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`707 Captain` FLIGHT MANUAL Part III – Operations

1. 1 Sim www captainsim com 707 Captain FLIGHT MANUAL Part III Operations DO NOT USE FOR FLIGHT FLIGHT PATTERNS NORMAL TAKEOFF FLAP SPEED SCHEDULE Minimum Maneuvering Speed for 30 Bank Best Angle of Climb V2 70 Kts Retract flaps on Enroute Climb 300 Kt or as flap speed schedule directed Set climb thrust 2 Va 10 kts NOTE Limit Bank to 15 until this speed attained a d Ec y Complete AFTER TAKEOFF checklist mo San Close In Turn Maintain p e Flaps 14 eva 10 kts Best angle or Maximum bank 30 enroute climb Set takeoff thrust VR Positive rate Altitude selected Straight Climbout prior to 80 Kts Rotate smoothly of climb for flap retraction Accelerate Gear up 400 ft FAA V2 30 kts minimum Monitor airspeed ini Retract flaps minimum Set climb thrust Complete AFTER TAKEOFF checklist 2010 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part III Operations 53 DO NOT USE FOR FLIGHT NOISE ABATEMENT TAKEOFF e Accelerate to 250 kts Complete AFTER TAKEOFF checklist M Say Lower nose to maintain 500 1000 FPM climb Set climb thrust Retract flaps At V5 30 kts 3000 ft Climb at best angie V2 70 knots Accelerate to 250 kts Sa Complete AFTER TAKEOFF checklist 1000 ft Pa NOTE No noise abatement climb z required if an emergency Close in t
2. All Boost Pumps ON Crossfeed Selectors 1 amp 4 OPEN Crossfeed Selectors 2 amp 3 CLOSE M Center tank fuel exceeds 20 000 Ibs 9 000 kgs and inflight weight does not ex ceed alternate max inflight weight flaps up Until 12 000 Ib 5 400 kg 16 000 Ib 7 300 kg to tal fuel burned 14 000 Ib 6 400 kg recommended All Main Tank Boost Pumps ON if Center tank fuel other ee T rd than payload fuel does not Crossfeed Selectors 1 3 amp 4 CLOSE exceed 20 000 Ibs 9 000 kgs and inflight weight less than reight lem 1 Until 12 000 Ib 5 400 kg 17 000 Ib 7 700 kg total ENES fuel burned 14 000 1b 6 400 kg recommended E Crossfeed Selectors 1 2 3 amp 4 OPEN E Main Tank Boost Pumps 2 amp 3 ON ordre iden Main Tank Boost Pumps 1 amp 4 OFF uta 1 gt Ctr Tank Boost Pumps ON Until Ctr tank empty other than payload fuel Main Tank Boost Pumps 2 amp 3 ON Main Tank Boost Pumps 1 amp 4 OFF Ctr Tank Boost Pumps OFF Crossfeed Selectors 1 2 3 amp 4 OPEN Until Main Tanks 2 amp 3 equal tanks 1 amp 4 plus Reserve Tanks 1 amp 4 and Gr Wt below 288 000 Ib 130 600 kg 283 000 15 128 400 kg C Model All Main Tank Boost Pumps ON Ctr Tank Boost Pumps OFF Crossfeed Selector 2 OPEN Crossfeed Selectors 1 3 amp 4 CLOSE Reserve Tank Transfer Selectors OPEN If Desired When tanks 1
3. DO NOT USE FOR FLIGHT FL VAS II TATAMIL PART III Normal Procedures www captainsim com DO NOT USE FOR FLIGHT ABOUT THIS MANUAL VERSION 19 OCTOBER 2010 WARNING THIS MANUAL IS DESIGNED FOR MICROSOFT FSX USE ONLY DO NOT USE FOR FLIGHT 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 Systems e Part III Normal Procedures this document 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 707 300 FLIGHT MANUAL Page 5 NORMAL CHECKLIST 5 BEFORE START 5 CLEARED FOR START 5 AFTER START 5 BEFORE TAKEOFF 6 CLEARED FOR TAKEOFF 6 AFTER TAKEOFF 6 AFTER LANDING 6 SHUTDOWN 6 TERMINATING FLIGHT NORMAL PROCEDURES GENERAL INFORMATION 7 SCAN FLOW PATTERNS L10 NORMAL PROCEDURES PREFLIGHT Sd 10 GENERAL 10 EXTERIOR SAFETY INSPECTION 10 COCKPIT SAFETY INSPECTION 11 PRELIMINARY COCKPIT PREPARATION 17 COCKPIT PREPARATION FLIGHT ENGINEER 18 COCKPIT PREPARATION CAPTAIN 20 COCKPIT PREPARATION FIRST OFFICER 21 COCKPIT PREPARATION NAVIGATOR 22 AMPLIFIED BEFORE START CHECKLIST 23 ENGINE START PROCEDURE 24 AFTER START PROCEDURE 25 AMP
4. Essential Power Source Selector EXT PWR Check essential power failure warning lights extinguish Air Conditioning Units ON OFF Essential Radio Bus 1 amp 2 ON PILOTS STATION Panel Lights TEST Check all panel lights can be adjusted to desired intensity Manual Trim Wheel TRIM MANUALLY IN BOTH DIRECTIONS Spoiler Switches GUARDS CLOSED Fire Warning TEST Engine Fire Switches IN Transfer Switches NORM Engine Fire Test Switch PRESS Check engine fire warning and W WELL FIRE warning lights illuminate Engine Fire Test Switch RELEASE Check engine fire warning and W WELL FIRE warning lights extinguish Engine Start Control Selectors OFF Wing Anti Ice Switch OFF 2010 Captain Sim www captainsim com DO NOT USE FOR FLIGHT Ground Start Switch GUARD CLOSED Passenger amp Personnel Accomodations Oxygen Switch NORM Seat Belts Switches ON Check chime sounds when seat belt switch positioned to ON Emergency Exit Lights TEST amp OFF Emergency Exit Lights Switch ON Window Heat TEST amp LOW OFF Window Heat Switches LOW Overheat Lights PRESS Check OVERHEAT lights illuminate Window Heat Switches OFF Check OVERHEAT lights extinguish Window Heat Switches if Required for Defogging LOW Probe Heaters TEST amp OFF Probe Heater Switches ON Check HEAT ON lights illuminate Probe Heater Switches OFF Check HEAT ON lights extinguish Wing and Navigation Light Switches ON Pneumatic
5. reading and responding in a normal voice those items accomplished by himself On a through flight the checklist will be read down to the line On a terminating flight complete the checklist Electrical EXTERNAL POWER ON F E Seat Belts Switch OFF F E Beacon OFF F O Exterior lights REQUIRED F O Check all exterior limits not required OFF Start levers CUTOFF C Parking Brakes RELEASED SET C Fuel Boost Pumps OFF F E AC Aux Pumps OFF F E Air Cond Units OFF F E Shutdown Checklist Through Flight COMPLETE F E 2010 Captain Sim www captainsim com DO NOT USE FOR FLIGHT INS Emergency Exit Lights Ext Power Battery Oxygen Regulators Oxygen Valve Shutdown Checklist Terminating Flight OFF OFF ON OFF ON OFF OFF 100 CLOSED COMPLETE 48 F O F O F E F E ALL F E F E www captainsim com T Normal Procediirec Normal Procedures 49 DO NOT USE FOR FLIGHT PERFORMANCE TABLES AKEOFF SPEEDS TEMPERATURE RANGE C 104 54to 21 20to 2 3to 29 54 to 20 to 0 1to 30 31 to 33 54to 40 39to 21 20 to Oto 13 14to 37 54to 10 9t0 0 1to 15to 38 39to 41 54to 6 7to 1
6. reduce 10 000 Feet airspeed IFR and VFR 1000 ft above initial 1000 Feet Above Initial approach altitude IFR First positive INWARD Localizer Alive motion of localizer bar Feet Altimeters And Instruments Crosschecked 1000 500 Feet Above Field ield elevation altimeter Itimeters and Instruments instrument and flag rosschecked rosscheck IFR VFR After 500 ft above field levation IFR and VFR deviations from program med airspeed descent and Reaching Decision Height Minimums IDH IFR approach strobe centerline lights in sight runway or no runway in sight Reaching Minimum Descent Minimums approach strobe centerline lights in sight runway in Reaching Missed Approach Point MAP IFR approach strobe centerline lights in sight runway or no runway in sight CHART I www captainsim com DO NOT USE FOR FLIGHT Category II And IIIA Callouts PF Pilot Flying PNF Pilot Not Flying STANDARD CALLOUTS CONDITION LOCATION CALLOUT Look PF calls based Left Right Ahead upon airplane drift angle PNF starts looking for visual FINAL APPROACH Indivudual SequencePNF Strobe Flasher Lights Visible Individual Approach PNF Approach Light Bars Visible ecision Bar 1000 PNF White Bar from threshold isible ermination Bar If PNF Red Bar installed hreshold Lights PNF Threshold F At DH Visual P Contact reference established i e PNF calling app
7. Auxiliary Pump No 2 Switch ON Check LOW PRESS light extinguishes Engine Pump No 3 Switch OFF Check LOW PRESS light illuminates and utility system pressure indicates 2800 3100 psiat idle thrust Engine Pump No 2 Switch OFF Check LOW PRESS light illuminates and utility pressure decreases indicating interconnect valve closed Engine Pump No 3 Switch ON Check LOW PRESS light extinguishes and utility system pressure indicates 2800 3100 psi at idle thrust Engine Pump No 2 Switch ON Check LOW PRESS light extinguishes Interconnect Valve Switch OFF Check utility brake and rudder pressure indicate 2800 3100 psi Air Compressor 2 3 and 4 Indications CHECK Check air compressor tachometers stabilized and LOW OIL PRESS lights extinguished Air Conditioning Unit Switches ON Doors CLOSED Check all door annunciator lights extinguished Ground Equipment DISCONNECT Request ground crew to remove all ground equipment Check external power CONNECTED light extinguishes when external power is disconnected 2010 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part III Normal Procedures 25 DO NOT USE FOR FLIGHT AMPLIFIED AFTER START CHECKLIST Prior to taxi and on the Captain s command the First Officer will read aloud each challenge and receive the appropriate response from the designated crew member Ground Equipment CLEAR C Observe ground equipment clear or receive signal from ground crew tha
8. Brake CHECK Check pneumatic brake handle safe tied Thrust Reverser Operating Lights EXTINGUISHED Engine Instruments CHECK Check EPR indicators 1 0 and bugs move freely N1 RPM indicators zero EGT indicators normal Fuel flow indicators minimum indication Landing Gear Lights TEST amp SET Check Landing GEAR warning light extinguished Landing gear DOOR warning light extinguished doors closed or illuminated doors open Landing GEAR down lights illuminated Flap Lever amp Indicators IN AGREEMENT Total Air Temperature Indicator CHECK Check TAT OFF flag not in view Static Air Temperature Indicator CHECK Check warning flag retracted and indication approximately ambient temperature or greater www captainsim com DO NOT USE FOR FLIGHT Flight Engineer s Station Panel Lights TEST amp SET AC Paralleling Selector ANY GEN Check synchronization lights illuminate Essential Power Failure Warning Lights TEST Rotate essential power source selector to any GEN position and check both essential power FAILURE lights illuminated Rotate selector back to EXT PWR position and check lights extinguished DC Load amp Volts Selector TEST Select TR No 3 2 and ESS TR and check 2 28v DC and equal load indication on DC meters at 3 amp 2 positions Leave selector in ESS TR position Galley Power Switch ON AC Electrical System CHECK Check Generator drive disconnect switch guards closed amp safetied Generator
