N844CA
Registered owner: WILMINGTON TRUST CO TRUSTEE, DE (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.
12 reports on file, 1995-03-13 – 2004-10-20.
Part: BOLT — BENT (RUDDER) · airframe 6,048 hrs
DURING INSPECTION, FOUND RUDDER CONTROL HORN CENTER PIVOT BOLT BENT. APPARENT CAUSE IS SHEAR STRESS. TOTAL OF 10 SIMILAR PROBLEMS DISCOVERED IN FLEET OF 26 AIRCRAFT SINCE 5/26/2002.
Part: GOVERNOR — FAILED (RT ENGINE)
A/C YAWS RIGHT ON LANDING. RIGHT PROPELLER GOVERNOR FAILURE. REPLACED RIGHT PROPELLER GOVERNOR. (M)
Part: TEMP SENSOR — FAILED (LT ENGINE)
LEFT OIL TEMPERATURE GAUGE INOPERATIVE. OIL TEMPERATURE BULB (SENSOR) FAILED. REMOVED AND REPLACED LT OIL TEMPERATURE BULB.
Part: SWITCH — FAILED (COCKPIT)
CO-PILOTS PUSH TO TALK SWITCH INOPERATIVE. SWITCH FAILURE. REMOVED AND REPLACED PTT SWITCH. (M)
Part: AMPLIFIER — FAILED (COCKPIT)
RIGHT FIRE LOOP WILL NOT TEST. FIRE LOOP AMPLIFIER APPARENTLY FAILED. REPLACED RT FIRE LOOP AMPLIFIER. (M)
Part: SEAL — FAILED (RADOME)
WEATHER RADAR (P/N 6228439003) BECAME INOPERATIVE DUE TO EXCESSIVE MOISTURE IN RADOME. EXCESSIVE MOISTURE DUE TO THE RADOME SEAL.
Part: ACTUATOR — LEAKING (RT MLG)
RT MLG ACTUATOR LEAKING.
Part: FUEL DRAIN — MISSING (RT ENGINE)
RIGHT ENGINE FUEL DRAIN PLUG MISSING. REPLACED FUEL DRAIN ASSEMBLY. (M)
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 AS OTHER PREVIOUS IDENTIFIED AREAS OF CONCERN IN THE EMPENNAGE SECTION MAY BE RELATED. REPAIR WAS ACCOMPLISHED PER BEECHCRAFT RECOMMENDED PROCEDURE.
Part: DE-ICE — MISSING (RT PROP)
DE-ICE BOOT NOT MAINTAINING BOND TO PROPELLER BLADE. ONE BOOT SEPARATED IN FLIGHT FROM BLADE S/N 409MA. BOOT WAS INSTALLED AT OVERHAUL BY HARTZELL ON 11/18/94 NEW BOOT WAS INSTALLED IAW CHAPTER 30 OF BEECH MANUAL. (M)
Part: DEICE BOOT — MISSING (RIGHT PROPELLER)
RIGHT PROP, BLADE SN 398MA, HALF OF DEICE BOOT MISSING. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL AT WHICH TIME NEW BOOTS WERE INSTALLED. UPON INSPECTION OF BLADE, IT'S APPARENT THE PROBLEM LIES WITH THE PAINT BEING APPLIED TO THE BLADES PRIOR TO BOOT INSTALLATION.
Part: DE-ICE BOOT — MISSING (LEFT PROPELLER)
DE-ICE BOOTS NOT MAINTAINING BOND TO PROPELLER BLADES. TWO DE-ICE BOOTS DISCOVERED MISSING FROM SAME PROPELLER ON TWO DIFFERENT OCCASIONS. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL AT WHICH TIME NEW BOOTS WERE INSTALLED. UPON INVESTIGATION, IT IS APPARENT THE PROBLEM LIES WITH THE PAINT THAT IS APPLIED PRIOR TO BOOT INSTALLATION.