Range Map

Origin: · two fingers to move map

×
1

Tank-dry, where fuel runs out at catalogue's stored cruise burn.

Excludes reserves: range beyond the dashed circle requires a leaner cruise than what we store. Great-circle, still air, book cruise. Estimates only: always verify against the POH.

Payload vs. Range

Occupants:

Fuel on board

Cargo

nm

Range

Cargo is additional payload after occupants and baggage.
full tanks
Available Range / nm
Mission capable. This load flies with full fuel.
Fuel reduced by . left aboard for nm range.
Over max payload by . At this load it cannot lift a single occupant.

Trip Preview

Mission Profile

Used market Only available used
140
KTAS
Cruise Speed
616
nm
Max Range
17,000
ft
Service Ceiling
5
Occupants
1,138
lbs
Wet Payload
Endorsements & ratings:
  • Complex
  • Multi-Engine
Piper PA-23 Apache (N1346P) at Rantoul, Kansas. Photo: Aeroprints.com, CC BY-SA 3.0.
Piper PA-23 Apache (N1346P) at Rantoul, Kansas. Photo: Aeroprints.com, CC BY-SA 3.0.

Estimated Ownership Costs

Create a free account to view or request ownership cost data.

About the Piper PA-23-150/160 Apache

Type certificated 1954 Source: FAA Type Certificate Data Sheet

Overview

The Piper PA-23 Apache is the airplane that put Piper in the twin-engine business. Piper acquired the twin-Stinson design and brought it to market in 1954 as the four-seat PA-23, then refined it in 1957 as the PA-23-160 with a pair of 160-horsepower Lycoming O-320 engines. Production ran until 1962, when the more powerful Aztec superseded it, and roughly 2,000 Apaches were built across the run. It remains one of the least expensive ways to own and fly a piston twin.

The Apache’s appeal is entry-level economics, not performance. A pair of small, carbureted, naturally aspirated O-320s gives docile, forgiving handling and modest running costs, which is why the type endured for decades as a multi-engine trainer and time-builder. Cruise is a leisurely 135 to 145 knots on about 16 gallons per hour combined, and single-engine climb is marginal by modern standards. The honest case against the Apache is its engine-out performance: with two 160-horsepower fours, single-engine climb is marginal, and density-altitude and weight planning matter on every flight. Accept that limit and it earns its keep as a low-cost path to a multi-engine rating, to time-building, or to affordable twin redundancy on shorter trips.

Key Features for GA Buyers

  • Acquisition and operating costs at the bottom of the light-twin market. A common first multi-engine airplane and time-builder.
  • Docile, forgiving handling. Type literature consistently describes the Apache as stable and easy to fly, well suited to multi-engine training and instrument practice.
  • Carbureted Lycoming O-320s. Two 160-horsepower fours with a 2,000-hour TBO and a deep parts and overhaul network, simple to maintain relative to turbocharged or fuel-injected twins.
  • Four to five seats with a baggage compartment. Capacity for two adults and bags, or a family on shorter legs.
  • Retractable gear and constant-speed propellers. A complex twin for rating and currency, with acquisition cost comparable to a high-performance single.

Trade-offs

  • Marginal single-engine performance. With two 160-horsepower engines, engine-out climb is anemic; density altitude and weight planning matter on every flight.
  • Slow by twin standards. A 140-knot cruise trails later light twins like the Aztec and Twin Comanche.
  • No altitude capability. Naturally aspirated engines limit useful performance to the low and middle teens.
  • Aging fleet. The newest Apache is over sixty years old; some model-specific interior, electrical, and airframe parts now come through salvage.
  • Insurance step-up for low-time multi pilots. As with any twin, premiums and minimum-experience requirements rise sharply versus a single.

See Also

Technical Specifications

Dimensions & Weights

Wingspan 37 ft
Height
10 ft
Length
28 ft
Parking area (ft²2)
1,539 ft²
Max Takeoff Weight
Source: FAA Type Certificate Data Sheet 3,800 lbs
Max Landing Weight
3,800 lbs
Useful Load
Source: third-party reference 1,570 lbs
Fuel Capacity
72 gal

Performance

Cruise Speed
Source: third-party reference 140 KTAS
Never-Exceed (VNE)
Source: FAA Type Certificate Data Sheet 197 KIAS
Max Structural Cruise (VNO)
Source: FAA Type Certificate Data Sheet 156 KIAS
Approach Speed
85 KIAS
Stall, Clean (VS1)
65 KIAS
Range
Source: third-party reference 616 NM
Service Ceiling
17,000 ft

Engines

Log in to view or request powerplant data.

Sources

Where the figures on this page come from. Piper PA-23-150/160 Apache specifications are traced to published references; estimated values are flagged inline next to the figure.

Similar to the Piper PA-23-150/160 Apache

Similar Pistons

Piper Seminole

Cruise
162 kts (higher than this aircraft)
Range
700 nm (higher than this aircraft)
Seats
4
2 × Piston Low Wing In production
Compare

Beechcraft 95 Travel Air

Cruise
174 kts (higher than this aircraft)
Range
689 nm (higher than this aircraft)
Seats
5
Compare

Tecnam P2006T

Cruise
145 kts (higher than this aircraft)
Range
670 nm (higher than this aircraft)
Seats
4
2 × Piston High Wing In production
Compare

Gulfstream American GA7

Cruise
160 kts (higher than this aircraft)
Range
1170 nm (higher than this aircraft)
Seats
4
Compare

Beechcraft Duchess 76

Cruise
158 kts (higher than this aircraft)
Range
780 nm (higher than this aircraft)
Seats
4
Compare

Compare the Piper PA-23-150/160 Apache to other aircraft