A.P. 2210G.-P.N.
Pilots's Notes
PART V
OPERATING DATA
94. Weight and C.G. data
(a) The weight and C.G. limitations are given in Part II,
para. 46(c) (d).
(b) The aircraft should always be loaded in accordance with
the instructions given in A.P.2210G, Vol.1, Section 4,
Chapter 1.
(c) The aircraft is at its maximum all up weight with two
pilots, full internal fuel, full ventral and wing drop tanks.
To reach the maximum landing weight from this condition,
all drop tank fuel must be used and approximately 40 gal-
lons of internal fuel.
(d) C.G. movement with consumption of fuel is as follows:-
Wing drop tank fuel .. Slightly forward
Ventral tank fuel .. .. Aft
Internal fuel .. .. Forward
95. Pressure error corrections
The following corrections (in knots) should be applied to
the A.S.I. readings to obtain R.A.S.
From To |
130 170 |
170 220 |
220 300 |
300 510 |
Subtract .. .. Add .. .. .. .. |
1 - |
0 0 |
- 2 |
- 4 |
96. Fuel consumptions
The following are the approximate fuel consumptions in
gallons/hour for various altitudes and power settings. The
figures quoted assume the use of AVTAG (7.7 lb./gall.);
if AVTUR is used, the figures are reduced by 4 per cent.66
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