N158BC

EUROCOPTER DEUTSCHLAND GMBH EC135P1 · 1999 · Valid Registration

Registered owner: METRO AVIATION INC, LA (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
METRO AVIATION, INC (HDNA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

O · 2024-01-18 Matched by certificate designator
ATA 5314

CORROSION FOUND ON LH FWD KEEL BEAM, DOUBLER AND FITTING - RDAS FROM AHI 135 53 014 23, AHI 135 53 014 23, RDAS EC135 53 2024 0009A FOR REPLACEMENT OF THE KEEL BEAM DOUBLER AND REPAIR.

Source: SDR HDNA2024011810001 · FAA SDRS
O · 2021-03-25 Matched by certificate designator
ATA 5311

FRAME 5 AND TRANSMISSION DECK CRACKING DISCOVERED DURING HEAVY MAINTENANCE EVENT. SERVICE BULLETIN SB 53 032 028 TO REPAIR FRAME 5 CRACKING WAS APPLIED AND COMPLIED WITH.

Source: SDR HDNA2021032510003 · FAA SDRS
M J · 2003-10-13 Matched by certificate designator
ATA 7921

DURING A LAW ENFORCEMENT FLIGHT, PART 91 THE NR 1 ENGINE OIL COOLER SHAFT SHEARED CAUSING ENGINE OIL TEMPERATURE TO INCREASE TO ABOUT 120 C WHILE ALL OTHER ENGINE PARAMETERS REMAINED NORMAL. AIRSPEED WAS INCREASED AS RECOMMENDED IAW MFG MM TO SLIGHTLY ABOVE 80 KNTS FROM 60 KNTS. OIL TEMPERATURE DID NOT DECREASE. PRECAUTIONARY LANDING WAS MADE. REPLACED OIL COOLER HUB WITH MFG PN L792M3007215. PERFORMED LEAK CHECK AND OPS CHECK, ALL ENGINE PARAMETERS ARE WITHIN LIMITS.

Source: SDR B1E2003F00001 · FAA SDRS
O · 2003-08-11 Matched by certificate designator
ATA 7714

ENGINE NR 2 ENCOUNTERED A FADEC FAILURE AT 50 PERCENT TORQUE DUE TO LOSS OF ELECTRICAL SIGNAL FROM COMPRESSOR TURBINE SPEED SENSOR. REPLACED SENSOR WITH PREVIOUSLY OVERHAULED UNIT WITH 1015.20 HOURS SINCE NEW. OPERATIONAL CHECK GOOD NO OTHER DEFECTS NOTICED AT THIS TIME.

Source: SDR B1E2003F00000 · FAA SDRS