(g)
AFDS MCP CRS 2 DC
(h)
FLAP POS IND - T.E.
(i)
ENGINES - IDLE CONT
(j)
ENGINES - ENGINE NO. 1 - LEFT
(k)
ENGINES - ENGINE NO. 2 - LEFT
(l)
FUEL SYSTEMS - QTY
(m)
LANDING GEAR AIR/GND RELAY AND LIGHTS
S 865-078
(10) Close these circuits breakers on the P18-1 circuit breaker panel:
(a)
AUTO FLIGHT CONTROL - AFDS MCP DC
(b)
AUTO FLIGHT CONTROL - AUTOTHROTTLE - AC
(c)
AUTO FLIGHT CONTROL - AUTOTHROTTLE - DC
(d)
AUTO FLIGHT CONTROL SYS A - SNSR EXC AC
(e)
AUTO FLIGHT CONTROL SYS A - FCC DC
(f)
AUTO FLIGHT CONTROL SYS A - ENGAGE INTLK A
(g)
AUTO FLIGHT CONTROL SYS A - WARN LIGHT (BAT)
(h)
AUTO FLIGHT CONTROL SYS A - MACH TRIM-AC
(i)
AUTO FLIGHT CONTROL SYS A - MACH TRIM-DC
(j)
AUTO FLIGHT CONTROL SYS A - NO. 1 NAVIGATION - DME-1
(k)
NO. 1 NAVIGATION - RADIO ALTM-1
S 865-079
(11) Close these circuits breakers on the P18-2 circuit breaker panel:
(a)
NO. 1 INSTRUMENTS - DAA FMC NO. 1
(b)
NO. 1 INSTRUMENTS - DAA NO. 1 - FMC AC
(c)
NO. 1 INSTRUMENTS - DAA NO. 1 - IRS - AC
(d)
NO. 1 INSTRUMENTS - IRS - DAA NO. 1 - DC
(e)
NO. 1 INSTRUMENTS - IRS NO. 1 - AC
(f)
NO. 1 INSTRUMENTS - IRS NO. 1 - DC
(g)
NO. 1 INSTRUMENTS - INSTR XFR
(h)
AIRPLANES WITH DUAL FMC;
NO. 1 INSTRUMENTS - INSTR XFMR-1
(i)
AIRPLANES WITH EFIS;
NO. 1 INSTRUMENTS - EFIS - SYM GEN L
(j)
AIRPLANES WITH EFIS;
NO. 1 INSTRUMENTS - EFIS - CONT PANEL L
(k)
AIRPLANES WITH EFIS;
NO. 1 INSTRUMENTS - EADI
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22-31-00
ALL ú ú 13 Page 505 ú Jul 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
(l)
AIRPLANES WITH EFIS;
NO. 1 INSTRUMENTS - EHSI
(m)
NO. 1 AIR DATA - COMPUTER-1 - AC
(n)
NO. 1 AIR DATA - COMPUTER-1 - 26VAC
(o)
NO. 1 AIR DATA - AUTO XFMR
(p)
NO. 1 AIR DATA - MACH ASI (26 VAC)
S 865-080
(12)
Close all circuits breakers on the P18-2 circuit breaker panel found under the FMCS heading.
S 825-088
(13)
Align the IRS (AMM 34-28-00/201 or AMM 34-28-01/201).
S 865-093
(14)
AIRPLANES WITHOUT EFIS; Set the two HSI selector switches on the pilots' lightshield to the NAV position.
S 865-053
(15)
Push the INIT/REF key on the FMCS CDU for the POS INIT or the PERF INIT page.
S 865-054
(16)
Push LSK 6L (<INDEX) for the INIT REF INDEX page 1/1 on the CDU.
S 865-055
(17)
Push LSK 6R (MAINT>) for the MAINT BITE INDEX page 1/1 on the CDU.
S 865-057
(18)
Push LSK 3L (<A/T) for the A/T BITE test page 1/2.
NOTE: If the red A/T warning lights come on, the A/T computer is in
____ the BITE mode. If the red A/T warning lights do not come on, A/T BITE INOP is shown on the CDU. You must have these two conditions to get access to the A/T BITE:
-
The two engines are off.
-
The landing gear lever is in the down position.
D. Current Status Quick Tests
S 865-059
(1)
Do these steps to prepare for the Current Status Quick Test:
(a)
Make sure these circuit breakers are closed: 1) AFC SYS A - SNSR EXC AC (P18-1 circuit breaker panel) 2) FLAP POS IND - TE (P6-2 circuit breaker panel)
(b)
Push LSK 1L (<CURRENT STATUS) for the A/T BITE TEST - CURRENT STATUS page.
(2)
Do the Current Status Quick Test (Fig. 502):
S 725-060
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
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本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 自動飛行 AUTOFLIGHT 2(155)
