83 FR 53166 - Special Conditions: Mitsubishi Aircraft Corporation Model MRJ-200 Airplane; Passenger Seats With Non-Traditional, Large, Non-Metallic Panels
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 83, Issue 204 (October 22, 2018)
Federal Aviation Administration
Federal Register Volume 83, Issue 204 (October 22, 2018)
| Page Range | 53166-53168 | |
| FR Document | 2018-22922 |
[Federal Register Volume 83, Number 204 (Monday, October 22, 2018)] [Rules and Regulations] [Pages 53166-53168] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2018-22922] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 25 [Docket No. FAA-2018-0932; Special Conditions No. 25-733-SC] Special Conditions: Mitsubishi Aircraft Corporation Model MRJ-200 Airplane; Passenger Seats With Non-Traditional, Large, Non-Metallic Panels AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final special conditions; request for comments. ----------------------------------------------------------------------- SUMMARY: These special conditions are issued for the Mitsubishi Aircraft Corporation Model MRJ-200 airplane. This airplane will have novel or unusual design features when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. These design features include passenger seats that incorporate non-traditional, large, non-metallic panels in lieu of the traditional metal frame covered by fabric. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards. DATES: This action is effective on Mitsubishi Aircraft Corporation on October 22, 2018. Send comments on or before December 6, 2018. ADDRESSES: Send comments identified by Docket No. FAA-2018-0932 using any of the following methods:Federal eRegulations Portal: Go to http://www.regulations.gov/ and follow the online instructions for sending your comments electronically. Mail: Send comments to Docket Operations, M-30, U.S. Department of Transportation (DOT), 1200 New Jersey Avenue SE, Room W12-140, West Building Ground Floor, Washington, DC 20590-0001. Hand Delivery or Courier: Take comments to Docket Operations in Room W12-140 of the West Building Ground Floor at 1200 New Jersey Avenue SE, Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. Fax: Fax comments to Docket Operations at 202-493-2251. Privacy: The FAA will post all comments it receives, without change, to http://www.regulations.gov/, including any personal information the commenter provides. Using the search function of the docket website, anyone can find and read the electronic form of all comments received into any FAA docket, including the name of the individual sending the comment (or signing the comment for an association, business, labor union, etc.). DOT's complete Privacy Act Statement can be found in the Federal Register published on April 11, 2000 (65 FR 19477-19478). Docket: Background documents or comments received may be read at http://www.regulations.gov/ at any time. Follow the online instructions for accessing the docket or go to Docket Operations in Room W12-140 of the West Building Ground Floor at 1200 New Jersey Avenue SE, Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. FOR FURTHER INFORMATION CONTACT: Nicholas Wilson, International Section, AIR-676, Transport Standards Branch, Policy and Innovation Division, Aircraft Certification Service, Federal Aviation Administration, 2200 South 216th Street, Des Moines, Washington 98198; telephone and fax 206-231-3230; email Nicholas.Wilson@faa.gov. SUPPLEMENTARY INFORMATION: The substance of these special conditions has been published in the Federal Register for public comment in several prior instances with no substantive comments received. The FAA, therefore, finds it unnecessary to delay the effective date and finds that good cause exists for making these special conditions effective upon publication in the Federal Register. Comments Invited We invite interested people to take part in this rulemaking by sending written comments, data, or views. The most helpful comments reference a specific portion of the special conditions, explain the reason for any recommended change, and include supporting data. We will consider all comments we receive by the closing date for comments. We may change these special conditions based on the comments we receive. [[Page 53167]] Background On August 19, 2009, Mitsubishi Aircraft Corporation applied for a type certificate for their new Model MRJ-200 airplane. The Mitsubishi Aircraft Corporation Model MRJ-200 airplane is a low-wing, conventional-tail design with two wing-mounted turbofan engines. The primary structure is metal with an aluminum wing and composite empennage. The airplane is equipped with an electronic flight control system. The airplane has seating for 96 passengers and a maximum takeoff weight of 98,800 lbs. Type Certification