83 FR 45037 - Special Conditions: Bombardier Inc., Model BD-700-2A12 and BD-700-2A13 Series Airplanes; Flight Envelope Protection: High Incidence Protection System
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 83, Issue 172 (September 5, 2018)
Federal Aviation Administration
Federal Register Volume 83, Issue 172 (September 5, 2018)
| Page Range | 45037-45037 | |
| FR Document | 2018-19215 |
[Federal Register Volume 83, Number 172 (Wednesday, September 5, 2018)] [Rules and Regulations] [Page 45037] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2018-19215] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 25 [Docket No. FAA-2018-0335; Special Conditions No. 25-725-SC] Special Conditions: Bombardier Inc., Model BD-700-2A12 and BD- 700-2A13 Series Airplanes; Flight Envelope Protection: High Incidence Protection System AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final special conditions; correction. ----------------------------------------------------------------------- SUMMARY: The FAA is correcting an error that appeared in the Federal Register on May 1, 2018, for special conditions No. 25-725-SC, Docket No. FAA-2018-0335. As published, there was an error in the citation and the correct citation has been added. DATES: Effective on Bombardier on September 5, 2018. FOR FURTHER INFORMATION CONTACT: Joe Jacobsen, Airplane and Flight Crew Interface, AIR-671, Transport Standards Branch, Policy and Innovation Division, Aircraft Certification Service, Federal Aviation Administration, 2200 South 216th Street, Des Moines, Washington 98198; telephone and fax 206-231-3158; email [email protected]. SUPPLEMENTARY INFORMATION: Background On April 25, 2018, the FAA issued Special Conditions No. 25-725-SC, Docket No. FAA-2018-0335, which was published in the Federal Register on May 1, 2018 (83 FR 18934). Those special conditions pertain to the high incidence protection system that replaces the stall warning system during normal operating conditions, prohibits the airplane from stalling, limits the angle of attack at which the airplane can be flown during normal low speed operation, and cannot be overridden by the flight crew for Bombardier Model BD-700-2A12 and BD-700-2A13 series airplanes. As published, part II, paragraph 7 of the final special conditions cited Sec. 25.143(j)(2)(i) instead of Sec. 25.143(j)(1). There are no substantive changes to the document and it was apparent that Sec. 25.143(j)(1) should have been referenced from the beginning. Correction In the final special conditions document FR Doc. 2018-09126 (Filed 4-30-2018; 8:45 a.m.), published on May 1, 2018 (83 FR 18934), make the following correction: On page 18938, column 2, under part II, paragraph 7, correct ``Sec. 25.143(j)(2)(i)'' to read ``Sec. 25.143(j)(1)''. Issued in Des Moines, Washington, on August 27, 2018. Victor Wicklund, Manager, Transport Standards Branch, Policy and Innovation Division, Aircraft Certification Service. [FR Doc. 2018-19215 Filed 9-4-18; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 83, No. 172 / Wednesday, September 5, 2018 / Rules and Regulations 45037
instrumentation specified in 49 CFR DEPARTMENT OF TRANSPORTATION May 1, 2018 (83 FR 18934), make the
part 572, subpart E filtered in following correction:
accordance with SAE International Federal Aviation Administration On page 18938, column 2, under part
(SAE) recommended practice J211/1, II, paragraph 7, correct
‘‘Instrumentation for Impact Test—Part 14 CFR Part 25 ‘‘§ 25.143(j)(2)(i)’’ to read
1—Electronic Instrumentation.’’ ‘‘§ 25.143(j)(1)’’.
[Docket No. FAA–2018–0335; Special
c. The occupant must not interact Conditions No. 25–725–SC] Issued in Des Moines, Washington, on
August 27, 2018.
with the armrest or other seat
components in any manner significantly Special Conditions: Bombardier Inc., Victor Wicklund,
different than would be expected for a Model BD–700–2A12 and BD–700– Manager, Transport Standards Branch, Policy
forward-facing seat installation. 2A13 Series Airplanes; Flight Envelope and Innovation Division, Aircraft
Protection: High Incidence Protection Certification Service.
5. Pelvis Criteria: System [FR Doc. 2018–19215 Filed 9–4–18; 8:45 am]
Any part of the load-bearing portion BILLING CODE 4910–13–P
AGENCY: Federal Aviation
of the bottom of the ATD pelvis must
Administration (FAA), DOT.
not translate beyond the edges of the
seat bottom seat-cushion supporting ACTION: Final special conditions; DEPARTMENT OF TRANSPORTATION
structure. correction.
Federal Aviation Administration
6. Femur Criteria: SUMMARY: The FAA is correcting an
Axial rotation of the upper leg (about error that appeared in the Federal 14 CFR Part 39
the z-axis of the femur per SAE Register on May 1, 2018, for special
conditions No. 25–725–SC, Docket No. [Docket No. FAA–2018–0163; Product
Recommended Practice J211/1) must be Identifier 2017–NM–168–AD; Amendment
limited to 35 degrees from the nominal FAA–2018–0335. As published, there 39–19386; AD 2018–18–07]
was an error in the citation and the
seated position. Evaluation during RIN 2120–AA64
correct citation has been added.
rebound does not need to be considered.
