July 27, 2015

Exemption No. 12151

Regulatory Docket No. FAA–2015–1639

Mr. Keith Redlin

49252 Kilkenny Drive

Macomb, MI 48044

Dear Mr. Redlin:

This letter is to inform you that we have granted your request for exemption. It transmits our 

decision, explains its basis, and gives you the conditions and limitations of the exemption, 

including the date it ends.

By letter dated April 26, 2015, you petitioned the Federal Aviation Administration (FAA) for 

an exemption. The petitioner requested to operate an unmanned aircraft system (UAS) to 

conduct aerial photography and videography.

See Appendix A for the petition submitted to the FAA describing the proposed operations and 

the regulations that the petitioner seeks an exemption.

The FAA has determined that good cause exists for not publishing a summary of the petition 

in the Federal Register because the requested exemption would not set a precedent, and any 

delay in acting on this petition would be detrimental to the petitioner.

Airworthiness Certification

The UAS proposed by the petitioner is a Blade 350QX and DJI Inspire 1.

In accordance with the statutory criteria provided in Section 333 of Public Law 112−95 in 

reference to 49 U.S.C. § 44704, and in consideration of the size, weight, speed, and limited 

operating area associated with the aircraft and its operation, the Secretary of Transportation 

has determined that this aircraft meets the conditions of Section 333. Therefore, the FAA 

finds that relief from 14 CFR part 21, Certification procedures for products and parts, 
2

Subpart H—Airworthiness Certificates, and any associated noise certification and testing 

requirements of part 36, is not necessary.

The Basis for Our Decision

You have requested to use a UAS for aerial data collection1. The FAA has issued grants of 

exemption in circumstances similar in all material respects to those presented in your petition. 

In Grants of Exemption Nos. 11062 to Astraeus Aerial (see Docket No. FAA−2014−0352), 

11109 to Clayco, Inc. (see Docket No. FAA−2014−0507), 11112 to VDOS Global, LLC (see

Docket No. FAA−2014−0382), and 11213 to Aeryon Labs, Inc. (see Docket No. 

FAA−2014−0642), the FAA found that the enhanced safety achieved using an unmanned 

aircraft (UA) with the specifications described by the petitioner and carrying no passengers or 

crew, rather than a manned aircraft of significantly greater proportions, carrying crew in 

addition to flammable fuel, gives the FAA good cause to find that the UAS operation enabled 

by this exemption is in the public interest.

Having reviewed your reasons for requesting an exemption, I find that—

 They are similar in all material respects to relief previously requested in Grant of 

Exemption Nos. 11062, 11109, 11112, and 11213;

 The reasons stated by the FAA for granting Exemption Nos. 11062, 11109, 11112, and 

11213 also apply to the situation you present; and 

 A grant of exemption is in the public interest.

Our Decision

In consideration of the foregoing, I find that a grant of exemption is in the public interest. 

Therefore, pursuant to the authority contained in 49 U.S.C. 106(f), 40113, and 44701, 

delegated to me by the Administrator, Mr. Keith Redlin is granted an exemption from 14 CFR 

§§ 61.23(a) and (c), 61.101(e)(4) and (5), 61.113(a), 61.315(a), 91.7(a), 91.119(c), 91.121, 

91.151(a)(1), 91.405(a), 91.407(a)(1), 91.409(a)(1) and (2), and 91.417(a) and (b), to the 

extent necessary to allow the petitioner to operate a UAS to perform aerial data collection.

This exemption is subject to the conditions and limitations listed below.

Conditions and Limitations

In this grant of exemption, Mr. Keith Redlin is hereafter referred to as the operator.

 

1 Aerial data collection includes any remote sensing and measuring by an instrument(s) aboard the UA. 

Examples include imagery (photography, video, infrared, etc.), electronic measurement (precision surveying, RF 

analysis, etc.), chemical measurement (particulate measurement, etc.), or any other gathering of data by 

instruments aboard the UA.
3

Failure to comply with any of the conditions and limitations of this grant of exemption will be 

grounds for the immediate suspension or rescission of this exemption.

1. Operations authorized by this grant of exemption are limited to the Blade 350QX and 

DJI Inspire 1 when weighing less than 55 pounds including payload. Proposed 

operations of any other aircraft will require a new petition or a petition to amend this 

exemption.

2. Operations for the purpose of closed-set motion picture and television filming are 

not permitted. 

3. The UA may not be operated at a speed exceeding 87 knots (100 miles per hour). The 

exemption holder may use either groundspeed or calibrated airspeed to determine 

compliance with the 87 knot speed restriction. In no case will the UA be operated at 

airspeeds greater than the maximum UA operating airspeed recommended by the 

aircraft manufacturer.

4. The UA must be operated at an altitude of no more than 400 feet above ground level 

(AGL). Altitude must be reported in feet AGL.

5. The UA must be operated within visual line of sight (VLOS) of the PIC at all times. 

This requires the PIC to be able to use human vision unaided by any device other than 

corrective lenses, as specified on the PIC’s FAA-issued airman medical certificate or 

U.S. driver’s license.

6. All operations must utilize a visual observer (VO). The UA must be operated within 

the visual line of sight (VLOS) of the PIC and VO at all times. The VO may be used 

to satisfy the VLOS requirement as long as the PIC always maintains VLOS 

capability. The VO and PIC must be able to communicate verbally at all times; 

electronic messaging or texting is not permitted during flight operations. The PIC 

must be designated before the flight and cannot transfer his or her designation for the 

duration of the flight. The PIC must ensure that the VO can perform the duties 

required of the VO.

7. This exemption and all documents needed to operate the UAS and conduct its 

operations in accordance with the conditions and limitations stated in this grant of 

exemption, are hereinafter referred to as the operating documents. The operating 

documents must be accessible during UAS operations and made available to the 

Administrator upon request. If a discrepancy exists between the conditions and 

limitations in this exemption and the procedures outlined in the operating documents, 

the conditions and limitations herein take precedence and must be followed. 

Otherwise, the operator must follow the procedures as outlined in its operating 

documents. The operator may update or revise its operating documents. It is the 

operator’s responsibility to track such revisions and present updated and revised 
4

documents to the Administrator or any law enforcement official upon request. The 

operator must also present updated and revised documents if it petitions for extension 

or amendment to this grant of exemption. If the operator determines that any update 

or revision would affect the basis upon which the FAA granted this exemption, then 

the operator must petition for an amendment to its grant of exemption. The FAA’s 

UAS Integration Office (AFS−80) may be contacted if questions arise regarding 

updates or revisions to the operating documents.

8. Any UAS that has undergone maintenance or alterations that affect the UAS operation 

or flight characteristics, e.g., replacement of a flight critical component, must undergo 

a functional test flight prior to conducting further operations under this exemption. 

Functional test flights may only be conducted by a PIC with a VO and must remain at 

least 500 feet from other people. The functional test flight must be conducted in such 

a manner so as to not pose an undue hazard to persons and property.

9. The operator is responsible for maintaining and inspecting the UAS to ensure that it is 

in a condition for safe operation.

10. Prior to each flight, the PIC must conduct a pre-flight inspection and determine the 

UAS is in a condition for safe flight. The pre-flight inspection must account for all 

potential discrepancies, e.g., inoperable components, items, or equipment. If the 

inspection reveals a condition that affects the safe operation of the UAS, the aircraft is 

prohibited from operating until the necessary maintenance has been performed and the 

UAS is found to be in a condition for safe flight.

11. The operator must follow the UAS manufacturer’s maintenance, overhaul, 

replacement, inspection, and life limit requirements for the aircraft and 

aircraft components.

12. Each UAS operated under this exemption must comply with all manufacturer 

safety bulletins.

13. Under this grant of exemption, a PIC must hold either an airline transport, 

commercial, private, recreational, or sport pilot certificate. The PIC must 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 must also meet the flight review requirements specified in 

14 CFR § 61.56 in an aircraft in which the PIC is rated on his or her pilot certificate.

14. The operator may not permit any PIC to operate unless the PIC demonstrates the 

ability to safely operate the UAS in a manner consistent with how the UAS will be 

operated under this exemption, including evasive and emergency maneuvers and 

maintaining appropriate distances from persons, vessels, vehicles and structures. PIC 

qualification flight hours and currency must be logged in a manner consistent with 
5

14 CFR § 61.51(b). Flights for the purposes of training the operator’s PICs and VOs 

(training, proficiency, and experience-building) and determining the PIC’s ability to 

safely operate the UAS in a manner consistent with how the UAS will be operated 

under this exemption are permitted under the terms of this exemption. However, 

training operations may only be conducted during dedicated training sessions. During 

training, proficiency, and experience-building flights, all persons not essential for 

flight operations are considered nonparticipants, and the PIC must operate the UA 

with appropriate distance from nonparticipants in accordance with 14 CFR § 91.119.

15. UAS operations may not be conducted during night, as defined in 14 CFR § 1.1. All 

operations must be conducted under visual meteorological conditions (VMC). Flights 

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

16. The UA may not operate within 5 nautical miles of an airport reference point (ARP) as 

denoted in the current FAA Airport/Facility Directory (AFD) or for airports not 

denoted with an ARP, the center of the airport symbol as denoted on the current 

FAA-published aeronautical chart, unless a letter of agreement with that airport’s 

management is obtained or otherwise permitted by a COA issued to the exemption 

holder. The letter of agreement with the airport management must be made available 

to the Administrator or any law enforcement official upon request.

17. The UA may not be operated less than 500 feet below or less than 2,000 feet 

horizontally from a cloud or when visibility is less than 3 statute miles from the PIC.

18. If the UAS loses communications or loses its GPS signal, the UA must return to a 

pre-determined location within the private or controlled-access property.

