Technical Demonstrations and Training

Using small UAS serves the p ublic i nterest :

• Demonstrations and training by a credentialed, experienced

, and Safety Management

System (SMS) disciplined flight company provide an ideal venue to discuss sUAS

technology, review regulations, and promote safe sUAS ope rations

.

• sUAS demonstrations and training promote STEM

- related career paths and support

workforce development.

• Demonstrations provide an opportunity to increase awareness of sUAS capability for

academia, industry, and government to make informed decisions regarding sUAS

program start

- up or how to become a service provider.

• Demonstrations offer customer markets the opportunity to understand the capabilities

and efficiencies of sUAS conducting an aerial survey with electro

- optical ( v isual,

infrared

, and hype r

- spectral spectrum) sensors.

• Delivering sUAS training by an experienced, professional, and skilled provider reduces

risk to the customer and public.

Aviation Systems Engineering Company

Aviation Systems Engineering Company (ASEC) , Inc. is a veteran

- owned small business

headquartered in Lexington Park, MD, with offices in Anacostia, VA, Jacksonville, FL, Dallas, TX,

and Seattle, WA. ASEC has the required corporate capability and proven aviation processes, tools,

and knowledge drawn from t en years of requirements development, acquisition support, systems

engineering, policy management, flight test conduct, outreach, and operational experience. This

background, along with a highly professional aviation

- safety culture, makes ASEC an ideal

can didate for being granted an exemption.

ASEC maintains a diversified technical staff that includes over 140 senior engineers, analysts, and

operators, including former military personnel who boast decades of engineering, operational, and

test experience. ASEC’s flight department is led by senior aviators, United States Navy Test Pilot

School (USNTPS) graduates, and instructors that bring decades of experience in the development

and conduct of airborne operations relevant to the support of UAS operations. A SEC employees

include experienced UAS and payload operators, airspace specialists, airfield site survey specialists,

test and evaluation professionals, UAS subject

- matter

- experts, and range safety support personnel.

As corporate policy, ASEC operates to t he standards developed and adopted by the International

Business Aviation Council (IBAC) and all of its Member Associations, including the National

Business Aviation Association (NBAA). These standards were developed using best practices

common throughout the business aviation community and, as such, reflect the high standards of

operational safety that we wish to achieve in this company. Our Flight Department is certified SMS

Stage 2 compliant by the International Standard for Business Aircraft Operations (IS

- BAO) and

offers a high level of safety and professional flight services to support the research and development

of new airborne technologies, payload integration and certification, and provisions for chase or

surrogate aircraft. ASEC ’ s best practices i nclude FAA elements that supplement our UAS SMS

approach. ASEC’s Flight Department was one of the first Flight Test Research and Development

organizations to implement IS

- BAO’s SMS practices and seek IS

- BAO review and certification.ASEC’s Flight Operation s Manual was the first ever reviewed by IS

- BAO to address UAS

operations.

In 2014, ASEC’s SMS process was validated by NASA

- Kennedy Space Center (KSC),

demonstrating our ability to provide a broad spectrum of independent, meticulous, and analytical

evaluat ion as well as range safety expertise and experience. ASEC led efforts to conduct multiple

small UAS aviation events by providing demonstration planning, design, and execution for Space

Florida in coordination with NASA

- KSC, US Air Force 45th Space Wing, t he FAA, and the

Association of Unmanned Vehicle Systems International (AUVSI). ASEC conducted individual

technical and training reviews for ten small UAS and their operators that included airworthiness

assessments and risk analyses. ASEC organized and led num erous stakeholder briefings, develop ed

processes and related documents

, and provided the range safety team to direct all sUAS flight

operations. As a member of the Mid

- Atlantic Aviation Partnership supporting UAS Test Site

, ASEC was requested to support sUAS requirements ’ development and range safety operations.

ASEC C orporate Aviation Safety and Compliance Culture

• ASEC personnel have limited their operation of sUAS to that of hobbyists or as employees performing duties in support of D epartment of Defense (D oD ) or D epartment

of Homeland Security (D HS ) operations

. To date, ASEC members have not engaged in

any commercial activity to ensure its compliance with applicable FARs or local, state,

and federal laws.

• ASEC has a detailed sUAS Flight Operati ons Manual, sUAS Maintenance Program

, and

sUAS Aircrew Training Program that it shall follow should this exemption be approved.

