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during start and taxi.
tare weight. The weight of any chocks or devices that are
used to hold an aircraft on the scales when it is weighed. The
tare weight must be subtracted from the scale reading to get
the net weight of the aircraft.
TEMAC. Trailing Edge of the Mean Aerodynamic Chord.
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.
Glossary– 6
Index– 1
Index
A
adverse-loaded CG checks ............................................... 5-4
aircraft specifications ....................................................... 2-7
arm .................................................................................... 2-1
B
balance control ................................................................. 1-4
ballast ....................................................................... 3-3, 5-7
bilge area ........................................................................... 3-2
C
cargo .................................................................................. 6-5
cargo changes—effects of ............................................... 6-5
cargo configuration ........................................................ 6-18
cargo pallet ....................................................................... 6-9
center of gravity (CG) ...................................................... 1-1
CG
determining .................................................. 2-2, 3-4, 4-1
shifting ................................................................. 2-4 –2-6
CG limits envelope .................................................. 4-2– 4-3
CG moment envelope ....................................................... 4-5
CG range chart ............................................................... 2-11
chart method ..................................................................... 4-7
chord ................................................................................. 3-7
computational method ..................................................... 4-1
D
datum, location of ................................................... 3-5– 3-6
density altitude, high ........................................................ 1-2
draining of fuel and oil .................................................... 3-3
dynamic loads ................................................................... 1-2
E
E6-B flight computer ....................................................... 8-1
electronic calculators ....................................................... 8-1
electronic flight computers .............................................. 8-3
empty weight .................................................................... 1-1
basic ............................................................................... 2-1
standard ......................................................................... 2-1
empty-weight center of gravity (EWCG) .............. 1-1, 3-5
helicopter ...................................................................... 7-2
range .............................................................................. 5-4
equipment list ........................................................ 2-13, 5-1
F
fleet weight .......................................................6-1–6-2, 6-2
floor loading limits ........................................................... 6-9
fuel jettison system ........................................................ 6-12
I
interpolation ............................................................. 4-8– 4-9
L
landing weight ................................................................ 6-10
law of the lever ................................................................. 2-2
　
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