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User Instructions

ManualsBrandsACSS an L-3 Communications and Thales ManualsElectronicsMode S Transponder
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SECURITY NOTATION SPEC
NO.
IT4061400-907
SEE PAGE INDEX
FOR THIS SHEET
REV LETTER
CAGE
CODE
58960
REV LTR
SEE THE TITLE PAGE FOR PROPRIETARY AND DATA RIGHTS NOTATIONS.
REV TEST SPECIFICATION PROCEDURE SPECIFICATION
LTR NO. OPR LIMITS C TEST DESCRIPTION SWITCH POS C WORK STEPS MFG LIMITS
AW/CRITICAL NOTATION
SUPPLEMENTS
70
SECURITY NOTATION PAGE
15101-000 (REV 970213 BCAS ASF5900/ENG_SPEC.DOT) (REV 07/18/2000 -OFC97-DATA SERVICES) HONEYWELL INTERNATIONAL INC.
ENGINEERING
SPECIFICATION
11.11 2.5 to 3.5 µs Measure and record the
reply delay. Delay shall
be as specified.
Observe the reply delay
field on the S-1403. Field
shall indicate as specified.
Record the value.
2.5 to 3.5 µs
ATCRBS Reply Power
ATCRBS Reply Power
11.12 N/A This test measures the
reply power.
N/A
11.13 250 to 630
Watts
Measure and record the
peak reply power of the
F1 pulse.
ATC-1400A
F2/P2
F1/P1: F1
On the ATC-1400A, select
the F1 pulse for power
detection. Observe and
record the XMTR PWR
display. Display shall
indicate as shown.
280 to 550
Watts
Select the ATCRBS F2
pulse for power detection.
S-1403
CONTROL
MENU 2,
Pulse Power
Gate: F2
On the S-1403, change
the pulse power gate
(PPG) field to F2.
11.14 250 to 630
Watts
Measure and record the
top antenna F2 pulse
power.
ATC-1400A
F2/P2
F1/P1: F2
On the ATC-1400A, select
the F2 pulse for power
detection. Observe and
record the XMTR PWR
display. This
measurement is the top
antenna F2 pulse power.
280 to 550
Watts
11.15 <1 dB Calculate and record the
absolute value of the
transmitter droop (in dB),
using the following
formula:
Droop = ABS [10(Log
10
P1 - Log
10
P2)], where P1
and P2 are the power
measurements taken in
tests 11.13 and 11.14,
respectively. The droop
shall not exceed the
specified limits.
Calculate and record the
absolute value of the
transmitter droop (in dB),
using the following
formula:
Droop = ABS [10(Log
10
P1 - Log
10
P2)], where P1
and P2 are the power
measurements taken in
tests 11.13 and 11.14,
respectively. The droop
shall not exceed the
specified limits.
<1 dB