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SECTION 6
Aircraft Operating Instructions Edge XT 912
WEIGHT BAL & EQUIP
January 2014
Issue 2.4
Page 90
6.3 Typical Aircraft Weights
Table 5 Section 6. Typical Aircraft Weights
6.3.1
Weighing Procedure
The trike base should be lifted by the suspension point on the top of the mast.
Prior to weighing ensure that all fuel is drained and all baggage is removed from the aircraft. The weight,
if changed due to option fitment should be recorded as a new issue and dated accordingly in section 6.2.
6.3.3 6.3.4 Fuel Conversions
Table 6 Section 6. Fuel Conversions
Payload calculator XT-912
Arrow
Arrow K
Merlin
MTOW
kg
lb
Typical Empty Weight
kg
238
233
230
Including unusable fuel
lb
525
514
507
Typical Weight (Crew Plus Min Fuel)
kg
420
415
412
Two crew (172kg) and minimum (10.3kg) fuel
lb
927
916
909
Total Useable Payload
kg
212
217
220
MTOW minus AUW
lb
467
478
485
450
992
Useful Fuel Conversions - Litres & Gallons to Kilograms
L
gall
kg
Minimum fuel (One hour) @ Cruise of 4900rpm
14
3.7
10.3
15
4.0
11.1
20
5.3
14.7
25
6.6
18.4
30
7.9
22.1
35
9.2
25.8
40
10.6
29.5
45
11.9
33.2
50
13.2
36.9
55
14.5
40.5
60
15.9
44.2
65
17.2
47.9
Fill tank from empty
70
18.5
51.6
