Piper PA-28-161 User Manual

SECTION2
UMITATIONS
PIPERAIRCRAFf CORPORATION
PA-28-161, WARRIOR
ll
2.9 POWER PLANT INSTRUMENT MARKINGS (Continued)
(c) Oil Pressure
Green Arc (Nonnal Operating Range)
Yellow Arc (Caution Range) (Idle)
Yellow Arc (Ground Warm-Up)
Red Line (Minimum)
Red Line (Maximum)
(d) Fuel Pressure
Green Arc (Normal Operating Range)
Red Line (Minimum)
Red Line (Maximum)
2.11 WEIGHT LIMITS
(a) Maximum Weight
(b) Maximum Ramp Weight
(c) Maximum Baggage
NOTE
Normal
2440LBS
2447LBS
200LBS
Refer to Section 5 (Performance) for maximum
weight as limited by performance.
60 to90PSI
25 to 60PSI
90 to lOOPSI
25PSI
100 PSI
.5 to 8 PSI
.5PSI
8PSI
Utility
2020LBS
2027 LBS
OLBS
I
REPORT: VB-1180
2-3a
ISSUED: SEPTEMBER 12, 1990

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)