Pilatus PC-7 Turbo-Trainer
Pilatus PC-7 Turbo-Trainer
Training Turboprop Aircrafts
Basic Information
Name
Pilatus PC-7 Turbo-Trainer
Designation
Pilatus PC-7 Turbo-Trainer
Alternate Designation
—
Equipment Type
Training Turboprop Aircrafts
Manufacturer
Pilatus Aircraft
Date of Introduction
1978
Description
The Pilatus PC-7 Turbo-Trainer is powered by a single Pratt & Whitney Canada PT6A-25A turboprop driving a three-blade propeller. PT6A-25A engine develops a maximum power of 550-shp. Optionally, the PC-7 can be equipped with Martin-Baker ejection seats. The PC-7 was replaced as the production standard by the PC-7 Mk II in 1994.
Air & Air Defense Specifications
Crew
2
Range
1200.0 km
Service Ceiling
10058 m
Wingspan
10.40 m
Overview (Deagel)
Group
Training Turboprop Aircrafts
Status
Active
Origin
Switzerland
Contractor
Pilatus Aircraft
Initial Operational Capability (IOC)
December 1978
First Flight
April 12, 1966
Total Production
?
Specifications (Deagel)
Crew
2
Number of Engines
1
Propeller Blades
3
Area — Wing Area
16.6 square meter
Dimensions — Height
3.2 meter
Dimensions — Length
9.8 meter
Dimensions — Wingspan
10.4 meter
Mass — Empty Weight
1,330 kilogram
Mass — Max Takeoff Weight
1,900 kilogram
Performance — Ceiling
33,000 foot
Performance — Max Range
1,200 kilometer
Performance — Operational Altitude
25,000 foot
Power — Max Power at TakeOff
550 shp
Speed — Climb Rate
2,150 fpm
Speed — Cruise Speed
412 kph
Speed — Economical Speed
317 kph
Gear (Deagel)
Item 1
Turboprop Engines: PT6A-25A (1)
Variants
Variant 1
Pilatus PC-7 Turbo-Trainer
Variant 2
Pilatus PC-7 Mk II
Variant 3
Pilatus PC-7 MKX
Details
Country of Origin
Switzerland
Sources
deagel.com: https://www.deagel.com/x/x/a002043
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
9.8 m
Width
10.4 m
Height
3.2 m
Weight
1900 kg
Operators (17)
France
Iran
Angola
Austria
Bolivia
Botswana
Chad
Chile
Guatemala
Malaysia
Mexico
Myanmar
Netherlands
Suriname
Switzerland
United Arab Emirates
Uruguay
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