N858CA
Registered owner: MGMB AERO LLC, ND (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
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, 1996-02-28 – 1998-10-24.
Part: ACTUATOR — FAILED (TE FLAP)
FLAPS STUCK AT 17 DEGREES. SECURED FLAPS TO UP POSITION. INSPECTION OF COMPONENTS FOUND LT INBD ACTUATOR FAILURE. REMOVED AND REPLACED LT INBD FLAP ACTUATOR IAW RAYTHEON MAINTENANCE MANUAL CHAPTER 27. (M)
Part: SWITCH — FAILED (LT MLG)
AUTOFEATHER OFF ANNUNCIATOR STAYS ON INFLIGHT. LEFT MAIN LANDING GEAR UPLOCK SWITCH FAILED. REPLACED LEFT MAIN LANDING GEAR UPLOCK SWITCH, RETRACTION CHECK SAT IAW CHAPTER 32. (M)
Part: PUMP — FAILED (LT ENGINE)
LEFT ENGINE FUEL LEAK NOTED. LEFT ENGINE LOW PRESURE PUMP LEAKING. REPLACED LT ENGINE LOW PRESSURE FUEL PUMP. (M)
Part: FUEL PUMP — LEAING (LT ENGINE)
FUEL LEAK UNDER LT COWL. FUEL PUMP LEAKING. REMOVED AND REPLACED FUEL PUMP. (M)
Part: WINDSHIELD — CRACKED (COCKPIT)
RIGHT WINDSHIELD CRACKED. REPLACED WINDSHIELD. (X)
Part: VOLTMETER — FAILED (COCKPIT)
AC VOLTMETER INOPERATIVE. REPLACED INDICATOR.
Part: DE-ICE BOOT — TORN (LT WING)
LEFT INBOARD DE-ICE BOOT BOTTOM SIDE LOOSE. INSTALLED NEW BOOT.
Part: PRESSURE SWITCH — STUCK (RT WING)
RIGHT ENGINE FUEL PRESSURE ANNUNCIATOR INOPERATIVE.
Part: INVERTER — SHORTED (RIGHT NACELLE)
RIGHT INVERTER INOPERATIVE.
Part: RT UNIT — SHORTED (RADAR)
RADAR FAULT ANNUNCIATOR ILLUMINATED.
Part: BEARINGS — WORN (AILERONS)
DURING ROUTINE MAINTENANCE, BOTH AILERONS WERE DISCOVERED AS HAVING EXCESSIVE FREE PLAY. UPON INSPECTION OF COMPONENTS, ALL THREE ATTACHMENT BEARINGS AND MOUNTING HARDWARE WERE FOUND WORN AND LOOSE. BEARINGS AND HARDWARE REPLACED WITH NEW. (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 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.