Ju l y 1 3, 20 1 5 U.S
. D e p artm e nt of T r an spo rt ati o n D ocket M an age me nt System 1 20 0 Ne w J e r sey Ave., SE W as hin gto n , D C 20590


### Petition of C & 

### H Drone Serv ices LL C for Exemption Purs uant to S ection 333 of the FAA Ref o rm Ac t
P e ti t io ne r 's Na me an d Addr ess: C & H Dro n e Ser v i ces LL C Owner : Mario n Stewar t C anty Jr Owner: Geo r ge Hooker Address: P.O. B o x 63 0 9 53 Nac ogdoch es, TX 759 6 3 Email : stewart cant y@ yahoo.com M o bil e P ho ne : 93 6-615-8247

To whom it m ay concern: Pur suant to Section 333 of the FAA Moderni zation and R e form A c t of 2 012 ( the Reform Act) and 14 C. F.R. Part 11 , C & H Drone Servic e s LLC operator of Small Unmanned Aircraft (UAS) equipp e d to conduct ae rial photography and videograph y , hereby applie s for an ex e mption from the li s ted F e deral Avi ation Regulation s ("FAR s ") to allow commercial operation of it s UAS , s o long a s s uch operation s are conducted within and under the conditions out line d h e rein or a s may be established by the FAA a s required by Section 333
. 1
A s describ e d more fully below , the requested exemption would permit the operation of small , unmanned , and relatively inexpen s ive UAS under controlled condition s in air s p ace that i s 1) limited 2) predetermined and 3) controlled
. The propo s ed e x emption , if g ranted , would allow C & H Drone Servic e s LLC to conduct commerci al operation s of UAS

## I
I meeting or exceeding all of the operational and safety requirements Congress has set forth in Section 333. C & H Drone Services LLC is a graphic design and photography company owned and operated by Marion Stewart Canty Jr and George Hooker. Marion Stewart Canty Jr is a Commercial instrument rated Pilot and has serveral years of experience flying RC airplanes. The purpose of C & H Drone Services LLC is to provide aerial photography and video service s for marketing purposes in the areas of East Texas.
C & H Drone Services LLC plans to use the capabilities of UAS to offer a multitude of services , including: • Aerial surveying of properties owned by clients • Architectural and landscape photography • Real Estate and Commercial Real Estate Photography and presentation • Aerial filmmaking and photography Statutory Authority Section 333, titled "Special Rules for Certain Unmanned Aircraft Systems" , provides a mechanism for seeking expedited FAA authorization of safe civil Unmanned Aircraft Systems (UAS) operations in the National Airspace System ("NAS"). Section 333(a) states that the FAA "shall determine if certain unmanned aircraft systems may operate safely in the national airspace system before completion of the (comprehensive) plan and rulemaking required by section 332(b)(l) of this Act or the guidance required by section 334 of this Act." 1n Section 332(b)(l), Congress made it clear that Section 333 provides a mechanism for "expedited operation authorization" if several factors are met. Petitioner meets all requirements to permit FAA approval of commercial UAS operations.

The name and address of the applicant are:Name: C & H Drone Services LLC Owner: Marion Stewart Canty Jr O wner: George Hook er Address: P.O. Box 630953 Phone:936-615-8247 Ema il : s tewartcanty @ya hoo. com
Re gulations fTo m which the exemption is requ ested : 14 C.F. R. Part 2 1 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
. 91.109 14 C.F.R. 91.119 14 C.F. R. 91.121Page 3 14 C.F.R. 91.151(a) 14 C.F
. R. 91.203 (a) & (b) 14 C.F.R. 91.205 (b) 14 C.F.R. 91.215 14 C.F.R. (91.401- 91.417)
UAS are oftentimes seen as superior to helicopters due to the lesser cost of equipment, the reduction of personnel needed to operate equipment, reduced noise levels and zero emissions into the environment. In addition to providing cost savings and having little to no impact on the environment, UAS provide enhanced safety. These factors are beneficial for, and in the best interest of, the public. Accordingly, the applicant respectfully requests that the FAA grant the requested exemption without delay
. Marion Stewart Canty Jr and George Hooker are requesting an exemption to enable C & H Drone Services LLC to operate a Yuneec Typhoon Q500, UAS that ha s b een upgradedto latest vers ion f i rmwa re, eq uipp e d with a 3 ax is stabili zation g imb al , which u ses a High

