.. October 26, 2015 U.S. Department of Transportation Docket Management System 1200 New Jersey Ave., SE Washington, DC 20590 Re: Exemption Request Section 33 3ofthe FAA Reform Act and Part 11ofthe Federal Aviation Regulations from 14 C.P.R. 45.23(b);14 CFR Part 21;14 CFR 61.113 (a)&(b); 91.7 (a);91.9 (b) (2);91.103(b); 91.109;91.119; 91.121; 91.151(a);91.203(a) & (b);91.405 (a); 91.407(a) (1); 1.409 (a) (2);91.417 (a)&(b). PETITION FOR SUMMARY EXEMPTION Summary Grant exemptions include 11822, 12339 Dear Siror Madam:Pursuant to Section 333 ofthe FAA Modernization and Reform Act of2012 (the Reform Act)

and14 C.P.R. Part 11,G2 Aerial, Inc. operator of Small Unmanned Aircraft Systems ("sUASs") equipped to offer commercial UAS operations for closed set/scripted filming and aerial data collection in the following applications:

• Filmmaking, Cinematography, and Videography • Precision Agriculture • Wildlife and Forestry Monitoring • Aerial Surveying • Inspection, Patrolling, and Monitoring • Security and Surveillance G2 Aerial, Inc. hereby applies foran exemption from the listed Federal Aviation Regulations ("F ARs") to allow commercial operation ofits sUASs, so long as such operations are conducted within and under the conditions outlined herein oras may be established bythe FAA as required by Section 333. As described more fully below, the requested exemption would permit the operation of small, unmanned and relatively inexpensive sUAS under controlled conditions in airspace thatis1) limited 2) predetermined 3) controlled asto access and4) would provide safety enhancements tothe already safe operations using conventional aircraft. Approval ofthis exemption would thereby enhance safety and fulfill the Secretary of Transportation's (the FAA Administrator's) responsibilities to"... establish requirements forthe safe operation of such aircraft systems inthe national airspace system." Section 333(c) ofthe Reform Act. The name and address ofthe petitioner is:

G2 Aerial, Inc. Attn: Gary Kaplan 3529 Cay Drive Carlsbad, Ca. 92010 Ph: 858-353-5322Email: Sales@G2Aerial.com Page 1of9Regulations from which the exemption is requested: 14 CFRPart21 14 C.F.R. 45.23(b) 14 CFR 61.113 (a)&(b) 14 C.F.R. 91.7 (a) 14 CFR 91.9 (b)(2) 14 C.F.R. 91.103 14 C.F.R. 91.109 14 C.F. R. 91.119 14 C.F.R. 91.121 14 CFR 91.151 (a) 14 CFR 91.203 (a)&(b) 14 CFR 91.405 (a) 14 CFR 407 (a)(1) 14 CFR 409 (a)(2) 14 CFR 417 (a)&(b) This exemption application is expressly submitted to fulfill Congress' goal in passing Section 333(a) through (c)ofthe Reform Act. This law directs the Secretary of Transportation to consider whether certain unmanned aircraft systems may operate safely inthe national airspace system (NAS)

before completion ofthe rulemaking required under Section 332 ofthe Reform Act. In making this determination, the Secretary is required to determine which types ofUASs donot create a hazard to users ofthe NAS orthe public or posea threat to national security in light ofthe following: •The UAS's size, weight, speed, and operational capability • Operation ofthe UAS in close proximity to airports and populated areas; and • Operation ofthe UAS within visual line of sight ofthe operator. Reform Act§ 333 (a). Lastly, ifthe Secretary determines that such vehicles "may operate safely inthe national airspace system, the Secretary shall establish requirements forthe safe operation of such aircraft inthe national airspace system." /d§333(c) Applicant interprets this provision to place the duty onthe Administrator tonot only process applications for exemptions under section 333, but forthe Administrator to craft conditions forthe safe operation ofthe UAS, ifit should be determined that the conditions set forth herein donot fulfill the statutory requirements for approval. The Federal Aviation Act expressly grants the FAA the authority to issue exemptions. This statutory authority byits terms includes exempting civil aircraft, asthe term is defined under §40l01of the Act that includes sUASs, from the requirement that all civil aircraft must havea current airworthiness certificate. The Administrator may grant an exemption froma requirement ofa regulation prescribed under subsection (a)or(b) ofthis section orany sections 44702-44716 ofthis titleifthe Administrator

