### Peter	Spero 

## -	C:	+1	847.902.9590	- Peter@AeroVistaInnovations.com

August	22,	2015

U.	S.	Department	of	Transportation

Docket	Management	System

1200	New	Jersey	Ave.,	SE

Washington,	D C	20590

Re:	Exemption	Request	Section	333	of	the	FAA	Reform	Act	and	Part	11	of	the	Federal

Aviation	Regulations	from	14	C.F.R.	45.23(b);	14	C.F.R.	Part	21;	14	C.F.R.	Part	61.113(a)	&

(b);	91.7	(a);	91.9	(b)	(2);	91.103	( b );	91.109;	91.119;	91.121;	91.15 1	( a );	91. 2 03	(a)	&	(b);

91.405	(a);	91.407	(a)	(1);	91.409	(a)	(2);	91.417	(a)	&	(b).

Dear	Sir	or	Madam,

Pursuant	to	Section	333	of	the	FAA	Modernization	and	Reform	Act	of	2012	(the	Reform	Act)

and	14	C.F.R.	Part	11, AeroVista	Innovations ,	operators of	Small	Unmanned	Aircraft	SYSTEMS

(“sUASs”)	equipped	to	conduct	aerial	photography	and	cinematography	for	commercial	and

reside n tial	real	estate	and	closed

- --set	special	events,	hereby	applies	for	an	exemption	from

the	listed	Federal	Aviation	Regulations (“FARs”)	to	allow	commercial	operation	of	its	sUASs,

so	long	as	such	operations	are	conducted	within	and	under	the	conditions	outlined	herein	or

as	may	be	established	by	the	FAA	as	requires	by	Section	333.

As	described	more	fully	below,	the	request	exe mption	would	permit	the	operation	of	small,

unmanned,	and	redundant	sUAS	under	controlled	conditions	in	airspace	that	is	1)	limited	2)

predetermined	3)	controlled	as	to	access	and	4)	would	provide	safe	operations	and

affordability	to	the	existing	real	est ate	and	close d

- --set	special	event	industries	currently

using	conventional	aircraft.	Approval	of	this	exemption	would	thereby	enhance	safety,

promote	industry	growth	and	fair	competition	through	affordability	of	aerial	photography

and	cinematography	and	fu lfill	the	Secretary	of	Transportation’s	(the	FAA	Administrator’s)

responsibilities	to	“...	establish	requirements	for	the	safe	operation	of	such	aircraft	systems

in	the	national	airspace	system.”	Section	333	of	the	Reform	Act.

The	name	and	address	of	th e	applicant	is:

AeroVista	Innovations,	LLC

Attn: Peter	Spero (Licensed	Pilot	and	co

- owner	of	Aero V ista	Innovations,	LLC )

Ph: 847.902.9590

Email:	Peter@AeroVistaInnovations.com

Address: 1344	Su nnyside	Ave.,	Highland	Park,	IL	60035

## Peter	Spero

– Cell:847.902.9590

– Peter@AeroVistaInnovations.com

Regulations	from	which	the	exemption	is	requested:

14	C.F.R.	Part	21

14	C.F.R.	45.23	(b)

14	C.F.R.	61.3

14	C.F.R.	91.7	(a)

14	C.F.R.	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

1 4	C.F.R.	91.151	(a)

14	C.F.R.	91.203	(a)	&	(b)

14	CFR	§	91.205(b)

14	CFR	§	91.215

14	C.F.R.	91.405	(a)

14	C.F.R.	407	(a)	(1)

14	C.F.R.	409	(a)	(2)

14	C.F.R.	417	(a)	&	(b)

This	exemption	application	is	expressly	submitted	to	fulfill	Congress’	goal	in	passi ng	Section

333(a)	through	(c)	of	the	Reform	Act.	This	law	directs	the	Secretary	of	Transportation	to

consider	whether	cert a in	unmanned	aircraft	systems	may	operate	safely	in	the	national

airspace	system	(NAS)	before	completion	of	the	rule	making	required	u nder	Section	332	of

the	Reform	Act.	In	making	this	determination,	the	Secretary	is	required	to	determine	which

types	of	UASs	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:

•	The	UAS ’s	size,	weight,	speed	and	operational capability;

•	Operation	of	the	UAS	in	close	proximity	to	airports	and	populated areas;	and

•	Operation	of	the	UAS	within	visual	line	of	sight	of	the	operator.

Reform	Act § 333	(a).	Lastly,	id	the	Secretary	determines that	such	vehicles	“may	operate

safely	in	the	national	airspace	system,	the	Secretary	shall	establish	requirements	for	the	safe

operation	of	such	aircraft	in	the	national	airspace	system.”	Id.	§333(c).

The	Federal	Aviation	Act	expressly	grants	the	FAA	th e	authority	to	issue	exemptions.	This

statutory	authority	by	its	terms	includes	exempting	civil	aircraft,	as	the	term	is	defined

under	§40101	of	the	Act,	that	includes	sUASs,	from	the	requirement	that	all	civil	aircraft

must	have	a	current	airworthiness	ce rtificate.

