March 14, 2015 U. S. Department of Transportation

, Docket Operations West Building Ground Floor, Room W12

- 140 1200 New Jersey Ave., SE Washington, DC 20590

Re: Exemption Request Section 333 of the FAA Reform Act and Part 11 of the Federal
Aviation Regulations from 14 CFR 61.113 (a) & (b); 91.103(b); 91.119; 91.121; 91.151(a); 91.405 (a); 91.407(a) (1); 91.409 (a) (2); 91.417 (a) & (b).

Dear Sir or Madam:

Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 (the Reform Act) and 14 C.F.R. Part 11, Patrick J. Cook, President of P.J.Cook Web Designs
and Overhead Real Estate.com

, a web design and photo/video company

, hereby applies for an exemption from the listed Federal Aviation Regulations (“FARs”) to allow commercial operation of i ts Small Unmanned Aircraft Systems (“ sUAS ”) for aerial imaging for safety

, monitoring and comparing work efforts/completion precentages

, and security of controlled environment of various sites , 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.

Patrick J. “PJ” Cook is a highly experienced USAF Special Operations Rotary
and Fixed

- Wing Aviator with over 4000hrs to include:

 FLIGHT CREW EXPERIENCE : Flight Record Logged Aircraft as USAF Special Operations Aviator

 Aircraft Models : AC

- 130H, AC

- 130A, CH

- 47D, CH

- 53A, CH

- 53C, HH

- 53B,

HH

- 53C, HH

- 53H, MH

- 47D, MH

- 53H, MH

- 53J, MH

- 60G, NCH

- 53A, TDH

47D, UH

- 1N, UH

- 60L.

 Total Hours : 4006.5 (2500+Rotary

- Wing), Instructor: 423.4

, Flight Examiner:

130.8

As a Career aviator and Flight Examiner, I have a solid knowledge of flight safety and fly with the creed “Safety is Paramont” at all times. I was also a crew resource management instructor that ensures my dedica ted observer keeps a keen scan and listens for aircraft at all times to increase my ground/flight safetyenvelope. Safety of flight is certainly no exception for the sUAS community . These are not to be treated like “toys” but precision GPS assisted craft that can safely assist in activities such as Photography/Videography where a conventional rotary

- wing aircraft could not safely operate and associated rotor wash c ould cause severe damage to area below.

As detailed in this document , the requested exemption would permit the operation
of sUAS under controlled conditions in airspace that is 1) limited 2) predetermined 3) controlled as to access and 4) would provide safety enhancements to the already best practices safety protocols followed by PJ COOK WEB DESIGNS at each one of its web design/photography sites. Approval of this exemption would thereby enhance safety and fulfill the Secretary of Transportation’s (the FAA Administrator’s) responsibilities to

1“...establish requirements for the safe operation o f such aircraft systems in the national airspace system.” Section 333 (c) of the Reform Act.

The name and address of the applicant is:

PJ COOK WEB DESIGNS 2034 Rainbow Farms Dr., Safety Harbor, FL 34695

PH: 727.744.2945
Email: pj@pjcook.com

Regulations from which the exemption is requested:

14 C

. F

. R

. Part 21 14 C.F.R. 45.23(b)

14 C

. F

. R

. 61.113 (a) & (b) 14 C.F.R. 91.7 (a)
14 C

. F

. R

. 91.9 (b) (2)
14 C.F.R. 91.103
14 C.F.R. 91.109
14 C.F.R. 91.119
14 C.F.R. 91.121
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

. 407 (a) (1)
14 C

. F

. R

. 409 (a) (2)
14 C

. F

. R

. 417 (a) & (b)

I. STATUTORY AUTHORITY FOR EXEMPTIONS

The Federal Aviation Act expressly grants the FAA authority to issue exemptions. This statutory authority includes exempting civil aircraft, as the term is defined under §40101 of the Act, including s UAS s , from the requirement that all civil aircraft must
have a current airworthiness certificate

. The Administrator may grant an exemption from a requirement of a regulation prescribed under subsection (a) or (b) of this section or any sections 44702

- 44716 of this title if the Administrator finds the exemption in the public interest. 49 U.S.C. §44701(f) See also 49 USC §44711(a); 49 USC §44704; 14 CFR §91.203(a) (1 ).

