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`707 Captain` FLIGHT MANUAL Part II – Aircraft

1. mm OPL DUNWAY COMM WEE RETRACTIBLE LANDING FIXED LANDING TUPNOEE BEACON WING RETRACT alu Edo gih rr ofr orr Dues dea que Wi mal P i r I ir H I r i ae A 1 S i pr a m d NE ON ye ACE y F a gi E E m a s aN NA 25 bale qu 3 z Ket a L X 1 2 3 4 6 7 8 9 10 11 12 1 4 Landing Lights Switch 1 2 Retractable Landing Light Switch ON Retractable landing lights illuminate 3 4 Retract Extend Switch Retract Retracts outboard landing lights Extend extends outboard landing lights 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 50 DO NOT USE FOR FLIGHT 5 6 Taxi Light Switch A taxi light is mounted on the nose wheel strut Fixed Landing Lights Switch ON Fixed landing lights illuminate 7 8 Runway Turnoff Lights Switch A RUNWAY TURNOFF light is adjacent to and inboard of the inboard fixed landing light The lights provide ground roll illumination and are controlled by two switches Note Do not illuminate LANDING and or RUNWAY TURNOFF lights for more than 5 minutes while stationary on the ground Allow a 5 minute cooling period before re illuminating ON Runway turnoff lights illuminate 9 Navigation Lights Switch White tip mounted tail lights are installed on the trailing edges of the wing tips to provide a
2. Fuel Leak failure Generator Eng 1 4 failure Hydraulic Leak Reservoir 1 4 failure Hydraulic Pump Eng 2 3 failure Hydraulic Pump Elec 1 2 failure Left Brake failure Left Gear failure Pitot Tube failure Right Brake failure Right Gear failure Static Port failure RADIOS ADF1 ADF2 failure COM1 COM2 failure NAV1 NAV2 failure ENGINES Complete Failure Eng 1 4 Fire Eng 1 4 Ignition failure Eng 1 4 Oil Leak Eng 1 4 Oil System failure Eng 1 4 CONTROLS Elevator failure Left Right Aileron failure Left Right Flap failure Rudder failure To set up the failures go FSX menu Aircraft gt Failures www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 10 DO NOT USE FOR FLIGHT CUSTOMER CARE You are invited to join Captain Sim community forum DAILY NEWS For Captain Sim daily news please follow us at Twitter or Facebook VIDEO CHANNEL For Captain Sim videos please watch our YouTube channel TECH SUPPORT The 707 Captain is the most advanced complete and accurate digital replica of the B707 ever available for any game platform Our product is not perfect unfortunately nothing is But we are working on improvements If you have some important issue to report please check in to Your Profile then click Product Name gt Customer Support gt and use the Trouble Ticket System We process all tickets
3. 1 Radar Mode Selector WY RADAR Seidi 2 ANT TILT itg s TH Y mg TEST Y X fv 1 Fa 1 Radar Mode Selector STBY Fully energizes the system circuitry but no radar transmissions occur in the SBY mode of operation The antenna is parked at O degrees azimuth and 30 degrees tilt down with the antenna drive motors locked WX NORM Selects the normal condition of op eration for weather detection The system will transmit after a 60 second warm up time is com pleted The radar system initializes to the Wx mode 50 nm Note The 60 second warm up period can be mon itored upon power up of the system When the knob is switched directly from OFF to ON mode the display will blank Just before the warm up period is complete the screen will turn black for a few seconds then the radar will begin transmitting and the screen will display radar returns No radar transmis sions occur until the warm up period is com plete 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 58 DO NOT USE FOR FLIGHT WX CTR Selects weather alert mode of opera tion Black color for heavy and intense returns TEST Transmitter de energized contrasting test signals are imposed on the indicator signify ing proper circuit functions ANT TILT Permits manual adjustment of antenna tilt 15 up right click or down left click for best indicator presen
4. 85 DO NOT USE FOR FLIGHT 1 Duct Overheat Light Amber Illuminated Duct temperature 195 F or above Cabin temperature control valves positioned to full cold Automatic system inoperative until reset with reset switch when cooled 2 Duct Overheat Reset Button Resets DUCT OVERHEAT or AIR COND UNIT pack OFF condition For DUCT OVERHEAT resets when duct temperature below 190 F Reactivates temperature selector CREW or MAIN light goes out For AIR COND UNIT pack OFF LEFT and RIGHT pack valve opens OFF light goes out 3 Main Duct Overheat Light Amber Lights when CREW or MAIN duct temperature over 190 F CREW or MAIN temperature selector deactivated Temperature control valve automatically driven full cold 4 Cabin Air Temperature Indicator Shows C air temperature of area selected by Cabin air temperature select switch 5 Cabin Air Temperature Source Selector Switch Arms TEMP indicator to show temperature of area selected OR On some airplanes AIR TEMP selects CABIN or DUCT temperature only 7 Main Temperature Selector AUTOMATIC Arms regulator which modulates control valves to maintain selected 65 to 85 F temperature Arms FAULT light MANUAL Deactivates regulator Deactivates FAULT light Allows fast direct adjustment of control valves COOLER Drives control valves toward full cold OFF Selector spring loaded to this position Maintains position of control valves
5. Connects VR output to generator field generator activated TRIP Disconnects VR output from generator field generator activated 46 49 KW KWAR Meter Indicates generator real KW or reactive KVAR load Indication is controlled by Powermeter Button 61 50 53 Frequency Control Knobs When rotated Permits frequency adjustment of an isolated generator Balances Kw loads when generators paralleled 54 Essential Power Failure Warning Light ON loss of essential power OFF Essential power being supplied 55 Essential Power Source Selector Selects power source for essential AC bus 56 Frequency Meter Indicates frequency as selected generator isolated bus tie sync tie bus or external power 57 AC Voltmeter Indicates voltage as selected generator isolated bus tie sync tie bus or external power A to 30 scale is used when checking residual voltage of an isolated generator A generator must be isolated to check its voltage The voltmeter will indicate bus tie voltage if a generator position is selected when generators are operating parallel 60 AC Paralleling Selector Connects frequency meter and voltmeter to generator bus tie sync tie bus or external power Connects sync lights for paralleling 61 Powermeter Button Changes U03 ELECTRICAL SYSTEM PANEL Power Meters indication from real KW to reactive KVAR load display www captainsim com 707 Captain FLIGH
6. 5 6 9 54 Engine 2 3 1 4 Valve Position Transit Lights Blue 7 8 14 15 Engine 2 3 4 1 Fuel Shutoff Valve Switches 10 13 20 23 36 37 Fuel Boost Pump Low Pressure Light 16 17 18 19 24 25 26 27 28 29 Fuel Boost Pump Switch 30 33 48 52 55 Fuel Quantity Gage 34 35 38 41 Fuel Shutoff Valve In Transit Lights Blue 42 45 Manifold Valve Switches 46 47 Transfer Valve Switches 49 Push To Test Button 50 Totalizer Gage 51 Fuel Temperature Indicator 52 Fuel Quantity Gage 53 Fuel Temperature Selector 2011 Captain Sim www captainsim com 89 DO NOT USE FOR FLIGHT 1 4 Engine 1 2 3 4 Fuel Pressure Gages Indicates pressure at engine driven fuel pump inlet Normal operating pressure is about 0 psi pumps off 15 psi main tank pumps on 40 psi center tank pumps on Fuel pressure decreases as fuel flow increases Pressure increases after shutdown due to expansion of fuel trapped in the engine feed line 5 6 9 Engine 2 3 1 4 Valve Position Transit Lights Blue ON during respective valve transit OFF Valve corresponds with the switch that activated it 7 8 14 15 Engine 2 3 4 1 Fuel Shutoff Valve Switches OPEN Permits fuel flow to engine CLOSE Shuts off fuel flow to engine at the pylon Valve closes and switch deactivated when fire handle pulled 16 17 18 19 24 25 26 27 28 29 Fuel Boost Pump Switch Control main tank and center tank boost pumps 10 13 20 23 36 37 Fuel Boost Pump L
7. 7 TRANSPONDER CONTROL PANEL 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 55 DO NOT USE FOR FLIGHT PO2 PO6 FLIGHT DIRECTOR CONTROLS Note Flight director is connected with the autopilot Do not engage the autopilot if you need to use F D only 1 Pitch Command Control Knob 2 F D Mode Selector 3 Altitude Hold 1 Pitch Command Control Knob Positions pitch command bar to selected pitch angle 2 F D Mode Selector Selects flight director mode VOR HDG and NAV LOC Pitch command bar manually positioned by pitch command control knob Roll command bar positioned by VOR or HDG steering commands from flight director computer NAV LOC Pitch command bar manually positioned by pitch command control knob Roll command bar positioned by Doppler Navigation System or or CIVA INS steering commands from flight director computer See Doppler Navigation System Section for details APP AUTO MAN Pitch command bar positioned by ILS glide slope steering commands from flight director computer Roll command bar positioned by ILS localizer steering commands from flight director computer 3 Altitude Hold Pitch command bar commands pitch input to hold constant altitude WEATHER RADAR THEORY OF OPERATION The primary use of this radar is to aid the pilot in avoiding thunderstorms and associated turbulence Since each operator normally develops specific operat
8. L17 DOPPLER INS SWITCH L18 MARKER LIGHTS 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 9 DO NOT USE FOR FLIGHT LO1 10 MILE ALERT LIGHT 1 10 Mile Alert Light e Iluminates when less then 10 miles to go on one stage e Intermittently illuminates when stage transfer has not taken place and aircraft has completed stage 000 miles to go L02 CLOCKS 1 Elapsed Time Hours Minutes Hands 2 4 Hours And Minute Hands 3 2 3 Elapsed Time Switch 4 5 Winding amp Setting Control 6 Lower Minute Register Hand 7 Sweep Second Hand 5 7 6 8 8 Push Button 1 Elapsed Time Hours Minutes Hands Controlled by elapsed time switch 3 Elapsed Time Switch e Rotating switch clockwise to 0 resets elapsed time hands to 12 o clock position e Rotating switch clockwise to GO starts elapsed time hands e Rotating switch clockwise to STOP stops elapsed time hands 6 Lower Minute Register Hand Controlled by push button 8 Push Button With sweep second hand at the 12 o clock position Pushing button once starts the second hand pushing a second time stops the hand pushing a third time resets hand to 12 o clock position Minute register hand indicates elapsed time in minutes of sweep second hand 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 10 DO NOT USE FOR FLIGHT AUTOPILOT DISENGAGED W
9. 2 OFF Light 3 Q inlet Heat Switch 1 Probe Heater Switch ON Applies electrical power to heat Captain s pitot Q inlet Attitude warning vanes 2 OFF Light Monitors power to Q inlet heater ON Indicates power failure to Q inlet heater OFF System normal or control switch off 3 Q inlet Heat Switch Controls power to Q inlet heater 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 52 DO NOT USE FOR FLIGHT O22 WINDOW HEAT PANEL 1 4 Window Heat Switches 2 3 Window Overheat Lights 1 4 Window Heat Switches With the switch in either HIGH or LOW the overheat protection system may be tested by pressing the overheat light cap This applies power to the windows and after about one second a simulated overheat condition is created the light illuminates power is removed and must be reset Note To reset power after actual or test overheat select window heat control to OFF then HIGH or LOW 2 3 Window Overheat Lights ON respective anti iced windows have overheated and power has been removed power must be reset OR power to respective system has failed OFF System normal O23 PITOT STATIC HEAT PANEL 1 2 3 1 Captain s Pitot and Attitude Warning Sensor Heat Switch 2 Ammeter Switch 3 First Officer s Pitot and Attitude Warning Sensor Heat Switch 4 Captain s Pitot Heater Ammeter ei 5 Fiirst Officer s or 3r
10. 7 Drift Angle and Ground Speed will be shown on the Doppler Indicator 8 Put Autopilot Mode Selector to NAV position aircraft will follow the route Point 3 Point 2 Leg B Leg A Point 1 where route activated Point 3 Leg B Point 2 Leg A Point 1 where route activated F MAN Mode MAN mode is for one leg route operations only Either leg A or B can be selected first If leg A is selected DNS will calculate the leg A as active going to point 2 Standby leg B can be corrected any at time Stage Selector can be turned to B position at any moment to activate the leg B If leg B is selected DNS will calculate the leg B as active going to point 3 Standby leg A can be corrected any at time Stage Selector can be turned to A position at any moment to activate the leg A AUTO Mode AUTO mode is for two and more legs route operations providing automatic activation of the next leg This is how the same route setup will work in AUTO mode If leg A is selected DNS will calculate the leg A as acive going to point 2 When the distance to go to the point 2 equals to aircraft turn radius to the leg B Stage Selector automatically turns to B position activating the leg B Notes Standby leg B can be corrected any at time before its automatic activation at the point 2 If Stage Selector is turned to middle position current route remains active until position A or B are selected If your rout
11. Aircraft and Systems 37 DO NOT USE FOR FLIGHT 2 OFF Flag Appears if power interrupted 3 SAT Indicator True SAT obtained from captain s CADS 4 OFF Flag Covers readout if power of CADS fails R14 RUDDER BOOST LOW PRESSURE LIGHT 1 1 Rudder Boost Low Pressure Light Deactivated above 250 kt ON below 250 kt indicates insufficient rudder boost pressure R17 HYDRAULIC SYSTEM PANEL 1 2 3 4 8 3 s HCA RE SYSTEkA L P 4 A n iJ La 1 2 Engine Pumps Low Pressure Lights 3 4 AC Auxiliary Pump Low Pressure Lights 5 7 Engine Pump Switches 6 Utility Hydraulic System Pressure 8 Hydraulic Brake Pressure Gage 9 10 AC Auxiliary Pump Switches 11 Rudder Hydraulic Pressure Gage 12 Interconnect Valve Switch 1 2 Engine Pumps Low Pressure Lights OUT Pressure normal ON Pressure below limits Light is deactivated when respective fire handle is pulled Powered from HYD PRESS amp DOOR WARN LT CB on P5 TR bus No 3 2011 Captain Sim www captainsim com 38 DO NOT USE FOR FLIGHT 3 4 AC Auxiliary Pump Low Pressure Lights OUT Pressure normal ON Pressure below limits Each light is powered from the other aux pump control CB 5 7 Engine Pump Switches When positioned to ON Allows pump to develop pressure OFF Shuts off pump s output but pump still rotates If electric power fails pump is reactivated Both switches are powered from a PUMP VALVES CB on P5 T
