Yakovlev Yak 52TW — Yak52TW_W&B_steve_dalton
NOT FOR FLIGHT — source fidelity: unreviewed | operational review: none | completeness: full
Source: Yakovlev/Yak 52TW/Yak52TW_W&B_steve_dalton.txt
Rights: licensed
Checklist hash: 5fed48ff1c8c57b303204711136bcc248ab3a20ad0612714da0687d99e8f5194
Verify against the aircraft's own approved documentation before use.
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WEIGHT AND BALANCE
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ENTER AMOUNTS IN YELLOW CELLS
N52SD
S/N: 0112226
DATE: 18 MAY 2002
[ ] Empty weight of Aircraft ................................ 2264.3 lbs.
[ ] Empty weight of Aircraft arm .................. 46.170532614936185 in
[ ] Empty weight of Aircraft moment .................. 104543.937 in-lbs.
[ ] Oil (1.9 lb/qt) ............................................ 0 Quarts
[ ] Oil weight ................................................... 0 lbs.
[ ] Oil arm ..................................................... 4.59 in
[ ] Oil moment ................................................ 0 in-lbs.
[ ] Main Fuel ................................................. 0 Gallons
[ ] Main Fuel weight ............................................. 0 lbs.
[ ] Main Fuel arm ............................................. 45.15 in.
[ ] Main Fuel moment ........................................... 0 in-lbs
[ ] Aux. Fuel ................................................. 0 Gallons
[ ] Aux. Fuel weight ............................................. 0 lbs.
[ ] Aux. Fuel arm ............................................. 71.76 in.
[ ] Aux. Fuel moment ........................................... 0 in-lbs
[ ] Smoke Oil ................................................. 0 Gallons
[ ] Smoke Oil weight ............................................. 0 lbs.
[ ] Smoke Oil arm ................................................ 65 in.
[ ] Smoke Oil moment ........................................... 0 in-lbs
[ ] Front Pilot .................................................. 0 lbs.
[ ] Front Pilot arm ............................................ 48.87 in
[ ] Front Pilot moment ......................................... 0 in-lbs
[ ] Rear Pilot ................................................... 0 lbs.
[ ] Rear Pilot arm ............................................ 99.48 in.
[ ] Rear Pilot moment .......................................... 0 in-lbs
[ ] Baggage ...................................................... 0 lbs.
[ ] Baggage arm .............................................. 117.79 in.
[ ] Baggage moment ............................................. 0 in-lbs
[ ] Total weight ............................................ 2264.3 lbs.
[ ] Total arm .................................... 46.170532614936185 in.
[ ] Total moment ...................................... 104543.937 in-lbs
[ ] Gear up? (YES or NO): ............................................ NO
[ ] % M.A.C. ........................................ 0.22532956150009692
[ ] Within Normal Limits?: .......................................... YES
[ ] Within Acro Limits?: ............................................ YES
** NOTE: Maximum Gross weight is 3,012 Lbs. (1,366 Kg.)
** NOTE: Aerobatic C.G. Limits (17.5% to 28% M.A.C.)
** NOTE: Normal C.G. Limits (17.5% to 31% M.A.C.)
** NOTE: Gear extension moves the C.G. aft .5% M.A.C.

WEIGHING INFORMATION
--------------------
ENTER WEIGHTS IN YELLOW CELLS
[ ] Left Main weight .......................................... 1086 lbs.
[ ] Left Main arm ............................................. 33.56 in.
[ ] Left Main moment .................................... 36446.16 in-lbs
[ ] Right Main weight ......................................... 1082 lbs.
[ ] Right Main arm ............................................ 33.56 in.
[ ] Right Main moment ......................... 36311.920000000006 in-lbs
[ ] Tail weight ................................................ 121 lbs.
[ ] Tail arm ................................................. 263.63 in.
[ ] Tail moment ......................................... 31899.23 in-lbs
[ ] Oil (1.9 lb/qt) .............................................. 13 qt.
[ ] Oil arm ..................................................... 4.59 in
[ ] Oil moment ............................................ 113.373 in-lb
[ ] Main Fuel .................................................... 0 gal.
[ ] Main Fuel arm ............................................. 45.15 in.
[ ] Main Fuel moment ............................................ 0 in-lb
[ ] Aux. Fuel .................................................... 0 gal.
[ ] Aux. Fuel arm ............................................. 68.38 in.
[ ] Aux. Fuel moment ............................................ 0 in-lb
[ ] Empty Totals weight ..................................... 2264.3 lbs.
[ ] Empty Totals arm ............................. 46.170532614936185 in.
[ ] Empty Totals moment ............................... 104543.937 in-lbs
** NOTE: Datum is front jacking point on firewall
** NOTE: Level aircraft using the front cockpit canopy rail