“This is a Yak 52W that is a beautiful aircraft with awesome performance. It has a 90 hour since new.



Item specifics Condition: Seller Notes:
Used
“This is a Yak 52W that is a beautiful aircraft with awesome performance. It has a 90 hour since new engine along with the MTV 3 bladed prop. Very well equipped with lots of extras you don't see on most aircraft like this. Check out the specs and pics below. The owner is motivated as it was a trade in on a newer G-35 Bonanza.”
Model Year: 1999 Make: Yakovlev
1999 YAK52W N52XS This 1999 model year 52W is a 2 seat tandem aircraft with fully inverted flight and aerobatic capabilities to +7g-5g’s with two pilots and full main tanks of fuel. Registration in the USA is required to be the “Experimental.” Both cockpits are equipped with gyro instruments, artificial horizon, and magnetic compass. All primary controls are fully duplicated. This is an easy airplane to fly aerobatics, instruments (IMC) cross-country. This is probably the most well equipped YAK 52 in the World! No expense was spared to make it comfortable for long distance flying in both VFR and IFR flying conditions. It has received excellent maintenance.The YAK 52 is a primary military trainer designed by the world renowned A.S. Yakovlev Bureau, Moscow and has proven to be a very successful aircraft series that preceded the YAK 52W. The aircraft is produced under license from Aerostar SA. Bacau, Romania. Over 1700 have been produced to date starting with YAK-52 first flight in 1974 with production starting in 1975. The Russians made no announcement about its existence until 1978. At the peak of production 150 aircraft were manufactured per year. The aircraft provides excellent handling from basic training through to advanced aerobatic training with G Limits of +7 -5g with 2 crew. VERY responsive and really fun to fly!The M14P engine f 360 HP is the world’s most reliable 9-cylinder radial engine and is produced by Aerostar at Bacau. A new engine was recently installed. Less than 90 hours since NEW! The aircraft can be operated from hard runways or unimproved grass surfaces The rugged undercarriage is strong and reliable This aircraft has been hangered since new. It only sits outside at airshows! The operation of several systems including retractable undercarriage, flaps, engine starting are provided by pneumatic pressure, for reliability and light weight. The hand brake for the differential braking with air activation has been eliminated on this aircraft. Cleveland brakes are installed. A/C electrical services are standard, 24V. Maintenance is easy and can be performed in the “field.” The YAK 52 offers performance and ease of operation, second-to-none. SPECIFICATIONS PRODUCT NAME YAK-52W (Western Version of Yak-52) DEVELOPMENT BASIS The SPECIFICATIONS for the 52W were finalized following a marketing study, as well as the specific requirements incorporating the recommendations of George Coy from Gesoco in the USA (802) 868-5633 or here DESTINATION AND FIELD OF APPLICATION The YAK-52W aircraft is designed for civil aviation use and in the standard design is intended for the following missions: Advanced Flight Instruction Pleasure flying Aerobatic training and competition “YAK-ING OFF” AIRCRAFT CHARACTERISTICS AND PERFORMANCES The characteristics and performance of the YAK-52W aircraft are similar to YAK 52 aircraft. However, several modifications and improvements have been incorporated into the design. Dimensions : Wing surface: 161 sq. ft Wingspan: 30 ft. 6 in. Length: 25 3 in. ft. Height: 8 ft. 2 in. Wheel Track: 8 ft. 7 in. Weight Weight, empty-equipped: 2293 lb. Max. Take off weight: With fuel 31 gal. 2899 lb With fuel 72 gal. (Integral auxiliary wing tanks) 3,120 lb Note: aerobatic maneuvers prohibited with fuel in auxiliary tanks PERFORMANCES AND SPEEDS Never exceed 243 Kts Stall speed: 56 Knots per book less w/V.G.’s Climb rate: 1,200 ft/min. Max. Ceiling: 13,000 ft Take off distance: With 31 gal fuel: 660 ft. With 74 gal fuel: 990 ft. Landing distance: 855 ft. Max. G-limit +7g to -5g Max. Flight range: With 31 fuel 270 Nm. With 74 fuel: 540 Nm. Economy (60%) 108 Kts Cruise (70%) 128 Kts Gear Extension 108 Kts Flaps 91 kts Stall 60 Kts Approach 87 Kts Maneuvering 194 Kts Note: The above data and performance specifications are based on standard atmospheric conditions. The aircraft design includes the ability to take off and land on grass fields. The aircraft design allows take off and landing with cross wind component of 11 Knots. The aircraft is equipped with a 360 Hp. M14-P piston engine and a MTV-9 three-blade constant speed propeller. Oil Type used is Phillips 25W60 radial engine oil THIS YAK 52W is a real Performer!!!! Current Times as of March 11,2019 Tach: 1007.6 AFTT: 1318.7 Engine: 90.2 SNEW Prop: 79.9 SPOH Condition Inspection due: May 1, 2019 The following modifications included in the YAK 52W make Experimental YAK 52XS…EXTRA SWEET! THE FUSELAGE The aircraft is fitted with an externally accessible baggage compartment and battery compartment located on the left side behind the rear cockpit. The aircraft is fitted with a permanent mounted step on the left side of the fuselage for the pilots and passenger