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© Copyright 2004
Murphy Aircraft Mfg.
Ltd.
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Maverick Technical Specifications
Introduction • Description • Specs • Performance • Order Info
Maverick Structural Analysis
The Design has been analyzed and tested to
meet these Regulations:
- Airworthiness Standards, Chapter 522
Subchapter C - Structures Gliders and
Powered Gliders issued by: Transport Canada, Jan. 1986
- European Joint Airworthiness Standards JAR 22
Subpart C - Structure
- British Civil Airworthiness Requirements
Section S Small Light Aeroplanes (CAP 482)
- FAA - CFR - Part 23 Airworthiness Standards,
Normal, Utility & Acrobatic Category Airplanes Subpart
C-Structure, Jan. 1982
Summary: The design described by the basic Drawing
List is eligible for certification in the:
- NORMAL CATEGORY at a Gross Weight of 950 lb.
to all the above Standards
| MAVERICK GENERAL SPECS |
| Gross Weight (max) |
950 LB. |
| Empty Weight * |
395-460 lb. |
| G-Loading (Normal
Category) |
+5.7 -3.8 |
| Power Range |
53-65 HP |
| Wing Span |
29'5" (std)
32"5" (ext.) |
| Length |
20'8" |
| Fuselage Width |
37" |
| Wing Chord |
60" |
| Tail Span |
106" |
| Airfoil |
4415 (modified) |
| * Note: The
Maverick conforms to Canadian Advanced Ultralight Regulation
TP 101.41. Empty weights may vary due to Avionics,
Instruments, type and amount of paint and upholstery selected
by the individual builder. |
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