N719CA
Registered owner: CENTRAL AIRLINES INC, KS (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| CENTRAL AIR SOUTHWEST, INC. (ZJWA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
FLIGHT 5174 - EN ROUTE CID-CVG RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REMOVED ICE BETWEEN THE LEFT AND RIGHT INBOARD FLAP LEADING EDGE AND THE MOVEABLE VANE.
FLIGHT 5164 - UPON REACHING FLIGHT LEVEL 330 DISPLAY COOL CAUTION MESSAGE APPEARED. AIRCRAFT DIVERTED TO GSO AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED FLOW SENSOR.
FLIGHT 5457 - EN ROUTE JFK TO BUF CAPTAIN`S WINDSHIELD CRACKED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LEFT WINDSHIELD.
FLIGHT 9479 - EN ROUTE CVG-MHT RECEIVED A DISPLAY COOL MESSAGE, FLIGHT DIVERTED TO PIT. REPLACED CLOGGED AIR FILTER FOR THE ELECTRONIC FLIGHT INSTRUMENT SYSTEM.
FLIGHT 5745 - DURING BTV APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO 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). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.
FLIGHT 5686 - DURING OPERATION OF FLAPS WHILE AT THE GATE RECEIVED A FLAP FAIL CAUTION MESSAGE. REPLACED THE RIGHT BRAKE POSITION SENSING UNIT.
FLIGHT 5673- ANTI ICE DUCT WARNING. REPLACED THE LT FUSELAGE SENSING ELEMENT A47WK.
FLIGHT 5450 DURING CRUISE FLIGHT RECEIVED A HYDRAULIC SYSTEM NR 2 LOW PRESSURE WARNING. CREW DECLARED AN EMERGENCY AND DIVERTED TO TYS. REPLACED FAILED NR 2 ENGINE DRIVEN HYDRAULIC PUMP.
FLIGHT 5921 HYDRAULIC SYSTEM 3 LOW PRESSURE CAUTION AND GEAR DISAGREE WARNING. REPLACED SYSTEM 3A HYDRAULIC PUMP.
FLIGHT 5158 RECEIVED A FLAP FAIL CAUTION MESSAGE DURING CLIMBOUT OF CVG. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. 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 MESSAGE.
FLIGHT 5803 ANTI ICE DUCT WARNING. REPLACED BLEED LEAK SENSING ELEMENT.
FLIGHT 5201 LEFT ANTI ICE DUCT WARNING. COULD NOT DUPLICATE. INSPECTED SYSTEM AND FOUND NO DEFECTS.
CRACK NOTED AT FLANGE RADIUS OF LT FRAME AT FS 718. REPARIED IAW SB 601R-53-055 PART B IAW EA NR 10-5320-00242.
FLIGHT 5533 RT ENGINE OIL PRESSURE WARNING. SERVICED RT ENGINE WITH 4.75 QTS OF OIL.
FLIGHT 5521 SMOKE IN COCKPIT AND CABIN.REPLACED THE APU.
FLIGHT 5469 LOUD BUZZING NOISE AND STALL FAIL CAUTION PLUS IAS MESSAGE.FOUND 02 SERVICE DOOR OPEN - CLOSED DOOR.
FLIGHT 5519 R/H ENG COWL ANTI-ICE CAUTION MESSAGE.REPLACED THE R/H COWL ANTI ICE VALVE.
FLIGHT #5407. EMERGENCY LIGHTS CIRCUIT BREAKER IS TRIPPED.RESET BREAKER AND FUNCTION CHECKED SYTEM. NO FAULTS FOUND.
FLIGHT 5068. DURING CRUISE FLIGHT RECEIVED A CARGO SMOKE CAUTION MESSAGE, CREW DECLARED AN EMERGENCY, DISCHARGED THE CARGO FIRE EXTINGUISHING BOTTLE AND RETURNED TO THE FIELD SAFELY. REPLACED DEFECTIVE CARGO SMOKE DETECTOR.
FLAPS FAILED.REPLACED THE LEFT HAND BPSU.
RT VERT STAB BUSHING IS MIGRATED AT HORIZONTAL STAB ATTACH POINT. REMOVED MIGRATED BUSHING. INSTALLED BUSHING P/N 600-21061-7 (THAT WAS MACHINED IAW WVAC EO 601R-55-2291) IAW CRJ AMM 20-26-00-910-803. REAMED BUSHING IAW DWG 600-21029.
CABIN DOOR OUTER HANDLE CAUTION MESSAGE. ADJUSTED DOOR HANDLE PROXIMITY SENSOR.
