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Piper PA-28-161 User Manual

Piper PA-28-161
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SECTION 9
SUPPLEMENT 3
SECTION 1 - GENERAL
PIPER AIRCRAFT CORPORATION
PA-28-161, WARRIOR
II
This supplement supplies information necessary for the operation
of
the
airplane
when the optional Piper control wheel clock
is
installed. The infor-
mation
contained within this supplement
is
to be used
in
conjunction with
the
complete handbook.
SECTION
2-
LIMITATIONS
No
change.
SECTION 3 - EMERGENCY PROCEDURES
No
change.
SECTION 4 - NORMAL PROCEDURES
(a) SETTING
While in the CLOCK mode, the time and the date can
be
set by the
operation
of
the
RST
button.
(b)
DATE
SETTING
Pressing
the
RST
button
once
will
cause the date to appear with the
month flashing.
Pressing the ST
-SP
button
will advance the month
at
one per second,
or
at
one per push, until the right month appears.
Pressing the
RST
button
once again will cause the date to flash,
and it can be set in a similiar manner.
(c)
TIME
SETTiNG
The
RST
button
must now
be
pressed two times to cause the
hour.s
digits to flash. The correct hour can
be
set in as described ab'ove.
REPORT:
VB-1180
ISSUED: AUGUST 13,
1982
9-12, 2
of
4

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Piper PA-28-161 Specifications

General IconGeneral
ManufacturerPiper Aircraft
ModelPA-28-161 Warrior II
EngineLycoming O-320-D3G
Horsepower160 hp
Seating Capacity4
Wingspan35 ft (10.7 m)
Length24 ft 0 in
Maximum Speed127 knots
Cruise Speed122 knots
Maximum Takeoff Weight2, 325 lb (1, 055 kg)
Fuel Capacity48 US gallons (182 L)

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