`727 Captain` FLIGHT MANUAL Part III – Operations
Contents
1. CLOSED Check that APU light S O lower panel illuminates This light illuminates only if the 1 DC bus is energized and therefore will not illuminate when the APU is being started from the battery alone 7 APU MASTER 5 1 START 8 APU CRANK LIGHT RR a a aa ae ae ccce a a ILLUMI NATES 9 MASTER SWITCHe eure rtt aA a res deo ETE ee Sg Sede ae RELEASE TO ON UPON OBSERVING CRANK LIGHT a APU CRANK EIGHT 2k ii ema e m a ae aa EXTINGUI SHES This indicates that the starter motor is de energized Light should extinguish in approx 10 seconds If APU crank light does not extinguish within 30 seconds after APU start initiation terminate APU start by pulling APU FIRE switch 10 APU EXHAUST GAS TEMPERATURE INDICATOR MONITOR 11 Check for stabilized speed by observing APU generator frequency approximately 400 CPS 12 ALL BUS TIE BREAKERS E Rn inn hm O ie i CLOSED 13 VOLTAGE CHECK WITHIN LIMITS 14 APU GENERATOR BREAKER 5 CLOSE Closing the APU GENERATOR BREAKER switch will trip the EXTERNAL POWER switch or the www captainsim com DO NOT USE FO2. CHECK Valve will be full cold if pack is off and normal if pack is on 3 DUCT OVERHEAT LIGHTS sisme RR Rm ba ee a XR RR PUSH TO TEST ENG NE BLEEDS cdit icm der a peti ona Ve D n T eve n a hE a Gad Bad OR I JA IRA T e Re n 4 OPEN js cT cv TITLE TIEFEERTUE AS REQUIRED USING APU BLEED AIR a RIGHT AIR CONDITIONING PACK 5 ON If the APU is providing electrical power monitor APU ammeter before starting packs Load must be under 120 amps before starting either first or second pack b LEFT AIR CONDITIONING PACK 5 ON AFTER SELECTING EITHER APU OR EXTERNAL PNEUMATIC 1 AIR TEMP INDICATORS tue air le cea gogo aot cu e d CHECK 2 TRIP OFF LIGHTS ra Goes ae ewe BE X ROAD ACCADE UU add DURS TEST 3 AUTO PACK TRIP ARM LIGHT aene li ge Us bm all mom E ER RR TEST 4 GASPER gla Si peur e lin a ur GG x adu a bos AS REQUIRED 5 PACK 1 1 CHECK COOLINGDOORS A MANUAL DOORS 33 2 te onm lg gg Gi ha e dae Bae OPEN 2 AUTOMATIC DOORS ci eeii wiv ate e gayi e ya ediz dns AUTO FL UEEJD MPB oss nl as ah AS ase v a da e ACA ALM DOOR CLOSED Door must be opened to check the in tran
3. S O CHALLENGE F O RESPOND Taxi Check S O ACCOMPLISH amp ADVISE CAPT WHEN COMPLETED FLAP LEVERS sama ate SET FLT GND SWITCH FLT FLT DIR FLAGS RMls CHECKED CABIN PRESS amp TEMP SET YAW DAMPERS CHECKED ENG BLEED SWITCHES 1 amp 3 OPEN CONTROLS CHECKED 2 L amp R CLOSED SPEED BRAKE CKD FULL FWD PACKS ii Xo Os 2 ON FLAPS __ GREENLT APUMASTERSW OFF STABILIZER TRIM SET SW ON APU LIGHT OUT O DATA amp BUGS CKD SET RLAP LEVER S ak jk en eo eire BAS Qo ence ah eee d aat Gta Gare el a ee a cia ep Ja SET Move flap selector lever to desired takeoff flap position FLIGHT DIRECTOR FLAGS RMI S soos ek RR RR ee A ee Ee CHECKED 1 Place MODE SELECTOR in OFF position Use of the v bar command indicator is not recommended during takeoff 2 All warning flags should be out of view 3 Pitch and roll attitude information on the flight director indicator should reflect the aircraft attitude the ramp approximately 0 in the pitch and roll axis 4 The compass information displayed beneath the lubber line on the azimuth scale of the course indicators should agree with the opposite RMDI S Electric compasses should agree within 4 of each other and within 10 of the standby magnetic compass 5 Set the course arrow and heading marker as required
4. CHECKED S OPANEL CHECKED ENG BLEEDS SWITCH amp PACKS AS REQUIRED PO CS PR steer ues at ous CHECKED amp SET S O CHALLENGE F O RESPOND Taxi Check S O ACCOMPLISH amp ADVISE WHEN COMPLETED FLAP LEVER SET CABIN PRESS amp TEMP FLT DIR FLAGS RMIs CHECKED ENG BLEED SWITCHES YAW DAMPERS CHECKED 5 CHECKED 5 SPEED BRAKE CKD FULL FWD APU MASTER SW 5 __9 9 GREENLT APULIGHT STABILIZER TRIM SET SW ON DATA amp BAGS CKD SET SET 1 amp 3 OPEN 2LER CLOSED 2 ON OFF OUT S O CHALLENGE F O RESPOND Before Takeoff S O ACCOMPLISH amp ADVISE CAPT WHEN COMPLETED NOTE CAPT WILL CALL FOR BEFORE T O CHECKLIST WHEN T O CLEARANCE HAS BEEN RECEIVED OR IS IMMI NENT STROBE LIGHTS ON PITOT HEAT sce secur a a ON TRANSPONDER amp DME ON amp NORM T OANNOUNCEMENT FUEL PANEL iaoa aae Rs BOOST PUMPS CSD OIL COOLER COMPLETED SET GROUND OFF www captainsim com DO NOT US E FOR FLIGHT S O CHALLENGE PILOT NOT FLYING After Takeoff S O ACCOMPLISH amp ADVISE CAPT RESPOND WHEN COMPLETED NOSMOKE OFF AUTOPACKTRIP CUTOUT GEAR e OFF LTS OUT FUELP
5. ON ENG BLEED SWITCHES amp PACKS AS REQUIRED COCKPIT DOOR LOCKED ENGINE ANTI ICE To prevent surging during prolonged periods of ground operation increase power on each engine to 50 Ni minimum every 5 minutes Wing anti ice is used if TAT is 8 C or less and visible moisture is present If 1 fuel tank temperature is 0 C or less operate the fuel filter heaters for 1 minute before takeoff ELEC PANEL The following automatic paralleling sequence is based on an engine start sequence of 1 2 3 J AC METERS SELECTOR sa s cc cae sce a n kk a eee GEN 1 2 GENERATOR IFRE GUENCY aaa SET 3 GENERATOR IVOLTAGE hh nn 115 5 VOLTS 4 GENERATOR BREAKER 1 ee rs D CLOSED pb AC METERS SELECTOR i 2 uiui aed Je ie ro e ae i on o ag RR TE ee de ese un GEN 2 6 SYNCHRONIZINGLIGHTS aaa aaa CHECK TAGENERATOR 32 5 duis RUN ADR game aa CHECK REPEAT ITEMS 2 3 6 8 GENERATOR BREAKER 4 2 ss Rm hmm moon xk ka eee mm CLOSED 9 AC METERS SELECTOR i cuc aaa a 3 OE cR E boh er ead a eR OR RALIS GEN 3 10 GENERATOR 3 nnn CHECK REPEAT ITEMS 2 3 6 11 GENERATOR BREAKER AEE EEEE CLOSED 12 ESSENTIAL POWER selector to Gen 1 2 3 13 Check that essential power will hold on each generator 14 DC POWER SWITCH aaa sca sioi aoa iao LR a Rn MESE CHECKED Aft
6. n www captainsim com 11 DO NOT USE FOR FLIGHT FLIGHT RECORDER 2 2 cite arar a C aa ae De ot ee ee e ik a en ee TEST The flight recorders off light will be illuminated as the flight recorder will not work Hold button depressed for testing EMERGENCY EXIT WIGHT Ss nutu Rn ee BR eb ape Wie evaded atm Hee ee gi CAPPED CAP the EMERGENCY EXIT LIGHTS switch The emergency lights unarmed annunciator will go out Subsequent loss of either 115V AC or 28V AC essential power will illuminate the emergency exit lights ALTERNATE FLAPS af aS AP A la oo CUN M URE ah sae ah ded e ua e ea ar CAPPED amp 2 OFF The ALTERNATE FLAPS switch must be in the CAPPED OFF position for the flaps to operate hydraulically The INBOARD and OUTBOARD FLAP ALTERNATE CONTROL switches must be in the OFF position WINDOW HEAT SWITCHES a u aaa a hh hh ih n s n rs TEST amp ON For a functional test of the windshield overheat trip system 1 WINDOW HEAT SWITCHES ON 2 OVERHEAT TEST SWITCH PUSH 3 OVERHEATLIGHIS ON 4 WINDOW HEAT SWITCHES OFF RESET THEN ON vM ant Gl ete Goh ate and CKD amp 3 OFF A complete check of the anti ice systems will be made prior to the first flight of the day and whenever icing conditions are anticipated Prior t
7. DO NOT USE FOR FLIGHT FLIGHT MANUAL PART III Operations www captainsim com DO NOT USE FOR FLIGHT ABOUT THIS MANUAL VERSION 02 MARCH 2009 WARNING THIS MANUAL 15 DESIGNED FOR MICROSOFT FSX USE ONLY DO NOT USE FOR FLIGHT The 727 Captain FLIGHT MANUAL is organized into three Parts Each Part is provided as a separate Acrobat PDF document Part User s Manual Part II Aircraft Systems Part 111 Operations this document Adobe Acrobat amp Reader Required FOR GENERAL INFORMATION ON THE 727 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 727 100 PRO PACK FLIGHT MANUAL PART 111 OPERATIONS CONTENTS Page 4 COCKPIT APU START PROCEDURE 6 COCKPIT CHECK LIST 10 NORMAL PROCEDURES 10 RECEIVING AIRCRAFT CHECK PILOTS 13 RECEIVING AIRCRAFT CHECK SECOND OFFICER 16 BEFORE STARTING ENGINES 16 NORMAL ENGINE START 17 AFTER START 18 TAXI CHECK 19 TAKEOFF PROCEDURE 19 PRE TAKEOFF BRIEFING 21 ABNORMAL TAKEOFF 21 AFTER TAKEOFF 22 CLIMB CRUISE amp DESCENT 22 CLIMB 22 CRUISE 22 EMERGENCY DESCENT 22 AIRWORK 22 DECSENT 23 IN RANGE 23 NOTES 23 APPROACH CHECK 25 LANDING 25 LANDING PROCEDURES 27 ABNORMAL LANDING 27 GO AROUND PROCEDURES 27 AFTER LANDING 28 ARRIVAL PROCEDURES 29 APPENDIX 29 V1 VR V2 30 CLIMB P
