Surender Payloads

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    PAYLOADS

    1. The details of an aircraft flight from M to N ( no fuel is available at N ) are given below:-

    Distance M to N 7! nm"verage T"# $%! &

    'ind comonent M to N $! & '

    "verage fuel flow 7!! &g*hr

    +uel reserve (assume unused) !! &g"c weight less fuel , a load !!! &g

    Ma/ T*0 weight at M 1!!! &g

    Ma/ T*0 weight at N %%!!! &g

    Ma/ 2anding weight at M 77!! &g

    Ma/ 2anding weight at N 7!!! &g

    +ind ma/ aload from M to N and N to M:-

    a. 13!!4 !! b. 1%!!4 !!!c. 1%!!4 13!! d. !!!4 !!.

    . Ma/ ta5e off weight 3!!! lbs.

    Ma/ landing weight 3!!!! lbs.

    +light fuel 3!!! lbs.

    6eserve fuel %!! lbs.

    mt weight !!! lbs.

    +ind a load and state if a*c can carr additional reserve fuel without affecting a load4 and if so

    how much8

    a. 1!!4 es4 1!!! lbs. b. 1!!4 no4 ! lbsc. 13!!4 es4 1!!! lbs d. 13!!4 no4 ! lbs.

    $. +rom 9 to ( where fuel is not available) , return to 9. Ma/imum aload is to be off loaded at ,

    ma/imum a load is to be ulifted from The data given is:

    Distance 9 to ;1! nm.

    'eight no fuel , no aload $;!! 5g.

    Ma/ landing weight 3!! 5g.

    Ma/ ta5e off weight ;$!!! 5g.

    6eserve fuel unused 3!!! 5g.

    "dditional fuel for each flight !! 5g.

    (T*0 circuit landing etc)

    Mean +uel consumtion 1$! 5g*r.

    Mean ground seed 9 to 3! & Mean ground seed to 9 %! &

    +ind fuel to be u lifted at 94 ma/imum a load 9 to 4 ma/imum a load to 9.

    a. 734 %374 11!! b. 3!!!4 11!!4 !7.c. 11$34 %374 11!! d. 4 11$34 !7.

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    Aalculate: Ma/ aload which can be carried from M to N and Ma/ aload which can be carried from

    N to M.

    a. 7%!4 7;3. b. 7;347%!.

    c. 734 7%!. d. 7%!4%1!.

    %. Ma/ T*0 weight 1.!! Tons.

    6T0' !.!! Tons.

    Ma/ 2anding 'eight 3$. Tons.

    Ma/ Bero +uel 'eight $.1! Tons

    "9# 'eight 7.! TonsTri +uel 3. Tons

    6eserve +uel 1.!! Ton

    +ind the aload that can be carried

    a. 13.7. b. 1%.$!.

    c. 17.$!. d. 11.;!.

    . Ma/ Ta5e off weight %!!!! 2bs

    Ma/imum 2anding 'eight ;!!!! 2bs

    =asic 'eight 3%!!! 2=#

    T"# !! &

    Trac5 $!

    '*C $!*!

    Distance 1$! nm

    +uel consumtion !! 2bs*r

    6eserve +uel $!! 2bs

    +ind the a load that can be carrieda. 7!. b. %!!.

    c. !!. d. %7!.

    1!. Ma/ T*0 'eight !!! 5g

    Ma/ 2anding 'eight !!! &g

    Ma/ Bero +uel 'eigh t $%!!! &g

    "*A weight without +uel , a load !!! &g

    +uel Aons 1;!! &g*r

    Distance 1!! nm

    6eserve +uel 7! &g

    T"# ;! &

    +ind ma/ a load in still and ma/ a load with a head wind of ! &.

    a. 1!!!!4 1!!!!. b. 11!!!4 11!!!.

    c. !!!4 !!!. d. 1!!!!4 !!!.

    $

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