Abbreviated (All–inclusive) Acceptance Tests
68P64115A18–1
Table 4-7: All RX ATP Test Procedure
Step
11
Action
NOTE
When testing diversity RX paths on companion frames, be sure to follow the RX test cable connection
information in Table 4-1 or Table 4-2, as applicable, during this step.
Follow cable connection directions as they are displayed, and click the Continue button to begin
testing.
– When the ATP process is completed, results will be displayed in the status report window.
12
Click the Save Results or Dismiss button.
NOTE
If Dismiss is used, the test results will not be saved in the test report file.
4-14
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Individual Acceptance Tests
68P64115A18–1
Individual Acceptance Tests
The following individual ATP tests can be used to evaluate specific
aspects of BTS operation against individual performance requirements.
All testing is performed using the LMF GUI environment.
TX Testing
TX tests verify any given transmit antenna path and output power
control. All tests are performed using the external, calibrated test
equipment. All measurements are made at the appropriate BTS TX OUT
connector(s).
TX tests verify TX operation of the entire CDMA forward link using
selected BBXs assigned to respective sector antennas. Each BBX is
keyed up to generate a CDMA carrier (using both bbxlevel and BLO)
at the CDF file–specified carrier output power level.
RX Testing
RX testing verifies receive antenna paths for BBXs selected for the test.
All tests are performed using the external, calibrated test equipment to
inject a CDMA RF carrier with all zero longcode at the specified RX
frequency at the appropriate BTS RX IN connector(s).
RX tests verify RX operation of the entire CDMA reverse link using all
equipped MCCs assigned to all respective sector/antennas.
Individual Tests
Spectral Purity TX Mask
This test verifies that the transmitted CDMA carrier waveform generated
on each sector meets the transmit spectral mask specification (as defined
in IS–97) with respect to the assigned CDF file values.
Waveform Quality (Rho)
This test verifies that the transmitted Pilot channel element digital
waveform quality (rho) exceeds the minimum specified value in IS–97.
Rho represents the correlation between the actual and perfect CDMA
modulation spectrums. 1.0000 represents 100% (or perfect correlation).
Pilot Time Offset
The Pilot Time Offset is the difference between the communications
system test set measurement interval (based on the BTS system time
reference) and the incoming block of transmitted data from the BTS
(Pilot only, Walsh code 0).
Code Domain Power/Noise Floor
This test verifies the code domain power levels, which have been set for
all ODD numbered Walsh channels, using the OCNS command. This is
done by verifying that the ratio of PILOT divided by OCNS is equal to
10.2 + 2 dB, and, that the noise floor of all EVEN numbered “OFF”
Walsh channels measures < –27 dB for IS–95A/B and CDMA2000 1X
with respect to total CDMA channel power.
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Individual Acceptance Tests
68P64115A18–1
BTS FER
This test verifies the BTS receive FER on all traffic channel elements
currently configured on all equipped MCCs (full rate at one percent
FER) at an RF input level of –119 dBm on the main RX antenna paths
using operator–selected, CDF–equipped MCCs and BBXs at the site.
Diversity RX antenna paths are also tested using the lowest equipped
MCC channel element ONLY.
NOTE
There are no pass/fail criteria associated with FER readings
taken at levels below –119 dBm, other than to verify that the
FER measurement reflects changes in the RX input signal level.
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68P64115A18–1
TX Spectral Purity Transmit Mask Acceptance Test
TX Spectral Purity Transmit Mask Acceptance Test
Background
Overview – This test verifies the spectral purity of each
operator–selected BBX carrier keyed up at a specific frequency specified
in the current CDF. All tests are performed using the external, calibrated
test equipment controlled by the same command. All measurements are
made at the appropriate BTS TX antenna connector.
Test Patterns – There are four operator–selectable test patterns with
which this acceptance test can be performed. The patterns, along with the
channels tested and gain setting for each, are listed in Table 3-34. Refer
to “TX Calibration and the LMF” in the Bay Level Offset Calibration
section of Chapter 3 for more information on the test patterns.
Equipment Operation During Testing – At least one MCC must be
selected to perform the Standard, CDF Pilot, and CDF test patterns. For
these test patterns, forward links will be enabled for synch channel
(SCH), paging channel (PCH), and traffic channel (TCH) elements from
the selected MCC(s), as shown in Table 3-34. Gain will be set for the
applicable channels on each antenna as shown in the table. The
operator–selected BBXs will be keyed using a BLO–corrected bbxlvl
value to generate a CDMA carrier. RF output power, as measured at the
appropriate frame TX antenna connector, will be set to one of the
following depending on the operating frequency spectrum:
S 800 MHz: 33.5 dBm
S 1.9 GHz: 31.0 dBm
Test Measurements – The test equipment will measure and return the
attenuation level in dB of all spurious and IM products with respect to
the mean power of the CDMA channel measured in a 1.23 MHz
bandwidth, verifying that results meet system tolerances at the following
test points (see also Figure 4-2):
S For 800 MHz:
– At least –45 dB @ + 750 kHz from center frequency
– At least –45 dB @ – 750 kHz from center frequency
– At least –60 dB @ – 1980 kHz from center frequency
– At least –60 dB @ + 1980 kHz from center frequency
S For 1.9 GHz:
– At least –45 dB @ + 885 kHz from center frequency
– At least –45 dB @ – 885 kHz from center frequency
– At least –55 dB @ – 1980 kHz from center frequency
– At least –55 dB @ + 1980 kHz from center frequency
Redundant BBX Testing – The BBX will then de–key, and if selected,
the redundant BBX will be assigned to the current TX antenna path
under test. The test will then be repeated.
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TX Spectral Purity Transmit Mask Acceptance Test
68P64115A18–1
Spectral Purity TX Mask Acceptance Test
Follow the steps in Table 4-8 to verify the transmit spectral mask
specification on the TX antenna paths for the selected BBXs.
Table 4-8: Test Spectral Purity Transmit Mask
Step
Action
Set up the test equipment for TX acceptance tests per Table 4-3.
Select the BBXs to be tested.
If the Test Pattern to be used is Standard, CDFPilot, or CDF; select at least one MCC (Refer to
“Test Pattern Drop–down Pick List” on page 3-90.)
Click on Tests in the BTS menu bar, and select TX > TX Mask... from the pull–down menus.
Select the appropriate carrier(s) and sector(s) (carrier-bts#-sector#-carrier#) from those displayed in the
Channels/Carrier pick list.
NOTE
To select multiple items, hold down the Shift or Ctrl key while clicking on pick list items to select
multiple carrier(s)–sector(s).
Verify that the correct channel number for the selected carrier is shown in the Carrier # Channels
box. If it is not, obtain the latest bts–#.cdf (or bts–#.necf) and cbsc–#.cdf files from the CBSC.
NOTE
If necessary, the correct channel number may be manually entered into the Carrier # Channels box.
If at least one MCC was selected in Step 3, select the appropriate transfer rate (1 = 9600, 3 = 9600 1X)
from the drop–down list in the Rate Set box.
NOTE
The Rate Set selection of 3 is only available if 1X cards are selected for the test.
In the Test Pattern box, select the test pattern to use for the calibration from the drop–down list (refer
to “Test Pattern Drop–down Pick List” under “TX Calibration and the LMF” in the Bay Level Offset
Calibration section of Chapter 3).
Click OK to display a status bar followed by a Directions pop-up window.
10
Follow the cable connection directions as they are displayed, and click the Continue button to begin
testing.
– As the ATP process is completed, results will be displayed in a status report window.
11
Click the Save Results or Dismiss button.
NOTE
If Dismiss is used, the test results will not be saved in the test report file.
4-18
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TX Spectral Purity Transmit Mask Acceptance Test
68P64115A18–1
Figure 4-2: TX Mask Verification Spectrum Analyzer Display
Mean CDMA Bandwidth
Power Reference
.5 MHz Span/Div
Ampl 10 dB/Div
Center Frequency Reference
Attenuation level of all
spurious and IM products
with respect to the mean
power of the CDMA channel
– 1980 kHz
+ 1980 kHz
– 885 kHz
+ 885 kHz
– 750 kHz
Mar 2003
+750 kHz
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4-19
TX Waveform Quality (Rho) Acceptance Test
68P64115A18–1
TX Waveform Quality (Rho) Acceptance Test
Background
Overview – This test verifies the transmitted pilot channel element
digital waveform quality of each operator–selected BBX carrier keyed up
at a specific frequency specified in the current CDF. All tests are
performed using the external, calibrated test equipment controlled by the
same command. All measurements are made at the appropriate TX
antenna connector.
Equipment Operation During Testing – Pilot gain will be set to 262
for each antenna, and all TCH elements from the MCCs will be
forward–link disabled. The selected BBXs will be keyed up using both
bbxlvl and BLO to generate a CDMA carrier (with pilot channel
element only, Walsh code 0). RF output power is set at 40 dBm as
measured at the appropriate BTS TX antenna connector.
Test Measurements – The test equipment will measure and return the
pilot channel element digital waveform quality (rho) percentage,
verifying that the result meets the following specification:
Waveform quality (Rho) should be > 0.912.
Redundant BBX Testing – The BBX will then de–key, and if selected,
the redundant BBX will be assigned to the current TX antenna path
under test. The test will then be repeated for the redundant BBX.
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TX Waveform Quality (Rho) Acceptance Test
68P64115A18–1
Waveform Quality (Rho) Acceptance Test
Follow the steps in Table 4-9 to verify the pilot channel element
waveform quality (rho) on the TX antenna paths for the selected BBXs.
