B KRA 405
Rev 6, June 2003 IM 006-00104-0006.dwd Page 1-3
TRANSMITTER OUTPUT:
Power:
Center Frequency:
Modulation Frequency:
Primary:
Secondary:
FM Deviation P-P:
Type of Service:
150 mW nominal, FMCW.
4300 +/- 15 MHz.
100 Hz nominal.
101 Hz nominal (in dual installation).
100 MHz.
Continuous.
WARNING SYSTEM:
FCS Warn:
Normal Operation:
Warn Condition:
Altimeter Valid
Normal Operation:
Warn Condition:
+20 to +32 Vdc at not greater than 100 mA.
Less that 10 uA.
+30 V no load (10 k ohms source impedance).
+20 V or less no load.
ALTITUDE TRIPS:
Tripped (Locked R/T):
Untripped (Unlocked R/T):
Less than +0.5 Vdc at not greater than 100 mA.
Less than 20 uA at not greater than +30 Vdc.
NOTES:
1. For Honeywell equipment refer to KDA 335, KPI 553A, KPI 553B, or KDI 573B manuals.
2. For Collins equipment refer to Collins manuals.
3. For Sperry equipment refer to Sperry manuals.
TABLE 1-1 KRA 405 Radar Altimeter Technical Characteristics
SPECIFICATION CHARACTERISTIC
RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION
UP536434