8. or as the end of the runway disappears under the nose in visual flight conditions The high rates of sink that develop with this maneuver are not readily apparent on either the airspeed indicator or the vertical speed indicator and may not be noticed until the flare point at 50 feet Rapid rotation to stop a high sink rate is relatively ineffective since the induced G tends to offset the increase in lift Thrust must be added to decrease a high sink rate when holding the proper approach speed and using a normal rotation d The desired visual final approach condition is airspeed at target Vrer wind additive and 3 glade path that will result in main landing gear touchdown at 1 000 feet beyond the threshold When the desired condition is established maintain it to flare height Do not DUCK UNDER an established glide path near the runway threshold to achieve an early touchdown FLARE AND LANDI NG During visual approach the main landing gear should cross the runway threshold at 50 feet Main gear touchdown will occur just beyond 1 000 feet assuming the glide path angle is 39 Do not deviated from the glide path in an attempt touchdown sooner Flare results in a change in attitude of only 2 3 At light weights the change is hardly noticeable As soon as pilot observes response of the airplane to the flare the throttles should be retarded smoothly to idle and any back pressure on the control column relaxed CROSSWIND LANDING The CRAB
9. GAUGES STABILIZER amp CRUISE CKD amp ON START LEVERS Ctri Shift Fl CUT OFF AUTOPILOT e i ha bs OD ERS SE ES ya ia au DISENGAGE SYS A TRIM TTABS dE Ta at ee al CKD amp ZERO PARKING BRAKE yere ri ew Iu ala ee aera a km SET THROUGH STOP STATIONS FIRST FLIGHT OF DAY LOG BOOK NOTE AIR MIC ONLY GEAR LEVER amp WIGHT kA ESS ec a Y eR ER ed amp and be ew ae Res DOWN amp 3 GREEN The GEAR handle is in the DOWN detent and that the downlocks on all 3 gear are engaged tc ee hah ata neat nine WY b Gala Nera Ne Ta d GA s e ee usas edad Bae ela CHECKED Navigation and communication radio equipment should be checked and set for takeoff requirements FLIGHT CONTROL SWITCHES x Se a RACE ee ey wa X RU YR ROLE S 9 CAPPED Check that the AILERON SYSTEM A amp B SPOILER INBOARD and OUTBOARD ELEVATOR SYSTEM A amp B and RUDDER SYSTEM B switches are all CAPPED NAW DAMPER ee i ed entend ide eire bl li Sa a dur do ede 2 CAPPED STALL WARNING 4a ntt oe eee e OE hee A d aid dd eda dius alas TEST amp NORMAL Operate STALL WARNI NG TEST switch observe the stall warning power failure light goes out indicating the sensing vane heater will operate and that the control columns shake and the spinner rotates
10. PUMPS is weet iat at a ak a abet Mitac Oh ind ON SAYD QUANTITY ariane oo Be ee eren 3 CHECKED GROUND 1 CLOSED AYD SHUT OFFS asuman keke a a CAPPED HYD BRAKE 1 CAPPED OL QUANTITY gt i c e ie m TESTED amp CKD CABIN PRESS Sider ep Don EI dta cel ced i Gs SET TEMP CONTROLS mm CU edere iri odd SET ENG BLEEDS e a a RU RUE EE Eng eue a a 4 OPEN PACKS uuu urs s dus eae dut d E urbe a x door us AS REQUI RED COOLING DOORS wens s 1 5 m t iy e S AS REQUI RED PUBL DUMP its aaa DOOR CLOSED FHIGHT RECORDER zz kii Rem mm Rex n m SET A P GROUND TEST 2552 2 20000 00 kk n honos NORMAL APU FIRE CONTROL 1 CHECKED LEADING EDGE LIGHTS 0 000 000 0000 00008 TEST amp OFF CABIINUAIRS LEVERS c c te ede hal ad a li A deque AS REQUIRED FIRE DETECTION FAULT LIGHTS CHECKED PDUMBS ues iy tts aw AR A ACE ea ac ur aa Jae Ue fale 1 ON STANDBY POWER 3 ceo RR e oe ee ae i a RE OA UE E Re ee ake Se ne CHECKED 1 ESSENMALPOWERSELECTOR GEN 3 2OR 1 2 AUTO STANDBY POWER TEST SWITCH TEST Check For The Following
11. been cleared for takeoff Flight attendants please take their seats BOOST PUMPS tiie awa wa wad booed SSR WER Sava waded NUR RU RUR UR XL A lie ON This is final check to see that all boost pumps are ON the respective low pressure light are off the 2 CROSSFEED valve is OPEN and the fuel heaters are OFF THRUST SETTING Prior to brake release or as the airplane is aligned with the runway the pilot faying will smoothly advance all engine throttles Insure even spooling of the engines prior to applying takeoff power After brake release and off with the airplane aligned and rolling advance the throttles to the TAKEOFF EPR The pilot not flying will make final adjustments as required to obtain takeoff EPR before reaching 60 knots This normal takeoff procedure will assist in avoiding engine surge at of takeoff It is therefore recommended for all takeoff conditions to counteract adverse wind conditions particularly when crosswind guests or tailwinds exist TAKEOFF ROLL Once the aircraft is aligned on the runway the pilot flying will hold forward pressure on the control column and maintain directional control with rudder pedal steering CROSSWIND TAKEOFF 1 The pilot flying should gradually relax forward pressure on control column so as to arrive at Va prepared to rotate 2 At Vp rotate the airplane smoothly to the takeoff attitude of approximately 13 The rate of rotation should be 2 per second When t
12. dtu oh he aid yar Sateen ce s dr Gee fo dk hod dl deed hide be eran ROTATION CHECKED 17 START LEVER AT 15 MINIMUM 20 5 IDLE T8 INUTIAE FUEL FLOW ocak eee eae dame eat he ii APPROX 900 1000 PPH TO EGT d im dese perve ae e Mayan wire bed un do d dad Peete a a Wide sro ud ami aera RISING 20 START SWITCH AFTER 35 AND BEFORE 40 RELEASE TO OFF NOTE Second Officer observes increase in pneumatic pressure and reports START VALVE CLOSED 21 ONL PRESSURE LOW LIGHT aia ea dos ada RD e te rn d de an en e i OUT 22 Idle stabilized observe the following a Ni sx er S WE ite t 30 3296 DON imi e e e ede et ad tra niti as 50 5 58 GEGT yaaa 380 C OR 480 C MAX d FUELFLOW 900 1000 PPH e OILPRESSURE 40 55 PSI 23 Repeat seguence for other engines 2009 Captain Sim www captainsim com DO NOT USE FOR FLIGHT AFTER START F O CHALLENGE CAPT RESPOND After Start S O ACCOMPLISH amp ADVISE CAPT WHEN COMPLETED START LEVERS Xi ve IDLE GALLERY POWER ON TRANSPONDER STANDBY ELEC PANEL asuman CHECKED S O PANEL amp DOOR LIGHTS CHECKED FUELPANEL SET ENGANTI ICE AS REQUIRED HYDSYSTENS CHECKED STERILE COCKPIT LIGHT
13. for the departure clearance CONTROLS iu ok Satie eee aw GS xU e cR eek aide ed a bg aed CHECKED The captain will make the rudder portion of the control check The first Officer will make the aileron and elevator portion of the control check SPEED BRAKE irc EHE RUM a E EE mje is eto Bde aL ae se oe ae Dow CHECKED amp FULL FORWARD FLAPS cea 444300000 madd ilemi 44 __ __ GREEN LT Check that the flap position as shown on the date card agrees with the flap gauges and the green leading edge flap light is illuminated O DATA amp BUGS esu m Ox eRe RT AR RE Ee SOR d CHECKED SET Vi Vr and V2 speed are checked for the ambient temperature and gross weight altitude runway slope wind and flap setting to be used An external bug will be set on V Manually set the internal bug on V2 The remaining external bugs will be set on minimum maneuvering speeds as indicated on the data card TAXI NOTES Make all turns at a slow taxi speed Steering When the aircraft is stationary it is recommended that it be allowed to move forward with the nose wheel straight centered a short distance before turning the nose wheel Powerback Powerback is authorized at specified gates at the selected airports Do not use brakes when aircraft is in rearward motion Do not exceed 80 N during Powerback Taxi Speed Use of reverse thrust from the 2 engine is permitted to aid to contr
