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Beech F33A Bonanza

Beechcraft F33A Bonanza · Pilot's Operating Handbook

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Overview

This document serves as the Pilot's Operating Handbook (POH) for the Beechcraft F33A Bonanza, detailing its specifications, performance, and operational guidelines. It is intended for pilots and aviation enthusiasts who seek comprehensive information about the aircraft's capabilities and features. The F33A is known for its combination of payload, performance, and price, making it a popular choice among general aviation pilots. The handbook includes critical data on the aircraft's engine, weight limits, fuel capacity, and performance metrics, ensuring that pilots can operate the aircraft safely and efficiently.

  • 285 horsepower engine with a maximum ramp weight of 3,412 pounds.
  • Cruise speed of 150 knots indicated at 8,500 feet with 75% power.
  • Best rate of climb is 96 KIAS with a climb rate of 1,200 feet per minute.
  • Standard fuel capacity is 80 gallons, with 74 gallons usable.
  • Max landing distance over a 50-foot obstacle is 1,300 feet.

Document

Source

Originally published by aeroresourcesinc.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Pilot's Operating Handbook
Year
1991
Pages
5
File size
4.8 MB
Publisher
aeroresourcesinc.com
Documentation completeness
4/7

Most owners only have the POH. Here's the essential set for the Beechcraft F33A Bonanza.

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In this document

Specifications

The Beechcraft F33A Bonanza is powered by a Teledyne Continental 10-520-BB engine, delivering 285 horsepower at 2,700 RPM. It features a McCauley three-blade constant-speed propeller with an 80-inch diameter. The aircraft has a maximum ramp weight of 3,412 pounds and a useful load of 1,175 pounds. Fuel capacity is 80 gallons, with 74 gallons usable, and the oil capacity is 12 quarts.

Performance

The F33A has a maximum level speed of 182 knots at sea level and a service ceiling of 17,858 feet. The best rate of climb is 96 KIAS, yielding a climb rate of approximately 1,200 feet per minute at full power. At 8,500 feet and 75% power, the aircraft achieves a cruise speed of 150 knots indicated, translating to 173 knots true airspeed.

Limiting and Recommended Airspeeds

Key airspeeds for the F33A include Vx (best angle of climb) at 77 KIAS, Vy (best rate of climb) at 96 KIAS, and Vfe (max flap extended) at 154 KIAS. The stall speed in a clean configuration is 64 KIAS, while the landing configuration stall speed is 52 KIAS.

Avionics and Equipment

The standard avionics package includes dual KX 155 nav/coms, a KR 87 ADF, a KN 63 DME, a KT 76A transponder, and a KMA 24 audio panel. An altitude encoder is included in the 1991 model, enhancing operational capabilities in controlled airspace.

Operational Considerations

The F33A is certified in the Utility category, allowing for higher load limits compared to Normal category aircraft. The aircraft's design includes features for smooth handling and effective performance in various flight conditions.

Safety notes

  • Ensure weight and balance calculations are performed before flight.
  • Monitor airspeed closely during climb and descent to avoid exceeding Vne.