19. The PIC must abort the flight in the event of unpredicted obstacles or emergencies.

20. The PIC is prohibited from beginning a flight unless (considering wind and forecast 

weather conditions) there is enough available power for the UA to conduct the 

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

power recommended by the manufacturer if greater.

21. Air Traffic Organization (ATO) Certificate of Waiver or Authorization (COA). All 

operations shall be conducted in accordance with an ATO-issued COA. The 

exemption holder may apply for a new or amended COA if it intends to conduct 

operations that cannot be conducted under the terms of the attached COA.

22. All aircraft operated in accordance with this exemption must be identified by serial 

number, registered in accordance with 14 CFR part 47, and have identification 

(N−Number) markings in accordance with 14 CFR part 45, Subpart C. Markings must 

be as large as practicable.
6

23. Documents used by the operator to ensure the safe operation and flight of the UAS and 

any documents required under 14 CFR §§ 91.9 and 91.203 must be available to the 

PIC at the Ground Control Station of the UAS any time the aircraft is operating. 

These documents must be made available to the Administrator or any law enforcement 

official upon request.

24. The UA must remain clear and give way to all manned aviation operations and 

activities at all times. 

25. The UAS may not be operated by the PIC from any moving device or vehicle. 

26. All Flight operations must be conducted at least 500 feet from all nonparticipating 

persons, vessels, vehicles, and structures unless:

a. Barriers or structures are present that sufficiently protect nonparticipating persons 

from the UA and/or debris in the event of an accident. The operator must ensure 

that nonparticipating persons remain under such protection. If a situation arises 

where nonparticipating persons leave such protection and are within 500 feet of 

the UA, flight operations must cease immediately in a manner ensuring the safety 

of nonparticipating persons; and

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

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

the risk of operating closer to those objects and determined that it does not 

present an undue hazard.

The PIC, VO, operator trainees or essential persons are not considered 

nonparticipating persons under this exemption.

27. All operations shall 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.

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

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

to the FAA's UAS Integration Office (AFS−80) within 24 hours. Accidents must be 

reported to the National Transportation Safety Board (NTSB) per instructions 

contained on the NTSB Web site: www.ntsb.gov.

If this exemption permits operations for the purpose of closed-set motion picture and 

television filming and production, the following additional conditions and limitations apply.

29. The operator must have a motion picture and television operations manual (MPTOM) 

as documented in this grant of exemption.
7

30. At least 3 days before aerial filming, the operator of the UAS affected by this 

exemption must submit a written Plan of Activities to the local Flight Standards 

District Office (FSDO) with jurisdiction over the area of proposed filming. The 3-day 

notification may be waived with the concurrence of the FSDO. The plan of activities 

must include at least the following:

a. Dates and times for all flights;

b. Name and phone number of the operator for the UAS aerial filming conducted 

under this grant of exemption;

c. Name and phone number of the person responsible for the on-scene operation of 

the UAS;

d. Make, model, and serial or N−Number of UAS to be used;

e. Name and certificate number of UAS PICs involved in the aerial filming;

f. A statement that the operator has obtained permission from property owners 

and/or local officials to conduct the filming production event; the list of those 

who gave permission must be made available to the inspector upon request;

g. Signature of exemption holder or representative; and

h. A description of the flight activity, including maps or diagrams of any area, city, 

town, county, and/or state over which filming will be conducted and the altitudes 

essential to accomplish the operation.

31. Flight operations may be conducted closer than 500 feet from participating persons 

consenting to be involved and necessary for the filming production, as specified in the 

exemption holder’s MPTOM.

Unless otherwise specified in this grant of exemption, the UAS, the UAS PIC, and the UAS 

operations must comply with all applicable parts of 14 CFR including, but not limited to, 

parts 45, 47, 61, and 91.
8

This exemption terminates on July 31, 2017, unless sooner superseded or rescinded.

Sincerely,

/s/

John S. Duncan

Director, Flight Standards Service

Enclosures
UNITED STATES OF AMERICA 

DEPARTMENT OF TRANSPORTATION 

FEDERAL AVIATION ADMINISTRATION 

WASHINGTON, DC

Regulatory Docket No. _______________

IN THE MATTER OF THE PETITION FOR EXEMPTION OF:

Keith A. Redlin

FOR AN EXEMPTION SEEKING RELIEF FROM THE REQUIREMENTS OF 

TITLE 14 OF THE CODE OF FEDERAL REGULATIONS

SECTIONS 61.113(a) & (b), 91.7(a), 91.121, 91.151(b), 91.405(a), 91.407(a)(1), 

91.409(a)(1) & (a)(2), AND 91.417(a) & (b) CONCERNING COMMERCIAL 

OPERATION OF BLADE 350QX AP AND DJI INSPIRE 1 UNMANNED 

AIRCRAFT SYSTEMS

PURSUANT TO SECTION 333 OF

THE FAA MODERNIZATION AND REFORM ACT OF 2012 

(PUBLIC LAW 112-95)

Submitted on April 26, 2015

Keith A. Redlin

49252 Kilkenny Drive

Macomb, MI 48044 

Tel: (248) 881-2861
2

TABLE OF CONTENTS

Page 

GLOSSARY OF ABBREVIATIONS...................................................................................3 

SUMMARY...........................................................................................................................4 

INTRODUCTION AND INTERESTS OF PETITIONER....................................................4 

BACKGROUND....................................................................................................................4 

BASIS FOR PETITION.........................................................................................................5 

NAME AND ADDRESS OF PETITIONER.............................................................7 

THE SPECIFIC SECTIONS OF 14 C.F.R. FROM WHICH KEITH A. REDLIN 

SEEKS EXEMPTION.................................................................8 

THE EXTENT OF RELIEF KEITH A. REDLIN SEEKS AND THE REASON 

KEITH A. REDLIN SEEKS THE RELIEF.........................11 

THE REASONS WHY GRANTING KEITH A. REDLIN’S REQUEST WOULD 

BE IN THE PUBLIC INTEREST .........................................................15 

THE REASONS WHY GRANTING THE EXEMPTION WOULD NOT 

ADVERSELY AFFECT SAFETY..........................................................................19 

SUMMARY THAT CAN BE PUBLISHED IN THE FEDERAL REGISTER......34 

ANY ADDITIONAL INFORMATION, VIEWS, OR ARGUMENTS 

AVAILABLE TO SUPPORT KEITH A. REDLIN’S REQUEST.........34 

CONCLUSION....................................................................................................................35 

APPENDICES........................................................................................37
3

GLOSSARY OF ABBREVIATIONS

AGL Above Ground Level

AOI Area of Interest

ATC Air Traffic Control

ATO Air Traffic Organization

AV Aerial Vehicle

CFR Code of Federal Regulations

COA Certificate of Authorization

FAA Federal Aviation Administration

FAR Federal Aviation Regulation 

GCS Ground Control Station 

GPS Global Positioning System

LOL Loss of Link 

NAS National Airspace System

NOTAM Notice to Airman

PIC Pilot In Command

Section 333 FAA Modernization and Reform Act of 2012 (FMRA) Section 333

SO Safety Observer

SOP Standard Operating Procedures

UA Unmanned Aircraft

UAS Unmanned Aircraft System

VFR Visual Flight Rules

VLOS Visual Line of Site

VMC Visual Meteorological Conditions

VTOL Vertical Takeoff and Landing
4

SUMMARY

KEITH A. REDLIN seeks exemption from the requirements of 14 C.F.R §§ 

61.113(a) & (b), 91.7(a), 91.121, 91.151(b), 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), 

and 91.417(a) & (b), to operate an Unmanned Aircraft System pursuant to Section 333 of 

the FAA Modernization and Reform Act of 2012 (FMRA). This exemption will permit 

KEITH A. REDLIN to operate an Unmanned Aircraft System (UAS) for the commercial 

purpose of conducting aerial video and photography of construction sites, real estate,

special events, and landscape over certain areas of the United States. 

INTRODUCTION AND INTERESTS OF THE PETITIONER

KEITH A. REDLIN provides its clients with expertise and knowledge in advanced 

technologies and solutions to increase efficiency, productivity and effectiveness. KEITH 

A. REDLIN also provides its clients with the highest quality digital content for use in their 

commercial, personal, and non-profit multimedia projects. KEITH A. REDLIN has over 15

years of professional experience in Information Technology and is recognized as an expert 

in network infrastructure, computer systems, and multimedia content creation. He has over 

3 years recreational/hobby experience in all aspects of aerial video and photography. 

Additionally, he is an active Police Reserve with the Dearborn Police Department. The 

objective of KEITH A. REDLIN’s aerial video and photography operations is to provide

high quality imaging (under 400 ft) for real estate, construction, and recreational markets 

in Michigan and the surrounding states as well as special events. 

BACKGROUND
5

Unmanned Aircraft Systems: BLADE 350 QX AP and INSPIRE I UASs

KEITH A. REDLIN seeks an exemption to operate DJI and Blade systems for 

compensation or hire within the NAS. The BLADE 350 QX AP and DJI Inspire 1 are 

vertical takeoff and landing (VTOL) Unmanned Aircraft (UA) with a Ground Control 

Station (GCS) utilizing electronic tablet or smart phone systems. The BLADE 350 QX AP

has a maximum gross weight of approximately 33.7 ounces, while having a length of 18.3

inches width of 18.3 inches, height of 7.48 inches, and a maximum speed of approximately 

20 knots. The DJI Inspire 1 has a maximum gross weight of 6 pounds 7.5 ounces, a length 

of 17.3 inches, width of 17.7 inches, height of 11.8 inches, and a maximum speed of 

approximately 42 knots. The BLADE 350 QX AP and DJI Inspire 1UAs are equipped with 

four main rotors; driven by Lithium Polymer battery powered electric motors. 

The BLADE 350 QX AP and DJI Inspire 1 UAs that will be operated by KEITH A. 