Basis Under the provisions of title 14, Code of Federal Regulations (14 CFR) 21.17, Mitsubishi Aircraft Corporation must show that the Model MRJ-200 airplane meets the applicable provisions of part 25, as amended by amendments 25-1 through 25-141; part 36, as amended by amendments 36-1 through 36-30; and part 34, as amended by amendments 34-1 through the amendment effective at the time of design approval. If the Administrator finds that the applicable airworthiness regulations (i.e., 14 CFR part 25) do not contain adequate or appropriate safety standards for the Mitsubishi Aircraft Corporation Model MRJ-200 airplane because of a novel or unusual design feature, special conditions are prescribed under the provisions of Sec. 21.16. Special conditions are initially applicable to the model for which they are issued. Should the type certificate for that model be amended later to include any other model that incorporates the same novel or unusual design feature, these special conditions would also apply to the other model under Sec. 21.101. In addition to the applicable airworthiness regulations and special conditions, the Mitsubishi Aircraft Corporation Model MRJ-200 airplane must comply with the fuel vent and exhaust emission requirements of 14 CFR part 34 and the noise certification requirements of 14 CFR part 36. The FAA issues special conditions, as defined in 14 CFR 11.19, in accordance with Sec. 11.38, and they become part of the type certification basis under Sec. 21.17(a)(2). Novel or Unusual Design Features The Mitsubishi Aircraft Corporation Model MRJ-200 airplane will incorporate the following novel or unusual design features: Passenger seats that incorporate non-traditional, large, non- metallic panels in lieu of the traditional metal frame covered by fabric. Definition of ``Non-Traditional, Large, Non-Metallic Panel'' A non-traditional, large, non-metallic panel, in this case, is defined as a panel with exposed surface areas greater than 1.5 square feet installed per seat place. The panel may consist of either a single component or multiple components in a concentrated area. Examples of parts of the seat where these non-traditional panels are installed include, but are not limited to: seat backs, bottoms and leg/foot rests, kick panels, back shells, credenzas and associated furniture. Examples of traditional exempted parts of the seat include: arm caps, armrest close-outs such as end bays and armrest-styled center consoles, food trays, video monitors and shrouds. Clarification of ``Exposed'' ``Exposed'' includes those panels directly exposed to the passenger cabin in the traditional sense, plus those panels enveloped such as by a dress cover. Traditional fabrics or leathers currently used on seats are excluded from these special conditions. These materials must still comply with 14 CFR 25.853(a) and (c) if used as a covering for a seat cushion, or 14 CFR 25.853(a) if installed elsewhere on the seat. Non- traditional, large, non-metallic panels covered with traditional fabrics or leathers will be tested without their coverings or covering attachments. Discussion In the early 1980s, the FAA conducted extensive research on the effects of post-crash flammability in the passenger cabin. As a result of this research and service experience, the FAA adopted new standards for interior surfaces associated with large surface area parts. Specifically, the rules require measurement of heat release and smoke emission (part 25, appendix F, parts IV and V) for the affected parts. Heat release has been shown to have a direct correlation with post- crash fire survival time. Materials that comply with the standards (i.e., Sec. 25.853, Compartment interiors, as amended by amendment 25- 61 and amendment 25-66) extend survival time by approximately two minutes over materials that do not comply. At the time these standards were written, the potential application of the requirements of heat release and smoke emission to seats was explored. The seat frame itself was not a concern because it was primarily made of aluminum and there were only small amounts of non- metallic materials. It was determined that the overall effect on survivability was negligible, whether or not the food trays met the heat release and smoke requirements. The requirements, therefore, did not address seats. The preambles to both the Notice of Proposed Rulemaking, Notice No. 85-10, 50 FR 15038, April 16, 1985, and the Final Rule, amendment 25-61, 51 FR 26206, July 21, 1986, specifically note that seats were excluded because the recently-adopted standards for flammability of seat cushions will greatly inhibit involvement of the seats. Subsequently, the Final Rule, amendment 25-83, 60 FR 6615, March 6, 1995, clarified the definition of minimum panel size by stating