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Aircraft Systems

1. SLIDING WINDOW HANDLE OVERHEAD PANEL EYEBROW INSTRUMENT PANEL COPILOT S SIDE PANEL AISLE STAND PILOT S INSTRUMENT PANEL 7 ALTIMETER CORRECTION CARD AND HOLDER 8 PILOT S SIDE PANEL 2010 Captain Sim www captainsim com mr augurs TC LIT MANII D sad IT A ir s ft anA c gt D LDIIVCI LI Cin VIANUAL Fart AlFCFart vysterrs VT z 7 i L i 2 F E zi LX L L Lz La Li a is LA Ln Ln J Ln LI Lil LT Ps LPS 2010 Captain Sim www captainsim com B 52 Driver FLIGHT MANUAL Part II Aircraft and Systems DO NOT USE FOR FLIGHT 22 35 30 31 23 19 30 49 42 44 48 2010 Captain Sim www captainsim com CENTER 19 40 39 41 38 OVERHEAD 2010 Captain Sim www captainsim com DO NOT USE FOR FLIGHT ANTI ICE CONTROL PANEL EVS CONTROL PANEL CLOCK FLIGHT COMMAND INDICATOR ALTIMETER MARKER BEACON LIGHT TEST SWITCH INDICATED AIRSPEED INDICATOR HORIZONTAL SITUATION INDICATOR MARKER BEACON LIGHT ATTITUDE DIRECTOR INDICATOR AUTOPILOT DISENGAGED LIGHT EVS MONITOR VERTICAL VELOCITY INDICATOR MACH INDICATOR RADAR ALTIMETER STANDBY HORIZONT IND RADAR ALTIMETER CAUTION LIGHT ENGINE PRESSURE RATIO GAGES WING FLAP POSITION INDICATOR LANDING GEAR P
2. Aircraft and Systems 51 DO NOT USE FOR FLIGHT CUSTOMER CARE FORUM DG l s l i l i l l i l i l i l l l l l A 88 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 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 and consider the most significant issues for further upgrades 2010 Captain Sim www captainsim com
3. 20 24 LANDING GEAR POSITON INDICATORS PANEL 20 25 LOW OIL PRESSURE WARNING LIGHTS 20 27 ACCELEROMETER 21 29 MAGNETIC STANDBY COMPASS 21 30 EXHAUST GAS TEMPERATURE GAGE 21 31 FUEL FLOWMETERS 21 32 DME INDICATOR 22 34 OIL PRESSURE GAGES 22 35 TACHOMETERS 22 36 MASTER CAUTION LIGHT 23 38 FUEL SYSTEM MANAGEMENT PANELS 24 39 TOTAL FUEL FLOW INDICATOR 24 40 LANDING GEAR LEVER 25 CROSSWIND CRAB SYSTEM 26 TURNING ANGLES AVAILABLE WITH MAXIMUM CROSSWIND CRAB SETTINGS 27 CONTROLS AND INDICATORS 27 P21 CROSSWIND CRAB CONTROL KNOB 27 P22 CROSSWIND CRAB CONTROL CENTERING BUTION 27 41 CROSSWIND CRAB POSITION INDICATOR 28 42 TOTAL FUEL QUANTITY INDICATOR 28 43 MAIN TANKS LOW WARNING LIGHT 28 44 SAS CONTROL PANEL 28 49 BOMB DOORS OPEN LIGHT 29 50 BOMB DOORS NOT LATCHED LIGHT 29 51 ANTISKID SWITCH 29 52 OUTSIDE AIR TEMPERATURE GAGE 29 53 BOMB DOORS SWITCH 30 54 RUDDER TRIM INDICATOR 30 55 AUTOPILOT TURN CONTROL SELECTOR SWITCH 30 57 WINDSHIELD WIPERS SWITCH 31 59 HEADING INDICATOR GYRO 31 60 TRUE AIRSPEED INDICATOR 31 62 MACH INDICATOR SWITCH 31 63 FLIGHT DIRECTOR SWITCH WWW captainsim com DO NOT USE FOR FLIGHT 32 OVERHEAD PANEL 33 O01 OVERHEAD LIGHTING PANEL 33 O03 UHF RADIO CONTROL PANEL 34 O04 UHF2 RADIO CONTROL PANEL 34 O05 TACAN RADIO CONTROL PANEL 34 O06 VOR CONTROL PANEL 35 PILOT S SIDE PANEL 36 01 HYDRAULIC PANEL 37 A04 PILOT S LIGHT CONTROL PANEL 38 A07 ANTI
4. DO NOT USE FOR FLIGHT 13 18 Hydraulic System Pressure Gages Six gages on the hydraulic control panel indicate pressure of the hydraulic systems The location of each gage on the control panel corresponds to the respective hydraulic system which it serves and which is shown by outline on the control panel A04 PILOT S LIGHT CONTROL PANEL The following lights can be controlled independently from the pilot s light control panel 1 1 Pilots Side Panel Instruments Lights Switch 2 Forward Center Panel Instruments Lights Switch 3 Panels Backlights Switch Shift L 4 Pilot s Panel Instruments Lights Switch 5 Eyebrow Panel Instruments Lights Switch 3 4 1 Pilot s Side Panel Instruments Lights Switch Turns pilot s side panel instrument lights on off 2 Forward Center Panel Instruments Lights Switch Turns forward center panel instruments lights on off 3 Panels Backlights Switch Shift L Turns panels backlights on off 4 Pilot s Panel Instruments Lights Switch Turns pilot s panel instruments lights on off 5 Eyebrow Panel Instruments Lights Switch Turns eyebrow panel instruments lights on off WWW captainsim com B 52 Driver FLIGHT MANUAL Part II Aircraft and Systems 38 DO NOT USE FOR FLIGHT A07 ANTISKID MACH 1 2 1 Antiskid Switch 2 MACH Switch 3 Gyro Power Switch 1 Antiskid Switch The switch has two positions ON OFF and is guarded to the ON position When the switch
5. GEN CENTRAL TIE BUS ENG 5 EN ENG 7 GEN positions The switch provides a means of selecting and reading frequency and voltage gt i the central bus tie and of each generator In ENG 1 GEN position the frequency and voltage of the No generator may be read on the frequency meter and voltmeter provided the generators are isolated The remaining positions will perform the above operation tor their respective generators as marked When the generators are in parallel all generator switch positions will be read the same as the CENTRAL TIE BUS position 30 Master Isolate Switch An isolate switch is marked Push to Isolate Central Tie Bus Pressing the switch energizes the master isolate relay which In turn trips the bus tie circuit breakers isolating all generators from the central bus tie B02 TEMP INDICATOR Shows static air temperature 1 2 3 4 5 6 7 8 1 8 Starter Switches 1 8 Starter Switches These switches select the engines pair for which a starting function is desired When the starter switch is in START the starter air valve is opened and ignition power is directed to that engines pair 2010 Captain Sim www captainsim com MANUAL Part II Aircraft and Systems 42 DO NOT USE FOR FLIGHT B11 COPILOT S LIGHT CONTROL PANEL The following lights can be controlled independently from the copilot s light control panel 1 Copilot s Side Panel Instruments Lights Switch Turns copilot s side panel instruments
6. PANEL 04 LIGHT CONTROL 07 ANTISKID MACH GYRO A08 OXYGEN QUANTITY A14 OXYGEN REGULATOR PANEL 2010 Captain Sim www captainsim com Uv EJ E m E s a aa 14 19 15 1 5 31 7 2 7 18 1 6 Engine Driven Hydraulic Pump Out Lights 7 10 Standby Pump Switches 11 12 RUD ELEV Hydraulic System Switches 13 18 Hydraulic System Pressure Gages 19 22 RUD ELEV Hydraulic System Lights 1 6 Engine Driven Hydraulic Pump Out Lights Each of the six individual hydraulic systems has an red pump out indicating light located on the hydraulic control panel at the pilots station Since the lights indicate engine driven pump pressure only a light will remain on after failure of a main pump even though for those systems which have a standby pump system pressure is restored to normal by the standby pump Only a return of the affected main pump to proper operation will extinguish the light 11 12 RUD ELEV Hydraulic System Switches Two rudder elevator hydraulic system switches are located on the lower portion of the hydraulic control panel These switches have ON OFF positions and in the ON position they energize ac motor driven pumps that operate the rudder elevator main No 1 and 2 hydraulic systems In the OFF position power is removed from the hydraulic pumps 2010 Captain Sim www captainsim com AlFCFart and sYStems 37
