n604rn.pdf by Federal Aviation Administration

Author:Federal Aviation Administration
Language: eng
Format: epub
Tags: documentcloud;cir
Published: 2012-08-12T16:00:00+00:00

Bavtheon

Revision History

Raytheon

Table of Contents

Aircraft Specifications 1

1. Define the experimental purpose(s) under which the aircraft is to be operated (14 CFR § 21.191) 2

2. Describe the purpose/scope of the experimental program for each 14 CFR § 21.191 experimental purpose sought (14 CFR § 21.193(b)(d)) 2

3. Define the area(s) in which the experimental flights will be conducted 3

4. Aircraft Configuration 8

5. Inspection And Maintenance (14 CFR 91.7) 12

6. Pilot Qualification (14 CFR §§ 61.3, 61.5) 13

7. Aircraft Marking (14 CFR § 45) 15

8. ATC Transponder and Altitude Reporting System Equipment and Use (14 CFR § 91.215) 15

9. Method for See and Avoid (14 CFR § 91.113a) 16

10. Safety Risk Management 16

11. System Configuration 17

12. System Safety - Flight Termination and Lost Link 17

13. Command and Control 19

14. Control Stations 20

15. Control Frequencies 21 Appendix A - Cobra Drawings and Photographs 23 Appendix B - Cloud Cap Piccolo II Users Guide 26 Appendix C - Raytheon UAS Flight Manual 27 Appendix D - Cobra Weight and Balance 27 Appendix E - Minimum Equipment List 28 Appendix F - System Configuration Diagram 32 Appendix G - FAA UAS Safety Checklist 35 Appendix H - Acronym List 36

Table of Figures

Figure: 1 Cobra UAS 2

Figure: 2 UVI Airfield 4

Figure: 3 Containment Area 6

Figure: 4 Cobra 3 View Drawing 8

Figure: 5 MVCS CUCS 11

Figure: 6 Piccolo Autopilot Limits 18

Aircraft Specifications

Registered Owner Name: Aircraft Builder:

Raytheon Company Raytheon Missile Systems

Registered Owner Address:

Raytheon Missile Systems Bldg M09, M/S 5 P.O.Box 11337 Tucson, AZ 85734-1337

Aircraft Description:

The aircraft is an unmanned, composite, mid-wing monoplane with standard tail surfaces and a tractor engine. The vertical and horizontal stabilizers are attached to a composite tail boom. The control surfaces consist of full span flaperons, elevator and rudder. The landing gear is tricycle type with a steerable nosewheel, and the main landing gear is equipped with pneumatic brakes. The engine is a 16 hp, air-cooled, 2-cycle, 2 cylinder, opposed, and carbureted powerplant with an electronic ignition system, using gasoline with a 100:1 2-cycle oil mix. Primary electrical power comes from a 500 watt generator with a 180 watt regulator. A Lithium Polymer rechargeable battery provides backup electrical power for 1 hour in the case of main power source failure. As a prototype airframe, Raytheon expects that there will be slight design changes based on the data collected from the initial test flights.

Aircraft Registration:

This will be an Experimental Aircraft Registration.

Unless otherwise specified in the certificate, the aircraft will be marked on the aft fuselage surface using the N12345 format. 3" lettering will be used due to the small size of the aircraft. The word "Experimental" will be displayed on the fuselage over the wing in Vi" letters.

Year Manufactured:

2006

Aircraft Serial Number:

Serial Number 004 ;

(Update serial number for each application)

Aircraft Registration Number:

N604RN

Aircraft Model Designation:

Cobra

Engine Model:

Desert Aircraft DA-150 http://www.desertaircraft.com/engines deta il.php?Page=DA-150

Fuel:

87-91 Octane Gasoline OR

100 Octane Aviation Fuel Oil:

Saber™ Professional Synthetic 100:1 Pre-Mix 2-Cycle Oil (ATP)

http://www.amsoil.com/storefront/atp.aspx Propeller Model:

Mejzlik 28 x 12 -3b; 28 x 12 W-3b; 30 x 12 http://meizlikmodellbau.inshop.cz

lafthefii

Download

Copyright Disclaimer:
This site does not store any files on its server. We only index and link to content provided by other sites. Please contact the content providers to delete copyright contents if any and email us, we'll remove relevant links or contents immediately.