This Musketeer became the Musketeer A23A Custom III in 1966 (Avco Lycoming panel these aircraft were mechanically identical to the earlier A23-24 model.

30-APR-1966, Beechcraft 23, N2333J, Aircraft Speci, 0, Vancouver WA, w/o. 18- MAY-1966, Beechcraft A23A Musketeer, 9V-BAH, Royal Singapore Flying Club

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(010-02301). 10-23A. (455 971). N/A. N/A. N/A. 12 VoltDry Charged Batteries for General Aviation.

Aircraft Bluebook Single Engine Piston Beechcraft. BEECH BONANZA A36TC/B36TC (1979 - 1995) BEECH BONANZA B36TC (1996 -- 2002) BEECH BONANZA A36/G36 (1996 & up)

It is a four cylinder, normally aspirated, direct drive, air cooled, horizontally opposed, carburetor equipped engine. Fuel tanks are located in each wing and have a capacity of 15 gallons each for a total of 30 gallons. A23A: Year Built: 1965: Manufacturer's Serial Number: M-928: Aircraft Type: Fixed wing single engine: Category: Land: Builder Certification: Type Certificated: Number of Seats: 4 seats: Weight Class: CLASS 1 (Up to 12,499 pounds gross take off weight) Engine Manufacturer: CONT MOTOR: Engine Model: IO-346 SERIES: Engine Type: Reciprocating: Number of Engines: 1 engine: Horsepower BEECH A23A.

Feb 27, 2001 By 1968, Beech had turned out more than 500 examples of the IO-346-powered A23. That year, though, saw another engine change, this time

TA754. TB704. TX900.

exception of FAA Approved Airplane Flight Manual Supplements. COPYRIGHT © BEECH 1994 BEECH AIRCRAFT CORPORATION. Wichita, Kansas 67201. document must be carried in the airplane at all times and be kept BEECH AIRCRAFT CORPORATION FAA APPROVED AIRPLANE FLIGHT MANUAL. Part Number, Rev, Description, Date, Download CSV (If available). +. 125 Series 1 A/B. IPC-125-1A, Rev 85, Hawker/125-1A Illustrated Parts Catalog, Dec 2001.
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The Musketeer A23 was a four-seat light cabin aircraft, fixed tricycle landing gear, powered by a 165 hp (123 kW) Continental IO-346-A piston engine, with a gross weight of 2,400 lb (1,089 kg). This model was first certified 5 November 1965.

It is a four cylinder, normally aspirated, direct drive, air cooled, horizontally opposed, carburetor equipped engine. Fuel tanks are located in each wing and have a capacity of 15 gallons each for a total of 30 gallons. The Beech Musketeer is a single-engine, piston aircraft with a fixed gear. The Musketeer Models 23, A23, A23A, A23-24 are low-wing airplanes produced by Beechcraft between the years 1963 and 1970.
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1967 Beechcraft A23A - Musketeer Aircraft, Registration No: VH-SDC, Date of Manufacture: 1967, Aircraft Manufacturer: Beechcraft, Aircraft Model No: A23A - Musketeer, Seats: 4, Aircraft Serial No: M-1035, Total Time in Service: 3388.3, Engine Hours to Run 781.7; Propeller to Run 1867.1; Operational Category: Aerial Work, Under Carriage Type: Fixed,

Total count: 54 aircraft. N1000J (1966) N1167M (1967) N16TH (1966) N202GS (1966) N21NL (1967) N2305W (1965) N2306W (1965) N2307W; N2308W (1965) N2311W (1965) N2314W (1965) N2321W (1965) N2330W (1965) N2331W (1965) N2333W (1965) N2335W (1965) Single engine piston aircraft with fixed landing gear. The A23A Musketeer Custom III seats up to 3 passengers plus 1 pilot. 1967 BEECHCRAFT A23A Musketeer Custom III - Specifications, Performance, Operating cost, Valuation, Brokers - planephd.com Browse Aircraft.com’s catalog of BEECHCRAFT A23A III MUSKETEER. Find tail numbers, view photos, and get detailed individual aircraft information BEECHCRAFT A23A III MUSKETEER | Aircraft.com FAA N-Number Database a23a Four-seat light cabin aircraft, fixed tricycle landing gear, powered by a 165 hp (123 kW) Continental IO-346-A piston engine, gross weight of 2,400 lb (1,089 kg), first certified November 5, 1965. Narrative: At 1420 hours WST on 8th January, 1970, a Beech A23A aircraft, registered VH-RWA, and a Piper PA24-250 aircraft, registered VH-PAR, collided at a height of approximately 100 feet above ground level, whilst on approach to Runway 24 at Jandakot Airport, Western Australia.