|
|
Maverick Structural Analysis
The Design has been analyzed and tested to meet these Regulations:
- 1. Airworthiness Standards, Chapter 522 Subchapter C - Structures Gliders and Powered Gliders issued by: Transport Canada, Jan. 1986
- 2. European Joint Airworthiness Standards JAR 22 Subpart C - Structure
- 3. British Civil Airworthiness Requirements Section S Small Light Aeroplanes (CAP 482)
- 4. 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
|
Murphy Maverick Specifications
|
| General Information
|
|
| GROSS WEIGHT |
950 LB. |
| EMPTY WEIGHT |
395-460 LB. |
| G-LOADING (NORMAL) |
+5.7 -3.8 |
| POWER RANGE |
53-65 HP |
| WING SPAN |
29' 5" (std) or 32' 5" (extended) |
| LENGTH |
20' 8" |
| FUSELAGE WIDTH |
37" |
| WING CHORD |
60" |
| TAIL SPAN |
106" |
| AIRFOIL |
4415 (MODIFIED) |
PLEASE 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.
|
