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Hartzell Propeller is an American manufacturer that was founded in 1917 by Robert N. Hartzell as the Hartzell Walnut Propeller Company. [1] It produces composite and aluminum propellers for certified , homebuilt , and ultralight aircraft.
Robert Norris Hartzell (born June 3, 1896 in Ohio, died December 11, 1968) was an American entrepreneur who started Hartzell Propeller in 1917, a company that produces aircraft propellers. [ 1 ] [ 2 ]
Data from www.socata.org SOCATA TB user group and TB21 POH General characteristics Crew: 1 Capacity: 4 passengers Length: 7.75 m (25 ft 5 in) Wingspan: 9.85 m (32 ft 4 in) Height: 2.85 m (9 ft 4 in) Airfoil: RA 16 3C3 Empty weight: 911 kg (2,008 lb) EFIS and MTV 9 propeller Max takeoff weight: 1,400 kg (3,086 lb) Fuel capacity: 336 Liters (88.8 U.S. Gallons) Powerplant: 1 × LYCOMING TIO-540 ...
The standard engine available is the 180 hp (134 kW) Lycoming O-360-C1 (CC363i) four-stroke powerplant, driving a Hartzell Trailblazer composite, constant speed propeller. In July 2019 a 215 hp (160 kW) version powered by a Lycoming IO-390 (CC393i) engine and a Hartzell Pathfinder three-bladed propeller was introduced as the CC19-215. [7]
Propellers: 5-bladed Hartzell Propeller constant speed reversible, 8 ft 8 in (2.64 m) diameter; Performance. Cruise speed: 307 kn (353 mph, 569 km/h) at 20,000 ft (6,096 m) Range: 640 nmi (740 mi, 1,190 km) with 50 passengers, 200 lb (91 kg) and IFR fuel reserves; Service ceiling: 25,000 ft (7,620 m) service ceiling with one engine out
The TBM 900 saw the adoption of a new five-bladed propeller, specially optimised by Hartzell based upon airflow simulations conducted of the TBM's forward section. According to SOCATA, Hartzell's selection over a similar advanced counterpart from MT-Propeller was made due to the former raising the cruise speed by around 3 to 5 kn (5.5 to 9 km/h).
The CS is the budget version, with fewer standard features. [2] Both CS and XLS versions of the DA40 use the Lycoming IO-360-M1A fuel injected engine. The major difference is the choice of propeller, with the CS using a Hartzell two-blade aluminum constant speed prop and the XLS using an MT composite three-blade unit. [3] [4]
McCulloch J-2 registered in the United Kingdom between 1972 and 1975. Early versions were equipped with a two-bladed wooden Sensenich propeller. A later "Super J-2" variant employed a three-bladed Hartzell controllable-pitch propeller, accompanied by an increase in allowable gross weight. Baggage of up to 95 pounds, to the extent permitted by ...