PART III - HANDLING
and the test switch is at NORMAL FLIGHT (see
para. 18(f) (iv)). Check that the hood locking
pointers are in line with their spigots.
(ii) Strap in, adjust the rudder pedals and then make
the main and emergency oxygen and anti-G suit
connections, have the radio plug connected and both
of the seat safety pins removed and stowed.
(b) Cockpit checks
NOTE.-The starred items are directly connected with
engine starting.
*Battery master switch ON-ensure that turn and
(68) slip indicator starts up.
Undercarriage emergency Pressure 2,000 lb./sq. in.
air pressure gauge (6)
Flaps emergency air pre- Pressure 2,000 lb./sq. in.
sure gauge (7)
Wheel brakes accumu- Min. pressure 750 lb./sq. in.
lator air pressure gauge
(9)
Tailplane actuator (4) In
and hood motor (5)
circuit breakers
Radar test switch (8) Switch to TEST. Check
aurally that the main in-
verter starts up, Art Hor.
flag-black, and the oil
pressure needle moves off
its stop to zero. Reset
switch to NORMAL, and
the battery master switch
OFF then ON.
Cockpit pressure warning Switch to TEST-cockpit
test switch (10) pressure warning light
comes on reset switch to
NORMAL.
Flood air flow switch (11) AUTO
Cockpit pressurization ON
switch (3)
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