1

July 8th, 2015

U. S. Department of Transportation 

Docket Management System

1200 New Jersey Ave., SE 

Washington, DC 20590

Re: Exemption Request Section 333 of the FAA Reform Act and Part 11 of the Federal Aviation 

Regulations from 14 CFR: Part 21 subpart H; 45.23(b); 61.113 (a) & (b); 91.7(a); 91.9(b) (2); 91.103 (b); 

91.109; 91.119; 91.121; 91.151(a); 91.203(a) & (b); 91.405 (a); 91.407(a) (1); 91.409 (a) (2); 91.417 (a) & 

(b).

Dear Sir or Madam:

Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 (the Reform Act) and 

14 C.F.R. Part 11, Dynegy Inc, an electric utility company, hereby applies for an exemption from the listed 

Federal Aviation Regulations (“FARS”) to allow commercial operation of its small Unmanned Aircraft 

System (“sUAS”) for aerial inspection of power plant facilities owned by subsidiaries of Dynegy Inc., which 

are secure and controlled sites, so long as operations are conducted within and under the conditions 

outlined herein or as may be established by the FAA as required by Section 333.

As detailed in this document, the requested exemption would permit the operation of sUAS under 

controlled conditions in airspace that is 1) limited 2) predetermined 3) controlled as to access and 4)

would provide safety enhancements to the safety protocols already followed by Dynegy at each of its

power plant sites. Approval of this exemption would thereby enhance safety and fulfill the Secretary of 

Transportation’s (the FAA Administrator’s) responsibilities to “...establish requirements for the safe 

operation of such aircraft systems in the national airspace system.” Section 333(c) of the Reform Act.

The name and address of the applicant is:

Dynegy Incorporated

1500 Eastport Plaza Drive

Collinsville, IL 62234

Matthew C. Rains

PH: 618-343-7764

Email: matthew.rains@dynegy.com

Regulations from which the exemption is requested: 

14 C.F.R. Part 21 subpart H

14 C.F.R. 45.23 (b)

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

14 C.F.R. 91.7 (a)

14 C.F.R. 91.9 (b) (2)

14 C.F.R. 91.103

14 C.F.R. 91.109

14 C.F.R. 91.119

14 C.F.R. 91.121

14 C.F.R 91.151 (a)

14 C.F.R. 91.203 (a) & (b) 

14 C.F.R. 91.405 (a)

14 C.F.R. 91.407 (a) (1)

14 C.F.R. 91.409 (a) (2)

14 C.F.R. 91.417 (a) & (b)
2

I. STATUTORY AUTHORITY FOR EXEMPTIONS

The Federal Aviation Act expressly grants the FAA authority to issue exemptions. This statutory 

authority includes exempting civil aircraft, as the term is defined under §40101 of the Act, including

sUASs, from the requirement that all civil aircraft must have a current airworthiness certificate.

The Administrator may grant an exemption from a requirement of a regulation prescribed under 

subsection (a) or (b) of this section or any sections 44702-44716 of this title if the Administrator finds the 

exemption in the public interest. 49 U.S.C. §44701(f) See also 49 USC §44711(a); 49 USC §44704; 14

CFR §91.203(a) (1).

Section 333(b) of the Reform Act assists the Secretary in determining whether sUAS may operate 

in the National Airspace System (NAS) without creating a hazard to the user, the public, or a threat to 

national security. In making this determination, the Secretary must consider:

 The sUAS’s size, weight, speed, and operational capability

 Whether the sUAS operates within the visual line of sight of the operator

 Whether the sUAS operates outside of highly populated areas and away from close proximity to 

airports

Reform Act §333(a). If the Secretary determines that a sUAS “may operate safely in the

national airspace system, the Secretary shall establish requirements for the safe operation of such aircraft 

in the national airspace system.” Id. §333(c).

Dynegy’s sUAS is a DJI Inspire One, multirotor vehicle, weighing 10 or fewer lbs. including 

payload. It operates under normal conditions at a speed of no more than 50 knots and has the capability 

to hover and move in the vertical and horizontal plane simultaneously. The sUAS will operate only in the 

pilot’s visual line of sight at all times and will operate within the property boundaries of any Dynegy power 

plant. See attached Exhibit 1 for a complete list of applicable properties. Dynegy intends to implement 

operating controls which will insure that the sUAS will “not create a hazard to users of the national

airspace system or the public.” Reform Act Section 333 (b).

