N918CA, cancelled Mar 9, 2011

Service difficulty reports · 114

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR COMA2009062950166Bulkhead · crackedFS 202.75 FWD PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE CUTOUT. REPAIRED PER REO 601R-53-11 AND EA 10-5311-02657.Jun 29, 2009 · N918CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA0860327Stiffener · crackedDURING 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)Jul 20, 2008 · N918CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0860319Frame · crackedDURING 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)Jul 8, 2008 · N918CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COM2008F00002Frame · crackedDURING 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)Jul 8, 2008 · N918CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA0860311Circuit Breaker · trippedRECEIVED 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)Jun 28, 2008 · N918CA · Cndair CL6002B19 · Hydraulic Power System WiringSDR COMA0860116Connector · looseFLIGHT 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.Feb 9, 2008 · N918CA · Cndair CL6002B19 · Door System WiringSDR COMA0760552Battery · dischargedFLIGHT 5348 - FORWARDS EMERGENCY LIGHTS WILL NOT COME ON. REMOVED AND REPLACED NR 1 BATTERY PACK.Sep 1, 2007 · N918CA · Cndair CL6002B19 · Emergency LightingSDR COMA0760502Valve · malfunctionedFLIGHT 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.Jul 28, 2007 · N918CA · Cndair CL6002B19 · Air Distribution SystemSDR COMA0760490Bulkhead · damagedPERMANENT 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.Jul 19, 2007 · N918CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA0760332Bulkhead · crackedDURING 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.Apr 19, 2007 · N918CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA0760122Wire Harness · faultyFLIGHT 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.Feb 2, 2007 · N918CA · Cndair CL6002B19 · Landing Gear System WiringSDR COMA0660569Caution Message · illuminatedFLIGHT 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.Oct 4, 2006 · N918CA · Cndair CL6002B19 · Cabin Pressure Control SystemSDR COMA0660560Status Message · illuminatedFLIGHT 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.Sep 25, 2006 · N918CA · Cndair CL6002B19 · Central WarningSDR COMA0660414Smoke Detector · malfunctionedFLIGHT 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.Jun 30, 2006 · N918CA · Cndair CL6002B19 · Smoke DetectionSDR COMA0660394Lever · out of positionFLIGHT 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 DEFEJun 19, 2006 · N918CA · Cndair CL6002B19 · AC Generator-AlternatorSDR COMA0660325Flap System · failedFLIGHT 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.May 2, 2006 · N918CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0560728Warning Light · false indicationFLIGHT 5001- FOUND CABIN DOOR WARNING. OPERATED CABIN DOOR, NO DEFECTS FOUND.Dec 16, 2005 · N918CA · Cndair CL6002B19 · Door Warning SystemSDR COMA0560656Switch · out of adjustFLIGHT 5672 - PARKING BRAKE CONFIG WARNING. ADJUSTED THE PARKING BRAKE MICROSWITCH.Nov 30, 2005 · N918CA · Cndair CL6002B19 · Tire TubeSDR COMA0560651Warning Light · illuminatedFLIGHT 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.Nov 27, 2005 · N918CA · Cndair CL6002B19 · Ice DetectionSDR COMA0460698Windshield · crackedFLIGHT 5435 CO-PILOTS WINDSHIELD CRACKED. REPLACED WINDSHIELD.Dec 19, 2004 · N918CA · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA0460675Warning System · activatedFLIGHT 5144 ANTI SKID CAUTION MESSAGE. COULD NOT DUPLICATE. INSPECTED SYSTEM AND OPERATIONAL CHECK, FOUND NO DEFECTS.Dec 10, 2004 · N918CA · Cndair CL6002B19 · Landing Gear Brake SystemSDR COMA0460669Oil System · overservicedFLIGHT 5729 HIGH OIL TEMP CAUTION MESSAGE. FOUND ENGINE OIL SYSTEM OVERFILLED. DRAINED SYSTEM AND SERVICED TO PROPER LEVEL.Dec 8, 2004 · N918CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR COMA0460656Control System · malfunctionedFLIGHT 5173 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.Dec 1, 2004 · N918CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0460505Torque Link · disconnectedFLIGHT 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.Sep 5, 2004 · N918CA · Cndair CL6002B19 · Landing Gear Position and WarningSDR COMA0460060Interphone · noisyFLIGHT 5718 LOUD TICKING NOISE IN HEADSET DURING T/O. REPLACED THE APU BAY INTERPHONE UNIT.Jan 15, 2004 · N918CA · Cndair CL6002B19 · Interphone/Passenger Announcement (PA) SystemSDR COMA0360565Door · openFLIGHT 5400 STALL FAIL WARNING AFTER T/O. LOUD BUZZ FROM NOSE AREA. FOUND 02 SERVICE DOOR OPEN. CLOSED SERVICE DOOR.Dec 18, 2003 · N918CA · Cndair CL6002B19 · Service DoorsSDR COMA0360488Pulley · defectiveFLIGHT 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 PULLNov 6, 2003 · N918CA · Cndair CL6002B19 · Aileron Control SystemSDR COMA0360324Skin Panel · crackedDURING 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 #610Jul 18, 2003 · N918CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR COMA0360149FlapFLIGHT 5885 FLAPS FAIL CAUTION DURING TAXI.