### Mark	Davies Mark	Davies	Media,	LLC 12	Grandview	Ave Lawrenceville,	NJ	08648

- 1034

U. S.	Department	of	Transportation Docket	Management	System 1200	New	Jersey	Ave.,	SE Washington,	DC	20590

December	1 6 , 2015

Re:	Exemption	Request	Pursuant	to	Section	333	of	the	FAA Modernization	and Reform	Act	and Part	11 of	the	Federal	Aviation	Regulations	from:

• 14	C.F.R.	21	Subpart	H

• 14	C.F.R.	Part	36	Subpart	A,	F	&	O

• 14	C.F.R.	§45.23(b)

• 14	C.F.R.	§61.113(a)	and	(b)

• 14 C.F.R.	§91.7(a)

• 14	C.F.R.	§91.9(b)	(2)

• 14	C.F.R.	§91.103(b)(2)

• 14	C.F.R.	§91.109

• 14	C.F.R.	§91.119(c)

• 14	C.F.R.	§91.121

• 14	C.F.R.	§91.151(a)

• 14	C.F.R.	§91.203	(a)	and	(b)

• 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)

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, Mark	Davies	Media,	LLC ( Mark	Davies	Media ) hereby	applies	for	an	exemption	from	the	listed Fe deral	Aviation	Regulations	(“FARs”)	to	allow	commercial	operation	of Small	Unmanned	Aircraft	Systems (sUAS), so	long	as	such	operations	are	conducted	within	and	under	the	conditions	outlined	herein	or	as	may be	established	by	the	FAA	as	required	by	Section 333. Commercial	operation	of sUAS,	as	described	herein,	which	are	equipped	with	camera(s)	and	sensors,	would operate	in	the	following	manner:

• Aerial	photography	and	video	for	public	and private	use	including	real	estate,	architecture,	land surveying,	engineering,	and	other	re lated	professional	activities.

• Aerial	video	and	photography	for	public	and private	use	including	closed

- set	motion	picture	and television fi lming,	public	events,	cin em atography,	and	news	gathering.

• Aerial	data	collection	applications to include	mapping,	topographical	surveying,	3D	modeli ng,	and precision	agriculture.

• Aerial	inspection	and	photography	of	residential	and	commercial	structures.

### • Aerial	inspection	of utili ty	infrastructure	including	but	not limited	to electrical	power	lines,	w ind turbines,	and	cell	towers.

• Aerial	video	and photography f or	providing	live	video	feed	to	assist	with	search	and	rescue	operations	in cases		of	an	emergency	or	natural	disaster	only when	the	local	authorities	or	government	has	requeste d	it by	contract		or	donation.

• The	ability	to	off er	training	to	persons and organizations that	have	interests	in	the	use and	safe	operation of sUAS

. Th e	requested	exemption would	permit	the	operation	o f sUAS	under	controlled	conditi ons	in	the National Airs pace System ( NAS ) that	would	be	limited,	controlled,	predetermined,	and will	provide	safety enhancements	to	the	the	industry	presently	using	conventional aircraft

. Approval	of	this	exemption	would ther eby	enhance	safety	and	ful fill the	Secretary	of	Transportation’s	(the	FAA	Administr ator’s)	responsibilities to	“.. .establish	requirements	for	the	safe	operation	of	such aircraft systems	in	the	national	airspace	system.”

Th e	name	and	address	of	the	applicant	is:
Mark	Davies Mark	Davies	Media,	LLC 12	Grandview	Ave Lawrenceville,	NJ	08648

- 1034 215	248	2727 MarkDaviesMedia@gmail.com

Regulations	from	which	the	exemptions	are	requested:

• 14	C.F.R.	Part	21	Subpart	H

• 14	C.F.R.	Part	36	Subpart	A,	F	&	O

• 14	C.F.R.	§45.23	(b)

• 14	C.F.R.	§61.113	(a)	&	(b)

• 14	C.F.R.	§91.7	(a)

• 14	C.F.R.	§91.9	(b)	(2)

• 14	C.F.R.	§91.103(b)(2)

• 14	C.F.R.	§91.109

• 14	C.F.R.	§91.119	(c)

• 14	C.F.R.	§91.121

• 14	C.F.R.	§91.151	(a)

• 14	C.F.R.	§91.203	(a)	&	(b)

• 14	C.F.R.	§91.405	(a)

• 14	C.F.R.	§91.407	(a)	(1)

• 14	C.F.R.	§91.409	(a)	(2)

• 14	C.F.R.	§91.417	(a)	&	(b)
Mark	Davies	Media propose s	to	operate	the	following	sUAS :

• 3DR	Solo

• 3DR	X8	Plus

• ALTUS	Delta	X8

• DJI	Flame	Wheel	F330

• DJI	Flame	Wheel	F450

• DJI	Flame	Wheel	F550

• DJI	Inspire	1

• DJI	Inspire	1	Pro

### • DJI	Matrice	100

• DJI	Phantom	2	Vision	Plus

• DJI	Phantom	3	Standard

• DJI	Phantom	3 Advanced

• DJI	Phantom	3	Professional

• DJI	Spreading	Wings	S900

• DJI	Spreading	Wings	S1000

• DJI	Spreading	Wings	S1000	Plus

• YUNEEC	Tornado	H920	A5

• YUNEEC	Typhoon	Q500

• YUNEEC	Typhoon	Q500	Plus

• YUNEEC	Typhoon	Q500	4K Similarly	sized	sUASs	have	been	approved	for	use	in	pri or	Section	333	Grants	of	Exemption	from	the	FAA. See e.g.,	Grant	of	Exemption	to	Shotover	Camera	Systems	L.P.	(Exemption	No.	11159);	Grant	of	Exemption	to VDOS	Global,	LLC	(Exemption	No.	11112);	Grant	of	Exemption	to	LowCountryRC,	Corp.	(Exemption	No. 1118 4);	Grant	of	Exemption	to	Alan	Purwin	(Exemption	No.	11161);	Grant	of	Exemption	to	Helinet	Aviation Services	(Exemption	No.	11160);	Grant	of	Exemption	to	Total	Safety	U. S.,	Inc.	(Exemption	No.	11156);	Grant of	Exemption	to	Price	Aviation	Group	(Exemption	N o.	11307A);	Grant	of	Exemption	to	Cable	News	Network (Exemption	No.	12174);	Grant	of	Exemption	to	Mr.	James	F.	Kasler	(Exemption	No.	12873); Grant	of Exemption	to	Mr.	Jeffrey	D.	Greer	(Exemption	No.	11587A); Grant	of	Exemption	to	XO Innovations	(Exemption No.	12378A);	Grant	of	Exemption	to	MCS	Communications	(Exemption	No.	11809A); Grant	of	Exemption	to	Iris	Magic	Photo	Studios	LLC	and	Iris	Magic	Media	LLC	(Exemption	No.	12718 ); Grant of	Exemption	to	Mr.	Carl	H.	Schneider	(Exemption	No.	12845); Grant	of	Exe mption	to	AGL	Imaging	LLC (Exemption	No.	12684); Grant	of	Exemption	to	Mr.	Joshua	L.	Vilches	C.E.T.	Aviation	(Exemption	No.	11492A); Grant	of	Exemption	to	Measure	(Exemption	No.	12646)

. G iven	the	small	size	of	sUAS and	the	controlled	environment	provided,	the	proposed	operations	will	adhere to	the	Reform	Act’s	safety	requirements. Th e	approval	of	this	application	presents	no	national	security	issues. Regarding	the	level	of	safety	surrounding	the	proposed	operations and	the	public	bene fi t,	reduction	in environmental	impacts,	including	but	not	limited	to	reduced	emissions	and	noise,	the	grant	of	the	requested exemption	is	in	the	public	interest.	Accordingly,	the	applicant	requests	that	the	FAA	grant	the	requested exemp tion.

AIRCRAFT AND	EQUIVALENT	LEVEL	OF	SAFETY
Th e	applicant	seeks	to	hav e	this	exemption	cover	the	sUAS used	to	carry	out	the	commercial	operations described	herein	which	are	subject	to	the	limitations	proposed	in	this	petition. Mark	Davies	Media propo ses and	agrees	to	the	following	limitations	and	conditions	for	commercial	sUAS	operations	conducted	under	a granted	FAA	exemption:

• Operations	will	be	limited	to	the	sUAS	listed	above	weighing	less	than	55	pounds	including	payload.

• The Unmanned	Aircraft ( UA ) will	not	be	operated	at	a	speed	exceeding	50	knots,	the	maximum	UA operating	airspeed	recommended	by	the	aircraft	manufacturer.

• The Pilot	in	Command	( PIC ) will	hold	either	an	airline	transport,	commercial,	private,	recreational,	or sport	pilot	certi ficate.	The	PIC	will	also	hold	a	current	FAA	airman	medical	certificate	or	a	valid	U.S. driver’s	license	issued	by	a	state,	the	District	of	Columbia,	Puerto	Rico,	a	territory,	a	possession,	or the	Federal	government.	The	PIC	will	also	meet	the	flight	revie w	requirements	specified	in	14	CFR	§ 61.56	in	an	aircraft	in	which	the	PIC	is	rated	on	his	or	her	pilot	certificate.

• PIC will	have	been	trained to	safely	operate	the	UAS,	including	evasive	and	emergency	maneuvers and	maintaining	appropriate	distances	from persons,	vessels,	vehicles	and	structures.

• All	operations	will	be	conducted	over	private	or	controlled

- access	property	with	permission	from	the property	owner/controller	or	authorized	representative.	Permission	from	property owner/controller	or	authorized representative	will	be	obtained	for	each	flight	to	be	conducted.

### • All	f light	operations will be	conducted	at	least	500	feet	from	all	nonparticipating	persons,	vessels, vehicles,	and	structures	unless	barriers	or	structures	are	present	that	sufficiently	pro tect nonparticipating	persons	from	the	UA	and/or	debris	in	the	event	of	an	accident.

• Operations	will	not	be	conducted	within	5	nautical	miles	of	an	airport	reference	point	(ARP)	as denoted	in	the	current	FAA	Airport/Facility	Directory	(AFD).

• Prior	to	each flight,	the	PIC	will	conduct	a	pre

- flight	inspection	and	determine	the	UAS	is	in	a condition	for	safe	flight.

• All	operations	will	be	conducted	under	visual	meteorological	conditions	(VMC).

• The	PIC	will	not	begin	a	flight	unless	there	is	enough	available	p ower	for	the	UA	to	conduct	the intended	operation	and	to	operate	after	that	for	at	least	five	minutes.

• The	UA	will	be	operated	at	an	altitude	of	no	more	than	400	feet	above	ground	level	(AGL).

• All	operations	will	utilize	a	visual	observer	(VO).

• The	UA	wil l	be	operated	within	the	visual	line	of	sight	(VLOS)	of	the	PIC	and	VO	at	all	times.

