N855CA
Registered owner: MOON MOUNTAIN MONTANA LLC, MT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
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.
15 reports on file, 1995-08-01 – 2002-10-30.
Part: CLAMP — CRACKED (PROPELLER) · airframe 3,995 hrs
PROPELLER WAS RECEIVED FOR OVERHAUL AND DURING DYE PENETRANT INSPECTION TWO CRACK INDICATIONS WERE NOTED IN THE BOLT HOLE AREA. THEN AN EDDY CURRENT INSPECTION WAS PERFORMED WHICH CONFIRMED PRIOR INDICATIONS. CLAMP WAS RED TAGGED AND REMOVED FROM SERVICE. PART RETURNED TO HARTZELL PROPELLER FOR FURTHER EVALUATION.
Part: BOLT — BENT (RUDDER)
DURING INSPECTION OF RUDDER CONTROL SYSTEM, FOUND TORQUE TUBE MOUNT BOLTS LOOSE AND CONTROL HORN MOUNT BOLT BENT. PARTS RETURNED TO MFG FOR ANALYSIS.
Earlier reports · 1995–1999 · 13 reports
1999
Part: GOVERNOR — FAILED (RT ENGINE)
RIGHT ENGINE OVERSPEED GOVERNOR WILL NOT TEST. REPLACED GOVERNOR WITH OVERHAULED UNIT. OPERATIONAL AND LEAK CHECK SATISFACTORY.
Part: BLADE — LOOSE (LT ENGINE)
LEFT PROPELLER BLADE MOVEMENT OUTSIDE ALOOWABLE LIMITS IN HARTZELL SERVICE INSTRUCTIONS. PROPELLER REMOVED AND REPLACED. (M)
1998
Part: FUEL PUMP — LEAKING (LT ENGINE)
LEFT GEAR DOORS SHOW SIGNS OF FLUID LEAKAGE. LEFT ENGINE DRIVEN FUEL PUMP LEAKING. REPLACED LT ENGINE DRIVEN FUEL PUMP P/N 114-389042-5 IAW CHP 71 BEECH MM. (M)
Part: TEE HANDLE — FAILED (COCKPIT)
LT TEE HANDLE WILL NOT ILLUMINATE AT AMP TEST. TEE HANDLE FAILURE. REMOVED AND REPLACED TEE HANDLE.
1997
Part: LIFT TRANSDUCER — FAILED (LT WING)
STALL WARNING INTERMITTENT. LIFT TRANDUCER FAILURE. REMOVED AND REPLACED STALL LIFT TRANSDUCER.
Part: WIRING HARNESS — FAILED (LT ENGINE)
LEFT PROPELLER AUTOFEATHER WILL NOT TEST. REPLACED LEFT ENGINE FORWARD WIRING HARNESS.
Part: BLADE — BROKEN (LT PROPELLER)
AIRCRAFT STRUCK DEER AS IT WAS CLEARING RUNWAY AFTER LANDING AT SLK. BROKEN LT PROPELLER BLADE. POSSIBLE ENGINE DAMAGE. SOME STRUCTURAL DAMAGE TO COWLINGS/NACELLE AREA.
Part: POWER SECTION — FAILED (RT ENGINE)
RIGHT TORQUE INDICATION STUCK AT 3,000 FEET LBS. REMOVED AND REPLACED ENGINE POWER SECTION.
Part: GEAR MODULE — FAILED (COCKPIT)
NOSE GEAR ANNUNCIATOR INOPERATIVE.
Part: LOW PRESS SWITCH — FAILED (LT ENGINE)
LEFT AUTOFEATHER WILL NOT TEST. INVESTIGATION FOUND LOW PRESSURE SWITCH FAILED.
1996
Part: RIVETS — LOOSE (VERT STAB)
DURING SCHEDULED INSPECTIONS, LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A SIMILAR PROBLEM WAS ADDRESSED IN SB 2004 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AT OTHER PREVIOUS IDENTIFIED AREAS OF CONCERN IN THE EMPENNAGE SECTION MAY BE RELATED. REPAIR WAS ACCOMPLISHED PER BEECHCRAFT RECOMMENDED PROCEDURE.
Part: RIVETS — LOOSE (VERT STAB)
DURING SCHEDULED INSPECTIONS, LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A SIMILAR PROBLEM WAS ADDRESSED IN SB 2044 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AS OTHER PREVIOUS IDENTIFIED AREAS OF CONCERN IN THE EMPENNAGE SECTION MAY BE RELATED. REPAIR WAS ACCOMPLISHED PER BEECHCRAFT RECOMMENDED PROCEDURE.
1995
Part: DEICE BOOT — MISSING (RT PROPELLER)
RIGHT PROPELLER MISSING DEICE BOOT BLADE, S/N UNKNOWN. FURTHER INSPECTION FOUND 3 SEPARATE CRACKS IN LEADING EDGE OF 2 BLADES, S/N UNKNOWN. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL.