WASP

Southwest Florida Aviation International, Inc.
An Opportunity
by
Southwest Florida Aviation Int’l., Inc.
For
Expansion in the medium helicopter field.
SOUTHWEST FLORIDA AVIATION INTERNATIONAL, INC.
28000-A7 AIRPORT ROAD, BLDG. 101
CHARLOTTE COUNTY AIRPORT
PUNTA GORDA, FLORIDA 33982

ALL INFORMATION INCLUDED IN THIS PROPOSAL IS THE SOLE PROPERTY OF JAMIE R. HILL. ANYONE, WHO WISHES TO UTILIZE THIS INFORMATION FOR ANY PURPOSE MUST OBTAIN WRITTEN CONSENT FROM JAMIE R. HILL. IF THIS INFORMATION IS UTILIZED WITHOUT WRITTEN CONSENT, LEGAL ACTIONS WILL BE INITIATED.

Southwest Florida Aviation International, Inc.
SECTION PAGE
I. SYNOPSIS 1-2
II. DESIGN OF THE ROTORCRAFT 3
III. POWER PLANT 4
IV. ARMOR 5
V. ARMAMENT 6
VI. PERFORMANCE 7
VII. FURTHER MODIFICATIONS 8
VIII. COSTS 9
IX. DELIVERY SCHEDULE 10
X. ATTACHMENT A 11-12
XI. ATTACHMENT B 13
XII. ATTACHMENT C 14-16
XIII. ATTACHMENT D 17-20
ALL INFORMATION INCLUDED IN THIS PROPOSAL IS THE SOLE PROPERTY OF JAMIE R. HILL. ANYONE, WHO WISHES TO UTILIZE THIS INFORMATION FOR ANY PURPOSES, MUST OBTAIN WRITTEN CONSENT FROM JAMIE R. HILL. IF THIS INFORMATION IS UTILIZED WITHOUT WRITTEN CONSENT, LEGAL ACTIONS MAY BE INITIATED.

TABLE OF CONTENTS

Southwest Florida Aviation International, Inc.
SECTION I
IT IS PROPOSED AGREEMENTS BE CONTRACTED BETWEEN CLIENTS/CUSTOMERS AND THE UNDERSIGNED TO MANUFACTURE A HELICOPTER FOR USE BY MEDIUM LIFT OPERATORS AND ARMED FORCES AND SALE THROUGHOUT THE WORLD. THE ROTORCRAFT WILL BE BASED ON A HIGHLY SUCCESSFUL AIRFRAME POWER TRAIN AND ENGINE, BUT WOULD BE MODIFIED SO AS TO PROVIDE GREATLY ENHANCED PERFORMANCE, PAYLOAD, SPEED AND MANEUVERABILITY. IT COULD BE ARMED WITH A NOSE TURRET REMOTE CONTROLLED 20MM CANNON OR HEAVY MACHINE GUN AND A WIDE SELECTION OF ROCKETS AND MISSILES ON STUB WINGS. THE VULNERABLE PORTIONS OF THE HELICOPTER, TO INCLUDE COCKPIT, ENGINE AND TRANSMISSION, WOULD BE ARMORED. GREAT EMPHASIS WOULD BE PLACED ON PRODUCING A TECHNICALLY SOUND, RELATIVELY UNSOPHISTICATED AND RUGGED ROTORCRAFT, WHICH WOULD ENJOY LOW OPERATING COSTS, SIMPLE MAINTENANCE PROCEDURES AND BE DESIGNED FOR USE IN THE LOW INTENSITY WARFARE, WHICH WILL CHARACTERIZE THE FORESEEABLE FUTURE. BY MODIFYING EXISTING AIRFRAMES AND USING TOTALLY REMANUFACTURED ENGINES AND COMPONENTS, IT IS ANTICIPATED THAT THE COST OF PRODUCTION OF THIS ROTORCRAFT WOULD BE ABOUT ONE THIRD THAT OF THE BELL AH- 1 COBRA ROTORCRAFT. THE RELATIVELY LOW COST, RELIABILITY AND PERFORMANCE OF THE ROTORCRAFT SHOULD INSURE A SUBSTANTIAL WORLDWIDE MARKET, PARTICULARLY AMONG COUNTRIES WHO DO NOT ANTICIPATE ENGAGEMENTS ON HIGH INTENSITY BATTLE FIELDS. ON THE FOLLOWING PAGES, THE PROPOSAL, AS WELL AS; THE DETAILS OF THE ROTORCRAFT WILL BE EXAMINED IN DEPTH. THIS VENTURE WOULD BE A HAPPY COMBINATION OF AMERICAN TECHNOLOGY AND FOREIGN CRAFTSMANSHIP. IT WOULD PROVIDE AN OPPORTUNITY TO ESTABLISH A PROFITABLE AVIATION INDUSTRY OUTSIDE OF THE UNITED STATES WITH CONSIDERABLE EXPORT EARNINGS, AS WELL AS PROVIDE ARMED FORCES WITH A MOST USEFUL TOOL FOR USE IN CURRENT OPERATIONS.

