23. ALL PITCH SYMPTOM Test Chart (Test Group 34 for A, 84 for B)
A. Symptoms Tests
DISP TEST .19 37 RAD ALT INTERFACE .20 30 ALT RATE .21 35 DADC ANALOG INTERFACE .22 36 ACCEL INTERFACE .23 20 PITCH CWS .24 17 V/G INTERFACE .25 33 ALPHA
B. Surface Tests
.26 27 ELEV CONTROL .27 29 STAB TRIM .28 34 FLAPS
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24. ALL ROLL SYMPTOM Test Chart (Test Group 35 for A, 85 for B)
A Symptom Tests
DISP TEST
.1 1   DISCRETES .2 50   BLANK ANN .2 61   HDG SEL ANN .2 62 LNAV .2 63   VOR LOC ARM/ENG ANN .2 65   CWS ROLL ANN .3 69 HSI .4 38   MCP PUSH BUTTONS .5 40   MCP BANK LIMIT SWITCH .6 47   MCP COURSE DISPLAY .7 48   MCP HEADING DISPLAY .8 5   CWS INTLKS .9 6   ENG INTLKS .10 4 D/A .11 24   R ATT, RATE .12 9 NAV RCVR INTERFACE .13 13   DADC INTERFACE .14 23  ENGAGE/DISENGAGE SYNC .15 19   ROLL CWS .16 25   VOR O/C TC .17 17   VG INTERFACE .18 18   COMPASS INTFC .19 8 DME .20 70 LNAV
5C9 22-11-01 Jun 20/83 Page 134C BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.

24. ROLL CRUISE Test Chart (Cont) (Test Group 35 for A, 85 for B) B. Surface Tests  DISP TEST  .21  22CONTROL       AILERON 
25. TEST OMEGA INTERFACE (Test Group 36)  DISP TEST  .1 1  .2  70      DISCRETES     LNAV 

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26.  Prepare for BITE Data Readout Presentation
A.  The operation of BITE provides diagnostic information to the LRU level. A detailed check is provided for checking faults to the logic bits and analog signals. This feature is enabled after BITE initialization by pressing CLR, selecting numerals 100 then pressing ENT. The PDU CDU lower line will display the value of the specific test involved.
B.  The following table provides the BITE TEST RESULTS in the same sequence as GROUND FUNCTIONAL TEST. NOTES on the charts refer to FCC connector and pins which are involved in the specific test or information on the signals involved. References are also provided for any observations which may be helpful in fault isolation. The description lists the specific type of test involved and provides listing of digital word and BIT which is involved.
C.  Use of test data should assist in system trouble shooting specifically for problems indicated for more than one LRU or involving inter system problems. The data provides the technician with added trouble shooting tools to enable more knowledgeable fault isolation in the most expeditious manner. The system will exit the test data made by pressing ENT on PDC CDU when the test requires a ENG (GO) signal to continue.
512 
Jun 20/84  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  22-11-01 Page 135 

GROUND FUNCTIONAL TEST CHART SUB TEST # DISP LIBRARY  TESTS
 - - INITIALIZATIONS 
.1  1  DISCRETES 
.2  50  BLANK ANN 
.2  51  A/T WARN ANN (OPTIONAL) (-114) (-214) (-314) 
.2  52  SPEED ANN 
.2  53  PDC SPD ANN 
.2  54  ALT ACQ ANN 
.2  55  ALT HOLD ANN 
.2  56  V/S ARM/ENG ANN 
.2  57  TO/GA ANN 
.2  59  CWS PITCH ANN 
.2  60  A/P OFF ANN 
.2  61  HDG SEL ANN 
.2  62  L NAV ANN (OPTIONAL) 
.2  63  VOR LOC ARM/ENG ANN 
.2  64  G/S ARM/ENG ANN 
.2  65  CWS ROLL ANN 
.2  66  SINGLE CHAN APP ANN 
.3  67/68  ILS DEV WARNING (OPTIONAL) 
.4  31  ALT ALERT 
.5  69  HSI 
.6  38  MCP PUSHBUTTONS (L NAV OPTIONAL) 
.7  39  MCP F/D SWITCHES 
.8  41  MCP C/O SWITCH 
.9  40  MCP B/A LIMIT SWITCH 
.10  42  MCP SPD CONTROL 
.11  44  MCP ALT SEL CONTROL 
.12  43  MCP V/S CONTROL 
.13  49  MCP IAS/MACH DISPLAY 
.14  46  MCP ALT SEL DISPLAY 
.15  45  MCP V/S DISPLAY 
　
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