All three documents are submitted with this request.

ASEC sUAS Description

• ASEC will operate DJI’s Inspire and Phantom sUAS multirotor aircraft

.

• DJI sUAS multirotor aircraft have fail

- safe features to include geo fencing and lost

- link

return

- home capability. DJI is the manufacturer of multirotor aircraft weighing less than

25 pounds and has developed technology that enhances safe sUAS operations within the

NAS.

Summary of sUAS Characteristics

Model Inspire T600

Weight (Battery Included) 2935 g 103.5 oz

6.5 lb

Hovering Accuracy Vertical: 0.5 m 1.6 ft

Horizontal: 2.5 m 8.2 ft

Max Angular Velocity Yaw: 150°/s

Max Tilt Angle 35°

Max Ascent Speed 5 m/s 16.4 ft/s

Max Descent Speed 4 m/s 13.1 ft/s

Max Speed 22 m/s 72.2 ft/s

Max Flight Time 18 min

Operating Temperature Range

- 10 ° to 40 ° CDimensions 438 × 451 × 301 mm 18 × 18 × 12 inches

Model Phantom

Weight (Battery Included) <1000 g 3 5

. 2 oz

2.2 lb

Hovering Accuracy Vertical: 0. 8 m 2.6 ft

Horizontal: 2.5 m 8.2 ft

Max Angular Velocity Yaw: 20 0°/s

Max Tilt Angle 4 5°

Max Ascent Speed 6 m/s 1 9

. 6 ft/s

Max Descent Speed 6 m/s 1 9

. 6 ft/s

Max Speed 10 m/s 32.8 ft/s

Max Flight Time 15 min

Operating Temperature Range

- 10 ° to 5 0 ° C

Di agonal Distance 350 mm 14 inches

Aircraft and an Equivalent Level of Safety

• ASEC proposes that the exemption requested apply to civil aircraft that have the

characteristics and operate with the limitations listed herein.

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

under the current regulatory structure because the proposed operations represent a

safety enhancement to the already safe operations conducted with conventional aircraft.This Exemption Request is for Use of sUAS subject to Extensive Operational and Safety

Requirements

At a minimum, t he limitations and conditions to which ASEC agrees to be bound when conducting

commercia l operations under an FAA issued exemption include :

• Operators

o The sUAS pilot

- in

- command (PIC) shall possess, at a minimum, a private

pilot certificate and current third

- class medical certificate. The PIC shall 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.

o The PIC shall be trained in the operation of the specific make and model of the

sUAS being piloted and have successfully complet ed all required training.

o The PIC shall have accumulated and logged, in a manner consistent with 14

CFR §61.51 (b), a minimum of 25 hours of total time as a sUAS rotorcraft

pilot and at least five hours logged as a sUAS pilot with a similar sUAS type

(mult irotor or helicopter). Prior documented flight experience obtained in

compliance with applicable regulations may satisfy this requirement.

o The PIC shall have accumulated and logged, in a manner consistent with 14

CFR §61.51 (b), a minimum of five hours as sUAS pilot operating the make

and model of sUAS to be utilized for operations under the exemption as well

as three take

- offs and three landings in the preceding 90 days.

o Training, proficiency, and experience

- building flights can also be conducted

under thi s grant of exemption to accomplish the required flight cycles and

flight time.

o During training, proficiency, and experience

- building flights, all persons not

essential for flight operations are considered nonparticipants, and the PIC must

operate the sUAS with appropriate distance from nonparticipants in

accordance with 14 CFR §91.119.

o The sUAS Visual Observer (VO) shall meet all training requirements and be

responsible for all of his or her duties as set forth by ASEC sUAS Flight

Operations Manual.

o The PIC and Sensor Operator (SO) will be designated before each flight. The

minimum crew for each flight operation will consist of the sUAS PIC, the SO

and the VO.

o The PIC and SO remains within visual line of sight (VLOS) of each other and

the VO and in direct ve rbal communication at all times.

o Safety briefings are conducted before each day’s activities to include, but not

limited to:

 Designated roles of PIC

, SO , and VO

 Risk management and mitigation

• Specifications and Designo All sUAS flown under this exemption sh all be less than 10 pounds including

aircraft and payload. This exemption requests permission only with respect to

the specific use of the DJI Inspire and Phantom models

, each weighing less

than 10 pounds including its payload.

