Ch 6 important notes Flashcards
Another important reason for concern about weight and balance is the efficiency of the aircraft. Improper loading reduces the efficiency of an aircraft from the standpoint of ceiling, maneuverability, rate of climb, speed, and fuel consumption
If an airplane is loaded in such a way that it is extremely nose heavy, higher than normal forces are exerted at the tail to keep the airplane in level flight.
he higher than normal forces at the tail create additional drag, which requires additional engine power and therefore additional fuel flow to maintain airspeed.
The weight and balance report identifies the empty weight of the aircraft and the location at which the aircraft balances, known as the center of gravity (CG).
IMPORTANT
The weight and balance report must include an equipment list showing weights and moment arms of all required and optional items of equipment included in the certificated empty weight.
As an alternative, the manufacturer is permitted to weigh an agreed upon percentage of a particular model of aircraft produced, perhaps 10 to 20 percent, and apply the average to all the aircraft.
IMPORTANT
For a small, GA airplane being used privately, such as a Cessna 172, there is no FAA requirement that it be periodically reweighed; but after each annual, the mechanic must ensure that the weight and balance data in the aircraft records is correct.
This depends on the type of aircraft and how its used
If the weight and balance report for an aircraft is lost, the aircraft must be weighed and a new report must be created.
IMPORTANT
When an aircraft has undergone extensive repair, major alteration, or has new equipment installed, such as a radio or a global positioning system, a new weight and balance report must be created.
The distance from this datum is measured in inches and can be either positive or negative depending upon where the equipment is located in relation to the datum.
IMPORTANT
The most important reason for weighing an aircraft is to find out its empty weight (basic empty weight) and to find out where it balances in the empty weight condition.
The location of the datum is identified in the Aircraft Specifications or Type Certificate Data Sheet (TCDS).
IMPORTANT
The algebraic sign of the moment, based on the datum location and whether weight is being installed or removed [Figure 6-3], would be as follows on page 224:
- Weight being added aft of the datum produces a positive moment (+weight, +arm).
- Weight being added forward of the datum produces a negative moment (+weight, -arm).
- Weight being removed aft of the datum produces a negative moment (-weight, +arm).
- Weight being removed forward of the datum produces a positive moment (-weight, -arm).
IMPORTANT
The aircraft should be weighed inside a hangar where wind cannot blow over the surface and cause fluctuating or false scale readings.