Hobby Master Archive

True 1/72 scale.

Professionally painted.

Great attention to detail.

All markings are Tampoed (pad applied).

Option to display the model on a stand that is provided.

Model can be shown with the landing gear in the down or up positions.

Canopy can be displayed open or closed.

Pilot figure included.

Extremely heavy metal with a minimum of plastic.

Highly collectable.

Hobby Master 1/72 Air Power Series HA6005 Su-27SK Flanker B TS-2702, 11th Squadron, Indonesian Air Force, 2003

The Su-27S (NATO reporting name - Flanker) is a single-seat highly- maneuverable fighter aircraft built by Sukhoi Design Bureau as the Soviet response to the U.S. F-14 and F-15 and entered service in 1985. The primary role of the Su-27 was to provide defense against American bombers, USN ships and provide Soviet bomber escorts. There have been many improvements over the years resulting in numerous variants of the Su-27. The export variant, the Su-27SK was sold to China and eventually developed into the license-built Shenyang J-11.

The Indonesian Air Force (Tentara Nasional Indonesia Angkatan Udara - TNI-AU) purchased several Su-27 family aircraft from Russia, Su-27SK, Su-27SKM, Su-30Mk and Su-30MK2. Between 2003 and 2013 sixteen Flankers were received by Skadron Udara11 (11 Squadron) at the Iswahyudi AB. Of the sixteen aircraft two were Su-27SKs with serials TS-2701 with code 01 and TS-02 with code 02. The Su-27SKs were modified from dedicated air-superiority fighters to multi-role fighter and attack aircraft. Part of the payment for these aircraft was completed using Indonesian palm oil.

Aircraft Type Su-27S Manufacturer Sukhoi OKB Role Multi-role Air Superiority Fighter Crew 1 Dimensions Maximum Length 21.935 m (71.96 ft) Wingspan 14.7 m (48.2 ft) Height 5.932 m (19.45 ft)

Weights Empty 16,300 kg (35,935 lbs) Normal Takeoff 23,000 kg (50,706 lbs) Maximum Takeoff 28,000 kg (61,730 lbs)

Performance Engines 2 X Saturn/Lyul’ka AL-31F afterburning turbofans Dry Thrust Per Engine 75.22 kN (16,910 lbf) Afterburner Thrust Per Engine 122.6 kN (27,560 lbf) Fuel Capacity 11,975 l (3,163 U.S. Gallons) Maximum Speed @ Altitude 2,500 km/h (1,553.43 mph) Maximum Speed @ Sea Level 1,400 km/h (870 mph) Maximum Mach 2.35 Service Ceiling 18,500 m (60,696 ft) Range @ High Altitude 3,900 km (2,423 miles) Range @ Sea Level 1,400 km (870 miles) Maximum G-Load .9 Takeoff Run 650 m (2,132 ft)

Armament Gun 1 X 30 mm GSh-301 Cannon with 149 Rounds Hardpoints 8 X External Plus 2 X Wingtip Rails Missiles Air-To-Air R-60/AA-8 Aphid, R-27/AA-10 Alamo,R-73/AA-11 Archer, R-33/AA-9 Amos Air-To-Ground NONE Bombs Dumb, Cluster Pods Rocket and ECM