'B ' CERTIFICATE EXAM

'B' CERTIFICATE EXAM WHICH WILL BE HELD ON 15 & 16 OF FEB2014 @ SOWDESWARI COLLEGE,SALEM

REPUBLIC DAY CELEBRATION @MEC

REPUBLIC DAY CELEBRATION

INTERNATIONAL DISASTER DAY RALLY

INTERNATIONAL DISASTER DAY RALLY

TECHNICAL DETAILS : ZEN AIR CH 701 STOL AC

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)

 

NCC SYLLABUS

NCC SYLLABUS

S. NO	SUBJECT	1ST YEAR	2ND YEAR	3RD YEAR	TOTAL PERIODS
1.	The NCC	03	00	00	03
2.	National Integration and Awareness	06	06	06	18
3.	Drill	16	19	08	43
4.	Weapon Training	12	10	10	32
5.	Personality Development & Leadership	10	15	20	45
6.	Disaster Management	03	03	04	10
7.	Social Awareness & Community Development	05	05	06	16
8.	Health & Hygiene	05	04	07	16
9.	Adventure	02	06	07	15
10.	Environment Awareness and Conservation	02	02	02	06
11.	Obstacle Training	02	02	02	06
	TOTAL	66	72	72	210

 

Happy Independence Day

Happy Independence Day

 

SELECTED FOR IGC/VSA CAMP

Reg.No: 12/41368 F/Cdt M PRADEEP KUMAR(III-ECE(B)) have been selected for INTER GROUP COMPETETION CAMP / VSC.