Beechcraft Bonanza 33

Piston single engine • Low Wing • Retractable gear

Range Map

Origin:

nm at current load

• two fingers to move map

Payload vs. Range

Configure weights

Default: 190 lbs

Default: 30 lbs

Occupants
lbs lbs / pax

gal

Fuel on board

lbs

Extra weight

nm

Range

Available Range / nm
Mission capable. Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required. You'll need to leave gallons of fuel behind ( gal usable for nm range).
Over max gross weight. Reduce payload by lbs to safely operate this aircraft.
Extra weight is the additional payload available with your selected passengers.

Mission Profile

Endorsements & ratings:
  • High-Performance
  • Complex
172
KTAS
Cruise Speed
717
nm
Max Range
17858
ft
Service Ceiling
6
Occupants
831
lbs
Wet Payload
Used market Only available used

Estimated Ownership Costs

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About the Beechcraft Bonanza 33

Type certificated 1959

Overview

The Beechcraft Bonanza 33 is a single-engine, four-to-six-seat retractable-gear piston aircraft built by Beech Aircraft (later Raytheon, then Hawker Beechcraft) from 1959 to 1995. It is the straight-tail member of the Bonanza family, sharing the V-tail Model 35’s fuselage and wing but substituting a conventional vertical fin and horizontal stabilizer. The line opened as the Debonair (Model 35-33 through D33) with a 225 to 260 hp Continental IO-470, was renamed Bonanza with the E33 in 1967, and matured into the F33A of 1970 to 1995, powered by the 285 hp Continental IO-520-BB. Certificated under FAA Type Certificate 3A15, the F33A carries a 3,400-pound maximum takeoff weight, 74 gallons usable fuel, and a book cruise near 172 knots.

The Bonanza 33 suits an owner who wants Bonanza handling and build quality without the V-tail’s distinctive rudder-elevator mixing. The cabin seats four as standard and accepts optional fifth and sixth seats on later serials, in the original narrower Bonanza fuselage rather than the stretched club cabin of the six-seat A36. It shares type certificate 3A15 with its V-tail sibling, the V35B, and with the larger Model 36. Buyers commonly cross-shop it against the Cessna 210, the Piper Cherokee Six, and the Cirrus SR22 when weighing speed, useful load, and cabin size against acquisition and maintenance cost. Choose the Bonanza 33 when you want a fast, conventionally-tailed Beechcraft single with proven IO-520 power and you do not need the A36’s larger six-seat cabin.

Key Features for GA Buyers

  • Continental IO-520-BB, 285 hp. The representative F33A pairs the 285 hp fuel-injected six with a 1,700-hour TBO, giving the airframe roughly 172-knot cruise on about 13 to 16 gallons per hour depending on power setting.
  • Conventional empennage. The straight tail removes the V-tail Bonanza’s coupled yaw-pitch behavior, which lowers the transition workload for pilots moving from conventional-tail aircraft and simplifies some inspections.
  • Beechcraft cabin and build. The 33 shares the Bonanza fuselage, control feel, and door layout, so it delivers the family’s ride and finish in a four-to-six-place configuration.
  • Single type certificate with the V35B and 36. Sharing TCDS 3A15 with the rest of the family means a deep parts ecosystem, broad type-club support through the American Bonanza Society, and well-documented airworthiness data.

Trade-offs

  • Cabin size versus the A36. The 33 seats four as standard and up to six with the optional seats, but in the original narrower Bonanza cabin; buyers who need the larger stretched six-seat club cabin step up to the A36.
  • Retractable-gear cost and discipline. The electric landing gear adds inspection, maintenance, and insurance cost over fixed-gear singles, and gear-up risk requires currency and procedure discipline.
  • IO-520 overhaul reserve. A standard-shop overhaul runs near $50,500, which at the 1,700-hour TBO adds roughly $30 per hour in reserve before fuel and routine maintenance.
  • Older airframes. With production ending in 1995, every example is at least three decades old; corrosion history, logbook continuity, and prior damage matter more than headline specs.

See Also

Technical Specifications

Dimensions & Weights

Wingspan 33.5 ft
Height
8.25 ft
Length
26.67 ft
Parking area (ft2)
1377.65 ft2
Max Takeoff Weight
3,400 lbs
Max Landing Weight
3,400 lbs
Useful Load
1,275 lbs
Fuel Capacity
74 gal

Performance

Cruise Speed
172 KTAS
Never-Exceed (VNE)
Source: FAA Type Certificate Data Sheet 197 KIAS
Max Structural Cruise (VNO)
Source: FAA Type Certificate Data Sheet 167 KIAS
Approach Speed
75 KIAS
Stall, Clean (VS1)
63 KIAS
Range
717 NM
Service Ceiling
17,858 ft
Rate of Climb
1167 fpm
Takeoff over 50 ft obstacle
1,769 ft
Landing ground roll
1,324 ft

Engine

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Sources

Where the figures on this page come from. Beechcraft Bonanza 33 specifications are traced to published references; estimated values are flagged inline next to the figure.

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