Weight & Balance Calculator
For training and reference only.
Not a substitute for the aircraft’s current weight-and-balance record.
Always verify against the actual airframe’s W&B sheet and the manufacturer’s flight manual before flight.
The pilot in command is responsible for ensuring the aircraft is loaded within limits.
Enter occupant weights
Both front and rear occupant weights are required. The CG envelope is for dual flight only.
CG Envelope
Dual Flight
Preliminary. The L-23 Super Blanik POH uses a graphical balance chart with no published numerical moment arms. Occupant station moment arms shown here are estimates back-solved from the POH solo minimum (front -47 in, rear +9 in from datum). Empty weight and CG default to POH typical (683 lb at 67.30% MAC). Verify against N8023’s current weight-and-balance record before relying on the result.
L-23 Super Blanik — Preliminary Data
Preliminary. The L-23 Super Blanik POH uses a graphical balance chart with no published numerical moment arms. Occupant station moment arms shown here are estimates back-solved from the POH solo minimum (front −47 in, rear +9 in from datum). Empty weight and CG default to POH typical (683 lb at 67.30% MAC).
Verify against N8023’s current weight-and-balance record before relying on the result.