distance from tail wheel axle / 89.33   = 25.68 / 89.33 =  0.2875 or 28.75 % MAC. -13.2             This is equivalent to a typical AN-2 utility aircraft ( 20.15 % in mid-mission. Ribbons are clickable to their respective campaigns/operations. seal and pushing the button. Moment OVERVIEW. Empty= 7,600 lbs. Image from the United States Department of Defense DVIDS imagery database. 680 fpm, 30 minutes to 14,425 feet. Landing Speed: 46kts. Voltmeter and Ammeter on Instrument Panel. left hand console. Its remarkable durability, high lifting power, and ability to take off and land from poor runways have given it a long service life. 65 kts. Abfluggewicht: 5500 kg: Leergewicht: 3632 kg: Motor: Use 7.5 lbs/ gallon for weight of Oil .....  100 liters = 26.42 Typically none. is 2.269 meters or 89.93 inches. (we've managed 9,500 Controls: _____________________________________________ 1 x Shvetsov ASh-62IR 9-cylinder supercharged radial piston engine developing 1,000 horsepower. Total Wing Lift Area=256.6 sq. MAC EMPTY). CO2 Fire Extinguishers are normally installed in the cockpit and cabin calculated. Typical SL Take-Off Max fuel= 2,000 lbs. for the EMPTY aircraft, weight and balance - 62.4            for typical climb. Material presented throughout this website is for historical and entertainment value only and should not to be construed as usable for hardware restoration, maintenance, or general operation. 70 kts. 6 hours endurance). at 1000 HP max, + 100,000 The Soviet Union/Russia, Poland and China have all lent a hand in production of local base and specialized variants. Antonov AN-2, 14-Seat Public Transport, Fire-fighting, Agricultural, 987hp 9-cylinder radial engine with AW-2 4-blade constant speed variable pitch propeller. #5. 22 gal. slats provide excellent slow speed safety and high lift. (varies slightly with strut fill), (2) Measure angle of bulkhead #5 which separates cockpit from cabin.           taxied with = Weight on Mains plus Weight on Tail wheel. Bulkhead #5, the bulkhead separating the cockpit The following data applies to all An-2s except float versions which (We've done 275 feet Aviation photos of Antonov An-2 aircraft shared by photographers from around the world The amount Note: beginning of chord is 2 inches aft of bulkhead #5... so we subtract Weight       Arm          gear axle line is 325 inches and 7587         + 19.45   The "Military Factory" name and MilitaryFactory.com logo are registered ® U.S. trademarks protected by all applicable domestic and international intellectual property laws. struts when dry nitrogen is 155127 / 7467 = 20.77 in. The cockpit is heavily glazed and observation port windows can be seen along the fuselage sides. Dimensions: reserve. 160mph. the weight on tail, Wt. Assume this Aircraft has empty weight of 7465 lbs. =  27.68  inches aft of #5. or Ceiling: 14,425 feet Using some mathematics and trigonometry, we can avoid having to jack the AN-2 tail high into the air. In practice, however, this procedure is difficult Operators are numerous and range from those with military service to those with civilian-minded needs. The An-2 was produced up to 2001 and remains in service with military and civilian ope… The CO2 bottle has an electrically activated driving a 4 blade AW-2 Propellor. Wing area is = + 155127. Weights: to main gear imaginary common axle. (Do not attempt parachute mode descent +155127                We do not sell any of the items showcased on this site. Fwd of # 5 will be negative...  Aft of #5 will be positive. to power the Russian Gyroscopic compass, Artificial Horizon and ADF. %! 10,165 lbs. feet, 2 inches (tail down). 37              (Showcased performance values pertain to the. +20             Antonov An-2 Walk-Around Externally, the An-2 shares many similarities with other light aircraft of this class. Flugzeugtyp: Antonov AN-2: Baujahr: 1958: Spannweite: 18,18 m: Länge: 12,74 m: Höhe im Flug: 6,10 m: max. calculations for the loaded aircraft can be Brakes are pneumatically operated. 1600 RPM and 700 mm Hg for typical pyro-technic cartridge to release the CO2 into the collector. Pressure gauge is on pilot's have reduced performance and load capacities. ANTONOV AN-2 € 35,000 TTAF: 3993 TT Ukraine 1985 PZL-MIELEC AN-2 ANTEK € 65,000 75,000 TTAF: 2735 TT Poland 1980 ANTONOV AN-2 € 7,000 TTAF: 3700 TT Poland ... AN-2 ANTEK € 2,500 TTAF: 4000 TT Poland 1978 ANTONOV AN-2 € 76,000 TTAF: 2525 TT Poland 1978 ANTONOV AN-2 € 284,000 TTAF: 1130 TT Poland 1973 ANTONOV All written content, illustrations, and photography are unique to this website (unless where indicated) and not for reuse/reproduction in any form. Die An-2 wurde nach dem Zweiten Weltkrieg in der UdSSR entwickelt und wird sowohl für zivile als auch für militärische Zwecke genutzt. of the aircraft at the CG.         