UNITED STATES OF AMERICA 

DEPARTMENT OF TRANSPORTATION 

FEDERAL AVIATION ADMINISTRATION 

RENTON, WASHINGTON 98057-3356 

In the matter of the petition of 

Exemption No. 11322 

Associated Air Center Regulatory Docket No. FAA-2014-1066 

for an exemption from§§ 25.785(h)(2), 

25.7850), 25.813(e), 25.815, and 

25.853(d) of Title 14, Code of Federal 

Regulations 

PARTIAL GRANT OF EXEMPTION 

By letter dated December 17, 2014, Mr. Jose Mora-Vargas, Certification Director, Associated 

Air Center, 8321 Lemmon Avenue, Dallas, Texas, 75209, petitioned the Federal Aviation 

Administration (FAA) for an exemption from the requirements of§§ 25.785(h)(2), 25.7850), 

25.813(e), 25.815, and 25.853(d) ofTitle 14, Code ofFederal Regulations (14 CFR). The 

proposed exemption, if granted, would permit relief from the requirements of flight attendant 

direct view, firm handholds in the passenger compartment, interior doors between passenger 

compartments, in-flight aisle width, and maximum heat release and smoke emissions 

flammability requirements for large interior panels. Although the petitioner did not specifically 

request relief from Special Conditions: Boeing Model 787 Series Airplanes; Seats With NonTraditional, Large, Non-Metallic Panels (25-370-SC), the interior arrangement for the project 

indicates these special conditions would apply. Therefore, these special conditions will be 

included in this partial grant. The proposed exemption is specifically for the installation of an 

executive interior on Boeing Model 787-8 airplane, serial number 40695, designated as "private 

use, not for hire, not for common carriage." 

The petitioner requests relief from the following regulations: 

Section 25.785(h)(2), Amendment 25-88, requires, in pertinent part, that flight attendant 

seats must be located to provide direct view of the cabin area. 

Section 25. 785U), Amendment 25-88, requires, in pertinent part, that there must be a 

firm handhold along each aisle. 
Section 25.813(e), Amendment 25-128, requires that no door may be installed in any 

partition between passenger compartments. 

Section 25.815, Amendment 25-38, requires minimum aisle widths in the passenger 

compartment. 

Section 25.853(d), Amendment 25-116, limits maximum heat-release rates and smoke 

emissions for large-panel cabin interior materials. 

Special Conditions 25-370-SC, "Boeing Model 787 Series Airplanes; Seats with NonTraditional, Large, Non-Metallic Panels," which specifies heat-release and smokeemission requirements for certain passenger-seating materials. 

The petitioner supports its request with the following information: 

This section quotes the relevant information from the petitioner's request, with minor edits for 

clarity. The complete petition is available at the Department of Transportation's Federal Docket 

Management System, on the Internet at http://regulations.gov, in Docket No. FAA-2014-1066. 

Background 

Associated Air Center requests that the relief provided for the airplanes covered by 

previously granted exemptions, relative to the subject requirements, be expanded to 

include the Boeing 787-8, SIN 40695: 

1. Exemption No. 8460, Docket No. FAA-2004-18913, Grant ofExemption from 

§§ 25.785(d) and 25.813(e) for Boeing Model 747-400 airplane. 

2. Exemption No. 10809, Docket No. FAA-2013-0277, Partial Grant of Exemption 

from§§ 25.785(h), 25.785G), 25.813(e), 25.815, and 25.853(d) for Boeing 747-8 

airplane. 

3. Exemption No. 10686, Docket No. FAA-2012-0707, Partial Grant of Exemption 

from§§ 25.785(h)(2), 25.785(j), 25.791(a), 25.795, 25.813(e), 25.815, and 

25.853(d) for Boeing Model 747-8 airplane. 

4. Exemption No. 10879, Docket No. FAA-2013-0015, Grant ofExemption from 

§ 25.813(e) for Boeing Model 787-8 and -9 airplane. 

5. Exemption No. 10868, Docket No. FAA-2013-0101 , Grant of Exemption from 

§ 25.853(d) for Boeing Model 787-9 airplane. 

