Aero Ae-45Role Utility aircraft

Manufacturer Aero Vodochody, Let

First flight 21 July 1947

Primary users Czechoslovakia

ChinaHungarySoviet Union

Produced 1951-1963

Number built 590

Specifications (Aero 145)General characteristics•Crew: one, pilot•Capacity: 3-4 passengers•Length: 7.77 m (25 ft 6 in)•Wingspan: 12.25 m (46 ft 21⁄2 in)•Height: 2.30 m (7 ft 6 in)•Wing area: 17.1 m² (184 ft²)•Airfoil: Aero No. 58-64•Empty weight: 960 kg (2,116 lb)•Loaded weight: 1,500 kg (3,306 lb)•Max. takeoff weight: 1,600 kg (3,527 lb)•Powerplant: 2 × Walter M 332-III air-cooled 4-cylinder inline engine, 104 kW (140 hp) each

Performance•Maximum speed: 282 km/h (152 knots, 175 mph)•Cruise speed: 250 km/h (135 knots, 155 mph)•Range: 1,700 km (918 nm, 1,055 miles)•Service ceiling: 5,900 m (19,360 ft)•Rate of climb: 5.0 m/s (985 ft/min)•Wing loading: 88 kg/m² (18 lb/ft²)•Power/mass: 0.08 kW/kg (0.05 hp/lb)

AS.10 Oxford

Role Training aircraft

Manufacturer

Airspeed Ltd

First flight 19 June 1937

Primary user

Royal Air Force

Number built

8,586

Developed from

Airspeed Envoy

Variants Airspeed Consul

Antonov An-12Role Civil and

Military transport aircraft

Manufacturer Antonov

First flight 16 December[1]

 1957Introduction 1959Status Active service

with various airlines (especially cargo) and Air Forces

Primary users Belarus Air Force

AeroflotPLA Air ForceProduced 1957–1973

Number built 1,248

Developed from Antonov An-10

Variants Shaanxi Y-8

SpecificationsGeneral characteristics•Crew: 5: 2 pilots, flight engineer, navigator, radio operator

•Payload: 20,000 kg (44,000 lb)

•Length: 33.10 m (108 ft 7 in)

•Wingspan: 38.00 m (124 ft 8 in)

•Height: 10.53 m (34 ft 7 in)

•Wing area: 121.7 m² (1,310 ft²)

•Empty weight: 28,000 kg (62,000 lb)•Useful load: 60 paratroopers (two BMD-1 armoured vehicles)

•Max. takeoff weight: 61,000 kg (130,000 lb)

Performance•Maximum speed: 777 km/h (419 knots, 482 mph)

•Cruise speed: 670 km/h (361 knots, 415 mph)

•Range:

• With maximum fuel: 5,700 km (3,075 nm, 3,540 mi)

• With maximum load: 3,600 km (1,945 nm, 2,235 mi))

•Service ceiling: 10,200 m (33,500 ft)

•Rate of climb: 10m/s (1960ft/min)

Avro AnsonRole Multirole

aircraft, primarily a trainer

Manufacturer

Avro

First flight 24 March 1935

Introduction 1936Retired 28 June

1968 (RAF)Primary users

Royal Air Force

Fleet Air ArmProduced 1930s–1952

Number built

11,020

SpecificationsGeneral characteristics•Crew: Three-four

•Length: 42 ft 3 in (12.88 m)

•Wingspan: 56 ft 6 in (17.22 m)

•Height: 13 ft 1 in (3.99 m)

•Wing area: 463 ft² (43.01 m²)

•Empty weight: 5,512 lb (2,500 kg)

•Loaded weight: 7,955 lb (3,608 kg)

•Max. takeoff weight: 8,500 lb (3,900 kg)

Performance•Maximum speed: 188 mph (163 kn, 302 km/h) at 7,000 ft (2,100 m)

•Range: 790 mi (690 nmi, 1,271 km)

