Oil; Maximum Weights; Standard Airplane Weight; Baggage Space - Piper WARRIOR III PA-28-161 Pilot Operating Handbook

SECTION 1
GENERAL
1.9

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

1.11 MAXIMUM WEIGHTS

(a) Maximum Takeoff Weight (lbs)
(b) Maximum Ramp Weight (lbs)
(c) Maximum Landing Weight (lbs)
(d) Maximum Weight in Baggage
Compartment (lbs)
1.13 STANDARD AIRPLANE WEIGHTS
Refer to Figure 6-5 for the Standard Empty Weight and the Useful
Load.

1.15 BAGGAGE SPACE

(a) Compartment Volume (cubic feet

1.17 SPECIFIC LOADINGS

(a) Wing Loading (lbs per sq ft)
(b) Power Loading (lbs per hp)
REPORT: VB-1565
1-4
PIPER AIRCRAFT CORPORATION
PA-28-161, WARRIOR III
Single
S.A.E. 50
S.A.E. 40
S.A.E. 30
S.A.E. 20
Normal
2440
2447
2440
200
ISSUED: JULY 1, 1994
Refer to latest issue
of Lycoming Service
Instruction 1014.
Multi
S.A.E. 40 or 50
S.A.E. 40
S.A.E. 40 or
20W-30
S.A.E. 20W-30
Utility
2020
2027
2020
14.4
15.3
8
0
24