Piper TOMAHAWK User Manual

2.21 FUEL LIMITATIONS
(a) Total Capacity 32 U.S. GAL.
(b) Unusable fuel 2 U.S. GAL .
The unusable fuel for this airplane has
been determined as 1.0 gallon in each
wing in critical flight attitudes.
(c) Usable Fuel 30 U.S. GAL.
The usable fuel in this airplane has
been determined as 15.0 gallons in each
wing.
(d) Fuel remaining when a quantity indi-
cator reads zero cannot be used safely
in flight.
2.23 NOISE LEVEL
The noise level of this aircraft is 67.8d B(A).
No determination has been made by the Federal Aviation
Administration that the noise levels of this airplane are or should be
acceptable or unacceptable for operation at, into, or out of any airport.
The above statement notwithstanding, the noise level stated above has
been verified by and approved by the Federal Aviation Administration in
noise level test flights conducted in accordance with FAR 36, Noise
Standards - Aircraft Type and Airworthiness Certification. This aircraft
model is in compliance with all FAR 36 noise standards applicable to this
type.
PIPER AIRCRAFT CORPORATION SECTION 2
PA-38-112, TOMAHAWK LIMITATIONS
ISSUED: JANUARY 20, 1978 REPORT: 2126
REVISED: OCTOBER 29, 1982 2-7
2.21 FUEL LIMITATIONS
(a) Total Capacity 32 U.S. GAL.
(b) Unusable fuel 2 U.S. GAL .
The unusable fuel for this airplane has
been determined as 1.0 gallon in each
wing in critical flight attitudes.
(c) Usable Fuel 30 U.S. GAL.
The usable fuel in this airplane has
been determined as 15.0 gallons in each
wing.
(d) Fuel remaining when a quantity indi-
cator reads zero cannot be used safely
in flight.
2.23 NOISE LEVEL
The noise level of this aircraft is 67.8d B(A).
No determination has been made by the Federal Aviation
Administration that the noise levels of this airplane are or should be
acceptable or unacceptable for operation at, into, or out of any airport.
The above statement notwithstanding, the noise level stated above has
been verified by and approved by the Federal Aviation Administration in
noise level test flights conducted in accordance with FAR 36, Noise
Standards - Aircraft Type and Airworthiness Certification. This aircraft
model is in compliance with all FAR 36 noise standards applicable to this
type.
PIPER AIRCRAFT CORPORATION SECTION 2
PA-38-112, TOMAHAWK LIMITATIONS
ISSUED: JANUARY 20, 1978 REPORT: 2126
REVISED: OCTOBER 29, 1982 2-7

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