Pilot's Operating Handbook
Section 7
Description
Edition 0 - March 05, 2019
Rev. 0
Page 7.6.9
MAN OVRD control
- see figure 7.6.2
MAN OVRD control (3) is normally notched in full backward position. In case of FCU or
THROTTLE failure, it allows setting engine power manually.
To quit full backward position (notched), move the MAN OVRD control forward
overriding the indexation.
●
NOTE
●
The power available if the THROTTLE fails will be limited by the position of the
lever.
●
Autothrottle is disconnected when the MAN OVRD lever is used.
Lever friction
- see figure 7.6.2
A thumbwheel located on right side of pedestal console allows the clamping of the
THROTTLE lever and MAN OVRD lever to prevent slipping of the controls once set.
Engine instruments
Engine indicating consists of :
-
engine torque expressed in percent (%), TRQ
-
propeller speed in RPM, PROP RPM
-
generator rotation speed expressed in percent (%), Ng
-
ITT expressed in °C,
-
oil pressure expressed in PSI.
-
oil temperature expressed in °C.
●
NOTE
●
Engine monitoring is ensured by
ITT
,
NG
,
ITT HI
,
NG HI
and
OIL PRESS
. Refer to the GARMIN Pilot's Guide for further details.
●
PIM - DO NOT USE FOR FLIGHT OPERATIONS