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Piper PA-28-161 Maintenance Manual

Piper PA-28-161
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PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 1
Nov 30/06
3C9
30-30-00
PITOT AND ST
A
TIC
The pitot heat system (optional) is activated by the PITOT HEAT switch located on the center instrument
panel just above the engine power quadrant. In addition to the switch, the system incorporates a heated
pitot-static head and the 10 amp PITOT HEAT circuit breaker.
The pitot-static head is installed on the left wing.
NOTE: Refer to Chapter 91 for pitot heat wiring schematic.
Heated Pitot-Static System Installation (Optional)
Figure 1

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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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