• The	VO	and	PIC	will	be	able	to	communicate	verbally	at	all	times.

• The	UA	will	not	be	operated	less	than	500	feet	below	or	less	than	2,000	feet	horizontally	from	a	cloud
o r	when	visibility	is	less	than	3	statute	miles	from	the	PIC.

• If	the	UAS	loses	communications	or	loses	its	GPS	signal,	the	UA	will	return	to	a	pre

- determined location	within	the	private	or	controlled

- access	property.

• The	PIC	will	abort	the	flight	in	the event	of	unpredicted	obstacles	or	emergencies.

• A	Motion	Picture	and	Television	Operations	Manual	(MPTOM)	will	be	used	to	help	govern	all	closed

set		motion	picture	and	television	filming	operations.

14	C .F.R.	Part	21,	Subpart	H:	Certifi cation	Procedur es - Airworthiness	Certi fi cates Subpart H,	entitled	Airworthiness	Certifi cates,	establishes	the	procedural	requirements	for	the issuance	of airworthiness	certifi cates	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	level	of	safety	under	Part	11	and Section	333	of	the	Reform	Act. Th e	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	require ment	for	an	airworthiness	certifi cate,	upon	consideration	of	the	size,	we ight ,	speed,
o perational	capability,	and	proximity	to	airports	and	populated	areas	of	the	particular	sUAS.	In	all	cases,	an analysis	of	these	criteria	demonstrates	that	the	sUAS	operated without	an	airworthiness	certifi cate,	in	the restricted	environment	and	under	the	c onditions	proposed	will	be	at	least	as	safe,	or	safer,	than	a conventional aircraft (fi xed	wing	or	rotorcra ft )	operat ing	with	an	airworthiness	certifi cate	without	the restrictions	and	conditions	proposed.

Th e	sUAS	to	be	operated are less	th an	55	lbs. fully	loaded ,	carry neithe r	a	pilot	nor	passenger,	carry no explosive	materials	or fl ammable	liquid fuels,	and	operate exclusively	within	a	secured	and	designated	area. Unlike	other	civil aircraft ,	operations	under	this	exemption	will	be	t ight ly	controlled and	monitored	by	the operator	in	compliance	with	local	public	safety	requirements. Th ese	enhancements	provide	a	greater	degree of	safety	to	the	public	and	property	owners	than	conventional	civil aircraft operations	con ducted	with airworthiness	certifi cate s	issued	under	14	C.F.R.	Part	21,	Subpart	H. Additionally ,	there	is	no	credible	threat to	national	security	posed	by	the	sUAS,	due	to	size,	speed	of	operation,	location	of	operation,	lack	of	explosive materials	or fl ammable	liquid	fuels,	and	inability	to	c arry	a	substantial	external	load. Th ere	have	been exemptions	granted	by	the	FAA	to	petitioners	seeking	identical	relief; See Grant	of	Exemption	No.	11062	to Astraeus	Aerial	(FAA

- 2014

- 0352	at	pgs.	13

- 14,	22).

14	C.F.R.	Part 36,	Subparts	A,	F	and	O:	Noise	Standards

- Aircraft	Type	and	Airworthiness	Certifi cation 14	C.F.R.	Part	36,	Subparts	A,	F	and	O,	establish	ce rtain	noise	standards	for	certifi cation	of	various aircraft types.	Because	the	sUAS	would	not	have	an	airworthin ess certificate ,	and	given	its	small	size	and	negligible noise	impact,	the	petitioner	requests	an	exemption	from	14	C.F.R.	Part	36.

### 14	C.F.R.	§	45.23	(b):	Display	of	Marks;	General. Pursuant	to	14	C.F.R.	45.23(b); “ When	marks	include only	the	Roman	ca pital	letter ‘ N ’ and	the	registration number	is	displayed	on	limited,	restricted	or	l ight

- sport	category aircraft or	expe rimental	or	provisionally certifi cated aircraft ,	the	operator	must	also	display	on	that aircraft near	each	entrance	to	the	cabin,	cockpit,	or pilot	station,	in	letters	not	less	than	2	inches	nor	more than	6	inches	high,	the	words	‘limited,’	‘restricted,’	‘ l ight

sport,’	‘experimental,’ o r	‘provisional,’ as	applicable.” While	the	sUAS	will	have	no	airw orthiness certificate ,	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	impractical. Th e	word	“Experim ental”	will	be	placed	on	the	fuselage	in compliance	with	§45.29	(f). Th e	equivalent	level	of	safety	will	be	provided	by	having	the	sUAS	marked	on	its fuselage	as	required	by	§45.29(f)	where	the	pilot,	observer,	and	others	working	with	the sUAS	will	see	the identification of	the	sUAS	as	“Experimental.”	In	a	previous	Grant	of	Exemption,	the	FAA	determined	that exemption	from	these	requirements	was	warranted	provided	that	the aircraft “have identification (N

Number)	markings	in	accordance	with	14	C.F.R	Part	45 ,	Subpart	C	if	the	markings	are	as	large	as	practicable.” See FAA	Docket	No. FAA

- 2014

- 0352.	All	sUAS own ed by Mark	Davies	Media will	bear	N

- number	markings that	are	as	large	as	practicable	in	accordance	with	14	C.F.R.	Part	45,	Subpart	C. 14	C.F.R.	§	61.1 13	(a)	and	(b):	Private	Pilot	Privileges	and	Limitations

- Pilot	in	Command. Pursuant	to	14	C.F.R.	61.113	(a)	&	(b); “ No	person	who	holds	a	private	pilot certificate may	act	as	a	pilot	in command	of	an aircraft that	is	carrying	passengers	or	property	for	compensation	or	hire. ” Because	the applicant’s	sUAS	does	not	carry	any	pilots,	passengers,	or	property, Mark	Davies	Media may	achieve	an equivalent	level	of	safety	as	achieved	under	current	regulations. Th e	risk s	attenda nt	to	the	operation	of	a sUAS	are far	less	than	the	risk	levels	inherent	in	the	commercial	activities	outlined	in	14	C.F.R.	61. Th e	PIC	of the	sUAS	will	have	an	airline	transport,	commercial,	private,	recreational,	or	sport	pilot certificate

. Th e PIC will	also	hold	a	current	FAA	airman	medical certificate or	a	valid	U.S.	driver’s	license	issued	by	a	state,	District of	Columbia,	Puerto	Rico,	a	territory,	a	possession,	or	the	Federal	government	of	the	United	States.	In	meeting those	limitations	as	li sted	in	previous	FAA	exemption	approvals,	the	PIC	of Mark	Davies	Media sUASs	will exceed	current	safety	levels	in	relation	to	14	C.F.R.	61.113	(a)	&	(b). 14	C.F.R.	§91.7(a):	Civil Aircraft Airworthiness. Pursuant	to	14	C.F.R.	91.7(a); “ No	person	may	o perate	a	civil aircraft unless	it	is	in	airworthy	condition. ” As there	will	be	no	airworthiness certificate issued	for	the	sUAS,	should	this	exemption	be	granted,	no	FAA regulatory	standard	will	exist	for	determining	airworthiness.	Given	the	size	of	the ai rcraft and	the maintenance	requirements	detailed	in	the	sUAS	User	and/or	Operations	Ma nual	combined	with	safety check lists	prior	to	each flight ,	an	equivalent	level	of	safety	will	be	provided. See Grant	of	Exemption	No.	11671 to	Dronair	Solutions	(FAA

– 2015

– 0648	page	18)	for	previous	FAA	granted	exemption. 14	C.F.R.	§	91.9	(b)	(2):	Civil Aircraft Flight Manual,	Marking,	and	Placard	Requirements. Section	91.9	(b)	(2)	provides: “ No	person	may	operate	a	U.S.

- registered	civil aircraft ...	(2)	For	which	an Airplane	or	Rotorcra ft Flight Manual	is	not	required	by	§21.5	of	this	chapter,	unless	there	is	available	in	the aircraft a	current	approved	Airplane	or	Rotorcra ft Flight Manual,	approved	manual	material,	markings,	and placards,	or	any combination thereof. ” Given	the	size	and	confi guration	of	the	sUAS	used	by Mark	Davies Media ,	there	is	no	capacity	to	carry	such	a flight manual	on	the aircraft .	An	equivalent	level	of	safety	will	be achieved	by	keeping	the	sUAS	Operation	Manual	at	the	gr ound	control	point	where	the	pilot	in	command	will have	immediate	access. See Memorandum	from	Mark	Bury,	FAA	Assistant	Chief	Counsel	for	International Law,	Legislation	and	Regulation,	to	John	Duncan,	FAA Flight Standards	Service	(Aug.	8,	2014);	see	also	Docket No.	FAA

- 2014

- 0352	at	16

- 18. 14	C.F.R.	§	91.103(b)(2):	General	O perating	and Flight Rules

- Pre flight Action. Pursuant	to	14	C.F.R.	91.103(b)(2); “ For	civil aircraft other	than	those	specifi ed	in	paragr aph	(b)(1)	of	this section,	other	reliable	information	appropriate	to	the aircraft ,	relating	to aircraft performance	under	expected

### values	of	airport	elevation	and	runway	slope, aircraft gross	w e ight ,	and	wind	and	temperature. ” An	equivalent level	of	s afet y	will	be	provided	by	a	pre flight checklist	and	other	safety	measures	detailed	in	the	sUAS Operation	Manual. Th e	PIC	will	take	actions	including	reviewing	weather, flight battery	requirements,	landing and	takeo ff distances, aircraft performance	data,	and	setting	the	pre

- determined	safe	landing	area	in	case	of loss	of	GPS	communication	before	initiation	of flight .	See	Grant	of	Exemption	No.	11671	to	Dronair	Solutions (FAA

– 2015

– 0648	page	18)
14	C.F.R.	§91.109: Flight instruction;	Sim ulated	Instrument Flight and	Certain Flight Tests. Section	91.109	provides	that “... no	person	may	operate	a	civil aircraft (except	a	manned	free	balloon)	that	is being	used	for flight instruction	unless	that aircraft has	fully	functioning	dual	controls. ” Remotely	piloted aircraft and	sUAS,	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 aircraft via	radio. Th e	FAA	has	approved exemptions	for flight train ing	without	fully	functional	dual	controls	for	a	number	of aircraft and	for flight instruction	in	experimental aircraft. Due	to	the	size	and	speed	of	the	sUAS	and	the	fact	that	neither	a	pilot	nor passengers	will	be	carried	in	the aircraft, and	all	persons will	be	a	safe	distance	away	in	the	event that	the UAS	experiences	any	diffi culties	during flight instruction,	an	equivalent	level	of	safety	is	provided. Th e	FAA has	granted	exemption	for	the	same	operation, See Grant	of	Exemption	No.	11671	to	Dronair Solutions	(FAA

