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  • 7/28/2019 Copy of UVA Planner

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    Fuel, Weight & Vspeed Planner 737-500Version 2.0, Release December 2006

    Copyright UVA, All rights reserved

    Use restricted to UVA operations

    Aircraft Type Empty Max T/O Max Lnding Maximum Max Zero Fuel BurnWeight Weight Weight Payload Fuel Weight PPH

    777-300R 370,000 775,000 554,000 154,000 524,000 16,000

    Enter Valu

    Here

    DEFINITION Hours

    Trip Length Total flying hours planned for flight from T/O to landing, excludes 8.2

    all other items. Enter amount in hours (ex 2hrs 12 min = 2.2 hrs)

    Headlwind Kn

    Wind Adjustment -40If winds aloft are unknown, plan for an average 40knts headwind. (-40)

    Hours

    Time to Alternate Enter as hours extra to account for fuel to alternate 1

    Hours

    Contingency Fuel Fuel for holds, 2 missed approaches, off optimum flight/route, long taxi, 0.5

    0.5 hrs is fairly typical.

    Lbs

    Captain's Fuel An additional safety margin, set from none, to say half an hour of cruise fuel. 0

    Minimum Landing Fuel Absolute minimum fuel on board, legally required on touchdown,will account for 45 min cruise, or 10% trip fuel, (whichever is greater)

    Hours

    Plan Fuel Required TOTAL AMOUNT OF FUEL REQUIRED FOR FLIGHT (time & amount) 11.20

    Endurance

    Lbs payload Percent of M

    Plan Payload 80,000 80%

    maximum. To specify a percentage, set Lbs to 0. in-use

    Plan Max Fuel Capacity This is determined by the maximum fuel capacity of the aircraft,

    as well as the amount of payload and maximum takeoff weight.

    Plan Zero Fuel Weight Weight of aircraft with payload, but no fuel

    Plan Takeoff Weight Takeoff weight for the Trip, with fuel and planned payload

    V1 Vr

    Plan Takeoff Vspeeds V2 is the safety climb speed,. For climb to acc'l height (1000AGL) 161 166Flaps 5

    decision speed on takeoff roll, after V1 you are committed to t/o.

    Vref30+80 is the minimum clean (flaps retracted) speed for Boeings

    Hours

    www

    Enter average winds aloft. Headwinds are (-), tailwinds are (+).

    Enter in pounds. Completely at discretion and optional.

    Planned payload, specifyeitherweight in Lbs or percent of

    use V2+10 knts. Vr is your rotation speed, and V1 is your

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    Vref+5 Steady wind Full gusts Correcte

    Plan Approach Vspeed 148 5 10 155Flaps 30 Flaps

    Vref+5 is the target speed only for a full autoland approach, the A/T will provide gust protection. For any other approach, the speed

    needs to be further adjusted. Specify the landing winds, this will add to Vref+5, of the steady headwind, plus the full excess gust; to a max of 20 additional knts.

    INSTRUCTIONS FOR USEThis Fuel & VSpeed Planner is targeted for those individuals that do not have custom planners and data for their aircraft, or just want

    something quick and easy to use. The UVA FVP will allow you to input the various required factors for your flight, and issue you a

    Finally it suggests the flaps to use for takeoff and landing, together with a calculation of the Vspeeds, your target speeds for takeoff and

    This FVP is designed to be used with any aircraft which has a model accurately representing the average fuel burn of the listed

    aircraft. The following is a list of step by step instructions, data is only entered in the red outlined grey rectangles.

    Specify the payload as a percentage of maximum, or enter a weight in pounds. To enter a percentage, the pounds cell must be set to ze

    Once the above has been entered, the FVP will calculate the required totals, and issue the fuel and weight totals. The first total is the

    within operational limits. Only adjust the payload down if you receive warnings.

    Vref30+80 at takeoff, is the Vref for flaps 30 for your takeoff weight. For Boeings, adding 80 knots to this figure will give you

    your minimum safe speed for flying with no flaps extended, or your Minimum Clean Speed. With flaps retracted, you should

    fly at least 10 to 20 knts over this speed, for safety.

    For a coupled A/P driven ILS approach, or a hand flown approach, the final corrected Vref speed should be used as your approach spee

    from the Final Approach Fix, to the runway threshold. Shortly after this point, you will flare the aircraft, and land. Your landing speed

    should be ideally (Vref + Gusts), but in any case, never less than (Vref 10) knts.

    Only advanced payware panels have true autoland capability. Such an approach is used in very poor visibility conditions, where a landin

    couldn't otherwise be safely accomplished. For a full autoland approach, (Vref + 5) is used for the approach speed, as with a true autola

    there is gust protection.

    Minimum Landing Fuelamount, as well as an Expected Landing Fuel, and a Total Fuel Requiredamount which can then be used

    to load the aircraft for your flight. It will also advise on aircraft weights, and ensure that you are within operational limits.