14. technique will be utilized and permits holding the wings level throughout the approach touchdown and landing roll O n final approach a crab angle is established to hold the airplane on www captainsim com 26 DO NOT USE FOR FLIGHT the desired truck until just prior to then remove the crab and align the airplane with the runway centerline As the rudder is applied the upwind wing will sweep forward developing roll Hold the wings level by simultaneous application of aileron into the wind The touchdown is made with cross controls The aileron can be held nearly constant during touchdown and start of landing roll Maintain directional control with rudder and use aileron as necessary to hold the wings level A slight wing down condition is acceptable BOUNCED LANDING In the event of a bounced landing hold or re establish normal landing attitude Add thrust as necessary to control the sink rate Do not push over as this may cause a second bounce and possibly damage the nose gear SPEED BRAKES When landing in adverse weather conditions rapid lowering of nose after touchdown and immediate application of speed brakes reverse thrust and brakes will result in minimum landing roll During normal weather conditions the speed brakes can be fully raised after touchdown while the nose wheel is being lowered to the runway with no adverse pitch effects The Captain will normally apply the speed brakes The pilot flying upon ap
15. 0 feet above and at each 100 foot increment thereafter call out altitude Deviations from target airspeed and rate of descent I E 400 feet plus 3 sink 700 C Call Approaching minimums approximately 100 feet prior to DH or MDA as applicable d Call runway in sight when appropriate e non precision approach call missed approach point as appropriate f Altitude call outs for non precision approaches and Category precision will be made off the barometric altimeters g Refer to the Category II discussion later in this chapter for special call out procedures www captainsim com DO NOT USE FOR FLIGHT LANDING S O CHALLENGE PILOT NOT FLYING RESPOND Landing S O ACCOMPLISH amp ADVISE CAPT WHEN COMPLETED DOWN 3 GREEN HYD PRESSURES CHECKED SMOKE ON START SWITCHES FLIGHT START ANTI 5 2 REL 5 REL SPEED BRAKE FULL FORWARD 5 __ GREEN LIGHT NOTE The Second Officer will make the P A Flight attendants please be seated for landing when the gear is extended LANDING PROCEDURES MANEUVERING SPEEDS The normal maneuvering speed for each flap position is shown on the profiles in this manual These speeds were selected considering bank angle capability airplane pitch attitude and thrust required They allow normal maneuvering 30 ban
16. 3 124 137 150 119 120 133 140 114 115 129 130 109 110 124 120 105 106 120 www captainsim com DO NOT USE FOR FLIGHT CLIMB PERFORMANCE SEE LEVEL ALL ENGINES OPERATING TAKEOFF GROSS WEIGHT 2ND SEGMENT RATE OF CLIMB 2ND SEGMENT RATE OF CLI MB LB V2 10 AT 200 KN FT MIN FT MIN 140 000 2790 3480 150 000 2560 3120 160 000 2340 2850 170 000 2180 2640 180 000 2020 2420 190 000 1880 2190 5000 FT ALL ENGINES OPERATING TAKEOFF GROSS WEIGHT 2ND SEGMENT RATE OF CLIMB 2ND SEGMENT RATE OF CLI MB LB V2 10 AT 200 KN FT MIN FT MIN 140 000 2350 2600 150 000 2100 2300 160 000 1960 2070 170 000 1820 1910 180 000 1610 1740 190 000 1350 1550 200 kn or minimum maneuver whichever is higher NORMAL Vrer AND MANEUVERING SPEEDS GROSS WEI GHT x1000 NOTE Minimum Ve 112 Kts www captainsim com DO NOT USE FOR FLIGHT CUSTOMER SUPPORT For Customer Support please visit http www captainsim com support Thank you Enjoy your flight Captain Sim Team www captainsim com www captainsim com
17. ALLS POSITION AND HOLD ONLY UNTIL LIGHTS ILLUMINATE ENGINE FIRE WARNING 5 ILLUMINATE FIRE ALARM BEUL 2s kk RR REE EG i A RR RR ee ee RR RINGS FIRE ALARM BELL CUTOUT 5 PRESS FIRE ALARM BELL Br ark kala a a a ae l o e STOP RINGING EMERGENCE BRAKE amp 55 OFF amp CHECKED Check that the PNEUMATIC BRAKE lever is safeties in the OFF position and pressure available is 1200 PSI 1100 DSI minimum FET INSTRUMENTS oa irrits si oon Ren ee ee ae de EO E e UR ce e m CHECKED ALTLMETERS amp CLOCKS si bekikbiusassma asbtininsmdepenmmesas didilidsssedi ai SET Electrical Altimeters Set local barometric correction and check within allowable tolerances Standby Altimeters Set local barometric correction and check within allowable tolerances Vibrator should be operating Altitude Alert Select an altitude at least 1 000 ft above field elevation Depress and slowly rotate the ALTITUDE SELECTOR in a COUNTERCLOCKWISE direction The alert lights will come on about 900 feet above the field elevation and go out about 300 feet above the field elevation Slowly rotate the ALTITUDE SELECTOR in a CLOCKWISE direction The alert lights will come on about 900 feet above the field elevation and remain on for all altitudes above that point Beeper will sound mom
18. ANEL SET FLAPS te UP LTS OUT TANLESKID sess te aa ee RETRACTED CABIN PRESS amp TEMP SET NOTE CAPTAIN WILL ASCERTAIN PROPER TIME TO TURN STERILE COCKPIT LIGHT OFF NORMALLY 10 000 S O ACCOMPLISH amp ADVISE CAPT WHEN COMPLETED Range S O CHALLENGE PILOT NOT FLYING In RESPOND SEAT BEET vw ae aes ON ANTI rs AS REQUIRED ALTIMETERS amp AIRSPEEDS SET amp CKD REFERENCE SPEEDS CKD amp SET NOTE CAPTAIN WILL ASCERTAIN PROPER TIME TO TURN STERILE COCKPIT LIGHT ON NORMALLY 10 000 FUELPANEL SET HYDSYSTENS CHECKED CABINPRESSURE SET COOLINGDOORS AS REQUIRED S O CHALLENGE PILOT NOT FLYING RESPOND Approach RADIOS COURSE ARROW CKD amp IDENTIFIED INBOUND COURSE S O ACCOMPLISH amp ADVISE CAPT WHEN COMPLETED Landing MODE SELECTOR SET ALTIMETER BUGS SET ADF VOR SWITCHES AS REQUIRED MARKER SWITCHES ON amp LOW WARNING FLAGS CHECKED S O CHALLENGE PILOT NOT FLYING RESPOND DOWN 3 GREEN SMOKE ON ANTI SKID a ue es kx aa 2 REL 5 REL SPEED BRAKE FULL FORWARD 5 __O GREEN LIGHT HYD PRESSURES START SWITCHES CHECKED FLIGHT START S O CHALLENGE F O RESPOND After Landing S O ACCOM
19. ERFORMANCE 30 5000 FT ALL ENGINES OPERATING 30 NORMAL VREF AND MANEUVERING SPEEDS 31 CUSTOMER SUPPORT www captainsim com DO NOT USE FOR FLIGHT COCKPIT APU START PROCEDURE 1 BATTERY SWITCH 5 eR GOOG dA KAA had ae ow dod oed ded de a p oe ode adus dude ON VOLTAGE 23 5 MIN 2 APU FIRE WARNING IF FIRST FLIGHT OF DAY sse hn TEST TEST PROCEDURE APU FIRE WARNING TEST PRIOR TO APU START a APU AUTOMATIC SHUTDOWN 5 ARMED b APU FIRE WARNING TEST RESET 5 2 FIRE TEST AND HOLD ONLY UNTIL THE FIRE WARNING LTS ILLUMI NATE MAX 60 SEC c APU FIRE WARNING TEST RESETSWITCH an RESET d APU FIRE WARNING TEST RESET 5 RESET END OF TEST PROCEDURE 3 AC METERS SELECTIONS aia oe ei ae os Ut EU Pe Reel de et ee a ef tace APU 4 AIR CONDITI ONING PACK SWITCHES FNOELECTRICALPOWERONA C hh s hh n n OFF The PACK switches are checked OFF to prevent high initial electrical loads from the pack cooling fans when APU of external power is connected 5 APU CONTROL PANEL uus Rd Remis Row kk m RR UR Re Ak LR ACA AL CHECKED a APU FIRE HANDLE maa aaa e eR ea ACE a ae mili CHECK IN b APU AUTOMATIC FIRE SHUTDOWN 5 1 CHECK ARMED c GENERATOR FIELD
