PMDG 737NGX FCOM Volume 2 - Precision Manuals Development Group PMDG

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Systems Description 1-Airplane General, Emergency Equipment, Doors, Windows Table Of Contents DO NOT USE FOR FLIGHT 737 Flight Crew Operations Manual Airplane General, Emergency Chapter 1 Equipment, Doors, Windows Table of Contents Section 0 Dimensions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10 Principal Dimensions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.1 Turning Radius . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.6 Instrument Panels. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.20 Panel Arrangement. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.20.1 Aft Flight Deck Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.20.2 Left Forward Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.20.3 Right Forward Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.20.4 Glareshield Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.20.5 Center Forward Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.20.7 Forward Aisle Stand . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.20.11 737-600/700 Forward Overhead Panel . . . . . . . . . . . . . . . . . . . . 1.20.13 737-800/900 Forward Overhead Panel . . . . . . . . . . . . . . . . . . . . 1.20.14 Aft Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.20.15 Control Stand . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.20.16 Aft Electronic Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.20.17 Auxiliary Panels. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.20.19 Attendant Panels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.20.20 Attendant Handset . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.20.21 Controls and Indicators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.30 Flight Deck Lighting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.30.1 Map and Chart Light Controls . . . . . . . . . . . . . . . . . . . . . . . . . 1.30.1 Main Panel Lighting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.30.1 Background and AFDS Flood Light Control . . . . . . . . . . . . . . 1.30.2 Flood and Aft Electronics Lights Controls. . . . . . . . . . . . . . . . 1.30.2 Overhead/Circuit Breaker Panel Light Controls . . . . . . . . . . . 1.30.3 Dome Light Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.30.3 Master Lights Test and Dim Switch . . . . . . . . . . . . . . . . . . . . . 1.30.4 Copyright © The Boeing Company. See title page for details. March 27, 2009 D6-27370-TBC 1.TOC.0.1 DO NOT USE FOR FLIGHT 737 Flight Crew Operations Manual Airplane General, Emergency Chapter 1 Equipment, Doors, Windows Dimensions Section 10 1.10 Airplane General, Emergency Equipment, Doors, Windows-Dimensions Volume Airplane 10 Dimensions Dimensions 2General, Emergency Equipment, Doors, Windows Principal Dimensions 112'-7" (34.40m) 47'-2" (14.30m) 18'-8" (5.70m) 41'-2" (12.50m) 36'-9" (11.20m) 97'-9" (29.80m) 102'-6" (31.20m) 737-600 Copyright © The Boeing Company. See title page for details. September 24, 2007 D6-27370-TBC 1.10.1 Airplane General, Emergency DO NOT USE FOR FLIGHT Equipment, Doors, Windows - Dimensions 737 Flight Crew Operations Manual 112'-7" (34.40m) 47'-2" (14.30m) 18'-8" (5.70m) 41'-2" (12.50m) 41'-3" (12.60m) 106'-7" (32.50m) 110'-4" (33.60m) 737-700 Copyright © The Boeing Company. See title page for details. 1.10.2 D6-27370-TBC September 24, 2007 Airplane General, Emergency DO NOT USE FOR FLIGHT Equipment, Doors,Dimensions Windows - 737 Flight Crew Operations Manual 117'-5" (35.79m) 47'-2" (14.30m) 18'-8" (5.70m) 41'-2" (12.50m) 21'-1" (6.42m) 51'-1" (15.60m) 124'-9" (38.00m) 129'-6" (39.50m) 737-800 With Winglets Copyright © The Boeing Company. See title page for details. September 24, 2007 D6-27370-TBC 1.10.3 Airplane General, Emergency DO NOT USE FOR FLIGHT Equipment, Doors, Windows - Dimensions 737 Flight Crew Operations Manual 112'-7" (34.40m) 47'-2" (14.30m) 18'-8" (5.70m) 41'-2" (12.50m) 56'-4" (17.20m) 133'-5" (40.70m) 138'-2" (42.10m) 737-900 Copyright © The Boeing Company. See title page for details. 