Bristol Sycamore Mk.14

 

Belgian Air Force version.

 

Source: ”Helicopters & Autogyros of the World”, Paul Lambermont with Anthony Pirie, Second edition 1970, Cassell & Company Ltd, SBN 304 93390 2

and,

Source: ”Bristol 171 Sycamore”, BAe Systems Heritage Team, BAe Systems Heritage Web site, Last accessed 11 Jul 2018 (with kind permission from BAe)

 

 

Image coming soon!

Overview
Parent type Bristol Type 171 Sycamore
Variant 171 Mk.4
Design authority Bristol Aeroplane Company Ltd - Helicopter Division
Primary manufacturer Bristol Aeroplane Company Ltd - Helicopter Division
Key Characteristics
Operational status No longer flying
Max gross weight (ground) 2,449 kg 5,399 lb
Crew 1
Seating arrangement Side-by-side
Configuration
VTOL type Helicopter
Compound type None
Lift configuration Single main rotor
Control device type Tail rotor
Features
Number of engines 1
Number of propulsors 0
Number of lift devices 1
Number of control devices 1

Bristol Sycamore Mk.14

 

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Bristol Sycamore Mk.14

 

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Bristol Sycamore Mk.14

 

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Bristol Sycamore Mk.14

 

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Bristol Sycamore Mk.14

 

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Bristol Sycamore Mk.14

 

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Bristol Sycamore Mk.14

 

Forum Proceedings related to the Bristol Sycamore Mk.14

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Vertiflite articles related to the Bristol Sycamore

Vertiflite, Spring 2001

Maple Seeds, Samaras and Sycamore Chats (What Was on Cayley's Mind?) -

 

 

Content from the AHS website related to the Bristol Sycamore

 

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Web pages

 

February 2017

 

 

Articles from the Journal of the American Helicopter Society related to the Bristol Sycamore

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Articles from NASA Technical Reports Server related to the Bristol Sycamore

 

Patent information from the US Patent and Trademark Office related to the Bristol Sycamore

 

Google Books related to the Bristol Sycamore

Bristol Sycamore Mk.14

 

Bristol Sycamore Mk.14

Aircraft Notes

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