20. HES 9 CAPPED YAW DAMPERS 22 3 2 HE Lad Wa ad a da dde 2 CAPPED ANTI SKIBD Mamak Sh SR E erede TEST CAPPED STALL WARNING coii doct ood es m ees dn TEST amp NORMAL FLIGHT RECORDER ii doen nom e monde ric TEST VOICE RECORDER sss ge x Ed dct e 8 TEST EMERGENCY 5 CAPPED START SWITCHES ei a ai mn mm me OFF ALTERNATE FLAPS 5 2 5 uoo wea a E CAPPED amp 2 OFF NO SMOKE SEAT 1 ON GROUND PROX isse eu wc uses de ii ddd a Ee Rt TEST WINDOW HEAT eki e RO mel ede nue ine TEST amp ON SA ANIMI ICE uiu Rr Re ONSE ERR Rehd dede e ees CKD amp 3 OFF EXTERIOR LIGHTS uii tut tos dones S dcs RIS ROS e qos sz ah AS REQUIRED FIRECONTROLPANEL 0 000 CHECKED MACH WARNING oo xeu kn ene a a e a TEST EMERGENCYBRAKEG amp PRESS OFF amp CKD FLTINSTRUMEN S 0 CHECKED ALTIMETERS amp 5 SET STATIC SOURCES Ee raaigras te alete e aa auem erc des NORMAL WARNING amp OPERATINGLIGHTS TEST RADAR Gamma di a i a a a AA TEST STBY SPEED BRAKE LE EG og e iie in es FULL FORWARD THROTTEES ie a ata eee I s FREE amp CLOSED FLAP LEVER aa REOR i say Ge a ce a E RC e n gata WITH
21. Indications Steady red essential power failure light on S O panel Captain s GYRO flag not visible Captain s RMDI OFF flag not visible Standby horizon flag not visible 3 AUTO STANDBY POWER TEST SWITCH RELEASE 4 ESSENTIAL POWER SELECTOR STANDBY Check For The Same Indications As In Step 2 5 ESSENTIAL POWER SELECTOR APU EXT BATTERY CONDITION use te Rae OS Rx a Q3 USC IRURE RORIS OR CR a RR ORC CHECKED This check is to be accomplished on the first flight of the day only 1 BATTERY CHARGER ss PULL Sim www captainsim com 14 DO NOT USE FOR FLIGHT 2 ESSENTIAL BUS TIE C B eei ewe ee o Pa OER EE OSE a i PULL 3 ESSENTALPOWERSELECTOR te eee STANDBY 4 Check that the Captain s GYRO flag not visible 5 DC METERS SELECTOR iia ise sede Mein A ale A eo a a a lk BAT BATTERY VOLTS 23 5 MINIMUM 6 BATTERY CHARGER AND ESSENTIAL BUS TIE 5 RESENT BATTERY AMPS ace X OO R aaa aa idi OBSERVE CHARGING Charging will be steady on external power and pulsing on APU 7 ESSENMALPOWERSELECTOR en APU EXT BATTERY SWITCH icc ns cee eae we Sea ee Rea RE RR AMAR AR RRR CR OR A UR EA ka km ON GALLEY POMER 22 ee Rr a ak yk gn ak ead Bla l le ak
22. PLISH amp ADVISE CAPT WHEN COMPLETED NOTE INITIATED ON CAPTAIN S COMMANDS W HEN CLEAR OF ACTIVE RUNWAY ICE 222232333243 ag ALL OFF RADAR TRANSPONDER DME STANDBY SPEED BRAKE i RA FULL FWD FLAPS s toc see mas same Bi Rog AL UP STAB TRIM aker 5 UNITS STROBELIGHTS OFF AC METERS SELECTOR SW APU ELECTRICALLOAD REDUCE AIR CONDITIONING AS REQUIRED APU xau x xxr xxx du dd START ESSENTIAL POWER APU www captainsim com DO NOT USE FOR FLIGHT F O CHALLENGE CAPT RESPOND Parking S ACCOMPLISH amp ADVISE CAPT WHEN COMPLETED PARKING BRAKE SET APU EXTERNAL POWER ON BUS STERILE COCKPIT LIGHT OFF GALLERY POWER ON SEAT BELT ceo tee ens OFF BOOST PUMPS OFF EMER EXIT LIGHTS AS REQUIRED BY PUMPS sx ERES FLIGHT RECORDER TEST ENG BLEEDS eva x 4 VOICE RECORDER TEST PARKS 2 AS REQUIRED RADAR amp TRANSPONDER OFF START LEVERS Ctrl Shift F1 CUTOFF www captainsim com DO NOT USE FOR FLIGHT NORMAL PROCEDURES RECEIVING AIRCRAFT CHECK PILOTS F O CHALLENGE CAPTAIN RESPOND GEAR LEVER amp LIGHT 19 a e e ae lili DOWN amp 3 GREEN RADIOS zi sini xs Romam ee une An iv lg CHECKED FLIGHT CONTROL SWITC
23. R FLIGHT engine driven generator s GEN BREAKERS if either were supplying the bus 15 ESSENTIAL POWER 5 APU CHECK ESSENTIAL POWER LIGHT OUT The 3 BUS TIE BREAKER must be CLOSED 16 VOLTAGE FREQUENCY AND 5 CHECK UNDER LOAD Electrical power during pre flight throughout engine start is normally furnished by the APU External power may be connected through the external power receptacle as an alternate source of electrical power Normal ground or flight operation is with the busses in parallel BUS TIA BREAKERS CLOSED lights out and operating as a synchronous bus www captainsim com DO NOT USE FOR FLIGHT COCKPIT CHECK LIST Pilots S O F O CHALLENGE CAPT RESPOND Receiving Aircraft F O CHALLENGE S O RESPOND GEAR LEVER amp LIGHT DOWN amp 3 GREEN CIRCUIT BREAKERS CHECKED RADIOS uem miens CHECKED CREW amp PASS OXYGEN CKD amp FLIGHT CONTROL SWITCHES 9 CAPPED NORMAL YAW DAMPERS 2 CAPPED STANDBY POWER CHECKED ANTI SKID CAPPED LIGHTS OUT BATTERY CONDITION CHECKED STALL WARNING TEST amp NORMAL GALLEY POWER ON FLIGHT RECORDER TEST BATTERY SWITCH ON VOICE RECORDER TEST DCPOWER CHECKED EMERGENCY EXIT LIGHTS CAPPED GEN DRIVE TEMPSW IN S
24. R LEVER AS REQUIRED FIRE DETECTION FAULT LIGHTS CHECKED B PUMPS 1 ON THROUGH STOP STATIONS FIRST FLIGHT OF DAY LOG BOOK NOTE AIR MIC ONLY F O CHALLENGE CAPT RESPOND Before Start F O CHALLENGE S O RESPOND FUEL QUANTITY CHECKED PACKS S X eae eee ees OFF ON GALLERY POWER OFF PARKING BRAKE AS REQUIRED BOOST PUMPS AS DOOR LIGHTS CHECKED REQUIRED PNEUMATIC PRESSURE MINIMUM FOR START www captainsim com DO NOT USE FOR FLIGHT CHALLENGE CAPT RESPOND After Start S O ACCOMPLISH amp ADVISE CAPT WHEN COMPLETED STARTLEVERS IDLE TRANSPONDER STANDBY S O PANEL amp DOOR LIGHTS CHECKED ENGANTI ICE AS REQUI STERILE COCKPIT LIGHT ON GALLERY POWER ON ELECPANEL CHECKED FUEL PANEL si ves eas SET RED HYDSYSTEMS CHECKED ENG BLEED SWITCHES amp AS REQUIRED PACKS COCKPITDOOR LOCKED F O CHALLENGE CAPT RESPOND Delayed Engine Start F O CHALLENGE S O RESPOND AFTER ENGINE STARTED START ENG BLEEDS PNEUMATIC PRESSURE NOTE APU WILL BE USED FOR DELAYED ENGINE OFF 4 OPEN MINIMUM FOR START AFTER ENGINE STARTED S O ACCOMPLISH AND ADVICE CAPTAIN WHEN COMPLETED START LEVER IDLE ELECPANEL
25. TART SWITCHES OFF GEN acsi doa aed CHECKED ALTERNATEFLAPS CAPPED amp 2 OFF FUEL QUANTITY TEST amp AMT NO SMOKE SEAT BELT ON ENG FUEL VALVES OPEN GROUND PROX TEST CAPPED iii sa tae ina Ria eme AS WINDOW HEAT TEST amp ON REQUIRED PANT CE caedes CKD amp 3 OFF PUMPS uiu se emn ON EXTERIOR LIGHTS AS REQUIRED HYDOUANTITY 3 CHECKED FIRE CONTROL PANEL CHECKED GROUND INTERCONNECT CLOSED EMERGENCY BRAKE amp PRESS OFF amp CKD HYD SHUT OFFS CAPPED FLT INSTRUMENTS CHECKED BRAKE INTERCONNECT CAPPED ALTIMETERS amp CLOCKS SET OILOGUANTITIY TESTED amp STATICSOURCES NORMAL CKD WARNING amp OPERATING TEST CABINPRESS SET LIGHTS TEMPCONTROLS SET SPEEDBRAKE FULL FORWARD ENGBLEEDS 4 OPEN THROTTLES FREE amp CLOSED PACKS c e en aed dee e AS FLAP LEVER e usi akon eons WITH GAUGES REQUIRED STABILIZER amp CRUISE TRIM CKD amp ON COOLING DOORS AS START LEVERS CUT OFF REQUIRED Ctri Shift F1 FUELDUMP DOOR AUTOPILOT sia a a a DISENGAGE SYS A CLOSED TRIM 5 CKD amp ZERO FLIGHT RECORDER SET PARKING BRAKE SET APU FIRE CONTROL PANEL CHECKED hb LEADING EDGE LIGHTS TEST amp OFF CABIN AI
26. an prior to entering an airport traffic area Further speed redactions and configuration changes should be planned in order to be of F15 man jast prior to turning base leg or intercepting the glide path Gear and flaps will be extended at speeds of 10 to 15 knots below placard speed when conditions permit Speed redactions below FO minimum maneuvering airspeed will be accomplished by flap extension to conform to the following minimum maneuvering airspeed Flaps Speed 0 FO Man 2 F29 Man 159 F159 Man 10 Kts 25 F15 Man 30 VREF 10 Kts Normally the landing gear should not be extended until after at least 5 of flaps have been extended When cleared for on approach in IFR conditions the pilot flying request an approach check Approaching the glideslope on a manually flown or coupled ILS the pilot flying should call for flaps 25 gear down flaps 30 when the gear is down and locked AND LANDING CHECKLIST This will result in minimal trim and power change requirements On other types of instrument approaches the facility and minimums may dictate the point at which the final landing flap configuration is established On a visual approach final landing configurations should be established so as to be stabilized no later than 500 AGL Altitude call outs CAT I non precision and visual approaches The pilot not flying will a At 1000 feet above touchdown zone elevation TDZE call out 1000 feet b At 50