1.10.4 D6-27370-TBC September 24, 2007 Airplane General, Emergency DO NOT USE FOR FLIGHT Equipment, Doors,Dimensions Windows - 737 Flight Crew Operations Manual 117'-5" (35.79m) 47'-2" (14.30m) 18'-8" (5.70m) 41'-2" (12.50m) 21'-1" (6.42m) 56'-4" (17.20m) 133'-5" (40.70m) 138'-2" (42.10m) 737-900ER With Winglets Copyright © The Boeing Company. See title page for details. September 24, 2007 D6-27370-TBC 1.10.5 Airplane General, Emergency DO NOT USE FOR FLIGHT Equipment, Doors, Windows - Dimensions 737 Flight Crew Operations Manual Turning Radius [Option: 737-600 without Winglets or 737-700 or 737-800 with Winglets] The wingtip swings the largest arc while turning and determines the minimum obstruction clearance path. All other portions of the airplane structure remain within this arc. [Option: 737-800 without Winglets or 737-900/737-900ER with winglets] The tail swings the largest arc while turning and determines the minimum obstruction clearance path. All other portions of the airplane remain within this arc. Copyright © The Boeing Company. See title page for details. 1.10.6 D6-27370-TBC May 15, 2008 Airplane General, Emergency DO NOT USE FOR FLIGHT Equipment, Doors,Dimensions Windows - 737 Flight Crew Operations Manual Nose radius Tail radius 51.5 Feet (15.7 Meters) 61.9 Feet (18.9 Meters) s iu ad il R Ta Effective Steering Minimum width angle 75° of pavement for 180° turn s d iu Ra s ip diu n gT Wi Ra se No Center of turn for Wing tip radius minimum turning radius. 69 Feet (20.9 Meters) (Slow continuous turning with minimum thrust on all engines. No Note: Minimum width of pavement for 180° turn: differential braking.) 60.8 Feet (18.5 Meters) CAUTION: Do not attempt to make a turn away from an obstacle within (17.3 feet/5.3m) of the wing tip or within (32.6feet/9.9m)of the nose. 737-600 Copyright © The Boeing Company. See title page for details. May 15, 2008 D6-27370-TBC 1.10.7 Airplane General, Emergency Equipment, Doors, Windows - Dimensions DO NOT USE FOR FLIGHT 737 Flight Crew Operations Manual Nose radius Tail radius 55.9 Feet (17.0 Meters) 65.5 Feet (20.0 Meters) s iu ad il R Effective Ta Steering Minimum width angle 75° of pavement for us 180° turn adi ip R gT us Win di Ra se No Center of turn for minimum turning radius. Wing tip radius (Slow continuous 69.6 Feet (21.2 Meters) turning with minimum thrust on all engines. No Note: Minimum width of pavement for 180° turn: differential braking.) 66.4 Feet (20.2 Meters) CAUTION: Do not attempt to make a turn away from an obstacle within (17.2 feet/5.2m) of the wing tip or within (29.0feet/8.8m)of the nose. 737-700 Copyright © The Boeing Company. See title page for details. 1.10.8 D6-27370-TBC May 15, 2008 Airplane General, Emergency DO NOT USE FOR FLIGHT Equipment, Doors,Dimensions Windows - 737 Flight Crew Operations Manual Nose radius Tail radius 65.9 Feet (20.1 Meters) 71.3 Feet (21.7 Meters) s iu ad il R Ta Effective Steering Minimum width angle 75° of pavement for s 180° turn d iu Ra us T ip di ing Ra W se No Wing tip radius 75.2 Feet (22.9 Meters) Center of turn for minimum turning radius. (Slow continuous Note: Minimum width of pavement for 180° turn: turning with minimum 79.1 Feet (24.1 Meters) thrust on all engines. No differential braking.) CAUTION: Do not attempt to make a turn away from an obstacle within (17.8 feet/5.4m) of the wing tip or within (24.3feet/7.4m)of the nose. 737-800 With Winglets Copyright © The Boeing Company. See title page for details. May 15, 2008 D6-27370-TBC 1.10.9 Airplane General, Emergency Equipment, Doors, Windows - Dimensions DO NOT USE FOR FLIGHT 737 Flight Crew Operations Manual Nose radius Tail radius 74.9 Feet (22.8 Meters) 78.0 Feet (23.8 Meters) s iu ad il R Effective Ta Steering angle 75° s d iu Minimum width Ra us Tip of pavement for di ing Ra W 180° turn se No Wing tip radius 73.5 Feet (22.4 Meters) Center of turn for minimum turning radius. Note: Minimum width of pavement for 180° turn: (Slow continuous 85.9 Feet (26.2 Meters) turning with minimum thrust on all engines. No differential braking.) CAUTION: Do not attempt to make a turn away from an obstacle within (19.5 feet/5.9m) of the wing tip or within (21.8feet/6.6m)of the nose. 737-900 Copyright © The Boeing Company. See title page for details. 