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E-9A

E-9A

Surveillance & Reconnaissance Airplanes
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Basic Information
Name
E-9A
Designation
E-9A
Alternate Designation
Equipment Type
Surveillance & Reconnaissance Airplanes
Manufacturer
Bombardier, Sierra Nevada Corporation
Date of Introduction
1988
Description

The United States Air Force E-9A is an airborne ocean surface surveillance and telemetry data recording and relay aircraft used as a surveillance platform to ensure the Gulf of Mexico waters are clear of civilian boaters and aircraft during live missile launches and other hazardous military activities. The twin turboprop is a derivative of the Q100 airliner fitted with the AN/APS-143(V)1 Airborne Sea Surveillance Radar to detect objects in the Gulf of Mexico. The aircraft was developed in the 1980s. Sierra Research carried out the modification work on the Q100 platform supplied by Bombardier. The E-9A also provides support for air-to-air weapons system evaluation, development and operational testing at Tyndall Air Force Base, Florida. Besides, this airplane can be used in short-haul regional airline operations in its civilian capacity. The first of two E-9As operated by the US Air Force was declared operational in June 1988. The E-9A aircraft can detect a person in a life raft up to 25 miles away in the water. It downlinks this telemetry data to the range safety officer who determines the shoot area for live-fire activity. The aircraft has a fixed antenna array that receives and records telemetry from test and drone vehicles flying over the Gulf of Mexico. It has the capability to relay two airborne UHF frequencies over the horizon to ground sites. The E-9A has a four-man crew, two pilots and two mission operators. So far, the 82nd Aerial Targets Squadron located at Tyndall Air Force Base (AFB) has supported proof of concept for the advanced cruise missile, the Navy Fjord missile program, and F-22 Raptor live missile testing.

Air & Air Defense Specifications
Crew 4
Range 1609.0 km
Service Ceiling 9144 m
Wingspan 25.91 m
Overview (Deagel)
Group Surveillance & Reconnaissance Airplanes
Status Active
Origin Canada
Contractors Bombardier, Sierra Nevada Corporation
Initial Operational Capability (IOC) June 1988
Total Production 2
Unitary Cost USD $16.5 million
Specifications (Deagel)
Crew 4
Number of Engines 2
Dimensions — Height 24.5 foot
Dimensions — Length 73 foot
Dimensions — Wingspan 85 foot
Mass — Fuel Load 5,600 pound
Mass — Max Takeoff Weight 34,500 pound
Mass — Payload 697 pound
Performance — Ceiling 30,000 foot
Performance — Max Range 1,000 mile
Power — Max Power at TakeOff 3,600 shp
Speed — Cruise Speed 280 mph
Gear (Deagel)
Item 1 Radar Systems: AN/APS-143(V)1 (1)
Item 2 Turboprop Engines: PW120A (2)
Details
Country of Origin Canada
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
22.25 m
Width
25.91 m
Height
7.47 m
Weight
15648.92 kg
Operators (1)
United States
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