N443CA
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
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.
32 reports on file, 2002-02-27 – 2025-03-17.
Part: ENGINE — SHUTDOWN (LEFT) · airframe 2,373 hrs · 2,547 cycles
APPROXIMATELY 30 MINUTES INTO THE FLIGHT, THE LT ENGINE DROPPED TO 15" MAP AND THEN RETURNED TO 36" MAP ~3 TIMES. AFTER ~10 MORE SECONDS THE LT ENGINE MAP DROPPED TO 0" AND THE POWER PERCENTAGE INDICATED 0 FOR ~20 SECONDS. THE LT ENGINE WAS SECURED AND THE AIRCRAFT DIVERTED TO KPWM. NO OBVIOUS DEFECTS OR LEAKS WERE NOTED DURING POST EVENT INSPECTION. POST EVENT GROUND RUNS WERE NORMAL. GARMIN AND DLU DATA FILES HAVE BEEN PROVIDED TO THE ENGINE MANUFACTURER FOR ANALYSIS. THE ENGINE AND ECU HARNESS HAVE BEEN RETURNED TO THE ENGINE MANUFACTURE FOR EVALUATION.
Earlier reports · 2002–2021 · 31 reports
2021
Part: WHEEL — BROKEN · airframe 341 hrs · 478 cycles
DURING POST-FLIGHT INSPECTION, TWO BOLTS ON THE RIGHT MAIN GEAR WHEEL ASSEMBLY WERE FOUND TO BE SHEARED OFF. THE WHEEL ASSEMBLY WAS REPLACED WITH NO ADDITIONAL DEFECTS NOTED.
2008
Part: CONTROLLER — MALFUNCTIONED (ANTI-ICE SYSTEM) · airframe 17,700 hrs · 15,635 cycles
EN ROUTE JFK-YUL RECEIVED MULTIPLE ANTI-ICE CAUTION MESSAGES, FLIGHT RETURNED TO JFK. PERFORMED RESET OF THE AIR DATA SYSTEM (ADS) CONTROLLER NR 2.
Part: SENSING ELEMENT — FAILED (RT FUSELAGE) · airframe 15,975 hrs · 14,241 cycles
FLIGHT 5104- EN ROUTE FROM BNA TO JFK RECEIVED ANTI-ICE DUCT WARNING MESSAGE. PERFORMED QRH, MESSAGE PERSISTED. EMERGENCY DECLARED AND AIRCRAFT DIVERTED TO GSO AND LANDED SAFELY. REMOVED AND REPLACED RIGHT SIDE FUSELAGE SENSING ELEMENT (A18WK).
2007
Part: BPSU — FAULTY (T/E FLAP) · airframe 15,341 hrs · 13,753 cycles
FLIGHT 5345 - RECEIVED FLAP FAIL CAUTION MESSAGE DURING CRUISE. LANDED CVG WITHOUT INCIDENT. REPLACED LEFT BPSU. NO FURTHER DEFECTS.
Part: ACTUATOR — FAULTY (LT TE FLAP) · airframe 15,294 hrs · 13,720 cycles
FLIGHT 5089 - FLAPS FAILED AT 8 DEGREES ON APPROACH INTO MSP. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED LEFT I/B FLAP O/B ACTUATOR.
Part: COMPUTER — FAULTY (TE FLAPS) · airframe 15,292 hrs · 13,718 cycles
FLIGHT 5086 - FLAPS FAIL ON TAXI OUT. AIRCRAFT RETURNED TO GATE. REMOVED AND REPLACED FECU.
Part: ACTUATOR — FAULTY (LT TE FLAP) · airframe 15,294 hrs · 13,720 cycles
FLIGHT 5089 - FLAPS FAILED AT 8 DEGREES ON APPROACH INTO MSP. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED LEFT I/B FLAP I/B ACTUATOR.
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 15,290 hrs · 13,716 cycles
FLIGHT 5641 - FLAPS FAIL CAUTION MESSAGE CAME ON AT FLIGHT LEVEL 320 WITH FLAPS AT 0 DEGREES. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.
Part: SEAL — FAILED (PAX DOOR) · airframe 14,569 hrs · 1,314 cycles
FLIGHT 5169 - LOUD NOISE AT MAIN PAX DOOR. AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED PAX DOOR SEAL.
Part: IDG — FAILED (NR 2 ENGINE) · airframe 14,475 hrs · 13,061 cycles
FLIGHT 5045 - ABORTED TAKEOFF FOR NR 2 GEN FAIL ON TAKEOFF. REMOVED AND REPLACED NR 2 IDG.
Part: FLAP — MALFUNCTIONED (WING) · airframe 13,613 hrs · 12,359 cycles
FLIGHT 5137 - DURING YYZ APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 13,578 hrs · 12,330 cycles
FLIGHT 9453 - FLAP CAUTION MESSAGE RECEIVED ON APPROACH. LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C) FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES.