o The radio frequency spectrum used for operation and control of the sUAS shall

comply with the Federal Communications Commission (FCC) or other

appropriate government oversight agency requirements.

o Maximum speed shall be less than 50 knots (84 f t/s ).

o The sU AS shall be equipped with inertial navigation s ensor (s) and gyroscopes

. (IRS/IRU/Accelerometer/MEMS Gyroscopes).

o The sUAS shall be equipped with a compass ( magnetometer / heading source ).

o The sUAS shall be equipped with a global positioning s ystem (GPS) guidance

system.

o The sUAS shall be designed, should it lose communications or lose its GPS

signal, to return to a predetermined location within a designated parameter and

land or be recovered in accordance with ASEC ’s sUAS Flight Operat ions

Manual.

• Mainten ance

o The s UAS shall be maintained in accordance with the manufacturer’s

recommendations and ASEC sUAS Flight Operat ions Manual and

Maintenance Program.

o ASEC will document and maintain a record of the sUAS maintenance,

preventative maintenance, alterations, and status of replacement, overhaul ed

component parts, and the total time in service of the sUAS. These records will

be maintained at the principle base for operation for the life of the aircraft or as

required by F AA regulations . See ASEC sUAS Flight Ope rati ons Manual and

Maintenance Program for additional details.

o ASEC shall comply with all manufacturer safety and service b ulletins or

equivalent documents pertaining to the sUAS aircraft.

o The PIC shall perform a preflight inspection of the sUAS, controlle r, and

ground control station prior to each flight to ensure it is operational with no

discrepancies. The sUAS will only be operated when all systems are

operating per manufacture r ’s specifications an d in a discrepanc y

- free

condition.

o Maintenance or repa irs that may affect the sUAS operation or flight

characteristics shall undergo a functional test flight when required in

accordance with manufacture r’ s recommendations and ASEC’s sUAS Flight

Operations Manual . This functional test flight shall be recorded in the sUAS’s

records. When the functional test flight is completed successfully, the sUAS

can be returned to service by the PIC.

o ASEC shall follow the manufacturer’s sUAS maintenance, overhaul,

replacement, inspection, and life limit requirements. When no t provided by themanufacturer

, specifications for aircraft, component, overhaul, replacement,

and inspection maintenance requirements shall be established and included in

ASEC’s sUAS Flight Operations Manual and Maintenance Program

. At a

minimum

, the following inspections will be established :

 Actuators/ s ervos

 Powerplant(s) (motors)

 Propellers

 Electronic speed controller(s)

 Batteries

 Remote controllers and g round control station

o All sUAS are identified by the serial number, registered in accordance with 14

CFR Part 47, and have identification (N

- number ) markings in accordance with

14 CFR Part 45 .29

, except with respect to the size of the markings. Markings

shall be as large as practicable.

• Operations

o All required permissions and permits shall be obtained from territorial, state,

county

, or city jurisdictions, including local law enforcement or other

appropriate governmental agencies.

 At least three days before a scheduled operational flight, ASEC shall

submit a written plan of activities to the local flig ht standards district

office (FSDO) with jurisdiction over the area of the proposed flight.

This three

- day notification may be waived with the concurrence of the

FSDO. The plan of activities shall include at least the following

information :

- Dates and times for all requested flights

- Name and phone number of ASEC sUAS Flight Operations

- Name, certificate, and phone number of the responsible PIC

- Make, model, and serial and N

- number of sUAS to be used

- Statement from ASEC that it will be operating on approved property

, and if requested by the inspector, a list of who provided permission

- Description of the flight activity, including maps or diagrams of any

area over which flights will be conducted, the relationship of that area

to any nearby city, town, etc., and the altitudes essential to accomplish

the operation

- Signature of exemption

- holder or representative

 Documents required under 14 CFR §91.9 and §91.203 shall be readily

available to the PIC any time the aircraft is in operation. These

d ocuments shall be made available to the FAA Administrator or any

law enforcement official upon request.

 ASEC shall obtain an air traffic organization (ATO) issued certificateof waiver or authorization (COA) prior to conducting any operations

under this gr ant of exemption.

 ASEC shall also request a notice to airman (NOTAM) not more than

72 hours in advance of , but not less than 48 hours prior to

, the

operation.