– 2015

– 0648	page	19)
14	C.F.R.	§91.119 (c) :	General	Operating	and Flight Rules

- Minimum	Safe	Altitudes. Section	91.119	establishes	safe	altitudes	for	operation	of	civil aircraft. Section	91.119	(d)	allows	helicopters to	be	operated	at	le ss	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	sUAS	operation	at altitudes	up	to	400	feet	AGL,	an	exemption	may	be	needed.	I n	cases	where	the	sUAS	is	used	to	survey,	inspect, or	photograph	a	structure	that	exceeds	400	feet	AGL,	the	sUAS	will	not	be	operated	more	than	200	feet	above the	highest	point	of	that	structure.	An	exemption	was	granted	by	the	FAA	for	like	operations

- Se e Grant	of Exemption	No.	11138	to	Douglas	Trudeau	(FAA

- 2014

- 0481	page	19)

. An	equivalent	level	of	safety	will	be	achieved	given	the	size,	we ight ,	and	speed	of	the	sUAS	as	well	as	the location	where	it	is	operated.	No flight will	be	taken	without	the	perm ission	o f	the	property	owner	or	local offi cials.	Compared	to flight operations	with aircraft or	rotorcra ft operating	below	500	feet	AGL,	weighing	far more	than	the	proposed	55	pound	maximum,	and	carrying fl ammable	fuel,	the	sUAS employed	by Mark Davies Media provide	a	much	safer	alternative.	In	addition,	the	low

- altitude	operations	of	the	sUAS	will ensure	safe	separation	from	those	of	conventional aircraft that	must	comply	with	Section	91.119. 14	C.F.R.	§91.121:	General	Operating	and Flight Rules

- Alt imeter	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	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	will	be	achieved	by	the	operator,	pursuant	to	the safety	check	list	and	live flight data	monitoring ,	confo rmin g	the	altitude	of	the	launch	site	shown	on	the	GPS altitude	indicator	before flight

. See e.g.,	Grant	of	Exemption	No.	11062	to	Astraeus	Aerial	(FAA

- 2014

- 0352	at 21). 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 in	an	airplane	under	VFR	conditions	unless (considering	wind	and	forecast	weather	conditions)	there	is	enough	fuel	to fl y	to	the fi rst	point	of	intended landing	and,	assuming	normal	cruising	speed

– (1)	D uring	the	day,	to fly	aft er	that	for	at	least	30	minutes;	or	(2) At	n ight ,	to fly	aft er	that	for	at	least	45	minutes.” For	similarly	FAA	granted	exemption, see Grant	of	Exemption to	Alan	Purwin	(Exemption	No.	11161). Th e	battery	powering	the	sUAS	provides approximately	30	minutes of	powered flight .	Because	the	30	minute	reserve	requirement	in	14	C.F.R.	§91.151	cannot	be	met	by	the sUAS,	an	exemption	is	needed.	With	a	limited flight time	of	25	minutes	or	25%	battery	power	and	line	of	s ight

### operation	in	a	limited	area,	an	equivalent	level	of	safety	is	achieved. Th is	time/power	restriction	is	more	than adequate	to	safely	return	the	sUAS	to	its	planned	landing	zone	from	anywhere	in	its	limited	operating	area. 14	C.F.R.	§91.203	(a)	and	(b):	C ivil Aircraft :	Certifi cations	Required

Th e	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	section or	a	special flight authorization	issued	under	§91.715	is	displayed	at	the	cabin	or	cockpit	entrance	so	that	it	is legible	to	passe ngers	or	crew. ” Th e	sUAS	fully	loaded	weighs	no	more	than	55	lbs.	and	is	operated	without	an onboard	pilot.	As	such,	i t	is	impractical	to	carry	certifi cation	and	registration	documents	or	to	display	them	on the	sUAS.	An	equivalent	level	of	safety	will	be	a chieved	by	keeping	these	documents	at	the	ground	control point	where	the	pilot	in	command	will	have	immediate	access. Th e	FAA	has	granted	exemption	for	same, See Grant	of	Exemption	No.	11671	to	Dronair	Solutions	(FAA

– 2015

– 0648	page	18)
14	C.F.R.	§91.405 (a);	§91.407	(a)	(1);	§91.409	(a)	(2);	§91.417(a)	&	(b):	Maintenance	required. Sections	91.405(a),	407(a)(1),	409(a)(2),	417(a)(b)	require	that	an aircraft operator	or	owner “shall	have that aircraft inspected	as	prescribed	in	Subpart	E	of	this	part	and	shall	between	required	inspections,	except	as provided	in	paragraph	(c)	of	this	section,	have	discrepancies	repaired	as	prescri bed	in	part	43	of	this	chapter... ” and	others	shall	inspect	or	maintain	the aircraft in	compliance	with	Part	43. Mark	Davies	Media proposes	that the	maintenance	of	the	sUAS	will	be	accomplished	by	the	owner/operator	according	to	the	operation	manual. As	provided	in	the	attached	manuals , the	operator	will	ensure	that	the	sUAS	is	in working	order	prior	to initiating flight ,	perform	required	maintenance,	and	keep	a	log	of	any	maintenance	that	is	performed. Moreover,	the	operator	is	the	person	most	familiar	with	the aircraft and	is	best	suited	to	maintain	the aircraft in	an	airworthy	c ondition	thereby	ensuring	an	equivalent	level	of	safety. See	e.g. ,	Grant	of	Exemption	No. 11671	to	Dronair	Solutions	(FAA

– 2015

– 0648	page	15)

PUBLIC	INTEREST

A pproval	of	the	exemptions	requested	in	this petition	is in	the	public’s	interest	due	to the	w ide	array	of applications	and	safety	enha ncements	that	sUAS	operations	off er	to	a	variety	of	existing	and	future	markets. Many	of	the	current flight operations	that	are	addressed	using	manned	civil aircraft can	be	performed	by sUAS with	reduced	environment al	impact,	lower	cost,	and	increased	safety.

The sUAS	is	smaller	and	weighs	considerably	less	than	manned	civil aircraft

.
• Reduces	hazard	to	property,	livestock,	and	the	general	population.

• Th e	sUAS	can	operate	in	smaller	areas	not	possible	with	large aircraft

. The sUAS	uses	batterie s	rather	than	combustible	fuel.

• Reduces	environmental	impact	by	eliminating	hydrocarbon	emissions.

• Non

- fl ammable	power	source	reduces fi re	risk.
The sUAS	does	not	require	onboard	crew	members fl ying	at	low	altitudes.

• R educes	risk	of	injury	to flight operations	personnel.

P roviding	safe	and	valuable	services as	described in	this	petition	are in	the	public’s	interest.

### Mark	Davies	Media would	like	to	thank	the	FAA	for	considering	this	request. Respectfully	Submitted,

Mark	Davies Mark	Davies	Media,	LLC 12	Grandview	Ave Lawrenceville,	NJ	08648

- 1034

/s/ Mark	Davies December	16,	2015

SUMMARY	OF	SECTION	333	EXEMPTION	REQUEST

### Mark	Davies	Media ,	LLC,	hereby	provides,	pursuant	to	14	C.F.R.	Part	11	Subpart	A	§11.81,	a	summary	of	our exemption	petition	to	allow	commercial	operation	of	sUAS	for	aerial	video	and	photography,	precision	aerial mapping,	3D modeling ,	surveying,	cataloguing,	and	inspectio n	services. Granting	this	exemption	will benefi t both	public and	governmental	sectors	including :

• Agriculture

• Land	Planning	&	Development

• Local	Infrastructure

• Solar	Power

• Power	Generation	and	Distribution

• Architecture	and	Engineering

• Environmental

• Search	&	Rescue
Mark	Davies	Media is	poised	to	provide	service	in	support	of	these	and	future	applications	with	the	utmost attention	to	quality	and	safety. Th erefore,	we	respectfully	request	exemption	from	the	following	regulations:

• 14	C.F.R.	Part	21	Subpart	H Certification	Procedures	for Products	and	Parts

– Airworthiness Certificates.

• 14 C.F.R.	Part	36	Subpart	A,	F	&	O Noise	Standards:	Aircraft	Type	and Airworthiness	Certification.

• 14	C.F.R.	§45.23	(b) Display	of Marks;	General.

• 14	C.F.R.	§61.113	(a)	&	(b) Private	Pilot	Privileges	and Limitations:	Pilot	In	Command.

• 14	C.F.R.	§91.7	(a) Civil	Aircraft	Airworthiness.

• 14	C.F.R.	§91.9	(b)	(2) Civil	Aircraft	Flight	Manual, Marking,	and	Placard Requirements.

• 14 C.F.R.	§91.103(b)(2) General	Operating	and	Flight	Rules

- Preflight	Action.

• 14	C.F.R.	§91.109 Flight	Instruction;	Simulated Instrument	Flight	and	Certain Flight	Tests. • 14	C.F.R.	§91.119 General	Operating	and	Flight	Rules

- Minimum	Safe	Altitudes.

• 14 C.F.R.	§91.121 General	Operating	and	Flight	Rules

- Altimeter	settings.

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

• 14	C.F.R.	§91.203	(a) &	(b) Civil	Aircraft	:	Certifications Required.

• 14	C.F.R.	§91.405	(a) Maintenance	Re quired.

• 14	C.F.R.	§91.407	(a) (1) Operation	After	Maintenance, Rebuilding,	or	Alteration.

• 14	C.F.R.	§91.409	(a) (2) Inspections.