27. e ON DC POWER mss ved aa eta sat atk wn e dad MA edn ak ah Ga e Mb OM dee CHECKED 1 DCMETERSSELECTOR CHECK EACH T R volts 24 6 to 27 8 Amps positive indication 50 max 2 DC METERS SELECTOR e ee ee awa UR UR TUUS med ESS T R GEN DRIVE TEMP SW 6x isa di DRA RR Be ub iei qc RR dieci a e Ee b RR d IN GEN amli CHECKED Check all generator breaker lights illuminated Bus tie breaker lights and generator field lights should be out EVEL QUANTITY e amam pi a A A A AEE a aaa a A ae TESTED amp AMOUNT Turn forward boost pumps in all tanks on Check that only the forward boost pumps low pressure lights are out Turn forward boost pumps off and the aft boost pumps on Check that only the aft boost pumps low pressure lights are out Turn the aft boost pumps off X FEEDS Ge ede ee ona ee de 2 OPEN 1 amp 3 CLOSED Move each CROSSFEED VALVE switch it OPEN and then to CLOSE Check that the respective in transit light illuminates and then goes out as the valve reaches the selected position The 2 crossfeed valve is left open for start taxi takeoff and landing FHYDRAULIC QUANTITY s 2 64 8 ep Mia add ae Be RR RM Cid tal tales Mei 3 CHECKED System A quantity should be approximately 4 4 gallons full and 3 gallons minimum System quantity should be appro
28. entarily each time the altitude alert lights illuminate Allow the ALTITUDE SELECTOR knob to spring out to its normal position and select the enroute flight plan altitude Radio Altimeters Test check 250 10 feet failure flag WARNING amp OPERATING LIGHTS 2 0 ee TEST In the TEST position the following lights should illuminate 1 nre disengage Es controls Autopilot elevator low pressure Stabilizer out of trim Reverses Engine low oil pressure Leading edge devices Landing gear amp doors Essential power failure Engine fire bottle discharged 12 Engine failure detection Marker beacon lights approach progress display lights and the instrument comparator lights must be tested separately 2 D 3 4 5 6 7 8 9 10 11 MIR ES prre ke SE P E AE ate ote a a ge a a FREE amp CLOSED Check throttles for full movement FLAP LEVER ii e a a eae aoe ear a PG a we ae a Gonna ee WITH GAUGES The FLAP lever should be at ZERO with the inboard and outboard flap gauges in agreement STABIEHIZER amp CRUISE xx aa eee RR eek CHECKED amp ON AUTOPIEQT isa ox a bir e Go a pl dom oe a Gar ii DISENGAGE SYSTEM A www captainsim com 13 DO NOT USE FOR FLIGHT This is the check that the AUTOPILOT AILERON and ELEVATOR switches on the autopilot control panel are in the DISENGAGED position and the war
29. er generators on Bus 15 GALLERY De cS Oe ebro ON T6 ELECTRICAL SYSTEM ira e nc n BOR WWE a aa a ae ce rrr CHECK a All lights off b KW amp KVAR within tolerance c CSD TEMPERATURE SELECTOR switch RISE then IN EVEL PANEL gus e eee e Te s OREN A BLS Maes aw D e V RD Ra kag GR SET Fuel is being supplied tank to engine All boost pumps should be on and the 2 crossfeed valve open HYDRAULIC SYSTEMS oi 3S RR RR ERR E RE Oh a eS Be eae Soe RC CHECKED Check that both system A PUMPS switches are ON both pump low pressure lights are out and ground interconnect closed Turn on remaining system B pump and check that its low pressure lights goes out ENGINE BLEED SWITCHES AND 5 a AS REQUIRED 1 ENGINE 2 BLEED AIR SWITCHES llle en CLOSE 2 LEFT AIR CONDITIONS PACK SWITCH eer ON 3 COCKPIT AIR CONDITIONS CHECK FOR AIR FLOW 4 LEFT PACK TEMPERATURE 1 1 MONI TOR FOR CHANGE After APU is SHUTDOWN 5 RIGHT AIR CONDITION PACK 5 1 ON 6 RIGHT PACK TEMPERATURE MONITOR FOR CHANGE Sim www captainsim com 18 DO NOT USE FOR FLIGHT TAXI CHECK
30. gine may also be shut down depending on taxi or delay considerations 2009 Captain Sim www captainsim com 727 Captain FLIGHT MANUAL Part 111 Operations 28 DO NOT USE FOR FLIGHT ARRIVAL PROCEDURES F O CHALLENGE CAPT RESPOND Parking S O ACCOMPLISH amp ADVISE CAPT WHEN COMPLETED PARKING BRAKE SET APU EXTERNAL POWER ON BUS STERILE COCKPIT LIGHT OFF GALLERY POWER ON SEAT BEL rana OFF BOOSTPUMPS OFF EMERGENCY EXITLIGHTS AS REQUIRED B PUMPBSs siri a ers OFF FLIGHT RECORDER TEST ENG BLEEDS sics cee aw 4 OPEN VOICE RECORDER TEST PARKS uae AS REQUIRED RADAR amp TRANSPONDER OFF START LEVERS Ctrl Shift F1 CUTOFF BEACON Sise OFF CREW CHANGE STATIONS 2009 Captain Sim www captainsim com FLAPS 15 25 DO NOT USE FOR FLIGHT APPENDIX 29 GROSS WEIGHT Vi Vr V2 x 1000 LB 210 165 166 175 200 161 162 171 190 156 157 167 180 151 152 163 170 146 147 159 160 140 141 153 150 135 136 149 140 129 130 145 130 124 125 139 120 119 120 134 210 156 157 166 200 152 153 162 190 147 148 158 180 142 143 154 170 137 138 150 160 132 133 145 150 127 128 141 140 122 123 137 130 117 118 132 120 112 113 127 210 146 147 157 200 142 143 153 190 137 138 149 180 133 134 145 170 128 129 141 160 12
31. he airplane is rotated at the proper rate liftoff will normally occur at approximately 10 of body angle The total time to rotate from Va to the initial climb attitude should be about 7 seconds 3 Excessive rate of rotation must be avoided If the rate of rotation exceeds the proper values it is possible to reach an attitude that will cause the tail skid to contact the runway before the airplane can liftoff www captainsim com 20 DO NOT USE FOR FLIGHT LIFTOFF AND INITIAL CLIMB 1 The airplane will attain V 10 approximately 35 feet above the runway 2 Gear retraction will not be initiated until positive rate of climb has been verified on the VSI and altimeter and CALLED by either pilot Until ground effect pressure is dissipated there may be a slight delay for these instruments read correctly 3 Do not apply brakes after becoming airborne 4 Adjust pitch attitude to maintain desired airspeed Because acceleration continues throughout the takeoff a false nose high attitude up to 49 could be indicated on the horizon display if the vertical gyro does not have pitch erection cutout 5 Target speed with takeoff flaps 259 15 or 59 should be V 10 knots This speed is very close to the maximum angle of climb maximum altitude in minimum distance for the takeoff flaps used 6 I nitial climb attitude amp takeoff profile The normal Initial climb attitude will vary from 11 to 15 max 20 The attit
32. ing of 15 When either pilot verifies and calls a positive rate of climb a GEAR UP call is made by the pilot flying If during the initial phase of the go ground a positive rate of climb is established prior to Vrer 10 the gear may be retracted before retracting the flaps to 15 Pitch should be adjusted so as to maintain Vrer 10 knots Unless otherwise specified in the missed approach procedure a turn should not be made until a minimum of 800 feet AGL is reached If a close in turn to a missed approach course is required maneuvering at F15 man will result in optimum turn radius and climb performance Where appropriate the aircraft should be established on the missed approach course and at missed approach altitude prior to further acceleration and clean up AFTER LANDING S O CHALLENGE F O RESPOND After Landing S O ACCOMPLISH amp ADVISE CAPT WHEN COMPLETED NOTE INITIATED ON CAPTAIN S COMMANDS WHEN CLEAR OF ACTIVE RUNWAY ANTI ICE 2223232 RS ALL OFF AC METERS SELECTOR SW APU RADAR TRANSPONDER DME STANDBY ELECTRICAL LOAD REDUCE SPEED BRAKE FULL FWD AIR CONDITIONING AS REQUIRED BARS uus A d Rus UP APU cus sx Gus EORR START STAB TRIM ru Res 5 UNITS ESSENTIAL POWER APU STROBE LIGHTS OFF NOTE For fuel conservation consider shutting down the 3 engine for taxi when conditions permit In addition 1 en