9. Flaps 25 Flight Director HDG Adjust engine thrust as Monitor forward engine et 10 pitch up with PITCHrequired Position flap lever instrument panel o 25 and monitor retraction UP and check for normal gear retraction Position flap lever to 14 Monitor flap and leading edge device retraction If directed set climb EPR Reduce to that required for missed approach pattern or limb If climb call for F E o set climb EPR EE a procedures all for AFTER TAKEOFF hecklist 1 Sim www captainsim com ptain FLIGHT MANUAL Part III Normal Procedures 44 DO NOT USE FOR FLIGHT LANDING ROLL PROCEDURE After touchdown and during landing roll the following tasks are accomplished during normal deceleration PILOT FLYING PILOT NOT FLYING FLIGHT ENGINEER ten nm Speed Brake Lever FULL UP and call SPEEDBRAKES UP If speedbrake lever not UP call SPEEDBRAKES Brakes APPLY Keep wings level Reverse Thrust ACTIVATE Rapidly raise reverse thrust spring detent CAUTION Exercise caution in use of reverse thrust The application of reverse hrust produces a nose up pitching moment herefore before reverse hrust actuation the nose heel should be lowering onto the runway through application of braking and nose down elevator At approximately 80 knots Hold forward pressure on start moving reverse thrust the control column levers forward and continue Keep wings level lever motio
10. Hebr DE ATGUHD FT Teie Fuel System SET FOR START If inflight flaps up weight will not exceed normal max inflight weight flaps up and center tank fuel other than payload fuel is less than 20 000 Ib 9000 kg or empty N iin Tank Boost Pumps 1 ON PER TANK Position one boost pump switch ON in tanks No 1 3 amp k Check No 2 ON Check associated LOW PRESSURE lights extinguished Crossfeed Selectors No 1 3 amp 4 CLOSE Check VALVE POSITION lights illuminate then extinguish Check crossfeed selector No 2 open If inflight flaps up weight will not exceed alternate max inflight weight flaps up and center tank fuel other than payload fuel exceeds 20 000 Ib 9000 kg Tank No 2 amp 3 amp Center Tank Boost Pumps 1 ON PER TANK Position one boost pump switch ON in tanks No 3 amp center Check No 2 ON Crossfeed Selectors No 2 amp 3 CLOSE Check VALVE POSITION lights illuminate then extinguish Check crossfeed selector No 1 amp k open When cleared for engine start Galley Power Switch OFF Air Conditioning Unit Switches OFF 2010 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part III Normal Procedures 18 DO NOT USE FOR FLIGHT ICOCKPIT PREPARATION CAPTAIN Life Vest STOWED Seat amp Rudder Pedals ADJUST Sun Visors STOWED Audio Selector Panel SET Oxygen amp Interphone TEST ON 100 Conduct oxygen check as described in Preliminary Cockpit Preparation Capta
11. Sim www captainsim com DO NOT USE FOR FLIGHT Altimeter CHECK amp SET Check warning flag retracted Current Barometric Pressure SET Check altitude comparable with field elevation Mode Switch CADC Check STDBY flag retracted and altitude comparable with previous value Radio Altimeter CHECK Check warning flag retracted and pointer at zero Clock WIND amp SET Turn amp Slip Indicator CHECK Check warning flag retracted HSI CHECK amp SET Set heading pointer and desired course for departure RMI CHECK amp SET Check warning flag retracted compass system synchronized and all compass headings comparable o Stow standby compass NOTE The standby magnetic compass is calibrated with landing gear lever lock solenoid energized inflight configuration so it is possible that discrepancies of 3 8 may exist on the ground Set ADF VOR switch as desired Vertical Speed Indicator CHECK Check pointer at zero INS RADIO Switch RADIO True Airspeed Indicator CHECK Check warning flag retracted Standby Altimeter SET Set current barometric pressure and cross check with field elevation Standby Horizon CHECK amp SET Check warning flag retracted gyro erect and airplane symbol properly positioned Weather Radar STANDBY Radar Indicator SET Range Marks SET AS DESIRED Speed Brake Lever FULL FORWARD Engine Controls SET FOR START Check reverse thrust levers full down thrust levers closed and engine start levers CUTOFF Pa
12. altitude Anti Ice OFF ON Check anti ice OFF or ON as required Descent INITIATE Coolant Air Valves 19 000 Feet OPEN Position inlet and exit valve switches to OPEN Open exit valve first then inlet in increments Check indicators move to full OPEN position Circuit Breakers CHECK Seat Belts Switch ON Landing Lights ON For collision avoidance turn ON the turn off lights when descending through 10 000 feet Altimeters SET amp CROSS CHECK When descending through transition altitude each pilot sets current altimeter setting and cross checks altimeter readings F E sets barometric correction indicator and cabin altimeter to altimeter setting of destination airport QNH www captainsim com 38 DO NOT USE FOR FLIGHT Radio Altimeter SET Set minimum decision altitude Flight Director If Required SET FOR DESCENT Autopilot If Desired SET FOR DESCENT Position mode selector to HDG or VOR LOC as desired and position altitude hold switch OFF Set heading pointer to desired heading Pitch control may be maintained using the pitch controller Check airplane tracks selected heading or radial and pitch angle Landing Data Card COMPLETE The F E will obtain compute and record the following data on the Landing Data Card Temperature elevation and QNH at destination airport plus gross weight and fuel He then extracts the Vpjgp and go around EPR from the QRH or performance chapter enters these plus the bug speed landing fla
13. each challenge and verify that the appropriate action has been accomplished If any action has not been accomplished he will read aloud the challenge to the designated crew member and after the action has been completed receive the correct response After all actions have been completed and verified the Flight Engineer will announce to the captain After Landing Checklist complete Anti Ice OFF ON F O Engine Start Control Selectors OFF F E Window Heat LOW OFF F O Window heat may remain in LOW if through flight is planned Probe Heat OFF F O Flaps UP NO LIGHTS F O Check flap indicator zero and LE FLAPS lights extinguished Speedbrake Lever FULL FORWARD C Radar amp Transponder STDBY OFF F O Galley Power OFF F E Fuel 1 PUMP ENGINE F E Check one boost pump is on in each main tank which is supplying fuel to an operating engine Hydraulics PRESS amp QTY NORMAL F E Outflow Valves OPEN F E After Landing Checklist COMPLETE F E PARKING PROCEDURE Allow the airplane to roll straight ahead a few feet before stopping following a turn to relieve torsional stresses in the main landing gear structure Parking Brake SET Check parking brake warning light illuminates Air Conditioning Units OFF Air Compressors STOP Anti ice OFF Check that the anti ice is OFF before engine shutdown Engine Start Levers 1 2 4 CUTOFF INS AS REQUIRED On terminating flights place INS mode switch to OFF On through flights INS may be left in NAV mode if G
14. 10 Captain Sim www captainsim com
15. 4 15to 38to 45 1000 54to 13 14to 33 34 to 43 to 47 54to 32 33to 37 38to 47 to 49 1000 54 to 37 38to 42 43 to 50 to 51 u TOGW i LBx1000 Vi Vr V2 Vi Vr V2 Vi Vr V2 Vi Vr V2 vi vr v2 Vi Vr V2 148 154 168 1150 155 168 146 152 167 148 153 167 I 145 150 165 1146 151 165 149 153 165 SPEEDS ARE 143 149 164 145 150 164 1147 151 164 KNOTS IAS 143 148 163 145 150 163 162 147 162 144 148 161 i 140 145 160 142 146 160 138 144 159 141 145 159 137 143 158 139 144 157 142 145 157 3 141 156 137 142 156 140 143 156 136 140 155 138 142 155 138 154 134 139 154 137 133 137 152 135 138 140 152 136 138 150 134 137 149 132 135 148 130 134 146 132 135 125 129 145126 130 145 128 132 145 131 133 123 127 144 125 129 144 127 130 143 129 132 121 125 142 123 127 142 125 128 1421127 130 120 123 141 121 125 141 123 127 141 126 128 118 122 139 120 123 139 122 125 139 124 126 120 138 118 121 138 120 123 138 122 125 118 137 116 119 136 118 121 136 120 123 116 135 118 121 116 119 112 116 132 114 117 114 130 112 115 110 113 108 111 106 109 125 107 124 170 165 amp Below 12 121 120 e Add 1 kt for each 20 kt of headwind Subtract 1 kt for each 2Yr kt of tailwind e Shaded areas show performance affected by minimum control speed If antiskid is inoperative see Performance General section Omit wind and slope corrections when V1 falls in shaded area e When V1 is shaded
16. Air Switch GUARD CLOSED Coolant Air System CHECK Valve Selector INLET Check LH AND RH valves indicate full open Valve Selector EXIT Check LH and RH valves indicate full closed Valve Selector SEC HEAT EXCH Check LH and RH valves indicate full open Valve Selector TURBOFAN EXIT Check LH and RH valves indicate full open Valve Selector TEMP CONTROL Check LH and RH valves indicate full closed modulating if A Cond on Turbofan Exit Valve Override L and R Switches NORMAL Main Cabin Heating Panels Switch AS REQUIRED NOTE Not normally required on ground unless outside temperatures are below freezing may be used as desired for passenger comfort Under these conditions surface covering temperatures are ther mostatically regulated to provide comfortable heat augmentation Gasper Air Fan Switch AS REQUIRED Cabin Temp Zone Control CHECK Check OVERHEAT light extinguished and valve indicators mid position valves closed Fuel Dump Door CLOSED Oxygen Pressure Indicators CHECK Verify bottles are serviced by reference to pressure temperature charts Oxygen amp Interphone TEST ON 100 Inspect mask hose and fittings for security grease or damage Hold mask away from face Oxygen Supply Lever ON Oxygen Diluter Lever 100 Emergency Oxygen Lever TEST MASK To clear mask Emergency Oxygen Lever NORMAL Oxygen Supply Lever OFF Adjust mask to face and inhale check mask pulls to face Oxygen Diluter Lever NO
17. Anti Ice OFF ON F O Check Anti ice OFF or ON as required Coolant Air Valves 19 000 feet OPEN F E Circuit Breakers CHECKED F E Sa ieee aie i aa 19 000 feet Complete the checklist after reaching final approach altitude Seat Belts Switch ON F E Landing Lights ON F O For collision avoidance check the fixed landing lights ON when descending through 10 000 feet EPR amp Airspeed Bugs SET C F O Altimeters SET amp X CHECKED ALL Check altimeters and barometric correction indicator set at current airport barometric pressure and altimeters in agreement Radio Altimeters SET C F O Set minimum decision altitude n Sim www captainsim com 40 DO NOT USE FOR FLIGHT Fit Dir Fit Inst amp Radios SET amp X CHECKED C F O Check flight directors flight instruments and radios set for approach and corresponding instruments in agreement Fuel SET FOR LANDING F E Check all main tank boost pump switches ON all main tank LOW PRESSURE lights extinguished system configured main tank to engine and fuel heater switches OFF Hydraulics PRESS amp QTY NORMAL F E Check utility and AC auxiliary pump switches ON all LOW PRESS lights extinguished and quantity normal Descent Approach Checklist COMPLETE F E www captainsim com 41 DO NOT USE FOR FLIGHT LANDING PROCEDURE Prior to and during the final approach accomplish the following tasks in sequence to properly c
