Pilot Operating Handbook KP-5 ASA
20
Note:
- do not use increased power of engine during flight (allowed for take-
off and in emergency cases only)
- take-off is prohibited if engine is running unnaturally or if data on
engine instruments is not in operating ranges
-
do not use change over of suction chamber for suction without filter
(preheated air) on the ground
2.4 Crosswind and wind limitations
Maximum wind speed component for take-offs and landings:
- in RWY direction (headwind)
23,3 kt
- crosswind
15,6 kt
2.5 Fuel capacity
Fuel capacity in one tank 8,45 (11,9) U.S.gal
Total fuel capacity 16,9 (23,8) U.S.gal
Min. allowed amount for take-off (in one fuel tank) 2,6 U.S.gal
The amount of fuel is indicated by electromechanical fuel gauges. The
reserved capacity of 1,3 ÷ 1,9 (3 ÷ 3,5) U.S. gal in each tank is indicated
by the yellow amber light in fuel gauges.
2.6
Service ceiling
Service ceiling [ft]
14750
2.7 Maneuvers approved
Manoeuvre
Max. initial airspeed in IAS
(knots)
(MPH)
Steep turn (60° bank)
84
97
Slip
54
62
