When the smaller in cre ment/dec re ment knob is pushed in, de press -
ing the NAV TRANS FER but ton will in ter change the USE and
STBY/RAD fre quen cies. The NAV IDENT knob is ac tive in the
pulled out po si tion so that both voice and ident can be heard.
When this knob is pushed in, the ident tone is at ten u ated. The vol -
ume of voice/ident can be ad justed by turn ing this knob.
Note: If dual Nav’s are in stalled a plac ard will be lo -
cated on the re ceiver and on the cor re spond ing NAV in -
di ca tor to cor re late the NAV re ceiver with the
ap pro pri ate NAV in di ca tor.
Am plified op er a tion in struc tions are pro vided in Bendix-King Pub -
li ca tion No. 006-8329-03.
KX 155 NAV/COMM Transceiver [TSO’d]
KX 165 NAV/COMM Transceiver [TSO’d]
SCHWEIZER MODEL 269C-1 HELICOPTER
CSP-C1-1A
FAA Approved: 03 Oct 1995
13
Revised: 17 Apr 1996
