Nivation - specialists in Russian aircraft, from purchasing to assembly, to ongoing aircraft maintenance and support. Nivation is a US-based company specializing in sale of new and used Russian aircraft, distribution of spare parts, airplane overhaul and repairs, technical assistance with assembly and dismantle of aircraft, translation of technical documentation, as well as assistance with and consultation on purchasing of aircrafts in Russia and Ukraine. The following models are serviced and supported: L-39, L-29, SU-25, YAK-52, and variety of MIGs.

Parts

Browse parts by Category, or by individual aircraft, below.

Aircraft

	AN-2 Colt	The world's largest single engine biplane, the 1000 hp radial engine and 60 foot wingspan allow short field take offs and landings. The first prototype flew on August 31, 1947, and the aircraft went in production in 1949. Over 5000 were built. The AN-2 Colt can be used in the following versions: cargo, cargo/passenger, agricultural, extinguishing forest fire, ambulance. The crew consists of two pilots and can accomodate eight passengers. The AN-2 is night capable but the cockpit is not adapted for NVG use. The biplane are rectangular-shaped with curved tips, with one high-mounted and one low-mounted (shorter), connected and braced by two struts. A single radial piston engine (some versions are turboprop) is mounted in the nose. The fuselage is Short and thick with solid, blunt nose, a stepped cockpit, and fixed landing gear. The tail fin is tapered with a large, round tip. The flats are low-mounted on the tail fin and rectangular-shaped with curved tips. AN-2 Colt parts for sale
	L-29	The L-29 DELFIN two-seat jet aircraft made by Aero Vodochody was designed by Z. Rublič and K. Tomáš. The first production aircraft was delivered in April 1963. The aircraft, which is intended for both initial and advanced training, has a robust air-frame; it can operate from rough grassy, sandy and muddy fields. It is designed so as to facilitate the pilots´ transfer to combat aircraft. Being of a totally new design, a tandem seating position was chosen with the best wing for subsonic flight, the straight wing. The wing has the ability to carry 150 lts drop tanks. The maximum speed with underwing stores is 0.7 mach and 0.75 without, while G limits being +8 -4 all this in an aircraft weighing just over 3,500 KGs. The mid-wing all-metal aircraft is powered by M-701 jet engine with a radial-flow compressor and a single-stage turbine made by Motorlet with the maximum thrust of 8,72 kN. The fuselage has a single engine with an air intake in each wing root. This is mounted about mid way and towards the rear of the wing. The Motorlet M-701c-500 turbojet rated is at 1,960 lbs. thrust. The M-701 is an early generation jet engine and features a single stage centrifugal compressor driven by a single stage axial flow turbine. 100% RPM is 15,300, this gives a whistling sound a bit like the fouger magister of similar vintage. There are 7 combustion chambers mounted around the engine. The semi-monocoque structure of the air-frame is divided into three compartments which are screwed together. The first compartment is the nose with the aerial, the second is a pressurized cockpit, and the third part of the fuselage contains the engine. The wing is a self-supporting one-sparred all-metal structure. On wingtips are pylons for auxiliary fuel tanks or optional missiles. The aircraft has a retractable three-wheel landing gear. The pupil and the instructor are seated one after the other in synchronised ejection seats. The aircraft was produced in Aero Vodochody and Let Kunovice from 1962 to 1973. Over 3500 were built. Specifications: Max. speed at 5,000m-655 km/h; at sea level-650 km/h; Max. ferry range-1600 km; Service ceiling-11 000 m; Max. climb (full load)-14 m/s; Endurance-2 h; Engine-M-701 Motorlet; Thrust-8,72 kN; Max. takeoff weight-3586 kg; Empty weight-2280 kg; Wingspan (including fuel tanks)-10,29 m; Length-10,81 m; Height-3,13 m; Wing area-19,8 m2. L-29 parts for sale
