Beech 56TC Turbo Baron (1967)
Beechcraft 56TC Baron · Pilot's Operating Handbook
Overview
This document serves as the Pilot's Operating Handbook (POH) for the Beechcraft 56TC Turbo Baron, a twin-engine aircraft known for its performance and reliability. The 56TC model, introduced in 1967, features two Lycoming TIO-541-E1B4 engines, each producing 380 horsepower. This handbook provides essential information for pilots, including specifications, performance data, and operational procedures necessary for safe and efficient flight. It is particularly useful for pilots who operate this specific model, offering insights into its capabilities and limitations, as well as maintenance recommendations.
- Maximum takeoff weight: 5,990 lbs
- Cruise speed: 188 knots at 65% power
- Service ceiling: 32,200 feet
- Vmc: 83 KIAS
- Recommended TBO: 1,600 hours
Document
Source
Originally published by www.aeroresourcesinc.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Pilot's Operating Handbook
- Year
- 1967
- Pages
- 4
- File size
- 3.4 MB
- Publisher
- www.aeroresourcesinc.com
Common. Rarer than 2% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Beechcraft 56TC Baron.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the 56TC to your watchlist and track it in one place.
More Beechcraft 56TC Baronmanuals & documents
See all 22 →- Short-Fuselage BaronsAvionics Manual
- ABS Performance Worksheet: Baron/Travel Air PilotsTraining Manual
- EASA AD No.: 2024-0221Supplemental Type Certificate
- 2022 Product CatalogueChecklist
- Part Design ApprovalType Certificate
- Innoviator, LLC. AMM Supplement - Wingtip Position/Anticollision Light Support BracketWeight And Balance
- American Bonanza Society Magazine - August 2020Other Documents
- ABS/BPPP Performance Worksheet: Baron/Travel Air PilotsWeight And Balance
- LP Aero Plastics Product CatalogSpecifications
- American Bonanza Society Magazine - September 2014Other Documents
- SERVICE BULLETIN SB 28-4120Maintenance Manual
- MASTER MINIMUM EQUIPMENT LISTFlight Manual
In this document
Specifications
The Beechcraft 56TC Turbo Baron is powered by two Lycoming TIO-541-E1B4 engines, each delivering 380 horsepower at 2,900 RPM. The aircraft has a maximum takeoff weight of 5,990 lbs and a maximum landing weight of 5,990 lbs. It features a wingspan of 37 ft 10 in and a wing area of 199.2 sq ft, with a maximum fuel capacity of 146 gallons (142 gallons usable).
Performance
The 56TC Turbo Baron has a maximum level speed of 260 knots at sea level and a cruise speed of 188 knots with a fuel consumption of 31 gallons per hour at 65% power. The aircraft can achieve a rate of climb of 2,020 feet per minute at sea level and has a single-engine rate of climb of 412 feet per minute. The service ceiling is 32,200 feet, with a single-engine service ceiling of 18,600 feet.
Limiting and Recommended Airspeeds
Key airspeeds for the 56TC include Vmc (minimum control speed with one engine inoperative) at 83 KIAS, Vx (best angle of climb) at 106 KIAS, and Vy (best rate of climb) at 96 KIAS. The never exceed speed (Vne) is 260 KIAS, while the stall speed in landing configuration (Vso) is 70 KIAS.
Weight and Balance
The empty weight of the Beechcraft 56TC Turbo Baron is 3,650 lbs, with a maximum useful load of 2,340 lbs. The useful load when fully fueled is 1,488 lbs. Pilots must ensure that weight and balance calculations are performed prior to flight to maintain safety.
Maintenance and TBO
The recommended time between overhaul (TBO) for the engines is 1,600 hours. Regular maintenance is crucial for the performance and safety of the aircraft, and pilots should be aware of the costs associated with parts and repairs.
Safety notes
- Ensure weight and balance calculations are performed before flight.
- Unmodified 56TCs have placards prohibiting takeoff, slips, and skids with less than 25 gallons of fuel in each main tank.
