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Type Certificate Data Sheets (TCDS). The official
specifications issued by the FAA for an aircraft, engine, or
propeller.
Undrainable Oil. Oil that does not drain from an engine
lubricating system when the aircraft is in the normal
ground attitude and the drain valve is left open. The weight
of the undrainable oil is part of the empty weight of the
aircraft.
Unusable Fuel. (GAMA) Fuel remaining after a runout
test has been completed in accordance with governmental
regulations.
Usable Fuel. (GAMA) Fuel available for flight planning.
Useful Load. (GAMA) Difference between takeoff
weight, or ramp weight if applicable, and basic empty
weight.
Utility Category. A category of aircraft certificated
under 14 CFR part 23 and CAR part 3 that permits limited
acrobatic maneuvers but restricts the weight and the CG
range.
Wing Chord. A straight-line distance across a wing from
leading edge to trailing edge.
Zero Fuel Weight. The weight of an aircraft without fuel.
Index–
I
Index
A
adverse-loaded CG checks...............................................5-4
aircraft specifications.......................................................2-6
arm...................................................................................2-1
B
balance control.................................................................1-3
ballast...............................................................................5-6
bilge area..........................................................................3-2
C
cargo.................................................................................7-4
cargo changes—effects of.......................................7-4– 7-6
cargo configuration........................................................7-16
cargo pallet...............................................................7-7– 7-8
center of gravity (CG)......................................................1-3
CG
determining.................................................. 2-2, 3-4, 4-1
shifting................................................................. 2-4 – 2-6
CG limits envelope.................................................. 4-2– 4-3
CG moment envelope.......................................................4-4
CG range chart...............................................................2-10
chart method.............................................................4-5– 4-6
chord................................................................................3-6
computational method......................................................4-1
D
datum, location of............................................................3-6
density altitude, high........................................................1-2
draining of fuel and oil.....................................................3-2
dynamic loads..................................................................1-1
E
E6-B flight computer........................................................8-1
electronic calculators.......................................................8-1
electronic flight computers...............................................8-3
empty weight................................................... 1-1, 1-3, 1-5
empty-weight center of gravity (EWCG)............... 1-1, 3-5
helicopter......................................................................6-2
range.................................................................. 2-10, 5-4
equipment list.............................................. 2-11– 2-13, 5-1
F
floor loading limits...........................................................7-7
fuel jettison system........................................................7-10
I
interpolation.....................................................................4-6
L
landing weight..................................................................7-8
law of the lever.................................................................2-1
leading edge of MAC (LEMAC).....................................3-7
lift, center of.....................................................................1-3
load factor........................................................................1-2
loading graph...........................................................4-3– 4-4
loading schedule.......................................................7-2– 7-3
Index–
M
major alteration................................................................5-1
maximum weight.............................................................1-1
　
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