Rules and Regulations. Final special conditions; correction

Agency: Federal Aviation Administration (FAA), DOT
Action: Final special conditions; correction
Citation: FR Doc. 2018-19215 · Docket No. FAA-2018-0335; Special Conditions No. 25-725-SC · 14 CFR 25

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.

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 § 25.143(j)(2)(i) instead of § 25.143(j)(1). There are no substantive changes to the document and it was apparent that § 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 “§ 25.143(j)(2)(i)” to read “§ 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]