	L-39C	The L-39 Albatross succeeds the L-29 Maya/Delfin. The L-39 basic and advanced jet trainer first flew on 4 November, 1968. The aircraft is the standard jet trainer for former Warsaw Pact countries. It is designed for initial and advanced training. Several modified and upgraded versions have been developed since 1968, known as L-39C, L-39V, L-39ZA, L-39MS and L-39ZO. From 1971 to 1999 a total of 2921 units of L-39/59 family were delivered. A low-wing aircraft with tandem seating and a classic all-metal airframe, it is equipped with a three-point hydraulically operated retractable landing-gear. Trapezoidal wings have fuel tanks on their tips. The wing has double-slotted flaps with a takeoff deflection of 25° and landing deflection of 44°. The fuselage consists of two construction parts - the forward and the rear one. The rear fuselage and tail are removable. The electronic equipment and oxygen system are located in a dielectric nose cover. In L-39, the canopy of the cockpit is hinged to the right. In newer development types L-59 (originally L-39MS) and L-139 it is hinged hydraulically upwards to the rear. The power plant is an Al-25TL by-pass double-shaft turbojet engine with max. static thrust of 16.87 kN. The engine is started by a Saphire 5 single-shaft gas turbine. The types with maximum takeoff weight of 5,700 kg are equipped with a more powerful DV-2 engine with max. thrust of 21.57 kN. There is a classic mechanical control system with power transmission over levers and pull rods from both pilot posts. The electrical equipment is powered by the main generator (9 kW) from an accumulator enabling autonomous operation. The electrical net includes inverters (115 V and 3x36 V). Radio equipment of the aircraft consists of radio, communication, radionavigation and identification devices. For the training of landing and approach, a RSBN-5S close navigation system and ILS landing system are used. The aircraft is also equipped with the RKL-41 radio compass, RV-5 radio altimeter, MRP-56PS marker and an identification device. Specifications: Max. speed at 11,000 m-850 km/h; at 5,000 m-755 km/h; at sea level-720 km/h; Max. range (w\out auxiliary fuel)-1000 km; Max. range (with auxiliary fuel)-1750 km; Service ceiling-11 500 m; Max. climb (full load)-22 m/s; Flt. endurance (auxiliary fuel)-3 h 50 min; Flt. endurance (w\out auxiliary fuel)-2 h 30 min; Engine-AI-25TL Progress (Ivchenko); Thrust-16,87 kN; Max. takeoff weight-4700 kg; Empty weight-3540 kg; Wingspan (including fuel tanks)-9,46 m; Capacity of auxiliary fuel tanks-2x420 lit.; Length-12,13 m; Height-4,77 m; Wing area-18,8 m2; Max. permitted g- -4/+8g. L-39C parts for sale
	Yak-52	The YAK 52 military trainer designed by the world renowned A.S. Yakovlev Bureau, Moscow from the very successful aircraft series that preceded the YAK 52. The aircraft provides excellent handling from basic training through to advanced aerobatic training with G Limits of +7 -5g with 2 crew. The M14P engine of 360 HP is the world's most reliable radial engine. As standard equipment instrumentation includes 3 gyro's per panel with the instructor's position providing simulated instrumentation failure to the front cockpit for trainee purposes. The aircraft can be operated from unimproved grass surfaces or hard runways. The services (retractable undercarriage, flaps, engine starting and brakes) are provided by pneumatic pressure, for reliability and light weight. Specifications: Maneuvering speed-360 km/h or 194 Kts: Gear extension speed-200 km/h or 108 Kts; Flap extension speed-170 km/h or 91 Kts; Stall speed-105 km/h or 60 Kts; Length-7.745 m; Wing span-9.300 m; Height-2.700 m; Propeller diameter-2.400 m; Wing area-15.00 m2; Tail plane area-1.325 m2; Fuel capacity- standard 120 Lts; Long range tanks-280 Lts; Fuel grade, min. 91 octane; Range-510 km; Long range tanks-about 6 hours or 1190 KM; Oil capacity-16 Lts; Oil grade Mineral or detergent-100 or 120; Engine-M14P, 360 HP or M14PF, 400HP 9 cylinder radial driving either 2 or 3 blade constant speed propellers; Speeds Economic (60%) 200kph/ 108 Kts; Cruise-(70%) 230kph/ 128 Kts; Max. continuous-(82%) 270kph/ 147 Kts. Yak-52 parts for sale