Discussion 

The Federal Aviation Regulations (F ARs) do not consider the situation of private use not 

for hire transport category airplanes, in the 14 CFR part 25 requirements. Those 

requirements are predicated on airline common carrier, commercial passenger operations 

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carrying fare paying passengers from the general public. Associated Air Center believes 

that the design of an airplane for private use, and the associated operation of the airplane 

in private use, should justify an exemption, based on the fact that 14 CFR part 25 

regulations do not currently cover or consider such a design and operation. 

The FAA's position of previous exemptions listed above for the Boeing Models 747-400, 

747-8, 787-8, and 787-9 not requiring flight attendant direct view, firm handhold along 

each aisle, interior doors permitted with provisions, reduced aisle width during noncritical flight phases, and reduced interior flammability requirements should also be 

granted to the Boeing Model 787-8, Serial Number 40695. These airplanes have the 

same or approximately the same cross section (wide body). These type airplanes can be 

considered the larger private use airplanes. Customers have purchased these large 

airplanes for the spacious and impressive atmosphere they desire. 

14 CFR 25.785(h)(2): Flight attendant direct view 

The requirement for flight attendant seats to be located to provide a direct view of the 

passenger cabin is not practical for compliance with executive type interior to be installed 

on the Boeing 787-8 airplane. The complexity of the interior arrangement, coupled with 

the need to retain proximity to emergency exits is impractical to demonstrate compliance. 

Reference Exemption No. 10809 and 10686 for compliance method to the requirements 

identified in these Exemptions. 

14 CFR 25.785G): Firm handholds along each aisle 

The requirement for a firm handhold along aisles cannot be met for certain areas in the 

passenger cabin due to wide open spaces between individual seat backs which typically 

provide an adequate handhold. This is prevalent in conference/dining rooms, lounges, 

offices, bedrooms and lavatories. With the cabin spaciousness, there is a readily 

identifiable "aisle" throughout. Any feature hanging down from the ceiling would 

diminish the appearance of the high quality interior and is not acceptable to the customer. 

Reference Exemption No. 8460, 10809, and 10686 for compliance method to the 

requirements identified in these exemptions. 

14 CFR 25.813(e): Prohibits installation of interior doors between passenger 

compartments and emergency exits 

Private areas or conference/meeting/dining rooms will often need to span the whole cabin 

or a portion of the cabin in order to be practical. For such arrangements, privacy can only 

be provided by means of doors, and therefore, an exemption is needed to allow full use of 

airplane capabilities without compromising safety for those onboard. Interior doors 

between passenger compartments and between the exits will be compliant with the 

requirements previously identified in Exemptions No. 8460, 10809, 10686 and 10879. 

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14 CFR 25.815: Prohibits aisle width reduction during all phases of flight 

Unlike typical commercial aircraft, private use airplanes (i.e., not for hire or common 

carriage) have seats that can be moved or rotated during flight operations. The seating 

can be reconfigured to accommodate meetings and other arrangements. Some of these 

arrangements can reduce the aisle widths below those specified in 14 CFR 25.815. 

Advisory Circular (AC) 25-17 A contains a "private use" provision which provided aisle 

width reduction acceptability only during en-route flight and only if clear instructions are 

provided requiring that the seats be positioned for taxi, takeoff and landing in an 

arrangement that meets the required aisle width. AAC proposes to be compliant with the 

criteria established in AC 25-17 A for private use aircraft. Reference Exemption 

No. 10809 and 10686 for the compliance method to the requirements identified in these 

exemptions. 

14 CFR 25.853(d): Limits maximum heat release rates for large panel cabin interior 

materials and large non-metallic seat panels 

Executive interiors often have specific needs for the use of exotic or extremely 

comfortable materials to be used in the cabin. These materials can not satisfy the 

flammability requirements of 14 CFR 25.853(d) requiring that cabin materials meet 

specific flammability standards for passenger capacities of 20 or more. AAC proposes to 

meet the requirements of previously granted exemptions that stated, "When materials are 

installed that do not comply with the requirements of appendix F, parts IV and V, it must 

be shown that the passengers and crewmembers can be evacuated in 45 seconds or less, 

under the conditions described in part 25, appendix J. This also includes the 

requirements of special conditions 25-370-SC, which addresses seats with nontraditional, large, non-metallic panels on the airplane." Reference Exemption No. 10809, 

1 0686, and 1 0868 for compliance criteria to the requirements identified in these 

exemptions. 

Basis for Exemption 

As stated in Exemptions No. 8460, 10809, 10686, 10879, and 10868, the FAA is aware 

that the precedent has been established for other private use wide body airplanes to be 

exempted from the subject requirements. 

