SURFACE TEST____________ GROUP NO./LIBRARY TEST NO.
ELEVATOR 60.30 *[4]
AILERON 60.31
STAB TRIM 60.32 *[1] *[2]
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737-300/400/500MAINTENANCE MANUAL
MACH TRIM 60.33
FLAPS 60.34
DUAL TEST 60.35 *[3] *[5]
NOTE: Pull "ENG 1 N1 C/B" or "ENG 2 N1 C/B" when you do
____ the DUAL TEST.
NOTE: If -914 FCC mixed with -913 or -912 FCC, ignore the
____ failure of subtests 32.S.24 and 32.S.25.
*[1] AIRPLANES WITH -911 FCC; Ignore the failure of test 60.32 if the subtests
32.S.30 and 32.S.31 cause the failure.
*[2] 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.
*[3] AIRPLANES WITH -911 FCC; For the Dual Test, the flaps must be down at the 1-unit position.
*[4] If library test 30 (Elevator) fails, put the code 100 into the CDU scratchpad then push LSK adjacent to RERUN>. If the result of subtests 30.S.19/20 and 30.S.22/23 is greater than or equal to 1.40, then ignore the failure of these subtests. If the result of these subtests is less than 1.40, do the rigging check of the pitch CWS sensor.
*[5] If library test 35 (Dual Test) fails, put the code 100 into the CDU scratchpad then push LSK adjacent to RERUN>. If the result of the subtests 35.S.18 and
35.S.38 is 1.0 plus or minus 0.25, then ignore the failure of these subtests.
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(d) 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 surface test again, push the LSK adjacent to the 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 the <CONTINUE to continue the surface test.
(e)
If no failure occurs, the CDU display shows *DFCS TEST PASSED*.
(f) 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(53)
