19.
ROLL CWS
20.
PITCH CWS
21.
EXTENDED MEMORY TEST
22.
AILERON AND SPOILER CONTROL
23.
ENG/DENG SYNCH
553
Sep 20/82 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 22-11-01 Page 107
5. BITE Test Library Chart (Cont) LIBRARY TEST (REF) TITLE
24.
ROLL ATTITUDE, RATE, DISENGAGE
25.
VOR O/C TIME CONSTANT
26.
APPROACH
27.
ELEVATOR CONTROL
28.
PITCH RATE, ATTITUDE, DISENGAGE
29.
STAB TRIM
30.
ALTITUDE RATE
31.
ALT ALERT (BARO for BA)
32.
CPU, MEMORY, INTERRUPTS
33.
ALPHA VANE
34.
FLAPS
35.
DADC ANALOG INTERFACES
36.
ACCEL INTERFACES
37.
RADIO ALTIMETER INTERFACE
38.
MCP PUSHBUTTONS
39.
MCP F/D SWITCHES
40.
MCP BANK ANGLE LIMIT SWITCH
41.
MCP IAS/MACH C/O SWITCH
42.
MCP SPEED KNOB
43.
MCP VERT SPEED KNOB
44.
MCP ALT SEL KNOB
45.
MCP VERT SPEED DISPLAY
46.
MCP ALTITUDE DISPLAY
47.
MCP COURSE DISPLAYS
48.
MCP HEADING DISPLAY
553
22-11-01 Page 108 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. May 20/82
5. BITE Test Library Chart (Cont) LIBRARY TEST (REF) TITLE
49.
MCP IAS/MACH DISPLAY
50.
ANN PANEL BLANK
51.
ANN PANEL A/T WARN (BA ONLY)
52.
ANN PANEL SPEED
53.
ANN PANEL PDC SPD
54.
ANN PANEL ALT ACQ
55.
ANN PANEL ALT HOLD
56.
ANN PANEL V/S
57.
ANN PANEL TO/GA
58.
ANN PANEL VNAV (provision)
59.
ANN PANEL PITCH CWS
60.
ANN PANEL A/P OFF
61.
ANN PANEL HDG SEL
62.
ANN PANEL NAV (provision)
63.
ANN PANEL VOR/LOC
64.
ANN PANEL G/S
65.
ANN PANEL ROLL CWS
66.
ANN PANEL SINGLE CHAN
67.
ILS DEV WARNING (DLH)
68.
ILS DEV WARNING (BA)
69.
HSI INTERFACE
70.
L NAV (Provisions)
5C9
Jun 20/83 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 22-11-01 Page 109
6. Flight Dir Symptom Tests Chart (Test Group 5 for A, 55 for B)
A. Selections
SYMPTOM/PIREP, FLIGHT DIR
B. Symptom Tests
LIBRARY DISPLAY TEST (REF) APPROX TOTAL TIME .1 1 DISCRETES 0 .2 50 BLANK ANN 5 .2 54 ALTACQANN 2 .2 55 ALT HOLD ANN 2 .2 56 V/S ARM/ENG ANN 5 .2 57 TO/GA ANN 2 .2 61 HDG SEL ANN 2 .2 62 L NAV ANN -.2 63 VOR/LOC ARM/ENG ANN 5 .2 64 G/S ARM/ENG ANN 5 .3 38 MCP PUSHBUTTONS 20 .4 39 MCP F/D SW 16 .5 43 MCP V/S KNOB 10 .6 44 MCP ALT SEL KNOB 10 .7 45 MCP V/S DISPLAY 26 .8 46 MCP ALT DISPLAY 30 .9 47 MCP COURSE DISPLAYS 35 .10 48 MCP HDG DISPLAY 25 .11 2 ADI 14 .12 6 ENG INTLKS 25
5C9
22-11-01 Page 110 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. Jun 20/83
6. Flight Dir Symptom Tests Chart (Test Group 5 for A, 55 for B) (Cont)
LIBRARY
DISPLAY TEST (REF) APPROX TOTAL TIME
.13 4 .14 9 D/A NAV RCVR 1 25
.15 13 DADC 429 1
.16 24 .17 28 .18 37 R ATT, RATE P ATT, RATE RAD ALT INTFC 12 31 0
.19 26 .20 30 APPROACH *[1] 169 ALT RATE 56
.21 35 DADC ANALOG INTFC 1
.22 36 ACCEL INTFC 1
.23 17 VG INTFC 1
.24 33 ALPHA VANE 1
.25 18 COMPASS INTFC 10
.26 8 DME 10
.27 70 L NAV -
___ 9.0 MIN
C. SURFACE TESTS
.27 34 FLAPS 21
.3 MIN
*[1] If BITE fails, on -114 FCC MOD A through D, with diagnostic; VOR/ILS 1 or (2); VG 1 or (2); MCP: ACCEL 1 or (2); FCC 1 of (2), enter engineering data mode (CLR-100 ENT) and repeat test. If test 2.33 subtest 2 (NOM-3.02 to -5.62) and 2.33 subtest 3 (NOM-.83 to -1.53) fail, ignore failure indication. Normal system operation can be ensured by performing Dual Channel Approach Test in AP/FD system A/T. 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(80)