The	Administrator	may	grant	an	exemption	from	a	requirement	of	a	regulation	prescribed

under	subsection	(a)	or	(b)	of	 this	section	or	any	sections	44702

- --	44716	of	 this	 title	if

the	Administrator	finds	the	exemption	in	the	public	interest.	49	U.S.C.	§44701(f)	See	also

49	USC	§44711(a);	49	USC	§44704;	14	CFR	§91.203	(a)	(1).

Flight	Vehicle:

## Peter	Spero

– Cell:847.902.9590

– Peter@AeroVistaInnovations.com

AeroVista	Innovations proposes	to	use	two	sUASs;	1)	DJI	Insp ire	1 & 2) 3D	Robotics	Solo

. Both	of	these	aircrafts	has	four	rotors	and	four	motors	in	a	quadcopter	configuration	(X4).

Both	sUASs	weigh	less	than	55	lbs.	including	payload.	They	operate,	under	normal	conditions

at	a	speed	of	no	more	than	50	knots	and	hav e	the	capability	to	hover,	and	move	in	the	vertical

and	horizontal	plane	simultaneously.	Both	sUASs	are	equipped	with	GPS	and	auto

- --return

function	to	the	predetermined	safe	landing	area	as	well	as	allowing	reading	of	magnetic

interference	that	can	cau se loss	off	GPS	signal.	The s UASs	will	operate	only	in	line	of	sight	and

will	operate	only	within	a	sterile	close d

- --set	area	of	a	reside n tial	or	commercial	listing	or	a

closed

- --set	special	event.	Such	operations	will	insure	that	the	sUASs	will	“not	create	a hazard

to	users	of	the	national	airspace	system	or	the	public.”	(Reform	Act	Section	333	(b)).

Given	the	small	size	of	the	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	of	UASs	to	commence immediately.	Also due	to	the	size	of	the	UASs

and	the	restricted	areas	in	which	the	relevant	sUASs	will operate,	approval	of	the

application	presents	no	national	security	issue.	Given	the	clear	direction	in	Section	333	of

the	Reform	Act,	the	authority	contained	in	the	Federal	Aviation	Act,	as	amended;	the	strong

equivalent	level	of	safety	surrounding	the	pro posed	operations,	and	the	significant	public

benefit,	including	enhanced	safety,	reduction	in	environmental	impacts,	including	reduced

emissions	associated	with	allowing	UASs	for	movie	and	television	operations,	the	grant	of

the	requested	exemptions	is	in the	public	interest.	Accordingly,	the	applicant	respectfully

requests	that	the	FAA	grant	the	requested	exemption	without	delay.

AIRCRAFT	AND	EQUIVALENT	LEVEL	OF	SAFETY

AeroVista	Innovations proposes	that	the	exemption	requested	herein	apply	to	civil	airc raft

that	have	the	characteristics	and	that	operate	with	the	limitations	listed	herein.	These

limitations	provide	for	at	least	an	equivalent	or	even	higher	level	of	safety	to	operations

under	the	current	regulatory	structure	because	the	proposed	operations represent	a	safety

enhancement	to	the	already	safe	aerial	photography	and	cinematography	filming	operations

conducted	with	conventional	aircraft.

These	limitations	and	conditions	to	which AeroVista	Innovations agrees	to	be	bound

when	conducting	commercia l	operations	under	an	FAA	issued	exemption	include:

ØØ The	sUAS	will	weigh	less	than	55	lbs.

ØØ Flights	will	be	operated	within	line	of	s i ght	of	a	pilot	and/or	observer.

ØØ Maximum	total	flight	time	for	each	operational	flight	will	be	30	minutes	or	less.

ØØ Flights	will	be	terminated	at	25%	battery	power	re serve	should	that	occur	prior	to

the	30	minute	limit.

ØØ Flights	will	be	operated	at	an	alt i tude	of	no	more	than	400	feet	AGL	or,	not	more	than

200	feet	above	an	elevated	platform	for	which	filming	is	planned.

ØØ Minimum	crew	for	each	operation	will	consis t	of	the	sUAS	Pilot,	the	Visual	Observer,

and	the	Camera	Operator.

ØØ sUAS	Pilot	will	also	meet	the	flight	review	requirements	specified	in	14	C.F.R	61.56	in

an	aircraft	in	which	the	Pilot	is	rated	on	his	or	her	pilot	certificate.

## Peter	Spero

– Cell:847.902.9590

– Peter@AeroVistaInnovations.com

ØØ The	sUAS	will	only operate	within	a	confined	sterile	closed

- --set	area	with	a	set

safety	perimeter,	the	boundaries	of	which	will	be	determined	by	production

personnel	and	the	sUAS	PIC	based	on	the	site

- --specific	filming	activities	and	speed

of	the	sUAS	required	for	the	oper ation,	and	coordinated	with	the	jurisdictional	FAA

FSDO	and	local	government	officials	as	applicable.

ØØ A	briefing	will	be	conducted	in	regards	to	the	planned	sUAS	operations	prior	to	each

day’s	production	activities.	It	will	be	mandatory	that	all	personn el	who	will	be

performing	duties	within	the	boundaries	of	the	safety	perimeter	be	present	for	this

briefing.

