737-700/800 SSM SYSTEM SCHEMATIC MANUAL

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CHAPTER
00
GENERAL
CH-SC-SU Schem Page Sheet Date
00–EFFECTIVE PAGES
1 Dec 01/2008
2 BLANK
00–CONTENTS
1 Jun 03/2008
2 BLANK
00–ALPHABETICAL INDEX
1 Mar 14/2007
2 BLANK
00-00-00
1 101 Jun 23/2005
2 101 Sep 21/2005
00-06-21
1 101 Jun 23/2005
102 Jun 03/2008
2 101 Jun 23/2005
00-06-30
101 Jun 03/2008
00-12-00
101 Jun 03/2008
1 101 Jun 23/2005
102 Jun 23/2005
CH-SC-SU Schem Page Sheet Date
CHAPTER 00
GENERAL
A = Added, R = Revised, D = Deleted, O = Overflow
00-EFFECTIVE PAGES
Page 1
D280A282 Dec 01/2008
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
737-700/800 SYSTEM SCHEMATIC MANUAL
Title CH-SC-SU Schem Page Sheet Date Effectivity
SYMBOLS
SYMBOLS - MECHANICAL 00-00-00 1 101 Jun 23/2005 ALL
SYMBOLS - ELECTRICAL 00-00-00 2 101 Sep 21/2005 ALL
DIMENSION AND EQUIPMENT LOCATION
AIRPLANE STATION BODY AND STABILIZER 00-06-21 1 101 Jun 23/2005 YK511-YK530
102 Jun 03/2008 YM551-YM570
AIRPLANE STATION WING AND NACELLE 00-06-21 2 101 Jun 23/2005 ALL
MAJOR EQUIPMENT CENTERS 00-06-30 101 Jun 03/2008 ALL
GROUND SERVICE ACCESS PANELS
GROUND SERVICE ACCESS PANELS 00-12-00 101 Jun 03/2008 YK511-YK530
1 Jun 23/2005 YK511-YK530
102 Jun 23/2005 YM551-YM570
CHAPTER 00
GENERAL
00-CONTENTS
Page 1
D280A282 Jun 03/2008
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
737-700/800 SYSTEM SCHEMATIC MANUAL
CH-SC-SU Title
00-06-21 AIRPLANE STATION BODY AND STABILIZER
00-12-00 GROUND SERVICE ACCESS PANELS
00-06-30 MAJOR EQUIPMENT CENTERS
00-00-00 SYMBOLS - MECHANICAL
CH-SC-SU Title
CHAPTER 00
GENERAL
00-ALPHABETICAL INDEX
Page 1
D280A282 Mar 14/2007
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
737-700/800 SYSTEM SCHEMATIC MANUAL
TWO WAY
CHARGING WITH CAP
RELIEF
CHECK
VALVES-FLUID OR PNEUMATIC
THERMOSTAT
TWO PORTED-MODULATING
POSITION
TWO PORTED-TWO
VALVES-PNEUMATIC
SELECTOR (TYP)
THREE POSTION
FOUR PORTEDSHUTTLE
COUNTER-CLOCKWISE ARROW
WHEN ACTIVATED UNLESS INDICATED BY A
VALVES ROTATE 90 CLOCKWISE TO OPEN
POSITION
FOUR PORTED-TWO
POSITION
THREE PORTED-TWO
TWO PORTED-TWO POSITION
CLOSED OPEN
VALVES-FLUID
PRESSURE DIFFERENTIAL
PRESSURE TEMPERATURE
SENSORS
ONE WAY
FLOW RESULATORS
REDUCED IN DIRECTION OF ARROW)
PRESSURE REDUCER (PRESSURE IS
CHECKED
ONE WAY
TWO WAY
RESTRICTORS
DISENGAGED ENGAGED
CLUTCH
GEAR BOX
OVERRIDE.
WHICH MAY BE USED FOR MANUAL