Table 4-9: Test Waveform Quality (Rho)
Step
Action
Set up the test equipment for TX acceptance tests per Table 4-3.
Select the BBXs to be tested.
Click on Tests in the BTS menu bar, and select TX > Rho... from the pull–down menus.
Select the appropriate carrier(s) and sector(s) (carrier-bts#-sector#-carrier#) from those displayed in the
Channels/Carrier pick list.
NOTE
To select multiple items, hold down the Shift or Ctrl key while clicking on pick list items to select
multiple carrier(s)–sector(s).
Verify that the correct channel number for the selected carrier is shown in the Carrier # Channels
box. If it is not, obtain the latest bts–#.cdf (or bts–#.necf) and cbsc–#.cdf files from the CBSC.
NOTE
If necessary, the correct channel number may be manually entered into the Carrier # Channels box.
Click OK to display a status bar followed by a Directions pop-up window.
Follow the cable connection directions as they are displayed, and click the Continue button to begin
testing.
– As the ATP process is completed, results will be displayed in a status report window.
Click the Save Results or Dismiss button.
NOTE
If Dismiss is used, the test results will not be saved in the test report file.
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TX Pilot Time Offset Acceptance Test
68P64115A18–1
TX Pilot Time Offset Acceptance Test
Background
Overview – This test verifies the transmitted pilot channel element Pilot
Time Offset of each operator–selected BBX carrier keyed up at a specific
frequency specified in the current CDF. All tests will be performed using
the external, calibrated test equipment controlled by the same command.
All measurements will be made at the BTS TX antenna connector.
Equipment Operation During Testing – The pilot gain will be set to
262 for each antenna and all TCH elements from the MCCs will be
forward–link disabled. The selected BBXs will be keyed using both
bbxlvl and BLO to generate a CDMA carrier (with pilot channel
element only, Walsh code 0). TX power output is set at 40 dBm as
measured at the TX output.
Test Measurements – The test equipment will measure and return the
Pilot Time Offset in ms, verifying that results meet the following
specification:
Pilot Time Offset should be within 3 ms of the target PT Offset
(zero ms).
Redundant BBX Testing – The BBX will then de–key, and if selected,
the redundant BBX will be assigned to the current TX antenna path
under test. The test will then be repeated for the redundant BBX.
NOTE
4-22
This test also executes and returns the TX Frequency and TX
Waveform Quality (rho) ATP tests, however, only Pilot Time
Offset results are written to the ATP test report.
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TX Pilot Time Offset Acceptance Test
68P64115A18–1
Pilot Time Offset Acceptance Test
Follow the steps in Table 4-10 to verify the Pilot Time Offset on the TX
antenna paths for the selected BBXs.
Table 4-10: Test Pilot Time Offset
Step
Action
Set up the test equipment for TX acceptance tests per Table 4-3.
Select the BBXs to be tested.
Click on Tests in the BTS menu bar, and select TX > Pilot Time Offset... from the pull–down menus.
Select the appropriate carrier(s) and sector(s) (carrier-bts#-sector#-carrier#) from those displayed in the
Channels/Carrier pick list.
NOTE
To select multiple items, hold down the Shift or Ctrl key while clicking on pick list items to select
multiple carrier(s)–sector(s).
Verify that the correct channel number for the selected carrier is shown in the Carrier # Channels
box. If it is not, obtain the latest bts–#.cdf (or bts–#.necf) and cbsc–#.cdf files from the CBSC.
NOTE
If necessary, the correct channel number may be manually entered into the Carrier # Channels box.
Click OK to display a status bar followed by a Directions pop-up window.
Follow the cable connection directions as they are displayed, and click the Continue button to begin
testing.
– As the ATP process is completed, results will be displayed in a status report window.
Click the Save Results or Dismiss button.
NOTE
If Dismiss is used, the test results will not be saved in the test report file.
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TX Code Domain Power/Noise Floor Acceptance Test
68P64115A18–1
TX Code Domain Power/Noise Floor Acceptance Test
Background
Overview – This test verifies the Code Domain Power and Noise Floor
of each operator–selected BBX carrier keyed at a specific frequency
specified in the current CDF. All tests are performed using the external,
calibrated test equipment controlled by the same command. All
measurements are made at the appropriate BTS TX antenna connector.
CDMA Channel Test Set–up – Pilot gain will be set to 262 for each
antenna and the selected MCCs will be configured to supply all
odd–numbered Walsh code traffic channel elements by enabling
Orthogonal Channel Noise Source (OCNS) on all odd MCC channel
elements (maximum 32 full rate channels with an OCNS gain of 81). All
even–numbered Walsh code traffic channel elements will not have
OCNS enabled, and are considered “OFF”. Selected MCCs will be
forward–link enabled for the antenna (sector) under test.
Equipment Operation During Testing – The BBX will be keyed up
using a BLO–corrected bbxlvl value to generate a CDMA carrier
consisting of pilot and OCNS channels. RF output power, as measured at
the appropriate frame TX antenna connector, is set at one of the
following values depending on the operating frequency spectrum:
S 800 MHz: 33.5 dBm
S 1.9 GHz: 31.0 dBm
Test Measurements – The test equipment will measure and return the
channel element power in dB of all specified Walsh channels within the
CDMA spectrum. Additional calculations will be performed to verify the
following parameters are met (refer to Figure 4-3 for graphic
representations):
S Traffic channel element power level will be verified by calculating the
ratio of Pilot power to OCNS gain of all traffic channels (root sum of
the square (RSS) of each OCNS gain divided by the Pilot power).
This value should be 10.2 dB + 2.0 dB.
S Noise floor (unassigned “OFF” even–numbered Walsh channels) is
verified to be < –27 dB for IS–95A/B and CDMA2000 1X with
respect to total CDMA channel power.
NOTE
When performing this test using the LMF and the MCC is an
MCC8E or MCC24E, the redundant BBX may fail or show
marginal performance. This is due to a timing mismatch that the
LMF does not address. Performing this test from the CBSC will
not have this timing problem.
Redundant BBX Testing – The BBX will then de–key, and if selected,
the redundant BBX will be assigned to the current TX antenna path
under test. The test will then be repeated for the redundant BBX. Upon
completion of the test, OCNS channels will be disabled on the specified
MCC channel elements.
4-24
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68P64115A18–1
TX Code Domain Power/Noise Floor Acceptance Test
Code Domain Power/Noise Floor Test
Follow the steps in Table 4-11 to verify the Code Domain Power/Noise
floor of each selected BBX carrier keyed up at a specific frequency.
Table 4-11: Test Code Domain Power/Noise Floor
Step
Action
Set up the test equipment for TX acceptance tests per Table 4-3.
Select the BBXs and MCCs to be tested.
Click on Tests in the BTS menu bar, and select TX > Code Domain Power... from the pull–down
menus.
Select the appropriate carrier(s) and sector(s) (carrier-bts#-sector#-carrier#) from those displayed in the
Channels/Carrier pick list.
NOTE
To select multiple items, hold down the Shift or Ctrl key while clicking on pick list items to select
multiple carrier(s)–sector(s).
Verify that the correct channel number for the selected carrier is shown in the Carrier # Channels
box. If it is not, obtain the latest bts–#.cdf (or bts–#.necf) and cbsc–#.cdf files from the CBSC.
NOTE
If necessary, the correct channel number may be manually entered into the Carrier # Channels box.
If at least one MCC was selected in Step 3, select the appropriate transfer rate (1 = 9600, 3 = 9600 1X)
from the drop–down list in the Rate Set box.
NOTE
The Rate Set selection of 3 is only available if 1X cards are selected for the test.
Click OK to display a status bar followed by a Directions pop-up window.
Follow the cable connection directions as they are displayed, and click the Continue button to begin
testing.
– As the ATP process is completed, results will be displayed in a status report window.
Click the Save Results or Dismiss button.
NOTE
If Dismiss is used, the test results will not be saved in the test report file.
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TX Code Domain Power/Noise Floor Acceptance Test
68P64115A18–1
Figure 4-3: Code Domain Analyzer CD Power/Noise Floor Display Examples
Pilot Channel
PILOT LEVEL
MAX OCNS
CHANNEL
8.2 dB
12.2 dB
MAX OCNS SPEC.
Active channels
MIN OCNS SPEC.
MIN OCNS
CHANNEL
MAX NOISE
FLOOR
MAXIMUM NOISE FLOOR:
< –27 dB FOR IS–95A/B AND
CDMA2000 1X
Inactive channels
Walsh 0 1 2 3 4 5 6 7
...
64
Code Domain Power/Noise Floor (OCNS Pass) Example
Pilot Channel
PILOT LEVEL
FAILURE – EXCEEDS
MAX OCNS SPEC.
8.2 dB
12.2 dB
MAX OCNS SPEC.
Active channels
FAILURE – DOES NOT
MEET MIN OCNS SPEC.
MIN OCNS SPEC.
FAILURE – EXCEEDS MAX
NOISE FLOOR SPEC.
MAXIMUM NOISE FLOOR:
< –27 dB FOR IS–95A/B AND
CDMA2000 1X
Inactive channels
Walsh 0 1 2 3 4 5 6 7
...
64
Code Domain Power/Noise Floor (OCNS Failure) Example
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RX FER Acceptance Test
68P64115A18–1
RX FER Acceptance Test
Background
Overview – This test verifies the BTS Frame Erasure Rate (FER) on all
TCHs currently configured on operator–selected MCCs (full rate at 1%
FER) at –119 dBm. All tests are performed using the external, calibrated
test equipment as the signal source controlled by the same command.
Measurements are made at the specified BTS RX antenna connection.
