BITE TEST RESULTS TABLE
Display Library/Sub
No. Test No. Nominal LL UL Description Notes
2.23 4 D/A
4.1 0.0 -0.8 0.8 Cruise CMD 83 Pitch
command
null reading.
4.2 0.0 -0.1 0.1 Bank Limiter 29 Roll
command
null reading.
4.3 0.0 -0.6 0.6 NORM 42 Versine null
Accel reading.
4.4 0.0 -0.1 0.1 A/D Wrap 87 D/A9-A/D87
4.5 3.87 3.47 4.25 Cruise CMD 83 Pitch
command
gradient.
4.6 3.15 2.68 3.62 Bank Limiter 29 Roll
command
gradient.
4.7 0.752 0.526 0.977 NORM 42 Versine
Accel gradient.
4.8 5.0 4.25 5.75 A/D Wrap 87 A/D Wrap
with signal.
2.24 24 Roll Att
Rate
24.1 -2.06 -2.77 -1.33 Prog. Roll 86 Roll Rate
Error Path
24.2 -1.35 -1.73 -0.93 R ATT Rate 26 Roll Bar left.
24.3 -3.18 -3.82 -2.54 R CMD 17 Roll attitude
path.
24.4 -1.7 92.0 -1.4 R ATT 18
24.5 2.54 1.78 3.32 R CMD 17 CWS roll
rate.
2.25 28 Pitch Att
Rate
28.1 5.36 3.82 6.90 APP INTG 81 Effect pitch
approach
mode only.
Pitch rate
circuitry
through
approach
path.
Jun 20/83 22-11-01
Page 145
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 - Unpublished Work - See title page for details.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
P Rate 28.2 -2.37 -3.08 -1.66 P Rate 20 Effect pitch approach mode only. Checks A/D 2D during above test 28.1.
28.3 3.87 2.9 4.84 Cruise CMD 83 Effect pitch cruise modes only. Pitch attitude and rate
circuitry in cruise path.
28.4 0.816 0.62 1.01 P ATT 44 Effect pitch cruise modes only. Checks A/D 44 during test 28.3.
28.5 -7.49 -9.74 -5.24 Value AMP 48 Effects all pitch cruise modes.
Checks cruise
CMD through the value amp.
28.6 1.15 0.92 1.61 Cruise CMD 83 Effects all pitch cruise modes g-limit at 150 Kts.
28.7 7.86 6.29 9.40 Cruise CMD 83 Effects all pitch cruise modes g-rate limit
28.8 3.83 3.06 5.36 Cruise CMD 83 Effects all pitch cruise modes g-limit at 600 Kts.
512
22-11-01 Page 146 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. Jun 20/83
Display No.
(Continued) Description
BITE TEST RESULTS TABLE
Library/Sub
Test No. Nominal LL UL
28.9 0.0 -0.30 0.30
9 9.1 9.2 Nav Receiver Interface 1.68 2.24 1.18 1.57 2.18 2.91
9.3 H 0040
9.4 H 00C0
9.5 9.6 9.7 FGN NAV RCVR Interface H 0040
9.8 H 00C0
Cruise CMD
GS BUF LOC BUF
GS Superflag VOR/LOC Superflag tuned to Localizer G/S BUF
LOC BUF G/S Superflag VOR/LOC Superflag tuned to localizer
Notes
83 Effects all pitch cruise modes. Elevator pressure discrete removed to go to high gain integrator.
41 G/S signal
1A VOR/LOC ATION Signal.
813-6=1 J1A-58.
812-6=1 J4A-30 812-7-1 J2A-59
41
1A
813-6=1
Tests foreign
812-6=1 nav switching
812-7=1 relay.
Jun 20/83 22-11-01
Page 147
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
BITE TEST RESULTS TABLE
Display Library/Sub No. Test No Nominal LL UL Description Notes
2.27 13 DADC Interface
13.1 H 00C1 ALT Label
13.2 H 6000 ALT Rec designation
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737 AMM 飞机维护手册 AUTO FLIGHT 自动飞行 1(88)
