1001 Pennsylvania Avenue, NW, Washington, DC 20004

- 2595  p202 624

- 2500  f202 628

- 5116

Marc L. Warren

(202) 624

- 2531

mwarren@crowell.com

June 30 , 2015

VIA FDMS

Ms. Cheryl Collins

Program Manager, Docket Operations

Docket Management Facility

U.S. Department of Transportation

1200 New Jersey Avenue, SE

West Building Ground Floor, Room W12

- 140

Attn: FAA Dockets

Washington, DC 20590

Re: Airware

– Petition for Exemption

Dear Ms. Collins :

Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 (“FMRA”) 1

and 14 C.F.R. Part 11, Unmanned Innovation

, Inc. d/b/a Airware (“ Airware ”)

, petitions for an

exemption from the Federal Aviation Regulations identified herein to authorize Airware to

operate small unmanned air craft systems (“sUAS”) for aerial data collection

, market surveys

and demonstrations

. 2 Airware ’ s sUAS o perations will be conducted under the safeguards

described in this petition and as may be further established by FAA.

FAA has now issued over 664 Section 333 exemptions to various commercial enterprises

for sUAS applications ranging from aerial photography and cinematography to precision

agriculture and flare stack, bridge and tower inspections. 3 Indeed, FAA has granted dozens of

Section 333 exemp tion s for aerial data collection

, market surveys and demonstrations in

circumstances that are similar in all material respects to those propose d here. 4 In issuing those

1 Pub. L. No. 112

- 95, § 333, 126 Stat. 76.

2 In addition to the information that is provided in this petition, Airware’s exemption request is

based on the user manuals for Airware’s sUAS and the Airware Regulatory Reference Guide (collectively, the

“Manuals”)

, and details on Airware’ s sUAS, which are being submitted to FAA under separate cover

. Airware is

submit ting the Manual s and the information on its sUAS in a separate, confiden tial filing pursuant to 14 C.F.R. §

11.35(b), as they con sist of confidential commercial and proprietary / trade secret information that Airware does

not make publicly available

. See also 5 U.S.C. § 552 (b)(4)

.

3 See FAA, Authorizations Granted Via Section 333 Exemptions (rev. Jun. 30 , 2015),

https://www.faa.gov/uas/legislative_programs/section_333/333_authorizations/

.

4 See, e.g., In the Matter of the Petition of Raven Aerial Imaging , Grant of Exemption No. 11862

( Jun

. 23 , 201 5 ), Docket No. FAA

- 2015

- 0891 (“Exemption No. 11862”) ; In the Matter of the Petition of RX AG

Services, LLC, Grant of Exemption No. 11882 ( Jun

. 23 , 2015), Docke t No. FAA

- 2015

- 1243 (“Exemption No. 11882”);

and In the Matter of the Petition of AgWorx, Inc.

, Grant of Exemption No. 11551 ( May 1 2, 2015), Docket No. FAA

2015

- 0435 (“Exemption No. 11551”)

.FAA Dockets

June 30 , 2015

Page 2

exemption s and other S ection 333 g rants

, FAA found that “the enhanced safety achieved using

an unmanned aircraft (UA) with the specificati ons described by the petitioner

... gives the FAA

good cause to find that the UAS operation enabled by this exemption is in the public interest

. ” 5

The same public interest and safety justifica tions apply to Airware ’s petition, and should enable

FAA to grant it on an expedited basis.

I. Petitioner

Founded in 2011

, Airware provides autopilot systems that act as development platforms

for micro to mid

- size fixed

- wing, helicopter, multiple

- rotor, and custom configuration s UAS.

Airware offers a common operating system that enables businesses to safely operate

commercial s UAS, manage a variety of aircraf t and integrate aerial data into design,

engineering, asset management and decision workflows. With Airware’s Aerial Information

Platform and growing ecosystem of global partners and service providers, businesses can put

s UAS to work for any application, including but not limited to infrastructure inspection, damage

assessment, environmental monitoring, search and rescue, land management, public safety and

survey and mapping.