 ASEC shall obtain the consent of all persons involved in the operation

and ensure that only consenting persons be allowed within 500 feet of

the operations area

.

o The sUAS shall not operate within five nautical miles of the geographic center

of any airport as designated on the 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. This letter of agreement with the airport management shall be

made available to the FAA Administrator upon request.

o The sUAS will only operate within the lateral boundaries of approved

property. An operations area within those boundaries will be established for

each flight. These are as will be free of unnecessary hazards or risks and

nonparticipating personnel.

o The sUAS shall only operate within a predefined operations area that shall be

thoroughly inspected by the PIC for buildings, overhangs, obstacles, wires,

poles, people, vehicl es, sun angle, shadows, glare, reflective surfaces, clouds,

smoke, and terrain among other potential hazards.

o Flights shall be conducted under day visual meteorological conditions (VMC).

 In addition, the sUAS shall 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.

 sUAS operations shall not be conducted during night, as defined in 14

CFR §1.1.

 Fl i ghts shall not be conducted under special visual flight rules (SVFR).

o Flights shall be operated at an altitude at or below 400 feet above ground level

( AGL ) , as indicated by the procedures specified in ASEC’s sUAS Flight

Operations Manual

.

o The PIC shall be prohibited from operating the sUAS from any moving device

or vehicle.

o The sUAS shall be operated within VLOS of the PIC.

 The PIC shall maintain VLOS without the aid of telescopes, cameras

, or other devices.

 The PIC will maintain VLOS with their own vision, which includes the

use of eyeglasses or corrective lenses as specified on the PIC’s medical

certificate.

o The sUAS shall remain clear and yield the right of way to manned operations

and activities at all times including, but not limited to, ultralight vehicles,parachute activities, parasailing activities, hang gl iders, etc.

o ASEC will require the PIC

, SO

, and VO to have successfully completed a

qualification process which will include ground and flight training, as outlined

in the ASEC sUAS Aircrew Training Program

.

o The PIC’s primary responsibility is the safe operation of the sUAS while in

flight

.

• SUAS Flight Time and Flight Durations

o DJI Inspire and Phantom operations complete within 15 and 18 minutes flight

time or with 25% battery power remaining whichever occurs first.Table 1

Regulations for Which Exemptions are Requested

Unless otherwise requesting an exemption, ASEC, the PIC, SO, VO , maintenance support,

and the sUAS shall comply with all applicable parts of 14 CFR including, but not limited

to, Parts 45, 47, 61, and 91.

ASEC is requesting exemptions from the following FAR to the extent necessary to enable

the requested sUAS operations for the reasons detailed below.

Relief sought from 14 CFR ASEC Statement

21 Stated Below

61.113(a) and (b) Stated Below

91.119(c) Stated Below

91.121 Stated Below

91.151(a)(1) Stated Below

91.405(a) Stated Below

91.407(a)(1) Stated Below

91.409(a)(1) and (2) Stated Below

91.417(a) and (b) Stated Below

14 CFR 21

– Requirements to Secure Airworthiness Certificates

1. Airworthiness exemptions should be given because size, weight, and operation areas

of the sUAS meet the level of safety necessary for exemption under Section 333 of

the Reform Act.

2. FAA has the authority to exempt aircraft from airworthiness certificate

requirements under the Act (49 U.S.C. § 44701 (f)) and Section 333 of the

Reform Act.

3. See Grant of Exemptions: 11062, 11063, 11064, 11065, 11066, 11067, 11080,

11109, 11110, 11111, 11112, 11114, 11136, and 11138

.

14 CFR 61.113 (a) and (b)

– Private Pilot Privileges and Limitations : Pilot in Command

1. Since there are no standards for private or commercial sUAS operations, ASEC

requests to utilize at least private pilots with a third class medical in support of its

own operations.

2. Knowledge of flight characteristics and the F ARs

, along with the ability to physically

manipulate the controls of the sUAS are the critical aspects of the requested operation.

ASEC can accomplish this by using a private pilot that has specific training on the

sUAS aircraft and operates in accordance with the ASEC sUAS Flight Operations

Manual

, F ARs

, and local, state

, and federal laws.

3. The risks associated with the operation of a sUAS are so diminished from the level of

risk associated with commercial aviation operations contemplated by Part 61 when

drafted, that allowing operations of the sUAS as requested with a private pilot as thePIC exceeds the present level of safety achieved by 14 C.F.R. §61.113 (a) & (b).

