ATC regularly instructs us to go "direct to (waypoint) XYZ". . Shortly before we start our takeoff roll, we do the following steps: Check PACKS as required V1: The speed beyond which takeoff should no longer be aborted. +64 79.6 136036F 42-42-43 +64 79.6 140085F 49-50-50 +64 79.6 140019F 49-50-50 After takeoff, the aircraft will use FLX/MCT or TO GA thrust until thrust reduction altitude is reached (typically ~1500ft above runway, this is part of the MCDU setup). - SPEED/FLAPS SCHEDULE: F=129 S=168 O=183, --------- ------ --------- ----- ----------- ----- ----- ----- --------------------- ), Ready-to-print and ready-to-save loadsheet, take-off and landing reports, Build your own Individual Runway Tables (IRTs) for your favourite airports, NOAA, IVAO, VATSIM and ActiveSky weather support (FS2004 and FSX), A wide variety of units: kilograms (kg), pounds (lb), meter (m), feet (ft), hPa (hecto pascal), inHg (Inches of mercury) for your personal needs, Editor to add or modify runways and airports. +64 79.6 139427F 48-48-49 +64 79.6 133297F 39-39-39 +64 79.6 134743F 40-40-41 Required Runway Length. - Airliners.net It allows time to double-check the systems by going through all ECAM pages, etc. Hope this can help you all with the Take Off Perf setting. If youve used this add-on, share your thoughts with other pilots. We do this in case the auto-turn-off has failed. Good evening, after several downloads of this file it is impossible for me to be able to obtain the small arrow which allows to change either the CWY - RWY COND or THRUST. right of this page to report dead links and we will try to fix it. How to calculate the Lift Coefficient for the A320? The author decided to only allow members to download this file. However, despite the improvements, it is still clear that the A340 has a long takeoff roll and cannot serve all airports across the globe. Lastly, we disarm the SPEED BRAKE and turn on the PACKS if we turned them off for takeoff. of thrust, resulting in longer on-wing lives. Take-off/Landing calculator VR: Rotation speed. It calculates trip and total fuel required based on CRZ FL, payload and TOW, (albeit at a fixed speed and without CRZ wind adjustments - yet ), and also a V speed calculator based on OAT and BRW. How do I go about doing this? FM271800 VRB03KT 4SM BR OVC004 /+66 79.4 136349F 47-47-47 /+66 79.4 130616F 38-38-39 /+66 79.4 131960F 40-40-41 21R 8501FT LT TO 'DM' 223 (275 INBD,RT) Repeat the climb process above until cruise level (e.g., FL240) is reached. HW/10 KT 0 +1623 0 KDTW 04L +2C 100/06 29.72 136971 CONF 1+F FLEX +66C 135 135 136 108441, RMKS - CALCULATIONS VALID AT ALT 29.57 AND ABOVE Does anybody know of a takeoff & landing performance calculator for the A340-600? Flaps 1 for a standard takeoff. Dividing 30 by 3,000 results in 0.01. For example, the length of the runway is 3,000 feet. KE*=n D*""`)-E_(8&I~,uU|RSUJnSrMB7dbdq>'I9R+O/KNrdJfD[rGIJ22'9\wAJR Notes. These add-ons may be required or recommended to use. Note: Your post will require moderator approval before it will be visible. For this calculator, a "stackable additional discount" means getting a further percent off of a product after a discount is applied. Largest member of Airbus twinjet family (2-engine version of A340). Each to be instructed and cleared by ATC. Even with these artificial runway restrictions, it does not seem like the A340 will be opened up for operations to and from additional airports. Takeoff, Climb and Cruise - FlyByWire Simulations Documentation Hey, would you share where exactly you find the FBW checklist? UTOPIA suggests a derate for a number of aircraft at a given runway, weight and weather conditions. . Quote. I've managed to go slightly better than that! +60 80.1 145312F 48-49-50 +60 80.1 138459F 39-40-41 +60 80.1 140356F 41-41-42 Landing calculation with custom flaps, autobrakes setting, and runway surface conditions. Airbus A-340 . Catherine BONNET. You must get permission from me first before you are allowed to use assets of my file. Direct course to a waypoint (DIR TO) Remove the hand from the thrust levers at V1 to avoid accidentally aborting after V1. AVSIM Library h|0_%O$"lPTKH;j?lopKdLlBGg>w +62 79.8 142471F 49-49-49 +62 79.8 135949F 39-39-40 +62 79.8 137613F 41-41-41 The speed at which the aircraft may safely climb with one engine inoperative.

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