that it is not possible to cite a specific size that will apply in all installations; however, as a general rule, components with exposed surface areas of one square foot or less may be considered small enough that they do not have to meet the new standards. Components with exposed surface areas greater than two square feet may be considered large enough that they do have to meet the new standards. Those with exposed surface areas greater than one square foot, but less than two square feet, must be considered in conjunction with the areas of the cabin in which they are installed before a determination could be made. The FAA issued Policy Statement PS-ANM100-97-112-39, Guidance for Flammability Testing of Seat/Console Installations, on October 17, 1997 (http://rgl.faa.gov). That document was issued when it became clear that seat designs were evolving to include large, non-metallic panels with surface areas that would impact survivability during a cabin fire event, comparable to partitions or galleys. The document noted that large surface area panels must comply with heat release and smoke emission requirements, even if they were attached to a seat. If the FAA had not issued such policy, seat designs could have been viewed as a loophole to the airworthiness standards that would result in an unacceptable decrease in survivability during a cabin fire event. In October of 2004, an issue was raised regarding the appropriate flammability standards for passenger seats that incorporated non- traditional, large, non-metallic panels in lieu of the traditional metal covered by fabric. The FAA determined that special conditions would be promulgated to apply the standards defined in 14 CFR 25.853(d) to seats with large, non-metallic panels in their design. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to [[Page 53168]] that established by the existing airworthiness standards. Applicability As discussed above, these special conditions are applicable to the Mitsubishi Aircraft Corporation Model MRJ-200 airplane. Should Mitsubishi Aircraft Corporation apply at a later date for a change to the type certificate to include another model incorporating the same novel or unusual design feature, these special conditions would apply to that model as well. Conclusion This action affects only a certain novel or unusual design feature on one model of airplane. It is not a rule of general applicability. List of Subjects in 14 CFR Part 25 Aircraft, Aviation safety, Reporting and recordkeeping requirements. Authority Citation The authority citation for these special conditions is as follows: Authority: 49 U.S.C. 106(f), 106(g), 40113, 44701, 44702, 44704. The Special Conditions Accordingly, pursuant to the authority delegated to me by the Administrator, the following special conditions are issued as part of the type certification basis for Mitsubishi Aircraft Company Model MRJ- 200 airplanes. 1. Except as provided in paragraph 3 of these special conditions, compliance with 14 CFR part 25, appendix F, part IV, Heat Release and part V, Smoke Emission, is required for seats that incorporate non- traditional, large, non-metallic panels that may either be a single component or multiple components in a concentrated area in their design. 2. The applicant may designate up to and including 0.139 square meter (1.5 square feet of non-traditional, non-metallic panel material per seat place that does not have to comply with paragraph 1 of these special conditions. A double seat assembly may have a total of 0.278 square meter (3.0 square feet) excluded on any portion of the assembly (e.g., outboard seat place 0.093 square meter [1 square foot] and inboard 0.185 square meter [2.0 square feet]). 3. Seats do not have to meet the test requirements of 14 CFR part 25, appendix F, parts IV and V, when installed in compartments defined in 14 CFR 25.853(e). Issued in Des Moines, Washington, on October 16, 2018. Victor Wicklund, Manager, Transport Standards Branch, Policy and Innovation Division, Aircraft Certification Service. [FR Doc. 2018-22922 Filed 10-19-18; 8:45 am] BILLING CODE 4910-13-P
![53166 Federal Register / Vol. 83, No. 204 / Monday, October 22, 2018 / Rules and Regulations
between the pelvis and shoulders Issued in Des Moines, Washington, on Ground Floor at 1200 New Jersey
during impact, including rebound, is October 4, 2018. Avenue SE, Washington, DC, between 9
not acceptable. During this type of Victor Wicklund, a.m. and 5 p.m., Monday through
contact, the interval for any rearward (X Manager, Transport Standards Branch, Policy Friday, except Federal holidays.
direction) acceleration exceeding 20g and Innovation Division, Aircraft • Fax: Fax comments to Docket
Certification Service.
must be less than 3 milliseconds as Operations at 202–493–2251.
