737 AMM 飞机维护手册 AUTO FLIGHT 自动飞行 1(89)

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13.3  H 0021 H BAR 1 Label
13.4  H 6000 H BAR 1
13.5  H 00A1 MACH Label
13.6  H 6000 MACH
13.7  H 0061 CAS IN Label
13.8  H 6000 CAS IN
13.9  H 0011 TAS IN Label
13.10  H 6000 TAS IN
13.11  H 0051 H DOT Label
13.12  H 6000 H DOT
13.13  H 0009 H BAR 2 Label
13.14  H 6000 H BAR 2
13.15  H 00F1 Static Pressure Label
13.16  H 6000 Static Pressure
2.28 14  MCP Interface
14.1 H 009D MCPPD Label  MCP Discretes.
14.2  H 00DD MCPKD Label MCP Display Change.
2.29  10 Single Chan App Logic
10.1  H 0004 APP 813-2=1

Tests verify APP 813-2=0
that a LOC frequency must be tuned to get APP logic.
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BITE TEST RESULTS TABLE BITE TEST RESULTS TABLE BITE TEST RESULTS TABLE BITE TEST RESULTS TABLE BITE TEST RESULTS TABLE
Display  Library/Sub 
No.  Test No.  Nominal  LL  UL  Description  Notes 
2.29  10.3  H 0010  G/S ENG  813-4=1  Verifies that 
(Continued)  10.4  H 0000  G/S ENG  813-4=0  Vertical Beam 
removes G/S  Sensor must 
signal  see a small 
Beam to get 
G/S engage 
logic. 
10.5  H 0000  G/S ENG  813-4=0  Verified latch 
of VBS. 
10.6  0  -2.00  +2.00  B/A Lim  29  Verifies that 
Roll 
Command is 
disabled in 
A/P LOC cap 
mode. 
10.7  H 8000  APP O/C  810-15-1  APP O/C 
independent 
of R/A (RA 
1700 and RA 
invalid). 
10.8  0  -2.00  +2.00  B/A Lim  29  R/A valid does 
not produce 
roll CMD 
enable logic. 
10.9  H 8000  APP O/C  810-15=1  APP O/C 
independent 
of R/A (RA 
1700 and RA 
valid). 

512 
Jun 20/83  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  22-11-01 Page 149 

Display No.  Library/Sub Test No.  Nominal  LL  UL  Description  Notes 
2.29 (Continued)  10.10  0  -2.00  +2.00  B/A Lim  29  Latch function on capture. Function 10.6 
10.11  H 8000  APP O/C  810-15=1 
10.12  0  -2.00  +2.00  B/A Lim  29  VOR/LOC OR’ed with APP 
Logic in generating roll CMD enable. 
10.13  H 0000  APP O/C  810-15=0  Removal of APP Logic removes G/S ENG logic, thereby removing APP O/C. 
10.14  4.40  +2.24  +6.56  B/A Lim  29  Loss of LOC freq. Enable roll command. 
10.15  H 0000  APP O/C  810-15-0  APP O/C has not returned. 

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Display No.  Library/Sub Test No.  Nominal  LL  UL  Description  Notes 
2.29 (Continued)  10.16 10.17  4.40 H 8000  +2.24  +6.56  B/A Lim APP O/C   29 810-15=0  Roll command is enabled if APP Logic and VOR/LOC low, APP O/C is low. 
10.18  4.40  2.24  6.56  B/A Lim  29  Roll CMD remains enabled 
after applying APP Logic once CAPT latch is 
10.19 10.20  H 0000 H 0000  APP O/C LCL CMD  810-15=0 810-6=0  open. APP Logic does not generate APP O/C once latch is open. Loss NAV 
RCVR valid 
during APP O/C. Disengages AP. 

512 
Jun 20/83  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  22-11-01 Page 151 

Display  Library/Sub 
No.  Test No.  Nominal  LL  UL  Description  Notes 
2.29  10.21  4.40  2.24  6.56  B/A Lim  29  Roll CMD is 
(Continued)  enabled with AP 
disengaged, 
10.22  H 0000  APP O/C   810-15=0  APP O/C logic 
low. With AP 
disengaged. 
2.30  12 A/T Interface 
12.1  H 0000  THR at aft Lim  811-2=0  J2B-33 
12.2  H 0000  THR at EPR  811-3, -5=0  J2B-33, -55 
　
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