- Def vi deo camera that ca n capture up to 4K (4096x2160p) video and 12M pix e l photo s. Th i s UAS h as a built-in capability to limit 1 ) th e height it flies above the ground an d 2) the rad iu s of the di s t ance it flie s from the operator. The Yuneec Typhoon Q500 a lso ha s fa il sa fe fu nctio n s of the au topilot system , which means , when the co mmuni catio n between the M ai n Co ntroll er and th e transmitter is di sc onnected, the output of all command s ti ck s fro m co ntroll er will go to the center po s ition
. If the GPS s ignal is good e nough , the sys tem will automatically trigger Return to Home and will l and safel y.
P l ease refer to Attachments! and 2 for the Yuneec Typhoon Q500, for the performance limi tations and flight operations. Aircraf t Weight is 1700 Grams or 3
. 98 pounds with battery , which is the total gross weight..
A pre -fli ght in s pection will be performed by the PIC in accordance with the factory instruction manual, as well as redundant checks to include the Internal Measurement Unit ( IMU) to make sure that the compass , gyro and acceleration values are within specs, positi v e GPS locks are secure , battery health in each individual LiPo cells are balanced, and radio signals are locked in.
The UAS will be maintained in accordance with the manufacturer's instruction manual and only manufacturer's authorized replacement parts will be used.



### FCC Information The Yuneec Typhoon Q500 transmitter used for controlling the UAS complies with part 15 of the FCC rules. Operation is subject to the following two conditions: (1) This device may not cause harmful interference, and (2) this device must accept anyI

interference received, including interference that m ay ca u se undesired operation. Th e Yuneec Typhoon Q500 radio transmitter used for controlling th e UAS i s wireless technology, whi ch h as been tested and found to be compliant with the applicable regu lation s govern in g a r ad io tran s mitter in the 2.400 GHz- 2.483 GH z range . Antenna Separation Distance When operatin g the Yuneec Typ h oo n Q500 tran s mitter, the PIC will maintain a separat i on distance of at least 5 em between his body (excluding fingers, hand s, wrists , ank les and feet) and t h e ant e nn a to mee t RF exposure safety requirements as determined by FCC regulations.
Pilot in Command and Observer Qualifications and Duties The PIC wi ll maintain at least a Private Pilot Certificate and a current Class III medical , p lu s at least 6 hours flying time and 5 takeoffs and landing s within 30 days in the type of UAS utili ze d in operations.
The PIC i s responsible for the safe and efficient operation of the aircraft. Specific duties include all preflight preparation and inspection, in flight operation, post flight requirements, and all procedures including but not limited to: • Safe in flight operations • Risk evaluation • Current weather conditions for safe flight
The Observer must have the visual acuity to observe the UAS and be able to communicate clearly with the PIC. The Observers duties are: • Warning the PIC of any impending obstacles in the flight path of the UAS. • Warning the PIC of any deviations in the planned flight path of the UAS. • Warning the PIC should any unauthorized personnel appear in the area of the planned flight. • The Observer will have the authority to order the PIC to terminate the flight should he feel the flight can not be conducted safely.



# -

### General Operating Standards • C & H Drone Services LLC wi ll o nl y operate it s UAS in line of s ig ht of a pilot and/or observer and wi ll opera t e at s ites that are a 'sufficient distance' from populate d areas. Such operati ons w ill in s ure that the UAS will "not create a ha za rd to u sers of the national airspace sys tem or the publi c." • Befor e an operation of the UAS within 5NM of an airport with a co ntrol tow er, the co ntrol tower wi ll b e ca ll ed to gai n permission to operate th e UAS. The PIC will give the position , altitud e a nd the times th e UAS will b e operated. The UAS will not be operated at an altitude of over 200 fee t AGL. Weather minimums will be 3 miles visibility an d a 1000 -foo t ceiling.

