CATALOGUE

ENGINES
AIRCRAFT ENGINEERING AND MAINTENANCE
D-18T SERIES 3
TUBRBOFAN AERO ENGINE
It is designed to power the AN-124, AN-
124-100 RUSLAN and AN-225 MRIYA
ramp-equipped heavy cargo aircrafts.
The engine design allows operating it on
technical condition up to depletion of the
engine main components life. The engine
has Type Certificate. It meets
the current environmental requirements
of ICAO standards.
Dimensions:
5400х2937х2792 mm
Weight, dry:
4100 kg
Main Specifications:
Take-off performance (SLS; ISA)
thrust
23430 kgf
specific fuel consumption
0,34 kg/kgf•h
Maximum cruise performance (Н=11000 m; Мfl=0,75; ISA)
thrust
4860 kgf
specific fuel consumption
0,546 kg/kgf•h
Main Specifications:
Automatic control system
adjustment types:
D-436-148B D-436-148D D-436TP D-436T1
Emergency performance (SLS)
thrust 7280* kgf 7690** kgf - -
Takeoff performance (S/L static; ISA)
thrust 6570* kgf 7010** kgf 7500 kgf 7500 kgf
specific fuel consumption 0,351 kg/kgf•h 0,351 kg/kgf•h 0,37 kg/kgf•h 0,37 kg/kgf•h
Max cruise rating (Н=11000 m, Mfl=0,75, MCA+10 o С)
thrust 1560 kgf 1560 kgf 1500 kgf 1670 kgf
specific fuel consumption 0,6 kg/kgf•h 0,6 kg/kgf•h 0,650 kg/kgf•h 0,608 kg/kgf•h
Dimensions 4,034 x 1,784 x 1,930 mm 4170х1640х1915 mm 4170х1802х1949 mm
Weight, dry 1400 kg 1450 kg
*-tAMB =+37,5 oC / **- tAMB =+30 oC
D-436-148FM
TUBRBOFAN AERO ENGINE
D-436-148FM Turbofan
Aero Engine is designed
to power the An-178 shortdistance
military transport
aircraft and regional An-
148 and An-158 passenger
aircraft. The engine has
Type Certificate. It meets
the effective environmental
requirements of ICAO
standards.
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