80 FR 58597 - Special Conditions: Flight Structures, Inc., Boeing Model 777-200 Dynamic Test Requirements for Single-Occupant, Oblique (Side-Facing) Seats With Airbag Devices
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 80, Issue 189 (September 30, 2015)
Federal Aviation Administration
Federal Register Volume 80, Issue 189 (September 30, 2015)
| Page Range | 58597-58599 | |
| FR Document | 2015-24727 |
[Federal Register Volume 80, Number 189 (Wednesday, September 30, 2015)] [Rules and Regulations] [Pages 58597-58599] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2015-24727] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 25 [Docket No. FAA-2015-3367; Special Conditions No. 25-596-SC] Special Conditions: Flight Structures, Inc., Boeing Model 777-200 Dynamic Test Requirements for Single-Occupant, Oblique (Side-Facing) Seats With Airbag Devices AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final special conditions; request for comments. ----------------------------------------------------------------------- SUMMARY: These special conditions are issued for Boeing Model 777-200 airplanes. This airplane, as modified by Flight Structures, Inc., will have novel or unusual design features associated with oblique-angled, single-occupant seats equipped with airbag systems. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for these design features. These special conditions contain the additional safety standards the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards. DATES: The effective date of these special conditions is September 30, 2015. We must receive your comments by November 16, 2015. ADDRESSES: Send comments identified by docket number FAA-2015-3367 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 Web site, 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), as well as at http://DocketsInfo.dot.gov/. 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: John Shelden, Airframe and Cabin Safety, ANM-115, Transport Airplane Directorate, Aircraft Certification Service, 1601 Lind Avenue SW., Renton, Washington 98057-3356; telephone 425-227-2785; facsimile 425-227-1149. SUPPLEMENTARY INFORMATION: The FAA has determined that notice of, and opportunity for, prior public comment on these special conditions are impracticable because these procedures would significantly delay issuance of the design approval and thus delivery of the affected airplane. In addition, the substance of these special conditions has been subject to the public-comment process in several prior instances with no substantive comments received. The FAA therefore finds that good cause exists for making these special conditions effective upon issuance. [[Page 58598]] 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. Background On July 7, 2014, Flight Structures, Inc., applied for a supplemental type certificate to allow the installation of oblique business-class passenger seats, positioned at 32.5 degrees to the vertical plane of the airplane longitudinal centerline, and to include inflatable lap belts, in Boeing Model 777-200 airplanes. The seating configuration Flight Structures, Inc., proposes in certification plan No. B3FS332-D10 includes the installation of TSO- 39c-approved, Zodiac Aries model, side-facing, pod-style, business- class seats (with surrounding shells and front-row furniture), installed at an angle of up to 32.5 degrees to the airplane longitudinal centerline. These seats will include restraint (airbag) systems for occupant restraint and injury protection. The Boeing Model 777-200 airplane, approved under Type Certificate No. T00001SE, is a swept-wing, conventional-tail, twin-engine, turbofan-powered transport airplane, with seating capacity for 440 passengers. Type Certification Basis Under the provisions of title 14, Code of Federal Regulations (14 CFR) 21.101, Flight Structures, Inc., must show that the Model 777-200 airplane, as changed, meets the applicable provisions of the regulations listed in Type Certificate No. T00001SE, or the applicable regulations in effect on the date of application for the change, except for earlier amendments as agreed upon by the FAA. The regulations listed in the type certificate are commonly referred to as the ``original type- certification basis.'' The regulations listed in Type Certificate No. T00001SE are as follows: 14 CFR part 25, Amendments 25-1 through 25-82, with exceptions listed in the type-certification data sheet. In addition, the certification basis includes certain special conditions, exemptions, or later amended sections of the applicable part that are not relevant to these special conditions. If the Administrator finds that the applicable airworthiness regulations (i.e., 14 CFR part 25) do not contain adequate or appropriate safety standards for Boeing Model 777-200 airplanes because of a novel or unusual design feature, special conditions are prescribed under Sec. 21.16. Special conditions are initially applicable to the model for which they are issued. Should the applicant apply for a supplemental type certificate to modify any other model included on the same type certificate to incorporate 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 Boeing Model 777-200 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. 