Cessna 150 COMMUTER 1976 Pilot Operating Handbook page 84

CESSNA 300 NA V /COM
(TYPE RT-528E-1)
PILOT!S OPERATING HANDBOOK
SUPPLEMENT
SECTION 2
LIMITATIONS
There is no change to the airplane limitations when this avionic
equipment is installed. However, the pilot should be aware that on
many Cessna airplanes equipped with the windshield mounted glide slope
antenna, pilots should avoid use of 2700 ±100 RPM (or 1800 ±100 RPM
with a three bladed propeller) during ILS approaches to avoid propeller
interference caused oscillations of the glide slope deviation pointer.
SECTION 3
EMERGENC Y P ROCED U RES
There is no change to the airplane emergency procedures when this
avionic equipment is installed.
SECT I ON 4
N ORMAL P RO CEDU RES
TO TRANSMIT :
(1) XMTR SEL Switch -- SELE CT tra nsceiver .
(2 ) COM Frequency Selector Knobs - - SE LECT operating fr equency.
(3) OFF/VOL Control -- ON.
(4) Mike
Button -- DEPRESS .
T O RECEIVE :
(1) XMTR SEL Switch -- SELE CT transceiver.
(2) SPEAKER/ PHONE Switch -- SELECT de s ir ed mode.
(3) COM/NAY F requency Se lector Knobs -- SELEC T freque ncy.
(4) VOL Control -- Adjust to listening l evel (OFF /VOL knob must
be ON).
(5) SQ Control -- ROTATE counterclockwise
t o decrease background
noise.
TO OPERATE IDENT FILTER:
4
(1 ) ID-T Switch -- CENTER (unmarked) to include filter in audio
circuit of both receivers.
PILOT'S OPERATING HANDBOOK
SUPPLEMENT
CESSNA 300 NAV/ M
(T YPE RT-528 ' - 1)
(2) ID-T Switch -- ID position disconnects filter from a.udio circuit
to hear navigation station identifier (Morse Code) Signal.
NOTE
The ID-T switch should be left in ID position for best
communications reception.
TO SELF TEST VOR NAVIGATION CIRCUITS:
(1) Tune to usable VOR signal from either a VOR station or a test
signal.
(2) OBS Knob -- ROTATE course index to 0°
(3) ID-T Switch -- T position. Vertical pointer should center and
OFF-TO-FROM indicator should show FROM.
(4) ID-T Switch -- T position and rotate OBS knob to displace course
index approximately 10° to either side of 0°. Vertical pointer should
deflect full scale in direction corresponding to course index displace-
ment.
(5) ID-T Switch -- CENTER (unmarked) position for normal VOR
operation.
NOTE
This test does not fulfill the requirements of FAR 91. 25.
SECTION 5
PERFORMANCE
There is no change to the airplane performance when this avionic
equipment is installed.
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