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