12. ram air exit valves as follows OPEN runs valve toward open position 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 97 DO NOT USE FOR FLIGHT OFF is spring loaded position with no valve movement CLOSE runs valve toward closed position if over 90 closed associated turbofan exit valve will open Note EXIT VALVE switches deactivated and exit valves overridden open when main cabin temperature control valve within 35 of full closed cold 7 8 Left amp Right Turbofan Exit Valve Override Switches OPEN overrides left L and right R turbofan exit valves open in flight NORMAL valve position controlled by landing gear oleo SQUAT switch 502 AUXILIARY TEMPERATURE CONTROL PANEL m AUX CREW HEAT VALVE 1 Main Cabin Heating Panels Switch j v 3 2 Gasper Air Fan Switch 3 3 Auxiliary crew heat valve switch 4 5 FWD and MID Zone Indicators 6 Overheat Light 4 5 7 8 Cabin Temperature Zone Control Switch 6 7 LO COMTROL 1 Main Cabin Heating Panels Switch ON sends electrical power to heating panels in cargo door OFF removes power from heating panels 2 Gasper Air Fan Switch When on applies power to electric fan in air distribution bay to accelerate airflow through various eyeball outlets 3 Auxiliary Crew Heat Valve Switch Controls valve that allows hot pneumatic air to flow into cockpit distribution duct via an alternate
13. Lights Amber 5 8 Fuel Heaters Eng 1 2 3 4 Switches 1 4 Fuel Icing Eng 1 2 3 4 Lights Amber Amber warning light that comes on when fuel flow through the filter is restricted by ice crystals or foreign matter 5 8 Fuel Heaters Eng 1 2 3 4 Switches Control the fuel heater bleed air valve When positioned to ON Valve opens N2 bleed air is ported through the fuel heater OFF Valve closes 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 91 DO NOT USE FOR FLIGHT W04 HYDRAULIC PANEL E on 1 Engine Oil Quantity Test Switch QUANT TY PUSH UP TO 2 GAGES No Airflow Warning Light 3 Valve Open Light 1 4 Blower Switch 2 5 Overboard Dump Valve Switch a 6 L H Bottle Inactive Light Red 7 Engine Start Air Pressure Indicator a 8 Hydraulic Reservoir Quantity Gage OPES 9 Hydraulic Fluid Shutoff Eng No 2 Switch OVRD DUM F 10 Hydraulic Fluid Shutoff Eng No 3 Switch 6 7 8 HYD FLUID SHUTOFF 9 AC 2011 Captain Sim www captainsim com DO NOT USE FOR FLIGHT 1 Engine Oil Quantity Test Switch Spring loaded Tests gage circuitry When pushed up all four quantity gages are monitorized to zero When released gages return to pretest indications 2 No Airflow Warning Light ON Insufficient cooling airflow Lights within 10 minutes of airflow loss 3 Valve Open Light ON Auto shutoff valve in any open positio
14. Master Switch ON or TEST Bypasses oleo relay on the ground 508 LIGHTS CONTROL PANEL 1 z 1 Upper Panel Background Lights Control Switch 2 Lower Panel Background Lights Control Switch OFF UPPER PAHEL LOWER PANEL S12 AUDIO SELECTOR PANEL 1 2 3 4 1 5 9 15 Communication Receiver Switches a NAVI24 6 Transmitter Selector Fa MI HIER OLE FAHRE Mo M V 7 Microphone Push to talk Switch WHF 3 HET 4 ENER PT 2 7 r ADF 1 COMM RECS ar ADF 2 WCE RANGE yer VEES VRE3 VO CE RANSE 1 5 9 15 Communication Receiver Switches Switches on each audio selector panel are used to connect audio from a selected facility to the associated crew member s headphones or loudspeaker at the Captain s F O s stations Any one or any combination of audio facilities can be monitored by moving the appropriate switches to the UP position provided the emergency audio switch is in NORM position 6 Transmitter Selector Selects desired transmitter 7 Microphone Push to talk Switch Press to transmit through oxygen mask or boom microphone 2011 Captain Sim www captainsim com 10 DO NOT USE FOR FLIGHT FAILURES The 707 Captain supports the following failures INSTRUMENTS Airspeed Indicator failure Altimeter failure Vertical Speed Indicator failure SYSTEMS Brake Hydraulic Source failure Center Gear failure Electrical failure
15. These two switches on the overhead panel are adjacent to the alternate flaps master switch The switches marked INBD and OUTBD have UP OFF DN positions and are spring loaded from the DN position to the OFF position When either alternate flap switch is in the DN position the corresponding trailing edge flaps extend electrically and the leading edge flaps standby drive shutoff valve will open causing all leading edge flaps and slats to extend When the alternate flap switches move from the DN position to the OFF position the leading edge flaps and slats will continue to extend or remain extended as long as the alternate flaps master switch is in the ON position The trailing edge flaps will stop When the alternate flap switches are in the UP position with the leading edge flaps and slats extended and the alternate flaps master switch in the ON position the leading edge flaps and slats will remain extended and the corresponding trailing edge flaps will retract The leading edge flaps and slats cannot be retracted using the alternate flap system 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 42 DO NOT USE FOR FLIGHT 002 LIGHTS CONTROLS 1 2 1 Overhead Panel Lights OVERHE ADIIP ANI TTE T 2 Dome White an oH 3 Left FWD Panel Lights 4 Center FWD Panel Lights CENTER FWD PANEL ARAITH p 1 Overhead Panel Lights Control integral instrument Illumination o
16. Valve Switches 5 6 Left amp Right Exit Valve Switches 7 8 Left amp Right Turbofan Exit Valve Override Switches ce W T J AY TURBOFAN EXIT YALWE OVERRIDE 1 Valve Position Indicator Shows positions of ram air and temperature control valves set by VALVE SELECTOR switch in 25 increments from CLOSED cold_ to OPEN hot LH CREW scale displays LH ram air duct valves or cockpit temperature control valve RH MAIN scale displays RH ram air duct valves or main cabin temperature control valve Note Ram inlet is open 12 square inches when indicator shows inlet valve full closed 2 Valve Selector Switch Connects VALVE POSITION indicator as follows OFF deactivates the indicator INLET gives ram air inlet valve display EXIT gives ram air exit valve display SEC HEAT EXCH gives secondary heat exchanger valves display TURBOFAN EXIT gives turbofan exit valves display TEMP CONTROL gives crew and main cabin temperature control valves display 3 4 Left amp Right Inlet Valve Switches Give manual control of left L and right R ram air inlet valves as follows OPEN runs valve toward open position OFF is spring loaded position CLOSE runs valve toward closed position Note INLET VALVE switches deactivated and inlet valves overridden open when main temperature control valve within about 35 of full closed cold 5 6 Left amp Right Exit Valve Switches Give manual control of left L and right R
17. WARMER Drives control valves towards full hot position 8 9 Fault Light White Neon Shows mailfunction of regulator topping or anticipator sensing circuitry 10 Cabin Pressure Override Switch NORM guard down Deactivates FWD VALVE and AFT VALVE switches Forward and aft outflow valves controlled pneumatically www captainsim com 86 DO NOT USE FOR FLIGHT OVERRIDE guard up Arms FWD VALVE and AFT VALVE switches to permit alternate electrical positioning of forward and aft outflow valves 11 Cabin Air Thrust Valve Position Switch NORMAL Allows the thrust recovery valves to operate pneumatically OFF Electrically overrides the thrust recovery valves to closed position www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 87 DO NOT USE FOR FLIGHT FLIGHT ENGINEER LOWER PANEL a RENE _ LLLI BELA wos WO1 FUEL SYSTEM PANEL W02 FUEL HEATERS PANEL W04 HYDRAULIC PANEL WO05 ENGINES GAUGES W06 DOOR ANNUNCIATOR PANEL W07 AIRBORNE VIBRATION MONITOR 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 88 WO1 FUEL SYSTEM PANEL 9 1 2 7 2 3 g 5 4 24 mU en xm 4 FUEL SEMIS ENQ 2 2 o l Tr L Liv RESERVE TAH K FUEL TEMP 3E PUSH TO TEST s S i FUEL aces nq A pA E ML G 48 49 t 21 3 32 1 4 Engine 1 2 3 4 Fuel Pressure Gages
18. adjacent targets in azimuth is a function of the beam width of the antenna and the range to the target The diameter of this radiated beam increases as it gets further away from the aircraft Targets separated by a distance less than the beam diameter at the target distance will merge and appear on the indicator as one PATH PLANNING Remember to plan a deviation path early Simply skirting the red or magenta portion of a cell is not enough Plan an avoidance path for all weather echoes which appear beyond 100 nautical miles since this indicates they are quite intense The most intense echoes are severe thunderstorms Remember that hail may fall several miles from the cloud and hazardous turbulence may extend as much as 20 nautical miles therefore echoes should be separated by at least 40 nautical miles before you fly between them As echoes diminish in intensity you can reduce the distance by which you avoid them PATH PLANNING CONSIDERATIONS e Avoid cells containing magenta and red areas by at least 20 nautical miles e Do not deviate downwind unless absolute necessary Your chances of encountering severe turbulence and damaging hail are greatly reduced by selecting the upwind side of the storm e If looking for a corridor remember corridors between two cells containing magenta and or red areas should be at least 40 nautical miles wide from the outer fringes of the radar echo The magenta displays areas of very heavy rainfall and
19. beam is seeing The following figure is a side view of the radar beam characteristic with a storm depicted at a distance that causes the size of the storm to just fill the 3 dB beamwidth This would be the typical situation for a storm at approximately 40 nautical miles with a 12 inch diameter antenna It s im portant to understand and visualize this situation to enhance your understanding of the rest of this manual ANTENNA GAIN vs ANGLE CHARACTERISTIC N Y SIDELOBS 3db BEAMWIDTH RADAR REFLECTIVITY What target will reflect the radar s pulses and thus be displayed on the indicator Only precipitation will be detected by an X band weather radar Therefore weather radar does not detect clouds thunderstorms or turbulence directly Instead it detects precipitation which may be associated with dangerous thunderstorms and turbulence The best radar reflectors are raindrops and wet snow or hail The larger the raindrop the 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 57 DO NOT USE FOR FLIGHT better it reflects Because large drops in a small concentrated area are characteristic of a severe thunder storm the radar displays the storm as a strong echo Drop size is the most important factor in high radar re flectivity The radar display has been calibrated to show five levels of target intensity Black level 0 and levels 1 4 grades of Amber PO3 RADAR CONTROL PANEL
20. consists of more than two legs As soon as the first leg becomes inactive upon automatic activation of the next leg you can setup the first leg to the next waypoint point 4 5 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 26 DO NOT USE FOR FLIGHT Route Corrections Only standby inactive leg can be corrected Use corresponding controls Course Selector and Mileage Set Knob to correct the leg If you need to correct an active leg Set Stage Selector the middle position Active leg will be permanently cleared Correct the leg usig corresponding controls Course Selector and Mileage Set Knob Set Stage Selector A or B position to activate the leg L16 DME INDICATOR 1 7 1 DME Indicator 2 Inop Flag Black Provides slant range in nautical miles to station tuned 1 DME Indicator For user convenience in MSFS on Left Forward Panel shows DME2 on Right Forward Panel shows DME1 2 Inop Flag Black Appears when power or locked signal not present 18 MARKER LIGHTS 1 Airways Light Clear 2 Middle Marker Light Amber 3 Outer Marker Light Blue 1 Airways Light Clear Illuminates steady when over airways beacon or flashing when over airway fan marker beacon 3000 Hz signal 2 Middle Marker Light Amber Illuminates flashing when over ILS middle marker beacon 1300 Hz signal 3 Outer Marker Light Blue Illuminates flashing whe
21. horizontal white beam aft Navigation lights red left and green right are provided in the outboard edge of each wing 10 Beacon Anti Collision Lights Switch The beacon lights on the top and bottom of the fuselage provide high intensity red flashes as a proximity warning of the aircraft ON Beacon anti collision lights illuminate 11 Wing Illumination Lights Switch Two wing illumination lights are mounted flush with the fuselage and forward of the wing leading edge ON illuminates the tops and leading edges of the wings and engine nacelle areas 018 CIVA INS CONTROL PANEL 1 Mode Selector Knob 2 READY NAV Light GREEN 3 BAT Light RED 4 6 INS Automatic Data Entry Unit Gauge Inop if Delco Carousel IV A INS is not installed For details see Delco Carousel IV A INS Manual 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 51 USE FOR FLIGHT 020 LIGHTS CONTROLS RIGHT FWD PANEL T m UGH COMPASS 1 Right Fwd Panel Lights gn bo 2 Light Override Switch 3 Compass Light 1 Right Fwd Panel Lights Control integral instrument illumination on the right forward panel 2 Light Override Switch OVERRIDE Turns the lights located under the Pilot s light shield and Engineer s panel fluorescent flood lights to full intensity 3 Compass Light Illuminates the standby compass O21 PROBE HEAT PANEL 1 2 3 1 Probe Heater Switch
22. is engaged NAV INS NAVIGATION MODE Autopilot intercepts and steers the INS track selected with INS no 1 HDG HEADING MODE Autopilot follows selected heading indicated on Captain s HSI MAN MANUAL MODE Mode used to engage autopilot Airplane will roll wings level and maintain existing pitch Autopilot holds clutched compass heading which can be adjusted with turn controller Pitch can be adjusted with pitch controller Mode selector will spring to MAN from any mode when turn controller is moved from center detent or Captain s RADIO INS switch is moved while the NAV or any radio mode LOC VOR LOCALIZER VOR MODE In this mode the hiding reference is supplied by use of the VOR or localizer signal If the airplane is placed on an intercept heading the autopilot can capture and track the centerline of a selected VOR or ILS course With a VOR frequency tuned when this mode is engaged the autopilot maintains the present heading until within 1 dot 5 degrees deviation from the captain s selected course The V L light goes amber when the VOR LOC mode is selected and switches to green when the autopilot captures the course At this time the previous heading reference is dropped and the airplane turns to track the course centerline A course error signal present heading vs selected course and a course deviation signal present radial vs selected radial are used to command roll During capture and tracking automatic cro
