Steamly S2-S/Weight and Balance - Revision history

Kelly: /* WEIGHT AND CG LIMITS */

2022-05-05T12:52:20Z

‎WEIGHT AND CG LIMITS

2022-05-05T12:14:48Z

‎EMPTY WEIGHT AND CG

2022-05-05T12:14:19Z

‎EMPTY WEIGHT AND CG

2022-05-05T12:13:54Z

‎WEIGHT AND CG CALCULATION

2022-05-05T12:13:28Z

‎WEIGHT AND CG CALCULATION

2022-05-05T12:13:16Z

‎WEIGHT AND CG CALCULATION

2022-05-05T12:09:06Z

‎CG ARM DATA

2022-05-05T12:06:09Z

‎EMPTY WEIGHT AND CG

2022-05-05T12:04:50Z

‎WEIGHT AND CG LIMITS

2022-05-05T11:56:15Z

‎WEIGHT AND CG LIMITS

@@ Line 13: / Line 13: @@
 !Limit
 |-
-|Max Gross Weight:	||2,000 lb
+|Max Gross Weight:	||2,100 lb
 |-
 |Max Forward CG:	||118 inches

@@ Line 23: / Line 23: @@
 === EMPTY WEIGHT AND CG ===
-The empty weight and CG of this aircraft are:
+The empty weight and CG of this aircraft are (Empty aircraft weight includes full water level in boiler with empty reservoir and fuel tank):
 {| class=wikitable
@@ Line 35: / Line 35: @@
 |Empty Moment:	||1.58 M-lb-in
 |}
 === CG ARM DATA ===

@@ Line 35: / Line 35: @@
 |Empty Moment:	||1.58 M-lb-in
 |}
 === CG ARM DATA ===

← Older revision		Revision as of 12:13, 5 May 2022
Line 51:		Line 51:

	=== WEIGHT AND CG CALCULATION ===		=== WEIGHT AND CG CALCULATION ===
−	Total weight is calculated by adding total weight of empty aircraft, fuel, passengers and baggage~~. Empty aircraft weight includes full water level in boiler with empty reservoir and fuel tank~~. Fuel weight can be calculated assuming 7.0 pounds per gallon of medium fuel oil. Water in the reservoir can be assumed to weight 8.3 pounds/gallon. 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.	+	Total weight is calculated by adding total weight of empty aircraft, fuel, passengers and baggage. Fuel weight can be calculated assuming 7.0 pounds per gallon of medium fuel oil. Water in the reservoir can be assumed to weight 8.3 pounds/gallon. 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.

← Older revision		Revision as of 12:13, 5 May 2022
Line 51:		Line 51:

	=== WEIGHT AND CG CALCULATION ===		=== WEIGHT AND CG CALCULATION ===
−	Total weight is calculated by adding total weight of empty aircraft, fuel, passengers and baggage. Empty aircraft weight includes full water level in boiler with empty reservoir and fuel tank.	+	Total weight is calculated by adding total weight of empty aircraft, fuel, passengers and baggage. Empty aircraft weight includes full water level in boiler with empty reservoir and fuel tank. Fuel weight can be calculated assuming 7.0 pounds per gallon of medium fuel oil. Water in the reservoir can be assumed to weight 8.3 pounds/gallon. 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.
−	Fuel weight can be calculated assuming 7.0 pounds per gallon of medium fuel oil. Water in the reservoir can be assumed to weight 8.3 pounds/gallon. 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.

@@ Line 43: / Line 43: @@
 !Limit
 |-
-|Pilot/Co-Pilot	||119 in (3.02 m)
+|Pilot/Co-Pilot	||79 in (2.01 m)
 |-
-|Fuel || 168 in (4.26 m)
+|Fuel || 114 in (2.89 m)
 |-
-|Water Reservoir|| 174 in (4.42 m)
+|Water Reservoir|| 139 in (3.53 m)
 |}
 === 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 5.8 pounds per gallon of (100LL) 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.

@@ Line 29: / Line 29: @@
 !Limit
 |-
-|Empty Weight:	||7,645 lb
+|Empty Weight:	||1,294  lb
 |-
-|Empty Aircraft CG:	||167.7 in
+|Empty Aircraft CG:	||122.8 in
 |-
-|Empty Moment:	||1.28 M-lb-in
+|Empty Moment:	||1.58 M-lb-in
 |}

@@ Line 15: / Line 15: @@
 |Max Gross Weight:	||2,000 lb
 |-
-|Max Forward CG:	||157 inches
+|Max Forward CG:	||118 inches
 |-
-|Max Aft CG:	        ||177 inches
+|Max Aft CG:	        ||127 inches
 |}