Piper TOMAHAWK User Manual

(d) Fuel Pressure
Green Arc (Normal Operating Range) .5 PSI to 8 PSI
Red Line (Minimum) .5 PSI
Red Line (Maximum) 8 PSI
2.11 WEIGHT LIMITS
Normal Utility
(a) Maximum Weight 1670 lbs. 1670 lbs.
(b) Maximum Baggage at Fuselage
Station 115.0 100 lbs. 100 lbs.*
CAUTION
Baggage compartment loading should not
exceed 25 lbs. per square foot.
2.13 CENTER OF GRAVITY LIMITS
(a) Normal Category
Weight Forward Limit Rearward Limit
Pounds Inches Aft of Datum Inches Aft of Datum
1670 73.5 78.5
1277 72.4 78.5
(b) Utility Category
Weight Forward limit Rearward Limit
Pounds Inches Aft of Datum Inches Aft of Datum
1670 73.5 78.5
1277 72.4 78.5
*No baggage allowed for spins.
SECTION 2 PIPER AIRCRAFT CORPORATION
LIMITATIONS PA-38-112, TOMAHAWK
REPORT: 2126 ISSUED: JANUARY 20, 1978
2-4 REVISED: JUNE 6, 1979
(d) Fuel Pressure
Green Arc (Normal Operating Range) .5 PSI to 8 PSI
Red Line (Minimum) .5 PSI
Red Line (Maximum) 8 PSI
2.11 WEIGHT LIMITS
Normal Utility
(a) Maximum Weight 1670 lbs. 1670 lbs.
(b) Maximum Baggage at Fuselage
Station 115.0 100 lbs. 100 lbs.*
CAUTION
Baggage compartment loading should not
exceed 25 lbs. per square foot.
2.13 CENTER OF GRAVITY LIMITS
(a) Normal Category
Weight Forward Limit Rearward Limit
Pounds Inches Aft of Datum Inches Aft of Datum
1670 73.5 78.5
1277 72.4 78.5
(b) Utility Category
Weight Forward limit Rearward Limit
Pounds Inches Aft of Datum Inches Aft of Datum
1670 73.5 78.5
1277 72.4 78.5
*No baggage allowed for spins.
SECTION 2 PIPER AIRCRAFT CORPORATION
LIMITATIONS PA-38-112, TOMAHAWK
REPORT: 2126 ISSUED: JANUARY 20, 1978
2-4 REVISED: JUNE 6, 1979

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