REDLIN will be registered in accordance with 49 U.S.C. 44103, Registration of Aircraft, 

as well as 14 C.F.R Part 47, Aircraft Registration, and marked in accordance with 14 

C.F.R. Part 45, Identification and Registration Marking.

BASIS FOR PETITION

Petitioner, KEITH A. REDLIN, pursuant to the provisions of the Federal Aviation 

Regulations (14 C.F.R. § 11.61) and the FAA Modernization and Reform Act of 2012 

(FMRA), Section 333, Special Rules for Certain Unmanned Aircraft Systems, hereby 

petitions the Administrator to commercially operate the BLADE 350 QX AP and DJI 

Inspire 1 UASs in the National Airspace System (NAS), and for an exemption from the 

requirements of 14 C.F.R §§ 61.113(a) & (b), 91.7(a), 91.121, 91.151(b), 91.405(a), 

91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b). 
6

In consideration of the speed, weight, size, and limited operating area associated 

with the unmanned aircraft and its operation, KEITH A. REDLIN’s operation of BLADE 

350 QX AP and DJI Inspire 1 UASs meets the conditions of FMRA Section 333 and 

therefore, will not require an airworthiness certificate in accordance with 14 C.F.R. Part 

21, Subpart H. 

Accordingly, KEITH A. REDLIN requests relief from Sections 91.405(a), 

91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b), as these sections set forth 

requirements for maintenance that only apply to aircraft with an airworthiness certificate. 

KEITH A. REDLIN submits that the requested relief is proper since an equivalent 

level of safety will be ensured. KEITH A. REDLIN will use experienced personnel or 

technicians to perform maintenance, alterations, or preventive maintenance on the UASs 

using the methods, techniques, and practices prescribed in the operating documents (i.e., 

Monthly Maintenance Log, and BLADE 350 QX AP and DJI Inspire 1 Instruction 

Manual). Furthermore, KEITH A. REDLIN will document and maintain all maintenance 

records for the BLADE 350 QX AP and DJI Inspire 1 UASs. 

Relief from certain requirements of Section 61.113(a) and (b), entitled Private pilot 

privileges and limitations: Pilot in command, is requested by KEITH A. REDLIN to the 

extent necessary to allow a Pilot in Command (PIC) holding a private pilot or higher level 

certificate, as well as an airman medical certificate, and who has demonstrated, by meeting 

minimum flight- hour and currency requirements, that the PIC is able to safely operate the 

BLADE 350 QX AP and DJI Inspire 1 UASs in a manner consistent with this exemption, 

including evasive and emergency maneuvers and maintaining appropriate distances from 

people, vessels, vehicles and structures. 
7

KEITH A. REDLIN seeks relief from Section 91.7(a), entitled Civil aircraft 

airworthiness, because the BLADE 350 QX AP and DJI Inspire 1 UASs do not require an 

airworthiness certificate in accordance with 14 C.F.R. Part 21, Subpart H. As such, KEITH 

A. REDLIN submits that he will ensure that the BLADE 350 QX AP and DJI Inspire 

1UASs are in an airworthy condition, prior to every flight, by determining that the UASs 

are in compliance with the operating documents (i.e., Monthly Maintenance Log, and

BLADE 350 QX AP and DJI Inspire 1 Instruction Manual), and that the aircraft are in a 

condition for safe flight. 

KEITH A. REDLIN also seeks an exemption from the requirements of Section 

91.121, entitled Altimeter Settings, as the BLADE 350 QX AP and DJI Inspire 1 UAs will 

not have a typical barometric altimeter onboard. However, altitude information of the 

BLADE 350 QX AP and DJI Inspire 1UAs will be provided to the PIC via Global 

Positioning System (GPS) equipment and radio communications telemetry data link, which 

downlinks from the UA to the GCS for active monitoring of the flight path. This altitude 

information, combined with KEITH A. REDLIN’s operation of the BLADE 350 QX AP

and DJI Inspire 1 UASs within visual line of sight, at or below 400 feet AGL, will ensure a 

level of safety equivalent to Section 91.121. 

Additionally, KEITH A. REDLIN seeks an exemption from the requirements of 

Section 91.151(b), entitled Fuel requirements for flight in VFR conditions. KEITH A. 

REDLIN submits that safety will not be affected by operation of the BLADE 350 QX AP

and DJI Inspire 1 UAs during daylight hours in visual meteorological conditions (VMC) 

under visual flight rules (VFR), with enough battery power to fly for a total duration of 
8

approximately 13.5 minutes to the first point of intended landing and, assuming normal 

cruising speed, to fly after that for at least 4.5 minutes. 

In accordance with 14 C.F.R. § 11.81, KEITH A. REDLIN provides the following 

information in support of its petition for exemption:

A. Name And Address Of The Petitioner.

The name and address of the Petitioner and point of contact is:

KEITH A. REDLIN

49252 Kilkenny Drive

Macomb, MI 48044 

Tel: (248) 881-2861

Email: keithredlin@yahoo.com

B. The Specific Sections Of 14 C.F.R. From Which KEITH A. REDLIN Seeks 

Exemption. 

1. KEITH A. REDLIN Seeks Exemption From The Requirements Of Section 

61.113(a) And (b). 

Section 61.113, entitled Private pilot privileges and limitations: Pilot in command, 

subsections (a) and (b) prescribe the following, in relevant part: 

(a) No person who holds a private pilot certificate may act as a pilot in command 

(PIC) of an aircraft that is carrying passengers or property for compensation or 

hire; nor may that person, for compensation or hire, act as PIC of an aircraft. 

(b) A private pilot may, for compensation or hire, act as PIC of an aircraft in 

connection with any business or employment if—

(1) The flight is only incidental to that business or employment; and 

(2) The aircraft does not carry passengers or property for compensation or hire. 

2. KEITH A. REDLIN Seeks Exemption From The Requirements Of Section 

91.7(a).

Section 91.7, entitled Civil aircraft airworthiness, subsection (a), states the 

following: 
9

(a) No person may operate a civil aircraft unless it is in an airworthy condition. 

3. KEITH A. REDLIN Seeks Exemption From The Requirements Of Section 

91.121. 

Section 91.121, entitled Altimeter settings, subsection (a), states the following, in 

part: 

(a) Each person operating an aircraft shall maintain the cruising altitude or flight 

level of that aircraft, as the case may be, by reference to an altimeter that is set, 

when operating--

(1) Below 18,000 feet MSL, to--

(i) The current reported altimeter setting of a station along the route and 

within 100 nautical miles of the aircraft; 

(ii) If there is no station within the area prescribed in paragraph (a)(1)(i) of 

this section, the current reported altimeter setting of an appropriate 

available station; or 

(iii) In the case of an aircraft not equipped with a radio, the elevation of the 

departure airport or an appropriate altimeter setting available before 

departure. 

4. KEITH A. REDLIN Seeks Exemption From The Requirements Of Section 

91.151(b).

Section 91.151, entitled Fuel requirements for flight in VFR conditions, subsection

(b), states the following: 

(b) No person may begin a flight in a rotorcraft under VFR conditions unless 

(considering wind and forecast weather conditions) there is enough fuel to fly 

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

fly after that for at least 20 minutes. 

5. KEITH A. REDLIN Seeks Exemption From The Requirement Of Section 

91.405(a).

Section 91.405, entitled Maintenance required, subsection (a), states the following: 

Each owner or operator of an aircraft—
10

(a) 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[.] 

6. KEITH A. REDLIN Seeks Exemption From The Requirements Of Section 

91.407(a)(1) 

Section 91.407, entitled Operation after maintenance, preventive maintenance, 

rebuilding, or alteration, subsection (a)(1), states the following: 

(a) No person may operate any aircraft that has undergone maintenance, preventive 

maintenance, rebuilding, or alteration unless--

(1) It has been approved for return to service by a person authorized under § 

43.7 of this chapter[.] 

7. KEITH A. REDLIN Seeks Exemption From The Requirements Of Sections 

91.409(a)(1) And 91.409(a)(2). 

Section 91.409, entitled Inspections, subsection (a), states the following:

(a) Except as provided in paragraph (c) of this section, no person may operate an 

aircraft unless, within the preceding 12 calendar months, it has had --

(1) An annual inspection in accordance with part 43 of this chapter and has 

been approved for return to service by a person authorized by § 43.7 of this 

chapter; or 

(2) An inspection for the issuance of an airworthiness certificate in accordance 

with part 21 of this chapter. 

8. KEITH A. REDLIN Seeks Exemption From The Requirements Of Sections 

91.417(a) And 91.417(b). 

Section 91.417, entitled Maintenance records, subsections (a) and (b), state the 

following: 

(a) Except for work performed in accordance with §§ 91.411 and 91.413, each 

registered owner or operator shall keep the following records for the periods 

specified in paragraph (b) of this section: 

(1) Records of the maintenance, preventive maintenance, and alteration and 

records of the 100-hour, annual, progressive, and other required or approved 

inspections, as appropriate, for each aircraft (including the airframe) and 
11

each engine, propeller, rotor, and appliance of an aircraft. The records must 

include--

(i) A description (or reference to data acceptable to the Administrator) of 

the work performed; and 

(ii) The date of completion of the work performed; and 

(iii) The signature, and certificate number of the person approving the 

aircraft for return to service. 

(2) Records containing the following information: 

(i) The total time in service of the airframe, each engine, each propeller, and 

each rotor. 

(ii) The current status of life-limited parts of each airframe, engine, 

propeller, rotor, and appliance. 

(iii) The time since last overhaul of all items installed on the aircraft which 

are required to be overhauled on a specified time basis. 

(iv) The current inspection status of the aircraft, including the time since the 

last inspection required by the inspection program under which the 

aircraft and its appliances are maintained. 

(v) The current status of applicable airworthiness directives (AD) and safety 

directives including, for each, the method of compliance, the AD or 

safety directive number and revision date. If the AD or safety directive 

involves recurring action, the time and date when the next action is 

required. 

