26 in. Hg. (65 Cm.Hg.)
Note:- Care must be taken to see that the tail does not lift when 1800
r.p.m. is exceeded, and it is advisable to have somebody holding this down
whilst running up.
(viii) Reset propeller switch to "automatic" position and check C.P.
controls.
TAXIING
6. Owing to the steerable tail wheel, brakes are not necessary in normal
circumstances. The view ahead is average and the machine is readily
controllable.
If the engine is kept ticking over for any period of time, it should be
cleared by being run up against the brakes prior to take-off.
ACTIONS PRIOR TO TAKE-OFF
7. Prior to actual take-off, check the following points by means of some
suitable reminder, such as "T" - "M" - "P" "FLAPS" - "RADIATOR"
(i) "T" - trimming tab controls for rudder and elevator should both be in
neutral as shown by the marks on the indicators.
(ii) "M" - mixture control should be at full rich.
Note:- It should be at auto-rich if aeroplane is above 3500 feet.
(iii) "P" - constant speed control should be set to give 3000 revs, and
check that toggle switch is in the UP (automatic) position.
(iv) "FLAPS" - may be used up to 20° for take-off if required, although
the advantage of so doing is very small. See paragraph 1 (iii).
(v) "RADIATOR" - position for this will be dependent on the outside air
temperature.
TAKE-OFF
8. The aircraft is very easy to take-off and shows scarcely any
inclination to swing, although a little right rudder may be needed. As the
Allison engine has a particularly quick pick-up, the opening of the
throttle must be done slowly and care must be taken to ensure that the
specified maximum manifold pressure of 41 in. Hg (104 Cm.Hg. on French
instruments) is not exceeded. See para. 27 for full engine take-off
limitations.
ACTIONS AFTER TAKE-OFF
9. (i) Once clear of the ground, raise the undercarriage and tail wheel by
pressing the release knob on the end of the undercarriage selector lever,
bringing the lever up to the undercarriage "UP" position, and pressing the
thumb operating switch on the top of the control column. [DF: Erik says
that on the AVG Tomahawks the button on top of the stick was replaced by a
toggle below the pistol grip.] This operation is rather slow and whilst
the undercarriage is going up -
(ii) reduce the boost pressure to 35 in. Hg. and reduce revs to 2600, and
(iii) maintain a flying speed of approximately 140 m.p.h.
(iv) When the indicator shows that the undercarriage and tail wheel are
finally up, check that they are locked into position by operating the
emergency hand pump, and if it is solid then the undercarriage and tail
wheel are full retracted. Return undercarriage selector lever to neutral
position, and
(v) If lowered, raise the flaps by selecting the "Up" position on the flap
selector lever, and press the thumb operating switch on the control
Summary of Contents for P-40 Tomahawk
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