Product
GP-42
Description  GP-42
Item No  9041
Category  Engine >>> Nitro Engine >>> 2-Stroke Aircraft GP Series
Update Data  2008-07-23
Basic Specification

Engine

GP-42

Displacement

6.90 c.c. / .421 cu.in.

Bore

21.5 mm / 0.846 in.

Stroke

19.0 mm / 0.748 in.

Practical R.P.M.

2,000 ~ 15,000 rpm

Output (BHP/RPM)

1.10 / 14,000

Weight (g/oz)

357.2 / 12.60

Gallery
Introduction

The GP series engines are equipped with maintenance-free bronze bushings, Schnuerle porting, a non-ring piston, an easily adjusted air bleed carburetor, and a safe angular needle valve. The GP-42 engine provide excellent performance and value for .40-powered trainers.

Features
One-piece crankcase with bronze oilite bushing for easier maintenance.(no bearings).
Aluminum piston with Nichel-plated brass cylinder liner.
Air bleed carburetor design for easier adjusting.
Swept back needle valve.
Side exhaust.
3-chamber muffler.
Redline R2 glow plug included.
Content
Other File Download
Instruction Manual
9041-manual (272 KB)
Parts Catalog
9041-Catalog (5 MB)
Mutuality Products
Have no data
Stock code 8033 Public of Stock website http://newmops.tse.com.tw
Map MMS CPFR_System Contact_us
NO.7, 6TH ROAD INDUSTRY PARK TAICHUNG. TAIWAN R.O.C. 407  Tel:886-4-23591616 FAX:886-4-23591902
Copyright 2005. Thunder Tiger CORP. All Rights Reserved.