(vi) Copies of the forms prescribed by § 43.9(d) of this chapter for each 

major alteration to the airframe and currently installed engines, rotors, 

propellers, and appliances. 

(b) The owner or operator shall retain the following records for the periods 

prescribed: 

(1) The records specified in paragraph (a)(1) of this section shall be retained 

until the work is repeated or superseded by other work or for 1 year after the 

work is performed. 

(2) The records specified in paragraph (a)(2) of this section shall be retained 

and transferred with the aircraft at the time the aircraft is sold. 
12

(3) A list of defects furnished to a registered owner or operator under § 43.11 of 

this chapter shall be retained until the defects are repaired and the aircraft is 

approved for return to service. 

C. The Extent Of Relief KEITH A. REDLIN Seeks And The Reason KEITH A. 

REDLIN Seeks The Relief. 

1. Extent Of Relief KEITH A. REDLIN Seeks And The Reason KEITH A. 

REDLIN Seeks Relief From Section 61.113(a) And (b). 

Relief from Section 61.113(a) and (b) entitled Private pilot privileges and 

limitations: Pilot in command, is requested to the extent necessary to allow a PIC holding a 

private pilot or higher level certificate, as well as a current and valid airman medical 

certificate, and who has met certain flight-hour and currency requirements, to conduct the 

proposed UAS flight operations for compensation or hire. 

This relief is requested since the limitations set forth in Section 61.113(a) and (b) 

state that a private pilot may, for compensation or hire, act as PIC of an aircraft in 

connection with any business or employment if: (1) The flight is only incidental to that 

business or employment; and (2) The aircraft does not carry passengers or property for 

compensation or hire. 

As set forth more fully below, KEITH A. REDLIN submits that an equivalent level 

of safety will be maintained because no PIC will be allowed to operate the BLADE 350 

QX AP UAS or DJI Inspire 1 UAS unless that PIC has met certain flight-hour and 

currency requirements, demonstrating that the PIC is able to safely operate either the 

BLADE 350 QX AP or DJI Inspire 1 UAS in a manner consistent with the operations 

specifications as described in this exemption, including evasive and emergency maneuvers, 

as well as maintaining appropriate distances from people, vessels, vehicles and structures.
13

Further, KEITH A. REDLIN submits that all flights of the BLADE 350 QX AP and 

DJI Inspire 1 UASs, conducted by the PIC pursuant to the grant of this Petition: (1) will be 

incidental to KEITH A. REDLIN’s business; and (2) will not carry passengers or property 

for compensation or hire. 

2. Extent Of Relief KEITH A. REDLIN Seeks And The Reason KEITH A. 

REDLIN Seeks Relief From Section 91.7(a). 

Relief from Section 91.7(a) entitled Civil aircraft airworthiness, is requested to the 

extent required to allow KEITH A. REDLIN to determine that the BLADE 350 QX AP

and DJI Inspire 1 UASs are in airworthy condition prior to every flight by ensuring that the 

UAS is in compliance with the operating documents (i.e., the KEITH A. REDLIN Aerial 

Operations Manual, Monthly Maintenance Log, and BLADE 350 QX AP and DJI Inspire 1 

Instruction Manual). 

KEITH A. REDLIN seeks the requested relief because the BLADE 350 QX AP

and DJI Inspire 1 UASs do not require an airworthiness certificate in accordance with 14 

C.F.R. Part 21, Subpart H. Therefore, KEITH A. REDLIN will ensure that the BLADE 

350 QX AP and DJI Inspire 1 UASs are in airworthy condition based upon its compliance 

with the operating documents (i.e., Monthly Maintenance Log, and BLADE 350 QX AP

and DJI Inspire 1 Instruction Manual) prior to every flight, and further, determine that the 

aircraft are in condition for safe flight, as stated in the conditions and limitations below.

3. Extent Of Relief KEITH A. REDLIN Seeks And The Reason KEITH A. 

REDLIN Seeks Relief From Section 91.121. 

Relief from Section 91.121, entitled Altimeter settings, may be required to allow 

flight operations of the BLADE 350 QX AP and DJI Inspire 1 UASs, which utilize a 

barometric pressure sensor, GPS equipment, and a radio communications telemetry data 

link to downlink altitude information from the UA to the PIC at the ground control station 
14

(GCS). Since the FAA requires that any altitude information concerning UAS operations 

be reported to air traffic control (ATC) in feet above ground level (AGL), KEITH A. 

REDLIN seeks the requested relief because the BLADE 350 QX AP and DJI Inspire 1 

UA’s altimeter may be set on the ground to zero feet AGL, rather than the local barometric 

pressure or field altitude, before each flight. 

Considering the limited altitude of the proposed operations, relief from 14 CFR 

91.121 is sought to the extent necessary to comply with the applicable conditions and 

limitations stated below. As more fully set forth herein, an equivalent level of safety will 

be maintained since the BLADE 350 QX AP and DJI Inspire 1 UAs are equipped with a 

barometric pressure sensor and GPS equipment, which automatically ensures that a ground 

level pressure setting will be established prior to each flight, and provides the PIC with 

altitude information of the UA on the heads-up display of the GCS. 

4. Extent Of Relief KEITH A. REDLIN Seeks And The Reason KEITH A. 

REDLIN Seeks Relief From Section 91.151(b). 

Relief from Section 91.151(b) entitled Fuel requirements for flight in VFR 

conditions, is requested to the extent required to allow flights of the battery powered 

BLADE 350 QX AP and DJI Inspire 1 UAs during daylight hours in visual meteorological 

conditions (VMC), under visual flight rules (VFR), for a total duration of 13.5 minutes to 

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

at least 4.5 minutes. KEITH A. REDLIN seeks the requested relief because without an 

exemption from Section 91.151(b), the flight time duration of the battery powered BLADE 

350 QX AP and DJI Inspire 1 UAs will severely constrain the practicality of any aerial 

video or still photo flight operations that KEITH A. REDLIN proposes to conduct pursuant 

to this Petition. 
15

Significantly, as set forth below, the technical specifications of the BLADE 350 

QX AP and DJI Inspire 1 UASs, the BLADE 350 QX AP and DJI Inspire 1 operating 

documents, and KEITH A. REDLIN’s proposed operating limitations, ensure that KEITH 

A. REDLIN will safely operate the battery powered BLADE 350 QX AP and DJI Inspire 1 

UAs during daylight hours in visual meteorological conditions (VMC), under visual flight 

rules (VFR), with enough battery power to fly for a total duration of 13.5 minutes to the 

first point of intended landing and, assuming normal cruising speed, to fly after that for at 

least 4.5 minutes.

5. Extent Of Relief KEITH A. REDLIN Seeks And The Reason KEITH A. 

REDLIN Seeks Relief From Sections 91.405(a), 91.407(a)(1), 91.409(a)(1) & 

(a)(2), And 91.417(a) & (b). 

Since Sections 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b) 

only apply to aircraft with an airworthiness certificate, KEITH A. REDLIN requests relief 

from these Sections because the BLADE 350 QX AP and DJI Inspire 1 UASs do not 

require airworthiness certificates. As set forth more fully below, the BLADE 350 QX AP

and DJI Inspire 1 UASs meet the conditions of FMRA Section 333 for operation without 

an airworthiness certificate. Accordingly, KEITH A. REDLIN will use trained technicians 

to perform maintenance, alterations, or preventive maintenance on the UASs using the 

methods, techniques, and practices prescribed in the UAS operating documents (i.e., the 

KEITH A. REDLIN Aerial Operations Manual, Monthly Maintenance Log, and BLADE 

350 QX AP and DJI Inspire 1 Instruction Manual). Furthermore, KEITH A. REDLIN will 

document and maintain all maintenance records for the BLADE 350 QX AP and DJI 

Inspire 1 UASs. 

D. The Reasons Why Granting KEITH A. REDLIN’s Request Would Be In The 

Public Interest; That Is, How It Would Benefit The Public As A Whole. 
16

Granting the present Petition will further the public interest by allowing KEITH A. 

REDLIN to safely, efficiently, and economically perform aerial video and photography of 

construction sites, real estate, special events, film sets, and landscape over certain areas of 

the United States.

Additionally, use of the BLADE 350 QX AP and DJI Inspire 1 UASs will decrease 

congestion of the NAS, reduce pollution, and provide significant benefits to the economy.

Notably, the benefits of KEITH A. REDLIN’s proposed operation of the BLADE 350 QX 

AP and DJI Inspire 1 UASs will be realized without implicating any privacy issues. 

1. The Public Will Benefit From Decreased Congestion Of The NAS. 

The BLADE 350 QX AP and DJI Inspire 1 UAs are battery powered and serve as a 

safe, efficient, and economical alternative to the manned aircraft traditionally utilized to 

obtain aerial imagery. By reducing the amount of manned aircraft needed to perform aerial 

acquisitions, an exemption allowing the use of a BLADE 350 QX AP or DJI Inspire 1 

UAS would reduce the amount of manned aircraft in the NAS, reduce noise and air 

pollution, as well as increase the safety of life and property in the air and on the ground. 

Furthermore, by reducing the number of manned aircraft operating in the NAS, 

congestion around airports caused by arriving and departing aircraft will be reduced. The 

BLADE 350 QX AP and DJI Inspire 1 UAs do not require an airport to takeoff or land. 

Likewise, a reduction of manned aircraft conducting aerial video and photography 

missions would result in fewer aircraft that must be handled by air traffic control during 

the ground, takeoff, departure, arrival, and landing phases of flight operations.

