Name: Piper PA-38-112
Brand: Piper
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1.9 OIL

(a) Oil Capacity (U.S. qts.) 6

(b) Oil specification Refer to latest issue

of Lycoming Service

Instruction 1014.

paragraph 8.19.

1.11 MAXIMUM WEIGHTS

Normal Utility

(a) Maximum Takeoff Weight (lbs.) 1670 1670

(b) Maximum Landing Weight (lbs.) 1670 1670

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