DESIGNATES A POSITION INDICATOR
CONNECTION WITH A VALVE SYMBOL,
MANUAL CONTROL-WHEN USED IN
NUMBER AND TURNBUCKLE
CONTROL CABLE WITH IDENTIFICATION
SHEAR RIVET OR PIN FLAGNOTE
IDENTIFICATION NUMBER
RIGGING PIN FLAG NOTE WITH PIN
BEARING
STRUCTURAL (FIXED) PIVOT OR
MOVABLE PIVOT OR BEARING
SPRING
DISCONNECT OR SIMPLE SWIVEL
MISCELLANEOUS MECHANICAL (CONT)
FLUID FUSE
ACCUMULATOR OR TRANSFER TUBE
CAP OR SEALING PLUG
MISCELLANEOUS MECHANICAL
SCREEN TYPE-FLUID COOLED
SCREEN TYPE-AIR COOLED
COIL TYPE-AIR COOLED
HEAT EXCHANGERS
AIR CLEANER
PRESSURE (POP-UP) INDICATOR
BYPASS WITH DIFFERENTIAL
BYPASS
DRAIN PLUG
NON-BYPASS WITH MAGNETIC
NON-BYPASS
FILTERS
MECHANICAL SYMB0LS
OFF UP
C1 C1
P R
C2 C2
3
2
C C
2
3
1
4
1
4
DN
B
A
B
A
B
P R
C2
P R
C1
XXX-X
XX-X
–
1
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D280A282
SYMBOLS - MECHANICAL 00-00-00
Schem 1
Page 101
Jun 23/2005
ALL
BOEING PROPRIETARY - Copyright # - Unpublished Work - See title page for details.
Q & Q WILL TOGGLE.
IF S=0 & R=0 & T GOES HI,
IF R GOES HI, Q=0 & Q=1
IF S GOES HI, Q=1 & Q=0
IF R GOES HI, Q=0 & Q=1
IF S GOES HI, Q=1 & Q=0
T
R Q
FF
S Q
R Q
FF
Q
NOT RESET AT PWR UP.
UNCHANGED. S/R FLIP FLOPS RETAIN PWR DOWN STATE IF
IF BOTH S & R GO HI SIMULTANEOUSLY. OUTPUT REAINS
S
RISING EDGE TRIGGERED
FLIP FLOPS
CONFIGURATION INFORMATION.
INDEX FOR INCORPORATION DATES AND
SEE THE SERVICE BUUETIN AND MODIFICATION
REQUEST.
’FINAL’CONFIGURATION, ACORDING TO CUSTOMER
THIS SCHEMATIC IN EITHER THE ’DUAL’OR THE
THE FLAGNOTE HAS BEEN INCORPORATED INTO
THE SERVICE BUUETIN LISTED ADJACENT TO
(SEE INTRODUCTION PAGE 1).
INTO THE MANUAL AT CUSTOMER REQUEST
CUSTOMER ORIGINATED MATERIAL INCORPORATED
FLAGNOTES
AND/NAND GATES OR/NOR GATES
OR GATE
EXCLUSIVE
TRUTH TABLE
OR
OR
OR
OR
NOR
NOR
NOR
NAND
NAND
NAND
AND
AND
AND
0 1 1 0
1 1 1 0
1 0 1 1
0 1 1 1
1 0 0 0
0 1 0 0
0 0 0 1
0 1 0 1
0 0 1 1
0 1 0 1
0 0 1 1
0 1 0 1
0 0 1 1
0 1 0 1
0 0 1 1
0 1 0 1
0 0 1 1
0 1 0 1
0 0 1 1
0 1 0 1
0 0 1 1
A B X
X B
A
X
B
A
X
B
A
X
B
A
X
B
A
X
B
A
X
B
A
X
B
A
X
B
A
X
B
A
X
B
A
X
B
A
X
B
A
EQUIVALENT LOGIC FUNCTIONS
(NON-LRU)
PANEL COMPONENT BORDER
WORD STATEMENT
LANDING RANGE
AND FLAPS ARE IN
FEAR IS DOWN & LOCKED
ACTIVATE HORN UNLESS
GND WILL BE APPLIED TO
THRUST LESS THAN CLIMB
WITH ALT LESS THAN 1000 FT
THRUST<CLIMB
TWO
ALTITUDE<1000 FT
FLAPS LANDING RANGE
GEAR LOCKED
GEAR DOWN
THRUST<CLIMB