2. The Public Will Benefit From The Safety And Efficiency Of The BLADE 

350 QX AP and DJI Inspire 1 UASs. 
17

Conducting aerial acquisitions with the BLADE 350 QX AP and DJI Inspire 1 

UASs, instead of manned aircraft, will greatly benefit the public by drastically reducing the 

levels of air and noise pollution generated during traditional aerial video and still 

photography flight operations. By using battery power and electric motors, the BLADE 

350 QX AP and DJI Inspire 1 UASs produce no air pollution, and is the most viable 

environmentally conscious alternative to the cabin class, six cylinder internal combustion 

engine aircraft that are typically utilized for aerial video and photography, while burning 

approximately 20-30 gallons per hour of leaded aviation fuel. The BLADE 350 QX AP

and DJI Inspire 1 UAs, while reducing the carbon footprint of aerial acquisitions, also 

eliminates noise pollution, as the UAs are propelled by battery powered electric motors, 

rather than an internal combustion engine. 

By using the BLADE 350 QX AP and DJI Inspire 1 UASs to perform aerial 

acquisitions, the substantial risk to life and property in the air and on the ground, which is 

usually associated with traditional manned aircraft flight operations, will be substantially 

reduced or completely eliminated. Aside from the lack of flight crew members located 

onboard the aircraft, the BLADE 350 QX AP and DJI Inspire 1 UAs (BLADE QX AP 

weighing approximately 33.7 ounces and the DJI Inspire 1 weighing approximately 6 

pounds respectively, at their maximum gross weights with BLADES 350 QX AP lengths 

of 18.3 inches and DGI Inspire 1 17.2 inches respectively, BLADE 350 QX AP widths of 

18.3 inches and DJI Inspire 1 17.8 inches respectively, and with no fuel on board), has less 

physical potential for collateral damage to life and property on the ground, and in the air, 

compared to the manned aircraft that typically conduct similar operations (weighing 
18

approximately 6,000 pounds with a wingspan of approximately 42 feet, a length of 34 feet, 

and a fuel capacity of 180 gallons). 

3. Performing Aerial Video and Photography Operations With The BLADE 

350 QX AP and DJI Inspire 1 UASs Will Benefit The Economy. 

In addition to being safe and efficient, the BLADE 350 QX AP and DJI Inspire 1

UASs are also an economical alternative to using manned aircraft to conduct similar aerial 

operations. As such, operation of the BLADE 350 QX AP and DJI Inspire 1 UASs will 

allow United States based companies, like KEITH A. REDLIN, to remain competitive and 

contribute to growth of the U.S. economy. Specifically, with the rising cost of aviation fuel 

and the Environmental Protection Agency (“EPA”) regulatory actions phasing out leaded 

aviation fuels, U.S. owned and operated companies must adopt new and alternative 

technology in order to remain competitive. Operating the battery powered BLADE 350 QX 

AP and DJI Inspire 1 UASs is one such technology that not only allows companies greater 

operational flexibility compared to manned aircraft, but provides such flexibility without 

the high operational cost of a traditional manned aircraft. 

By operating the BLADE 350 QX AP and DJI Inspire 1 UASs, companies such as 

KEITH A. REDLIN, can remain competitive and profitable, and therefore, provide greater 

job stability to employees and contractors, which will ultimately contribute to growth of 

the U.S. economy. Improved financial performance of U.S. companies, through 

commercial use of the BLADE 350 QX AP and DJI Inspire 1 UASs, provides a stable 

workforce that increases consumer spending; improves local, state, and federal tax 

revenues; and allows companies to invest in research and development in order to remain 

competitive both in the United States and abroad. 

4. There Are No Privacy Issues. 
19

Similar to the manned aerial acquisition flight operations that have been conducted for 

decades, KEITH A. REDLIN’s proposed operation of the BLADE 350 QX AP and DJI 

Inspire 1 UASs will not implicate any privacy issues. Specifically, the BLADE 350 QX 

AP and DJI Inspire 1 UASs will be operated only in compliance with operating documents 

(i.e., the KEITH A. REDLIN Aerial Operations Manual, Monthly Maintenance Log, and 

BLADE 350 QX AP and DJI Inspire 1 Instruction Manual) which requires property owner 

involvement as well as local law enforcement notification, and in accordance with the 

Federal Aviation Regulations, including the minimum altitude requirements of 14 C.F.R. § 

91.119. 

E. The Reasons Why Granting The Exemption Would Not Adversely Affect Safety, 

Or How The Exemption Would Provide A Level Of Safety At Least Equal To That 

Provided By The Rule From Which KEITH A. REDLIN Seeks Exemption. 

1. Reasons Why The BLADE 350 QX AP and DJI Inspire 1 UAs Meet The 

Conditions Of The FAA Modernization and Reform Act of 2012 (FMRA) 

Section 333. 

In consideration of the size, weight, speed, and limited operating area associated 

with the unmanned aircraft and its operation, KEITH A. REDLIN’s operation of the 

BLADE 350 QX AP and DJI Inspire 1 UASs meet the conditions of FMRA Section 333, 

and will not require an airworthiness certificate in accordance with 14 C.F.R. Part 21, 

Subpart H. 

Section 333 provides authority for a UAS to operate without airworthiness 

certification and sets forth requirements for considering whether a UAS will create a 

hazard to users of the NAS or the public, or otherwise pose a threat to national security. 

Specifically, FMRA Section 333 states the following, in part: 

(a) In General.--Notwithstanding any other requirement of this subtitle, and not 

later than 180 days after the date of enactment of this Act, the Secretary of 

Transportation shall determine if certain unmanned aircraft systems may 
20

operate safely in the national airspace system before completion of the plan 

and rulemaking required by section 332 of this Act or the guidance required by 

section 334 of this Act. 

(b) Assessment of Unmanned Aircraft Systems.--In making the determination under 

subsection (a), the Secretary shall determine, at a minimum--

(1) which types of unmanned aircraft systems, if any, as a result of their 

size, weight, speed, operational capability, proximity to airports and 

populated areas, and operation within visual line of sight do not create 

a hazard to users of the national airspace system or the public or pose a 

threat to national security; and

(2) whether a certificate of waiver, certificate of authorization, or 

airworthiness certification under section 44704 of title 49, United States 

Code, is required for the operation of unmanned aircraft systems 

identified under paragraph (1). 

(c) Requirements for Safe Operation.--If the Secretary determines under this 

section that certain unmanned aircraft systems may operate safely in the 

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

operation of such aircraft systems in the national airspace system. 

In seeking this exemption, KEITH A. REDLIN submits that the BLADE 350 QX 

AP and DJI Inspire 1 UASs can operate safely in the NAS pursuant to FMRA Section 333, 

as demonstrated by: (a) the characteristics of the BLADE 350 QX AP and DJI Inspire 1 

UASs; (b) the pilot certification requirement; and (c) the specific operating limitations. 

a. The Specifications Of The BLADE 350 QX AP and DJI Inspire 1 UASs 

Demonstrate Its Safe Characteristics.

The BLADE 350 QX AP and DJI Inspire 1 UASs do not create a hazard to users of 

the NAS or the public, or otherwise pose a threat to national security considering its size, 

weight, speed, and operational capability. 

i. Technical Specifications Of The BLADE 350 QX AP and DJI Inspire 

1 UASs. 
21

The technical specifications of the BLADE 350 QX AP and DJI Inspire 1 UASs are 

set forth by the BLADE 350 QX AP and DJI Inspire 1 Specifications and Data Sheet, 

attached hereto as Exhibit A and B. 

ii. The BLADE 350 QX AP and DJI Inspire 1 UASs Autonomous Flight 

And Navigation Modes Enable The UASs To Remain Within A 

Defined Operational Area. 

The BLADE 350 QX AP and DJI Inspire 1 UASs may be operated in both manual 

and fully autonomous flight modes. A complete description of the flight and navigational 

modes of the BLADE 350 QX AP and DJI Inspire 1 UASs is provided at page 8 of the 

BLADE 350 QX AP and pages 12-16 and 45-50 of the DJI Inspire 1 User Manuals, 

attached hereto as Exhibit C and D. 

iii. The BLADE 350 QX AP and DJI Inspire 1 UASs Are Designed For 

Automatic Return To Home Point Or Hover In The Event Of Loss 

Of The Control Link Or Navigation. 

When the Control Link is lost, the BLADE 350 QX AP and DJI Inspire 1 UAs will 

remain stationary, in flight, for 3 seconds or more. If, after 3 seconds, the BLADE 350 QX 

AP and DJI Inspire 1 UAs do not reacquire control link data from the GCS, the UAs will 

assume that the Control Link is lost and the UAs will return to the home position (i.e., 

failsafe mode) via GPS, and will descend to the takeoff position and shutdown. 

A complete description of the Failsafe Functions of the BLADE 350 QX AP UAS 

are set forth at pages 27 through 29 and for the DJI Inspire 1 at pages 11 of the BLADE 

350 QX AP and DJI Inspire 1 User Manuals, attached hereto as Exhibit C and D. 

iv. The BLADE 350 QX AP and DJI Inspire 1 GCS And Its Operation.

A complete description of the operation and specifications of the BLADE 350 QX 

AP and DJI Inspire 1 GCS and flight control software is provided at pages 1 through 18 of 

the BLADE 350 QX AP User Manual and pages 40 through 47 of the DJI Inspire 1 User 
22

Manual. BLADE 350 QX AP and DJI Inspire 1 User Manuals are attached hereto as 

Exhibits C and D.

b. Flight Operations Of BLADE 350 QX AP and DJI Inspire 1 UASs Are 

Limited To The Line Of Sight Of A Certificated Pilot in Command With 

A Safety Observer. 

KEITH A. REDLIN will only utilize certificated pilots who possess a current and 

valid airman medical certificate to act as a pilot in command (PIC) of the BLADE 350 QX 

AP and DJI Inspire 1 UASs. Additionally, a safety observer will assist all pilots during 

flight time. 

c. Flights Of BLADE 350 QX AP and DJI Inspire 1 UASs Will Be 

Conducted Pursuant To Specific Operating Limitations. 

