Piper Malibu PA-46-310P Pilot Operating Handbook page 232

1~372B
~A-46-310P
s/n 46-8408083
All items installed according to King installation maunal
and
Piper
installation drawing #84384. The antenna was belly
mounted
aft of the
entrance door with
the
transceiver nearby while the indicator was mounted
in the top aft comer of the instrument panel. FAA
"AC.
43.13-lA, chapter
15 and 43.13-2A, chapter 1,2, and 3 also cited.
3. Installed Wulfsberg Flitefone System into the aircraft consisting of
the
follCMi.ng:
WH-5-102 Cabin Control Unit
AT-461
Antenna
RI'-18B Transceiver
Mr-28A Mount
p/n 400-0116-007
p/n 121-0011-000
p/n 400-0115-000
p/n 300-2202-000
Transceiver mounted on lower rear avionics shelf.
Antenna
mounted on
aircraft belly aft of
the
wing spar. Cabin control m:>unted on cabinet
between righthand crew
and
cabin seats. Installation ccil'plies with
Wulfsberg installation manual 150-0114-000
and
FAA AC 43.13-lA
and
2A.
4. Installed Ryan/3M WX-11 Stonnscope System into the aircraft consisting of
the following:
WX-11 Processor
Control Display Unit
Mounting Tray
Antenna
p/n 78-8047-0958-8
p/n 78-8047-0966-1
p/n 78-8041-7628-3
p/n 78-8041-7950-1
The
coo
was mounted in the lower lefthand side of the instrument panel.
The
processor
was mounted
on the
upper
rear avionics shelf. The
antenna
was
belly
nounted
aft of the entrance door. Installation caaplies with
· Ryan/31VrinSta.LLa:tiorrmanuar~a~ao41.;;.;921--2-anct
FAA "AC-11·3'
.-1~ana···
2A;-----~..c- - ---- -~-;
5. Installed King Radio Corporation KAS-297B Vertical
Speed and
Altitude
Selector/Yaw Damper System into the aircraft approved under FAA STC
SAl
778CE-D. Crnq;>onents consist of
the
following:
KC-296 Yaw Coupler
I<M-275 Servo Mount
KS-271A Tr.im
Servo
KAS-297B Altitude Selector
KRG-331 Rate Gyro
p/n 065-0036-01
p/n 085-0030-00
p/n 055-0060-04
p/n 065-0065-00
p/n 060-0024-00
Altitude selector
mounted
in lefthand side of the instrument panel.
Servo mounted in aft carpartment. Yaw coupler
and
rate gyro mounted on
bottan of upper rear avionics shelf. Installation done according to
Piper drawing 84397-7, King installation manual 006-0287-00
and
FAA 43 .13-lA
and
2A.