Piper ARCHER III - Oil; Maximum Weights; Standard Airplane Weights

SECTION 1
GENERAL PA-28-181, ARCHER III
SECTION 1
GENERAL PA-28-181, ARCHER III
REPORT: VB-1611 ISSUED: JULY 12, 1995
1-4
REPORT: VB-1611 ISSUED: JULY 12, 1995
1-4
1.9 OIL
(a) Oil Capacity (U.S. quarts) 8
(b) Oil Specification Refer to latest issue
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) 0°F to 70°F S.A.E. 30 S.A.E. 40 or
20W-30
(4) Below 10°F S.A.E. 20 S.A.E. 20W-30
1.11 MAXIMUM WEIGHTS
Normal Utility
(a) Maximum Ramp Weight (lbs.) 2558 2138
(b) Maximum Takeoff Weight (lbs.) 2550 2130
(c) Maximum Landing Weight (lbs.) 2550 2130
(d) Maximum Weights in Baggage
Compartment (lbs.) 200 0
1.13 STANDARD AIRPLANE WEIGHTS
Refer to Figure 6-5 for the Standard Empty Weight and the Useful Load.
1.9 OIL
(a) Oil Capacity (U.S. quarts) 8
(b) Oil Specification Refer to latest issue
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) 0°F to 70°F S.A.E. 30 S.A.E. 40 or
20W-30
(4) Below 10°F S.A.E. 20 S.A.E. 20W-30
1.11 MAXIMUM WEIGHTS
Normal Utility
(a) Maximum Ramp Weight (lbs.) 2558 2138
(b) Maximum Takeoff Weight (lbs.) 2550 2130
(c) Maximum Landing Weight (lbs.) 2550 2130
(d) Maximum Weights in Baggage
Compartment (lbs.) 200 0
1.13 STANDARD AIRPLANE WEIGHTS
Refer to Figure 6-5 for the Standard Empty Weight and the Useful Load.