2-4-8
Starter
The engine starting cycle shall be limited to the following intervals:
−
Sequence, 60 seconds OFF
−
Sequence, 60 seconds OFF
−
Sequence, 30 minutes OFF.
Note
A dry motoring cycle is to be counted as a sequence. In case of start abort and automatic
dry motoring commanded by EPECS, wait for an additional 10 minutes before a new start
is attempted.
2-4-9
Generator
Maximum generator load limits are given in
Table 2-4-4: Maximum Generator Load Limit
GENERATOR
MAX CONTINUOUS LOAD
MAX LOAD FOR 2 MINUTES *
Generator 1
300 AMP
450 AMP
Starter/Generator 2
300 AMP
450 AMP
*Maximum load permitted for a 2 minute period per each one hour of operation.
2-4-10
Power Control Lever Operation
Power Control Lever operation aft of the idle detent is prohibited during flight. Such operation
may lead to loss of airplane control and total power loss.
2-4-11
Chip Detector
Takeoff is not approved with ENGINE CHIP caution annunciator illuminated.
2-4-12
Feather Inhibit (optional)
After nine consecutive engine shutdowns using the propeller feather inhibit function, the next
engine shutdown must be a normal shutdown.
Section 2 - Limitations (EASA Approved)
Starter
Pilot's Operating Handbook
Report No: 02406
Issue date: Dec 18, 2020
Page 2-4-6
12-C-A15-10-0204-00A-043A-A
FOR
GENERAL
AND
FAMILIARIZATION
PURPOSES
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