User's Manual

ROCKWELL COLLINS
COMPONENT MAINTENANCE MANUAL with IPL
TDR-94, PART NO 622-9352
STEP PROCEDURE DESIRED RESULTS
e. Via the selected Control Input Data Bus, provide the
transponder with the appropriate labels and data indicated in
Figure 1023/GRAPHIC 34-50-96-99B-094-A01. Each data
parameter shall be updated at least once per second.
f. Interrogate the transponder with the Mode-S interrogation
indicated in Figure 1023/GRAPHIC 34-50-96-99B-094-A01 to
request BDS Register 0,8.
g. Verify that the transponder responds properly with a DF20
reply containing the exact structure for the ”MB” field indicated
in Figure 1023/GRAPHIC 34-50-96-99B-094-A01.
h. Connect TYPE_3 (F) (P1-23) discrete input to ground in
order to Select Aircraft Type Set B.
i. Connect TYPE_1 (F) (P1-21) discrete input to ground and
verify that TYPE_2 (F) (P1-22) and TYPE_0 (F) (P1- 20) are
in the open-circuit state in order to Select Aircraft Type 2, i.e.,
Lighter-than-Air.
j. Repeat Step f
k. Verify that the transponder responds properly with a DF20
reply containing the exact structure for the ”MB” field indicated
in Figure 1023/GRAPHIC 34-50-96-99B-094-A01.
9.8 AIS/ADSS Primary Data (-008 and -108 status TDR-94/94D)
a. Ensure that neither Air/Ground discrete inputs #1 or #2
(P2-53 or P1-27) are connected to ground (i.e., establishes
the airborne state).
b. Ensure that all GPS labels are removed from the GPS Input
Data Bus.
c. Ensure that all GPS labels are removed from the FMS/IRS
Input Data Bus.
d. Ensure that Configuration Select S0 discrete input (P1-28)
is in the open-circuit state.
e. Connect Configuration Select S1 discrete input (P1-17) to
ground to select configuration 2.
f. Via the AIS/ADS Input Data Bus, provide the transponder
with the appropriate labels and data indicated in Figure
1014/GRAPHIC 34-50-96-99B-032-A01. Each data
parameter must be updated at least once per second.
Final Performance (Customer Acceptance) Test. Cont.
Table 1001/Table 34-50-96-99A-009-A01
34-50-96
Page 1036.2
May 07/07