1.10.10 D6-27370-TBC May 15, 2008 Airplane General, Emergency DO NOT USE FOR FLIGHT Equipment, Doors,Dimensions Windows - 737 Flight Crew Operations Manual Nose radius Tail radius 74.9 Feet (22.8 Meters) 78.0 Feet (23.8 Meters) s iu ad il R Ta Effective Steering angle 75° s Minimum width diu Ra s ip of pavement for u gT di n 180° turn Ra Wi se No Wing tip radius Center of turn for 76.6 Feet (23.3 Meters) minimum turning radius. (Slow continuous Note: Minimum width of pavement for 180° turn: turning with minimum 85.9 Feet (26.2 Meters) thrust on all engines. No differential braking.) CAUTION: Do not attempt to make a turn away from an obstacle within (16.2 feet/5.0m) of the wing tip or within (21.8feet/6.6m)of the nose. 737-900ER With Winglets Copyright © The Boeing Company. See title page for details. May 15, 2008 D6-27370-TBC 1.10.11 Airplane General, Emergency DO NOT USE FOR FLIGHT Equipment, Doors, Windows - Dimensions 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 1.10.12 D6-27370-TBC May 15, 2008 DO NOT USE FOR FLIGHT 737 Flight Crew Operations Manual Airplane General, Emergency Chapter 1 Equipment, Doors, Windows Instrument Panels Section 20 1.20 Airplane General, Emergency Equipment, Doors, Windows-Instrument Panels 2324B299A2720 Instrument PanelsInstrument Panels Panel Arrangement AFT OVERHEAD PANEL FORWARD OVERHEAD PANEL GLARESHIELD PANEL RIGHT LEFT FORWARD FORWARD PANEL PANEL FIRST CAPTAIN OFFICER SIDE SIDE PANEL PANEL CENTER INSTRUMENT PANEL FORWARD ELECTRONIC PANEL AFT ELECTRONIC PANEL CONTROL STAND STABILIZER AUTOPILOT DISENGAGE SWITCH TRIM SWITCH MEMORY DEVICE WRITING PAD HOLDER CLIP WITH CHECKLIST PUSH-TO-TALK SWITCH CAPTAIN CONTROL WHEEL DETAIL On the following pages, circled numbers refer to chapters where information on the item may be found. The panels, controls, and indicators shown in this chapter are representative of installed units and may not exactly match the latest configuration. Refer to the appropriate chapter system descriptions for current information. Copyright © The Boeing Company. See title page for details. March 29, 2004 D6-27370-TBC 1.20.1 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels DO NOT USE FOR FLIGHT 737 Flight Crew Operations Manual Aft Flight Deck Overview P6-1 NAV, WHITE DOME LIGHT INST, & COMM OBSERVER OXYGEN MASK WHITE DOME LIGHT P6-2 SYSTEMS P18-1 NAV P6-3 FUEL SYSTEM, COAT LIGHTING & STOWAGE LANDING GEAR P18-2 INST P6-STBY & COMM POWER CONTROL P18-3 UNIT ANTI-ICE LIGHTING OBSERVERS SEATS P6-12 FIRE EXTINGUISHER WINDOW HEAT MANUAL GEAR RELEASE P6-4 AIR COND & ELECTRICAL P6-11 WINDOW HEAT AFT FLIGHT DECK OVERVIEW Copyright © The Boeing Company. See title page for details. 1.20.2 D6-27370-TBC March 29, 2004 Airplane General, Emergency DO NOT USE FOR FLIGHT Equipment,Instrument Doors, Windows - Panels 737 Flight Crew Operations Manual Left Forward Panel [Option - Typical] 10 4 15 11 15 10 LIGHTS MAIN PANEL DUs OUTBD PFD NORM ENG PRI ENG PRI LOWER DU NORM ND A/P A/T FMC P/RST P/RST P/RST TEST 1 2 TEST BRT 1 DIM PFD INBD 4 STAB MFD OUT OF BELOW G/S TAKEOFF CABIN TRIM P-INHIBIT CONFIG ALTITUDE CHR TIME/DATE 60 MAN UTC 9 TIME SET 50 10 10 40 DAY MOYR 20 ET RUN ET CHR HLD 30 RESET 10 NOSE WHEEL STEERING 14 A N L O T R M REGISTRATION SELCAL 1 PANEL UPPER BACKGROUND AFDS FLOOD BRT OFF WIND- OFF OFF FOOT AIR SHIELD OUTBD INBD LOWER AIR BRT BRT BRT 3 10 1 CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Copyright © The Boeing Company. See title page for details. September 18, 2008 D6-27370-TBC 1.20.3 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels DO NOT USE FOR FLIGHT 737 Flight Crew Operations Manual Right Forward Panel [Option - Typical] 4 11 4 10 3 2 4 LOWER DU MAIN PANEL DUs BRAKE NORM NORM 14 PRESS 1 1 PSIx1000 A/P A/T FMC ND ENG ENG OUTBD PFD 0 P/RST P/RST P/RST PRI PRI 2 TEST PFD INBD MFD CABIN TAKEOFF SPEEDBRAKES BELOW G/S ALTITUDE CONFIG EXTENDED P-INHIBIT 15 CHR TIME/DATE MAN UTC 60 9 50 TIME 10 SET 40 DAY MOYR 20 10 ET RUN ET CHR 15 HLD 30 RESET 10 REGISTRATION SELCAL PANEL GROUND PROXIMITY FLAP GEAR TERR INOP INHIBIT INHIBIT INHIBIT OFF WIND- FOOT INBD OUTBD SHIELD AIR BRT BRT AIR SYS TEST NORM NORM NORM 15 10 3 CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Copyright © The Boeing Company. See title page for details. 