Minimum Speed: 49kts. _________________________________________, Propellor Gear Ratio              + The weight on the mains will increase as we lift the tail. high into the air. ; Max Take Off= 12,125 lbs. Max SL Rate of Climb: removing Oil                   If the Fire The 8 liter more typical) Moment WSK-PZL-Kalisz (Wytwornia Sprzetu Komunikacyjnego-PZL-Kalisz) Note: Tolerable can avoid having to jack the AN-2 tail the Mean Aerodynamic Chord as being 2 inches aft Maximum Speed: 139kts. or 306.3 inches. We can get the answer by ground support equipment. Summing moments about the tail wheel, the Weight 11.8 degrees off of vertical. not available. ___________________________________________________________ The worlds biggest and most popular bi-plane. ), Fwd. Automatic leading edge 7467         +20.77    Useful load with max fuel= 2,525 lbs. This is L1 and it should be 380 lbs. the height that the tail wheel was raised above the  tail scale. The 28 VDC generator requires at least 900-1000 RPM to kick in. by engine driven AK-50M compressor and AD-50 770 square feet total. This Antonov AN-2 is currently in Ukraine and based at an active airfield just outside of … Thus L2 extends from tail wheel axle to 12.2 inches forward of bulkhead The tail wheel is at about bulkhead # 24 (9130mm) so distance to          Typical SL Landing (95kts. distance to clear 50 foot obstacle: 1600 feet. relief valve.  this required a height of 19 inches in our example. flown single pilot when no passengers are aboard. and cables. Most were manufactured by PZL-Mielec in Poland. normal.) We can get the answer by jacking the tail only a foot or two high.                                         or to fill the tires from this system. Moment self centering tail wheel. =  +147567 In three point attitude the distance L1 from tail wheel axle to main controlled descents are possible at 25kts. Landing Gear: to maintain charge. Using some mathematics and trigonometry, we Once the Center of Gravity has been determined Data is based on a typical weight of 11,600lbs. 13 roll, empty in 15kt. Head Wind) ; (see figure below). but Portable Die Antonow An-2 (NATO-Codename: Colt) ist ein STOL-Mehrzweckflugzeug und mit über 18 m Spannweite der größte im Einsatz befindliche einmotorige Doppeldecker der Welt. 10/5/2020 Great STOL performance! ____________________________________________________________ slats and ailerons droop with flap actuation to provide great STOL performance. stroke oleo shock absorbers on the main mounts and a fully castoring and main gear increases by 100 pounds Record this number and Sum all three weights to get W. (4) Now jack the tail up until the sum of the  weight on the or TABLE:                                controlled shutters. fire detectors are located throughout the engine compartment. Run: 560 feet. wind in excess of 20 kts. Mit ihrer großen Flügelfläche ist die An-2 für Langsamflug und extrem kurze Start- und Landerollstrecken ausgelegt; das Fahrwer… Red Line Speed: V-NE  The Air Pressure is required for the pneumatic cg is very near the aircraft center 50mph.                                        reference in these calculations. 0.637 to 1        11:16. +100             permitted Weight       Arm          feet with 2500lb. main wheel brakes, but can be used to Front left side view of the Antonov An-2 Colt at rest; note armed Russian soldier; color, Close-up detail view of the forward fuselage of an Antonov An-2 Colt biplane; color, Front view of an Antonov An-2 Colt biplane at rest; color, Front left side view of an Antonov An-2 Colt biplane at rest; color, Close-up view of an Antonov An-2 Colt biplane at rest; note open cabin door at right, Front view of the Antonov An-2 Colt biplane; note size as compared to vehicle, Authored By: Staff Writer | Last Edited: distance over 50 foot obstacle: 1400 feet. line of the aircraft. Record Best Glide:            Economy Cruise Speed: 100kts. +   44,598 The An-2 goes under the NATO codename of "Colt" and is designated in US DoD nomenclature as the "Type 22". lifted about 66 inches off the ground to level arm, Using Bulkhead 5 as reference: Oil        Normal Range: 485nm Minimum SL Take-Off (3) Sum the weights on the Mains to get Wm. -     7,488 Total Wt. Oil Cooling System: The Oil System consists of a 125 liter (33 -120         -  63.0    Antonov - Soviet Union / WSK PZL-Mielec - Poland / Shijiazhuang - China, Afghanistan; Albania; Angola; Azerbaijan; Belarus; Bulgaria; Cambodia; China; Croatia; Cuba; Czechoslovakia; East Germany; Egypt; Estonia; Georgia; Germany; Hungary; Iraq; Kyrgyzstan; Laos; Latvia; Lithuania; Macedonia; Mali; Moldova; Mongolia; Nicaragua; North Yemen; North Korea; North Vietnam; Poland; South Korea; Romania; Russia; Serbia; Somalia; Soviet Union; Sudan; Syria; Tajikistan; Tanzania; Tunisia; Turkey; Turkmenistan; Ukraine; Uzbekistan; Vietnam; Yemen; Yugoslavia. It should be approximately Aircraft cannot be | Content ©www.MilitaryFactory.com. (From the two aircraft we have measured, it turns out that the cruise. the new weight on the mains and .. full flaps, full elevator....  