23. route as follows OPEN runs valve to open for alternate route of hot air supply OFF is spring loaded position CLOSE is guarded and saftied with alternate route blocked 4 5 FWD and MID Zone Indicators Show zone valve positions and whether air to FWD or MID zones is cooler or warmer than that supplied to aft zone reference as follows WARMER sector shows amount of FWD or MOD zone valve opening 0 neutral shows that air being supplied to that zone is same temperature as air being supplied to aft zone COOLER sector shows amount of aft zone valve opening 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 98 DO NOT USE FOR FLIGHT 6 Overheat Light When out shows distribution duct air temperature to three main cabin zones below 190 F When illuminated shows distribution duct temperature to any one main cabin zone over 190 F related zone valve overridden closed and valve manual control deactivated 7 8 Cabin Temperature Zone Control Switch These spring loaded switches operate the zone control valves when moved from center position WARMER drives FWD or MID zone valve towards open with relative position shows on FWD or MOD zone indicator COOLER drives respective zone valve toward closed When valve closed drives aft zone valve toward open as shown by FWD and MID zone indicator 503 FUEL DUMP PANEL The dump chutes extend from the lower wing surface outboard
24. AL Part II Aircraft and Systems 47 DO NOT USE FOR FLIGHT 4 Test Meter During test if needle reads Steadily in green for 5 seconds all channels recording OK O11 ANTI ICE PANEL 1 2 3 1 2 Duct Temperature Gage 3 Wing Anti Ice Switch 4 Anti Ice Duct Temperature Selector 5 Overheat Light 1 2 Duct Temperature Gages Indicate either both inboard or both outboard duct temperatures as selected 3 Wing Anti Ice Switch Controls all wing anti ice shutoff valves GRD TEST spring loaded to OFF activated in ground mode opens all shutoff valves deactivated in flight mode OFF closes all shutoff valves ON activated in flight mode 4 Duct Temperature Selector Selects inboard or outboard for temperature indication 5 Overheat Light Amber activated only in ground mode 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 48 DO NOT USE FOR FLIGHT 012 OXYGEN PRESSURE PANEL 1 Passenger Oxygen Light 2 Pers Accom Light 3 Passenger Oxygen Switch 1 Passenger Oxygen Pressure Indicating Light Amber ON amber PASS illuminates when system pressurized 2 Personnel Accomodations Oxygen Pressure Indicating Light Amber ON amber PERS ACCOM illuminates when system pressurized 3 Passenger Oxygen Switch ON opens manual trigger valve and actuates personnel accommodation system NORM guarded position sets system in a
25. ARNING LIGHT 1 A P Disengagement Light DISCE AGED A red light marked AUTOPILOT DISENGAGED is on both the Captain s and the First Officer s panel With the autopilot engaged the lights will come on flashing any time either or both channels of the autopilot become disengaged for any reason LO4 AIRSPEED INDICATOR 2 1 VMO Pointer 2 Airspeed Pointer 3 Movable External Reference Marker 4 Mach Number Indicator 4 1 120 4 2 140 2 KNOTS kang Fe onan qon ANS 200 180 gul no IAS e Obtained from Pt and Ps 3 Solid pointer IAS e Barber pole indicates maximum operating speed for existing pressure altitude e Three movable reference bugs MACH M e True mach readout from CADS Calculated Air Data System e Black flag covers readout if below 40M e Red striped flag covers readout when power interrupted 2011 Captain Sim www captainsim com Aircraft and T GHT MANUAL Par systems 11 DO NOT USE FOR FLIGHT LO5 RADIO MAGNETIC INDICATOR RMI 1 Synchronizing Annunciators 2 2 Synchronizing Knob 3 Compass Warning Flag 4 7 ADF VOR Selector Knob 3 5 6 ADF VOR Pointers A radio magnetic indicator RMI is provided on each pilot s panel to furnish the radio and magnetic bearing information required for navigation The components of each RMI consist of an azimuth card a lubber line two ADF VOR pointers No 1 and No 2 two ADF VOR switches No 1 and No 2 a synch
26. DO NOT USE FOR FLIGHT Pag V d 7 o T ATAA MESIAL PART II Aircraft and Systems DO NOT USE FOR FLIGHT ABOUT THIS MANUAL VERSION 04 MARCH 2011 The 707 Captain FLIGHT MANUAL is organized into three Parts Each Part is provided as a separate Acrobat PDF document e Part I User s Manual e Part II Aircraft and Systems this document e Part III Normal Procedures Adobe Acrobat Reader Required FOR GENERAL INFORMATION ON THE 707 CAPTAIN PRODUCT PLEASE USE WWW CAPTAINSIM COM THIS MANUAL PROVIDES ADDITIONAL INFORMATION ONLY WHICH IS NOT AVAILABLE ON THE WEB SITE WWW captainsim com DO NOT USE FOR FLIGHT 707 CAPTAIN FLIGHT MANUAL CONTENTS Page 6 SYSTEMS DESCRIPTION PANELS LAYOUT 8 LEFT FORWARD PANEL 9 9 10 10 11 12 13 15 17 17 18 18 19 20 21 22 22 23 24 24 26 26 LOL L02 LO3 104 LOS LO6 LO7 108 LOO Lii 12 L13 L14 10 MILE ALERT LIGHT CLOCKS AUTOPILOT DISENGAGED WARNING LIGHT AIRSPEED INDICATOR RADIO MAGNETIC INDICATOR RMI ANNUNCIATOR PANEL HORIZON FLIGHT DIRECTOR HFD MAGNETIC HEADING PICTORIAL DEVIATION INDICATOR MHPDI FLIGHT DIRECTOR ANNUNCIATOR LIGHTS IVSI INSTANTANEOUS SPEED INDICATOR PNEUMATIC BRAKE LEVER LOW RANGE RADIO ALTIMETER ELECTRIC ALTIMETER DOPPLER NAVIGATION SYSTEM L15 L17 DOPPLER INDICATOR DOPPLER INS SWITCH O08 DOPPLER CONTROL UNIT PO1 DOPPLER NAVIGATION CONTROLLER DIGI
27. GHT MANUAL Part II Aircraft and Systems 17 DO NOT USE FOR FLIGHT 09 FLIGHT DIRECTOR ANNUNCIATOR LIGHTS 1 2 1 2 The V L and GS Lights Located on each pilot s instrument panel on MHPDI airplanes Each light can illuminate either amber or green V L light with NAV AUTO selected Amber when flight director computer is commanding capture of the selected course Green when flight director computer senses that the desired course has been captured within 2 LOC dots G S light with LOC frequency selected Off prior to localizer capture Amber when flight director computer captures localizer Green when flight director computer senses that the glideslope has been captured within 1 4 GS dot 1 2 The V L and GS Lights Indicate status of VOR LOC and glideslope mode when OFF neither mode is armed AMBER respective mode is armed GREEN respective mode is in a capture or tracking status 11 IVSI INSTANTANEOUS SPEED INDICATOR 1 Vertical Speed Pointer Two vertical speed indicators are used on the airplane one located on the Captain s panel and the other on the First Officer s instrument panel Each indicator operates from the airplane static pressure system and provides instantaneous display of airplane vertical speed in the range of 0 to 6 000 feet per minute up or down These instruments differ from a conventional vertical speed instrument by the addition of two accelerometers which gene
28. ILES 2 3 Offset Miles Indicators e LET bw j 4 Offset Miles Control i ee LS ey 5 7 Miles To Go Indicator P MILES TO MILES TO GQ 7 1 12 6 8 Mileage Set Knobs h 9 Stage Selector a Qo Soo ma E HIS gt TEH 10 12 Selected Course Indicator SELECTED COURSE SELECTED COURSE F cud 11 13 Course Selector 0 0 Na No WV M OT 10 11 12 13 1 NAV Controller OFF computer is off STBY Computer is powered but not operating MAN computer operates indicating offset miles and miles to go but will not shift legs AUTO Same as MAN but will shift between A and B when distance to go reaches zero 2 3 Offset Miles Indicators Displays distance aircraft is offset from selected track on active stage RIGHT 00 is the on course indication 6 8 Mileage Set Knobs gradual adjustment speed Use to set desired stage mileage May be reset at any time without disrupting computer operation 9 Stage Selector Automatically or manually selects route stage for use 11 13 Course Selector gradual adjustment speed Selects desired course Selected course is compared with actual track and ground speed when in MAN or AUTO 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 24 DO NOT USE FOR FLIGHT DIGITAL MAP The digital map is not
29. ILLUMINATION 56 RADAR REFLECTIVITY 57 PO3 RADAR CONTROL PANEL 59 P04 RADAR DISPLAY UNIT 59 PREFLIGHT PROCEDURES 60 OPERATION IN FLIGHT GENERAL 60 TILT MANAGEMENT 60 EARLY DETECTION OF ENROUTE WEATHER 60 TARGET RESOLUTION 60 RANGE RESOLUTION 61 AZIMUTH RESOLUTION 61 PATH PLANNING 61 PATH PLANNING CONSIDERATIONS 62 PO5 CIVA INS CONTROL PANEL 63 07 TRANSPONDER CONTROL PANEL 64 PO8 CONTROL STAND AFT AISLE STAND 68 PO9 P10 VHF NAV COMM CONTROL PANEL 69 P11 AUTOPILOT PANEL 71 P12 P13 AUDIO SELECTOR PANEL 71 P14 AFT PEDESTAL PANEL FLIGHT ENGINEER UPPER PANEL 74 UO1 ELECTRICAL PANEL 78 U10 PNEUMATIC SYSTEM PANEL 80 U11 CABIN ALTITUDE PRESSURE SYSTEM PANEL 81 U12 AIR CONDITIONING PANEL 85 FLIGHT ENGINEER LOWER PANEL 86 WO1 FUEL SYSTEM PANEL 88 W02 FUEL HEATERS PANEL 89 W04 HYDRAULIC PANEL 91 WO05 ENGINE GAUGES 92 W06 DOOR ANNUNCIATOR PANEL 92 W07 AIRBORNE VIBRATION MONITOR WWW captainsim com DO NOT USE FOR FLIGHT K 93 SECOND OFFICER S AUXILIARY PANEL 94 S01 COOLANT AIR SYSTEM PANEL 95 S02 AUXILIARY TEMPERATURE CONTROL PANEL 96 S03 FUEL DUMP PANEL SECOND OFFICER S AUXILIARY 2 PANEL 98 S04 OXYGEN PRESSURE PANEL 98 S05 OXYGEN PANEL 98 S06 SERVICE PANEL 99 S08 LIGHTS CONTROL PANEL 99 S12 AUDIO SELECTOR PANEL 2 100 FAILURES 101 CUSTOMER WWW captainsim com DO NOT USE FOR FLIGHT SYSTEMS DESCRIPTION The 707 Captain is one of the most advan
30. LL UP Push To Test LIGHT Red 4 Warning Lights 1 VOR LOC Annunciator P DIM Press dims V L G S and MDA lights AMBER System armed in VOR LOC GS AUTO or GS MAN modes prior to intercept of VOR radial or localizer beam GREEN e Radial or localizer captured Capture of localizer in GS MAN mode also forces capture of glide slope 2 Glide Slope Annunciator AMBER e System armed in GS AUTO mode prior to intercept of glide slope System armed in GS MAN mode prior to intercept of localizer beam GREEN e Glide slope captured 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 13 DO NOT USE FOR FLIGHT LO7 HORIZON FLIGHT DIRECTOR HFD Gyro G Warning Flag 2 Bank Angle Scale 3 Roll Index 4 Pitch Scale 5 Computer FD Warning Flag 7 6 Altimeter Bar 7 Rate of Turn RT Warning Flag 8 Pitch Command Bar 9 Attitude Sphere 10 Turn and Slip Indicator 11 Expanded Localizer 12 Test Button Momentary 13 Horizon Line 14 Fixed Symbolic Airplane 15 Roll Command Bar 1 Gyro G Warning Flag Appears if e Power loss to or not developed in gyro e Power output of pitch or roll amplifiers is not proper 2 Bank Angle Scale Calibrations at 10 20 30 and 60 degrees in either direction 3 Roll Index Represents vertical plane of VG 4 Pitch Scale Calibrated in degrees 2 4 etc where 2 indicates 20 degr
31. ON FLIGHT DIRECTOR HFD RO8 MAGNETIC HEADING PICTORIAL DEVIATION INDICATOR MHPDI RO9 FLIGHT DIRECTOR ANNUNCIATOR LIGHTS R10 STANDBY ALTIMETER R11 IVSI INSTANTANEOUS SPEED INDICATOR R12 TEMPERATURE INDICATORS R13 LOW RANGE RADIO ALTIMETER R14 RUDDER BOOST LOW PRESSURE LIGHT R15 DOPPLER INDICATOR R16 DME INDICATOR R17 HYDRAULIC SYSTEM PANEL R18 MARKER LIGHTS 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 36 DO NOT USE FOR FLIGHT R10 STANDBY ALTIMETER An absolute pressure measuring altimeter is provided as a standby altimeter The indicator has a range of 1 000 to 50 000 feet indicated by a drum and pointer 1 1 Digital Display 2 100 Foot Pointer 3 Barometric Setting Control 4 5 Altimeter Setting Windows 1 Digital Display Shows altitude in increments of 100 ft 2 100 Foot Pointer Displays attitude in 100 foot Increment smallest division equals 20 feet One full rotation of pointer equals 1000 feet 3 Barometric Setting Control Rotation of the control adjusts the barometric setting on the inches of mercury in HG indicator 4 5 Altimeter Setting Windows Can be set in millibars or inches Hg R12 TEMPERATURE INDICATORS 1 RAT Indicator 1 2 OFF Flag 3 SAT Indicator 2 4 OFF Flag 1 RAT Indicator Senses true RAT directly 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II
32. R bus No 2 6 Utility Hydraulic System Pressure Displays hydraulic system pressure Powered from HYD PRESS CB on P7 8 Hydraulic Brake Pressure Gage This indicator indicates pressure on the air side of the brake accumulator The indicator will display precharge pressure when the brake hydraulic system is depressurized and will display zero if the precharge pressure is lost When the brake system hydraulic pressure exceeds precharge pressure the indicator will display brake system hydraulic pressure 9 10 AC Auxiliary Pump Switches When positioned to ON Activates pump motor OFF Shuts off pump motor Switch No 1 is powered from an AUX PUMP CONT No 1 CB on P5 TR bus No 4 the No 2 switch from an AUX HYD PUMP CONT 2 CB on P5 TR bus No 3 11 Rudder Hydraulic Pressure Gage Displays rudder hydraulic fluid pressure If airspeed is below 250 kt indication also represents auxiliary hydraulic pressure Powered from a RUDDER BOOST amp AIR BOTTLE on CB on P7 12 Interconnect Valve Switch When positioned to AUX 1 amp 2 BRAKE No 1 and No 2 auxiliary pumps can pressurize the brake system OFF Auxiliary system is isolated from utility system AUX 1 TO SYSTEM No 1 auxiliary pump can pressurize utility system and utility system can pressurize entire auxiliary system WWW captainsim com 39 DO NOT USE FOR FLIGHT GLARESHIELD PANEL 2 3 4 5 Engine Fire Handles 6 Main Wheel Well Warning Light 7 Fi
33. T MANUAL Part II Aircraft and Systems 79 DO NOT USE FOR FLIGHT U10 PNEUMATIC SYSTEM PANEL t 1 3 Air Compressor Tachometers AIR ONDITIONING amp PRESSURIZATIOM 3 4 6 Turbocompressor Low Oil Pressure Lights R COMPRESSOR eea Amber 2h J 2p lk 7 9 Turbocompressor Overspeed Trip Lights 0 Mb 3 Amber 10 12 Turbocompressor Switches 13 14 17 18 Engine Bleed Air Switches 15 16 Wing Valve Switches 19 20 Air Conditioning Unit Overheat Light 21 22 Air Conditioning Unit OFF Light 23 24 Left amp Right Air Conditioning Unit Pack Switches d ipw r E iG 25 Ram Air Switch XM an m AIR FICHT HG EHG gt f D AIF F COFED UNIT T T FT NG Pas ge EM 26 Air Supply Duct Pressure Gage FI HEAR JAY 1 aa slg HIGH PRESS 406 i Li d y ae i L F ra NY sz WA 1 3 Air Compressor Tachometers Indicates turbocompressor speed in percent of shaft rpm Indicator accuracy tolerance 1 5 NORMAL INDICATIONS shutdown 20 normal maximum 96 overspeed 115 4 6 Turbocompressor Low Oil Pressure Lights Amber ON Oil pressure is low or has Turbocompressor shutdown due to mailfunctions Note Light is wired through switch When switch held momentarily to START light goes on until oil pressure is normal On all 300C airplanes light is not wired through swi