7. is ON the antiskid system is in operation 2 MACH Switch Mach Indicator is a servo type indicator receiving power from the true airspeed computer through a Mach indicator switch on the pilot s side panel 3 Gyro Power Switch Two gyro power switches on the pilot s panel and pilot s side panel have ON OFF positions In ON position the pilots gyro power switch supplies power to the pilot s attitude indicating system and the heading indicator 2010 Captain Sim www captainsim com COPILT S SIDE PANELS UPPER DO NOT USE FOR FLIGHT B01 BO LOWER B14 B12 B13 BOL B02 B03 B07 B08 B11 B12 B13 B14 ELECTRICAL PANEL TEMP INDICATOR OIL TEMP INDICATOR ENG START CONTROL PANEL GYRO POWER SWITCH LIGHT CONTROL HF RADIO PANEL OXYGEN REGULATOR PANEL BATTERY SWITCH PANEL n Sim www captainsim com B 52 Driver FLIGHT MANUAL Part II Aircraft and Systems 40 DO NOT USE FOR FLIGHT B01 ELECTRICAL PANEL 12 1 7 8 13 2 5 14 3 10 11 154 3 6 28 2016 24 23 21 1730 2922 1826 27 23 19 1 4 Ammeter 5 Voltmeter 6 Frequency Meter 7 8 10 11 Generator Switch 9 Main External Power Switch 12 15 Generator Circuit Breaker Position Indicator 16 19 Bus Tie Circuit Breaker Position Indicator 20 23 Generator Drive Overheat Light 24 27 Generator Drive Decoupler Switch 28 Frequency And Voltmeter Selector Switch 29 External Power Circuit Breaker Position Indicator 30 Master Isolate S
8. lights on off 2 Panels Backlights Switch Shift L Turns panels backlights on off 3 Copilot s Panel Instruments Lights Switch Turns copilot s panel instruments lights on off B12 HF RADIO PANEL 1 3 4 5 NAV1 Frequency Selection Knobs 2 NAV1 Frequency Selection Indicator 2010 Captain Sim www captainsim com L 43 DO NOT USE FOR FLIGHT B14 BATTERY SWITCH PANEL 1 Battery Switch Shift M An ON OFF battery switch on the copilot s side panel routes battery power to the essential battery buses When the battery switch is placed in ON position battery power is directed to the essential buses through the essential dc battery relays and when TR power is available relays are energized to transfer essential buses to TR power When the battery switch is in OFF position no battery power is available to the essential battery buses Battery power is supplied directly from each battery to individual direct battery buses at all times regardless of the position of the battery switch 10 Captain Sim www captainsim com 44 AISLE STAND www captainsim com i UNE B 52 Driver FLIGHT MANUAL Part II Aircraft and Systems 45 DO NOT USE FOR FLIGHT P02 AIRBRAKE LEVER AUTOPILOT TURN AND PITCH CONTROLLER P04 AUTOPILOT COMMAND SELECTOR PANEL 05 CROSSWIND CRAB CONTROL KNOB P06 LANDING LIGHTS PANEL P10 STABILIZER TRIM WHEEL AND
9. steering bar will will respond to the heading set by the heading set knob on the captain s horizontal situation indicator The bar will indicate zero deflection when the aircraft has the correct bank angle to arrive at the selected heading The heading can be maintained by keeping the bank steering bar at zero deflection The autopilot localizer and glide slope can be energized only when the nav mode select switch is in ILS or ILS APP position respectively and the omni range radio system is on and tuned to an ILS frequency WWW captainsim com MANUAL Part II Aircraft and Systems 48 DO NOT USE FOR FLIGHT PO6 LANDING LIGHTS PANEL 1 2 Landing Lights ON OFF Switch Ctr L Turn landing lights on off Crosswind Landing Light Switch Turn crosswind landing lights on off Taxi Lights Switch Turn taxi lights on off P10 STABILIZER TRIM WHEEL AND INDICATOR 1 Copilot s Trim wheel 2 Stabilizer Trim Indicator 1 Manual control of the stabilizer trim metering valve is provided by rotation of the stabilizer trim wheels on the aisle stand The pilot s trim wheel is attached to the throttle shaft and 3 operates through a chain sprocket linkage to move a trim indicator located forward and inboard of the wheel The copilot s trim wheel and trim indicator are located opposite to the pilot s trim indicator The manual trim wheels can be used to override the electric trim control system or autopilot trim system The tr
10. 2010 Captain Sim www captainsim com B 52 Driver FLIGHT MANUAL Part II Aircraft and Systems 28 DO NOT USE FOR FLIGHT 42 TOTAL FUEL OUANTITY INDICATOR Indicates total quantity of fuel in the aircraft MAIN TANKS LOW WARNING LIGHT Illuminates when there is low fuel in main tanks 44 SAS CONTROL PANEL 1 Yaw SAS Switch The pitch and yaw SAS provides increased aircraft stability and structural life with improved handling qualities over non SAS operation The yaw SAS commands the rudder to dampen aircraft oscillations in yaw as measured by triply redundant yaw rate and lateral acceleration sensors located the fuselage Electrical signals from these sensors are fed to the rudder hydraulic actuator The yaw SAS can command maximum rudder deflections of 10 49 BOMB DOORS OPEN LIGHT A green caution light marked Bomb Doors Open When illuminated they indicate that the bomb doors are fully open that the bomb doors will be held open until the bomb doors close circuit is energized and that the bomb door safety switches are positioned so bomb release may be made by either the normal or the jettison system The lights will remain illuminated as long as the bomb doors are fully open 2010 Captain Sim www captainsim com B 52 Driver FLIGHT MANUAL Part II Aircraft and Systems 29 DO NOT USE FOR FLIGHT 50 BOMB DOORS NOT LATCHED LIGHT An amber caution light marked Bom