18. Check fuel loading per tank in accord with manifest and appropriate boost pumps on for engine start Air Cond Units OFF Continue the checklist after receiving start clearance from the tower and ground personnel Galley Power OFF Start Pressure PSI Check air supply duct pressure indicator and announce the pressure INS Mode Selectors NAV Beacon ON Before Start Checklist COMPLETE ALL ALL F E F E C F O F O 2010 Captain Sim www captainsim com 707 Captain GHT MANU art III Normal Procedures 23 DO NOT USE FOR FLIGHT ENGINE START PROCEDURE The normal engine starting sequence is 3 4 2 1 heck decrease in duct pressure and announce Start Valve Open Announce N2 Rotating Oil pressure rising within 30 i Eo NH Position Engine Start Lever pec Announce 15 N2 o IDLE detent when 15 N2 RPM reported and N1 rotation observed heck fuel flow and EGT indication At 35 N2 command Release Engine Start all 35 N2 Release ontrol Selector at 35 N2 Check rapid increase in duct or on command Release pressure and announce or Starter Cutout Starter Cutout heck ENG LOW PRESS light extinguished heck oil pressure stabilizes ithin limits heck EGT stabilized and engine instruments for normal indications NOTE heck generator drive LOW Use same procedures for starting remaining engines PRESSURE light extinguished CAUTION Airplane Elect Power ADVANCING ENGINE START LEV
19. ER PREMATURELY CAN Establish After Starting AUSE A HOT START Engines 3 and 4 KEEP HAND ON ENGINE START LEVER WHILE AC Paralleling selector GEN OBSERVING RPM EGT AND FUEL FLOW UNTIL GEN 3 STABILIZED Check voltage and LEVER IN AN ATTEMPT TO RESTART ENGINE Check essential power FAILURE TO HOLD ENGINE START CONTROL SELECTOR FAILURE warning light IN GRD UNTIL STARTER CUTOUT RPM IS REACHED CANextinguished in both RESULT IN A HOT START DO NOT RE ENGAGE positions ENGINE START CONTROL SELECTOR UNTIL ENGINE SHEAR IF STARTER IS ENGAGED DURING COAST GEN 3 CLOSE DOWN Check generator breaker IRCUIT OPEN lights extinguished Sim www captainsim com 707 Captain FLIGHT MANUAL Part III Normal Procedures 24 DO NOT USE FOR FLIGHT AFTER START PROCEDURE Airplane Electrical Power ESTABLISH AC Paralleling Selector GEN 2 GEN 1 return to GEN 3 Check voltage and frequency in GEN 2 and GEN 1 positions Essential Power Selector GEN 2 GEN 1 return to GEN 3 Check Essential Power FAILURE warning light extinguished in GEN 2 and GEN 1 positions Generator Breaker Switches GEN 2 CLOSE GEN 1 CLOSE Check generator breaker CIRCUIT OPEN lights extinguish Air Compressor 2 3 and 4 Start Switches START Galley Power Switch ON Fuel Boost Pump Switches ON Position appropriate boost pump switches ON for fuel configuration and check associated LOW PRESSURE lights extinguish Hydraulic System CHECK AC
20. Flight Director SET FOR APPROACH Position mode selector from HDG to AUTO APP and check flight director V L and G S annunciators illuminate amber Check command bar directs flight on selected heading until localizer capture Engage altitude hold when appropriate Localizer CAPTURE AUTOPILOT At 2 dots displacement of course bar check airplane banks to align with localizer and autopilot V L annunciator illuminates green Check airplane tracks localizer Localizer CAPTURE FLIGHT DIRECTOR At 2 dots displacement of course bar check command bar directs a bank to align with localizer and flight director V L annunciator illuminates green Check comnand bars track localizer Glide Slope CAPTURE AUTOPILOT At glide slope capture check autopilot G S annunciator illuminates green and altitude hold switch trips OFF Check airplane tracks glide slope Glide Slope CAPTURE FLIGHT DIRECTOR Immediately prior to glide slope beam center check command bars direct a pitch down to track glide slope altitude hold switch trips OFF and flight director G S an nunciator illuminates green AMPLIFIED DESCENT APPROACH CHECKLIST When commanded by the Captain the Flight Engineer will read aloud each challenge and receive the appropriate response for the items accomplished by Captain and First Officer reading and responding in a normal voice those items accomplished by himself Pressurization SET F E Verify cabin altitude selector set for landing
21. K Check generator drive oil temperature rise indicators in green band and generator drive LOW PRESSURE CIRCUIT OPEN and essential power FAILURE warning lights extinguished Check KW loads on all 4 generators are approximately equal Fuel System SET FOR TAKEOFF CAUTION FUEL FROM TANKS TO BE USED FOR TAKEOFF MUST BE SAMPLED FOR A MINIMUM OF 4 MINUTES AT IDLE THRUST Recheck configuration for fuel load and gross weight Check fuel heater switches OFF and engine fuel temperatures decreasing or low readings Hydraulic System CHECK Check pressures and quantity normal pump LOW PRESS lights extinguished Equipment Cooling NO AIRFLOW Light EXTINGUISHED Air Conditioning and Pressurization Systems CHECK NOTE The airplane may be pressurized to a maximum of 125 psi positive cabin differential during takeoff and landing Check Duct temperature normal for conditions MAIN and CREW duct overheat lights extinguished Unit OVERHEAT and OFF lights extinguished Operating air compressors for RPM indication and LOW OIL PRESS light extinguished Temperature control valve posi tioned as required for existing conditions www captainsim com 707 Captain FLIGHT MANUAL Part III Normal Procedures 27 DO NOT USE FOR FLIGHT Check coolant air system valve selector in TEMP CONTROL and valve position indicator for appropriate indications Takeoff Briefing CONDUCT Pilot making takeoff will brief other pilot and Flight Engineer to monit
22. LIFIED AFTER START CHECKLIST P25 TAXI OUT AND TAKEOFF SCs 25 TAXI OUT PROCEDURE 27 AMPLIFIED BEFORE TAKEOFF CHECKLIST 29 TAKEOFF PROCEDURE 30 REJECTED TAKEOFF PROCEDURE 31 ENGINE FIRE FAILURE AFTER V1 32 AFTER TAKEOFF PROCEDURE 33 AMPLIFIED AFTER TAKEOFF CHECKLIST 34 CLIMB PROCEDURE CRUISE PROCEDURE DESCENT APPROACH PROCEDURE 39 AMPLIFIED DESCENT APPROACH CHECKLIST 41 LANDING PROCEDURE 42 AMPLIFIED LANDING CHECKLIST 43 GO AROUND PROCEDURE 44 LANDING ROLL PROCEDURE www captainsim com DO NOT USE FOR FLIGHT 45 TAXI IN AND PARK 45 AFTER LANDING PROCEDURE 46 AMPLIFIED AFTER LANDING CHECKLIST 46 PARKING PROCEDURE 47 AMPLIFIED SHUTDOWN CHECKLIST 49 PERFORMANCE TABLES 49 TAKEOFF SPEEDS 50 CRITICAL SPEEDS 51 FLIGHT PATTERNS 51 NORMAL TAKEOFF 52 NOISE ABATEMENT TAKEOFF 53 TAKEOFF ENGINE FIRE FAILURE AFTER V1 54 NORMAL OR ONE ENGINE INOPERATIVE VOR APPROACH 55 NORMAL OR ONE ENGINE INOPERATIVE ILS APPROACH 56 ILS AUTOPILOT 57 NORMAL OR ONE ENGINE INOPERATIVE LANDING 58 CUSTOMER SUPPORT www captainsim com 707 Captain FLIGHT MANUAL Part III Normal Procedures DO NOT USE FOR FLIGHT NORMAL CHECKLIST BEFORE START Cockpit Preparation COMPLETE ALL Interphone CHECKED ON amp ALL Emergency Flaps OFF C Anti Skid CHECKED amp ON Rudder amp Spoiler Switches ON C Emergency Exit Lights ARMED C Seat Belts Switches ON F O INS CHECKED amp SET CrF O Radio A
23. M Autopilot engage switch Engaged CAUTION Do not use Auto pilot for LS approach if radio altimeter warning flag in view Localizer q NOTE Rearm at 1500 ft if glide Capture at Fix LOM MKR DME slope capture was greater 2 dots K Verify crossing altitude than 1500 ft above field Glide slope j 7 elevation if not equipped armed l Xx q with a radio altimeter Heading bug b vase Missed Approach ing i APD Annunciator er Switch V L green a e G S amber Fly manually Glide slope Capture Altitude hold trips off automatically Autopilot starts descent Glide slope atten uation starts APD annunciator V L green G S green If the glide slope flag will appear the MM Middle Marker glide slope signal fails the bar will center and the autopilot will indicate glide slope capture and start a descent w A S 2010 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part III Operations 58 DO NOT USE FOR FLIGHT NORMAL OR ONE ENGINE INOPERATIVE LANDING APPROACH PREPARATIONS Turning Base Flaps 25 Flaps 14 Bug 30 kts V Start descent 300 500 fpm Bug 20 kts ug paid tomter APPROACH 25 bank r O checklist 309 maximum Gear down 9 gt e Missed Approach 9 uy sec 1500 ft Go around thrust and rotate to go around attitude EL Flaps 40 Flaps 25 Bug 10 k
24. NT PITCHING OF MAIN GEAR TRUCK AND INDUCES HEAVY LOADS ON TRUCK LEVELING SYSTEM IF BRAKE PEDALS HAVE BEEN ACTUATED INADVERTENTLY DURING GEAR RETRACTION MAINTENANCE INSPECTION MUST EE CARRIED OUT Flaps UP NO LIGHTS F E Check flaps retracted and LE FLAPS lights extinguished Hydraulics PRESS amp QTY NORMAL F E Check utility system and brake pressures 2800 psi after landing gear and flap retraction Air Cond amp Press CHECKED amp SET F E Check cabin altitude selection indicator set to planned cruise altitude plus 1500 to 2000 feet cabin rate of climb normal cabin air duct pressure in green band crew and main cabin temperature selectors in automatic range After Takeoff Checklist COMPLETE F E 2010 Captain Sim www captainsim com 34 DO NOT USE FOR FLIGHT CLIMB PROCEDURE Autopilot If Desired ENGAGE Radios SET FOR VOR NAVIGATION Tune radios to desired frequencies check warning flags retracted and identify stations Set course pointer as desired Autopilot If Desired SET FOR VOR NAVIGATION With autopilot engaged position mode selector to HDG and select desired heading When aircraft is on intercept heading rotate mode selector to LOC VOR and check autopilot V L light on approach progress display illuminates amber When airplane has captured selected radial observe autopilot V L light illuminates green Flight Director If Desired SET FOR NAVIGATION Check ADI and HSI warning flags retracted Positio
