Beechcraft F33A Bonanza Performance and Specifications
Beechcraft F33A Bonanza · Performance Data
Overview
This document provides detailed performance data and specifications for the Beechcraft F33A Bonanza, a single-engine aircraft manufactured between 1970 and 1994. It is intended for pilots and aviation enthusiasts seeking to understand the aircraft's capabilities, including speed, climb rates, and weight limits. The performance section outlines critical flight parameters such as stall speeds, takeoff distances, and maximum speeds, while the specifications section includes information on dimensions, engine details, and fuel capacity. This reference is essential for flight planning and operational awareness.
- Max Speed (Vne): 197 Knots
- Takeoff Distance (50Ft Obstacle): 1,769 Feet
- Stall Speed (Vs): 63 Knots
- Max Takeoff Weight: 3,400 Lbs
- Usable Fuel: 74 Gallons
- Rate Of Climb: 1,167 fpm
- Service Ceiling: 17,858 Feet
Document
Source
Originally published by airmart.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Performance Data
- Pages
- 1
- File size
- 16 KB
- Publisher
- airmart.com
Most owners only have the POH. Here's the essential set for the Beechcraft F33A Bonanza.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Performance
The performance section details the flight characteristics of the Beechcraft F33A Bonanza. Key metrics include a maximum speed (Vne) of 197 knots and a maximum structural cruise speed (Vno) of 167 knots. The stall speeds are noted as 63 knots (Vs) and 51 knots (Vso). Takeoff performance is highlighted with a takeoff distance over a 50-foot obstacle of 1,769 feet and a ground roll of 1,002 feet. Landing distances are also specified, with a 50-foot landing distance of 1,324 feet and a landing ground roll of 763 feet. The aircraft has a rate of climb of 1,167 feet per minute and a service ceiling of 17,858 feet.
Specifications
The specifications section outlines the manufacturing details and physical characteristics of the Beechcraft F33A Bonanza. It was manufactured from 1970 to 1994, with a serial number range from CE-290 to CE-1791. The aircraft is powered by a TCM IO-520-BA engine, producing 285 BHP with a time between overhaul (TBO) of 1,700 hours. The aircraft dimensions include a length of 26 feet 8 inches, a wingspan of 33 feet 6 inches, and a tail height of 8 feet 3 inches. It seats four people, including the pilot, and has a cabin length of 141 inches, width of 42 inches, and height of 50 inches. The usable fuel capacity is 74 gallons, and the total oil capacity is 12 quarts.
Weight Limits
The weight limits for the Beechcraft F33A Bonanza are crucial for safe operation. The maximum ramp weight is 3,412 pounds, while the maximum takeoff and landing weights are both 3,400 pounds. The baggage limit is set at 270 pounds. The aircraft has a range of 717 nautical miles, making it suitable for various flight operations.
Full document text
Beechcraft F33A Bonanza Performance and Specifications Performance • Max Speed Vne - 197 Knots • Max Structural Cruise Vno - 167 Knots • Flaps Ext Speed 15° Vfe - 154 Knots • Landing Gear Extension - 154 Knots • Stall Speed Vs - 63 Knots • Stall Speed Vso - 51 Knots • Maneuvering Speed Va - 134 Knots • TakeOff Distance (50Ft Obstacle) - 1,769 Feet • TakeOff Ground Roll - 1,002 Feet • 50’ Landing Distance - 1,324 Feet • Landing Ground Roll - 763 Feet • Rate Of Climb - 1,167 fpm • Service Ceiling - 17,858 Feet Specifications • Manufactured - 1970 thru 1994 • S/N Range - CE-290 thru CE-1791 • Engine - TCM IO-520-BA, 285 BHP, TBO 1,700 • Dimensions - Length - 26’8”, Wingspan 33’6””, Tail Height 8’3” • Total seats including Pilot - 4 • Cabin Dimensions - Length 141”, Cabin Width 42”, Height 50” • Usable Fuel - 74 Gallons • Total Oil – 12 Quarts • Wing Area - 181 SF • Wing Loading - 18.3 Lbs/SF • Power Loading - 11.6 Lbs/HP Weight Limits • Max Ramp Weight – 3,412 Lbs • Max TakeOff Weight - 3,400 Lbs • Max Landing Weight – 3,400 Lbs • Baggage - 270 Lbs • Range - 717 NM