XtremeAIR XA41, Руководство по обслуживанию

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Maintenance Manual XA41/XA42
AMM-XA42-0040-001 C.00
Page 2 Page date:
Chapter 28 25.09.2018
28-00-00 GENERAL
The fuel system has these components:
 The acro tank
 Two integral wing tanks
 A fuel selector valve
 A fuel filter
 An electrically operated auxiliary fuel pump (boost pump)
 A mechanical fuel pump operated by the engine.
The acro tank is used for aerobatic flight, take-off and landing. The wing tanks are used only
for utility flight.
Figure 28-1: Overview - Fuel system
The fuel tanks capacities (refer to chapter 12-10-08) are:
Total fuel capacity: 277 (L) / 73.2 (US gal)
• Wing tanks: 2x 105 (L) / 2x 27.7 (US gal)
• Acro tank: 67 (L) / 17.7 (US gal)
Usable fuel capacity (Total):
266 (L) / 70.3 (US gal)
Usable fuel capacity (Acro): 57 (L) / 15.1 (US gal)
FUEL
INJECTION
SERVO
Attached to the engine
Firewall
FUEL
PUMP
B
O
O
S
T
P
U
MP
ACRO
TANK
FUEL INJECTION
SERVO