· Before an oper ation of a UAS within 5NM of a non-tower controlled, airport operators will be notified and th e PIC will give the right of way to avoid flying in the proximity of full-scale aircraft. At no time will the UAS be operated within the final approach course and the takeoff co urse of any runway. The UAS will not be operated at an altitude of over 200 feet AGL. Weather minimums will be 3 mile s visibility and a 1000-foot ceiling
. • Maximum flight time for each operational flight will be 15 minutes. • Flights will be terminated at 30 % battery power reserve should that occur prior to the 15 minute limit. • The UAS will be programmed so that they will not be operated at an altitude of no more than 200 feet AGL, and not more than 200 feet above an elevated platform from which filming is planned. • Minimum crew for each operation will consist of the UAS Pilot, and Vi s ual Observer. • The UAS operated by the petitioner weigh less than 55 pounds , including the payloads (i.e. camera, lens, and gimbals). • The UAS will operate at speeds of no more than 25 knots, can hover, and can simultaneously move vertically and horizontally
. • Given the small size of the UAS and the restricted sterile environment within which they will operate, my UAS operations adhere to the Reform Act's safety requirements.The UAS, pow ered by b atte ri es, are s maller, li ghter and more maneuv e ra bl e th an larger aircraft runnin g on co mbu stibl e fue l. The UAS operate at low er altitude s with no pers ons on board and w ill thereby reduce current ri sk leve l s, e nhan ce safety and dimini s h the like lihood of d eat h or seriou s b o dil y injury . With a s mall payload and maximum flight time of o nly 15 minut es, thi s offers littl e or no ri sk to nation al sec urity
. Low level oblique photos and v ideo from several angle s are far more effec tive than g round based imagery for displaying the charac ter ist ics of larg e, complex propertie s with severa l buildin gs and large tree s. The benefits of red u ce d costs and improv e d quality of presentation fro m the UAS over mann ed airc raft will be valuable to and benef it many buyers and sellers of real property including commercial building s, all while remaining subje c t to a ll limitations c ited b e low: a No flight will b e made with a Gro ss weight exceeding 55 pound s; b All operations must occur in FAA Class G airspace at no more than 200ft AGL , at an air speed of no more than 25 knots and no further than 1600 ft, or 0
. 263 NM from the PIC ; c All operations mu s t utilize a visual observer (VO). The VO and PIC must be able to co mmunicate by voice at all times during a flight operation; d Operation s will be re s tricted to flights over private property with the permission of the property owner; e All required permits will be obtained from state and local government prior to operation; f C & H Drone Services LLC will not be operated over densely populated areas; g C & H Drone Services LLC will not be operating over any open-air assembly of people ; h C & H Drone Services LLC will not be operating over heavily trafficked roads; (i) C & H Drone Services LLC will not be operating at night.


### EXEMPTION REQUESTS AND EQUIVALENT LEVEL OF SAFETY C & H Drone Services LLC requests an exemption from the following regulations as well as any additional regulations that may technically apply to the operation of the UAS Systems:

### 14 CFR Part 21, Airworthiness Certificates Thi s part estab li s h es th e procedures for the is s uan ce of an airworthine ss certificate . While th e FAA continues to work to develope airworthine ss s tandards for Unmanned Aerial Sys tem s, I reque s t an experimental certificate be iss u ed for the Yuneec Typhoon Q500 under either or both of the following provi s ion s: 21.191 Experimental certifi cates. Exper im enta l certificat es are issued for the following purpo ses: b 

### R esearch and development
. Te s ting new aircraft de s i g n concepts, new aircraft e quipment , n e w airc raft in sta llation s, new aircraft operating techniques, or new u ses for aircraft. c 

### Showing compliance with regulations. Conducting flight te s ts and other operations to s how comp liance with the airworthiness regulation s including flights to s how comp liance for issuance of type and supplemental type certificates, flights to Sub s tantiate major design changes, and flight s to show compliance with the function and reliability requirements of the regulations. Since the experimental certificate can be used for commercial purposes such as market surveys, sa les demonst rations , and customer crew training , I would expect that an experimental certificate would permit my commercial purpose as well. The aircraft will not carry person s or property, will not carry fuel, and will only fly under strict operational requirements. Combined with the UAS lightweight , being constructed primarily of carbon fiber and plastic, I propose that the UAS will be at least as safe, if not safer , than a conventionally certificated aircraft performing the same mission. If an experimental airworthiness certificate is not appropriate for this application, then I request an exemption of 14 CFR Part 21 , Subpart H, and the requirement for an airworthiness certificate in general, citing the equivalent level of safety outlined in the previous paragraph. 

