Take Off Speed Margin Eng Fail V2 gives stall margin for 15 + 15 overbank V2 + 15 gives stall margin for 30 + 15 overbank select LVL CHG and MAX CONT after flaps up Climb w/o FMC best angle Flaps up maneuvring speed best rate Flaps up maneuvring speed + 50 kts /.74 Econ 280 /.74 1 Eng Inop Flaps Up Maneuvring Speed / Max Continuous Cruise Max Altitude Margin Max Altitude is the minimum of certified altitude, thrust capability to climb or buffet margin limited altiude ( 0.3 g / 40 bank ) Optimum Altitude Provides +/- 1.5 load factor ( 48 bank ) 2000 ft above allows +/- 45 bank prior buffet 2000 ft above / below optimum increase fuel by 1 / 2 % 4000 ft below optimum increase fuel by 3 / 5 % Optimum calculation altitude: Distance + ½ distance 8000 ft below optimum increase fuel by 8 / 14 % Long Range Cruise provides fuel mileage 1 % less than Max Range M.01 above LRC increase fuel by 1 / 2 % M.74 gives LRC within 2000 ft of optimum LRC provides best buffet margin at all cruise altitude 4000 ft climb needs 135 to 225 kgs but climb only if you cruise 20 min or more Fuel temperature rate of cooling is 3 C per hour up to 12 C Increase of M.01 increase TAT by 0.5 to 0.7 C Engine Failure 1 Eng Inop Distance At cruise level & speed : 260 Nm
Descent Planning Speed Target Deceleration Holding 3 Nm / 1000 ft M.74 / 280 kts gives 2100 / 3000 ft/min 250 kts gives 1700 / 2400 ft/min 210 kts gives 1400 / 1900 ft/min 10 000 ft, 250 kts at 30 Nm Flaps Up maneuvring at 12 Nm for Straight In Flaps Up maneuvring at 8 Nm Out for Abeam 25" - 2 Nm from 280 to 250 kts in Level 25" - 3 Nm from 250 to 210 kts in Level Rem: Time and speed decrease by 50% with speedbrake Minimum fuel is Flaps Up maneuvring Speed Above FL 250, take VREF 40 + 100 kts Flaps 1 increase Fuel by 10% Approach Engine Failure On Final Flaps 15 Landing All Eng retract flaps to 15 and increase Vref by 15 kts Use Flaps 1 for go-around Rudder authority and rudder pedal steering are not affected by rudder trim Landing Braking with A/S Braking without A/S Reverse thrust with X wind X wind landing Overweight Landing Apply full braking Apply progressive constant braking Avoid reverse trust if A/C in crab Reduce X wind by 5 knots if assymetric reverse zero crab landing not recommanded if x wind exceeds 17 kts or 23 with flaps 40 Use Flap 30 for speed margin Landing distance is less than TO distance Except on Wet/Contaminated RWY ( check PI ) Reduce Weight by increasing drag Brake Energy Limits not exceeded for F30 or F40 You can go to speed 20 kts below Maneuvring Speed with normal bank. No 15 protection overbank No Autoland recommanded Maneuvers Rapid Descent 1 Lights, 2 Start Switches, 3 Altitude, 4 LVL CHG, 5 Thrust Levers and 6 Speed Brake Check MSA, ATC, QNH Stall Speed Fup: 160, F5 : 135, F15 : 118, F30 : 108 Stick Shaker Speed Fup: 180, F5 : 145, F15 : 125, F30 : 116 Rem: Fup and F5 is for MTOW, others for MLW
NN Operations Ditching Loss Of Thrust On High Vibration All Flaps Up Landing Leading Edge Flaps Trans Trailing Edge Flaps Alternate Flaps Extens. Jammed Flight Controls Jammed Stabiliser Fuel Imbalance Low Fuel (>453 kgs) Manual Reversion Landing Gear Lever Jam. Tire Failure Partial Gear Up Landing One Main Gear Down Tailstrike Window Damage Slide Window Open Use F40, Reduce Fuel and pitch +/- 10 for touch Use TO EGT Limit for restart Reduce Power, Speed and Altitude Fly manually on Final, Use A/B and full Reverse Vref gives protection for 15 + 15 Overbank Config Wanrning can occur if gear up and F>15 No Assymetry Protection and Slower Speed Override with big constant force to keep control No breakthrough system like the 146 Force on stabiliser trim wheel Full control by elevator still available Limit is for structural life not for controlability Smooth handling in pitch and roll Leave wings pumps on even with low pressure light Gear and leading edge devices cannot retract Extend and retract trailing edge flaps electrically Plan a long final, smooth thrust reduction on flare Use if gear transfer valve stuck and if time Advise ATC to check the rwy and land normally Go to your destination if rwy long enough Don't use the autobrake, use max reverse Do not recycle the lever. Don't waiste time Ask fire truck to check your gear condition Do not arm the speedbrakes Shutdown fuel pumps and critical engine on flare Do not pressurize tha A/C Risk in late go-around if you refuse the touchdown With both window 1 damaged, do an autoland may be open at or below holding speed calm air area over the open window Low Visibility Procedure Low Vis Take Off CATII/CATIII Approach Visibility less than 400m Check Airport Minimas Visibility down to 200m Captain make a good briefing Synthesis 1 Verify A/C status 2 Verify airport status 3 Verify weather 4 Verify crew qualification
General Info Passenger Weight Charter Flight Europe Male: 83 kgs Female: 69 kgs All Adult : 76 kgs Child ( 2 to 12 ): 35 kgs Infant ( under 2 ) : 0 kg Baggage Weight Charter Flight Europe Fuel Consumption Engine APU 1 piece : 13 kgs 3200 kgs for 1 st hour 2500 kgs/h Or check QRH (ground) 115 kg/hr Perfo Improvement Method 1 Bleeds off or unpressurized TO 2 Use another rwy 3 Take headwind into account 4 Use improve climb 5 Improve climb + bleeds off Perfo Information At TO thrust, each 3T below the max climb weight, you increase your climb gradient by 1% Both engine running: climb gradient multiplied by 4: 2,4% x 4 = 9,6%
FCT 4.10
FCT 5.54 FCT 5.49 FCT 6.35
FCT 8.22