In seeking this exemption, KEITH A. REDLIN proposes to commercially operate 

BLADE 350 QX AP and DJI Inspire 1 UASs for the special purpose of conducting aerial 

video and photography over certain areas of United States, pursuant to the following 

specific operating limitations:

1. Operations authorized by this grant of exemption will be limited to the following 

aircraft described in the operating documents, rotorcraft UASs weighing less 

than 55 pounds maximum gross weight: BLADE 350 QX AP and DJI Inspire 1

Unmanned Aircraft Systems. Proposed operations of any other aircraft will 

require a new petition or a petition to amend this grant. 

2. UAS operations under this exemption will be limited to conducting operations 

for the purpose of aerial video and photography. 

3. The UAs may not be flown at an indicated airspeed exceeding 20 knots.

4. The UA must be operated at an altitude of no more than 500 feet above ground 

level (AGL), as indicated by the procedures specified in the operating 

documents unless a special request is made and approved by ATC. All altitudes 

reported to ATC must be in feet AGL. 

5. The UAs must be operated within visual line of sight (VLOS) of the PIC at all 

times. This requires the PIC to be able to use human vision unaided by any 

device other than corrective lenses, as specified on the PIC’s FAA-issued airman 

medical certificate. 
23

6. The use of first person view (FPV) by the PIC or safety observer (SO) is not 

permitted. 

7. All operations must utilize a safety observer (SO). The SO may be used to satisfy 

the VLOS requirement as long as the PIC always maintains VLOS capability. 

The SO and PIC must be able to communicate verbally at all times. Electronic 

messaging or texting is not permitted during flight operations. The PIC must be 

designated before the flight and cannot transfer his or her designation for the 

duration of the flight. The PIC must ensure that the SO can perform the 

functions prescribed in the operating documents. 

8. The SO must not perform any other duties beyond assisting the PIC with seeing 

and avoiding other air traffic and other ground based obstacles/obstructions and 

is not permitted to operate the camera or other instruments. 

9. The operating documents and the grant of exemption must be accessible during 

UAS operations and made available to the Administrator upon request. If a 

discrepancy exists between the conditions and limitations contained in the grant 

of exemption and the procedures outlined in the operating documents, the 

conditions and limitations contained in the grant of exemption take precedence 

and must be followed. Otherwise, the operator must follow the procedures as 

outlined in its operating documents. The operator may update or revise its 

operating documents. It is the operator’s responsibility to track such revisions 

and present updated and revised documents to the Administrator upon request. 

The operator must also present updated and revised documents if it petitions for 

extension or amendment to the grant of exemption. If the operator determines 

that any update or revision would affect the basis upon which the FAA granted 

the exemption, then the operator must petition for amendment to its grant of 

exemption. The FAA’s UAS Integration Office (AFS-80) may be contacted if 

questions arise regarding updates or revisions to the operating documents. 

10. Prior to each flight the PIC must inspect the UAS to ensure that it is in a 

condition for safe flight. If the inspection reveals a condition that affects the 

safe operation of the UAS, the aircraft is prohibited from operating until the 

necessary maintenance has been performed and the UAS is found to be in a 

condition for safe flight. The Ground Control Station must be included in the 

preflight inspection. All maintenance and alterations must be properly 

documented in the aircraft records.

11. Any UAS that has undergone maintenance or alterations that affect the UAS 

operation or flight characteristics, e.g. replacement of a flight critical 

component, must undergo a functional test flight. The PIC who conducts the 

functional test flight must make an entry in the aircraft records. 

12. The pre-flight inspection must account for all potential discrepancies, e.g. 

inoperable components, items, or equipment, not already covered in the 

relevant sections of the operating documents. 
24

13. The operator must follow the UAS manufacturer’s aircraft/component, 

maintenance, overhaul, replacement, inspection, and life limit requirements. 

14. The operator must carry out its maintenance, inspections, and record keeping 

requirements, in accordance with the operating documents. Maintenance, 

inspection, alterations, and status of replacement/overhaul component parts 

must be noted in the aircraft records, including total time in service, description 

of work accomplished, and the signature of the authorized person returning the 

UAS to service. 

15. Each UASs operated under this exemption must comply with all manufacturer 

Safety Bulletins. 

16. The authorized person must make an entry in the aircraft record of the 

corrective action taken against discrepancies discovered between inspections. 

17. The PIC must possess at least a private pilot certificate and at least a current 

third- class medical certificate. 

18. The operator may not permit any PIC to operate unless the PIC meets the 

operator’s qualification criteria and demonstrates the ability to safely operate 

the UAS in a manner consistent with how the UAS will be operated under the 

exemption, including evasive and emergency maneuvers and maintaining 

appropriate distances from persons, vessels, vehicles and structures. PIC 

qualification flight hours must be logged in a manner consistent with 14 C.F.R. 

§ 61.51(b). Flights for the purposes of training the operator’s PICs are 

permitted under the terms of the exemption. However, training operations may 

only be conducted during dedicated training sessions. During training, 

proficiency, and experience-building flights, all persons not essential for flight 

operations are considered nonparticipants, and the PIC must operate the UA 

with appropriate distance from nonparticipants in accordance with 14 C.F.R. § 

91.119. 

19. UAS operations may not be conducted during night, as defined in 14 C.F.R. § 

1.1. All operations must be conducted under visual meteorological conditions 

(VMC). If flight at night is required, a special request will be made at the FAA 

office closest to proposed area of operations. Flights under special visual flight 

rules (SVFR) are not authorized. 

20. The UA may not operate within 5 nautical miles of an airport reference point as 

denoted on a current FAA-published aeronautical chart unless a letter of 

agreement with that airport’s management is obtained, and the operation is 

conducted in accordance with a NOTAM as required by the operator’s COA.

The letter of agreement with the airport management must be made available to 

the Administrator upon request. 
25

21. The UA may not be operated less than 500 feet below or less than 2,000 feet 

horizontally from a cloud or when visibility is less than 3 statute miles from the 

PIC. 

22. If the UA loses communications or loses its GPS signal, it must return to a predetermined location within the planned operating area and land or be recovered 

in accordance with the operating documents. 

23. The PIC must abort the flight in the event of unpredicted obstacles or 

emergencies in accordance with the operating documents. 

24. The PIC is prohibited from beginning a flight unless (considering wind and 

forecast weather conditions) there is enough power to fly at normal cruising 

speed to the intended landing point and land the UA with 25% battery power 

remaining. 

25. The operator must obtain an Air Traffic Organization (ATO) issued Certificate 

of Waiver or Authorization (COA) prior to conducting any operations under the 

grant of exemption. This COA will also require the operator to request a Notice 

to Airman (NOTAM) not more than 72 hours in advance, but not less than 48 

hours prior to the operation. All operations shall be conducted in accordance 

with airspace requirements in the ATO issued COA including class of airspace, 

altitude level and potential transponder requirements. 

26. All aircraft operated in accordance with the exemption must be identified by 

serial number, registered in accordance with 14 C.F.R. part 47, and have 

identification (N- Number) markings in accordance with 14 C.F.R. part 45, 

Subpart C. Markings must be as large as practicable. 

27. Before conducting operations, the radio frequency spectrum used for operation 

and control of the UA must comply with the Federal Communications 

Commission (FCC) or other appropriate government oversight agency 

requirements. 

28. The documents required fewer than 14 C.F.R. 91.9 and 91.203 must be 

available to the PIC at the Ground Control Station of the UAS any time the 

UAS is operating. These documents must be made available to the 

Administrator or any law enforcement official upon request. 

29. The UA must remain clear and yield the right of way to all manned aviation 

operations and activities at all times. 

30. The UAS may not be operated by the PIC from any moving device or vehicle.

31. Flight operations must be conducted at least 500 feet from all nonparticipating 

persons (persons other than the PIC, SO, operator trainees or essential persons), 

vessels, vehicles, and structures unless: 
26

a. Barriers or structures are present that sufficiently protect nonparticipating 

persons from the UA and/or debris in the event of an accident. The 

operator must ensure that nonparticipating persons remain under such 

protection. If a situation arises where nonparticipating persons leave such 

protection and are within 500 feet of the UA, flight operations must cease 

immediately and/or; 

b. The aircraft is operated near vessels, vehicles or structures where the 

owner/controller of such vessels, vehicles or structures has granted 

permission and the PIC has made a safety assessment of the risk of 

operating closer to those objects and determined that it does not present 

an undue hazard, and; 

c. Operations nearer to the PIC, SO, operator trainees or essential persons 

do not present an undue hazard to those persons per § 91.119(a). 

32. All operations shall be conducted over private or controlled-access property 

with permission from the land owner/controller or authorized representative. 

Permission from land owner/controller or authorized representative will be 

obtained for each flight to be conducted.

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

vertical boundaries of the operational area as defined by the applicable COA 

must be reported to the FAA's UAS Integration Office (AFS-80) within 24 

hours. Accidents must be reported to the National Transportation Safety Board 

(NTSB) per instructions contained on the NTSB Web site: www.ntsb.gov. 

2. Reasons Why An Exemption From The Requirements Of Section 61.113(a) 

And (b) Would Not Adversely Affect Safety.

KEITH A. REDLIN submits that the equivalent level of safety established by 

Section 61.113(a) and (b) will be maintained because no PIC will be allowed to operate the 

BLADE 350 QX AP and DJI Inspire 1 UASs unless that PIC has demonstrated, by meeting 

minimum flight-hour and currency requirements, that the PIC is able to safely operate the 

BLADE 350 QX AP or DJI Inspire 1 UAS in a manner consistent with the exemption, 

including evasive and emergency maneuvers and maintaining appropriate distances from 

people, vessels, vehicles and structures. 

