Super Mushshak
Photo Credit Pakistan Aeronautical Complex
Introduction
Super Mushshak is a variant upgraded version of Super Mushshak fitted with a more
powerful 260 HP engine, cockpit air-conditioning, electrical instruments,
and electric cum manual elevator and rudder trim. The aircraft has been
developed to meet FAR part 23 certification in categories normal, utility
and aerobatics. It has a spacious side by side cockpit giving a good view to the pilot
(instructor) and co pilot (student) for the effective "watch me" instruction.
Super Mushshak meets the requirements of a modern primary training syllabus
and is an ideal basic trainer for basic flight training and instrument
flying. The aircraft is available for both civilian and military use.
This aircraft is available for sale to any private/civilian individual or business.
Price
Pakistani Rupees 6 million (Rs. 60 Lakhs) (Unofficial estimate. Real price may be different)
Engine
Type = Textron Lycoming IO-540 V4A5
Power = 260 HP (at 2700 RPM at ISA conditions)
Cylinder = 06
Propeller
The aircraft has been qualified with three and two blade propellers from Mccauley and
Hartzell of USA.
TBO
Time between overhaul (TBO) of engine and propeller is 2000 hours.
Cockpit
Spacious side by side cockpit giving good contact between the pilot and the co-pilot / observer or between the student and the instructor for effective " watch me" instruction.
• Adjustable seats fitted with straps incorporating lockable inertia reels
• Typical avionic equipment configuration includes UHF/VHF radio, GPS, VOR, Transponder and ADF.
• Third crew member can be accommodated in the rear cabin
Training Role
Super Mushshak meets the requirement of a modern primary training syllabus and is an ideal basic trainer. Aircraft is ideal for:
• Basic Flight Training
• Instrument flying
• Aerobatics, stalls and spins
• Night flying
• Navigation flying
• Formation flying
Army Co-operation Missions
Besides primary flying training, the Super Mushshak is also suited for a wide range of army co-operation missions including:
• Forward air control
• Forward area support with droppable supply containers
• Reconnaissance
• Artillery Fire Observation
• Camouflage inspection
• Border patrol
• liaison
• Target flying and target towing for training of ground units
Fuel system
• Based on two integral fuel tanks holding a total of 48 US gallons
• Bendix RSA type fuel injection system
• Houses engine driven fuel pump for normal operation
• Electric fuel pump for emergency conditions.
Flight Control System
• Efficient dual flight controls including conventional stick type control columns and adjustable rudder pedals. Primary control surfaces are operated through a direct mechanical linkage.
Design Criteria
The basic design philosophy behind Mushshak offers an aircraft with:
• Flexibility, covering both Army Co-operation and primary flying training
• Excellent forward and downward visibility supplemented by a good rearward visibility
• Good ground clearance even with bulky under wing stores and high crosswind capability for operation from narrow strips and roads
• Upto 300 Kg/660 lbs external load carrying capability (including pylons).
• Heavy-duty landing gear
• Large baggage compartment in the rear part of the cabin easily accessible through a door on the port side of the fuselage. This space can also accommodate a third crew member
• Good handling characteristics
• Good short/rough field performance
• Fully aerobatic capability, maximum limit load factor +6/-3 in Aerobatics category
• Ease of maintenance and repair even in combat conditions
• 8300 hrs structure life
• Low radar signature
Optional Equipment
The following alternate/optional equipment can also be made available on request:
a. Blind flying screen: There is a provision for installation and removal of blind screen for instrument flying.
b. Sun Blinds: Canopy perspex as well as rear cabin perspex can be provided with adjustable sunblind.
c. Third Seat: Aircraft incorporate fitting for the installation of third seat in the rear portion of the cabin.
d. Advance Avionics: Includes ILS alongwith standard avionics package
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Technical Specifications
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GENERAL
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|
Span
|
29
feet |
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Length
|
23.5
feet |
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Height
|
8
feet 6.5 inch |
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Wing
Area
|
128
sq. feet |
|
|
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WEIGHTS
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|
Max.
Take off Weight
|
2645
lb |
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Max.
Landing Weight
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2515
lb |
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POWER PLANT
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Type
Textron Lycoming
|
10
- 540 - V4A5 |
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Power
|
260
HP |
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|
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PERFORMANCE
|
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Max.
SL Speed
|
145
kts |
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Cruise
Speed SL
|
130
kts |
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TOD
(50 feet)
|
900
feet |
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LD (50
feet)
|
970
feet |
|
Rate
of Climb
|
1700
fpm |
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Range
|
440
nm |
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Endurance
|
4
: 15 hrs |
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Load
Factor
|
+6,
-3 |
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Back
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