Full document text
BYMARK M. LACAGNINA At 40 gph~ this piston twin buys peace of mind and King Air speed. AOPA PILOT. 29 ,'tmtillucd the first pilot to make a round-trip, transcontinental flight in a rotary-wing aircraft. When he was not touring the autogiro, Miller managed Poughkeep- sie Airport and one of the first aircraft repair shops in the country. Ouring his early career, Miller also joined the Ma- rine Reserve and was trained as a na- val aviator. Wasps were very reliable engines, and Miller never did find out how a Boeing 2470 would react to an engine failure over the Rockies. He left United Airlines after two years to test-fly John Kellett's "wingless" autogiros. With Kellett, Miller logged another first-the first scheduled operation of a rotary- wing aircraft. It was a demonstration project for Eastern Airlines. Ten times each day, for a year, Miller flew a six- mile route between the Philadelphia airport and the roof of the city's post office, carrying up to 350 pounds of mail in an autogiro. World War II inter- rupted the project, and Miller turned to flying the line in Oouglas OC-2s and -3s for Eastern and test-flying amphibi- ous naval aircraft for Columbia Air- craft. He went on to fly OC-4s and -7s and Lockheed Constellations and Elec- tras for Eastern. Miller retired as a OC-8 captain in 1965. Now 78 years old, Miller, AOPA 58843, often still flies over the Rockies, but the trips are much more comfortable than they were in the right seat of a Boeing 2470. The ramifications of an engine failure are clear. If his airplane should lose an engine, he can feather it and climb. Miller's airplane is a 1967 Beech 56TC Turbo Baron. (His other airplane is a 1951 Bonanza-the first Model C35 off the line.) The Turbo Baron is a rare bird and a hot rod. Introduced in PHOTOGRAPHY BY WIL.I.IAM A. FORD Cockpit small talk inevitably would succumb to the per- vading drone of the Pratt & Whitney Wasps. The sound was reassuring, and the young copilot tried not to dwell on what might hap- pen if the engines' duet should become a solo performance. He knew the as- surances by airline management that the Boeing 2470's single-engine ser- vice ceiling. was higher than the high- est mountain peak along the route. He also knew this might be perfectly true under standard conditions; but condi- tions on the route from Cheyenne to Oakland seldom were standard. No one knew what would happen once the aircraft drifted down into the clouds and began to pick up ice. The copilot did not want to be the one to find out. Although only 31 years old, the co- pilot, John MacOonald Miller, already was an experienced and seasoned avia- tor. He had learned to fly when flight instruction was a do-it-yourself affair. His reward for a hard summer's work assisting a barnstormer had been the barnstormer's airplane-a Curtiss IN-4 in atrocious condition. On his third flight, Miller began hopping passengers in the Jenny from a pasture near his home in Poughkeepsie, New York. Af- ter high school and a degree in me- chanical engineering from Pratt Insti- tute, he worked as a mechanic for a flying circus. He rebuilt a wrecked Standard J-1 and set off on his own to barnstorm the eastern states. In the early 1930s, Miller bought a Pitcairn PCA-2 autogiro and for three years gave aerobatic exhibitions all over the country. He performed loops, rolls on top of the loops and other maneuvers that did not have names. He became TURBO BARON The 56TC is a rare bird, a 760-harsepawer hat rod built far anly five years. nll/tillllt',I 1967, the Model 56TC was the same size as the C55 Baron (albeit a bit heavier; 5,990 versus 5,300 pounds), had as much power as the Queen Air and was a few knots faster than Beech's flagship, the A90 King Air. Each of the Turbo Baron's 540-cubic- inch Lycoming engines produces 380 horsepower at 41.5 inches and 2,900 rpm, maximum continuous power. Sin- gle-engine rate of climb varies from 32. OCTOBER 1984 412 fpm at sea level to 50 fpm at 18,600 feet. With both engines produc- ing 79-percent power at 12,000, true airspeed is about 222 knots and fuel consumption is about 282 pounds (47 gallons) per hour. Only 94 Turbo Barons were built. Production dwindled from 51 airplanes in 1967 to only produced two in 1971. The hot-rod Beech Turbo Baron was eclipsed by the Duke, introduced in All allgle-of-attack illdicator alld a low-tllrust detector supplemellt N516Q's pallc/. A StorTI/scope is to replace tile coffee call lid. late 1968 with 380-hp engines and a pressurized cabin. There were few changes to the origi- nal design of the Turbo Baron. Beech switched from vacuum pumps to' pres- sure pumps after the first year of pro- duction. In 1970, the model designa- tion was changed to A56TC. There were some tweaks to the panel layout and to the flap system, but the most significant change was baffled fuel r TURBO BARON tanks. The baffles were installed to prevent unporting. Beech also offered baffle kits for retrofitting earlier Turbo Barons. Unmodified 56TCs have plac- ards prohibiting takeoff, slips and skids with less than 25 gallons of fuel in each of the main fuel tanks. Miller bought his Turbo Baron, N516Q, in 1971 and bases it at Dutchess County Airport in Pough- keepsie. The C35 Bonanza shares a T- hangar next to the Baron's with two Mazda RX-3 automobiles that he is re- storing. Miller uses an RE-5 Rotary Suzuki motorcycle when the weather is nice to make the commute between his home and his airplanes. A certified airframe and powerplant mechanic, Miller does most of the work on his airplanes himself. His 35,000 hours of flying has left him with a strong motivation to avoid sur- prises, and he has installed a number of supplementary performance- and hardware-monitoring systems in the Baron. It has an Advanced Aero Safety low-thrust detection system, which provides aural and visual warnings of a