21.101. Novel or Unusual Design Features The business-class seating configuration Flight Structures, Inc., proposes is novel and unusual due to the seat installation at 32.5 degrees to the aircraft centerline, the airbag-system installation, and the seat/occupant interface with the surrounding furniture that introduces occupant alignment and loading concerns. The proposed business-class seating configuration also is beyond the limits of current acceptable equivalent-level-of-safety findings. Ongoing research is progressing to establish acceptable limits. Until those limits become available, the FAA proposes a set of interim limits based on the current literature available, current National Highway Traffic Safety Administration (NHTSA) regulations, and preliminary test data from the research program. The existing regulations do not provide adequate or appropriate safety standards for occupants of oblique-angled seats with airbag systems. To provide a level of safety that is equivalent to that afforded occupants of forward- and aft-facing seats, additional airworthiness standards, in the form of special conditions, are necessary. These special conditions supplement part 25 and, more specifically, supplement Sec. Sec. 25.562 and 25.785. The requirements contained in these special conditions consist of both test conditions and injury pass/fail criteria. Discussion Amendment 25-15 to part 25, dated October 24, 1967, introduced the subject of side-facing seats, and a requirement that each occupant in a side-facing seat must be protected from head injury by a safety belt and a cushioned rest that will support the arms, shoulders, head, and spine. Subsequently, Amendment 25-20, dated April 23, 1969, clarified the definition of side-facing seats to require that each occupant of a seat, positioned at more than an 18-degree angle to the vertical plane of the airplane longitudinal centerline, must be protected from head injury by a safety belt and an energy-absorbing rest that will support the arms, shoulders, head, and spine; or by a safety belt and shoulder harness that will prevent the head from contacting any injurious object. The FAA concluded that an 18-degree angle would provide an adequate level of safety based on tests that were performed at that time, and thus adopted that standard. Part 25 was amended June 16, 1988, by Amendment 25-64, to revise the emergency-landing conditions that must be considered in the design of the airplane. Amendment 25-64 revised the static-load conditions in 14 CFR 25.561, and added the new Sec. 25.562 that requires dynamic testing for all seats approved for occupancy during takeoff and landing. The intent of Amendment 25-64 is to provide an improved level of safety for occupants on transport-category airplanes. Because most seating is forward-facing on transport-category airplanes, the pass/ fail criteria developed in Amendment 25-64 focused primarily on these seats. As a result, the FAA issued Policy Memorandums ANM-03-115-30 and PS-ANM-100-2000-00123 to provide the additional guidance necessary to demonstrate the level of safety required by the regulations for side- facing seats. To reflect current research findings, the FAA developed a methodology to address all fully side-facing seats (i.e., seats positioned in the airplane with the occupant facing 90 degrees to the vertical plane of the airplane centerline), and has documented those requirements in a set of new special conditions. The FAA issued Policy Statement PS-ANM-25-03-R1 to define revised injury criteria associated with neck and leg injuries. The proposed Model 777-200 airplane business-class seat installation is novel such that the current Model 777-200 airplane certification basis does not adequately protection of the occupant's neck and spine for seat [[Page 58599]] configurations that are positioned at an angle greater than 18 degrees from the airplane centerline. Therefore, the Flight Structures, Inc., proposed configuration will require new special conditions. These special conditions will provide head injury criteria, neck injury criteria, spine injury criteria, and body-to-wall contact criteria. They 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. Applicability These special conditions are applicable to the Boeing Model 777-200 airplanes configured with the business-class seating defined in Flight Structures, Inc., certification plan No. B3FS332-D10. Should Flight Structures, Inc., apply at a later date for a supplemental type certificate to modify any other model included on Type Certificate No. T00001SE to incorporate the same novel or unusual design feature, these special conditions would apply to the other model as well. Conclusion This action affects only certain novel or unusual design features on one model of airplane. It is not a rule of general applicability, and affects only the applicant who applied to the FAA for approval of these features on the airplane. The substance of these special conditions has been subjected to the notice and comment period in several prior instances, and has been derived without substantive change from those previously issued. It is unlikely that prior public comment would result in a significant change from the substance contained herein. Therefore, because a delay would significantly affect the certification of the airplane, the FAA has determined that prior public notice and comment are unnecessary and impracticable, and good cause exists for adopting these special conditions upon publication in the Federal Register. The FAA is requesting comments to allow interested persons to submit views that may not have been submitted in response to the prior opportunities for comment described above. List of Subjects in 14 CFR Part 25 Aircraft, Aviation safety, Reporting and recordkeeping requirements. The authority citation for these special conditions is as follows: Authority: 49 U.S.C. 