34. TAL MAP NORMAL OPERATION L16 L18 DME INDICATOR MARKER LIGHTS CENTER FORWARD PANEL 28 29 29 30 32 33 34 CO1 ALTIMETER C02 ARTIFICIAL HORIZON C03 C08 LOW OIL PRESSURE LIGHTS C04 ENGINE INSTRUMENT PANEL C05 LANDING GEAR CONTROL PANEL C06 ESSENTIAL POWER FAILURE WARNING LIGHT C07 FLAPS INDICATORS PANEL 35 RIGHT FORWARD PANEL 36 36 37 37 R10 STANDBY ALTIMETER R12 TEMPERATURE INDICATORS R14 RUDDER BOOST LOW PRESSURE LIGHT R17 HYDRAULIC SYSTEM PANEL 39 GLARESHIELD PANEL 40 OVERHEAD PANEL 41 42 42 43 44 O01 EMERGENCY FLAP SWITCHES 002 LIGHTS CONTROLS O03 ANTI SKID CONTROL PANEL 004 HYDRAULIC POWER SYSTEM O05 ANTI ICE CONTROLS WWW captainsim com DO NOT USE FOR FLIGHT 45 O06 ENGINE START CONTROL PANEL 45 007 LIGHTS CONTROL PANEL 46 009 019 ADF CONTROL PANEL 46 010 COCKPIT VOICE RECORDER UNIT 47 O11 ANTI ICE PANEL 48 O12 OXYGEN PRESSURE PANEL 48 O13 SEAT BELTS SWITCH 48 O14 EMERGENCY EXIT LIGHTS SWITCH 49 O15 CABIN CALL PANEL 49 O16 WINDSHIELD WIPERS SWITCH 49 O17 EXTERIOR LIGHTING PANEL 50 O18 CIVA INS CONTROL PANEL 51 O20 LIGHTS CONTROLS 51 O21 PROBE HEAT PANEL 52 022 WINDOW HEAT PANEL 52 023 PITOT STATIC HEAT PANEL 53 025 STANDBY MAGNETIC COMPASS 54 FORWARD AISLE STAND aa 55 P0O2 P06 FLIGHT DIRECTOR CONTROLS 55 WEATHER RADAR THEORY OF OPERATION 55 RADAR PRINCIPLES 56 WEATHER RADAR PRINCIPLES 56 RADAR BEAM
35. TROL PANEL S12 AUDIO SELECTOR PANEL OATGEN REGULATOR DILUTER DEMAND EM rcv xXYS EH OH 2 OFF lt PANEL LOWER FANEL FLIGHT p lt AACE MEE 3 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 10 DO NOT USE FOR FLIGHT 504 OXYGEN PRESSURE PANEL CREW pass 1 Crew Oxygen Gage 2 Passenger Oxygen Gage 1 Crew Oxygen Gage Indicates pressure in crew oxygen cylinders 2 Passenger Oxygen Gage Indicates pressure in passenger oxygen cylinders S05 OXYGEN PANEL 1 2 3 4 1 Oxygen Emergency Lever OXYGEN REGULATOR 2 Oxygen Diluter Lever DILUTER DEMAND 3 Oxygen Flow Indicator 4 Oxygen Supply Lever HORHAL OFF 1 Fuel Flowmeter Reset Button 2 Oxy Mask Mic Switch 3 Service Interphone Switch FUEL FLOW 4 Flight Recorder Master Switch FLIGHT FCORDER 2 Oxy Mask Mic Switch ON Connects oxygen mask microphone to transmitter selected with MIC SELECTOR button on audio selector panel OFF Guarded position with oxygen mask microphone inoperative 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 10 DO NOT USE FOR FLIGHT 3 Service Interphone Switch ON connects ground service locations to interphone system 4 Flight Recorder
36. The autopilot should not be operated in LOC VOR GS AUTO or GS MAN modes when the No 1 VHF navigation receiver is inoperative 2 4 Pitch Trim Wheels Mechanically joined to one another Free to rotate without limit in either direction Activated when autopilot engaged so that when rotated new attitude reference is set and airplane pitches to maintain it Deactivated when ALT is selected or when glideslope is captured Can effect a maximum pitch up or down of about 30 3 Turn Controller Detented at center position May be rotated at 140 degrees in either direction When rotated causes airplane to turn and mode selector to return to MAN regardless of mode selected Rate and amount of rotation determines rate and amount of airplane roll Will remain in any position Can effect a maximum bank angle of 35 5 Autopilot Damper Switch Spring loaded to OFF When positioned to AUTOPILOT Engages all 3 or 4 servos for normal operation DAMPER Engages rudder servo on airplanes equipped with a parallel yaw damper Position is deactivated on airplanes equipped with series yaw damper 6 Altitude Hold Elevator Disconnect Switch Spring loaded to OFF When positioned to ALT Deactivates pitch trim wheels and controls pitch to maintain the existing pressure altitude Switch will return to OFF from this position when autopilot goes into a glideslope capture mode ELEV DISC Declutches elevator servo from pitch co
37. Warning flag When the altimeter is operating properly the flag is retracted Appears when power is off radio signal is invalid radio altimeter is tested 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 19 E DO NOT USE FOR FLIGHT test switch is actuated 6 Push to Test Button Operating the test switch will cause the altimeter to indicate 250 10 feet and the warning flag to appear 7 Decision Height Set Knob Positions bug to selected DH 8 Pointer Mask Covers pointer when above 2500 ft L14 ELECTRIC ALTIMETER The pilot s altimeters are electrically operated The Captain operates from the 1 air data computer and furnishes the air data computer with barometer corrections These corrections are applied to the altitude signals sent from the air data computer to the altitude alerting system The First Officer s altimeter operates from the air data sensor This altimeter is the secondary altitude source for the ATC transponder On some aircraft a servo pneumatic altimeter on the Captain s panel is normally driven by the Air Data System and provides corrected altitude signals to the altitude alert system The altimeter reverts to pneumatic operation in the event of power or air data failure A pneumatic altimeter is provided on the F O s panel which operates from the F O s static system An altitude alerting system gives audible and visual indicatio
38. a part of the Doppler navigation system but provided to facilitate operation of the Doppler Navigation System in FSX environment The map simulates pictorial rendition of the old times paper nav maps route calculations and position updates realtime NORMAL OPERATION DOPPLER NAVIGATION SYSTEM Check On DOPPLER CONTROL UNIT O08 switch Function Selector to TEST position It introduces test signal which should give following indicator readouts Drift angle of 20 0 5 L Ground speeds of 608 3 SEA and 600 3 LAND System setup On DOPPLER CONTROL UNIT 008 1 Switch Function Selector to ON position 2 Switch LAND SEA switch as required 3 Make sure Alarm Light is out On DOPPLER NAVIGATION CONTROLLER P01 Set Nav Controller 1 to STBY Set Stage Selector 9 in the middle position Set distance and course for legs A and or B using Mileage Set Knobs 6 8 and Course Selector 11 13 Set Nav Controller to MAN or AUTO position To activate the route leg set Stage Selector to A or B position Route will be drawn on the digital map UR WN Note All legs are always calculated drawn and initiated from the current aircraft position point 1 at the moment when Stage Selector is turned from the middle to A or B position 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 25 DO NOT USE FOR FLIGHT pm A oM B SELECTED COURSE SELECTED COURSE
39. and consider the most significant issues for the next service packs 2011 Captain Sim www captainsim com
40. aptain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 46 DO NOT USE FOR FLIGHT 2 Dome Red Three red dome lights provide general diffused illumination of the control cabin Two lights are installed on the left and right supports of the overhead panel and the other in the center of the aft control cabin area 009 019 ADF CONTROL PANEL 1 2 3 4 1 Loop Control 2 Beat Frequency Oscillator BFO Switch 3 Frequency Indicator 4 Tuning Meter 5 Volume Control 6 Volume Control Function Selector 7 Frequency Band Selector 8 Frequency Band Selector Tuning Control 4 Tuning Meter Displays relative strength of signal being received Most desirable reception is achieved by tuning for maximum needle deflection 6 Function Selector ADF Both the sense and loop antennas operate bearing information is displayed on the RMI s 010 COCKPIT VOICE RECORDER UNIT COCKPIT VOICE RECORDER 1 Voice Recorder Area Microphone 2 Voice Recorder Erase Button 3 Voice Recorder Test Button 4 Test Meter 5 Headset Jack 2 Voice Recorder Erase Button Push in for 2 seconds If airplane is on the ground and parking brake is set Entire tape is erased in 10 seconds and 400 Hz eraze tone is activated during erasure 3 Voice Recorder Test Button Push in for 5 seconds Activates test and 600 Hz test tone 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANU
41. ator Shows readout from respective NAV receiver not transferable When unusable covered by a warning flag 2011 Captain Sim www captainsim com 16 DO NOT USE FOR FLIGHT Note For user convenience in MSFS on Left Forward Panel shows DME1 on Right Forward Panel shows DME2 7 Glide Slope Deviation Bar and Glideslope Scale green on some airplanes Indicates glideslope deviation with ILS facility selected Out of view with VOR frequency selected Centers with loss of ILS signal Glideslope Scale 1 dot equals 14 degree 8 Glide Slope Warning Flag Covers glideslope scale if glideslope signal is invalid 9 Navigation Warning Flag Indicates loss of VOR LOC power or signal 10 Course Deviation Bar Indicates course deviation Centers with loss of radio signal 11 Course Selector Positions packplate Sets course counter Positions course cursor about inner edge of azimuth card 1 dot equals 1 4 degree 12 Course Deviation Scale Reference for measuring displacement from selected course course bar One dot deviation of course bar represents approximately 1 dot equals 5 degrees in VOR 1 degrees in LOC 13 Symbolic Airplane Fixed Airplane Reference 14 TO FROM Indicator To From Arrow Points toward a line through the VOR station perpendicular to selected course 15 Heading Selector Heading Selector Positions heading cursor about azimuth card WWW captainsim com 707 Captain FLI
42. ced complete and accurate airliner expansions for MSFS But the 707 Captain same as MSFS itself and any MSFS expansion is a flight simulation software game Therefore this product should not be used as flight training device FTD and or simulator for flight training purposes All items should work as described in this manual If something is not described as functional therefore it does not work or does not exist in the model it is not a system bug but a reasonable simplification WWW captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 7 DO NOT USE FOR FLIGHT PANELS LAYOUT GLARESHIELD RIGHT FORWARD FLIGHT ENGINEER OVERHEAD CENTER FORWARD UPPER PANEL LEFT FORWARD SIDE PANEL 2 FORWARD CONTROL STAND AFT AISLE STAND FLIGHT ENGINEER L R AISLE STAND LOWER PANEL 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 8 DO NOT USE FOR FLIGHT LEFT FORWARD PANEL 01 10 MILE ALERT LIGHT LO2 CLOCKS LO3 AUTOPILOT DISENGAGED WARNING LIGHT LO4 AIRSPEED INDICATOR LO5 RADIO MAGNETIC INDICATOR RMI LO6 ANNUNCIATOR PANEL LO7 HORIZON FLIGHT DIRECTOR HFD LO8 MAGNETIC HEADING PICTORIAL DEVIATION INDICATOR MHPDI 09 FLIGHT DIRECTOR ANNUNCIATOR LIGHTS L11 IVSI INSTANTANEOUS SPEED INDICATOR L12 PNEUMATIC BRAKE LEVER L13 LOW RANGE RADIO ALTIMETER L14 ELECTRIC ALTIMETER L15 DOPPLER INDICATOR L16 DME INDICATOR
43. centigrade Requires ac power for operation No 1 3 and 4 are powered by their respective numbered bus No 2 is powered by P7 GREEN BAND Normal operating temperature RED RADIAL 132 C Maximum continuous temperature RED RADIAL 143 C Maximum time limited temperature 11 14 No 1 2 3 4 Engine Oil Pressure Indicators Displays the pressure of the oil being pumped to the engine bearings and gear trains in psi Requires ac power for operation No 1 3 and 4 are powered by their respective numbered bus No 2 is powered by P7 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 94 DO NOT USE FOR FLIGHT W06 DOOR ANNUNCIATOR PANEL buy cage eti M 1 10 Door Warning Annunciation Panel n DOOR _ fs 11 Door Warning Switch BELL D 1 5 6 10 11 1 10 Door Warning Annunciation Panel 6 FWD Cargo External Door Open Light 1 FWD Main Door Open Light 7 AFT Cargo External Door Open Light 2 AFT Main Door Open Light 8 AFT Cargo Door No 1 Open Light 3 FWD Galley Door Open Light 9 AFT Cargo Door No 2 Open Light 4 AFT Galley Door Open Light 10 Main Cargo Door Open Light 5 Radio Access Door Open Light 11 Door Warning Switch The lights indicate the open or closed status of the main entry galley radio access and cargo doors When a light is on the corresponding door is unlocked BELL ARMED th
44. charge switch is located under each engine fire handle When armed by respective fire handle and pressed opens that engine s selector valve discharges a fire bottle www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 40 OVERHEAD PANEL O01 EMERGENCY FLAP SWITCHES O13 SEAT BELTS SWITCH O02 LIGHTS CONTROLS O14 COCKPIT EMERGENCY EXIT LIGHTS SWITCH O03 ANTI SKID CONTROL PANEL O15 CABIN CALL PANEL O04 HYDRAULIC POWER SYSTEM O16 WINDSHIELD WIPERS SWITCH O05 ANTI ICE CONTROLS O17 EXTERIOR LIGHTING PANEL O06 ENGINE START CONTROL PANEL O18 CIVA INS CONTROL PANEL O07 LIGHTS CONTROL PANEL O20 LIGHTS CONTROLS O08 DOPPLER CONTROL UNIT See page 22 for O21 PROBE HEAT PANEL details 022 WINDOW HEAT PANEL O09 O19 ADF CONTROL PANEL O23 PITOT STATIC HEAT PANEL O10 COCKPIT VOICE RECORDER UNIT O24 RAIN REPELLENT CONTROL BUTTON O11 ANTI ICE PANEL O25 STANDBY MAGNETIC COMPASS O12 OXYGEN PRESSURE PANEL 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 4 DO NOT USE FOR FLIGHT 001 EMERGENCY FLAP SWITCHES 1 2 3 1 NORM Bypass Switch 2 3 INBD and OUTBD Switches 1 NORM Bypass Switch NORM Disarms electric operation of trailing edge flaps and permits hydraulic operation BYPASS Bypasses hydraulic trailing edge flap system and arms adjacent INBD OUTBD switches 2 3 Emergency Flap Directional Control Switches
45. craft and Systems 68 DO NOT USE FOR FLIGHT PO9 P10 VHF NAV COMM CONTROL PANEL 1 6 1 COMM Frequency Indicator COMM oom HAV 2 7 VOL 128739 171739710 F 3 4 COMM Frequency Selectors H m E 5 Tone IN CE ANON a mE NIE wow 6 NAV Frequency Indicator o Es ET a P zA H e AN 8 9 NAV Frequency Selectors Pw 10 DME Function Switch 3 2 d 4 9J 8 10 2 VOL Rotating clockwise Turns equipment on Increases receiver sensitivity and volume level ATC Menu will tune selected COM 5 Tone Push button to transmit 400 Hz tone Permits ground station to determine airplane location 6 NAV Frequency Indicator Displays the selected frequency and facility VOR 108 00 to 111 85 all even tenth MHz 112 00 to 117 95 all MHz ILS 108 10 to 111 95 all odd tenth MHz DME TACAN or VORTAC frequencies For short range 0 50 miles 108 0 to 111 9 For full range 0 to 199 miles 112 0 to 117 9 8 9 NAV Frequency Selectors Selects desired frequency and facility 2011 Captain Sim www captainsim com systems P DO NOT USE FOR FLIGHT AICi dl L q TU T 7 Lj MAN IGHI MANUAL P11 AUTOPILOT PANEL AUTO PILOT 1 Autopilot Mode Selector 2 4 Pitch Trim Wheels 3 Turn Controller 5 Autopilot Damper Switch 6 Altitude Hold Elevator Disconnect Switch 1 Autopilot Mode Selector Spring loaded to MAN Functions only when autopilot
46. d Locked Lights 6 Bright Dim Switch 7 Gear Handle 8 Override Trigger 9 Lever Latch ELIT 53 27 Jean OPERA LT BELOW 30 0 SFT 270K ABOVE DOT 280 eesti ee eee 25 FISK E Mus s 1 Door Open Light When this red light is on a gear door is not closed 2 Gear Unsafe Light This red light comes on if any gear is not locked e notup with the handle up not down with the handle down e not down with a throttle retarded The light can be extinguished in this case by pulling the horn cutout lever e flaps at 40 or 50 position with gear up 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 33 DO NOT USE FOR FLIGHT 3 5 Down and Locked Lights When its green light is on the respective gear is down and locked Note In addition viewing ports permit visual confirmation of the gear position Wheel well lights controlled by a switch on the overhead panel illuminate lock alignment marks on each gear 7 Gear Handle UP Ports hydraulic pressure to the gear doors gear up lines and auto braking OFF Ports both the up and down lines to return Gear locked mechanically DOWN Ports hydraulic pressure to the gear doors gear down lines and with nose gear down nose wheel steering 8 Override Trigger Pulling the trigger overrides the lever latch 9 Lever Latch On gear handle behind panel Prevents raising gear ha