finds the exemption inthe public interest. 49 U.S.C. §44701(f) See also 49 USC §44711(a); 49 USC §44704; 14 CFR §91.203 (a) (1). G2 Aerial, Inc. sUASs are rotorcraft, weighting 55or fewer lbs. including payload. They operate, under normal conditions ata speed ofno more than 87 knots and have the capability to hover, and move inthe vertical and horizontal plane simultaneously. They will operate only inline of sight and will operate only within a sterile area described inthe Motion Picture and Television Operations Manual (MPTOM) that will be submitted confidentially. Such operations will ensure that the sUAS will "not create a hazard to users ofthe national airspace system orthe public." Page 2of9G2 Aerial, Inc. intends to operate the following sUASs: ManufacturerDJIAlignAlign DZY'NE Technologies, Inc. ModelSlOOO690L Hexacopter 800 TrekkerAtlas-8 Max Gross Weight 21 pounds11.5 pounds 26 pounds 54 pounds. The sUAS that will be operated byG2 Aerial, Inc. will be registered in accordance with 49 U.S.C. 44103, Registration of Aircraft, as well as14 C.F.R Part 47, Aircraft Registration, and marked in accordance with 14 C.F.R Part 45, Identification and Registration Marking. Reform Act Section 333 (b). Given the small size ofthe sUASs involved and the restricted sterile environment within which they will operate, the applicant falls squarely within that zone of safety (an equivalent level of safety) in which Congress envisioned that the FAA must, by exemption, allow commercial operations ofUASs to commence immediately. Also duetothe size ofthe UASs and the restricted areas in which the relevant sUASs will operate, approval ofthe application presents no national security issue. Given the clear direction in Section 333 ofthe Reform Act, the authority contained inthe Federal Aviation Act, as amended; the strong equivalent level of safety surrounding the proposed operations, and the significant public benefit, including enhanced safety, reduction in environmental impacts, including reduced emissions associated with allowing UASs, the grant ofthe requested exemptions isinthe public interest. Accordingly, the applicant respectfully requests that the FAA grant the requested exemption without delay. AIRCRAFT AND EQUIVALENT LEVEL OF SAFETY The applicant proposes that the exemption requested herein apply to civil aircraft that have the characteristics and that operate with the limitations listed herein. These limitations provide forat least an equivalent or even higher level of safety to operations under the current regulatory structure because the

proposed operations represent a safety enhancement tothe already safe operations conducted with conventional aircraft.These limitations and conditions to which G2 Aerial, Inc. agrees tobe bound when conducting

commercial operations under an FAA issued exemption include: 1.The sUAS will weigh less than 55lbs. 2. Flights will be operated within line of sight ofapilot and/or observer. 3. Maximum total flight time for each operational flight will be45 minutes. Flights will be terminated at 25% battery power reserve should that occur prior tothe45 minute limit. 4. Flights will be operated atan altitude ofno more than 400 feet AGL or, not more than 200 feet above an elevated platform from which filming is planned. 5. Minimum crew for each operation will consist ofthe sUAS Pilot, the Visual Observer, and/or the Camera Operator. 6. sUAS pilot will bean FAA licensed airman with at leasta sport pilot certificate anda valid US Driver's License. 7. sUAS Pilot will be Pilot in Command (PIC). Ifapilot certificate holder other than the sUAS Pilot, who possess the necessary PIC qualifications, isalso present (i.e. the Visual Observer), that person can also be designated asthe PIC. 8.The UAS will only operate within a confined "Sterile Area" ofthe flight operations area. Page 3of99.A briefing will be conducted in regard tothe planned sUAS operations prior to each day's activities. It will be mandatory that all personnel who will be performing duties within the boundaries ofthe safety perimeter be present for this briefing. 10. The operator will obtain the consent ofall persons involved and ensure that only consenting persons will be allowed within 100 feet ofthe flight operation, and this radius may be reduced to30 feet based upon an equivalent level of safety determination.