SYNOPSIS

ALL INFORMATION INCLUDED IN THIS PROPOSAL IS THE SOLE PROPERTY OF JAMIE R. HILL. ANYONE, WHO WISHES TO UTILIZE THIS INFORMATION FOR ANY PURPOSES, MUST OBTAIN WRITTEN CONSENT FROM JAMIE R. HILL. IF THIS INFORMATION IS UTILIZED WITHOUT WRITTEN CONSENT, LEGAL ACTIONS MAY BE INITIATED.

Southwest Florida Aviation International, Inc.
ALL INFORMATION INCLUDED IN THIS PROPOSAL IS THE SOLE PROPERTY OF JAMIE R. HILL. ANYONE, WHO WISHES TO UTILIZE THIS INFORMATION FOR ANY PURPOSES, MUST OBTAIN WRITTEN CONSENT FROM JAMIE R. HILL. IF THIS INFORMATION IS UTILIZED WITHOUT WRITTEN CONSENT, LEGAL ACTIONS MAY BE INITIATED.

SYNOPSIS (continued)

ALL INFORMATION INCLUDED IN THIS PROPOSAL IS THE SOLE PROPERTY OF JAMIE R. HILL. ANYONE, WHO WISHES TO UTILIZE THIS INFORMATION FOR ANY PURPOSES, MUST OBTAIN WRITTEN CONSENT FROM JAMIE R. HILL. IF THIS INFORMATION IS UTILIZED WITHOUT WRITTEN CONSENT, LEGAL ACTIONS MAY BE INITIATED.

Southwest Florida Aviation International, Inc.
SECTION II

DESIGN OF THE ROTORCRAFT

THE ROTORCRAFT WOULD BE BUILT UP FROM A SKELETON OF AN EXISTING HELICOPTER AIRFRAME (ATTACHMENT A). IT WOULD USE THE SAME ENGINE, TRANSMISSION AND OTHER DYNAMIC COMPONENTS TO INSURE RELIABILITY AND EASE OF MAINTENANCE.
EXTENSIVE AIRFRAME MODIFICATIONS WOULD REDUCE THE TOTAL WIDTH OF THE FUSELAGE TO ABOUT 3'8", MODIFY THE COCKPIT TO SINGLE OR DUAL PILOT CONFIGURATION, SLIGHTLY SHORTEN THE MACHINE OVERALL, GIVE IT A MORE AERODYNAMIC NOSE AND PROVIDE FOR THE INSTALLATION OF WINGS (ATTACHMENT B). THE DRAWINGS FOR THE PROTOTYPE HELICOPTER ARE LOCATED IN ATTACHMENT C.

ALL INFORMATION INCLUDED IN THIS PROPOSAL IS THE SOLE PROPERTY OF JAMIE R. HILL. ANYONE, WHO WISHES TO UTILIZE THIS INFORMATION FOR ANY PURPOSES, MUST OBTAIN WRITTEN CONSENT FROM JAMIE R. HILL. IF THIS INFORMATION IS UTILIZED WITHOUT WRITTEN CONSENT, LEGAL ACTIONS MAY BE INITIATED.