Show full textShow less
power loss, including identification of the affected engine (see "The Which Hunter," August 1983 Pilot, p. 45). It also has a Teledyne angle-of-attack in- dicator. A Ward Aero system warns of impending alternator failure. (Miller said the device alerted him to a failing - ...•. Captaill Johll M. Miller has logged more thall 35,000 hours ill everythillg from Je/lllies to DC-8s. Now, he takes his pick betweell a Turbo Baroll alld a C35 BOllallza. alternator while he was taxiing out, with his wife aboard, for takeoff in very low IFR weather conditions. They took the Bonanza, instead.) In the sumps of each engine is a device that, by detecting the presence and the amount of metal particles in the oil, monitors internal engine wear. The air- plane also has six-probe exhaust gas temperature gauges and turbocharger turbine inlet temperature indicators. . Miller notes that none of this equip- ment is overly complicated or difficult to install, and he wonders why all multi-engine aircraft do not have all of it before they leave the factory. "The manufacturers don't seem to realize that when you're flying a twin, you need all the help you can get." He recently took the Turbo Baron on a long trip to California, Arizona, Colo- rado, Texas and Florida. One leg of the trip was very near the route he used to fly in a Boeing 2470 years ago. "That was a pretty good airplane in its day," Miller recalls, "but the Baron has more range, speed and altitude. "However," he adds with a chuckle, "you have to be a bit crazy to own a 56TC. It is expensive." For flight plan- ning, Miller figures 40 gallons of fuel per hour, block to block; and the air- plane requires substantial maintenance. Although he enjoys working on the airplane, the cost for parts is high. (During a recent annual, for instance, the exhaust manifolds on each engine had to be replaced, and they cost $2,000 each.) He jokes that he has dis- covered how manufacturers price their parts: "It's easy. They put a dollar sign in front of the part number." It is not likely that Miller will get rid of his hot rod, though. He calls it his "Baby P-38." And though he may sometimes grumble good-naturedly about how much it costs to operate the Turbo Baron, he always concludes that the airplane is worth every cent. 0 Powerplants Recommended TBO Length Height Wingspan Wing area Wing loading Power loading Seats Cabin length Cabin width Cabin height Empty weight Empty weight, as tested Gross weight Max useful load Useful load, as tested Max payload w /full fuel Payload w /full fuel, as tested Max takeoff weight Max landing weight Fuel capacity, std Performance Takeoff distance, ground roll Takeoff distance over 50-ft obst Accelerate/stop distance Rate of climb, sea level Single-engine ROC, sea level .Max level speed, sea level Max level speed, 25,000 ft Cruise speed/Endurance w /45-min rsv, 1,068 Ib fuel (total fuel consumption) @ 65% power 10,000 ft 106 KIAS 96 KIAS 117 KIAS 99 KIAS 159 KIAS 125 KIAS 143 KIAS 143 KIAS 143 KIAS 202 KIAS 227 KIAS 84 KIAS 74 KIAS Max operating altitude 30.000 ft Service ceiling 32,200 ft Single-engine service ceiling 18,600 ft Absolute ceiling 33,100 ft Single-engine absolute ceiling 20,300 ft Landing distance over 50-ft obst 2,665 ft Landing distance, ground roll 1,290 ft Limiting and Recommended Airspeeds Vmc (Min control w lone 83 KIAS engine inoperative) Vx (Best angle of climb) Vy (Best rate of climb) Vxse (Best single-engine angle of climb) Vyse (Best single-engine rate of climb) Va (Design maneuvering) Vfe (Max flap extended) Vie (Max gear extended) Vlo (Max gear operating) Extend Retract Vno (Max structural cruising) Vne (Never exceed) Vs 1 (Stall clean) Vso (Stall in landing ~onfiguration) All specifications are based on manufacturer's calculations. All performance figures are based on standard day, standard atmosphere, at sea level and gross weight, unless otherwise noted. 1,482 ft 2,050 ft 3,200 ft 2,020 fpm 412 fpm 260 kt 252 kt 188 kt/4.6 hr (186 pph/31 gph) 204 kt/4.5 hr (186 pph/31 gph) 202 kt/3.9 hr (219.6 pph/36.6 gph) 221 kt/3.8 hr (219.6 pph/36.6 gph) 170 kt/5.2 hr (164.4 pph/27.4 gph) 184 kt/5.0 hr (164.4 pph/27.4 gph) 146 gal (142 gal usable) 1,902 Ib (1,068 lb usable) 182 gal (178 gal usable) 1,248 Ib (1,224 Ib usable) 208 gal (204 gal usable) 13 qt 820 Ib, 70 cu ft 20,000 ft 20,000 ft 20,000 ft @ 55% power 10,000 ft @ 45% power 10,000 ft Fuel capacity, opt Fuel capacity, opt Oil capacity. ea engine Baggage capacity Beech 56TC Turbo Baron (1967) Base price $89,950 Current'market value $40,000 to $50.000 Specifications 2 Lycoming TlO-541-E1B4 380 hp ea @ 2,900 rpm, 41.5 in Recommended TBO 1,600 hr Propellers Hartzell three-blade, constant-speed, full-feathering, 74-in diameter 1,600 hr or 4 yr 28 ft 3 in 9 ft 7 in 37 ft 10 in 199.2 sq ft 30 Ib/sq ft 7.9Ib/hp 4-6 8 ft 6 in 3 ft 6 in 4 ft 2 in 3,650 Ib 4,044 Ib 5,990 Ib 2,340 Ib 1,9461b 1,488 Ib 8781b 5,9901b 5,9901b 876 Ib (852 Ib usable) AOPA PILOT • 33
What's in the Beechcraft 56TC Baron TCDS
A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.