Equipment Operation During Testing – The pilot gain on each MCC
will be set to 262 for each TX antenna, and the forward link for all TCH
elements from the MCCs will be enabled. Appropriate BBX(s) must be
keyed in order to enable the RX receive circuitry. Operator–selected
BBXs will be keyed using only bbxlvl, to generate a CDMA carrier
with pilot channel element only. Transmit power output is set at –40
dBm. Test equipment output power is set so that the received power at
the BBX is –119 dBm. The final output power setting of the test
equipment takes into account the MPC type, BTS RF path losses, and
test cable losses. If selected, the redundant BBX will be assigned to the
current RX antenna paths under test.
Test Measurements – The LMF will prompt the MCC channel element
under test to measure all–zero longcode and provide the FER report on
the selected active MCC on the reverse link for the main and, if selected,
diversity RX antenna paths. Results are evaluated to ensure they meet
the following specification:
FER returned less than 1% and Total Frames measured is 1500
Redundant BBX Testing – After the test, the BBX and the test
equipment will be de–keyed to shut down the pilot signal and the active
channel element, respectively. If the redundant BBX was tested, BBXR
assignment to an active sector will also be reset.
Antenna Connections for Companion Frame RX Diversity Tests – At
a site equipped with companion frames, RX diversity for each
SC4812ET Lite frame is provided by the receive antennas for the
collocated companion frame. Because of this, performing FER on
companion frame diversity RX requires different RX test cable
connections than on a starter frame. When performing companion frame
diversity RX FER, use Figure 4-1 and Table 4-1 or Table 4-2 to
determine the correct location for the RX test cable connections.
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RX FER Acceptance Test
68P64115A18–1
FER Acceptance Test
Follow the steps in Table 4-12 to verify the FER on RX antenna paths
using selected MCCs and BBXs.
Table 4-12: Test FER
Step
Action
Set up the test equipment for RX acceptance tests per Table 4-3.
If a companion frame is being tested and either BOTH or DIV is to be selected in step NO TAG,
perform the additional test equipment set–up in Table 4-4 for the diversity RX portion of the ATP.
NOTE
If the LMF has been logged into the BTS with a different Multi–Channel Preselector setting than the
one to be used for this test, the LMF must be logged out of the BTS and logged in again with the new
Multi–Channel Preselector setting. Using the wrong MPC setting can cause a false test failure.
Select the BBXs and MCCs to be tested.
Click on Tests in the BTS menu bar, and select RX > FER... from the pull–down menu.
Select the appropriate carrier(s) and sector(s) (carrier-bts#-sector#-carrier#) from those displayed in the
Channels/Carrier pick list.
NOTE
To select multiple items, hold down the Shift or Ctrl key while clicking on pick list items to select
multiple carrier(s)–sector(s).
Verify that the correct channel number for the selected carrier is shown in the Carrier # Channels
box. If it is not, obtain the latest bts–#.cdf (or bts–#.necf) and cbsc–#.cdf files from the CBSC.
NOTE
If necessary, the correct channel number may be manually entered into the Carrier # Channels box.
Select the appropriate RX branch (Both, Main, or Diversity) in the drop–down list.
NOTE
If a companion frame with the inter–frame diversity RX cabling disconnected is being tested do not
select BOTH in this step. The RX main and diversity paths must be tested separately for this
configuration because each requires a different Multi–Coupler Preselector type to provide the proper
test signal gain.
In the Rate Set box, select the appropriate data rate (1=9600, 2=14400, 3=9600 1X) from the
drop–down list.
NOTE
The Rate Set selection of 2 is only available if non–1X cards are selected for the test.
The Rate Set selection of 3 is only available if 1X cards are selected for the test.
Click OK to display a status bar followed by a Directions pop-up window.
10
NOTE
When testing diversity RX paths on companion frames, be sure to follow the RX test cable connection
information in Table 4-1 or Table 4-2, as applicable, during this step.
Follow cable connection directions as they are displayed, and click the Continue button to begin
testing. As the ATP process is completed, results will be displayed in the status report window.
11
4-28
Click the Save Results or Dismiss button. If Dismiss is used, the test results will not be saved in the
test report file.
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Generating an ATP Report
68P64115A18–1
Generating an ATP Report
Background
Each time an ATP test is run, ATP data is updated and must be saved to
an ATP report file using the Save Results button to close the status
report window. The ATP report file will not be updated if the status
reports window is closed using the Dismiss button.
ATP Report
A separate report is created for each BTS and includes the following for
each test:
Test name
PASS or FAIL
Description information (if applicable)
BBX number
Channel number
Carrier number
Sector number
Upper test limit
Lower test limit
Test result
Time stamp
Details/Warning information (if applicable)
Follow the procedures in the Table 4-13 to view and create a printable
file for the ATP report.
Table 4-13: Generating an ATP Report
Step
Mar 2003
Action
Click on the Login tab (if not in the forefront).
Click on the desired BTS in the Available Base Stations pick
list to select it.
Click on the Report button.
If a printable file is not needed, click on the Dismiss button.
If a printable file is required, perform the following:
5a
– Select the desired file type (text, comma–delimited,
HTML) for the report file from the drop–down list at the
bottom of the screen.
5b
– Click the Save button to save the file.
–– The file will be saved in the selected format in the
bts–# folder for the BTS selected.
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Generating an ATP Report
68P64115A18–1
Notes
4-30
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Chapter 5
Leaving the Site
Mar 2003
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5-1
Updating Calibration Data Files
68P64115A18–1
Updating Calibration Data Files
After completing the TX calibration and audit, updated CAL file
information must be moved from the LMF Windows environment back
to the CBSC, a Unix environment. The following procedures detail
moving files from one environment to the other.
Copying CAL files from LMF to a Diskette
Follow the procedures in Table 5-1 to copy the CAL files from an LMF
computer to a 3.5 diskette.
Table 5-1: Copying CAL Files to a Diskette
Step
Action
With Windows running on the LMF computer, insert a disk into Drive A:\.
Launch the Windows Explorer application program from the Start > Programs menu list.
Select the applicable :\).
With Solaris versions of Unix, create a Unix–formatted version of the bts–#.cal file in the home
directory by performing the following:
. . . continued on next page
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Updating Calibration Data Files
68P64115A18–1
Table 5-2: Copying CAL Files from Diskette to the CBSC
Step
9a
Action
– Type the following command:
dos2unix /floppy/no_name/bts–#.cal bts–#.cal
Where: # = BTS number for which the CAL file was created
9b
– Press the Enter key.
NOTE
Other versions of Unix do not support the dos2unix command. In these cases, use the Unix cp
(copy) command. The copied files will contain DOS line feed characters which must be edited out
with a Unix text editor.
10
Type in ls –l *.cal and press the Enter key. Verify the CAL files have been copied.
– Verify all CAL files to be transferred appear in the displayed listing.
11
Type eject, and press the Enter key.
12
Remove the diskette from the workstation.
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Prepare to Leave the Site
68P64115A18–1
Prepare to Leave the Site
Removing External Test Equipment
Perform the procedure in Table 5-3 to disconnect the test equipment and
configure the BTS for active service.
Table 5-3: Remove External Test Equipment
Step
Action
n WARNING
Be sure no BBXs are keyed before performing this step. Failure to do so can result in personal injury
and damage to BTS LPAs.
Disconnect all external test equipment from all TX and RX connectors at the rear of the frame.
Reconnect and visually inspect all TX and RX antenna feed lines at the frame RF interface panel.
NOTE
Verify that all sector antenna feed lines are connected to the correct antenna connectors on the frame.
Crossed antenna cables will degrade call processing.
Reset All Devices and Initialize Site Remotely
Generally, devices in the BTS should not be left with data and code
loaded from the LMF. The configuration data and code loads used for
normal operation could be different from those stored in the LMF files.
By resetting all devices, the required data and code can be loaded from
the CBSC using the DLM when spans are again active.
To reset all devices and have the OMCR/CBSC bring up the site
remotely, perform the procedure in Table 5-4.
Table 5-4: Reset BTS Devices and Remote Site Initialization
Step
Action
Terminate the LMF session by following the procedures in Table 5-6.
Cycle BTS power off, as specified in Table 2-9 and Table 2-10, and on, as specified in Table 2-11 and
Table 2-12.
Reconnect spans by following the procedure in Table 5-7.
Notify the OMCR/CBSC to take control of the site and download code and data to the BTS.
Verify the CBSC can communicate with the GLIs.
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Prepare to Leave the Site
68P64115A18–1
Bringing Modules into Service with the LMF
NOTE
Whenever possible, have the CBSC/MM bring up the site and
enable all devices at the BTS.
If there is a reason code and/or data should or could not be loaded
remotely from the CBSC, follow the steps outlined in Table 5-5 as
required to bring BTS processor modules from OOS to INS state.
Table 5-5: Bring Modules into Service
Step
Action
In the LMF GUI environment, select the device(s) to be enabled by clicking on each one.
NOTE
S The MGLI and CSM must be INS_ACT (bright green) before an MCC can be enabled.
S Processors which must be enabled and the order of enabling are as follows:
1. MGLI
2. CSMs
3. MCCs
Click on Device in the BTS menu bar, and select Enable from the pull–down list.
– A status report window is displayed.
NOTE
If a BBX is selected, a transceiver parameters window is displayed to collect keying information. Do
not enable the BBX.
Click Cancel to close the transceiver parameters window, if applicable.
Click OK to close the status report window.
– The color of devices which successfully change to INS will change bright green.
Terminating LMF Session/Removing Terminal
Perform the procedure in Table 5-6 as required to terminate the LMF
GUI session and remove the LMF computer.
