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SINGLE-ENGINE PISTON

Beechcraft Bonanza 35

One model from FAA type certificate data sheet A-777. Every figure below is quoted from the sheet. Open any “Source” to see the words it comes from.

THE DATA SHEET

Authority
Federal Aviation Administration (United States)
Sheet
Type Certificate Data Sheet A-777
Revision
62
Date
November 27, 2017
Holder
Textron Aviation Inc.
Licence
US Government work, public domain (17 U.S.C. 105)

Open the sheet on the FAA Dynamic Regulatory System (opens in a new tab)

Performance figures (stall speeds, take-off and landing distances, climb, cruise and fuel burn) are in the aircraft's flight manual (POH/AFM), which we cannot reproduce. Always use the flight manual for the aircraft you fly.

This is a United States Federal Aviation Administration sheet. We show it as a US certification document, not as an Australian or New Zealand rule. Units are the sheet's own: pounds, US gallons and quarts, and knots or mph as stated.

How we copied the sheet. Quotes are from our stored text copy of the sheet, taken from the text layer of the FAA's online viewer. We rebuilt lines from the text positions, joined wrapped lines, marked wide gaps between table cells with |, removed page headers and footers, and replaced symbol-font characters with the symbols they print as. Check the original sheet before relying on any figure.

Models not shown. The sheet also covers the 35, A35 to F35 and 35R. We include the G35, the last model on the sheet.

SPEC SHEET

Beechcraft Bonanza 35: G35

Bonanza

The sheet's heading for this modelModel G35, Bonanza, 4 PCLM (Utility Category)

Source for the model heading

IX. Model G35, Bonanza, 4 PCLM (Utility Category), Approved December 1, 1955

Compare the G35 with another aircraft

Engine

Engine
Continental E-225-8Engine serial numbers as the sheet gives them.
Source for Engine

Engine | Continental E-225-8 with S/N 30087 and On

Rated power
225 hptake-off, one minuteThe sheet gives a lower rating for all other operations.
Source for Rated power

Engine Limits | Takeoff (one minute) | 2650 rpm (225 hp)

Engine speed limit
2,650 rpmtake-off, one minute
Source for Engine speed limit

Engine Limits | Takeoff (one minute) | 2650 rpm (225 hp)

Propeller

Left out. The sheet lists propellers as equipment items, not in this model's section.

Fuel and oil

Fuel capacity
20 US galeach main tank≈ 75.7 L (converted)Left and right main tanks. The sheet lists optional auxiliary tanks.
Source for Fuel capacity

Fuel Capacity | Tank | Capacity Gal. | Usable Gal. | Arm L & R Main | 20 ea. | 17 ea. | (+ 75)

Usable fuel
17 US galeach main tank≈ 64.4 L (converted)
Source for Usable fuel

Fuel Capacity | Tank | Capacity Gal. | Usable Gal. | Arm L & R Main | 20 ea. | 17 ea. | (+ 75)

Oil capacity
10 US qt≈ 9.5 L (converted)
Source for Oil capacity

Oil Capacity | 10 qt. (+36)

Weights and loading

Maximum weight
Utility category2,775 lb≈ 1,259 kg (converted)
Source for Maximum weight, Utility category

Maximum Weight | 2775 lb.

Seats
4
Source for Seats

No. of Seats | 4 (2 at +86, 2 at +118)

Baggage limit
270 lb≈ 122 kg (converted)
Source for Baggage limit

Maximum Baggage | 270 lb. (+140).

C.G. range
Landing gear extended: (+83.2) to (+85.1) at 2775 lb; (+79.9) to (+85.7) at 2525 lb; (+76.5) to (+85.7) at 2265 lb or less
Source for C.G. range

C.G. Range (landing gear | (+83.2) to (+85.1) at 2775 lb. extended) | (+79.9) to (+85.7) at 2525 lb. (+76.5) to (+85.7) at 2265 lb. or less

Airspeed limits

Never exceed speed (Vne)
176 kt true indicatedThe sheet gives mph with knots in brackets. We show the knots.
Source for Never exceed speed (Vne)

Never exceed | 202 mph (176 knots) True Ind.

