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Jabiru Aircraft
Pilot Operating Handbook
Model J170-D
JP-FM-13
Revision:
0
1
2
3
4
28 Feb 2020
Page 2-19
2.3 LIMIT LOAD FACTORS
Flap Position
Speed
Positive
Negative
UP
UP
DOWN
V
A
V
NE
V
FE
+ 4g
+ 4g
+ 2.0g
-2g
-2-g
0g
2.4 FLIGHT OPERATION LIMITATIONS
Manoeuvres in the course of normal flying are approved.
Stalls may be carried out at bank angles of up to 60°.
All aerobatic manoeuvres including spins are prohibited.
Flight Operations are limited to VMC (Visual Meteorological Conditions).
Flight Operations in IMC (Instrument Meteorological Conditions) are prohibited.
2.5 FUEL
Total Capacity:
140L (37 USgal) Total (2 OFF 67.5L Wing Tanks + 5L Header
Tank)
Usable Capacity:
135L (35.6 USgal) Useable
Grade:
Avgas 100LL, Avgas 100/130 or MOGAS with RON of 95 or
higher. See Section 8.6
Max zero wing fuel weight: Equal to gross weight, 600kg (1323 lb)
(W
ZWF
)
2.6 FUEL GAUGES (where equipped)
Fuel pickups are in wing roots. Care must be taken to maintain balanced flight at low fuel levels to
ensure that fuel can be drawn from both tanks. If the aircraft is flown for extended periods in an
unbalanced condition, it is possible to fully drain one tank while there remains fuel in the other.
2.7 POWERPLANT LIMITATIONS
POWER
R
P
M
Maximum
Temperatures
Fuel Pressure
Limits
Oil Pressure
Limits
Cyl
Head
Oil
Min
Max
Min
Max
Absolute
Limits
Maximum
Take-Off
(80 BHP)
3300
200 °C
(392
°
F)
(Note #1)
118°C
(244
°
F)
5 kPa
(0.75psi)
35 kPa
(5.0psi)
220 kPa
(31 psi)
525 kPa
(76psi)
Continuous
Limits
Maximum
Cont
(80 BHP)
3300
180°C
(356°F)
100°C
(212°F)
5 kPa
(0.75psi)
35 kPa
(5.0psi)
220 kPa
(31 psi)
525 kPa
(76 psi)
Limits For
Ground
Running
N/A
N/A
180°C
(356°F)
(Note #2)
100°C
(212°F)
(Note #2)
5 kPa
(0.75psi)
35 kPa
(5.0psi)
80 kPa
(11 psi)
525 kPa
(76 psi)
Note #1 Time with CHT at between 180°C and 200°C is not to exceed 5 Minutes