N466CA
Registered owner: HYANNIS AIR SERVICE INC DBA, 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
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
24 reports on file, 2002-06-03 – 2021-04-14.
Part: FUEL LINE — CRACKED (HEATING SYSTEM) · airframe 15,774 hrs · 6,393 cycles
THE PILOT REPORTED A FUEL SMELL WHEN THE HEATER WAS ON IN FLIGHT. MAINTENACE INSPECTED AND FOUND THE FUEL LINE AT THE FUEL NOZZLE CRACKED. THE LINE WAS REPAIRED AND REINSTALLED WITH NO FURTHER DEFECTS NOTED.
Part: HEATER — ODOR (CABIN) · airframe 15,672 hrs · 6,310 cycles
THE PILOT REPORTED A BURNING SMELL IN THE CABIN IN FLIGHT WITH THE HEATER TURNED ON. MAINTENANCE INSPECTED AND REPLACED THE HEATER ASSEMBLY WITH NO FURTHER DEFECTS NOTED.
Earlier reports · 2002–2014 · 22 reports
2014
Part: HSI — FAILED (COCKPIT) · airframe 8,768 hrs
HSI HAD FAILED DURING CRUISE FLIGHT ON AN IFR FLIGHT PLAN. SMOKE EMITTED FROM THE INSTRUMENT WITH THE BREAKER TRIPPING. SMOKE WAS BOTH VISIBLE & WAS ABLE TO BE SMELLED. QRH WAS IN HAND IN CASE SMOKE WAS NOT SUBSIDING & AN EMER LANDING AIRPORT WAS FOUND BUT NOT NEEDED. ATC WAS INFORMED OF SITUATION NO EMER WAS DECLARED DUE TO SMOKE SUBSIDING. R & R HSI.
Part: HEATER — LEAKING (COCKPIT) · airframe 8,554 hrs
DURING A TRAINING FLIGHT THE PILOT REPORTED A FUEL SMELL IN THE COCKPIT WHEN THE HEATER WAS ON. HE SHUT OFF THE HEATER & REPORTED THE DISCREPANCY TO MX. SECURED THE B NUT AT THE HEATER FUEL NOZZLE. OPERATIONAL & LEAK CHECKS WERE PERFORMED WITH NO DISCREPANCIES.
2008
Part: LINE — LEAKING (HYD SYSTEM)
FLIGHT 5581, IND TO IAH. DURING CRUISE THE FLIGHT CREW RECEIVED A HYD 2 SYS LOW PRESS MESSAGE. THE HYDRAULIC PAGE WAS BROUGHT UP IT WAS CONFIRMED THAT THE SYSTEM WAS INDICATING 0% QUANTITY AND VERY LOW PRESSURE. THE QRH PROCEDURES WERE FOLLOWED, AND THE FLIGHT DIVERTED TO KBNA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE HYDRAULIC SYSTEM AND FOUND A PIN-HOLE IN THE SYSTEM 2 HYDRAULIC LINE GOING THROUGH THE AFT EQUIPMENT BAY. THE HYDRAULIC LINE WAS REPLACED ALONG WITH THE HYDRAULIC PUMP AND THE SYSTEM LEAK AND OPS CHECKED GOOD. (A)
Part: OIL COOLER — CLOGGED (APU) · airframe 14,442 hrs · 12,652 cycles
FLIGHT 5756, IAH TO SDF - DURING CRUISE, THE CREW RECEIVED AN APU HIGH OIL TEMPERATURE MESSAGE ON EICAS. THE FLIGHT DIVERTED TO LIT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE APU AND VERIFIED THE OIL WAS SERVICED TO THE CORRECT LEVEL. THE CONNECTOR TO THE HIGH OIL TEMPERATURE BULB WAS CLEANED AND RESECURED. THE APU WAS RUN WITHOUT FURTHER DEFECTS. ON THE 31ST,THE OIL COOLER WAS REPLACED DUE TO INTERNAL CLOGGING AND LEAKAGE.
Part: OIL COOLER — LEAKING (APU) · airframe 14,430 hrs · 12,643 cycles
FLIGHT 5601, IAH TO JAX - DURING CRUISE THE CREW RECEIVED AN APU OIL TEMP MESSAGE ON EICAS. THE PROPER QRH CHECKLISTS WERE FOLLOWED, AND THE FLIGHT DIVERTED TO PNS, WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE APU AND FOUND THAT IT WAS LOW ON OIL. AFTER SERVICING THE OIL TO THE CORRECT LEVEL THE APU THEN OPERATED NORMALLY AND THE AIRCRAFT WAS RELEASED FOR SERVICE. ON THE 31ST OF MARCH, THE APU WAS TROUBLESHOT DUE TO THE HIGH OIL TEMPERATURE PROBLEMS AND THE APU OIL COOLER WAS FOUND TO BE CLOGGED AND LEAKING OIL. THE OIL COOLER WAS REPLACED AND THE APU OPERATED NORMALLY.