47. d Pitot Heater Ammeter PITOT Wars 1 Captain s Pitot and Attitude Warning Sensor Heat Switch Controls power to captain s pitot heater both attitude sensor heaters 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 53 DO NOT USE FOR FLIGHT 2 Ammeter Switch F O PITOT Ammeter indicates current first officer s pitot heater 3RD PITOT Ammeter indicates current to 3rd pitot heater 3 First Officer s Pitot and Attitude Warning Sensor Heat Switch Controls power to first officer s pitot heater both attitude sensor heaters B ADV 4 Captain s Pitot Heater Ammeter Indicates current to captain s pitot heater 5 First Officer s or 3rd Pitot Heater Ammeter Indicates current to selected pitot heater 025 STANDBY MAGNETIC COMPASS 1 1 Compass Correction Card 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 54 DO NOT USE FOR FLIGHT FORWARD AISLE STAND m h a Lac AIC OFFSET MILES u OD E LEET MRES TO Er P TE Io co 3 PI Pari c Yi SELECTED COURSE SELECTED COLERSE z EL no FS 0 m ANT B ATC TRANS PO1 DOPPLER NAVIGATION CONTROLLER See page 23 for details 02 PO6 FLIGHT DIRECTOR CONTROLS RADAR CONTROL PANEL P04 RADAR P05 CIVA INS CONTROL PANEL
48. d amplifiers and respective circuits Attitude sphere should indicate 10 degrees pitch up and about a 20 degree right roll 13 Horizon Line White line represents horizontal plane of VG and earth s horizon 15 Roll Command Bar Positioned by steering commands from flight director computer Note Flight director is connected with the autopilot Do not engage the autopilot if you need to use F D only www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 15 DO NOT USE FOR FLIGHT Course Counter 2 Course Cursor 3 Azimuth Card and Lubber Line 4 MHPDI OFF Flag 5 Heading Cursor Bug 6 DME Indicator 7 Glide Slope Deviation Bar and 8 Glide Slope Warning Flag 9 Navigation Warning Flag 10 Course Deviation Bar 11 1213 14 15 11 Course Selector 12 Course Deviation Scale 13 Fixed Airplane Reference 14 TO FROM Indicator 15 Heading Selector 1 Course Counter Indicates selected VOR LOC course 2 Course Cursor T Symbol Points to selected course Once set moves with azimuth card 3 Azimuth Card and Lubber Line Repeater from adjacent RMI cards should always agree 4 MHPDI OFF Flag Indicates heading failure Compass system power fails Backplane drive course selector out 5 Heading Cursor Bug Double Bar e Provides heading reference for flight directors and autopilot captain s e Once set moves with azimuth card 6 DME Indic
49. degrees above or below the horizon 3 Pitch Trim and Gyro Caging Control A knob at the bottom of the instrument dial permits adjustment of the instrument to any fore and aft attitude of the airplane within limits of plus or minus 7 CO8 LOW OIL PRESSURE LIGHTS 1 4 Low Oil Pressure Lights PRESSURE PRESSURE WARNING WARNING 4 amber generator drive low pressure lights are located on the Second Officer s panel Oil pressure supplied by pumps in each drive Come on when oil pressure is below 32 psi Goes out when oil pressure is above 36 psi 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 30 DO NOT USE FOR FLIGHT C04 ENGINE INSTRUMENT PANEL 1 2 3 4 1 4 Thrust Reverser Operating Lights 5 8 Engine Pressure Ratio Indicator Pointer 13 16 N1 Tachometers 5 8 17 20 Engine Exhaust Gas Temperature Indicators 21 24 N2 Tachometers 13 16 25 28 Engine Flowmeter Indicators 1 80 70 AN LITE Mug SN SX 17 20 21 24 25 28 1 4 Thrust Reverser Operating Lights Amber Comes on when either reverser on respective engine is not locked in the forward thrust position Engine Pressure Ratio Indicators Indicates the ratio of exhaust gas pressure Pt7 to inlet air pressure Pt2 EPR Pt7 Pt2 and is a parameter of the thrust developed by the engine The indicator is used as a primary thrust setting instrument
50. dge shaped striped indicator appears whenever the current altitude is less than 10000 feet 3048 meters For example if the long needle is on 5 and the short needle is between the 2 and 3 you are at 2500 feet 762 meters MSL If the striped indicator is not visible the same needle orientation shows that you are 12500 feet 3810 meters MSL 4 Barometric Setting Control To display altitude accurately the altimeter must be set to the current barometric pressure adjusted to sea level pressure 5 Kohlsman Window This setting appears in the Kohlsman window the scale between the 2 and 3 on the dial Before takeoff the pilot turns a setting knob to set the correct pressure When properly set the altimeter indicates the airport elevation not zero before the airplane takes off 6 Runway Height This pointer will indicate the runway elevation in feet above mean sea level MSL when pointers 1 and 2 are set to zero 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 29 DO NOT USE FOR FLIGHT CO2 ARTIFICIAL HORIZON 1 1 Bank Indicator 2 Symbolic Airplane 3 Pitch Trim and Gyro Caging Control 4 Horizon Bar 5 Bank Scale The artificial horizon is powered by the vacuum system Its horizon bar gives adive climb and angle of bank indication 1 Bank Indicator Moves along a scale with marks of bank 2 Symbolic Airplane Shows the aircraft s pitch attitude in
51. e system When flying at high altitudes the use of proper tilt management ensures observation of weather targets without over scanning For example a low altitude storm detected on the long range setting may disappear from the display as it is approached While it may have dissipated during your approach toward the storm don t count on it It may be that you are directing the radiated energy from the antenna above the storm as you get closer Judicious management of the antenna tilt control will avoid over scanning a weather target EARLY DETECTION OF ENROUTE WEATHER To set the antenna tilt to optimize the radar s ability to quickly identify significant weather follow these steps 1 Select the NORM mode of operation Adjust Brightness control as desired 2 Select the 50 or 150 nm range 3 Adjust the antenna tilt to watch the strongest returns seen on the display TARGET RESOLUTION The ability of a weather avoidance radar system to resolve and display two or more closely spaced targets is limited in range by the transmitted pulse width and display range and in azimuth by the antenna beam width RANGE RESOLUTION The transmitter pulse width in the radar is 4 micro seconds yielding a receiver range resolution of approximately 1 3 nautical mile 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 61 DO NOT USE FOR FLIGHT AZIMUTH RESOLUTION The ability of the radar to resolve
52. ees pitch up or down As pitch increases markings are longer to maintain horizon reference 5 Computer FD Warning Flag Appears if power is lost to Flight director computer e VG providing attitude information to flight director computer 2011 Captain Sim www captainsim com 14 DO NOT USE FOR FLIGHT 6 Altimeter Bar Driven by radio altimeter Appears from behind expanded localizer scale at 200 ft on radio altimeter to display rate in closure with terrain or runway Moves upward to touch bottom of fixed symbolic airplane at zero altitude 7 Rate of Turn RT Warning Flag Appears when signal is not available to rate of turn needle No transfer capability available 8 Pitch Command Bar Positioned by commands from selected flight director computer pitch command set knob or glideslope receiver 9 Attitude Sphere Displays airplane attitude Positioned by pitch or roll amplifiers with signals from vertical gyro 10 Turn and Slip Indicator Turn indicator is operated by signals from a rate gyro in the Lower 41 11 Expanded Localizer Pip is positioned by localizer displacement error when tuned to ILS frequency e Limit marks on each side of scale represent 1 4 dot displacement of PDI or MHPDI course deviation bar which at runway threshold places the airplane within 50 ft of runway centerline 12 Test Button Momentary When pressed Provides integrity check of attitude sphere relate
53. ional procedures for use of weather avoidance radar the fol lowing information is presented for use at the operator s discretion Operational techniques for the radar are similar to earlier generation weather avoidance radars The profi cient operator manages antenna tilt control to achieve best knowledge of storm height size and relative dir ection of movement RADAR PRINCIPLES Radar is fundamentally a distance measuring system using the principle of radio echoing The term RADAR is an acronym for Radio Detecting and Ranging It is a method for locating targets by using radio waves The transmitter generates microwave energy in the form of pulses These pulses are then transferred to the an tenna where they are focused into a beam by the antenna The radar beam is much like the beam of flash light The energy is focused and radiated by the antenna in such a way that it is most intense in the center 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 56 DO NOT USE FOR FLIGHT of the beam with decreasing intensity near the edge The same antenna is used for both transmitting and re ceiving When a pulse intercepts a target the energy is reflected as an echo or return signal back to the antenna From the antenna the returned signal is transferred to the receiver and processing circuits located in the receiver transmitter unit The echoes or returned signals are displayed on an indica
54. is position is deactivated OFF Door warning light system operates normally LIGHT TEST Momentary illuminates all door warning lights During pretaxi push to test the door warning lights Any door with its light on must be visually checked for closure W07 AIRBORNE VIBRATION MONITOR 1 4 No 1 2 3 4 Engine Vibration Indicators ME HERALOH MONITOR 5 Engine Vibration Push To Test Button 6 Engine Vibration Pickup Select Switch 7 Engine Vibration Filter Select Switch 5 Engine Vibration Push To Test Button Used in conjunction with Pickup Select switch to check system operation 6 Engine Vibration Pickup Select Switch When positioned to TURB or DIFF Vibration sensed in the selected engine area is displayed on the respective indicator 7 Engine Vibration Filter Select Switch Being removed If installed leave in LOW 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 95 DO NOT USE FOR FLIGHT SECOND OFFICER S AUXILIARY PANEL KERE SYSTEM icc 501 COOLANT AIR SYSTEM PANEL ra TCH S02 AUXILIARY TEMPERATURE CONTROL PANEL 503 FUEL DUMP PANEL 15d i MAIR 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 96 DO NOT USE FOR FLIGHT 501 COOLANT AIR SYSTEM PANEL O 1 Valve Position Indicator AIR SYSTEM ax 2 2 Valve Selector Switch 3 4 Left amp Right Inlet
55. mObjects Airplanes CS_B707 300 panel folder 2 Rename civa panel cfg file to panel cfg file If you decide to uninstall CIVA INS you should restore original panel cfg file For details on CIVA INS ops see its manual and video tutorial O08 DOPPLER CONTROL UNIT ON Pe yt ae 1 Function Selector Switch ap NE p Ec 2 Slew Switch b Jf Fama 3 Alarm Light 4 Sea Land Switch 1 Function Selector Switch Applies power and test signal to doppler system OFF System inoperative REC ONLY receiver inoperative transmitter off ON receiver and transmitter operative TEST pulled out position of switch in which transmitter inoperative Introduces test signal which should give following indicator readouts Drift angle of 20 0 5 L Ground speeds of 608 3 SEA and 600 3 LAND 3 Alarm Light Lights when signal output from receiver to tracker is below minimum acceptable strength or after mechanical or electrical failure of sensor sensor is out Groundspeed and drift angle are frozen at existing value 4 Sea Land Switch Adjusts groundspeed computation for reflected signal differences over land and water Adds 8 kt to computed groundspeed in SEA position 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 23 DO NOT USE FOR FLIGHT PO1 DOPPLER NAVIGATION CONTROLLER 1 2 3 4 1 NAV Controller f SIBY MAN MIO d JOFFSETA A
56. metrical spoiler extension from to 60 degrees 2 3 4 5 Reverse Thrust Levers Control reverse thrust from idle to maximum reverse Mounted on corresponding engine throttles Reverse lever positions forward thrust idle reverse thrust reverse interlock Provides sufficient engine bleed air to position reverses 2011 Captain Sim www captainsim com 65 DO NOT USE FOR FLIGHT Prevents further application of thrust until both reversers approach reverse thrust position Prevents application of forward thrust until reversers are in forward thrust position spring stop Limits maximum reverse thrust If necessary may be overridden in an emergency Maximum reverse thrust Note During application of reverse thrust if a reverser goes to forward thrust a follow up mechanism in the reverse system will retard the reverse lever forward idle Similarly during application of forward thrust if a reverser goes to the reverse thrust position the mechanism will retard a throttle to a low thrust level 6 Flap Control Lever The lever controls both inboard and outboard flap hydraulic drive units Five detented flap handle positions from 0 to 50 degrees are provided The flap position is shown on two cockpit indicators Airplane Flap position 0 14 25 40 50 300B Adv X KOK K X K 300C Normal takeoff setting DETENTS PLACKARDS Where shown 0 KTS IAS 14 223 25 215 40 200 50 195 7 10 Engine Thro
57. mum Caused by CSD disconnected engine shutdown or low oil quantity During turbulence light may come on intermittently CSD operation is normal OFF CSD oil pressure normal 9 12 Generator Drive Disconnect Switches Disconnects CSD drive from engine generator deactivated Trips GB Note The generator drive can only be reconnected on the ground 13 Battery Switch ON battery power available to battery bus on P6 allows battery to be charged permits checking external TR voltage OFF battery power not available to battery bus on P6 but still available to aux battery bus on P6 Permits checking battery voltage 14 DC Meters Selector Connects loadmeter and voltmeter to selected source OFF loadmeter and voltmeter deactivated 15 18 Gen Drive Oil Temp Rise Gage Displays difference between oil in and oil out temperature www captainsim com 77 DO NOT USE FOR FLIGHT Reflects generator load on CSD Range marks coincide with generator KW loads Green band safe Yellow band caution 20 External Power Switch Magnetically held to ON and GROUND SERVICE ON All GBs trip PWR ON BUS light comes on External power is connected to sync tie bus if BTBs closed external power is connected to generator load buses Essential power can be supplied from external power GROUND SERVICE Powers the 28 VOLT SERVICE LTS bus on P1 with 28V ac if 115 200V ac external power c
