carenado c340 ii checklistfinal
TRANSCRIPT
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8/16/2019 Carenado C340 II Checklistfinal
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Carenado C340 II Checklist
PREFLIGHT INSPECTION
Control Lock(s)………………… REMOVE and STOW
Parking Brake ……………………………….……………SET
All Switches………………………………….………….. OFF
All Circuit Breakers………………………..……………ON
Landing Gear Switch.……………………..……..DOWN
Right Fuel Selector…………………..…..RIGHT MAINOxygen…………………………………CHECK QUANTITY
Battery Switch…………………..….…………………….ON
Fuel Gauges……………………..…..CHECK QUANTITY
Wing Flaps……………………………..…………….EXTEND
Left Fuel Selector……………………..……..LEFT MAIN
Trim Tab Controls (3)………………..……….NEUTRAL
Windows……………………………..CHECK for CRACKS
BEFORE STARTING THE ENGINES
Preflight Inspection…………………….……COMPLETE
Cabin Door……………………………….…………..CLOSED
Brakes……………………………………….….TEST and SET
Landing Gear Switch………………………………DOWN
Emergency Alternator Field Switch….............OFF
Alternate Avionics Power Switch………………..OFF
Circuit Breakers…………………………………………….IN
All Switches………………………………………………..OFF
Auxiliary Fuel Pump Switch.…….………………….OFF
Avionics Master Switch………………….……………OFF
Battery and Alternators…………………….…………ON
Altimeter and Clock…………………………………….SET
Annunciator Light Panel…………...PRESS-TO-TEST
Cabin Door Not Locked Light………………………OFF
Landing Gear Position Lights………………….GREEN
Cabin Air Controls…………………….….AS REQUIRED
Fuel Quantity…………………………….……………CHECK
Throttles……………………………….…ONE INCH OPEN
Propellers……………………….………..FULL FORWARD
Mixtures…………………………………….……..FULL RICH
Cowl Flaps……………………………………………….OPEN
Fuel Selectors
a. Left Engine – LEFT MAIN
b.
Right Engine – RIGHT MAIN
Pressurization Air Controls
c. PUSH IN
d. PULL OUT
Ram Air Control
e. PUSH IN (for pressurization)
f. PULL OUT (for ventilation)
Cabin Altitude – SET 500 FEET ABOVE
Alternate Air Controls – IN
STARTING ENGINES (Left Engine First)
Propeller…………………………..…………………..CLEAR
Magneto Switches……………………………..………ON
Engine…………………………………………….…….START
g.
Starter Button – PRESS
h.
Primer Switch
i. Left Engine – LEFT
ii. Right Engine – RIGHT
Auxiliary Fuel Pump……………………….……….LOW
Throttle…………………………….1000 to 1200 RPM
Oil Pressure………………………………………….10 PSI(minimum in 30 seconds in normal weather or 60 seconds in
cold weather. If no indication appears, shut down engine and
investigate.)
Right Engine…………………………………………START
Alternators………………………………………….CHECK
Wing Flaps………………………………………………..UP
Rotating Beacon……………………………………….ON
Avionics Master Switch…………………………….ON
Radios ……………………………………………………..SET
BEFORE TAKEOFF
1.
