| Page Range | 43471-43472 | |
| FR Document | 2016-15784 |
[Federal Register Volume 81, Number 128 (Tuesday, July 5, 2016)] [Rules and Regulations] [Pages 43471-43472] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2016-15784] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 25 [Docket No. FAA-2015-8298; Special Conditions No. 25-611-SC] Special Conditions: JAMCO America, Inc., Boeing Model 777-300ER, Dynamic Test Requirements for Single-Occupant Oblique (Side-Facing) Seats With Inflatable Restraints AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final special condition; request for comments; corrections. ----------------------------------------------------------------------- SUMMARY: This document corrects omissions in docket no. FAA-2015-8298, special conditions no. 25-611-SC, which was published in the Federal Register on March 16, 2016 (81 FR 13969). The special conditions in the published document are incomplete. This correction replaces the entire special conditions section from that which appeared in the original Federal Register publication. DATES: This action is effective on JAMCO America, Inc., on July 5, 2016. We must receive your comments August 19, 2016. FOR FURTHER INFORMATION CONTACT: John Shelden, FAA, Airframe and Cabin Safety Branch, ANM-115,Transport Airplane Directorate, Aircraft Certification Service, 1601 Lind Avenue SW., Renton, Washington 98057- 3356; telephone (425) 227-2785; facsimile (425) 227-1320. SUPPLEMENTARY INFORMATION: On March 16, 2016, the Federal Register published a document designated as ``Docket No. FAA-2015-8298; Special Conditions No. 25-611-SC,'' (81 FR 13969). That document issued special conditions pertaining to dynamic test requirements for single-occupant oblique (side-facing) seats with inflatable restraints on Boeing Model 777-300ER airplanes. As published, the special conditions are incomplete. The applicant was aware of the complete set of conditions at the time of the original, incomplete publication. Correction The following special conditions replace the entire special conditions section of the final special conditions document [FR Doc. 2016-05995 Filed 3-15-16; 8:45 a.m.], published on March 16, 2016 (81 FR 13969). The introductory language was previously published and is not changed. The Special Conditions 0 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 Boeing Model 777-300ER airplanes modified by JAMCO. Oblique (Side-Facing) Seats Special Conditions In addition to the requirements of Sec. 25.562: 1. Head Injury Criteria (HIC) Compliance with Sec. 25.562(c)(5) is required, except that, if the anthropomorphic test device (ATD) has no apparent contact with the seat and related structure but has contact with an airbag, a 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. interior wall or furnishings) that does not provide a homogenous contact surface for the expected range of occupants and yaw angles, then [[Page 43472]] additional analysis and tests 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 device performance, then additional analysis or separate tests may be necessary to evaluate performance. 3. Neck Injury Criteria a. 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. b. 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 c. In addition, peak upper neck Fz must be below 937 lb in tension and 899 lb in compression. d. Rotation of the head about its vertical axis relative to the torso is limited to 105 degrees in either direction from forward- facing. e. The neck must not impact any surface that would produce concentrated loading on the neck. 4. Spine and Torso Injury Criteria a. 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-axis 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 recommended practice J211/1, ``Instrumentation for Impact Test-- Part 1--Electronic Instrumentation.'' c. The 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. Pelvis Criteria Any part of the load-bearing portion of the bottom of the ATD pelvis must not translate beyond the edges of the seat bottom seat- cushion supporting structure. 6. Femur Criteria Axial rotation of the upper leg (about the Z-axis of the femur, per SAE J211/1) must be limited to 35 degrees in the strike direction from the normal seating position. Evaluation during rebound need not be considered. 7. ATD and Test Conditions Longitudinal tests conducted to measure the injury criteria above must be performed with the FAA Hybrid III ATD, as described in SAE 1999-01-1609, ``A Lumbar Spine Modification to the Hybrid III ATD For Aircraft Seat Tests.'' The tests must be conducted with an undeformed floor, at the most-critical yaw cases for injury, and with all lateral structural supports (e.g. armrests or walls) installed. Inflatable Lapbelt Special Conditions The inflatable lapbelts must meet special conditions no. 25-187A- SC, ``Boeing Model 777 Series Airplanes; Seats with Inflatable Lapbelts.'' 1. Because this type of protection system may or may not activate during various crash conditions, the applicant must demonstrate that the injury criteria listed in these special conditions are not exceeded in an event which is slightly below the activation level of the airbag system. 2. Additionally, as indicated in special conditions no. 25-187A-SC, inflatable lapbelts must be shown to not affect emergency-egress capabilities in the main aisle, cross-aisle, and passageway. Issued in Renton, Washington, on June 17, 2016. Michael Kaszycki, Assistant Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2016-15784 Filed 7-1-16; 8:45 am] BILLING CODE 4910-13-P
| 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 condition; request for comments; corrections. | |
| Dates | This action is effective on JAMCO America, Inc., on July 5, 2016. We must receive your comments August 19, 2016. | |
| Contact | John Shelden, FAA, Airframe and Cabin Safety Branch, ANM-115,Transport Airplane Directorate, Aircraft Certification Service, 1601 Lind Avenue SW., Renton, Washington 98057- 3356; telephone (425) 227-2785; facsimile (425) 227-1320. | |
| FR Citation | 81 FR 43471 |