Jabiru Aircraft
SECTION 2
CASA APPROVED
Model J160-C
LIMITATIONS
JP-FM-06
Revision:
0
1
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1 Dec 2008
Page 2-10
System Instruments and/or
Equipment
VFR
Day
Remarks
Engine Indicating
Cylinder Head Temperature
1
Tachometer
1
Oil Pressure
1
Oil Temperature
1
Fuel Pressure
1
Oil Quantity (Dip Stick)
1
Caution Warning System
1
Fuel, electrical, and
vacuum systems
Approved Flight Manual
1
Table 2.11.2
2.14
FUEL LIMITATIONS
Fuel Quantity
Total
Useable
Wing Tanks (each)
67.5 litres (17.8 US Gal)
67 litres (17.6 US Gal)
Sump Tank
6 litres
(1.6 US Gal)
0 litres
(0 US Gal)
Cumulative System Capacity
140 litres (37.3 US Gal)
135 litres (35.2 US Gal)
Table 2.12
NOTE:
•
The total contents of the sump tank are considered to be unusable fuel.
•
For Fuel Grade refer to section 2.4.3 Fuel Grade
•
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 is still
fuel in the other.
2.15
MAXIMUM PASSENGER SEATING LIMITS
The maximum passenger seating capacity is one seated beside the pilot.
2.16
OTHER LIMITATIONS
•
As the seat beside the pilot's seat is equipped with a functioning set of flight controls, refer
to operational requirements for the occupation of this seat by a passenger.
•
Cockpit doors may not be opened in flight except for emergency smoke/fume evacuation
purposes.
•
Maximum operating altitude is 10 000 feet.
Summary of Contents for J160-C
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