• 14	C.F.R.	§91.417	(a) &	(b) Maintenance	Records.

sUAS	User	Manuals3DR	SOLO	user	manual https://3drobotics.com/wp

- content/uploads/2015/07/v4_07_07_15.pdf
3DR	X8	PLUS	user	manual https://3drobotics.com/wp

- content/uploads/2015/04/X8

- Operation

- Manual

- vC.pdf DJI	FLAME	WHEEL	F330	User_Manual_v1.6_en http://dl.djicdn.com/downloads/flamewhe el/en/F330_User_Manual_v1.6_en.pdf DJI	FLAME	WHEEL	F450	User_Manual_v2.2_en http://dl.djicdn.com/downloads/flamewheel/en/F450_User_Manual_v2.1_en.pdf DJI	FLAME	WHEE L	F550	User_Manual_v2.0_en http://dl.djicdn.com/downloads/flamewheel/en/F550_User_Manual_v1.8_en.pdf DJI	INSPIRE	1	PRO	User	Manual_en_v1.0_1201 www.dji.com/product/inspire

- 1

- pro - and

- raw DJI	INSPIRE	1	User	Manual_V1.8 https://dl.djicdn.com/d ownloads/inspire_1/en/Inspire%20_1_User_Manual__V1.8.pdf DJI	MATRICE	100	User	Manual_v1.4_en https://developer.dji.com/matrice

- 100 DJI	PHANTOM	2	VISION_PLUS	User	Manual_v1.8_en http://www.dji.com/product/phantom

- 2

- vision

- plus DJI	PHANTOM	3	PROFESSIONAL	User	Manual_V1.6 http://www.dji.com/product/phantom

- 3 DJI	PHANTOM	3	STANDARD	User Manual_V1.4 http://www.dji.com/product/phantom

- 3

- standard DJI	SPREADING	WINGS	S900	User	Manual_v1.2_en http://www.dji.com/product /spreading

- wings

- s900 DJI	SPREADING	WINGS	S1000	User	Manual_v1.10_en http://dl.djicdn.com/downloads/s1000/en/S1000_User_Manual_v1.10_en.pdf DJI	SPREADING	WINGS	S1000_P LUS	User	Manual_v1.2_en http://www.dji.com/product/spreading

- wings

- s1000

- plus
YUNEEC	TORNADO	H920	A5	user_manual https://www.yuneec.com/download/manuals/TORNADO

- H920

- User

- Manual

- A5

- (NO

- SONY7)

- 20151019.pdf YUNEEC	TYPHOON	4K	q500_4k_user_manual https://www.yuneec.com/download/manuals/q500_4k_user_manual.pdf YUNEEC	TYPHOON	Q500	PLUS	user_manual https://www.yuneec.com/download/manuals/typhoon_q500plus_user_manual_v2.0.pdf YUNEEC	TYPHOON	Q500	user_manual https://www.yuneec.com/download/manuals/typhoon _q500_instruction_manual_v2.1.pdf71 

# 11 Appendix

11.1 Specifications
Solo is a quad-rotor aerial vehicle powered by the 3DR Pixhawk 2 autopilot system and APM:Copter flight control software. Solo communicates with the controller and Solo app over the 3DR Link secure Wi-Fi connection.

Autopilot: 3DR Pixhawk 2 Flight code: ArduPilot Copter Control: 3DR Solo Controller Wireless communication: 3DR Link 1.0 Frequency: 2.4 GHz Height: 10 in. (25 cm) Motor-to-motor dimension: 18 in. (26 cm) Propulsion: 880 K V 

### motors, two clockwise rotating motors and two counterclockwise rotating motors Propeller: 10 in. x 4.5 in. (25 cm x 11.4 cm) Weight with battery: 3.3 lbs. (1.5 kg) Controller battery life: 3 hours Extended controller battery life: 6 hours Controller battery: Li-ion 2600 mAh 7.2 Vdc (5200 mAh for extended battery) Power: Electric (rechargeable lithium polymer battery) Battery: Lithium polymer, 5200 mAh, 14.8 Vdc Battery weight: 1 lb. (.5 kg) Estimated flight time: 25 minutes*
Maximum altitude: 328 ft. (100 m) Range: .5 miles** (.8 km) Payload capacity: 1.1 lbs. (500 g) Cruise speed: 5.7 mph (2.5 m/s) Maximum speed: 55 mph (25.5 m/s) Maximum climb rate: 11 mph (5.0 m/s) Maximum descent rate: 5.5 mph (2.5 m/s) Headwind limitation: 25 mph (11 m/s) Crosswind limitation: 25 mph (11 m/s)
Camera: Streaming video compatible with GoPro® HERO 3, 3+ or 4 Full compatibility with GoPro® HERO 4 Solo app compatibility: iOS 8.0 or later / Android 4.3 or later Operating temperature: 32° F - 113° F (0° C - 45° C) Operating relative humidity: 0-85% RH

*Flight time varies with payload, wind conditions, elevation, temperature, humidity, flying style, and pilot skill. Listed flight time applies to elevations less than 2,000 ft above sea level. **Range varies with location, antenna orientation, background noise and multi-path.33SpecsBattery:4S 14.8V 10,000 mAh 10CBattery Dimensions:6.6 in x 2.6 in x 1.4 in (16.7 cm x 6.5 cm x 3.5 cm)Battery Weight:803 gAutopilot Hardware:Pixhawk v2.4.5Autopilot Firmware:ArduCopter 3.2GPS:3DR u-blox GPS with Compass (LEA-6H module, 5 Hz update)Ground Station Radio:3DR Radio v2 (915 MHz or 433 MHz)Motors:SunnySky V2216-12 KV800 IIFrame Type:XPropellers:APC Propeller 11x4.7 SF (4)APC Propeller 11x4.7 SFP (4)Vehicle Dimensions:13.7 in x 20.1 in x 11.8 in (35 cm x 51 cm x 20 cm)Payload Capacity:800 g (1.7 lbs)Vehicle Weight with Battery:2.56 kg (5.6 lbs)Maximum Altitude*:100 mRange*:300 m from launch point (1 km when geofence disabled)Maximum Estimated Flight Time:15 min*While geofence enabled (default)

## www.altusuas.com+ 

# DELTA X8 – Industrial Grade Survey Multirotor
Wingspan (propellers fitted) 140cm (55”) Motors 8 x 400kV Propellors 8 x 18” Battery type LiPo 6S, 22V, 16,000/22,000mAh Empty Weight 5.5kg (12 lb ) Takeo ff Weight 9.5kg (21 lb ) Max Takeo ff Weight 22.5kg (49 lb) Max climb rate (under AP) 2 m/s (6.6ft/s) Max descent rate (under AP) 2 m/s (6.6ft/s) Maximum speed (under AP) 12 m/s (27mph) Endurance (with Payload) 10-14 minutes Command and Control Frequency 2.4Ghz ( Spektrum DSMX modulation) Telemetry (WiFi) 2.4Ghz (meets Directive 1999/5/EC specs) Telemetry (Datalink) 915-928 Mhz FHSS (complies with AS/NZS 4268:2012) 868-869 MHz FHSS Failsafes Automatic Return to Home on Command & Control Failure Automatic Parachute deployment at 70 degrees of roll Automatic Parachute deployment on violent shake state Automatic Parachute deployment on power loss Dual AP, GPS and IMU for comparison checks X-8/LRX: Motor redundancy configuration Wind Speed (max tolerance) 16 m/s (35mph) Minimum Air Temp -5° C (23° F) Maximum Air Temp 50° C (122° F) Humidity 0% to 95% Visibility 400m + Prohibited Environmental Conditions Heavy Rain (gimbal sensor is the limiting factor), Snow, Fog©2012 DJI Innovation s . All Rights Reserved. 

### 7 

# ESC Sound Introduction

ESC State Sound Ready ♪1234567
Throttle stick is not at bottom BBBBBB... Input signal abnormal B

-------- B

-------- B... Input voltage abnormal BB

--- BB

--- BB

--- BB... 

### Tips: DJI ESCs are specially designed for multi

- rotors. When use with DJI autopilot systems, you do not
have to setup any parameters or calibrate travel range. 

# Specifications

Frame Diagonal Wheelbase 330 mm Frame Weight 156 g Takeoff Weight 6 00g ~ 1 2 00g 

### ESC
Current 18 A OPTO Signal Frequency 30Hz ~ 45 0 Hz Battery 3S ~ 4 S LiPo 

### Motor
Stator size 22 × 1 2 mm KV 9 20 rpm/V Propeller 8 × 4.5inFlameWheel 450 User Manual

8 © 2015 DJI. All Rights Reserved. Note that arms 12 point to the nose of aircraft and arms 34 point to the tail of

aircraft. It is recommended to choose the same color arms for the same direction. See from top, motors on arms 13 rotate counter-clock wise and motors on arms 24 rotate clock wise.



# Specifications

Frame Diagonal Wheelbase 450 mm Frame Weight 282 g Takeoff Weight 800 g ~ 1600 g ESC Max Allowable Voltage 17.4 V Max Allowable Current (Persistent) 20 A Max Allowable Peak Current (3 seconds) 30 A PWM Input Signal Level 3.3 V / 5 V Compatible Signal Frequency 30 Hz ~ 450 Hz Battery 3 S ~ 4S LiPo Weight (without cable) 12.5 g Weigh (with cable) 27 g Motor Stator size 23 × 12 mm KV 960 rpm/V Weight 57 g Propeller Diameter / Thread Pitch 24 × 12.7 cm (9.4 × 5.0inch) Weight (Single) 13 g Normal Description

1234 Ready Abnormal Description BBBBBB
... No signal input, or throttle stick is not in the bottom position

Y ou can instantly tell what the unit ’ s status is by listening to the sounds emitted from the ESC. 

# ESC Sound DescriptionFlameWheel 550 User Manual

8 © 2015 DJI. All Rights Reserved. Note that arms 12 point to the nose of aircraft and arms 45 point to the tail of

aircraft. It is recommended to choose the same color arms for the same direction. See from top, motors on arms 135 rotate counter-clock wise and motors on arms 246 rotate clock wise.



# Specifications

Frame Diagonal Wheelbase 550 mm Frame Weight 478 g Takeoff Weight 1200 g ~ 2400 g ESC Max Allowable Voltage 17.4 V Max Allowable Current (Persistent) 20 A Max Allowable Peak Current (3 seconds) 30 A PWM Input Signal Level 3.3 V / 5 V Compatible Signal Frequency 30 Hz ~ 450 Hz Battery 3 S ~ 4S LiPo Weight (without cable) 12.5 g Weigh (with cable) 27 g Motor Stator size 23 × 12 mm KV 960 rpm/V Weight 57 g Propeller Diameter / Thread Pitch 9.4 × 5.0 inch Weight (Single) 13 g 

# ESC Sound Description
Normal Description

1234 Ready Abnormal Description BBBBBB
... No signal input, or throttle stick is not in the bottom position

Y ou can instantly tell what the unit ’ s status is by listening to the sounds emitted from the ESC.62 © 2015 DJI. All Rights Reserved. 