ØØ The	sUAS	Pilot	and/or	Aerial	Coordinator	will	ensure	this	safety	perimeter	that	only

consenting	production	personnel	will	be	allowed	within	100 feet	of	the	sUAS

operation	by	not	permitting	anyone	who	had	not	been	briefed	or	whom	is	not

involved	in	produ c tion	to	be	in	the	close d

- --set	area.

ØØ Observer	and	PIC	will	at	all	times	be	able	to	communicate	by	voice	and/or	two	way

radio	communication	syst em.

ØØ Written	and/or	oral	permission	from	the	relevant	property	holders	will	be	obtained.

ØØ If	applicable,	all	required	permissions	and	permits	will	be	obtained	from	territorial,

state,	county	or	city	jurisdictions,	including	local	law	enforcements,	fire ,	or	other

appropriate	governmental	agencies.

ØØ If	the	sUAS	loses	communications	or	loses	its	GPS	signal,	the	sUAS	will	have	the

capability	to	return	to	a	pre

- --determined	location	within	the	Security	Perimeter

and	land	safely.

ØØ The	sUAS	will	have	the	c apability	to	abort	flight	in	case	of	unpredicted	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	for

the	i ssuance	of	airworthiness	certificates	as	required	by	FAR	§91.203	(a)	(1).	Given	the	size

and	limited	operating	area	associated	with	the	aircraft	to	be	utilized	by	the	Applicant,	an

exemption	from	Part	21	Subpart	H	meets	the	requirements	of	an	equivalent	le vel	of	safety

under	Part	11	and	Section	333	of	the	Reform	Act. The	Federal	Aviation	Act	(49	U.S.C.§44701

(f))	and	Section	333	of	the	Reform	Act	both	authorize	the	FAA	to	exempt	aircraft	from	the

requirement	for	an	airworthiness	certificate,	upon	considerat ion	of	the	size,	weight,	speed,

operational	capability,	and	proximity	to	airports	and	populated	areas	of	the	particular	UAS.

In	all	cases,	an	analysis	of	these	criteria	demonstrates	that	the	UAS	operated	without	an

airworthiness	certificate,	in	the	restric ted	environment	and	under	the	conditions	proposed

will	be	at	least	as	safe,	or	safer,	than	a	conventional	aircraft	(fixed w ing	or	rotorcraft)

operating	with	an	airworthiness	certificate	without	the	restrictions	and	conditions

proposed.

14	C.F.R.	§	45.23	( b).	Marking	of	the	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	to	the	ca bin,	cockpit,	or	pilot	station,	in	letters	not	less	than	2	inches	nor	more	than

## Peter	Spero

– Cell:847.902.9590

– Peter@AeroVistaInnovations.com

6	inches	high,	the	words	"limited,"	"restricted,"	"light

- --sport,"	"experimental,"	or

"provisional,"	as	applicable.

Even	though	the	sUAS	will	have	no	airworthiness	certifica te,	an	exemption	may	be	needed

as	the	sUAS	will	have	no	entrance	to	the	cabin,	cockpit	or	pilot	station	on	which	the	word

“experimental”	can	be	placed.	Given	the	size	of	the	sUAS,	two	inch	lettering	will	be

impossible.	The	word	“Experimental”	will	be	place d	on	the	fuselage	in	compliance	with

§45.29	(f).

The	equivalent	level	of	safety	will	be	provided	by	having	the	sUAS	marked	on	its	fuselage	as

required	by	§45.92	(f)	where	the	pilot,	observer	and	others	working	with	the	sUAS	will	see

the	identification	of the	sUAS	as	“Experimental”.	The	FAA	has	issued	the	following

exemptions	to	this	regulation	to	Exemptions	Nos.	10700,	8738,	10167	and	10167A.

14	C.F.R.	§91.7(a):	Civil	aircraft	airworthiness.

The	regulation	requires	that	no	person	may	operate	a	civil	aircr aft	unless	it	is	in	airworthy

condition. As	there	will	be	no	airworthiness	certificate	issued	for	the	aircraft,	should	this

exemption	be	granted,	no	FAA	regulatory	standard	will	exist	for	determining	airworthiness.

Given	the	size	of	the	aircraft	and	the	re quirements	contained	in	the	Manual	for	maintenance

and	use	of	safety	check	lists	prior	to	each	flight,	as	set	forth	in	Sections	J,	L	and	Q,	an

equivalent	level	of	safety	will	be	provided.

14	C.F.R.	§	91.9	(b)	(2):	Civil	Aircraft	Flight	Manual	in	the	Aircr aft.

Section	91.9	(b)	(2)	provides:

No	person	may	operate	a	U.S.

- --registered	civil	aircraft	...

The	sUAS,	given	its	size	and	configuration	has	no	ability	or	place	to	carry	such	a	flight

manual	on	the	aircraft,	not	only	because	there	is	no	pilot	on	board,	but	because	there	is	no

room	or	capa city	to	carry	such	an	item	on	the	aircraft. The	equivalent	level	of	safety	will	be

maintained	by	keeping	the	flight	manual	at	the	ground	control	point	where	the	pilot	flying

the	sUAS	will	have	immediate	access	to	it.The	FAA	has	issued	the	following	exempti ons	to

this	regulation:	Exemption	Nos.	8607,	8737,	8738,	9299,	9299A,	9565,	9565B,	10167,

10167A,	10602,	32827,	and	10700.