Exemption Will Be in the American Public Interest 

Approval of this request for certain exemptions for the Boeing Model 787-8, when 

configured for executive application, and operated under FAR part 91 or part 125, is in 

the public interest of the people ofthe United States of America. 

1. Given the proliferation of executive configured transport category airplanes 

currently taking place, and anticipated in the near future, approval of these 

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exemptions will enable the United States manufacturers of transport category 

airplanes to effectively compete in this expanding market. 

2. Additional sales ofUnited States manufactured airplanes outside ofthe traditional 

airline market, and completion of many of them at United States owned and 

operated aircraft completion facilities, will serve to increase the profitability of 

these manufacturers and their supplying/supporting companies. 

3. Stability and improved financial performance ofthese United States companies 

gives greater job stability to the workers employed by the companies, causing a 

stabilizing influence to the United States economy, due to the consumer spending 

activities associated with stable workers. 

4. Improved financial performance ofUnited States owned and operated 

corporations and increased work force stability translates to continued and 

improved local, state, and federal tax revenues which in turn add to the stability of 

the total United States economy. 

5. Improved financial performance allows United States corporations to continue to 

invest in research and development allowing the United States to maintain or 

improve its competitive position in the world economy. 

6. A large number of these types of airplanes will probably be sold to "offshore" 

clients, improving the United States balance of trade. 

7. Since the passengers aboard these airplanes will not be revenue paying customers 

of the airlines, there can be no degradation to airline passenger safety, and 

therefore no detrimental impact on the public at large. 

In reference to the previously noted partial/granted exemptions, Associated Air Center 

seeks similar relief with the same provisions for the Boeing Model 787-8, SIN 40695 

airplane. Granted exemptions, as described above, were subject to the following 

prOVISIOnS: 

• The airplane must not be operated for hire or offered for common carriage. This 

provision does not preclude the operator from receiving remuneration to the 

extent consistent with 14 CFR parts 125 and 91 , subpa11 F, as applicable. 

• A majority of flight-attendant seats must be oriented to face the passenger cabin. 

• Each door between passenger compartments must be frangib le (only manually 

operated pocket doors are installed -no electrical doors). 

• Doors that fall into Category 1 must be in the open position during taxi, takeoff, 

and landing when the room is occupied. 

• Doors that fall into Categories 2, 3, or 4 must be in the open position during taxi, 

takeoff and landing, regardless of occupancy of the room. 

• Doors that fall into Category 5 must be in the closed position during taxi, takeoff, 

and landing (TT &L). 

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• Appropriate procedures must be established to both signal the flight crew in the 

event a door between passenger compartments is not in the proper position, and 

prohibit TT &L. Doors in Category 5 do not need to comply with this 

requirement. For Category 5 doors, installing placards located on or near the 

door, and indicating that the door must be closed for TT &L, is acceptable. 

• Doors between passenger compartments must have dual means to retain them in 

the open position. Each means must be capable of withstanding the inertia loads 

specified in§ 25.561. Doors in Category 5 do not need to comply with this 

requirement because they are required to be closed for TT &L. 

• When materials are installed that do not comply with the requirements of 14 CFR 

pmt 25, appendix F, parts IV and V, it must be shown that the passengers and 

crewmembers can be evacuated in 45 seconds or less, under the conditions 

described in part 25, appendix J. This also includes the requirements of Special 

Conditions 25-3 70-SC, which addresses seats with non-traditional, large, 

nonmetallic panels on the airplane. 

• A means to signal the flight crew must be in place in the event of a fire in an 

isolated passenger compartment, and the detection system must meet the 

requirements of§ 25.858(a) through (d). 

• Compliance is required with § 25.815, except that aisle width may be reduced to 

zero inches between any cabin furnishing (e.g., seat, table, or divider) during inflight operations only, provided that all areas of the cabin remain easily accessible 

in the event of an emergency (e.g., in-flight fire or decompression) with interior 

furnishings in the most adverse positions. Accessibility must be demonstrated to 

the FAA by test or analysis supp01ted by test data, or, in circumstances agreed to 

by the FAA, by inspection. 

• Aisle width requirements of§ 25.815 must be maintained during taxi, takeoff, and 

landing. 

