Diamond DA 62 - Page 189

Normal Operating
Procedures
DA 62 AFM
Test sequence completed.
14. ECU TEST button . . . . . . . . . . . . . . . . . . . . . release
15. Parking brake. . . . . . . . . . . . . . . . . . . . . . . . . release
Available power check:
1. POWER lever. . . . . . . . . . . . . . . . . . . . . . . . . MAX for 10 seconds
2. Annunciations . . . . . . . . . . . . . . . . . . . . . . . . check OK/normal range
3. Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . check within normal range
4. RPM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . stabilizes at 2250 to 2300 RPM
5. LOAD indication . . . . . . . . . . . . . . . . . . . . . . . stabilizes at 89% to 100%
CAUTION
The load indications in the table below are minimum values
to be indicated with the airplane stationary in no wind
conditions. If the engine does not stabilize at the target RPM
and the required load indication, terminate flight preparation.
CONTINUED
Page 4A - 32 Rev. 0 11-Jan-2019 Doc. No. 11.01.05-E