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Beechcraft K35 Bonanza (4-seat, main tanks only) Weight and Balance Calculator

This calculator represents the K35 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


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

SpecificationValue
Maximum takeoff weight2,950 lbs
Maximum landing weight represented2,950 lbs
Usable fuel represented44 US gal
Fuel arm75 in
Fuel density used by calculator6 lbs/US gal
Reference datumDatum defined by FAA TCDS 3A15

Beechcraft K35 Bonanza (4-seat, main tanks only) CG limits

WeightForward CGAft CG
2,475 lbs or less77 in85.7 in
2,525 lbs77.5 in85.7 in
2,950 lbs82.1 in84.7 in

Where a published limit changes between points, WBcalc uses straight-line interpolation between those points.

Beechcraft K35 Bonanza (4-seat, main tanks only) loading stations

StationArmLimit
Front seats85 in
Rear seats121 in
Baggage140 in270 lbs

Configuration represented by this calculator

K35 Bonanza four-seat configuration using main tanks only; optional fifth seat and auxiliary fuel not represented. Main tanks provide 44 US gal usable total at +75 in. Eligible serials D-5726 through D-6161.

Basic empty weight

Basic empty weight and empty CG are intentionally not prefilled. Use the current values from the individual aircraft's certified weight and balance record.

WBcalc is a planning aid. Verify serial-number applicability, POH/AFM revisions, supplements, STCs and the current aircraft weight and balance record before flight.

About this Beechcraft K35 Bonanza (4-seat, main tanks only) configuration

This page represents the normal-category Beechcraft K35 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 H35 Bonanza (main tanks only), Beechcraft M35 Bonanza (4-seat, main tanks only)

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

What maximum takeoff weight does this Beechcraft K35 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 K35 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 K35 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.

Weight and balance guides: Weight and balance · Center of gravity · CG envelope · Moment · Basic empty weight · Fuel weight

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