82 FR 50502 - Special Conditions: Embraer, S.A., Model ERJ 190-300 Airplane; Dive-Speed Definition With High-Speed-Protection System
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 82, Issue 210 (November 1, 2017)
Federal Aviation Administration
Federal Register Volume 82, Issue 210 (November 1, 2017)
| Page Range | 50502-50502 | |
| FR Document | 2017-23697 |
[Federal Register Volume 82, Number 210 (Wednesday, November 1, 2017)] [Rules and Regulations] [Page 50502] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2017-23697] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 25 [Docket No. FAA-2016-9403; Special Conditions No. 25-643-SC] Special Conditions: Embraer, S.A., Model ERJ 190-300 Airplane; Dive-Speed Definition With High-Speed-Protection System AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final special conditions; correction. ----------------------------------------------------------------------- SUMMARY: This document corrects an error that appeared in Docket No. FAA-2016-9403, Special Conditions No. 25-643-SC, which was published in the Federal Register on March 17, 2017 (82 FR 14117). The error is an incorrect citation of a section in a cited advisory circular. DATES: The effective date of this correction is November 1, 2017. FOR FURTHER INFORMATION CONTACT: Greg Schneider, FAA, Airframe and Cabin Safety Section, AIR-675, Transport Standards Branch, Policy and Innovation Division, Aircraft Certification Service, 1601 Lind Avenue SW., Renton, Washington, 98057-3356; telephone 425-227-2116; facsimile 425-227-1320. SUPPLEMENTARY INFORMATION: Background On March 17, 2017, the Federal Register published a document designated as Docket No. FAA-2016-9403, Final Special Conditions No. 25-643-SC (82 FR 14117). The document issued special conditions pertaining to dive-speed definition with a high-speed-protection system. As published, the document contained an error in a citation to an advisory circular section. Correction In the final special conditions document (FR Doc. 2017-05329), published on March 17, 2017 (82 FR 14117), make the following correction. On page 14119, second column, correct the last sentence in special condition no. 2 to read: The upset maneuvers described in Advisory Circular 25-7C, ``Flight Test Guide for Certification of Transport Category Airplanes,'' Chapter 2, section 8, paragraph 32, sub-paragraphs c(3)(a) and (c), may be used to comply with this requirement. Issued in Renton, Washington, on October 25, 2017. Victor Wicklund, Manager, Transport Standards Branch, Policy and Innovation Division, Aircraft Certification Service. [FR Doc. 2017-23697 Filed 10-31-17; 8:45 am] BILLING CODE 4910-13-P
![50502 Federal Register / Vol. 82, No. 210 / Wednesday, November 1, 2017 / Rules and Regulations
Should Boeing apply at a later date for as to achieve a roll rate not less than one On page 14119, second column,
a change to the type certificate to third of that obtained in condition 2, correct the last sentence in special
include another model incorporating the above. condition no. 2 to read:
same novel or unusual design feature, Issued in Renton, Washington, on October The upset maneuvers described in
these special conditions would apply to 25, 2017. Advisory Circular 25–7C, ‘‘Flight Test
that model as well. Victor Wicklund, Guide for Certification of Transport
Manager, Transport Standards Branch, Policy Category Airplanes,’’ Chapter 2, section
Conclusion
and Innovation Division, Aircraft 8, paragraph 32, sub-paragraphs c(3)(a)
This action affects only certain novel Certification Service. and (c), may be used to comply with
or unusual design features on one model [FR Doc. 2017–23701 Filed 10–31–17; 8:45 am] this requirement.
series of airplane. It is not a rule of BILLING CODE 4910–13–P Issued in Renton, Washington, on October
general applicability. 25, 2017.
List of Subjects in 14 CFR Part 25 Victor Wicklund,
DEPARTMENT OF TRANSPORTATION Manager, Transport Standards Branch, Policy
Aircraft, Aviation safety, Reporting
and Innovation Division, Aircraft
and recordkeeping requirements. Federal Aviation Administration Certification Service.
The authority citation for these [FR Doc. 2017–23697 Filed 10–31–17; 8:45 am]
special conditions is as follows: 14 CFR Part 25
BILLING CODE 4910–13–P
Authority: 49 U.S.C. 106(g), 40113, 44701, [Docket No. FAA–2016–9403; Special
44702, 44704. Conditions No. 25–643–SC]
The Special Conditions DEPARTMENT OF TRANSPORTATION
Special Conditions: Embraer, S.A.,
■ Accordingly, pursuant to the authority Model ERJ 190–300 Airplane; Dive- Federal Aviation Administration
delegated to me by the Administrator, Speed Definition With High-Speed-
the following special conditions are Protection System 14 CFR Part 71
issued as part of the type certification AGENCY: Federal Aviation
basis for Boeing Model 777–8 and 777– Administration (FAA), DOT. [Docket No. FAA–2017–0219; Airspace
9 airplanes. ACTION: Final special conditions;
Docket No. 17–AWP–5]
In lieu of compliance to 14 CFR correction.
