Mahindra GIPPSAERO GA8-TC 320 - Fuel and Other Limitations

C01-01-08 5 Feb 2009 Page 2-9
Section 2
Model GA8-TC 320 Limitations
2.12. FUEL LIMITATIONS
Fuel Quantity
Total Useable
Wing Tanks (each) 170 litres (44.9 US Gal) 166 litres (43.85 US Gal)
Sump Tank 9 litres (2.4 US Gal) 0 litres (0 US Gal)
Cumulative
System Capacity
349 litres (92.2 US Gal) 332 litres (87.7 US Gal)
NOTES:
1. The total contents of the sump tank are considered to be unusable fuel.
2. Maximum allowable lateral differential fuel loading - 100 litres (26.4 US Gal).
3. For Fuel Grade refer to paragraph 2.4.3 Fuel Grade.
2.13. MAXIMUM PASSENGER SEATING LIMITS
The maximum passenger seating capacity is seven - one seated beside the pilot and three rows
of two passengers behind.
2.14. OTHER LIMITATIONS
1. If the seat beside the pilot’s seat is equipped with a functioning set of ight controls, refer
to operational requirements for the occupation of this seat by a passenger.
2. Cockpit doors may not be opened in ight except for emergency smoke/fume evacuation
purposes.
CAUTION:
MAXIMUM ALLOWABLE AIRSPEED WITH COCKPIT DOORS OPEN: 100 KIAS.
3. Maximum operating altitude is 20,000 ft. See paragraph 4.4.13 for use of supplemental
oxygen.
4. Smoking is not permitted.
5. The aircraft may be operated onto and from hard sealed, gravel and grass surfaces.
2.15. PLACARDS
The following placards are required, and are to be located in the area indicated. Each placard
is to contain wording conforming with the illustrations. The shape and layout of production items
may vary between individual aircraft. Consult the manufacturer for individual aircraft placard
variations.
01 Aug 2011