11. DER TRIM INDICATOR 55 AUTOPILOT TURN CONTROL SELECTOR SWITCH The indicator provides an indication of rudder trim input This switch is of the solenoid locking type and has PILOT BOMB positions for selecting either the autopilot flight controller PILOT or the BNS BOMB respectively for turn command of the autopilot Interlocks will return the turn control selector switch from BOMB to PILOT position without disengaging the autopilot when the pilots turn knob is rotated out of center detent BOMB position is INOP 57 WINDSHIELD WIPERS SWITCH 2010 Captain Sim www captainsim com Electrically operated windshield wipers clear the windows in front of the pilot and copilot A separate motor drives each of the two blades Both wipers are controlled by a single rotary type switch on the pilots Instrument panel The switch has PARK OFF 1 2 3 positions giving a choice of wiper speeds The switch is spring loaded from PARK to OFF position After use the switch is held in PARK position until the blades move to the stowed position and stop The switch is then placed to OFF position B 52 Driver FLIGHT MANUAL Part II Aircraft and Systems 31 DO NOT USE FOR FLIGHT 59 HEADING INDICATOR A Type C 2A heading indicator gyro is located on the left side of the pilots instrument panel The heading indicator is an unslaved gyro which X provides auxiliary headings for navigational purposes and is also used to provi
12. DO NOT USE FOR FLIGHT y i P 1 Je d 4 au Z d D lah tal PART II Aircraft and Systems WWW captainsim com DO NOT USE FOR FLIGHT ABOUT THIS MANUAL VERSION 08 DECEMBER 2010 WARNING THIS MANUAL IS DESIGNED FOR MICROSOFT FSX USE ONLY DO NOT USE FOR FLIGHT The B 52 Driver FLIGHT MANUAL is organized into three Parts Each Part is provided as a separate Acrobat PDF document e Part I User s Manual Part II Aircraft and Systems this document Part III Normal Procedures FOR GENERAL INFORMATION ON THE B 52 DRIVER 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 PART II AIRCRAFT SYSTEMS Page Contents 5 INTRODUCTION 6 PANELS LAYOUT 7 PILOT S INSTRUMENT PANELS 11 1 ANTI ICE CONTROL PANEL 11 2 EVS CONTROL PANEL 12 3 CLOCK 12 4 FLIGHT COMMAND INDICATOR 12 5 ALTIMETER 13 8 MARKER BEACON LIGHT TEST SWITCH 13 9 INDICATED AIRSPEED INDICATOR 13 10 HORIZONTAL SITUATION INDICATOR 14 11 MARKER BEACON LIGHT 15 12 ATTITUDE DIRECTOR INDICATOR 16 TERRAIN AVOIDANCE RADAR SYSTEM 17 CONTROLS AND INDICATORS 17 14 EVS MONITOR 17 P20 TERRAIN DISPLAY CONTROL PANEL 18 15 VERTICAL VELOCITY INDICATOR 18 16 MACH INDICATOR 18 17 RADAR ALTIMETER 19 18 STANDBY HORIZONT INDICATOR 19 22 ENGINE PRESSURE RATIO GAGES 19 23 WING FLAP POSITION INDICATOR
13. Driver FLIGHT MANUAL Part II Aircraft and Systems 19 DO NOT USE FOR FLIGHT 1 2 1 Attitude Sphere 2 Miniature Aircraft 3 Pitch Trim Knob 4 Bank Scale 5 Bank Pointer Pitch Trim Knob permits zeroing the horizon line with reference to the miniature aircraft 22 ENGINE PRESSURE RATIO GAGES An engine pressure ratio EPR gage for each engine is located on the pilots instrument panel These gages indicate the ratio of engine inlet to exhaust pressures which is used as a measure of engine thrust The engine inlet and exhaust indications are compared by a computer transmitter which electrically transmits an indication to the engine pressure ratio gage 23 WING FLAP POSITION INDICATOR A wing flap position indicator is provided on the pilots instrument panel This indicator reads from 0 to 100 of wing flap travel 2010 Captain Sim www captainsim com Cy 52 Driver FLIGHT MANUAL Part II Aircraft and Systems 20 DO NOT USE FOR FLIGHT 1 2 3 4 1 6 Landing Gear Position Indicators LANDING Six tab window type landing gear position GEAR indicators in the lower center of the pilots instrument panel indicate landing gear position Each tab indicator has three visual indicators to register landing gear position When the landing gear is up and locked the word UP appears in the tab window A gear in an intermediate position is indicated by slanting alternate black and ivory stripes The ap
14. GHT 38 FUEL SYSTEM MANAGEMENT PANELS I z 3 45 6 7 8 9101112 13 17 18 19 222324 252627282930 31 32 33 34 353637 3B 3940 1 3 7 8 16 18 22 25 28 31 36 39 Fuel Quantity Gages 2 4 9 10 15 17 24 27 30 32 35 38 Fuel Flow Indicator Lights 5 6 13 14 Auxiliary Tank Engine Feed Control Valve Switches 11 12 20 21 29 33 41 42 Auxiliary Tank Fuel Flow Control Switches 19 Wing Tank Warning Light 23 26 37 40 Main Tank Fuel Level Control Valves Switches 34 Main Mainfold Interconnect Valves Switch 1 3 7 8 16 18 22 25 28 31 36 39 Fuel Quantity Gages The quantity of available fuel in each tank is indicated in pounds by 12 fuel quantity gages on the fuel system panel Fuel probes in each tank sense quantity indications The fuel probe signals are relayed to amplifiers which operate the gages Due to the type of fuel quantity probes used changes in fuel density have little if any effect upon quantity indications 2 4 9 10 15 17 24 27 30 32 35 38 Fuel Flow Indicator Lights Twelve amber fuel flow indicator lights are located on the fuel system panel adjacent to the fuel quantity gages Those indicator lights indicate no fuel flow from the corresponding tank during fuel feed operations 5 6 13 14 Auxiliary Tank Engine Feed Control Valve Switches Four auxiliary tank engine feed control valve I switches on the fuel system panel have unmarked OP EN CLOSED positions These rotary switches are control operation of valves of corresponding numbers to d
15. INDICATOR P11 THROTTLES P12 THROTILE BRAKE LEVER P13 PARKING BRAKE LEVER Ctr P15 DRAG CHUTE LEVER P17 WING FLAP LEVER P18 NAVIGATION SYSTEM SELECT PANEL P19 TERRAIN DISPLAY CONTROL PANEL P21 RUDDER TRIM KNOB P22 CROSSWIND CRAB CONTROL CENTERING BUTION PO2 AIRBRAKE LEVER The airbrake lever on the pilot s side of the aisle stand operates airbrakes PO3 AUTOPILOT TURN AND PITCH CONTROLLER 1 z 1 1 Pitch Controllers 2 Turn Controller 1 Pitch Controllers 2 controllers 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 Altitude Hold is selected or when glideslope is captured 2 Turn Controller e Detented at center position e Maybe rotated at 130 degrees in either direction e When rotated causes airplane to turn Rate and amount of rotation determines rate and amount of airplane roll e Will remain in any position e Can effect a maximum bank angle of 509 2010 Captain Sim www captainsim com 46 DO NOT USE FOR FLIGHT P04 AUTOPILOT COMMAND SELECTOR PANEL 1 2 3 1 Autopilot Master Pilot Switch 2 Servos Engage Switch 3 Altitude Control Switch 4 Automatic Approach Localizer Switch 5 Automatic Approach Glide Slope Switch 4 1 Autopilot Master Pilot Switch Z key An autopilot master pilot s
