Piper TOMAHAWK User Manual

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

Piper TOMAHAWK Specifications

General

Manufacturer	Piper Aircraft
Model	PA-38 Tomahawk
Role	Trainer aircraft
First flight	1977
Number built	2, 484
Engine type	Lycoming O-235-L2C
Horsepower	112 hp (84 kW)
Max takeoff weight	1, 670 lb (757 kg)
Wingspan	34 ft 0 in (10.36 m)
Height	9 ft 0 in
Range	500 miles
Rate of Climb	720 ft/min