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1992 AN74T-100 cargo

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Seller: aeroasia | Seller Information
State: none
Country: Kazakhstan
Price Call for Pricing
Link to your website: http://www.aeroasia.ucoz.kz/...
Views: 1816
Year: 1992
Aircraft Type: Antonov AN74T-100
Location: Russia
Condition: Used
Serial Number: TBD
Registration Number: RA
Total Time: 4765
Airframe: Date of manufacture 29.04.1992
Registration RA
Insurance NO
Max. no. of passenger seats 8
Total airframe hours/land 4765/1768
Specified Life: Hrs/ landings/years 40000/20 000/30
Noise abatement- in accordance with ICAO Annex 16 Chapter 3
Maximum range – 4700 km, Cruse speed – 550-650km/h , Cruising altitude - 10100m (FL310-330), MTOW - 36500kg
Engine Specification: Engine # 1 left D-36 ser. 3A
Serial number 708036313А 001
Date of manufacture 16..09.1991
Date of overhaul Nil
№;overhaul Nil
Specified Life Hrs/cycles 9000/7273
Hours since new, h/cycle 4852
Life until first overhaul, Hrs/cycle 5250/2 000
will be prolonged
Life limit available - further prolongation for 2 years

Engine # 2 right D-36 ser. 3A
Serial number 708036413А 011
Date of manufacture 05.08.1994
№;overhaul -
Date of overhaul -
Hours since new, h/cycle 4846
Life until first overhaul, Hrs/cycles 5250/2 000
will be prolonged
Life limit available - will be prolonged for 2 years

APU ТА-12
Serial number 33012028
Date of manufacture 01.08.1993
№;overhaul 1
Date of overhaul 28.06.2002
Hours since new, h/cycle 415
Flight hours since last overhaul, h 227
Life limit available, h/cycle 273
Avionics/Radios: EGPWS +
ТCAS +
RVSN +
Interior/Exterior: http://www.aeroasia.ucoz.kz/load/2-1-0-8
Additional Equipment: Number of crew members 4-6
Number of passenger seats 8
Max take-off weight 36,5
Max payload 7500 - 10000 kgs
Length 28.07 m
Wing span 31.89 m
Height 8.75 m
Cruising speed 550 km/hr Maximum speed 700 km/hr Flight altitude 10.100 km
Dimensions of cargo compartment (bxhxl) 9.5 x 2.15 x 2.2
Cargo door size 2.4 x 2.27 m
Volume of cargo compartment 45-50 m3
Engine two turbofan engines D-36 3A series, chapter III complian
Inspection Status: Date heavy form (Contrl Regenerative Check) at an operating time
CR CHECK -3 –15.09.2006 2189 h,
Life limit between Contrl Regenerative Check further it is necessary CR CHECK-4 + Prolongation

Specified Life:
Frame 40 000 Hrs, 20 000 landings, 30 years
Left engine 9 000 Hrs, 7 273 cycles, 18 years
Right engine 9 000 Hrs, 7 273 cycles, 18 years
The appointed resource:
- The plane - 40000 of flight hours, 20000 landings, 30 years.
- The engine - 9000 of hours.
- APU - restrictions are removed.
Description:
The Price - CALL.
(Load up to 10.0 tones).
Date of delivery – within 30 days !
The Buyer will give the Letter on interest and will confirm readiness to buy the plane for a suggested price. Lets out LOI for a suggested price and will approve, that the Buyer is ready to expose the deposit of 5 % before survey of the plane and not later than within 10 days from date of the LOI. Conditional deposition should be in the Europe.
The plane will be removed from the market for the coordinated per

 

 

 

 

 

 

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