T B M
PILOT’S INFORMATION MANUAL 700
SECTION 4
NORMAL PROCEDURES
D.G.A.C. Approved
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Page 4.4.48
Rev. 9
AMPLIFIED PROCEDURES
CLIMB (Cont’d)
3 – ECS panel
– Cabin altitude selector Cruise altitude + 1000 feet. . . . . . . . .
– Cabin rate selector ADJUST so as to obtain. . . . . . . . . . . . . .
a cabin climb rate
of about 500 ft/min
It concerns the control on triple indicator of cabin rate, as well as
increasing of differential pressure and cabin altitude.
– Pressurization CHECK. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
–”CABIN TEMP” selector ADJUST. . . . . . . . . . . . . . . . . . . . . . . . .
Anticipate setting to hot position during climb. Do not wait a fresh
sensation to perform this setting. Desired temperature will be as
longer to obtain as setting is made later.
4 – Fuel tank gages CHECK / CORRECT. . . . . . . . . . . . . . . . . . . . . . .
(Quantity / Symmetry)
In spite of fuel selector automatic operation, a non–negligible
dissymmetry may be observed at the end of climb, for example
when 10 minutes of climb have been performed on the same fuel
tank. Tolerated maximum dissymmetry is 25 us gal (95 Litres).
5 – DE ICE SYSTEM As required. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Refer to Chapter 4.5
”PARTICULAR PROCEDURES”
CAUTION
IF HEAVY PRECIPITATION, TURN IGNITION
AND INERT SEP ON
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