All communications regarding Airware ’s petition should be directed to:

Jesse Kallman

Director of Business Development

& Regulatory Affairs

Airware

1045 Bryant St., Ste. 300

San Francisco, CA 94103

jkallman@airware.com w ith a copy to: Marc L. Warren

Crowell & Moring LLP

1001 Pennsylvania Ave NW

Washington, DC 20004

mwarren@crowell.com

II. Section 333

Airware ’s petition is consistent with Congress’ s goal set forth in Section 333 of the

FMRA, which directs the Secretary of Transportation to consider whether certain UAS may

operate safely in the national airspace system ( “ NAS ” ) before completion of the rulemaking s

required under Section 332 of th at legislation

. In making this determination, the Secretary is

required to deter mine which types of UAS do not create a hazard to users of the NAS or the

public or pose a threat to national security in light of the following: (1 ) t he UAS’ size, weight,

speed, and operational capability; (2 ) o peration of the UAS in close proximity to airports and

populated areas; and (3 ) o peration of the UAS within visual line of sight of the operator. 6 To

implement Section 333, FAA has the authority to issue exemptions from its safety regulations

5 See, e.g., Exemption No. 11862 at 2; Exemption No. 11882 at 2; and Exemption No. 11551 at 2.

6 FMRA § 333(a).FAA Dockets

June 30 , 2015

Page 3

and minimum standards when the Administrator decides a requested exemption is in the public

interest. 7

Airware ’ s proposed s UAS operations meet the requirements of, and qualify for

expedited approval under, Section 333. Airware ’ s sUAS weigh less than 55 pound s , will operate

at less than 400 feet above ground level ( “ AGL ” )

, within visual line of sight ( “ VLOS ” )

, at speeds

of no more than 87 knots, and will generally comply with the same conditions and limitations

FAA established in issuing previous Section 333 g rants

. 8 Operations conducted under these

safeguards will provide at least an equivalent level of safety compared to the current regulatory

structure. Moreover, Airware ’ s operations will not “create a hazard to users of the national

airspace system or the public or pose a threat to na tional security” due to the size of the sUAS

and the restricted areas in which it will operate. 9

III. Regulations from Which an Exemption is Requested

Airware requests an exemption from the following regulations to the extent necessary

for Airware to conduct the operations described in this petition :

 14 C.F.R. § § 61.23(a) and (c)

 14 C.F.R. §§ 61.101(e)(4) and (5)

 14 C

. F

. R

. § 61.113(a)

 14 C

. F

. R

. § 61. 315 (a)

 14 C.F.R. § 91. 7(a)

 14 C.F.R. § 91.119 (c)

 14 C.F.R. § 91.121

 14 C

. F

. R . § 91.151(a) (1)

 14 C

. F

. R . § 91.405(a)

 14 C

. F

. R . § 91. 407(a)(1)

 14 C

. F

. R . §§ 91. 409(a) (1) and (2)

 14 C

. F

. R . §§ 91. 417(a) and (b)

The following subsections describe Airware ’s request for an exemption from each of

these regulations and demonstrate how Airware ’ s operations will provide for at least an

equivalent level of safety compared to the current regulatory structure that applies to manned

aircraft

.

7 See 49 U.S.C. § 106(f) and 49 U.S.C. § 44701(f).

8 See supra note 3

.

9 See, e.g., In the Matter of the Petition of Astraeus Aerial , Grant of Exemption No. 11062 (Sep. 25,

2014), Docket No. FAA

- 2014

- 0352 (“Exemption No. 11062”) at 8 ( citing FMRA § 333(b)).FAA Dockets

June 30 , 2015

Page 4

A. 14 C.F.R. §§ 61.23(a) and (c)

– Medical certificates: Requirement and

duration

Sections 61.23(a) and (c) generally require pilots of manned aircraft to hold a FAA

medical certificate in ord er to exercise pilot privileges

. As of March 24, 2015, however, FAA

determined as a matter of policy that operators hold ing a valid driver’s license in lieu of a third

cla ss medical certificate may conduct commercial sUAS operations under a Section 333 grant

. 10

Accordingly, Airware requests an exemption from these provisions to the extent necessary to

give Airware the same relief from medical certificate requirements that FAA has afforded to

hundreds of other operators pursuant to Section 333

. 11

B. 14 C.F.R. §§ 61.101(e)(4) and (5) ; 61.113(a); and 61.315(a)

– P ilot P rivileges

and L imitations

Section 61.113(a) limits private pilots to conducting non

- commercial operations.

