Piper PA-28-161 User Manual

SECTION 2
LIMITATIONS
PIPER AIRCRAFT CORPORATION
PA-28-161, WARRIOR II
(c) Day IFR
( 1) All equipment required for Day VFR
(2) Vacuum pump
(3) Gyro suction indicator
(d) Night IFR
( 1) All equipment required for Day and Night VFR
(2) All equipment required for Day IFR
NOTE
The above system and equipment list does not
include specific flight instruments and commu-
. nication/ navigation equipment required by the
FAR Part 91 and 135 operating requirements.
2.21 FUEL LIMITATIONS
(a) Total Capacity
(b) Unusable Fuel
The unusable fuel for this airplane has
been determined as 1.0 gallon in each
wing in critical flight attitude-:.
(c) Usable Fuel
The usable fuel in this airplane has been
determined as 24.0 gallons in each wing.
2.23 NOISE LEVEL
The noise level of this aircraft is 72.9 dB(A).
50 U.S. GAL
2 U.S. GAL
48 U.S. GAL
No determination has been made by the Federal Aviation Admini~
tration that the noise levels of this airplane are or should be acceptable or
unacceptable for operation at. into, or out of, any airport.
The above statement notwithstanding, the noise level stated above has
been verified by and approved by th.: federal Aviatiuu Aomini~tration in
noise level test flights conducted in accordance with FAR 36. :\ oise
Standards - Aircraft Type and Airworthiness Certification. This aircraft
model is in compliance with all FAR 36 noise standards applicable to thi~
type.
REPORT: VB-1180
2-6
ISSUED: AUGUST 13, 1982
REVISED: JUNE 28, 1984

Piper PA-28-161 Specifications

General

Manufacturer	Piper Aircraft
Model	PA-28-161 Warrior II
Engine	Lycoming O-320-D3G
Horsepower	160 hp
Seating Capacity	4
Wingspan	35 ft (10.7 m)
Length	24 ft 0 in
Maximum Speed	127 knots
Cruise Speed	122 knots
Maximum Takeoff Weight	2, 325 lb (1, 055 kg)
Fuel Capacity	48 US gallons (182 L)