4. See Grant of Exemptions: 11062, 11063, 11064, 11065, 11066, 11067, 11080, 11109,

11110, 11111, 11112, 11114, 11136, and 11138

.

14 CFR 91.119(c)

– Requirements for Minimum Safe Altitudes for Civil Aircraft Operation

1. The sUAS wil l be operated at or below 400 feet AGL.

2. ASEC shall obtain the consent of all persons involved in the operation and ensure

that only consenting persons be allowed within 500 feet of the operations area

.

3. The sUAS will only operate within the lateral boundaries of approved property. An

operations area within those boundaries will be established for each flight. These

areas will be free of unnecessary hazards or risks and non participating personnel.

4. Given the size, weight, speed, material, and operation of the sUAS aircraft,

equivalent levels of safety will be achieved.

5. See Grant of Exemptions: 11062, 11063, 11064, 11065, 11066, 11067, 11080, 11109,

11110, 11111, 11112, 11114, 11136, and 11138.

14 CFR 91.121

– Altimeter Settings

1. Since the sUAS will not have a barometric altimeter and may use a GPS

altitude read

- out indication instead, an exemption may be needed.

2. An equivalent level of safety will be achieved by the operator as the sUAS uses AGL

height from its initialization/takeoff point.

3. See Grant of Exemptions: 11062, 11063, 11064, 11065, 11066, 11067, 11080, 11109,

11136, and 11138.

14 CFR 91.151 (a) (1)

– Fuel Requirements for Flights in VFR Conditions

1. ASEC feels an equivalent level of safety can be obtained by terminating the flight

relative to specific aircraft fuel (battery power) requirements for the planned sUAS, the

DJI Inspire. ASEC plans to terminate DJI Inspire and Phantom flight prior to 15 an d

18 minutes respectively, or 25% remaining battery power, whichever occurs first.

2. Both the DJI Inspire and Phantom models have a second level of safety that is achieved

through the use of an aircraft battery monitoring system. The se aircraft system s alert

the operator of low battery voltage and return the respective aircraft to its takeo ff

location before its battery capacity is depleted.

3. ASEC will not operate sUAS at night in accordance with 14 CFR 1.1

4. See Grant of Exemptions: 11062, 11063, 11064, 11065, 11066, 11067, 11080, 11109,

11110 , 11112 , 11136, and 11138.

14 CFR 91.405 (a)

– Maintenance Required

This section and Part 43 apply only to aircraft with an airworthiness certificate; therefore

, these sections will not apply to our request

.

ASEC and the aircraft manufacturer (DJI) are the most familiar with the aircraft and best

suited to maintain the aircraft in an airworthy condition. This maintenance process allowsfor an equivalent level of safety to be achieved due to the limited size, s cope

, and area of

operations.

In the absence of regulatory provisions addressing sUAS required maintenance, see the

ASEC sUAS Flight Operations Manual

, ASEC sUAS Maintenance Program

, and

manufacturer’s maintenance recommendations for requirements

.

1. Maintenance will be accomplished by ASEC pursuant to the manufacturer’s

recommendations and ASEC’s sUAS Flight Operations Manual and

Maintenance Program.

2. Maintenance, preventive maintenance, rebuilding, and alteration will be

successfully accomplished by trained personnel only.

3. The ASEC sUAS Flight Operations Manual and ASEC sUAS Maintenance

Program detail how to enter work performed in the maintenance log for scheduled

and unscheduled maintenance or functional test flights that are performed.

4. ASEC shall only operate its sUAS with all systems functioning per

manufacture r’ s specification in a discrepancy

- free condition.

5. Maintenance records will be maintained at the principle base for operation for the

life of the aircraft or as required by FAR

.

6. See Grant of Exemptions: 11062, 11063, 11064, 11065, 11066, 11067, 11080,

11109, 11136, and 11138.

14 CFR 91.407 (a) (1)

– Operation after Maintenance, Preventive Maintenance, Rebuilding or

Alteration

This section and Part 43 apply only to aircraft with an airworthiness certificate; therefore

these sections will not apply to our request

.

ASEC and the aircraft m anufacturer (DJI) are the most familiar with the aircraft and best

suited to maintain the aircraft in an airworthy condition. These maintenance proced ures allow for an equivalent level of safety to be achieved due to the limited size, scope

, and

area of operations.