1.20.4 D6-27370-TBC September 18, 2008 Airplane General, Emergency DO NOT USE FOR FLIGHT Equipment,Instrument Doors, Windows - Panels 737 Flight Crew Operations Manual Glareshield Panel [Option - Honeywell mode control panel without speed and altitude intervention] 15 MINS FPV MTRS BARO RADIO BARO IN HPA 10 RST STD FIRE MASTER FLT CONT ELEC WARN CAUTION VOR MAP 40 IRS APU VOR 1 APP PLN 20 80 VOR 2 BELL CUTOUT PUSH TO RESET 10 160 FUEL OVHT/DET OFF 5 TFC 320 OFF CTR ADF 1 640 ADF 2 WXR STA WPT ARPT DATA POS TERR 4 COURSE A/T IAS/MACH V NAV HEADING L NAV ALTITUDE VERT SPEED A/P ENGAGE COURSE ARM CMD A CMD B C/O 30 10 DN CWS A CWS B VOR LOC MA MA OFF SEL F/D F/D ON 10 30 DISENGAGE ON N1 SPEED LVL CHG HDG SEL APP ALT HLD V/S UP OFF OFF 15 MINS FPV MTRS BARO RADIO BARO IN HPA RST STD ANTI-ICE ENG MASTER FIRE 10 VOR 1 OFF APP VOR MAP PLN 20 10 40 80 160 VOR 2 HYD DOORS OVERHEAD AIR COND CAUTION PUSH TO RESET WARN BELL CUTOUT CTR 5 TFC 320 OFF ADF 1 640 ADF 2 WXR STA WPT ARPT DATA POS TERR CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Copyright © The Boeing Company. See title page for details. March 29, 2004 D6-27370-TBC 1.20.5 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels DO NOT USE FOR FLIGHT 737 Flight Crew Operations Manual [Option - Collins mode control panel with speed and altitude intervention] 15 MINS FPV MTRS BARO RADIO BARO IN HPA 10 RST STD FIRE MASTER FLT CONT ELEC WARN CAUTION VOR MAP 40 IRS APU VOR 1 APP PLN 20 80 VOR 2 BELL CUTOUT PUSH TO RESET 10 160 FUEL OVHT/DET OFF 5 TFC 320 OFF CTR ADF 1 640 ADF 2 WXR STA WPT ARPT DATA POS TERR 4 COURSE A/T IAS/MACH HEADING ALTITUDE VERT SPEED A/P ENGAGE COURSE ARM A B V NAV L NAV CMD CMD C/O 10 30 DN MA VORLOC MA OFF CWS CWS SPD ALT F/D F/D INTV INTV ON ON DISENGAGE N1 SPEED LVLCHG HDGSEL APP ALTHLD V/S UP OFF OFF 15 MINS FPV MTRS BARO RADIO BARO IN HPA RST STD ANTI-ICE ENG MASTER FIRE 10 VOR 1 OFF APP VOR MAP PLN 20 10 40 80 160 VOR 2 HYD DOORS OVERHEAD AIR COND CAUTION PUSH TO RESET WARN BELL CUTOUT CTR 5 TFC 320 OFF ADF 1 640 ADF 2 WXR STA WPT ARPT DATA POS TERR CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Copyright © The Boeing Company. See title page for details. 1.20.6 D6-27370-TBC March 29, 2004 Airplane General, Emergency DO NOT USE FOR FLIGHT Equipment,Instrument Doors, Windows - Panels 737 Flight Crew Operations Manual Center Forward Panel [Option - Typical 737-600 with EFIS/MAP displays] 7 10 14 9 YAW DAMPER AUTO BRAKE N1 SET SPD REF AUTO AUTO AUTO BRAKE 1 BOTH V1 DISARM NOSE 2 5 GEAR 2 SET VR 2 1 10 NOSE 1 3 GEAR WT UP 15 GYRO 30 FUEL FLOW VREF OFF MAX LEFT RIGHT FLAPS 25 GEAR GEAR 20 RESET 10 MFD RTO 30 40 LEFT RIGHT RATE ENG SYS ANTISKID GEAR GEAR 10 USED ANTISKID LE FLAPS LE FLAPS 20 INOP INOP TRANSIT EXT 30 APP OFF B/CRS UP L A 9 0 1 7 14 9 N D I 16 0 0 0 2 N G OFF 7 3 10 ALT MB IN HG 6 4 1013 5 2992 G E 250 300 A R BARO IAS KNOTS DN HDG LANDING GEAR LIMIT (IAS) V OPERATING V EXTEND 270-.82M O O RETRACT 235K R R EXTENDED 320K-.82M FLAPS LIMIT (IAS) ADF ADF 1-250K 15-185K 2-250K 25-175K INOP 5-250K 30-160K 10-210K 40-155K 12 13 7 230K ALT FLAP EXTEND CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Copyright © The Boeing Company. See title page for details. March 29, 2004 D6-27370-TBC 1.20.7 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels DO NOT USE FOR FLIGHT 737 Flight Crew Operations Manual [Option - Typical 737-700 with EFIS/MAP displays] 7 10 14 9 YAW DAMPER AUTO BRAKE N1 SET SPD REF AUTO AUTO AUTO BRAKE 1 BOTH V1 DISARM NOSE 2 5 GEAR 2 SET VR 2 1 10 NOSE 1 3 GEAR WT UP 15 GYRO 30 FUEL FLOW VREF OFF MAX LEFT RIGHT FLAPS 25 GEAR GEAR 20 RESET 10 MFD RTO 30 40 LEFT RIGHT RATE ENG SYS ANTISKID GEAR GEAR 10 USED ANTISKID LE FLAPS LE FLAPS 20 INOP INOP TRANSIT EXT 30 APP OFF B/CRS UP L A 9 0 1 7 14 9 N D I 16 0 0 0 2 N G OFF 7 3 10 ALT MB IN HG 6 4 1013 5 2992 G E 250 300 A R BARO IAS KNOTS DN HDG LANDING GEAR LIMIT (IAS) V OPERATING V EXTEND 270-.82M O O RETRACT 235K R R EXTENDED 320K-.82M FLAPS LIMIT (IAS) ADF ADF 1-250K 15-195K 2-250K 25-170K 5-250K 30-165K 10-210K 40-156K 12 13 7 230K ALT FLAP EXTEND CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Copyright © The Boeing Company. See title page for details. 1.20.8 D6-27370-TBC March 29, 2004 Airplane General, Emergency DO NOT USE FOR FLIGHT Equipment,Instrument Doors, Windows - Panels 737 Flight Crew Operations Manual [Option - Typical 737-800/900 with PFD/ND displays] 7 10 14 9 YAW DAMPER AUTO BRAKE N1 SET SPD REF AUTO AUTO AUTO BRAKE 1 BOTH V1 DISARM NOSE 2 5 GEAR 2 SET VR 2 1 10 NOSE 1 3 GEAR WT UP 15 GYRO 30 FUEL FLOW VREF OFF MAX LEFT RIGHT FLAPS 25 GEAR GEAR 20 RESET 10 MFD RTO 30 40 LEFT RIGHT RATE ENG SYS ANTISKID GEAR GEAR 10 USED ANTISKID LE FLAPS LE FLAPS 20 INOP TRANSIT EXT 30 APP OFF B/CRS UP L A 9 0 1 7 14 9 N D I 16 0 0 0 2 N G OFF 7 3 10 ALT MB IN HG 6 4 1013 5 2992 G E 250 300 A R BARO IAS KNOTS DN HDG LANDING GEAR LIMIT (IAS) V OPERATING