ALTITUDE<1000 FT
FLAPS LANDING RANGE
GEAR LOCKED
GEAR DOWN
ONE
+V
+V
LOGIC DIAGRAMS
LRU COMPONENT/INDENTIFICATION
BORDERS
PROVISIONAL LRU COMPONENT
XX-XX-XX
XX-XX-XX
DIRECTION OF ARROW
OR DROP-OUT ACCORDING TO
DELAY IN SECONDS FOR PULL=IN
TIME DELAY RELAY COIL WITH
IN SECONDS
IN-LINE TIME DELAY WITH DELAY
D T
X SEC
XXS
TIME DELAYS
RESET
SET
TWO INPUT COMMAND SIGNALS
INPUT TO TWO OUTPUTS WITH
SHOW STABLE SWITCHING OF ONE
THIS SYMBOL MAY BE USED TO
SHOW THE SWITCHING FUNCTION
TO RIGHT IF REQUIRED TO
MAY ALSO BE REVERSED LEFT
PULSE INPUT COMMAND. IT
SWITCHING WITH A SINGLE
SHOW ALTERNATE ACTION
THIS SYMBOL MAY BE USED TO
TWO COMMAND SIGNALS
INPUTS TO ONE OUTPUT WITH
SHOW STABLE SWITCHING OF TWO
THIS SYMBOL MAY BE USED TO
ALT
NORM
TO CLOSE
THE NORMALLY OPEN CONTACTS
CLOSED CONTACTS TO OPEN AND
SIGNAL CAUSES THE NORMALLY
THE PRESENCE OF THE DRIVE
THE ARROW INDICATES THAT
CONVENTIONAL SWITCHING SYMBOLOGY:
SOLID STATE SWITCHES ARE SHOWN USING
ELECTRONIC SWITCHES
THERMAL RESISTOR
Z
Y
X
CLOSED)
THERMAL SWITCH (SHOWN NORMALLY
RS (RESOLVER)
TX (TORQUE TRANSMITTER)
TR (TORQUE RECEIVER)
TDX (TORQUE DIFFERENTIAL TRANSMITTER)
TDR (TORQUE DIFFERENTIAL RECEIVER)
CX (CONTROL TRANSMITTER)
CT (CONTROL TRANSFORMER)
CDX (CONTROL DIFFERENTIAL TRANSMITTER)
THERMAL DEVICES
SYNCHRO
PROXIMITY SWITCH
TARGET
BLU
YEL
RED
-V
+V
IDENTIFIER
LOCATION
ALPHA NUMERIC
XX-XX-XX
NAME
BUS
AMP
TITLE (GXX)
BREAKER
CXXX CIRCUIT
ELECTICAL OR ELECTRONIC SYMBOLS
AMPLIFIERS
CIRCUIT BREAKER
INTERGRATING DIFFERENTIAL
NON-INVERTING INVERTING
C
H
XX
T
LRU SHOWN COMPLETE
LRU COMPONENT BORDERIN
DIFFERENT CHAPTER/SECTION)
REFERENCE TO HOME SCHEMATIC
LRU SHOWN INTERFACING (WITH
LRU COMPONENT BORDERIN
SAME CHAPTER/SECTION)
REFERENCE TO HOME SCHEMATIC
LRU SHOWN INCOMPLETE (WITH
LRU COMPONENT BORDER-
-B
1
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D280A282
SYMBOLS - ELECTRICAL 00-00-00
Schem 2
Page 101
Sep 21/2005
ALL
BOEING PROPRIETARY - Copyright # - Unpublished Work - See title page for details.
747
STA
500
STA
.5
589
STA
E
520
STA
CARGO DOOR FRAME
794
STA
SECTION 44 SECTION 47
737-800
208.1
WL
1064
STA
86
251.
F.S.S.
66
205.
F.S.S.
70
102.
F.S.S.
82.50
F.S.S.
FRONT SPAR
158
WL
150
WL
0
STA
LE
15.10
27.75
83.05
113.25
151.000
111.10
STA
STAB
50
221.
STA
STAB
FRONT SPAR
28
258.
STA
STAB
90
24.
E.S.
28
215.
S.B.L.
44.27
33.21
24.35
4.43
BODY STATIONS
727