16. OSITON INDICATORS PANEL LOW OIL PRESSURE WARNING LIGHTS ACCELEROMETER MAGNETIC STANDBY COMPASS EXHAUST GAS TEMPERATURE GAGE FUEL FLOWMETERS DME INDICATOR OIL PRESSURE GAGES TACHOMETERS MASTER CAUTION LIGHT FUEL SYSTEM MANAGEMENT PANELS TOTAL FUEL FLOW INDICATOR LANDING GEAR LEVER CROSSWIND CRAB POSITION INDICATOR TOTAL FUEL QUANTITY INDICATOR MAIN TANKS LOW WARNING LIGHT SAS CONTROL PANEL TOTAL OXYGEN QUANTITY GAGE BOMB DOORS OPEN LIGHT BOMB DOORS NOT LATCHED LIGHT ANTISKID SWITCH OUTSIDE AIR TEMPERATURE GAGE BOMB DOORS SWITCH LATERAL TRIM INDICATOR AUTOPILOT TURN CONTROL SELECTOR SWITCH WINDSHIELD WIPERS SWITCH HEADING INDICATOR GYRO TRUE AIRSPEED INDICATOR LANDING GEAR CONTROLS PANEL MACH INDICATOR SWITCH FLIGHT DIRECTOR SWITCH WWW captainsim com 10 11 DO NOT USE FOR FLIGHT 1 ANTI ICE CONTROL PANEL 1 1 2 Pitot Heat Switches 3 Engine Nacelle And Scoops Anti Icing Switch 1 Pitot Heat Switches Two ON OFF pitot heat switches are located on the left side of the pilots instrument panel ON position of each switch energizes the I pitot tube heaters on the respective left or right side of the aircraft to prevent pitot tube stoppage by icing The left pitot heat switch also controls the Q spring ram air inlet heater OFF position removes power from the heaters 3 Engine Nacelle and Scoops Anti Icing Switch The ON OFF
17. SKID MACH 39 COPILT S SIDE PANEL 40 BO1 ELECTRICAL PANEL 41 B02 TEMP INDICATOR 41 B07 ENG START CONTROL PANEL 42 B11 COPILOT S LIGHT CONTROL PANEL 42 B12 HF RADIO PANEL 43 B14 BATTERY SWITCH PANEL 44 AISLE STAND 45 P02 AIRBRAKE LEVER 45 P03 AUTOPILOT TURN AND PITCH CONTROLLER 46 P04 AUTOPILOT COMMAND SELECTOR PANEL 47 P18 NAVIGATION SYSTEM SELECT PANEL 48 P06 LANDING LIGHTS PANEL 48 P10 STABILIZER TRIM WHEEL AND INDICATOR 49 P11 THROTTLES 49 P15 DRAG CHUTE LEVER 50 P17 WING FLAP LEVER 51 CUSTOMER CARE 51 FORUM 51 VIDEO CHANNEL 51 TECH SUPPORT WWW captainsim com DO NOT USE FOR FLIGHT INTRODUCTION The B 52 Driver is one of the most advanced complete and accurate digital replicas of the B 52 aircraft ever available for any game platform But the B 52 Driver 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 Moreover the B 52 Driver is Fun Line product so it features some of essential systems programming 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 B 52 Driver FLIGHT MANUAL Part II Aircraft and Systems DO NOT USE FOR FLIGHT PANELS LAYOUT
18. TH MAXIMUM CROSSWIND CRAB SETTINGS RELATIVE es ipe WIND 35 1 56 NEW NEUTRAL POSITION 20 NOSE LEFT CRAB SETTING REMARKS Crab setting refers to direction of the nose of the aircraft relative to desired heading CONDITIONS e Aircraft taxiing with 20 nose left crosswind crab setting e Steering ratio lever in TAKI 1 Turning angle available in direction of crab setting is 559 from new neutral position 2 Turning angle available in direction opposite crab setting is 359 55 minus 209 from new neutral position 2010 Captain Sim www captainsim com B 52 Driver FLIGHT MANUAL Part II Aircraft and Systems 27 DO NOT USE FOR FLIGHT CONTROLS AND INDICATORS P21 CROSSWIND CRAB CONTROL KNOB The crosswind crab control knob is recessed in the rudder trim control knob on the aft end of the aisle stand The control sets the amount of nose left or right trim selected When the crosswind crab control knob is turned for trim cable linkage moves the jackscrew at the differential coordinating unit The jackscrew positions the rear drum of the coordinating unit to move cable and mechanical linkage to operate the forward gear steering metering valves The jackscrew also moves cable and mechanical linkage to operate the rear gear steering metering valves It is to be noted that the rear main gear can be steered only through movement of the jackscrew of the coordinating unit while the forward main gea
19. agnetic Course Indicator 4 TA return 5 Radar Altitude Indicator up 5000 feet 6 Brightness Knob P20 TERRAIN DISPLAY CONTROL PANEL 1 Mode Selector Switch MAP PEAK 2 Range Selector Knob Note The higher an aircraft above the terrain is the more difference between MAP and PEAK mode returns MAP Mode PEAK Mode 2010 Captain Sim www captainsim com B 52 Driver FLIGHT MANUAL Part II Aircraft and Systems 18 DO NOT USE FOR FLIGHT 15 VERTICAL VELOCITY INDICATOR An MS28049 vertical velocity indicator is located at both the right and left sides of the pilots instrument panel The pointer shows aircraft vertical speed 16 MACH INDICATOR 1 M Pointer 2 Rotating Subdial Indicates the ratio of aircraft speed to the speed of sound at the particular pressure altitude at any time during flight The instrument has a range of 0 5 to 1 0 which is indicated on a stationary dial by a rotating pointer Note Mach Indicator Switch must be in ON position 17 RADAR ALTIMETER 1 Radar Altimeter Caution Light 2 Altitude Indicator Needle The instrument provides for measuring absolute altitude from 0 to 5000 feet An altitude indicator needle indicates altitude from O to 1000 feet in 20 foot increments and from 1000 to 5000 feet in 100 foot increments 2 1 Radar Altimeter Caution Light is ON if aircraft is lower than 150 feet above ground 2010 Captain Sim www captainsim com B 52
20. b Doors Not Latched Will illuminate when the forward bomb door latch is unlatched These lights will remain on until the bomb doors are closed and the forward bomb door is latched 51 ANTISKID SWITCH The switch has two positions ON OFF and is guarded to the ON position When the switch is ON the antiskid system is in operation 52 OUTSIDE AIR TEMPERATURE GAGE A Type G 10 outside air temperature gage is located on the left side of the pilot s instrument panel The air temperature gage is operated by an electrical resistance thermometer bulb located flush with the body skin on the lower left side of the forward pressurized section of the radar navigators escape hatch The temperature range of the gage is 70 to 50 C The pointer should rest off the scale with power off and should register outside air temperature with power on 53 BOMB DOORS SWITCH A pilots bomb door on the pilots instrument panel provides a means of controlling the bomb doors The switch has OPEN OFF CLOSED positions and is spring loaded to OFF position Actuating this switch to OPEN or CLOSED position will energize the bomb doors open circuit or the bomb doors close circuit which positions the bomb door control valves which in turn directs hydraulic pressure to the bomb door actuators 2010 Captain Sim www captainsim com B 52 Driver FLIGHT MANUAL Part II Aircraft and Systems 30 DO NOT USE FOR FLIGHT 54 RUD