Similarly, Sections 61.101(e)(4) and (5) prohibit a recreational pilot from ac ting as pilot in

command of an aircraft for compensation or hire or in furtherance of a business. Section

61.315(a) aut horizes a sport pilot certificate holder to act as pilot in com m and of a light

- sport

aircraft, subject to certain restrictions specified in Section 61.315(c), including a prohibition on

doing so for compensation or hire or in furtherance of a business, amo ng other restrictions.

FAA has already determined

, however, that a private

, recreational or sport pilot certificate is

sufficient to conduct commercial sUAS flights in a wide variety of operational environment s

. 12

Since Airware will be conducting its sUAS operations for compensation in further ance of its

business

, Airware requests an exemption from these provisions to the extent necessary.

Airware notes that FAA has provide d such relief to hundreds of other Section 333 operators. 13

Consistent with the operating conditions and limitations specified in similar Section 333

g rants, 14 Airware will utilize only pilots holding a FAA airline transport, commercial, private,

recreational, or sport pilot certificate and at least a valid U.S. driver’s license . The sUAS will be

operated with in VLOS of the pilot

- in

- command (“ PIC ”) at all times , and all operations will utilize

a visual observer ( “ VO ” ) , who will be able to communicate verbally with the PIC at all times

during the operation. And b ecause the area of operation will be controlled and restricted in

accordance with the safeguards contained in the Manual s and the FAA

- approved conditions

and limitations described in Section VI, infra , permitting the sUAS operations as requested

would provide for the level of safety otherwise achieved through these Part 61 provisions

.

10 See, e.g., In the Matter of the Petition of EnviroMINE, Inc. , Grant of Exemption No. 11227 (Mar.

24, 2015), Docket No. FAA

- 2014

- 0678 at 4 , 8; see also FAA, FAA Summary Grants Speed UAS Exemptions (Apr. 9,

2015), https://www.faa.gov/news/updates/?newsId=82485

.

11 See supra note 3

.

12 Id.

13 Id

.

14 See, e.g

. , Exemption Nos. 11862, 11882, and 11551

.FAA Dockets

June 30 , 2015

Page 5

Accordingly, grant of the requested exemption, subject to the conditions and limitations

specified herein, would not adversely affect the safety of the NAS.

C. 14 C.F.R. § 91.7(a)

– Civil aircraft airworthiness

Section 91.7(a) prohibits any person from operating a civil aircraft unless it is in an

airworthy condition. FAA has stated that no exemption is required for 14 C.F.R. § 91.7(a) to the

extent that the airworthiness certificate requirements of Part 21 15 are waived or inapplicable.

Such airworthiness certificate requirements are inapplicable here, i nsofar as Airware ’ s sUAS

provide s for an equivalent level of safety when compared to manned aircraft, consis tent with

the relevant language of the FMRA and the precedent FAA has established under Section 333

. 16

D. 14 C.F.R. § 91.119 (c)

– Min imum Safe Altitudes

Section 91.119 establishes safe altitudes for operation of civil aircraft. Specifically,

Section 91.119(c) provides that except when necessary for takeoff or landing, no person may

operate an aircraft below an altitude of 500 feet above the surface except over open water or

sparsely populated areas and that in such cases, the aircraft may not be operated closer than

500 feet to any person, vessel, vehicle or structure. As detailed in previous Section 333 g rants

