(c)
Push LSK 6R and make sure the CDU display shows ARM adjacent to 6R.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú
34-62-01
ú ú 05 Page 531 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
(d)
Use the CDU keyboard to put the correct MIN R/C CRZ value into the CDU scratch pad.
(e)
Push LSK 4R and make sure the CDU display shows the MIN R/C CRZ adjacent to LSK 4R.
S 825-035
(19) Do the minimum rate-of-climb (MIN R/C), engine out (ENG OUT) verification:
NOTE: The minimum rate-of-climb (MIN R/C), engine out (ENG
____ OUT) values are used to find the minimum rate of climb margin. They are also used to calculate the flight envelope at the engine out speed. Maximum altitude is calculated to make sure there is some more thrust available, equivalent to the minimum rate-of-climb values. These values can be different for each thrust level (CLB, CRZ and ENG OUT). The permitted entry range is 0-500 F.P.M (Feet Per Minute).
(a) Make sure the CDU display shows the PERF FACTOR 1/1 page.
CAUTION: MAKE SURE THAT YOU HAVE THE CORRECT VALUE BEFORE YOU DO
_______ THE ADJUSTMENT FOR THE MIN R/C ENG OUT. YOU CAN GET THE CORRECT VALUE OF MIN R/C ENG OUT FROM THE AIRLINE DEPARTMENT.
(b)
Use the CDU keyboard to put ARM into the CDU scratch pad.
(c)
Push LSK 6R and make sure the CDU display shows ARM adjacent to 6R.
(d)
Use the CDU keyboard to put the correct MIN R/C ENG OUT value into the CDU scratch pad.
(e)
Push LSK 5R and make sure the CDU display shows the MIN R/C ENG OUT adjacent to LSK 5R.
S 865-036
(20) Push the LSK adjacent to <INDEX to go back to FMCS BITE 1/1 page.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú
34-62-01
ú ú 03 Page 532 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
G. FMC/DAA Interface Test
S 715-104
(1)
Do the prepare for test in this task: "Operational Test - FMCS" if it is necessary.
S 285-126
(2)
Align the IRS (AMM 34-28-01/201).
S 825-105
(3)
Do the FMC/DAA Interface Test:
(a)
Push the INIT REF key on the CDU front panel to show the POS INIT or PERF INIT page.
(b)
Push the PROG key on the CDU keyboard to show the PROGRESS 1/3 page.
(c)
Put the AUTO/MAN switches, on the VHF NAV control panel, to the MAN position.
(d)
Make sure there is an M in front of the NAV tuner frequencies between LSKs 6L and 6R on the CDU display.
(e)
Turn the frequency select control, on the captain's VHF NAV control panel, to 115.80 Mhz.
(f)
Make sure the CDU display shows 115.80 between the LSKs 6L and 6R.
(g)
Turn the Captain's frequency control to 117.10 Mhz.
(h)
Make sure the CDU display shows 117.10 between the LSKs 6L and 6R.
(i)
Turn the frequency control, on the first officer's VHF NAV control panel, to 115.80 Mhz.
(j)
Make sure the CDU display shows 115.80 between the LSKs 6L and 6R.
(k)
Turn the First Officer's frequency select control to 117.50 Mhz.
(l)
Make sure the CDU display shows 117.50 between the LSKs 6L and 6R.
(m)
Put the captain's AUTO/MAN switch in the AUTO position.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 導(dǎo)航 NAVIGATION 5(109)