25. O 1 TANK ENG 1 ENG 2 ENG 3 ENG 4 Check temperature indication at each position Fuel Temperature Selector NO 1 TANK Fuel Heat Switches OFF Check fuel icing lights extinguished Hydraulic Systems TEST amp SET www captainsim com DO NOT USE FOR FLIGHT Hydraulic Reservoir Indicator FULL Ground Clearance for Hydraulic Pump Operation OBTAIN Engine 2 and 3 Pump Switches ON Hydraulic Fluid Shutoff Switches GUARDS CLOSED amp SAFE TIED Interconnect Valve Switch BRAKE AC Auxiliary Pump No 2 Switch ON Check AC auxiliary pump No 2 LOW PRESS light extinguished and AC auxiliary pump No 1 LOW PRESS and both engine driven pump LOW PRESS lights illuminated Rudder pressure at least 2800 psi RUDDER BOOST LOW PRESS light extinguished and hydraulic brake pressure at least 2800 psi Check utility hydraulic pressure remains at precharge Interconnect Valve Switch SYSTEM Check utility hydraulic pressure remains at precharge and hydraulic brake pressure at least 2800 psi Parking Brakes SET AC Auxiliary Pump No 2 Switch OFF AC Auxiliary Pump No 1 Switch ON Engine Vibration Monitor Systems TEST Pickup Selector DIFF Test Switch PRESS amp HOLD Check amplitude 4 0 0 5 mils on each indicator in each position of vibration filter selector Pickup Selector TURB Check amplitude 4 0 0 5 mils on each indicator in each position of vibration filter selector Test Switch RELEASE Engine Start Air P
26. P Reverse UP hrust applied symmetrically Apply maximum allowable all out any omitted action items reverse thrust on symmetric engines consistent with onditions ontinue maximum braking until certain the airplane will on the runway Field lenath permitting all 80 knots Monitor hydraulic brake and pressure indicators Initiate movement of the ommunicate the rejected takeoff reverse thrust levers forward decision to the control tower and at approximately 80 knots appropriate crew members as soon as practical At approximately normal taxi speed slowly move the reverse thrust levers to the full down position Observe REVERSER OPERATING Lights or proper indication hen the airplane is stopped perform procedures as required Review Brake Cooling Schedule for brake cooling time and precautions refer to Ops Man Ch 04 18 onsider the following he possibility of wheel fuse plugs melting the need to clear the runway the requirement for remote parking alerting fire equipment not setting parking brakes unless passenger evacuation is necessary advising the ground crew of the hot brake hazard advising passengers of the need to remain seated or evacuate and completion of the Emergency Abnormal checklist if appropriate for conditions which aused the RTO m www captainsim com tain FLIGHT MANUAL Part III mal Procedures 31 Fly the airplane Maintain directional control hen posit
27. RMAL Inhale and check unrestricted flow Oxygen Supply Lever ON Inhale and check flow indicator white Oxygen Diluter Lever 100 Inhale and check flow indicator white Emergency Oxygen Lever EMERGENCY Check flow indicator white and slight pressure in mask Emergency Oxygen Lever TEST MASK Check flow indicator white and increased pressure in mask Emergency Oxygen Lever NORMAL Oxygen Mask Interphone TEST Adjust headset over oxygen mask and place OXY BOOM switch to OXY Press radio intercom switch to 1C Speak into oxygen mask and check transmission Remove oxygen mask and stow Flight Recorder SET Emergency Equipment CHECK www captainsim com DO NOT USE FOR FLIGHT I www captainsim com 707 Captain FLIGHT MANUAL Part III Normal Procedures 17 DO NOT USE FOR FLIGHT COCKPIT PREPARATION FLIGHT ENGINEER Airplane Loading CHECK Check Fuel quantity agrees with flight plan fuel and is distributed properly Airplane gross weight agrees with flight plan weight Airplane CG within limits Takeoff Data Card PREPARE Using the airplane gross weight and center of gravity information current OAT pressure altitude runway slope and wind factor and appropriate charts compute the takeoff data Data will include EPR settings VI VR V2 stabilizer trim setting and fuel dump time The data will be entered on the takeoff data card and passed to the First Officer for verification of data HDINAL FE
28. TENT TO ALERT TAKEOFF WARNING SYSTEM 2010 Captain Sim www captainsim com 30 DO NOT USE FOR FLIGHT REJECTED TAKEOFF PROCEDURE The decision to reject a takeoff rests solely with the CAPTAIN The decision must be made so stopping action can begin by V1 If the Captain decides to reject the takeoff he she should clearly announce REJECT commence the stopping action and assume control of the airplane If the First Officer is making the takeoff he she should not abandon control of the airplane until the Captain makes a positive input to the controls Prior to 80 knots the takeoff should be rejected for system failure s unusual noise or vibration tire failure abnormally slow acceleration engine failure engine fire unsafe takeoff configuration warning or if the airplane is unsafe or unable to fly Above 80 knots reject for engine failure engine fire or if the airplane is unsafe or unable to fly During the takeoff the crewmember recognizing the malfunction calls it out clearly and precisely CAPTAIN FIRST OFFICER FLIGHT ENGINEER erify actions as follows Monitor engine instruments Advise Captain of any limits Simultaneously close the hrust levers closed Maximum brakes being approached or other hrust levers and apply applied Verify speedbrake lever UP abnormalities Verify imaximum wheel brakes and call SPEEDBRAKES UP If speedbrake lever UP speedbrake lever not UP call Speedbrake Lever FULL SPEEDBRAKES NOT U
29. amp 4 less than 12 000 Ibs 5 400 kg each and Gr Wt less than 288 000 1b 130 600 kg 283 000 Ib 128 400 kg C Model Reserve Tank Transfer Selectors CLOSE When drained Until Flight completed 2010 Captain Sim www captainsim com 37 DO NOT USE FOR FLIGHT CRUISE PROCEDURE Cruise Thrust SET When cruise altitude is reached allow airplane to accelerate slightly higher than cruise chart speed Cruise Thrust EPR SET Adjust cruise thrust according to gross weight as fuel is burned off to maintain charted speed schedule NOTE If indicated speed falls below charted value use up to maximum continuous thrust to recover charted speed Autopilot If Desired SET FOR DESIRED NAVIGATION Flight Director If Desired SET FOR DESIRED NAVIGATION Fuel Management MONITOR Accomplish fuel management according to fuel usage procedure Monitor fuel quantities at frequent intervals Compute total fuel and gross weight hourly and as required for navigation reports Operating Systems MONITOR Continue monitoring operating systems for normal indications Cabin Temperature Zone Control as desired ADJUST DESCENT APPROACH PROCEDURE Pressurization SET Move cabin altitude selection indicator to landing field elevation minus 200 to 250 feet Check cabin rate of descent normal Cabin Air Thrust Valve Switch NORMAL OFF Close cabin air thrust valves or adjust thrust levers to maintain the desired rate of change of
30. available runway length must be sufficient for highest TOGW in shaded area otherwise runway length is insufficient V1 CORRECTION Add 1 kt for each 1 9o upslope Subtract 1 kt for each Y 9o downslope e Add 1 kt for each 20 kt of headwind Subtract 1 kt for each 2 kt of tailwind n Sim www captainsim com DO NOT USE FOR FLIGHT 50 www captainsim com 1 FLIGHT MANUAL Part III Normal Procedures DO NOT USE FOR FLIGHT CRITICAL SPEEDS ae CRITICAL SPEEDS IAS 2 amp 3 ENG MINIMUM WEIGHT THRESH SPEED STALL SPEED KNOTS CLIMB CONTROL 1000 LB FLAPS FLAPS FULL ET SPEED SPEEDS 50 40 160 110 111 112 175 3 ENG 170 113 114 E D a gt 115 180 BOOST 180 116 118 93 95 97 100 119 186 190 119 121 96 97 99 103 123 191 ON OFF 200 122 124 98 99 102 106 126 196 210 125 127 101 102 105 109 130 201 2 ENG 128 130 103 105 108 112 133 206 BOOST 131 133 105 107 110 114 136 211 ON OFF 134 136 107 109 113 117 139 215 250 137 139 110 112 115 120 142 220 260 139 142 112 114 117 122 144 225 270 142 144 114 116 120 125 147 229 280 145 147 116 118 122 128 150 233 290 147 150 118 121 124 130 152 237 300 150 153 120 123 127 133 155 242 310 152 155 122 125 129 135 157 246 320 155 158 124 127 131 138 160 250 330 157 160 126 129 133 140 162 253 2010 Car
31. cklist REVIEWED BUGS SET ALL SET FOR T O F E ON F O BOTH F E ON F O COMPLETE F E AFTER TAKEOFF Anti Ice OFF ON F E Engine Start Control Selectors OFF ON F E Seat Belts Switches OFF ON F E Gear UP amp OFF F E Flaps UP NO LIGHTS F E Hydraulics PRESS amp QTY NORMAL F E Air Cond amp Press CHECKED amp SET F E Anti Ice Engine Start Control Selectors Window Heat Probe Heat Flaps Speedbrake Lever OFF ON F O OFF F E LOW OFF F O OFF F O UP NO LIGHTS F O FULL FORWARD C Radar amp Transponder STBY OFF F O Galley Power OFF F E Fuel 1 PUMP ENGINE F E Hydraulics PRESS amp QTY NORMAL F E Outflow Valves OPEN F E After Landing Checklist COMPLETE F E HUTDOWN Electrical EXTERNAL POWER ON F E Seat Belts Switch OFF F E Beacon OFF F O Exterior Lights AS REQUIRED F O Start Levers CUTOFF C Parking Brakes RELEASED SET C Fuel Boost Pumps OFF F E AC Aux Pumps OFF F E Air Cond Units OFF F E Shutdown Checklist Through Flight ERMINATING FLIGHT INS Emergency Exit Lights External Power Battery Oxygen Regulators Oxygen Valve Shutdown Checklist Terminating Flight COMPLETE F E OFF F O OFF F O ON OFF F E ON OFF F E OFF 10096 ALL CLOSED F E COMPLETE F E 2010 Captain Sim www captainsim com tain FLIGHT MANUAL Part III DO NOT USE FOR FLIGHT NORMAL PROCEDURES GENERAL INFORMATION SCAN FLOW PATTERNS Normal procedures are accomplished by recall Normal checklist
32. drive LOW PRESSURE lights illuminated Bus Tie breaker CIRCUIT OPEN lights extinguished KW KVAR meters zero Fuel System TEST amp SET Note initial fuel quantity indications Fuel Quantity Gages Test Switch PRESS amp HOLD Check each tank quantity indication decreases Fuel Quantity Gages Test Switch RELEASE Check all quantity indicators stabilize at original indications Check fuel totalizer quantity agrees with sum of fuel quantity indications All Forward Boost Pump Switches ON Check all forward LOW PRESSURE lights extinguish and all aft LOW PRESSURE lights remain illuminated Center Tank Left Boost Pump Switch ON Only when tank contains fuel Check center tank left LOW PRESSURE light extinguishes and right LOW PRESSURE light remains illuminated All Forward Boost Pump Switches OFF Center Tank Left Boost Pump Switch OFF Check all LOW PRESSURE lights illuminated Repeat procedure for all aft boost pumps and center tank right boost pump Tank No 2 Aft Boost Pump Switch ON All Crossfeed Selectors CLOSE Check VALVE POSITION lights illuminate momentarily then extinguish All Crossfeed Selectors OPEN Check VALVE POSITION lights illuminate momentarily then extinguish Reserve Tank Fuel Transfer Selectors OPEN Check VALVE POSITION lights illuminate momentarily then extinguish Reserve Tank Fuel Transfer Selectors CLOSE Check VALVE POSITION lights illuminate momentarily then extinguish Fuel Temperature Selector N
