N190CH

BOEING-VERTOL 107-II · 1962 · Valid Registration

Registered owner: COLUMBIA HELICOPTERS INC, OR (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
COLUMBIA HELICOPTERS, INC (CHIA)Certificate holderMatched by certificate designator

Accident & incident history

Accident · 1983-08-20 Matched by aircraft (N-number)
BOEING VERTOL BV-107-II Fatal injuryCOLUMBIA HELICOPTERS, INC
Source: NTSB case LAX83FA395

Maintenance disclosures

M Y · 2026-06-22 Matched by certificate designator
ATA 7200

DURING CRUISE FLIGHT, STRAIGHT AND LEVEL, ACFT SHUTTERED BRIEFLY THEN IN PILOTS HEADSETS HEARD AN AUDIBLE ENGINE OVER-TEMP ALARM. NG AND ENGINE OIL PRESSURE ON THE NR 1 ENGINE WERE AT ZERO AND PILOTS CONDUCTED SINGLE ENG FAILURE PROCEDURE. AFTER DEALING WITH THE ENG FAILURE & WE WERE ESTABLISHED IN SINGLE ENG FLT WE ATTEMPTED AN IN AIR RESTART OF THE NR 1 ENG. WERE UNSUCCESSFUL 3 TIMES TO RESTART DUE TO THERE BEING NO NG INDS. SECURED THE NR 1 ENG AND CONTINUED SINGLE ENG FLT BACK TO ZAMBOANGA. PILOTS DISCUSSED WHAT COULD HAVE FAILED AND CAME UP WITH THE ASSUMPTION THAT THE RADIAL DRIVESHAFT FROM THE COMPRESSOR HAD FAILED AND THE ACCESSORY DRIVE GEARBOX WAS NO LONGER BEING POWERED. WE HAD NOTICED THAT WHEN ATTEMPTING TO RESTART THE ENGINE, TIT WOULD DROP BECAUSE COLD AIR WAS BEING DRAWN IN, SO THE COMPRESSOR WAS ROTATING BUT WE RECEIVED NO NG OR ENGINE OIL INDICATIONS.

Source: SDR CHIA2026062210939 · FAA SDRS
R J · 2013-08-13 Matched by certificate designator
ATA 7200

PILOTS REPORTED THAT DURING A DESCENT, NR 1 ENGINE TORQUE WAS AT 25 PERCENT AND NR 2 ENGINE TORQUE WAS AT 7 PERCENT. PULLED IN POWER TO INCREASE TORQUE ON THE NR 2 ENGINE. DURING PULL IN OF POWER, NR 2 ENGINE TORQUE DECREASED TO 1 PERCENT MOMENTARILY PRIOR TO MATCHING UP ALL PARAMETERS (TORQUE, NG, T5). RETURNED ACFT TO MX BASE. REPLACED THE NR 2 ENGINE.

Source: SDR CHIR20131608001 · FAA SDRS