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.Mar 13, 2003 · N918CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0360073Wire Harness · defectiveFLIGHT 5767 INBD ANTI SKID INOP CAUTION MESSAGE.REPLACED ANTI-SKID WIRE HARNESS.Jan 31, 2003 · N918CA · Cndair CL6002B19 · Landing Gear Brake SystemSDR COMA0360031Actuator · unreliableFLIGHT 5575 FLAPS FAIL MESSAGE DURING APPROACH.REPLACED THE L/H #1 FLAP ACTUATOR.Jan 14, 2003 · N918CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0360027Flap · out of rigFLIGHT 5133 FLAPS FAIL MESSAGE DURING TAXI. FOUND THE FLAPS TO BE OUT OF RIG 130TH MECHANICALLY AND ELECTRICALLY. RIGGED FLAPS TO M/M SPECIFICATIONS.Jan 13, 2003 · N918CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0360022Pdu · malfunctionedFLIGHT 5621 FLAPS FAILED WHEN SELECTED TO 30 DEGREES.REPLACED THE PDUJan 11, 2003 · N918CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0260727FlapFLAPS FAILED DURING TAXI.INSPECTED FLAP SYSTEM IAW AD 98-20-01.Dec 19, 2002 · N918CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0260615Coalescer Bag · dirtyFLIGHT 5906 BURNING SMELL FILLED COCKPIT.REPLACED THE COALESCER SOCKS ON THE L/H AND R/H ACM WATER SEPERATORS.Oct 27, 2002 · N918CA · Cndair CL6002B19 · Cabin Cooling SystemSDR COMA0260604Oil SystemFLIGHT 5796 APU LOW OIL PRESSURE CAUTION MESSAGE.SERVICED APU OIL - G OPERATONAL CHECKS NORMAL.Oct 24, 2002 · N918CA · Cndair CL6002B19 · APU Oil SystemSDR COMA0260597ApuFLIGHT 5502 APU OIL PRESSURE CAUTION MESSAGE.COULD NOT DUPLICATE. OPERATIONAL CHECK OF APU WAS NORMAL.Oct 20, 2002 · N918CA · Cndair CL6002B19 · APU Oil SystemSDR COMA0260542Landing GearFLIGHT 5968 GEAR DISAGREE MESSAGE - NLG DID NOT RETRACT.SERVICED THE NLG SHOCK STRUT WITH OIL AND N2 PER AMM.Sep 25, 2002 · N918CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0260544FlapFLIGHT 5258 FLAPS FAILED WHEN SELECTED UP AFTER T/O.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01.Sep 23, 2002 · N918CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0260540Element · false activationFLIGHT 5064 R/H ANTI ICE DUCT WARNINGREPLACED FUSELAGE SECTION OF BLEED LEAK SENSING ELEMENT.Sep 18, 2002 · N918CA · Cndair CL6002B19 · Pneumatic Indicating SystemSDR COMA0260203Trim SwitchFLIGHT 5407 T/O CONFIG TRIM WARNING.FOUND AILERON TRIM OUT OF T/O RANGE - OPERATIONAL CHECK OF TRIM SYSTEM WAS NORMAL.Mar 19, 2002 · N918CA · Cndair CL6002B19 · Rudder Control SystemSDR COMA0260087Fuel Tank · damagedWHEN L/H BOOST PUMP CANISTER WAS REMOVED FOR REPAIR, FOUND THE WIRING INSULATION PULLED BACK AND WIRE CONDUCTORS EXPOSED.REPLACED CANISTER.Jan 28, 2002 · N918CA · Cndair CL6002B19 · Fuel System WiringSDR COMA0260067Skin · crackedLT 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 IAJan 27, 2002 · N918CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA0260046Element · malfunctionedFLIGHT 5991 L/H 14TH STAGE BLEED DUCT WARNING.REPLACED THE L/H PYLON LEAK DETECTOR ELEMENT.Jan 13, 2002 · N918CA · Cndair CL6002B19 · Overheat DetectionSDR COMA0160930Beam · crackedENGINE SUPPORT BEAM CRACKED.REPAIRED DAMAGE I/A/W REO 601-53-345.Nov 28, 2001 · N918CA · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR COMA0160769LightFLIGHT 5362. DURING INSPECTION FOUND THE FLOOR EMERGENCY EXIT FLOOR LIGHT BY THE CABIN DOOR INOPERATIVE.REPLACED FAULTY LIGHT ASSEMBLY.Sep 30, 2001 · N918CA · Cndair CL6002B19 · Emergency LightingSDR COMA0160659Uplock · faultyFLIGHT #5266. SHORTLY AFTER TAKE OFF RECEIVED A NOSE LANDING GEAR DISAGREE LIGHT, AIRCRAFT RETURNED TO THE FIELD.REPLACED THE NOSE LANDING GEAR UPLOCK ASSEMBLY.Aug 29, 2001 · N918CA · Cndair CL6002B19 · Landing Gear Position and WarningSDR COMA0160649SensorFLIGHT #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.Aug 27, 2001 · N918CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0160479Beam · crackedR/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.Jul 15, 2001 · N918CA · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR COMA0160359Intercostal · crackedFS 484 ANGLES CRACKED T LBL 27 INBOARD AND OUTBOARD. REPAIRED INTERCOSTALS AND ANGLES AT FS 484 IAW WVAC EO 601R-53-2375.Apr 10, 2001 · N918CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
Back to N918CA, cancelled Mar 9, 2011