Beechcraft L-23 Seminole

· Beechcraft · 2 × Lycoming O-480

Airplanes

Length

9.4488 m

Flat Wing Span

13.716 m

Height

3.3528 m

Flat Wing Area

25.7341 m²

Max Seating

Cruise Speed

289.6819 km/h

Max Speed

374.9772 km/h

Max Ceiling

8229.6 m

Number of Engines

Aircraft Engine

First Flight

1949-01-01

Entry Into service

1952-01-01

Number Built

288

Maximum Take-Off Weight

3.3112 t (paragliders: kg)

Total Fuel Capacity

681.3741

Maximum Range

2172.615 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Beechcraft L-23 Seminole	3.3112	681.3741	2172.615

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Beagle B.206	Continental IO-520	10.0584	13.716	6	Compare
Beechcraft Twin Bonanza	Lycoming O-480	9.4488	13.716	5	Compare
Duverne-Saran 01		9.4	13.5		Compare
Yakovlev Yak-2	Klimov M-103	9.34	14		Compare
De Havilland Dragonfly		9.4488	13.1064		Compare
United Consultants Twin Bee	Lycoming O-360	9.55	13.18		Compare

All data (25 fields)

Name: Beechcraft L-23 Seminole
Manufacturer: Beechcraft
Description: The Beechcraft L-23 Seminole (later designated U-8) was the United States Armed Forces designation for the Beechcraft Twin Bonanza and Queen Air aircraft in its inventory.
First Flight: 1949-01-01
Entry Into service: 1952-01-01
Production End: 1961-01-01
Service End: 1992-01-01
Designer: Beechcraft
Type: Utility aircraft
Length (m): 9.4488
Height (m): 3.3528
Cockpit Crew: 2
Max Seating: 6
Max Speed (km/h): 374.9772
Cruise Speed (km/h): 289.6819
Max Ceiling (m): 8229.6
Capacity Description: 6 passengers
Number Built: 288
Powerplant Description: 2 × Lycoming GSO-480-A1A6 (Military designation O-480-1), 254 kW (340 hp) each
Primary Users: United States Army, Pakistan Army
Wikipedia Article (URL): en.wikipedia.org/wiki/Beechcraft_L-23_Seminole
Flat Wing Span (m): 13.716
Flat Wing Area (m²): 25.7341
Aircraft Engine: Lycoming O-480
Number of Engines: 2