Viper Aircraft ViperJet MkII, Руководство по эксплуатации

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P I L O T ’ S O P E R A T I N G H A N D B O O K V I P E R J E T M K I I
Revision 1
2-2
June 1, 2008
POWERPLANT LIMITATIONS
Engine Manufacturer : Viper Aircraft Corporation (Experimental)
Engine Model Number : VA J-85-17A
Engine Operating Limits for Takeoff and Continuous Operations :
Maximum Thrust : 2850 lbs.
Maximum N
1
: 101.2% (5 minute limit)
Maximum EGT (START): 780° C (10 second limit)
Maximum EGT (TAKEOFF): 704° C. (5 minute limit)
Normal Oil Temperature Operating Range : 60 – 185° C
Normal Oil Pressure Operating Range : 20 – 55 PSI
Ignition System (time limit 1): 2 minutes ON; 3 minutes OFF; 2 minutes ON; 23
minutes OFF
Ignition System (time limit 2): 5 minutes ON; 25 minutes OFF
WEIGHT LIMITS
Maximum Takeoff and Landing Weight : 5500 lbs.
Maximum Weight in Baggage Compartment : 50 lbs.
CENTER OF GRAVITY LIMITS
Center of Gravity Range :
Forward : Appx. 158.0 inches aft of datum (15% of Mean Aerodynamic Cord)
Aft : Appx. 162.50 inches aft of datum (25% of Mean Aerodynamic Cord)
Reference Datum : Nose of aircraft at base of pitot tube (if bayonet pitot installed).
MANEUVERS
This aircraft is designed for aerobatics; however, all maneuvers must first be performed in
the flight testing period and signed off in the aircraft logbook in accordance with the
Operating Limitations that accompany the Airworthiness Certificate. The following are
suggested entry speeds and do not constitute an endorsement for any aerobatic
maneuvers which are performed. All maneuvers are subject to the Flight Load Factor
Limits contained herein.