Difference between revisions of "Enstrom 280C/Weight and Balance"
(Created page with "<span class=sa-section>SECTION 5. WEIGHT AND BALANCE</span> === WEIGHT AND CG LIMITS === The weight and CG limits for this aircraft are: {| class=wikitable |Max Gross Weight...") |
(→WEIGHT AND CG LIMITS) |
||
| Line 5: | Line 5: | ||
The weight and CG limits for this aircraft are: | The weight and CG limits for this aircraft are: | ||
{| class=wikitable | {| class=wikitable | ||
| − | |Max Gross Weight:|| | + | |Max Gross Weight:|| 2600 lb |
|- | |- | ||
| − | |Max Forward CG:|| | + | |Max Forward CG:|| 103 inches |
|- | |- | ||
| − | |Max Aft CG:|| | + | |Max Aft CG:|| 111 inches |
|} | |} | ||
Revision as of 04:16, 31 July 2021
SECTION 5. WEIGHT AND BALANCE
1 WEIGHT AND CG LIMITS
The weight and CG limits for this aircraft are:
| Max Gross Weight: | 2600 lb |
| Max Forward CG: | 103 inches |
| Max Aft CG: | 111 inches |
2 EMPTY WEIGHT AND CG
The empty weight and CG of this aircraft are:
| Empty Weight: | 1824lb |
| Empty Aircraft CG: | 125.1in |
| Empty Moment: | 228182 lb-in |
3 CG ARM DATA
The following arm data can be used to calculate moment at each of these stations.
| Pilot | 77.6 in (1.97 m) |
| Rear Seats | 122.0 in (3.10m) |
| Fuel | 172.8 in (4.39m) |
| Baggage | 211.0 in (5.36m) |
4 WEIGHT AND CG CALCULATION
Total weight is calculated by adding total weight of empty aircraft, fuel, passengers and baggage. Fuel weight can be calculated assuming 6 pounds per gallon of fuel. The CG is obtained by dividing total moment by total weight. Moment at each station is obtained by multiplying the arm of that station by the weight at that station. Total moment is obtained by adding moment for each station and the moment for the empty aircraft.
As an example, consider a 180 lb pilot, a 160 lb passenger and 41 gallons of fuel. Weight of the fuel will be 41*6=246 lb.
| Item | Weight | Arm | Moment |
|---|---|---|---|
| Aircraft | 1824 | 125.1 | 2282182 |
| Pilot | 180 | 77.6 | 13968 |
| Co-Pilot | 160 | 77.6 | 12416 |
| Passenger (back) | 190 | 122.0 | 23180 |
| Fuel | 246 | 172.8 | 42509 |
| Total | 2600 | x | 320355 |
The final CG is calculated by dividing the total moment 320255 by the total weight 2600 yielding 123.2 inches. Cross checking the total weight and CG with the weight/CG limits indicates the aircraft is within limits. The "CG" is also calculated and displayed on the main menu for convenience.