25.349(a), the Model 777–8 and 777–9 Amendment of Class E Airspace;
airplanes must comply with the SUMMARY: This document corrects an Lemoore NAS, CA
following: error that appeared in Docket No. FAA– AGENCY: Federal Aviation
The following conditions, speeds, and 2016–9403, Special Conditions No. 25– Administration (FAA), DOT.
cockpit roll control motions (except as 643–SC, which was published in the
ACTION: Final rule, technical
the motions may be limited by pilot Federal Register on March 17, 2017 (82
effort) must be considered in FR 14117). The error is an incorrect amendment, correction.
combination with an airplane load citation of a section in a cited advisory SUMMARY: This action corrects a final
factor of zero, and of two-thirds of the circular. rule, technical amendment published in
positive maneuvering factor used in DATES: The effective date of this Federal Register on September 21, 2017,
design. In determining the resulting correction is November 1, 2017. that removes the Notice to Airmen
control-surface deflections, the torsional FOR FURTHER INFORMATION CONTACT: Greg (NOTAM) part-time status information
flexibility of the wing must be Schneider, FAA, Airframe and Cabin contained in the legal description of
considered in accordance with Safety Section, AIR–675, Transport Class E airspace designated as an
§ 25.301(b). Standards Branch, Policy and extension at Lemoore NAS (Reeves
1. Conditions corresponding to steady Innovation Division, Aircraft Field), Lemoore, CA. The airspace
rolling velocities must be investigated. Certification Service, 1601 Lind Avenue description contained the following
In addition, conditions corresponding to SW., Renton, Washington, 98057–3356; wording in error: ‘‘. . . within a 5.2-
maximum angular acceleration must be telephone 425–227–2116; facsimile mile radius of Lemoore NAS (Reeves
investigated for airplanes with engines 425–227–1320. Field), and . . . .’’ This wording is
or other weight concentrations outboard SUPPLEMENTARY INFORMATION: removed. This action does not affect the
of the fuselage. For the angular charted boundaries or operating
acceleration conditions, zero rolling Background
requirements of the airspace.
velocity may be assumed in the absence On March 17, 2017, the Federal DATES: Effective 0901 UTC, November 1,
of a rational time history investigation Register published a document
of the maneuver. 2017. The Director of the Federal
designated as Docket No. FAA–2016– Register approves this incorporation by
2. At VA, sudden movement of the 9403, Final Special Conditions No. 25–
cockpit roll control up to the limit is reference action under title 1, Code of
643–SC (82 FR 14117). The document Federal Regulations, part 51, subject to
assumed. The position of the cockpit issued special conditions pertaining to
roll control must be maintained until a the annual revision of FAA Order
dive-speed definition with a high-speed- 7400.11 and publication of conforming
steady roll rate is achieved and then protection system. As published, the
must be returned suddenly to the amendments.
document contained an error in a
sradovich on DSK3GMQ082PROD with RULES
neutral position. FOR FURTHER INFORMATION CONTACT:
citation to an advisory circular section.
3. At VC, the cockpit roll control must Robert LaPlante, Federal Aviation
be moved suddenly and maintained so Correction Administration, Operations Support
as to achieve a roll rate not less than In the final special conditions Group, Western Service Center, 1601
that obtained in condition 2, above. document (FR Doc. 2017–05329), Lind Avenue SW., Renton, WA 98057;
4. At VD, the cockpit roll control must published on March 17, 2017 (82 FR telephone (425) 203–4566.
be moved suddenly and maintained so 14117), make the following correction. SUPPLEMENTARY INFORMATION:
VerDate Sep<11>2014 17:12 Oct 31, 2017 Jkt 244001 PO 00000 Frm 00012 Fmt 4700 Sfmt 4700 E:\FR\FM\01NOR1.SGM 01NOR1](https://thefederalregister.org/doc/82_FR_50712/page/1.svg)
Document Created: 2017-11-01 02:02:44
Document Modified: 2017-11-01 02:02:44
| 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 | The effective date of this correction is November 1, 2017. | |
| Contact | Greg Schneider, FAA, Airframe and Cabin Safety Section, AIR-675, Transport Standards Branch, Policy and Innovation Division, Aircraft Certification Service, 1601 Lind Avenue SW., Renton, Washington, 98057-3356; telephone 425-227-2116; facsimile 425-227-1320. | |
| FR Citation | 82 FR 50502 |
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