2006
Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 12,997 hrs · 11,851 cycles
FLIGHT 5081- EMERGENCY LIGHT STRIPS NEXT TO DOOR INOP. REMOVED AND REPLACED LAMP FLEX WITH ARROWS (LIGHT STRIP).
Part: TRANSDUCER — FAULTY (LEFT ENGINE) · airframe 12,635 hrs · 11,481 cycles
FLIGHT 5230 - DURING TAKEOFF ROLL THE LEFT ENGINE OIL PRESSURE DROPPED TO ZERO PSI WITH NO AURAL WARNINGS. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE LEFT ENGINE OIL PRESSURE TRANSDUCER.
Part: WINDOW — CRACKED (COCKPIT) · airframe 11,904 hrs · 10,746 cycles
FLIGHT 5878 - EN ROUTE BOS-DCA THE CAPTAIN'S WINDSHIELD CRACKED. REPLACED THE CAPTAIN'S WINDSHIELD.
Part: ACTUATOR — FAULTY (TE FLAPS) · airframe 11,805 hrs · 10,642 cycles
FLIGHT 5332 - DURING APPROACH INTO LAN, RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREES, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LEFT FLAP INBOARD FLAP ACTUATOR.
Part: ACTUATOR — FAULTY (TE FLAP) · airframe 11,805 hrs · 10,642 cycles
FLIGHT 5332 - DURING APPROACH INTO LAN, RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREES, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT FLAP INBOARD FLAP ACTUATOR.
Part: PDU — FAULTY (TE FLAPS) · airframe 11,802 hrs · 10,638 cycles
FLIGHT 5017 - DURING CVG APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREES. CREW DECLARED AN EMERGENCY, ABORTED APPROACH THEN LANDED WITHOUT INCIDENT ON SECOND ATTEMPT. REPLACED THE FLAP POWER DRIVE UNIT ASSEMBLY.
Part: ECU — FAULTY (TE FLAPS) · airframe 11,802 hrs · 10,638 cycles
FLIGHT 5017 - DURING CVG APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREES. CREW DECLARED AN EMERGENCY, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT ON SECOND ATTEMPT. REPLACED THE FLAP ELECTRONIC CONTROL UNIT.
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 11,799 hrs · 10,636 cycles
FLIGHT 5327 - DURING APPROACH INTO YUL RECEIVED A FLAP FAIL CAUTION MESSAGE. 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: COMPUTER — MALFUNCTIONED (AVIONICS) · airframe 9,385 hrs · 8,499 cycles
FLIGHT 5250 FUEL CHANNEL 1 AND 2 FAIL. NO FUEL INDICATION. REPLACED THE FUEL COMPUTER.
2004
Part: PUMP — FAILED (HYD SYSTEM) · airframe 6,480 hrs · 5,964 cycles
FLIGHT 5232 GEAR DISAGREE WARNING AND HYDRAULIC SYSTEM 3 CAUTION. REPLACED THE SYSTEM 3A ACMP.
Part: ODOR — DETECTED (COCKPIT) · airframe 5,859 hrs · 5,470 cycles
FLIGHT 5603 BURNING ODOR IN COCKPIT. COULD NOT DUPLICATE. RAN ENGINES AND APU AND NO BURNING ODOR FOUND.
2003
Part: ACTUATOR — FAILED (T/E FLAP) · airframe 5,528 hrs · 5,185 cycles
FLIGHT 5768 DURING DESCENT TO ERI RECEIVED A FLAP FAIL CAUTION MESSAGE AT TWO DEGREES FLAP POSITION. REPLACED THE RIGHT NR 2 INBOARD FLAP ACTUATOR.
Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 5,522 hrs · 5,184 cycles
FLIGHT 5006 DURING APPROACH TO YUL RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO DEGREES FLAP POSITION. 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.
Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 5,477 hrs · 5,135 cycles
FLIGHT 5332 FLAPS FAILED WARNING. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
Part: BPSU — MALFUNCTIONED (TE FLAPS) · airframe 5,483 hrs · 5,138 cycles
FLIGHT 5375 FLAPS FAILED. REPLACED THE RT BPSU.
Part: ACTUATOR — UNRELIABLE (R/H WING) · airframe 3,129 hrs · 3,090 cycles
FLIGHT 5194 FLAPS FAIL MESSAGE DURING APPROACH.COULD NOT DUPLICATE; REPLACED ALL 4 R/H WING FLAP ACTUATORS FOR TROUBLESHOOTING.
Part: FLAP · airframe 3,124 hrs · 3,084 cycles
FLIGHT 5617 FLAPS FAIL CAUTION MESSAGE FLAPS FAILED AT 26 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01.
2002
Part: VIBRATOR · airframe 566 hrs · 630 cycles
FLIGHT 5980 VERY LOUD NOISE AND VIBRATION FROM FORWARD HALF OF AIRCRAFT.COULD NOT DUPLICATE. INSPECTION OF AIRCRAFT FOUND NO DEFECTS.
Part: FLAP · airframe 542 hrs · 607 cycles
FLIGHT 551 FLAPS FAILED AT 17 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.