Full document text

King Air C90A, which appeared as the Model 90 in 1964. However, the 33 and 90 have a few years to go to equal the V- tail Model 35 Bonanza's 35-year produc- tion run, which ended in 1982.) What gives the F33A such value today is its combination of payload, perfor- mance, and price. Stultz and I flew N1550D, a 1989 F33A that Beech has assigned to its transportation department for use by employees on company business. De- spite its 500 hours, it is a cream puff- shiny clean and well-equipped with an optional Bendix/King KFC 150 flight control system and air conditioning. It also has dual controls, a mixed blessing. Two can fly, but the massive yoke bar obscures the entire subpanel containing electrical switches and circuit breakers; gear, flap, cowl flap, and trim switches and indicators; and the power controls. My only real beef with the F33A is the outdated panel configuration. Avionics are shunted off to the right side of the panel, while the engine instrument clus- ter is assigned center stage. Just about everything else is hidden away down on the subpanel. The flap switch is to the left of the gear switch, and the throttle and prop controls are separated by an auxiliary fuel pump switch, while the mixture control is below the throttle. Beech fixed the panel layout on the 36 series in 1984, but the F33A remains unchanged. It's the little things that, even after all these years, set the F33A apart. The bag- gage door is cargo size and fitted with large, robust latches. The baggage area is cavernous and can swallow 270 pounds of cargo. A fifth seat can be in- stalled in the baggage hold, but its use is limited by weight and balance restric- tions. All placards are silkscreened onto the panels rather than applied as adhe- sive labels. Strobe and recognition lights are faired into the metal wing tips. The three-light strobe system is standard equipment, as are the heated pitot tube and a profusion of static wicks. The cabin is tall, with plenty of leg- and headroom. The generously sized windows contribute to the feeling of spaciousness and make for excellent in- flight visibility. The standard F33A inte- rior is by no means Spartan. Cloth seats and carpeting throughout are included in the base price. Leather is not listed as an option, but in fact, if a customer de- mands to lounge on King Air leathers, it will be done. The leather upholstery shown in the photographs \o\jth this 70. JANUARY 1991 - • story is in a 1990 F33A offered by United Beechcraft in Wichita. The F33A is a solid "full fuel and three adults" airplane. N1550D was topped off with 74 gallons usable fuel when three of us boarded for a lunch flight to Ponca City, south of Wichita. The cal- culations showed that we could top off the tanks at Ponca City, then go in and eat 30 pounds of excellent Mexican food at the airport cafe and still stay on the legal side of the 3,412-pound maximum ramp weight. This despite Beech's in- house F33A being a bit heavy on empty weight due to the 70-pound air con- ditioning system. Minus the AC and 10 gallons of fuel, another Beechcrafter could have joined us for lunch. The 285-horsepower Teledyne Conti- nental 10-520 engine and three-blade, 80-inch McCauley propeller give the F33A good performance. After takeoff, power was reduced from full throttle and 2,700 rpm to 25 inches manifold pressure and 2,500 rpm. The initial 96- knot best rate climb speed yielded 1,200 feet per minute and no view over the nose. At a more comfortable 115 knots, the rate was 800 fpm, which decreased to 600 fpm as we passed through 8,000 feet. The F33A does not have rudder trim, but the engine is canted to offset torque, and it took minimal rudder pres- sure in the climb to center the ball. Bonanzas have a deserved reputation for smooth, effortless handling, espe- cially in roll. Control surfaces are at- tached with roller bearings, and the aile- rons and rudder are interconnected. In steep turns, the airplane can be trimmed for hands-off flying. Once at altitude, we sampled a variety of cruise power configurations and found performance to be slightly better than promised in the pilot's operating handbook. At 8,500 feet and 75-percent power (2,500 rpm and full throttle), in- dicated airspeed was 150 knots for 173 knots true on 14.4 gallons per hour. But engine and airframe seemed to prefer 65-percent power (2,300 rpm). Vibration was noticeably less than at 75 percent or even 55 percent (2,100 rpm). At 65 percent, cruise true airspeed worked out to be about 165 knots on just under 14 gph. Four hours flown at 65- percent power would be a comfortable leg. That would leave a full hour's fuel in the tanks for insurance. Don't want to stop enroute? Then back the power off to 45 percent and drone along at about 135 knots for 6.5 hours. Bonanzas build up speed quickly in a AOPA PILOT. 71 descent, but the F33A has some built-in safeguards: The landing gear and ap- proach flaps can be extended at 154 knots, 12 knots below Vno. The drag from gear and flaps is such that the nose can be pushed over and the VSI pegged at better than 4,000 fpm down without exceeding 154 knots. The high gear and flap speed allows for great flexibility in the terminal area. We practiced a couple of high-speed in- strument approaches, flying the local- izer course at 165 knots. Coming up on the outer marker or final approach· fix, reduce power to slow to 154, then dump gear and flaps and slide down the final approach course at about 120 knots, which is within the white arc. H the landing is the measure of a llight, then an F33A pilot will finish with a flourish every time. Dual pitch-trim tabs are helpful for nailing the final ap- proach speed and angle, and the over- size main tires help to make each touch- down a squeaker. It really is one of the nicest-landing airplanes. The F33A is certified in the Utility cat- egory to higher load limits than is a Nor- mal category airplane. Beech built an