21. de headings in the event of failure of the main compass system 60 TRUE AIRSPEED INDICATOR A true airspeed indicator is a remote indicating unit A main dial and subdial in the true airspeed indicator repeat airspeed information transmitted from the true airspeed computer A cutout and reference mark on the main dial permit reading of the subdial The power to operate this indicator is supplied by the true airspeed computer The true airspeed computer uses static pressure pitot pressure and temperature to compute true airspeed and Mach information 62 MACH INDICATOR SWITCH Mach Indicator power switch on the pilot s panel has ON OFF positions In ON position the switch supplies power to the pilot s Mach Indicator 63 FLIGHT DIRECTOR SWITCH Flight Director switch on the pilot s panel has ON OFF positions In ON position the switch supplies power to the Flight Director indicators 2010 Captain Sim www captainsim com 32 DO NOT USE FOR FLIGHT OVERHEAD PANEL 2010 Captain Sim www captainsim com O06 O01 OVERHEAD LIGHTING PANEL O03 UHF RADIO CONTROL PANEL O04 UHF2 RADIO CONTROL PANEL O05 TACAN RADIO CONTROL PANEL O06 VOR CONTROL PANEL B 52 Driver FLIGHT MANUAL Part II Aircraft and Systems 33 DO NOT USE FOR FLIGHT O01 OVERHEAD LIGHTING PANEL The following lights can be controlled independently from the overhead light control panel 1 2 3 1 Dome Flood Light Switch 2 Navi
22. ding distance Captain Sim www captainsim com B 52 Driver FLIGHT MANUAL Part II Aircraft and Systems 50 DO NOT USE FOR FLIGHT P17 WING FLAP LEVER The wing flap system includes four separate wing flap sections The flaps are of the Fowler type with high liftdrag ratio resulting in shortened takeoffs and reduced landing speeds All four flap sections are simultaneously driven by a single power unit located in the fuselage aft of the center section gear spar During the first 37 of extension the flaps rotate downward 35 with little rearward movement For the remainder of the extension the flaps move rearward only Most of the drag increase occurs during the first 20 of the flap motion This initial 20 rotates the flaps down 29 in approximately 12 seconds leaving only 6 of rotation in the remaining 809 of flap extension The flaps are electronically controlled by a single flap lever No emergency control system is provided for the flaps 2010 Captain Sim www captainsim com Control of the wing flaps is accomplished by moving a lever with an airfoil type knob on a detent quadrant located on the right side of the aisle stand This lever can be moved from either the UP or DN position When the lever is placed in the UP or DN position a circuit is closed to supply TR power to left and right flap extend or retract relays The flaps extend retract fully in approximately 60 seconds B 52 Driver FLIGHT MANUAL Part II
23. e In VOR position the omnirange radio navigation system is selected and NAV1 may be placed in operation The bank steering bar will respond to NAV1 Ctr N e In ILS positions the instrument landing system mode of navigation is selected The bank steering bar will respond to ILS localizer If Autopilot is engaged ILS position allows the lateral controls of the autopilot to be controlled by the localizer beam after it has been intercepted Ctrl 0 e In ILS APP positions the instrument landing system mode of navigation is selected The bank steering bar will respond to ILS localizer The pitch steering bar will will respond to ILS glideslope If Autopilot is engaged ILS APP position allows the lateral and pitch controls of the autopilot to be controlled by the localizer and glide slope beams after they have been intercepted Ctr A Note Nav Mode Selector Switch is active only if Heading Selector Switch in NOR position 2 Heading Selector Switch Ctr H A heading selector switch located on the navigation system select panel on the aisle stand is marked HDG Select The switch has MAN NOR positions and controls the input source for signals to the bank steering bar on the attitude director indicator In NOR normal position the information displayed on the flight director indicator will be determined by the position of the mode select switch In MAN manual position the flight director system will overrides Nav Mode Selector Switch The bank
24. engine nacelle and scoops anti icing switch on the anti ice control panel controls anti icing of engine inlet components nacelle leading edge areas the ram airscoop lip in the left wing and the cabin emergency rain airscoop ON position makes the connections to supply TR power to energize the various solenoids and relays which cause the anti icing air valves to open and turn on the electrical heater power OFF position deenergizes the solenoids and relays causing engine nacelle and scoop anti icing to be shut off The emergency ram airscoop is electrically heated and will also cycle approximately 1 minute open and 15 seconds closed to prevent ice formation when the engine nacelle and scoops anti Icing switch is ON and the air conditioning master switch is in RAM 2 EVS CONTROL PANEL 1 Power Switch The power switch on the pilots EVS control panel is a push on push off type switch having an ON position depressed switch face flush with switch housing and an OFF position extended switch face extends approximately 1 8 inch from switch housing which is mechanically latched in each position The switch is used to turn on and place the EVS monitor in standby mode When depressed in ON position the word ON green is illuminated on the switch face provided power is on in the aircraft When the switch is pressed again and the switch face extends from its housing the switch is OFF and the EVS monitor is deactivated and power is
25. erate the gages which are independent of the aircraft electrical power system Fuel flow to the engine is shown by eight fuel flowmeters on the pilots instrument panel These indicators read in pounds per hour and operate on TR power 32 DME INDICATOR Indicates the line of sight distance to DME station 2010 Captain Sim www captainsim com B 52 Driver FLIGHT MANUAL Part II Aircraft and Systems 22 DO NOT USE FOR FLIGHT 34 OIL PRESSURE GAGES Engine oil pressure is indicated by eight oil pressure gages located on the eyebrow instrument panel 35 TACHOMETERS 1 1 Larger Pointer 2 Small Pointer Speed of the high pressure compressor rotor in percent rpm is indicated by eight tachometers on the pilot s instrument panel Engine driven tachometer generators supply power to operate the indicators which are independent of the aircraft electrical system Each instrument has two pointers 1 Larger Pointer Is read on a dial calibrated from 0 to 100 rpm 2 Small Pointer Indication is read on a dial calibrated from 0 to 10 rpm 36 MASTER CAUTION LIGHT Is ON if any of the following occurs 1 In the fuel tank there is less than 10 of fuel 2 Vertical speed is more than 7000 ft per minute 3 Altitude is less than 200 ft and speed is more than 250 Knots 2010 Captain Sim www captainsim com IANUAL Part II Aircraft and Systems 23 DO NOT USE FOR FLI
