|
| |
Back
Figure 9–68. Squat Switch System Components | Up
TM-1-1520-238-T-6 Army Model AH-64 Helicopter (NSN
1520-01-106-9519) (EIC: RHA) Manual | Next
9–6. CONTROLS AND INDICATORS (cont) |
TM 1-1520-238-T-6
9–70
9–3.
EQUIPMENT DATA
9–3
AC Electrical Power Generation System Produces:
2000 amperes for 0.050 seconds
1400 amperes for one second
1000 amperes for six seconds
Battery
Power rating . . . . . . . . . . . . . . . . . . . . . .
33 amperes for 12 minutes
Navigation Lights
Power requirement . . . . . . . . . . . . . . . .
28 VDC
Formation Lights
Power requirement . . . . . . . . . . . . . . . .
115 VAC, single phase
Anti-Collision Lights
Power requirement . . . . . . . . . . . . . . . .
115 VAC
Power supply output . . . . . . . . . . . . . . .
400 VDC anode voltage
200 VDC trigger voltage
Squat Switch
Power requirement . . . . . . . . . . . . . . . .
28 VDC
9–4.
EQUIPMENT CONFIGURATION
9–4
Not applicable.
9–5.
SAFETY, CARE AND HANDLING OF EQUIPMENT
9–5
Not applicable.
9–6.
CONTROLS AND INDICATORS
9–6
The electrical system is controlled by switches in the pilot station (fig. 9–69) and provides fault signals to the
caution/warning/advisory system in both the pilot station and the CPG station (fig. 9–70). Table 9–1 provides a
listing of the controls, switches and indicators pertaining to the electrical system along with a description of their
function.
|