Given the nature of power plant inspections, stacks can range from less than 300’ AGL to 1000’ 

AGL. Visual inspection of these stacks are required every three years at most, but often annual 

inspections are required. Dynegy has over 50 stacks which could lead to 15 inspections a year. Stack 

inspections are always high risk tasks given the height and environmental factors required for an “eyes 

on” inspection. Dynegy believes it is in the public’s best interest to greatly reduce the number of 

inspections performed by employees and replace the inherent danger with our sUAS. 

Dynegy does possess power plants which are located within 5NM of airports, within populated 

areas as defined on FAA sectionals, and has direct need to fly the sUAS above 400’AGL only for the 

power plant exhaust stack external inspections. However, Dynegy has the authority to manage all 

personnel within its property boundaries and during any aerial inspection by the sUAS, all personnel will 

be 1) made fully aware of the inspection and 2) cleared from the area unless operations dictate otherwise. 

Dynegy will NOT fly above 400’AGL outside of Dynegy property boundaries. Any flight not in Class G 

airspace will be done with a VHF aviation radio with contact and radio calls made to the appropriate 

Control Tower or CTAF as applicable. No flight will be performed where a Mode C Transponder is 

required unless explicit permission from local Class B or Class C Control Tower has been issued. 
3

Based on the small size of the sUAS involved, the controlled boundaries of each power plant

within which they will operate, and complete control of minimal population of personnel which will be 

below the flight path, Dynegy’s application falls squarely within the level of safety in which Congress 

envisioned that the FAA may, by exemption, allow commercial operations of sUAS to commence 

immediately. 

Given the clear direction in Section 333 of the Reform Act, the authority contained in the Federal 

Aviation Act, as amended; the strong equivalent level of safety surrounding the proposed operations, and 

the significant public benefit, including enhanced safety, the grant of the requested exemptions is in the 

public interest. Accordingly, Dynegy Inc respectfully requests that the FAA grant the requested exemption 

without delay.

II. PUBLIC INTEREST

This exemption application is expressly submitted to fulfill Congress’ goal in passing Section 

333(a) through (c) of the Reform Act. This law directs the Secretary of Transportation to consider whether 

certain unmanned aircraft systems may operate safely in the NAS before completion of the rulemaking 

required under Section 332 of the Reform Act. By granting an exemption, the FAA will fulfill Congress’s 

intent of allowing UAS to operate with significant safety precautions in low risk environments.

The use of sUAS on a power plant site can significantly reduce the risk to workers of falls while 

inspecting, surveying, or monitoring site facilities. Small UAS can inspect, photograph, and collect data on 

hard to access areas that otherwise would require employee or contractor inspections. Falls are always a 

major concern when working at power plant sites, and reducing the potential of falls through sUAS use for 

site imaging and inspections will minimize the number of potential hazards from elevated locations.

Finally, sUAS will aid in reducing the environmental impact of power plants. By visually inspecting 

areas difficult to access more regularly and with a wider range of views, overall plant efficiency will be 

improved. Improved plant efficiency dramatically decreases amount of carbon and waste required to 

produce the same amount of power. The long term returns from this reduction of resources and resultant 

waste will greatly benefit the environment. Additionally, the current energy use for facility inspection, 

aerial imaging and data collection over a plant site requires a distinctly greater amount of resources and 

power compared to a sUAS which uses use rechargeable lithium ion batteries as opposed to fossil fuels.

Due to the significantly reduced situations which current employees and contractors work in 

dangerous locations to inspect plant facilities, the decreased environmental footprint which can be 

achieved through plant efficiencies gained by more thorough inspections, and the reduced energy cost to 

perform such inspections, Dynegy requests the FAA accept these factors as adequate for evidence of 

benefits to the public sectors by granting this exemption application.

III. EQUIVALENT LEVEL OF SAFETY

Dynegy proposes that the exemption requested herein apply to sUAS that have the 

characteristics and that operate with the limitations listed herein. These limitations provide for at least an 

equivalent or even higher level of safety to operations under the current regulatory structure because the 

proposed operations represent a safety enhancement to the already safe protocols followed on 

construction sites and imaging and surveying operations conducted with helicopters and other 

conventional aircraft.
4

Dynegy will be bound by the following limitations when conducting its sUAS operations under an FAA 

issued exemption:

1. The sUAS will be less than 10 pounds.

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

3. Maximum total flight time for each operational flight will be 30 minutes. The UAS calculates 

battery reserve in real time, and will return to its ground station with at least 20% battery power 

reserve should that occur prior to the 30 minute limit.

