N699CA
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 |
| CATSKILL AIRWAYS,INC. | Operator | on 1987-02-11 | Operator named in NTSB report |
Accident & incident history
Operated by CATSKILL AIRWAYS,INC. (per NTSB report)
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.
8 reports on file, 2017-07-01 – 2025-12-05.
Part: ELEC CONNECTOR — BURNED (ZONE 100) · airframe 3,611 hrs · 3,614 cycles
PILOT REPORTED PITOT HEAT INOP. UPON INSPECTION THE PITOT SWITCH & SWITCH CONNECTION WERE FOUND TO BE BURNT. BOTH WERE REPLACED WITH NO ADDITIONAL DEFECTS NOTED.
Part: NUT — BROKEN (ENG CYLINGER) · airframe 3,540 hrs · 3,556 cycles
DURING TROUBLESHOOTING FOR A HIGH OIL CONSUMPTION CONCERN, IT WAS DISCOVERED THE RH ENG #2 CYLINDER BASE NUTS 1/2 IN. #3 AND 3/8 # 2,3,4 BROKEN AND MISSING FROM THROUGH STUDS. THE ENGINE WAS REPLACED WITH NO FURTHER ISSUES NOTED.
Part: PUMP — LEAKING (FUEL) · airframe 3,300 hrs · 3,358 cycles
PILOT REPORTED A SMELL OF GAS IN THE CABIN DURING FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT PRIMARY FUEL BOOT PUMP WITH NO ADDITIONAL FAULTS FOUND.
Part: FUEL RAIL — LEAKING · airframe 1,641 hrs · 1,731 cycles
PILOT REPORTED FUEL SMELL DURING FLIGHT. MAINTENANCE INSPECTED AND WHILE TROUBLESHOOTING FOUND RIGHT ENGINE INBOARD FUEL RAIL LEAKING AT WELD IN VICINITY OF #2 CYLINDER INJECTOR AT MALE B NUT. THE FUEL RAIL ASSEMBLY WAS REPLACED WITH NO FURTHER DEFECT NOTED. ENGINE MODEL NUMBER NOT LISTED IN SECTION 3. ENGINE MODEL TEO-540-C1A
Part: TRUNNION — DAMAGED (NLG) · airframe 91 hrs · 47 cycles
THE NLG ATTACH STRUCTURE WAS FOUND TO BE DAMAGED DURING AN INSPECTION INITIATED DUE TO SIMILAR FINDINGS ON OTHER COMPANY AIRCRAFT. THE DAMAGE IS LOCATED AT FWD MOST FUSELAGE BULKHEAD, LWR CENTER SECTION, IN THE AREA CORRESPONDING TO THE NLG MOUNTS. THE STRUCTURE AFT OF NLG BULKHEAD WAS INSPECTED WITH THE FOLLOWING DEFECTS NOTED: 1) THE FWD SECTIONS OF FLOORBOARD SUPPORTS AS THEY ARE RIVETED TO FORWARD-MOST FUSELAGE BULKHEAD ARE CRACKED. TECNAM SB387-CS EDITION 1 REVISION 0 PRESCRIBES REPAIR AND MODIFICATION OF THESE AREAS AND WILL SERVE AS CORRECTIVE ACTION FOR THIS DAMAGE.
Part: COOLING FAN — FAILED (E/E BAY) · airframe 55 hrs · 50 cycles
WHEN EXTERNAL POWER WAS APPLIED TO AIRCRAFT AN ELECTRICAL SMOKE ODOR WAS DETECTED IN COCKPIT. THE AVIONICS COOLING FAN WAS FOUND TO BE THE CAUSE OF ODOR.
Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 294,627 hrs · 21,449 cycles
LEFT FWD VERTICAL STAB, AFT DRAG ANGLE IS CRACKED. CUT OUT THE DAMAGE, FABRICATED A REPAIR, AND INSTALLED IAW REO 670-55-31-098, REO 670-55-31-018, REV A, AND SRM 51-25-01.
Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 294,627 hrs · 21,449 cycles
LEFT AFT VERTICAL STAB, AFT DRAG ANGLE IS CRACKED. CUT OUT THE DAMAGE, FABRICATED A REPAIR AND INSTALLED IAW REO 670-55-31-098, REO 670-55-31-018, REV A, AND SRM 51-25-01.