33. k throughout the approach APPROACH PATTERN The illustrated pattern represents the ideal approach situation Flap and landing gear extension points were selected to minimize crew workload and thrust changes during the approach Airplane must be stabilized on final approach at least 500 feet above field elevation FINAL APPROACH a Once landing flap have been established target speeds will be Vree 5 knots However the decrease in wind velocity approaching the surface of the earth has the effect of a decrease in airplane velocity Consequently caution must be exercised to prevent airspeed bleed of and increased sink rate during the last stage of the approach Target approach speed is Vrer 5 knots for landing in reported winds of zero to light and variable up to 10 knots When landing in higher wind conditions add the steady headwind and the full value of the gust to Vper The total wind additive should not exceed 20 knots b The pilot should aim for a constant angle relationship with the 1 000 ft mark on the runway coordinating pitch attitude and power changes As the end of the runway and then 1 000 ft mark disappear under the nose maintain the stabilized attitude around 2 3 nose up and power setting that have made good this constant angle until the 50 foot level is reached c The pilot should restrain himself from the tendency to DIVE at the runway when breaking clear of the clouds allow altitude under instrument conditions
34. l may be difficult On a wet or slippery runway use normal on the center engine www captainsim com 727 Captain FLIGHT MANUAL Part 111 Operations 27 DO NOT USE FOR FLIGHT ABNORMAL LANDING ONE ENGINE INOPERATI VE Landing with one engine inoperative is the same as a normal landing except Vrer 10 knots is maintained after extension of landing flaps TWO ENGINE I NOPERATI VE 1 landing Pattern preparations and procedure are illustrated on the TWO ENG NE INOPERATI VE LANDING profile in the approach procedures 2 Final Approach Extend the landing gear when starting decent Commit point is gear extension Extend the flap to 5 Plan a bleeding airspeed final approach so as to cross the threshold at the two engine inoperative Vrer wind additive Use of rudder trim during landing is at the option of the pilot GO AROUND PROCEDURES A If the decision is made to go around during a circling approach the missed approach specified for the approach procedure utilized to get to the airport must be followed To become established on the prescribed missed approach course make an initial climbing turn toward the landing runway and continue the turn until established on the missed approach course B To execute a go around SIMULTANEOUSLY apply power call for flaps 25 and smoothly rotate the aircraft to a minimum pitch setting of 10 at an approximate rotation rate of 2 sec At Vrer 10 call for a flap sett
35. lled back rapidly until the spring force buildup becomes limiting and then held in this position until the desired results are achieved Generally try to achieve about 84 Ni RPM Prompt application of reverse thrust will provide for max deceleration at touchdown speed when reversing is most effective b The Second Officer will monitor reverse and call out only 1 Engine s that fail to spool or no light 2 RPM in excess of 85 96 3 80 knots when aircraft decelerates through 80 knots c Below O F immediately ease the reverse thrust levers forward to the 70 knots detent Above O F ease the reverse thrust levers forward to the 70 knots detent at approximately 70 knots while using moderate wheel braking The reverse thrust levers may be left in the 70 knots detent until the aircraft is fully stopped without engine surging Normally however the reverse thrust levers are modulated forward with decreasing speed to full forward and down at approximately 10 to 15 knots d Rudder control is effective down to approximately50 knots This combined with rudder pedal steering is usually sufficient for maintaining directional control during the rollout Maintain the wings level DIRECTIONAL CONTROL DURING REVERSING On dry runway directional control is easily maintained by nose wheel steering through the rudder pedals However when the runway is wet or slippery and the effectiveness of nose will steering is reduced directional contro
36. n each position except T PROBE AUX P where reading may be slightly different c PITOT HEAT SWITCHES io ia eR RR b gideli ask ae OR 5 OFF Observe HEATER OFF light illuminate FIRE CONTROL PANEL e i ec tate aca RR a ei ox OS ee ken ae Roe RR ne CHECKED FIRE HANDLESS 3 23323 22 ER mE E eee s pomum RR ee ake AD RD AD ER 3 FULL IN 2 BOTTLE TRANSFER 5 1 LEFT 3 ENGINES AND WHEEL WELL FIRE DETECTION SYSTEMS TEST FIRE TEST SWITCH Shift F HOLD IN ENGS amp WHEEL WELLS POSITION Wheel well fire warning ON IMMEDIATELY Fire alarm bell aaau RINGS IMMEDIATELY While Continuing to Hold the Fire Test Switch b FIRE ALARM BELL CUTOUT SWITCH Shift B PRESS Wheel well fire warning REMAINS ON www captainsim com 12 DO NOT USE FOR FLIGHT Firealarmbell ee STOP RINGING Continuing to Hold the Fire Test Switch ENGINE FIRE WARNING 5 ILLUMINATE d FIRE ALARM BER L doa sar GO Am m De b a e ts es ea RINGS AGAIN e FIRE TEST SWITCH 5 RELEASE IMMEDIATELY 4 FIREWALLS DETECTION SYSTEM 1 1 hinh hs TEST FIRE TEST SWITCH Shift F FIREW
37. necessary 2009 Captain Sim www captainsim com 727 Captain FLIGHT MANUAL Part 111 Operations 23 DO NOT USE FOR FLIGHT S O CHALLENGE PILOT NOT In Range S ACCOMPLISH amp ADVISE CAPT FLYING RESPOND WHEN COMPLETED SEAT BELT iceus tasasi ON FUEL PANEL RES SET GBs eta s AS REQUI RED HYD SYSTEMS c Rn CHECKED ALTIMETERS amp AIRSPEEDS SET amp CKD CABIN PRESSURE SET REFERENCE SPEEDS CKD amp SET COOLING DOORS AS REQUIRED NOTE CAPTAIN WILL ASCERTAIN PROPER TIME TO TURN STERILE COCKPIT LIGHT ON NORMALLY 10 000 NOTES Holding Planning Make all turns during entry and while holding at 1 30 bank angle or 2 25 bank angle using the flight director system Configurations Above 14 000 feet hold clean and used PDCS or chart speed At or Below 14 000 feet extensive holds should be made in the clean configuration Maximum Airspeeds a Sea level 6 000 ft MSL 200 kts IAS b Above 6 000 14 000 ft MSL 210 kts IAS c Above 14 000 ft MSL 230 kts IAS Procedure Turn Unless specified on the approach plate the point at which the procedure turn is started is left to the discretion of the pilot It is recommended that the turn to the outbound heading be commenced 1 minute past the final approach fix on a non precision approach and 30 second past the final approach fix on an ILS approach Timing on the outbound leg sh