## Appendix Specifcations

Aircraft Model T600 Weight 2870 g (Battery and propellers included, Zenmuse X5 excluded) 3400 g (Battery, propellers and Zenmuse X5 included) Max Takeoff Weight 3500 g
Hovering Accuracy (P Mode) Vertical: 0.5 m Horizontal: 2.5 m
Max Angular Velocity Pitch: 300°/s Yaw: 150°/s Max Tilt Angle 35° Max Ascent Speed 5 m/s Max Descent Speed 4 m/s Max Speed 18 m/s (ATTI mode, no wind) Max Service Ceiling Above Sea Level 4,500 m (Software altitude limit: 120 m above takeoff point)
Max Wind Speed Resistance 10 m/s Max Flight Time Approx. 15 minutes Motor Model DJI 3510H Propeller Model DJI 1345T Indoor Hovering Enabled by default Operating Temperature 14° to 104° F (-10° to 40° C) Diagonal Distance 559 mm Gimbal and Camera General Name Zenmuse X5 Dimensions 120 (W) x 135 (H) x 140 (D) mm Weight 530 g (Including original lens, balancing ring, lens hood, Micr o SD card) Operating Temperature 32° to 104° F (0° to 40° C) Camera

Lens Replaceable lens M43 mount supporting auto-focus

Supported Lenses DJI MFT 15mm f/1.7 ASPH Panasonic Lumix G Leica DG Summilux 15mm f/1.7 ASPH Olympus M.Zuiko Digital ED 12mm f/2.0 Olympus M.Zuiko 17mm f/1.8 (Balancing ring will be available on the DJI Store soon)© 2015 DJI. All Rights Reserved. 63 INSPIRE 1 PRO User Manual

Sensor Type 4/3 CMOS sensor Effective Pixels 16 M Max Resolution 4608x3456 ISO Range 100-25600 Electronic Shutter Speed 8 s-1/8000 s Field of View DJI MFT 15mm f/1.7 ASPH 72°

Still Photography Modes Single shot Burst shooting:3/5/7 frames Auto Exposure Bracketing (AEB):3/5 bracketed frames at 0.7EV bias Timelapse (3/5/7/10/20/30/60 sec)

Video Resolution UHD:4K (4096×2160) 24/25p, 4K (3840×2160) 24/25/30p, 2.7K (2704×1520) 24/25/30p; FHD:1920×1080 24/25/30/48/50/60p Max Video Bitrate 60 Mbps Supported File Systems FAT32 (≤ 32 GB), exFAT (> 32 GB) Photo Formats JPEG, DNG (RAW) Video Formats MP4/MOV (MPEG-4 AVC/H.264) Supported Storage Devices Class 10 or UHS-1 or above Micro SD cards Max capacity of 64 GB Default Lens Name DJI MFT 15mm f/1.7 ASPH Focal Length f=15 mm (35 mm format equivalent 30 mm) Aperture Type 7 diaphragm blades/circular aperture diaphragm Maximum Aperture F1.7 Minimum Aperture F16 Lens Construction 9 elements in 7 groups (3 aspherical lenses) In Focus Distance 0.2 m to ∞ (from the focus distance reference line) Mount Micro Four Thirds Mount Angle of View 72° Max Diameter Approx. 2.26 inches (57.5 mm) Overall Length Approx. 1.42 inches (36 mm) Weight Approx. 115 g Gimbal Angular Vibration Range ±0.02° Mount Detachable Controllable Range Pitch:-90° to +30° Pan:±320° Max Controllable Speed Pitch:120°/s Pan:180°/s64 © 2015 DJI. All Rights Reserved. INSPIRE 1 PRO User Manual

Remote Controller Name C1 Operating Frequency 922.7MHz~927.7 MHz (Japan Only) 5.725~5.825 GHz;2.400~2.483 GHz
Max Transmitting Distance FCC Compliant: 3.1 miles (5 km); CE Compliant: 2.1 miles (3.5 km) (unobstructed, free of interference) EIRP 10 dBm@900 MHz, 13 dBm@5.8 GHz, 20 dBm@2.4 GHz Video Output Ports USB, Mini HDMI Power Supply Built-in battery Charging DJI charger Dual User Capability Host-and-Slave connection Mobile Device Holder Tablet or Smart Phone Max Mobile Device Width 170 mm Output Power 9 W Operating Temperature 14° to 104° F (-10° to 40° C) Storage Temperature Less than 3 months: -4° to 113° F (-20° to 45° C) More than 3 months: 72° to 82° F (22° to 28° C) Charging Temperature 32° to 104° F (0° to 40° C) Battery 6000 mAh 2S LiPo Charger Model A14-100P1A Voltage 26.3 V Rated Power 100 W Battery (Standard) Name Intelligent Flight Battery Model TB47 Capacity 4500 mAh Voltage 22.2 V Battery Type 6S LiPo High voltage battery Energy 99.9 Wh Net Weight 570 g Operating Temperature 14° to 104° F (-10° to 40° C) Storage Temperature Less than 3 months: -4° to 113° F (-20° to 45° C) More than 3 months: 72° to 82° F (22° to 28° C) Charging Temperature 32° to 104° F (0° to 40° C) Max Charging Power 180 W Battery (Optional) Name Intelligent Flight Battery© 2015 DJI. All Rights Reserved. 65 INSPIRE 1 PRO User Manual

Model TB48 Capacity 5700 mAh Voltage 22.8 V Battery Type 6S LiPo High voltage battery Energy 129.96 Wh Net Weight 670 g Operating Temperature 14° to 104° F (-10° to 40° C) Storage Temperature Less than 3 months: -4° to 113° F (-20° to 45° C) More than 3 months: 72° to 82° F (22° to 28° C) Charging Temperature 32° to 104° F (0° to 40° C) Max Charging Power 180 W Max Flight Time Approx. 18 minutes Vision Positioning Velocity Range < 8 m/s @altitude 6.56 feet (2 m) Altitude Range 0.16 - 16.4 feet (5-500 cm) Operating Environment Surfaces with clear patterns and adequate lighting (> 15 lux) Operating Range < 9.84 feet (300 cm) DJI GO App Mobile Device System Requirements iOS 8.0 (or later) and Android 4.1.2 (or later)

Supported Mobile Devices Compatible with iPhone 5s, iPhone 6, iPhone 6 Plus, iPad Air, i Pad Air Wi-Fi + Cellular, iPad mini 2, iPad mini 2 Wi-Fi + Cellular, iP ad Air 2, iPad Air 2 Wi-Fi + Cellular, iPad mini 3, and iPad mini 3 Wi-Fi + Cellular. This app is optimized for iPhone 5s, iPhone 6, and iPhone 6 Plu s. Compatible with Samsung tabs 705c, Samsung S6, Samsung S5, Samsung NOTE4, Samsung NOTE3, Google Nexus 9, Google Nexus 7 II, Ascend Mate7, Huawei P8 Max, Nubia Z7 mini, SONY Z3 EXPERIA, MI 3, MI PAD, Smartisan T1. *Support for additional Android devices available as testing and development continues.
Aircraft Status Indicator Description

Normal Red, Green and Yellow Flash Alternatively Power on and self-check Green and Yellow Flash Alternatively Aircraft warming up Green Flashes Slowly Safe to Fly (P mode with GPS and Vision Positioning)
X2 Green Flashes Twice Safe to Fly (P mode with Vision Positioning but without GPS) Yellow Flashes Slowly Safe to Fly (A mode but No GPS and Vision Positioning)© 2015 DJI. All Rights Reserved. 57Appendix 

## Appendix Specifcations

Aircraft Model T600 Weight (Battery Included) 2935 g
Hovering Accuracy (P Mode) Vertical: 0.5 m Horizontal: 2.5 m
Max Angular Velocity Pitch: 300°/s Yaw: 150°/s Max Tilt Angle 35° Max Ascent Speed 5 m/s Max Descent Speed 4 m/s Max Speed 22 m/s (ATTI mode, no wind) Max Service Ceiling Above Sea Level 4,500 m (Software altitude limit: 120 m above takeoff point) Max Wind Speed Resistance 10 m/s Max Flight Time Approximately 18 minutes Motor Model DJI 3510 Propeller Model DJI 1345 Indoor Hovering Enabled by default Operating Temperature Range -10° to 40° C Diagonal Distance 559 to 581 mm Dimensions 438x451x301 mm Gimbal Model ZENMUSE X3 Output Power (With Camera) Static: 9 W; In Motion: 11 W Operating Current Station: 750 mA; Motion: 900 mA Angular Vibration Range ±0.03° Mounting Detachable
Controllable Range Pitch: -90° to +30° Pan: ±320°
Mechanical Range Pitch: -125° to +45° Pan: ±330°
Max Controllable Speed Pitch: 120°/s Pan: 180°/s58 © 2015 DJI. All Rights Reserved.Appendix INSPIRE 1 User Manual

Camera Name X3 Model FC350 Total Pixels 12.76M Effective Pixels 12.4M Image Max Size 4000x3000 ISO Range 100-3200 (video) 100-1600 (photo) Electronic Shutter Speed 8 s to 1/8000 s FOV (Field Of View) 94° CMOS Sony EXMOR 1/2.3”

Lens 20mm (35mm format equivalent) f/2.8 focus at ) 9 Elements in 9 groups Anti-distortion

Still Photography Modes Single shoot Burst shooting: 3/5/7 frames Auto Exposure Bracketing (AEB): 3/5 bracketed frames at 0.7EV Bias Time-lapse

Video Recording Modes UHD (4K): 4096x2160p24/25, 3840x2160p24/25/30 FHD: 1920x1080p24/25/30/48/50/60 HD: 1280x720p24/25/30/48/50/60 Max Bitrate Of Video Storage 60 Mbps

Supported File Formats FAT32/exFAT Photo: JPEG, DNG Video: MP4/MOV (MPEG-4 AVC/H.264)
Supported SD Card Types Micro SD Max capacity: 64 GB. Class 10 or UHS-1 rating required. Operating Temperature Range 0° to 40° C Remote Controller Name C1
Operating Frequency 922.7MHz~927.7 MHz (Japan Only) 5.725~5.825 GHz;2.400~2.483 GHz

Transmitting Distance Up to 5.0 km or 3.1 miles (unobstructed, free of interferences and FCC compliant) when it is FCC compliant. Up to 3.5 km or 2.1 miles (unobstructed, free of interferences) when it is CE compliant. EIRP 10dBm@900m, 13dBm@5.8G, 20dBm@2.4G Video Output Port USB, Mini-HDMI© 2015 DJI. All Rights Reserved. 59Appendix INSPIRE 1 User Manual

Power Supply Built-in battery Charging DJI charger Dual User Capability Host-and-Slave connection Mobile Device Holder Tablet or Smart Phone Output Power 9 W Operating Temperature Range -10° to 40° C
Storage Temperature Range Less than 3 months: -20° to 45° C More than 3 months: 22° to 28° C Charging Temperature Range 0-40° C Battery 6000 mAh LiPo 2S Charger Model A14-100P1A Voltage 26.3 V Rated Power 100 W Battery (Standard) Name Intelligent Flight Battery Model TB47 Capacity 4500 mAh Voltage 22.2 V Battery Type LiPo 6S High voltage battery Energy 99.9 Wh Net Weight 570 g Operating Temperature Range -10° to 40° C
Storage Temperature Range Less than 3 months: -20° to 45° C More than 3 months: 22° C to 28° C Charging Temperature Range 0° to 40° C Max Charging Power 180 W Battery (Optional) Name Intelligent Flight Battery Model TB48 Capacity 5700 mAh Voltage 22.8 V Battery Type LiPo 6S Energy 129.96 Wh Net Weight 670 g Operating Temperature Range -10 to 40° C60 © 2015 DJI. All Rights Reserved.Appendix INSPIRE 1 User Manual

Storage Temperature Range Less than 3 months: -20 to 45° C More than 3 months: 22° to 28° C Charging Temperature Range 0° to 40° C Max Charging Power 180 W Vision Positioning Velocity Range Below 8 m/s (2 m above ground) Altitude Range 5-500 cm Operating Environment Brightly lit (lux > 15) patterned surfaces Operating Range 0-300 cm DJI GO App Mobile Device System Requirements iOS version 7.1 or later; Android version 4.1.2 or later

Supported Mobile Devices * iPhone 6 Plus, iPhone 6, iPhone 5S, iPad Air 2, iPad Mini 3, iPad Air, iPad Mini 2, iPad 4;* Samsung Note 3, Samsung S5, Sony Z3 EXPERIA;* Note: It is recommended that you use a tablet for the best experience



### Intelligent Flight Intelligent Flight mode includes Course Lock, Home Lock, Point of Interest (POI), Follow Me and Waypoints features to assist users to create professional shoots during the fight. Course Lock and Home Point lock helps to lock the orientation of aircraft so that the user can focus more on other operations.Point of Interest, Follow Me and Waypoints mode enable aircraft to fy automatically according to the preset fight maneuvers.

