIT FLOOR LIGHT BY THE CABIN DOOR INOPERATIVE.REPLACED FAULTY LIGHT ASSEMBLY.
- [SDR COMA0160659](https://openairdocs.org/sdr/COMA0160659.md): Uplock · faulty · Aug 29, 2001 · N918CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > FLIGHT #5266. SHORTLY AFTER TAKE OFF RECEIVED A NOSE LANDING GEAR DISAGREE LIGHT, AIRCRAFT RETURNED TO THE FIELD.REPLACED THE NOSE LANDING GEAR UPLOCK ASSEMBLY.
- [SDR COMA0160649](https://openairdocs.org/sdr/COMA0160649.md): Sensor · Aug 27, 2001 · N918CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > FLIGHT #5572. AFTER TAKE OFF FROM GRB RECEIVED A NOSE LANDING GEAR DISAGREE CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD.ADJUSTED THE NOSE LANDING GEAR PS3GA PROXIMITY SENSOR, OPERATIONAL GEAR SWING WAS SATISFACTORY.
- [SDR COMA0160479](https://openairdocs.org/sdr/COMA0160479.md): Beam · cracked · Jul 15, 2001 · N918CA · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > R/H ENGINE SUPPORT BEAM CRACKED FWD L/H SIDE.R/H ENGINE SUPPORT BEAM REPAIRED I/A/W REO 601R-53-61-366 REV B.
- [SDR COMA0160359](https://openairdocs.org/sdr/COMA0160359.md): Intercostal · cracked · Apr 10, 2001 · N918CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 484 ANGLES CRACKED T LBL 27 INBOARD AND OUTBOARD. REPAIRED INTERCOSTALS AND ANGLES AT FS 484 IAW WVAC EO 601R-53-2375.

Next page: https://openairdocs.org/deregistered/N918CA-2011-03-09/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 = 'N918CA' AND deregistration_id = 'N918CA-2011-03-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N918CA-2011-03-09/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.