Southwest Florida Aviation International, Inc.
SECTION III

POWERPLANT

THE STANDARD LYCOMING T53-L– 703 ENGINE WOULD BE FITTED TO THE ROTORCRAFT IN ITS ORIGINAL CONFIGURATION. THIS IS CONSIDERED TO BE ADEQUATE GIVEN THE VERY CONSIDERABLE REDUCTION IN WEIGHT ACHIEVED BY CUTTING THE CREW FROM FOUR MEN TO ONE, AND THE REDUCTION OF ABOUT 1,000 LBS. FROM THE FUSELAGE AND AIRFRAME

ALL INFORMATION INCLUDED IN THIS PROPOSAL IS THE SOLE PROPERTY OF JAMIE R. HILL. ANYONE, WHO WISHES TO UTILIZE THIS INFORMATION FOR ANY PURPOSES, MUST OBTAIN WRITTEN CONSENT FROM JAMIE R. HILL. IF THIS INFORMATION IS UTILIZED WITHOUT WRITTEN CONSENT, LEGAL ACTIONS MAY BE INITIATED.

Southwest Florida Aviation International, Inc.
SECTION IV

ARMOR

IT WILL BE HIGHLY DESIRABLE TO ARMORPLATE CERTAIN VULNERABLE PORTIONS OF THE ROTORCRAFT. RECENT EXPERIENCES OF HOSTILITY HAS INDICATED THE NEED FOR ARMOR AROUND THE ENGINE, PILOT AND CERTAIN OTHER COMPONENTS. IT IS
CALCULATED THAT ABOUT 1,000 LBS. OF THE OPERATING WEIGHT CAN BE DEVOTED TO ARMOR PLATING OF AMPLE THICKNESS TO
TURN A 7.62 MM RIFLE BULLET AT CLOSE RANGE. ACTUAL DETAILS OF THE ARMORING, INCLUDING A DECISION TO INSTALL BULLETPROOF GLASS, WOULD BE LEFT TO THE DISCRETION OF THE PURCHASER.

ALL INFORMATION INCLUDED IN THIS PROPOSAL IS THE SOLE PROPERTY OF JAMIE R. HILL. ANYONE, WHO WISHES TO UTILIZE THIS INFORMATION FOR ANY PURPOSES, MUST OBTAIN WRITTEN CONSENT FROM JAMIE R. HILL. IF THIS INFORMATION IS UTILIZED WITHOUT WRITTEN CONSENT, LEGAL ACTIONS MAY BE INITIATED.

Southwest Florida Aviation International, Inc.
SECTION V

ARMAMENT

IT IS ANTICIPATED THAT THE STANDARD PERMANENTLY INSTALLED MAIN ARMAMENT WILL BE A RAPIDFIRE .50 CALIBER OR 20MM CANNON IN A REMOTE CONTROLLED AUTOMATIC TURRET LOCATED UNDER THE CHIN OF THE HELICOPTER. THE LUCAS GUN TURRET COUPLED WITH A SPERRY HELMET SIGHT APPEARS TO BE THE MOST READILY AVAILABLE RIG AT THIS TIME. ADDITIONAL ROCKETS AND MISSILES CAN BE MOUNTED ON THE STUB WINGS, TO INCLUDE THE 2.75 AIR-TO-GROUND ROCKET, VARIOUS ANTITANK MISSILES, NAPALM CANISTERS, GAS DISPENSERS AND OTHER MUNITIONS.

ALL INFORMATION INCLUDED IN THIS PROPOSAL IS THE SOLE PROPERTY OF JAMIE R. HILL. ANYONE, WHO WISHES TO UTILIZE THIS INFORMATION FOR ANY PURPOSES, MUST OBTAIN WRITTEN CONSENT FROM JAMIE R. HILL. IF THIS INFORMATION IS UTILIZED WITHOUT WRITTEN CONSENT, LEGAL ACTIONS MAY BE INITIATED.

Southwest Florida Aviation International, Inc.
SECTION VI

PERFORMANCE

BY SUBSTANTIALLY MODIFYING THE ORIGINAL DESIGN WITH THE ADDITION OF STUB WINGS AND REDUCTION OF THE FRONTAL AREA OF THE HELICOPTER, THE OVERALL WEIGHT OF THE ROTORCRAFT WILL BE LIGHTENED. IT IS EXPECTED THAT PERFORMANCE FIGURES WILL DRAMATICALLY INCREASE, ESPECIALLY IN THE REALM OF ACCELERATION, CLIMB RATES, CRUISE AND TOP SPEED. THE AIRFOIL CROSS SECTION OF THE STUB WING WILL BE DESIGNED TO MAXIMIZE LIFT IN THIS FLIGHT REGIME. IT IS EXPECTED THAT THE ACTUAL LENGTH OF THE WINGS WILL BE LONGER THAN MOST CURRENTLY IN VOGUE WITH U.S. STUB WINGS, SO AS TO INCREASE LIFT APPRECIABLY.