4. Flights will typically be operated below an altitude of 400 feet AGL. However, some facility 

inspections of power plants will require flight up to 1000’ AGL. These inspections will be for the 

exhaust stacks which are inherently designated dangerous airspace to manned aircraft.

Sectionals with plant locations plotted are available upon request due to total file size.

5. Crew for each operation will consist of the sUAS Pilot who will keep the sUAS within visual line of 

sight at all times. An additional Visual Observer / Camera Crew-Member may be involved, but is 

not required for safe flight.

6. The sUAS Pilot will be trained in flight, operations, and safety procedures.

7. The sUAS will only operate within the boundaries of a Dynegy owned and operated utility power 

station property. This includes enclosed structures, exhaust stacks, coal yards, ash ponds, and 

cooling water sources if located on Dynegy property.

8. A briefing will be conducted in regard to the planned sUAS operations prior to each day’s 

production activities. Personnel performing duties within the area of the flight plan will receive a 

safety briefing and ensure personnel are cleared from areas below flight paths as practical unless 

essential to plant operations.

9. Pilot will have been trained in operation of UASs generally and received up-to-date information on 

the particular UAS to be operated.

10. All required permissions and permits will be obtained from territorial, state, county or city 

jurisdictions, including local law enforcement, fire, or other appropriate governmental agencies.

11. Dynegy agrees that in the event of any mishap in the National Airspace System, the event will be 

reported to the FAA as soon as practicable once safety has been ensured.

12. If the sUAS loses communications or loses its GPS signal, it will have capability to enter “loitermode” and hover, reestablish satellite connection, and return to a pre- determined location within 

the property boundary and land in a safe zone.

13. Flights will not be performed in areas which require a transponder.

************

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

should it be determined that publication is needed:

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

C.F.R. §§ 61.113(a) & (b);91.7(a); 91.9 (b) (2);91.103(b);91.109; 91.119; 91.121; 91.151(a);91.203(a) and 

(b); 91.405 (a); 91.407 (a) (1); 91.409 (a) (2); 91.409 (a) (2) and 91.417 (a) & (b) to operate commercially 

a small unmanned vehicle (55lbs or less) in construction operations.

Approval of exemptions allowing commercial operations of sUAS in the power utility industry enhances 

safety while reducing risk. A sUAS weighing fewer than 10 lbs. and powered by batteries eliminates 

virtually all risk inherent to elevated visual inspections on facilities and structural components of a power 

plant. 

The operation of sUAS, weighing less than 10 lbs., conducted in the strict conditions outlined above, will 

provide an equivalent level of safety supporting the grant of the exemptions requested herein, including 
5

exempting the applicant from the requirements of Part 21 and allowing commercial operations. These 

lightweight aircraft operate at slow speeds, close to the ground, and in a sterile environment and, as a 

result, are far safer than conventional operations conducted with turbine helicopters operating in close 

proximity to the ground and people.

Privacy

All flights will occur over private or controlled access property with the property owner’s prior consent and 

knowledge. Images taken will be of individuals who have also consented to being filmed or otherwise 

have agreed to be in the area where aerial photography will take place.

**************

Satisfaction of the criteria provided in Section 333 of the Reform Act of 20l2 - size, weight, speed, 

operating capabilities, proximity to airports and populated areas and operation within visual line of sight 

and national security - provide more than adequate justification for the grant of the requested exemptions 

allowing commercial operation of applicant’s sUAS in electric power plant use for inspections, 

photographic imagery, and surveying Dynegy owned property and structures.

