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PANEL
CB
LOCATION
NOTES
Potable Water
System Controller WATER
SYSTEM AC SERVICE 2 D8
Vol. 1 21--30--1
WATER AND WASTE SYSTEMS
Lavatory Waste System REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
1. LAVATORY WASTE SYSTEM
The lavatory waste system provides a means of flushing the toilet and holding waste
material from the forward and aft lavatory toilets. Each system consists of a seat and bowl
assembly, tank assembly, flush handle and service panel. The tank assembly is
self-contained and consists of a electric pump, timer and filter. The tank holds the deodorant
flushing solution and waste material until removed by ground servicing personnel.
When the toilet flush handle is pushed, a timer energizes the electric pump for 10 seconds.
The pump draws the flushing fluid from the tank, through a filter basket, and sends it out
through the bowl assembly flush ring.
The systems are serviced by means of lavatory service panels, located on the right side of
the forward and aft fuselage. When the service vehicle drain line is connected to the drain
port, the T-handle is rotated to the left and pulled. This opens the drain valve, located at the
bottom of the holding tank, allowing the tank to empty through the drain line.
Once the holding tank is emptied, rinsing agent and flushing fluid are sent through the
charging port, flushing and cleaning the tank and lines. The T-handle is then turned to the
right and pushed in to close the drain valve. The tank is then filled with precharge flushing
fluid until the fluid level light on the service panel illuminates.
The toilet requires a precharge of 2.3 US gallons (8.7 liters) of flushing fluid.
Vol. 1 21--30--2
WATER AND WASTE SYSTEMS
Lavatory Waste System REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
Lavatory Waste System --- Lavatory Service Panel
Figure 21---30---1
Waste Valve
Used to drain tank.
T Handle
Used to open drain valve.
Precharge Port
Used to flush tank and
precharge system.
Precharge Lamp Vent
Indicates system is at
precharge level.
Push light to test lamp.
NOTE
Access panel can not be closed
unless waste valve and precharge
port covers are closed and locked
and drain valve T handle is locked.
WASTE DUMP
RINSE CABLE T--HANDLE
CONNECTION
DRAIN
CONNECTION
FILTER BASKET
AND PUMP
VENT
LINE
MOTOR
TIMER
FLUSH
HANDLE
BOWL
ASSEMBLY
CHECK
VALVE
HOLDING
TANK
DRAIN VALVE
ASSEMBLY
LAVATORY
SERVICE
PANEL
Mechanical connection
Lavatory waste duct assembly
LEGEND
Ground rinse inlet tubing
SERVICE
PANEL
Vol. 1 21--30--3
WATER AND WASTE SYSTEMS
Lavatory Waste System REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
A. System Circuit Breakers
SYSTEM SUB--SYSTEM CB NAME BUS BAR CB
PANEL
CB
LOCATION
NOTES
Lavatory Toilet TOILET AC SERVICE D5
Waste
S t Waste
WASTE SYST
DC SERVICE
2 M9
System WATER CONT
M10
Vol. 1 21--30--4
WATER AND WASTE SYSTEMS
Lavatory Waste System REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
THIS PAGE IS INTENTIONALLY LEFT BLANK
Enhanced Ground Proximity Warning System (EGPWS)
and Runway Awareness Advisory System (RAAS) Pilot Guide
060-4241-000 • Rev. E - December 2003
MK V & MK VII EGPWS Pilot Guide
MK V and MK VII
060-4241-000 • Rev. E - December 2003
MK V & MK VII EGPWS Pilot Guide
This document is an unpublished work
Copyright 2003
Honeywell International Inc.
A l l r i g h t s r e s e r v e d
T h i s d o c u m e n t a n d a l l i n f o r m a t i o n a n d e x p r e s s i o n
c o n t a i n e d h e r e i n a r e t h e p r o p e r t y o f H o n e y w e l l
I n t e r n a t i o n a l I n c . , a n d i s p r o v i d e d t o t h e r e c i p i e n t i n
confidence on a “need to know” basis. Yo u r u s e o f t h i s
d o c u m e n t i s s t r i c t l y l i m i t e d t o a l e g i t i m a t e b u s i n e s s
p u r p o s e r e q u i r i n g t h e i n f o r m a t i o n c o n t a i n e d t h e r e i n .
Your use of this document constitutes acceptance of these
terms.
060-4241-000 • Rev. E - December 2003
MK V & MK VII EGPWS Pilot Guide 1
TABLE OF CONTENTS
SECTION 1 Introduction .................................................................... 2
SECTION 2 System Description .......................................................... 5
　
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