Pilot´s Operating Handbook
EXTRA 200
907.6
WEIGHT AND BALANCE
LOADING WEIGHTS AND MOMENTS
TOTAL FUEL CAPACITY: 190 LITER (52,2 US GAL.)
ACRO & CENTER TANK
LITER
(US GAL)
5
(1,3)
10 (2,6)
15 (4,0)
20 (5,3)
25 (6,6)
30 (7,9)
36 (9,5)
907.7
DESCRITPTION OF THE SYSTEM
Wing tank:
The leading edge section of each wing in front of main spars forms an integral fuel tank
providing two interconnected tanks with 154 litres (40,7 US GAL.) total capacity. Each side
of the wing has a 2" diameter filler cap for gravity refuelling. The long range tank has two
compartments in either wing which are separated by a slosh rib. Due to the interconnection
the fuel level of the left and right integral tank will equalize during refuelling within reason-
able time. For max. fuel capacity, the first filled side have to be filled once again! Further-
more the wing tank is connected directly to the engine by the fuel selector valve. Unusable
fuel is approximately 1 liter (0.3 US Gal.).
Page Date: 20. April 2002
KG
KG x CM
(LBS)
(LBS x IN)
3,6
(8)
126
(109)
7,2
(16)
252
(218)
10,8
(24)
378
(327)
14,4
(32)
504
(437)
18,0
(40)
630
(546)
21,6
(48)
756
(655)
25,9
(58)
932
(799)
FUEL
WING TANK
LITER
KG
(US GAL)
(LBS)
10 (2,6)
7,2
20 (5,3)
14,4
30 (7,9)
21,6
40 (10,6)
28,8
50 (13,2)
36,0
60 (15,8)
43,2
70 (18,5)
50,4 (111)
80 (21,1)
57,6 (127)
90 (23,7)
64,8 (143)
100 (26,4)
72,0 (158)
110 (29,0)
79,2 (174)
120 (31,7)
86,4 (190)
130 (34,3)
93,6 (206)
140 (36,9)
100,8 (222)
150 (39,6)
108,0 (238)
154 (40,6)
110,9 (244)
Section 907
Long Range Wing Tank Capacity
KG x CM
(IN x LBS)
(16)
361
(312)
(32)
721
(625)
(48)
1082 (937)
(63)
1443 (1250)
(79)
1804 (1562)
(95)
2164 (1875)
2525 (2187)
2886 (2499)
3246 (2812)
3607 (3124)
3968 (3437)
4329 (3749)
4689 (4062)
5050 (4374)
5411 (4687)
5555 (4811)
907 - 5
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