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Eads Eurocopter BO 105 CBS-5 - Deceleration Check

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FLIGHT MANUAL BO 105 CB-5/CBS-5
EUROCOPTER
4 - 18
LBA APPROVED
Rev. 0
4.9.2 Deceleration Check
NOTE Perform this check after first flight of each day and for each engine separately.
Cyclic stick Trim neutral
Collective lever lock Engage
All electrical consumers Off except anti-collision lights and fuel
pumps
Generator switches Off
N
2
(BENDIX fuel controls only) Stabilize at 100% for 15 seconds
Power lever of check engine Snap to IDLE, start clock (stopwatch)
When N
1
of check engine passes 65%:
Clock Stop, note time
NOTE D Minimum allowable deceleration time is 2 seconds. If deceleration time is less
than 2 seconds, perform two more checks to confirm time.
D Maintenance action is required when:
- confirmed deceleration time is less than 2 sec,
-N
1
drops below 59%,
- flameout is experienced.
Power lever of check engine FLIGHT
Remaining engine Perform deceleration check
Both power levers IDLE
Cyclic stick lock (if fitted) Engage
After 2 min:
Power levers OFF
CAUTION
IF TOT DOES NOT DECREASE WITH N
1
, CLOSE EMERG FUEL VALVE AND,
WHILE HOLDING POWER LEVER OFF, VENTILATE AFFECTED ENGINE UNTIL
TOT SUBSTANTIALLY DECREASES. MAINTENANCE ACTION IS REQUIRED BE-
FORE NEXT START.
TOT and N1 Monitor decreasing
Fuel pumps (4) Off
OIL COOL warning light (if installed) Check on below 20% N
Ro
Circuit breakers As required
All switches Off
Engine compressor rinse Perform as required

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