Section 333(b) of the Reform Act assists the S ecretary in determining whether

s UAS may operate in the National Airspace System (NAS) without creating a hazard to the user, the public, or a threat to national security . If the Secretary determines that a

s UAS “may operate safely in the national airspace system, the Secretary shall establish requirements for the safe operation of such aircraft in the national airspace system.” Id

. §333(c).

PJ COOK WEB DESIGNS ’ s UAS are multirotor vehicles , weighing 10 or fewer lbs. including payload. They operate under normal conditions at a speed of no more than 50 knots and have the capability to hover, and move in the vertical and horizontal plane

2simultaneously. The sUAS will operate only in the Pilot’s visual line of sight at all times and will operate only within the sterile area described in the DJI Phantom Vision 2+ Flight Manual, attached as Exhibit 1 (hereinafter “the Manual”). Such operations will
insure that the s UAS will “not create a hazard to users of the national airspace system or the public.” Reform Act Section 333 (b).

Given the small size of the sUAS involved and the restricted and sterile environment within which they will operate, our application falls squarely within the zone of safety (an equival ent level of safety) in which Congress envisioned that the FAA must, by exemption, allow commercial operations of s UAS to commence immediately.
Also due to the small size of the s UAS and the low altitudes and restricted areas in which
the s UAS will operate, approval of the application presents no national security issue.

Given the clear direction in Section 333 of the Reform Act, the authority contained in the Federal Aviation Act, as amended; the strong equivalent level of safety surrounding the proposed operations, and the significant public benefit, including enhanced safety, the grant of the requested exemptions is in the public interest. Accordingly, PJ COOK WEB DESIGNS respectfully requests that the FAA grant the requested exemption witho ut delay.

II. PUBLIC INTEREST

This exemption application is expressly submitted to fulfill Congress’ goal in passing Section 333(a) through (c) of the Reform Act. This law directs the Secretary of Transportation to consider whether certain unmanned airc raft systems may operate safely in the NAS before completion of the rulemaking required under Section 332 of the
Reform Act. By granting an exemption the FAA will fulfill Congress’s intent of allowing UAS to operate with significant safety precautions in l ow risk environments.

The use of s UAS on a construction site for example can significantly reduce the risk to workers of falls while inspecting, surveying, or monitoring site progress. s UAS can inspect, photograph, and collect data on hard to get to areas that otherwise would require worker inspection. Falls are a leading source of workplace fatality and injury on
construction sites 1 , and reducing falls through s UAS use for site imaging could save
workers lives.

The s UAS we propose to fly in this application are under five pounds, and carry
no combustible material on board , as opposed to the much larger conventionally powered
small aircraft

. Lastly, s UAS reduce the environmental impact by dramatically decreasing the

ene rgy used for aerial imaging and dat a collection over a photographed site. Our s UAS

use rechargeable lithium ion batteries, as opposed to foss il fuels burned in operation of small aircraft that are many hundreds of times heavier.

1 “Commonly Used Statistics”, Occupational Safety & Health Administration. Available at: https://www.osha.gov/oshstats/commonstats.html

3III. EQUIVALENT LEVEL OF S AFETY

PJ COOK WEB DESIGNS proposes that the exemption requested herein apply to

sUAS that have the characteristics and that operate with the limitations listed herein. These limitations provide for at least an equivalent or even higher level of safety to operations under the current regulatory structure because the proposed operations represent a safety enhancement to the already safe protocols followed on construction sites and imaging and surveying operations conducted with helicopters and other
conventi onal aircraft.

