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The MA60 is a reliable aircraft for an airline to develop regional transportation business for its excellent cost effectiveness, high airport adaptability and being environmentally- friendly.
Cost effective: The MA60 is designed with an optimized aerodynamic configuration, a long service life, high fuel efficiency and low maintenance cost, which all contribute to its low operation cost.
Comfort: The MA60’s airframe section is designed to the civil aircraft economic and comfort standards and its cabin is designed by reference to the typical size of an American or European man (1.805m tall), which make it satisfy with the passenger’s request for comfortability.
Airport adaptive: The MA60 is not restrictive in runway length and runway surface quality. It is capable of taking-off/landing on soil, cement, pitch and gravel or grass runway, as well as capable of instrument meteorological conditions flight. Therefore, it has good airport adaptability.
Environmentally-friendly: The turboprop engine is quite environmentally-friendly for its low emission which minimizes the affect to environment.
Performance Geometric Data
|Aircraft Length||24.708 m|
|Parking Height (free condition)||8.853 m|
|Wing Span||29.2 m|
|Horizontal Tail Wing Span||9.996 m|
|Main Wheel Track||7.90 m|
|Wheel Base||9.564 m|
|Maximum Width of the Fuselage||2.9 m|
|Cabin Width||2.686 m|
|Cabin Length||10.794 m|
|Cabin Height||1.896 m|
|Passenger door||0.750×1.405 m|
|Forward Cargo Door||1.190×1.220 m|
|Rear Cargo Door||0.750×1.410 m|
|Emergency Exit||0.510×0.927 m|
|Maximum Taxiing Weight||21900 kg|
|Maximum Take-off Weight||21800 kg|
|Maximum Landing Weight||21200 kg|
|Maximum Payload||550 kg|
|Maximum Fuel Weight||4030 kg|
|Business Weight||375 kg|
|Sea level, ISA condition, Flaps 15°||1660 m|
|Sea level, ISA condition, Flaps 5°(optional)||1705 m|
|Dry runway, Target airport (coefficient 1.667)|
|Sea level, ISA condition||1460 m|
|ISA condition, APU bleed||3825 m|
|Maximum Operation Altitude||7620 m|
Leg Performance ISA, calm wind, cruising altitude:6096 m,IFR backup fuel:
|Block Distance||970 km|
|Block Fuel||1600 kg|
|Block Time||2.77 h|
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