V EXTEND 270-.82M O O RETRACT 235K R R EXTENDED 320K-.82M FLAPS LIMIT (IAS) ADF ADF 1-250K 15-200K 2-250K 25-190K 5-250K 30-175K 10-210K 40-162K 12 13 7 230K ALT FLAP EXTEND CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Copyright © The Boeing Company. See title page for details. March 29, 2004 D6-27370-TBC 1.20.9 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels DO NOT USE FOR FLIGHT 737 Flight Crew Operations Manual [Option - Typical 737-900 with Integrated Standby Flight Display and PFD/ND] 7 10 14 9 YAW DAMPER AUTO BRAKE N1 SET SPD REF AUTO AUTO AUTO BRAKE 1 BOTH V1 DISARM NOSE 2 5 GEAR 2 SET VR 2 1 10 NOSE 1 3 GEAR WT UP 15 FUEL FLOW VREF OFF MAX LEFT RIGHT FLAPS 25 GEAR GEAR RESET 30 MFD RTO 40 LEFT RIGHT RATE ENG SYS ANTISKID GEAR GEAR USED ANTISKID LE FLAPS LE FLAPS INOP TRANSIT EXT UP L APP HP/IN A APP 29.92 IN 13200 7 14 9 N D 240 I 13000 N 220 10 G OFF 10 1 200 40 12 720 12600 G 180 10 E A 160 R DN ATT RST BARO LANDING GEAR LIMIT (IAS) OPERATING EXTEND 270-.82M RETRACT 235K EXTENDED 320K-.82M FLAPS LIMIT (IAS) 1-250K 15-200K 2-250K 25-190K 5-250K 30-175K 10-210K 40-162K 12 13 7 230K ALT FLAP EXTEND CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Copyright © The Boeing Company. See title page for details. 1.20.10 D6-27370-TBC March 29, 2004 Airplane General, Emergency DO NOT USE FOR FLIGHT Equipment,Instrument Doors, Windows - Panels 737 Flight Crew Operations Manual Forward Aisle Stand [Option - Typical Liquid Crystal Display MCDU] 11 7 11 INIT BRT INIT BRT REF RTE CLB CRZ DES REF RTE CLB CRZ DES DEP DEP MENU LEGS ARR HOLD PROG EXEC MENU LEGS ARR HOLD PROG EXEC N1 FIX N1 FIX LIMIT A B C D E LIMIT A B C D E PREV NEXT NEXT PREV NEXT NEXT C PAGE PAGE PAGE F G H I J C PAGE PAGE PAGE F G H I J A N A N L S L S L 1 2 3 K L M N O G L 1 2 3 K L M N O G F O F O A F A F I 4 5 6 P Q R S T S I 4 5 6 P Q R S T S L T L T 7 8 9 U V W X Y 7 8 9 U V W X Y . 0 +/- Z SP DEL / CLR . 0 +/- Z SP DEL / CLR CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Copyright © The Boeing Company. See title page for details. March 29, 2004 D6-27370-TBC 1.20.11 Airplane General, Emergency DO NOT USE FOR FLIGHT Equipment, Doors, Windows - Instrument Panels 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 1.20.12 D6-27370-TBC March 29, 2004 Airplane General, Emergency DO NOT USE FOR FLIGHT Equipment,Instrument Doors, Windows - Panels 737 Flight Crew Operations Manual 20 Instrument Panels 737-600/700 Forward Overhead Panel [Option - Typical 737-600/700 Forward Overhead Panel] 9 13 6 VOICE AUTO 5 OVERHEAT OVERHEAT OVERHEAT OVERHEAT RECORDER ON ON ON ON ON L WINDOW HEAT R FLT CONTROL STANDBY DC AMPS CPS FREQ OVHT SIDE FWD FWD SIDE AIR TEMP PASS CABIN 1 A B HYD CONT CABIN OFF OFF SUPPLY PASS LOW DUCT CABIN QUANTITY STBY STBY ON PWR TEST ON AIR MIX AIR MIX RUD RUD LOW VALVE VALVE H H OFF OFF PRESSURE CAPT PROBE F/O D D COL COL OT OT STBY PITOT A B PITOT OFF A ON B ON RUD ON L ELEV R ELEV PITOT PITOT ALTERNATE FLAPS 60 OFF CIRCUIT BREAKER L ALPHA ON R ALPHA 40 TEMP DC VOLTS / AC AMPS / AC VOLTS VANE VANE 80 LOW LOW UP HEAT DUCT DUCT TEMP AUX OVERHEAT 20 OVERHEAT 2 PRESSURE PRESSURE PROBE PITOT OFF BAT DISCHARGE TR UNIT ELEC 100 SPOILER 0 DOWN MAINT °C A B ARM OFF AUTO AUTO 3 TR1 APU GEN NORMAL NORMAL BAT TR2 GEN1 GEN2 PANEL COOL WARM OFF OFF COOL WARM BAT TR3 GRD INV FEEL COWL COWL COOL WARM COOL WARM DIFF PRESS BUS PWR ANTI-ICE ANTI-ICE OFF OFF ON ON MANUAL MANUAL SPEED TRIM STBY TEST STBY TEST L VALVE R VALVE COWL VALVE COWL VALVE FAIL PWR PWR OPEN OPEN OPEN OPEN MACH TRIM OFF ENG YAW DAMPER FAIL OFF OFF OFF WING ANTI-ICE ANTI-ICE DUAL RAM DOOR RAM DOOR YAW OFF AUTO SLAT BAT OFF BLEED FULL OPEN FULL OPEN DAMPER FAIL ON ON LAVATORY 2 ON ON CAB/UTIL IFE/PASS ON OFF 13 SEAT 1 2 RECIRC FAN DC AC 8 ON SMOKE OFF 1 STANDBY PWR OFF 2 EQUIP COOLING 60 AUTO 2 11 NAVIGATION 80 DRIVE DRIVE EXHAUST DUCT OVHT SUPPLY R L OVERHEAT OVERHEAT 40 VHF NAV IRS STANDBY POWER PRESS NORMAL PSI LOW LOW LOW LOW 0 BOTH BOTH BOTH BOTH DISCONNECT DISCONNECT PRESSURE PRESSURE PRESSURE PRESSURE 20 ON 1 ON 2 ON L ON R TEST ENG 1 ELEC 2 ELEC 1 ENG 2 ALTERNATE NORMAL NORMAL OFF OFF L PACK ISOLATION R PACK BAT OFF AUTO OFF VALVE OFF OFF OFF 1 DISPLAYS AUTO CLOSE AUTO ON ON HIGH HIGH SOURCE CONTROL PANEL A HYD PUMPS B AUTO ALL AUTO ALL EMER EXIT LIGHTS WING PACK PACK WING 10 ON 1 ON 2 BOTH BOTH ANTI TRIP OFF OPEN TRIP OFF ANTI ON 1 ON 2 ICE WING-BODY TRIP