MD Helicopters MD900 with PW206E, Flight Manual

Page: 60 / 450

CSP–900RFM206E–1
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
Limitations
FAA Approved
Original
2–8
2–12.FUEL SYSTEM LIMITATIONS
Table 2–1. Fuel Specifications
PRIMARY FUELS
(1)
SECONDARY FUELS
(2)
Jet A (ASTM−D−1655) Jet B (ASTM−D−1655)
Jet A−1 (ASTM−D−1655) JP−4 (MIL−T−5624)
JP−5 (MIL−T−5624)
JP−8 (MIL−T−83133)
Notes:
(1). Using these primary fuels, the engine shall operate satisfactorily throughout the
altitude/temperature envelope (Ref. Figure 2−1).
Notes:
(2). Using these secondary fuels, the engine shall operate satisfactorily up to 10,000 FT
(Ref. Figure 2−1).
Additional fuel specifications may be found in Section VIII.
Maximum 140 KIAS low fuel warning tick mark ON.
During operations in temperatures of 13
_
F (−10
_
C) or colder, fuel added to the tank
must contain either anti−icing additive PFA555MB or anti−icing additive per
MIL5I527868 or MIL5I585470 with a minimum concentration of 0.06% by volume
and a maximum concentration of 0.15% by volume. Follow manufacturer’s instruc5
tions.
WARNING