MD Helicopters MD900 with PW206E, Flight Manual

Page: 66 / 450

CSP–900RFM206E–1
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
Limitations
FAA Approved
Original
2–14
DURING OPERATIONS IN TEMPERATURES OF 13
_
F (–10
_
C)
OR COLDER, FUEL ADDED TO THE TANK MUST CONTAIN
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 VOLUME.
SEE FLIGHT MANUAL FOR MIXING PROCEDURES.
F92–020–2
STATIC PORT
KEEP HOLES AND
SURFACE CLEAN
NO STEP
USEABLE CAP. 158.5 U.S. GALS.
WITH RANGE EXTENDER INSTALLED
LOCATED ABOVE FUEL FILLER
LOCATED ABOVE FUEL FILLER
LOCATED ON RANGE EXTENDER FILLER
LOCATED ON RANGE EXTENDER FILLER
LOCATED ABOVE STATIC PORT
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 OPERATED
IN COMPLIANCE WITH THE OPERATING
LIMITATIONS SPECIFIED IN THE FAA
APPROVED ROTORCRAFT FLIGHT MANUAL
LOCATED ON INSTRUMENT PANEL
LOCATED ON INSTRUMENT PANEL
LOCATED ON INSTRUMENT PANEL
LOCATED ADJACENT TO ROTOR BRAKE
V
NE
CHART:
LOCATED ON INSTRUMENT PANEL
APPROVED FOR
VFR DAY/NIGHT
Figure 2–14. Decals and Placards (Sheet 2 of 2)