PJ COOK WEB DESIGNS will be bound by the following limitations when conducting its s UAS operations under an FAA issued exemption:

1. The s UAS will be less than 10 pounds.

2. Flights will be always operated within visual line of sight of a pilot.

3. Maximum total flight time for each operational flight will be 25 minutes. The UAS calculates battery reserve in real time, and will return to its ground station with at
least 20 % battery power reserve should that occur prior to the 25 minute limit.
Normal flight duration is 15 minutes with camera/gimbal payload.

4. Flights will normally be operated at an altitude of 200 feet AGL, never exceeding 400
feet AGL

. 5. Any site within 5 miles of an airport will not be flown without notification and approval of the lo cal FAA Flight Standards District Office (FSDO) and airport
controller.

6. C rew for each operation will consist of the s UAS Pilot who will keep the s UAS within his visual line of sight at all times and an observer who will be continually scanning for aircraft /obstacles/any safety considerations

. 7. The s UAS P ilot is a military aviation career (22yrs/4000+ flight hrs) trained in flight, operations, and safety procedures as detailed in the Flight Manual and experienced throught his aviation career

. 8. The s UAS will only operate within a confined “Sterile Area” as defined in the
Manual. The Manual also requires the establishment of a “Security Perimeter” for the flight operations area.

9. A briefing will be conducted in regard to the planned s UAS operations prior to each day’s production activities. It will be mandatory that all personnel who will be performing duties within the boundaries of the safety perimeter be present for this briefing.

10. All onsite personnel will consent to the UAS flyover o n site by waiver, and t he operator will obtain additional verbal or written consent of all persons who will be allowed within 100 feet of the flight operation

. 11. Pilot will have been trained in operation of UAS s generally and received up

- to

- date
information on the particular UAS to be operated as required by Section F of the
Manual.

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

13. All required permissions and permits will be obtained from territorial, state, county or
cit y jurisdictions, including local law enforcement, fire, or other appropriate governmental agencies.

414. If the s UAS loses communications or loses its GPS signal, it will have capability to
enter “loiter mode” and hover , reestablish satellite connection, and r eturn to a pre

determined location within the Security Perimeter and land.
15. Anytime a rotary wing aircraft is heard (Police/medical/news/etc.) the PIC will land the uAUS immeadiately to prevent any possible safety issues as these craft often fly
below the F AA 500ft minimum doing normal takeoff/landings in remote LZs.

16. Safety is paramont at all times. Recovery of the sUAS will always be secondary whenever a issue presents itself.

17. Care will be given to avoid at all times overflying people, homes, and property not involved in filming activities.

18. When overfyling any areas such as beaches, the PIC will take care to conduct prior to flight briefings with bystanders to ensure they are satified of sUAS safety and address any privacy concerns to be a good steward of t he community and overall flight good

manners.

5IV. DESCRIPTION OF SPECIFIC REGULATIONS

14 CFR 61.113 (a) & (b) : Private pilot privileges and limitations: Pilot in command

Sections 61.113 (a) & (b) limit private pilots to non

- commercial operations. Because the

s UAS will not carry a pilot or passengers, the proposed operations can achieve the equivalent level of safety of current operations by requiring the Pilot operating the
aircraft to have (1 ) completed a s UAS flight training course of 100 hours before flying a

s UAS (See Section F of the Manual for more details) and (2) a Sport Pilot certificate

. The FAA has previously acknowledged in prior grants of exemption under Section 333 that a
commerci al pilot’s certificate was not necessary to operate a sUA S , but that the FAA could not waive the requirement for an FAA

- issued pilot’s license. A Sport Pilot certificate addresses the FAA’s requirement that the Pilot in command have the requisite training and understanding of the National Airspace System, and also ensures that the Pilot is registered with the FAA and will not pose a risk to national security. The Sport Pilot certificate also does not require the Pilot to undertake the additional cost and t ime of additional manned aviation flight time that the Private Pilot’s license requires and which will not translate to skill or competency operating the sUA S

.

