N989CA
Registered owner: HYANNIS AIR SERVICE INC, MA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| HYANNIS AIR SERVICE INC. (HYIA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
PILOT REPORTED AN UN-COMMANDED FEATHER ON THE RIGHT ENGINE. MAINTENANCE INSPECTED RH PROP AND FOUND NO DEFECTS NOTED AT THIS TIME. REMOVED RH PROP GOVERNOR AND INSPECTED INSIDE CRANK CASE AND FOUND NO DEFECTS. NOTED THAT RH PROP GOVERNOR NOT HITTING BOTH STOPS COMPLETELY. REMOVED AND REPLACED RH PROP GOVERNOR WITH NO FURTHER DEFECTS NOTED.
PILOT REPORTED PITOT HEAT NOT WORKING. MAINTENANCE INSPECTED AND FOUND THE LEFT PIOTO HEAT SWITCH CONNECTOR MELTED. REPLACED WITH NEW SWITCH WITH NO FURTHER DEFECTS NOTED.
DURING ROUTINE INSPECTION THE NUMBER ONE CYLINDER THROUGH STUD WAS FOUND TO BE SHEARED. THE ENGINE IS BEING REPLACED.
DURING MAINTENANCE INSPECTION ONE BOLT ON THE LEFT MAIN GEAR WHEEL ASSEMBLY WAS FOUND TO BE SHEARED OFF. THE WHEEL ASSEMBLY WAS REPLACED WITH NO ADDITIONAL DEFECTS NOTED
THE PILOT REPORTED A BURNING SMELL IN CABIN DURING FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE COMBUSTION HEATER/FAN SWITCHES.
FLIGHT 5021 - ON APPROACH INTO JFK SELECTED GEAR DOWN AND RECEIVED GEAR DISAGREE WARNING MESSAGE, FOLLOWED BY AMBER NOSE GEAR INDICATION AND NOSE DOOR WARNING. ALL CLEARED WITHIN APPROX 30 SECONDS. AIRCRAFT LANDED SAFELY IN JFK. REMOVED AND REPLACED MLG PRIORITY VALVE.
FLIGHT 5163 - EN ROUTE CVG-FSD PRIOR TO APPROACH RECEIVED A FLAPS FAIL CAUTION, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE FLAP ELECTRONIC UNIT.
FLIGHT 5652 - INFLIGHT AT 12000 FT RECEIVED PAX DOOR WARNING MESSAGE. QRH FOLLOWED AND AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REINSTALLED BUSHING IN UPPER FORWARD CAM LEVER OF PAX DOOR.
FLIGHT 5535 - LEFT MAIN GEAR DISAGREE AFTER GEAR SELECTED UP. FOLLOWED QRH, THREE GREEN AFTER MANUAL GEAR EXTENSION. EMERGENCY DECLARED AND AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED LEFT MLG DOOR BELL CRANK.
FLIGHT 5030 - VIBRATION JUST BEFORE ROTATION SPEED. WOW INPUT CAUTION, AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. BOTH LEFT MLG TIRES BLOWN. REMOVED AND REPLACED LEFT MLG O/B WHEEL ASSY.
FLIGHT 5030 - VIBRATION JUST BEFORE ROTATION SPEED. WOW INPUT CAUTION. AIRCRAFT RETURNED TO CVG AND LANDED SAFELY. REMOVED AND REPLACED LEFT MLG I/B WHEEL ASSY.
FLIGHT 5204 - LEFT BRAKE INOPERATIVE WHILE THE RIGHT BRAKE INDICATED HOT DURING ARRIVAL AT BOS. RECONNECTED THE LEFT MLG INBOARD AND OUTBOARD BRAKE QUICK DISCONNECT FITTINGS.
FLIGHT 5576 - LEFT WING OVERHEAT ON BEGINNING OF TAKEOFF THRUST. DEFERRED PER MEL 30-12-03-1.
FLIGHT 9426 - AFTER TAKEOFF, SELECTED GEAR UP, MAINS RETRACTED BUT NOSE GEAR HAD A LOUD CONTINUOUS BANGING NOISE WITH ON INDICATION OF GEAR UP OR DOWN. SERVICED OIL AND NITROGEN OF NLG STRUT. PERFORMED EXTENSION / RETRACTION TEST, OPS TEST GOOD.
FLIGHT 5463 - AIRCRAFT RETURNED TO JFK AFTER TAKEOFF DUE TO A RED CABIN DOOR WARNING MESSAGE. CLEANED THE CABIN DOOR PROXIMITY SWITCH AND CLEANED THE UPPER DOOR CAM ROLLERS.