Table 5-6: Remove LMF
Step
Action
! CAUTION
Do not power down the LMF terminal without performing the procedure below. Corrupted/lost
data files may result.
Log out of all BTS sessions and exit LMF by clicking on File in the LMF window menu bar and selecting Logout and Exit from the pull–down list.
In the Windows Task Bar, click Start and select Shutdown.
Click Yes when the Shut Down Windows message appears
Wait for the system to shut down and the screen to go blank.
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Prepare to Leave the Site
68P64115A18–1
Table 5-6: Remove LMF
Step
Action
Disconnect the LMF terminal Ethernet port from the BTS frame.
Disconnect the LMF terminal serial port, the RS–232–to–GPIB interface box, and the GPIB
cables as required for equipment transport.
Connecting BTS T1/E1 Spans
Before leaving the site, connect any T1 or E1 span connectors removed
previously to allow the LMF to control the BTS. Refer to Table 5-7 and
Figure 3-2.
Table 5-7: Connect T1 or E1 Spans
Step
Action
Re–connect any disconnected span connectors to the Span I/O A and B boards.
If equipped, ensure the CSU is powered on.
Verify span status, ensuring the OMC–R/CBSC can communicate with the BTS.
Before Leaving the site
Be sure all requirements listed in Table 5-8 are completed before leaving
the site.
Table 5-8: Check Before Leaving the Site
Step
Action
When backup batteries are installed, all battery circuit breakers are ON (pushed in).
Both heat exchanger circuit breakers on the DC PDA are set to ON (pushed in), and the heat
exchanger blowers are running.
The External Blower Assembly (EBA) power cable is connected, and the EBA is running.
The MAP power switch is set to ON, and the POWER (green) LED is lighted.
The MAP TCP switch is set to ON.
The BATT TEST switch on the MAP is set to OFF, and the BATT. TEST (amber) LED is not lighted.
No alarm conditions are being reported to the CBSC with all frame doors closed.
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Chapter 6
Basic Troubleshooting
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6-1
Basic Troubleshooting: Overview
68P64115A18–1
Basic Troubleshooting: Overview
Overview
The information in this chapter addresses some of the scenarios likely to
be encountered by Customer Field Engineering (CFE) team members
while performing BTS optimization and acceptance testing. This
troubleshooting guide was created as an interim reference document for
use in the field. It provides “what to do if” basic troubleshooting
suggestions when the BTS equipment does not perform according to the
procedures documented in the manual.
Comments are consolidated from inputs provided by CFEs and
information gained from experience in Motorola labs and classrooms.
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Troubleshooting: Installation
68P64115A18–1
Troubleshooting: Installation
Cannot Log into Cell-Site
Table 6-1: Login Failure Troubleshooting Procedures
n Step
Action
If the MGLI LED is solid RED, it implies a hardware failure. Reset MGLI by re-seating it. If this
persists, install GLI card in MGLI slot and retry. A Red LED may also indicate no termination on
an external LAN connector (power entry compartment at rear of frame).
Verify that the span line is disconnected at the Span I/O card. If the span is still connected, verify
the CBSC has disabled the BTS.
Try to ‘ping’ the MGLI.
Verify the LMF is connected to the primary LAN (LAN A) at the LAN shelf below the SCCP
cage. If LAN A is not the active LAN, force a LAN switch to LAN A by following the procedure
in Table 6-2.
Verify the LMF was configured properly.
If a Xircom parallel BNC LAN interface is being used, verify the BTS-LMF cable is RG-58
(flexible black cable less than 2.5 feet in length).
Verify the external LAN connectors are properly terminated (power entry compartment at rear of
frame).
Verify a T-adapter is not used on LMF computer side connector when connected to the primary
LAN at the LAN shelf.
Try connecting to the Ethernet Out port in the power entry compartment (rear of frame). Use a
TRB–to–BNC (triax–to–coax) adapter at the LAN connector for this connection.
10
Re-boot the LMF and retry.
11
Re-seat the MGLI and retry.
12
Verify GLI IP addresses are configured properly by following the procedure in Table 6-3.
Table 6-2: Force Ethernet LAN A to Active State as Primary LAN
n Step
Action
If LAN A is not the active LAN, make certain all external LAN connectors are either terminated
with 50Ω loads or cabled to another frame.
If it has not already been done, connect the LMF computer to the stand–alone or starter frame, as
applicable (Table 3-5).
If it has not already been done, start a GUI LMF session and log into the BTS on the active LAN
(Table 3-6).
Remove the 50Ω termination from the LAN B IN connector in the power entry compartment at the
rear of the stand–alone or starter frame. The LMF session will become inactive.
Disconnect the LMF computer from the LAN shelf LAN B connector and connect it to the LAN A
connector.
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Troubleshooting: Installation
68P64115A18–1
Table 6-2: Force Ethernet LAN A to Active State as Primary LAN
n Step
Action
If the LAN was successfully forced to an active state (the cards in any cage can be selected and
statused), proceed to step 13.
With the 50Ω termination still removed from the LAN B IN connector, remove the 50Ω
termination from LAN B OUT connector. If more than one frame is connected to the LAN,
remove the termination from the last frame in the chain.
If the LAN was successfully forced to an active state (the cards in any cage can be selected and
statused), proceed to step 13.
With the 50Ω terminations still removed from LAN B, unseat each GLI card in each frame
connected to the LAN, until all are disconnected from the shelf backplanes.
10
Reseat each GLI card until all are reconnected.
11
Allow the GLIs to power up, and attempt to select and status cards in the CCP shelves. If LAN A
is active, proceed to step 13.
12
If LAN A is still not active, troubleshoot or continue troubleshooting following the procedures in
Table 6-1.
13
Replace the 50Ω terminations removed from the LAN B IN and OUT connectors.
Table 6-3: GLI IP Address Setting
n Step
Action
If it has not previously been done, establish an MMI communication session with the GLI card as
described in Table 3-10.
Enter the following command to display the IP address and subnet mask settings for the card:
config lg0 current
A response similar to the following will be displayed:
GLI2>config lg0 current
lg0: IP address is set to
DEFAULT (configured based on card location)
lg0: netmask is set to
DEFAULT (255.255.255.128)
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Troubleshooting: Installation
68P64115A18–1
Table 6-3: GLI IP Address Setting
n Step
Action
If the IP address setting response shows an IP address rather than “Default (configured
based on card location),” enter the following:
config lg0 ip default
A response similar to the following will be displayed:
GLI2>config lg0 ip default
_param_config_lg0_ip(): param_delete(): 0x00050001
lg0: ip address set to DEFAULT
If the GLI subnet mask setting does not display as “DEFAULT (255.255.255.128),” set it to
default by entering the following command:
config lg0 netmask default
A response similar to the following will be displayed:
GLI2>config lg0 netmask default
_param_config_lg0_netmask(): param_delete(): 0x00050001
lg0: netmask set to DEFAULT
Set the GLI route default to default by entering the following command:
config route default default
A response similar to the following will be displayed:
GLI2>config route default default
_esh_config_route_default(): param_delete(): 0x00050001
route: default gateway set to DEFAULT
NOTE
Changes to the settings will not take effect unless the GLI is reset.
When changes are completed, close the MMI session, and reset the GLI card.
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Troubleshooting: Installation
68P64115A18–1
Table 6-3: GLI IP Address Setting
n Step
Action
Once the GLI is reset, re–establish MMI communication with it and issue the following command
to confirm its IP address and subnet mask settings:
config lg0 current
A response similar to the following will be displayed:
GLI2>config lg0 current
lg0: IP address is set to
DEFAULT (configured based on card location)
lg0: netmask is set to
DEFAULT (255.255.255.128)
Repeat steps 1 through 7 for all remaining GLIs, including those in any additional,
inter–connected frames.
Cannot Communicate with Power Meter
Table 6-4: Troubleshooting a Power Meter Communication Failure
n Step
6-6
Action
Verify power meter is connected to LMF with GPIB adapter.
Verify cable connections as specified in Chapter 3.
Verify the GPIB address of the power meter is set to the same value displayed in the applicable
GPIB address box of the LMF Options window Test Equipment tab. Refer to Table 3-23 or
Table 3-24 and the Setting GPIB Addresses section of Appendix NO TAG for details.
Verify the GPIB adapter DIP switch settings are correct. Refer to Test Equipment Preparation
section of Appendix NO TAG for details.
Verify the GPIB adapter is not locked up. Under normal conditions, only 2 green LEDs must be
‘ON’ (Power and Ready). If any other LED is continuously ‘ON’, then cycle GPIB box power and
retry.
Verify the LMF computer COM1 port is not used by another application; for example, if a
HyperTerminal window is open for MMI, close it.
Reset all test equipment by clicking Util in the BTS menu bar and selecting Test Equipment >
Reset from the pull–down lists.
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Cannot Communicate with Communications System Analyzer
Table 6-5: Troubleshooting a Communications System Analyzer Communication Failure
n Step
Action
Verify analyzer is connected to LMF with GPIB adapter.
Verify cable connections as specified in Chapter 3.
Verify the analyzer GPIB address is set to the same value displayed in the applicable GPIB
address box of the LMF Options window Test Equipment tab. Refer to Table 3-23 or Table 3-24
and the Setting GPIB Addresses section of Appendix F for details.
Verify the GPIB adapter DIP switch settings are correct. Refer to Test Equipment Preparation
section of Appendix NO TAG for details.
Verify the GPIB adapter is not locked up. Under normal conditions, only 2 green LEDs must be
‘ON’ (Power and Ready). If any other LED is continuously ‘ON’, then cycle GPIB box power and
retry.