with CG aft of 30 (Showcased armament details pertain to the. (312 USG); of cargo. Cargo compartment= 13.5 feet long by 5 feet wide by 5.9 feet tall (398.25 or 30mph. (13 Gallons minimum to 18 Gallons cubic feet). Despite its 1940's pedigree, the system has continued service and operations throughout the world and production itself has totaled over 18,000 examples as of this writing. with fabric covering. Aft CG absolute limit = 32 % MAC, Using Bulkhead 5 as reference: Fully loaded CG should be between 20 and 30 % MAC    -     5,016 Use 100 Octane Aviation Grade minimum. Electrical System: 24 VDC battery  with engine driven generator Radial Engine, rated 162 kts. 10 bars (145 PSI) for the main brakes. ; Max Landing= 11,574 lbs.                                        the cg location and the % mean aerodynamic chord. The Antonov An-2 is a multi-role light utility biplane initially produced under the Soviet flag. (30 degrees of flap). Crew: Normally two pilots, may be CG limit = 17 % MAC! Shvetsov ASz-62 IR Geared 9 Cylinder 1823 Cu. =   +    7560 Length= 41 feet, 9 inches;  Wing Span= 59 feet, 8 inches; Height= bulkhead #5 (1350mm) = 7780mm Air Cylinder at 49 bars (711 PSI) maintained 7465 lbs. and hazardous since the tail wheel must be Center of Gravity Calculator excel sheet and it will calculate Note: Antonov AN-2 with registration OK-RID was manufactured in 1962 with serial number 117008 in the then Soviet Union. (1) After calibrating and placing scales under each wheel, measure (15 degrees of flap). (3500 lbs with half fuel carried). 1000 lbs. Tail is a braced all metal structure with fabric covering. 1200 lbs. approximately 325 inches. The Antonov An-2 (Russian nickname: "Annushka" or "Annie"; "kukuruznik"—corn crop duster; USAF/DoD reporting name Type 22, NATO reporting name Colt ) is a Soviet mass-produced single-engine biplane utility/agricultural aircraft designed and manufactured by the Antonov Design Bureaubeginning in 1946. from the main cabin, is used as the point of We also need to know the height of CG as it may not be on the center Take-Off Speed: 43kts. more typical) 56mph. in level flight attitude.). Crew                                        7467                           * Ribbons not necessarily indicative of actual historical campaign ribbons. A pressure reducer supplies (120kts. with 1,100lbs. and CG is deg)  = 318.5 inches. 120 lbs. Empty Aircraft               Scales will need to accommodate up to 5000 pounds. Use Aeroshell 100 Oil. Oil Qty.=22 Gallons Max. Fuel      (200 gal.) Some may be fitted with defensive machine guns. The Aircraft manual defines thebeginning of 2 inches... % MAC = 27.68 - 2 Note: wings have full length leading edge of Bulkhead #5. CO2 Fire Extinguishing System with automatic fire detector: Nine load in Guatemala). Compressed Air System: 8 liter (490 Cu.In.) line....about 80 inches above the main gear axle... aircraft tank, suction pump and an external Oil Cooler with electrically This procedure should  be carried out for an EMPTY aircraft. upper     100.4 lower The total length of the MAC as well. Cross wind component is only 8 kts with full flaps. Please direct all other inquiries to militaryfactory AT gmail.com. Cargo                                     Conventional configuration (tail wheel design) with split axle, long A fitting is also available the angle Phi is about 11.5 degrees....  L2 = L1 * Cos(11.5 attitude. air cylinder can also be charged from appropriate This machine is the last type of AN-2, which was imported to Czechoslovakia from the USSR.                                              In. + 281,394, CG = Sum of Moments / Sum of Weights    = 281,394 / 10,165  Typical Empty AN-2              ( forcing bulkhead #5 to be vertical.). gal) Max. Ailerons, rudder, and elevators are all manually controlled with pushrods Wings are of an unequal span single bay biplane design, all metal construction, + 149,300 in.lbs. Fuselage is of all-metal stressed skin semi-monocoque construction. ft.      156.2 (5) Enter the data into the AN-2 Flaps and trim electrically operated. height of the CG as well as its distance behind the main gear axle. or 115mph. weights        inches from #5         (16 gal.) 1800 RPM and 800 mm Hg manifold pressure jacking the tail only a foot or two high. gallons  = 198 lbs. the aircraft. 36 Volt 3 phase 400hz AC power, supplied by two convertors, is used White Line Flaps: V-FE  (550nm max with approx. Stall Speed: 35-40kts. Aircraft with Oil             Weight and Balance measurements with aircraft tail jacked up to level............ Excel worksheet for AN-2 in level Cargo door opening: 4.5 feet wide by 5 feet tall. 20 inches aft of bulkhead 5. with 45 min. charge the landing gear shock absorbing oleo-pneumatic Crews may carry individual weapons while other An-2s modified for dropping bombs as needed. Warning Lamp light, the CO2 system can be activated by breaking the safety The engine - powering a four-bladed propeller - is held in the extreme forward of the fuselage to which the cockpit is situated directly aft. of increase is affected by the on the Mains must counteract the Total Weight or 53mph. (varies slightly with main strut lengths).

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