FLIGHT 5071 - ON CLIMB, RECEIVED PAX DOOR LATCH CAUTION MESSAGE (7500FT) FOLLOWED BY AURAL WARNING (11000FT) ON DESCENT, MESSAGE RETURNED TO CAUTION. RETURNED TO AIRPORT. LANDED WITHOUT INCIDENT. REPLACED SPRING AND ROLLER ON INNER HANDLE LEVER LATCH MECHANISM. NO FURTHER DEFECTS.
FLIGHT 5071 - ON CLIMB, RECEIVED PAX DOOR LATCH CAUTION MESSAGE (7500FT) FOLLOWED BY AURAL WARNING (11000FT) ON DESCENT, MESSAGE RETURNED TO CAUTION. RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. REPLACED SPRING AND ROLLER ON INNER HANDLE LEVER LATCH MECHANISM. NO FURTHER DEFECTS.
FLIGHT 5555- ENROUTE, LOST CABIN PRESSURE AT 10,000 FT, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED AT LGA WITHOUT INCIDENT. REPLACED THE VACUUM REGULATOR.
FLIGHT 5454 - FLAP FAIL CAUTION. REPLACED THE LT NR 1 FLEY DRIVE SHAFT.
FLIGHT 5116 DURING DESCENT RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY. ABORTED 1ST APPROACH AT YYZ, 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.
WING OVERHEAT WARNING. REPLACED THE RT WING STANDBY THERMAL SWITCH.
FLIGHT 5142 FLAPS FAIL CAUTION. REPLACED THE RT BPSU.
FLIGHT 5061, GEAR DISAGREE WARNING. FOUND NLG TORQUE LINKS DISCONNECTED. RECONNECTED TORQUE LINKS AND A/C RETURNED TO SERVICE.
FLIGHT 5397 AFTER TAKEOFF FROM CVG NOTICED OIL ODOR IN COCKPIT. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. REPLACED THE APU.
FLIGHT 9494 FLAPS FAIL CAUTION MESSAGE. REPLACED BROKEN FLEX SHAFT, RIGHT NR 4 POSITION.
FLIGHT 5890 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU.
FLIGHT 5518 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
FLIGHT 5206 DURING DTW APPROACH RECEIVED A FLAP FAIL CAUTION AT 30 DEGREES WHEN SELECTED TO 45. 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 5279 STALL FAIL CAUTION MESSAGE. RESET THE STALL COMPUTER.
FLGIHT 5675 STALL FAIL CAUTION MESSAGE. RESET THE STALL COMPUTER.
FLIGHT 5882 GEAR DISAGREE WARNING DURING CRUISE FLIGHT. REPLACED THE NLG DOWNLOCK PROXIMITY SENSOR.
THE LT VERTICAL STABILIZER LUG BUSHING WAS MIGRATED .025 INCH AT THE HORIZONTAL STABILIZER PIVOT POINT. REMOVED THE MIGRATED BUSHING. PERFORMED NDT/LP1 TO ENSURE NO DAMAGE TO LUG BORE. MACHINED AND INSTALLED A 1ST OVERSIZED BUSHING I/A/W REO 601R-55-31-044.
LT FS 484 INTERCOSTAL ATTACHMENT FLANGE LBL 36 IS CRACKED. REPAIRED LT FS 484 INTERCOSTAL ATTACHMENT FLANGE LBL 36 I/A/W WVAC E.O. 601R-53-3826.
L.H. F.S. 484 INTERCOSTAL ATTACHMENT FLANGE LBL 36 IS CRACKED.REPAIRED L H F.S. 484 INTERCOSTAL ATTACHMENT FLANGE LBL 36 I/A/W WVAC E.O. 601R-53-3826.
THE PREVIOUS REPAIR AT THE R/H SIDE FS 621, WL73.5 BETWEEN RBL36 AND RBL42 UNDER FLOOR SUPPORT STRUCTURE WAS CRACKED.REMOVED THE CRACKED PREVIOUS REPAIR PARTS AND INSTALLED NEW REPAIR PARTS I/A/W REO 601R-53-61-004 REV B
FLIGHT 6562 TAT AND R/H PITOT HEAT CAUTION MESSAGE.REPLACED THE #2 ADSHC.
FLIGHT 5562 TAT AND R/H PITOT HEAT CAUTION MESSAGE.RESET SYSTEM CIRCUIT BREAKERS, FAULT CLEARED.
FLIGHT 5784 FLAPS FAILED AT 20 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
FLIGHT 5675 FORWARD SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOPERATIVE.REPLACED STRIP LAMP.
FLIGHT 5624 AC ESS BUSS INOP MESSAGE.COULD NOT DUPLICATE. PERFORMED AC ELECTRICAL SYSTEM CHECK, NO FAULTS FOUND.
FLIGHT 5602 EMERGENCY FLOOR PATH LIGHTING IS INOPERABLE AT LAST ROW.DEFERRED MAINTENANE PER MEL.