Unlike a conventional aircraft that carries the pilot and passengers, the s UAS is remotely

cont rolled with no living thing or cargo on board. DJI Phantom Vision 2+ ’s sUAS is also operated by an autopilot, which greatly reduces the danger of human error. The area of operation is controlled and restricted to hard hat areas , and all flights are planned and
coordinated in advance as set forth in the Manual.

The sUAS to be operated hereunder is less than 10 lbs. fully loaded, carries neither a pilot nor passenger, carries no explosive materials or flammable liquid fuels, and operates exclusively within a secured area as set out in the Manual. Like other civil aircraft, operations under this exemption will be tightly controlled and monitored by the operator, pursuant to the Manual’s requirements, and under the requirements and in compliance with local public safety requirements, to provide security for the area of operation as is currently done on active construction sites . The FAA will have advance notice of all operations.

The risks associated with the operation of the s UAS are therefore diminished from the level of risk associated with commercial operations contemplated by Part 61 when drafted, and allowing operations of the s UAS as requested with a Pilot who has met the minimum requirements stated in Section F of the Manual achieves the level of safety contemplated by 14 C.F.R. §61.113 (a) & (b).

14 C.F.R. 91.103 : Preflight Action

This regulation requires each pilot in command take certain actions before flight to

ensure the safety of flight. An exemption is needed from this requirement as the Pilot will take separate preflight actions, including checking for weather conditions, checking flight battery requirements, checking takeoff and landing distances, and all other actions in the

6Preflight Checklist in the Manual . These actions will provide an equivalent level of safety. See Appendix A of the Manual.

14 C.F. R. 91.119 : Minimum Safe Altitudes

Section 91.119 establishes safe altitudes for operation of civil aircraft. Section 91.119 (d)
allow s helicopters to be operated at less than the minimums prescribed, provided the person operating the helicopter complies with any route or altitudes prescribed for helicopters by the FAA. This exemption is for a multirotor craft that flies similarly to a

h elicopter, with vertical take off and vertical landing, which will typically operate at
altitudes of 200 AGL , so an exemption may be needed to allow such operations. The

s UAS will never operate at altitude higher than 4 00 AGL and will be in a restricted ar ea with security perimeter, where buildings and people will not be exposed to operations without their pre

- obtained consent. See Manual for detailed procedures

.

The equivalent level of safety will be achieved given the size, weight, speed of the s UAS as well as the location where it is operated. No flight will be taken without the permission of the property owner or local officials. Because of the advance notice to the property
owner and any onsite personnel as outlined in the Manual , all affected ind ividuals will be aware of the planned flight operations. Unlike flight operations with aircraft or rotorcraft weighing far more than the maximum 10 lbs. proposed herein , our sUAS will not carry flammable fuel. In addition, the low

- altitude operations of t he sUAS will ensure separation between s UAS operations and the operations of conventional aircraft that must comply with Section 91.119.

14 C.F.R. 91.121 : Altimeter Settings

This regulation requires each person operating an aircraft to maintain cruising altitude by reference to an altimeter that is set “...to the elevation of the departure airport or an appropriate altimeter setting available before departure.” As the sUAS may not have a barometric altimeter, but instead a GPS altitude read out, an exempt ion may be needed. An equivalent level of safety will be achieved by the operator, pursuant to the Manual and Safety Check list, confirming the altitude of the launch site shown on the GPS altitude indicator before flight.

14 CFR 91.151 (a) : Fuel requireme nts for flight in VFR conditions Section 91.151 (a) outlines fuel requirements for beginning a flight in VFR conditions.

Our s UAS is limited to operations in sterile and controlled environments as outlined in the Manual, and has a limited range and flight time which require an exemption from 14 CFR 91.151(a).

