MD Helicopters MD900 with PW206E, Flight Manual

Page: 103 / 450

CSP–900RFM206E–1
Emergency and
Malfunction Procedures
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
FAA Approved
Original
3–33
SINGLE FUEL PROBE FAILURE
Indications: Digital fuel quantity indicator blanked.
Vertical fuel quantity segments indicate approximately half the remaining fuel
quantity.
Procedures:
NOTE
: Continuous display of fuel flow is available on the IIDS as a top level menu item:
L ENG WF XXX PPH
L ENG WF XXX PPH
F
Continue the flight using consumption and time calculations.
DUAL FUEL PROBE FAILURE
Indications: Digital fuel quantity indicator blanked.
Vertical quantity segments blanked.
NOTE
: The low fuel warning tick mark indication remains operational with a dual fuel
probe failure.
Procedures:
F
Continue the flight using consumption and time calculations.
NOTE
: Continuous display of fuel flow is available on the IIDS as a top level menu item:
L ENG WF XXX PPH
L ENG WF XXX PPH
IMPENDING FUEL FILTER BYPASS
Indications:
Impending bypass is shown by an inverted ‘‘U’’
above affected fuel flow line.
Procedures:
F
Continue flight
F
If other bypass indicator is displayed LAND AS SOON AS POSSIBLE