N49KC

BEECH 200 · 1977 · 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.

5 reports on file, 1998-11-02 – 2020-11-05.

PARTIAL RPM/PWR LOSS; WARNING INDICATION · 2020-11-05 Matched by certificate designator
ATA 2822

Part: BEARING — FAILED (FCU DRIVESHAFT) · airframe 19,295 hrs · 18,950 cycles

FUEL CONTROL UNIT DRIVE SHAFT BEARINGS STARTED TO FAIL CAUSING ENGINE TORQUE AND FUEL FLOW FLUCTUATIONS. ENGINE WAS NOT SHUT DOWN IN FLIGHT, REMOVED FUEL CONTROL UNIT TO FIND DRIVE SHAFT BEARINGS FAILING AND FUEL CONTROL UNIT TO HIGH PRESSURE FUEL PUMP DRIVE (PLASTIC) COUPLING ALMOST SHEARED.

Source: SDR ABOR20201113001
OTHER · 2015-07-23 Matched by certificate designator
ATA 5510

Part: HINGE FITTING — CRACKED (HORIZONTAL STAB) · airframe 16,952 hrs · 16,645 cycles

FOUND LT HORIZONTAL STABILIZER MIDDLE ELEVATOR HINGE LOWER OTBD HINGE CLIP CRACKED, THIS WAS FOUND DURING THE HORIZONTAL STABILIZER ANNUAL INSPECTION.

Source: SDR 2015FA0000329
PARTIAL RPM/PWR LOSS · 2014-10-08 Matched by certificate designator
ATA 7603

Part: FRICTION LOCK — BROKEN (POWER LEVER) · airframe 16,624 hrs · 16,305 cycles

FRICTION LOCK ON THE POWER LEVER BROKE DURING CLIMB, WHICH ALLOWED THE POWER LEVER TO GO TO IDLE.

Source: SDR ABOA2015F00000
FALSE WARNING · 2012-10-16 Matched by certificate designator
ATA 2612

Part: FIRE LOOP — CONTAMINATED (LT NACELLE) · airframe 15,471 hrs · 15,117 cycles

AIRCRAFT WAS FLYING IN HEAVY RAIN AND THE LEFT ENGINE FIRE WARNING LIGHT CAME ON AND PILOTS HSI FAILED, PILOT SHUTDOWN THE LEFT ENGINE AND LANDED. MX FOUND AVIONICS BAY VERY WET, SEALED NOSE AVIONICS BAY TO PREVENT MOISTURE FROM ENTERING. FOUND LEFT ENGINE FORWARD FIRE DETECTOR WIRING VERY WET, INSTALLED SEALED WIRE SPLICES ON FIRE DETECTION WIRING. DRYED AVIONICS BAY, HSI AND FIRE DETECTION WORKED NORMAL.

Source: SDR ABOA2012F00217
OTHER · 1998-11-02 Matched by certificate designator
ATA 5620

Part: WINDOW — CRACKED (CABIN)

DURING POST-FLIGHT INSPECTION, FLIGHT CREW DISCOVERED A 6 INCH CRACK IN RIGHT 'VESTIBULE' WINDOW. THEY REPORTED NO PRESSURE LOSS OR NO ABNORMAL INDICATION DURING THEIR FLIGHT. MAINTENANCE REMOVED AND REPLACED WINDOW AND FOUND NO OBVIOUS REASON FOR THE CRACK.

Source: SDR 99ZZZX971