The battery powering the sUAS provides approximately 35 minutes of powered flight. To meet the 30 minute reserve requirement in 14 CFR §91.151, sUAS flights would be limited to approximately 1 5 minutes in length. The sUAS does have at all times a “Return to Home” enabled to automatically recall the craft when the battery voltage drops to the

7final 20 percent capacity. This setting will be enable at all times to prevent flyaways and any associat ed issue that could arise by the craft not landing in the intended Landing Zone as flight planned. Given the limitations on the s UAS ’s proposed flight area and the location of its proposed operations within a predetermined area, a longer time frame for

fl ight in daylight or night VFR conditions is reasonable.

PJ COOK WEB DESIGNS believes that an exemption from 14 CFR §91.151(a) falls within the scope of prior exemptions. See Exemption 10673 (allowing Lockheed Martin Corporation to operate without complianc e with FAR 91.151 (a)). Operating the small

s UAS , in a tightly controlled area where only people and property owners or official representatives who have signed waivers will be allowed, with less than 30 minutes of reserve fuel, does not engender the type of risks that Section 91.151(a) was intended to alleviate given the size and speed of the small UAS . Additionally, limiting sUAS flights to 10 minutes would greatly reduce the utility for which the exemption will be granted.

A n equivalent level of safety c an be achieved by limi ting flights to 30 minutes

, or enough battery reserve to ensure that the sUAS lands at the ground station with at least 20 % of battery power (as determined by the onboard monitoring system and the Pilot ), whichever happens first. This restriction would be more than adequate to return the sUAS to its planned landing zone from anywhere in its limited operating area.

Similar exemptions have been granted to other operations, including Exemptions 2689F, 5745, 10673, and 10808.

14 CFR 91.405 (a) ; 407 (a) (1) ; 409 (a) (2) ; 417 (a) & (b) : Maintenance inspections

These regulations require that an aircraft operator or owner “shall have that aircraft inspected as prescribed in subpart E of this part and shall between required inspections,
except as provided in paragraph (c) of this section, have discrepancies repaired as prescribed in part 43 of this chapter...,” and others shall inspect or maintain the aircraft in compliance with Part 43.

Given that these section s and Part 43 apply only to aircraft with an airworthiness certificate, these sections will not apply to PJ COOK WEB DESIGNS . Maintenance will be accomplished by the operator pursuant to the flight manual and operating handbook as
referenced in the Manual. An equivalent level of safety will be achieved because these
small s UAS are very limited in size and will carry a small payload and operate only in restricted areas for limited periods of time. If mechanical issues arise the s UAS can land immediately and w ill be operating from no higher than 400 feet AGL. As provided in the Manual, the Pilot will ensure that the s UAS is in working order prior to initiating flight, perform required maintenance, and keep a log of any maintenance performed. Moreover,
the Pilot is the person most familiar with the aircraft and best suited to maintain the aircraft in an airworthy condition to provide the equivalent level of safety.

*******

8Pursuant to 14 C.F.R. Part 11, the following summary is provided for publication in the

F ederal Register, should it be determined that publication is needed:

Applicant seeks an exemption from the following rules: 14 C.F.R. §21, subpart H; 14 C.F.R 45.23(b);14 C.F.R. §§ 61.113( a) & (b);91.7

(a); 91.9 (b) (2);91.103(b);91.109; 91.119; 91.121; 9 1.151(a);91.203(a) and (b); 91.405 (a); 91.407 (a) (1); 91.409 (a) (2); 91.409 (a) (2) and 91.417 (a) & (b) to operate commercially a small unmanned vehicle (55lbs or less) in construction operations.

Approval of exemptions allowing commercial operations o f sUAS in the construction industry enhances safety while reducing risk

. Manned aircraft monitoring and surveying creates a greater risk because the craft are much larger, have combustible fuel, and carry an onboard human pilot. In contrast, a sUAS weighin g fewer than 10 lbs. and powered by batteries eliminates virtually all of that risk given the reduced mass and lack of combustible fuel carried on board. The sUAS will carry no passengers or crew and, therefore, will not expose them to the risks associated with manned aircraft flights.