DJI Inspire One Owner’s Manual with pre-flight checklist 

http://download.dji-innovations.com/downloads/inspire_1/en/Inspire_1_User_Manual_v1.2_en.pdf

DJI Inspire One Maintenance Manual 

http://download.dji-innovations.com/downloads/inspire_1/en/Inspire_1_Maintenance_ManualV1.0_en.pdf

DJI’s Website resource to locate NO FLY ZONEs near your current location:

http://www.dji.com/fly-safe/category-mc
6

APPENDIX A: DESCRIPTION OF SPECIFIC REGULATIONS

14 CFR Part 21 subpart H: Airworthiness Certificates

Section 91.203 requires all civil aircraft to have a certificate of airworthiness. Part 21, Subpart H,

entitled Airworthiness Certificates, establishes the procedural requirements for the issuance of 

airworthiness certificates as required by FAR § 91.203(a). Given the size of the sUAS, its light weight, and 

the limited operating area associated with its utilization, it is unnecessary to go through the certificate of 

airworthiness process under Part 21 Subpart H in order to achieve or exceed current safety levels.

Such an exemption meets the requirements of an equivalent level of safety under Part 11 and

Section 333 of the Reform Act. The Federal Aviation Act and Section 333 of the Reform Act both

authorize the FAA to exempt aircraft from the requirement for an airworthiness certificate, upon

consideration of the size, weight, speed, operational capability, and proximity to airports and populated 

areas of the sUAS involved. An analysis of these different criteria demonstrates that the sUAS operated 

without an airworthiness certificate, under the conditions proposed in that exemption, will be at least as 

safe, or safer, than a conventional aircraft with an airworthiness certificate.

14 CFR 45.23 (b): Display of marks; general

When marks include only the Roman capital letter "N" and the registration number is displayed on 

limited, restricted or light-sport category aircraft or experimental or provisionally certificated aircraft, the 

operator must also display on that aircraft near each entrance to the cabin, cockpit, or pilot station, in 

letters not less than 2 inches nor more than 6 inches high, the words "limited," "restricted," "light-sport," 

"experimental," or "provisional," as applicable. Even though the UAS will have no airworthiness certificate, 

an exemption may be needed as the UAS will have no entrance to the cabin, cockpit or pilot station on 

which the word “Experimental” can be placed. Given the size of the sUAV, two-inch lettering will be

impossible.

Dynegy is seeking relief from the requirement of marking the sUAS given the small fuselage 

siding does not offer enough space to mark “Experimental” and have it legible from ground view. The 

equivalent level of safety will be provided by having the sUAV controlled within the Dynegy property 

boundary only with the pilot/controller available and within Line of Sight at all times. The FAA has issued 

the following exemptions to this regulation to Exemptions Nos. 10700, 8738, 10167 and 10167A.

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

Pilot in command Sections 61.113 (a) & (b) limit private pilots to non-commercial operations. 

Because the sUAS will not carry a pilot or passengers, the proposed operations can achieve the 

equivalent level of safety of current operations by requiring the Pilot operating the aircraft to have 

completed a sUAS flight training course of 100 hours before flying a sUAS. Unlike a conventional aircraft 

that carries the pilot and passengers, the sUAS is remotely controlled with no living thing or cargo on 

board. Dynegy’s sUAS has back-up autopilot systems with a return-to-base option which greatly reduces 

the danger of human error. The area of operation will be controlled and restricted to hard hat areas. All 

flights will be planned and coordinated in advance. The sUAS to be operated hereunder is less than 10 

lbs. fully loaded, carries neither a pilot nor passenger, carries no explosive materials or flammable liquid 

fuels, and operates exclusively within controlled areas. Like other civil aircraft, operations under this 

exemption will be tightly controlled and monitored by the operator and in compliance with local public 

safety requirements. 

The risks associated with the operation of the sUAS are therefore diminished from the level of risk 

associated with commercial operations contemplated by Part 61 when drafted, and allowing operations of 

the sUAS as requested with a Pilot who has met the level of safety contemplated by 14 C.F.R. §61.113

(a) & (b).
7

14 CFR 91.7 (a): Civil aircraft airworthiness

The regulation requires that no person may operate a civil aircraft unless it is in airworthy

condition. As there will be no airworthiness certificate issued for the aircraft, should this exemption be 

granted, no FAA regulatory standard will exist for determining airworthiness. Given the size of the aircraft 

and the requirements contained in the DJI Owner’s Manual for maintenance and use of safety check lists 

prior to each flight, an equivalent level of safety will be provided.