• Any cabin furnishing (e.g., seat, table, or divider) that can be positioned to intrude 

into the aisle must be clearly placarded to be in the proper location (i.e., not 

intruding into the minimum required aisle) during taxi, takeoff and landing. 

Federal Register publication 

The FAA has determined that good cause exists for waiving the requirement for Federal Register 

publication for public comment because the request is identical in all material respects to 

previously granted exemptions; including, in pertinent part, those exemptions the petitioner lists 

in their petition; and the exemption, if granted, would not set a precedent. Any delay in acting on 

this petition would be detrimental to Associated Air Center. 

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The FAA's analysis 

The FAA considers that granting this petition is in the public interest for the reasons stated by the 

petitioner and because the FAA is directed to take into account the type of operation when 

establishing standards under Title 49 of the United States Code (49 U.S.C. 44701 (d)). 

As more transport-category airplanes have been configured (or reconfigured) for private use, the 

FAA has given considerable attention to the issue of appropriate regulation of such airplanes. 

Some of the current regulations governing design certification of transport-category airplanes are 

not compatible with private use of such airplanes. Because of this, we have received a number of 

petitions for exemption from certain regulations. We have granted such exemptions when we 

find that to do so is in the public interest and does not adversely affect the level of safety 

provided by the regulations. We published Special Requirements for Private Use Transport 

Category Airplanes, SF AR 109, which significantly reduces the need for case-by-case review of 

individual petitions for exemption for private-use airplanes within the limitation of SF AR 109. 

The Boeing 787-8 airplane under consideration has a passenger seating capacity greater than the 

60-passenger seating limitation in SF AR 1 09; therefore, the SF AR is not applicable to this 

airplane. 

Our analysis of this petition considered each ofthe following design features proposed by the 

petitioner. 

1. Direct View 

The petitioner has identified the requirement for flight attendant seats to be located to provide a 

direct view of the passenger cabin as not practical for compliance with the executive-type interior 

to be used on this Boeing 787-8 airplane. The complexity of the interior arrangement, coupled 

with the need to retain proximity to emergency exits, is cited as the primary reason that 

compliance is impractical. 

The FAA has considered the requirement for direct view in the context of private-use airplanes 

and agrees that much of the justification for the requirement is based on air-carrier-type 

operations. The practicality of locating flight attendant seats near emergency exits so that there is 

a direct view of occupants inside the rooms is questionable, at best. In this regard, we believe 

that some relief may be appropriate for airplanes intended for private use. However, we note that 

the justification for the requirement for direct view is not limited to observation of passengers 

that are not familiar with the interior. Flight attendant seats should be located so that a direct 

view is provided for the cabin area whenever practical. For example, flight attendant seats 

should not face away from the cabin. In those areas of the airplane where traditional seating 

arrangements are used, the FAA believes that a direct view should be provided. 

In considering the need for direct view, the FAA agrees that the restricted nature of the operation 

of a private-use airplane mitigates much of the need. That is, the operator has control of, and can 

restrict the population of, passengers, unlike an air carrier. The risk of passengers engaging in 

hazardous or malicious activity is essentially eliminated, and the need for direct view is limited 

7 
to those cases where a passenger might need assistance. We consider that this objective is met by 

requiring that a majority of flight attendant seats face the cabin. 

2. Firm Handholds 

We have considered the requirement for firm handholds in the context of private-use airplanes, 

and have determined that it would be impractical for this type of operation and interior 

configuration with meeting rooms, offices, bedrooms, lavatories, and lounges rather than 

traditional airline-type seating. However, in those areas ofthe airplane where traditional seating 

arrangements are used, the FAA believes that firm handholds should be provided. 

3. Interior Doors 

The placement of interior doors is clearly quite significant to the owner/operator of the airplane. 

The flexibility to partition the airplane into individual rooms, such as private meeting rooms or 

bedrooms, is paramount to an acceptable interior. The FAA acknowledges the desirability of 

these features from the operator's point of view. 

When the regulations pertaining to interior doors were adopted, they did not consider "rooms." 

They considered two possible types of interior doors in a passenger compartment. The first type 

is an interior door between passenger compartments. The second type is an interior door between 

an exit and the passenger compartment. 

