Radar And Transponder - Beechcraft C-12C Operator And Technical Reference Manual

SENSOR
MODE
SENSOR
MODE
* Automatic navaid selection does not occur when operating the system in AUTO/LEG, VOR or TACAN,
RNV APR. The pilot must specify a reference navaid for each waypoint in the reference name field of each
waypoint page. This reference navaid is the particular navaid which the VOR navigation receiver and DME will
be turned to when this waypoint is activated.
q. Shutdown Procedure.
1. ON / OFF rocker switch – Press lower
half.
r. Emergency Procedures.
system information is intermittent or lost, secure the
system and utilize
navigation equipment as required.
3B-27. PILOT'S ALTIMETER.
a. Description.
servoed counter drum/pointer display of barometrically
corrected pressure altitude derived from the air data
system. Refer to Figure 3B-19.
Table 3B-4. Methods of Operation
OBS METHOD OF OPERATION
BLEND
RNV ENR
AUTO/LEG METHOD OF OPERATION
BLEND
RNV ENR
If the KNS-660
the remaining operational
Section IV. RADAR AND TRANSPONDER
The altimeter provides a
The barometric
VOR
RNV ENR RNV ENR
RNV APR RNV APR
NAV
VOR
RNV ENR RNV ENR
RNV APR* RNV APR*
1. FMS/NAV CTL switch – Press.
NAV CTL illuminated.
2. CDU ON / OFF switch – Off.
3. FMS circuit breaker – Pull.
pressure is set manually with the baro knob and
displayed in units of inches mercury and millibars on
baro counters. The altimeter is ac powered and is
protected through
placarded PILOT ALTM (AC) located on the overhead
circuit breaker panel, Figure 2-16, Sheet 3.
TM 1-1510-218-10
TACAN OMEGA
RNV ENR
NAV
TACAN OMEGA
RNV ENR
a 1-ampere circuit
Verify
breaker,
3B-55