Tests verify APP 813-2=0
that a LOC frequency must be tuned to get APP logic.
512
22-11-01 Page 148 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. Jun 20/83
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 - Unpublished Work - See title page for details. 22-11-01 Page 149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.
512
22-11-01 Page 150 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. Jun 20/83
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 - Unpublished Work - See title page for details. 22-11-01 Page 151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
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737 AMM 飛機維護手冊 AUTO FLIGHT 自動飛行 1(89)
