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pressure switch.
Automatic operation of the stabilator control unit has failed, or manual
control has been selected.
No. 1 engine nose gearbox oil contains metal fragments.
No. 1 engine nose gearbox oil pressure is below 26-30 psi.
No. 1 engine nose gearbox oil temperature is above 274 - 294°F
(135 -145°C).
Failed system.
Failed system or canopy temperature has exceeded limits.
No. 1 engine nose gearbox heater and engine inlet temperature sensors
are not at operating temperature. After reaching operating
temperature, indicates No. 1 engine anti-ice subsystem has failed.
No. 2 engine nose gearbox heater and engine inlet temperature sensors
are not at operating temperature. After reaching operating
temperature, indicates No. 2 engine anti-ice subsystem has failed.
I
Failed system.
Failed system.
Failed system.
Change 2 2-80.1/(2-80.2 blank)

TM 1-1520-238-10
Table 2-4. Pilot Caution/Warning Light Segments - continued
Word Segment
PRI HYD PSI
OIL LOW PRI HYD
OIL BYP PRI HYD
OIL PSI MAIN
XMSN 1
OIL HOT MAIN
XMSN 1
GEN 1
RECT 1
HOT RECT 1
SHAFT DRIVEN
COMP
PRI MUX
UTIL HYD PSI
OIL LOW UTIL HYD
OIL BYP UTIL HYD
OIL PSI MAIN
XMSN 2
OIL HOT MAIN
XMSN 2
GEN 2
RECT 2
HOT RECT 2
CANOPY
Color
AMBER
AMBER
AMBER
AMBER
AMBER
AMBER
AMBER
AMBER
AMBER
AMBER
AMBER
AMBER
AMBER
AMBER
AMBER
AMBER
AMBER
AMBER
AMBER
Illumination Parameter or Fault
Primary system hydraulic oil pressure is below 1250 psi.
Primary system hydraulic fluid is at minimum operating level.
A pressure differential of 60 to 80 psi has been detected in either the
pressure or return filter of the primary hydraulic system. The return
filter will bypass; the pressure filter will not.
Main transmission No. 1 system pressure is below 26-30 psi.
Main transmission No. 1 oil system temperature is above 274°- 294 °F
(135° -145 °C).
No. 1 generator is not on line.
Transformer-rectifier has failed, or there is no ac input to the rectifier.
Temperature 190 °F (87 °C) at transformer-rectifier is excessive.
Rectifier fan has probably failed.
Shaft driven compressor oil temperature is above 340°- 360 °F
(171° -182 °C); or shaft driven compressor pressurized air output is
less than 5-9 psi. No 1 engine bleed air will automatically supply the
pressurized air system if No. 1 engine is operating.
The selected multiplex bus controller has malfunctioned and the other
bus controller has assumed control of the multiplex bus. Light will
extinguish when the operating bus controller is selected with the MUX
switch on the CPG fire control panel.
Utility system hydraulic oil pressure is below 1250 psi.
Utility hydraulic fluid is at minimum operating level.
A pressure differential of 60 to 80 psid has been detected in either the
pressure or return filter of the utility hydraulic system. The return
filter will bypass; the pressure filter will not.
Main transmission No. 2 oil system pressure is below 26 - 30psi.
Main transmission No. 2 oil system temperature is above 274°- 294 °F
(135° -145 °C).
No. 2 generator is not on line.
Transformer-rectifier has failed, or there is no ac input to the rectifier,
Temperature 190 °F (87 °C) at transformer-rectifier is excessive.
Rectifier fan has probably failed.
Canopy doors are not properly closed.
2-81
TM 1-1520-238-10
Table 2-4. Pilot Caution/Warning Light Segments - continued
Word Segment
EXT PWR
HOT BAT
CHARGER
CHIPS MAIN XMSN
TEMP TR
CHIPS NOSE GRBX 2
OIL PSI NOSE GRBX 2
OIL HOT NOSE
GRBX 2
ASE
Color
AMBER
AMBER
AMBER
AMBER
AMBER
AMBER
AMBER
AMBER
AMBER
Illumination Parameter or Fault I
Access door to external power receptacle is open.
Battery temperature is in excess of 134 °F (57 °C), or a defective cell
has been detected. Battery charging is discontinued.
Charger has failed to charge during a programmed charging cycle.
Main transmission chip detector has detected metal fragments.
Tail rotor gearbox temperature is above 274°-294 °F (135° - 145 °C).
No. 2 engine nose gearbox oil contains metal fragments.
No. 2 engine nose gearbox oil pressure is below 26 - 30 psi.
No. 2 engine nose gearbox oil temperature is above 274°- 294 °F
(135° - 145 °C).
　
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