T-6 Texan II
T-6 Texan II
Training Turboprop Aircrafts
Operational Photo













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
Sources
deagel.com: https://www.deagel.com/x/x/a000247
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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