33. dwind corrections are made for any steady wind in the forward 180 arc 90 on each side of the runway heading When the wind is reported calm or light and variable and no wind shear exists Vref 5 knots is the recommended airspeed on the final approach The 5 knots will normally bleed off during the flare as the airplane approaches touchdown AMPLIFIED LANDING CHECKLIST Prior to landing when directed by the Captain the Flight Engineer will read the following challenges and receive the specified response from the appropriate crew member Speedbrake Lever FULL FORWARD C Spoiler Switches ON Engine Start Control Selectors BOTH F E Gear DOWN IN 3 GREEN C Check landing gear lever positioned down and in and 3 green landing GEAR DOWN lights illuminated Anti Skid 4 RELEASES F E Flaps 50 50 GREEN LIGHTS C Check inboard and outboard flaps at selected landing flap position and green LE FLAP lights illuminated Hydraulics PRESS amp QTY NORMAL F E Landing Checklist COMPLETE F E 2010 Captain Sim www captainsim com AL Part III Normal Procedures 43 DO NOT USE FOR FLIGHT GO AROUND PROCEDURE The following procedures will be accomplished in the event of a missed approach or other circumstances necessitating a go around with the airplane in the landing configuration MONITOR EPR Indicators O AROUND EPR and Autopilot if applicable DISENGAGE Rotate to Go Around attitude Call out Go Around
34. eceleration to holding speed 3 min prior to fix APPROACH PREPARATIONS Set bug VRet Complete DESCENT APPROACH checklist Approximately 1 min past LOM Review approach and go around procedure depending on wind Flaps 25 HA Set radios start procedure turn Bug 20 kts AL e Flaps 14 UO Go around thrust Descend go around attitude i ocedure Flaps oun oF on final LIG Complete P Positive rate of climb GEAR UP as required LANDING e erri to bug 10 kts tene e Accelerate to bug 20 kts m Retract flaps on Glide Stope 1 Dots up SA flap speed schedule Gear down gt Glide Slope 1 Dot up Fix LOM MKR Bug 10 kts e Verify crossing altitude Touchdown Glide slope intercept target 1000 ft Flaps 50 Bug wind gust Bug wind gust Standard callouts Zero rudder trim if one engine inoperative O 2010 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part III Operations 27 ILS AUTOPILOT Mode Selector Setting Intercept GS AUTO Below glide slope and before localizer reaches 2 dots APD Annunciator a V L Amber DAI G S Amber e i A DO NOT USE FOR FLIGHT Auto Pilot Mode Selector HOG HDG As required ALT HOLD As required Course setting Inbound final A Course AT APPROACH PREPARATIONS VHF NAV 1 and 2 ILS frequency LO
35. essors operating and cabin altitude 200 to 250 feet below airport elevation Transponder ON F O Engine Start Control Selectors BOTH F E landing Lights ON F O For collision avoidance check the fixed landing lights ON Before Takeoff Checklist COMPLETE F E www captainsim com ptain FLIGHT MANUAL Part III Normal Procedures 29 DO NOT USE FOR FLIGHT AKEOFF PROCEDURE PILOT FLYING PILOT NOT FLYING FLIGHT ENGINEER Align airplane on runway ransponder ON Advance thrust levers to normal Advance thrust levers to takeoff thrust erify correct takeoff thrust Adjust takeoff EPR between Monitor forward engine is set 40 and 80 knots if instrument panel Scan for required Monitor engine any abnormal indications instruments NOTE After takeoff thrust is set the Captain s hand must be on the thrust levers until V1 Monitor airspeed Monitor airspeed indications and call out any abnormalities erify V1 speed Rotate at Call out Vi and ROTATE R and establish a positive lat VR Monitor airspeed and rate of climb ertical speed erify 80 knots all 80 KNOTS BEEN all for GEAR UP when erify positive rate of Scan panel for warning positive rate of climb is limb then position lights and hydraulic established Landing Gear UP quantity hen landing gear lights extinguish position landing gear lever OFF WARNING NO 3 ENGINE THRUST LEVER MUST BE MOVED TO A QUADRANT POSITION FORWARD OF ZERO DE
36. eter SET Set current barometric pressure and cross check with field elevation RMI CHECK Check warning flag retracted Cross check heading with all com passes VOR ADF Switch AS DESIRED True Airspeed Indicator CHECK Check warning flag retracted Audio Selector Panel SET Oxygen amp Interphone TEST ON 100 Conduct oxygen check as described in Preliminary Cockpit Preparation 2010 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part III Normal Procedures 22 DO NOT USE FOR FLIGHT AMPLIFIED BEFORE START CHECKLIST When all appropriate preflight procedures are completed the Captain will call for the Before Start Checklist The First Officer will read aloud each challenge and receive the appropriate response from the designated crew member Cockpit Preparation COMPLETE Oxygen amp Interphone CHECKED ON amp 100 Emergency Flaps OFF Mach Airspeed Warning CHECKED Anti Skid CHECKED amp ON Rudder amp Spoiler Switches ON Emergency Exit Lights ARMED Seat Belts Switches ON INS CHECKED amp SET Radio Altimeters CHECKED Window Heat LOW Pneumatic Brake CHECKED Fit Inst Altimeter amp Fit Dir SET amp X CHECKED Compasses SYNC amp X CHECKED Radios Radar amp Transponder SET amp STANDBY Check radios set for departure and radar and transponder set to STBY Start Levers CUTOFF Parking Brakes SET Rudder amp Aileron Trim FREE amp ZERO Battery ON Fuel KGS SET FOR START
37. in s Sliding Window TEST Check window opens and closes properly and is clean and undamaged Evacuation Strap STOWED Panel Lights SET Flight Recorder ON Check OFF light extinguished Mach Airspeed Warning CHECK Anti Skid ON amp TEST Check anti skid switch guard closed Anti Skid Test Switch OUTBD amp HOLD Check inboard REL lights illuminate and outboard REL lights remain extinguished Anti Skid Test Switch INBD amp HOID Check outboard REL lights illuminate and inboard REL lights extinguish Anti Skid Test Switch RELEASE Check all REL lights extinguished INS CHECK amp SET Emergency Exit Lights Switch GUARD CLOSED Exterior Lights Check Wheel well lights switch NORM Wing lights switch ON OFF Beacon light switch OFF Runway tumoff lights switch OFF Standby Compass EXTEND Flight Director If Required TEST amp SET Pneumatic Brake CHECK Check pneumatic brake handle safe tied and emergency brake pressure indicates 1200 50 psi Originating flight or crew change check is accomplished by Flight Engineer Instrument Panels SECURE Check forward and center panels in place and fasteners secured and locked Flight Instruments CHECK amp SET Mach Airspeed Indicator CHECK amp SET Check airspeed pointer zero Mach indicator warning flag retracted Set VI VR and V2 airspeed bugs in accordance with takeoff data card if available ADI CHECK Check GYRO warning flag retracted 2010 Captain
38. is Positive rate of climb gear up Accelerate to bug 10 kts 4 LANDING Flaps 14 A checklist Accelerate to bug 20 kts to flaps Retract flaps on flap speed schedule if desired 14 2 mi MAXIMUM 400 500 ft BANK 309 Stabilize in slot gt Final 700 900 ft Flaps 50 e Reduce speed to bug wind gust Complete LANDING checklist Standard callouts Thrust to idle e Speed brakes up Complete down Braking as required AFTER Bug gust target Reverse thrust LANDING 1000 ft checklist Zero Rudder Trim If 1 Engine Inoperative 2010 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part III Operations 59 DO NOT USE FOR FLIGHT USTOMER CARE You are invited to join Captain Sim community forum DAILY NEWS For Captain Sim daily news please follow us at Twitter or Facebook 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 and consider the most significant issues for the next service packs 20
39. ive rate of climb indicated call GEAR UP limb at V2 limit bank angle to 15 ommand initiation of appropriate checklist Accomplish recall actions if appropriate At desired speed and flap retraction altitude retract schedule omplete appropriate hecklist Determine next course of action DO NOT USE FOR FLIGHT all or verify ENGINE FIRE or ENGINE FAILURE and engine number all positive rate of climb On command position landing gear lever UP Observe warning lights illuminate hen landing gear warning lights extinguish position landing gear lever OFF Assist pilot flying as directed Retract flaps on command Monitor flap indicators and LE flaps lights omplete appropriate hecklist On command notify ATC and advise of next course of action all or verify ENGINE FIRE or ENGINE FAILURE and engine number Scan Flight Engineer s panel or abnormal indications Monitor forward engine instrument panel Accomplish recall actions of appropriate checklist Scan panels for abnormal indications Read appropriate checklists and complete appropriate hecklist items On command set Maximum ontinuous thrust as required 1 If an engine failure occurs prior to V2 maintain V2 up to height required for obstacle clearance If an engine failure occurs after V2 but less than V2 10 knots maintain speed reached at time of the engine failure If an engine failure occurs at V2 10 kn
40. lights ist extinguished Silently accomplish AFTER AKEOFF checklist Announce After Takeoff Rescan panel for possible abnormal indications The hird air compressor may be started Monitor radio ommunications during departure and climb to level off Sim www captainsim com 707 Captain FLIGHT MANUAL Part III Normal Procedures 33 DO NOT USE FOR FLIGHT AMPLIFIED AFTER TAKEOFF CHECKLIST When commanded by the Captain the Flight Engineer will read silently each challenge and verify that the appropriate action has been accomplished If any action has not been accomplished he will read aloud the challenge to the designated crew member and after the action has been completed receive the correct response After all actions have been completed and verified the Flight Engineer will announce to the Captain After Takeoff Checklist complete Anti Ice OFF ON F E Engine Start Control Selectors OFF ON F E Check engine start control selectors set as required for flight conditions Seat Belts Switches OFF ON F E Check switches OFF if flight conditions permit Gear UP amp OFF F E Check landing GEAR down light ard GEAR and DOOR warning lights extinguished and landing gear lever in OFF position CAUTION DO NOT ACTUATE BRAKE PEDALS DURING GEAR RETRACTION SUFFICIENT BRAKING IS AUTOMATICALLY APPLIED TO WHEELS WHEN HANDLE IS UP AND GEAR IS IN TRANSIT SUDDEN APPLICATION OF BRAKE PEDAL FORCE DURING RETRACTION CAUSES VIOLE
