Piper PA-38-112 - CLIMB; APPROACH AND LANDING

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CLIMB

Best rate (flaps up)............................................................................70 KIAS

Best angle (flaps up).........................................................................61 KIAS

Electrical fuel pump....................................................OFF at desired altitude

CRUISING

Reference performance charts and Avco-Lycoming Operator’s Manual.

Normal max power ..................................................................................75%

Power................................................................................set per power table

Mixture..................................................................................................adjust

APPROACH AND LANDING

Fuel selector..................................................................................proper tank

Seat backs ...............................................................................................erect

Belts/harness .........................................................................................fasten

Electric fuel pump.....................................................................................ON

Mixture.......................................................................................................set

Flaps..................................................................................set - 89 KIAS max

Trim to 70 KIAS.

Final approach speed

Full flaps (Outboard Flow Strips Installed) ..................................62 KIAS

Full flaps (Outboard and Inboard Flow

Strips Installed) ............................................................................67 KIAS

STOPPING ENGINE

Flaps.....................................................................................................retract

Electric fuel pump ...................................................................................OFF

Radios......................................................................................................OFF

Throttle ................................................................................................full aft

Mixture..........................................................................................idle cut-off

Magnetos .................................................................................................OFF

Master switch ..........................................................................................OFF

PIPER AIRCRAFT CORPORATION SECTION 4

PA-38-112, TOMAHAWK NORMAL PROCEDURES

ISSUED: JANUARY 20, 1978 REPORT: 2126

REVISED: DECEMBER 18, 1978 4-9