PIPER AIRCRAFT CORPORATION
PA-28-161, WARRIOR
II
2.17 FLIGHT LOAD FACTORS
(a) Positive Load
Factor
(Maximum)
(b) Negative Load
Factor
(Maximum)
SECTION 2
LIMITATIONS
Normal
3.8 G
Utility
4.4 G
No
inverted maneuvers
approved
2.19 KINDS
OF
OPERATION EQUIPMENT
LIST
This airplane may be operated in
day
or
night
VFR,
day
or
night
IFR
when
the
appropriate equipment
is
installed
and
operable.
The
following equipment list identifies the systems
and
equipment
upon
which type certification for each kind
of
operation was predicated
and
must
be installed
and
operable for the particular kind
of
operation indicated.
However, certain operations may be authorized with certain listed equip-
ment
and/
or
systems inoperative under certain conditions
and
under
provisions defined by a
current
Minimum Equipment List (MEL) approved
by the
FAA
which
is
dated concurrently with
or
after this Pilot's Operating
Handbook
and
FAA
Approved Airplane Flight Manual
and
authorized
under
an
operating regulation which provides for use
of
an
MEL.
(a) Day
VFR
(l)
Airspeed indicator
(2) Altimeter
(3) Magnetic compass
(4)
Tachometer
(5) Oil pressure indicator
(6)
Oil temperature indicator
(7) Fuel pressure indicator
(8) Fuel quantity indicator - each
tank
(9) Volt-ammeter
(10) Elevator/
rudder
trim indicator
(11) Alternator
( 12)
Safety restraint - each occupant
(b) Night
VFR
(I)
All equipment required for Day
VFR
(2) Position lights
(3) Instrument lights
(4) Anti-collision (strobe) lights
ISSUED:
AUGUST
13,
1982
REPORT:
VB-1180
2-5
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