In the absence of regulatory provisions addressing sUAS operation after maintenance,

preventive maintenance, rebuilding, alteration or functional test flights, ASEC has

developed requirements to address these topics. See the ASEC sUAS Flight Operations

Manual

, ASEC sUAS Maintenance Program

, and Aircraft Manufa cturer’s Users Guide

.

1. Maintenance will be accomplished by ASEC pursuant to the manufacturer’s

recommendations and ASEC’s sUAS Flight Operations Manual and

Maintenance Program.

2. Maintenance, preventive maintenance, rebuilding, and alteration will be

successfully accomplished by trained personnel only.

3. Functional test flights will be performed by the PIC when required ; the sUAS return

to service only when a functional test flight is successfully completed. When a

mechanical issue arises

, the sUAS will land safely or be recovered within the

operations area

.4. The ASEC sUAS Flight Operations Manual details how to enter performance of

scheduled and unscheduled maintenance or functional test flights in the

maintenance log

.

5. ASEC shall only operate its sUAS with all systems functioning per

manufacture r’ s specification in a discrepancy

- free condition.

6. These records will be maintained at the principle base for operation for the life of

the aircraft or as required by FAR

.

7. See Grant of Exemptions: 11062, 11063, 11064, 11065, 11066, 11067, 11080,

11109, 11136, and 11138.

14 CFR 91.409 (a) (1) and (2)

– Inspections

This section and Part 43 apply only to aircraft with an airworthiness certificate; therefore

these sections will not apply to our request

.

ASEC and the aircraft manufacturer (DJI) are the most familiar with the aircraft and best

suited to maintain the aircraft in an airworthy condition. These maintenance inspections

allow for an equivalent level of safety to be achieved due to the limited size, scope

, and

area of operations.

In the absence of regulatory provisions addressing sUAS inspections, ASEC has developed

requirements to address this topic. See the ASEC sUAS Flight Operations Manual

, Maintenance Program, and Aircraft Manufacturer’s Users Guide

1. Maint enance will be accomplished by ASEC pursuant to the manufacturer’s

recommendations and ASEC’s sUAS Flight Operations Manual and

Maintenance Program.

2. Maintenance, preventive maintenance, rebuilding, and alteration will be

successfully accomplished by trained personnel only.

3. The ASEC sUAS Flight Operations Manual details how to enter performance of all

inspections into the maintenance log

.

4. Functional test flight s will be performed by the PIC when required after inspections ;

the sUAS shall return to service when the flight is successfully completed. When a

mechanical issue arises

, the sUAS will land safely or be recovered within the

operations area

.

5. ASEC shall only operate its sUAS with all systems functioning per

manufacture r’ s specification in a discrepancy

- free condition.

6. These records will be maintained at the principle base for operation for the life of

the aircraft or as required by FAR

.

7. See Grant of Exemptions: 11062, 11063, 11064, 11065, 11066, 11067, 11080,

11109, 11136, and 11138.

14 CFR 91.417(a) and (b)

– Maintenance Records

This section and Part 43 apply only to aircraft with an airworthiness certificate; therefore

these sections will not apply to our request

.ASEC and the aircraft manufacturer (DJI) are the most familiar with th e aircraft and best

suited to maintain the aircraft in an airworthy condition. These maintenance records allow

for an equivalent level of safety to be achieved due to the limited size, scope

, and area of

operations.

In the absence of regulatory provisions addressing sUAS maintenance records, ASEC has

developed requirements to address this topic. See the ASEC sUAS Flight Operations

Manual and Maintenance Program.

1. Maintenance will be accomplished by ASEC pursuant to the

manufacturer’s recommendations and ASEC’s sUAS Flight Operations

Manual

.

2. Maintenance, preventive maintenance, rebuilding, and alteration maintenance will be

performed by trained personnel and detailed records entered in the respective aircraft

maintenance log at the completion of each event. The ASEC sUAS Flight Operations

Manual details how entries are to be made in the aircraft maintenance log for

scheduled and unscheduled maintenance or functional test flights that are performed.

3. These records will be maintained at the principle base for operation for the life of

the aircraft or as required by FAR.

4. See Grant of Exemptions: 11062, 11063, 11064, 11065, 11066, 11067, 11080,

11109, 11136, and 11138.