The airframe has plenty of resource available before next overhaul and a healthy remaining life. Both engines and propellers have good resource remaining but require a routine overhaul. Engine 1 and Propeller 2 have far greater resource remaining.
By information of ANTONOV Company today more than 430 the AN-24 airplanes continue working in 26 countries of the world.
ORIGINAL MANUFACTURER: Poland PZL, Mielec
CATEGORY: Passenger Transport / Cargo
CURRENT LOCATION: Peru
PERFORMANCE CHARACTERISTICS
Max level: 500km/h, 269kts
Cruise: 450km/h, 242kts
Range: 1,070m/1,710km
Take-off run: 1,750m, 5,775ft
Landing distance: 1,590m, 5,250ft
WEIGHTS:
Empty weight: 13,300kg
MTOW: 21,000kg;
Useful load: 7,700kg
Pilots/Passengers: 4/50
FUEL DETAILS:
Fuel Type: Jet A1
Fuel Capacity: 7,000 litres
AIRFRAME DETAILS:
Resource remaining: 20,135 hrs, TBO: 1,855 hrs
Year: 1973, TTSN: 24,900 hrs, SMOH: 1,855 hrs
ENGINE DETAILS:
Engine 1 - Resource remaining: 9,625 hrs
Year: 1965, Type: Motor Sich AI-24 Series II Turboprop (2,400ehp)
TTSN: 10,374 hrs, SMOH: 3,656 hrs, TBO: 0 hrs
Engine 2 - Resource remaining: 3,687 hrs
Year: 1975. Type: Motor Sich AI-24 Series II Turboprop (2,400ehp)
TTSN: 16,312 hrs, SMOH: 3,835 hrs, TBO: 0 hrs
PROPELLER DETAILS:
Propeller 1 - Resource remaining: 3,903 hrs
Year: 1980, Type: Aerosila AV-72T Series 2A 4-blade
TTSN: 8,096 hrs, SMOH: 1,272 hrs, TBO: 0 hrs
Propeller 2 - Resource remaining: 8,126 hrs
Year: 1992, Type: Aerosila AV-72T Series 2A 4-blade
TTSN: 5,873 hrs, SMOH: 1,323 hrs, TBO: 0 hrs
Airframe has plenty of resource available before next overhaul and a healthy remaining life. Both engines and propellers have good resource remaining but require a routine overhaul. Engine 1 and Propeller 2 have far greater resource remaining.
On September 28, 2009 EASA issued a type certificate for the AN-26 and the AN-26Б allowing continued successful operation of these airplanes registered in the countries of the EU. In particular they are actively used for transportation of mail and urgent cargo in the airlines of Latvia, Lithuania, Hungary and Poland.
ORIGINAL MANUFACTURER: Poland PZL, Mielec
CATEGORY: Passenger Transport / Cargo
CURRENT LOCATION: Peru
PERFORMANCE CHARACTERISTICS
Max level: 540km/h, 291kts
Cruise: 440km/h, 238kts
Range: 680-1,550m/1,080-2,480km
Take-off run: 1,240m, 4,090ft
Landing distance: 1,740m, 5,740ft
WEIGHTS:
Empty weight: 15,020kg
MTOW: 24,000kg;
Useful load: 8,980kg
Pilots/Passengers: 5/40
FUEL DETAILS:
Fuel Type: Jet A1
Fuel Capacity: 6,800 litres
AIRFRAME DETAILS: (this is the best of the 4 available aircraft)
Resource remaining: 14,930 hrs, TBO: 3,419 hrs
Year: 1979, TTSN: 5,069 hrs, SMOH: 580 hrs
ENGINE DETAILS:
Engine 1 - Resource remaining: 11,973 hrs
Year: 1976, Type: Motor Sich AI-24VT Turboprop (2,820ehp)
TTSN: 3,026 hrs, SMOH: 38 hrs, TBO: 0 hrs
Engine 2 - Resource remaining: 12,788 hrs
Year: 1976. Type: Motor Sich AI-24VT Turboprop (2,820ehp)
TTSN: 2,211 hrs, SMOH: 38 hrs, TBO: 0 hrs
PROPELLER DETAILS:
Propeller 1 - Resource remaining: 7,150 hrs
Year: 1990, Type: Aerosila AV-72T Series 2A 4-blade
TTSN: 849 hrs, SMOH: 556 hrs, TBO: 0 hrs
Propeller 2 - Resource remaining: 6,743 hrs
Year: 1979, Type: Aerosila AV-72T Series 2A 4-blade
TTSN: 1,256 hrs, SMOH: 556 hrs, TBO: 0 hrs
Airframe has plenty of resource available before next overhaul and a healthy remaining life. Both engines and propellers have good resource remaining but require a routine overhaul. Engine 1 and Propeller 2 have far greater resource remaining.