Verify the LMF computer COM1 port is not used by another application; for example, if a
HyperTerminal window is open for MMI, close it.
Reset all test equipment by clicking Util in the BTS menu bar and selecting Test Equipment >
Reset from the pull–down lists.
Cannot Communicate with Signal Generator
Table 6-6: Troubleshooting a Signal Generator Communication Failure
n Step
Action
Verify signal generator is connected to LMF with GPIB adapter.
Verify cable connections as specified in Chapter 3.
Verify the signal generator GPIB address is set to the same value displayed in the applicable GPIB
address box of the LMF Options window Test Equipment tab. Refer to Table 3-23 or Table 3-24
and the Setting GPIB Addresses section of Appendix NO TAG for details.
Verify the GPIB adapter DIP switch settings are correct. Refer to Test Equipment Preparation
section of Appendix NO TAG for details.
Verify the GPIB adapter is not locked up. Under normal conditions, only 2 green LEDs must be
‘ON’ (Power and Ready). If any other LED is continuously ‘ON’, then cycle GPIB box power and
retry.
Verify the LMF computer COM1 port is not used by another application; for example, if a
HyperTerminal window is open for MMI, close it.
Reset all test equipment by clicking Util in the BTS menu bar and selecting Test Equipment >
Reset from the pull–down lists.
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6-7
Troubleshooting: Download
68P64115A18–1
Troubleshooting: Download
Table 6-7: Troubleshooting Code Download Failure
n Step
Action
Verify T1 or E1 span is disconnected from the BTS at Site I/O boards (Figure 3-2).
Verify LMF can communicate with the BTS devices using the LMF Status function.
Communication with MGLI must first be established before trying to communicate with any other
BTS device. MGLI must be INS_ACT state (bright green).
Verify the target card is physically present in the cage and powered-up.
If the target card LED is solid RED, it implies hardware failure. Reset card by re-seating it. If LED
alarm persists, replace with same type of card from another slot and retry.
Re-seat card and try again.
If a BBX reports a failure message and is OOS_RAM, the code load was OK. Use the LMF
Status function to verify the load.
If the download portion completes and the reset portion fails, reset the device by selecting the
device and Reset.
If a BBX or an MCC remains OOS_ROM (blue) after code download, use the LMF
Device > Status function to verify that the code load was accepted.
10
If the code load was accepted, use LMF Device > Download > Flash to load RAM code into flash
memory.
Cannot Download DATA to Any Device (Card)
Table 6-8: Troubleshooting Data Download Failure
n Step
6-8
Action
Re-seat card and repeat code and data load procedure.
Verify the ROM and RAM code loads are of the same release by statusing the card. Refer to
Download the BTS section of Chapter G for more information.
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Troubleshooting: Download
68P64115A18–1
Cannot ENABLE Device
Before a device can be enabled (placed in service), it must be in the
OOS_RAM state (yellow in LMF display) with data downloaded to the
device. The color of the device on the LMF changes to green once it is
enabled.
The four device states that can be displayed by the LMF are:
Enabled (bright green, INS_ACT)
Stand–by (olive green, INS_SBY – redundant CSM and GLI only)
Disabled (yellow, OOS_RAM)
Reset (blue, OOS_ROM)
Table 6-9: Troubleshooting Device Enable (INS) Failure
n Step
Action
Re-seat card and repeat code and data load procedure.
If CSM cannot be enabled, verify the CDF has correct latitude and longitude data for cell site
location and GPS sync.
Ensure primary CSM is in INS_ACT (bright green) state.
NOTE
MCCs will not enable without the CSM being INS.
Verify 19.6608 MHz CSM clock is present; MCCs will not enable without it.
BBXs should not be enabled for ATP tests.
If MCCs give “invalid or no system time,” verify the CSM is enabled.
Log out of the BTS, exit the LMF, restart the application, log into the BTS, and re–attempt
device–enable actions.
LPA Errors
Table 6-10: LPA Errors
n Step
Action
If LPAs give continuous alarms, cycle power with the applicable DC PDA circuit breakers.
Establish an MMI session with the LPA (Table 3-10), connecting the cable to the applicable MMI
port on the ETIB.
2a
– Type alarms at the HyperTerminal window prompt and press Enter.
–– The resulting display may provide an indication of the problem.
2b
– Call Field Support for further assistance.
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Troubleshooting: Calibration
68P64115A18–1
Troubleshooting: Calibration
Bay Level Offset Calibration Failure
Table 6-11: Troubleshooting BLO Calibration Failure
n Step
Verify the power meter or communications system analyzer is configured correctly (see the Test
Equipment Set–up section of Chapter 3), and is connected to the proper BTS TX antenna
connector.
If a power meter is being used:
2a
– Re-calibrate the Power Meter and verify it is calibrated correctly with cal factors from the
power sensor (refer to Appendix F).
2b
– Verify the power sensor is functioning properly by checking it with the 1–mW (0 dBm) Power
Ref signal.
2c
– Verify communication between the LMF and Power Meter is working by checking that the
meter display is showing RES :
Verify the parameters in the bts–#.cdf file are set correctly for the BTS operating band as
follows:
For 1900 MHz:
Bandclass=1; Freq_Band=16
For 800 MHz:
Bandclass=0; Freq_Band=8
Verify that no LPA on the carrier is in alarm state (rapidly flashing red LED).
4a
6-10
Action
– If any are, reset the LPA(s) by pulling the applicable circuit breaker on the DC PDA, and,
after 5 seconds, pushing back in.
Verify GPIB adapter is not locked up. Under normal conditions, only 2 green LEDs must be ‘ON’
(Power and Ready). If any other LED is continuously ‘ON’, power-cycle (turn power off and on)
the GPIB Box and retry.
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Troubleshooting: Calibration
68P64115A18–1
Calibration Audit Failure
Table 6-12: Troubleshooting Calibration Audit Failure
n Step
Action
Verify the power meter or communications system analyzer is configured correctly (see the Test
Equipment Set–up section of Chapter 3), and is connected to the proper BTS TX antenna
connector.
If a power meter is being used:
2a
– Re-calibrate the Power Meter and verify it is calibrated correctly with cal factors from the
power sensor (refer to Appendix F).
2b
– Verify the power sensor is functioning properly by checking it with the 1–mW (0 dBm) Power
Ref signal.
2c
– Verify communication between the LMF and Power Meter is working by checking that the
meter display is showing RES :
3a
Verify that no LPA on the carrier is in alarm state (rapidly flashing red LED).
– If any are, reset the LPA(s) by pulling the applicable circuit breaker on the DC PDA, and,
after 5 seconds, pushing back in.
After calibration, the BLO data must be re-loaded to the BBXs before auditing. Click on the
BBX(s), and in the BTS menu bar select Device > Download >BLO.
Re-try the audit.
Verify GPIB adapter is not locked up. Under normal conditions, only 2 green LEDs must be ‘ON’
(Power and Ready). If any other LED is continuously ‘ON’, power-cycle (turn power off and on)
the GPIB Box and retry.
If calibration was being performed for the redundant BBX, be sure the Single–Sided BLO
checkbox was not checked in the CDMA Test Parameters test set–up window.
If additional items, such as directional couplers or combiners, have been installed in the TX path,
be sure that one of the following has been done:
S Verify BLO checkbox in the CDMA Test Parameters test set–up window is unchecked.
S The additional path losses have been added into each applicable sector using the Util > Edit >
TX Coupler Loss... function.
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Basic Troubleshooting: RF Path Fault Isolation
68P64115A18–1
Basic Troubleshooting: RF Path Fault Isolation
Overview
The optimization (RF path characterization or calibration) and
post-calibration (audit) procedures measure and limit-check the BTS
reported transmit and receive levels of the path from each BBX to the
back of the frame. When a fault is detected, it is specific to a receive or
transmit path. The troubleshooting process in this section determines the
most probable cause of the fault.
As the calibration and audit tests are performed, results are displayed in
the LMF test status report window. When faults are encountered, the test
procedure in progress continues running and displaying any further
faults. If it appears that there are major faults, the test can be aborted.
The test results can be saved to a bts–#.rpt file in the:\ and enter 10, to obtain an average Rho
value. This is an indication the GPS has not stabilized before going INS and may need to be
re-initialized.
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Troubleshooting: Transmit ATP
68P64115A18–1
Cannot Perform Code Domain Power and Noise Floor Measurement
Table 6-16: Troubleshooting Code Domain Power and Noise Floor Measurement Failure
n Step
Action
Verify presence of RF signal by switching to spectrum analyzer screen on the communications
system analyzer.
Verify PN offset displayed on analyzer is same as PN offset being used in the CDF file.
Disable and re-enable MCC (one or more MCCs based on extent of failure).
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Troubleshooting: Receive ATP
68P64115A18–1
Troubleshooting: Receive ATP
Multi–FER Test Failure
Table 6-17: Troubleshooting Multi-FER Failure
n Step
Action
Verify test equipment is configured correctly for a FER test.
Verify test equipment is locked to 19.6608 and even second clocks. On the HP 8921 analyzer, the
yellow LED (REF UNLOCK) must be OFF.
Verify MCCs have been loaded with data and are INS_ACT.
Disable and re-enable the MCC (1 or more based on extent of failure).
Disable, re-load code and data, and re-enable MCC (one or more MCCs based on extent of
failure).
Verify antenna connections to frame are correct based on the LMF directions messages.
For diversity RX FER failures in companion frame configurations, verify the following:
7a
– Inter–frame diversity RX cables are correctly connected between RX EXPANSION
connectors on each frame (refer to SC4812ET Lite Installation; 68P09253A36.
