DA 40 NG AFM
Abnormal Operating
Procedures
4B.4 CANOPY IN COOLING GAP POSITION
CAUTION
If take-off was inadvertently done with the canopy in the cooling gap position, do not attempt to close the canopy in flight. Land the airplane and close the canopy on ground.
Doc. # 6.01.15-E |
Rev. 1 |
15-Mar-2011 |
Page 4B - 17 |
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Abnormal Operating
DA 40 NG AFM
Procedures
4B.5 FAILURES IN FLAP OPERATING SYSTEM
Failure in Position Indication or Function
1. |
FLAPS position . . . . . . . . . . . . . . . . . . . . . . . |
check visually |
2. |
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
keep in white range |
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(max. 98 KIAS) |
3. |
FLAPS switch . . . . . . . . . . . . . . . . . . . . . . . . |
re-check all positions |
Modified Approach Procedure Depending on the Available Flap Setting
NOTE
For landing distances with an abnormal flap position refer to 5.3.12 - LANDING DISTANCE - ABNORMAL FLAP
POSITION.
(a) Only UP Available:
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . see table below:
940 kg |
1000 kg |
1080 kg |
1160 kg |
1216 kg |
up to |
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1280 kg |
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(2072 lb) |
(2205 lb) |
(2381 lb) |
(2557 lb) |
(2681 lb) |
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(2822 lb) |
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71 KIAS |
73 KIAS |
78 KIAS |
81 KIAS |
82 KIAS |
83 KIAS |
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NOTE
If the landing mass exceeds 1216 kg (2681 lb), the landing constitutes an abnormal operating procedure. Refer to Section
4B.7 - LANDING WITH HIGH LANDING MASS.
Land at a flat approach angle, use POWER lever to control airplane speed and rate of descent.
CONTINUED
Page 4B - 18 |
Rev. 1 |
15-Mar-2011 |
Doc. # 6.01.15-E |
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DA 40 NG AFM
Abnormal Operating
Procedures
(b) Only T/O Available:
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . see table below:
940 kg |
1000 kg |
1080 kg |
1160 kg |
1216 kg |
up to |
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1280 kg |
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(2072 lb) |
(2205 lb) |
(2381 lb) |
(2557 lb) |
(2681 lb) |
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(2822 lb) |
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68 KIAS |
70 KIAS |
73 KIAS |
76 KIAS |
77 KIAS |
78 KIAS |
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NOTE
If the landing mass exceeds 1216 kg (2681 lb), the landing constitutes an abnormal operating procedure. Refer to Section
4B.7 - LANDING WITH HIGH LANDING MASS.
Land at a flat approach angle, use POWER lever to control airplane speed and rate of descent.
(c) Only LDG Available:
Perform normal landing.
END OF CHECKLIST
Doc. # 6.01.15-E |
Rev. 1 |
15-Mar-2011 |
Page 4B - 19 |
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Abnormal Operating
DA 40 NG AFM
Procedures
4B.6 LIGHTNING STRIKE
1. |
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
as low as practicable, do not |
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exceed vO (refer to Section 2.2) |
2. |
Grasp airplane controls firmly |
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% 3. |
Autopilot (if installed) . . . . . . . . . . . . . . . . . . . |
disengage (check) |
%4. PFD (if G1000 is installed) /
backup instruments . . . . . . . . . . . . . . . . . . . |
verify periodically |
5.Continue flight below vO (refer to Section 2.2)
6.Land on the next suitable airfield
CAUTION
Due to possible damage to the airplane obey the following instructions:
-Avoid abrupt or full control surface movements.
-Avoid high g-loads on the airframe.
-Avoid high yaw angles.
-Avoid turbulent air as far as possible (e.g. lee effects).
-Do not fly into areas of known or forecast icing.
END OF CHECKLIST
Page 4B - 20 |
Rev. 1 |
15-Mar-2011 |
Doc. # 6.01.15-E |
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