CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Emergency and
Malfunction Procedures
FAA Approved
Reissue 2
Original
3
−
36
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
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:
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:
Continue flight
If other bypass indicator is displayed
LAND AS SOON AS POSSIBLE
Summary of Contents for MD900 Explorer
Page 4: ......
