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  Aircraft History, Specification and Information
Piper PA-23 Apache / Aztec / Geronimo
1958 Piper PA-23-160 Apache - N34DA (sn 231469)
Photo taken Jul. 29, 2010
Oshkosh (EAA AirVenture Fly-in), WI - USA (OSH / KOSH)
Photo © AirplaneMart.com

The Piper PA-23, named Apache and later Aztec, is a four-to-six-seat twin-engined light aircraft aimed at the general aviation market that also saw service with the United States Navy and other countries' military forces in small numbers. Originally designed in the 1950s by the Stinson Aircraft Company, the Apache and its more powerful development the Aztec were manufactured from the 1950s to the 1980s by Piper Aircraft in the United States.

Design and development

1976 Piper PA-23-250 Aztec - N404CH (sn 27-7654191)
NMC Aviation - Northwestern Michigan College
Photo taken Jul. 29, 2010
Oshkosh (EAA AirVenture Fly-in), WI - USA (OSH / KOSH)
Photo © AirplaneMart.com
1957 Piper PA-23/150 Apache - N2287P (sn 23-898)
Photo taken Jul. 27, 2010
Oshkosh (EAA AirVenture Fly-in), WI - USA (OSH / KOSH)
Photo © AirplaneMart.com
1957 Piper PA-23 Geronimo - N103RS (sn 23-1165)
Photo taken Apr. 19, 2007
Sun 'n Fun Fly-in - Lakeland Linder Airport, FL - USA (LAL / KLAL)
Photo © Marcel Siegenthaler
1963 Piper PA-23-235 Apache - N4981P (sn 27-585)
Photo taken Apr. 19, 2007
Sun 'n Fun Fly-in - Lakeland Linder Airport, FL - USA (LAL / KLAL)
Photo © Marcel Siegenthaler
1955 Piper PA-23 Apache - N123P (sn 23-397)
Photo taken Jul. 29, 2010
Oshkosh (EAA AirVenture Fly-in), WI - USA (OSH / KOSH)
Photo © AirplaneMart.com

The PA-23 was the first twin-engined Piper aircraft and was developed from a proposed "Twin Stinson" design, inherited when Piper bought the Stinson Division of the Consolidated Vultee Aircraft Corporation.[1] The prototype PA-23 was a four-seat low-wing all-metal monoplane with a twin tail, powered by two 125 hp Lycoming O-290-D piston engines;[1] it first flew on 2 March 1952. The aircraft performed badly and it was redesigned with a single vertical stabilizer and an all-metal rear fuselage and more powerful 150 hp Lycoming O-320-A engines.[1] Two new prototypes of the redesigned aircraft, now named Apache, were built in 1953[1] and entered production in 1954; 1,231 were built. In 1958 the Apache 160 was produced by upgrading the engines to 160 hp (119 kW); 816 were built before being superseded in 1962 by the Apache 235. With a 1962 price of $45,000, the Apache 235 was a derivative of the Aztec, fitted with 235 hp (175 kW) versions of the engines used on the Aztec and swept tail surfaces (119 built).

In 1958 an upgraded version with 250 hp (186 kW) Lycoming O-540 engines and a swept vertical tail was produced as the PA-23-250 and was named Aztec. These first models came in a five-seat configuration which became available in 1959. In 1961 a longer nosed variant, the Aztec B, entered production. 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.

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

In 1974, Piper produced a single experimental PA-41P Pressurized Aztec concept. This concept was short-lived, however, as the aspects of the Aztec that made it so popular for its spacious interior and ability to haul large loads did not lend themselves well to supporting the sealed pressure vessel required for a pressurized aircraft. The project was scrapped, and the one pressurized Aztec produced, N9941P, was donated to Mississippi State University, where it was used for testing purposes. In 2000, N9941P was donated to the Piper Aviation Museum in Lock Haven, Pennsylvania, on condition that it never be flown again. It is now there on display.


  • PA-23 Twin-Stinson
    Original designation of the Piper PA-23 Apache.
  • PA-23 Apache
    Initial production version, 2047 built (including the Apache E, G and H).
  • PA-23-150 Apache B
    1955 variant with minor changes.
  • PA-23-150 Apache C
    1956 variant with minor changes.
  • PA-23-150 Apache D
    1957 variant with minor changes.
  • 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
    Apache with five 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.
  • PA-23T-250 Turbo-Aztec
    Generally similar to the Aztec F, powered by two TIO-540 piston engines, fitted with a Garret turbocharging system.
  • U-11A
    United States Navy designation formerly UO-1.
  • UO-1
    United States Navy designation for PA-23-250 Aztec with additional equipment; 20 delivered, later re-designated U-11A.
  • PA-41P Pressurized Aztec
    Pressurized Aztec concept, one built.
  • Seguin Geronimo
    Apache with a series of modifications to the engines, nose and tail.