38. neuvering airspeed at all takeoff flap settings Flaps 15 minimum maneuvering 10 kts provide minimum maneuvering for flaps 5 www captainsim com 727 Captain FLIGHT MANUAL Part 111 Operations 21 DO NOT USE FOR FLIGHT ABNORMAL TAKEOFF When the aborted takeoff becomes necessary for any reason use normal after touchdown technique i e sped brakes reverse thrust and brakes If engine failure is recognized after attaining Vi speed the takeoff will be continued Use rudder as necessary to stay on center line Rotate the aircraft smoothly to takeoff attitude of approx 13 AFTER TAKEOFF S O CHALLENGE PILOT NOT FLYING After Takeoff S O ACCOMPLISH amp ADVISE CAPT WHEN RESPOND COMPLETED AUTO PACK CUTOUT NOSMOKE OFF FUELPANEL SET GEAR sima xA e OFF LIGHTS OUT TAILSKID RETRACTED oL lle IRR UP LIGHTS OUT CABIN PRESS amp TEMP SET NOTE CAPTAIN WILL ASCERTAIN PROPER TIME TO TURN STERILE COCKPIT LIGHT OFF NORMALLY 10 000 OFF LIGHTS OUT The red gear unsafe lights and the gear door light should all be out 2009 Captain Sim www captainsim com 727 Captain FLIGHT MANUAL Part 111 Operations 22 DO NOT USE FOR FLIGHT CLIMB CRUISE amp DESCENT CLIMB Normally the PDCS or computer flight plan indicated climb speeds will be utilized In the absence of thi
39. ning light is not illuminated Normally autopilot elevator system A is utilized with B selected if A hydraulic system fails or malfunctions NOTE The reset function of the warning light or one of the autopilot release switches will have to be operated after the engines are started and the S O puts the engine driven generators on the bus as this causes the autopilot disengage lights to flash SIERIMSTABS os ee ense aed ee Gee ea CHECKED amp ZERO Check the rudder and aileron trim wheels are free and set zero PARKING BRAKE tu be ale ge Ws ROL ACE doa ect ae n SET RECEIVING AIRCRAFT CHECK SECOND OFFICER F O CHALLENGE S O RESPOND CIRCUIT BREAKERS 5 6 alee le Ros a bom aa CHECKED CREW amp PASS OXYGEN ee CKD amp NORMAL STANDBYPOWER 0 0 CHECKED BATTERY 1 CHECKED GALLEY POWER sein oe e a eae o o el ae dd ON BATTERY SWITCH ss iota ee ee a eee ON DC POWER ses eee she um onlin a ge e ed ELE CHECKED GEN DRIVE TEMP SW se mama ama ayla IN GEN uuo oo ee Ok ee a ea a ee ee SOY ee CHECKED FUEL QUANTITY sis m ee alana ala lala 4 m as TEST amp AMT ENGFUELVALVES iie OPEN odd PTT AS REQUI RED
40. o other flights a check of all agreement lights will be made WING ANTI ICING SYSTEM a ANTI ICE VALVE POSITION LIGHT 5 WING VALVE POSITIONILIGHTS termed tuse tree gem edu e VOR ES ow o ei ea e SiGe t ON b ENGINES 1 amp 3 WINGANTI ICINGSWITCHES GRD TEST amp HOLD VALVE POSITION HIGHT Sie 21x x eae xoxo hx eee ed e e Roo s OFF THEN ON C ENGINES 1 amp 3 WING ANTI ICING SWITCHES RELEASE TO CLOSE VALVE POSITION LIGHTS ss ui a axo mtt te e Ro AA OFF THEN ON ENGINE amp COWL ANTI ICING SYSTEM a ENGINE INLET ANTI ICING SWITCHES THREE b ANTI ICE VALVE POSITION LIGHT SELECTOR POSITION ENGINE INLET ANTI ICE VALVE POSITION 5 ALL 3 ON IN EACH POSITION c ENGINE INLET ANTI ICING SWITCHES CLOSE ENGINE INLET ANTI ICE VALVE POSITION 5 ALL 3 ON IN EACH POSITION PUO L ee EA OPEN xus fae Gh tc dai ROTATE TO L COWL amp R PITOT AND STATIC HEAT PI TOT AND STATIC HEAT 2 ee eee Oe Oe Oe ee E CHECKED amp OFF a AND STATIC HEAT 5 1 5 rns ON Observe HEATER OFF light extinguish b PITOTSTATICHEATAMMETERSELECTOR a ALL POSITION Observe equal amperage readings i
41. olling taxi speed however only small thrust inputs should be used Turns Make all turns with as large a radius as possible conditions permitting The required nose wheel control motion is less then on other type airplanes When an outboard engine is used to assist in turning use as little power as possible and do not allow the airplane to stop The engine are effective on minimum radius turns n www captainsim com DO NOT USE FOR FLIGHT TAKEOFF PROCEDURE PRE TAKEOFF BRIEFING It is recommended that the Captains conduct a pre takeoff briefing when 1 Adverse weather conditions exist 2 At max gross weight for the takeoff runway 3 Unusual conditions exist S O CHALLENGE F O RESPOND Before Takeoff S O ACCOMPLISH amp ADVISE CAPT WHEN COMPLETED NOTE WILL CALL FOR BEFORE T O CHECKLIST WHEN T O CLEARANCE HAS BEEN RECEIVED OR IS IMMINENT STROBE LIGHTS ON T OANNOUNCEMENT COMPLETED PITOT HEAT 2 FUEL PANE RR SET TRANSPONDER amp DME ON amp NORM BOOST PUMPS ON CSD OIL COOLER GROUND OFF TRIMMER amp FLAPS POSITION FOR TAKE OFF seh SET Recommended position for MTOW ANNOUNCEMENT cee nee ee aa aae E S ee a Pe E O3 Eos COMPLETED Second Officer will pick up handset and make the takeoff announcement using the following phraseology We have
42. ould be a minimum of 30 second and maximum 1 minute depending on wind conditions Normally the procedure turn will be accomplished with a 15 flap setting and maneuvering airspeed When established on the inbound course of the procedure turn and cleared for the approach an approach check should be accomplished APPROACH CHECK S O CHALLENGE PILOT NOT FLYING Approach RESPOND RADIOS e e ts CKD amp IDENTIFIED COURSE ARROW INBOUND COURSE MODE SELECTOR SET ALTIMETER BUGS SET ADF VOR SWITCHES AS REQUIRED MARKER SWITCHES ON amp LOW WARNING FLAGS CHECKED MODE SELECTOR 5 2 ciem a ade Ge Ore Gad HR a nod nd Me a an Gc hd el ined Mei iq SET Flight director mode selector as desired Autopilot mode selector to AUTO G S for coupled approaches MISSED APPROACH PROCEDURE occore a e e aaa hh ke n REVIEWED 2009 Captain Sim www captainsim com 24 DO NOT USE FOR FLIGHT INHIBIT glideslope below 1 000 ft AGL and above 300 ft AGL if intended flight path does not follow glideslope Pilots will review approach plate and missed approach procedures Good operating practice would include the use of all available navigation aids for visual approaches APPROACH NOTES 1 2 3 8 9 Initial pattern entry will normally be in a clean configuration Reduce speed to FO m
43. plication of speed brakes call for flaps 25 If an aileron control deflection exists at this time the double action from partially raised speed brakes will only be transitory and have a negligible effect on lateral control The speed brakes spoil the lift over the wing and apply a downward force which places the airplane weight on the main landing gear providing excellent brake effectiveness Unless speed brakes are raised after touchdown very little weight will be on the wheels and any brake application may cause rapid anti skid cycling Braking will be ineffective and landing distances will be considerable increased WHEEL BRAKES Immediately after raising the speed brakes and with the nose gear on the ground apply wheel brakes Make this first brake application with only light braking Apply just enough brakes to feel their effectiveness and to check operation On or normal landing with the touchdown near the 1 000 foot point only the light braking need be used to complete the stop THRUST REVERSERS a After the speed brakes are raised quickly use alt pressure on thrust levers to check the engines in idle and at the same time raise the reverse thrust levers rapidly up and back Thrust reverser operating lights will illuminate when the lockout actuator piston has retracted If the interlock stop is felt hold light back pressure The interlock will release when the clamshell doors are fully closed The reverse thrust levers should be pu