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 the Boeing Model 777-200 airplane. Side-Facing Seats Special Conditions In addition to the requirements of Sec. 25.562: 1. Head-Injury Criteria Compliance with Sec. 25.562(c)(5) is required, except that, if the anthropomorphic test device (ATD) has no apparent contact with the seat/structure but has contact with an airbag, a head-injury criterion (HIC) unlimited score in excess of 1000 is acceptable, provided the HIC15 score (calculated in accordance with 49 CFR 571.208) for that contact is less than 700. 2. Body-to-Wall/Furnishing Contact If a seat is installed aft of structure (e.g., an interior wall or furnishing) that does not provide a homogenous contact surface for the expected range of occupants and yaw angles, then additional analysis and/or test(s) may be required to demonstrate that the injury criteria are met for the area that an occupant could contact. For example, if different yaw angles could result in different airbag performance, then additional analysis or separate test(s) may be necessary to evaluate performance. 3. Neck Injury Criteria The seating system must protect the occupant from experiencing serious neck injury. The assessment of neck injury must be conducted with the airbag device activated, unless there is reason to also consider that the neck-injury potential would be higher for impacts below the airbag-device deployment threshold. a. The Nij (calculated in accordance with 49 CFR 571.208) must be below 1.0, where Nij =Fz / Fzc + My /Myc , and Nij critical values are: i. Fzc = 1530 lb for tension ii. Fzc = 1385 lb for compression iii. Myc = 229 lb-ft in flexion iv. Myc = 100 lb-ft in extension b. In addition, peak Fz must be below 937 lb in tension and 899 lb in compression. c. Rotation of the head about its vertical axis, relative to the torso, is limited to 105 degrees in either direction from forward- facing. d. The neck must not impact any surface that would produce concentrated loading on the neck. 4. Spine and Torso Injury Criteria a. The shoulders must remain aligned with the hips throughout the impact sequence, or support for the upper torso must be provided to prevent forward or lateral flailing beyond 45 degrees from the vertical during significant spinal loading. Alternatively, the lumbar spine tension (Fz ) cannot exceed 1200 lb. b. Significant concentrated loading on the occupant's spine, in the area between the pelvis and shoulders during impact, including rebound, is not acceptable. During this type of contact, the interval for any rearward (X-direction) acceleration exceeding 20g must be less than 3 milliseconds as measured by the thoracic instrumentation specified in 49 CFR part 572, subpart E, filtered in accordance with SAE International (SAE) J211-1. c. Occupant must not interact with the armrest or other seat components in any manner significantly different than would be expected for a forward-facing seat installation. 5. Longitudinal test(s), conducted to measure the injury criteria above, must be performed with the FAA Hybrid III ATD, as described in SAE 1999-01-1609. The test(s) must be conducted with an undeformed floor, at the most-critical yaw case(s) for injury, and with all lateral structural supports (armrests/walls) installed. Note: Boeing must demonstrate that the installation of seats via plinths or pallets meets all applicable requirements. Compliance with the guidance contained in FAA Policy Memorandum PS-ANM-100- 2000-00123, dated February 2, 2000, titled ``Guidance for Demonstrating Compliance with Seat Dynamic Testing for Plinths and Pallets,'' is acceptable to the FAA. Inflatable Lap Belt Special Conditions If inflatable lap belts are installed on single-place side-facing seats, the lap belts must meet Special Conditions No. 25-187A-SC. Issued in Renton, Washington, on September 2, 2015. Jeffrey E. Duven, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2015-24727 Filed 9-29-15; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 80, No. 189 / Wednesday, September 30, 2015 / Rules and Regulations 58597
installed such that the inflatable lap belt demonstrated to reliably operate Mail: Send comments to Docket
would not properly deploy. between inspection intervals. Operations, M–30, U.S. Department of
Alternatively, it must be shown that 14. The inflatable material may not Transportation (DOT), 1200 New Jersey
such deployment is not hazardous to the have an average burn rate of greater than Avenue SE., Room W12–140, West
occupant, and will provide the required 2.5 inches per minute when tested using Building Ground Floor, Washington,
head-injury protection. the horizontal-flammability test as DC, 20590–0001.
