AIRCRAFT
SA 160
AIRCRAFTA I R C R A F T
Symphony
4-20
SECTION 4
NORMAL PROCEDURES
damage. The security of attachment of the aileron counter weight is
tobechecked.
At the wing trailing edge, the ailerons and wing flaps as well as its
hinges are to be checked for damage and condition, the ailerons for
smoothness and freedom of operation. Bonding straps and static
dischargersshouldbefirmly attached and in good condition.
Next, through the quick drain of the right wing fuel tank sump drain
fuel into clear cup and check for water and sediment. Drain until
waterorsedimentisgone.
The right main gear strut and wheel fairing is to be checked for
damage. The tire should be checked for proper inflation and
condition.
Verify the 20° flap position color marking on the inboard flap track is
presentandingoodcondition.
The quick-release locks of the top-deck hatches for the right wing are
tobecheckedfor proper lock.
5. Fuselage
The fuselage skins are to be checked for damage such as
delaminations or tears and the antennae for their integrity and
security.
Checkthestaticportsforobstructions and integrity.
The empennage should be clear of ice, frost, snow or other extraneous
substances.
The security of attachment of the horizontal stabilizer, and the
freedom of movement of the elevator are to be checked. The piano
type hinges of the elevator show no damage and are secured properly
as well as the elevator pushrod. The trim tab is in neutral position.
Check trim tab pushrod. Rudder as well as its hinges are to be
checkedfor damage, smoothness and freedom of operation there.
The static dischargers should be firmly attached and in good
condition.
The baggage in the baggage compartment should be securely
anchored down. Close the baggage door and lock it by means of both
locks.
Feb 25, 2005
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