44. s cd en a hee ele a ie GE tena a e bt EORR a ole ae SE oe ENGINE 1 2 3 Oc s esee Cx noma cce e Bue e A pp ar RUNNING 3 APU GENERATOR FIELD SWITCH unen eee Rod ae n CLOSED LIGHT OFF 4 APU GENERATOR BREAKERSWITCH n CLOSED LIGHT OFF 5 HYDRAULIC SYSTEM B PUMP SWITCH see ra aa adada kn m RR xx ON 6 ENGINE1BLEEDAIRSWITCH hh n hr eh n en ON 7 ENGINE 2 BLEED AIR SWITCHES BOTH aaa ON 8 ENG NE 3 BLEED ALIR SWITCH 5 ns uir tc s an 6 28 I be bbs Od EA A ON DC METERS SELECTOR 6 2229494 4a age m qoe Murat Waa dede de ied hbase aan kd BAT 1LO ESSENTIAL POWER SELECTOR o idonee ta Je UR Rus ea eat Zap Wl aE cn APU AG METERS SELECTOR wa aa RS sumak gp kanan amk me ma a gi APU 12 ENGINE START LEVERS Ctri ShifttF4 START ENG NE STARI SWITCH ae use mer a ee desde e ol Oa a a Be a ra Be GROUND NOTE The pilot must hold the switch in the GROUND position until 35 40 Nb then release the START switch closing the starter shutoff valve La ae Ue ae Gb a tah co tal d ed alude ean ain we sr ROTATION CHECKED T5 OU PRESSURE yg edota thd ik Sede ae desde Po oe Gh ath aed S O REPORT RISING TENT RPM
45. s information the following speed schedules should be followed as applicable 280 kts 78 Mach is the turbulence airspeed and the optimum rate of climb 300 kts 78 Mach is normal climb speed 340 kts 78 Mach is optimum NAUTICAL AIR MILES PER POUND OF FUEL speed when climbing into significant headwind Turbulent penetration speed is 280 knots below 34 000 feet approx and Mach 80 above 34 000 feet will call 18 000 feet as a reminder to set an altimeter setting of 29 92 Additionally he will call 1000 feet below assigned altitudes CRUISE The airplane is climbed leveled off the initial cruise altitude and accelerated with CLIMB thrust setting to 01 Mach or more above the desired cruise CRUISE thrust is now set The airplane will then stabilize at or very near the target Mach number Adjust the throttles to give the desired Mach Operating with the autopilot engaged and altitude hold selected allows closer adherence to the desired performance EMERGENCY DESCENT Any situation in the loss of cabin pressure requires an emergency descent to a lower altitude Prior to beginning the descent the immediate and secondary action checklist items for the decompression should be accomplished It should then be determined if control of the cabin is possible If not check for factors which main affect the descent maneuver While still on autopilot close the throttles and extend the speed brakes Then disconnect the autopilot and smoothly initia
46. sit lights LEADING EDGE LIGHTS s4 sms Ee REUS ilanla ill amam ENG MA 3 XX a TEST amp OFF Test the lights on the leading edge device flap annunciator FIRE DETECTION FAULT LIGHTS ra a l a code cte ae ee ei CHECKED Visually check engine fire detector circuit ground light off then push to test B PUMPS 8 uu ek ct a aan eh ee RR ORE ERE me Oe ee ak AR EGRE EE EA i 1 ON NOTE Prior to turning a pump on check that the low pressure light for that pump only goes out and that system B pressure rises to 3000 PSI 2800 PSI minimum CAUTIONS 1 Ensure that the 1 fuel tank which contains the system B heat exchanger contains at least 1700 Ibs of fuel 2 Do not start any one B pump more than 5 times in any five minute period After five starts leave pump on for at least 5 minutes or 4 off for 30 minutes www captainsim com 727 Captain FLIGHT MANUAL Part 111 Operations 16 DO NOT USE FOR FLIGHT BEFORE STARTING ENGINES F O CHALLENGE CAPT RESPOND Before Start F CHALLENGE 5 O RESPOND FUEL QUANTITY CHECKED PACKS 24 ari OFF ON GALLERY POWER OFF eee PARKINGBRAKE AS eee AS REQUIRED sep dm REQUIRED BOOST PUMPS MINIMUM FOR DOOR LIGHTS CHECKED STA PNEUMATIC PRESSURE A STARTING SEQUENCE lt c
47. te a 30 bank turn letting the nose of the aircraft fall to an approximate 10 nose low pitch attitude AIRWORK Steep Turns Steep turns in both directions will be accomplished during normal training recurrent training and proficiency checks as an exercise in instrument crosscheck and aircraft control 1 Entry Stabilize and trim at 250 knots on heading and altitude In order to avoid gaining altitude during roll out pitch trim is not used during the turn As the bank is increased past normal 25 30 loss of vertical lift requires a pitch adjustment Maintain 45 of bank 2 During turn Varying the angle of bank while turning makes pitch control more difficult Excursion from the entry conditions should be corrected by smooth positive inputs and or thrust 3 Altimeter and VSI The Altimeter is primary performance instrument during the turn Be alert to the direction and rate of altimeter needle movement and use smooth elevator control pressure changes for corrections Due to the location of the static ports the VSI will indicate a slight rate of the climb even though the aircraft is in level flight For purposes of fuel economy descent from cruise altitude is accomplished at idle power in a clean configuration If optimum range or turbulent air is consideration descend at 80 Mach to 34 000 feet and then descend at a constant airspeed of 280 KIAS Speed brakes may be used in the event a high rate of descent or a speed reduction is
48. ude that will satisfy the most critical situation will result in an airspeed very near V 10 with all engines operating Takeoff to 1000 Feet AGL 1 Maintain takeoff power 2 Climb at V 10 max body angle 20 3 Maintain takeoff flap setting until attaining an altitude of 1000 feet 4 If 25 flap used for takeoff 15 may be selected at 400 ft 1000 to 3000 Feet AGL 1 Lower the nose to approx 10 2 Retract flaps to 59 3 Reduce thrust to climb power 4 Retract flaps on schedule 5 Complete AFTER TAKEOFF checklist 6 Climb to 3000 feet at 0 flap man speed At 3000 Feet AGL 1 Accelerate to 250 knots IAS 2 Establish normal enroute climb 7 Close in turn after takeoff 8 A good operating practice is to delay making turns after takeoff until reaching 800 to 1000 feet unless otherwise instructed MANEUVERING SPEED Maneuvering airspeed is the airspeed which safely allows 30 of bank angle with a safety margin for a 15 overshoot At speed below maneuvering limit the bank angle to 15 Maneuvering speed for operations below 10 000 ft GROSS WGT x1000 110 120 130 140 150 160 170 172 5 MIN MAN dM 129 135 140 145 150 156 161 164 MIN MAN 160 167 175 182 188 194 201 204 MIN E 168 176 183 190 197 203 210 213 V2 does not provide normal maneuvering margin during takeoff There force limit bank angle to 15 at V V 10 provides minimum ma
49. ximately 1 8 gallons full Standby system quantity should be approximately 5 2 gallons full and 28 gallons minimum GROUND INTERCONNECT ei xam RR Oe OS de d EON a lama ee CLOSED Obtain ground clearance prior to opening ground interconnect valve HYDRAULIC SHUT ORES ka waren Rad a deed Pea dee eam Ea RA CAPPED Both system A hydraulic fluid shutoff valves should be capped open and safetied HYDRAULICBRAKE NTERCONNECT ee CAPPED The hydraulic brake interconnect valve is normally left closed capped In this position the green indicator light will not illuminate if the valve is closed CSD ONE COOLER s sm cuz ee hehe Beal od eX eee ee Ue ee ee o Ses eee bg dk NORMAL Cooler if off in flight and on on the ground OIE QUANTITY 123 2 Rm RE a Rx Ye eae ae e gc TESTED amp CHECKED It is recommended to have at least 5 gts before starting and at least 3 gals When engines stabilize at idle RPM GABINIPRESSURIZATEON cit ve t Ne init qus d me ae PE in Ga Nadia I S n un GE dete dod SET TEMP CONTROLS n amima me ka moment xe Ve x e Re m ee n Dn n ee nura A SEQ jeux el dom e m CUR SET 1 PASSENGER amp COCKPIT TEMP SELECTORS a ee AUTO Monitor cabin temperatures and adjust temp selector as required www captainsim com 15 DO NOT USE FOR FLIGHT 2 MIX VALVE POSITION 1 1 5
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