| Role | Six seat utility light aircraft |
| Country of Origin | United States |
| Manufacturer | Cessna |
| First Flight | 1962 |
| Total Production | 577 |
| Primary users | United States Air Force |
| Status | Remodelled |
| Variants | P-206, 207A, |
| Length | 8.62 m |
| Height | 2.92 m |
| Wingspan | 10.92 m |
| Role | Large cargo transport aircraft |
| Country of Origin | Russia |
| Manufacturer | Aviant State Aviation Plant |
| Total Production (units) | 60 |
| Primary users | Russian Air Force
United Kingdom Russian State Transport Company |
| Status | Out of operation |
| Cruising speed | 800 Km/hr |
| Length | 69.10 meter |
| Height | 21.80 meter |
| First Flight | December 1982 |
| Role | Cargo airlifter |
| National origin | Soviet Union-Ukraine |
| Manufacturer | Antonov |
| Introduced | 1988 |
| First Flight | 21 December 1988 |
| Primary User | Antonov |
| Status | In service |
| Primary User | Antonov Airlines |
| Designed | 1980 (Antonov Design Bureau) |
| Wingspan | 88m |
| Length | 84m |
| Crew | 4 (2 pilots, 1 navigator, 1 flight engineer) |
| Capacity | 300 troops/206 stretcher cases |
| Weight | 66.23 tonnes (empty)/145 tonnes (maximum at takeoff) |
| Payload | 47 tonnes (cargo) |
| Length | 40.7 metres |
| Height | 16.38 metres |
| Wingspan | 44.6 metres |
| Engine | 4 Progress D-27 with SV-27 counter-rotating turboprop fans |
| Power | 13,880 hp/10,350 kW per unit |
| Rate of Climb | 24.9 m/s |
| Service Ceiling | 12,000 metres |
| Speed | 780 km/h (maximum), 750 km/h (cruise), 113 km/h (stall) |
| Range | 6,600 km (20 tonnes: minimum cargo) |
| Origin | Ukraine |
| Developer | Antonov Design Bureau |
| Crew | 6 |
| Passengers | 130 |
| Weight | 30.5 tonnes (empty), 61 tonnes (maximum at take-off) |
| Load | 18 tonnes (maximum) |
| Length | 37 m |
| Height | 10.5 m |
| Usable Volume | 90 m³ |
| Cargo Volume | 13.5 x 2.95 x 2.47 m³ |
| Wingspan | 38 m |
| Wing-area | 121.7 m² |
| Fuel Capacity | 22,066 kl |
| Engine | 4 x ZMKB/Ivchenko/Iwtschenko Progress AI-20M Turboprop |
| Power | 3,125 kW |
| Fuel Economy | 2.3 tonnes/h |
| Speed | 600/h (cruise), 640 km/h (maximum) |
| Range | 5,700 km (ferry), 2,100 km (loaded) |
| Service Ceiling | 10 km |
| Runway | 1,230 m (take-off), 1,125 m (landing) |
| Armament | 2 x 23 mm NR-23 machine-guns |
| Purpose | Tactical airlift |
| NATO Code | Cub |
| IATA Code | ANF |
| ICAO Code | AN12 |
| Production-Phase | 1958 – 73 |
| Deployment | 1959 |
| Total Production | 1248 |
| Designer | Oleg Antonov |
| Manufacturer | Antonov Hongdu Aviation Industry Group |
| First Flight | 31 August 1947 |
| Produced | 1947-2002 |
| Fleet | 18000 and up |
| Primary Users | Soviet Union, China, North Korea |
| Role | Agriculture and utility biplane |
| Variants | Antonov An-3 |
| Length | 2m |
| Wingspan | 18.2 m(upper), 14.2m (lower) |
| Top Speed | 258 km/h |
| Developer | Lockheed Martin |
| Founded | 1947 |
| Variants | C-5A, C-5B, C-5C, C-5M Super Galaxy, C-5 RERP, |
| Number Produced | 131 |
| Status | Operational; production discontinued |
| Engine | 4 GE CF-80C2 turbofans |
| Fuel-Capacity | 150,819 kl |
| Length | 75.53 m |
| Height | 19.84 m |
| Speed (normal) | 817 km/hr |
| Wingspan | 67.91 m |
| Stabiliser Span | 20.95 m |
| Operating Weight | 181,437 kg |
| Maximum Payload | 129,274 kg |
| Maximum Take-off Weight | 381,018 kg |
| Crew/Passenger | 6/70 |
| Takeoff Distance/Landing Distance | 3,697 m/1485 m |
| Primary Function | Strategic airlift, military equipment transport |
| Role | Military freighter, gunship, air dropper |
| Country of Origin | USA |
| Manufacturer | Fairchild Corporation |
| First Flight | November 1947 |
| Introduction | 1949 |
| Status | Retired from use in 1974 |
| Primary users | United States Air Force
Royal Canadian Air Force United States Navy |
| Total number built | 1112 |
| Length | 86.48ft |
| Variants | XC-82, C-82A, |
| Topmost speed | 292 miles per hour |
| Role | Bomber warplane |
| Manufacturer | North American Aviation |
| First Flight | 19th August, 1940 |
| Country of Origin | United States |
| Total production (units) | 9816 |
| Primary users | RAF Desert Air Force
United States Military Royal Australian Air Force Royal Canadian Air Force |
| Length | 53 feet |
| Unit cost | $ 109,670 in 1943 |
| Variants | B-25J , B-25C, B-25D |
| Topmost speed | 272 miles per hour |
| Role | Light aerial offensive, private, peasantry |
| National Origin | China |
| Manufacturer | Hongdu Aviation Industry Group |
| Inauguration | 1958 |
| Introduction | 1957 |
| Numbers Produced | 10,000 (all variants) |
| Variants | CJ-6A, CJ-6B, BT-6, PT-6A, Haiyan A, Haiyan B, Haiyan C |
| Engine | 285-hp Quzhou Huosai-6A HS6A |
| Weight | 997.90 kg (empty) |
| Wing Span | 10.18 m |
| Length | 8.45 m |
| Height | 3.26 m |
| Top Speed | 514 km/hr |
| Range | 724.20 km |