Oil; Maximum Weights; Standard Airplane Weights; Baggage Space - Piper Archer III PA-28-181 Handbook

SECTION 1
GENERAL

1.11 OIL

(a) Oil Capacity (U.S. quarts)
(b) Oil Specification
(c) Oil Viscosity per Average Ambient
Temp. for Starting
(1) Above 60°F
(2) 30°F to 90°F
(3) 0°F to 70°F
(4) Below 10°F

1.13 MAxIMUM WEIGHTS

(a) Maximum Ramp Weight (lbs.)
(b) Maximum Takeoff Weight (lbs.)
(c) Maximum Landing Weight (lbs.)
(d) Maximum Weights in Baggage
Compartment (lbs.)

1.15 STANDARD AIRPLANE WEIGHTS

Refer to Figure 6-5 for the Standard Empty Weight and the Useful Load.

1.17 BAGGAGE SPACE

(a) Compartment Volume (cubic feet)
(b) Entry Width (inches)
(c) Entry Height (inches)

1.19 SPECIFIC LOADINGS

(a) Wing Loading (lbs. per sq. ft.)
(b) Power Loading (lbs. per hp)
REPORT: VB-2749
1-6
PA-28-181, ARCHER III
Refer to latest issue
of Lycoming Service
Instruction 1014.
Single
S.A.E. 50 S.A.E. 40 or 50
S.A.E. 40
S.A.E. 30
S.A.E. 20 S.A.E. 20W-30
Normal
2558
2550
2550
200
ISSUED: December 22, 2017
8
Multi
S.A.E. 40
S.A.E. 40 or
20W-30
Utility
2138
2130
2130
0
24
22
20
15.0
14.2