WING-BODY ICE FWD FWD FWD OVERHEAT OVERHEAT NORMAL OFF ENTRY SERVICE CARGO BLEED BLEED EQUIP LEFT RIGHT AFT TRIP OFF TRIP OFF ARMED 1 A OVERWING OVERWING CARGO RESET NR AFT AFT GRD POWER OM ON ENTRY SERVICE OFF OFF ENG VALVE ENG VALVE AVAILABLE TE 5 CLOSED 0 CLOSED D FUEL 20 -20 TEMP GRD ON ON SPAR VALVE SPAR VALVE PWR 1 APU 2 CLOSED CLOSED OFF NO FASTEN -40 40 SMOKING BELTS TEST ERASE BLEED C OFF AUTO OFF SCHED ALTN MANUAL ON AUTO FAIL DESCENT ON HEADSET FILTER VALVE FILTER BUS TRANSFER 600 OHMS AUTO MANUAL BYPASS OPEN BYPASS O A COCKPIT VOICE RECORDER TRANSFER F U TRANSFER CROSS FEED BUS OFF F T BUS OFF GRD O PRESS0 ALT V ATTEND CALL DIFF I SOURCE SOURCE 10 PS 1 A OFF OFF HORN FLT ALT L 0 GEN OFF APU GEN GEN OFF 9 50 2 CUTOUT V BUS OFF BUS BUS 40 CABIN 5 E ALT C LOW LOW 35 O PRESSURE PRESSURE L P OFF OFF CALL 30 O 8 3 12 E FUEL PUMPS 25 10 S E N OFF ON ON GEN 1 APU GEN GEN 2 20 15 ALTN 2 7 L R 4 AUTO MAN APU 6 LAND ALT ON 5 CTR MAINT LOW OIL PRESSURE FAULT OVER SPEED LOW LOW LOW LOW PRESS DIFF PRESSURE PRESSURE PRESSURE PRESSURE L WIPER R WIPER LIMIT:TAKE- 1 2 OFF & LDG PARK PARK .5 AFT FWD FWD AFT 10 EGT INT INT .125 PSI UP ABI N CLIM 3 2 OFF OFF 8 B C CAB ALT LAND ALT 2000 FUEL 0 4 4000 6000 8000 6 LOW LOW FLT ALT 7 PUMPS MIN <FL160 FL220 FL260 FL320 FL410 100 0 DN 0F ON ON 4 EET PER 3 2 .5 HIGH HIGH 1 2 1 2 N T I O D L E X RETRACT LANDING OFF L RUNWAY TURNOFF R TAXI APU 3 GRD OFF CONT ENGINE START GRD OFF CONT LOGO OFF STEADY ANTI POSITION COLLISION WING OFF OFF WHEEL WELL OFF N T I O D L E O T OFF OFF BOTH E O X C E OFF FLT IGN IGN FLT OFF X C K K N ON ON L R D L ON R L ON R ON ON STROBE & ON ON ON RETRACTABLE FIXED STEADY START 1 2 1 1 7 CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Copyright © The Boeing Company. See title page for details. September 24, 2007 D6-27370-TBC 1.20.13 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels DO NOT USE FOR FLIGHT 737 Flight Crew Operations Manual 737-800/900 Forward Overhead Panel [Option - Typical 737-800/900 Forward Overhead Panel] 9 13 6 FLT CONTROL STANDBY OVERHEAT OVERHEAT OVERHEAT OVERHEAT A B HYD LOW QUANTITY ON ON ON ON STBY STBY RUD RUD LOW L WINDOW HEAT R PRESSURE OVHT OFF OFF DC AMPS CPS FREQ PASS SIDE FWD FWD SIDE AIR TEMP 1 STBY A ON B ON RUD ON OFF OFF CAB ALTERNATE FLAPS ON ON 120 160 TEMP . S U D AFT FWD AFT PWR TEST 80 OFF 200 P U F UP P C W R LOW LOW CAPT PROBE F/O 40 P PRESSURE PRESSURE PITOT A OFF B PITOT F L T D A OFF Y SPOILER L ELEV R ELEV CONT L C PITOT PITOT TRIM AIR CAB K A B DOWN 2 ARM CIRCUIT BREAKER L ALPHA ON R ALPHA OFF DC VOLTS / AC AMPS / AC VOLTS VANE VANE HEAT TEMP AUX BAT PROBE PITOT ON OFF OFF DISCHARGE TR UNIT ELEC FEEL ZONE ZONE ZONE DIFF PRESS MAINT TEMP TEMP TEMP ON ON OFF 3 SPEED TRIM FAIL TR1 APU GEN CONT CAB FWD CAB AFT CAB BAT TR2 GEN1 GEN2 AUTO AUTO AUTO MACH TRIM PANEL YAW DAMPER FAIL BAT TR3 GRD INV YAW AUTO SLAT BUS PWR COWL COWL DAMPER FAIL ANTI-ICE ANTI-ICE 8 STBY TEST STBY TEST PWR L VALVE R VALVE COWL VALVE COWL VALVE C W C W C W OFF PWR OPEN OPEN OPEN OPEN OFF OFF OFF OFF ENG ON OFF OFF OFF WING ANTI-ICE ANTI-ICE DUAL RAM DOOR RAM DOOR OFF BAT OFF BLEED FULL OPEN FULL OPEN ON ON LAVATORY 2 NAVIGATION ON CAB/UTIL IFE/PASS ON ON 13 SEAT 1 2 L RECIRC FAN R RECIRC FAN VHF NAV IRS DC AC SMOKE OFF OFF BOTH BOTH BOTH BOTH ON 1 ON 2 ON L ON R 1 STANDBY PWR OFF 2 EQUIP COOLING AUTO 60 AUTO 2 11 80 NORMAL NORMAL DRIVE DRIVE DUCT OVHT SUPPLY EXHAUST R L OVERHEAT OVERHEAT 40 STANDBY POWER PRESS FMC NORMAL LOW LOW LOW LOW PSI DISCONNECT DISCONNECT 20 0 BOTH BOTH PRESSURE PRESSURE PRESSURE PRESSURE TEST ON L ON R ENG 1 ELEC 2 ELEC 1 ENG 2 ALTERNATE NORMAL OFF OFF L PACK ISOLATION R PACK BAT OFF AUTO OFF VALVE OFF OFF OFF 1 DISPLAYS AUTO CLOSE AUTO ON ON HIGH HIGH SOURCE CONTROL PANEL A HYD PUMPS B AUTO ALL AUTO ALL EMER EXIT LIGHTS WING PACK PACK WING 10 ON 1 ON 2 BOTH BOTH FWD FWD ANTI TRIP OFF OPEN TRIP OFF ANTI ON 1 ON 2 ENTRY SERVICE ICE WING-BODY TRIP WING-BODY ICE OVERHEAT OVERHEAT NORMAL OFF LEFT FWD RIGHT FWD AIRSTAIR OVERWING OVERWING FWD CARGO BLEED BLEED AFT TRIP OFF TRIP OFF ARMED LEFT AFT RIGHT AFT 1 A EQUIP RESET OVERWING OVERWING CARGO NR GRD POWER OM ON AFT AFT ENG VALVE ENG VALVE AVAILABLE ENTRY SERVICE OFF OFF TE 5 CLOSED 0 CLOSED D FUEL 20 -20 TEMP GRD ON ON SPAR VALVE SPAR VALVE PWR 1 APU 2 CLOSED CLOSED OFF NO FASTEN -40 40 SMOKING BELTS TEST ERASE BLEED C OFF AUTO OFF SCHED ALTN MANUAL ON AUTO FAIL