FLIGHT 5400 FLAPS FAILED AT 26 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
ENGINE SUPPORT BEAM CRACKED.REPAIRED DAMAGE I/A/W REO 601R-53-61-366.
LEFT SIDE FS 718.0 FRAME AND AFT DOUBLER AND RT SIDE AFT DOUBLER AT FS 718.0 BETWEEN STR 11 AND 12 CRACKED. DOUBLER P/N 600-3603-31/32. REPAIRED LT FRAME AND AFT DOUBLER AT FS 718.0 AND RT SIDE AFT DOUBLER AT FS 718.0 BETWEEN STR 11 AND 12 IAW REO 601R-53-61-193 REV A.
FS 310 REPAIR DOUBLER BETWEEN STR 16 AND 17 HAS TEMP REPAIR. REMOVED TEMPORARY REPAIR AND INSTALLED PERMANENT REPAIR IAW REO 601R-53-21-180 REV NC.
SMOKE IN CABIN. SECURED THE RT COOLING PACK AND DEFERRED MAINTENANCE PER M.E.L.
LEFT HAND 10TH STAGE BLEED AIR DUCT LEAK MESSAGE.REPLACED THE BLEED LEAK CONTROL UNIT.
PILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD.
FLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
RIGHT HAND FORWARD EMERGENCY LIGHT IS INOPERABLE. REPLACED LIGHT BULB.
GEAR DISAGREE MESSAGE DURING LANDING GEAR EXTENSION. COULD NOT DUPLICATE. NO FAULT CODES IN PSEU. AIRCRAFT RETURNED TO SERVICE.
FLAPS FAILED AT 8 DEGREES. REPLACED THE FCU.
CRACKS DETECTED IN WING FUEL PANEL OPENING AT 650 FB WS 274.319. REPAIRED AFFECTED AREAS IAW CANADAIR REO 601R-57-21-030.
CARGO DOOR MESSAGE. FOUND DOOR HANDLE IN RELEASED POSITION. CLOSED DOOR HANDLE. DOOR WARNING INDICATION NORMAL.
FLAPS FAILED AT 26 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
FLOOR SUPPORT ANGLE AT FS 621.0 LEFT SIDE IS CRACKED. REPAIRED FLOOR SUPPORT ANGLE AT FS 621.0 LEFT SIDE IAW REO 601R-53-61-117 REV A.
FLAPS FAILED AT 3 DEGREES. REPLACED THE FECU.
FLAPS FAILED WHEN SELECTED FOR LANDING APPROACH. REPLACED THE RIGHT HAND OUTBOARD FLAP ACTUATOR.
FUSELAGE SKIN DAMAGED BY IMPACT WITH PASSENGER DOOR BTM LOCKPINS AT FS 310.00 LHS STR 16 AND FS 349.00 LHS STR 16. PERFORMED A MAJOR REPAIR TO DAMAGED FUSELAGE SKIN AT FS 310.00 LHS STR 16 IAW CRJ REO 601R-53-21-180 REV NC AND FS 349.00 LHS STR 16 IAW REO 601-53-21-183 REV NC.
EMERGENCY FLOOR LIGHT AT CABIN ENTRANCE IS INOPERABLE. REPLACED LIGHT STRIP.
CONFIG SPOILER WARNING DURING TAKEOFF. REPLACED THE NR 1 SEC U.
FLAPS FAIL CAUTION MESSAGE AFTER LANDING. RESET FLAP SYSTEM CIRCUIT BREAKERS, SYSTEM OPERATION NORMAL.
DURING CLIMBOUT OF CVG, CARGO DOOR CAUTION WARNING ACTIVATED. AIRCRAFT RETURNED TO THE FIELD. PERFORMED OPERATIONAL CHECK FOR THE CARGO DOOR, NO DEFECTS NOTED.
RT ENGINE N1 AND ITT FLUCTUATIONS WHICH EXCEED LIMITS. COULD NOT DUPLICATE FLUCTUATIONS DURING GROUND RUN. REPLACED CONTROL AMPLIFIER FOR TROUBLESHOOTING.
THE NR 2 ENGINE HAD ROLL BACK DURING LANDING APPROACH. REPLACED THE FUEL CONTROL UNIT.
LANDING GEAR DISAGREEMENT WARNING DURING GEAR EXTENSION. REPLACED SYSTEM 3A HYRAULIC PUMP.
LANDING GEAR DISAGREE MESSAGE, CYCLED GEAR ONCE FOR NORMAL GEAR DOWN INDICATION. REPLACED THE NLG PRIORITY VALVE.
LANDING GEAR DID NOT EXTEND WHEN SELECTED DOWN FOR LANDING. MANUAL RELEASE SYSTEM USED TO EXTEND GEAR. REPLACED THE PSEU.