CSP
−
902RFM207E
−
1
Limitations
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
FAA Approved
Reissue 2
Revision 4
2
−
17
f92
−
020
−
2B
DURING OPERATIONS IN TEMPERATURES OF 13
F
(-10
C)
OR COLDER, FUEL ADDED TO THE TANK MUST CON
TAIN
EITHER ANTI‐ICING ADDITIVE PFA‐55MB OR ANTI‐ICING
ADDITIVE PER MIL‐I‐27868 OR MIL‐I‐85470 WITH A
MINIMUM CONCENTRATION OF .06% BY VOLUME
AND A MAXIMUM CONCENTRATION OF .15% BY VOL
UME.
SEE FLIGHT MANUAL FOR MIXING PROCEDURES.
STATIC PORT
KEEP HOLES AND
SURFACE CLEAN
LOCATED ABOVE STATIC PORT
100 KT
CAPABIL
ITY
MODIFIED FITTING WITH DECALS
NO STEP
LOCATED ABOVE FUEL FILLER
LOCATED ABOVE FUEL FILLER
LOCATED ON FILLER NECK
LOCATED ON FILLER NECK
RADIO CALL
N X X X X X
ROTOR
BRAKE
LIFT HANDLE,
ROTATE CW,
PULL DOWN
DO NOT
ENGAGE ROTOR
BRAKE ABOVE
70% N
R
THIS HELICOPTER MUST BE OP
ERATED
IN COMPLIANCE WITH THE OPER
ATING
LIMITATIONS SPECIFIED IN THE FAA
APPROVED ROTORCRAFT FLIGHT
MANUAL
LOCATED ON INSTRUMENT PANEL
LOCATED ADJACENT TO ROTOR BRAKE
V
NE
CHART: LOCATED ON INSTRUMENT PANEL
APPROVED FOR
VFR DAY/NIGHT
LOCATED ON INSTRUMENT PANEL
LOCATED ON INSTRUMENT PANEL
USEABLE CAP. 158.5 U.S. GALS (600 LITERS)
WITH RANGE EXTENDER INSTALLED
USEABLE CAP. 158.5 U.S. GALS
WITH RANGE EXTENDER INSTALLED
Summary of Contents for MD900 Explorer
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