DATES: Effective on Bombardier on
7. ATD and Test Conditions: Airworthiness Directives; The Boeing
September 5, 2018. Company Airplanes
Longitudinal tests conducted to FOR FURTHER INFORMATION CONTACT: Joe
measure the injury criteria above must Jacobsen, Airplane and Flight Crew AGENCY: Federal Aviation
be performed with the FAA Hybrid III Interface, AIR–671, Transport Standards Administration (FAA), DOT.
ATD, as described in SAE 1999–01– Branch, Policy and Innovation Division, ACTION: Final rule.
1609, ‘‘A Lumbar Spine Modification to Aircraft Certification Service, Federal
the Hybrid III ATD for Aircraft Seat Aviation Administration, 2200 South SUMMARY: We are adopting a new
Tests.’’ The tests must be conducted 216th Street, Des Moines, Washington airworthiness directive (AD) for certain
98198; telephone and fax 206–231– The Boeing Company Model 757
with an undeformed floor, at the most-
3158; email Joe.Jacobsen@faa.gov. airplanes. This AD was prompted by an
critical yaw cases for injury and with all
evaluation by the design approval
lateral structural supports (e.g. armrests SUPPLEMENTARY INFORMATION:
holder (DAH) indicating that the
or walls) installed. longitudinal lap splices of the fuselage
Background
Note: Boeing must demonstrate that skin are subject to widespread fatigue
the installation of seats via plinths or On April 25, 2018, the FAA issued
damage (WFD). This AD requires
Special Conditions No. 25–725–SC,
pallets meets all applicable repetitive inspections of the
Docket No. FAA–2018–0335, which was
requirements. Compliance with the longitudinal lap splices of the fuselage
published in the Federal Register on
guidance contained in policy skin for cracking and protruding
May 1, 2018 (83 FR 18934). Those
memorandum PS–ANM–100–2000– fasteners, and applicable corrective
special conditions pertain to the high
00123, ‘‘Guidance for Demonstrating actions. We are issuing this AD to
incidence protection system that
Compliance with Seat Dynamic Testing address the unsafe condition on these
replaces the stall warning system during
for Plinths and Pallets,’’ dated February products.
normal operating conditions, prohibits
2, 2000, is acceptable to the FAA. the airplane from stalling, limits the DATES: This AD is effective October 10,
8. Inflatable Airbag Restraint Systems angle of attack at which the airplane can 2018.
Special Conditions: be flown during normal low speed The Director of the Federal Register
operation, and cannot be overridden by approved the incorporation by reference
If inflatable airbag restraint systems of a certain publication listed in this AD
the flight crew for Bombardier Model
are installed, the airbag systems must as of October 10, 2018.
BD–700–2A12 and BD–700–2A13 series
meet the requirements in one of the ADDRESSES: For service information
airplanes. As published, part II,
airbag (inflatable restraint) special paragraph 7 of the final special identified in this final rule, contact
conditions applicable to the Boeing conditions cited § 25.143(j)(2)(i) instead Boeing Commercial Airplanes,
Model 747–8 airplane. of § 25.143(j)(1). There are no Attention: Contractual & Data Services
Issued in Des Moines, Washington, on substantive changes to the document (C&DS), 2600 Westminster Blvd., MC
August 22, 2018. and it was apparent that § 25.143(j)(1) 110–SK57, Seal Beach, CA 90740–5600;
telephone 562–797–1717; internet
daltland on DSKBBV9HB2PROD with RULES
Victor Wicklund, should have been referenced from the
Manager, Transport Standards Branch, Policy beginning. https://www.myboeingfleet.com. You
and Innovation Division, Aircraft may view this service information at the
Correction FAA, Transport Standards Branch, 2200
Certification Service.
[FR Doc. 2018–19216 Filed 9–4–18; 8:45 am]
In the final special conditions South 216th St., Des Moines, WA. For
document FR Doc. 2018–09126 (Filed information on the availability of this
BILLING CODE 4910–13–P
4–30–2018; 8:45 a.m.), published on material at the FAA, call 206–231–3195.
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Document Created: 2018-09-05 01:58:58
Document Modified: 2018-09-05 01:58:58
| 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; correction. | |
| Dates | Effective on Bombardier on September 5, 2018. | |
| Contact | Joe Jacobsen, Airplane and Flight Crew Interface, AIR-671, Transport Standards Branch, Policy and Innovation Division, Aircraft Certification Service, Federal Aviation Administration, 2200 South 216th Street, Des Moines, Washington 98198; telephone and fax 206-231-3158; email [email protected] | |
| FR Citation | 83 FR 45037 |
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