NOTE.-Throughout this publication the following con-
(a) Words in capital letters indicate the actual
markings on the controls concerned.
(b) The numbers quoted in brackets after items
in the text refer to the illustrations in Part
(c) Unless otherwise stated, all airspeeds and
Mach numbers quoted are "Indicated".
(d) Fuel poundage figures are all calculated at
7.7 lb./gallon (Normal AVTAG).
(a) The Hunter F.6 is a single-seat fighter aircraft powered
by a single Avon 203 axial-flow gas turbine engine. (See
(b) The aileron and elevator, which are fully powered, both
have manual reversion; a variable-incidence tailplane is
fitted. Provision is made for fitting an electric flying
tail. The cockpit is pressurized and fitted with a Mk. 2H
or Mk. 3H pilot ejection seat which is interconnected
with the hood jettison mechanism.