Piper TOMAHAWK User Manual

3.3 EMERGENCY PROCEDURES CHECKLIST
SPEEDS
Stall speeds
1670 lbs (0° flap) (Outboard Flow Strips Installed)......................48 KIAS
1670 lbs. (full flap) (Outboard Flow Strips Installed)...................47 KIAS
1670 lbs. (0° flap) (Outboard and Inboard Flow
Strips Installed) ............................................................................52 KIAS
1670 lbs. (full flap) (Outboard and Inboard Flow
Strips Installed) ............................................................................49 KIAS
Maneuvering speeds
1670 lbs......................................................................................103 KIAS
1277 lbs........................................................................................90 KIAS
Never exceed speed.........................................................................138 KIAS
Power off glide speeds
1670 lbs. (0° flap).........................................................................70 KIAS
ENGINE INOPERATIVE PROCEDURES
ENGINE POWER LOSS DURING TAKEOFF (NOT AIRBORNE)
Sufficient runway remaining:
Throttle ..............................................................................close immediately
Brakes..................................................................................apply as required
Stop straight ahead.
Insufficient runway remaining:
Throttle ..............................................................................close immediately
Brakes..................................................................................apply as required
Mixture .................................................................................IDLE CUT-OFF
Fuel selector ............................................................................................OFF
Master switch ..........................................................................................OFF
Magnetos .................................................................................................OFF
Maintain directional control and maneuver to avoid obstacles.
ENGINE POWER LOSS DURING TAKEOFF (IF AIRBORNE)
Sufficient runway remaining:
Airspeed..........................................................................maintain above stall
Directional control ............................................................................maintain
Land straight ahead.
SECTION 3 PIPER AIRCRAFT CORPORATION
EMERGENCY PROCEDURES PA-38-112, TOMAHAWK
REPORT: 2126 ISSUED: JANUARY 20, 1978
3-2 REVISED: DECEMBER 18, 1978
3.3 EMERGENCY PROCEDURES CHECKLIST
SPEEDS
Stall speeds
1670 lbs (0° flap) (Outboard Flow Strips Installed)......................48 KIAS
1670 lbs. (full flap) (Outboard Flow Strips Installed)...................47 KIAS
1670 lbs. (0° flap) (Outboard and Inboard Flow
Strips Installed) ............................................................................52 KIAS
1670 lbs. (full flap) (Outboard and Inboard Flow
Strips Installed) ............................................................................49 KIAS
Maneuvering speeds
1670 lbs......................................................................................103 KIAS
1277 lbs........................................................................................90 KIAS
Never exceed speed.........................................................................138 KIAS
Power off glide speeds
1670 lbs. (0° flap).........................................................................70 KIAS
ENGINE INOPERATIVE PROCEDURES
ENGINE POWER LOSS DURING TAKEOFF (NOT AIRBORNE)
Sufficient runway remaining:
Throttle ..............................................................................close immediately
Brakes..................................................................................apply as required
Stop straight ahead.
Insufficient runway remaining:
Throttle ..............................................................................close immediately
Brakes..................................................................................apply as required
Mixture .................................................................................IDLE CUT-OFF
Fuel selector ............................................................................................OFF
Master switch ..........................................................................................OFF
Magnetos .................................................................................................OFF
Maintain directional control and maneuver to avoid obstacles.
ENGINE POWER LOSS DURING TAKEOFF (IF AIRBORNE)
Sufficient runway remaining:
Airspeed..........................................................................maintain above stall
Directional control ............................................................................maintain
Land straight ahead.
SECTION 3 PIPER AIRCRAFT CORPORATION
EMERGENCY PROCEDURES PA-38-112, TOMAHAWK
REPORT: 2126 ISSUED: JANUARY 20, 1978
3-2 REVISED: DECEMBER 18, 1978

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