(2)	For	which	an	Airplane	or	Rotorcraft	Flight	Manual	is	not	required	by	§21.5	of	this

chapter,	unless	there	is	available	in	the	airc raft	a	current	approved	airplane	or	Rotorcraft

Flight	Manual,	approved	manual	material,	markings,	and	placards,	or	any	combination

thereof.

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	not	be	provided	for	the

aircraft	an	exemption	will	be	needed.	An	equivalent	level	of	safety	will	be	set	forth	by the

pre

- --flight	checklist	as	set	forth	in	the	Flight	Operations	Manual.The	PIC	will	take	all

actions	including	reviewing	weather,	flight	battery	requirements,	landing	and	takeoff

distances,

aircraft	performance	data	and	setting	the	pre

- --determined	safe	l anding	area	in	case	of	loss	of

GPS	communication	before	initiation	of	flight.

14	C.F.R.	§91.109:	Flight	instruction:

Section	91.103	provides	that	no	person	may	operate	a	civil	aircraft	(except	a	manned	free

balloon)	that	is	being	used	for	flight	instru c ti on	unless	that	aircraft	has	fully	functioning

## Peter	Spero

– Cell:847.902.9590

– Peter@AeroVistaInnovations.com

dual	controls.	sUASs	and	remotely	piloted	aircraft,	by	their	design	do	not	have	fully

functional	dual	controls.	Flight	control	is	accomplished	through	the	use	of	a	control	box	that

communicates	with	the	airc raft	via	radio	communications. The	FAA	has	approved

exemptions	for	flight	training	without	fully	functional	dual	controls	for	a	number	of	aircraft

and	for	flight	instruction	in	experimental	aircraft.	See	Exemption	Nos.5778K	&	9862A.The

equivalent	level	of safety	provided	by	the	fact	that	neither	a	pilot	nor	passengers	will	be

carried	in the	aircraft	and	by	the	size	and	speed	of	the	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	to	be	operated	at	less	than	the	minimums	prescribed,	provided	the	person

operating	the	helicopter	complies	with	any	route	or	altitudes	prescribed	for	helicopters	by

the	FAA.As	this	exemption	is	for	a	sUAS	that	is	a	he licopter	and	the	exemption	requests

authority	to	operate	at	altitudes	up	to	400	AGL,	or	not	more	than	200	above	an	elevated

platform	from	which	filming	is	planned,	an	exemption	may	be	needed	to	allow	such

operations. The	sUAS	will	never	operate	at	higher	t han	400	AGL.	It	will	however	be	operated

in	a	restricted	area	with	security	perimeter,	where	buildings	and	people	will	not	be	exposed

to	operations	without	their	pr e

- --obtained	consent.

The	equivalent	level	of	safety	will	be	achieved	given	the	size,	weight ,	speed	of	the	UAS	as

well	as	the	location	where	it	is	operated.	No	flight	will	be	taken	without	the	permission	of

the	property	owner	or	local	officials.	Because	of	the	advance	notice	to	the	property	owner

and	participants	in	the	filming	activity,	all	affe cted	individuals	will	be	aware	of	the	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 is far	less	than	those	presently	presented	with

conventional	aircraft	operating	at	or	below	500	AGL	in	aerial	photography	and

cinematography	industry.	In	addition,	the	low

- --	altitude	operations	of	the	sUAS	will

ensure	separation	between	these	sUAS	operati ons	and	the	operations	of	conventional

aircraft	that	must	comply	with	Section	91.119.

14	C.F.R.	§91.121	Altimeter	Settings

This	regulation	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	setting	available	before	departure.”	As	the	sUAS	may	not	have	a

barometric	altimeter,	but	instead	a	GPS	altitude	read	out,	an	exemption	may	be	needed.	An

equivalent	level	of	safety	wil l	be	achieved	by	the	operator,	pursuant	to	the	Pre	Flight	Check

list,	confirming	the	altitude	of	the	launch	site	shown	on	the	GPS	altitude	indicator	before

flight.

14	C.F.R.	§	91.151(a):	Fuel	Requirements	for	Flight	in	VFR	Conditions

Section	91.151	(a)	pr o hibits	an	individual	from	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.”

## Peter	Spero

– Cell:847.902.9590

– Peter@AeroVistaInnovations.com

The	battery	powering	the	sUAS	provides	approximately	40	minutes	of	powered	flight.	To

meet	the	30	minute	reserve	requirement	in	14	CFR	§91. 151,	sUAS	flights	would	be	limited

to	approximately	10	minutes	in	length.	Given	the	limitations	on	the	UAS’s	proposed	flight

area	and	the	location	of	its	proposed	operations	within	a	predetermined	area,	a	longer	time

frame	for	flight	in	daylight	or	night	V FR	conditions	is	reasonable.

AeroVista	Innovations 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)).	O perating	the	small	UAS,	in	a	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	91.1 51(a)	was	intended	to	alleviate	given	the	size

and	speed	of	the	small	UAS.	Additionally,	limiting	sUAS	flights	to	10	minutes	would	greatly

reduce	the	utility	for	which	the	exemption	will	be	granted.