14 CFR 91.9 (b) (2): Civil aircraft flight manual, marking, and placard requirements

This regulation provides that no person may operate an aircraft unless a current, approved flight

manual is in the aircraft. Dynegy proposes to provide an equivalent level of safety by maintaining a copy 

of all documents used by the operator to ensure the safe operation and flight of the UAS as well as 

documentation of an exemption and COA with the ground control station and accessible to the PIC during 

flight operations.

14 C.F.R. 91.103: Preflight Action

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

safety of flight. An exemption is needed from this requirement as the Pilot will take separate preflight 

actions, including checking for weather conditions, checking flight battery requirements, checking takeoff 

and landing distances, and all other actions in a sUAV Preflight Checklist. These actions will provide an 

equivalent level of safety.

14 C.F. R. 91.109: Flight instruction

The regulation provides that "No person may operate a civil aircraft that is being used for flight

instruction unless that aircraft has fully functioning dual controls."

The equivalent level of safety will be achieved through Dynegy’s sUAS flight training program and

conducting flight training within controlled environments.

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

Section 91.119 establishes safe altitudes for operation of civil aircraft. Section 91.119 ((1) allows 

helicopters to be operated at less than the minimums prescribed, provided the person operating the 

helicopter complies with any route or altitudes prescribed for helicopters by the FAA. This exemption is for 

a multirotor craft that flies similarly to a helicopter, with vertical take off and vertical landing, which will 

typically operate at altitudes of 200’ AGL, so an exemption may be needed to allow such operations. The 

sUAS will never operate at altitude higher than 400’ AGL unless explicit approval from the FAA and local 

ATC has been granted and only then for exhaust and plant inspections within the Dynegy power plant 

boundaries. Flights will be in a restricted area with security perimeter, where buildings and people will not 

be exposed to operations without their pre—obtained consent. 

The equivalent level of safety will be achieved given the size, weight, speed of the sUAS as well

as the location where it is operated. No flight will be taken without the permission of the property owner or 

local officials. Because of the advance notice to the property owner and any onsite personnel, all affected 

individuals will be aware of the planned flight operations. Unlike flight operations with aircraft or rotorcraft 

weighing far more than the maximum 10 lbs. proposed herein, our sUAS will not carry flammable fuel. In 

addition, the low—altitude operations of the sUAS will ensure separation between SUAS operations and 

the operations of conventional aircraft that must comply with Section 91.119.

14 C.F.R. 91.121: Altimeter Settings

This regulation requires each person operating an aircraft to maintain cruising altitude by 

reference to an altimeter that is set “...to the elevation of the departure airport or an appropriate altimeter 

setting available before departure.” As the sUAS may not have a barometric altimeter, but instead a GPS
8

altitude read out, an exemption may be needed. An equivalent level of safety will be achieved by the 

operator and Safety Check list, confirming the altitude of the launch site shown on the GPS altitude 

indicator before flight.

14 CFR 91.151 (a): Fuel requirements for flight in VFR conditions

Section 91.151 (a) outlines fuel requirements for beginning a flight in VFR conditions. Dynegy’s

sUAS is limited to operations in controlled environments, and has a limited range and flight time which 

require an exemption from 14 CFR 91.151(a). The battery powering the SUAS provides approximately 20 

minutes of powered flight. To meet the 30 minute reserve requirement in 14 CFR §91.151, sUAS flights 

would not be feasible to even lift-off. Given the immediate proximity of flight to landing zone, Dynegy 

requests an exemption to establish a 20% battery remaining or 5 minutes of flight time remaining for 

minimum fuel restrictions. 

Dynegy believes that an exemption from 14 CFR §91.151(a) falls within the scope of prior 

exemptions. Operating the small sUAS, in a tightly controlled area where only people and property 

owners or official representatives who have signed waivers will be allowed, with less than 30 minutes of 

reserve fuel, does not endanger the type of risks that Section 91 .151(a) was intended to alleviate given 

the size and speed of the small UAS. 

An equivalent level of safety can be achieved by limiting flights to 20 minutes, or enough battery 

reserve to ensure that the sUAS lands at the ground station with at least 20% of battery power (as 

determined by the onboard monitoring system and the Pilot), whichever happens first. This restriction 

would be more than adequate to return the sUAS to its planned landing zone from anywhere in its limited 

operating area.

14 CFR 91.203 (a) & (b): Carrying civil aircraft certification and registration

This regulation provides as follows:

• No person may operate a civil aircraft unless it has an appropriate and current airworthiness 

certificate.