measured by the thoracic [FR Doc. 2018–22933 Filed 10–19–18; 8:45 am]
Privacy: The FAA will post all
instrumentation specified in 49 CFR BILLING CODE 4910–13–P
comments it receives, without change,
part 572, subpart E, filtered in to http://www.regulations.gov/,
accordance with SAE recommended including any personal information the
DEPARTMENT OF TRANSPORTATION
practice J211/1, ‘‘Instrumentation for commenter provides. Using the search
Impact Test–Part 1–Electronic Federal Aviation Administration function of the docket website, anyone
Instrumentation.’’ can find and read the electronic form of
c. The occupant must not interact 14 CFR Part 25 all comments received into any FAA
with the armrest or other seat docket, including the name of the
[Docket No. FAA–2018–0932; Special
components in any manner significantly Conditions No. 25–733–SC]
individual sending the comment (or
different than would be expected for a signing the comment for an association,
forward-facing seat installation. Special Conditions: Mitsubishi Aircraft business, labor union, etc.). DOT’s
Corporation Model MRJ–200 Airplane; complete Privacy Act Statement can be
5. Pelvis Criteria Passenger Seats With Non-Traditional, found in the Federal Register published
Large, Non-Metallic Panels on April 11, 2000 (65 FR 19477–19478).
Any part of the load-bearing portion
Docket: Background documents or
of the bottom of the ATD pelvis must AGENCY: Federal Aviation
comments received may be read at
not translate beyond the edges of the Administration (FAA), DOT.
http://www.regulations.gov/ at any time.
seat bottom seat-cushion supporting ACTION: Final special conditions; request
Follow the online instructions for
structure. for comments. accessing the docket or go to Docket
6. Femur Criteria SUMMARY: These special conditions are Operations in Room W12–140 of the
issued for the Mitsubishi Aircraft West Building Ground Floor at 1200
Axial rotation of the upper leg (about Corporation Model MRJ–200 airplane. New Jersey Avenue SE, Washington,
the z-axis of the femur per SAE This airplane will have novel or DC, between 9 a.m. and 5 p.m., Monday
Recommended Practice J211/1) must be unusual design features when compared through Friday, except Federal holidays.
limited to 35 degrees from the nominal to the state of technology envisioned in FOR FURTHER INFORMATION CONTACT:
seated position. Evaluation during the airworthiness standards for Nicholas Wilson, International Section,
rebound does not need to be considered. transport category airplanes. These AIR–676, Transport Standards Branch,
7. ATD and Test Conditions design features include passenger seats Policy and Innovation Division, Aircraft
that incorporate non-traditional, large, Certification Service, Federal Aviation
Longitudinal tests conducted to non-metallic panels in lieu of the Administration, 2200 South 216th
measure the injury criteria above must traditional metal frame covered by Street, Des Moines, Washington 98198;
be performed with the FAA Hybrid III fabric. The applicable airworthiness telephone and fax 206–231–3230; email
ATD, as described in SAE 1999–01– regulations do not contain adequate or Nicholas.Wilson@faa.gov.
1609, ‘‘A Lumbar Spine Modification to appropriate safety standards for this
design feature. These special conditions SUPPLEMENTARY INFORMATION: The
the Hybrid III ATD for Aircraft Seat substance of these special conditions
Tests.’’ The tests must be conducted contain the additional safety standards
that the Administrator considers has been published in the Federal
with an undeformed floor, at the most- Register for public comment in several
necessary to establish a level of safety
critical yaw cases for injury, and with prior instances with no substantive
equivalent to that established by the
all lateral structural supports (e.g., comments received. The FAA, therefore,
existing airworthiness standards.
armrests or walls) installed. finds it unnecessary to delay the
DATES: This action is effective on
Note: Boeing must demonstrate that the effective date and finds that good cause
Mitsubishi Aircraft Corporation on
installation of seats via plinths or pallets exists for making these special
October 22, 2018. Send comments on or
meets all applicable requirements. conditions effective upon publication in
before December 6, 2018.
Compliance with the guidance contained in the Federal Register.
