Categorized | Current Affairs, Pak CA

Pakistan is now exporting planes

PAC starts defence exports

Islamabad—Pakistan Aeronautical Complex (PAC) Kamra has started defence exports that include sale of 05 Super Mushshak aircraft and 03 Mushshak retrofitted to Super Mushshak aircraft and the first sale of Mushshak 17-1 aircraft to the civil market segment in South Africa. This was informed to the National Assembly Standing Committee on Defence Production that visited PAC under the Chairmanship of Sheikh Aftab Ahmad, MNA where it was briefed in detail about various functions of PAC and was subsequently shown the facilities associated with various projects in hand, said a press release issued here.

The Committee appreciated overall performance and professionalism of Pakistan Aeronautical Complex (PAC) Kamra which carries out the manufacturing of fighter aircraft JF-17.

The Committee was informed that Pakistan Aeronautical Complex Kamra comprises four factories and is spread over an area of 10 Square Kilometers and has become a center of excellence in aviation engineering based on more than 30 years of experience in maintenance, repair and overhaul (MRO) of fighter aircraft, components and engines. It was stated that the technological advancement from manufacturing of Mushshak and Super Mushshak primary flight trainer aircraft to JF-17 Thunder fighter aircraft endorses the strength of PAC to meet future defence challenges. The JF-17 Thunder is a single-seat, single-engine, all-weather, day-night air superiority fighter aircraft with a mix of conventional and fly-by-wire controls that make it highly agile and maneuverable. It can fly at the speed of Mach 1.6, has high thrust to weight ratio and can engage targets at all speeds and altitudes within the conventional flying envelope. The aircraft has state of the art avionics package on board for high degree of survivability through automated system of threat detection, analysis and counter threat measures and to enable effective management of weapons and firepower.

It was informed that in 1972, PAC started with the MRO of aircraft of Chinese origin and subsequently progressed towards MRO of Mirage III and V aircraft and ATAR 09C engine, F100-220E engine of F-16 aircraft, T-56 engine of C-130 aircraft and avionics upgrade of fighter aircraft. The Committee was told that PAC manufactures Mushshak and Super Mushshak aircraft for primary flight training, sub-assemblies of K-8 advanced jet trainer aircraft as well as Baaz and Ababeel aerial target drones. The Mushshak aircraft is Type Certified by Pakistan Civil Aviation Authority and has been issued Type Acceptance Certificate by South Africa Civil Aviation Authority.—Online

Super Mushshak — the Agile — is a variant upgraded version of 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.
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
Technical Data
Main Data

o Length7.15 m/23.5 ft
o Height2.60 m/8 ft 6 ½ in
o Span8.85 m/29 ft
o Wheel Track2.2 m/7 ft 2 ½ in
o Wheel base1.6 m/5 ft 3 in
Wing
o Wing Area, reference11.9 m²/128 sq ft
o Sweep Forward5°
o Airfoil Thickness10%
o Dihedral1.5°
o Mounting angle of incidence+2.8° nose up
Horizontal Tail
o Span2.80 m/9 ft 2 in
o Area2.10 m²/22.6 sq ft
o Sweep0°
o Airfoil Thickness12%
o Dihedral0°
Vertical Tail
o Height1.32 m/4 ft 4 in
o Area, reference1.52 m²/16.3 sq ft
o Airfoil Thickness12%
o Sweep, Leading Edge36°
o Sweep, Trailing Edge8°

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