STA
C
727
STA
787
STA
827
STA
887
STA
HATCH
ESCAPE
.5
627
STA
400
STA
480
STA
520
DOOR LH STA
FWD ENTRY
328
STA
.5
259
STA
WHEEL WELL
COMPT
CARGO
FWD
DOOR LH
FWD CARGO
EQUIPMENT
ELECTRONICS
440
STA
176
STA
227
STA
277
STA
DOOR
ENTRY
LH
DOOR
ACCESS
APU
DOOR
ACCESS
BODY
AFT
DOOR
CARGO
AFT
847
STA
972
STA
1112
STA
1217
STA
1217
STA
WL 105
1016
STA
540
STA
360
STA
130
STA
FAIRING
BODY
WING TO
WING CENTER SECTION WHEEL WELL
SECTION 46 SECTION 48
BULKHEAD
PRESSURE
AFT
SECTION 41 SECTION 43
CABIN
CONTROL
RADOME
TYPICAL CROSS SECTION
ELEVATOR STATIONS
HORIZONTAL STABILIZER AND
RUDDER STATION
VERTICAL STABILIZER AND
FLOOR
TOP OF
L C
RUDDER HINGE
REAR SPAR
TIP
RUDDER
0
BL
50
232.
WL
10
208.
WL
74.0R
TRAILING
EDGE
CARGO FLOOR
LEADING EDGE
0
STA
STAB
SPAR
REAR
(TYP 8 PLACES)
HINGE POINT
ELEVATOR HINGE
–
2
737-700/800 SYSTEM SCHEMATIC MANUAL
D280A282
AIRPLANE STATION
BODY AND STABILIZER 00-06-21
Schem 1
Page 101
Jun 23/2005
YK511-YK530
BOEING PROPRIETARY - Copyright # - Unpublished Work - See title page for details.
WIRING DIAGRAMS
747
STA
500
STA
.5
589
STA
C
520
STA
CARGO DOOR FRAME
794
STA
SECTION 44 SECTION 47
737-700
208.1
WL
1016
STA
86
251.
F.S.S.
66
205.
F.S.S.
258
132.
F.S.S.
82.50
F.S.S.
FRONT SPAR
148.5
WL
0
STA
LE
15.10
27.75
83.05
113.25
151.000
111.10
STA
STAB
50
221.
STA
STAB
FRONT SPAR
28
258.
STA
STAB
90
24.
E.S.
28
215.
S.B.L.
30.60
22.95
19.36
4.43
BODY STATIONS
727
STA
C
727
STA
787
STA
827
STA
887
STA
EXIT DOOR
OVERWING
.5
627
STA
400
STA .4
492
STA
520
DOOR LH STA
FWD ENTRY
328
STA
.5
259
STA
WHEEL WELL
COMPT
CARGO
FWD
DOOR RH
FWD CARGO
EQUIPMENT
ELECTRONICS
460
STA
178
STA
.8
224
STA
277
STA
DOOR
ENTRY
LH
DOOR
ACCESS
APU
DOOR
ACCESS
BODY
AFT
DOOR
CARGO
AFT
847
STA
1016
STA
1112
STA
1217
STA
1217
STA
WL 105
1016
STA
540
STA
360
STA
130
STA
FAIRING
BODY
WING TO
WING CENTER SECTION WHEEL WELL
SECTION 46 SECTION 48
BULKHEAD
PRESSURE
AFT
SECTION 41 SECTION 43
CABIN
CONTROL
RADOME
TYPICAL CROSS SECTION
ELEVATOR STATIONS
HORIZONTAL STABILIZER AND
RUDDER STATION
VERTICAL STABILIZER AND
FLOOR
TOP OF
L C
RUDDER HINGE
REAR SPAR
TIP
RUDDER
0
BL
50
232.
WL
10
208.
WL
74.0R
TRAILING
EDGE
CARGO FLOOR
LEADING EDGE
0
STA
STAB
SPAR
REAR
(TYP 8 PLACES)
HINGE POINT
ELEVATOR HINGE
–
6
737-700/800 SYSTEM SCHEMATIC MANUAL
D280A282
AIRPLANE STATION
BODY AND STABILIZER 00-06-21
Schem 1
Page 102
Jun 03/2008
YM551-YM570