The operation of small s UAS , weighing less than 10 lbs., conducted in the strict conditions outlined above, will provide an equivalent level of safety supporting the grant of the exemptions requested herein, including exempti ng the applicant from the requirements of Part 21 and allowing commercial operations. These lightweight aircraft operate at slow speeds, close to the ground, and in a sterile environment and, as a result, are far safer than conventional operations conducte d with turbine helicopters operating in close proximity to the ground and people.

Privacy

All flights will occur over private or controlled access property with the property owner’s prior consent and knowledge. Images taken will be of individuals who have also consented to being filmed or otherwise have agreed to be in the area where aerial photography will take place.

*******

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

-- size, weight, speed, operating capabiliti es, controlled operating environment and operation within visual line of sight and national security

– provide more than adequate justification for the grant of the requested exemptions allowing commercial operation of applicant’s

s UAS in web design/photog raphy industry pursuant to the Manual appended hereto.

9Sincerely,

Patrick J. “PJ” Cook
President

PJ COOK WEB DESIGNS , Inc.
727.744.2945 pj@pjcook.com

APPENDIX

– A
DJI PHANTOM 2 VISION+ TECHNICAL SPECIFICATIONS

Patrick J. Cook only utilizes safe and reliable UASs. DJI is an industry leader in small UAS production. DJI UASs are loaded with ground breaking software enabling the user to set parameters which will not allow flight into controlled airspace. Parameters can also be set to limit flight to no higher than a predetermined and set altitude as well as limit flight to a predetermined and set distance. In addition, DJI software provides real

- time
altitude and location information to the PIC via the linked monitor (smart phone/tablet devices)

1.1 DJI Phantom 2 Vision+

1.1.1 Aircraft 1.1.1.1 Supported Battery

– DJI 5200mAH LiPo Battery 1.1.1.2 Weight (Battery & Propellers Included)

– 2lbs 11.810oz (1242g) 1.1.1.3 Hover Accuracy (Ready to Fly)

– Vertical: .8m; Hor izontal: 2.5m 1.1.1.4 Max Yaw Angular Velocity

- 200 0 /s 1.1.1.5 Max Tilt Angel

- 35 0 1.1.1.6 Max Ascent Speed

– 6m/s 1.1.1.7 Max Descent Speed

– 2m/s 1.1.1.8 Max Flight Speed

– 15m/s (NOT RECOMMENDED)

1.1.2 Gimbal 1.1.2.1 Working Current

– Static: 750mA; Dynamic: 900mA 1.1.2.2 Control Accuracy

- ±0.03 0 1.1.2.3 Controllable Range

– Pitch:

- 90 0

- 0 0 1.1.2.4 Maximum Angular Speed

– Pitch: 90 0 /s

1.1.3 Camera 1.1.3.1 Operating Temperature Range

- 32 0 F

- 104 0 F (0 0 C

- 40 0 C)
1.1.3.2 Sensor Size

– 1/2.3”
1.1.3.3 E ffective Pixels

– 14M

101.1.3.4 Resolution

– 4384x3288 4.1.3.5 HD Video Recording

– 1080p30 & 720p 4.1.3.6 Recording Field of View

- 110 0 /85 0

1.1.4 Transmitter 1.1.4.1 Operating Frequency

– 5.728GHz

– 5.85GHz 1.1.4.2 Communication Distance (unobstructed)

– FCC Compliance: 800m 1.1.4.3 Receiver Sensitivity (1%PER)

- - 93dBm
1.1.4.4 Transmitter Power

– FCC Compliance: 100mW 1.1.4.5 Working Voltage

– 120mA@3.7V

1.1.5 Range Extender 1.1.5.1 Operating Frequency

– 2412

- 2462MHz
1.1.5.2 Communication Distance (unobstructed)

