Saunders A.14

Length
14.83 m
Flat Wing Span
22.86 m
Height
5.7 m
Flat Wing Area
134.5 m²
Cruise Speed
140 km/h
Max Speed
156 km/h
Max Ceiling
2590 m
Number of Engines
2
Aircraft Engine
First Flight
1928-01-01
Number Built
1
Maximum Range
965 km

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Aircraft Weight Variants

Aircraft Maximum Range (km)
Saunders A.14 965

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All data (23 fields)
Name
Saunders A.14
Manufacturer
Saunders-Roe
Description
The Saunders A.14 was a test aircraft for Saunders' new metal hull construction method, being a Supermarine Southampton fitted with the Saunders' fuselage.
First Flight
1928-01-01
Designer
Harry Knowler
Length (m)
14.83
Height (m)
5.7
Cockpit Crew
5
Max Speed (km/h)
156
Cruise Speed (km/h)
140
Max Ceiling (m)
2590
Rate of Climb (m/s)
2
Endurance (h)
6.5
National Origin
United Kingdom
Number Built
1
Powerplant Description
2 × Napier Lion VA W-12 watercooled, 370 kW (496 hp) each
Primary Users
Royal Air Force
Status
Prototype
Wikipedia Article (URL)
en.wikipedia.org/wiki/Saunders_A.14
Flat Wing Span (m)
22.86
Flat Wing Area (m²)
134.5
Aircraft Engine
Napier Lion
Number of Engines
2