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Piper Aztec

By Wikipedia,
the free encyclopedia,


PA-23 Apache/Aztec
PA-23 Aztec
Role Twin-engined light piston utility
Manufacturer Piper Aircraft
First flight 1952
Introduction 1954
Primary user United States Navy
Produced 1952-1981
Number built 6,976
Developed from Twin Stinson

The Piper PA-23, named Apache and later Aztec, was an American twin-engined monoplane, the first twin-engine aircraft built by Piper Aircraft.

Originally to be named the "Twin-Stinson" and designed as a four-seater low-wing all-metal monoplane with a twin tail, the prototype first flew 2 March 1952. The prototype was then named the PA-21 to conform to Piper's numerical nomenclature[1] It was redesigned with a single vertical stabilizer and an all-metal rear fuselage and renamed to Apache 150 when it entered production in 1954; 1,231 were built. In 1958, the Apache 160 was produced by upgrading the engines to 160 hp (119 kW), and 816 were built before being superseded by the Apache 235, which went to 235 hp (175 kW) engines and swept tail surfaces (119 built).

Declining sales of the Apache prompted the redesign dubbed PA-23-250 Aztec, with 250 hp (186 kW) Lycoming O-540 carburetor engines. These first models came in a five-seat configuration which became available in 1959. The later models of the Aztec were equipped with IO-540 fuel-injected engines and six-seat capacity, and continued in production until 1982. There were also turbocharged versions of the later models, which were able to fly at higher altitudes.

Among other light twin-engined airplanes of its generation, the Aztec was known for its good load hauling, long endurance, stable handling, and respectable single-engine performance, at the cost of higher fuel consumption and a draggier (slower) airframe. Part of the drag was due to use of the same basic wing design (albeit with substantially different dimensions and construction) as the Piper Cub series of aircraft. The Piper Cub airfoil (USA35B) gave the Aztec superior short field operation characteristics at the price of lower performance at cruising speeds.

The US Navy acquired 20 Aztecs, designating them UO-1, which changed to U-11A when unified designations were adopted in 1962.


PA-23 Apache
Initial production version, 2047 built (including the Apache E, G and H).
PA-23-160 Apache E
PA-23 powered by two 160 hp O-320-B engines.
PA-23-160 Apache G
PA-23 with longer internal cabin and extra window.
PA-23-160 Apache H
Apache G with 0-320-B2B engines and minor changes.
PA-23-235 Apache 235
Aztec with 5 seats and 235 hp O-540 engines, 118 built.
PA-23-250 Aztec
Apache G with modified rear fuselage, new fin and rudder and 250hp Lycoming O-540-A1D engines, 4811 built (including sub-variants)
PA-23-250 Aztec B
Aztec with longer nose for a baggage compartment, six-seats, new instrument panel and changes to systems.
PA-23-250 Aztec C
Aztec B with either IO-540-C4B5 engines or turbocharged TIO-540-C4B5 as an option, also modified engine nacelles and modified landing gear.
PA-23-250 Aztec D
Aztec B with revised instrument panel and controls.
PA-23-250 Aztec E
Aztec D with longer pointed nose and a single piece windshield.
PA-23-250 Aztec F
Aztec E with improved systems and cambered wingtips and tailplane tip extensions.
United States Navy designation formerly UO-1.
United States Navy designation for PA-23-250 Aztec with additional equipment, 20 delivered later re-designated U-11A.

Military Operators

 Costa Rica
 El Salvador
 United States

Specifications (model E, normally aspirated)

General characteristics

  • Crew: one, pilot
  • Capacity: pilot plus 5 passengers (3 in the early models)
  • Length: 31 ft 3 in (9.51 m)
  • Wingspan: 37 ft 2 in (11.3 m)
  • Height: 10 ft 4 in (3.14 m)
  • Wing area: 208 ft² (19.3 m²)
  • Empty weight: 3,300 lb (1500 kg)
  • Max takeoff weight: 5,200 lb (2360 kg)
  • Powerplant:Lycoming IO-540-C4B5, 250 hp (186 kW) each


See also

Related development Helio Twin Courier
Comparable aircraft

Text from Wikipedia is available under the Creative Commons Attribution/Share-Alike License; additional terms may apply.

Published in July 2009.

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