DESCENT ON HEADSET FILTER VALVE FILTER BUS TRANSFER 600 OHMS AUTO MANUAL BYPASS OPEN BYPASS O A COCKPIT VOICE RECORDER TRANSFER F U TRANSFER CROSS FEED BUS OFF F T BUS OFF GRD O PRESS0 ALT V ATTEND CALL DIFF I SOURCE SOURCE 10 PS 1 A OFF OFF HORN FLT ALT L 0 GEN OFF APU GEN GEN OFF 9 50 2 CUTOUT V BUS OFF BUS BUS 40 CABIN 5 E ALT C LOW LOW 35 O PRESSURE PRESSURE L P OFF OFF CALL 30 O 8 3 12 E FUEL PUMPS 25 10 S E N OFF ON ON GEN 1 APU GEN GEN 2 20 15 ALTN 2 7 L R 4 AUTO MAN APU 6 LAND ALT ON 5 CTR MAINT LOW OIL PRESSURE FAULT OVER SPEED LOW LOW LOW LOW PRESS DIFF PRESSURE PRESSURE PRESSURE PRESSURE L WIPER R WIPER LIMIT:TAKE- 1 2 OFF & LDG PARK PARK .5 AFT FWD FWD AFT 10 EGT INT INT .125 PSI UP ABI N CLIM 3 2 OFF OFF 8 B C CAB ALT LAND ALT 2000 FUEL 0 4 4000 6000 8000 6 LOW LOW FLT ALT 7 PUMPS MIN <FL160 FL220 FL260 FL320 FL410 100 0 DN 0F ON ON 4 EET PER 3 2 .5 HIGH HIGH 1 2 1 2 N T I O D L E X RETRACT LANDING OFF L RUNWAY TURNOFF R TAXI APU 3 GRD OFF CONT ENGINE START GRD OFF CONT LOGO OFF STEADY ANTI POSITION COLLISION WING OFF OFF WHEEL WELL OFF N T I O D L E O T OFF OFF BOTH E O X C E OFF FLT IGN IGN FLT X C K K N ON ON L R D L ON R L ON R ON ON STROBE & ON ON ON RETRACTABLE FIXED STEADY START 1 2 1 1 7 CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Copyright © The Boeing Company. See title page for details. 1.20.14 D6-27370-TBC September 27, 2004 Airplane General, Emergency DO NOT USE FOR FLIGHT Equipment,Instrument Doors, Windows - Panels 737 Flight Crew Operations Manual Aft Overhead Panel [Option - Typical Aft Overhead Panel] MIC SELECTOR 5 1-VHF-2-VHF-3 HF SERV INT FLT INT PA IRS DISPLAY 10 15 1-NAV-2 1-ADF-2 MKR SPKR DSPL SEL PPOS WIND N 7 R/T MASK V B R ALT 5 TK/GS HDG/STS 1 3 TEST 2 BRT W H E I/C BOOM NORM 4 5 6 S ENGINE MACH SYS DSPL 1 2 L R 7 8 9 FLIGHT RECORDER AIRSPEED REVERSER REVERSER WARNING ENT CLR TEST 0 EEC EEC TEST NORMAL NO 1 NO 2 SERVICE 11 INTERPHONE ENGINE ON ON ENGINE OFF OFF CONTROL CONTROL ALTN ALTN GPS CREW PASS OXYGEN STALL WARNING TEST ON TRANSIT LE DEVICES TRANSIT ALIGN ON DC ALIGN ON DC OXYGEN NO. 1 NO. 2 FLAPS EXT 1 4 EXT NORMAL 2 3 1 FAULT DC FAIL FAULT DC FAIL 10 FULL FULL EXT EXT 5 15 ALIGN NAV ALIGN NAV 1 8 ON 2 7 OFF ATT OFF ATT 3 6 20 4 5 OXY PRESS SLATS SLATS PASS OXY 15 PSI X 100 ON L IRS R TEST DOME WHITE LEFT RIGHT GEAR GEAR DIM N T I O D L E O 9 PSEU 15 BRIGHT OFF NOSE GEAR 14 N T I O D L E O X C X C K K CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Copyright © The Boeing Company. See title page for details. September 27, 2004 D6-27370-TBC 1.20.15 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels DO NOT USE FOR FLIGHT 737 Flight Crew Operations Manual Control Stand [Option - Typical Control Stand] 7 9 S BR PE AK ED E DOWN ARMED FLAP UP 9 0 1 FLAP STAB STAB TRIM 1 2 TRIM APL 2 APL NOSE FLIGHT NOSE DOWN 5 DETENT DOWN 0 0 15 TAKE-OFF CG-% MAC 5 5 CG-% MAC TAKE-OFF 10 UP 10 10 15 15 APL 15 APL 25 NOSE NOSE UP UP 30 40 PARKING FLAP BRAKE DOWN PULL 14 1 A/T DISENGAGE 2 A/T DISENGAGE 1 2 7 STAB TRIM MAIN AUTO ELECT NORMAL PILOT CUT OUT INTERPHONE 9 5 ELEX PANEL LIGHTS FWD AFT CAPT PASS CENTER ADDRESS F/O 5 CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Copyright © The Boeing Company. See title page for details. 1.20.16 D6-27370-TBC September 27, 2004 Airplane General, Emergency DO NOT USE FOR FLIGHT Equipment,Instrument Doors, Windows - Panels 737 Flight Crew Operations Manual Aft Electronic Panel [Option - Typical Aft Electronic Panel] OVHT DET WHEEL BELL CUTOUT OVHT DET L BOTTLE R BOTTLE WELL DISCHARGED DISCHARGED A B A B ENGINES DISCH FAULT DISCH NORMAL DISCH NORMAL ET XE ENG 1 L R APU DET ENG 2 L R TS 1 2 OVERHEAT OVERHEAT T R INOP TEST L F OF FIRE SWITCHES AIN VI APU BOTTLE (FUEL SHUTOFF) UO DISCHARGED PULL WHEN ILLUMINATED LP HR LOCK OVERRIDE: PRESS TE T BUTTON UNDER HANDLE APU TFR 8 EXT FWD AFT DET SELECT NORM NORM DETECTOR TFR 5 V C C A A B A B FAULT F V C 5 FREQ SEL DISCH I FREQ SEL O R FWD AFT O H G ARM R H M TEST E M F COMM TEST O F COMM TEST M ARMED ARMED M DISCH FWD AFT ACTIVE TFR STANDBY ALT OFF ALT ON 5 10 15 ACTIVE TFR STANDBY STBY TA ATC12 R ATC 3 FL TEST TA/RA FAIL N A V TEST 1 ATC TCAS RANGE ABOVE N A V TEST 11 ATC NORM 11 2 IDENT BELOW 11 MIC SELECTOR WX RADAR MIC SELECTOR WX WX/TURB TEST MAP TILT 5 10 GAIN SERV FLT UP 15 SERV FLT 1-VHF-2-VHF-3 HF INT INT PA 1-VHF-2-VHF-3 HF INT INT PA 0 DN 15 AUTO MAX 5 1-NAV-2 1-ADF-2 MKR SPKR 5 10 