### 14 CFR 45.23 Display of marks; general and 45.29 Size of marks. These regulations provide that each aircraft must display "N" and the aircraft's registration number in letters at least 3 inches high. Additionally, the aircraft must displaythe wo rd "EX PERIMENTAL" in le tte r s at l east 2 inc hes hi g h n ea r th e e ntra nc e to t h e cabin , cockpi t , o r pil ot stat i o n . T he UAS d o no t h ave an e ntr ance in w hi ch t h e word "EX PE RIM ENTAL " can b e p l ace d , a nd m ay n o t h ave a reg i s trati o n numb e r a ss i gn e d to it b y th e FAA. I p ro p ose to achi eve an equi vale nt l evel of sa fet y by including the word "EXPERIM ENTAL " i n th e pl aca rd on the top of th e airc raft s, as shown above , where th e PI C ( Pil ot In Co ntro l ), VO (Vi s u a l Ob server) and o th e rs in th e vi c inity of the airc raft w hil e it i s prepari ng f o r l aunc h w ill b e abl e to see th e d es ig n ation. Additi o nally , I fee l th at th e perm an e nt p l acard d iscu ss ed in th e pr ev i o us parag r aph will provide the a ircraft' s regi s tration i nfo rmation at th e gr o und s tation . F inall y, 1 will di s pl ay at th e g round s t at ion a h igh co ntra s t flag o r ba nne r that co nt ain s th e word s "Unmanne d Aircraft Ground Station" in l etters 5 i nch es hi g h o r g r eater. Sinc e the airc raft will operate within 0.263 NM of the grou n d s tatio n , th e b ann e r s h o uld be vi s ible to anyone that ob s erves the aircraft an d chooses to inves ti gate its point of origin.
14 CFR 61 . 113 Private pilot privileges and limitations: Pilot in Command and 61.133 Commercial pilot privileges and limitations. Th e regulation pro v ide s that no pers on that holds a Private Pilot certificate may act as p ilot i n Co mmand of an aircraft for compensation or hire
. Subparagraph (b) allow s a pri vate pilot to act as pilot in command of an aircraft in connection with any busine s s or e mplo y ment if : (1) The flight is only incidental to that busines s or employment; and (2) The aircraft does not carry passengers or property for compen s ation or hire. Our proposed operation s require that the PIC mu s t hold at least a Private Pilot Certificate with a Cla ss III Medical is s ued by the FAA and since the aircraft cannot carry passengers or property, I feel I meet the intent of 61.113 Subparagraph (b) even though the intent of this application is to conduct a busine s s . 14 CFR 91.7 Prohibits the Operation of an aircraft without an airworthiness certificate. As no such certificate will be applicable in the form contemplated by the F ARs, thi s Regulation is inapplicable
. 14 CFR 91.9 Civil aircraft flight manual, marking, and placard requirements.Thi s regulation provides that no perso n may oper ate an aircraft un less a current, ap pro ved flight manual is in the airc raft. I a ss ume that the intent of this r e quirement i s to ens ure that flight manual information is available to th e a ir crew while operating th e aircraft. I reque s t an exemption to this requirement s ince the ai r craft i s n ot o nl y too sma ll to can·y documentation , the documentation wo uld not be ava il ab l e to the crew durin g fli ght operations. To obtain an e qui valent level of sa fety and m eet th e intent of 91.9, I propo se that a cunent, approved UAS Fli g ht Manual s mu s t be ava il ab le to the c rew at th e gr ou nd s tation anytime the ai rc raft is in , or preparing fo r flight , and b e ready for pre s entation for any goveming official upon reque s t.



### 14 CFR 91.109 Flight Instruction; Simulated instrument flight and certain flight te sts The regulation s tate s that "No person may operate a civil aircraft that is being u sed for flight in structi o n unless that aircraft ha s fully functioning dual co ntrol s. C & H Drone Service s LLC will b e operating with a s ingle remote controller for the Yuneec Typhoon Q500. 

### 91.119 Minimum safe altitudes: General. The regulation states that over s p a rs ely populated are as the ai rc r af t cannot be ope rated closer than 500 feet to any perso n , vessel , vehicle , or s tructure. Since the typical mi ss ion of the UAS would be to acquire photograph s or video of buildings or commercial st

ru ct ure s, it would be nece ssary to operate closer than 500 feet to the item s listed
. Operations will only be flown over property where petmission has been obtained and careful preplanned flight path ha s been performed. The aircraft will be operat e d at a low altitude allowing, if a power unit fails, an emerg e ncy landing without undu e hazard to p erson s or property on the surface. Ther e fore I maintain that due to the small size of the UAS, the hazard to persons, vehicles and structures i s minimal compared to manned aircraft, which should be considered in granting the exemption.