Considering KEITH A. REDLIN’s proposed area of operations, and the operating 

limitations set forth-above; the parallel nature of private pilot aeronautical knowledge 
27

requirements to those of commercial pilot requirements (See Exemption No. 11062); and 

the airmanship skills necessary to safely operate the BLADE 350 QX AP or DJI Inspire 1

UAS, KEITH A. REDLIN submits that the additional manned airmanship experience of a 

commercially certificated pilot would not correlate to the airmanship skills necessary for 

KEITH A. REDLIN’s specific proposed flight operations. 

The FAA has previously granted relief from Section 61.113(a) and (b) specific to 

UAS, in circumstances similar, in all material respects, to those presented herein (e.g. 

Exemption Nos. 11062, 11063, 11064, 11065, 11066, 11067, 11080, 11109, 11110, 11112, 

11136, 11138, 11150, 11153, 11156, 11158, 11159, 11160, 11161). 

KEITH A. REDLIN will not allow any PIC to operate the BLADE 350 QX AP or

DJI Inspire 1 UAS unless that PIC has demonstrated, by meeting minimum flight-hour 

requirements or the BLADE 350 QX AP or DJI Inspire 1 UAS training and currency 

requirements, that the PIC is able to safely operate the BLADE 350 QX AP or DJI Inspire 

1 UAS in a manner consistent with this exemption, including evasive and emergency 

maneuvers and maintaining appropriate distances from people, vessels, vehicles and 

structures. 

Specifically, the PIC must have accumulated and logged, in a manner consistent 

with 14 C.F.R. § 61.51(b), 25 hours of total time as a UAS rotorcraft pilot (with a 

minimum of 5 hours of those hours as a UAS pilot operating the same make and model of 

UAS to be used for operations under the exemption). In addition to the hour requirements, 

the PIC must accomplish 3 takeoffs and landings in the preceding 90 days (for currency 

purposes). 
28

As in Exemption Nos. 11062, 11138, and 11153, prior documented flight 

experience that was obtained in compliance with applicable regulations will ensure an 

equivalent level of safety during KEITH A. REDLIN’s proposed operations. The 

Administrator has held that prior documented flight experience that was obtained in 

compliance with applicable regulations would ensure safe operations, stating as follows: 

In Exemption No. 11062, the FAA required that prior to conducting operations for 

the purpose of motion picture filming (or similar operations), the PIC must have 

accumulated and logged, in a manner consistent with 14 CFR 61.51(b), 25 hours of 

total time as a UAS rotorcraft pilot including at least 10 hours logged as a UAS 

pilot with a multi-rotor UAS. Prior to operations under Exemption No. 11062, the 

PIC must also have accumulated and logged a minimum of 5 hours as a UAS pilot 

operating the same make and model of UAS to be used for operations under the 

exemption. For clarification, the FAA considers these minimum hour requirements 

to be inclusive rather than additive; i.e. 5 hours make and model time may be 

included in the 10 hours of multi-rotor time and the 10 hours may be included in 

the total 25 hours of UAS rotorcraft time. In addition to the hour requirements, the 

PIC must accomplish 3 takeoffs and landings in the preceding 90 days (for 

currency purposes). The FAA finds that at a minimum, the flight-hour requirements 

in Exemption No. 11062 are appropriate to practice and build proficiency in the 

skills necessary to safely conduct the petitioner’s proposed operations. The FAA 

also finds that prior documented flight experience that was obtained in compliance 

with applicable regulations would satisfy this requirement. Training, proficiency, 

and experience-building flights can also be conducted under the grant of exemption 

to accomplish the required flight time. During training, proficiency, and 

experience-building flights the PIC is required to operate the UA with appropriate 

distances in accordance with 14 C.F.R 91.119. 

Exemption No. 11138 at page 15. 

Accordingly, KEITH A. REDLIN will ensure safe operations by not allowing any 

PIC to operate the BLADE 350 QX AP or DJI Inspire 1 UAS unless that PIC has 

demonstrated, by meeting minimum flight-hour and currency requirements, that the PIC is 

able to safely operate the BLADE 350 QX AP or DJI Inspire 1 UAS in a manner consistent 

with the exemption, including evasive and emergency maneuvers and maintaining 

appropriate distances from people, vessels, vehicles and structures. 
29

3. Reasons Why An Exemption From The Requirements Of Section 91.7(a) 

Would Not Adversely Affect Safety. 

The equivalent level of safety established by Section 91.7(a) will be maintained 

because prior to every flight, KEITH A. REDLIN will ensure that the BLADE 350 QX AP

or DJI Inspire 1 UAS is in an airworthy condition based upon the UAS’s compliance with 

its operating documents and as stated in the conditions and limitations herein. 

Additionally, the FAA has previously granted relief from Section 91.7(a) specific 

to UAS, in circumstances similar, in all material respects, to those presented herein (e.g. 

Exemption Nos. 11062, 11063, 11064, 11065, 11066, 11067, 11080, 11109, 11110, 11112, 

11136, 11138, 11150, 11153, 11156, 11157, 11158, 11159, 11160, 11161). 

4. Reasons Why An Exemption From The Requirements Of Section 91.121 

Would Not Adversely Affect Safety.

The equivalent level of safety established by Section 91.121 will be maintained 

because the altitude information of the BLADE 350 QX AP and DJI Inspire 1 UAs will be 

provided to the PIC via GPS equipment and a radio communications telemetry data link, 

which downlinks from the UA to the GCS for active monitoring of the flight path and 

altitude. This altitude information, combined with KEITH A. REDLIN’s operation of the 

BLADE 350 QX AP and DJI Inspire 1 UAs within visual line of sight, at or below 500 feet 

AGL, will ensure a level of safety equivalent to Section 91.121. The altitude information 

will be generated by GPS equipment installed onboard the aircraft. Prior to each flight, a 

zero altitude initiation point is automatically established by the UASs at ground level. 

The FAA has previously granted relief from Section 91.121 specific to UAS, in 

circumstances similar, in all material respects, to those presented herein (e.g. Exemption 

Nos. 11062, 11063, 11064, 11065, 11066, 11067, 11080, 11109, 11112, 11136, 11138, 

11150, 11153, 11156, 11157, 11158, 11159, 11160, 11161). 
30

5. Reasons Why An Exemption From The Requirements Of Section 91.151(b) 

Would Not Adversely Affect Safety.

A grant of this exemption would ensure an equivalent level of safety established by 

14 C.F.R. Section 91.151(b) as a result of (1) the technical specifications of the BLADE 

350 QX AP and DJI Inspire 1 UASs; (2) the limitations on the proposed flight operations; 

and (3) the location of the proposed flight operations. Accordingly, KEITH A. REDLIN

will ensure that it will safely operate the battery powered BLADE 350 QX AP and DJI 

Inspire 1 UAs during daylight hours in VFR conditions, with enough battery power to fly 

for a total duration of 13.5 minutes to the first point of intended landing and, assuming 

normal cruising speed, to fly after that for at least 4.5 minutes. 

Here, as in Exemption No. 11109, the technical specifications of the BLADE 350 

QX AP and DJI Inspire 1 UASs; the limitations on the proposed flight operations; and the 

location of the proposed operations, will ensure an equivalent level of safety established by 

14 C.F.R. Section 91.151(b). Furthermore, safety will be ensured as the BLADE 350 QX 

AP and DJI Inspire 1 UASs provide audible and visual warnings to the PIC at the GCS 

when the UAs experiences low battery voltage, the first warning occurring at 

approximately 33% remaining battery power, and again at approximately 10% remaining 

battery power. At the critically low battery level, the DJI Phantom Vision+ and DJI Inspire 

1 UASs will descend and land automatically. 

Significantly, previous exemptions granted by the FAA concerning Section 91.151 

establish that safety is not adversely affected when the technical characteristics and 

operating limitations of the UAS are considered. Relief has been granted for manned 

aircraft to operate at less than the minimums prescribed in Section 91.151, including 

Exemption Nos. 2689, 5745, and 10650. Moreover, the FAA has previously granted relief 
31

from Section 91.151 specific to UAS, in circumstances similar, in all material respects, to 

those presented herein (e.g. Exemption Nos. 8811, 10808, 10673, 11042, 11062, 11063, 

11064, 11065, 11066, 11067, 11080, 11109, 11110, 11136, 11138, 11150, 11153, 11156, 

11157, 11158, 11159, 11160, 11161). 

6. Reasons Why An Exemption From The Requirements Of Sections

91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), And 91.417(a) & (b) Would 

Not Adversely Affect Safety. 

In seeking this exemption, KEITH A. REDLIN submits that the equivalent level of 

safety with regard to the regulatory maintenance and alteration requirements established by 

Sections 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b) will be met 

because KEITH A. REDLIN will use trained technicians to perform maintenance, 

alterations, or preventive maintenance on the UASs using the methods, techniques, and 

practices prescribed in the operating documents (i.e., the KEITH A. REDLIN Aerial 

Operations Manual, Monthly Maintenance Log, and BLADE 350 QX AP and DJI Inspire 1 

Instruction Manual). Furthermore, KEITH A. REDLIN will document and maintain all 

maintenance records for the BLADE 350 QX AP and DJI Inspire 1 UASs. 

Since the BLADE 350 QX AP and DJI Inspire 1 UASs will be inspected as 

prescribed by the operating documents, KEITH A. REDLIN will maintain the equivalent 

level of safety established by Sections 91.405(a), 91.409(a)(1), and 91.409(a)(2). A copy 

of the BLADE 350 QX AP and DJI Inspire 1 User Manuals are attached hereto as Exhibit 

C and D; a copy of the BLADE 350 QX AP and DJI Inspire 1 UAS Maintenance LOG is 

attached hereto as Exhibit E. 

Likewise, the exemption sought will not adversely affect safety because KEITH A. 

