SusiAir PILATUS PORTER PC6, Maintenance Program

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FORM ASI-PC6 PILATUS PC6 – 3500 Hours / Partial Overhaul Inspection Aircraft Reg.: __________
Reissued: 2
Revision: 1
Date: July 2020 Page 6 of 13
NO. DESCRIPTION TASK NO. MECH. ENG. RII
5
Access door - RH rear fuselage
N/A
Latching mechanism - Do an Operational test. Lubricate mechanism
(Material No. P04-037)
Chapter 53 - Fuselage
1
Fuselage - external
N/A
Examine.
2
Fuselage - internal
N/A
Examine.
3
Fuselage
N/A
Make sure that the drain holes are not blocked.
4
Wing attachment brackets and adjacent structure
N/A
Examine.
Use a light magnifying glass.
5
Fuselage - wing strut attachment brackets and structure internal and
external
04-00-00 N/A
Examine (Using Fluorescent Dye penetrant Inspection.
6
V-strut attachment brackets
N/A
Examine.
7
Access panels
N/A
Examine panels, fairings and fasteners.
8
Stabilizer Trim Attachment Components FR12A Support Brackets
53-30-00,
04-00-00
N/A
Examine.
9
Stabilizer Trim Attachment Components FR12A Where the Horizontal Trim
Actuator Support is Installed.
53-30-00,
04-00-00
N/A
Examine.
Chapter 55 - Stabilizers
1
Elevators
55-21-11
Remove.
2
Rudder
55-31-11
Remove.
3
Empennage - internal
N/A
Examine as far as possible.
Make sure that the water drain holes are not blocked.
4
Dorsal fin and attachments
N/A
Examine.
5
Vertical stabilizer
N/A
Examine.
6
Rudder bearings
N/A
Replace rudder hinge bearings.
7
Rudder torque shaft upper and lower bearing
27-22-01 N/A
Replace.
8
Empennage
N/A
Examine panels, fairings and fasteners.
9
Torque tube
N/A
Examine.
10
Rudder and trim tab
N/A
Examine.
11
Horizontal stabilizer
N/A
Check for excessive play at attachment points by rocking stabilizer ends
and listening for movement at attachment points. Maximum play is 1,5
mm (0.06 in.).