Photos from the personal collection of Christos Fotiadis
Technical specifications
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OKB Antonov, has successfully completed testing a new modernized version of the four-engined heavy transport aircraft An-124-100M-150, which was based on the An-124-100M.
An-124-100M - 150 Commercial Cargo Aircraft © Konstantinos Panitsidis
Antonov is working on modernization of the An-124-100. The An-124-100M-150 version
- includes the main components of the ?N-124-100 program development:
- payload increased from 120 tons to 150 tons;
- take-off weight increased from 392 tons to 402 tons;
- flight range increased, including for cargo of 120 tons from 4650 km to 5400 km;
- aircraft assigned service life is increased to 24,000 flight hours; works on its extension up to 50 000 flight hours/10 000 flights/45 years service life are being performed;
- the new PO-500 schedule of maintenance has been introduced (maintenance every 500 flight hours);
- onboard crane equipment providing loading-unloading operations of a single piece of cargo up to 40 tons weight;
- fuselage structure had been strengthened to enable airlift of a single piece of cargo up to 150 tons weight;
- Navigation System and radar have been updated;
- digital anti-skid braking system allowing to reduce landing distance up to 30% have been installed;
- crew reduced from 6 to 4 members, and the comfort level of the crew rest cabin has been improved;
- military oxygen equipment has been exchanged for the civil one;
- reinforced wheels and tires have been installed;
- new devices for engine control have been installed;
- modernized systems of reverse control and engine vibration state monitoring have been developed;
- the SRPPZ-2000 ground proximity warning system installed;
- A826 inertial navigation system upgraded;
- Enhanced observation (EHS) has been applied;
- Mail Minimum Equipment List has been developed and is now being implemented
On June 19, 2007, the An-124-100M-150 obtained an Annex to the Type Certificate issued by Aviation Register of the Interstate Aviation Committee (AR IAC) and an updated Type Certificate was obtained for the An-124-100 aircraft issued by State Aviation Authority of Ukraine.
THREE-VIEW DRAWING
TECHNICAL SPECIFICATIONS
DESIGNER
|
Antonov
|
---|---|
COUNTRY
|
Russia / Ukraine
|
TYPE
|
Commercial Cargo Aircraft
|
CREW
|
4
|
POWER-PLANT
|
4 TSE Progress (V.A. Lotarev) D-18T III-series
|
Thrust, kN
|
4 x 234,9
|
DIMENSIONS
|
|
Length, m
|
69,10
|
Height, m
|
21,08
|
Wing span, m
|
73,30
|
Wing area, m2
|
628,50
|
WEIGHT
|
|
Maximum take-off, kg
|
405.000
|
Normal take-off, kg
|
392.000
|
Empty aircraft
|
173.000
|
Internal fuel, kg
|
212.350
|
PERFORMANCE
|
|
Maximum speed, km/h
|
865
|
Cruising speed, km/h
|
800-850
|
Ferry range, km
|
16.500
|
Range, km
|
4.800
|
Service ceiling, m
|
11.600
|
Payload, kg
|
88 passengers or 150.000 kg freight.
|
ARMAMENT
|
-
|
PHOTOS An-124-100M-150