7b
– The RX test cable is connected to the correct RX antenna connector on the opposite
companion frame (refer to Table 4-1).
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Troubleshooting: CSM Check–list
68P64115A18–1
Troubleshooting: CSM Check–list
Problem Description
Many Clock Synchronization Manager (CSM) board problems may be
resolved in the field before sending the boards to the factory for repair.
This section describes known CSM problems identified in field returns,
some of which are field-repairable. Check these problems before
returning suspect CSM boards.
Intermittent 19.6608 MHz Reference Clock / GPS Receiver Operation
If having any problems with CSM board kit numbers, SGLN1145 or
SGLN4132, check the suffix with the kit number. If the kit has version
“AB,” then replace with version ‘‘BC’’ or higher, and return model AB
to the repair center.
No GPS Reference Source
Correct Hardware
Check the CSM boards for proper hardware configuration for the type of
GPS in use and the cage slot where they are installed.
RF–GPS (Local GPS) – CSM kit SGLN1145, which should be installed
in Slot l, has an on-board GPS receiver; while kit SGLN4132, in Slot 2,
does not have a GPS receiver.
Remote GPS (RGPS) – Kit SGLN4132ED or later, which should be
installed in both Slot 1 and Slot 2, does not have a GPS receiver.
Any incorrectly configured board must be returned to the repair center.
Do not attempt to change hardware configuration in the field. Also,
verify the GPS antenna is not damaged and is installed per recommended
guidelines.
RGPS Expansion Cabling
20–pair Punchblock Connections – For companion frame installations
with RGPS, verify the 20–pair punchblock RGPS distribution
connections in the RGPS expansion primary frame are correctly punched
down in accordance with NO TAG.
50–pair Punchblock Connections – For companion frame installations
with RGPS, verify the 50–pair punchblock RGPS distribution
connections in both the RGPS expansion primary and secondary frames
are correctly punched down in accordance with NO TAG and NO TAG.
Checksum Failure
The CSM could have corrupted data in its firmware resulting in a
non-executable code. The problem is usually caused by either electrical
disturbance, or interruption of data during a download. Attempt another
download with no interruptions in the data transfer. Return CSM board
back to repair center if the attempt to reload fails.
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Troubleshooting: CSM Check–list
68P64115A18–1
GPS Bad RX Message Type
This is believed to be caused by a later version of CSM software (3.5 or
higher) being downloaded, via LMF, followed by an earlier version of
CSM software (3.4 or lower), being downloaded from the CBSC.
Download again with CSM software code 3.5 or higher. Return CSM
board back to repair center if attempt to reload fails.
CSM Reference Source Configuration Error
This is caused by incorrect reference (clock) source configuration
performed in the field by software download. CSM kit SGLN1145 and
SGLN4132 must have proper reference sources configured, as shown in
Table 6-18, to function correctly.
Table 6-18: CSM Reference (Clock) Sources by GPS Type and Kit Number
GPS Type
RF GPS
REMOTE
GPS
CSM Kit No.
Hardware
Configuration
CSM
Slot No.
Reference Source Configuration
SGLN1145
With GPS Receiver
Primary = Local GPS
Backup = Either LFR or HSO
SGLN4132
Without GPS
Receiver
Primary = Mate GPS
Backup = Either LFR or HSO
SGLN4132ED
or later
Without GPS
Receiver
Primary = Remote GPS
Backup = Either LFR or HSO
Primary = Remote GPS
Backup = Either LFR or HSO
Takes Too Long for CSM to Come INS
This may be caused by a delay in GPS acquisition. Check the accuracy
flag status and/or current position. Refer to the CSM System Time/GPS
and LFR/HSO Verification section of Chapter 3. At least one satellite
should be visible and tracked for the “surveyed” mode, and four
satellites should be visible and tracked for the “estimated” mode. Also,
verify correct base site position data used in “surveyed” mode.
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6-19
Troubleshooting: SCCP Backplane
68P64115A18–1
Troubleshooting: SCCP Backplane
Introduction
The SCCP backplane is a multi–layer printed circuit board that
interconnects all the SCCP modules. The complexity of this board lends
itself to possible improper diagnoses when problems occur.
Connector Functionality
The following connector overview describes the major types of
backplane connectors along with the functionality of each. This will
assist the CFE to:
S Determine which connector(s) is associated with a specific problem
type.
S Isolate problems to a specific cable or connector.
Span Line Connector
The span line input is an 8 pin RJ–45 connector that provides a primary
and secondary (if used) span line interface to each GLI in the SCCP
shelf. The span line is used for MM/EMX switch control of the Master
GLI and also all the BBX traffic.
Power Input (Return A and B connectors)
Provides 27 volt input for use by the power supply modules.
Power Supply Module Interface
Each power supply module has a series of three different connectors to
provide the needed inputs/outputs to the SCCP backplane. These include
a VCC/Ground input connector, a Harting–style multiple pin interface,
and a +15V/Analog Ground output connector. The Transceiver Power
Module converts 27/48 Volts to a regulated +15, +6.5, +5.0 volts to be
used by the SCCP shelf cards.
GLI Connector
This connector consists of a Harting 4SU digital connector and a
6–conductor coaxial connector for RDM distribution. The connectors
provide inputs/outputs for the GLIs in the SCCP backplane.
GLI Ethernet “A” and “B” Connections
These SMB connectors are located on the SCCP backplane and connect
to the GLI board. This interface provides all the control and data
communications over the Ethernet LAN between the master GLI, the
redundant GLI, and the LMF.
BBX Connector
Each BBX connector consists of a Harting 2SU/1SU digital connector
and two 6–conductor coaxial connectors. These connectors provide DC,
digital, and RF inputs/outputs for the BBXs in the SCCP backplane.
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Troubleshooting: SCCP Backplane
68P64115A18–1
CIO Connectors
S RF RX antenna path signal inputs are routed through RX paths of the
DRDCs or TRDCs at the RF interface panel (rear of frame), and
through coaxial cables to the two MPC modules. The three “A” (main)
signals go to one MPC; the three “B” (diversity) to the other. The
MPC outputs the low–noise–amplified signals through the SCCP
backplane to the CIO where the signals are split and sent to the
appropriate BBX.
S A digital bus then routes the baseband signal through the BBX, to the
backplane, and then on to the MCC slots.
S Digital TX antenna path signals originate at the MCCs. Each output is
routed from the MCC slot through the backplane to the appropriate
BBX.
S TX RF path signal originates from the BBX, travels through the
backplane to the CIO, through the CIO, and then through
multi-conductor coaxial cabling to the trunking module and LPAs in
the LPA shelf.
SCCP Backplane Troubleshooting Procedure
The following tables provide standard procedures for troubleshooting
problems that appear to be related to a defective SCCP backplane. The
tables are broken down into possible problems and steps which should
be taken in an attempt to find the root cause.
NOTE
All steps in all tables should be followed before any attempt to
replace the SCCP backplane.
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6-21
Troubleshooting: SCCP Backplane
68P64115A18–1
Digital Control Problems
No GLI Control via LMF (all GLIs)
Table 6-19: No GLI Control Through LMF (All GLIs)
Step
Action
Check the Ethernet LAN for proper connection, damage, shorts, or opens.
Be sure the LAN IN and OUT connectors in the power entry compartment are properly terminated.
Be sure the proper IP address is entered in the Network Login tab of the LMF login screen.
Logout and Exit the LMF, restart the LMF, and re–login to the BTS.
Verify SCCP backplane Shelf ID DIP switch is set correctly.
Visually check the master GLI connectors (both module and backplane) for damage.
Replace the master GLI with a known good GLI.
No GLI Control through Span Line Connection (All GLIs)
Table 6-20: No GLI Control Through Span Line Connection (Both GLIs)
Step
Action
Verify SCCP backplane Shelf ID DIP switch is set correctly.
Verify that the BTS and GLIs are correctly configured in the OMCR/CBSC database.
Verify the span configurations set in the GLIs match those in the OMC–R/CBSC database (refer to
Table 6-31).
Visually check the master GLI connectors (both module and backplane) for damage.
Replace the master GLI with a known good GLI.
Check the span line cabling from the punchblock to the master GLI for proper connection and damage.
Table 6-21: MGLI Control Good – No Control Over Co–located GLI
Step
Action
Verify that the BTS and GLIs are correctly configured in the OMCR/CBSC data base.
Check the ethernet for proper connection, damage, shorts, or opens.
Visually check all GLI connectors (both module and backplane) for damage.
Replace the remaining GLI with a known good GLI.
No AMR Control (MGLI good)
Table 6-22: MGLI Control Good – No Control Over AMR
Step
Action
Visually check the master GLI connectors (both module and backplane) for damage.
Replace the master GLI with a known good GLI.
Replace the AMR with a known good AMR.
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Troubleshooting: SCCP Backplane
68P64115A18–1
No BBX Control in the Shelf
Table 6-23: MGLI Control Good – No Control over Co–located BBXs
Step
Action
Visually check all GLI connectors (both module and backplane) for damage.
Replace the remaining GLI with a known good GLI.
Visually check BBX connectors (both module and backplane) for damage.
Replace the BBX with a known good BBX.
No (or Missing) Span Line Traffic
Table 6-24: BBX Control Good – No (or Missing) Span Line Traffic
Step
Action
Visually check all GLI connectors (both module and backplane) for damage.
Replace the remaining GLI with a known good GLI.
Visually check all span line distribution (both connectors and cables) for damage.
If the problem seems to be limited to one BBX, replace the BBX with a known good BBX.