    #1. Select Aircraft Type (aircraft data will continue to be tweaked, and we expect to have Vspeeds for the entire fleet in a future update.)

    #2. Input length of flight in Trip Length box. (see definition on how to properly input flight time)

    #3. Input Winds aloft Correction (see definition on how to properly input wind)

    #4. Input Alternate Fuel (see definition on how to properly input alternate time)

    #5. Input Contingency Fuel (see definition on how to properly input contingency fuel)

    #6. Input Captain's Fuel (see definition on how to properly input Captain's fuel)

    #7. Enter the payload weight that you are planning to carry

    For most aircraft, you cannot carry both a maximum payload and maximum fuel capacity. This is an issue for longer trips.

    Minimum Landing Fuel. This amount is the FAR required fuel amount that should be remaining in the aircraft upon

    landing. The second total is the Plan Fuel Required. This amount will be the amount of total fuel that you put in the

    aircraft for the flight. It will also advise an Expected Landing Fuel, if no contingencies are exercised.

    Also calculated is the Plan Takeoff Weightand Expected Landing Weight. Ensure that you do not exceed the maximums.

    If you have any warnings in the Advice column, you may have to adjust down your payload for the trip, or other factors, to stay

    Finally note that the Vspeeds for takeoff (V1, Vr, V2) and for landing (Vref) are calculated, for the suggested flap settings.

    #8. Enter the landing winds, you may not have this available until shortly before landing.

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    `

    Advice

    Vref30+80

    246

    om

    http://www.united-virtual.com/http://www.united-virtual.com/
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    Tables

    Page 5

    Burn Reserve Max Fuel Capacity Max T/O Max Landing

    747-400 21700 16275 383810 874999 630002

    777-300R 16000 12000 390000 775000 554000

    767-300 10000 7500 160666 408000 300001

    757-200 7100 5325 76956 255031 209990

    737-500 5000 3750 35583 133490 110011

    737-300 5200 3900 35583 135003 113979

    A319/320 5400 4050 42200 169800 145503

    ERJ-170 3000 2250 20576 82012 72312

    ERJ-145 2253 1689.75 11256 45415 41226

    CRJ-700 2750 2062.5 19880 72750 66999

    CRJ-200 2500 1875 17654 53001 47000

    DASH8-200 1325 993.75 5595 36299 34500

    B1900D 726 544.5 4484 17120 16765

    EMB-120 1000 750 4925 26433 25794

    SF-340 1096 822 5800 28000 27200

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    Tables

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    Max Payload Avg Cruise TAS Empty Weight Max ZFW Emp+MaxPy v1-m

    157399 485 394090 542500 551489 0.130

    154000 480 370000 524000 524000 0.165

    98099 462 196000 294100 294099 0.281

    58863 462 136907 188054 195770 0.418

    33510 440 69005 102515 102515 0.933

    35605 440 69446 106483 105051 1.067

    42093 455 93035 138020 135128 0.480

    19842 450 35165 79344 55007 0.000

    12159 450 25722 37698 37881 2.111

    18800 448 43500 62300 62300 0.700

    13100 424 30292 44000 43392 2.056

    6000 238 23003 29000 29003 0.000

    4375 260 10650 15165 15025 2.609

    7319 260 15655 24030 22974 0.000

    7500 260 19000 25700 26500 5.596

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    Tables

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    v1-i vr-m vr-i V2-m V2-i Vref-m Vref-i

    43.000 0.124 64.400 0.120 78.000 0.140 66.000

    57.250 0.140 78.000 0.135 85.750 0.165 62.250

    49.500 0.256 64.500 0.238 77.000 0.263 62.000

    57.090 0.427 57.640 0.373 73.360 0.427 48.640

    30.670 0.800 48.000 0.600 78.000 0.636 64.360

    17.330 1.167 8.330 0.933 40.670 0.667 60.330

    64.600 0.540 60.800 0.500 69.000 0.600 50.000

    0.000 0.000 0.000 0.000 0.000 0.000 0.000

    33.670 1.944 41.670 1.667 63.000 1.222 77.330

    83.100 0.750 80.250 0.550 104.650 1.000 68.000

    31.110 1.944 37.890 1.611 62.220 1.611 65.220

    0.000 0.000 0.000 0.000 0.000 0.000 0.000

    64.700 3.043 63.480 2.609 71.700 3.043 64.480

    0.000 0.000 0.000 0.000 0.000 0.000 0.000

    -16.170 5.293 -6.830 4.386 25.170 3.759 41.290

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    Tables

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    Takeoff Landing

    Flaps 20 Flaps 30

    Flaps 5 Flaps 30

    Flaps 5 Flaps 30

    Flaps 5 Flaps 30

    Flaps 5 Flaps 30

    Flaps 5 Flaps 30

    Flaps 1+F Flaps Full

    Flaps 9 Flaps 45

    Flaps 9 Flaps 45

    Flaps 8 Flaps 45

    Flaps 8 Flaps 45

    Flaps 10 Flaps 35

    Flaps 15 Flaps 35