Brakes………………………………….……………SET
2. Engine Runup
a. Throttles – 1700 RPM
b. Alternators – CHECK
c. Magnetos – CHECK
150 RPM maximum drop with a maximum
differential of 50 RPM
d. Propellers – CHECK FEATHERING to 1200
RPM; return to high RPM (full forwardposition)
e. Engine Instruments – CHECK in GREEN ARC
f. Vacuum System – CHECK
(4.75 to 5.25 inches Hg)
g. Throttles – 1000 RPM
Flight Controls…….…CHECK FREE and CORRECT
Trim Tabs………………………………….………………SET
Cowl Flaps………………………………….………….OPEN
Alternate Air Controls………………….…..CHECK IN
Altimeters…………………………………..….………….ON
Fuel Selectors………………………….……….RECHECKa. Left Engine – LEFT MAIN
b. Right Engine – RIGHT MAIN
Wing Flaps………..………………….……AS REQUIRED
Fuel Quantity…………………………..……………CHECK
Flight Instruments and Radios……..…………….SET
Lights………………………………………….AS REQUIRED
Annunciator Panel…………………..…………….CLEAR
Auxiliary Fuel Pumps………………..………………..ON
Cabin Pressurization……………………………….PRESS
Brakes…………………………………………………RELEASE
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8/16/2019 Carenado C340 II Checklistfinal
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TAKEOFF
Power………..……..2700 RPM and FULL THROTTLE
Minimum Control Speed – 84 KIAS
Rotate at 91 KIAS
AFTER TAKEOFF
Brakes………………………….…APPLY MOMENTARILY
Landing Gear…………...........………….UP NO LIGHTS
Wing Flaps……………………….……………………………UP
Climb Speed……………………..………………….108 KIAS
Auxiliary Fuel Pumps……….………………. CHECK ON
CLIMB (normal)
Power…………………2450 RPM and 28.0 inches Hg
Airspeed…………………………………..115 to 140 KIAS
Mixtures…………………………………..…………..ADJUST
Cowl Flaps……………………………..…….AS REQUIRED
Auxiliary Fuel Pumps…………………..……………….ON(above 10,000 feet altitude to minimize vapor formation)
Cabin Altitude Control………………..……………….SET(after cabin pressure has stabilized). Reset cabin altitude control to
destination pattern altitude plus 500 feet (inner scale) or cruise altitude
plus 500 feet (outer scale) whichever gives the highest cabin altitude
Cabin Rate Control……………………………..……….SETto reach selected cabin altitude at approximately the same time that the
aircraft reaches cruise altitude
CRUISING
Cruise Power:
2100 to 2450 RPM and 17 to 28 inches Hg
Mixtures………………………………………..…………..LEANfor desired cruise fuel flow as determined by your power computer.
Recheck mixtures if power, altitude or OAT changes.
Cowl Flaps……………………………………..AS REQUIRED
Auxiliary Fuel Pumps
a. Main Tanks – ON (first 5 to 15 minutes to
minimize vapor formation)
b.
Auxiliary Tanks – OFF
c. Switching Tanks – LOW
Fuel Selectors
a.
Left Engine – LEFT MAIN
b. Right Engine – RIGHT MAIN
Cabin Altitude Control…………………….…………...SET(if cruising altitude changes). Reset cabin altitude control to destination
pattern altitude plus 500 feet (inner scale) or cruise altitude plus 500 feet
(outer scale) whichever gives the highest cabin altitude
Trim Tabs………………………………………………..ADJUST
DESCENT
Power……………………………………….……….AS REQUIRED
(Maintain sufficient power for pressurization requirements.)
Mixtures…………………………………………….……….ADJUSTfor smooth operation with gradual enrichment as altitude is lost.
Cowl Flaps……………………………………………..………CLOSE
Cabin Altitude Control……………………………..………..SETDuring the initial portion of the letdown, set the cabin altitude control to
pattern altitude plus 500 feet (inner scale)Cabin Rate Control………………..……………………………SETto reach selected cabin altitude (zero cabin pressure) at approximately the
same time as the aircraft reaches pattern altitude plus 500 feet
APPROACH
Fuel Selectors
a.
Left Engine – LEFT MAIN
b. Right Engine – RIGHT MAIN
Auxiliary Fuel Pumps……………………………….…………..ON
Alternate Air ControlS……………………….……….CHECK IN
Mixtures……………………………………….…………..FULL RICHor lean as required for smooth operation
BEFORE LANDING
Propellers……………………………….………..FULL FORWARD
Altimeters………………………………………….………………..SET
Wing Flaps…………………………………………………DOWN 15°below 160 KIAS
LANDING
Landing Gear………………………………..…………………DOWNbelow 140 KCAS
Cabin Differential Press…………………..……….………..ZERO
Wing Flaps…………………………………………………DOWN 45°below 140 KIAS
Minimum Multi-Engine Approach Speed – 94 KIAS
Minimum Single-Engine Control Speed – 84 KIAS
AFTER LANDING
Auxiliary Fuel Pumps………………………………….………LOW(during landing roll)
Cowl Flaps………………….………………….………………….OPENWing Flaps…………………………………….………………………UP
Transponder……….………………………………………………STBY