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SKY899 

Installation Manual 

 

Page 3-8 - Installation Checkout 

009-11900-001 

July 18, 2013 

 

Revision F 

 

Figure 3-4: Typical Patch Antenna Tripod Mount 

13.

 

From each test point (see step 12): 

a.  Position the TT391 Patch Antenna facing the SKYWATCH HP aircraft under test. 

b.  Set the TT391 POWER switch to the ON position. 

c.  Verify that the display shows, in the direction (± 30 degrees) of the TT391, two targets; a Traffic 

Advisory (i.e., a solid circle) at ¼ nm and Other Traffic (i.e., open diamond) at 4.5 nm. Both 
targets will be displayed in level flight at own aircraft altitude (i.e., "00" displayed above the 
traffic symbol). 

NOTES 

1.

 

If the display reflects a gross error in target bearing, check the 
directional antenna cables at TRC connectors J9 (sum port) and J11 
(difference port). They may be reversed. A further indication of this 
condition would be a target that moved in a counter-clockwise 
direction when the TT391 is moved in a clockwise direction. 

2.

 

Multiple targets or a faulty bearing may result from multipath 
distortion (see step 1). 

3.

 

During these tests, the SKY899 may detect and display other active 
targets. 

4.

 

To obtain a better line of sight, it may be necessary to elevate the patch 
antenna. 

d.  Set the TT391 POWER switch to the OFF. Repeat procedure from each test point. Step 15 can be 

done from the last test point. 

NOTE 

To prevent SKYWATCH HP from tracking the movement of the test-set, it 
is necessary to set the TT391 POWER switch to OFF after completing 
each bearing measurement. 

14.

 

Return the TT391 assemblies to their position in the aluminum carrying case. 

15.

 

Restart SKY899 by cycling power OFF and then ON. 

16.

 

Connect an oscilloscope to the suppression bus and verify that the SKY899 suppression pulse (100 

µ

±

µ

s) e15 V dc. If less than +15 V dc the suppression bus is overloaded. Check all 

equipment connected to the bus. Repair/replace the offending device. 

17.

 

Cycle power to the SKY899 and verify the standby screen appears after approximately 30 seconds. 
Press OPR soft-key (4) and verify the MSG label does not appear on the display after 10 seconds.  

NOTE 

The document reference is online, please check the correspondence between the online documentation and the printed version.

Summary of Contents for SKY899

Page 1: ... 2 All test equipment used in completing these tests shall be calibrated in accordance with the manufacturer s recommendations 3 This section provides checkout information for the SKY899 using the WX 1000 Display If using an alternate display use Appendix F for installation checkout 4 Checkout of the WX 1000 processor should be done in accordance with the procedures detailed in the WX 1000 Install...

Page 2: ...a Traffic Advisory i e a solid circle at nm and Other Traffic i e open diamond at 4 5 nm Both targets will be displayed in level flight at own aircraft altitude i e 00 displayed above the traffic symbol If the indications given in the following procedure except for the Flightline Tester are not obtained refer to the troubleshooting procedures in Chapter 4 If indications given for the Flightline Te...

Page 3: ...ge Calibration will be done during system setup verification and operation Figure 3 3 Standby Screen 3 3 1 System Setup The system configuration can be done using the service menu or it can be downloaded with a previously saved configuration using the Compact Flash Card Both setup procedures are described below and assume familiarity with service menu operation see chapter 4 for operation informat...

Page 4: ...d at a comfortable level then select exit to return to setup menu 5 From the Setup menu select ARINC 429 ports and manually configure each receiver channel Refer to paragraph 4 4 1 4 NOTES 1 It is possible for multiple data inputs barometric altimeter radio altimeter magnetic heading and GPS navigation from one source to be received on one channel e g ARINC 429 superbus Multiple data inputs will b...

Page 5: ...eturn to Service Menu e The Save or Revert menu will appear upon exiting setup menu Select Save Changes to keep current configuration Selecting Revert to Old Settings will cause system to exit the service menu without saving changes 7 To verify changes made to the configuration module turn the SKY899 OFF and then enter the Service Menu see paragraph 4 4 and repeat Step 6 8 Perform system setup ver...

Page 6: ...h altitude and heading sensor Verify data monitors show the correct input changes i e sensing of these signals b If the information is not correct the sensor has failed to communicate with the TRC Check operation of the sensor and connections between the TRC and sensor c Select exit until you return to the Service Menu 4 From the Service Menu select Ground Test see paragraph 4 4 4 5 From the Groun...

Page 7: ... to sub step f If the Flightline Tester AC Converter Power Supply is to be utilized proceed to sub step d d Connect the AC Converter Power Supply cable connector to the chassis external connector e Connect the AC Converter Power Supply input power cable connector to one of the following AC sources 115 Vac 60 Hz 115 Vac 400 Hz f Set the Flightline Tester POWER switches to the ON position g Verify t...

Page 8: ...path distortion see step 1 3 During these tests the SKY899 may detect and display other active targets 4 To obtain a better line of sight it may be necessary to elevate the patch antenna d Set the TT391 POWER switch to the OFF Repeat procedure from each test point Step 15 can be done from the last test point NOTE To prevent SKYWATCH HP from tracking the movement of the test set it is necessary to ...

Page 9: ...are cleared from the aircraft s instruments 2 Turn SKY899 ON The display should show a start up screen similar to one shown in Figure 3 2 3 After approximately thirty seconds observe the STANDBY screen and then press the TEST button soft key 2 4 The display should present a screen similar to that shown in Figure 3 5 Figure 3 5 Self Test Screen 5 If the SKY899 passes the self test the system will r...

Page 10: ...be connected to P1 89 AUDIO_H 2 150 ohm audio systems should be connected to P1 90 AUDIO_L 3 Audio common is connected to P1 91 AUDIO_C NOTE Audio output from the TRC is transformer isolated 7 If SKY899 fails the self test a The SKY899 Failed screen with an error message indicating the type of failure will be displayed b The voice message SKYWATCH SYSTEM TEST FAILED will be enunciated over the coc...

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