26. eration when the NAV1 fails or a glide slope signal of dependable strength is not being received 2010 Captain Sim www captainsim com B 52 Driver FLIGHT MANUAL Part II Aircraft and Systems 16 DO NOT USE FOR FLIGHT TERRAIN AVOIDANCE RADAR SYSTEM The terrain avoidance TA system comprises a special mode of radar an electronic terrain computer radar scan converter video distribution unit and the pilot s and copilot s terrain display indicators EVS monitors and their associated electronic components The TA system provides a monochromatic radar display of actual FSX terrain rrelief along the flight path of the aircraft By interpreting the display and manoeuvring the aircraft accordingly the pilot is able to fly the aircraft at low absolute altitudes aircraft to terrain separation distance RADAR ALTIMETER COVERAGE UPPER ACCURACY LIMIT AREA s OF ACCURATE CLEARANCE PLANE E TA COMPUTATION REFERENCE LINE a j y s kJ m rinm 400 lt 800 A Ree RS SOC AN a aa N Red c mer oe rm Siren ayasa 1800 amp 2 Zh D m o WOKE e 7 b PRO aa x 7 RANGE NAUTICAL MILES 2010 Captain Sim www captainsim com FLIGHT MANUAL Part II Aircraft and Systems 17 DO NOT USE FOR FLIGHT CONTROLS AND INDICATORS 14 EVS MONITOR EVS monitor is located at both pilots stations 1 2 3 4 2 6 1 Indicated Airspeed Indicator 2 EVS monitor 3 M
27. ever are GEAR UP GEAR DOWN 2010 Captain Sim www captainsim com 25 DO NOT USE FOR FLIGHT CROSSWIND CRAB SYSTEM A crosswind crab system is provided on this aircraft to facilitate making crosswind landings and takeoffs and to reduce the hazards of crosswind conditions The crosswind crab system provides a means of turning all four main gear to align with the runway while the aircraft is flown in a wings level attitude compensating for drift This system utilizes the steering actuators on the front main gear and a similar set on the rear main gear The landing gear can be preset and turned up to 20 left or right of center during the approach The maximum of 209 crab will accommodate landings in crosswinds up to and including 43 knots blowing 90 to the runway at a landing weight of 270 000 pounds The direction of the landing gear is preset by a crosswind crab control knob which mechanically operates the steering metering valves on each main gear These valves meter hydraulic pressure to the actuating cylinders to position the gear as desired The crosswind crab system is automatically centered when the landing gear lever is moved to the GEAR UP position On the ground after landing the gear is quickly centered by a pilot operated centering button or by turning the crosswind crab control knob to center WWW captainsim com B 52 Driver FLIGHT MANUAL Part II Aircraft and Systems 26 DO NOT USE FOR FLIGHT TURNING ANGLES AVAILABLE WI
28. f the pilots instrument panel By the use of two pointers the pilots can observe the airspeed indication and the maximum allowable airspeed 1 indication at the same time The airspeed dial is graduated from 50 to 650 in 10 knot increments 10 HORIZONTAL SITUATION INDICATOR 1 2 5 7 Range Indicator Range Indicator Warning Flag Heading Marker Lubber Line Compass Card Course Deviation Indicator Warning Flag Course Selector Window Power Off Flag Course Arrow Head 10 To From Indicator 11 Course Deviation Indicator 12 Course Set Knob 13 Heading Set Knob 14 Course Arrow Tail 12 15 Aircraft Symbol 16 Course Deviation Scale 17 Bearing Pointer head 13 1B 15 106 18 Bearing Pointer tail 16 O Q N 11 14 It is an electrically operated instrument and replaces the bearing distance indicator the radio course indicator and the directional indicator heading system In the event of loss of all ac power no information will be available from either the pilot s or copilot s horizontal situation indicator 1 Range Indicator Will give a digital display of the line of sight distance 2 Range Indicator Warning Flag The display will be covered by a range indicator warning flag if the NAV1 radio system is not tuned to a surface beacon that is within 300 nautical miles of the aircraft and will also be covered if the NAV1 station is not transmitting a signal of depe
29. gational Lights Switches 3 Anti collision Lights Switch Strobe Lights FSX key 4 Overhead Instruments Lights Switch 4 1 Dome Flood Light Switch Red and white lights are controlled by a RED OFF WHITE toggle switch 2 Navigational Lights Switches ON position selects illumination of all navigational lights while OFF position turns the lights out O03 UHF RADIO CONTROL PANEL 1 1 COMM 1 Frequency Indicator 2 5 COMM 1 Frequency Selector Knobs 2010 Captain Sim www captainsim com 34 FLIGHT MANUAL Part II Aircraft and Systems DO NOT USE FOR FLIGHT 004 UHF2 RADIO CONTROL PANEL 12 34 5 6 78 3 10 1 3 5 7 9 COMM 2 Frequency Indicator 2 4 6 8 10 COMM 2 Frequency Selector Knobs O05 TACAN RADIO CONTROL PANEL 1 NAV2 Frequency Indicator Window 2 NAV2 Frequency tens and units Selector Knob 3 NAV2 Frequency tenth and hundredth Selector Knob 1 NAV2 Frequency Indicator Window Indicates selected NAV2 frequency Note As the first digit of the frequency is always 1 so it is not shown on the indicator O06 VOR CONTROL PANEL 2 1 NAV1 Frequency Indicator 2 NAV1 Frequency Selector Switch Note As the first digit of the frequency is always 1 so it is not shown on the indicator 2010 Captain Sim www captainsim com LIC IANUAL Part II Aircraft and Systems 35 DO NOT USE FOR FLIGHT PILOT S SIDE PANELS UPPER PANEL 404 AU LOWER PANEL 01 HYDRAULIC
30. im wheel face and periphery is painted in alternate black and white segments as a visual aid and reminder when the electric trim control system is being used 2010 Captain Sim www captainsim com LIGHT MANUAL Part II Aircraft and Systems 49 DO NOT USE FOR FLIGHT P11 THROTTLES Eight throttles control eight engines Due to MSFS limitations the eight throttles combined as four pairs of engines Note Place all throttles to idle position F1 before engines starting up P15 DRAG CHUTE LEVER Positions of the lever are DEPLOY LOCKED JETTISON This lever manually operates the drag chute release and jettison mechanisms through a cable system Normally the lever must be moved to DEPLOY before it can be moved to JETTISON position LOCKED position holds the spring loaded drag chute compartment door securely closed JETTISON position causes release of the jettison mechanism and allows the chute to pull free of the aircraft Drag Chute Limitations e During the deceleration of a landing or refused take off the drag chute may be deployed at 135 knots IAS Deployment at higher speeds may result in failure of the chute or the shear pin Drag chute will not deploy at or over 200 knots IAS Once deployed the drag chute will automatically jettison at 20 knots IAS To deploy the drag chute while in exterior views use Wing Fold FSX key should be assigned Drag chute is visual feature it does not affect lan