Until recently, only the first type of door was prohibited by§ 25.813(e). However, part 25, as 

amended by Amendment 25-116, prohibits interior doors between the exit and the passenger 

compartment. In addition, Amendment 121-306 prohibits these doors in airplanes manufactured 

after November 27,2006, operated under 14 CFR part 121. Amendments 25-116 and 121-306, 

titled Miscellaneous Cabin Safety Changes, were published in the Federal Register on October 

27,2004. 

Airplanes configured for private-use, not-for-hire, and not-for-common-carriage typically use any 

of five different door categories in the passenger cabins: 

Category 1: A door in a room and the room is less than the full width of the airplane. 

An aisle is outside the room. This type of room may be occupied during takeoff and 

landing, and only the occupants of the room must use the door to reach an exit. 

Category 2: A door in a room that is the same as Category 1, except a single emergency 

exit or pair of emergency exits is within the room. 

Category 3: A door, or doors, in a compartment and the compartment is the full width of 

the airplane. Passengers are seated on both sides (fore and aft) of the door(s), and the 

main aisle leads out of, or passes through, the compartment. The compartment does not 

have emergency exits. This type of compartment may be occupied during takeoff and 

landing. 

8 
Category 4: A door in a room and the room is the full width of the airplane. Passengers 

are seated on both sides (fore and aft) of the door, and a pair of emergency exits is at one 

end of the room. This type of room may be occupied during takeoff and landing. 

Category 5: A door in a room that may be the full width of the airplane. This type of 

room is not occupied during takeoff and landing. This room is only occupied during 

flight. Passengers are not seated on both sides of the door during taxi, takeoff, and 

landing. Passengers seated in taxi, takeoff, and landing seats must not need to pass 

through this door to get to any emergency exits. 

Because not all interior doors between passenger compartments are equivalent, the FAA has 

determined that the following requirements will produce an adequate level of safety: 

a. To maximize the level of safety, doors in Category 2, 3, or 4, installed across the main 

cabin aisle, must open and close in a transverse direction. That is, the direction of motion 

of the door must be at a right angle to the longitudinal axis of the airplane. A "pocket 

door" is one example of such a design. This minimizes the chance that the inertia forces 

of an accident could force the door closed. 

b. Redundant means are necessary to latch doors open for takeoff and landing. Each 

latching device must have the capability of retaining the door in the takeoff and landing 

position under the inertia forces of§ 25.561. 

c. Each interior door must be frangible, in the event that it is jammed in the closed position 

in flight or during taxi, takeoff, or landing. Frangibility is intended to ensure that if a 

door is jammed closed, occupants can escape in either direction and emergency 

equipment can be moved. Frangibility may be demonstrated in either of the following 

ways: 

• A 51

h percentile female can break through the door, creating a large enough 

opening that a 95th percentile (or larger) male can pass through. See Advisory 

Circular 25-17A, Transport Airplane Cabin Interiors Crashworthiness Handbook, 

paragraph 43b(2). 

• A 5th percentile female can break a hinge on the door or a hinge on a smaller door 

within the door such that the door can swing, so as to allow a 95th percentile (or 

larger) male to pass through the opening with the door swung open. This 

evaluation must be made with any cabin furnishing or equipment installed that 

could limit the swing arc of the door and placed in the most adverse position. In 

using this approach, one must consider the possibility that the door is physically 

jammed in the closed position by distortion of the fuselage or furnishings. This 

possibility must be considered even if the door normally translates into the open 

and closed positions. 

d. Doors that fall into Category 1 must be in the open position during taxi, takeoff, and 

landing, only when the room is occupied. 

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e. Doors that fall into Categories 2, 3, or 4 must be in the open position during taxi, takeoff, 

and landing, regardless of occupancy. 

f. Doors that fall into Category 5 must be in the closed position during taxi, takeoff, and 

landing. 

With respect to the possibility that a door remains closed when it should not be, we have 

determined that a higher level of awareness is required to address this issue. Due to the relative 

complexity of the cabin interior, we have determined that inspection by flight attendants prior to 

takeoff and landing is not sufficient to verify that interior doors are in a required open position. 

Therefore, some type of remote indication is necessary. The petitioner's proposal to provide 

remote indication to the flightcrew that these doors are in the open position during taxi, takeoff, 

and landing is considered adequate for doors that fall into Categories 1, 2, 3, and 4. Doors in 

Category 5 do not need to comply with this requirement. For Category 5 doors, placards located 

on or near the door that indicate that the door must be closed for taxi, takeoff, and landing are 

acceptable. 

