C-101 Aviojet
C-101 Aviojet
Training Jets
Operational Photo
Basic Information
Name
C-101 Aviojet
Designation
C-101 Aviojet
Alternate Designation
A-36 Halcon, C-101BB, C-101CC, C-101DD, C-101EB, T-36
Equipment Type
Training Jets
Manufacturer
Airbus Group
Date of Introduction
1977
Description
C-101 is a subsonic, single-engine, tandem two-seat, training/light attack aircraft developed by CASA to meet the requirements of the Spanish Air Force. It is powered by a fuel-efficient TFE731 turbofan engine rated at 4,700 pounds of thrust. C-101 was developed as a replacement for Saeta trainer/jet aircraft. In addition to training, C-101 provides limited ground attack capability. T-36 and A-36 designations refer to C-101s employed by the Chilean Air Force for training and attack roles respectively.
Air & Air Defense Specifications
Crew
2
Max Speed
835.2 km/h
Range
3700.0 km
Service Ceiling
13411 m
Wingspan
10.60 m
Overview (Deagel)
Group
Training Jets
Status
Active
Also Known As
A-36 Halcon, C-101BB, C-101CC, C-101DD, C-101EB, T-36
Origin
Spain
Contractor
Airbus Group
Initial Operational Capability (IOC)
1977
Total Production
149
Specifications (Deagel)
Crew
2
Number of Engines
1
Dimensions — Height
4.3 meter
Dimensions — Length
12.5 meter
Dimensions — Main Gun Caliber
30 millimeter
Dimensions — Wingspan
10.6 meter
Mass — Empty Weight
3,470 kilogram
Mass — Max Takeoff Thrust
4,700 pound
Mass — Max Takeoff Weight
6,300 kilogram
Performance — Ceiling
13,411 meter
Performance — Max Range
3,700 kilometer
Speed — Cruise Speed
170 mps
Speed — Top Speed at High Altitude
232 mps
Time — Flight Endurance
7 hour
Gear (Deagel)
Item 1
Turbofan Engines: TFE731 (1)
Details
Country of Origin
Spain
Sources
deagel.com: https://www.deagel.com/x/x/a000714
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
12.5 m
Width
10.6 m
Height
4.3 m
Weight
6300 kg
Operators (4)
Spain
Chile
Honduras
Jordan
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