Weight & Balance for Beechcraft V35B Bonanza
Beechcraft V35B Bonanza · Weight & Balance
Overview
This document provides the weight and balance information for the Beechcraft V35B Bonanza, specifically for aircraft N149BD with serial number D-9924. It outlines the procedures for weighing the aircraft, determining the center of gravity (CG), and calculating the moment based on various load configurations. The document is intended for pilots and maintenance personnel who need to ensure the aircraft is within its weight limits and properly balanced for safe operation. It includes detailed measurements and calculations necessary for accurate weight and balance assessments, which are critical for flight safety.
- Total weight of the aircraft: 2,243 lbs
- Empty CG: 80.12737 inches
- Nose wheel arm: 12 inches
- Main wheel arm: 96.1 inches
- Total moment: 179,725.7 lb-in
- Weight of fuel: 444 lbs at 75 inches
- Weight of front seat passengers: 340 lbs at 87 inches
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at www.bonanza.org. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Weight & Balance
- Pages ·
- 1
- File size ·
- 115 KB
- Copy found at ·
- www.bonanza.org
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In this document
Weighing Procedure
The document outlines a step-by-step procedure for weighing the Beechcraft V35B Bonanza. It includes draining all fuel, leveling the aircraft using plumb bobs, and marking datum points for accurate measurements. Specific measurements from the datum to the nose wheel axle and main wheel axle are provided to determine the weight arms.
Weight and Moment Calculations
The weight and moment calculations are detailed in a table format, showing the weights of the right main wheel, left main wheel, and nose wheel, along with their respective arms and moments. The total weight of the aircraft is calculated as 2,243 lbs with a total moment of 179,725.7 lb-in.
Center of Gravity (CG)
The document provides the empty center of gravity (CG) as 80.12737 inches. It also includes calculations for various load configurations, such as front seat passengers, fuel, and baggage, to determine the overall CG and ensure it remains within safe limits.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Safety notes
- Ensure the aircraft is level before taking measurements.
- Verify that the total weight does not exceed the maximum allowable weight for safe flight.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Full document text
N149BD - S/N D-9924 1. Drain all fuel. 2. Place plane on the scales. 3. Level the plane front to back using a plumb bob to align the leveling screws on the left side of the fuselage. Level the plane left to right by measuring each wing tip to the floor. 4. Drop a plump bob from the center of the jack points to the floor and mark the floor. 5. Measure 83.1" forward from the jack point mark and mark the floor. This is datum. 6. Measure from datum to the center of the nose wheel axle and note the measurement (12"). This is the nose wheel arm. 7. Pull a string between the main axle centers. Drop a plumb bob from this string to the floor and make a mark. 8. Measure from the main axle center line mark to the datum mark and note this measurement (96.1"). This is the main wheel arm. Weight Arm Moment Right Main Wheel 904 96.1 86874.4 Left Main Wheel 913 96.1 87739.3 Nose Wheel 426 12 5112 Total 2243 179725.7 Empty CG 80.12737 Weight Arm Moment/100 AC Empty Weight 2,243 80.13 1,797.32 Front Seat (85-89) 340 87.00 295.80 Rear Seat (121-127) 0 127.00 0.00 Fuel 444 75.00 333.00 Baggage 0 154.00 0.00 3,027 2,426