N265CA
Registered owner: ZACHERL RANDALL L, PA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Comair Limited | Operator | on 1997-01-09 | Operator named in NTSB report |
Accident & incident history
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.
14 reports on file, 1995-03-03 – 1997-01-01.
Part: REGULATOR — MALFUNCTION (WING)
OUTBD WING ANTI-ICE SYSTEM FAIL WARNING ON BOTH TIMERS AND 2. REPLACED THE WING DE-ICE PRESSURE REGULATOR.
Earlier reports · 1995–1996 · 13 reports
1996
Part: PITCHLOCK SCREW — FAILED (PROP ACTUATOR)
PROPELLER ASSEMBLY WAS ORIGINALLY REMOVED FROM AIRCRAFT FOR ENGINE RELATED MAINTENANCE. ONCE REMOVED, IT WAS DISCOVERED THAT THE ACTUATOR FEATHER STOP TAB HAD BEEN DISPLACED APPROXIMATELY .25 INCH. PITCH LOCK SCREW WAS REMOVED FROM SERVICE AND RETURNED TO MANUFACTURER.
Part: INDICATOR — MALFUNCTION (INST PANEL)
CABIN PRESSURIZATION FLUCTUATED 1,500 FT IN AUTO MODE BUT WAS STABLE IN MANUAL. REPLACED THE CABIN PRESSURIZATION TRIPLE INDICATOR SYSTEM, CHECK NORMAL.
Part: COMPRESSOR — DAMAGED (LT ENGINE)
LEFT ENGINE HAS FOD DAMAGE ON COMPRESSOR BLADES. REPLACED ENGINE.
Part: AIR SPEED IND — FAILED (RT INST PANEL)
COPILOT'S AIR SPEED INDICATOR FAILED DURING TAKEOFF. REPLACED THE AIR SPEED INDICATOR. PART TOTAL CYCLES, 7,765.
Part: RELIEF VALVE — MALFUNCTIONED (LT PROP)
LEFT PROPELLER HAS UNUSUAL VIBRATION AND IS SLOW TO ACCELERATE WHEN COMING OUT OF FEATHER. REPLACED THE PROPELLER HUB RELIEF VALVE.
Part: PROX SENSOR — DEFECTIVE (RT MLG)
NOSE WHEEL STEERING FAILED DURING LANDING. REPLACED THE RT MLG WEIGHT ON WHEELS PROXIMITY SENSOR.
Part: RELAY — FAILED (NLG STEERING)
NOSE WHEEL STEERING FAILED DURING LANDING. REPLACED RELAY KO 123.
Part: CIRCUIT BREAKER — TRIPPED (AURAL WARNING)
TRIM AURAL WARNING SOUNDED DURING TAKEOFF ROLL. FOUND AURAL WARNING CIRCUIT BREAKER TRIPPED. RESET BREAKER AND SYSTEM TEST NORMAL.
1995
Part: DOOR WARNING — MALFUNCTIONED (CARGO DOOR)
CARGO DOOR WARNING LIGHT CAME ON DURING CLIMB. FOUND TO BE FALSE WARNING. PLACED DOOR WARNING SYSTEM ON DEFERRED MAINT LIST AND ACFT CONTINUED SERVICE.
Part: ACTUATOR — LEAKING (NLG)
HYDRAULIC FLUID LEAKING FROM NOSE GEAR WHEEL WELL. FOUND NOSE GEAR ACTUATOR LEAKING. REMOVED AND REPLACED ACTUATOR WITH SERVICEABLE UNIT.
Part: SUPPORTS — CRACKED (LT/RT WING)
THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION ASK NR 5720-551/651-01I AT WING RIBS NR 15 AND 16. THE SKIN SUPPORTS WERE REPAIRED IAW AERODESIGN REPORT NR 1327-2 AND EMB SRM P/N: 120-17056-019, 1 EA; 120-17056-017, 2 EA; 120-17056-015, 4 EA; 120-17057-006, 1 EA; 120-17057-005, 1 EA.
Part: ACTUATOR — LEAKING (LT)
LEFT ENGINE LEAKING OIL FROM THE PROPELLER AREA. REPLACED THE PROPELLER ACTUATOR ASSY.
Part: ANGLE — CRACKED (LT MLG DOOR)
LEFT MLG DOOR OPENED IN FLIGHT. REPLACED CRACKED AFT HINGE BRACKET ON MLG DOOR.