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IA-63 Pampa

IA-63 Pampa

Training Jets
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Basic Information
Name
IA-63 Pampa
Designation
IA-63 Pampa
Alternate Designation
AT-63 Pampa
Equipment Type
Training Jets
Manufacturer
FAdeA, Lockheed Martin
Date of Introduction
1988
Description

IA-63 Pampa is a single-engine, twin-seat, subsonic trainer developed in the early 1980s to meet the requirements of the Argentinean Air Force. It was originally developed by Argentina's FMA which was purchased by Lockheed Martin in the mid 1990s becoming Lockheed Martin Aircraft Argentina. Pampa's design was influenced by Alpha Jet ultimately adopting a similar aerodynamic configuration. Powered by a fuel efficient TFE731 turbofan engine Pampa is able to reach a top speed of Mach 0.62+ at high altitude. Besides, the IA-63 is able to perform ground attack missions utilizing free fall bombs and its 30mm DEFA cannon. So far, the Argentinean Air Force is the only known Pampa operator. Starting in 1988 the Argentinean Air Force took delivery of a first lot of 18 Pampas with a second order for 46 aircraft delivered from the late 1990s. Currently, Lockheed Martin Aircraft Argentina is developing a modular low-cost advanced trainer and light attack variant called the AT-63 Pampa for the Argentinean Air Force. Its first flight occurred on June 30, 2005. The AT-63 features digital avionics and upgraded crew station including sophisticated mission computers to support advanced weapon systems. Overall the new upgraded Pampa may reduce maintenance costs using modular approach to systems design.

Air & Air Defense Specifications
Crew 2
Max Speed 752.4 km/h
Range 1000.0 km
Service Ceiling 12900 m
Wingspan 9.70 m
Overview (Deagel)
Group Training Jets
Status Active
Also Known As AT-63 Pampa
Origin Argentina
Contractors FAdeA, Lockheed Martin
Initial Operational Capability (IOC) 1988
Total Production 64
Specifications (Deagel)
Crew 2
Number of Engines 1
Dimensions — Height 4.3 meter
Dimensions — Length 10.9 meter
Dimensions — Main Gun Caliber 30 millimeter
Dimensions — Wingspan 9.7 meter
Mass — Empty Weight 2,820 kilogram
Mass — Max Takeoff Thrust 35,000 pound
Mass — Max Takeoff Weight 5,000 kilogram
Mass — Payload 1,550 kilogram
Performance — Ceiling 12,900 meter
Performance — Max Range 1,000 kilometer
Speed — Top Speed at High Altitude 209 mps
Time — Flight Endurance 3.8 hour
Gear (Deagel)
Item 1 Turbofan Engines: TFE731 (1)
Details
Country of Origin Argentina
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
10.9 m
Width
9.7 m
Height
4.3 m
Weight
5000 kg
Operators (1)
Argentina
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