, however, FAA has determined that adherence to certain safety measures is sufficient to

warrant an exemption from Section 91.119(c) for sUAS operations

. 17 Consistent with the relief

provided to other sUAS operators under Section 333

, Airware requests an exemption to the

extent necessary to permit Airware to operate below an altitude of 500 feet AGL and closer

than 500 feet to any person, vessel or structure. An equivalent level of safety will be achieved

given the size, weight and speed of Airware ’ s sUAS, as well as the location s where it will be

operated ( i.e., nowhere near other aircraft)

. In addition, c onsistent with t he flexibility that FAA

has already provided to other Section 333 operators for aerial data collection

, market surveys

and demonstrations

, 18 Airware requests permission to operate a minimum distance of 200 feet

from any non

- participating persons so long as sufficient barriers exist to protect such persons

from debris in the event of an accident. 19

15 FAA has concluded that no exemption from Part 21, Subpart H (Airworthiness Certificates) is

needed if the agency makes a finding under the FMRA that the UAS selected provides an equivalent level of safety

when compared to aircra ft normally used for the same application. As t hese criteria are met here, no exemption is

needed. See

, e.g., Exemption No. 11062 at 13

- 14, 22. But to the extent FAA determines that there are some

characteristics of Airware ’s sUAS that may not meet this standard , an exemption is requested.

16 See, e.g., id.

17 See, e.g., supra note 3

.

18 See supra note 4

.

19 See In the Matter of the Petition of Team 5, LLC , Grant of Exemption No. 11158 (Jan. 29, 2015),

Docket No. FAA

- 2014

- 0783, at 16

- 17; In the Matter of the Petition of Picture Factory, Inc. , Grant of Exemption No.

11178 (Feb. 18, 2015), Docket No. FAA

- 2014

- 0794, at 23; In the Matter of the Petition of Shot over Camera Systems,

L.P. , Grant of Exemption No. 11159 (Jan. 30, 2015), Docket No. FAA

- 2014

- 0784, at 12; see also FAA Order 8900.1,

Vol. 3, Ch. 8, Sec. 1 (allowing certain relief from 14 C.F.R. § 119(c) in the filming context, including the 200 ft.

minimu m distance standard requested herein).FAA Dockets

June 30 , 2015

Page 6

E. 14 C.F.R. § 91.121

– Alti meter Settings

Section 91.121 requires each person operating an aircraft to maintain cruising altitude

by reference to an altimeter that is set “to the elevation of the departure airport or an

appropriate altimeter setti ng available before departure

. ” Since Airware ’ s sUAS will not be

equipped with a typical barometric altimeter, Airware requests relief from this provision

consistent with the relief that FAA has already granted to other sUAS operators flying at

similarly low altitudes. 20 Airware will operate the sUAS wi thin VLOS at or below 400 feet AGL

and provide altitude information to the PIC via a digitally encoded telemetric data feed that

downlinks from the aircraft to a ground

- based on

- screen display. The altitude information will

be generated by equipment insta lled on the sUAS, and prior to each flight a zero altitude

initiation point will be established and confirmed for accuracy by the PIC.

F. 14 C.F.R. § 91.151(a)

– Fuel Requirements for Flight in VFR Conditions

Section 91.151(a) prohibits an individual f rom beginning “a flight in an airplane under

VFR conditions unless (considering wind and forecast weather conditions) there is enough fuel

to fly to the first point of intended landing, and, assuming normal cruising speed

– (1) During

the day, to fly after that for at least 30 minutes; or (2) At night, to fly after that for at least 45

minutes.” But provided certain operational parameters are established, FAA has found that

good cause exists for granting exemptions from this provision for operations in a m ultitude of

contexts

. 21

Airware will be operating a less than 55

- pound sUAS in tightly

- controlled en vironment s

at speeds below 87 knots and within VLOS. Combined with the fact that Airware will not

conduct operations unless a sUAS has enough available power for the intended mission

, and

will not continue unless there is at least five minutes of power remaining

, relief from Section

91.151(a) is warranted

, in accordance with the conditions and limitations specified in Section

VI, infra

.