Applicant	believes	that	an	equivalent	level	of	safety	ca n	be	achieved	by	limiting	flights	to	30

minutes	or	25%	of	battery	power	whichever	happens	first.	This	restriction	would	be	more

than	adequate	to	return	the	sUAS	to	its	planned	landing	zone	from	anywhere	in	its	limited

operating	area.

Similar	exemptions	hav e	been	granted	to	other	operations,	including	Exemptions	2689F,

5745,	10673,	and	10808.

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	a	civil	aircraft	unless	it	has

within	it	the	following:

(1)	An	appropriate	and	current	airworthiness	certificate.	.	.	.

(b)	No	person	may	operate	a	civil	aircraft	unless	the	airworthiness	certificate	required	by

paragraph	(a)	of	this	se ction	or	a	special	flight	authorization	issued	under	§91.715	is

displayed	at	the	cabin	or	cockpit	entrance	so	that	it	is	legible	to	passeng e rs	or	crew.

The	UAS	fully	loaded	weighs	no	more	than	55	lbs	and	is	operated	without	an	onboard	pilot.

As	such,	there is	no	ability	or	place	to	carry	certification	and	registration	documents	or	to

display	them	on	the	sUAS.

An	equivalent	level	of	safety	will	be	achieved	by	keeping	these	documents	at	the	ground

control	point	where	the	pilot	flying	the	sUAS	will	have	immedi ate	access	to	them,	to	the

extent	they	are	applicable	to	the	sUAS.The	FAA	has	issued	numerous	exemptions	to	this

regulation.	A	representative	sample	of	other	exceptions	includes	Exemption	Nos.	9565,

9665,	9789,	9789A,	9797,	9797A,	9816A,	and	10700.

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	E	of	this	part	and	shall	between	required	inspectio ns,

except	as	provided	in	paragraph	(c)	of	this	section,	have	discrepancies	repaired	as

prescribed	in	part	43	of	this	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	to	the	applicant.	Maintenance	will	be

accomplished	by	the	operator	pursuant	to	the	flight	manual	and	operating	handbook.	An

## Peter	Spero

– Cell:847.902.9590

– Peter@AeroVistaInnovations.com

equivalent	level	of	safety	will	be	achieved	because these	small	UASs	are	very	limited	in	size

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.The	o perator	will	ensure	that	the	UAS	is	in	working	order	prior	to

initiating	flight,	perform	required	maintenance,	and	keep	a	log	of	any	maintenance

performed.	Moreover,	the	operator	is	the	person	most	familiar	with	the	aircraft	and	best

suited	to	maintain	the aircraft	in	an	airworthy	condition	to	provide	the	equivalent	level	of

safety.

Pursuant	to	14	C.F.R.	Part	11,	the	following	summary	is	provided	for	publication	in	the

Federal	Register,	should	it	be	determined	that	publication	is	needed:

Applicant	seeks	a n	exemption	from	the	following	rules:

14	C.F.R.	§21,	subpart	H;	14	C.F.R	45.23(b);14	C.F.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)	in	aerial	photography	and	cinematography	for	residential

and	commercial	real	estate	and	closed

- --set	special	events.

Approval	of	exemptions	allowing	commercial	operatio ns	of	sUASs	for	aerial	photography

and	cinematography	for	real	estate	and	close

- --set	special	events	will	enhance	safety	by

reducing	risk.	Conventional	real	estate	aerial	photography	and	cinematography	use	jet	or

piston	powered	aircraft	which	carry	large	a mounts	of	combustible	fuel	posing	increased

risk.	Conversely,	sUASs	carry	no	combustible	fuel,	weigh	only	55	lbs.	or	less	comparatively

to	3,000+	lbs.	of	a	conventional	aircraft,	are	much	more	easily	maneuverable	and	do	not

ferry	to	and	from	the	production location.	Additionally,	flying	at	or	below	400	AGL	sUAS	will

be	no	factor	with	fixed	wing	and	rotor	wing	aircraft.

The	operation	of	small	UASs,	weighting	less	than	55	lbs.,	conducted	in	the	strict	conditions

outlined	above,	will	provide	an	equivalent	lev el	of	safety	supporting	the	grant	of	the

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	to	the	ground,	and	in	a	st erile	environment	and,	as	a	result,	are	far	safer	than

conventional	operations	conducted	with	traditional	aircraft	which	pose	a	safety	risk. There

are	no	personnel	on	board	the	sUASs	and	therefore	the	likelihood	of	death	or	serious	bodily

injury	is	signifi cantly	diminished.	All	flights	will	occur	over	private	or	controlled	access

property	with	the	property	owner’s	prior	consent	and	knowledge.	Filming	will	be	of	people

who	have	also	consented	to	being	filmed	or	otherwise	have	agreed	to	be	in	the	area	where

f ilming	will	take	place. AeroVista	Innovations will	provide	an	equivalent	or	better	level	of

safety	as	that	achieved	under	the	current	FAR’s. All	Aerovista	sUAV	operators	are

licensed	pilots

.

## Peter	Spero

– Cell:847.902.9590

– Peter@AeroVistaInnovations.com

AeroVista	Innovations respectfully	request	that	the	FAA	grants th e	exemption	request.

