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Beechcraft M35 Bonanza Weight and Balance Calculator

Aircraft reference: Beechcraft M35 Bonanza production years, model information and certification

This calculator represents the M35 Bonanza four-seat configuration using main tanks only; optional fifth seat and auxiliary fuel not represented. Enter the current basic empty weight and arm from the certified weight and balance record for the individual aircraft.

Maximum takeoff weight: 2,950 lbs. Usable fuel represented: 44 US gal. Fuel arm: 75 in.

Data source: FAA Type Certificate Data Sheet 3A15. How WBcalc sources aircraft data

Enter the aircraft loading and fuel plan to check takeoff and expected landing conditions. After calculating, you can print or save the completed weight and balance worksheet as a PDF.


Beechcraft M35 Bonanza (4-seat, main tanks only) specifications

SpecificationValue
Maximum takeoff weight2,950 lbs
Maximum landing weight2,950 lbs
Forward CG at 2,475 lbs or less77 in
Forward CG at 2,525 lbs77.5 in
Forward CG at 2,950 lbs82.1 in
Aft CG limit84.7 in
Usable fuel44 US gal
Fuel arm75 in

Source: FAA Type Certificate Data Sheet 3A15.

Beechcraft M35 Bonanza (4-seat, main tanks only) CG limits

Aircraft weightForward CG limitAft CG limit
2,475 lbs77 in85.7 in
2,525 lbs77.5 in85.7 in
2,950 lbs82.1 in84.7 in

The calculator uses the published CG envelope points and linear interpolation between forward-limit breakpoints where applicable.

Beechcraft M35 Bonanza (4-seat, main tanks only) loading stations

StationArmLimit
Front seats85 in
Rear seats121 in
Baggage140 in270 lbs

Beechcraft M35 Bonanza (4-seat, main tanks only) fuel capacity

This calculator uses 44 US gallons of usable fuel at an arm of 75 inches.

Beechcraft M35 Bonanza (4-seat, main tanks only) baggage limits

Baggage is limited to 270 lbs

Utility category limits

The CG envelope on this page is for the utility category.


About this Beechcraft M35 Bonanza (4-seat, main tanks only) configuration

This page represents the utility-category Beechcraft M35 Bonanza (4-seat, main tanks only) configuration identified in FAA Type Certificate Data Sheet 3A15. The calculator uses a maximum takeoff weight of 2,950 lb and 44 US gal of usable fuel.

The reference datum for the loading arms on this page is Datum defined by FAA TCDS 3A15.

Need help with the terminology? Read the aircraft weight and balance guide or the CG envelope guide.

Related aircraft

Beechcraft J35 Bonanza (main tanks only), Beechcraft K35 Bonanza (4-seat, main tanks only), Beechcraft H35 Bonanza (main tanks only)

Beechcraft M35 Bonanza (4-seat, main tanks only) FAQ

What maximum takeoff weight does this Beechcraft M35 Bonanza (4-seat, main tanks only) calculator use?

This calculator uses a maximum takeoff weight of 2,950 lb for the configuration identified on this page.

How much usable fuel is represented for the Beechcraft M35 Bonanza (4-seat, main tanks only)?

This page uses up to 44 US gal of usable fuel at an arm of 75 in.

What baggage limit is represented for the Beechcraft M35 Bonanza (4-seat, main tanks only)?

Baggage is limited to 270 lb on this page.

Source and applicability

Source: FAA Type Certificate Data Sheet 3A15. Check the current POH or AFM, aircraft weight and balance record, equipment list and applicable supplements for the individual aircraft.

WBcalc is a planning aid. Check the current POH or AFM, aircraft weight and balance record, equipment list and applicable supplements before flight.

Need model context? View the Beechcraft M35 Bonanza Aircraft Reference page for production years, family information and certification details.
Weight and balance guides: Weight and balance · Center of gravity · CG envelope · Moment · Basic empty weight · Fuel weight

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