CSP–900RFM206E–1
Normal Procedures
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
FAA Approved
Original
4–23
F
Lighting control panel:
F
F
LT MSTR
AS REQUIRED
F
F
CONSOLE/IIDS/FLOOD/INSTR
AS DESIRED
F
F
STROBE/POSN/AREA
AS DESIRED
F
Electrical master panel:
F
F
Avionics
AS DESIRED
F
F
L GEN and R GEN
ON (OFF FOR GPU
START)
F
F
POWER
OFF
F
Fuel system panel:
F
F
L BOOST AND R BOOST
OFF
F
F
LEFT/RIGHT FUEL SHUTOFF
ON; COVER CLOSED
F
Engine control panel:
F
F
L ENGINE and R ENGINE
OFF
ELECTRICAL POWER – ON
F
Electrical master panel:
F
F
POWER
BAT/EXT
F
IIDS:
F
F
Monitor BIT
FIRE WARNING ANNUNCIATORS
ON FOR 2 SECONDS; CHECK IIDS
FOR ADVISORIES
NOTE
:
Perform a commanded IIDS BIT if the helicopter has been statically exposed to
temperatures below 0
°
C for 12 hours or longer.
F
F
Fuel quantity display
CHECK
F
F
DISP (display by exception)
AS DESIRED
Содержание MD900 with PW206E
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