4. The inflatable lap-belt system must defined in 14 CFR part 25, Appendix F, Hand Delivery or Courier: Take
be shown not to be susceptible to Part I(b)(5). comments to Docket Operations in
inadvertent deployment as a result of 15. The airbag system in the lap belt,
Room W12–140 of the West Building
wear and tear, or inertial loads resulting once deployed, must not adversely
Ground Floor at 1200 New Jersey
from in-flight or ground maneuvers affect the emergency-lighting system
Avenue SE., Washington, DC, between 9
(including gusts and hard landings), (i.e., block floor-proximity lights to the
a.m. and 5 p.m., Monday through
likely to be experienced in service. extent that the lights no longer meet
Friday, except Federal holidays.
5. Deployment of the inflatable lap their intended function).
belt must not introduce injury Fax: Fax comments to Docket
Issued in Renton, Washington, on
mechanisms to the seated occupant, nor September 1, 2015. Operations at 202–493–2251.
result in injuries that could impede Jeffrey E. Duven, Privacy: The FAA will post all
rapid egress. This assessment should Manager, Transport Airplane Directorate, comments it receives, without change,
include an occupant who is in the brace Aircraft Certification Service. to http://www.regulations.gov/,
position when it deploys, and an [FR Doc. 2015–24725 Filed 9–29–15; 8:45 am] including any personal information the
occupant whose inflatable lap belt is BILLING CODE 4910–13–P
commenter provides. Using the search
loosely fastened. function of the docket Web site, anyone
6. An inadvertent deployment that can find and read the electronic form of
could cause injury to a standing or DEPARTMENT OF TRANSPORTATION all comments received into any FAA
sitting person must be shown to be docket, including the name of the
improbable. Federal Aviation Administration individual sending the comment (or
7. It must be shown that inadvertent signing the comment for an association,
deployment of the airbag system in the 14 CFR Part 25 business, labor union, etc.). DOT’s
lap belt, during the most critical part of complete Privacy Act Statement can be
[Docket No. FAA–2015–3367; Special
the flight, either will not cause a hazard Conditions No. 25–596–SC] found in the Federal Register published
to the airplane or its occupants, or meets on April 11, 2000 (65 FR 19477–19478),
the requirement of § 25.1309(b). Special Conditions: Flight Structures, as well as at http://DocketsInfo.
8. The inflatable lap belt must be Inc., Boeing Model 777–200 Dynamic dot.gov/.
shown to not impede rapid egress of Test Requirements for Single- Docket: Background documents or
occupants 10 seconds after its Occupant, Oblique (Side-Facing) Seats comments received may be read at
deployment. With Airbag Devices http://www.regulations.gov/ at any time.
9. The inflatable lap-belt system must
AGENCY: Federal Aviation Follow the online instructions for
be protected from lightning and HIRF.
Administration (FAA), DOT. accessing the docket or go to Docket
The threats specified in existing
ACTION: Final special conditions; request
Operations in Room W12–140 of the
regulations regarding lightning,
for comments. West Building Ground Floor at 1200
§ 25.1316, and HIRF, § 25.1317, are
New Jersey Avenue SE., Washington,
incorporated by reference for the
SUMMARY: These special conditions are DC, between 9 a.m. and 5 p.m., Monday
purpose of measuring lightning and
issued for Boeing Model 777–200 through Friday, except Federal holidays.