ADDRESSES: Send comments identified
policy memorandum PS–ANM–100–2000– Comments Invited
by Docket No. FAA–2018–0932 using
00123, ‘‘Guidance for Demonstrating
any of the following methods:
Compliance with Seat Dynamic Testing for
• Federal eRegulations Portal: Go to We invite interested people to take
Plinths and Pallets,’’ dated February 2, 2000,
http://www.regulations.gov/ and follow part in this rulemaking by sending
is acceptable to the FAA. written comments, data, or views. The
the online instructions for sending your
comments electronically. most helpful comments reference a
8. Inflatable Airbag Restraint Systems • Mail: Send comments to Docket specific portion of the special
Special Conditions Operations, M–30, U.S. Department of conditions, explain the reason for any
recommended change, and include
daltland on DSKBBV9HB2PROD with RULES
If inflatable airbag restraint systems Transportation (DOT), 1200 New Jersey
Avenue SE, Room W12–140, West supporting data.
are installed, the airbag systems must
Building Ground Floor, Washington, DC We will consider all comments we
meet the requirements in one of the
20590–0001. receive by the closing date for
airbag (inflatable restraint) special
• Hand Delivery or Courier: Take comments. We may change these special
conditions applicable to the Boeing
comments to Docket Operations in conditions based on the comments we
Model 777 series airplanes. Room W12–140 of the West Building receive.
VerDate Sep<11>2014 16:28 Oct 19, 2018 Jkt 247001 PO 00000 Frm 00008 Fmt 4700 Sfmt 4700 E:\FR\FM\22OCR1.SGM 22OCR1](https://thefederalregister.org/doc/83_FR_53370/page/1.svg)
![53168 Federal Register / Vol. 83, No. 204 / Monday, October 22, 2018 / Rules and Regulations
that established by the existing Issued in Des Moines, Washington, on • Hand Delivery or Courier: Take
airworthiness standards. October 16, 2018. comments to Docket Operations in
Victor Wicklund, Room W12–140 of the West Building
Applicability Manager, Transport Standards Branch, Policy Ground Floor at 1200 New Jersey
As discussed above, these special and Innovation Division, Aircraft Avenue SE, Washington, DC, between 9
Certification Service. a.m. and 5 p.m., Monday through
conditions are applicable to the
[FR Doc. 2018–22922 Filed 10–19–18; 8:45 am] Friday, except Federal holidays.
Mitsubishi Aircraft Corporation Model
MRJ–200 airplane. Should Mitsubishi BILLING CODE 4910–13–P • Fax: Fax comments to Docket
Aircraft Corporation apply at a later date Operations at 202–493–2251.
for a change to the type certificate to Privacy: The FAA will post all
DEPARTMENT OF TRANSPORTATION comments it receives, without change,
include another model incorporating the
same novel or unusual design feature, to http://www.regulations.gov/,
Federal Aviation Administration including any personal information the
these special conditions would apply to
that model as well. commenter provides. Using the search
14 CFR Part 25 function of the docket website, anyone
Conclusion [Docket No. FAA–2018–0714; Special can find and read the electronic form of
Conditions No. 25–734–SC] all comments received into any FAA
This action affects only a certain
docket, including the name of the
novel or unusual design feature on one Special Conditions: Bombardier, Inc., individual sending the comment (or
model of airplane. It is not a rule of BD–700–2A12 and BD–700–2A13 signing the comment for an association,
general applicability. Airplanes; Multiple-Place Side-Facing business, labor union, etc.). DOT’s
List of Subjects in 14 CFR Part 25 Seats With Active Leg-Flail Restraint complete Privacy Act Statement can be
Device and Shoulder-Belt Airbags found in the Federal Register published
Aircraft, Aviation safety, Reporting on April 11, 2000 (65 FR 19477–19478).
AGENCY: Federal Aviation
and recordkeeping requirements. Docket: Background documents or
Administration (FAA), DOT.
Authority Citation ACTION: Final special conditions; request comments received may be read at
for comments. http://www.regulations.gov/ at any time.
The authority citation for these Follow the online instructions for
special conditions is as follows: SUMMARY: These special conditions are accessing the docket or go to Docket
Authority: 49 U.S.C. 106(f), 106(g), 40113, issued for the Bombardier, Inc., Operations in Room W12–140 of the
44701, 44702, 44704. (Bombardier) BD–700–2A12 and BD– West Building Ground Floor at 1200
700–2A13 airplanes, marketed New Jersey Avenue SE, Washington,
The Special Conditions respectively as Global 7000 and Global DC, between 9 a.m. and 5 p.m., Monday
Accordingly, pursuant to the 8000. These airplanes, as modified by through Friday, except Federal holidays.