Course Lock Lock the current nose direction as the aircraft’s forward direction. The aircraft will move in the locked directions regardless of its orientation (yaw angle).

Home Lock Pull the pitch stick backward to move the aircraft toward its recorderd Home Point.

Point of Interest The aircraft will orbit around the subject automatically to allow the operator can be more focus on framing their shoot on the subject in Point of Interest.

Waypoints Record a fight path, then the aircraft will fy along the same path repeatedly while you control the camera and orientation. The fight path can be saved and re-apply in the future.
Enable Multiple Flight Mode by launching the DJI GO app > Camera View > > Advanced Settings > Mulitple Flight Mode before using the Intelligent Flight Mode f or the frst time.© 2015 DJI. All Rights Reserved. 61 

## Appendix Product Specifcations

Structure Diagonal Wheelbase 650 mm Weight (with TB47D battery) 2355 g Weight (with TB48D battery) 2431 g Max Takeoff Weight 3400 g Optional Accessories Expansion Bay Weight 45 g Battery Compartment Weight 160 g Zenmuse X3 Gimbal with Camera Weight 247 g Performance Hovering Accuracy (P-Mode, with GPS) Vertical: 0.5 m, Horizontal: 2.5 m Max Angular Velocity Pitch: 300°/s, Yaw: 150°/s Max Pitch Angle 35° Max Speed of Ascent 5 m/s Max Speed of Descent 4 m/s Max Wind Resistance 10 m/s
Max Speed 22 m/s (ATTI mode, no payload, no wind) 17 m/s (GPS mode, no payload, no wind)
Hovering Time (with TB47D battery) No payload: 22 min; 500g payload: 17 min; 1kg payload: 13 min
Hovering Time (with TB48D battery) No payload: 28 min; 500g payload: 20 min; 1kg payload: 16 min Hovering Time (with two TB47D batteries) No payload: 33 min Hovering Time (with two TB48D batteries) No payload: 40 min Hovering Time (with TB47D battery and Zenmuse X3) No payload: 19 min Hovering Time (with TB48D battery and Zenmuse X3) No payload: 23 min

* The hovering time is based on fying at 10m above sea level in a no-wind environment and landing

with 10% battery level.62 © 2015 DJI. All Rights Reserved. DJI MATRICE 100 User Manual

Propulsion System Motor Model DJI 3510 Propeller Model DJI 1345s ESC Model DJI E SERIES 620D Flight Control System Model N1 Other Operating Temperature -10 to 40 °C Remote Controller Name C1

Operating Frequency 5.725~5.825 GHz 922.7MHz~927.7 MHz (Japan) 2.400~2.483 GHz (Lightbridge) Max Transmission Distance (unobstructed, free of interference) FCC Compliant: 3.1 miles (5 km) CE Compliant: 2.1 miles (3.5 km)

EIRP 10dBm@900M 13dBm@5.8G 20dBm@2.4G Video Output USB, Mini-HDMI Power Supply Built-in battery Charger DJI approved charger Dual Users Capability Master-and-Slave control Mobile Device Holder Supports smartphones and tablets Output Power 9 W Operating Temperature -10 to 40 °C
Storage Temperature < 3 months: -20 to 45 °C

> 3 months: 22 to 28 °C Charging Temperature 0 to 40 °C Battery 6000 mAh LiPo 2S Max Tablet Width 170 mm Charger Model A14-100P1A Voltage Output 26.3 V Power Rating 100 W Battery (Standard) Name Intelligent Flight Battery Model TB47D Capacity 4500 mAh© 2015 DJI. All Rights Reserved. 63 DJI MATRICE 100 User Manual

Voltage 22.2 V Type LiPo 6S High voltage battery Energy 99.9 Wh Net Weight 600 g Operating Temperature -10 to 40 °C
Storage Temperature < 3 months: -20 to 45 °C

> 3 months: 22 to 28 °C Charging Temperature 0 to 40 °C Max Charging Power 180 W Battery (Optional) Name Intelligent Flight Battery Model TB48D Capacity 5700 mAh Voltage 22.8 V Type LiPo 6S Energy 129.96 Wh Net Weight 676 g Operating Temperature -10 to 40 °C
Storage Temperature < 3 months: -20 to 45 °C

> 3 months: 22 to 28 °C Charging Temperature 0 to 40 °C Max Charging Power 180 W


### Aircraft Status Indicator Description

Normal Flashing Red, Green and Yellow Alternatively Power on and self-check Flashing Green and Yellow Alternatively Aircraft warming up Flashing Green Slowly Safe to Fly (P-Mode with GPS) Flashing Yellow Slowly Safe to Fly (No GPS)

f 2 Flashing Green Twice at a Time Safe to Fly (P-Mode with the DJI Guidance system but without GPS) Flashing Blue Slowly (Alternates with Safe to Fly pattern) The Obstacle Sensing Mode of the DJI Guidance system is enabled. Warning Flashing Yellow Rapidly Remote controller signal Lost48 © 2015 DJI. All Rights Reserved. 

### Appendix 1 Rear LED Flight Indicator Status

Rear LED Flight Indicators Normal status (Red, Green, Yellow fashes in turn) Power On Self-Test (Green, Yellow fashes in turn) Warming Up (Slow Green fashes) Ready to Fly (Slow Yellow fashes) Ready to Fly (non-GPS) Rear LED Flight Indicators Abnormal status (Quick Yellow fashes) Remote Controller Signal Lost (Slow Red fashes) Low Battery Level Warning (Quick Red fashes) Critical Low Battery Level Warning

(Three Red fashes off and on) Not Stationary or Sensor Bias is too big —— (Solid red) Error* (Red, Yellow fashes in turn) Compass Needs Calibration *You can learn more about error by connecting the Phantom 2 Vision+ to the Assistant. 2 Specifcations

Aircraft Supported Battery DJI 5200mAh Li-Po Battery Weight (Battery & Propellers included) Recommend payload Maximum payload 1242g ≤1300g 1350g Hovering Accuracy (Ready to Fly) Vertical: 0.8m; Horizontal: 2.5m Max Yaw Angular Velocity 200°/s Max Tiltable Angle 35° Max Ascent / Descent Speed Ascent: 6m/s; Descent: 2m/s Max Flight Speed 15m/s (Not Recommended) Motor Diagonal Length 350mm 3-axial stabilized Gimbal Working Current Static : 750mA; Dynamic : 900mA Control Accuracy ±0.03° Controllable Range Pitch :

- 90° - 0° Maximum Angular Speed Pitch : 90°/s Camera Operating Environment Temperature 0°C - 40°C Sensor Size 1/2.3” Effective Pixels 14 Megapixels Resolution 4384×3288 HD Recording 1080p30 /1080i60 Recording FOV 110° / 85°AppendixAppendix

© 2015 DJI. All Rights Reserved. 49 Remote Controller Operating Frequency 5.728 GHz - 5.85 GHz Communication Distance (open area) CE Compliance: 400m; FCC Compliance: 800m Receiver Sensitivity (1%PER) -93dBm Transmitting Power (EIRP) CE Compliance: 25mW; FCC Compliance: 100mW Working Current/Voltage 120mA@3.7V Battery 2000mAh rechargeable LiPo battery Range Extender Operating Frequency 2412MHz - 2462MHz Communication Distance (open area) 500m - 700m Transmitting Power 20dBm Power Consumption 2W
3 Troubleshooting (FAQ)

3.1 How to solve large margin(s) mid-point error? If the Remote Controller stick(s) mid-point margin of error is too big, the motors will fail to start when you execute the CSC and the Phantom will not take off. The below are some possi ble fxes for this. (1) One of the Remote Controller’s stick positions (except the throttle stick) is not centered when powering on the Phantom 2 Vision+. Solution: Place all Remote Controller sticks at their mid-point positions and then power cycle the Phantom 2 Vision+ to re-record the mid-point. (2) The Remote Controller sticks have been trimmed, leading to a de viation in the mid-point position. Solution: Use Assistant to perform a Remote Controller calibrat ion. a) Connect to Assistant, tap Basic -> RC -> Command Sticks Calibration and push all Remote Controller sticks

through their complete travel range to see if any stick cannot reach its outermost position. b) Power cycle the Phantom 2 Vision+. Power cycling is required. c) Re-attempt Remote Controller calibration in Assistant. If the above solutions do not solve your issue, please send you r Remote Controller to DJI Customer service for repair.
3.2 How to restore a video fle if power is turned off during a recording session? Solution: Keep or place the Micro-SD card back into the camera. Power cycle the camera and wait about 30 seconds for the video fle to be restored.
3.3 Failure to acquire the SSID. Solution: Double check whether both the camera and Range Extender are powered on and the power switch of the camera is switched to “Wi-Fi ON.”
3.4 What to do if Phantom 2 Vision+ is out of sight and the Wi-Fi connections is lost? Solution: Turn off the Remote Controller to trigger the Failsafe mode and the aircraft will start to fy back, descend, and land at the Home point. Please make sure there are no obstacles between the Phantom and the home point and that you are familiar with the procedure for regaining control.
3.5 Wi-Fi connection fails all the time. Solution: Double check the current Wi-Fi connection status of the mobile device. The mobile device may be connecting to other Wi-Fi networks after a connection breaks with the Phan tom 2 Vision+.
3.6 Files fail to synchronize. Solution: Video fles that are too large (fle sizes close to 4GB) cannot be synchronized to the mobile device. Some mobile devices do not support the synchronization of the 1080i6 0 video fles.Appendix54 © 2015 DJI. All Rights Reserved.Appendix 

