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时间:2011-03-30 06:50来源:蓝天飞行翻译 作者:航空
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.16  47  MCP COURSE DISPLAY 
.17  48  MCP HDG DISPLAY 
.18  2  ADI TEST 
.19  3  MASI TEST 
.20  5  CWS INTLKS 
.21  6  ENG INTLKS 
.22  7  A/P DISENGAGE WARN 
.23  4  D/A 
.24  24  R ATT, RATE 
.25  28  P ATT, RATE 
.26  9  NAV RCVR INTERFACE s 
.27  13  DADC INTERFACE 
.28  14  MCP INTERFACE 
.29  10  SINGLE CHAN APP LOGIC 
.30  12  A/T INTERFACE 
.31  23  ENGAGE/DISENGAGE SYNC 
.32  37  RAD ALT INTERFACE 

512 
22-11-01 Page 136  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  Jun 20/88 


GROUND FUNCTIONAL TEST CHART
SUB  
TEST # DISP  LIBRARY  TESTS 
.33  26  APPROACH 
.34  30  ALT RATE 
.35  35  DADC ANALOG INTERFACE 
.36  36  ACCEL INTERFACE  
.37  19  ROLL CWS 
.38  20  PITCH CWS 
.39  25  VOR O/C TC 
.40  17  VG INTERFACE (INSTR SWITCHING) 
.41  18  COMPASS INTERFACE   
.42  33  ALPHA VANE        
.43  21  EXTENDED RAM TESTS 
.44  8  DME INTERFACE 
.45  70  L NAV (OPTIONAL)
 - INITIALIZATION 
.46  27  ELEV CONTROL 
.47  22  AILERON CONT 
.48  29  STAB TRIM 
.49  34  FLAPS 
.50  11  DUAL APP LOGIC 

5B8
Jun 20/88 22-11-01 Page 137
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.

BITE TEST RESULTS TABLE
Display No.  Library/Sub  Test No.  Nominal  LL  UL  Description  Notes 
Part of BITE  X-CHAN 
Initialization Tests.  TRANSN/RECVR INTERFACE 

16.1 H 0015 XBXFLG-0000 0015
16.2 H 0000
16.3 H AA95 XBCKS0-2AAA 5555
16.4 H 2AAA
16.5 H 5555 XBXT1X-0000 D055
16.6 H D055
16.7  H 0000 A/C user identification. Sync in and out per test and foreign channel.
NOTE:  This test is run whenever channel A/B test selected, or operator informs BITE that both FCCs are installed.
512 
22-11-01 Page 138  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  Jun 20/83 


BITE TEST RESULTS TABLE
Display
No. Library/Sub Test No. Nominal LL UL Description Notes

2.1 1 Discretes
1.1 H 0000  T-Pulse-Memory and CPU Check.
 1.2 810 MEM H 7F82*  TO/GA Sw, FGN CMD, FGN (CWS +
LOC   CMD), FGN First Up, LCL CWS, LCL CMD, DG Valid, VG Valid, APP O/C.
1.3 811 MEM H 3FFD* Gear Up, P Dual Cont, R/A Valid, Trim LOC Down, Trim Up.
1.4 812 MEM H DD76*  Ail Act Detent Pressure, R Dual Cont, R
LOC  CWS O/D, Valid LOC . A/P G/A,  R A/P G/A, LCL LOC Tuned,  Digital Intg Reset, Monitors Bypassed, h ≤ 400 ft, DADC Valid, Ail Act Eng, Squat Sw.
1.5 813 MEM H FDF6*  Elev Act Detent Pressure, APPROACH, P
LOC  CSW O/D, G/S ENG, P A/P G/A, Elev Act Eng, FLARE . APP
1.6 807 MEM H
LOC FFFF*

[1]
1.7 815 MEM H F7DF* NAV Interrupt, 28VDC Valid, A/S WARN LOC Reset, ILS DEV Reset, Trim Warn
RST = Reset
* Refer to the following bit data chart for identification of which discrete was failed.
*[1] These discretes are all "DON'T CARE" for the discrete input tests
512 
Oct 20/89  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  22-11-01 Page 139 


BITE TEST RESULTS TABLE BITE TEST RESULTS TABLE
Dis-play No.  Test Name 
2.1  Discretes 
Sub-test  Nominal  Data 
2  H 7F82 1 2 0XXX X1X1 BIT 15  3 X000 0  4 00X0  1 2 3 4  APP O/C (FF82) X X FGN (CMD+CWS) (7F8A)  X X X VG Valid 7B82 X DG VALID (7E82) LCL CMD LCL CWS FGN 1st Up (7FC2) (7FA2) (7F92) FGN X THROTTLE CMD (7F86) PALM SWITCH (7F83) 
3  H 3FFD 001X XX1X  XXXX  XX0X  1  Trim up (BFFD)  Trim down (7FFD)  R/A valid (1FFD) D ual  X X

 

 2 3  X X  X X  Cont. (3DFD) X  X 
4  X  X  Gear up (3FFF)  X 
4  H  DD76 
1X0X  1101  0X11  0X10  1 2  Squat Sw (5D76) DADC valid (D576)  X h 400 ft (D976)  Ail Act Eng (FD76) X Monitors Dig. Intg. Bypassed Reset (DC76) (DF76) 
 
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