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Piper PA-23 Apache and Aztec

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United States Piper PA-23 Apache and Aztec
Piper PA-23 Apache and Aztec. Photo: FlugKerl2, CC BY-SA 3.0, via Wikimedia Commons
Piper PA-23 Apache and Aztec. Photo: FlugKerl2, CC BY-SA 3.0, via Wikimedia Commons
Make Piper
Model Piper PA-23 Apache and Aztec
Type Twin-engined light piston utility
Country United States United States
First flight 2 March 1952
Built 1952–1981
Number built 6,976
Registered in the US 1,290 (FAA register, October 30, 2026)
Seats 1, 5 passengers
Engine 2 × Lycoming IO-540-C4B5, 250 hp
Cruise speed 172 mph (PA-23-250F, normally aspirated)
Range 1,519 mi (PA-23-250F, normally aspirated)
Service ceiling 18,950 ft (PA-23-250F, normally aspirated)
Max weight 5,200 lb (PA-23-250F, normally aspirated)


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The Piper PA-23, named the Apache and later the Aztec, is a four- to six-seat, twin-engine light airplane, also used in small numbers by the U.S. Navy and other military forces. It began in the 1950s as the Twin Stinson, designed by the Stinson Aircraft Company, and Piper built it as the Apache and the more powerful Aztec from the 1950s to the 1980s.[1] In the U.S. there are 1,290 with a valid registration.[2]

History

The PA-23 was Piper's first twin. Piper inherited the "Twin Stinson" design when it bought the Stinson Division of Consolidated Vultee. The prototype, a four-seat, low-wing, all-metal airplane with a twin tail and two 125 hp Lycoming O-290-D engines, first flew on March 2, 1952. It flew poorly, so Piper redesigned it with a single tail fin, an all-metal rear fuselage and 150 hp Lycoming O-320 engines.[1]

Piper built 2,047 Apaches, including the 160 hp Apache E, G and H; the five-seat Apache 235 had 235 hp O-540 engines.[1] The Aztec followed with more power, and the 250 hp PA-23-250 is the most common PA-23 on the U.S. register today.[1][2]

Registered in the United States

The FAA register lists 1,290 of these airplanes with a valid U.S. registration. Here they are by the model name the FAA uses.[2]

FAA model name Registered
PA-23-250 879
PA-23-160 186
PA-23 151
PA-23-150 43
PA-23-235 25
PA-23-250 (6PCLM) 4
PA-23-180 2

Specifications (PA-23-250F, normally aspirated)

Item PA-23-250F, normally aspirated
Crew 1
Passengers / capacity 5 passengers
Length 31 ft 2+3/4 in
Wingspan 37 ft 2+1/2 in
Height 10 ft 4 in
Wing area 207.56 sq ft
Empty weight 3,180 lb
Maximum takeoff weight 5,200 lb
Fuel 140 USgal usable fuel (normal), optional extra tanks with 40 USgal
Engine 2 × Lycoming IO-540-C4B5, 250 hp (normally aspirated air-cooled flat-six piston engines)
Propeller Hartzell HC-E2YK-2RB constant-speed propellers
Maximum speed 215 mph
Cruise speed 172 mph
Stall speed 68 mph
Never-exceed speed 277 mph
Range 1,519 mi
Service ceiling 18,950 ft
Rate of climb 1,400 ft/min

Figures as given in the Wikipedia article and its sources.[1]

Owner and mechanic notes: coming soon. What to check before you buy, common problems and what they cost to fix. Airplane Wiki is gathering this from owners and mechanics.

Photos

All photos are from Wikimedia Commons; click a photo for its full credit and license.

Buying a Piper PA-23 Apache and Aztec

For sale listings: coming soon. Airplane Wiki will list Piper PA-23 Apache and Aztecs for sale here, with the facts on this page beside every listing.

Sources

  1. ↑ 1.0 1.1 1.2 1.3 1.4 Wikipedia, "Piper PA-23", read November 1, 2026. Airplane Wiki's text is written in its own words; facts are checked against this article and its sources.
  2. ↑ 2.0 2.1 2.2 Federal Aviation Administration, Releasable Aircraft Database, file dated October 30, 2026. Valid registrations of fixed-wing airplanes whose FAA maker and model names belong to this family. Airplane Wiki uses only counts from this file, never owner names or addresses.