Piper ARCHER II Pilot Operating Handbook page 25

SECTION 1 PIPER AIRCRAFT CORPORATION
of Lycoming Service
Instruction 1014.
(c) Oil Viscosity per Average Ambient
Temp. for Starting
Single Multi
(1} Above 60°F
S.A.E. 50
S.A.E. 40 or 50
(2) 30°F to 90°F
S.A.E. 40
S.A.E. 40
(3) O°F to 70°F
S.A.E. 30
S.A.E. 40 or
20 W-30
(4) Below 10°F
S.A.E. 20
§.A.E. 20W-30
1.11 MAXIMUM WEIGHTS
Normal Utility
(a) Maximum Ramp Weight (lbs.) 2558 2138
(b) Maximum Takeoff Weight (Ibs.)
2550
2130
(c) Maximum Landing Weight (Jbs.)
2550
2130
(d) Maximum Weights in Baggage
Compartment (lbs.)
200
0
1.13 STANDARD AIRPLANE WEIGHTS