•Service ceiling: 19,000 ft (5,791 m)

•Rate of climb: 750 ft/min (3.8 m/s)

•Wing loading: 17.2 lb/ft² (83.9 kg/m²)

•Power/mass: 0.088 hp/lb (140 W/kg)

Dassault OuraganRole Fighter-bomb

erManufacturer Dassault Avia

tionDesigner Marcel Dassa

ultFirst flight 28 February

1949Introduction 1952Retired 1980sPrimary users

French Air Force

Indian Air Force

Israeli Air Force

El Salvador Air Force

Specifications 

General characteristics•Crew: One•Length: 10.73 m (35 ft 2 in)•Wingspan: 13.16 m (43 ft 2 in)•Height: 4.14 m (13 ft 7 in)•Wing area: 23.8 m² (256.2 ft²)•Aspect ratio: 7.3:1•Empty weight: 4,142 kg (9,132 lb)•Loaded weight: 7,404 kg (16,323 lb)•Max. takeoff weight: 7,900 kg (17,416 lb)•Powerplant: 1 × Rolls-Royce Nene 104B turbojet, 22.2 kN (4,990 lbf)

Performance•Never exceed speed: Mach 0.83•Maximum speed: 940 km/h (508 knots, 584 mph) (Mach 0.76) at sea level•Cruise speed: 750 km/h (405 knots, 465 mph)•Combat radius: 450 km (245 nm, 280 mi)•Ferry range: 920 km (500 nm, 570 mi)•Service ceiling: 13 000 m (42,650 ft)•Rate of climb: 38 m/s (7,480 ft/min)

•Takeoff distance: 783 m (2,570 ft)•Landing distance: 910 m (2,985 ft)

HAL AjeetRole FighterManufacturer

Hindustan Aeronautics Limited

First flight 1976Introduction 1977Retired 1991Primary user

Indian Air Force

Number built

89 (including 10 upgraded Gnats)

Developed from

Folland Gnat

SpecificationsGeneral characteristics•Crew: 1•Length: 9.04 m (29 ft 8 in)•Wingspan: 6.73 m (22 ft 1 in)•Height: 2.46 m (8 ft 1 in)•Wing area: 12.69 m² (136.6 ft²)•Aspect ratio: 3.56•Empty weight: 2,307 kg (5,086 lb)•Loaded weight: 3,539 kg (7,803 lb) clean take-off weight•Max. takeoff weight: 4,173 kg (9,200 lb)•Powerplant: 1 × TJE HAL/Bristol Siddeley Orpheus 701-01 turbojet, 20.0 kN (4,500 lbf)

Performance•Maximum speed: 1,152 km/h (622 knots, 716 mph) at sea level

•Combat radius: 172 km (93 nmi, 107 mi) low level, with two 250 kg bombs

•Service ceiling: 45,000 ft (13,720 m)

•Wing loading: lb/ft² (kg/m²)

•Climb to 12,000 m (39,375 ft): 6 min 2 s

Specifications (HAL Ajeet)General characteristics•Crew: 1

•Length: 9.04 m (29 ft 8 in)

•Wingspan: 6.73 m (22 ft 1 in)

•Height: 2.46 m (8 ft 1 in)

•Wing area: 12.69 m² (136.6 ft²)

•Aspect ratio: 3.56

•Empty weight: 2,307 kg (5,086 lb)

•Loaded weight: 3,539 kg (7,803 lb) clean take-off weight

•Max. takeoff weight: 4,173 kg (9,200 lb)

Performance•Maximum speed: 1,152 km/h (622 knots, 716 mph) at sea level

•Combat radius: 172 km (93 nmi, 107 mi) low level, with two 250 kg bombs

•Service ceiling: 45,000 ft (13,720 m)

•Wing loading: lb/ft² (kg/m²)

•Climb to 12,000 m (39,375 ft): 6 min 2 s