HIRF protection. For the purposes of
airplanes. This airplane, as modified by
complying with HIRF requirements, the FOR FURTHER INFORMATION CONTACT: John
Flight Structures, Inc., will have novel
inflatable lap-belt system is considered Shelden, Airframe and Cabin Safety,
or unusual design features associated
a ‘‘critical system’’ if its deployment ANM–115, Transport Airplane
with oblique-angled, single-occupant
could have a hazardous effect on the Directorate, Aircraft Certification
seats equipped with airbag systems. The
airplane; otherwise it is considered an Service, 1601 Lind Avenue SW.,
applicable airworthiness regulations do
‘‘essential’’ system. Renton, Washington 98057–3356;
10. The inflatable lap belt must not contain adequate or appropriate
telephone 425–227–2785; facsimile
function properly after loss of normal safety standards for these design
425–227–1149.
airplane electrical power, and after a features. These special conditions
contain the additional safety standards SUPPLEMENTARY INFORMATION: The FAA
transverse separation of the fuselage at
the Administrator considers necessary has determined that notice of, and
the most critical location. A separation
to establish a level of safety equivalent opportunity for, prior public comment
at the location of the lap belt does not
to that established by the existing on these special conditions are
have to be considered.
11. The inflatable lap belt must be airworthiness standards. impracticable because these procedures
shown to not release hazardous DATES: The effective date of these would significantly delay issuance of
quantities of gas or particulate matter special conditions is September 30, the design approval and thus delivery of
into the cabin. 2015. We must receive your comments the affected airplane.
12. The inflatable lap-belt installation by November 16, 2015. In addition, the substance of these
mstockstill on DSK4VPTVN1PROD with RULES
must be protected from the effects of fire ADDRESSES: Send comments identified special conditions has been subject to
such that no hazard to occupants will by docket number FAA–2015–3367 the public-comment process in several
result. using any of the following methods: prior instances with no substantive
13. A means must be available for a Federal eRegulations Portal: Go to comments received. The FAA therefore
crewmember to verify the integrity of http://www.regulations.gov/ and follow finds that good cause exists for making
the inflatable-lap-belt-activation system the online instructions for sending your these special conditions effective upon
prior to each flight, or it must be comments electronically. issuance.
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![Federal Register / Vol. 80, No. 189 / Wednesday, September 30, 2015 / Rules and Regulations 58599
configurations that are positioned at an The Special Conditions 4. Spine and Torso Injury Criteria
angle greater than 18 degrees from the Accordingly, pursuant to the
airplane centerline. Therefore, the Flight a. The shoulders must remain aligned
authority delegated to me by the with the hips throughout the impact
Structures, Inc., proposed configuration Administrator, the following special
will require new special conditions. sequence, or support for the upper torso
conditions are issued as part of the type must be provided to prevent forward or
These special conditions will provide certification basis for the Boeing Model
head injury criteria, neck injury criteria, lateral flailing beyond 45 degrees from
777–200 airplane.
spine injury criteria, and body-to-wall the vertical during significant spinal
contact criteria. They contain the Side-Facing Seats Special Conditions loading. Alternatively, the lumbar spine
additional safety standards that the In addition to the requirements of tension (Fz) cannot exceed 1200 lb.
Administrator considers necessary to § 25.562: b. Significant concentrated loading on
establish a level of safety equivalent to the occupant’s spine, in the area
that established by the existing 1. Head-Injury Criteria
between the pelvis and shoulders
airworthiness standards. Compliance with § 25.562(c)(5) is during impact, including rebound, is
Applicability required, except that, if the not acceptable. During this type of
anthropomorphic test device (ATD) has contact, the interval for any rearward
These special conditions are no apparent contact with the seat/ (X-direction) acceleration exceeding 20g
applicable to the Boeing Model 777–200 structure but has contact with an airbag, must be less than 3 milliseconds as
airplanes configured with the business- a head-injury criterion (HIC) unlimited measured by the thoracic
class seating defined in Flight score in excess of 1000 is acceptable, instrumentation specified in 49 CFR
Structures, Inc., certification plan No. provided the HIC15 score (calculated in
part 572, subpart E, filtered in
B3FS332–D10. Should Flight Structures, accordance with 49 CFR 571.208) for
accordance with SAE International
Inc., apply at a later date for a that contact is less than 700.
supplemental type certificate to modify (SAE) J211–1.
