(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
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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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