No (or Missing) MCC24E/MCC8E Channel Elements
Table 6-25: No MCC–1X/MCC24E/MCC8E Channel Elements
Step
Action
Verify channel elements on a co–located MCC of the same type (CDF MccType codes: MCC8E = 0;
MCC24E = 2; MCC–1X = 3)
Check MCC connectors (both module and backplane) for damage.
If the problem seems to be limited to one MCC, replace it with a known good MCC of the same type.
If no channel elements on any MCC, verify clock reference to CIO.
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6-23
Troubleshooting: SCCP Backplane
68P64115A18–1
DC Power Problems
WARNING
Potentially lethal voltage and current levels are routed to the
BTS equipment. This test must be carried out with a second
person present, acting in a safety role. Remove all rings, jewelry,
and wrist watches prior to beginning this test.
No DC Input Voltage to SCCP Shelf Power Supply
Modules
Table 6-26: No DC Input Voltage to Power Supply Module
Step
Action
Verify DC power is applied to the frame. Determine if any circuit breakers are tripped.
NOTE
If a breaker has tripped, remove all modules from the SCCP shelf and attempt to reset it.
– If breaker trips again, there is probably a cable or breaker problem within the frame or DC PDA.
– If breaker does not trip, there is probably a defective module or sub–assembly within the shelf.
Perform the tests in Table 2-3 to attempt to isolate the module.
Verify that the PS1 and PS2 circuit breakers on the DC PDA are functional.
Remove the frame rear access panel (Figure 2-2), and use a voltmeter to determine if the input voltage
is being routed to the SCCP backplane. Measure the DC voltage level between:
S The PWR_IN_A and PWR_RTN_A contacts on the extreme right side at the rear of the backplane
S The PWR_IN_B and PWR_RTN_B contacts on the extreme right side at the rear of the backplane
– If the voltage is not present, there is probably a cable or circuit breaker problem within the frame
or DC PDA.
If everything appears to be correct, visually inspect the PS1 and PS2 power supply module connectors.
Replace the power supply modules with known good modules.
If steps 1 through 4 fail to indicate a problem, an SCCP backplane failure has occurred (possibly an
open trace).
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Troubleshooting: SCCP Backplane
68P64115A18–1
No DC Voltage (+5, +6.5, or +15 Volts) to a Specific GLI,
BBX, or Switch Module
Table 6-27: No DC Input Voltage to any SCCP Shelf Module
Step
Action
If it has not been done, perform the steps in Table 6-26.
Inspect SCCP shelf module connectors (both module and backplane) for damage.
Replace suspect modules with known good module.
TX and RX Signal Routing Problems
Table 6-28: TX and RX Signal Routing Problems
Step
Action
Inspect all Harting cable connectors and backplane connectors for damage in all the affected board
slots.
Perform steps outlined in the RF path troubleshooting flowchart in Figure 6-1.
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Troubleshooting: RFDS
68P64115A18–1
Troubleshooting: RFDS
Introduction
The RFDS is used to perform Pre–Calibration Verification and
Post-Calibration Audits which limit-check the RFDS-generate and
reported receive levels of every path from the RFDS through the
directional coupler coupled paths. In the event of test failure, refer to the
following tables.
All Tests Fail
Table 6-29: RFDS Fault Isolation – All Tests Fail
Step
Action
Check the TX calibration equipment for proper operation by manually setting the signal generator
output attenuator to the lowest output power setting and connecting the output port to the spectrum
analyzer RF input port.
Set the signal generator output attenuator to –90 dBm, and switch on the RF output. Verify that the
spectrum analyzer can receive the signal, indicate the correct signal strength, (accounting for the cable
insertion loss), and the approximate frequency.
Visually inspect RF cabling. Make sure each directional coupler forward and reflected port connects to
the RFDS antenna select unit on the RFDS.
Check the wiring against the site documentation wiring diagram or the SC4812ET Lite Installation;
68P09253A36.
Verify any changes to the RFDS parameter settings have been downloaded.
Status the TSU to verify the TSIC and SUA software versions are correct.
Check to see that all RFDS boards show green on the front panel LED indicators. Visually check for
external damage.
If any board LEDs do not show green, replace the RFDS with a known–good unit. Re–test after
replacement.
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Troubleshooting: RFDS
68P64115A18–1
All RX and TX Paths Fail
If every receive or transmit path fails, the problem most likely lies with
the rf converter board or the transceiver board. Replace the RFDS with a
known–good unit and retest.
All Tests Fail on a Single Antenna
If all path failures are on one antenna port, forward and/or reflected,
make the following checks.
Table 6-30: RFDS Fault Isolation – All Tests Fail on Single Antenna Path
Step
Action
Visually inspect the frame internal RFDS cabling to the suspect TRDC or DRDC.
Verify the forward and reflected ports connect to the correct RFDS antenna select unit positions on the
RFDS ASU card. Refer to the RFDS installation manual for details.
Replace the RFDS with a known–good unit.
Replace the RF cables between the affected TRDC or DRDC and the RFDS.
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Module Front Panel LED Indicators and Connectors
68P64115A18–1
Module Front Panel LED Indicators and Connectors
Module Status Indicators
Each of the non-passive plug-in modules has a bi-color (green and red)
LED status indicator located on the module front panel. The indicator is
labeled PWR/ALM. If both colors are turned on, the indicator is yellow.
Each plug-in module, except for the fan module, has its own alarm
(fault) detection circuitry that controls the state of the PWR/ALM LED.
The fan TACH signal of each fan module is monitored by the AMR.
Based on the status of this signal the AMR controls the state of the
PWR/ALM LED on the fan module.
Module LED Status (except GLI2, CSM, BBX, MCC)
PWR/ALM LED
The following list describes the states of the module status indicator.
S Solid GREEN – module operating in a normal (fault free) condition.
S Solid RED – module is operating in a fault (alarm) condition due to
electrical hardware failure.
Note that a fault (alarm) indication may or may not be due to a complete
module failure and normal service may or may not be reduced or
interrupted.
DC/DC Converter LED Status Combinations
The PWR CNVTR has its own alarm (fault) detection circuitry that
controls the state of the PWR/ALM LED.
PWR/ALM LED
The following list describes the states of the bi-color LED.
S Solid GREEN – module operating in a normal (fault free) condition.
S Solid RED – module is operating in a fault (alarm) condition due to
electrical hardware problem.
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Module Front Panel LED Indicators and Connectors
68P64115A18–1
CSM LED Status Combinations
PWR/ALM LED
The CSMs include on-board alarm detection. Hardware and
software/firmware alarms are indicated via the front panel indicators.
After the memory tests, the CSM loads OOS–RAM code from the Flash
EPROM, if available. If not available, the OOS–ROM code is loaded
from the Flash EPROM.
S Solid GREEN – module is INS_ACT or INS_SBY no alarm.
S Solid RED – Initial power up or module is operating in a fault (alarm)
condition.
S Slowly Flashing GREEN – OOS_ROM no alarm.
S Long RED/Short GREEN – OOS_ROM alarm.
S Rapidly Flashing GREEN – OOS_RAM no alarm or
INS_ACT in DUMB mode.
Short RED/Short GREEN – OOS_RAM alarm.
Long GREEN/Short RED – INS_ACT or INS_SBY alarm.
Off – no DC power or on-board fuse is open.
Solid YELLOW – After a reset, the CSMs begin to boot. During
SRAM test and Flash EPROM code check, the LED is yellow. (If
SRAM or Flash EPROM fail, the LED changes to a solid RED and
the CSM attempts to reboot.)
Figure 6-2: CSM Front Panel Indicators & Monitor Ports
SYNC
MONITOR
PWR/ALM
Indicator
FREQ
MONITOR
FW00303
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Module Front Panel LED Indicators and Connectors
68P64115A18–1
FREQ Monitor Connector
A test port provided at the CSM front panel via a BNC receptacle allows
monitoring of the 19.6608 MHz clock generated by the CSM. When
both CSM 1 and CSM 2 are in an in-service (INS) condition, the CSM 2
clock signal frequency is the same as that output by CSM 1.
The clock is a sine wave signal with a minimum amplitude of +2 dBm
(800 mVpp) into a 50 Ω load connected to this port.
SYNC Monitor Connector
A test port provided at the CSM front panel via a BNC receptacle allows
monitoring of the “Even Second Tick” reference signal generated by the
CSMs.
At this port, the reference signal is a Transistor–Transistor Logic (TTL)
active–high signal with a pulse width of 153 nanoseconds.
MMI Connector
Behind front panel – only accessible when card is partially extended
from SCCP shelf slot. The RS–232 MMI port connector is intended to
be used primarily in the development or factory environment, but may
be used in the field for debug/maintenance purposes.
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68P64115A18–1
Module Front Panel LED Indicators and Connectors
GLI2 LED Status Combinations
The GLI2 module indicators, controls, and connectors are described
below and shown in Figure 6-3.
The indicators and controls consist of:
S Four LEDs
S One pushbutton
ACTIVE LED
Solid GREEN – GLI2 is active. This means that the GLI2 has shelf
control and is providing control of the digital interfaces.
Off – GLI2 is not active (i.e., Standby). The mate GLI2 should be
active.
MASTER LED
S Solid GREEN – GLI2 is Master (sometimes referred to as MGLI2).
S Off – GLI2 is non-master (i.e., Slave).
ALARM LED
S Solid RED – GLI2 is in a fault condition or in reset.
S While in reset transition, STATUS LED is OFF while GLI2 is
performing ROM boot (about 12 seconds for normal boot).
S While in reset transition, STATUS LED is ON while GLI2 is
performing RAM boot (about 4 seconds for normal boot).
