I A P 2 0 2 0 . 0 0 1 - A F M /
J A B I R U J 1 6 0 / J 1 7 0
P a g e
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54
FOR SIMULATION USE ONLY
Enroute climb
Enroute climbs are performed with flaps up, full throttle, and at speeds 5 to 10
knots higher than the initial scheduled climb speed.
This provides better engine cooling with little loss of climb performance.
Cruise
The power setting and cruising altitude are the two major factors that will
affect the cruising speed and range of the J160/J170.
Other influencing factors include the weight and loading, temperature and
equipment installed in a given aircraft. The maximum power setting normally
used for cruise is 75% of the engine’s rated power.
Power settings below this will result in increased range and endurance
corresponding with the reduced fuel consumption.
At a power setting of 45% the J160/J170 is capable of attaining an
endurance of close to 13 hours, for a range of over 1000 nautical miles.
For efficient and economical operation as well as to achieve maximum
engine service life the engine must always be operated in accordance with
the procedures and specifications set out in the engine manufacturer’s
operator's manual.
75% Power
2800 RPM (14 L/hr)
Stalls
In any attitude or under any loading condition there is no natural stall
warning.
An artificial stall warning horn is set to activate 5 to 10 KIAS above the stall
speed in any configuration.
All controls are effective up to and completely through the stall and there is
no noticeable tendency to enter a spin after the stall.
Descent
Power
As required
Carburettor heat
As required