Satisfaction	of	the	criteria	provided	in	Section	333	of	the	Reform	Act	of	2012

- -- - --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	for	the	grant	of	the	requested	exemptions	allowing	commercial	operation	of

applicant’s	UAS	in	aerial	photography	and	cinematography	for	the	real	estate	industry	and

close

- --set	special	events	pursuant	to	the	Manua ls	appended	hereto.

Sincerely,

Peter	Spero

AeroVista	Innovations ,	LLC.

## Peter	Spero

– Cell:847.902.9590

– Peter@AeroVistaInnovations.com

App e nd i x

FA R secti o n Sub jec t J u stifi ca ti o n

14 CFR §

45

. 23 ( b ) Requ ir e m en t t o d is p l ay r eg istr a ti on

nu m b er o n v e h i c le I n s u fficie n t s pa ce on v e h icle

14 CFR Pa rt 21 A ir c r a ft c ertifi ca ti on re qu ire m e n ts an d

p r o c edu r e s D esi gn e d f o r m ann e d a ir c r a ft; no t s u it ab le f o r o ff

- ---

t he

- -- - s he lf s UA S

14 CFR § 61

. 3 Requ ir e m en t f o r p il o t c e rtific a t e Pa rt 61 r equ ir e m en ts de si gne d f o r m anned a ircr a ft,

no t s UAS ; p etiti o n de s c ri b es tr a i n i ng f o r s UAS ope r

a t o r

14 CFR § 91

. 7

( a ) A ir w o rt h i n ess re qu ire m e n t D esi gn e d f o r m ann e d a ir c r a ft; no t s u it ab le f o r o ff

- ---

t he

- -- - s he lf s UA S

14 CFR § 91

. 9

( b ) ( 2 ) Requ ir e m en t f o r m anua l t o be

ava il ab l e i n t h e c o c kp it N o on e a bo ar d t o rea d m a nu al

14 CFR §

91

. 103 ( b ) Re qu ir e m en t f o r cr e w m e m be rs t o be

onboa r d Un m ann e d v e h i c le

14 CFR §

91

. 109 Requ ir e m en t f o r dua l c on tr o ls du ri ng

fli gh t i n str u cti on N o on e a bo ar d t o op erate c on tr o ls

14 CFR §

91

. 119 M i n i m u m a ltit ude s f o r s a f e fli gh t Sa fet y re qu ires op er a ti on b el o w t h ese a ltit ud es

14 CFR §

91

. 121 A lti m eter setti ng s N o on e a bo ar d t o rea d alti m eter

14 CFR §

91

. 151 ( a ) Fue l r equ ir e m en ts Veh icl e doe s no t u s e f ue l

14 CFR §

91

. 203 ( a ) & ( b ) Requ ir e m en t f o r r eg istr a ti on and

a ir w o rt h i ne ss c e rtific a t e s t o b e on

boa r d N o on e a bo ar d t o rea d certificates

14 CFR §

91

. 205 ( b ) Cockp it i n str u m e n ts N o on e a bo ar d t o rea d

Requ ir e m en t I n str u m e n ts

14 CFR § 91

. 215 T r an s ponde r r equ ir e m en t Veh icl e ha s i n s u ffici en t u s e f u l l oad ; w ill be ope r a t ed

be l o w ATC r ada r c ove r age

14 CFR § 91

. 405 ( a ) I n s p ecti on re qu ire m e n ts D esi gn e d f o r m ann e d a ir c r a ft; no t s u it ab le f o r o f f

- -- - t he

- ---

s he lf s UA S

14 CFR § 91

. 407 ( a )

( 1 ) I n s p ecti on app r ova l

re qu ire m e n t s De si gned f o r m anned a ircr a ft; no t s u it ab l e f o r o ff

- -- - t he

- ---

s he lf s UA S

14 CFR § 91

. 409 ( a )

( 2 ) A ir w o rt h i n ess i n s p e c ti on D esi gn e d f o r m ann e d a ir c r a ft; no t s u it ab le f o r o ff

- -- - t he

- ---

s he lf s UA S

14 CFR § 91

. 417 ( a ) M a i n t enan c e r e c o r d s D esi gn e d f o r m anned a ircr a ft; no t s u it ab l e f o r o ff

- -- - t he

- ---

## Peter	Spero

– Cell:847.902.9590

– Peter@AeroVistaInnovations.com

& ( b ) re qu ire m e n t s s he lf s UA S



# D J I I NSP I R E SPEC S

Aircraft M od e l

T600

W ei gh t ( Ba tter y I n cl ud e d )

293 5 g

Hover i n g Accurac y ( GP S M ode )

V erti ca l : 0

. 5 m

Hori z o n t a l : 2

. 5 m

M a x Angu l a r V el o cit y

P it ch : 300 °/ s

Yaw : 150 °/ s

M a x T il t Ang l e

35°

M a x A sce n t Sp ee d

5 m / s

M a x D esce n t Sp ee d

4 m / s

M a x Sp ee d

2 2 m / s ( ATT I m o de

, n o w i n d )

