CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Normal Procedures
FAA Approved
Reissue 2
Revision 1
4
−
18
NAV
COM 1
ESS
BUS R
GCU
R
ENG
FIRE R
XMSN
FIRE
FUEL
VLV R
PITOT
HEAT R
IIDS
VSCS
R
TRIM
AUDIO
AP/SAS
ALERT
INSTR
LTG
EADI
R
PRIMARY
NAV
COM 2
LDG
LT
AIR
DATA
CFU
AHRS 1
ESS
BUS L
GCU
L
ENG
FIRE L
FUEL
VLV RL
VSCS
L
R ESS BUS
L ESS BUS
FUEL
PROBE
GPS
BLD AIR
LEAK
STBY
ATT
AP/SAS
EHSI
R
CMPTR DISC
ACCEL
L DC BUS
R DC BUS
INSTR
FLOOD ANNUN
XPNDR
1
BLD AIR
HEAT
COCKPIT
HEAT
CONTROL
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
f927
−
006B
KEY SWITCH
OFF
IDLE FLY TRAIN
UTILITY PANEL
NOTE
HELICOPTERS WITH
IPS ONLY
STROBES
BOTH
RED
OFF
NACA
INLET
CLOSE
NORMAL
STROBES
RED
WHITE
OFF
Figure 4
−
4. Switches and Circuit Breakers
−
Console Mounted (Typical)
Summary of Contents for MD900 Explorer
Page 4: ......
