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C-101 Aviojet Jet Trainer and Ground Attack Aircraft

Overall length

12.50m (41ft)

Wing span

10.60m (34ft 9in)


4.25m (13ft 11in)

Wheel track

3.18m (10ft 5in)

Wing area

20m² (215ft²)

Wing thickness


Normal fuel capacity

1,300kg (2,865lb)

Total internal fuel capacity

1,820kg (4,015lb)

Equipped empty weight

2,855kg (7,650lb)

Typical training weight (50 % normal fuel)

4,350kg (9,590lb)

Maximum take-off weight

6,300kg (13,589lb)

Load factors

+7.5g to -3.9g

Turbofan engine

Garrett TFE-731-5

Thrust ISA, sea level

2,132kg (4,700lb)

Specific fuel consumption

0.48lb/hr x lb

Take-off distance


Landing distance


Stall speed with flaps down

85 knots

Maximum level speed

450 knots

Maximum sustained load factor


Maximum rate of climb


Time to 25,000ft

6 min 30 sec

Service ceiling


Training mission time on internal fuel

2 hr 15 min

Range on internal fuel


Endurance on internal fuel

7 hr

Maximum dive speed

0.8 Mach

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