标题: 737-700/800 SSM SYSTEM SCHEMATIC MANUAL [打印本页] 作者: 航空 时间: 2011-6-10 00:55:12 标题: 737-700/800 SSM SYSTEM SCHEMATIC MANUAL
作者: 航空 时间: 2011-6-10 00:56:10
作者: 航空 时间: 2011-6-10 00:56:55
作者: 航空 时间: 2011-6-10 00:57:12
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R = Revised, D = Deleted, O = Overflow 00-EFFECTIVE PAGES Page 1 D280A282 Dec 01/2008 BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details 737-700/800 SYSTEM SCHEMATIC MANUAL Title CH-SC-SU Schem Page Sheet Date Effectivity SYMBOLS SYMBOLS - MECHANICAL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Jun 23/2005 YM551-YM570 CHAPTER 00 GENERAL 00-CONTENTS Page 1 D280A282 Jun 03/2008 BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details 737-700/800 SYSTEM SCHEMATIC MANUAL CH-SC-SU Title 00-06-21 AIRPLANE STATION BODY AND STABILIZER 00-12-00 GROUND SERVICE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CH-SC-SU Title CHAPTER 00 GENERAL 00-ALPHABETICAL INDEX Page 1 D280A282 Mar 14/2007 BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details 737-700/800 SYSTEM SCHEMATIC MANUAL TWO WAY CHARGING WITH CAP RELIEF CHECK VALVES-FLUID OR PNEUMATIC THERMOSTAT TWO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 – 1 737-700/800 SYSTEM SCHEMATIC MANUAL 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 1 737-700/800 SYSTEM SCHEMATIC MANUAL 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 – 1 737-700/800 SYSTEM SCHEMATIC MANUAL D280A282 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.作者: bocome 时间: 2011-7-31 03:34:08
737-700/800 SSM SYSTEM SCHEMATIC MANUAL作者: ding2 时间: 2011-10-7 15:12:24
谢谢楼主，辛苦！作者: Skydrolor5606 时间: 2011-10-13 09:35:06
thank you very much for the information作者: liuwh_99 时间: 2012-4-13 18:58:30