convenience to enter the cockpit. THE WING In order to increase the fuel capacity, the wing has been fitted with an additional integral fuel tank between ribs no 5-9 on both left and right wings. In the right and left leading edge, between ribs 6-7, the wing has been fitted with recessed landing and taxi lights for night operations. The wing was strengthened in the tip area, for optional wing-tip tanks. Tip Rib no. 15 has been fitted with strobe and navigational lights for night operations. Tubing was added for fuel supply system and for the electric fuel pressure pup installation. The fuel filler caps for the aux fuel system were modified to a less prone to leak style. CONTROL SERVICES The fabric skins of aileron, elevator and rudder have been improved and fitted with aluminum skins and the attach brackets and balance weights were modified for the different skins. THE LANDING GEAR The Russian style wheels of the main landing gear, which were with pneumatic drum brakes, were replaced with Cleveland wheels using hydraulic disk brakes and standard western tires. The nose wheel assembly was replaced with a Cleveland wheel with standard Western tires. This above improvements required the modification of the wheel axles and brake system. CONTROLS The aircraft has been fitted with rudder steering bars that allow a wider adjustment range for pilot comfort. The aileron and elevator centering springs were eliminated. THE PNEUMATIC SYSTEM - The air charged starting system of the engine remained as currently on the standard Yak-52. - The landing gear retract and flap-operating system was retained and is operable from both cockpits. - The pneumatic system water drain is operable from the cockpit. THE HYDRAULIC SYSTEM - A hydraulic brake system was added, and includes toe brakes for both cockpits. THE SMOKE SYSTEM - A 3 gallon tank sits in the rear cockpit. Right Hand side fuselage filler tube. THE PVD SYSTEM (Fault simulation system) - The system for instructors simulation of failures in the front cockpit was eliminated. THE POWER UNIT As part of the aircraft being fitted with additional tanks, the fuel system has been supplemented with the required lines; valves and the fuel pump to transfer fuel from the auxiliary tanks into the main tanks. The engine has been modified with a train system to avoid the hydraulic lock. (Clean Kit) The system includes a scavenge ump and drain valve shut off which also safety for starting system disengaged. The oil dilution system was eliminated. The aircraft is fitted with a three-blade “Climb” propeller and the governor has been modified to allow the higher pressures required. The cowl flaps and the oil cooler door can be controlled from both cockpits. Oil cooler restriction plate included. The fuel lines in the engine compartment have fire sleeves. The start switch is located in the front cockpit only. Solo from the front cockpit only. Both cockpits are equipped with magnet switches. It has impulse coupling mags and the shower of sparks has been eliminated. The failure prone UMA engine tach was replaced with digital tach. ELECTRICAL SYSTEM The basic electric source is a 35 amp B&C Systems 28 volt engine driven alternator. The battery system includes sealed lead acid batteries of sufficient capacity to allow 25 minute of flight with an inoperable alternator. The electric installation is protected against over voltage variations and short-circuit conditions. The electric installation is configured to ensure power, control and protection for the following: 1. Landing and Taxi lights are located in the leading edge of both wings and are wired to have a “flash” circuit for enhanced visibility. 2. Night Navigation and anti-collision strobe lights at the wing tips 3. Cockpit lighting for instructions and radios. INSTRUMENTATION, COM AND NAV EQUIP. Both cockpits are equipped as follows: 1. Engine instruments 2. Light signal warnings for flaps and gear 3. Basic flight instruments 45. All markings and tags are in English 5. Ultra violet resistant canopies were installed recently (Grayish Tint) The minimum equipment for flight and navigation instruments that are in compliance with the requirements of FAR 23.1303: 1. Speed indicator 2. Altimeter 3. Magnetic compass 4. G-factor indicator 5. Accelerometer 6. Gyro-horizon 7. Gyro-compass or compass system These instruments are present in both cockpits. The front cockpit shall also have the following flight and navigation instruments: 1. Turn and slide indicator This YAK-52W has the following Avionics equipment 1. Dynon EFIS-D10A w/Outside Air – D.G. – Rate of Climb – Altitude – Airspeed 2. Apollo SL30 Nav and Com #1 coupled to OBS w/Glideslope 3. Garmin 340 Audio Panel Garmin 4. Garmin GTX 327 Transponder with AmeriKing Altitude Encoder 5. ICOM IC-A200 Com #2 Radio 6. JPI 9 cyl. Engine analysis w/fuel flow 7. Tru Trac Auto pilot. The device is wired to take GPS Nav input 8. Horizon 1000 Digital Tachometer. (programmed to rpm operating limits) 9. Helmet power supply 10. Clock 11. Audio input from iPod device/phone THE SEATS Both cockpits are equipped with Hooker Harnesses.
CONTACT CJ AVIATION SERVICES flycjprice@earthlink.net 336-253-8209 Current date: 2019-03-11