Maximum structural cruising speed (Vno)
152 kt true indicated
Source for Maximum structural cruising speed (Vno)

Maximum structural cruising | 175 mph (152 knots) True Ind.

Manoeuvring speed (Va)
113 kt true indicated
Source for Manoeuvring speed (Va)

Airspeed Limits | Maneuvering | 130 mph (113 knots) True Ind.

Maximum flap extended speed (Vfe)
104 kt true indicated
Source for Maximum flap extended speed (Vfe)

Flaps extended (normal) 120 mph (104 knots) True Ind.

Reference

Datum
83.1 inches forward of the jack pads on the front spars
Source for Datum

Datum | 83.1 inches forward of the jack pads on the front spars.

Specifications pertinent to all models: datum. FAA Type Certificate Data Sheet A-777, revision 62. This part of the sheet covers several models. Open the sheet (opens in a new tab)
Certification basis
Part 03 of the Civil Air Regulations effective November 13, 1945
Source for Certification basis

Certification Basis | Part 03 of the Civil Air Regulations effective November 13, 1945.

COCKPIT

The G35 limits on an airspeed indicator

Where the sheet gives them in knots, the dial shows Vne as a red line, the caution range from Vno to Vne as a yellow arc, a green tick at Vno and white ticks at the flap limit speeds (Vfe). The sheet gives flap limits, not instrument markings, and the stall speeds where the green and white arcs start are not in it.

PANEL LAYOUT

Classic six-pack

These are example panels drawn by us. They do not show the panel fitted to any Beechcraft Bonanza 35. Only the airspeed markings come from this model's data sheet.

  • 406080100120140160180200VfeVnoAIRSPEEDKNOTSAirspeed indicator
  • 2020101010102020Attitude indicator
  • 01234567891013hPaALTFEETAltimeter
  • LRTURN COORDINATOR2 MINNO PITCH INFORMATIONTurn coordinator
  • N36E1215S2124W3033Heading indicator
  • 0.5.5111.51.522UPDOWNVERTICAL SPEED1000 FT/MINVertical speed indicator
  • 05101520253035RPM×100Tachometer
  • 075150OIL°COil temperature
  • 060120OILPSIOil pressure
  • EEFFLRFUELFuel quantity
  • 0510SUCTIONin HgSuction gauge
0 kt

What the dial shows

  • Red line: never exceed speed (Vne)176 kt true indicated
    Source for the red line

    Never exceed | 202 mph (176 knots) True Ind.

  • Yellow arc: caution rangeFrom Vno to Vne, 152 kt true indicated to 176 kt true indicated
  • Green tick: Vno, top of the green arc152 kt true indicated
    Source for the green tick

    Maximum structural cruising | 175 mph (152 knots) True Ind.

  • White tick: Vfe, a flap limit speed104 kt true indicated
    Source for the white tick

    Flaps extended (normal) 120 mph (104 knots) True Ind.

  • Marks are drawn at the sheet's speeds in knots, which the sheet calls true indicated.
  • White tick marks the flap limit speed (Vfe) the sheet gives. The sheet gives flap limits, not instrument markings, so the flight manual says where this aircraft's white arc ends.
  • The low ends of the white and green arcs are stall speeds. They come from the flight manual, so we have left them unmarked.

The other instruments are drawn at rest and are not linked to this aircraft. Learn what each instrument shows in the cockpit explorer.

For learning only. Not for flight planning or use in flight. Figures are certification limits from Federal Aviation Administration, Type Certificate Data Sheet A-777, Revision 62, retrieved 31 October 2026. Conversions marked “converted” are our own arithmetic. No manufacturer images are used. The instruments are drawn by us. Back to all aircraft.