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Emergency

DA 40 NG AFM

Procedures

3.9 OTHER EMERGENCIES

3.9.1 ICING

Unintentional Flight Into Icing Conditions

1.

Leave the icing area (by changing altitude or turning back, in order to reach zones

 

with a higher ambient temperature).

 

2.

Pitot heating . . . . . . . . . . . . . . . . . . . . . . . . .

ON

3.

Cabin heat . . . . . . . . . . . . . . . . . . . . . . . . . .

ON

4.

Cabin air . . . . . . . . . . . . . . . . . . . . . . . . . . . .

DEFROST

5.

POWER lever . . . . . . . . . . . . . . . . . . . . . . . .

increase power, in order to prevent

 

 

ice build-up on the propeller blades

 

 

apply power changes periodically

6.

Alternate air . . . . . . . . . . . . . . . . . . . . . . . . .

OPEN

7.

Emergency windows . . . . . . . . . . . . . . . . . .

open if required

CAUTION

Ice build-up increases the stalling speed.

8. ATC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

advise if an emergency is expected

CAUTION

When the Pitot heating fails expect loss of airspeed indication.

END OF CHECKLIST

Page 3 - 46

Rev. 1

15-Mar-2011

Doc. # 6.01.15-E

 

 

 

 

DA 40 NG AFM

Emergency

Procedures

3.9.2 SUSPICION OF CARBON MONOXIDE CONTAMINATION IN THE CABIN

Carbon monoxide (CO) is a gas which is developed during the combustion process. It is poisonous and without smell. Since it occurs however usually together with flue gases, it can be detected. Increased concentration of carbon monoxide in closed spaces can be fatal. The occurrence of CO in the cabin is possible only due to a defect. If a smell similar to exhaust gases is noticed in the cabin, the following measures should be taken:

1. Cabin heat . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

2. Ventilation . . . . . . . . . . . . . . . . . . . . . . . . . . open

3. Emergency windows . . . . . . . . . . . . . . . . . . open

4. Forward canopy . . . . . . . . . . . . . . . . . . . . . . unlatch, push up and lock in 'Cooling Gap' position

CAUTION

The maximum demonstrated airspeed for opening the front canopy in flight is 117 KIAS.

NOTE

In case of suspicion of carbon monoxide contamination in the cabin, the front canopy may be unlatched during flight. This allows it to partially open, in order to improve ventilation. The canopy will remain open in this position. Flight characteristics will not be affected significantly.

END OF CHECKLIST

Doc. # 6.01.15-E

Rev. 1

15-Mar-2011

Page 3 - 47

 

 

 

 

Emergency

 

DA 40 NG AFM

Procedures

 

 

 

 

 

 

3.9.3 UNLOCKED DOORS

 

 

1.

Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . .

reduce immediately

2.

Canopy . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

check visually if closed

3.

Rear door . . . . . . . . . . . . . . . . . . . . . . . . . . .

check visually if closed

Canopy Unlocked

4. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . below 140 KIAS 5. Land at next suitable airfield.

END OF CHECKLIST

Rear Door Unlocked

4. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . below 140 KIAS 5. Land at the next suitable airfield.

WARNING

Do not try to lock the rear door in flight. The safety latch may disengage and the door opens. Usually this results in a separation of the door from the airplane.

NOTE

If the rear door has been lost the airplane can be safely flown to the next suitable airfield.

END OF CHECKLIST

Page 3 - 48

Rev. 1

15-Mar-2011

Doc. # 6.01.15-E

 

 

 

 

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