STALL FAIL CAUTION DURING T/O.RESET THE STALL COMPUTER.
THE FORWARD ATTACH FOR THE CARGO NET WAS TORN FROM THE CARGO DOORSILL. TRIMMED THE TORN SILL TO A SMOOTH RADIUS AND FABRICATED A REPAIR DOUBLER AND INSTALLED DOUBLER IAW WVAC EO 601R-53-2142.
LOUD UNUSUAL NOISE FROM OUTSIDE THE AIRCRAFT. NOSE SERVICE DOOR NOT LATCHED. SECURED DOOR AND AIRCRAFT RETURNED TO SERVICE.
STALL FAIL AND STICK SHAKER AFTER TAKEOFF. RESET THE STALL COMPUTER. COULD NOT DUPLICATE.
RIGHT AND LEFT CARGO FLOOR SUPPORT ANGLES ARE CRACKED AT FS 621.0. REPAIRED RT AND LT SIDE CARGO FLOOR SUPPORT ANGLES IAW REO 601R-53-61-117 REV A.
PILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD.
CARGO SMOKE MESSAGE. FALSE WARNING. DEFERRED CARGO FIRE EXTINGUISHERS.
SMOKE IN COCKPIT. RAN ENGINES TO BURN RESIDUAL OIL FROM AIRCRAFT PACKS. SMOKE AND FUMES CEASED.
SMOKE IN COCKPIT AND CABIN WHEN BLEED AIR TRANSFERRED TO APU. DEFERRED THE APU PER MEL.
FS 718.00 LEFT AND RIGHT SIDES, AFT DOUBLERS CRACKED BETWEEN STRINGERS 11 AND 12. FS 718.00 LEFT AND RIGHT SIDES AFT DOUBLERS REPLACED IAW REO 601R-53-61-192 REV A.
CONFIG SPOILER WARNING DURING TAKEOFF.. REPLACED THE RIGHT SPOILERON PCU.
LEFT ENGINE COWL ANTI-ICE MESSAGE. REPLACED COWL ANTI-ICE VALVE.
FLOOR PATH EMERGENCY LIGHTS ARE INOPERABLE FROM ROW 8 AFT. REPLACED FLOOR LIGHTING.
WHEN FLAPS WERE SELECTED TO 45 DEGREES FLAP FAIL CAUTION MESSAGE ILLUMINATED AT 32 DEGREES. REMOVED AND REPLACED LEFT WING BPSU WIRING HARNESS. CHECKED TORQUE OF FLAP SYSTEM RIGGED FLAP SYSTEM.
FLAP FAIL ON APPROACH 19 DEGREES. REMOVED AND REPLACED FLAP CONTROL HANDLE.
FLAP FAIL ON APPROACH 19 DEGREES. REMOVED AND REPLACED RT OUTBOARD FLAP INBOARD ACTUATOR.
FLAP FAIL ON APPROACH AT 19 DEGREES. REMOVED AND RELACED LT OUTBOARD FLAP INBOARD ACTUATOR.
FLAP FAIL ON APPROACH 19 DEGREES. REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT (FECU).
FLAPS FAILED ON APPROACH AT 19 DEGREES. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATORS.
FLAPS FAILED 42 DEGREES ON APPROACH. REMOVED AND REPLACED BOTH LEFT INBOARD FLAP ACTUATORS (FAILED TORQUE CHECK).
FLAPS FAIL MESSAGE. REPLACED THE LT BPSU.
FLAPS FAIL MESSAGE. REPLACED THE LEFT AND RIGHT BPSU.
WHILE CLIMBING THROUGH 23,000, PAX DOOR LATCH CAUTION AND PAX DOOR EMERGENCY WARNING ILLUMINATED. AIRCRAFT WAS DIVERTED TO SDF AND THEN FERRIED TO CVG WHERE THE UPPER CAMS AND CAM PROX SENSOR TARGETS WERE ADJUSTED. ALSO, CHECKED RIIGGING OF ENTIRE PAX DOOR.
FLAPS FAILED AT 17 DEGREES. REPLACED RIGHT HAND OUTBOARD FLAP ACTUATOR.
FLAPS FAILED IN FLIGHT AT ZERO DEGREES. REPLACED LEFT BPSU.
FLAPS FAILED WHEN SELECTED FOR LANDING. COULD NOT DUPLICATE PROBLEM. REPLACED LT BPSU FOR TROUBLESHOOTING.