## Appendix Specifcations

Aircraft Weight (Battery & Propellers Included) 1280 g Max. Ascent Speed 5 m/s Max. Descent Speed 3 m/s Max. Speed 16 m/s (ATTI mode, no wind) Max Service Ceiling Above Sea Level 6000 m (Software altitude limit: 120 m above takeoff point) Max. Flight Time Approximately 23 minutes Operating Temperature 0°C to 40°C GPS Mode GPS/GLONASS Gimbal Controllable Range Pitch: - 90° to + 30° Vision Positioning Velocity Range < 8 m/s (2 m above ground) Altitude Range 30 cm-300 cm Operating Range 30 cm-300 cm Operating Environment Brightly lit (lux > 15) patterned surfaces Camera Sensor Sony EXMOR 1/2.3” Effective pixels:12.4 M (total pixels: 12.76 M) Lens FOV 94° 20mm(35mm format equivalent ) f/2.8 ISO Range 100-3200(video) 100-1600(photo) Electronic Shutter Speed 8s -1/8000s Image Max. Size 4000 x 3000

Still Photography Modes Single shot Burst shooting: 3/5/7 frames Auto Exposure Bracketing (AEB): 3/5 Bracketed frames at 0.7EV Bias Time-lapse Supported SD Card Types Micro SD Max. capacity: 64 GB. Class 10 or UHS-1 rating required

Video Recording Modes UHD : 4096x2160p 24/25, 3840x2160p24/25/30 FHD:1920x1080p 24/25/30/48/50/60 HD:1280x720p 24/25/30/48/50/60 Max. Bitrate Of Video Storage 60 Mbps

Supported File Formats FAT32/exFAT Photo: JPEG, DNG Video: MP4/MOV (MPEG-4 AVC/H.264) Operating Temperature Range 0°C to 40°C© 2015 DJI. All Rights Reserved. 55Appendix Phantom 3 Professional User Manual

Remote Controller Operating Frequency 2.400 GHz-2.483 GHz

Transmitting Distance Up to 5.0 km or 3.1 miles (unobstructed, free of interferences and FCC compliant) when it is FCC compliant Up to 3.5 km or 2.1 miles (unobstructed, free of interferences) when it is CE compliant Video Output Port USB Operating Temperature Range 0°C- 40°C Battery 6000 mAh LiPo 2S Mobile Device Holder Tablets and smartphones Transmitter Power(EIRP) FCC: 20 dbm; CE:16 dbm Working Voltage 1.2 A @7.4 V Charger Voltage 17.4 V Rated Power 100 W Intelligent Flight Battery ( PH3-4480 mAh-15.2 V ) Capacity 4480 mAh Voltage 15.2 V Battery Type LiPo 4S Energy 68 Wh Net Weight 365 g Operating Temperature -10°C- 40°C Max. Charging Power 100 W Aircraft Status Indicator Description

Normal Red, Green and Yellow Flash Alternatively Turning on and Self-Diagnostics Green and Yellow Flash Alternatively Aircraft Warming Up Green Flashes Slowly Safe to Fly (P-mode with GPS and Vision Positioning)
X2 Green Flashes Twice Safe to Fly (P-mode with Vision Positioning but without GPS) Yellow Flashes Slowly Safe to Fly (A-mode but No GPS and Vision Positioning) Warning Fast Yellow Flashing Remote Controller Signal Lost Slow Red Flashing Low Battery Warning Fast Red Flashing Critical Battery Warning Red Flashing Alternatively IMU Error

— Solid Red Critical Error Red and Yellow Flash Alternatively Compass Calibration Required50 © 2015 DJI. All Rights Reserved.Appendix 

## Appendix Specifcations

Aircraft Weight (Incl. Battery and Propellers) 1216 g Max Ascent Speed 5 m/s Max Descent Speed 3 m/s Max Speed 16 m/s (A-Mode, no wind) Max Service Ceiling Above Sea Level 6000 m (Software altitude limit: 120 m above takeoff point) Max Flight Time Approx. 25 min Operating Temperature 0° to 40° C GPS System Built-in GPS Gimbal Controllable Range Pitch: -90° to +30° Angular Vibration Range ±0.02° Camera Sensor 1/2.3” Photo Resolution 12 Megapixels Lens 94° FOV, 20 mm (35 mm format equivalent) f/2.8, focus at 

### ∞ ISO Range 100-3200 (video); 100-1600 (photo) Electronic Shutter Speed 8 s -1/8000 s Max Image Size 4000 x 3000 pixels

Still Photography Modes Single shot Photo burst mode: 3/5/7 shots Auto Exposure Bracketing (AEB): 3/5 bracketed frames at 0.7EV bias Time-lapse

Video Recording Modes 2.7K: 2704x1520p30 FHD: 1920x1080p 24/25/30 HD: 1280x720p 24/25/30/48/50/60 Max Video Bitrate 40 Mbps

Supported File Formats FAT32/exFAT Photo: JPEG, DNG Video: MP4/MOV (MPEG-4 AVC/H.264) Supported SD Card Types Micro SD, Max Capacity: 64GB. Class 6 or higher Operating Temperature 0° to 40° C WiFi Operating Frequency 2.400 GHz - 2.483 GHz

Max Transmission Distance FCC: 1000 m ; CE: 500 m (outdoors and unobstructed, aircraft’s altitude at 400 feet/120 m) Transmitter Power (EIRP) FCC: 27 dBm ; CE: 20 dBm© 2015 DJI. All Rights Reserved. 51Appendix Phantom 3 Standard User Manual

Remote Controller Operating Frequency 5.725 GHz - 5.825 GHz
, 922.7 MHz - 927.7 MHz ( Japan )

Max Transmission Distance FCC: 1000 m ; CE: 500 m (outdoors and unobstructed, aircraft’s altitude at 400 feet/120 m) Operating Temperature 0° to 40° C Battery 2600 mAh LiPo 18650 Transmitter Power (EIRP) FCC: 19 dBm ; CE: 14 dBm Operating Voltage 600 mA @ 3.7V Charging Port Micro USB Battery Charger Output Voltage 17.4 V Rated Power 57 W Intelligent Flight Battery (PH3 - 4480 mAh - 15.2 V) Capacity 4480 mAh Voltage 15.2 V Battery Type LiPo 4S Energy 68 Wh Net Weight 365 g Operating Temperature -10° to - 40° C Max Charging Power 100 W
Aircraft Status Indicator Blinking Patterns

Normal Operations Flashes red, green and yellow alternatively Powered on and self-testing Flashes green and yellow alternatively Aircraft warming up Flashes green slowly Safe to Fly (P-Mode with strong GPS signal) Flashes yellow slowly Safe to Fly (A-Mode without GPS signal) Warnings Flashes yellow quickly Remote controller signal lost Flashes red slowly Low Battery Warning Flashes red quickly Critically Low Battery Warning
Flashes red (Alternates with other patterns) IMU eror

— Glows solid red Critical error Flashes red and yellow alternatively Compass calibration required22 © 2014 DJI. All Rights Reserved. 

## Appendix
ESC Sound

ESC State Sound Ready 1234567--B--B Throttle stick is not at bottom BBBBBB... Input signal abnormal B

-------- B

-------- B... Input voltage abnormal BB

--- BB

--- BB

--- BB...


### ESC LED

ESC State LED Standby Off Motor rotating Solid Red or Green On Motor rotating at full throttle position Solid Yellow On

DJI ESCs are specifically designed for multi-rotors. When used with DJI autopilot systems parameters and travel ranges do not have to be calibrated.



### Specifcations

Frame Diagonal Wheelbase 900mm Frame Arm Length 358mm Frame Arm Weight (with Motor, ESC, Propeller ) 316g

Center Frame Diameter 272mm Center Frame Weight (with Landing Gear Mounting Base, Servos) 1185g

Landing Gear Size 460mm(Length)×450mm(Width)×360mm(Height) 

### Motor
Stator Size 41×14mm
KV 400rpm/V
Max Power 500WAppendixSpreading Wings S900 User Manual

© 2014 DJI. All Rights Reserved. 23 Weight (with Cooling Fan) 158g 

### ESC Working Current 40A Working Voltage 6S LiPo Signal Frequency 30Hz ~ 450Hz Drive PWM Frequency 8KHz Weight (with Radiators) 35g 

### Foldable Propeller (1552/1552R)
Material High strength performance engineered plastics
Size 15×5.2 inch Weight 13g 

### Flight Parameters Takeoff Weight 4.7Kg ~ 8.2Kg Total Weight 3.3Kg Power Battery LiPo (6S,10000mAh~15000mAh,15C(Min)) Max Power Consumption 3000W Hovering Power Consumption 1000W (@6.8Kg Takeoff Weight) Hovering Time 18min (@12000mAh & 6.8Kg Takeoff Weight) Working Environment Temperature -10° C ~ 40° C



### Gain Value Settings

Flight Control Basic Attitude
Pitch Roll Yaw Pitch Roll Vertical
A2 110% 110% 120% 220% 220% 120% WooKong-M 160% 160% 160% 190% 190% 100%Appendix© 201 4 DJI. All Rights Reserved. 

### 23 

# Appendix

ESC Sound

ESC State Sound Ready ♪ 1234567

-- B

-- B
Throttle stick is not at bottom BBBBBB... Input signal abnormal B

-------- B

-------- B... Input voltage abnormal BB

--- BB

--- BB

--- BB...



### ESC LED

ESC State LED
S tandby Off Motor rotating Solid Red or Green On Motor rotating at full throttle position Solid Yellow On


### Tips: DJI ESCs are specially designed for multi

- rotors. When use d with DJI autopilot systems parameters and travel ranges do not have to be calibra ted.


### Specifications

Frame Diagonal Wheelbase 1045mm Frame Arm Length 386mm Frame Arm Weight (with Motor, ESC, Propeller ) 325g

Center Frame Diameter 33 7.5 mm Center Frame Weight ( with Landing Gear Mounting Base, Servos ) 1330g

Landing Gear Size 460 mm( Length )×511mm( Width )×3 05 mm( Height ) (Top width: 155 mm ) 

### Motor Stator Size 41×14mm
kV 400rpm/V
Max Power 500W Weight ( with Cooling Fan) 158 g© 201 4 DJI. All Rights Reserved. 

### 24 

### ESC Working Current 40A Working Voltage 6 S LiPo Signal Frequency 30Hz
~ 450Hz Drive PWM Frequency 8 KHz Weight (with Radiators) 35g 

### Foldable Propeller (1552/1552R)
Material High strength performance engineered plastics Size 15×5.2inch Weight 13g 

### Flight Parameters Takeoff Weight 6.0K g ~ 11.0K g Total Weight 4.2Kg Power Battery LiPo (6S 、 10000mAh~20000mAh 、 15C(Min)) Max Power Consumption 4 000 W
Hover ing Power Consumption 15 00 W (@9.5Kg Takeoff Weight)
Hover ing Time 15min (@15000mAh& 9.5Kg Takeoff Weight) Working Environment Temperature

- 10 o C ~ +40 o C



### Gain Value Settings (with the A2 flight control) B asic A ttitude P itch R oll Y aw P itch R oll Y aw 120% 120% 120% 17 0% 17 0% 120%22 © 2014 DJI. All Rights Reserved. 