M a x F li gh t A ltit ud e

450 0 m

M a x W i n d Sp ee d R esist an c e

1 0 m / s

M a x F li gh t T i m e

App ro x i m a tel y 1 8 m i n ute s

M o t o r M od e l

D J I 351 0

P r op elle r M od e l

D J I 134 5

I ndoo r Hover in g

Enab le d b y def a u l t

Opera ti n g Te m pera t ur e Rang e

- 10 ° t o 40 ° C

D i agona l D ist an c e

5 5 9 t o 58 1 m m

D i m e n si on s

438x451x30 1 m m



## Gimbal M od e l

ZE N MU S E X 3

Ou t pu t Pow e r ( W it h Ca m era )

S t a ti c : 9 W

I n M otio n : 1 1 W

Opera ti n g Curren t

## Peter	Spero

– Cell:847.902.9590

– Peter@AeroVistaInnovations.com

S t a tio n : 75 0 m A

M otio n : 90 0 m A

Angu l a r V i b r a ti o n Rang e

±0

. 03°

M oun ti n g

Det achab le

Con tr o ll ab l e Rang e

P it ch :

- 9 0 ° t o +30°

Pan : ±320 °

M ec han ic a l Rang e

P it ch :

- 125 ° t o +45°

Pan : ±330 °

M a x Con tr o ll ab l e Sp ee d

P it ch : 120 °/ s

Pan : 180 °/ s



## Camera Na m e

X3

M od e l

F C 35 0

To t a l P ixel s

12

. 76M

E ffecti v e P ixel s

12

. 4M

I m ag e M a x S i z e

4000 x 3000

I S O Rang e

100

- 320 0 ( v ideo )

100

- 160 0 ( ph oto )

E lectr on i c Shu tte r Sp ee d

8 s

- 1 / 8000s

F O V ( F iel d O f V ie w )

94°

C MO S

S o n y E X M O R 1 / 2

. 3 ”

L e n s

20 m m ( 35 m m for m a t eq u i va le n t)f/ 2

. 8 fo c us a t ∞

9 E le m e n t s i n 9 gro u p s

An ti

- d i s tortio n

S til l Pho t og r aph y M od e s

S i n gl e s h oo t

B u r s t s h ooti n g : 3 / 5 / 7 fr a m e s

A ut o Exp o s ur e B r ack eti n g ( AE B ) : 3 / 5 b r ack ete d fr a m e s a t 0

. 7E V B i a s

T i m e

- l ap s e

V i d e o R ec o r d i n g M od e s

U H D ( 4 K ) : 4096x2160p24 / 25

, 3840x2160p24 / 25 / 3 0

FH D : 1920x1080p24 / 25 / 30 / 48 / 5 0 / 60

HD : 1280x720p24 / 25 / 30 / 48 / 50 / 6 0

M a x B itr a t e O f V i d e o S t o r ag e

6 0 M bp s

Supp orte d F il e Fo r m a t s

## Peter	Spero

– Cell:847.902.9590

– Peter@AeroVistaInnovations.com

FAT32 /e xFA T

Ph oto : JPE G

, DN G

V ideo : M P4 / M O V ( M PE G

- 4 AV C/H. 264)

Supp orte d S D Ca r d Typ e s

M i c r o S D

M a x capac it y : 6 4 G B

. Cl a s s 1 0 o r U H S

- 1 r a ti n g req u ired

.

Opera tin g T e m p er a t u r e Range

0 ° t o 40 ° C



## Remote Controller Na m e

C1

Opera ti n g Frequenc y

92 2

. 7~927

. 7 M H z ( Japa n On l y )

5

. 725~5

. 82 5 GH z

2

. 400~2

. 48 3 GH z

T r an s m itti n g D ist an c e ( O u t doo r An d Unob str u cte d )

2 k m

E I R P

10 d Bm@ 900 m

, 13 d Bm@ 5

. 8 G

, 20 d Bm@ 2

. 4G

V i d e o Ou t pu t Po r t

U S B

, m i n i

- H D M I

Pow e r Supp l y

B u ilt

- i n ba tter y

Cha r g i n g

D J I cha r g e r

Dua l U se r Capab ilit y

Ho s t

- an d

- S l av e c o nn e c tio n

M ob il e D e v ic e Ho l d e r

Tab le t o r Ph o ne

M a x M ob il e D e v ic e W i d t h

170 m m

Ou t pu t Pow e r

9 W

Opera ti n g Te m pera t ur e Rang e

- 10 ° t o 40 ° C

S t o r ag e T e m p er a t u r e Rang e

Le s s t ha n 3 m o n t h s :

- 20 ° t o 45 ° C

M or e t ha n 3 m o n t h s : 22 ° t o 28 ° C

Cha r g i n g T e m p er a t u r e Rang e

0

- 40 ° C

Ba tter y

600 0 m A h Li P o 2S



## Charger M od e l

A14

- 100P1A

Vo lt ag e

26

. 3 V

Ra te d Po w e r

10 0 W

## Peter	Spero

– Cell:847.902.9590

– Peter@AeroVistaInnovations.com

Battery (Standard) Na m e

I n tellige n t F lig h t B a tter y

M od e l

T B 47

Capa cit y

450 0 m A h

Vo lt ag e

22

. 2 V

Ba tter y Typ e

Li P o 6 S Hig h v olt a g e ba ttery

En er g y

99

. 9 W h

N e t W ei gh t

57 0 g

Opera ti n g Te m pera t ur e Rang e

- 10 ° t o 40 ° C

S t o r ag e T e m p er a t u r e Rang e

Le s s t ha n 3 m o n t h s :

