Piper PA-28-161 Maintenance Manual

COMPONENT LUBRICANT FREQUENCY
1. OLEO STRUT FILLER POINT MIL-H-5606G AS REQUIRED
(See Spec. Instr. 4 and Note 1)
2. STEERING BELLCRANK PIVOT POINT MIL-L-7870 100 HOURS
(See Spec. Instr. 2)
3. SHIMMY DAMPENER PIVOT POINT (See Spec. Instr. 2) MIL-L-7870 100 HOURS
4. TORQUE LINK ASSEMBLY (See Spec. Instr. 2) MIL-L-7870 100 HOURS
5. NOSE WHEEL BEARING MIL-G-81322E
(See Spec. Instr. 3) 100 HOURS
6. NOSE GEAR STEERING ROD END BEARINGS MIL-L-7870 100 HOURS
(See Spec. Instr. 2)
7. EXPOSED OLEO STRUT CARBON DIOXIDE RELEASE
(See Spec. Instr. 6) AGENT DRY LUBRICANT
MS-122N/CO
2
100 HOURS
PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 11
Nov 30/06
1I17
12-20-00
Lubrication Chart - Landing Gear, Nose
Figure 5

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)