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aerobatic version, the F33C, that is iden- tical to the 33A except for some struc- tural strengthening in the fuselage. The standard Bendix/King avionics package in the F33A includes a pair of KX 155 nav /coms (one with glideslope receiver) and indicators, KR 87 ADF and indicator, KN 63 DME and indicator, KT 76A transponder, KMA 24 audio panel with marker beacon, and avionics mas- ter switch. Up to now, Beech has not included an altitude encoder in the standard pack- age. To do so would have affected the bottom line, and not every customer wanted one. But with altitude encoding now a prerequisite for operating in ARSAs as well as within 30 miles of a terminal control area airport, Beech has decided to add a Bendix/King KEA 130A encoding altimeter to the standard equipment list for 1991. Few factory-installed options are available for the F33A compared to the 36-series Bonanzas. The most popular is the Bendix/King KFC 150 llight control system, which includes a two-axis auto- pilot, horizontal situation indicator, and llight director. Other avionics options include a 3M WX-lOOO Stormscope,. yaw damper, control-wheel microphone button, and ground communications switch. This year, Beech is adding a Bendix/King KLN 88 loran and control- 72 • JANUARY 1991 The generously sized windows contribute to the feeling of spaciousness and make for excellent in-flight visibility. Beech F33A Bonanza Base price: $156,000 Specifications Teledyne Continental 10-520-BB, 285 hp at 2,700 rpm Recommended TBO 1,700 hr Propeller McCauley, three-blade, constant- speed, 80-in diameter 26.7 ft 8.25 ft 33.5 ft 181 sq ft 18.8 lb/sq ft 11.9Ib/hp 4-5 10.08 ft 3.5 ft 4.17 ft 2,237 Ib 2,365 lb 3,4121b 1,1751b 1,0471b 731lb 603lb 3,400 lb 3,400 lb 80 gal (74 gal usable) 480 lb (444 lb usable) 12 qt 270 lb, 35 cu ft wheel-mounted transponder ident but- ton to the options list. Back in 1985, Beech Aircraft Corpora- tion launched an effort to boost sagging sales of the F33A, the sole remaining four-place, piston-powered single pro- duced by the company. It was a simple plan: Make the most popular optional features, including IFR avionics, stand- ard equipment, and price the equipped airplane attractively. Although the $171,000 price repre- sented a saving of about $11,000, the cut was not deep enough to pull customers off the street. Beech bit the bullet again and dropped the price further, to $164,750. Still the response was modest. In 1987, Beech recalculated. To roll back the price even further, some econo- mies of scale were necessary. Production was increased to 100 airplanes for the year. (About 30 had been built the year before.) Equipping each identically and offering few options made for more effi- cient and less costly manufacturing. In addition, Beech got commitments from Teledyne Continental and Bendix/King to provide engine and avionics at special prices and passed the savings along. The savings were extraordinary, given the history then of large annual price hikes for general aviation airplanes. List price of a 1987 F33A was $131,750-a $33,000 discount over the 1986 model. Prices have since crept up incremen- tally, an average of about 5 percent per year. A 1990 F33A listed for $156,000. Beech has not announced the 1991 price, but it will be higher. One reason is the addition of the encoding altimeter. Another is that Beech's profit margin on the F33A is said to be slim to none. Late in 1990, rumors began to surface that Beech would back out of building piston-powered models entirely. Not true, according to Beech. In fact, an in- crease in production had been planned for 1991. However, rising fuel prices and uncertainty over the direction of the economy softened the market for new airplanes. Beech now plans to build 100 F33As in 1991. There may not be much that is new about the F33A, but it still is one of the most popular singles on the market and has been since Beech began its special pricing program. That says a lot about the depth of pilots' regard for the name . Bonanza. And there is one other remark- •. able fact: You probably can buy one in 1991 for no more than you would have paid a half-dozen years ago. Not a bad value, that. 0 154 KIAS 154 KIAS 167 KIAS 196 KIAS 64 KIAS 52 KIAS Max demonstrated crosswind component 17 kt Rate of climb, sea level 1,157 fpm Max level speed, sea level 182 kt Cruise speed/endurance w/45-min rsv, std fuel (fuel consumption) @ 75% power, best economy 172 ktj4.2 hr 6,000 ft (91.4 pph/15.2 gph) @ 65% power, best economy 168 kt/5.15 hr 10,000 ft (73.8 pph/12.3 gph) @ 55% power, best economy 157 kt/6 hr 12,000 ft (62.1 pph/l0.4 gph) Service ceiling 17,858 ft Landing distance over 50-ft obstacle 1,300 ft Landing distance, ground roll 760 ft Limiting and Recommended Airspeeds Vx (best angle of climb) 77 KIAS Vy (best rate of climb) 96 KIAS Va (design maneuvering) 134 KIAS Vfe (max flap extended) 154 KIAS VIe (max gear extended) 154 KIAS Vlo (max gear operating) Extend Retract Vno (max structural cruising) Vne (never exceed) Vs, (stall, clean) Vso (stall, in landing configuration) All specifications are based on manufacturer's cal- culations. All performance figures are based on stand- ard day, standard atmosphere, sea level, gross weight conditions unless otherwise noted. For more information, contact Beech Aircraft Cor- poration, Post Office Box 85, Wichita, Kansas 67201- 0085; telephone 316/681-7111. 0 1,000 ft 1,740 ft Powerplant Length Height Wingspan Wing area Wing loading Power loading Seats Cabin length Cabin width Cabin height Empty weight Empty weight, as tested Max ramp weight Useful load Useful load, as tested Payload w/full fuel Payload w/full fuel, as tested Max takeoff weight Max landing weight Fuel capacity, std Oil capacity Baggage capacity Performance Takeoff distance, ground roll Takeoff distance over 50-ft obstacle AOPA PilOT • 73