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LM-100J

Detailed profile for this aircraft model.

Overview

LM-100J is a airplane model with turboprop engine(s).

Specifications

ICAO: -

IATA: -

Engine Count: 4

Fuel capacity: 25817 litre

MLW: 64864 kilogram

MTOW: 74389 kilogram

MTW: 74389 kilogram

MZFW: 58513 kilogram

Maximum operating altitude: 32200 foot

Vfe: 149 knot

Vle: 170 knot

Vlo: 170 knot

Aircraft Type

L-382J Hercules II

Manufacturer

Lockheed Martin