AIM OF NCC

AIMS OF NCC

  • * To develop character, comradeship, discipline, leadership, secular outlook, spirit of adventure and the ideals of selfless service amongst the youth of the country.
  • * To create a human resource of organised, trained and motivated youth, to provide leadership in all walks of life and always available for the service of the nation.
  • * To provide a suitable environment to motivate the youth to take up a career in the Armed Forces.


Thursday, 17 October 2013

TECHNICAL DETAILS : ZEN AIR CH 701 STOL AC

Untitled Document

TECHNICAL DETAILS : ZEN AIR CH 701 STOL AC

LEADING PARTICULARS       
  

Length : 20 feet      Wing Span   : 27  feet    Wing Area     : 127 sq ft
Fuel Cap        : 42 Lit    Max speed   : 80 mph Cruise speed     : 80 mph
Tailplane span: 87.5” Mainplane chord  :58.9” 

Wheel track   : 68.8”
Empty Wt       : 209kg Gross Wt       : 436kg

Useful load   : 227kg
Wing Load     :37kg/m² Cabin width     : 42”

Aileron dfln   :15+1ºup/dn
Flaps dfln      : 26+2ºup/dn Elevator dfln up :32º-35º

Elevtr dfln dn       :28º-30º
Rudder dfln   : 23+2º Endurance       :     hrs Ceiling Ht      :14000feet
Type of Wing:Height:11 feet

T/O length     :      feet

  
Take off speed: 40mph Cross wind limit  :15mph

Stalling speed : 30mph
Never exceed speed (VNE) : 110mph

Normal operating speed range: 35 to 85 mph 2.2lbs=1kg

LIMITATIONS OF THE MICROLIGHT AC

  1. No aerobatics & spinning permitted on this aircraft
  2. No inverted flying permitted.
  3. Flying can be undertaken only at day time under VFR conditions.
  4. Aircraft has to be properly secured before starting.
  5. Do not run the engine with bystanders standing loose.
  6. Never leave the aircraft unattended with the engine running.
  7. Do not operate in strong winds or turbulent conditions.
  8. Always remove the IGNITION KEY after switching of f the engine
  9. Never accelerate the engine below the recommended oil temperature.
  10. Always use the correct and recommended grade fuel, oils, lubricants and coolants to prolong engine life and health.
  11. Always use the correct and recommended tools only for the maintenance of the aircraft.
  12. On change of spark plugs always change both the spark plugs of a cylinder. Never interchange spark plugs between cylinders.
  13. Never exceed the maximum rated engine RPM.
  14. Always allow the engine to cool for several minutes before switch off
  15. Do not operate under sustained negative G.

 

AIRCRAFT PERFORMANCE

Limit load factor- Flaps up              : +4 G to -2 G
Limit load factor- Flaps dn              : +2 G
Design load factor                           : +6 G to -3 G

TECHNICAL PARTICULARS  


Engine : Rotax 912A:-4stroke- 4 cylinder, horizontally opposed, spark ignition, 80 BHP Engine having a displacement of 1211cm³ with a compression ratio of 9:1. Swept volume of cylinder 79.5mm Ø and stroke 61mm. Cylinder head liquid cooled, Dry sump lubrication system. Electrical system is AC generator with rectifier-regulator (12V 20 Amp DC)

 

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