Diamond DA20-C1 Maintenance Manual page 126

Maintenance Practices
14. Lock the handles of the main bolts with the
locking device.
15. Remove the trestles under the wings.
16. Connect the flap control rods at the bellcrank
on the bulkhead, aft control.
17. Connect the aileron control rods at the bell-
crank on the bulkhead, aft control.
18. Do a check of the flap controls for correct
connection and operation.
19. Do a check of the Aileron controls for correct
connection and operation.
20. Do a low-range static leak test.
21. Do a pitot leak test.
22. Install the following items:
- Pilots' seats.
- Access panels below the fuselage for the
control connections.
- Access panels below the wing roots for
the B-bolts.
Page 206
30 Oct 09
Detail Steps/Work Items
57-10-00
Key Items/References
Pull it up against the spring. Then turn it to
engage both of the handles.
Refer to Chapter 27-50.
Through the panels below the fuselage.
Refer to Chapter 20 for standard torque
values.
Refer to Chapter 27-10.
Through the panels below the fuselage.
Refer to Chapter 20 for standard torque
values.
Obey the instructions of your airworthiness
authority for control checks.
Obey the instructions of your airworthiness
authority for control checks.
Refer to Chapter 34-10.
Refer to Chapter 34-10.
Refer to Chapter 25-10.
Refer to Chapter 52-40.
Refer to Chapter 52-40.
DA20-C1 AMM
DA201-C1
Rev 16