Piper PA-28-161 Maintenance Manual

PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 7
Nov 30/06
1E7
5-50-00
5. Flood Damage, Immersion in
W
ater (continued)
Item Inspection Inspection Interval
 Vacuum and Pitot-Static Replace gyros. If immersed, each event,
Systems. before further flight.
Replace filters.
Clean and inspect all lines, and pitot
and static vents.
Clean and check all regulating valves.
Remove and inspect engine driven and
auxiliary vacuum pumps.
 Induction System. Clean and inspect for silt and If immersed, each event,
corrosion. Check all ducts and gaskets. before further flight.
Replace as necessary.
Clean and inspect all heat shrouds
and ducting.
 Fuel System. Perform Fuel Tank/Wing Spar Corrosion If immersed, each event,
Inspection, 28-10-00. Remove and clean before further flight.
fuel cells and fuel cells wing area. Clean
all associated lines and pumps.
Clean and inspect all fuel tank vents,
cap vents and vent lines.
 Instruments. Clean and inspect instruments. Bench If immersed, each event,
check per appropriate maintenance before further flight.
manual.
 Heating and Ventilating Replace blower, if installed. If immersed, each event,
Systems. before further flight.
Clean and inspect all distribution boxes,
ducting and valves.
Inspect and check system control cables.
Replace corroded or binding cables.
If installed, clean and inspect air
conditioning evaporator, condenser,
and compressor.

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)