Pilot's Operating Handbook
Section 4
Normal procedures
EASA Approved
Edition 1 - January 15, 2018
Rev. 2
Page 4.4.16
Preflight inspection 16/16
► Continuing
129 - ELT door Closed / Locked. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
● NOTE ●
Access to ELT is possible through an inspection door located on R.H. side of
fuselage rear section.
●
130 - Static pressure ports Clean. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
131 - Ventral fins Condition / Attachments. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
● NOTE ●
Ventral fins are made of two parts (one fixed part and one removable part with
rear lower inspection door). Check that these two parts are connected by the
locking roller.
●
132 - Inspection door under fuselage Attachments - Closed
. . . . . . . . . . . . . . . . . . .
133 - Horizontal stabilizer deicer boots (R.H. side) Condition / Attachments. . . . . .
134 - Elevator and trim Condition / Deflection free movement /. . . . . . . . . . . . . . . .
Trim position
● NOTE ●
To check the deflection, hold the two half-elevators near fuselage, inside both
elevator trims to avoid stresses.
●
135 - Static dischargers Condition. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
136 - Vertical stabilizer deicer boots Condition / Attachments. . . . . . . . . . . . . . . . . .
137 - Rudder and trim Condition / Trim position. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
138 - Static dischargers Condition. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
139 - Tail cone / nav. lights / strobe Condition. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
140 - Static pressure ports Clean
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
End of procedure.
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