Exhibit 10.21


 


UTILICRAFT AEROSPACE INDUSTRIES, INC.

554 Briscoe Blvd. Lawrenceviile, GA 30045

Phone: (678) 376-0898 Fax: (678) 376-9093


 


Purchase Order


 


PO
Number:                           D3-07-05-SOW-1


 


Date:                                      July 25, 2005


 


	
  Amount:

  	
  $

  	
  137,750

  	
   

  



 


Terms:                   Invoice Bi-Weekly - Payment Net 15 days


 


Deliverables
(A and B):


 


A.            FF-1080-300 Wind Tunnel
Support


 


	
  $145/hr (not to exceed 50 hrs)

  	
  $

  	
  7,250

  	
   

  



 


1.     D3 shall review the fwd fuselage loft and
provide cross sections to enlarge the lower fuselage corners accommodating
adequate frame depth. If feasible, D3 shall perform a quick frame analysis
using an assumed payload scenario for this purpose.


 


2.     D3 shall review the mid-fuselage loft and
provide cross sections to enlarge the upper fuselage corners accommodating
adequate frame depth to support wing to body joint. If feasible, D3 shall
perform a quick frame analysis using an assumed payload scenario for this purpose.


 


3.     D3 shall review the aft fuselage loft and
provide a cross section at the approximate location of the vertical tail front
spar which will provide sufficient depth for strength of the vertical tail attachment
and space for upper cargo door stowage. This data is to be used by AMI for aerodynamic
design of the transition from the flat upper fuselage to a curved upper
fuselage to improve the vertical tail aerodynamics.


 


4.     D3 shall use the preliminary landing gear
loads (or make assumptions as needed) and perform a quick analysis defining a
desired depth for the landing gear boom.


 


5.     D3 shall review the wing loads and make a quick
analysis of wing displacement for positioning of the wing on the top of the
fuselage with adequate gap for wing flexing.


 


6.     D3 shall review the overall landing gear wing
arrangement configuration and provide guidance regarding adequate ground
stability and take-off rotation.


 


7.     D3 recommends that the engine longitudinal
position be re-evaluated incorporating the rotor burst criteria. D3 will review
its recent experience in this respect and provide guidance material to AMI.


 


TECHNICAL DATA REQUIRED FROM
AMI:


 


1.     IGES model of loft (received 6/28).


2.     Max shear/moment values for wing at approx.
BL 50.


3.     Max shear/moment values for root of vertical
tail.


4.     Fwd/uppermost CG location for stability
analysis.


 

















 


B.            FF-1800-300 Development of
Program Plan And Specification Documents


 


	
  $145/hr (not to exceed 900 hrs)

  	
  $

  	
  130,500

  	
   

  



 


Program
Planning (Phase I)

Project Structure

Project Reporting and Reviews

Work Breakdown Structure

Document Control

Buyer Furnished Item Requirements


 


Technical
Specifications

Design Requirements
and Objectives (DR & O)

Description of Aircraft Configurations, System Definitions and Principal
Structural Concepts

List of Development Tools and Software

Implementation of Product Development Management System


 


Program
Plan Outline

Systems Integration
and Concept Verification Design Phase (Phase II)

Aircraft Configuration Development and Definition

Aerodynamic Design and Validation

Preliminary Design Phase (Phase III)

Detail Design Phase (Phase IV)

Systems Integration

Quality Assurance Plan

Certification Planning and Support

Production Support

Program Management

Program Schedule

Program Staffing

Assumptions
Deliverables


 


Program
Price Estimation

Planning (Phase I)

Systems Integration and Concept Verification Design Phase (Phase II)

Preliminary Design Phase (Phase Ill)

Detail Design Phase (Phase IV)

Performance Flight Test Aircraft

Production (Phase V)


 


 


	
  Authorized
  By:

  	
  

  	
   

  
	
   

  	
  John J. Dupont

  
	
   

  	
  Chairman, President - CEO

  
	
   

  	
  Utilicraft Aerospace
  Industries, Inc.