G. 14 C.F.R. §§ 91.405(a); 91.407(a)(1); 91.409(a)(1) and (2); and 91.417(a) and

(b): Maintenance Inspections

These provisions require that an aircraft operator or owner “shall have that aircraft

inspected as prescribed in subpart E of this part and shall b etween required inspections, except

as provided in paragraph (c) of this section, have discrepancies repaired as prescribed in part 43

of this chapter.

. .,” and that other persons shall inspect or maintain the aircraft in compliance

with Part 43. Under S ection 333

, however, FAA has established safety measures for certain

sUAS operations sufficient to warrant an exemption from these provisions. 22

20 See supra note 3.

21 Id.

22 Id

.FAA Dockets

June 30 , 2015

Page 7

Airware will strictly adhere to the maintenance

- and inspection

- related requirements

set forth in its Manual s

, which are consistent with applicable conditions and limitations

described in Section VI, infra

.

IV. Unmanned Aircraft System

Airware will operate a battery

- powered sUAS weighing less than 55 pounds that will be

flown in acc ordance with strict operating safeguards as more fully described in Section VI, infra

,

as well as those described in the Manual s

. T he sUAS will operate at a speed of no more than 87

knots and have the capability to hover, and move in the vertical and horizontal plane

simultaneously.

Airware will incorporate the Airware flight control system into its sUAS. Airware’s

systems are commercial grade, engineered to enable safe and relia ble commercial UAS

applications and have been built from the ground up by leading aerospace engineers consistent

with industry best practices. The system safety features of Airware ’ s sUAS include geofencing,

a full suite of contingency management function s, user and flight plan management and

approval functionality, and many more

. These and other features will ensure the safety of

persons and property within and surrounding the limited operating area. In the event the sUAS

lose s communications or its GPS signal, it will have the capability to return to a pre

- determined

location and land. The sUAS will also have the capability to abort a flight in the event of

unpredicted obstacles or emergencies. A comprehensive description of Airware ’ s sUAS and its

specifications and capabilities is contained in the Manual s

.

As FAA has recognized, the limited weight of less than 55

- pound sUAS significantly

reduces the potential for harm to participating and nonparticipating individuals or property in

the event of an accident or incident, and the risk to an onboard pilot and crew is eliminated

with the use of sUAS. 23

In addition, prior to each flight, the PIC will conduct a pre

- flight inspection of the sUAS,

and maintenance will be performed to address any conditio n potentially affecting safe

operations. All maintenance and alterations will be documented in the aircraft records. The

safety guidelines specified in the Manuals address the following key areas : ( 1 ) individual parts

( e.g., remote controller, compass, parameter settings, battery, storage and transportation,

maintenance and upkeep, etc.); (2) flight environment requirements ; ( 3 ) flight warnings ( e.g.,

failsafe and return to home, low battery, vision positioning system, transf ormation function,

etc.) ; (4 ) pre

- flight checklist ; and (5 ) maintenance checks concerning the battery,

transformation sy stem, motors

, and vision positioning system.

23 See supra note 3

.FAA Dockets

June 30 , 2015

Page 8

V. Unmanned Aircraft PIC

As described above

, the PIC will be a FAA licensed airman with either an airline

transport, commercial, private, recreational, or sport pilot certificate, that holds a current FAA

airman medical certificate or a valid U.S. driver’s license

. The PIC will also meet the flight

review requirements specified in Section 61 .56 in an aircraft in which the PIC is rated on his or

her pilot certificate. And, p rior to conducting commercial operations under this exemption, t he

PIC will have accumulated and logged sufficient UAS

- specific flight experience

, including at least

12 ho urs on its sUAS before being designated to operate it commercially.

In addition, the PIC and the VO will have successfully com pleted a qualification process

and a sUAS flight demonstration administered by a n Airware

- approved and

- qualified pilot.

VI. Operation of the Unmanned Aircraft

Airware will conduct all flights under the requested exemption subject to the following

conditions and limitations, and as further detailed in the Manual s : 24

A. The sUAS will weigh less than 55 pounds (25 kilograms ), including payload

.