11. Pilot and observer will have been trained in operation ofUAS generally and received up-to-date information onthe particular UAS tobe operated. 12. Observer and pilot willatall times are able to communicate by voice and/or text. 13. Written and/or oral permission from the relevant property holders will be obtained. 14.All required permissions and permits will be obtained from territorial, state, county orcity jurisdictions, including local law enforcement, fire, or other appropriate governmental agencies. 15.Ifthe sUAS loses communications or loses its GPS signal, the UAS will have capability to return toa pre-determined location within the Security Perimeter and land. 16. The sUAS will have the capability to abort a flight in case ofunpredicted obstacles or emergencies. 14 C.F.R. Part 21, Subpart H: Airworthiness Certificates 14 C.F.R. §91.203 (a)(1) Subpart H, entitled Airworthiness Certificates, establishes the procedural requirements forthe issuance of airworthiness certificates as required by FAR §91.203 (a) (1). Given the size and limited operating area associated with the aircraft tobe utilized bythe Applicant, an exemption from Part 21

Subpart H meets the requirements ofan equivalent level of safety under Part 11and Section 333 ofthe Reform Act. The Federal Aviation Act (49 U.S.C.§44701 (f)) and Section 333 ofthe Reform Act both authorize the FAA to exempt aircraft from the requirement foran airworthiness certificate, upon consideration ofthe size, weight, speed, operational capability, and proximity to airports and populated areas ofthe particular UAS.In all cases, an analysis of these criteria demonstrates that the UAS operated without an airworthiness certificate, inthe restricted environment and under the conditions proposed will beat least as safe, or safer, thana conventional aircraft (fixed wing or rotorcraft) operating with an airworthiness certificate without the restrictions and conditions proposed. The sUAS tobe operated hereunder isless than 55lbs. fully loaded, carries neither apilot nor passenger, carries no explosive materials or flammable liquid fuels, and operates exclusively within a secured area asset outinthe

Manual. Unlike other civil aircraft, operations under this exemption will be tightly controlled and monitored by both the operator, pursuant tothe Manual's requirements, and under the requirements andin compliance with local public safety requirements, to provide security forthe area of operation asisnow done with conventional filming. The FAA will have advance notice ofall operations. These safety enhancements, which already apply to civil aircraft operated in connection with motion picture and television production, provide a greater degree of safety tothe public and property owners than conventional operations conducted with airworthiness certificates issued under 14C.F.R. Part 21, Subpart H. Lastly, application of these same criteria demonstrates that there isno credible threat to national security posed bythe UAS, duetoits size, speed of operation, location of operation, lack of explosive materials or flammable liquid fuels, and inability to carry a substantial external load. The FAA has issued the following exemption tothis regulations Exemptions Nos. 11251. Page 4of914 C.F.R. § 45.23 (b). Marking ofthe Aircraft The regulation requires: When marks include only the Roman capital letter "N" and the registration number is displayed on limited, restricted or light-sport category aircraft or experimental or provisionally certificated aircraft, the operator must also display on that aircraft near each entrance tothe cabin, cockpit, or pilot station, in letters not less than2 inches nor more than6 inches high, the words "limited," "restricted," "light-sport," "experimental," or "provisional," as applicable. Even though the UAS will have no airworthiness certificate, an exemption may be needed asthe UAS will have no entrance tothe cabin, cockpit or pilot station on which the word "Experimental" canbe placed. Given the size ofthe sUAS, two-inch lettering will be impossible. The word "Experimental" will be placed onthe fuselage in compliance with §45.29 (f). The equivalent level of safety will be provided by having the sUAS marked onits fuselage as required by §45.29 (f) where the pilot, observer and others working with the sUAS will see the identification ofthe UAS as "Experimental." The FAA has issued the following exemptions tothis regulation to Exemptions, but not limited to, Nos. 10700, 8738, 10167 and 10167A, 11256, 11251. 14 C.F.R. § 61.113 (a)&(b): Private Pilot Privileges and Limitations: Pilot in Command. Sections 61.113 (a)&(b) limit private pilots to non-commercial operations. Because the sUAS will not carry apilot or passengers, the proposed operations can achieve the equivalent level of safety of current operations by requiring the PIC operating the aircraft to havea private pilot's license rather thana commercial pilot's license to operate this small UAS. Unlike a conventional aircraft that carries the pilot and passengers, the sUAS is remotely controlled with no living thing on board. The area of operation is controlled and restricted, andall flights are planned and coordinated in advance. The level of safety