BOEING PROPRIETARY - Copyright # - Unpublished Work - See title page for details.
124.8268
00
73.
WBL
132.15
WL
145.63 NAC
WL
NAC
129.074
STA
NAC
314.24
STA
NAC
257.25
STA
196.84 NAC
STA
NAC
166.50
STA
NAC
100.
WL
NAC
92.5
WBL
FAIRING NO. 3
FLAP TRACK
00
355.
WBL
00
157.
WBL
288.0968
185.6
113.1701
41.5233
21.8721
24
71.
WBL
114
WSTA
00
213.
WSTA
00
191.
WBL
07
342.
WBL
05
177.
WBL
254
WSTA
75
329.
WSTA
453
WSTA
531
WSTA
NO.3
SLAT
583
WSTA
OUTBOARD REAR SPAR
00
560.
WBL
50
571.
WBL
63.83
36.44
21.98
NO.4
SPOILER
ENGINE & NACELLE STATIONS
WING STATIONS
PROPULSION SYSTEM
0.0
BL
’C’ DUCT (L.H.)
NOSE COWL
L.H. HINGED SIDE COWL
R.H. HINGED SIDE COWL
SUPPORT
SIDE COWL
AIRCRAFT PYLON
MOUNT
FRONT
MOUNT
REAR
NACELLE STRUT
UPPER LINK
STRUT FAIRING
AFTERBODY AND
EXHAUST COLLECTOR
NOSE COWL
C NACELLE
L
NO.1
SLAT
NO.2
SLAT
LEADING EDGE
NO.4
SPOILER
INBD FLAP
AILERON
FAIRING NO.2
FAIRING NO.1 FLAP TRACK
FLAP TRACK
FLAP
OUTBD
NO.1
SPOILER
NO.2
SPOILER
NO.3
SPOILER
–
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AIRPLANE STATION
WING AND NACELLE 00-06-21
Schem 2
Page 101
Jun 23/2005
ALL
BOEING PROPRIETARY - Copyright # - Unpublished Work - See title page for details.
E6
E5-1
E5-2
E4-1
E4-2
E1-4
E1-2
E11
COMPARTMENT
E11 RACK
VIEW D
VALVE
OPENING
INWARD
VALVE
OPENING
OUTWARD
VALVE (TYPICAL)
PRESSURE EQUALIZATION
VIEW C
SEE
VIEW D
SEE
FLIGHT DATA RECORDER
VOICE RECORDER
CEILING BLOWOUT PANEL
COMPARTMENT ACCESS AND
AFT CARGO AREA
RACK COMPARTMENT
ELECTRONIC EQUIPMENT
VIEW C
E3-3
E3-2
E3-1
E2-2
E2-1
E1-5
E1-3
E1-1
AREA PANEL LOCATION
REAR OF FLIGHT DECK
VIEW B
P6 P18
VIEW A
AREA PANEL LOCATION
FRONT OF FLIGHT DECK
P5
P9
P8
P7
P5
P1 P2 P3
FWD
UP
VIEW B
SEE
VIEW A
SEE
-B
1
737-700/800 SYSTEM SCHEMATIC MANUAL
D280A282
MAJOR EQUIPMENT
CENTERS 00-06-30
Page 101
Jun 03/2008
ALL
BOEING PROPRIETARY - Copyright # - Unpublished Work - See title page for details.
APU OIL
VACUUM LAV SERVICE
HYDRAULIC RESEROIR
CONTROL (R.H. ONLY)
FUELING
(RIGHT SIDE OF ENGINE)
ENGINE OIL
PORTABLE WATER
CONDITIONED AIR
ELECTRICAL
PNEUMATICS
OXYGEN SERVICE (OPT)
(LEFT SIDE OF ENGINE)
ENGINE OIL
BRAKE ACCUMULATOR
–
1
737-700/800 SYSTEM SCHEMATIC MANUAL
D280A282
GROUND SERVICE
ACCESS PANELS 00-12-00
Page 101
Jun 03/2008
YK511-YK530
BOEING PROPRIETARY - Copyright # - Unpublished Work - See title page for details.
VIEW FROM BOTTOM LOOKING UP.
1217
STA
1016
STA
727
STA
1
