(p)
Use the CDU keyboard to put the memory location 3309 into scratchpad.
(q)
Push the LSK 6L.
(r)
Make sure that the data in the memory location 3309 on line 12 of the CDU display is 8XXX.
(s)
Use the CDU keyboard to put B into the scratchpad.
(t)
Push the LSK 6R to show the FCC memory contents of channel B.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú
22-11-00
ú ú 05 Page 536 ú Jul 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
(u)
Make sure that the data in the memory location 3309 on line 12 of the CDU display is 8XXX.
(v)
Use the CDU keyboard to put the memory location 3307 into scratchpad.
(w)
Push the LSK 6L.
(x)
Make sure that the data in the memory location 3307 on line 12 of the CDU display is XXFX.
(y)
Use the CDU keyboard to put the memory location 32FF into scratchpad.
(z)
Push the LSK 6L. (aa) Make sure that the data in the memory location 32FF on line 12 of the CDU display is XFXX.
(ab) Push the INIT/REF key on the CDU keyboard to get out of the BITE.
O. Baro Input Test
S 735-041
(1) Do the Baro Input Test:
(a)
Adjust the BARO set on the captain's and first officer's altimeter to the nearest 100-foot increment of the field elevation.
(b)
Adjust the MCP altitude to the same altitude as shown on the altimeters.
(c)
Adjust the captain's altimeter to 400 feet above the MCP altitude.
(d)
Set the captain's flight director to the ON position.
(e)
Make sure that ALT ACQ does not show on the captain's FMA.
(f)
Adjust the captain's altimeter to 200 feet above the MCP altitude.
(g)
Make sure that ALT ACQ shows on the captain's FMA.
(h)
Set the captain's flight director to the OFF position.
(i)
Adjust the captain's altimeter to 400 feet above the MCP altitude.
(j)
Adjust the first officer's altimeter to 400 feet above the MCP altitude.
(k)
Set the captain's flight director to the ON position.
(l)
Make sure that ALT ACQ does not show on the captain's FMA.
(m)
Adjust the first officer's altimeter to 200 feet above the MCP altitude.
(n)
Make sure that ALT ACQ does not show on the captain's FMA.
(o)
Set the captain's flight director to the OFF position.
(p)
Set the first officer's flight director to the ON position.
(q)
Make sure that ALT ACQ shows on the first officer's FMA.
(r)
Set the first officer's flight director to the OFF position.
(s)
Adjust the first officer's altimeter to 400 feet above the MCP altitude.
(t)
Set the first officer's flight director to the ON position.
(u)
Make sure that ALT ACQ does not show on the first officer's FMA.
(v)
Adjust the captain's altimeter to 200 feet above the MCP altitude.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú
22-11-00
ú ú 09 Page 537 ú Nov 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
(w)
Make sure that ALT ACQ does not show on the first officer's FMA.
(x)
Set the first officer's flight director to the OFF position.
P. Mach Trim Schedule Test
S 755-126
(1) Do the mach trim schedule test:
(a)
Connect the Pitot-Static Pressure test equipment to the DADC pitot-static source (AMM 34-11-00/501).
(b)
Set the voltmeter to the 15v dc scale.
(c)
Connect the (+) polarity of the voltmeter J6-37 and the (-) polarity of the voltmeter to J6-1 of the FCC-A Front Test Connector Breakout Box.
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本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊(cè) 自動(dòng)飛行 AUTOFLIGHT 1(60)