B. The s UA S will not be flown at a ground speed exceeding 87 knots ( i.e. 100 miles per

hour)

.

C. Flights will be operated at an altitude of no more than 400 feet AGL. All altitudes

reported to ATC will be in feet AGL

.

D. The s UA S will be o perated within VLOS of the PIC and/or VO at all times.

E. All operations will utilize a VO , who may be used to satisfy the VLOS requirement as long

as the PIC always maintains VLOS capability. The VO and PIC will be able to

communicate verbally at all times.

F. The grant of exemption and Manual s will be accessible during Airware ’ s sUAS

operations and made available to FAA upon request. If a discrepancy exists between

the conditions and limitations in the grant of e xemption and the procedures outlined in

the Manual s , the conditions and limitations in the exemption take precedence and will

be followed.

G. Prior to each operation, the PIC will inspect the s UAS to ensure it is in a condition for

safe flight. If the insp ection reveals a condition that affects the safe operation of the

24 The conditions and limitations detailed in this section are consistent with those set forth in the

previous FAA Section 333 grants for operations similar to those Airware seeks to conduct through this petition

. See, e.g

., supra note 4

.FAA Dockets

June 30 , 2015

Page 9

s UAS, it will not be operated until the necessary maintenance has been performed and

the s UAS is found to be in a condition for safe flight. The ground control station will also

be included in the preflight inspection. All maintenance and alterations will be

documented in the sUAS records.

H. Any s UAS that has undergone maintenance or alterations that affect its operation or

flight characteristics ( e.g

. , replacement of a flight critical component ) will undergo a

functional test flight prior to resumption of operations

. The PIC who conducts the

functional test flight will make an entry in the s UAS aircraft records of the flight.

I. Airware will follow the manufacturer’s s UAS aircraft/component, maintenance,

overhaul, replacement, inspection, and life limit requirements.

J. The PIC will possess either an airline transport, commercial, private, recreational, or

sport pilot certificate, and a current FAA airman medical certificate or a valid U.S.

driver’s license. The PIC will undergo at least 12 hours of training to ensure that he or

she can fol low these procedures. The PIC will also meet the flight review requirements

specified in Section 61.56 in an aircraft in which the PIC is rated on his or her pilot

certificate.

K. Prior to conducting commercial operations under this exemption:

1. T he PIC will have accumulated and logged, in a manner consistent with Section

61.51(b)

, a minimum of : 12 hours of flying Airware’s sUAS or 24 flights accrued

bef ore being designated to operate it for commercial aerial data collection

, market surveys and demonstrat ions

. During training, proficiency, and

experience

- building flights, the PIC will operate the s UA S with appropriate

distance from nonparticipants in accordance with Section 91.119.

2. A flight demonstration, administered by a Airware

- approved and

- qualified

pilot

, will be successfully completed and documented. This documentation will

be available for review upon request by FAA

.

L. The s UA S will be operated at least 500 feet from all nonparticipating persons, vessels,

vehicles, or structures unless both of t he following conditions are met :

1. Barriers or structures are present that sufficiently protect nonparticipating

persons in the event of an accident; and

2. The owner/controller of any vessels, vehicles or structures has granted

permission for operating closer to those objects and the PIC has made a safety

assessment of the risk of operating closer to those objects and determined that

it does not present an undue hazard.FAA Dockets

June 30 , 2015

Page 10

M. If the s UAS loses communications or loses its GPS signal, it will return to a

predetermined location within the security perimeter and land or be recovered in

accordance with the Manual s

.

N. The s UAS will abort the flight in the event of unpredicted obstacles or emergencies in

accordance with the Manual s

.

O. The sUAS will n ot be operated unless it has enough available power to conduct the

intended operation and to operate after that for at least five minutes, or with the

reserve power recommended by the manufacturer, whichever is greater.

