(c)
During this test, follow the instructions and push the LSK adjacent to <CONTINUE as shown on the CDU.
(d)
Make sure that the interactive test is completed with no failure.
NOTE: If a failure occurs, the test will stop and the TEST
____ FAILED indication will show on the CDU display.
INTERACTIVE TEST________________ GROUP NO./LIBRARY TEST NO.
IRU 60.01 VOR/ILS 60.02 ADI 60.08
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú
22-11-01
ú ú 07 Page 519 ú Jul 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
MACH/AS 60.09 LNAV 60.11 AFDS FMA 60.13 HSI HDG/CRS 60.14 SPEED TRIM 60.36 MCP PUSHBUTTON 60.50 MCP F/D SW 60.51 MCP C/O SW 60.52 MCP BNK LMT 60.53 MCP SPD KNOB 60.54 MCP ALT KNOB 60.55 *[2] MCP V/S KNOB 60.56 MCP DISPLAY 60.57 INTERLOCK 60.58 ILS DEV WARN 60.60 *[1] ALT ALERT 60.61 DISENGAGE 60.62 *[1] Ignore the question "ARE CPT AND F/O EADI G/S AND LOC
SCALES WHITE?" shown on the CDU display. Push the LSK adjacent to <YES. Ignore the question "ARE CPT AND F/O EADI G/S AND LOC SCALES YELLOW?" shown on the CDU display. Push the LSK adjacent to <YES.
*[2] AIRPLANES WITH -932 AND SUBSEQUENT MCP; Ignore the instruction "PUSH THE ALT SELECT KNOB" shown on the CDU display.
(e) If a failure occurs, do these steps:
1) From the CDU display, make a note of the test name, the channel, and the LRU that caused the failure.
NOTE: The number XX.YY at the far right on the second line
____ is the Group number and Library Test number. The first two digits are the Group number and the last two digits are the Library number.
2) If it is necessary to do the interactive test again, push the LSK adjacent to RERUN>.
3) To get the test result data, use the CDU keyboard to put the engineering code 100 into the scratchpad. Push the LSK 6R.
4) To get out of the test result data, push the E key on the CDU keyboard. Push the LSK 6R. 5) Push the LSK adjacent to <CONTINUE to continue the interactive test.
(f) If no failure occurs, the autopilot surface test will start automatically.
S 745-024
(3) Do the BITE ground functional surface test:
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú
22-11-01
ú ú 01 Page 520 ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
WARNING:_______ MAKE SURE THAT PERSONS AND BLOCKAGES ARE CLEAR OF ALL
CONTROL SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER.
AILERONS, RUDDER, ELVATORS, FLAPS, SLATS, SPOILERS,
LANDING GEAR, AND THRUST REVERSERS CAN MOVE QUICKLY WHEN
YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO
PERSONS AND EQUIPMENT.
(a)
Do the preparation steps as shown on the CDU display.
(b)
Follow the instructions and push the LSK adjacent to <CONTINUE as shown on the CDU.
(c)
Make sure that the surface test is completed with no failure.
NOTE: If a failure occurs, the test will stop and the TEST
____ FAILED indication will show on the CDU display.
SURFACE TEST____________ GROUP NO./LIBRARY TEST NO.
ELEVATOR 60.30 *[2]
AILERON 60.31
STAB TRIM 60.32 *[1]
MACH TRIM 60.33
FLAPS 60.34
DUAL TEST 60.35 *[3] *[4]
NOTE: Open EIS PRIMARY 1 and EIS PRIMARY 3 circuit
____ breakers when you do the DUAL TEST.
If -914 FCC mixed with -913 or -912 FCC, ignore the failure of subtests 32.S.24 and
32.S.25.
*[1] If library test 32 (stabilizer trim) fails, put the code 100 into the CDU scratch pad then push LSK adjacent to RERUN>. If subtests 32.S.5 thru 32.S.8 fail, go to the elevator rigging test 51.01 and set the stabilizer trim at A = +2.88 +/- 0.07 (ignore the UL and LL limits shown on the screen). Do the library test 32 again but do not move the stabilizer trim.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737-300 400 500 AMM 飞机维护手册 自动飞行 AUTOFLIGHT 1(123)