provided by the requirements included inthe Manual exceeds that provided bya single individual holding a commercial pilot's certificate operating a conventional aircraft. The risks associated with the operation ofthe sUAS areso diminished from the level ofrisk associated with commercial operations contemplated by Part 61 when drafted, that allowing operations ofthe sUAS as requested witha private pilot asthe PIC exceeds the present level of safety achieved by14 C.F.R. §61.113 (a)&(b). 14 C.F.R. §91.7(a): Civil aircraft airworthiness. The regulation requires that no person may operate acivil aircraft unless itisin airworthy

condition. As there will beno airworthiness certificate issued forthe aircraft, should this exemption be

granted, no FAA regulatory standard will exist for determining airworthiness. Given the size ofthe aircraft and the requirements contained inthe Manual for maintenance and useof safety check lists prior to each flight, asset forth in Sections J, Land Q,an equivalent level of safety will be provided. 14 C.F.R. §91.9 (b) (2): Civil Aircraft Flight Manual inthe Aircraft. Section 91.9 (b) (2) provides: No person may operate a U.S.-registered civil aircraft ... (2) For which an Airplane or Rotorcraft Flight Manual isnot required by §21.5 ofthis chapter, unless there is available inthe aircraft a current approved airplane or Rotorcraft Flight Manual, approved manual material, markings, and placards, orany combination thereof. Page 5of9The sUAS, given its size and configuration hasno ability or place to carry sucha flight manual onthe aircraft, not only because there isno pilot on board, but because there isno room or capacity to carry such an item onthe aircraft. The equivalent level of safety will be maintained by keeping the flight manual atthe ground control point where the pilot flying the sUAS will have immediate access toit.The FAA has issued the following exemptions tothis regulation, but not limited to: Exemption Nos. 8607, 8737, 8738, 9299, 9299A,9565,9565B, 10167, 10167A, 10602,32827,10700, 11251,and11256. 14 C.F.R. § 91.103: Preflight action This regulation requires each pilot in command to take certain actions before flight to insure the safety of flight. As FAA approved rotorcraft flight manuals will notbe provided forthe aircraft an exemption will be needed. The PIC will take all actions including reviewing weather, flight battery requirements, landing and takeoff distances and aircraft performance data before initiation of flight. 14 C.F.R. §91.109: Flight instruction: Section 91.103 provides that no person may operate acivil aircraft (except a manned free balloon) thatis being used for flight instruction unless that aircraft has fully functioning dual controls. sUASs and remotely piloted aircraft, by their design donot have fully functional dual controls. Flight control is accomplished through the useofa control box that communicates with the aircraft via

radio communications. The FAA has approved exemptions for flight training without fully functional dual controls fora number of aircraft and for flight instruction in experimental aircraft. See Exemption Nos.5778K & 9862A. The equivalent level of safety provided bythe fact that neither apilot nor passengers will be carried inthe aircraft and bythe size and speed ofthe aircraft. 14 C.F.R. §91.119: Minimum safe altitudes Section 91.119 establishes safe altitudes for operation of civil aircraft. Section 91.119 (d) allows helicopters tobe operated atless than the minimums prescribed, provided the person operating the helicopter complies with any route or altitudes prescribed for helicopters bythe FAA. As this exemption isfora sUAS thatisa helicopter or multirotor and the exemption requests authority to operate at altitudes upto400 AGL, ornot more than 200 above an elevated platform from which filming is planned, an exemption may be needed to allow such operations. Asset forth herein, except for the limited conditions stated inthe Manual, the UAS will never operate at higher than 400 AGL. Itwill however be operated in a restricted area with security perimeter, where buildings and people will notbe exposed to operations without their pre-obtained consent. The equivalent level of safety will be achieved given the size, weight, and speed ofthe UAS as well asthe location where itis operated. No flight will be taken without the required permission ofthe property owner or local officials. Because ofthe advance notice tothe property

