Piper PA-38-112, Pilot'S Operating Handbook And Faa Approved Airplane Flight Manual

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4.7 AMPLIFIED NORMAL PROCEDURES (GENERAL)
The following paragraphs are provided to supply detailed information
and explanations of the normal procedures necessary for the safe operation
of the airplane.
4.9 PREFLIGHT CHECK
The airplane should be given a thorough preflight and walk-around
check. The preflight should include a check of the airplane’s operational
status, computation of weight and C.G. limits, takeoff distance and
in-flight performance. A weather briefing should be obtained for the
intended flight path, and any other factors relating to a safe flight should be
checked before takeoff.
COCKPIT
Upon entering the cockpit, release any restraints securing the control
wheel. Check that the ignition switch is OFF, that the throttle is closed, and
that the mixture control is in idle cut-off. Then turn the master switch ON.
Check the fuel quantity gauges for sufficient fuel. Check that the alternator
warning light illuminates. After completing these checks, turn the master
switch OFF.
Exercise the controls through their full travel and lower and raise the
flaps to check for proper operation. The static drain valve on the lower left
sidepanel should be opened and drained. Check for unobstructed visibility
and clean windows. See that the baggage is stowed properly and tied down.
Make sure that all necessary charts and papers are on board and in order.
Before leaving the cockpit for the external check, set the parking brake.
LEFT WING
Check that the wings and control surfaces are free of snow, ice, frost or
any other foreign matter. Check for damage and loose screws or rivets.
Check the control surfaces and hinges for damage and operational
interference. Check the wing tip and lights for damage.
Open the fuel cap and visually check the fuel for color and quantity.
Replace the fuel cap securely after the check is complete. Be sure that the
fuel tank vent is unobstructed. Using the underwing fuel tank drain, drain
sufficient fuel from the tank to ensure the removal of contaminants. It is
PIPER AIRCRAFT CORPORATION SECTION 4
PA-38-112, TOMAHAWK NORMAL PROCEDURES
ISSUED: JANUARY 20, 1978 REPORT: 2126
REVISED: JUNE 23, 1978 4-11
4.7 AMPLIFIED NORMAL PROCEDURES (GENERAL)
The following paragraphs are provided to supply detailed information
and explanations of the normal procedures necessary for the safe operation
of the airplane.
4.9 PREFLIGHT CHECK
The airplane should be given a thorough preflight and walk-around
check. The preflight should include a check of the airplane’s operational
status, computation of weight and C.G. limits, takeoff distance and
in-flight performance. A weather briefing should be obtained for the
intended flight path, and any other factors relating to a safe flight should be
checked before takeoff.
COCKPIT
Upon entering the cockpit, release any restraints securing the control
wheel. Check that the ignition switch is OFF, that the throttle is closed, and
that the mixture control is in idle cut-off. Then turn the master switch ON.
Check the fuel quantity gauges for sufficient fuel. Check that the alternator
warning light illuminates. After completing these checks, turn the master
switch OFF.
Exercise the controls through their full travel and lower and raise the
flaps to check for proper operation. The static drain valve on the lower left
sidepanel should be opened and drained. Check for unobstructed visibility
and clean windows. See that the baggage is stowed properly and tied down.
Make sure that all necessary charts and papers are on board and in order.
Before leaving the cockpit for the external check, set the parking brake.
LEFT WING
Check that the wings and control surfaces are free of snow, ice, frost or
any other foreign matter. Check for damage and loose screws or rivets.
Check the control surfaces and hinges for damage and operational
interference. Check the wing tip and lights for damage.
Open the fuel cap and visually check the fuel for color and quantity.
Replace the fuel cap securely after the check is complete. Be sure that the
fuel tank vent is unobstructed. Using the underwing fuel tank drain, drain
sufficient fuel from the tank to ensure the removal of contaminants. It is
PIPER AIRCRAFT CORPORATION SECTION 4
PA-38-112, TOMAHAWK NORMAL PROCEDURES
ISSUED: JANUARY 20, 1978 REPORT: 2126
REVISED: JUNE 23, 1978 4-11