Piper PA-28-161 Pilot Operating Handbook page 219

SECTION 9
SUPPLEMENT 6
Figure 7-7 (cont)
PIPER AIRCRAFT CORPORATION
PA-28-161, WARRIOR II
13. COURSE DEVIATION SCALE- A course deviation bar displace-
ment of 5 dots represents full scale ( VOR
=
± 10°, LOC = ±2 I
I
2°,
RNAV
=
5NM, RNAV APR- I I/4NM) deviation from beam
centerline.
14. HEADING BUG - Moved by (
Q )
knob
(9)
to select desired
heading.
KG 107 NON-SLAVED DIRECTIONAL GYRO
Figure 7-9
5
REPORT: VB-1180
ISSUED: AUGUST 13, 1982
9-42, 16 of
20