owner and participants inthe aerial activity, all affected individuals will be aware ofthe planned flight operations. Compared to flight operations with aircraft or rotorcraft weighting far more than the maximum 55lbs. proposed herein and the lack of flammable fuel, any risk associated with these operations isfar less than those presently presented with conventional aircraft operating ator below 500 AGL other industries. In addition, the low-altitude operations ofthe sUAS will ensure separation between these small-VAS operations and the operations of conventional aircraft that must comply with Section 91.119. Page 6of914 C.F.R. §91.121 Altimeter Settings This regulation requires each person operating an aircraft to maintain cruising altitude by reference toan altimeter thatisset"...tothe elevation ofthe departure airport oran appropriate altimeter setting available before departure." Asthe sUAS may not havea barometric altimeter, but instead aGPS altitude read out, an exemption may be needed. An equivalent level of safety will be achieved bythe operator, pursuant tothe Manual and Safety Check list, confirming the altitude of the launch site shown onthe GPS altitude indicator before flight. 14 C.F.R. § 91.151(a): Fuel Requirements for Flight in VFR Conditions Section 91.151 (a) prohibits an individual from beginning "a flight inan airplane under VFR conditions unless (considering wind and forecast weather conditions) there is enough fueltoflytothe first point of intended landing, and, assuming normal cruising speed - (1) During the day, tofly after that

forat least 30 minutes; or(2)At night, tofly after that forat least 45 minutes." The battery powering the sUAS provides approximately 30-50 minutes of powered flight. To meet the 30-minute reserve requirement in14 CFR §91.151, sUAS flights would be limited to approximately 20 minutes in length. Given the limitations onthe UAS's proposed flight area and the location ofits proposed operations within a predetermined area,a longer time frame for flight in daylight or night VFR conditions is reasonable. Applicant believes that an exemption from 14 CFR §91.151(a) falls within the scope of prior exemptions. See Exemption 10673 (allowing Lockheed Martin Corporation to operate without compliance with FAR 91.151 (a)). Operating the small UAS, ina tightly controlled area where only people and property owners or official representatives who have signed waivers will be allowed, with less than 30 minutes of reserve fuel, does not engender the type of risks that Section 91.151(a) was intended to alleviate given the size and speed ofthe small UAS. Additionally, limiting sUAS flights to20 minutes

would greatly reduce the utility for which the exemption will be granted. Applicant believes that an equivalent level of safety canbe achieved by limiting flights to45 minutes or 25% of battery power which ever happens first. This restriction would be more than adequate to return the sUAS toits planned landing zone from anywhere inits limited operating area. Similar exemptions have been granted to other operations, including Exemptions 2689F, 5745, 10673, 10808, and 11251.14 C.F.R. §91.203 (a) and (b): Carrying Civil Aircraft Certification and Registration The regulation provides in pertinent part:

(a) Except as provided in§ 91.715, no person may operate acivil aircraft unless ithas within it the following:(1)An appropriate and current airworthiness certificate .... (b)No person may operate acivil aircraft unless the airworthiness certificate required by

paragraph (a)ofthis section ora special flight authorization issued under §91.715 is displayed atthe cabin or cockpit entrance sothatitis legible to passengers or crew. Page 7of9The UAS fully loaded weighs no more than 55lbs. andis operated without an onboard pilot. As such, there isno ability or place to carry certification and registration documents orto display them onthe sUAS. An equivalent level of safety will be achieved by keeping these documents atthe ground control

point where the pilot flying the sUAS will have immediate access to them, tothe extent they are applicable tothe sUAS. The FAA has issued numerous exemptions tothis regulation. A representative sample of other exceptions includes Exemption Nos. 9565, 9665, 9789, 9789A, 9797, 9797A, 9816A, 10700, 11251, and 11256. 14 C.F.R. §91.405 (a); 407 (a) (1); 409 (a) (2); 417(a) &(b): Maintenance Inspections These regulations require that an aircraft operator or owner "shall have that aircraft inspected as prescribed in subpart Eofthis part and shall between required inspections, except as provided in paragraph (c)ofthis section, have discrepancies repaired as prescribed inpart 43ofthis chapter ...,"and others shall inspect or maintain the aircraft in compliance with Part 43. Given that these section and Part 43 apply only to aircraft with an airworthiness certificate, these sections will not apply tothe applicant. The operator pursuant tothe flight manual and operating handbook will accomplish maintenance. An equivalent level of safety will be achieved because these small UASs are very limited insize and will carry a small payload and operate only in restricted areas for limited periods of time. If mechanical issues arise the UAS can land immediately and will be operating from no higher than 400 feet AGL. As provided inthe Manual, the operator will ensure that the UAS isin working order prior to initiating flight, perform required maintenance, and keepalogofany maintenance performed. Moreover, the operator isthe person most familiar with the aircraft and best suited to maintain the aircraft inan airworthy condition to provide the equivalent level of safety. Pursuant to14 C.P.R. Part 11,the following summary is provided for publication inthe Federal Register, should itbe determined that publication is needed: Applicant seeks an exemption from the following rules: 14 C.P.R. §21, subpart H;14 C.F.R 45.23(b);14 C.P.R.§§ 61.113( a)& (b);91.7 (a); 91.9 (b) (2);91.103(b);91.109; 91.119; 91.121; 91.151(a);91.203(a) and (b); 91.405 (a); 91.407 (a) (1); 91.409 (a) (2); 91.409 (a)(2) and 91.417 (a)&(b)to operate commercially a small unmanned vehicle (55lbs or less). Approval of exemptions allowing commercial operations of sUASs, will enhance safety by reducing risk. Conventional operations, using jetor piston power aircraft, operate at extremely low altitudes just feet from the subjects being filmed andin extreme proximity to people and structures and

