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B. Hot engine procedure
"Alternate Air" (if installed)   Pushed
Propeller   FULL FORWARD
Throttle   FULL POWER
Mixture   IDLE CUT-OFF
Fuel pump  ON
Mixture
 BOTH
ABAA
Validity : S / N 1 - 9999 05-30-01Page 204
(CA) JUN 01
 
Mixture   FULL RICH
Throttle   REDUCED
Oil pressure   Green sector
If no oil pressure indication after 30 sec.,
shut down engine.
4. AFTER ENGINE STARTING
CAUTION : AVOID EXCEEDING 1200 RPM AS LONG AS THE OIL TEMPERATURE INDICATOR POINTER IS WITHIN YELLOW SECTOR.
Advisory panel test   Positive
5. ENGINE RUN-UP
Engine control friction   Adjusted
Oil temperature   Green sector
Oil pressure   Green sector
Mixture   FULL RICH
"Alternate Air" (if installed)   Pushed
Fuel selector   Set to fullest tank
A. Propeller check
Propeller   FULL FORWARD
Throttle   2000 RPM
Propeller   Cycle twice (maxi. 500 RPM drop)
Return to high RPM (FULL FORWARD)
B. Magneto check
Throttle   2000 RPM
Magneto selector   L. then BOTH
R. then BOTH
Maximum RPM drop on each magneto   175 RPM
Maximum difference between magnetos   50 RPM
C. Spark plug clearing in case of RPM drop on each magneto exceeds 175 RPM
Throttle   2200 RPM
Mixture  FULL RICH
Magneto selector   BOTH
Mixture  Slowly lean until EGT peak
Maintain during 30 seconds
Mixture  Return to FULL RICH
CHT must not exceed 500°F (260°C).
Perform a magneto check again.
If the RPM drop still exceeds 175 RPM, then abort the mission for further investigations.
ABAA
Validity : S / N 1 - 9999 05-30 01Page 205
(CA) JUN 01
 
6. SHUT-DOWN / SECURING AIRCRAFT
Anti-collision lights (if installed)   OFF
Throttle   REDUCED
WARNING : THE TEST HEREAFTER MUST BE IMPERATIVELY CARRIED OUT WITH ENGINE POWER LOWER THAN 1000 RPM ; THE FAILURE TO OBSERVE THIS RULE MAY LEAD TO EXHAUST SYSTEM DAMAGE.
Magneto cut-off test   OFF, then BOTH
Propeller   FULL FORWARD
Throttle   1800 RPM for 15 sec., then 1200 RPM
Mixture   IDLE CUT-OFF
AFTER ENGINE STOPS :
Magneto selector   OFF
Alternator switch-breaker   OFF
Oil pressure warning light   Illuminated
Main switch   OFF
Fuel selector   OFF
Parking brake   Released
Control lock   Installed
 Chocks / Tie-downs   Installed
ABM
Validity : S / N 1 - 9999 05 30 01Page 206
(CA) JUN 01
 
TEST RUN-UP
1. PRELIMINARY INSPECTION (Figure 201) NOTE : Place the aircraft into the wind. A. Airframe
　
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