Piper PA-31 Navajo

· Embraer · 2 × Lycoming O-540

Airplanes

Length

9.7536 m

Flat Wing Span

12.192 m

Height

3.9624 m

Flat Wing Area

21.2748 m²

Max Seating

Cruise Speed

383.0239 km/h

Max Speed

420.0388 km/h

Max Ceiling

8016.24 m

Number of Engines

Aircraft Engine

First Flight

1964-09-30

Entry Into service

1967-03-30

Number Built

3942

Maximum Take-Off Weight

2.9484 t (paragliders: kg)

Total Fuel Capacity

719.2282

Maximum Range

1874.886 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Piper PA-31 Navajo	2.9484	719.2282	1874.886

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Cessna 411	Continental IO-520	10.0584	11.8872		Compare
Beechcraft Duke		10.0584	11.8872	5	Compare
Fokker D.XXIII	Walter Sagitta	10.2	11.5		Compare
Fouga CM.170 Magister	Turbomeca Marboré	10.06	12.15		Compare
Fouga CM.175 Zéphyr	Turbomeca Marboré	10.06	12.15		Compare
Helio Twin Courier	Lycoming O-540	9.7536	12.4968	5	Compare

All data (26 fields)

Name: Piper PA-31 Navajo
Manufacturer: Embraer
Description: The Piper PA-31 Navajo is a family of twin-engined low-wing tricycle gear utility aircraft designed and built by Piper Aircraft for small cargo and feeder airlines, and as a corporate aircraft.
First Flight: 1964-09-30
Entry Into service: 1967-03-30
Production End: 1984-01-01
Designer: Embraer
Type: Utility aircraft
Length (m): 9.7536
Height (m): 3.9624
Cockpit Crew: 1
Max Seating: 5
Max Speed (km/h): 420.0388
Cruise Speed (km/h): 383.0239
Min Speed (km/h): 117.4821
Max Ceiling (m): 8016.24
Rate of Climb (m/s): 7.3406
Capacity Description: 5 to 7 passengers
Number Built: 3942
Powerplant Description: 2 × Lycoming TIO-540-A air-cooled six-cylinder horizontally opposed piston engine, 231 kW (310 hp) each
Status: Active service
Wikipedia Article (URL): en.wikipedia.org/wiki/Piper_PA-31_Navajo
Flat Wing Span (m): 12.192
Flat Wing Area (m²): 21.2748
Aircraft Engine: Lycoming O-540
Number of Engines: 2