SECTION 3
EMERGENCY PROCEDURES
D.G.A.C. Approved
T B M
700 PILOT’S INFORMATION MANUAL
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Page 3.9.5
Rev. 2
3.9 – ELECTRICAL SYSTEM
AMBER WARNING LIGHT ”LO VOLT” ON functioning
on ”ST–BY GENERATOR” (after ”MAIN GEN” failure) (Cont’d)
9 –”GENERATOR” selector OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
If conditions allow : VMC and non icing conditions
10 – Descend Altitude 3 12000 ft. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
11 –”ESS BUS TIE” reverse switch Cover up. . . . . . . . . . . . . . . . . . . .
EMER position
In this configuration, only both ”ESS BUS” bars and ”BUS BAT” bar
are directly supplied by the battery
Available ancillary systems – see Figure 3.9.1
12 – LAND as soon as possible
If necessary, it is always possible to use other ancillary systems by
selecting :
–”ESS BUS TIE” reverse switch NORMAL. . . . . . . . . . . . . . . . . .
If flight conditions do not allow :
13 – Manually disconnect all ancillary systems which are not essential
14 – LAND as soon as possible
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