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737-300/400/500MAINTENANCE MANUAL
4) NO. 2 AIR DATA ALTM-2 26V AC 5) NO. 2 AIR DATA AUTO XFMR 6) NO. 2 AIR DATA COMPUTER-2 26V AC 7) NO. 2 AIR DATA COMPUTER-2 AC 8) ADI 9) COMPASS-1 XFMR ALTN 10) VERT SPEED IND 11) MACH ASI 12) MACH WARN SYS-2 13) CAPT ADI ALTM 14) RADIO ALTM-2 15) DME-2 16) DAA NO. 2 FMC AC 17) DAA NO. 2 IRS AC 18) DAA NO. 2 IRS DC 19) IRS NO. 2 AC 20) IRS NO. 2 DC 21) DAA FMC NO. 2
(b)
P6-2/-3 Circuit Breaker Panel 1) HYD SYSTEM ELEC PUMP SYS B 2) HYD SYSTEM HYD CONT SYS A 3) AFCS B MACH TRIM DC 4) AFCS B MACH TRIM AC 5) AFDS MCP CRS-2 DC 6) STABILIZER TRIM ACTUATOR 3 PHASE 7) STABILIZER TRIM CONT 8) AFCS B SNSR EXC AC 9) AFCS B FCC DC 10) AFCS B ENGAGE INTLK B 11) AFCS B WARN LIGHT (BAT) 12) TACH IND ENG 2 N1 13) TACH IND ENG 2 N2 14) TACH IND ENG 1 N1 15) TACH IND ENG 1 N2 16) PRESS IND SYS B 17) PRESS IND SYS A 18) F/O BAT 19) F/O NO. 2 BUS 20) AURAL WARN 21) LANDING GEAR AIR/GND RELAY & LTS 22) ANTI-SKID INBD 23) ANTI-SKID OUTBD 24) ANTI-SKID FAIL WARN & PARK BK
(c)
P18-0 Circuit Breaker Panel 1) STAB TRIM
(d)
P18-1 Circuit Breaker Panel 1) NO. 1 NAVIGATION VHF NAV-1 VOR/ILS 2) VHF NAV-1 G/S
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú
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737-300/400/500MAINTENANCE MANUAL
3) RADIO ALTM-1
4) DME-1
5) AFDS MCP DC
6) AUTOTHROTTLE AC
7) AUTOTHROTTLE DC
8) AFDS AIL FORCE LIM
9) AFCS A SNSR EXC AC
10) AFCS A FCC DC
11) AFCS A ENGAGE INTLK A
12) AFCS A WARN LIGHT (BAT)
13) AFCS A MACH TRIM AC
14) AFCS A MACH TRIM DC
(e) P18-2 Circuit Breaker Panel
1) INST XFMR-1
2) INST XFR
3) NO. 1 AIR DATA AUTO XFMR
4) NO. 1 AIR DATA COMPUTER-1 AC
5) NO. 1 AIR DATA COMPUTER-1 26V AC
6) ADI
7) F/O ADI ALTN
8) COMPASS-2 XFMR ALTN
9) VERT SPEED IND
10) MACH WARN SYS-1
11) ALTM 26V AC
12) STBY ALTM/ASI VIBR
13) MACH ASI
14) DAA FMC NO. 1
15) DAA NO. 1 FMC AC
16) DAA NO. 1 IRS AC
17) DAA NO. 1 IRS DC
18) IRS NO. 1 AC
19) IRS NO. 1 DC
20) FMCS CDU NO. 2
21) FMCS MODE ANN
22) FMCS CMPTR
23) FMCS CDU NO. 1
S 865-143
(5)
Align the IRS (AMM 34-28-00/201).
(6)
Make sure that all instrument switches are in the NORMAL position.
(7)
Make sure that the airplane is in the ground mode.
(8)
Make sure that the autopilot is disengaged.
S 865-173
S 865-174
S 865-176
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S 865-147
(9) Make sure that the IRS ground speed is less than 20 knots or the FMC ground speed is less than 20 knots.
E. Current Status Quick Test (Group 10)
S 745-181
(1) Do the current status quick test:
(a)
Push the INIT/REF key on the Flight Management Computer System (FMCS) Control Display Unit (CDU) (Fig. 501) to show the POS INIT page or PERF INIT page.
(b)
Push the line-select key (LSK) adjacent to <INDEX to show the INIT REF INDEX 1/1 page.
(c)
Push the LSK adjacent to MAINT> to show the MAINT BITE INDEX 1/1 page.
NOTE: It is not possible to get access to the MAINT BITE INDEX
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