CSP
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E
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1
ROTORCRAFT FLIGHT MANUAL
Emergency and
Malfunction Procedures
MD 500E
(Model 369E)
Revision 14
3
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2
FAA Approved
3
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2. WARNING AND CAUTION INDICATORS
Warning and caution indicators are located at the top of the instrument panel
(Ref. Figure 3−1).
A red warning or yellow caution indicator will illuminate and in some cases,
an audible warning will sound announcing a failure or malfunction.
Audible and visual warnings are provided for:
ENGINE OUT
LOW ROTOR
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
ENGINE OUT AUDIBLE
WARNING HORN
(SEE NOTE)
CAUTION AND
WARNING LIGHTS
*OPTIONAL EQUIPMENT
NOTE:
ON LATER MODEL 369E HELICOPTERS,
ENGINE OUT AUDIBLE WARNING HORN
RELOCATED ADJACENT TO COCKPIT
UTILITY LIGHT ON MAP CASE PANEL.
F03
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011
1. ENGINE OUT
2. TRANSMISSION OIL PRESSURE
3. TRANSMISSION OIL TEMPERATURE
4. BATTERY TEMPERATURE 160
°
F
5. BATTERY TEMPERATURE 140
°
F
6. RE−IGN PRESS TO RESET
7. FUEL LEVEL LOW
8. FUEL FILTER
9. MAIN ROTOR TRANSMISSION CHIPS
10. TAIL ROTOR TRANSMISSION CHIPS
11. ENGINE CHIPS
12. GENERATOR OUT
13. AIR FRAME FILTER*
14. AIR FILTER CLOGGED*
15. FLOAT PRESS TO TEST*
16. PRESS TO TEST WARNING AND CAUTION LIGHTS
Figure 3
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1. Warning and Caution Indicators