S Off – No Alarm.
STATUS LED
S Flashing GREEN– GLI2 is in service (INS), in a stable operating
condition.
S On – GLI2 is in OOS RAM state operating downloaded code.
S Off – GLI2 is in OOS ROM state operating boot code.
SPANS LED
S Solid GREEN – Span line is connected and operating.
S Solid RED – Span line is disconnected or a fault condition exists.
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Module Front Panel LED Indicators and Connectors
68P64115A18–1
GLI2 Pushbuttons and Connectors
RESET Pushbutton – Depressing the RESET pushbutton causes a
partial reset of the CPU and a reset of all board devices. GLI2 will be
placed in the OOS_ROM state (blue).
MMI Connector – The RS–232MMI port connector is intended
primarily for development or factory use but may be used in the field for
debug/maintenance purposes.
Figure 6-3: GLI2 Front Panel Operating Indicators
LED
ALARM LED
ALARM
SPANS LED
SPANS
MASTER LED
ACTIVE
ACTIVE LED
STATUS
OFF − operating normally
ON − briefly during powerup when the Alarm LED turns OFF.
SLOW GREEN − when the GLI2 is INS (inservice)
RESET
All functions on the GLI2 are reset when pressing and releasing
the switch.
ALARM
OFF − operating normally
ON − briefly during powerup when the Alarm LED turns OFF.
SLOW GREEN − when the GLI2 is INS (inservice)
SPANS
OFF − card is powered down, in initialization, or in standby
GREEN − operating normally
YELLOW − one or more of the equipped initialized spans is receiving
a remote alarm indication signal from the far end
RED − one or more of the equipped initialized spans is in an alarm
state
MASTER
The pair of GLI2 cards include a redundant status. The card in the
top shelf is designated by hardware as the active card; the card in
the bottom shelf is in the standby mode.
ON − operating normally as active card
OFF − operating normally as standby card
MMI PORT
CONNECTOR
An RS232, serial, asynchronous communications link for use as
an MMI port. This port supports 300 baud, up to a maximum of
115,200 baud communications.
ACTIVE
Shows the operating status of the redundant cards. The redundant
card toggles automatically if the active card is removed or fails
ON − active card operating normally
OFF − standby card operating normally
MMI
MMI PORT
CONNECTOR
MASTER
RESET
RESET
PUSHBUTTON
STATUS
STATUS LED
OPERATING STATUS
FW00225
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Module Front Panel LED Indicators and Connectors
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BBX LED Status Combinations
PWR/ALM LED
The BBX2 and BBX–1X modules have their own alarm (fault) detection
circuitry that controls the state of the PWR/ALM LED.
The following list describes the states of the bi-color PWR/ALM LED
for both BBX2 and BBX–1X cards:
Solid GREEN – INS_ACT no alarm
Solid RED Red – initializing or power-up alarm
Slowly Flashing GREEN – OOS_ROM no alarm
Long RED/Short GREEN – OOS_ROM alarm
Rapidly Flashing GREEN – OOS_RAM no alarm
Short RED/Short GREEN – OOS_RAM alarm
Long GREEN/Short RED – INS_ACT alarm
MCC LED Status Combinations
The MCC24E and MCC–1X modules have bi–color LED indicators and
two connectors as described below. See Figure 6-4. Note that the figure
does not show the connectors because they are concealed by the
removable lens.
The LED indicators and their states are as follows:
PWR/ALM LED
S RED – fault on module
ACTIVE LED
S Off – module is inactive, off-line, or not processing traffic.
S Slowly Flashing GREEN – OOS_ROM no alarm.
S Rapidly Flashing Green – OOS_RAM no alarm.
S Solid GREEN – module is INS_ACT, on-line, processing traffic.
PWR/ALM and ACTIVE LEDs
S Solid RED – module is powered but is in reset or the Board Control
Processor (BCP) is inactive.
MMI Connectors
S The RS–232 MMI port connector (four-pin) is intended primarily for
development or factory use but may be used in the field for debugging
purposes.
S The RJ–45 Ethernet port connector (eight-pin) is intended primarily
for development use but may be used in the field for high data rate
debugging purposes.
. . . continued on next page
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Module Front Panel LED Indicators and Connectors
68P64115A18–1
Figure 6-4: MCC24 and MCC–1X Front Panel LEDs and LED Indications
PWR/ALM
PWR/ALM LED
LED
COLOR
PWR/ALM
RED
OFF – Operating normally
ON – Briefly during power–up and during
failure conditions
An alarm is generated in the event of a failure
LENS
(REMOVABLE)
ACTIVE
GREEN
RED
ACTIVE
ACTIVE LED
OPERATING STATUS
RAPIDLY FLASHING – Card is code–loaded but
not enabled
SLOW FLASHING – Card is not code–loaded
ON – Card is code–loaded and enabled (INS_ACT)
ON – 1) Briefly during power–up
2) Continuously during fault conditions
SLOW FLASHING (alternately with green) –
Concentration Highway Interface (CHI) bus
inactive on power–up
4812ETL0030–1
LPA LED Status Combinations
LPA Module LED
Each LPA module is provided with a bi–color LED on the ETIB module
next to the MMI connector. Interpret this LED as follows:
S GREEN — LPA module is active and is reporting no alarms (Normal
condition).
S Flashing GREEN/RED — LPA module is active but is reporting an
low input power condition. If no BBX is keyed, this is normal and
does not constitute a failure.
S Flashing RED — LPA is in alarm.
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Troubleshooting: Span Control Link
68P64115A18–1
Troubleshooting: Span Control Link
Span Problems (No Control Link)
Table 6-31: Troubleshoot Control Link Failure
n Step
Action
Connect the LMF computer to the MMI port on the applicable MGLI2/GLI2 as shown in
Figure 6-5.
Start an MMI communication session with the applicable MGLI2/GLI2 by using the Windows
desktop shortcut icon (refer to Table 3-10).
Once the connection window opens, press the LMF computer Enter key until the GLI2> prompt
is obtained.
At the GLI2> prompt, enter:
config ni current (equivalent of span view command)
The system will respond with a display similar to the following:
The frame format in flash
Equalization:
Span A – Default (0–131
Span B – Default (0–131
Span C – Default (0–131
Span D – Default (0–131
Span E – Default (0–131
Span F – Default (0–131
is set to use T1_2.
feet
feet
feet
feet
feet
feet
for
for
for
for
for
for
T1/J1,
T1/J1,
T1/J1,
T1/J1,
T1/J1,
T1/J1,
120
120
120
120
120
120
Ohm
Ohm
Ohm
Ohm
Ohm
Ohm
for
for
for
for
for
for
E1)
E1)
E1)
E1)
E1)
E1)
Linkspeed: Default (56K for T1 D4 AMI, 64K otherwise)
Currently, the link is running at the default rate
The actual rate is 0
NOTE
Defaults for span equalization are 0–131 feet for T1/J1 spans and 120 Ohm for E1.
Default linkspeed is 56K for T1 D4 AMI spans and 64K for all other types.
There is no need to change from defaults unless the OMCR/CBSC span configuration requires it.
The span configurations loaded in the GLI must match those in the OMCR/CBSC database for the
BTS. If they do not, proceed to Table 6-32.
Repeat steps 1 through 5 for all remaining GLIs.
If the span settings are correct, verify the edlc parameters using the show command.
Any alarm conditions indicate that the span is not operating correctly.
S Try looping back the span line from the DSX panel to the MM, and verify that the looped signal
is good.
S Listen for control tone on the appropriate timeslot from the Base Site and MM.
Mar 2003
Exit the GLI MMI session and HyperTerminal connection by selecting File from the connection
window menu bar, and then Exit from the pull–down menu.
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Troubleshooting: Span Control Link
68P64115A18–1
Figure 6-5: MGLI/GLI Board MMI Connection Detail
STATUS LED
STATUS
RESET ALARM SPANS MASTER MMI ACTIVE
To MMI port
RESET
Pushbutton
ALARM LED
SPANS LED
MASTER LED
MMI Port
Connector
ACTIVE LED
8–PIN
NULL MODEM
BOARD
(TRN9666A)
8–PIN TO 10–PIN
RS–232 CABLE (P/N
30–09786R01)
LMF
COMPUTER
RS–232 CABLE
COM1
OR
COM2
6-36
DB9–TO–DB25
ADAPTER
1X SC 4812T Lite BTS Optimization/ATP Software Release R2.16.1.x
DRAFT
Mar 2003
Troubleshooting: Span Control Link
68P64115A18–1
Set BTS Site Span Configuration
NOTE
Perform the following procedure ONLY if span configurations
loaded in the MGLI2/GLI2s do not match those in the
OMCR/CBSC data base, AND ONLY when the exact
configuration data is available. Loading incorrect span
configuration data will render the site inoperable.
Table 6-32: Set BTS Span Parameter Configuration
n Step
Action
If not previously done, connect the LMF computer to the MMI port on the applicable
MGLI2/GLI2 as shown in Figure 6-5.
If there is no MMI communication session in progress with the applicable MGLI2/GLI2, initiate
one by using the Windows desktop shortcut icon (refer to Table 3-10).
At the GLI2> prompt, enter:
config ni format
Source Exif Data:
File Type : PDF
File Type Extension : pdf
MIME Type : application/pdf
PDF Version : 1.3
Linearized : No
Modify Date : 2003:04:11 11:43:21-05:00
Create Date : 2003:04:11 11:42:57-05:00
Title : TLite
Author : Win32 user
Producer : Acrobat Distiller 5.0 (Windows)
Page Count : 178