Part: OIL SYSTEM — LOW (APU) · airframe 14,426 hrs · 12,640 cycles
IAH TO ATL - AFTER LEVELING OFF IN CRUISE FLIGHT, THE CREW RECEIVED AN APU HIGH TEMP MESSAGE ON EICAS. AFTER FOLLOWING THE APPROPRIATE QRH CHECKLISTS THE FLIGHT DIVERTED TO MGM WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE APU AND FOUND IT WAS LOW ON OIL. AFTER PROPERLY SERVICING THE APU WITH OIL, IT OPERATED NORMALLY AND THE AIRCRAFT WAS RELEASED TO SERVICE.
2006
Part: COALESCER BAG — ODOR (CABIN AIR) · airframe 11,142 hrs · 9,894 cycles
FLIGHT 5378- DURING CLIMB-OUT OF OMA RECEIVED A MOMENTARY MESSAGE INDICATING SMOKE IN LAVATORY, FLIGHT RETURNED TO OMA. REMOVED, CLEANED, INSPECTED AND REINSTALLED LEFT AND RIGHT COALESCER FILTER ELEMENTS.
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 11,021 hrs · 9,781 cycles
FLIGHT 5384 - DURING LGA 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.
2005
Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 10,113 hrs · 8,976 cycles
FLIGHT 5463- FLAPS FAIL CAUTION. REPLACED THE FECU.
Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 8,679 hrs · 7,718 cycles
FLIGHT 5465- FLAP FAIL CAUTION. REPLACED THE FECU.
Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 8,679 hrs · 7,718 cycles
FLIGHT 5379 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
Part: FAN — FAILED (CARGO BAY) · airframe 8,314 hrs · 7,412 cycles
FLIGHT 5752 CARGO FAN FAIL. DEFERRED MAINT PER MEL.
Part: CONTROL SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 8,239 hrs · 7,341 cycles
FLIGHT 5004 - DURING CVG APPROACH RECEIVED A FLAP FAIL MESSAGE, CREW DECLARED AN EMERGENCY AND 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 CAUTION MESSAGES.
Part: DRIVE SHAFT — LACK OF LUBE (TE FLAPS) · airframe 8,203 hrs · 7,310 cycles
FLIGHT 4995 DURING APPROACH TO MHT RECEIVED A FLAP FAIL MESSAGE. FERRIED AIRCRAFT TO CVG FOR LUBRICATION OF THE FLEX DRIVE SHAFTS.
Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 8,191 hrs · 7,303 cycles
FLIGHT 5614 FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
2004
Part: CONNECTOR — CORRODED (EMERGENCY LIGHT) · airframe 6,940 hrs · 6,206 cycles
FLIGHT 5460 EMERGENCY FLOOR PATH LIGHTS INOP AT ROWS 6 TO 8. REPLACED CORRODED CONNECTOR WIRE.
Part: IDG — FAILED (LEFT) · airframe 5,638 hrs · 5,131 cycles
FLIGHT 5182 LEFT IDG TRIPPED OFF LINE. REPLACED THE LEFT IDG.
2003
Part: PRESSURE SWITCH — FAILED (APU) · airframe 2,914 hrs · 2,782 cycles
FLIGHT 5779 APU OIL PRESSURE CAUTION MESSAGE. REPLACED THE APU LOW OIL PRESSURE SWITCH.
Part: FLAP · airframe 2,307 hrs · 2,250 cycles
FLIGHT 5161 FLAPS FAIL MESSAGE DURING APPROACH.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 9-20-01.
2002
Part: BPSU — FAILED (T/E FLAP) · airframe 589 hrs · 646 cycles
FLIGHT 5117 FLAPS FAILED WHEN SELECTED UP AFTER T/O. REPLACED THE LT BPSU.
Part: BPSU — MALFUNCTIONED (L/H) · airframe 584 hrs · 640 cycles
FLIGHT 5324 FLAPS FAILED AT GATE WHEN SELECTED TO 20 DEGREES.REPLACED THE L/H BPSU.
Part: BPSU — MALFUNCTIONED (L/H) · airframe 548 hrs · 600 cycles
FLIGHT 5740 FLAPS FAILED AT GATE.REPLACED THE L/H BPSU.