Saro Cutty Sark

Airplanes

Length

10.3632 m

Flat Wing Span

13.716 m

Height

3.3528 m

Flat Wing Area

29.729 m²

Cruise Speed

149.669 km/h

Max Speed

172.1998 km/h

Max Ceiling

2743.2 m

Number of Engines

Aircraft Engine

First Flight

1929-07-04

Entry Into service

1930-01-01

Number Built

Total Fuel Capacity

181.8436

Maximum Range

506.9434 km

Pictures

No pictures yet for this family.

Aircraft	Total Fuel Capacity	Maximum Range (km)
Saro Cutty Sark	181.8436	506.9434

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
SIPA S.70	Mathis G.8R	10.2	13.8	8	Compare
Yakovlev Yak-6	Shvetsov M-11	10.35	14		Compare
Savoia-Marchetti SM.85		10.4	14		Compare
Beagle B.206	Continental IO-520	10.0584	13.716	6	Compare
De Havilland Hornet		10.668	13.716		Compare
Yakovlev Yak-4	Klimov M-105	10.18	14		Compare

All data (22 fields)

Name: Saro Cutty Sark
Manufacturer: Saunders-Roe
Description: The Saro A17 Cutty Sark was a British amphibious aircraft from the period between World War I and World War II, built by the British firm Saunders-Roe (also known as SARO).
First Flight: 1929-07-04
Entry Into service: 1930-01-01
Designer: Saunders-Roe
Type: Amphibian
Length (m): 10.3632
Height (m): 3.3528
Max Speed (km/h): 172.1998
Cruise Speed (km/h): 149.669
Max Ceiling (m): 2743.2
Rate of Climb (m/s): 2.54
Capacity Description: Two passengers or up to 510 lb payload
National Origin: United Kingdom
Number Built: 12
Powerplant Description: 2 × Armstrong-Siddeley Genet Major seven-cylinder air-cooled radial piston engines, 104 kW (140 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/Saro_Cutty_Sark
Flat Wing Span (m): 13.716
Flat Wing Area (m²): 29.729
Aircraft Engine: Armstrong Siddeley Genet Major
Number of Engines: 2