Normal Operating
Procedures
DA 62 AFM
4A.6.14 SHUT-DOWN
1. Parking brake. . . . . . . . . . . . . . . . . . . . . . . . . set
2. POWER lever. . . . . . . . . . . . . . . . . . . . . . . . . up to 10% load for 1 minute
3. Engine/System Page . . . . . . . . . . . . . . . . . . . check
4. ELT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . check not activated
5. AVIONIC MASTER . . . . . . . . . . . . . . . . . . . . OFF
6. Electrical consumers . . . . . . . . . . . . . . . . . . . OFF
7. ENGINE MASTER . . . . . . . . . . . . . . . . . . . . . OFF
8. Anti collision lights (ACL) . . . . . . . . . . . . . . . . OFF
CAUTION
After turning the ENGINE MASTER OFF, wait until the G1000
engine indications are red X'd or yellow X’d prior to switching
the ELECT. MASTER OFF. This ensures that engine and
flight data can be written to non-volatile memory before
removing electrical power.
NOTE
During engine shut down at altitudes greater than 7500 ft,
it is possible that the propeller will feather due to the
increased engine idle power. As the increase in propeller
RPM can prevent the propeller start locks from engaging,
proceed with steps 9.1 through 9.3.
9.1 Engine Master . . . . . . . . . . . . . . . . . . . . . ON (5 seconds)
9.2 Propeller. . . . . . . . . . . . . . . . . . . . . . . . . . verify start lock position
9.3 Engine Master . . . . . . . . . . . . . . . . . . . . . OFF
10. ELECT. MASTER . . . . . . . . . . . . . . . . . . . . . OFF
CONTINUED
Page 4A - 62 Rev. 0 11-Jan-2019 Doc. No. 11.01.05-E