58. n OUT Auto shutoff valve fully closed 4 Blower Switch Provides electrical override of blower operation NORM Blower operates continuously OFF Stops blower 5 Overboard Dump Valve Switch Provides outlet to ambient pressure if blower is inoperative NORM Overboard dump valve closed OPEN Overboard dump valve open bypassing auto shutoff valve in blower discharge duct 8 Hydraulic Reservoir Quantity Gage Indicates utility reservoir quantity 3 2 gal Line is yellow Powered from a RUDDER SEL amp OIL QTY ind cb on P5 TR bus No 3 10 Hydraulic Fluid Shutoff Eng No 3 Switch When positioned to OPEN Opens hydraulic fluid shutoff valve to allow fluid to flow from reservoir to pump CLOSE Closes the hydraulic fluid shutoff valve to respective engine driven pump www captainsim com 92 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 93 DO NOT USE FOR FLIGHT 1 2 Source Selector Switches 3 6 No 1 2 3 4 Engine Oil Quantity Gage 7 10 No 1 2 3 4 Engine Oil Temperature Indicators 11 14 No 1 2 3 4 Engine Oil Pressure 3 6 n wg Indicators Tayi Langi z 15 18 No 1 2 3 4 Engine N2 Tachometers 6 7 10 11 14 15 18 3 6 No 1 2 3 4 Engine Oil Quantity Gage Indicates gallons of oil in respective tank Requires ac power from respective numbered bus for operation 7 10 No 1 2 3 4 Engine Oil Temperature Indicators Shows oil temperature in degrees
59. n Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 45 DO NOT USE FOR FLIGHT O06 ENGINE START CONTROL PANEL ENGINE START CONTROL ENGINE START CONTROL PUSH KO 13 FISH ENOB TO ROTAN 1 2 4 5 Engine Start Control Switch GROUND START Arms start lever switch to provide ignition through both exciters Opens the low pressure start air valve Note If the No 3 engine is being used for a high pressure start the No 3 ENGINE START CONTROL switch opens the high pressure start air valve FLIGHT START always armed Energizes both exciters directly to provide continuous ignition It is used during takeoff for immediate relight in the event of a flameout for windmill starting in flight before applying nacelle anti ice during turbulence during landing The IGN 1 and IGN 2 selections provide for single continuous ignition 3 Ground Start Selector Switch LOW PRESS Arms all four ENGINE START CONTROL switches for control of the low pressure start air valve Places turbocompressors in ground mode to increase output for crossfeed starting HIGH PRESS Arms No 3 ENGINE START CONTROL switch for control of the high pressure start air valve 007 LIGHTS CONTROL PANEL 1 2 3 1 Control Stand White Light 2 Dome Red 3 Flood Light 1 Control Stand White Light Controls white light located in overhead panel 2011 C
60. n of approaching an altitude acquisition or departing from an altitude deviation In the acquisition mode an aural signal tone will sound momentarily and the alert lights will come on when passing through a point approximately 900 feet above or below the selected altitude The light will remain on until approximately 300 feet from the selected altitude In the deviation mode when departing the selected altitude the aural signal will sound momentarily and the alert lights will come on at approximately 300 feet above or below the selected altitude The alert light will remain on until reset by pressing the alert light A failure flag will appear in the alert indicator if a failure occurs in the Captain s altimeter or the alert indicator The altitude alerting system may be tested by turning the altitude selector toward the airplane altitude and then up through more than 900 feet above the airplane altitude The aural signal sounds momentarily and the alert light illuminates when the indicator reads 300 feet from the airplane altitude and remains extinguished until 300 feet from the airplane altitude When indicator altitude exceeds airplane altitude by 300 feet the aural signal sounds momentarily and the alert lights illuminate 1 2 3 1 Failure Warning Flag 2 Reference Altitude Bug 3 100 Foot Pointer 4 Altitude Numerical Counter 5 6 Altimeter Setting Windows 7 Barometric Setting Control 8 Reference Altitude Bug Selector 1 Failure Wa
61. n over ILS outer marker beacon 400 Hz signal 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 27 DO NOT USE FOR FLIGHT CENTER FORWARD PANEL OL PRESSURE p LET PIA CO1 ALTIMETER C02 ARTIFICIAL HORIZON C03 C08 LOW OIL PRESSURE LIGHTS C04 ENGINE INSTRUMENT PANEL C05 LANDING GEAR CONTROL PANEL C06 ESSENTIAL POWER FAILURE WARNING LIGHT C07 FLAPS INDICATORS PANEL 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 28 DO NOT USE FOR FLIGHT CO1 ALTIMETER 1 6 1 1000 Feet Pointer 2 100 Feet Pointer 3 Altitude Indicator 4 Barometric Setting Control 5 Kohlsman Window 6 Runway Height The altimeter is a sensitive barometer that measures air pressure It is calibrated to display that air pressure as height usually in feet above mean sea level MSL The altimeter is connected to the static ports The air pressure inside the instrument case decreases as the airplane climbs and increases at its descends As the pressure in the case drops sealed wafers in the instrument case expand Increasing pressure squeezes the wafers As the wafers expand and contract needles connected to them rotate around the altimeter dial like hands on a watch 1 1000 Feet Pointer The short handle points to thousands of feel 2 100 Feet Pointer The long needle shows hundreds of feet 3 Altitude Indicator A we
62. n overhead panel 2 Dome White Controls two dome lights in cockpit above the pilot s section 3 Left FWD Panel Lights Control integral instrument illumination on center panel 4 Center FWD Panel Lights Control integral instrument illumination on center panel ANTI SKID CONTROL PANEL 1 2 3 4 3 6 1 Anti Skid Switch 2 5 Brake Released Indicator 6 Anti Skid Test Switch T AMTI SKID 1 Anti Skid Switch ON System energized OFF System deenergized 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 43 DO NOT USE FOR FLIGHT 2 5 Brake Released Indicator REL Antiskid valve is porting part of all brake pressure to return In flight with gear down constant release signal is commanded to prevent locked wheel landing BLANK Antiskid valves deenergized Blanks also show when system is off 6 Anti Skid Test Switch When the system is on the gear is down and when the test switch is actuated The indicators on the selected position OUTBD or INBD show BLANK The indicators of the other position show REL 004 HYDRAULIC POWER SYSTEM 1 3 1 Rudder Switch 2 Outboard Spoiler Switch 3 Inboard Spoiler Switch im n mn JRUDDER suren 10 SPOILER Als 1 Rudder Switch ON Opens rudder boost shutoff valve OFF Shuts off rudder boost pressure and series yaw damper 2 Outboard Spoiler S
63. ndle up if any of the following exists e Airplane is on the ground or oleo strut is not extended in flight e Main gear trucks are not level Nose wheels are not centered some airplanes only e No electrical power to lever latch solenoid C06 ESSENTIAL POWER FAILURE WARNING LIGHT 1 1 Essential Power Failure Warning Light can be reset Flashing red Loss of essential power essential ac bus OFF Essential power being supplied 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 34 DO NOT USE FOR FLIGHT C07 FLAPS INDICATORS PANEL 1 2 Flap Position Indicators 3 4 Leading Edge Flap Lights 1 2 Flap Position Indicators Two dual flap position indicators on the pilots center panel are marked OUTBD and INBD respectively Two needles in each indicator marked L and R indicate corresponding flap positions White bands indicate maximum allowable needle deviation at each flap position Show position of trailing edge flaps 3 4 Leading Edge Flap Lights ON Indicate all respective edge flaps are extended MAXIMUM SPEED 223 KIAS 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 35 DO NOT USE FOR FLIGHT RIGHT FORWARD PANEL RO1 10 MILE ALERT LIGHT R02 CLOCKS RO3 AUTOPILOT DISENGAGED WARNING LIGHT R04 AIRSPEED INDICATOR RO5 RADIO MAGNETIC INDICATOR RMI RO6 ANNUNCIATOR PANEL RO7 HORIZ
64. nsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 21 DO NOT USE FOR FLIGHT L15 DOPPLER INDICATOR 1 2 1 Drift Angle 2 Indicator Flag 3 3 GS Knots Window 4 4 Course Offset Scale 5 5 Course Offset Pointer 6 Course Offset Flag 1 Drift Angle Pointer gives difference between airplane s magnetic heading and magnetic track 2 Indicator Flag Flag appears when e sensor system in memory operation and or e ground speed is less than 90 kt 3 GS Knots Window Displays ground speed in knots 4 Course Offset Scale One dot deviation equals 2 miles 5 Course Offset Pointer Indicates aircraft deviation from selected course 6 Course Offset Flag Appears when Nav controller is OFF STBY Nav Computer power fails 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 22 DO NOT USE FOR FLIGHT L17 DOPPLER INS SWITCH NAVIGATION 1 Doppler INS Switch DHOFFLER 2 Doppler INS Switch Cover DOPPLER Autopilot in NAV mode tracks Doppler Navigation System Heading Bug on Captain s HSI controlled by HSI Heading Selector INS Inop if Delco Carousel IV A INS is not installed If installed Autopilot in NAV mode tracks CIVA INS Heading Bug on Captain s HSI controlled by CIVA INS If you have CIVA INS installed you should use CIVA INS panel cfg file 1 Backup rename original panel cfg file in Si
65. ntrol system and deactivates horizontal stabilizer trim servo Airplane is now flown by autopilot in roll and by the pilot for pitch Note www captainsim com DO NOT USE FOR FLIGHT Flight director is connected with the autopilot Do not engage the autopilot if you need to use F D only www captainsim com 71 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 72 DO NOT USE FOR FLIGHT P12 P13 AUDIO SELECTOR PANEL 2 3 4 1 5 9 15 Communication Receiver Switches NAMI24 6 Transmitter Selector MER VOE e 7 Microphone Push to talk Switch WHE HORAL IHT 8 Mic Selector Switch sage E germ 7 6 RO TEMP L WP B e MV L EL ADE COMM AL 2 4 VOCE RANGE Yer VED VRE3 VOICE RANGE 1 i F rnin fw AM A 6 Transmitter Selector Selects desired transmitter Stations Morse codes 1 NAV1 station 2 NAV2 station 10 ADF1 station 15 ADF2 station 14 PEDESTAL PANEL 1 2 1 Radio Panels Lights Control Was 1 Z z p 7 TEE 2 Rudder Trim Crank and Indicator Z lt MTS 3 Horn Cutout Lever or AMBI Try RADIO PANELS Z lt i 1 f 4 Radio Panel Flood Light Control 5 Aileron Trim Control Wheel and Indicator 6 Stabilizer Brake Release Knob 1 Radio Panels Lights Control Controls intensity for the dial lights on the electronic control
66. nues as in previous modes until the glideslope is intercepted at 1 4 dot deviation At interception the pitch trim knobs are deactivated and the altitude hold switch is released if engaged The airplane is then controlled by the glideslope beam For proper flightpath control down to minimums the localizer signals are attenuated and bank angle is limited as a function of altitude Attenuation begins at 1000 ft as determined By an altitude signal from the radio altimeter If the radio altimeter fails the autopilot will automatically refer to a backup barometric altitude signal for attenuation during a 1500 ft descent from the glideslope intercept altitude GS MAN Operation in the GS MAN mode is identical to that of the GS AUTO mode except that when GS MAN is selected the autopilot immediately pitches and rolls the airplane to capture both the localizer and glideslope Thus the airplane will fly to the localizer and glideslope centerline by the most direct route REVERSION TO MANUAL MODE The autopilot reverts to the MAN mode from any mode if autopilot turn knob is used the captain s compass transfer switch is used It reverts to MAN from radio modes if the captain s deviation transfer switch is used the series yaw damper goes off which can be caused by moving the switch or by loss of rudder boost pressure After reversion all modes may be reselected except the radio modes after loss of the series yaw damper Note
67. of the main gear They must be fully extended before the dump valves can be opened Standpipes in the main and center tanks prevent total duel depletions The average total dump rate is 3150 pounds per minute Total undumpable fuel is about 16 900 Ib 7 11 1 2 de 1 2 Dump Chute Switches RETRACT open 3 8 Dump Valve Light 9 10 Dump Chute Light EXTEND CLOSE VALY nt 11 16 Fuel Dump Valve Switches BO NOT RETRACT LUE LIOHT OF VALY 10 UNTIL ALL VALVES A Ie FOR 2 MIN a or e 6 Gis CHUTES NOT VALVE in AETRACTEO POSITION z MAIN TAR RS 13 14 15 16 1 2 Dump Chute Switches RETRACT Releases downlocks and powers actuators to retract chutes OFF Removes power from chute actuators EXTEND Releases uplatches and powers actuators to extend chutes 3 8 Dump Valve Light ON Dump valve and control switch not in agreement OFF Dump valve and control switch in same position 9 10 Dump Chute Light ON Chute not retracted OUT Chute retracted 11 16 Fuel Dump Valve Switches Control main tank and center tank dump valves Switches 1 and 4 also control adjacent reserve tank transfer valve Armed only when dump chute is down and locked 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 99 DO NOT USE FOR FLIGHT SECOND OFFICER S AUXILIARY 2 PANEL Row PASE S04 OXYGEN PRESSURE PANEL S05 OXYGEN PANEL S06 SERVICE PANEL S08 LIGHTS CON
68. onnected 28V dc if 115 200V dc external power connected OFF The switch will automatically trip to OFF from either the ON or GROUND SERVICE position if the external power supply is interrupted The switch will also trip to OFF from the ON position when a GB is closed or when there is a sync tie bus fault 21 External Power Connected Light Clear ON Ground power available at external power connection OFF External ac power not available 22 25 BTB Circuit Open Trip Light ON BTB tripped and generator and its load bus are isolated from the sync tie bus OFF BTB closed 26 29 Bus Tie Breaker Switches Guarded and spring loaded to center position CLOSE Connects generator and or its load bus to the sync tie bus No autoparalleling protection provided TRIP Disconnects generator and or its load bus from the sync tie bus 30 33 GB Circuit Open Trip Light ON GB tripped and generator and its load bus are isolated from the sync tie bus OFF GB closed 34 37 Generator Breaker Switches CLOSE Connects generator to its distribution bus and sync tie bus through BTB Autoparalleling protection is provided TRIP Isolates generator from load bus and sync tie bus 38 41 GCR OFF Trip Light ON GCR open Generator is deactivated OFF GCR closed www captainsim com 78 DO NOT USE FOR FLIGHT 42 45 Generator Control Relay GCR Switch Guarded and spring loaded to center position CLOSE