31. irect auxiliary tank fuel to the engines 11 12 20 21 29 33 41 42 Auxiliary Tank Fuel Flow Control Switches With an auxiliary tank fuel flow control switch in ENGINE FEED position the boost pumps in the corresponding auxiliary tank supply fuel to the main manifold 19 Wing Tank Warning Light Wing tank warning light on the fuel system panel is provided to warn the crew that fuel is being used from the external or outboard wing tanks out of sequence 34 Main Mainfold Interconnect Valves Switch A main mainfold interconnect valves switch on the fuel system panel lias unmarked OPEN CLOSED positions This rotary switch controls the operation of main manifold interconnect valves When the white stripe on the switch is aligned with the flow line on the panel the switch is OPEN and left TR power is supplied to open valve Opening these valves interconnects the right and left sides of the main manifold CLOSED position closes the two valves 2010 Captain Sim www captainsim com B 52 Driver FLIGHT MANUAL Part II Aircraft and Systems 24 DO NOT USE FOR FLIGHT 39 TOTAL FUEL FLOW INDICATOR This instrument uses 115 volL ac power to electrically add the flow rates indicated on the eight individual fuel flowmeters The totalizer indication is accurate within 3 When all engines are operating 40 LANDING GEAR LEVER A landing gear lever is located on the pilots instrument panel ahead of the aisle stand Positions of the l
32. lip indications In addition it provides glide slope and localizer information in that it shows the aircraft position above or below the glide slope and whether the aircraft has the correct bank angle and rate of turn to intercept and maintain a heading or course 3 Course Warning Flag A course warning will come into view during TACAN VOR ILS or ILS APP mode of operation when the NAV1 fails or signals from the URN 3 beacon or the VOR or ILS stations are lost or become unreliable 4 Pitch Steering Bar A pitch steering bar will indicate whether the aircraft has the proper pitch to intercept the glide slope correctly The bar will operate in ILS APP mode only When not in operation and normal power is available the pitch steering bar will be out of view 6 Bank Steering Bar A bank steering bar will indicate whether the aircraft has the correct bank angle and rate of turn to intercept the localizer beam on course if the NAV1 is tuned to an ILS frequency 8 Pitch Trim Knob A pitch trim knob permits zeroing the horizon line with reference to the miniature aircraft 10 Turn and Slip Indicator Indications of aircraft rate of turn and slip are provided by the needle and ball arrangement at the bottom center of the instrument 11 OFF Flag An OFF flag will appear upon interruption of power to the attitude indicating system 13 Glide Slope Warning Flag A glide slope warning flag will come into view during ILS or ILS APP mode of op
33. ndable strength 2010 Captain Sim www captainsim com 14 DO NOT USE FOR FLIGHT 3 Heading Marker Indicates a desired heading The heading marker will rotate with the compass card after the desired heading has been selected by the heading set knob 4 Lubber Line and 5 Compass Card Provide an indication of aircraft heading 7 Course Selector Window Gives a digital display of the desired course selected by the course set knob 9 14 Course Arrow Indicates the desired course selected by the course set knob during ILS ILS APP VOR and TACAN modes The course arrow will rotate in step with the compass card 10 To From Indicator Indicates whether the selected course if intercepted and flown will take the aircraft to the selected facility or vice versa 11 Course Deviation Indicator referenced to the course arrow that indicates whether the aircraft is left or right of the desired course or perpendicular to the course arrow represent of course deviation and 1 4 of the localizer width The deviation indicator provides information relative to the localizer beam when the nav mode select switch is in ILS or ILS APP and the NAV1 is on and tuned to an ILS frequency For all other conditions the course deviation indicator provides information relative to the desired course provided NAV1 radio is tuned to the respective surface beacon or omni range station 12 Course Set Knob Used to set the course arrow and the digital display in
34. pearance of DWN indicates a gear down and locked 25 LOW OIL PRESSURE WARNING LIGHTS Low engine oil pressure is indicated by eight amber low oil pressure warning lights located over each oil pressure gage on the eyebrow instrument panel A pressure switch is installed on each engine that will illuminate the light when a decreasing oil pressure reaches 37 2 psi and extinguish the light when an increasing oil pressure reaches 37 2 psi These lights will complement the oil pressure indicating system to provide a cross check to establish if a malfunction is occurring in the oil pressure indicating system or in the engine 27 ACCELEROMETER An accelerometer is located on the pilots eyebrow panel The accelerometer is a self contained unit requiring no external n n connections The dial is calibrated in g units from 2 to 44 g s 2010 Captain Sim www captainsim com B 52 Driver FLIGHT MANUAL Part II Aircraft and Systems 21 DO NOT USE FOR FLIGHT 29 MAGNETIC STANDBY COMPASS A pilot s magnetic standby compass is located on the eyebrow instrument panel between the oil pressure gages 30 EXHAUST GAS TEMPERATURE GAGE 31 FUEL FLOWMETERS Exhaust gas temperature of each engine is indicated by eight gages on the pilots instrument panel These gages are calibrated in degrees centigrade and indicate the temperature of the exhaust gases of each engine Engine thermocouples supply power to op
