Preflight Inspection 15 / 15
► Continuing
NOTE
Access to ELT is possible through an inspection door located on the right side
of fuselage rear section.
123 - Static pressure ports ............................................................................. Clean
124 - 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.
125 - Inspection door under fuselage .................................... Attachments / Closed
126 - Horizontal stabilizer deicer boots (right side) ........... Condition / Attachments
127 - 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.
128 - Static dischargers ............................................................................ Condition
129 - Vertical stabilizer deicer boots .................................. Condition / Attachments
130 - Rudder and trim ....................................................... Condition / Trim position
131 - Static dischargers ............................................................................ Condition
132 - Tail cone / nav. lights / strobe .......................................................... Condition
133 - Static pressure ports ............................................................................. Clean
End of procedure.
Pilot's Information Manual
Section 4
Normal Procedures
PIM TBM 960 - Edition 0
Rev. 01
Page 4.4.15
PIM - DO NOT USE FOR FLIGHT OPERATIONS