C-101 Aviojet
Initial Operational Capability (IOC) : 1977
Total Production : 149
Model | Status | Year | Produced |
---|---|---|---|
C-101 Aviojet | Active | 1977 | 149 |
C-101 Aviojet
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
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.
Operators
Specifications
Notes | ||
---|---|---|
Crew | 2 | |
Number of Engines | 1 | |
Dimensions | ||
Height | 4.3 meter | |
Length | 12.5 meter | |
Main Gun Caliber | 30 millimeter | |
Wingspan | 10.6 meter | |
Mass | ||
Empty Weight | 3,470 kilogram | |
Max Takeoff Thrust | 4,700 pound | |
Max Takeoff Weight | 6,300 kilogram | |
Performance | ||
Ceiling | 13,411 meter | |
Max Range | 3,700 kilometer | |
Speed | ||
Cruise Speed | 170 mps | |
Top Speed at High Altitude | 232 mps | |
Time | ||
Flight Endurance | 7 hour |
Gear
Turbofan Engines | ||
---|---|---|
TFE731 | 1 |
News

The Spanish Air Force, Ejército del Aire, is the third European air force to opt for the Swiss-produced PC-21, the Next Generation Trainer.
Photo Gallery
November 2006

C-101 Aviojet
Notes
State Latest Known holdings/Original Procurement
Com - Date of Commissioning
Decom - Date of Decommissioning
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