N847BA

BEECH 200 · 1981 · Fixed-wing multi-engine · 2 engines · 11 seats · Valid Registration

Registered owner: BEECH TRANSPORTATION INC, MN (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
Aviation Charter Inc (ABOA)Certificate holderMatched by certificate designator

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.

3 reports on file, 2000-11-25 – 2018-09-05.

FALSE WARNING · 2018-09-05 Matched by certificate designator
ATA 2612

Part: FIRE DETECTOR — FALSE ACTIVATION (RT ENGINE) · airframe 15,007 hrs · 15,840 cycles

RIGHT ENGINE FIRE LIGHT IN FLIGHT. FALSE INDICATION DUE TO LIGHT HITTING FIRE DETECTOR AT 12 O CLOCK POSITION ON RIGHT ENGINE. INSPECTED AND TESTED SYSTEM ON GROUND. OPERATIONAL CHECK GOOD.

Source: SDR ABOA2019F00045
ENGINE FLAMEOUT; WARNING INDICATION · 2009-04-28 Matched by certificate designator
ATA 7322

Part: PUMP — SEIZED (FUEL) · airframe 9,276 hrs · 9,478 cycles

ON CLIMB OUT FROM AIRPORT THE RT ENGINE EXPERIENCED A FLAMEOUT AND SHUTDOWN, THE CREW DECLARED AN EMERGENCY AND LANDED AT AIRPORT WITHOUT FURTHER INCIDENT. MX FOUND THE ENGINE DRIVEN HIGH PRESSURE FUEL PUMP TO BE FAULTY. THE PUMP WAS REPLACED, ENGINE GROUND PERFORMANCE RUNS WERE ACCOMPLISHED, AND ACFT WAS RELEASED BACK TO SERVICE. THIS ENGINE IS OPERATED UNDER THE MORE PROGRAM STC NR SE00001EN, REV 3 DATED DEC 28, 2000, WITH AN ACCESSORY TBO OF 4100 HOURS. THE FUEL PUMPS TIME SINCE OVERHAUL WAS 3,701.1.

Source: SDR ABOA475B001
FLUID LOSS · 2000-11-25 Matched by certificate designator
ATA 2820

Part: PUMP — LEAKING (ENG ACCY CASE)

DURING FLIGHT, THE FUEL FLOW DROPPED OFF UNTIL THE ENGINE TORQUE DROPPED ENOUGH TO FEATHER THE PROPELLER. THE CREW THEN SHUT THE ENGINE OFF WITH THE FUEL CONDITION LEVER. MAINTENANCE FOUND THE 4 SCREWS (THAT WERE SAFTIED) HOLDING THE PRESSURE RELIEF ADJUSTMENT PLATE ONTO THE LOW PRESSURE FUEL PUMP LOOSE, AND FUEL LEAKING, SUSPECT AIR WAS BEING INTRODUCED INTO THE FUEL SYSTEM HERE AND CAVITATED THE HIGH PRESSURE PUMP CAUSING LOSS OF FUEL TO FCU. (X)

Source: SDR 20001214SH028