41. lluminated Fit Dir Fit Inst and Radios SET FOR DEPARTURE C F O Speedbrake Lever FULL FORWARD C Flaps 14 14 GREEN LIGHTS Check both flap position indicators indicate 14 and green LE FLAP lights illuminated Start Levers IDLE DETENT C Stabilizer Trim UNITS C Check stabilizer trim setting agrees with computed setting 2010 Captain Sim www captainsim com 28 DO NOT USE FOR FLIGHT Flight Controls CHECKED C INS CHECKED F O Electrical NO LIGHTS ESS 3 F E Check all generator drive LOW PRESSURE CIRCUIT OPEN and essential power FAILURE warning lights are extinguished and essential power selector is positioned to GEN 3 Galley Power ON F E Fuel SET FOR T O F E Check fuel system set for proper takeoff configuration appropriate boost pump switches ON and LOW PRESSURE lights for operating boost pumps extinguished Fuel Heat OFF F E Hydraulics PRESS amp QTY NORMAL F E Check system pressures normal AC auxiliary and engine pump LOW PRESS lights extinguished and tank quantity at least full Cockpit Door LOCKED F E Takeoff Briefing amp Data REVIEWED BUGS SET ALL The pilot making the takeoff shall review the takeoff data and brief the other crew members on their expected actions during and immediately after takeoff Check that airspeed and EPR bug settings agree with the computed data Continue the checklist after receiving takeoff clearance Air Cond amp Press SET FOR T O F E Check only two air compr
42. ltimeter CHECKED F O Window Heat LOW F O Pneumatic Brake CHECKED C Fit Inst Altimeter amp Fit Dir SET amp X CHECKED ALL Compasses SYNC amp X CHECKED C F 0 Radios Radar amp Transponder SET amp STANDBY C F O Start Levers CUTOFF C Parking Brakes SET C Rudder amp Aileron Trim FREE amp ZERO C Battery ON F E Fuel KGS SET FOR START F E Air Cond Units OFF F E CLEARED FOR START Galley Power OFF F E Start Pressure PSI F E INS Mode Selectors Doppler C Beacon ON C Before Start Checklist COMPLETEF O AFTER START Ground Equipment CLEAR C Hydraulics PRESS amp QTY NORMAL F E INTERCONNECT CLOSED Doors CLOSED F E After Start Checklist COMPLETE F O BEFORE TAKEOFF Nacelle Anti Ice OFF ON F O Ground Start Switch OFF F O Window Heat HIGH F O Probe Heaters ON F O Fit Dir Fit Inst amp Radios SET FOR DEPARTURE C F O Speedbrake Lever FULL FORWARD C Flaps 14 14 GREEN LIGHTS C Start Levers IDLE DETENT C Stabilizer Trim UNITS C Flight Controls CHECKED C INS CHECKED F O Electrical NO LIGHTS ESS 3 F E Galley Power ON F E Fuel SET FOR T O F E Fuel Heat OFF F E Hydraulics PRESS amp QTY NORMAL F E Cockpit Door LOCKED F E 2010 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part III Normal Procedures DO NOT USE FOR FLIGHT Takeoff Briefing amp Data LEARED FOR TAKEOFF Air Cond amp Press Transponder Engine Start Control Selectors Landing Lights Before Takeoff Che
43. m 707 Captain FLIGHT MANUAL Part III Operations 55 DO NOT USE FOR FLIGHT NORMAL OR ONE ENGINE INOPERATIVE VOR APPROACH If holding is required approach fix with gear up flaps up APPROACH PREPARATIONS Set bug VRef Approximately 1 start deceleration to holding Complete DESCENT APPROACH min past radio fix speed 3 min prior to fix checklist depending on wind Review approach and go around procedure start procedure turn Flaps 14 Set radios Bug 30 kts Flaps 25 Missed Approach Bug 20 kts e Go around thrust Rotate to go around attitude Flaps 25 LANDING Positive rate of climb gear up Descend in checklist to flaps Accelerate to bug 10 kts procedure turn Standard callouts or on final as required Minimum descent Accelerate to bug 20 kts El Retract flaps on flap speed schedule Radio Fix e Start time ON DAD Runway in sight Flaps 25 is bio Bug 20 kts Initiate ee e Establish landing profile Bug gust e Flaps 50 Touchdown Complete LANDING checklist target 1000 ft Bug wind gust e Standard callouts Zero rudder trim if one en gine inoperative 2010 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part III Operations 56 DO NOT USE FOR FLIGHT NORMAL OR ONE ENGINE INOPERATIVE ILS APPROACH NOTE If holding is required approach fix with gear up flaps up start d
44. n controls on flight director control panel as desired for enroute navigation Climb Thrust MONITOR Reset climb EPR as necessary using quick reference data and existing TAT and altitude Landing lights OFF Fixed landing lights should be turned OFF when passing through 10 000 feet Operating Systems MONITOR Monitor the following operating systems periodically as flight conditions permit Electrical System CHECK Check AC voltage and frequency within limits DC system voltmeter amp load meter indications normal Generator drive LOW PRESSURE lights extinguished Generator drive oil temperature rise indications normal Bus tie breaker CIRCUIT OPEN lights extinguished Generator breaker CIRCUIT OPEN lights extinguished KW KVAR loads within limits and balanced Fuel System CHECK Check Operating boost pump LOW PRESSURE lights extinguished Quantity indicator operation and fuel used consistent with operation Fuel temperature at least 3 C above fuel freezing point Hydraulic System CHECK Check Hydraulic quantity indicator reflects gear and flap retraction Note quantity decreases as OAT decreases due to cold soak effect at high altitude Utility hydraulic system pressure normal and rudder pressure reduced to 2250 psi above 245 kt IAS AC auxiliary and engine pump LCW PRESS lights extinguished Engine Operation CHECK Check Engine vibration indications HI amp N2 indications within limits EGT indications stabilized amp withi
45. n limits Fuel flow approximately equal for each engine Engine oil pressure and temperature indications within limits Engine oil quantities sufficient for remainder of flight Air Conditioning and Pressurization Systems CHECK Coolant Air System CHECK www captainsim com 35 DO NOT USE FOR FLIGHT Check Inlet and exit valves positioned OPEN or as desired for performancee Secondary heat exchanger valves positioned to agree with temperature control valve position Turbo fan exit valve positioned closed Temperature control valve positioned as required for existing conditions Main Cabin Heating Panels AS DESIRED Gasper Fan Switch AS REQUIRED FOR VENTILATION Oxygen Systems CHECK Check pressures normal Cruise Data PRECOMPUTE Compute projected gross weight at level off Use appropriate performance tables to determine indicated Mach No if required indicated airspeed average EPR and fuel flow for cruise Altimeters SET amp CROSS CHECK At transition altitude each pilot and navigator sets altimeters to 1013 MB 29 92 in Hg and crosschecks F E resets cabin altimeter Fuel Management As Required ACCOMPLISH Establish fuel usage for all inflight operations according to the diagram below www captainsim com 707 Captain FLIGHT MANUAL Part III Normal Procedures 36 DO NOT USE FOR FLIGHT INITIAL FUEL DISTRIBUTION FUEL USAGE PROCEDURE Observe Recommendations and Limitations Chapters 1 4 and 15
46. n toward reverse idle at a rate which ill avoid engine surge At approximately normal axi speed slowly move reverse thrust levers to full down position Observe REVERSER OPERATING lights for normal indication erify speedbrake lever UP erify speedbrake lever UP Monitor REVERSER OPERATING lights for normal indication Monitor engine instruments Advise pilots of any engine limits being exceeded or abnormalities Monitor Hydraulic Brake and ystem Pressure Indicators Observe reverser lights Advise pilot flying of reverser lights remaining illuminated WARNING AFTER INITIATING THE LANDING PROCEDURE A FULL STOP LANDING SHOULD BE MADE A GO AROUND OR TAKEOFF MUST NOT BE ATTEMPTED AFTER REVERSE THRUST HAS BEEN INITIATED Deployed speed brakes or reversers not retracted in the full forward and locked position could result in an unsuccessful go around or takeoff 2010 Captain Sim www captainsim com MANUAL Part III Normal 45 edi OR FLIGHT Proc DO NOT USE F TAXI IN AND PARK TAXI IN AND PARK AFTER LANDING PROCEDURE CAUTION OPERATING TWO ENGINES IN REVERSE TO DECREASE TAXI SPEEDS MAY RESULT IN ENGINE DAMAGE SINCE THE REVERSE JET BLAST MAY BE SUFFICIENTLY STRONG TO LIFT FOREIGN OBJECTS UP IN FRONT OF ENGINE INLETS TAXIING IN REVERSE MAY ALSO RESULT IN INGESTION OF EXHAUST GASES INTO AIR CONDITIONING SYSTEM Exterior Lights AS REQUIRED Flaps UP NO LIGHTS Retract flaps when convenien
47. nd pneumatic power to be safely applied to the airplane at the proper time Emergency Flap Switches OFF Check Arming switch guard closed Inboard and outboard switches off Landing Lights Switches OFF Landing Gear Lever DOWN amp IN CAUTION LANDING GEAR LEVER SHOULD NOT BE PLACED IN OFF DURING GROUND OPERATION DUE TO POSSIBILITY OF COLLAPSING NOSE GEAR Radar Mode Selector OFF Transponder Mode Selector STBY Galley Power Switch OFF AC Aux Pump Switches OFF Fuel Dump Panel Cover CLOSED 2010 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part III Normal Procedures 11 DO NOT USE FOR FLIGHT PRELIMINARY COCKPIT PREPARATION Be power on airp Cockpit systems and controls are checked for normal operation and the airplane is configured for exterior inspection if required and engine start Circuit Breakers CHECK Check circuit breakers set or collared Essential Radio Bus 1 amp 2 OFF External Power Switch OFF Battery Switch ON Position battery switch and check generator breaker CIRCUIT OPEN lights illuminated Check DC volt meter indicates 24v amp load meter indicates positive or zero External Power CHECK Check external power CONNECTED light illuminated AC Paralleling Selector EXTERNAL POWER Check voltage and frequency stabilized within limits External Power Switch ON Check PWR ON BUS light illuminates ammeter indicates load Voltage and frequency remain stabilized within limits