SERVICE ACCESS PANELS
1 SEE 71-00-00 FOR VIEW OF POWER PLANT/NACELLE STRUT
AND POSN SNSR
HYD, ELEC
CONTROL LINKAGE,
ELEVATOR;
HYD AND ELEC
CONTROL LINKAGE,
ELEVATORS;
SERVICE
POTABLE WATER
PUMPS
ELECTRIC MOTOR
ACCUMULATION CHARGING
FILL SYSTEM AND BRAKE
MOTOR PUMPS CENTRAL
RESERVOIR, ELECT
AND CONTROL LINKAGE
ELEVATOR, PCU’S
ACCESS
APU
CONTROLS
ELEVATOR
CONTROL (R.H. ONLY)
FUELING
GEAR ACTUATOR
T/E LANDING
CONTROL SWITCHES
GEAR GROUND DOOR
NOSE AND MAIN
VALVE AND REFILL
TOILET DRAIN
DRIVEN HYD PUMP
RAM AIR TURBINE
GEARBOX
L/E SLAT DRIVE
START
ENGINE GROUND
ACTUATOR
AC INLET DUCT
DRAIN MAST
GROUND SERVICE
CONDITIONING
AIR
LUBRICATION
TRACK ROLLER
MAIN AND AUX
INBOARD L/E
RECEPTICLE
GROUND POWER
CONTROLS
RADAR AND
RADOME
ELECTRONICS BAY
ELECTRICAL/
SERVICE
FWD LAVATORY ACTUATOR
DUCT
AC INLET
GROUND START
ENGINE
540
STA
360
STA
130
STA
NOTE:
LUBRICATION
TRACK ROLLER
MAIN AND AUX
OUTBOARD L/E
-A
1
737-700/800 SYSTEM SCHEMATIC MANUAL
D280A282
GROUND SERVICE
ACCESS PANELS 00-12-00
Schem 1
Page 101
Jun 23/2005
YK511-YK530
BOEING PROPRIETARY - Copyright # - Unpublished Work - See title page for details.
ACCESS
(R.H. SIDE)
EXTERIOR
CONTROLS
ELEVATOR
ACCESS
APU
PANEL
WASTE SERVICE
1217
STA
1016
STA
706
STA
1
SERVICE ACCESS PANELS
1 SEE 71-00-00 FOR VIEW OF POWER PLANT/NACELLE STRUT
AND POSN SNSR
HYD, ELEC
CONTROL LINKAGE,
ELEVATOR;
HYD AND ELEC
CONTROL LINKAGE,
ELEVATORS;
PANEL
WATER SERVICE
PUMPS
ELECTRIC MOTOR
AND BRAKE ACCUMULATION CHARGING
PUMPS CENTRAL FILL SYSTEM
RESERVOIR, ELECT MOTOR
ACCESS
APU
CONTROLS
ELEVATOR
CONTROL (R.H. ONLY)
FUELING
GEAR ACTUATOR
T/E LANDING
START
ENGINE GROUND
RAM AIR INLET
DRAIN MAST
GROUND SERVICE
CONDITIONING
AIR
LUBRICATION
TRACK ROLLER
MAIN AND AUX
INBOARD L/E
ACCESS DOOR
ELECTRICAL EQUIPMENT
FWD ACCESS DOOR
RADOME
INLET
RAM AIR
GROUND START
ENGINE
FWD ACCESS DOOR
RADOME
540
STA
360
STA
130
STA
NOTE:
LUBRICATION
TRACK ROLLER
MAIN AND AUX
OUTBOARD L/E
DRAIN MAST
–
2
737-700/800 SYSTEM SCHEMATIC MANUAL
D280A282
GROUND SERVICE
ACCESS PANELS 00-12-00
Schem 1
Page 102
Jun 23/2005
YM551-YM570
BOEING PROPRIETARY - Copyright # - Unpublished Work - See title page for details.

bocome

737-700/800 SSM SYSTEM SCHEMATIC MANUAL

ding2

谢谢楼主，辛苦！

Skydrolor5606

thank you very much for the information

liuwh_99

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lc8372616

好东西，谢谢。拿走了。

goodmangood

期待其内容。