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T-6 Texan II

T-6 Texan II

Training Turboprop Aircrafts
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Basic Information
Name
T-6 Texan II
Designation
T-6 Texan II
Alternate Designation
Equipment Type
Training Turboprop Aircrafts
Manufacturer
Beechcraft Corporation
Date of Introduction
Description

The Hawker Beechcraft T-6 Texan II is a single-turboprop engine, tandem two-seat primary trainer designed to train students in basic flying skills common to US Air Force (USAF) and US Navy pilots. The T-6 Texan II derived from the Raytheon's Beech/Pilatus PC-9 Mk II turboprop trainer. The United States Joint Services awarded the Joint Primary Aircraft Training System (JPATS) contract to Raytheon (now Hawker Beechcraft Corporation) in 1996. The T-6A Texan II achieved initial operational capability as a training system in 2001.

Air & Air Defense Specifications
Crew 2
Max Speed 515.0 km/h
Range 1667.0 km
Overview (Deagel)
Group Training Turboprop Aircrafts
Status Active
Also Known As AT-6 (light attack variant), Effroni (Israel Air Force), JPATS (Joint Primary Aircraft Training Program)
Origin United States of America
Contractor Beechcraft Corporation
Initial Operational Capability (IOC) October 2001
Total Production 852
Unitary Cost USD $7.0 million
Specifications (Deagel)
Crew 2
Number of Engines 1
Dimensions — Height 3.2 meter
Dimensions — Length 10.2 meter
Dimensions — Wingspan 10.2 meter
Mass — Empty Weight 2,268 kilogram
Mass — Max Takeoff Weight 2,949 kilogram
Performance — Ceiling 9,449 meter
Performance — Max Range 1,667 kilometer
Power — Max Power at TakeOff 1,100 shp
Speed — Top Speed at High Altitude 143 mps
Gear (Deagel)
Item 1 Bombs: GBU-58 Paveway
Item 2 Turboprop Engines: PT6A-68 (1)
Variants
Variant 1 T-6A Texan II
Variant 2 T-6B Texan II
Details
Country of Origin United States
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
10.2 m
Width
10.2 m
Height
3.2 m
Weight
2949 kg
Operators (1)
United States
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