CSP
−
902RFM207E
−
1
Emergency and
Malfunction Procedures
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
FAA Approved
Reissue 2
Original
3
−
27
PITOT HEAT FAILURE
Indications:
Yellow pitot heat caution light (if installed)
PITOT
L
R
ON.
Conditions:
Flight conditions requiring use of pitot heat.
Procedures:
Left or right pitot heat failure.
Continue flight.
Procedures:
Left and right pitot heat failure.
Land as soon as practical.
3
−
11. ENGINE AND GENERATOR MALFUNCTION INDICATIONS
NOTE
:
Certain malfunctions may require an engine to be shutdown, however, the pilot
must assess the type of problem and decide if the affected engine is to remain
operational.
FIRE
CHIPS
%PSI
°
C
%LOAD
NG
GEN
ENGINE FIRE WARNING
ANNUNCIATOR (RED)
ENGINE CHIPS CAUTION
ANNUNCIATOR (YELLOW)
HIGH ENGINE OIL PRESSURE
CAUTION ANNUNCIATOR (YELLOW)
LOW ENGINE OIL PRESSURE
CAUTION ANNUNCIATOR (YELLOW)
WARNING ANNUNCIATOR (RED)
HIGH ENGINE OIL TEMPERATURE
WARNING ANNUNCIATOR (RED)
CAUTION ANNUNCIATOR
(YELLOW)
ENGINE LOW OIL TEMPERATURE
CAUTION ANNUNCIATOR (YELLOW)
N
G
HIGH
WARNING ANNUNCIATOR (RED)
N
G
HIGH
CAUTION ANNUNCIATOR (YELLOW)
GENERATOR OUT CAUTION
ANNUNCIATOR (YELLOW)
GENERATOR HIGH LOAD
CAUTION ANNUNCIATOR (YELLOW)
GENERATOR LOAD
DIGITAL DISPLAY (WHITE)
F92
−
025
N
G
LOW WARNING
ANNUNCIATOR (RED)
Figure 3
−
5. Engine and Generator Malfunction Annunciators
Summary of Contents for MD900 Explorer
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