Piper PA-23-150/160 Apache

Piston • twin engine • Low Wing • Retractable gear

Range Visualization

Origin: · click map to move · nm at current load

Payload vs. Range

Customize assumptions

Default: 190 lbs (FAA standard)

Default: 30 lbs

Passengers
lbs @ lbs / pax
0 lbs
Fuel on board
gal
+ Weight
Range
Available Range / nm
Mission capable — Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required — You'll need to leave gallons of fuel behind ( gal usable for nm range).
Over max gross weight — Reduce payload by lbs to safely operate this aircraft.

Mission Profile

Endorsements & ratings:
  • Complex
  • Multi-Engine
182
KTAS
Cruise Speed
6
Occupants
nm
Max Range
-
lbs
Wet Payload

Estimated Ownership Costs

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Technical Specifications

Dimensions

Wingspan
37.2 ft
Length
27.6 ft
Height
10.3 ft
Parking area (ft2)
1538.72 ft2

Weights

Max Takeoff Weight
4,800 lbs
Max Landing Weight
4,800 lbs

Performance

Cruise Speed
182 KTAS
Never-Exceed (Vne)
207 KIAS
Approach Speed
85 KIAS
Stall, Clean (Vs1)
65 KIAS
Service Ceiling
17,000 ft

Engines

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178 kts (lower than this aircraft)
Range
955 nm
Seats
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Piston twin engine High Wing
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Range
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Cruise
182 kts
Range
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Seats
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Piston twin engine High Wing
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See how the Piper PA-23-150/160 Apache stacks up against similar aircraft

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