Airplanes of the AN-28 family were manufactured serially in Poland at the aviation plant in Mielez town. In common in 1984-1992 170 airplanes were built in Poland. 157 of them were delivered to Aeroflot. Morethan 10 airplaneswerebuiltforthePolishcustomers.
ORIGINAL MANUFACTURER: Poland PZL, Mielec
CATEGORY: Passenger Transport / Cargo
CURRENT LOCATION: Peru
PERFORMANCE CHARACTERISTICS
Max level: 350km/h, 189kts
Cruise: 335km/h, 181kts
Range: 320m/510km
Take-off run: 370m, 1,220ft
Landing distance: 590m, 1,950ft
WEIGHTS:
Empty weight: 3,900kg
MTOW: 6,100kg;
Useful load: 2,200kg
Pilots/Passengers: 1-2/18
FUEL DETAILS:
Fuel Type: Jet A1
Fuel Capacity: 2,660 litres
AIRFRAME DETAILS:
Resource remaining: 2,796 hrs, TBO: 2,796 hrs
Year: 1988, TTSN: 3,203 hrs, SMOH: ? hrs
ENGINE DETAILS:
Engine 1 - Resource remaining: 1,165 hrs
Year: 1989, Type: Glushenkov TVD-10B Turboprop (960shp)
TTSN: 1,829 hrs, SMOH: 335 hrs, TBO: 0 hrs
Engine 2 - Resource remaining: 1,500 hrs
Year: 1990. Type: Glushenkov TVD-10B Turboprop (960shp)
TTSN: 2,493 hrs, SMOH: 0 hrs, TBO: 0 hrs
PROPELLER DETAILS:
Propeller 1 - Resource remaining: 954 hrs
Year: 1989, Type: Aerosila AV-24AN 3-blade
TTSN: 2,046 hrs, SMOH: 2,046 hrs, TBO: 0 hrs
Propeller 2 - Resource remaining: 506 hrs
Year: 1989, Type: Aerosila AV-24AN 3-blade
TTSN: 2,046 hrs, SMOH: 994 hrs, TBO: 0 hrs
This airframe has plenty of resource available before next overhaul and a healthy remaining life. Both engines and propellers have good resource remaining but require a routine overhaul. Engine 1 and Propeller 2 have far greater resource remaining.
Nowadays, a number of enterprises of the aviation industry of Ukraine including ANTONOV Company, “410 plant of Civil Aviation” State Enterprise continue works on overhaul and modernization of the AN-32 aircraft for the Indian Air Force.
At present more than 240 of the AN-32 aircraft are being operated in countries with adverse climate conditions, including CIS, India, Sri-Lanka, Bangladesh, Columbia, Peru, Mexico, Afghanistan, African countries, etc.
ORIGINAL MANUFACTURER: Poland PZL, Mielec
CATEGORY: Passenger Transport / Cargo
CURRENT LOCATION: Peru
PERFORMANCE CHARACTERISTICS
Max level: 530km/h, 286kts
Cruise: 470km/h, 254kts
Range: 1,350m/2,160km
Take-off run: 1,240m, 4,090ft
Landing distance: 1,700m, 5,600ft
WEIGHTS:
Empty weight: 16,800kg
MTOW: 27,000kg;
Useful load: 10,200kg
Pilots/Passengers: 4/50
FUEL DETAILS:
Fuel Type: Jet A1
Fuel Capacity: 5,450 litres
AIRFRAME DETAILS:
Resource remaining: 20,135 hrs
Year: 1988, TTSN: 5,178 hrs, SMOH: 1,839 hrs
ENGINE DETAILS:
Engine 1 - Resource remaining: 9,625 hrs
Year: 1989, Type: Ivchenko AI-20D Series V Turboprop (5,180ehp)
TTSN: 2,792 hrs, SMOH: 2,792 hrs, TBO: 0 hrs
Engine 2 - Resource remaining: 3,687 hrs
Year: 1991. Type: Ivchenko AI-20D Series V Turboprop (5,180ehp)
TTSN: 2,777 hrs, SMOH: 2,777 hrs, TBO: 0 hrs
PROPELLER DETAILS:
Propeller 1 - Resource remaining: 3,903 hrs
Year: 1998, Type: Aerosila AV-67DM 4-blade
TTSN: 2,271 hrs, SMOH: 266 hrs, TBO: 0 hrs
Propeller 2 - Resource remaining: 8,126 hrs
Year: 2002, Type: Aerosila AV-67DM 4-blade
TTSN: 1,016 hrs, SMOH: 74 hrs, TBO: 0 hrs
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