PART III-MANAGEMENT OF SYSTEMS
low B.P.C. pressure and low forward speed leading
to reduced fuel flow at the burners. Goblin Mod.
1130 increases both the B.P.C. pressure setting and
minimum fuel flow. Until the Mod. is embodied
it is recommended that, to reduce the possibility of
flame-out engine r.p.m. in stall manoeuvres should
not be less than the following:-
20,000 ft. .. .. 5,500 r.p.m.
30,000 ft. .. .. 7,500 r.p.m.
35,000 ft. .. .. 8,500 r.p.m.
(iii) During sustained turns at all altitudes there may be
a tendency for engine r.p.m. to fall off slightly, up
to a maximum of 1,000 r.p.m. The original r.p.m.
will be regained when straight and level flight is
resumed.
(b) H.P. pump isolating check
(i) Increase engine r.p.m. to 4,000 and set the isolating
switch ON. This should result in an increase of
about 1,000 r.p.m., pre-mod. 1130, or of about 800-
900 r.p.m. post-mod. 1130. Should the desired
increase not be achieved the system is unserviceable
and the aircraft must not be flown.
(ii) After the check return the switch to off and note
that the r.p.m. drop to the original figure.
(c) Use of the H.P. pump isolating switch for take-off
If the isolating switch has been set to ON for. take-off
it must be returned to off at a safe height whilst still at
full throttle. This should cause little or no drop in
r.p.m.; the engine can then be throttled to the desired
power. If the isolating switch is switched to off after
power has been reduced a sudden drop of approximately
1,000 r.p.m. will result.
(d) Use of the H.P. pump isolating switch in flight
If a sudden inexplicable drop in engine r.p.m. occurs the
throttle should be closed and the isolating switch set to
ON. (If the isolating switch is not switched to ON
within 4 seconds there is a probability of flame extinc-
tion). Once the switch has been set to isolate it must
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