48. onfigure the airplane for landing The pilot not flying executes standard callouts in the approach PILOT FLYING PILOT NOT FLYING FLIGHT ENGINEER Speedbrake Lever FULL FORWARD Spoiler Switches ON all for flap extension on Position flap lever as heck hydraulic system he flap speed schedule in directed Monitor flap quanity accordance with the landinglextension and leading edge approach requirements laps operation Prior to crossing the outer marker cross check all flight and navigation instruments check warning flags retracted tune and identify radios and check LOC and S displayed all GEAR DOWN in Position landing gear lever Engine Start Control accordance with the landingDOWN Observe lights for Selectors BOTH No approach requirements proper landing gear Smoking ON extension heck 4 REL s on brake release indicators If conditions require use heck landing gear down indshield wipers and rain fand locked hydraulic quantity and pressure normal all for LANDING Checklist Read LANDING Checklist down to FLAPS down to flaps At final approach fix OM verify crossing altitude MEN all for Flaps 50 and Select flaps for landing heck hydraulic brake and Complete Landing Monitor extension system pressure indicators hecklist and system quantity indicators normal One Air ompressor OFF Read LANDING checklist heck landing gear down Monitor all systems with and locked both flap particular attention to p
49. or engine instruments and call out any failure affecting safety He will request other pilot to hold column forward with displaced lateral control if in crosswind to set takeoff EPR to computed value by 80 kts to call out VI and Rotate at VR and to silence fire bell if it rings When cleared onto the runway Flight Engineer s Seat POSITION FOR TAKEOFF Position seat facing forward or a maximum of 30 right WARNING WHILE THIS POSITION IS THE MOST CONVENIENT FOR FLIGHT ENGINEER MAXIMUM SAFETY CONFIGURATION IS WITH SEAT FACING FORWARD AND SHOULDER HARNESS ON One Air Compressor Normally No 4 OFF Pressurization System SET FOR FLIGHT Prepare for Takeoff ANNOUNCE Notify cabin attendants and passengers over PA system to prepare for takeoff When cleared for takeoff Transponder Mode Selector ON Engine Start Control Selectors BOTH Landing Lights ON AMPLIFIED BEFORE TAKEOFF CHECKLIST After leaving the gate and prior to taking the runway the Captain will call for the Before Takeoff Checklist The Flight Engineer will read aloud each challenge and receive the appropriate response from the designated crew member Nacelle Anti Ice OFF ON F O Check nacelle anti ice valves positioned OFF or ON as required Attitude Warning CHECKED F O Ground Start Switch OFF F O Window Heat HIGH F O Check window heat switches on HIGH and OVERHEAT lights extinguished Probe Heaters ON F O Check probe heater switches ON and HEAT ON lights i
50. osition indicators at landing flap position and green LE FLAPS light CAUTION RE TRIM AIRPLANE ON APPROACH TO MAINTAIN ZERO ELEVATOR CONTROL FORCES SUFFICIENT ELEVATOR CONTROL FOR FLARE MAY NOT BE AVAILABLE IF STABILIZER TRIM IS SET SO AS TO REQUIRE SUBSTANTIAL BACK PRESSURE ON CONTROL COLUMN TO MAINTAIN FLIGHT PATH AND APPROACH AIRSPEED LANDING FLARE SHOULD BE PERFROMED BY USE OF ELEVATOR CONTROL ONLY The Boeing recommended approach speed and wind correction is Y2 the steady headwind component plus all of the gust value up to a maximum of 20 knots In all cases the gust correction should be maintained to touchdown while the steady wind correction may be bled off as the airplane approaches touchdown Fly the airplane onto the runway at the desired touchdown point Do not bleed off excess airspeed in the air by holding the airplane off the runway as a long landing will result It is recognized that the actual wind encountered on the approach may vary from that reported by the tower due to terrain or climatic phenomenon However unless actual conditions are known i e reported wind shears or known terrain induced turbulence areas it can be considered reasonable for convience of operation and to avoid additional cockpit workload to adjust the approach speed by the V2 steady wind plus gust www captainsim com 707 Captain FLIGHT MANUAL Part III Normal Procedures 42 DO NOT USE FOR FLIGHT values as reported by the Tower Hea
51. ots maintain speed V2 10 knots If an engine failure occurs at a speed higher than V2 10 knots with flaps at takeoff setting increase pitch attitude and reduce speed to and maintain V2 10 knots until clear of obstacles 2010 Captain Sim www captainsim com DO NOT USE FOR FLIGHT At altitude selected for flap Position flap lever to UP Monitor hydraulic quantity retraction accelerate to V2 position Monitor flap during flap retraction 30 Minimum retraction and leading edge all Flaps Up device operation Monitor forward panel warning lights and engine instruments all Landing Lights OFF Place landing lights not Obtain readings from TAT being used for Collision indicator and altimeter Avoidance to OFF ompute climb EPR After flap retraction reduce Set climb thrust hrust to approximately 100 N1 and call Set Nacelle and or wing anti icelEngine start control AS REQUIRED selectors AS REQUIRED No Smoking and Seat Belts Switches At Captains ommand OFF ontinue to accelerate to Exit Valves OPEN Turbofan 2 50 Maneuvering Exit Valves CLOSED apability at 0 flaps Then 2 70 Best Climb Angle Speed then appropriate limb speed 250 Kts maximum below 10 000 ft Monitor hydraulic systems or normal operation Maintain traffic surveillance Re adjust engine climb and monitor flight hrust as required instruments hen flaps selected up calliCheck flaps indicate UP and or AFTER TAKEOFF LE FLAPS
52. ow Heat LOW CAUTION SLIDING WINDOWS SHOULD BE CLOSED TO AVOID OVERHEATING Flight Director If required TEST amp SET Flight Instruments CHECK amp SET Check and set as described for Captain Ground Proximity System TEST Ground Proximity System Test Switch PUSH amp HOLD GRD PROXIMITY lights illuminate momentarily Transponder SET amp STANDBY Set desired code 2010 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part III Normal Procedures 21 DO NOT USE FOR FLIGHT Stabilizer Trim TEST Coordinate with Captain s stabilizer trim test Stabilizer Trim Switches NOSE UP THEN NOSE DOWN Verify stabilizer trim wheels move for corresponding switch position and stabilizer trim light illuminates during the test Stabilizer Trim SET Set stabilizer trim units in accordance with takeoff data card VHF Navigation SET FOR DEPARTURE Departure Frequency SET Identify station Check HSI VOR LOC warning flag retracted Check RMI pointers for proper bearing Perform system test if required DME Mode Selector TEST amp NORM Mileage indicators on HSI and opposite instrument panel indicate all zeroes and off flags retract Communications SET FOR DEPARTURE ADF SET FOR DEPARTURE ICOCKPIT PREPARATION NAVIGATOR Table Panel and Flood Lights SET Adjust lights to desired intensity Static Air Temperature Indicator CHECK Check warning flag retracted and indication approximately ambient or greater Altim
53. ps and go around speed bug 10 knots in the appropriate spaces on the data card The F 0 will verify the entries EPR amp Airspeed Bugs SET mL eer uu Fuel System SET FOR LANDING Position all main tank fuel boost pump switches ON and observe all main tank WW PRESSURE lights extinguish Check fuel heater switches OFF Set main tank to engine configuration Hydraulic Systems PRESSURES amp QUANTITY NORMAL NOTE If brake pressure increases above 3500 psi actuate brakes momentarily to bleed off pressure Speed Brake Lever FULL FORWARD Spoiler Switches GUARDS CLOSED ADF Radios SET FOR APPROACH Tune to frequency of outer marker or other fix and identify station Verify RMI bearing to station VHF NAV Radios SET FOR APPROACH Tune to ILS frequency identify station and observe appropriate ADI and HSI warning flags retracted Set course pointers counters to localizer course Autopilot SET FOR APPROACH With autopilot engaged position mode selector to HDG Select desired heading When aircraft is on intercept heading rotate mode selector to G S AUTO and observe amber illumination of autopilot www captainsim com 707 Captain FLIGHT MANUAL Part III Normal Procedures 39 DO NOT USE FOR FLIGHT V L and G S annunciators At ILS entry altitude place altitude hold switch ON If ILS coupled approach is not desired use autopilot in manual mode to make approach tracking raw data or flight director indications
54. ressure Indicator CHECK Check L amp R pressure 2700 3000 psi Engine Instruments CHECK Check N2 RPM and oil pressure indicators zero Oil temperature indicators within normal range Equipment Cooling System CHECK Equipment Cooling Blower Switch NORM Overboard Dump Switch NORM Engine Oil Quantity Indicators TEST Note initial oil quantity indications Engine Oil Quantity Test Switch PRESS amp HOLD Check all oil quantity indications decrease Engine Oil Quantity Test Switch RELEASE Check all oil quantity indications stabilize at approximately original indications Engine Oil Quantities CHECK Check oil quantities adequate for dispatch Pressurization System TEST amp SET Air Conditioning System TEST amp SET Cabin Air Temperature Source Selector CHECK Rotate selector to FWD MID AFT and INLET DUCT and check for normal indications at each position Air Supply Duct Pressure CHECK Zero unless ground air supplied Conditioned Air Duct Pressure Indicator CHECK Zero unless air conditioning unit operating or conditioned air being supplied www captainsim com DO NOT USE FOR FLIGHT Crew amp Main Temperature Selectors AUTOMATIC amp SET Air Conditioning Unit Switches OFF ON Check unit OVERHEAT lights extinguished Engine Bleed Air Switches OFF Wing Valve Switches L and R OPEN Air Compressor LOW OIL PRESS Lights ILLUMINATED Air Compressor RPM Indicators Eng s 2 3 amp 4 20 Ram
55. rking Brake SET VHF Navigation SET FOR DEPARTURE Departure Frequency SET Identify station Check HSI VOR LOC warning flag retracted Check RMI bearing pointers for proper bearing Perform system test if required DME Mode Selector TEST amp NORM Mileage indicators on HSI and opposite instrument panel indicate all zeroes and off flags retract Communications SET FOR DEPARTURE Autopilot DISENGAGED ADF SET FOR DEPARTURE Rudder Trim FREE amp ZERO www captainsim com 707 Captain FLIGHT MANUAL Part III Normal Procedures 20 DO NOT USE FOR FLIGHT Rudder Trim FULL LEFT THEN FULL RIGHT Check for freedom of travel and corresponding rudder Rudder Trim ZERO Aileron Trim FREE amp ZERO Aileron Trim FULL LEFT THEN FULL RIGHT Check for freedom of travel and corresponding control wheel movement Aileron Trim ZERO When cleared for engine start INS Mode Selectors Doppler Beacon Switch ON COCKPIT PREPARATION FIRST OFFICER Life Vest STOWED Seat amp Rudder Pedals ADJUST Briefcase Light CHECK Sun Visors STOWED Audio Selector Panel SET Oxygen amp Interphone TEST ON 100 Conduct oxygen check as described in Preliminary Cockpit Preparation First Officer s Sliding Window TEST Check window opens and closes properly and is clean and undamaged Evacuation Strap STOWED Panel Lights SET Radio Altimeters TEST MDA Bugs SET APPROXIMATELY 20 FEET MDA Bug Controls SET AT ZERO Wind