• No person may operate a civil aircraft unless the airworthiness certificate required by paragraph 

(a) of this section or a special flight authorization issued under §91.715 is displayed at the cabin or 

cockpit entrance so that it is legible to passengers or crew.

To obtain an equivalent level of safety and meet the intent of 91.203, Dynegy proposes to 

maintain a copy of all documents used by the operator to ensure the safe operation and flight of the sUAS

as well as documentation of an exemption and COA with the ground control station and these will be

available to the Administrator or any law enforcement official upon request.

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

These regulations require that an aircraft operator or owner “shall have that aircraft inspected as 

prescribed in subpart E of this part and shall between required inspections, except as provided in 

paragraph (c) of this section, have discrepancies repaired as prescribed in part 43 of this chapter...,” and 

others shall inspect or maintain the aircraft in compliance with Part 43.

Given that these sections and Part 43 apply only to aircraft with an airworthiness certificate, these 

sections will not apply to Dynegy. Maintenance will be accomplished by the operator pursuant to the 

manufacturer’s flight manual and operating handbook. An equivalent level of safety will be achieved 

because these small sUAS are very limited in size, will carry a small payload and operate only in 

restricted areas for limited periods of time. If mechanical issues arise, the sUAS can land immediately 

within the boundaries of a Dynegy owned property. The Pilot will ensure that the sUAS is in working order 

prior to initiating flight, perform required maintenance, and keep a log of any maintenance performed. 

Moreover, the Pilot is the person most familiar with the aircraft and best suited to maintain the aircraft in 

an airworthy condition to provide the equivalent level of safety.
Map # Plant Name Nearest Town Stack Ht Airspace Min Max Airport Radio Freq Mode C

1 Baldwin Energy Complex Baldwin, IL 350' AGL Class G SFC 1200' AGL SAR CTAF 123.075

10 Casco Bay Veazie, ME <400' AGL Class C SFC 4200' MSL BGR CT 120.700 X

1, 2, 4 Coffeen Coffeen, IL 600' AGL Class G SFC 1200' AGL VLA CTAF 122.800

9 Conesville Station Conesville, OH 800' AGL Class G SFC 1200' AGL I40 CTAF 123.000

Class G SFC 700' AGL CVG CT 118.300

Class E 700' AGL FLT LVL MWO CTAF 123.000

12, 19 Dighton Power Dighton, MA <400' AGL Class G SFC 1200' AGL TAN CTAF 122.700

Class G SFC 700' AGL PIA CT 124.000

Class E 700' AGL FLT LVL CTK CTAF 122.800

MOA 9000' MSL FLT LVL Kansas City CNTR 127.270

5, 6 Edwards Peoria, IL 500' AGL Class C SFC 4700' MSL PIA CT 124.000 X

Class G SFC 700' AGL JOT CTAF 122.700

Class E 700' AGL FLT LVL ORD CT 120.750

Class G SFC 700' AGL WAY CTAF 122.800

Class E 700' AGL FLT LVL MGW CT 125.100

Class G SFC 700' AGL DWU CTAF 122.800

Class E 700' AGL FLT LVL Huntington TRSA 128.400

5 Havana Havana, IL 500' AGL Class G SFC 1200' AGL 9I0 CTAF 122.900

6, 17 Hennepin Hennepin, IL 275' AGL Class G SFC 1200' AGL VYS CTAF 123.000

16 Independence Oswego, NY <400' AGL Class G SFC 1200' AGL FZY CTAF 123.000

3 Joppa Metropolis, IL 550' AGL Class G SFC 1200' AGL M30 CTAF 122.800

Class G SFC 700' AGL JOT CTAF 122.700

Class E 700' AGL FLT LVL ORD CT 120.750

8, 15 Killen Wrightsville, OH 900' AGL Class G SFC 1200' AGL AMT CTAF 122.800

4 Kincaid Generation Kincaid, IL 650' AGL Class G SFC 1200' AGL TAZ CTAF 122.800

Class G SFC 700' AGL

Class E 700' AGL FLT LVL

Class G SFC 700' AGL

Class E 700' AGL FLT LVL

18, 18a Liberty Electric Power Philadelphia, PA 256' AGL Class B SFC 7000' MSL PHL CT 118.200 X