present the risks associated with vehicles that weigh inthe neighborhood of 4,000lbs, carrying large amounts ofjetAor other fuel. Such aircraft must flytoand from the operational location. In contrast, a sUAS weighing fewer than 55lbs. and powered by batteries eliminates virtually allofthat risk given the reduced mass and lack of combustible fuel carried on board. The sUAS is carried tothe operation site and not flown. The sUAS will carry no passengers or crew and, therefore, will not expose them tothe risks associated with manned aircraft flights. The operation of small UASs, weighting less than 55 lbs., conducted inthe strict conditions outlined above, will provide an equivalent level of safety supporting the grant ofthe exemptions requested herein, including exempting the applicant from the requirements of Part 21 and allowing commercial operations. These lightweight aircraft operate at slow speeds, close tothe ground, andina sterile environment and, asa result, arefar safer than conventional operations conducted with turbine helicopters operating in close proximity tothe ground and people. Page 8of9Privacy All flights will occur over private or controlled access property with the property owner's prior consent and knowledge. Filming will beof people who have also consented to being filmed or otherwise have agreed tobeinthe area where filming will take place. The grant ofthis exemption request will provide improved safety in both day and night operations. Satisfaction ofthe criteria provided in Section 333 ofthe Reform Act of2012 -size, weight, speed, operating capabilities, proximity to airports and populated areas and operation within visual line of sight and national security - provide more than

adequate justification forthe grant ofthe requested exemptions allowing commercial operation of applicant's UAS. Itisof note that certain public safety operations may involve advanced monitoring technology such as Infrared Red, Night Vision, etc. These specific operations will be governed pursuant toall applicable Local, State, and Federal laws regarding search and seizure including court approval of said operations via search warrant. Conclusion Asset forth herein, G2 Aerial, Inc. seeks an exemption pursuant to14C.F.R 11.61 and Section 333 ofthe FAA Modernization and Reform Act of2012 (FMRA), which will permit safe operation ofthe DJIS 1000, Align 690L Hexacopter, Align 800 Trekker, and DZYNE Technologies, Inc. Atlas-8 commercially, without an airworthiness certificate, forthe limited purpose of conducting the aforementioned on-demand commercial sUAS operations that include: • Filmmaking, Cinematography, and Videography • Precision Agriculture • Wildlife and Forestry Monitoring • Aerial Surveying • Inspection, Patrolling, and Monitoring • Security and Surveillance By granting this Petition, the FAA Administrator will be fulfilling the Congressional mandate of the FAA Modernization and Reform Act of 2012, while also advancing the interests ofthe public, by allowing G2 Aerial, Inc.to safely, efficiently, and economically operate sUASs commercially within the NAS. WHEREFORE, in accordance with the Federal Aviation Regulations and the FAA Modernization and Reform Act of2012, section 333, G2 Aerial, Inc. respectfully requests that the Administrator grant this Petition foran exemption from the requirements of14 C.F.R Sections 45.23(b); Part 21; 61.113(a) &(b), 91.7(a); 91.9(b); 91.103(b); 91.109; 91.119; 91.121; 91.151(a); 91.203(a); 91.405(a), 91.407(a)(l); 91.409(a)(1) & (a)(2), and 91.417(a) &(b). Respectfully Submitted,**w~0**Gary Kaplan G2 Aerial, Inc. 3529 Cay Drive Carlsbad, Ca. 92010 Ph: 858-353-5322Email: Sales@G2Aerial.com Page 9of9