Piper TOMAHAWK User Manual

In full view of the pilot:
TAKEOFF CHECK LIST
Fuel - Proper Tank Belts/harness - Fastened
Mixture - Set Flaps - Set
Electric Fuel Pump - On Trim - Set
Carburetor Heat - Off Controls - Free
Engine Gages - Checked Doors - Latched
Seats & Backs - Latched
LANDING CHECK LIST
Fuel - Proper Tank Seats & Backs - Latched
Mixture - Rich Flaps - Set (White Arc)
Electric Fuel Pump - On Belts/Harness - Fastened
On baggage compartment aft bulkhead:
BAGGAGE
MAX. 100 LBS
SEE PILOTS OPERATING HANDBOOK
FOR LOAD DISTRIBUTION
In full view of the pilot, near the airspeed indicator:
MANEUVERING SPEED 103 KIAS
AT 1670 LBS (SEE P.O.H.)
In full view of the pilot, on the throttle quadrant:
FUEL REMAINING WHEN THE QUANTITY
INDICATORS READ ZERO CANNOT BE USED
SAFELY IN FLIGHT
15 U. S. GAL. FUEL 15 U. S. GAL.
USABLE USABLE
LR
TANK TANK
PIPER AIRCRAFT CORPORATION SECTION 2
PA-38-112, TOMAHAWK LIMITATIONS
ISSUED: JANUARY 20, 1978 REPORT: 2126
REVISED: JANUARY 15, 1981 2-9
In full view of the pilot:
TAKEOFF CHECK LIST
Fuel - Proper Tank Belts/harness - Fastened
Mixture - Set Flaps - Set
Electric Fuel Pump - On Trim - Set
Carburetor Heat - Off Controls - Free
Engine Gages - Checked Doors - Latched
Seats & Backs - Latched
LANDING CHECK LIST
Fuel - Proper Tank Seats & Backs - Latched
Mixture - Rich Flaps - Set (White Arc)
Electric Fuel Pump - On Belts/Harness - Fastened
On baggage compartment aft bulkhead:
BAGGAGE
MAX. 100 LBS
SEE PILOTS OPERATING HANDBOOK
FOR LOAD DISTRIBUTION
In full view of the pilot, near the airspeed indicator:
MANEUVERING SPEED 103 KIAS
AT 1670 LBS (SEE P.O.H.)
In full view of the pilot, on the throttle quadrant:
FUEL REMAINING WHEN THE QUANTITY
INDICATORS READ ZERO CANNOT BE USED
SAFELY IN FLIGHT
15 U. S. GAL. FUEL 15 U. S. GAL.
USABLE USABLE
LR
TANK TANK
PIPER AIRCRAFT CORPORATION SECTION 2
PA-38-112, TOMAHAWK LIMITATIONS
ISSUED: JANUARY 20, 1978 REPORT: 2126
REVISED: JANUARY 15, 1981 2-9

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