### CFR 91.121 Altimeter settings.The regu lati o n r e quires th at a irc r aft s h a ll maintain c rui s ing altitud es b y referenc e to an altimet e r setting avai l ab l e within 100 NM of th e aircraft. The UAS will alway s fly below 200 fee t AGL and w ill not n eed to m a inta in crui s in g a ltitudes in o rder to pre v en t conflict with other aircraft. An Above Gro und Level altimeter meas ur e ment above the takeoff point i s transmitted via radio from the UAS on - b oard com puter to th e di s pla y screen held by the PI C, pro v idin g a co n s tantly updated AGL r eado ut. 14 CFR 91.151 Fuel requirements for flight in VFR conditions. The regulation prov id es th at no p ers on may begin a flight in an airplane und e r clay- VFR conditi o n s unl ess there is e nou gh fuel to fly to the first point of intended landing and to fly after that for at lea s t 30 minute s. I feel the intention of this paragraph i s to provide an ene r gy re serve a s a sa fety buff er for delays to landing
. The UAS is battery operated and the max imum duration of flight from a s ingle battery charge is 18 minute s with a 20 % reserve. Since the aircraft will never fly more than 0
. 263 NM from the point of intended landi n g, a fu ll battery charge at launch will ensure that I meet the re serve energy require ment of thi s paragraph. I reque s t an exemption to the word "fuel" and ask for an equiva le nt interpretation with the word "energy".
14 CFR 91.203(a) & (b) Civil aircraft: Certifications required. The regulation provides that an airworthine ss certificate, with th e regi s tration number as s igned to th e aircraft and a registration certificate mu s t be aboard the aircraft. Additionally, subparagraph (b) provides that the airworthines s certificate b e "displayed at the cabin or cockpit entrance so that it is legible to passengers or crew." At a maximum gross weight of 3.98 pounds and, the UAS is too small to carry documentation, do not have an entrance , and are not capable of can·ying passengers or crew. To obtain an equivalent level of safety and meet the intent of 91.203 , I propose that document s deeme d appropriate for these aircraft by the FAA will be with the crew at the ground control station and available for inspection upon request. In order to identify the aircraft, I propose that the information found on airworthine ss and registration certificate s be permanently affixed to the aircraft via placard containing the following information plu s the word "EXPERIMENTAL" to satisfy the requirement of 14 CFR 45
. 23.14 C FR Subpart E (91.401- 91.417 )

- Mainte n a nce , Pre ventiv e Maintenan ce, Alteration s T h e r eg ul at io n provi d es th at th e op er at or is prima r i ly res p o n s ibl e fo r maint ainin g th e a irc r a ft in a n airworth y c ond itio n , includin g co m p li a n c e w ith p art 3 9 and 4 3
. Parag r aph s 9 1. 4 0 7 and 9 1 .409 re qui re t h at the a ir c raft b e "ap prov e d for re turn to s erv i ce by a p er s o n a uthori zed under 4 3.7" aft er ma inte n a n c e a nd in sp e c ti o n. It is my inte nti on th at t h e PIC p e tform m a inte n ance and i n s p ect io n o f th e a irc raft a nd "b e auth orize d to appro ve th e airc ra ft fo r re turn to servi ce ." T he PI C will e n s ure that th e a ircrafts a r e in an airworthy c onditi o n pri or to every fli g h t and in additi o n c onduct detailed in s pec tion s af ter e v ery t wo h o ur s of fli gh t. M a i n te n ance per f

ormed by the PIC i s limited to , repl acing a pro p e ll er, checking e lectri ca l co nne c tion s and updating s oftw a re and firmw a re for the onbo ard c omput e r. T h e manu fac turer or th e ir de s ignated repair facility will p erform all other m ainte nan c e . T he PI C will document work performed in acc orda nce with 9 1.417. I f

eel that du e to th e s i ze , c on s tru c tion , and s implicity of the aircraft , the PIC can e n s ur e an equ iv alen t l e ve l of safety. Safet y and Benefits of the UAS C & H Drone Servi c e s LLC will be u s ing the UAS in a v ariety of appli c ation s that gen erall y require e xpen s ive full- s ize manned aircr af t to complete. Small , light, unmanned aeri al vehicle s offer more efficient and safer benefit s ove r the use o f full- s ized manned aircraft for aerial photography, film and still photography , real e s tate and commercial real e s tate marketing. C & H Drone Service s will be able to provide s ervices to clients that hav e not been available before the technology bec ame acce s sible. The benefits that come a long with the permitted u s e of the UAS are immen s e , and provide valuable image and video , u seful for garn ering intere s t s in potential con s umers , b e n efiting all partie s involved. Replacing significantly larger manned aircraft carrying crew and flamm able fuel with s mall UAS c arrying no passengers or crew cre ate s a much greater margin of s af ety for the pilots and crew . By granting C & H Drone Service s LLC 's reque s te d ex e mpti o n s, theFAA w ill h e lp drive d eve lopm ent of safe and s u ccessf ul co mme rcial UAS operations and will advance the publi c kn ow led ge b ase for s uc h operations. C & H Dron e S e rvice s LLC i s committed to promoting the UAS re se arch effo rt s of poli cy makers including th e FAA , NASA, DOD a nd DARPA b y s h a ring data fro m it s commercial UAS operations and servin g as a r eso urc e for future UAS re searc h operations. Thu s, th e FAA ha s good cause to g r a nt this P eti t i o n . 

