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STEMME S6 User Manual

STEMME S6
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Flight Manual STEMME S6
Doc.-No.:P400-006.000 E Page: 1-9 Revision: ---
Date of Issue: 07. October 2008 Date of Rev.: --.--.----
1.6.3 Mass and Balance
RP Reference Plane, an imaginary vertical plane which forms the
origin for all center-of-gravity calculations
MAC
Mean Aerodynamic Chord
MTOM
Maximum Take-Off Mass (cf. MTOW)
Empty Mass Mass of the Airplane including non-useable fuel, all operating-
fluids and max. amount of oil. It does not contain payload and
trip-fuel and fuel-reserves.
Center-of-
Gravity
Imaginary point, at which gravity acts on the aircraft
Lever
Horizontal distance between the center-of-gravity of a body and
the reference plane
Moment
Product of Mass and Lever of a body
Non-useable
Fuel
Fuel which remains in the tank and is not available for the flight
Useable Fuel
Amount of fuel which is available for the flight
Payload
Difference between empty-mass and take-off-mass
NLP
Non Lifting Parts
1.6.4 Abbreviations for Aircraft and Powerplant
A/C
Aircraft
XPDR
Transponder
MCP
Maximum Continuous Power
MTOP
Maximum Take-Off Power
CD
Constant Depression
TCU
Turbo Control-Unit
CHT
Cylinder-Head Temperature
S/N
Serial Number
S/N
Serial Number
MAP
Manifold Air Pressure

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STEMME S6 Specifications

General IconGeneral
BrandSTEMME
ModelS6
CategoryAircrafts
LanguageEnglish

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