Normal Operating			DA 42 NG AFM
	Procedures
4A.6.12 GO AROUND
1.		POWER lever . . . . . .	. . . . . . . . . . . . . . . . . . MAX
2.		Airspeed . . . . . . . . . .	. . . . . . . . . . . . . . . . . . min. 90 KIAS
3.		FLAPS . . . . . . . . . . . .	. . . . . . . . . . . . . . . . . . position APP

when a positive rate of climb is established:

4. Landing gear . . . . . . . . . . . . . . . . . . . . . . . . . UP, check unsafe light off

5. FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . retract, position UP

when a safe climb is established:

6. Fuel pumps LH/RH . . . . . . . . . . . . . . . . . . . .

OFF

END OF CHECKLIST

GFC 700 Operation During Go Around
1.	Control stick . . . . . . . . . . . . . . . . . . . . . . . . .	GRASP FIRMLY
2.	GA button . . . . . . . . . . . . . . . . . . . . . . . . . . .	PUSH - verify GA/GA on
		PFD in lateral and vertical mode
		fields

NOTE

After the GA button is pressed, the autopilot disconnects and the flight director indicates a 7° pitch up altitude.

3.	Balked landing . . . . . . . . . . . . . . . . . . . . . . . .	execute
4.	Missed approach procedure . . . . . . . . . . . . .	execute (as applicable)
5.	Altitude preselelect . . . . . . . . . . . . . . . . . . . .	set to appropriate altitude

CONTINUED

Page 4A - 56	Rev. 1	18-Feb-2009	Doc. No. 7.01.15-E

DA 42 NG AFM

Normal Operating

Procedures

At an appropriate safe altitude:

6.	Autopilot mode controller . . . . . . . . . . . . . . .	select appropriate lateral
		and vertical mode on controller
7.	Autopilot . . . . . . . . . . . . . . . . . . . . . . . . . . . .	RE-ENGAGE if desired

NOTE

If the missed approach procedure requires tracking the localizer outbound from the airport, use NAV mode to prevent inadvertent coupling to glideslope.

END OF CHECKLIST
4A.6.13 AFTER LANDING
1.	POWER lever . . . . . . . . . . . . . . . . . . . . . . . .	IDLE
2.	Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . .	as required
3.	Transponder . . . . . . . . . . . . . . . . . . . . . . . . .	OFF / STBY
4.	Pitot heating . . . . . . . . . . . . . . . . . . . . . . . . .	OFF
5.	Avionics . . . . . . . . . . . . . . . . . . . . . . . . . . . .	as required
6.	Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .	as required
7.	FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . .	UP
8.	Fuel pumps LH/RH . . . . . . . . . . . . . . . . . . . .	OFF

END OF CHECKLIST

Doc. No. 7.01.15-E	Rev. 1	18-Feb-2009	Page 4A - 57

	Normal Operating			DA 42 NG AFM
	Procedures
4A.6.14 SHUT-DOWN
1.		Parking brake . . . . . . . . . . . . . . . . . . . . . . . .	set
2.		POWER lever . . . . . . . . . . . . . . . . . . . . . . . .	10 % load for 1 minute
3.		Engine/System Page . . . . . . . . . . . . . . . . . . .	check
4.		ELT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .	check not transmitting on
			121.5 MHz
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 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.

9. ELECT. MASTER . . . . . . . . . . . . . . . . . . . . .

OFF

CAUTION

Before shut-down the engine must run for at least 1 minute with the power lever at 10% to avoid heat damage of the turbo charger.

CAUTION

Do not shut down an engine with the FUEL SELECTOR valve.

The high pressure fuel pump can otherwise be damaged.

END OF CHECKLIST

4A.6.15 EXIT AIRPLANE

Page 4A - 58	Rev. 1	18-Feb-2009	Doc. No. 7.01.15-E

DA 42 NG AFM

Normal Operating

Procedures

Exit the airplane to the aft on designated areas on the inner wing section LH or RH.

4A.6.16 POST FLIGHT INSPECTION

1.Record any problem found in flight and during the post-flight check in the log book.

2.Park the airplane.

3.If necessary, moor the airplane.

END OF CHECKLIST

4A.6.17 PARKING
1.	Parking brake . . . . . . . . . . . . . . . . . . . . . . . .	release, use chocks
2.	Airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . .	moor, if unsupervised for
		extended period
3.	Pitot probe . . . . . . . . . . . . . . . . . . . . . . . . . .	cover

END OF CHECKLIST

Doc. No. 7.01.15-E	Rev. 1	18-Feb-2009	Page 4A - 59