P. Airware will obtain an Air Traffi c Organization ( “ ATO ” ) issued Certificate of Waiver or

Authorization ( “ COA ” ) prior to conducting any operations above 200 f ee t AGL under the

exemption. 25

Q. All sUAS operated in accordance with this exemption will be identified by serial number,

registered in accordance with 14 C

. F

. R

. P art 47, and have identification (N

- Number)

markings in accordance with 14 C

. F

. R

. P art 45, Subpart C. Markings will be as large as

practicable.

R. Airware will follow the procedures established in the Manuals for documenting and

maintaining records of the s UAS maintenance, preventative maintenance, alterations,

status of replacement/overhaul component parts, and the total time in service of the

s UAS

.

S. Each s UAS operated under this exemption will comply with all manufacturer Sa fety

Bulletins.

T. The preflight inspection section described in the Manual s will account for all

discrepancies ( i.e

. , inoperable components, items, or equipment )

.

U. Airware ’ s use of radio frequency spectrum for operation and control of the s UA S will

comply with the Federal Communications Commission ( “ FCC ” ) or other appropriate

government oversight agency requirements.

25 Pursuant to its “blanket” COA, FAA will automatically grant a COA for flights at or below 200 feet

to any UAS operator with a Section 333 exemption for aircraft that weigh less than 55 pounds, operate during

daytime VFR conditions, operate within VLOS, and stay certain prescribed distances away from airports or

heliports. See FAA, FAA Streamlines UAS COAs for Section 333 (rev. Mar. 24, 2015),

https://www.faa.gov/news/updates/?newsId=82245 . Thi s blanket COA allows flights anywhere in the country

except restricted airspace and certain other prohibited areas

, and FAA automatically issues it at the time the

exemption is approved. Id

. T o the extent Airware plans to operate its sUAS above 200 ft. A GL, it will apply for a

COA authorizing it to do so.FAA Dockets

June 30 , 2015

Page 11

V. The documents required under Sections 91.9 and 91.203 will be available to the PIC at

the ground control station of the s UAS any ti me the aircraft are operating. These

documents will be made available to FAA or any law enforcement official upon request.

W. The s UA S will remain clear and yield the right of way to all other manned operations and

activities at all times (including, but no t limited to, ultralight vehicles, parachute

activities, parasailing activities, hang gliders, etc.).

X. s UAS operations will not be conducted during night, as defined in Section 1.1. All

operations will be conducted under visual meteorological conditions ( “ VMC ” ). Flights

under special visual flight rules ( “ SVFR ” ) are not authorized.

Y. The s UAS will not be operated by the PIC from any moving device or vehicle.

Z. The s UA S will not be operated less than 500 feet below or less than 2,000 feet

horizontally from a cloud or when visibility is less than three statute miles from the PIC.

AA. The s UA S will not be operate d within five nautical miles of an airport reference point

( “ ARP ” ) as denoted in the current FAA Airport/Facility Directory ( “ AFD ” ) or for airports

not denot ed with an ARP, the center of the airport symbol as denoted on the current

FAA

- published aeronautical chart

, unless a letter of agreement with that airport’s

management is obtained or otherwise permitted by a COA issued to Airware

. The letter

of agreement with the airport management will be made available to FAA and any law

enforcement official upon request.

BB. Any incident, accident, or flight operation that transgresses the lateral or vertical

boundaries of the operational area as defined by the applicable COA will be reported to

FAA’s UAS Integration Office (AFS

- 80) within 24 hours and the National Transportation

Safety Board ( “ NTSB ” ) , as applicable

.

VII. Public Interest

Authorizing Airware to use sUAS for aerial data collection

, market surveys and

demonstrations under the conditions specified herein w ill bring immediate and significant

safety improvement in various commercial industries and for Airware ’s myriad customers. In

particular, Airware ’s sUAS operations will:

 Improve the safety of operations of their enterprise customers around the country by

providing examples of safe flight operations conducted in accordance with the Manual s

.

 Improve the safety of preflight inspections and the integration of Airware hardware

onto sUAS , and demonstrate how the Air ware system can safely respond to a wide

number of issues during flight.