authority delegated to me by the Bombardier, will have novel or unusual FOR FURTHER INFORMATION CONTACT:
Administrator, the following special design features when compared to the Alan Sinclair, Airframe and Cabin
conditions are issued as part of the type state of technology envisioned in the Safety Section, AIR–675, Transport
certification basis for Mitsubishi airworthiness standards for transport- Standards Branch, Policy and
Aircraft Company Model MRJ–200 category airplanes. These design Innovation Division, Aircraft
airplanes. features are multiple-place side-facing Certification Service, Federal Aviation
seats with active leg-flail restraint Administration, 2200 South 216th
1. Except as provided in paragraph 3 devices and shoulder-belt airbags. The Street, Des Moines, Washington 98198;
of these special conditions, compliance applicable airworthiness regulations do telephone and fax 206–231–3215; email
with 14 CFR part 25, appendix F, part not contain adequate or appropriate alan.sinclair@faa.gov.
IV, Heat Release and part V, Smoke safety standards for this design feature.
Emission, is required for seats that SUPPLEMENTARY INFORMATION: The
These special conditions contain the substance of these special conditions
incorporate non-traditional, large, non- additional safety standards that the
metallic panels that may either be a has been published in the Federal
Administrator considers necessary to Register for public comment in several
single component or multiple establish a level of safety equivalent to
components in a concentrated area in prior instances with no substantive
that established by the existing comments received. The FAA therefore
their design. airworthiness standards. finds it unnecessary to delay the
2. The applicant may designate up to DATES: This action is effective on effective date and finds that good cause
and including 0.139 square meter (1.5 Bombardier on October 22, 2018. Send exists for making these special
square feet of non-traditional, non- comments on or before December 6, conditions effective upon publication in
metallic panel material per seat place 2018. the Federal Register.
that does not have to comply with
ADDRESSES: Send comments identified
paragraph 1 of these special conditions. Comments Invited
by Docket No. FAA–2018–0714 using
A double seat assembly may have a total We invite interested people to take
any of the following methods:
of 0.278 square meter (3.0 square feet) • Federal eRegulations Portal: Go to part in this rulemaking by sending
excluded on any portion of the assembly http://www.regulations.gov/ and follow written comments, data, or views. The
(e.g., outboard seat place 0.093 square the online instructions for sending your most helpful comments reference a
meter [1 square foot] and inboard 0.185 specific portion of the special
daltland on DSKBBV9HB2PROD with RULES
comments electronically.
square meter [2.0 square feet]). • Mail: Send comments to Docket conditions, explain the reason for any
3. Seats do not have to meet the test Operations, M–30, U.S. Department of recommended change, and include
requirements of 14 CFR part 25, Transportation (DOT), 1200 New Jersey supporting data.
appendix F, parts IV and V, when Avenue SE, Room W12–140, West We will consider all comments we
installed in compartments defined in 14 Building Ground Floor, Washington, DC receive by the closing date for
CFR 25.853(e). 20590–0001. comments. We may change these special
VerDate Sep<11>2014 16:28 Oct 19, 2018 Jkt 247001 PO 00000 Frm 00010 Fmt 4700 Sfmt 4700 E:\FR\FM\22OCR1.SGM 22OCR1](https://thefederalregister.org/doc/83_FR_53370/page/3.svg)
Document Created: 2018-10-20 01:50:31
Document Modified: 2018-10-20 01:50:31
| Category | Regulatory Information | |
| Collection | Federal Register | |
| sudoc Class | AE 2.7: GS 4.107: AE 2.106: | |
| Publisher | Office of the Federal Register, National Archives and Records Administration | |
| Section | Rules and Regulations | |
| Action | Final special conditions; request for comments. | |
| Dates | This action is effective on Mitsubishi Aircraft Corporation on October 22, 2018. Send comments on or before December 6, 2018. | |
| Contact | Nicholas Wilson, International Section, AIR-676, Transport Standards Branch, Policy and Innovation Division, Aircraft Certification Service, Federal Aviation Administration, 2200 South 216th Street, Des Moines, Washington 98198; telephone and fax 206-231-3230; email [email protected] | |
| FR Citation | 83 FR 53166 | |
| CFR Associated | Aircraft; Aviation Safety and Reporting and Recordkeeping Requirements |
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