Class D SFC 2700' MSL CT 134.850

Class E 2700' MSL FLT LVL CTAF 122.950

Class G SFC 700' AGL CT 118.300

Class E 700' AGL 2100' MSL CTAF 122.950

Class B 2100' MSL FLT LVL I67 CTAF 123.000

Class D SFC 2500' MSL CT 133.600

Class E 2500' MSL FLT LVL CTAF 123.000

CT 124.000

CTAF 122.950

Class G SFC 700' AGL WVI CTAF 122.800

Class E 700' AGL FLT LVL MRY CT 118.400

2 Newton Effingham, IL 530' AGL Class G SFC 1200' AGL 1H2 CTAF 122.800

Class G SFC 700' AGL SFO CTAF 122.950

Class E 700' AGL 1500' MSL Norcal APP 125.350

Class C 1500' MSL 3000' MSL OAK CT 118.300

Class B 3000'MSL FLT LVL SFO CT 120.500

24 Ontelaunee Reading, PA 400' AGL Class D SFC 2800' MSL RDG CT 119.900

Class G SFC 700' AGL DFI CTAF 122.700

Class E 700' AGL FLT LVL 0G6 CTAF 122.800

Class G SFC 700' AGL 0G6 CTAF 122.800

Class E 700' AGL FLT LVL DFI CTAF 122.700

8, 15 Stuart Washington, OH 800' AGL Class G SFC 1200' AGL FGX CTAF 123.000

26 Washington Energy Beverly, OH <400' AGL Class G SFC 1200' AGL I71 CTAF 122.800

Class D SFC 3000' MSL ALN CT 126.000

Class E 3000' MSL 5000' MSL STL CTAF 122.950

Class B 5000' MSL 8000' MSL STL CT 118.500

I69 CTAF 122.975

K62 CTAF 122.700

CVG CT 118.300

7, 8 Zimmer Moscow, OH

Dynegy Power Plant Airspace Information

20 JUNE 2015

500' AGL Class G SFC 1200' AGL X

1 Wood River Alton, IL 350' AGL X

Defiance, OH <400' AGL

25 Stryker Facility Stryker, OH <400'AGL

12, 19

7

21

25 Richland Facility

13, 17

14

5

11

13, 17

15

23, 23a

22

20

19

17

Moss Landing Monterey Bay, CA 500' AGL

Oakland Power Station Oakland, CA 300' AGL X

X

Dicks Creek Combustion 

Turbine Site

Middletown, OH <400' AGL

Duck Creek Canton, IL 600' AGL

Elwood Energy Joliet, IL <400' AGL

Fayette Energy Facility Masontown, PA <400' AGL

Ironton, OH <400' AGL Hanging Rock Energy 

Facility

Kendall Joliet, IL <400' AGL

Lake Road Generating Dayville, CT <400' AGL LZD CTAF 123.000

Lee Energy Facility

Masspower Springfield, MA <400' AGL CEF

Dixon, IL <400' AGL C73 CTAF 123.050

X

CVG

Miami Fort Cincinnati, OH 400' AGL

Milford Power Milford, CT <400' AGL BDR

Morro Bay San Luis Obispo, CA 450' AGL Class G SFC 1200' AGL SBP
 

U.S. Department

of Transportation

Federal Aviation

Administration

Flight Standards Service

Airmen Certification Branch, AFS-760

P.O. Box 25082

Oklahoma City, Oklahoma 73125-0082

WEB Address: http://registry.faa.gov

Sincerely,

5RELQ07KXUPDQ

Manager, Airmen Certification Branch

 

JUNE 17, 2015

MATTHEW C RAINS

5 HILLWOOD DR

CASEYVILLE IL 62232-1936

OUR RECORDS SHOW YOU HOLD COMMERCIAL PILOT CERTIFICATE 002796384 WITH RATINGS

ROTORCRAFT-HELICOPTER, INSTRUMENT HELICOPTER, PRIVATE PRIVILEGES AIRPLANE

SINGLE ENGINE LAND, ENGLISH PROFICIENT, ISSUED 06/17/2015.

IF YOU REQUIRE FURTHER ASSISTANCE, PLEASE CONTACT THE AIRMEN CERTIFICATION

BRANCH TOLL FREE AT 1-866-878-2498 7:30AM - 3:30PM CST MONDAY THROUGH FRIDAY.