4. In-flight Aisle Width 

The FAA has considered the requirement for in-flight width of the aisle in the context of privateuse airplanes and installed cabin furnishings (e.g., seat, table, or divider) that are movable during 

in-flight operations and would reduce the width of the aisle. This issue is clearly quite significant 

to the owner/operator of the airplane. Policy Statement No. PS-ANM-25.815-01, Compliance 

with the Aisle Width Requirements of§ 25.815, dated December 17,2012, addresses this issue. 

However, that policy is limited to airplanes with 19 or fewer passenger seats. The airplane that is 

the subject of this exemption has more than 19 passenger seats. The petitioner has stated that the 

airplane is intended for private-use only, not-for-hire, and not-for-common-carriage service. We 

have determined that because the airplane is limited to this type of operation, some in-flight 

width-of-aisle relief would be acceptable, similar to what is described in the above-mentioned 

policy statement. 

5. Interior Materials 

With respect to the flammability of interior materials, the petitioner has accurately summarized 

the purpose of the requirements. The petitioner correctly notes that the requirements are related 

to prolonging the time available for evacuation from the airplane. This also includes the 

requirements of Special Conditions 25-370-SC, which addresses seats with non-traditional, large, 

non-metallic panels on the airplane. The panels on the subject airplane seats would need to meet 

the maximum heat-release and smoke-emissions flammability requirements for large interior 

panels. 

When the standards for heat release and smoke emissions of interior materials were developed, 

the FAA incorporated a discriminant based on passenger capacity. This approach was intended 

to address smaller airplanes where the ratio of exits to passengers is typically quite good and the 

evacuation times are expected to be quite low. Under these conditions, the benefits of improved 

materials were expected to be negligible. The airplane type discussed in the petition was not 

10 
envisioned by the rulemaking, insofar as the large size with low passenger count is concerned. 

We have considered the issue of the evacuation capability of the airplane relative to the 

flammability of the materials and find that some relief may be possible. However, the issue of 

flammability is not limited to post-crash scenarios; the in-flight fire threat must also be 

addressed. We note that the petitioner has not proposed an alternative to the heat-release and 

smoke-emission standards, but rather an exemption from the requirement to assess the heat 

release and smoke emissions of certain materials. 

Because the main benefit of improved interior materials is to lengthen the time available for 

evacuation, an arrangement that effectively provides the same evacuation capability would satisfy 

many of the concerns addressed by the requirement, albeit indirectly. The FAA has reviewed the 

full-scale, fire-test data used in developing the heat-release and smoke-emissions requirements, 

and also considered accident data relevant to this issue. This review is not complete, but it does 

suggest that a quantifiable improvement in evacuation capability could warrant a relaxation of 

the heat-release and smoke-emissions requirements. 

The petitioner has proposed that an evacuation analysis be performed to show that all occupants, 

including crew, can be safely evacuated in less than 45 seconds. The FAA has determined that a 

45-second evacuation time would provide an acceptable level of safety over that allowed by the 

regulation and would allow a relaxation of the heat-release and smoke-emissions requirements. 

Precedents have been set for this decision and apply to other private-use airplanes. This also 

includes the requirements of Special Conditions 25-370-SC, which addresses seats with nontraditional, large, non-metallic panels on the airplane. The panels on the subject airplane seats 

would not need to meet the maximum heat-release and smoke-emissions flammability 

requirements for large interior panels as part of this exemption. 

The in-flight fire scenario also needs to be addressed. The major issue with respect to in-flight 

fires is timely recognition. On some airplanes, the interior includes isolated areas that do not 

lend themselves to timely detection of a fire. For purposes of this exemption, an isolated 

passenger compartment is defined as a room that does not contain an egress path (e.g., main 

cabin aisle, cross aisle, or passageway), or is isolated by a door. To address the in-flight case, the 

FAA believes that installing a smoke detector in such areas would compensate for the potential 

for an increased in-flight fire threat. Therefore, each isolated passenger compartment must 

incorporate a fire-detection system that meets the requirements of§ 25.858. While this section is 

written for cargo-compartment fire-detection systems, the criteria contained therein are 

considered appropriate to this application. 