2. Body-to-Wall/Furnishing Contact c. Occupant must not interact with
any other model included on Type
Certificate No. T00001SE to incorporate If a seat is installed aft of structure the armrest or other seat components in
the same novel or unusual design (e.g., an interior wall or furnishing) that any manner significantly different than
feature, these special conditions would does not provide a homogenous contact would be expected for a forward-facing
apply to the other model as well. surface for the expected range of seat installation.
occupants and yaw angles, then 5. Longitudinal test(s), conducted to
Conclusion additional analysis and/or test(s) may be
measure the injury criteria above, must
This action affects only certain novel required to demonstrate that the injury
be performed with the FAA Hybrid III
or unusual design features on one model criteria are met for the area that an
ATD, as described in SAE 1999–01–
of airplane. It is not a rule of general occupant could contact. For example, if
different yaw angles could result in 1609. The test(s) must be conducted
applicability, and affects only the
different airbag performance, then with an undeformed floor, at the most-
applicant who applied to the FAA for
additional analysis or separate test(s) critical yaw case(s) for injury, and with
approval of these features on the
airplane. may be necessary to evaluate all lateral structural supports (armrests/
performance. walls) installed.
The substance of these special
conditions has been subjected to the 3. Neck Injury Criteria Note: Boeing must demonstrate that the
notice and comment period in several installation of seats via plinths or pallets
prior instances, and has been derived The seating system must protect the meets all applicable requirements.
without substantive change from those occupant from experiencing serious Compliance with the guidance contained in
previously issued. It is unlikely that neck injury. The assessment of neck FAA Policy Memorandum PS–ANM–100–
prior public comment would result in a injury must be conducted with the 2000–00123, dated February 2, 2000, titled
significant change from the substance airbag device activated, unless there is ‘‘Guidance for Demonstrating Compliance
contained herein. Therefore, because a reason to also consider that the neck- with Seat Dynamic Testing for Plinths and
delay would significantly affect the injury potential would be higher for Pallets,’’ is acceptable to the FAA.
certification of the airplane, the FAA impacts below the airbag-device
has determined that prior public notice deployment threshold. Inflatable Lap Belt Special Conditions
and comment are unnecessary and a. The Nij (calculated in accordance
with 49 CFR 571.208) must be below If inflatable lap belts are installed on
impracticable, and good cause exists for single-place side-facing seats, the lap
adopting these special conditions upon 1.0, where Nij =Fz/Fzc + My/Myc, and Nij
critical values are: belts must meet Special Conditions No.
publication in the Federal Register. The
i. Fzc = 1530 lb for tension 25–187A–SC.
FAA is requesting comments to allow
interested persons to submit views that ii. Fzc = 1385 lb for compression Issued in Renton, Washington, on
may not have been submitted in iii. Myc = 229 lb-ft in flexion September 2, 2015.
response to the prior opportunities for iv. Myc = 100 lb-ft in extension Jeffrey E. Duven,
comment described above. b. In addition, peak Fz must be below
Manager, Transport Airplane Directorate,
937 lb in tension and 899 lb in Aircraft Certification Service.
List of Subjects in 14 CFR Part 25 compression.
mstockstill on DSK4VPTVN1PROD with RULES
[FR Doc. 2015–24727 Filed 9–29–15; 8:45 am]
Aircraft, Aviation safety, Reporting c. Rotation of the head about its
vertical axis, relative to the torso, is BILLING CODE 4910–13–P
and recordkeeping requirements.
limited to 105 degrees in either
The authority citation for these direction from forward-facing.
special conditions is as follows: d. The neck must not impact any
Authority: 49 U.S.C. 106(g), 40113, 44701, surface that would produce
44702, 44704. concentrated loading on the neck.
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Document Created: 2015-12-15 09:31:38
Document Modified: 2015-12-15 09:31:38
| 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 | The effective date of these special conditions is September 30, 2015. We must receive your comments by November 16, 2015. | |
| Contact | John Shelden, Airframe and Cabin Safety, ANM-115, Transport Airplane Directorate, Aircraft Certification Service, 1601 Lind Avenue SW., Renton, Washington 98057-3356; telephone 425-227-2785; facsimile 425-227-1149. | |
| FR Citation | 80 FR 58597 | |
| CFR Associated | Aircraft; Aviation Safety and Reporting and Recordkeeping Requirements |
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