### Conclusion As p ointed o ut in this application, th e Yuneec Typhoon Q500 , which I would u s e under authorization b y th e US DOT -FAA, i s a s mall , light-weight device operated within the line of s i g ht of the Pilot-in-Command (PIC), less than 200 feet above the ground and outside 5 miles from any airport, heliport, seaplane base, spaceport, or other location with aviation ac ti vities, unle ss the air traffic control authorities (A TC) have been notified and h ave aut hori ze d each flight within a radius of this distance. The Yuneec Typhoon Q500 has been proven capable for controlled flight. This UAS is offered for general sale on the market around the world and have often been used as Model Aircraft in the USA. I am certain that the studies conducted until now by the FAA, about Section 332, Public Law 112-95, 2014, have already provided you with the ass urances on the airworthiness of UAS such as mine
. For the foregoing reasons, the exemptions requested herein should be granted and C & H Drone Services LLC s hould be permitted to conduct small UAS operations in accordance with its manuals and all other operating parameters deemed necessary and appropriate by the FAA.
The submission of this application and its contents is the best demonstration that indeed it is possible to pursue the authorization process so that some UAS may be used for legitimate commercial activities and under reasonably safe conditions. Thank you for your time
. Formally Signed

### Marion Stewart Canty JR George Hooker C & 

### H Drone Services LLC

# QS 0 TYPHOO : N Atrcra t Fl l ight Time Up 

# to 25 

# Min 1 utes Height 240mm (9. 4 5 in) 

# Width 420mm

**(16 .5**  **4** 

# in)

**iagonal** 

# Len gth Wit ho u 1 t 

# Rotor Blades 565mm 

# (22.2 i ) Prope ler/Main Roto r

**Diam eter**  

# 330mm (13
. 0 in) 

# eight 

# Withou t 

# Battery

**an d**  

# Payload 

# 1130g (4 0.0 oz) 

# Battery 5400mAh 

# 35 11.1V LiPo (inc l uded) 

# C h arger 35 1 1 

# 1.1 1 

# V

**Po** 

# DC Ba l a: nc i ng Smart 

# Charger with AC Adapter Oncluded) 

# Transmitter 10 - -channe l 2
. 4GHz with 

# 5.8GHz video downlilnk 

# (included) 3 Flight ! Modes Smart, Angle 

# and

**om e**  

# Modes 

# Maximum Flying Height Default 

# 400 Feet Above Ground Level

**(Ad ustable**  

# via

**the**

**~ QSOO** 

**~** 

# GUI) 

# Maximum Rotational Velocity

**5°/s** 

# Maximum Bank

**An gle**  

# 35° 

# Maxim , u :m Climb Rate 

# in Smart 

# and ! Angle mode 3m/s Max i mum Descent Rate 

# in Smart 

# and Ang , e



# . 

# - .

# CG02-GB Camera G i m b al 

# System F ocusing 

# System Aerial Optimized Fi , xed Focus V i deo 

# Resolution FU LL HD 108 0 p - 

# Adjus t able 60 , 50 

# o r 48 FPS 

# Photo Re solution 1 2 

# M eg apix e l s Fi e l d o f 

# View 155° 

# ST1 0 Personal Ground**ation ~**  

# Operating System An d r o· id : TM 

# Number of Chann els 10 Control T ra n smission Distance/Range (Optimum 

# Conditi 1 ons) FCC Compliance: 

# Up to 8 00m (2624.67 ft) 

# CE Complia n ce:**p** 

# to 400m (1312.34 ft) 

# Robust Radio Control Modulation Yuneec Protocol 

# Video link**Frequ ency**  

# Band 5
. 8GHz Video Transmission Distance/Rang , e 

# {Optimum Conditions) FCC Compliance: Up to 600 ·m (1968.5 

# ft) 

# CE 

# Compliance : Up 

# to 300m (984.252 

# ft ) 

# Flight Systems Telemetry Data On Screen Display (,OSD) 

# Yes LED Backlit LCD Screen**Caoac:itiv~** 

# M ! ulti-Touch