DV 20 E AFM
Normal Operating
Procedures
Doc. No. 4.01.25-E Rev. 2 22-Mar-2022
EASA
approved
Page 4 - 5
4.3.2 PRE-FLIGHT INSPECTION
I. Cabin Check
1. Structural temperature indicator
(if OAT exceeds 38 °C (100 °F)) .......... check that structural temperature
does not exceed 54 °C (129 °F),
a red ‘55' indicates a temperature
above the limit.
2. Airplane documents ................... complete and up to date
3. Flight control lock ..................... removed
4. Flight controls ........................ check free and correct movement
up to full deflection
5. Alternate air ......................... free, OFF
6. Cabin heat .......................... free
7. Both brake pedals ..................... push
8. Parking brake ........................ SET, release brake pedals
9. Throttle ............................. free, IDLE
10. Propeller speed lever .................. free, HIGH
11.ELECTRIC MASTER .................. ON
12. Annunciation lights
(EMU, VOLTAGE, START and CANOPY) . . check
13. Fuel quantity ......................... sufficient
14.Engine instruments, ammeter............ check
15.Circuit breakers ...................... pressed in
16.Map light............................ operational
17.Instrument lights ...................... operational and dimmable
18.Trim ............................... NEUTRAL
CONTINUED
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