Martin Maryland

Airplanes

Length

14.2 m

Flat Wing Span

18.7 m

Height

5 m

Flat Wing Area

49.9 m²

Cruise Speed

399 km/h

Max Speed

489 km/h

Max Ceiling

8991.6 m

Number of Engines

First Flight

1939-03-14

Entry Into service

1940-01-01

Number Built

450

Maximum Take-Off Weight

7.624 t (paragliders: kg)

Maximum Range

2100 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Martin Maryland	7.624	2100

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Henschel Hs 124		14.5	18.2		Compare
FMA IA 50 Guaraní II	Turbomeca Bastan	14.86	19.53	15	Compare
Lockheed Model 14 Super Electra		13.51	19.96	14	Compare
Caproni Ca.135		14.3256	18.5928		Compare
Douglas A-20 Havoc		14.3256	18.5928		Compare
Rikugun Ki-93		14.215	19		Compare

All data (23 fields)

Name: Martin Maryland
Manufacturer: Glenn L. Martin Company
Description: The Martin Model 167 Maryland was an American light bomber that first flew in 1939.
First Flight: 1939-03-14
Entry Into service: 1940-01-01
Service End: 1945-01-01
Designer: Glenn L. Martin Company
Type: Light bomber
Length (m): 14.2
Height (m): 5
Max Speed (km/h): 489
Cruise Speed (km/h): 399
Max Ceiling (m): 8991.6
Rate of Climb (m/s): 12
Armament: 4 × .303 in Browning Mk II machine guns in outer wings with 750 rpg, 1 × .303 in Vickers K machine gun in a dorsal step position with 5 × 97-round magazines, 1 × .303 in Vickers K machine gun in a ventral step position with 5 × 97-round magazines; 2,000 lb (907 kg) internally; (usually 4 × 500 lb (227 kg) bombs)
National Origin: United States of America
Number Built: 450
Powerplant Description: 2 × Pratt & Whitney R-1830-S1C3-G Twin Wasp radial engines, 783 kW (1050 hp) each
Primary Users: Royal Air Force, South African Air Force, French Air Force, French Navy
Wikipedia Article (URL): en.wikipedia.org/wiki/Martin_Maryland
Flat Wing Span (m): 18.7
Flat Wing Area (m²): 49.9
Number of Engines: 2