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Frazer Nash Falcon 6

Bodywork

type 4/5S DHC
doors 2

Engine information

Bore × stroke 65.00 mm × 96.00 mm 2.56 in × 3.78 in
Cylinders S-6
Displace 1.9 litre 1911 cc (116.616 cu in)
Engine type OHV
Valves 2 valves per cylinder | 12 valves in total
Engine construction
Sump
Compression ratio 6.80:1
Fuel system 3 SU carbs
Maximum power
0-50 mph
0-60 mph
0-100 mph
0-100 km/h
80 - 120 km/h
402 m (Quarter mile)
Standing km
Top speed
Fuel consumption
CO2 emissions
Power to weight ratio
Specific output
Maximum torque
bmep
Specific torque
Maximum rpm
Code
Main bearings
Coolant Water
Bore / stroke ratio 0.68
Unitary capacity 318.5 cc/cylinder
Aspiration Normal
Compressor type N/A
Intercooler None
Catalytic converter N

Dimensions and weight

wheelbase 2591 mm
wheelbase 102 in
Length (milimeters) 3658 mm
Length (inches) 144 in
Width (milimeters) 1372 mm
Width (inches) 54 in
Height (milimeters)
Height (inches)
L:W ratio 1.41
Ground clearance (milimeters)
Ground clearance (inches)
Kerb weight (kilograms) 740 kg
Kerb weight (pounds) 1631 lb
Weight distribuiton
Fuel capacity (litres) 40.9 litre
Fuel capacity (UK Ga) 9 UK Gal
Fuel capacity (US Gal) 10.8 US Gal

Aerodynamics

Drag coefficient
Frontal area
Cx

Chassis

Engine location Front
Engine alignment Longitudinal
Drive RWD
Steering
Turns lock-to-lock
Turning circle 10.40 m
Tyres
Wheels
Brakes F/R Dr/Dr
Brake ∅
Braked area
Transmission 4M
Top gear ratio 1.00
Final drive ratio 3.80

General information

RAC rating 15.7
Number made
Model code
Model family
Insurance classification No information available
Tax band No information available

Manual Download

Download 1937 Frazer Nash Falcon 6 PDF Manual
Designer unknown
Year 1937

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