ALL INFORMATION INCLUDED IN THIS PROPOSAL IS THE SOLE PROPERTY OF JAMIE R. HILL. ANYONE, WHO WISHES TO UTILIZE THIS INFORMATION FOR ANY PURPOSES, MUST OBTAIN WRITTEN CONSENT FROM JAMIE R. HILL. IF THIS INFORMATION IS UTILIZED WITHOUT WRITTEN CONSENT, LEGAL ACTIONS MAY BE INITIATED.

Southwest Florida Aviation International, Inc.
SECTION VII

FURTHER MODIFICATIONS

IT WOULD BE HIGHLY DESIRABLE TO EVENTUALLY PRODUCE A ROTORCRAFT WITH TWIN ENGINES, PROBABLY, THE WELL PROVEN P&W PT6 TWINPAC, WHICH WOULD PROVIDE A DRAMATIC INCREASE IN LIFTING POWER, RELIABILITY AND CONFLICT SURVIVABILITY. AN INTERIM MODIFICATION WOULD BE INSTALLATION OF THE LYCOMING T53-L-703 ENGINE WITH 1,800 SHP RATHER THAN THE STANDARD DASH 13 WITH 1,400 SHP. ANOTHER USEFUL MODIFICATION WOULD BE THE REPLACEMENT OF THE SKIDS WITH RETRACTABLE, OR SEMI-RETRACTABLE, LANDING GEAR, OR FIXED WHEELS. SUCH A MODIFICATION WOULD ALLOW EASIER GROUND MANEUVERING, LESS DRAG AIRBORNE AND THE ABILITY TO TAKEOFF WITH HEAVIER WARFARE LOADS THAN WITH SKIDS AS THE ROTORCRAFT COULD BE ROLLED OFF THE GROUND. THE INITIAL ROTORCRAFT WILL BE SINGLE-PILOTED, BUT A GROWTH VERSION WITH A CO-PILOT/GUNNER, MOUNTED IN TANDEM WOULD BE DESIRABLE AS THE ROTORCRAFT GROWS FROM A DAYTIME VFR ROTORCRAFT TO ONE WITH ALL WEATHER CAPABILITIES.

ALL INFORMATION INCLUDED IN THIS PROPOSAL IS THE SOLE PROPERTY OF JAMIE R. HILL. ANYONE, WHO WISHES TO UTILIZE THIS INFORMATION FOR ANY PURPOSES, MUST OBTAIN WRITTEN CONSENT FROM JAMIE R. HILL. IF THIS INFORMATION IS UTILIZED WITHOUT WRITTEN CONSENT, LEGAL ACTIONS MAY BE INITIATED.

Southwest Florida Aviation International, Inc.
SECTION VIII

COSTS

THE ROTORCRAFT WILL BE AVAILABLE AT AN ESTIMATED $6.8 MILLION US$ COMPLETE WITH BASIC ARMAMENT AND SPECIFICATIONS AS NOTED IN ATTACHMENT D.

ALL INFORMATION INCLUDED IN THIS PROPOSAL IS THE SOLE PROPERTY OF JAMIE R. HILL. ANYONE, WHO WISHES TO UTILIZE THIS INFORMATION FOR ANY PURPOSES, MUST OBTAIN WRITTEN CONSENT FROM JAMIE R. HILL. IF THIS INFORMATION IS UTILIZED WITHOUT WRITTEN CONSENT, LEGAL ACTIONS MAY BE INITIATED.

Southwest Florida Aviation International, Inc.
SECTION IX

DELIVERY SCHEDULE

THE INITIAL ROTORCRAFT WILL BE DELIVERED ONE TO TWO YEARS AFTER A CONTRACT IS SIGNED. ALL SUBSEQUENT HELICOPTERS COULD BE DELIVERED AT FIVE MONTH INTERVALS UNTIL THE CONTRACT IS COMPLETED.

ALL INFORMATION INCLUDED IN THIS PROPOSAL IS THE SOLE PROPERTY OF JAMIE R. HILL. ANYONE, WHO WISHES TO UTILIZE THIS INFORMATION FOR ANY PURPOSES, MUST OBTAIN WRITTEN CONSENT FROM JAMIE R. HILL. IF THIS INFORMATION IS UTILIZED WITHOUT WRITTEN CONSENT, LEGAL ACTIONS MAY BE INITIATED.