## Appendix
ESC Sound

ESC State Sound Ready 1234567--B--B Throttle stick is not at bottom BBBBBB... Input signal abnormal B

-------- B

-------- B... Input voltage abnormal BB

--- BB

--- BB

--- BB...


### ESC LED

ESC State LED Standby Off Motor rotating Solid Red or Green On Motor rotating at full throttle position Solid Yellow On

DJI ESCs are specifically designed for multi-rotors. When used with DJI autopilot systems parameters and travel ranges do not have to be calibrated.



### Specifcations

Frame Diagonal Wheelbase 1045mm Frame Arm Length 386mm Frame Arm Weight (with Motor, ESC, Propeller ) 325g

Center Frame Diameter 337mm Center Frame Weight (with Landing Gear Mounting Base, Servos) 1520g

Landing Gear Size 460mm(Length)×511mm(Width)×305mm(Height) 

### Motor
Stator Size 41×14mm
KV 400rpm/V
Max Power 500WAppendixSpreading Wings S1000 + User Manual

© 2014 DJI. All Rights Reserved. 23 Weight (with Cooling Fan) 158g 

### ESC Working Current 40A Working Voltage 6S LiPo Signal Frequency 30Hz ~ 450Hz Drive PWM Frequency 8KHz Weight (with Radiators) 35g 

### Foldable Propeller (1552/1552R)
Material High strength performance engineered plastics
Size 15×5.2 inch Weight 13g 

### Flight Parameters Takeoff Weight 6.0Kg ~ 11.0Kg Total Weight 4.4Kg Power Battery LiPo (6S,10000mAh~20000mAh,15C(Min)) Max Power Consumption 4000W Hovering Power Consumption 1500W (@9.5Kg Takeoff Weight) Hovering Time 15min (@15000mAh & 9.5Kg Takeoff Weight) Working Environment Temperature -10° C ~ 40° C



### Gain Value Settings

Flight Control Basic Attitude
Pitch Roll Yaw Pitch Roll Vertical
A2 120% 120% 120% 170% 170% 120% WooKong-M 130% 130% 100% 180% 180% 100%Appendix

### SPECIFICATIONS

TORNADO H920 Air Time: 24 Minutes (H920/GB603/GH4/2pcs 6S 4,000mAh LiPo) Dimension: 38.1x33.4x18.1in (969x849x461mm) Diagonal Length Without Rotor Blades: 36.2 in(920mm) Propeller/Main Rotor Diameter: 17.3 in (440mm) Take-off Weight with GB603, GH4 Camera and Battery: 176.0 oz (4990g) Battery: LiPo 6s 4000mAh 8C Charger: 100W 2 x output AC-DC Balancing Charger Transmitter: 24-channel 2.4GHz with 5.8GHz video downlink (included) Flight Modes: Smart, Angle and Home Modes Maximum Flying Height (Absolute altitude): 4000m (13123 ft) Maximum Flying Height (Relative altitude): 122m(400 ft) Maximum Rotation Rate: 100°/s Maximum Roll Angle: 35° Maximum Horizontal Speed (GPS ON): 40km/h Radio Control Frequency Band: 2.4GHz Operating Temperature Range:

- 10 °C to 50 °C

ST24 PERSONAL GROUND STATION Operating System: AndroidTM Number of Channels: 24 Control Transmission Distance/Range (Optimum Conditions): Max 2km Robust Radio Control Modulation: Yuneec Protocol Video link Frequency Band: 5.8GHz WiFi Video Transmission Distance/Range (Optimum Conditions): FCC Compliance: Up to 700m ( 2296.59ft ) CE Compliance: Up to 300m (984.25 ft) Flight Systems Telemetry Data On Screen Display (OSD): Yes LED Backlit LCD Screen: 7” Tactile (Vibrating) and Audible Feedback: Yes Built-In LiPo Battery Voltage / Capacity: 1S 3.6V 8700mAh 31.32Wh Li-ion 

### NOTICES AND WARNINGS IMPORTANT NOTE: All safety precautions and warnings, instructions, warranties and other collateral information is subject to change at the sole discretion of Yuneec. For the most up-to-date information please visit the corresponding product page at www.Yuneec.com or contact the nearest Yuneec of f ce or authorized distributor. The following special language terms are used throughout the product literature to indicate various levels of potential harm when operating this product: NOTICE: Procedures, which if not properly followed, create a possibility of property damage and/or little to no possibility of injury. CAUTION: Procedures, which if not properly followed, create the probability of property damage and/or a possibility of serious injury. WARNING: Procedures, which if not properly followed, create the probability of property damage, collateral damage and/or serious injury or create a high probability of super f cial injury. WARNING: Read the ENTIRE quick start guide and instruction manual to become familiar with the features of the product before operating. Failure to operate the product correctly can result in damage to the product, property and/or cause serious injury. WARNING: This is a sophisticated consumer product. It must be operated with caution and common sense, and requires some basic mechanical ability. Failure to operate this product in a safe and responsible manner could result in damage to the product, property and/or cause serious injury. This product is not intended for use by children without direct adult supervision. Do not use with incompatible components or alter this product in any way outside of the instructions provided by Yuneec. The quick start guide and instruction manual contain instructions for safety, operation and maintenance. It is essential to read and follow all the instructions and warnings prior to assembly, setup and/or use in order to operate the product correctly and avoid damage or serious injury. AGE RECOMMENDATION: NOT FOR CHILDREN UNDER 14 YEARS. THIS IS NOT A TOY.



### GENERAL SAFETY PRECAUTIONS AND WARNINGS
WARNING: Failure to use this product in the intended manner as described in the quick start guide and instruction manual can result in damage to the product, property and/or cause serious injury. A Radio Controlled (RC) multirotor aircraft, APV platform, drone, etc. is not a toy! If misused it can cause serious bodily harm and damage to property. WARNING: As the user of this product you are solely and entirely responsible for operating it in a manner that does not endanger yourself and others or result in damage to the product or the property of others. • Keep your hands, face and other parts of your body away from the spinning propellers/rotor blades and other moving parts at all times. Keep items that could impact or become entangled away from the propellers/rotor blades including debris, parts, tools, loose clothing, etc. • Always operate your aircraft in open areas that are free from people, vehicles and other obstructions. Never f y near or above crowds, airports or buildings. • To ensure proper operation and safe f ight performance never attempt to operate your aircraft nearby buildings or other obstructions that do not offer a clear view of the sky and can restrict GPS reception. • Do not attempt to operate your aircraft in areas with potential magnetic and/or radio interference including areas nearby broadcast towers, power transmission stations, high voltage power lines, electrical storms, etc. • Always keep a safe distance in all directions around your aircraft to avoid collisions and/or injury. This aircraft is controlled by a radio signal subject to interference from many sources outside your control. Interference can cause momentary loss of control. • To ensure proper and safe operation of the automatic landing function in Home Mode you must start the motors with the aircraft in a position that has at least 10 feet (approximately 3 meters) of clear and open space around it and achieve a proper GPS lock. • Do not attempt to operate your aircraft with any worn and/or damaged components, parts, etc. (including, but not limited to, damaged propellers/rotor blades, old batteries, etc.). • Never operate your aircraft in poor or severe weather conditions including heavy winds, precipitation, lightning, etc. • Always operate your aircraft starting with a fully charged battery. Always land as soon as possible after the f rst level low voltage battery warning or land immediately after the second level low voltage battery warning (as indicated by the vibrations and audible alerts from the transmitter/personal ground station). • Always operate your aircraft when the voltage of the battery in the transmitter/personal ground station is in a safe range (as indicated by the battery charge status icon on the screen of the transmitter/personal ground station). • Always keep the aircraft in clear line of sight and under control, and keep the transmitter/personal ground station powered on while the aircraft is powered on. • Always move the throttle control stick down fully and turn off the motors in the event the propellers/rotor blades come into contact with any objects. • Always allow components and parts to cool after use before touching them and f ying again. • Always remove batteries after use and store/transport them per the corresponding guidelines. • Avoid water exposure to all electronic components, parts, etc. not speci f cally designed and protected for use in water. Moisture causes damage to electronic components and parts. • Never place any portion of the aircraft or any related accessories, components or parts in your mouth as doing so could cause serious injury or even death. • Always keep chemicals, small parts and electronic components out of the reach of children. • Carefully follow the instructions and warnings included with this aircraft and any related accessories, components or parts (including, but not limited to, chargers, rechargeable batteries, etc.). CAUTION: The electronic speed controls (ESCs) installed in the TORNADO are not compatible with any other product, and the TORNADO is not compatible with any other ESCs. Use of any other ESCs in the TORNADO will cause a crash, which may result in damage to the product, property and/or cause serious injury. 42 

## INTRODUCTION
Change your perspectve with the Yuneec Q500 Typhoon aerial photography and videography (APV) system. The system arrives 100% factory-assembled and test flown including the innovatve 3-axis CGO2-GB that records full HD 1080p (60, 50 or 48 fps) video and takes 12 megapixel stll photos. And the built-in digital video downlink delivers streaming video that can be viewed right on the screen of the included ST10 transmiter and Personal Ground Staton. With the Q500 it’s never been easier to capture amazing photographs and video footage for a wide variety of uses. And although the Q500 is nearly ready to fly right out the box, please take the tme to read through this entre instructon manual for more informaton on safety, batery charging, flight controls and more before making your first flight. Please also visit www.Yuneec.com for additonal informaton including product updates, bulletns, videos and more. 

## SPECIFICTATIONS

Q500 Height: 210mm (8.3 in) Length (without rotor blades): 420mm (16.5 in) Width (without rotor blades): 420mm (16.5 in) Diameter (without rotor blades): 565mm (22.2 in) Propeller/Rotor Blade Diameter: 330mm (13.0 in) Weight (without batery and payload): 1130g (40.0 oz) Takeoff Weight (with batery and CGO2-GB): 1700g (60.0 oz) Batery: 5400mAh 3S 11.1V LiPo (included) Charger: DC 3S 11.1V LiPo balancing and AC adapter (included) Transmiter: ST10 10-channel 2.4GHz with 5.8GHz video link (included) Flight Time: 20-25 minutes CGO2-GB Height: 115mm (4.5 in) Width: 75mm (2.9 in) Depth: 135mm (1.4 in) Weight: 185g (6.5 oz) Video Resoluton: 1080p 60, 50 or 48 fps Photo Resoluton: 12 megapixels Transmission Distance/Range: Up to 600m (1970 f) depending on receiving device Transmission Band: 5.8GHz Storage (memory): microSD Class 10 up to 128GB ST10 Number of Channels: 10 RC Band: 2.4GHz RC Modulaton: Yuneec Video Downlink Band: 5.8GHz Telemetry/OSD: Yes SD Card Compatble: Yes LCD Screen Size: 4.5” Touchscreen: Yes