PART 1II-HANDLING
L.P. booster pump circuit breakers may cancel in flight;
should this happen, they should be pressed in again.
Electrical failure should not be assumed unless the button
will not stay in.
48. Engine handling
(a) Starting
Either engine may be started first but the order in which
the engines are started should be alternated on each sortie
in order to check the functioning of the vacuum pumps.
(b) Take-off and climb
With the throttles fully open, r.p.m. at take-off are governed
at 14,550. During the climb, r.p.m. will gradually increase
to 14,700. A close watch should be kept on the j.p.t.,
which must not be allowed to exceed 680°C. (700°C. above
20,000 feet for 10 minutes). If climbing at less than full
power, it will be necessary to reduce the throttle setting to
maintain the selected r.p.m. If surging occurs-recognised
by a muffled detonation in the engine-the r.p.m. should
be reduced until it ceases.
(c) General
(i) There is little or no risk of flame extinction at altitude,
providing throttle movements are made smoothly and
not too rapidly. Coarse opening of the throttles will,
however, cause surging and excessive j.p.t.
(ii) The throttles may be closed fully at any altitude.
During descent, the throttles will have to be opened
progressively to maintain a selected r.p.m.
(iii) False indication of oil pressure failure may be given
whilst at height. A descent to a lower altitude should
return the oil pressure indication to normal.
(iv) After periods at height, the H.P. cock may freeze in
the on position. It will free during the descent.
STARTING, TAXYING AND TAKE-OFF
49. External checks
(a) Before starting the external checks, look inside the front
cockpit and ensure that the undercarriage selector lever is
oxygen. Ensure also that the control locks are removed. 35
|