2.  P5-3 Module Removal  (Fig. 401)
A.  References
(1)  AMM 24-22-0/201, MANUAL CONTROL
B.  Access
(1)  Location Zones
(a)  101, 102 Flight Control Cabin
C.  Procedure
(1)  
Remove electrical power (AMM 24-22-0/201).

(2)  
Open these circuit breakers on the P6 Circuit Breaker Panel and
attach DO-NOT-CLOSE tags:

(a)  
SHUTOFF VALVES - FLT CONT (2 Locations)

(b) 
 SHUTOFF VALVES -SPOILER

(c)  
SHUTOFF VALVES - STBY RUD

(d)  
SHUTOFF VALVES - FLAP

(e)  
ALT T.E. FLAP DRIVE AC

(f)  
SECT 4

(g)  
INDICATOR MASTER DIM BUS -BAT

(h)  
INDICATOR MASTER DIM BUS - NO. 1 DC

(i)  
INDICATOR MASTER DIM BUS - NO. 2 DC

(j)  
MASTER CAUTION - ANNUNCIATOR NO. 1

(k)  
MASTER CAUTION - ANNUNCIATOR BAT

(l) 
 AIRPLANES POST-SB 27-1252;
FORCE FIGHT MONITOR

(m)  
RUDDER LOAD LIMITER

(n)  
AUTO PILOT - YAW DAMPER AC

(o)  
AUTO PILOT - YAW DAMPER DC

(p)  
AUTO PILOT - SYS A AC (2 Locations)

(q)  
AUTO PILOT - SYS A DC (2 Locations)

(r)  
AUTO PILOT - SYS B AC (2 Locations or NONE)

(s)  
AUTO PILOT - SYS B DC (2 Locations or NONE)

(t)  
NO. 2 GEN BUS - STBY HYD PUMP (ALT)

(u)  
NO. 1 GEN BUS -STBY HYD PUMP NORMAL

(3)  
Remove the module.

(a)  
Release the fasteners that hold the module.

(b)  
Lower the module.

(c)  
Disconnect the electrical connectors in the back of the module.

500 
May 01/03  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  27-09-45 Page 401 

W29570
Flight Controls Module Assembly (P5-3) Installation  500 
27-09-45  Figure 401  May 01/03 
Page 402 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 

3.  P5-3 Module Installation  (Fig. 401)
A.  References
(1)  AMM 24-22-0/201, MANUAL CONTROL
B.  Access
(1)  Location Zones
(a)  101, 102 Flight Control Cabin
C.  Procedure
(1)  
Connect the electrical connectors in the back of the module.

(2)  
Push the module into the overhead panel.

(3)  
Tighten the fasteners that hold the module.

(4)  
Remove the DO-NOT-CLOSE tags and close these circuit breakers on the P6 Circuit Breaker Panel:

(a)  
SHUTOFF VALVES - FLT CONT (2 Locations)

(b) 
 SHUTOFF VALVES -SPOILER

(c)  
SHUTOFF VALVES - STBY RUD

(d)  
SHUTOFF VALVES - FLAP

(e)  
ALT T.E. FLAP DRIVE AC

(f)  
SECT 4

(g)  
INDICATOR MASTER DIM BUS -BAT

(h)  
INDICATOR MASTER DIM BUS - NO. 1 DC

(i)  
INDICATOR MASTER DIM BUS - NO. 2 DC

(j)  
MASTER CAUTION - ANNUNCIATOR NO. 1

(k)  
MASTER CAUTION - ANNUNCIATOR BAT

(l) 
 AIRPLANES POST-SB 27-1252;
FORCE FIGHT MONITOR

(m)  
RUDDER LOAD LIMITER

(n)  
AUTO PILOT - YAW DAMPER AC

(o)  
AUTO PILOT - YAW DAMPER DC

(p)  
AUTO PILOT - SYS A AC (2 Locations)

(q)  
AUTO PILOT - SYS A DC (2 Locations)

(r)  
AUTO PILOT - SYS B AC (2 Locations or NONE)

(s)  
AUTO PILOT - SYS B DC (2 Locations or NONE)

(5)  
Supply electrical power (AMM 24-22-0/201).

(6)  
Supply hydraulic power to rudder system A and B (AMM 27-21-0/201).

(7)  
Do a test of the lights on the P5-3 module:

(a)  
Hold the LIGHTS switch on the P2 Pilot Main Panel to the TEST position. 1) Make sure all the lights on the P5-3 panel come on.

NOTE:  Other lights on the P5 Overhead and adjacent panels will be illuminated while the LIGHTS switch is in the TEST position.

(b)  
Release the LIGHTS switch. 1) Make sure all the lights on the P5-3 panel and adjacent panels go off.

(8)  
Do a test of these STANDBY HYD lights on the P5-3 module:

500 
May 01/03  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  27-09-45 Page 403 

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