35. r are steered by movement of the rear drum of the coordinating unit The rear drum can be moved both by the jackscrew for crosswind crab and by the forward drum of the coordinating unit for steering by the rudder pedals This action allows steering of the forward gear even when the forward gear are preset for crosswind crab P22 CROSSWIND CRAB CONTROL CENTERING BUTION A crosswind crab centering button located to the right of the crosswind crab control knob on the aisle stand is used to center all four main landing gear from a turned position to neutral The crosswind crab centering button controls an electric motor which turns the jackscrew in the coordinating unit in the desired direction to center all four gear When the left rear gear is centered power to the motor is interrupted causing all centering action to stop The centering button a push type switch that is spring loaded to OFF position is supplied TR power It is covered with a moisture and dust proof rubber cap which must be pressed to actuate the centering button 41 CROSSWIND CRAB POSITION INDICATOR The indicator is centrally located on the lower part of the pilots instrument panel and shows in a relative plan view presentation the amount in degrees that the landing gear is turned to compensate for aircraft crab during crosswind conditions The indicator has a diagram marked with a miniature runway and a scale calibrated from 0 to 20 both right and left
36. removed from the other circuits provided through the switch 2010 Captain Sim www captainsim com B 52 Driver FLIGHT MANUAL Part II Aircraft and Systems 12 DO NOT USE FOR FLIGHT 3 CLOCK 1 2 3 1 Winding Knob 2 3 Hands 4 FLIGHT COMMAND INDICATOR The AN ASQ 38 V BNS flight command indicator FCI located on the pilots instrument panel provides localizer information 5 ALTIMETER 1 100 Foot Pointer 2 Barometric Scale 3 100 Foot Drum 4 Barometric Pressure Set Knob 5 1000 Foot Counter 6 10 000 Foot Counter A type AAU 19 A altimeters on the pilot s and copilot s instrument panels The altimeter has a counter drum pointer display Tne counters and drum provide a direct digital readout in hundreds and thousands of feet The single pointer repeats the 100 foot indications of the drum serving both as a vernier for the drum and as a quick indication of the rate and direction of altitude change A barometric pressure set knob and barometric scale are provided for adjusting the altimeter setting 2010 Captain Sim www captainsim com B 52 Driver FLIGHT MANUAL Part II Aircraft and Systems 13 DO NOT USE FOR FLIGHT 8 MARKER BEACON LIGHT TEST SWITCH Marker beacon indicator lights are tested by pushing the central caution panel test switch 9 INDICATED AIRSPEED INDICATOR 1 Maximum Allowable Airspeed Indicator 2 Indicated Airspeed Pointer Located at both the left and right sides o
37. the course selector window to the desired course When the nav mode select switch is in VOR position and the NAV1 is tuned to an ILS frequency the course set knob will have no functional effect on the course deviation indicator however the course deviation indicator will rotate in conjunction with the course set knob 13 Heading Set Knob Is used to set the heading marker to the desired heading 17 Bearing Pointer head A Bearing Pointer indicates the bearing heading to VOR station 11 MARKER BEACON LIGHT The marker beacon indicator light is used as a navigational and landing aid The light is located just above the respective pilot s horizontal situation indicator 2010 Captain Sim www captainsim com D ET ANriuear T LIT MANIIIAI Dart TT Airrraft and Chretnme B 52 Driver FLIGHI MANUAL Part 11 Aircraft and Systems 15 DO NOT USE FOR FLIGHT Glide Slope Indicator Attitude Sphere Course Warning Flag Pitch Steering Bar Bank Steering Bar Shield Bank Steering Bar Bank Scale Pitch Trim Knob Bank Pointer 12 10 Turn And Slip Indicator 6 11 OFF Flag 7 12 Miniature Aircraft 13 Glide Slope Warning Flag 14 Glide Slope Indicator 15 Glide Slope Deviation Scale OO l O 1 Q N 11 9 10 An ARU 49 A attitude director indicator located on both the pilot s and copilot s instrument panel provides an indication of aircraft pitch and roll attitudes and rate of turn and s
38. witch 1 4 Ammeter Provides indication of output in amperes supplied by each individual generator The ammeters indicate from 0 to 500 amperes 6 Frequency Meter A frequency meter provides a means of reading individual frequencies of the generators and central bus tie 7 8 10 11 Generator Switch Generator switches on the copilot s ac control panel are marked ON and OFF When the switch is held momentarily in ON position 28 volt nominal dc essential power closes the generator control relay and the generator circuit breaker and energizes the generator field 9 Main External Power Switch Main external power switch on the ac control panel is marked ON and OFF The switch is provided for controlling the main external power system 2010 Captain Sim www captainsim com B 52 Driver FLIGHT MANUAL Part II Aircraft and Systems 41 DO NOT USE FOR FLIGHT 12 15 Generator Circuit Breaker Position Indicator and 16 19 Bus Tie Circuit Breaker Position Indicator Eight tab indicators one for each generator circuit breaker and one for each bus tie circuit breaker are located on the ac control panel and provide a means of indicating the position of the respective circuit breakers 24 27 Generator Drive Decoupler Switch The switches are marked NORM and i ECPI at the extreme positions and MON at the center position 28 Frequency And Voltmeter Selector Switch A five position frequency and voltage selector switch has ENG GEN ENG 3
39. witch on the autopilot selector panel has ON OFF positions ON position puts power to the servo control drive motor and permits ready engagement of the servos OFF position cuts off power to the servo control drive motor and also disengages the autopilot 3 Altitude Control Switch Ctr Z An altitude control switch has ON OFF positions In ON position the elevator servo is controlled by a barometric pressure control unit Rotating the pitch knob drops the altitude control switch to OFF and deactivates altitude control operation Moving the glide slope switch to ON will drop the altitude control switch to OFF position The altitude control switch will remain locked in OFF as long as the glide slope switch is in ON position 4 Automatic Approach Localizer Switch Dummy on this panel See description of ILS position of Nav Mode Select Switch for details 5 Automatic Approach Glide Slope Switch Dummy on this panel See description ILS APP positions Nav Mode Select Switch for details WWW captainsim com 47 DO NOT USE FOR FLIGHT P18 NAVIGATION SYSTEM SELECT PANEL 1 T 1 Nav Mode Select Switch 2 Heading Selector Switch 1 Nav Mode Selector Switch Nav mode select switch marked Mode Select is located on the navigation system select panel The rotary switch has TACAN VOR ILS ILS APP positions e In TACAN position the bank steering bar will respond to the MSFS flight plan if loaded Ctrl Shift should be assigned

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