1-NAV-2 1-ADF-2 MKR SPKR 5 B B R/T MASK V R ALT R/T MASK V R ALT I/C BOOM NORM I/C BOOM NORM TFR SQUELCH ADF ANT ADF ANT C 5 A O H M D ADF ANT OFF ON F OFF USB AM M F 11 TONE RUDDER TRIM 15 10 5 0 5 10 15 LEFT RIGHT AILERON FLOOD PANEL NOSE NOSE STAB TRIM LEFT RIGHT R U OVERRIDE 1 D LEFT RIGHT WING WING D DOWN DOWN E NORMAL R OFF OFF 9 9 CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Copyright © The Boeing Company. See title page for details. September 27, 2004 D6-27370-TBC 1.20.17 Airplane General, Emergency DO NOT USE FOR FLIGHT Equipment, Doors, Windows - Instrument Panels 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 1.20.18 D6-27370-TBC March 31, 2003 Airplane General, Emergency DO NOT USE FOR FLIGHT Equipment,Instrument Doors, Windows - Panels 737 Flight Crew Operations Manual 20 Instrument Panels Auxiliary Panels [Option - Typical with HUD and EFB installed] (TYPICAL) SPARE BULB B STOWAGE C A D E F G H I J K L SUNVISOR STOWAGE 1 5 10 14 C ESCAPE STRAP D SPEAKER STANDBY H NOSE WHEEL STOWAGE G MAGNETIC STEERING E MAP LIGHT COMPASS F CHART LIGHT 5 I CHART AND MAP LIGHT CONTROLS J OXYGEN MASK BRT MENU DIM PGUPPGDN XFRENTER PWR PANEL HEAD PHONE BOOM MIKE HAND MIKE BOOM MIKE HEAD PHONE L A K B EFB CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Copyright © The Boeing Company. See title page for details. March 27, 2009 D6-27370-TBC 1.20.19 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels DO NOT USE FOR FLIGHT 737 Flight Crew Operations Manual Attendant Panels Forward Attendant Panel [Option - Typical] LIGHTING DIM MEDIUM DIM BRIGHT OFF BRIGHT OFF NIGHT ENTRY CEILING 1 DIM OFF BRIGHT WINDOW GROUND WORK SERVICE 6 CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Aft Attendant Panel [Option - Typical] POTABLE WATER WASTE SYSTEM LIGHTING F DIM F OFF BRIGHT 3/4 3/4 1/2 1/2 1 1/4 E CLEAN/CHECK SENSOR 1/4 E ENTRY LAVS INOP PRESS TO EMERGENCY VIEW BITE TEST EXIT LIGHTING CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Copyright © The Boeing Company. See title page for details. 1.20.20 D6-27370-TBC March 31, 2003 Airplane General, Emergency DO NOT USE FOR FLIGHT Equipment,Instrument Doors, Windows - Panels 737 Flight Crew Operations Manual Attendant Handset [Option - Typical] LIFT HANDSET PILOT 2 ATTENDANT 5 PA 8 PILOT ALERT 222 1 2 3 5 4 5 6 7 8 9 * 0 # PASSENGER ADDRESS PUSH TO TALK RESET CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Copyright © The Boeing Company. See title page for details. March 31, 2003 D6-27370-TBC 1.20.21 Airplane General, Emergency DO NOT USE FOR FLIGHT Equipment, Doors, Windows - Instrument Panels 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 1.20.22 D6-27370-TBC March 31, 2003 DO NOT USE FOR FLIGHT 737 Flight Crew Operations Manual Airplane General, Emergency Chapter 1 Equipment, Doors, Windows Controls and Indicators Section 30 1.30 Airplane General, Emergency Equipment, Doors, Windows-Controls and Indicators 30 Controls Controls andand Indicators Indicators Flight Deck Lighting Map and Chart Light Controls MAP 1 CHART INOP 2 SIDEWALL PANELS 1 MAP Light Control Rotate – adjusts brightness of Captain/First Officer map lights 2 CHART Light Control Rotate – adjusts brightness of Captain/First Officer chart lights Main Panel Lighting MAIN PANEL 1 OFF LEFT/RIGHT FORWARD PANELS Copyright © The Boeing Company. See title page for details. March 29, 2004 D6-27370-TBC 1.30.1 Airplane General, Emergency DO NOT USE FOR FLIGHT Equipment, Doors, Windows - Controls and Indicators 737 Flight Crew Operations Manual 1 MAIN PANEL Light Control Rotate – • Captain – controls brightness of Captain’s panel and instrument lighting, center instrument panel, and AFDS panel displays and edge lighting • First Officer – controls brightness of First Officer’s panel and instrument lighting. Background and AFDS Flood Light Control BACKGROUND AFDS FLOOD 1 2 OFF OFF LEFT FORWARD PANEL 1 BACKGROUND Light Control Rotate – controls incandescent lighting brightness for Captain’s panel, First Officer’s panel, and center panel. 2 AFDS FLOOD Light Control Rotate – controls brightness of lighting directed at AFDS panel. Flood and Aft Electronics Lights Controls FLOOD PANEL 1 2 OFF OFF AISLE STAND 1 FLOOD Light Control Rotate – controls overhead spotlight brightness directed at thrust lever quadrant. Copyright © The Boeing Company. See title page for details. 1.30.2 D6-27370-TBC March 29, 2004