SECTION X
ATTACHMENT A

SECTION X
ATTACHMENT A

SECTION XI
ATTACHMENT B

SECTION XII
ATTACHMENT C

SECTION XII
ATTACHMENT C

SECTION XII
ATTACHMENT C

Southwest Florida Aviation International, Inc.
SECTION XIII

ATTACHMENT D

HELICOPTER DIMENSION
LENGTH 57 FEET 1 INCH
HEGHT 13.4 FEET
WIDTH AT ELEVATORS 7 FEET
WIDTH FUSELAGE 3 FEET 8 INCHES
ROTOR SPAN 48 FEET
WEIGHT (empty) approximately 5,000 POUNDS
PERFORMANCE
VNE 165 KNOTS
CRUISE 150 KNOTS
GROSS WT. 10,500 POUNDS
PAYLOAD 5,500 POUNDS PLUS
RATE OF CLIMB (approximate) 3,000 FEET PER MINUTE
Performance specifications will be verified and adjusted by test flight.
AIRFRAME
Aluminum alloy fuselage
Fresh-air ventilators with adjustable outlets
Bleed-air heater and defroster with air noise suppression
Tinted overhead windows
Swing out jettisonable doors
Swing out panels for extended access to aft cabin (2)
Fixed step for entry to forward seats
Wheel-type landing gear
Mooring and jacking fittings (4)
External attachment fittings (12)
Semi-monocoque tailboom and vertical fin
Elevator (synchronized with fore and aft cyclic control)
Tail skid (tail rotor guard)
POWER PLANT
Lycoming T53-L-703 engine (1,800 SBP gas turbine)
(T53-L-13B is an alternate engine)
Starter (integral with generator)
Governor (automatic)
Power turbine control actuator
Ice detector with automatic anti-ice
Magnetic chip detector
Fuel system (220 U.S. gal. capacity, 215 U.S. gal. usable)
Pumps (submerged in tanks and on engine)
Fuel filter assembly
Oil tank (3 U.S. gal. capacity)
Oil cooler (turbine type)
Fire detection system
RPM warning system
Hinged cowling
TRANSMISSION DRIVE SYSTEM
Transmission (1,250 SBP T.O., 1,100 SBP Continuous)
Transmission oil cooler
Hydraulic pump for controls
Freewheeling unit (between engine and main transmission)
ROTOR AND CONTROLS
Semi-rigid type main rotor
Semi-rigid, two-bladed all metal tail rotor
Stabilizer bar and dampers
All controls hydraulically boosted
Forced system on cyclic and directional controls
RPM governor selector control
INSTRUMENTATION
Free air temps indicator
Altimeter (pressure)
Clock (8 day)
Magnetic compass
Airspeed indicator
Exhaust gas temperature indicator
Gas producer tachometer indicator
Torque meter indicator
D.C. voltmeter
A.C. voltmeter
Load meter
Engine out
Rate of climb indicator
Turn and slip indicator
Attitude indicator (3 axis Gyro 5 inch)
Dual tachometer (rotor and engine)
INSTRUMENTATION (CONTINUED)
Engine oil-temperature indicator
Engine oil-pressure indicator
Master caution indicator
RPM warning light
Fuel pressure indicator
Transmission oil-temperature indicator
Transmission oil-pressure indicator
CAUTION PANEL
Master Caution System - When limits are approached, warning lights (with appropriate wording) draws attention to:
Engine oil pressure
Engine icing
Engine ice detector
Engine de-ice on
Left fuel boost
Right fuel boost
Engine fuel pump
20 minute fuel
Fuel filter
Emergency governor
Oil filter
Transmission oil pressure
Transmission oil hot
Hydraulic pressure
Instant inverter
D.C. generator
Spares
ELECTRICAL
Generator (30 volt, 300 ampere D.C. starter-generator)
Inverters (2) (Class B, 250 volt ampere, 3 phase)
Nickel cadmium battery (34 amp hours)
Voltage regulator
Navigation lights
Landing light - retractable
Anti-collision lights
Searchlight - controllable
Cockpit light
External power receptacle
MISCELLANEOUS
Ground handling wheels
Turbine air inlet covers
Tail pipe cover
Pitot tube cover
Tail rotor tie-down strap
Rotor tie-down assembly
Maintenance and Overhaul manual
Parts Catalog
Flight Manual
Engine Log Book
This aircraft will be equipped with engine exhaust and 20 infrared suppression kit.