Military Operators

  • Argentina
  • Bolivia
  • Brazil
  • Cameroon
  • Colombia
  • Costa Rica
  • El Salvador
  • Honduras
  • Madagascar
  • Mexico
  • Nicaragua
    Nicaraguan Air Force
  • Spain
    Spanish Air Force (Escuadrón 912 / Escuadrilla de Enlace 905)
  • Paraguay
    Paraguayan Air Force (Grupo Aéreo de Transporte Especial/GATE)
  • Uganda
  • United States
    United States Navy
  • Venezuela

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

General characteristics

Crew: one
Capacity: five passengers
Payload: 1,600 lb (725 kg) cargo
Length: 31 ft 2¾ in (9.52 m)
Wingspan: 37 ft 2½ in (11.34 m)
Height: 10 ft 4 in (3.15 m)
Wing area: 207.6 ft² (19.28 m²)
Airfoil: USA 35-B (modified)
Aspect ratio: 6.8:1
Empty weight: 3,180 lb (1,442 kg)
Max. takeoff weight: 5,200 lb (2,360 kg)
Powerplant: 2 × Lycoming IO-540-C4B5 normally aspirated air-cooled flat-six piston engines, 250 hp (187 kW) each
Propellers: two bladed Hartzell HC-E2YK-2RB constant speed propeller


Never exceed speed: 277 mph (240 knots, 446 km/h)
Maximum speed: 215 mph (187 knots, 346 km/h)
Cruise speed: 172 mph (150 knots, 278 km/h) at 10,200 ft (3,110 m) (long-range cruise)
Stall speed: 68 mph (59 knots, 109 km/h) (flaps down)
Range: 1,519 miles (1,320 nmi, 2,445 km) at long-range cruise
Service ceiling: 18,950 ft (5,775 m) (absolute ceiling)
Rate of climb: 1,400 ft/min (7.1 m/s)

Specifications (Piper Geronimo)

Engine make/model: Lycoming 0-360-A1D
Horsepower@rpm@altitude: 180@2700@SL
Horsepower for takeoff: 180
TBO hrs.: 2000
Fuel type: 100/100LL
Propeller type: Hartzell, 2-blade, CS
Landing gear type: Tri./retr.
Max ramp weight (lbs.): 3800
Empty weight, as tested (lbs): 2423
Useful load, as equipped (lbs.): 1377
Payload, full normal fuel (lbs.): 729
Usable fuel, normal (gals.): 108
Optional fuel (gals.): 156
Oil capacity (qts.): 8
Wingspan: 37 ft.
Overall length: 31 ft. 6 in.
Height: 31 ft. 6 in
Wing area (sq. ft.): 207.6
Wing loading (lbs./sq. ft.): 18.3
Power loading (lbs./hp.): 10.6
Wheel base: 7 ft. 3 in.
Wheel track: 11 ft. 3 in.
Wheel size (in.): 6.00 x 6
Seating capacity: 4-6
Cabin doors: 1
Cabin width (in.): 48
Cabin height (in.): 50
Baggage capacity (lbs./cu. ft.): 200


Cruise speed (kts.):
75% power: 170
60% power: 163

Max range (w/ reserve) (nm):
75% power: 663
60% power: 880

Fuel consumption (gph):
75% power: 18.5
60% power: 17

Estimated endurance (60%) (hrs): 5.5
Vs (kts.): 52
Vso (kts.): 47
Best rate of climb (SL fpm): 1500
Best rate of climb,8,000 ft. (fpm): 1000*
Single-engine rate of climb, SL (fpm): 600+*
Service ceiling (ft): 23,000
Single-engine service ceiling (ft.): 12,000
Takeoff ground roll (ft.): 400
Landing ground roll (ft.): 400
Landing over 50-ft. obstacle (ft.): 1400


Accidents and incidents

On 18 April 1974, Aztec G-AYDE was involved in a ground collision with BAC One-Eleven G-AXMJ at London Luton Airport after the pilot of the Aztec entered the active runway without clearance. He was killed and his passenger was injured. All 91 people on board the One-Eleven successfully evacuated after the takeoff was aborted.

On 29 November 1975, retired Formula One racing driver and Embassy Hill car owner Graham Hill was piloting a Piper PA-23-350 Aztec, marked as N6645Y, from Circuit Paul Ricard, France to London, United Kingdom. His passengers were Embassy Hill race driver Tony Brise, team manager Ray Brimble, designer Andy Smallman and mechanics Terry Richards and Tony Alcock. They were returning from Circuit Paul Ricard, Var, where they had been testing the Hill GH2 car being prepared for the 1976 Formula One season. They were due to land at Elstree Airfield, Hertfordshire, before onward travel to London to attend a party. Shortly before 10pm, the aircraft hit trees on a golf course at Arkley, Hertfordshire, in thick fog. The ensuing crash and explosion killed everyone on board.

On 15 April 1978, Hollywood stunt flyer Frank Tallman was ferrying a Piper Aztec from Santa Monica Airport, California, to Phoenix, Arizona under visual flight rules when he continued the flight into deteriorating weather, a lowering ceiling and rain. He struck the side of Santiago Peak in the Santa Ana Mountains near Trabuco Canyon at cruise altitude, dying in the ensuing crash.

Last updated February 22, 2016  
This article is licensed under the GNU Free Documentation License. It uses material from the Wikipedia article "Piper PA-23".
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