Normal Operating |
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DA 40 NG AFM |
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Procedures |
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4A.5.2 BEFORE STARTING ENGINE |
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1. |
Pre-flight inspection . . . . . . . . . . . . . . . . . . . |
complete |
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2. |
Rudder pedals . . . . . . . . . . . . . . . . . . . . . . . |
adjusted and locked |
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3. |
Passengers . . . . . . . . . . . . . . . . . . . . . . . . . |
instructed |
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4. |
Safety harnesses . . . . . . . . . . . . . . . . . . . . . |
all fastened |
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5. |
Rear door . . . . . . . . . . . . . . . . . . . . . . . . . . . |
closed and locked |
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6. |
Door lock (if installed) . . . . . . . . . . . . . . . . . . |
unlocked, key removed |
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7. |
Front canopy . . . . . . . . . . . . . . . . . . . . . . . . |
Position 1 or 2 (“cooling gap”) |
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8. |
Canopy lock (if installed) . . . . . . . . . . . . . . . |
unlocked, key removed |
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CAUTION
When operating the canopy, pilots / operators are to ensure that there are no obstructions between the canopy and the mating frame, for example seat belts, clothing, etc. When operating the locking handle do NOT apply undue force.
NOTE
A slight downward pressure on the canopy may be required to ease the handle operation.
9. |
Parking brake . . . . . . . . . . . . . . . . . . . . . . . . |
set |
10. |
Flight controls . . . . . . . . . . . . . . . . . . . . . . . . |
free movement |
11. |
Trim wheel . . . . . . . . . . . . . . . . . . . . . . . . . . |
T/O |
12. |
POWER lever . . . . . . . . . . . . . . . . . . . . . . . . |
check IDLE |
13. |
Friction device on POWER lever . . . . . . . . . |
adjusted |
14. |
Alternate air . . . . . . . . . . . . . . . . . . . . . . . . . |
check CLOSED |
15. |
Alternate static valve . . . . . . . . . . . . . . . . . . |
check CLOSED |
CONTINUED
Page 4A - 12 |
Rev. 1 |
15-Mar-2011 |
Doc. # 6.01.15-E |
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DA 40 NG AFM |
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Normal Operating |
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Procedures |
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16. |
VOTER switch . . . . . . . . . . . . . . . . . . . . |
. . . check AUTO |
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17. |
Fuel pumps . . . . . . . . . . . . . . . . . . . . . . . |
. . check OFF |
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18. |
AVIONIC MASTER . . . . . . . . . . . . . . . . . |
. . check OFF |
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19. |
ELECTRIC MASTER . . . . . . . . . . . . . . . . |
. . ON |
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% |
20. |
G1000 (if installed) . . . . . . . . . . . . . . . . . . |
. . wait until power-up completed. |
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Press ENT on MFD to |
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acknowledge |
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NOTE |
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% |
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If the G1000 avionics system |
is installed, the engine |
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instruments are only available on the MFD after item 20 has |
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been completed. |
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% |
21. |
White Wire annunciator panel (if installed) . |
. . check and press acknowledge button |
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% 22. COOL LVL caution on G1000 (if installed) or |
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% |
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WATERLEV caution on SED (if installed) |
. . check OFF |
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23. |
Fuel temperature . . . . . . . . . . . . . . . . . . . |
. . check |
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WARNING
Never rotate the propeller by hand.
END OF CHECKLIST
Doc. # 6.01.15-E |
Rev. 1 |
15-Mar-2011 |
Page 4A - 13 |
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Normal Operating
DA 40 NG AFM
Procedures
4A.5.3 STARTING ENGINE
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CAUTION |
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Do not operate the engine starter motor for more than |
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10 seconds, because of possible overheating of the starter |
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motor. |
% |
If the STARTER annunciation on the G1000 (if installed) or |
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START on the White Wire annunciator panel (if installed) |
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comes on after the engine has started and the START KEY |
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has been released, set the ENGINE MASTER to OFF and |
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investigate the problem. |
WARNING
If the oil pressure has not moved from the red range within 3 seconds after starting, set the ENGINE MASTER switch to OFF and investigate problem.
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NOTE |
% |
At low ambient temperatures it is possible that the engine will |
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not start at the first attempt. In this case wait 60 seconds |
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between the start attempts. |
1.Strobe lights (ACL) . . . . . . . . . . . . . . . . . . . . . ON
2.ENGINE MASTER . . . . . . . . . . . . . . . . . . . . . ON
CONTINUED
Page 4A - 14 |
Rev. 1 |
15-Mar-2011 |
Doc. # 6.01.15-E |
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DA 40 NG AFM
Normal Operating
Procedures
%3. Annunciations / GLOW ON (if G1000
%is installed) or GLOW (if White Wire
%annunciator panel is installed) . . . . . . . . . . . . check ON
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NOTE |
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GLOW ON (if G1000 is installed) or GLOW (if White Wire |
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annunciator panel is installed) is indicated only when the |
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engine is cold. |
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4. Annunciations / engine indications . . . . . . . . . |
check |
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WARNING |
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Before starting the engine the pilot must ensure that the propeller area is free, and no persons can be endangered.
%After the GLOW ON (if G1000 is installed) or GLOW (if White Wire annunciator panel
%is installed) indication is extinguished:
5.START KEY . . . . . . . . . . . . . . . . . . . . . . . . . . START as required / release
when engine has started.
%6. Annunciations / engine indications . . . . . . . . . check OK/normal range
7.Annunciations / STARTER
%(if G1000 is installed) or START (if
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White Wire annunciator panel is installed) . . check OFF |
CONTINUED
Doc. # 6.01.15-E |
Rev. 1 |
15-Mar-2011 |
Page 4A - 15 |
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Normal Operating
DA 40 NG AFM
Procedures
8. |
Annunciations / Oil pressure . . . . . . . . . . . . . |
check OK |
% 9. |
Circuit breakers . . . . . . . . . . . . . . . . . . . . . . . |
check all IN |
10. |
Idle RPM . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
check, 710 ±30 RPM |
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(above 7,000 ft pressure altitude |
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idle RPM might be higher) |
11. |
Warm up . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
IDLE for 2 minutes, then |
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at 50% load until: |
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oil temperature |
reaches 50°C (122°F)
and the coolant temperature reaches 60 °C (140°F)
END OF CHECKLIST
Page 4A - 16 |
Rev. 1 |
15-Mar-2011 |
Doc. # 6.01.15-E |
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