69. ow Pressure Light Amber On when boost pump pressure is below 6 psi 30 33 48 52 Fuel Quantity Gage Indicates tank fuel quantity in LBx1000 The small needle indicates LBx100 34 35 38 41 Fuel shutoff Valve In Transit Lights Blue ON during respective valve transit OFF Valve corresponds with the switch that activated it 42 45 Manifold Valve Switches Controls manifold valve When turned horizontally valve closes When turned vertically valve opens 46 47 Transfer Valve Switch Control reserve tank transfer valve When turned horizontally valve closes When turned horizontally valve closes 49 Push To Test Button Respective quantity indicator drives toward zero Pointer returns to original position after switch released 50 Totalizer Gage Indicates sum of all fuel quantity indications in LB x 10 000 Small needle indicates in LB x 1000 WWW captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 90 DO NOT USE FOR FLIGHT 51 Fuel Temperature Gage Shows fuel temperature in degrees centigrade at location selected with FUEL TEMP SELECTOR Requires ac power from P7 to operate 53 Fuel Temperature Selector Arms FUEL TEMP gage according to selection When positioned to ENG 1 2 3 OR 4 FUEL TEMP gage shows temperature of fuel downstream of respective engine s fuel filter W02 FUEL HEATERS PANEL FUEL HEATERS 1 4 Fuel Icing Eng 1 2 3 4
70. panels 2 Rudder Trim Crank and Indicator Movement of trim crank relocates neutral position of rudder pedals 2011 Captain Sim www captainsim com DO NOT USE FOR FLIGHT 3 Horn Cutout Lever PULL Silences landing gear warning horn unless flaps are at 40 or 50 position 5 Aileron Trim Control Wheel and Indicator Movement of trim wheel relocates neutral poition of control wheel www captainsim com 73 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 74 DO NOT USE FOR FLIGHT FLIGHT ENGINEER UPPER PANEL UO1 ELECTRICAL PANEL U10 PNEUMATIC SYSTEM PANEL U11 CABIN ALTITUDE PRESSURE SYSTEM PANEL U12 AIR CONDITIONING PANEL 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 75 U01 ELECTRICAL PANEL 10 7 12 3 13 4 14 6 2 1 ALTORMATE FUEL FLOWMETER POWER DRIVEJEAN BE amp E COMMECIIEn Per Je Tor een GALLEY EMG 4 X gt LOAD a VO CAUNO COSRNECTIDS sSERWPCE i EXTERNAL POWER F GEH 4 onu EXT PWK CIRCUIT e OPER sfa 3 IET L J GEM i IREAXER E GEH 42 LE E CONTRO RESIDUAL Wi SYNCHKOHIZED WHEN LIGHTS cfs 3 25 ri TRIP 46 30 47 21 48 22 49 3B 60 61 239 1 Fuel Flowmeter Power Selector 20 External Power Switch 2 Galley Power Switch 21 External Power Connected Light Clea
71. pplied IDLE Fuel is supplied ignition is cut off 20 Parking Brake Warning Light This red light on the control stand will illuminate when the parking brake handle is in the SET position 21 Parking Brake Handle The parking brake handle on the control stand can be set when the brakes are fully applied to latch the brakes in the depressed position When the parking brake is set hydraulic return from the main gear antiskid valves will be blocked and the anti skid system will be de energized 22 23 Stabilizer Trim Indicators Green band calibrated in CG percentage www captainsim com Captain FLIGHT MANUAL Part II Aircraft and Systems 67 28730 113970 2 La AUTONWLOT n WHE HAWA F MWe HF BAN zu PAE WCE RANGE MER yroce VOICE RAMGE MEE WONGE RANG as w cE a m ee NOI INT WHE PEE 1 1 thee iT IX nr NER p PIT 7 ge mm Et TE EL r ADF ena COMM RECS mn pe AD ADEs r COMM r ADP gt Ls el RAE Vat un 3 vr ur d DET vul VR 2 va 1 at RA RI E E OFF af RADIO PANELS 198 46 4 Ti 2 468610 O A hik ny S RPI eet Les PO9 P10 VHF NAV COMM CONTROL PANEL P11 AUTOPILOT PANEL P12 P13 AUDIO SELECTOR PANEL P14 AFT PEDESTAL PANEL 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Air
72. r 3 DC Power Voltmeter 22 25 BTB Circuit Open Trip Light 4 DC Power Loadmeter 26 29 Bus Tie Breaker Switch 5 8 Generator Drive Low Pressure Lights 30 33 GB Circuit Open Trip Light 9 12 Generator Drive Disconnect Switches 34 37 Generator Breaker Switch 13 Battery ON OFF master switch 38 41 GCR OFF Trip Light 14 DC Meters Selector 42 45 Generator Control Relay GCR Switch 15 18 Gen Drive Oil Temp Rise Gage 46 49 KW KWAR Meter 19 Power on BUS Light 50 53 Frequency Control Knob 2011 Captain Sim www captainsim com 76 DO NOT USE FOR FLIGHT 54 Essential Power Failure Warning Light 58 59 Synchronizing Lights Clear 55 Essential Power Source Selector 60 AC Paralleling Selector 56 Frequency Meter 61 Powermeter Button 57 AC Voltmeter 1 Fuel Flowmeter Power Selector When positioned to NORMAL The flowmeters are powered from P2 through a static frequency controller which maintains 400 Hz ALTERNATE The flowmeters are powered directly from P1 in which case flowmeter accuracy is maintained only if bus frequency is held at 400 Hz Expect 1 error for each 4 Hz deviation from 400 Hz 3 DC Power Voltmeter Indicates DC voltage of selected TR unit or battery 4 DC Power Loadmeter Indicates current load of selected TR unit or battery With the BATT position selected shows negative while charging shows positive while supplying load 5 8 Generator Drive Low Pressure Lights ON CSD oil pressure below mini
73. rate pressure differences whenever there is a change in the normal acceleration of the airplane 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 18 DO NOT USE FOR FLIGHT L12 PNEUMATIC BRAKE LEVER 1 Pneumatic Brake Lever The lever has an OFF position and a range marked INCREASE In the OFF position gas pressure is isolated from the transfer tube and the pneumatic brake line is vented to ambient pressure When the lever is in the INCREASE range metered pneumatic pressure depending on the position of the pneumatic brake lever reaches the transfer tube and applies all main gear brakes simultaneously 13 LOW RANGE RADIO ALTIMETER 1 8 34 5 1 Decision Height Light 3 Decision Height Bug 4 Pointer 5 Warning flag ALT 5 17 AN A 6 Push to Test Button o Ro 3S 7 Decision Height Set Knob 6 7 8 Pointer Mask A low range radio altimeter is provided on each of the pilot s panels The low range altimeter displays height above terrain with an altitude pointer moving over a circular scale The range of the altimeter is from O feet to 2 500 feet 1 Decision Height Light Illuminates at and below decision height bug setting 3 Decision Height Bug This cursor can be moved about the periphery of the altimeter with the DH selector thus selecting the altitude at which a decision height light will illuminate 4 Pointer Indicates height AGL 5
74. re Alarm Bell Cutout Switch 8 Fire Test Switch 11 12 Bottle Transfer Selector Switch 13 16 Bottle Discharge Buttons 2 3 4 5 Engine Fire Handles Illuminates when a temperature rise is sensed in its engine or strut or handle When pulled arms discharge button closes respective engine s nacelle anti ice valves low pressure bleed fuel shutoff valve hydraulic pump supply valve inboards only deactivates respective engine s fuel shutoff valve switch and hydraulic pump low pressure lights inboards only trips respective generator s GCR and GB Used to prevent smoke contamination of pneumatic manifold and loss of pneumatic manifold air into inoperative engine if check valve fails With the engine fire handle pulled out and the bottle discharge switch depressed the actual fire extinguishing process will commence 7 Fire Alarm Bell Cutout Switch Will silence the bell and horn The lights will remain illuminated as long as the fire condition exists 8 Fire Test Switch The switch has a single test position that checks all loops and warnings When positioned to TEST if normal fire warning bells sounds all fire handle warning lights come on 11 12 Bottle Transfer Selector Switch When positioned to NORM Arms fire bottle of respective numbered engine to discharge TRANS Arms the other fire bottle in respective wing to discharge 13 16 Bottle Discharge Buttons A push button type bottle dis
75. rees positions 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 60 DO NOT USE FOR FLIGHT 7 Return the function switch to TEST or STBY before taxiing 8 When you are ready for weather detection after takeoff or just before place the function switch to NORM OPERATION IN FLIGHT GENERAL It is the purpose of this section to help you become a proficient radar operator as soon as possible However it is realized that proficiency can only improve with usage It is therefore recommended that the operator become familiar with the operation of the system during fair weather instead of while trying to penetrate a storm front This section concerns itself with a more detailed discussion of some of these controls and how to make the most efficient use of them Note Your radar is a weather avoidance device It should never be used for weather penetration It will help you see and plan avoidance maneuvers around significant weather encountered during flight TILT MANAGEMENT Effective antenna tilt management is the single most important key to more informative weather radar displays The prime factors must be kept in mind for proper tilt management e The center of the radar beam is referenced to the horizon by the aircraft vertical reference system e Adjusting the antenna tilt control will cause the center of the radar beam to scan above or below the plane of the attitude referenc
76. rning Flag In view indicating loss of signals power or altitude error 3 100 Foot Pointer Displays altitude in 100 foot increments One full rotation of pointer equals 1000 feet 2011 Captain Sim www captainsim com 20 DO NOT USE FOR FLIGHT 4 Altitude Numerical Counter Displays altitude in thousands and hundreds of feet 5 6 Altimeter Setting Windows Can be set in Millibars or inches Hg 7 Barometric Setting Control Rotation of the control adjusts the barometric setting on the inches of mercury in hg indicator 8 Reference Altitude Bug Selector Turn clockwise for higher reference altitude DOPPLER NAVIGATION SYSTEM The doppler system is a radar type navigation aid The system measures frequency changes in reflected micro wave radiation Known as doppler effect to provide ground speed drift angle Aircraft heading is combined with ground speed and drift angle to compute miles to go along track to a selected check point miles left or right of a selected track DOPPLER SENSOR Each sensor has a transmitter receiver frequency tracker indicator and control unit and shares an antenna assembly common to both systems Each sensor functions to determine and display ground speed and drift angle provide ground speed and track information to its navigation computer Transmitter energy is beamed sequentially in four directions downwards by a switching assembly The four element antenna arra
77. ronizing knob a synchronizing annunciator and a compass warning flag The compass card rotates in a manner such that the heading of the airplane will always be read under a fixed reference index lubber line at the top of the instrument Also fixed indices are provided at 45 90 135 180 225 270 and 315 The rotating compass card or azimuth card is graduated form O to 360 degrees clockwise in two degree increments The card is driven by a motor which receives signals from the directional gyro 2 SYNC Knob Rotates azimuth card for synchronization with flux valve 3 Compass Warning Flag A compass warning flag on the lower right hand corner of the RMI is marked OFF The warning flag will appear with loss of electrical power to the compass system 5 6 ADF VOR Pointers Pointers indicate ADF and VOR bearing as selected by the ADF VOR knobs at the bottom of the instrument A narrow pointer marked with a dashed line displays bearings from VOR No 1 or ADF No 1 as selected by the switch in the lower left corner of the instrument A wide pointer marked with two parallel solid lines displays bearings from VOR No 2 or ADF No 2 if installed as selected by the switch in the lower right corner 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 12 DO NOT USE FOR FLIGHT LO6 ANNUNCIATOR PANEL 1 z 1 VOR LOC Annunciator 2 Glide Slope Annunciator 3 GPWS PU
78. rs OFF Closes pack valves with both switches OFF MAIN and CREW temperature selectors deactivated and cockpit and main cabin temperature valves driven to full cold Warning Airplane will depressurize if both pack switches are OFF 25 Ram Air Switch Controls both left and right ram air valves CLOSE is the normal guarded position OPEN drives both ram air valves open admitting ambient air for ventilation unpressurized flight only 26 Air Supply Duct Pressure Gage www captainsim com DO NOT USE FOR FLIGHT Indicates pressure in pneumatic manifold Shows pneumatic manifold air pressure in 5 psi increments www captainsim com 81 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 82 DO NOT USE FOR FLIGHT U11 CABIN ALTITUDE PRESSURE SYSTEM PANEL PRESSURE DIFFERENTPAL PARE CE T Lee ER M FH ALG iGOL HDRH CUTOUT 11 12 14 13 16 17 18 1 Conditioned Air Duct Pressure Indicator 10 Cabin Altimeter 11 Rate Knob 12 Automatic Cabin Pressure Control Indicator 13 Barometric Correction Knob 14 Cabin Altitude Knob 15 Cabin Rate of Climb Indicator 16 Cabin Altitude Warning Horn Cutout Switch 17 18 Manual Cabin Pressure Control Indicator 1 Conditioned Air Duct Pressure Indicator Displays pressure differential between main cabin and distribution duct Reflects ventilation flow rate 6 10 INCHES Desired operating rate GREEN BAND Operating range 10 Cabin altimeter Shows cabin pre
79. since EPR is directly proportional to thrust 13 16 N1 Tachometers Indicates low pressure compressor rpm larger dial shows 2 increments smaller dial shows 1 increments Powered by a tachometer generator which is driven by the N1 shaft GREEN BAND Normal operating range RED RADIAL Maximum operating RPM VERNIER DIAL Fine reading 17 20 Engine Exhaust Gas Temperature Indicators Indicates turbine exhaust gas temperature in hundreds of degrees centigrade EGT indicator system is self powered GREEN BAND Normal operating range YELLOW BAND Approaching overtemperature RED RADIAL Maximum temperature for takeoff acceleration 2011 Captain Sim www captainsim com 31 DO NOT USE FOR FLIGHT 21 24 N2 Tachometers Indicates high pressure compressor rpm larger dial shows 2 increments smaller dial shows 1 increments Powered by a tachometer generator which is driven by the engine accessory gear box GREEN BAND Normal operating range RED RADIAL Maximum operating RPM 25 28 Engine Flowmeter Indicators Bug shows fuel flow to respective engine in pounds per hour X 1000 Digital counter shows total pounds consumed Requires ac power from the respective numbered bus for operation WWW captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 32 DO NOT USE FOR FLIGHT LANDING GEAR CONTROL PANEL 1 Door Open Light 2 Gear Unsafe Light 3 5 Down an
