| Murphy Maverick | |
|---|---|
| Role | Two-seat high-wing ultralight |
| National origin | Canada |
| Manufacturer | Murphy Aircraft |
| Introduction | 1993 |
| Status | In production (2011) |
| Number built | 105 (2011) |
The Murphy Maverick is a Canadian two-seat fixed-wing ultralight monoplane designed by Murphy Aircraft of British Columbia.[1] The type is sold as a kit for home construction.[2]
Designed as a smaller version of the Rebel, the Maverick is an all-metal high-wing braced monoplane with two side-by-side seats and a tailwheel landing gear.[1] The aircraft was designed around the Rotax 503 powerplant, with the goal of producing an economical ultralight trainer.[3]As a homebuilt it can also be fitted with a number of different piston engines including the HKS 700, Rotax 582 and Jabiru 2200.[1][4]
The aircraft is mainly built from sheet aluminium, with the tail and rear sections of the wings fabric covered to save weight.[1] The wings are constructed using a "D" cell, with stamped ribs and a single wing strut. Standard wing span on the Maverick is 29ft 6in (9m), but an optional wing extension is available to increase the wingspan to reduce the wing loading.[3]
The standard landing gear is of a taildragger configuration and bungee suspended, with sprung steel main gear as an option. Additional options include 24 US gal (91 l) wing-mounted fuel tanks and fittings for installing floats.[3]
Data from World Directory of Leisure Aviation[1] & Cliche[3]
General characteristics
Performance
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