CSP–900RFM206E–1
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
Normal Procedures
FAA Approved
Original
4–18
COCKPIT HEAT CONTROL
ESSENTIAL BUS
GCU
L
R
FUEL VLV
L
XFD
R
IIDS
FUEL
PROBE
AUDIO
PNL 1
NAV
COM 1
XPNDR
1
DIR
GYRO 1
XMSN
FIRE
PITOT
HEAT 1
BLD AIR
HEAT
ENG FIRE
L
R
LEAK
BLD AIR
TRIM
INST
FLOOD
STBY
ATT
5
7
5
5
5
5
5
5
5
5
5
7
7
VSCS
ENGINE CONTROL
OVSP TEST
L ENGINE
R ENGINE
OFF
IDLE FLY TRAIN
FUEL SYSTEM
L BOOST
R BOOST
ON
OFF
BOTTLE
PRI
ALT
LEFT OFF
RIGHT OFF
ON
OFF
FUEL SHUTOFF
DISCHARGE
O
F
F
ELECTRICAL MASTER
AVIONICS
L GEN
R GEN
POWER
ON
OFF
RESET
RESET
ON
ON
OFF
OFF
OFF
BAT/EXT
ESNTL
LIGHTING CONTROL
LT MSTR
CONSOLE
IIDS
FLOOD
INSTR
STROBE
AREA
POSN
ON
OFF
OFF
OFF
ON
OFF
ON
OFF
OFF
BOTH
CKP
CAB
IPS
HEAT
AC/VENT
PITOT
HEAT
HYD
TEST
OFF
ON
SYS 1
OVRD
SYS 2
COOL
LOW
COOL
HIGH
VENT
HIGH
VENT
LOW
OFF
OFF
OFF
ON
ON
L VSCS R
ON
OFF
TEST
CAB
F92E–029–1
KEY SWITCH
OFF
IDLE FLY TRAIN
UTILITY PANEL
5
5
LAND
LGT
10
NACA
INLET
CLOSE
NORMAL
UTILITY PANEL
NOTE: FOR
AIRCRAFT
WITH IPS
AND NACA
INLET
Figure 4–4. Switches and Circuit Breakers – Console Mounted (Typical)
Summary of Contents for MD900 with PW206E
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