Pilot Operating Handbook KP-5 ASA
19
2.1 Structural regulations
The KP - 5 aircraft construction, materials and performance correspond
with UL – 2 regulations issue
d by LAA ČR (Light Aircraft Association
of Czech Rep.)
2.2
Operational speed limitations
Airspeed
Abbrevia
tion
CAS
(knots)
CAS
(MPH)
Never exceed airspeed
V
NE
140
162
Max. speed of horizontal flight
V
H
120
138
Max. manouvering speed
- do not execute full deflections of control
surfaces above this velocity
V
A
84
97
Maximum velocity with flaps fully
extended
V
FE
59
68
Stalling speed in landing configuration
V
S0
35
40
Stalling speed with retracted flaps
V
S
42
48
2.3 Engine operational limitations
Specifications stated in this article are not complete.
For more
information, see Operator‘s Manual for all versions of ROTAX 912
Engine
Value
Oil pressure
max. 7 bar, min. 0,8 bar
normal 2.0 –5,0 bar
Oil temperature
R 912 UL
min. 50
°
C, max. 140
°
C
R 912 ULS
min. 50°C, max. 130°C
normal 90-110
°
C
Cylinder head
temperature
R 912 UL
max. 150
°
C
R 912 ULS
max. 135°C
Exhaust gas temperature
max. 880
°
C – at T-O
max. 850
°
C – during fly
normal 800
°
C
Fuel pressure
max. 0,4 bar, min. 0,15 bar
normal 0,15-0,4 bar