The FAA's decision 

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

Therefore, pursuant to the authority contained in 49 U.S.C. §§ 40113 and 44701 delegated to me 

by the Administrator, I grant Associated Air Center an exemption from§§ 25.785(h)(2), 

25.7850), 25.813(e), 25.815, 25.853(d), and Special Conditions 25-370-SC. The exemption is 

granted to the extent necessary to allow Associated Air Center to install an executive interior on 

a private, not-for-hire, not-for-common-carriage, Boeing Model 787-8 airplane, serial no. 40695. 

Specifically, the exemption allows relief from the requirements for: 

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• Flight attendant direct view in the passenger compartment in areas such as meeting 

rooms, offices, bedrooms, lavatories, lounges, etc.; except that, in areas of the airplane 

where traditional seating arrangements are used, direct view should be provided. 

• Firm handholds in the passenger compartment in areas such as meeting rooms, offices, 

bedrooms, lavatories, lounges, etc.; except that firm handholds are required in hallways 

and areas of the airplane where traditional airline seating is installed. 

• Interior doors between passenger compartments. 

• In-flight minimum aisle width. 

• Maximum heat-release and smoke-emissions flammability requirements for large interior 

panels. This also includes the requirements of Special Conditions 25-370-SC, which 

addresses seats with non-traditional, large, non-metallic panels on the airplane. 

The following conditions apply, and limitations numbers 1, 4, 5, 6, and 12 must be documented 

in the limitations section of the airplane flight manual: 

1. The airplane must not be operated for hire or offered for common carriage. This 

provision does not preclude the operator from receiving remuneration to the extent 

consistent with 14 CFR parts 125 and 91, subpart F, as applicable. 

2. A majority of flight attendant seats must be oriented to face the passenger cabin. 

3. Each door between passenger compartments must be frangible. 

4. Doors that fall into Category 1 must be in the open position during taxi, takeoff, and 

landing when the room is occupied. 

5. Doors that fall into Categories 2, 3, or 4 must be in the open position during taxi, takeoff, 

and landing, regardless of occupancy of the room. 

6. Doors that fall into Category 5 must be in the closed position during taxi, takeoff, and 

landing. 

7. Appropriate procedures must be established to both signal the flightcrew in the event a 

door between passenger compartments is not in the proper position, and prohibit taxi, 

takeoff, and landing. Doors in Category 5 do not need to comply with this requirement. 

For Category 5 doors, placards located on or near the door that indicate the door must be 

closed for taxi, takeoff, and landing, is acceptable. 

12 
8. Doors between passenger compartments must have dual means to retain them in the open 

position. Each means must be capable of withstanding the inertia loads specified in 

§ 25.561. Doors in Category 5 do not need to comply with this requirement because they 

are required to be closed for taxi, takeoff, and landing. 

9. When materials are installed that do not comply with the requirements of appendix F, 

parts IV and V, it must be shown that the passengers and crewmembers can be evacuated 

in 45 seconds or less, under the conditions described in part 25, appendix J. This also 

includes the requirements of Special Conditions 25-370-SC, which addresses seats with 

non-traditional, large, non-metallic panels on the airplane. The panels on the subject 

airplane seats are not required to meet the maximum heat-release and smoke-emissions 

flammability requirements for large interior panels. 

10. A means to signal the flightcrew must be in place in the event of a fire in an isolated 

passenger compartment, and the detection system must meet the requirements of 

§ 25.858(a) through (d). 

11. Compliance is required with§ 25.815, except that aisle width may be reduced to zero 

inches between any cabin furnishing (e.g., seat, table, or divider) during in-flight 

operations only, provided that all areas of the cabin remain easily accessible in the event 

of an emergency (e.g., in-flight fire or decompression) with interior furnishings in the 

most adverse positions. Accessibility must be demonstrated to the FAA by test, analysis 

supported by test data, or, in circumstances agreed to by the FAA, by inspection. 

12. Aisle-width requirements of§ 25.815 must be maintained during taxi, takeoff, and 

landing. 

13. Any cabin furnishing (e.g., seat, table, or divider) that can be positioned to intrude into 

the aisle must be clearly placarded to be in the proper location (i.e., not intruding into the 

minimum required aisle width) during taxi, takeoff, and landing. The effectiveness and 

meaning of the placard must be demonstrated to be easily viewed and understood by 

nai"ve test subjects. 

Issued in Renton, Washington, on APR 14 2015 

~~ Michael Kaszycki 

Acting Manager, Transport Airplane Directorate 

Aircraft Certification Service 

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