ALL INFORMATION INCLUDED IN THIS PROPOSAL IS THE SOLE PROPERTY OF JAMIE R. HILL. ANYONE, WHO WISHES TO UTILIZE THIS INFORMATION FOR ANY PURPOSES, MUST OBTAIN WRITTEN CONSENT FROM JAMIE R. HILL. IF THIS INFORMATION IS UTILIZED WITHOUT WRITTEN CONSENT, LEGAL ACTIONS MAY BE INITIATED.

Southwest Florida Aviation International, Inc.
SECTION XIII

STANDARD EQUIPMENT

ALL INFORMATION INCLUDED IN THIS PROPOSAL IS THE SOLE PROPERTY OF JAMIE R. HILL. ANYONE, WHO WISHES TO UTILIZE THIS INFORMATION FOR ANY PURPOSES, MUST OBTAIN WRITTEN CONSENT FROM JAMIE R. HILL. IF THIS INFORMATION IS UTILIZED WITHOUT WRITTEN CONSENT, LEGAL ACTIONS MAY BE INITIATED.

Southwest Florida Aviation International, Inc.
SECTION XIII

STANDARD EQUIPMENT (CONTINUED)

ALL INFORMATION INCLUDED IN THIS PROPOSAL IS THE SOLE PROPERTY OF JAMIE R. HILL. ANYONE, WHO WISHES TO UTILIZE THIS INFORMATION FOR ANY PURPOSES, MUST OBTAIN WRITTEN CONSENT FROM JAMIE R. HILL. IF THIS INFORMATION IS UTILIZED WITHOUT WRITTEN CONSENT, LEGAL ACTIONS MAY BE INITIATED.

Southwest Florida Aviation International, Inc.
SECTION XIII

STANDARD EQUIPMENT (CONTINUED)

ALL INFORMATION INCLUDED IN THIS PROPOSAL IS THE SOLE PROPERTY OF JAMIE R. HILL. ANYONE, WHO WISHES TO UTILIZE THIS INFORMATION FOR ANY PURPOSES, MUST OBTAIN WRITTEN CONSENT FROM JAMIE R. HILL. IF THIS INFORMATION IS UTILIZED WITHOUT WRITTEN CONSENT, LEGAL ACTIONS MAY BE INITIATED.

Southwest Florida Aviation International, Inc.
SECTION XIII

STANDARD EQUIPMENT (CONTINUED)

ALL INFORMATION INCLUDED IN THIS PROPOSAL IS THE SOLE PROPERTY OF JAMIE R. HILL. ANYONE, WHO WISHES TO UTILIZE THIS INFORMATION FOR ANY PURPOSES, MUST OBTAIN WRITTEN CONSENT FROM JAMIE R. HILL. IF THIS INFORMATION IS UTILIZED WITHOUT WRITTEN CONSENT, LEGAL ACTIONS MAY BE INITIATED.

Southwest Florida Aviation International, Inc.

PROTOTYPE PICTURE

The WASP by Southwest Florida Aviation International
(Right view)

ALL INFORMATION INCLUDED IN THIS PROPOSAL IS THE SOLE PROPERTY OF JAMIE R. HILL. ANYONE, WHO WISHES TO UTILIZE THIS INFORMATION FOR ANY PURPOSES, MUST OBTAIN WRITTEN CONSENT FROM JAMIE R. HILL. IF THIS INFORMATION IS UTILIZED WITHOUT WRITTEN CONSENT, LEGAL ACTIONS MAY BE INITIATED.

Southwest Florida Aviation International, Inc.

PROTOTYPE PICTURE

The WASP by Southwest Florida Aviation International
(Left view)

ALL INFORMATION INCLUDED IN THIS PROPOSAL IS THE SOLE PROPERTY OF JAMIE R. HILL. ANYONE, WHO WISHES TO UTILIZE THIS INFORMATION FOR ANY PURPOSES, MUST OBTAIN WRITTEN CONSENT FROM JAMIE R. HILL. IF THIS INFORMATION IS UTILIZED WITHOUT WRITTEN CONSENT, LEGAL ACTIONS MAY BE INITIATED.

GUNSHIP