80. software It works with 707 Captain in 2D mode only INOP in VC To provide full VC compatibility we need additional tech info from the CIVA INS third party developer 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 63 DO NOT USE FOR FLIGHT PO7 TRANSPONDER CONTROL PANEL 1 Function Selector 2 ATC Display Window 3 Mode Selector 4 Altitude Reporting Switch 5 6 8 9 Code Selector Knobs 7 ATC Ident Button 4 6 7 B 85 10 10 Relative Altitude Display Limit Selector 1 Function Selector Selects operating mode STBY mode places transponder system to standby 2 ATC Display Window Displays Code set by ATC Code Selectors 5 6 8 9 Code Selector Knobs Rotate to set code on ATC display Window 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 64 DO NOT USE FOR FLIGHT P08 CONTROL STAND 1 11 a cya Bur PU 1 mii r 19 22 21 20 15 16 17 18 12 1 Speedbrake Control Lever and Indicator 2 5 Reverse Thrust Levers 6 Flap Control Lever 7 10 Engine Throttles 11 19 Stabilizer Trim Control Wheel 12 Stabilizer Trim Warning Light 13 Stabilizer Cruise Trim Switch 14 Mach Trim Switch 15 18 Engine Start Levers 20 Parking Brake Warning Light 21 Parking Brake Handle 22 23 Stabilizer Trim Indicator 1 Speedbrake Control Lever and Indicator Controls sym
81. ssure altitude in feet x 1000 Small needle indicates barometric altitude in feet x 1000 11 Rate Knob Adjusts cabin of change as shown on Cabin Climb Indicator DEC Establishes minimum change rate of about 50 fpm Centered pip black triangle position Establishes change rate of about 300 to 500 fpm INC Establishes maximum change rate of about 2000 fpm 2011 Captain Sim www captainsim com DO NOT USE FOR FLIGHT 12 Automatic Cabin Pressure Control Indicator Show selected cabin altitude 13 Barometric correction knob Sets barometric correction Moves 28 0 to 31 0 in Hg scale behind window to show correction applied 14 Cabin Altitude Knob Selects desired cabin altitude 15 Cabin Rate of Climb Indicator Shows rate of change in cabin altitude FPMx1000 WWW captainsim com 83 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 84 DO NOT USE FOR FLIGHT 012 AIR CONDITIONING PANEL 1 Duct Overheat Light Amber 2 Duct Overheat Reset Button 3 Main Duct Overheat Light Amber 4 Cabin Air Temperature Indicator 5 Cabin Air Temperature Select Switch 6 Crew Temperature Selector 7 Main Temperature Selector 8 9 Fault Light White Neon 10 Cabin Pressure Override Switch 11 Cabin Air Thrust Valve Position Switch ne S B COGLEA HARMER MAUL T OFF CABIN AIR THRUST VALVE Qy 2011 Captain Sim www captainsim com
82. sswind corrections are provided When crossing over the station the autopilot automatically switches from the VOR signal to the heading reference based on the captain s selected course for approximately 120 seconds It then reverts to normal VOR tracking This prevents nuisance corrections while in the cone of confusion With a LOC frequency tuned operation is similar to VOR with the following two exceptions Capture is initiated at 2 dots 212 degrees deviation from the localizer centerline The course set in the course counter determines only the initial heading to be flown since the localizer signal has specific orientation Theoretically no matter where the course was set the autopilot would eventually correct a mistake and fly down the localizer centerline However for quick and smooth capture and tracking the inbound front course is set in the course counter GS AUTO This mode provides automatic glideslope and localizer capture from above or below the glideslope Roll command is the same as in the VOR LOC mode with a LOC frequency tuned In addition following glidesfope capture part of the roll command signal is sent to the yaw control system either series or parallel yaw damper This crossfeed signal coordinates rudder and aileron control to provide greater stability and tighter tracking of the localizer during a coupled approach 2011 Captain Sim www captainsim com 70 DO NOT USE FOR FLIGHT Pitch command conti
83. statistically indicates a high probability of hail Note Do not approach a storm cell containing magenta and red any closer than 20 nautical miles Echoes should be separated by at least 40 nautical miles before attempting to fly between them Cells beyond 75 nautical miles are areas of substantial rainfall do not wait for red or magenta to appear Plan and execute evasive action quickly to minimize doglegging 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 62 DO NOT USE FOR FLIGHT When a complete detour is impractical penetration of weather patterns may be required Avoid adjacent cells by at least 20 nautical miles A Blind Alley or Box Canyon situation can be very dangerous when viewing the short ranges Periodically switch to longer range displays to observe distant conditions As shown below the short range returns show an obvious corridor between two areas of heavy rainfall but the long range setting shows a larger area of heavy rainfall PO5 CIVA INS CONTROL PANEL 1 2 d 4 J amp 7 8 9 1 HOLD Key 2 Waypoint DME Switch 3 REMOTE Key 4 Left Data Display 5 INSERT Key 6 ALERT Light 7 Right Data Display 8 BAT light 9 WARN Light 1011 12 13 14 15 24 25 10 Data Selector 11 Dim Switch 12 From To Display 13 Auto Man Switch TEST Switch 14 WYPT CHG key 15 24 Keyboard 25 CLEAR Key Delco Carousel IV A INS is freeware third party
84. tation 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 59 DO NOT USE FOR FLIGHT P04 RADAR DISPLAY UNIT 2 T 3 1 Range Selector Knob 2 Dimmer Knob 3 Erase Button 5 4 Gain Control Knob 5 Rotating Sweep Line 6 Weather Returns 1 Range Selector Knob Clears the display and advances the indicator to the next range The radar display ranges are 50 150 300 right click to increase range 2 Dimmer knob Controls brightness of the indicator display right click to increase brightness 4 Gain Control Knob The gain knob adjusts the radar gain from to 20 dB CCW rotation reduces gain PREFLIGHT PROCEDURES The system never transmits in the OFF STBY or TEST modes Note A 60 second warm up time period is required before the system will transmit 1 Place the radar controls in the following positions e Function switch to TEST e Tilt to UP 7 The test pattern will appear 2 With the function switch in TEST or STBY taxi to a clear area where there are no people aircraft vehicles or metallic buildings within approximately 100 yards 3 Rotate the function switch to NORM The indicator will automatically display in the Wx mode Weather targets will be displayed in grades of amber 4 Select 50 nm range 5 Select CTR mode to observe black contour areas if any 6 Repeat the manual tilt adjustment this time between the 0 and down 15 deg
85. tch Light is on any time turbocompressor is not operating OUT Oil pressure is normal or Turbocompressor has been stopped by switch 2011 Captain Sim www captainsim com 80 DO NOT USE FOR FLIGHT 7 9 Turbocompressor Overspeed Trip Lights Amber Turbocompressor has reached overspeed condition and has automatically shut down Can be reset only on the ground Shutoff valve has closed Pressure regulator valve has closed 10 12 Turbocompressor Switches Spring loaded to center position START opens turbine inlet shutoff valve arms open coil of pressure regulator arms LOW OIL PRESS light STOP closes turbine inlet shutoff valve disarms other start functions 13 14 17 18 Engine Bleed Air Switches Controls engine N1 bleed air valve ON Opens valve OFF Closes valve 15 16 Wing Valve Switches Controls wing valve in the pneumatic manifold OPEN Opens valve CLOSE Closes valve 19 20 Air Conditioning Unit Overheat Light Lights when LEFT or RIGHT ACM compressor outlet temperature excessive Resets automatically when temperature normal 21 22 Air Conditioning Unit OFF Light Lights when LEFT or RIGHT pack valve automatically closed as result of excessive ACM turbine inlet temperature condition Control is locked out until reset by DUCT OVERHEAT RESET button 23 24 Left amp Right Air Conditioning Unit Pack Switches ON Opens pack valves Arms MAIN and CREW temperature selecto
86. tor Radio waves travel at the speed of 300 million meters per second and thus yield nearly instantaneous in formation when echoing back Radar ranging is a two way process that requires 12 36 micro seconds for the radio wave to travel out and back for each nautical mile of target range As shown in the distance illustration below it takes 123 6 micro seconds for a transmitted pulse of radar energy to travel out and back from an area of precipitation 10 nautical miles away 20 NM ROUND TRIP IN 123 6 MICROSECONDS ba gt 10 WEATHER RADAR PRINCIPLES Airborne weather avoidance radar as its name implies is for avoiding severe weather not for penetrating it Whether to fly into an area of radar echoes depends on echo intensity spacing between the echoes aircraft capabilities and pilot experience Remember that weather radar detects only precipitation drops it does not detect minute cloud droplets nor does it detect turbulence Therefore the radar provides no assurance of avoiding instrument weather in clouds and fog The indicator may be clear between intense echoes this clear area does not necessarily mean it is safe to fly between the storms and maintain visual sighting of them RADAR BEAM ILLUMINATION Probably the most important aspect of a weather radar is the antenna beam illumination characteristic To make a proper interpretation of what you are seeing on the display you must have an understanding of what the radar
87. ttles Control engine forward thrust from idle to maximum Actuate landing gear warning horn 11 19 Stabilizer Trim Control Wheel Rotate whenever stabilizer is being positioned Contain integral handles which can be extended to manually trim stabilizer 10 revolutions equal one degree trim 12 Stabilizer Trim Warning Light An amber light on the control stand will illuminate when the stabilizer main electric trimmotor is operating or when the cruise and autopilot trim motor is operated by the stabilizer cruise trim switch The light will not be on when the autopilot operates the cruise and autopilot trim motor 15 18 Engine Start Levers Three engine start levers with CUTOFF IDLE detents are on the control stand This lever operates the windmill bypass and shutoff valve in the FCU With this lever in the IDLE detent fuel if supplied to the engine In the CUTOFF detent all fuel supply to the engine is shut off With this lever in the IDLE detent and with the engine start switch in the GROUND or FLIGHT position the 20 joule ignition system is energized WWW captainsim com 66 DO NOT USE FOR FLIGHT The start levers control the main fuel shutoff valves when in the CUTOFF position Used to start and stop the engines Connected by cables and linkage to each engineer s fuel control unit Three detended positions lifting knob enables movement CUTOFF Fuel and ignition are cut off START Ignition then fuel are su
88. utomatic mode Both systems pressurized automatically when cabin altitude reaches 14 000 ft 013 SEAT BELTS SWITCH 1 Seat Belts Switch A switch marked SEAT BELTS with ON OFF positions With this switch in the ON position a chord chime will sound 014 COCKPIT EMERGENCY EXIT LIGHTS SWITCH EMER EXIT LIGHTS 1 Cockpit Emergency Lights Switch 1 OFF Light will not illuminate Closing the guard will move switch to the ARMED position if it is in the OFF position 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 49 DO NOT USE FOR FLIGHT O15 CABIN CALL PANEL 1 2 1 Ground Crew Call Switch 2 Pers Accom Switch 3 Cabin Attendant Call Switch 4 Cabin Attendant Call Light blue 4 Cabin Attendant Call Light blue Illuminates while captain call switch is pressed at either attendant s panel 016 WINDSHIELD WIPERS SWITCH 1 Windshield Wipers Switch Each pilot s No 1 window is provided with an 28V DC DC2 for LI DC1 for RI electric 4 speed windshield wiper The two wipers are separate independent systems with a single 6 position PARK OFF LOW 1 2 3 4 HIGH control switch located on the pilot s overhead panel The PARK position stows the wipers at the bottom of the windshield and is spring loaded to the OFF position The LOW through HIGH positions select the speed of the wipers 017 EXTERIOR LIGHTING PANEL EXTERIOR LIGHTING
89. witch OFF Shuts off utility system pressure to outboard spoilers causing nose down pitch with speedbrake lever aft 3 Inboard Spoiler Switch OFF Shuts off auxiliary system pressure to inboard spoilers causing nose up pitch with speedbrake lever aft 2011 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part II Aircraft and Systems 44 DO NOT USE FOR FLIGHT 005 ANTI ICE CONTROLS 1 2 3 4 1 4 Nacelle Anti Ice Switches T 5 8 Valve Open Lights HACILLE ANTI 9 Nacelle Valve Selector Y M lhe 10 Rain Repellent Control Button AF A t WALVE OPEN HOSE COWL L R OFF ja ah ACELLE VALVE RAIN REPELLENT F F 1 4 Nacelle Anti Ice Switches Each controls its respective engine s LH RH and noze cowl valve ON Open all three valves Provides power to VALVE OPEN light OFF Closes all three valves Removes power from the VALVE OPEN light 5 8 Valve Open Lights ON Selected anti ice valve is open OFF Selected anti ice valve is not fully open The NACELLE VALVE selector is OFF The NACELLE ANTI ICE switch is OFF 9 Nacelle Valve Selector Controls the four VALVE OPEN lights With the selector positioned OFF all lights out L Each light monitors its left hand anti ice valve NOSE COWL Each light monitors its nose cowl anti ice valve R Each light monitors its right hand anti ice valve 2011 Captai
90. y is common to doppler systems The receiver portion of the transmitter receiver accepts the reflected energy from each beam and passes it to the tracker The receivers of doppler system can be operated simultaneously and normally are Magnetic heading information from either compass system is fed through a compass selector switch to doppler system trackers Each tracker measures the average frequency shift from the return signals of the four beams and computes ground speed and drift angle which is displayed on the indicator computes actual magnetic track from magnetic heading and drift angle and transmits this and ground speed to the navigation computer monitors return signals NAVIGATION COMPUTER The navigation computer uses track and ground speed information from the tracker to compute the aircraft s progress relative to a geographic position Progress is displayed as miles to go and miles left or right of track on the control panel Two positions labeled A and B may be selected Shifting from one position to another can be done automatically when miles to go reaches zero or may be done manually at any time DNS may be selected to provide heading commands to the autopilot NAV mode With the autopilot engaged in the NAV mode the selected doppler track will be intercepted and maintained Doppler navigation procedures are to be followed on all route segments over land or water when doppler navigation is required www captai

`707 Captain` FLIGHT MANUAL Part II – Aircraft

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`707 Captain` FLIGHT MANUAL Part II &ndash; Aircraft

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`707 Captain` FLIGHT MANUAL Part II – Aircraft