- 20 ° t o 45 ° C

M or e t ha n 3 m o n t h s : 22 ° C t o 28 ° C

Cha r g i n g T e m p er a t u r e Rang e

0 ° t o 40 ° C

M a x Cha r g i n g Pow e r

18 0 W



## Battery (Optional) Na m e

I n tellige n t F lig h t B a tter y

M od e l

T B 48

Capa cit y

570 0 m A h

Vo lt ag e

22

. 8 V

Ba tter y Typ e

Li P o 6 S

En er g y

129

. 9 6 W h

N e t W ei gh t

67 0 g

Opera ti n g Te m pera t ur e Rang e

- 10 ° t o 40 ° C

S t o r ag e T e m p er a t u r e Rang e

Le s s t ha n 3 m o n t h s :

- 2 0 t o 45 ° C

M or e t ha n 3 m o n t h s : 22 ° t o 28 ° C

Cha r g i n g T e m p er a t u r e Rang e

0 ° t o 40 ° C

M a x Cha r g i n g Pow e r

18 0 W



## Vision Positioning V el o cit y Rang e

B elo w 8 m / s ( 2 m ab o v e gro u n d )

## Peter	Spero

– Cell:847.902.9590

– Peter@AeroVistaInnovations.com

A ltit ud e Rang e

5

- 50 0 c m

Opera ti n g Env ir on m e n t

B rig h tl y li t (l ux > 15 ) pa tter n e d s u rf ac e s

Opera ti n g Rang e

0

- 25 0 c m



# 3D	Robotics	Solo	Specs

Aircraft W ei gh t (I n cl ud i n g Ba tter y, Propellers, and Gimbal )

1 800 g

D i agona l S iz e (I n cl ud i n g P r op ellers )

580 m m

M a x A sce n t Sp ee d

5 m / s

M a x D e sce n t Sp ee d

5 m / s

M a x Sp ee d

55 mph ( ATT I m ode

, n o w i n d )

M a x Payload

420g

Flight M od e

G P S

Auto Pilot

Pixhawk2

Opera ti n g Te m pera t ur e

0 ° C t o 40 ° C GP S



## Camera Type

GoPro Hero 4 Black

S e n s o r

Optical Sensor

- CMOS

L e n s

Ultra Wide FOV

I S O Rang e

100

- 6400 ( v ideo ) 100

- 800 ( ph oto )

Shu tte r Sp ee d

Video: Shutter Speed

- Max:1/fps Min:1/8192

Photo: Shutter Speed

– Max:0.5 sec. Min. 1/8192

## Peter	Spero

– Cell:847.902.9590

– Peter@AeroVistaInnovations.com

V i d e o R ec o r d i n g M od e s

4K 30/25/24 fps

, Ultra Wide FOV

2.7K 50/48/30/25/24 fps Ultra Wide, Medium FOV

1410p 80, 60, 50, 48, 30, 25, 24 fps Ultra Wide FOV

1080p 120, 90, 60, 50, 48, 30, 25, 24 fps

Ultra Wide, Medium (excludes 120 and 90 fps), Narrow FOV

Supp orte d S D Ca r d Typ e s

M i c r o S D

M a x capac it y : 6 4 G B

. Cl a s s 1 0 o r U H S

- 1 r a ti n g req u ire d

M a x B itr a t e O f V i d e o S t o r ag e

6 0 M bp s

Supp orte d F il e Fo r m a t s

AT32 /e xFA T

P h oto : JPE G

, DN G

V ideo : M P4

, M O V ( M PE G

- 4 AV C/ H

. 264 )

Software

APM:Copter

Opera ti n g Te m pera t ur e

0 ° C t o 40 ° C



## Gimbal Con tr o ll ab l e Rang e

P it c h

- 0 ° t o

- 9 0°

S t ab iliz a ti o n

3

- ax i s ( p it ch

, r oll

, yaw )



## Remote Controller Opera ti n g Frequenc y

2

. 40 0 GH z

M a x D ist an c e

.5 miles

V i d e o Ou t pu t Po r t

HDMI

Opera ti n g Te m pera t ur e

0 ° C t o 40 ° C

## Peter	Spero

– Cell:847.902.9590

– Peter@AeroVistaInnovations.com

Controller Ba tter y

2600 mAh 7.2 Vdc

lithium ion

M ob il e D e v ic e Ho l d e r

F o r t ab le t o r ph o n e

**Communication** :

3DR Link secure WiFi network



## Intelligent Flight Battery Capa cit y

5200 m A h

Vo lt ag e

14.8 V Ba tter y

Typ e Lithium

Polymer

M a x F li gh t T i m e

App ro x i m a tel y 2 5 m i n ute s

Opera ti n g Te m pera t ur e

- 10 ° C t o 40 ° C

M a x Cha r g i n g Pow e r

10 0 W 

## App / Live View M ob il e Ap p

3DR Solo App

L i v e V ie w

Solo Secure WiFi Network

– Tablet of SmartPhone

L i v e V ie w Q ua lit y

720 P @ 30 f p s (de p e n di n g o n c o n ditio n s an d m o b il e de v i c e )

La te n c y

- 180 m s (de p e n di n g o n c o n ditions)