56. roach At DH Visual Go around reference not established i e PNF does not call any visual cues or alls only strobe CHART II www captainsim com 707 Captain FLIGHT MANUAL Part III Normal Procedures 10 DO NOT USE FOR FLIGHT NORMAL PROCEDURES PREFLIGHT All preflight procedures are completed prior to each originating flight Only those items marked with an asterisk need be accom plished on through flights when there is no crew change Any lights which are not illuminated during a system test should be checked by press to test EXTERIOR SAFETY INSPECTION This inspection is performed on each originating trip or crew change before entering the airplane to ascertain that no obiously unsafe conditions exist Chocks IN PLACE Landing Gear Doors CHECK WARNING IF ANY GEAR DOOR IS OPEN ENSURE RESPECTIVE DOOR RELEASE HANDLE IS IN OPEN DETENT IF HANDLE IS IN RETRACTED POSITION AND DOOR IS OPEN DOOR WILL CLOSE WHEN HYDRAULIC SYSTEM IS PRESSURIZED WHICH COULD RESULT IN PERSONNEL INJURY Flight Control Surfaces CLEAR Ensure proper clearance of flight controls from all ground equipment or other obstructions Maintenance Status amp Dispatch Deviations CHECK Verify maintenance status agrees with authorized dispatch deviations COCKPIT SAFETY INSPECTION This inspection is performed on each originating trip or crew change to ensure the cockpit controls are configured so as to permit electrical by hydraulic a
57. round power is of proper quality and will not be interrupted INS accuracy was within 1 5 miles per hour in NAV mode on previous flight Sufficient equipment cooling will be maintained NOTE Ground power interruption will deplete INS battery units Electrical Power EXTERNAL ON 2010 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part III Normal Procedures 47 DO NOT USE FOR FLIGHT Check external power CONNECTED light illuminates Position AC paralleling selector to EXT and check frequency and voltage within limits Position external power switch generator switch to ON and essential power source selector to EXT Engine Start Lever No 3 CUTOFF Beacon Light Switch OFF Emergency Exit Lights Switch ARMED OFF Seat Belts Switch OFF Communications SET FOR RAMP OPERATIONS Parking Brake RELEASE Release Parking Brakes when CHOCKS are in place Check parking brake warning light extinguishes Galley Power Switch If Required ON Fuel Boost Pumps OFF AC Au CUTOFF auxiliary Pumps OFF Temperature Control Valves FULL CLOSED Oxygen Regulators ON OFF 100 Oxygen supply levers may remain ON if through flight is planned If terminating flight External Power ON OFF Battery ON OFF AMPLIFIED SHUTDOWN CHECKLIST After parking the airplane and when commanded by the Captain the Flight Engineer will read aloud each challenge and receive the appropriate response for the items accomplished by Captain and First Officer
58. s SET Retractable and Fixed landing lights Runway Turn off lights AS REQUIRED Nacelle Anti Ice TEST OFF ON Attitude Warning TEST Ground Start Switch GUARD CLOSED 2010 Captain Sim www captainsim com 26 DO NOT USE FOR FLIGHT Window Heat Switches HIGH Probe Heater Switches ON Check probe heater HEAT ON lights illuminated Flight Directors Flight Instruments and Radios CHECK SET FOR DEPARTURE Check flight director set to desired heading and pitch attitude Compare indication of all ADI s HSI s RMI s and standby compass during turns Check radios and HSI s set for departure Stabilizer Trim SET FOR TAKEOFF Set stabilizer trim in accordance with computed data Setting the stabilizer trim anywhere in the green band range is not necessarily satisfactory for takeoff Flight Controls CHECK Rotate control wheel full left then full right Push then pull control column through its full fore and aft travel Note that initial travel during control tab movement requires only light forces but heavy forces are required to move control surfaces Move rudder pedals through full travel and check for freedom of movement Check RUDDER LOW PRESS light extinguished and normal pressure fluctuations in utility and rudder system pressures as controls are exercised INS CHECK Check present position changes Monitor ground speed Engine Operation CHECK Check engine indicators normal warning lights extinguished Electrical System CHEC
59. s are read at specified points to verify that certain critical or essential steps of the preceding procedures have been accomplished Where possible these steps and checklists follow a standardized scan flow for each panel as indicated below This provides the flight crew with established patterns for performing the normal procedures and checklists P 3 Se a START ee Xx The following charts identify the standard callouts required during CLIMB DESCENT and FINAL APPROACH for either IFR or VFR conditions Chart 1 contains all recommended standard callouts for a normal IFR or VFR flight Chart 2 contains additional callouts to be made when accomplishing a category II or category IMA approach The pilot not flying should accomplish these callouts on every flight while the flight engineer monitors Airplanes with special alerting equipment i e terrain warning etc still require these callouts to be performed because these alerting systems normally monitor altitudes from the radio altimeter which can be influenced by irregular ground levels NOTE DO NOT use radio altimeter as the instrument for standard callout references 2010 Captain Sim www captainsim com DO NOT USE FOR FLIGHT STANDARD CALLOUTS CONDITION LOCATION CALLOUT FINAL APPROACH Approaching Transition Altitude ransition Altitude IFR and Altimeters Reset FR 1000 ft above below 1000 Feet to Level Off assigned altitude IFR 10 000 ft MSL
60. t all ground equipment has been removed Hydraulics PRESS amp QTY NORMAL INTERCONNECT CLOSED F E Check utility and AC aux pump switches ON all pressures including hydraulic brake and quantity normal Check interconnect valve switch OFF Doors CLOSED F E Check all door annunciator lights extinguished After Start Checklist COMPLETE F O TAXI OUT AND TAKEOFF AXI OUT PROCEDURE Good taxi technique requires an awareness of the proximity of obstacles the effects of excessive noise the force of the jet exhaust and the possibility of ingestion of foreign objects Nose wheel steering and engine thrust are used for directional control To make smooth turns grasp the steering wheel firmly and pressure it in the desired direction The airplane should be taxied with all four engines at idle thrust When an outboard engine is used to assist in a turn use as little power as possible Differential braking is not normally used for steering during taxi and should not be used in conjunction with nose wheel steering At light gross weights allow the airplane to accelerate then brake to a very slow taxi speed release the brakes and repeat the sequence Taxi Clearance OBTAIN Parking Brake RELEASE Check parking brake lever returns to OFF position and parking brake warning light extinguishes Taxi INITIATE Flaps EXTEND Check LE FLAPS lights illuminate and both outboard and inboard flap position indicators indicate 14 Exterior Light
61. t prior to entering a congested area Speedbrake Lever FULL FORWARD Anti Ice Switches OFF ON As required by ground conditions Window Heat LOW OFF On through flights all window heat switches may be left in the LOW position if conditions require On terminating flights position all switches to OFF Probe Heat Switches OFF Radar Mode Selector STBY OFF Position selector to STBY on through flights and to OFF on terminating flights Transponder Mode Selector STBY OFF Position selector to STBY on through flights and to OFF on terminating flights Radios SET FOR GROUND OPERATION Engine Start Control Selectors OFF AC Paralleling Selector EXTERNAL POWER Galley Power Switch OFF DC Meter Selector BATT Boost Pumps ONE PER ENGINE Hydraulic amp Brake Pressure MONITOR Outflow Valves CHECK OPEN Air Compressor Switches AS DESIRED Operate at least 2 air compressors for ventilation Coolant Air Valves CHECK POSITION Position coolant air valve selector to EXIT and check CLOSED Position coolant air valve selector to TURBOFAN EXIT and check OPEN Reposition selector to TEMP CONTROL Gasper Fan Switch ON Position gasper fan switch as desired 2010 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part III Normal Procedures 46 DO NOT USE FOR FLIGHT AMPLIFIED AFTER LANDING CHECKLIST When clear of the active runway the Captain will call for the After Landing Checklist The Flight Engineer will read silently
62. urn to s or severe icing condition ar 3000 ft occurs Flaps a a 10 kts mum bank 30 gt kts mu Ea Set takeoff thrust Vn Positive rate Straight Climbout prior to 80 kts Rotate smoothly of climb Maintain Monitor airspeed to proper attitude Gear up Takeoff flap setting Va 10 kts 2010 Captain Sim www captainsim com 707 Captain FLIGHT MANUAL Part III Operations 54 DO NOT USE FOR FLIGHT TAKEOFF ENGINE FIRE FAILURE AFTER Vi Retract flaps on flap speed schedule Set MCT Accomplish ENGINE FIRE SEVERE DAMAGE OR SEPARATION or ENGINE FAILURE amp SHUTDOWN checklist 2 Close In Turn e Maintain Flaps 14 Va Maximum bank 15 e Set takeoff thrust eVR Positive rate Altitude selected for Prior to 80 kts e Rotate smoothly of climb flap retraction Monitor airspeed Gear up FLAP SPEED FLAP SPEED SCHEDULE ET Maneuvering lee for 30 Bank Limit Bank to eee until NOTE Straight Climbout Maintain Vo Takeoff flap setting Accelerate to V5 30 kts in level flight or slight rate of climb Retract flaps Accelerate to V5 50 kts Set MCT Climb to 1500 ft at V3 50 kts Complete ENGINE FIRE SEVERE DAMAGE OR SEPARATION or ENGINE FAILURE amp SHUTDOWN checklist Complete AFTER TAKEOFF checklist if required e Notify ATC of intended action 2010 Captain Sim www captainsim co

`707 Captain` FLIGHT MANUAL Part III – Operations

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`707 Captain` FLIGHT MANUAL Part III &ndash; Operations

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`707 Captain` FLIGHT MANUAL Part III – Operations