REDLIN will use trained technicians to perform maintenance, alterations or preventive 
32

maintenance on the UAS using the methods, techniques, and practices prescribed by the 

operating documents. 

Furthermore, the exemption sought would maintain an equivalent level of safety 

established by Sections 91.407, 91.417(a) and 91.417(b), because all maintenance of the 

BLADE 350 QX AP and DJI Inspire 1 UASs will be performed by trained technicians. 

Maintenance will be documented and maintained utilizing the monthly maintenance log. 

Significantly, previous exemptions granted by the FAA concerning Sections 

91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b) establish that safety is 

not adversely affected when the technical characteristics and operating limitations of the 

UAS are considered. 

In consideration of KEITH A. REDLIN’s proposed operating limitations, the 

operating documents, and the technical aspects of the BLADE 350 QX AP and DJI Inspire 

1 UASs, KEITH A. REDLIN submits that safety will not be adversely affected by granting 

exemption from 14 C.F.R. Sections 91.405(a), 91.407(a)(1) and (a)(2), 91.409(a)(2), and 

91.417(a) and (b). The FAA has previously granted relief specific to UAS in circumstances 

similar, in all material respects, to those presented herein (e.g. Exemption Nos. 11062, 

11063, 11064, 11065, 11066, 11067, 11080, 11109, 11110, 11112, 11136, 11138, 11150, 

11153, 11156, 11157, 11158, 11159, 11160, 11161). 

7. The FAA May Prescribe Any Other Conditions For Safe Operation. 

In accordance with Section 333 of the FAA Modernization and Reform Act of 2012 

(FMRA) and 14 C.F.R. § 21.16 entitled Special Conditions, KEITH A. REDLIN requests 

that the FAA prescribe special conditions for the intended operation of the BLADE 350 

QX AP and DJI Inspire 1 UASs, which contain such safety standards that the 
33

Administrator finds necessary to establish a level of safety equivalent to that established by 

14 C.F.R. Part 21, Subpart H, and 14 C.F.R §§ 61.113(a) & (b), 91.7 (a), 91.121, 

91.151(b), 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b). Such 

special conditions will permit safe operation of the UAs for the limited purpose of 

conducting aerial video and photography over certain areas of the United States for 

compensation or hire. FMRA Section 333 sets forth the requirements for considering 

whether a UAS will create a hazard to users of the NAS or the public, or otherwise pose a 

threat to national security; and further, provides the authority for such UAS to operate 

without airworthiness certification in accordance with any requirements that must be 

established for the safe operation of the UAS in the NAS. 

Likewise, the Administrator may prescribe special conditions pursuant to 14 C.F.R.

§ 21.16, for operation of the BLADE 350 QX AP and DJI Inspire 1 UASs, since the 

airworthiness regulations of 14 C.F.R. Part 21 do not contain adequate or appropriate 

safety standards, due to the novel or unusual design features of the aircraft. Section 21.16, 

entitled Special Conditions, states the following: 

If the FAA finds that the airworthiness regulations of this subchapter do not contain 

adequate or appropriate safety standards for an aircraft, aircraft engine, or propeller 

because of a novel or unusual design feature of the aircraft, aircraft engine or 

propeller, he prescribes special conditions and amendments thereto for the product. 

The special conditions are issued in accordance with Part 11 of this chapter and 

contain such safety standards for the aircraft, aircraft engine or propeller as the 

FAA finds necessary to establish a level of safety equivalent to that established in 

the regulations. 

See 14 C.F.R. § 21.16.

Therefore, in accordance with FMRA Section 333 and 14 C.F.R. § 21.16, the FAA 

may prescribe special conditions for Leading Edge’s intended operation of the BLADE 

350 QX AP and DJI Inspire 1 UASs, which contain such safety standards that the 
34

Administrator finds necessary to establish a level of safety equivalent to that established by 

14 C.F.R. Part 21, Subpart H, and 14 C.F.R Sections 61.113(a) & (b), 91.7(a), 91.121, 

91.151(b), 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b).

F. A Summary That Can Be Published In The Federal Register, stating: The Rules 

From Which KEITH A. REDLIN Seeks Exemption: 

KEITH A. REDLIN seeks exemption from the requirements of 14 C.F.R Sections 

61.113(a)&(b), 91.7(a), 91.121, 91.151(b), 91.405(a), 91.407(a)(1), 91.409(a)(1) & 

(a)(2), and 91.417(a) & (b). 

A Brief Description Of The Nature Of The Exemption KEITH A. REDLIN

Seeks: 

This exemption will permit KEITH A. REDLIN to commercially operate an 

Unmanned Aircraft System (UAS) for the purpose of conducting aerial video and 

photography over certain areas of the United States.

G. Any Additional Information, Views, Or Arguments Available To Support KEITH 

A. REDLIN’s Request. 

This Petition is made pursuant to the FAA Modernization and Reform Act of 2012 

(FMRA) Section 333, which directs the Secretary of Transportation to determine if certain 

UAS may operate safely in the NAS. As such, KEITH A. REDLIN’s request for 

exemption may be granted pursuant to the authority of FMRA Section 333 and 14 C.F.R. 

Part 11, as set forth above. 

FMRA Section 333 sets forth the requirements for considering whether a UAS will 

create a hazard to users of the NAS or the public, or otherwise pose a threat to national 

security; and further, provides the authority for such UAS to operate without airworthiness 

certification. 

As discussed in detail above, KEITH A. REDLIN will operate the BLADE 350 QX 

AP and DJI Inspire 1 UASs safely in the NAS, without creating a hazard to users of the 

NAS, or the public, or otherwise pose a threat to national security. 
35

CONCLUSION

As set forth herein, KEITH A. REDLIN seeks an exemption pursuant to 14 C.F.R. 

§ 11.61 and Section 333 of the FAA Modernization and Reform Act of 2012 (FMRA), 

which will permit safe operation of the BLADE 350 QX AP and DJI Inspire 1 UASs 

commercially, without an airworthiness certificate, for the limited purpose of conducting 

aerial video and photography over certain areas of the United States. By granting this 

Petition, the FAA Administrator will be fulfilling the Congressional mandate of the FAA 

Modernization and Reform Act of 2012, while also advancing the interests of the public, 

by allowing KEITH A. REDLIN to safely, efficiently, and economically operate the 

BLADE 350 QX AP and DJI Inspire 1 UASs commercially within the NAS. 

WHEREFORE, in accordance with the Federal Aviation Regulations and the FAA 

Modernization and Reform Act of 2012, Section 333, KEITH A. REDLIN respectfully 

requests that the Administrator grant this Petition for an exemption from the requirements 

of 14 C.F.R Sections 61.113(a) & (b), 91.7(a), 91.121, 91.151(b), 91.405(a), 91.407(a)(1), 

91.409(a)(1) & (a)(2), and 91.417(a) & (b), and permit Leading Edge to operate the 

BLADE 350 QX AP and DJI Inspire 1 UASs commercially for the purpose of conducting 

aerial video and photography over certain areas of the United States.

Dated: April 11, 2015

Respectfully submitted,

KEITH A. REDLIN

_________________________
36

KEITH A. REDLIN

49252 Kilkenny

Macomb, MI 4804

Tel: (248) 881-2861

Appendices:

A – BLADE 350 QX AP Specifications Data Sheet

B – DJI Inspire 1 Specifications Data Sheet

C – BLADE 350 QX AP Manufacturer’s User Manual

D – DJI Inspire 1 Manufacturer’s User Manual

E – Monthly Maintenance Log
37

APPENDIX – A

BLADE 350 QX APTECHNICAL SPECIFICATIONS

KEITH A. REDLIN only utilizes safe and reliable UASs. BLADE is an industry leader in 

small UAS production. BLADE 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, BLADE software provides 

real-time altitude and location information to the PIC via the linked monitor (smart 

phone/tablet devices)

1.1 BLADE 350 QX AP

1.1.1 Aircraft

1.1.1.1 Supported Battery – 3000mAh 3S 11.1V 20C Li-Po Battery

1.1.1.2 Weight (Battery & Propellers Included) – 35.5 oz (1006 g)

1.1.1.3 Hover Accuracy (Ready to Fly) – Vertical: .8m; Horizontal: 2.5m

1.1.1.4 Max Yaw Angular Velocity - 2000/s

1.1.1.5 Max Tilt Angel - 350

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 – GB200 2-Axis Brushless Gimbal

1.1.2.2 Control Accuracy - ±0.030

1.1.2.3 Controllable Range – Pitch: -900 - 00

1.1.2.4 Maximum Angular Speed – Pitch: 900/s

1.1.3 Camera

1.1.3.1 Operating Temperature Range - 320F - 1040F (00C - 400C)

1.1.3.2 Sensor Size – 1/2.3”

1.1.3.3 Effective Pixels – 14M

1.1.3.4 Resolution – 4384x3288

4.1.3.5 HD Video Recording – 1080p30 & 720p

4.1.3.6 Recording Field of View - 1100/850

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
38

APPENDIX – B
39

DJI INSPIRE 1 TECHNICAL SPECIFICATIONS

KEITH A. REDLIN 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)

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

2.2.1.13 Propeller Model – DJI 1345

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: 1200/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
40

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
41

APPENDIX – C

BLADE 350 QX AP Manufacturer’s User Manual
42

APPENDIX – D

DJI Inspire 1 Manufacturer’s User Manual
43

APPENDIX – E

month:_________(year:________

UAS$#:$___________

Date(Issue(

Discovered

Date(Issue(

Addressed

Software(Updates

Airframe(

Engines

Propellers

Camera(Gimbal

Landing(Gear

Vibration(Dampening

Other:

MONTHLY$MAINTENANCE$LOG

Issue(Description(&(Maintenance(Conducted Maintenance(Performed(By:(((

Print(&(Sign