1.9 OIL
(a) Oil Capacity (U.S. qts.)
6
(b) Oil specification
Refer to latest issue
of Lycoming Service
Instruction 1014.
(c) Oil Viscosity
Refer to Section 8 -
paragraph 8.19.
1.11 MAXIMUM WEIGHTS
Normal
Utility
(a) Maximum Takeoff Weight (lbs.)
1670
1670
(b) Maximum Landing Weight (lbs.)
1670
1670
(c) Maximum Weight (lbs.) in Baggage
Compartment at Fuselage Station
115.0
100
100
1.13 STANDARD AIRPLANE WEIGHTS*
(a) Standard Empty Weight (lbs.):
Weight of a standard airplane includ-
ing unusable fuel, full operating
fluids and full oil.
1128
(b) Maximum Useful Load (lbs.): The
difference between the Maximum
Takeoff Weight and the Standard
Empty Weight.
542
1.15 BAGGAGE SPACE
(a) Compartment Volume (cu. ft.)
20
(b) Floor Loading (lbs. per sq. ft.)
25
* These values are approximate and vary from one aircraft to another. Refer
to Figure 6-7 for the Standard Empty Weight value and the Useful Load
value to be used for C.G. calculations for the aircraft specified.
SECTION 1
PIPER AIRCRAFT CORPORATION
GENERAL
PA-38-112, TOMAHAWK
REPORT: 2126
ISSUED: JANUARY 20, 1978
1-4
REVISED: JANUARY 15, 1981
1.9 OIL
(a) Oil Capacity (U.S. qts.)
6
(b) Oil specification
Refer to latest issue
of Lycoming Service
Instruction 1014.
(c) Oil Viscosity
Refer to Section 8 -
paragraph 8.19.
1.11 MAXIMUM WEIGHTS
Normal
Utility
(a) Maximum Takeoff Weight (lbs.)
1670
1670
(b) Maximum Landing Weight (lbs.)
1670
1670
(c) Maximum Weight (lbs.) in Baggage
Compartment at Fuselage Station
115.0
100
100
1.13 STANDARD AIRPLANE WEIGHTS*
(a) Standard Empty Weight (lbs.):
Weight of a standard airplane includ-
ing unusable fuel, full operating
fluids and full oil.
1128
(b) Maximum Useful Load (lbs.): The
difference between the Maximum
Takeoff Weight and the Standard
Empty Weight.
542
1.15 BAGGAGE SPACE
(a) Compartment Volume (cu. ft.)
20
(b) Floor Loading (lbs. per sq. ft.)
25
* These values are approximate and vary from one aircraft to another. Refer
to Figure 6-7 for the Standard Empty Weight value and the Useful Load
value to be used for C.G. calculations for the aircraft specified.
SECTION 1
PIPER AIRCRAFT CORPORATION
GENERAL
PA-38-112, TOMAHAWK
REPORT: 2126
ISSUED: JANUARY 20, 1978
1-4
REVISED: JANUARY 15, 1981