– 500

- 700m
1.1.5.3 Transmitter Power

– 20dBm 1.1.5.4 Power Consumption

– 2W

APPENDIX

– B
DJI INSPIRE 1 TECHNICAL SPECIFICATIONS

Patrick J. Cook only utilizes safe and reliable UASs. DJI is an industry leader in small UAS production. DJI U ASs are loaded with ground breaking software enabling the user to set parameters which will not allow flight into controlled airspace. Parameters can also be set to limit flight to no higher than a predetermined and set altitude as well as limit flight to a predetermined and set distance. In addition, DJI software provides real

- time altitude and location information to the PIC via the linked monitor (smart phone/tablet devices)

2.2 DJI Inspire 1

2.2.1 Aircraft
2.2.1.1 Model

– T600 2.2.1.2 Weight (Battery Included)

– 6lbs 7.5291oz (2935g) 2.2.1.3 Hovering Accuracy (GPS Mode)

– Vertical: 0.5m; Horizontal:
2.5m 2.2.1.4 Max Angular Velocity

– Pitch: 3000/s; Yaw: 1500/s 2.2.1.5 Max Tilt Angle

- 350 2.2.1.6 Max Ascent Speed

– 5m/s 2.2.1.7 Max Descent Speed

– 4m/ s 2.2.1.8 Max Speed

– 22m/s (ATTI mode, no wind

– NOT RECOMMENDED) 2.2.1.9 Max Flight Altitude

– 4500m
2.2.1.10 Max Wind Resistance

– 10m/s 2.2.1.11 Max Flight Time

– Approximately 18 minutes
2.2.1.12 Motor Model

– DJI 3510

112.2.1.13 Propeller Model

– DJI 1 345 2.2.1.14 Operating Temperature Range

– 140F to 1040F (

- 100C to 400C)

2.2.1.15 Dimensions

– 17 1⁄4” x 17 3⁄4” x 12”

2.2.2 Gimbal
2.2.2.1 Model

– ZENMUSE X3 2.2.2.2 Output Power (with camera)

– Static: 9W; In Motion: 11W 2.2.2.3 Operating Current

– Static: 750mA; In Motion: 900mA 2.2.2.4 Angular Vibration Range

- ±0.030 2.2.2.5 Mounting

– Detachable 2.2.2.6 Controllable Range

– Pitch:

- 900 to +300; Pan: ±3200 2.2.2.7 Mechanical Range

– Pitch:

- 1250 to 450; Pan: ±3300 2.2.2.8 Max Controllable Speed

– Pitch: 1 200/s; Pan: 1800/s

2.2.3 Camera

2.2.3.1 Name

– X3
2.2.3.2 Model

– FC350
2.2.3.3 Total Pixels

– 12.76M
2.2.3.4 Effective Pixels

– 12.4M 2.2.3.5 Image Max Size

– 4000x3000 2.2.3.6 ISO Range

– 100

- 3200
2.2.3.7 Field of View

- 940

2.2.3.8 CMOS

– Sony EXMOR 1/2.3” 2.2.3.9 HD Video Recording

– UHD(4K): 4096x2160p24/25, 3840x2160p24/25/30; FHD: 1920x1080p24/25/30/48/50/60; HD: 1280x720p24/25/30/48/50/60 2.2.3.10 Operating Temperature Range

- 320F

- 1040F (00C

- 400C)

2.2.4 Transmitter

2.2.4.1 Name

– C1

2.2.4.2 Operating Frequency

– 5.728

- 5.850GHz; 2.400

- 2.483GHz 2.2.4.3 Communicating Distance (unobstructed)

– 2000m 2.2.4.4 Output Power

– 9W 2.2.4.5 Operating Temperature Range

- 140F to 1040F (

- 100C to 400C) 2.2.4.6 Battery

– 600mAh LiPo 2S

ADDITIONAL DOCUMENTS ATTACHED

DJI Inspire Manual
DJI Phantom Vision 2+ Manual

12