Exhaust Emission Standards for New Aircraft Turbine Engines and Identification Plate for Aircraft Engines
---
identifier: "/us/fr/C1-2013-24712"
source: "fr"
legal_status: "authoritative_unofficial"
title: "Exhaust Emission Standards for New Aircraft Turbine Engines and Identification Plate for Aircraft Engines"
title_number: 0
title_name: "Federal Register"
section_number: "C1-2013-24712"
section_name: "Exhaust Emission Standards for New Aircraft Turbine Engines and Identification Plate for Aircraft Engines"
positive_law: false
currency: "2013-11-01"
last_updated: "2013-11-01"
format_version: "1.1.0"
generator: "[email protected]"
agency: "Transportation Department"
document_number: "C1-2013-24712"
document_type: "rule"
publication_date: "2013-11-01"
agencies:
- "Transportation Department"
- "Federal Aviation Administration"
cfr_references:
- "14 CFR Part 34"
- "14 CFR Part 45"
rin: "2120-AK15"
fr_citation: "78 FR 65554"
fr_volume: 78
docket_ids:
- "Docket No.: FAA-2012-1333"
- "Amendment No. 34-5A"
---
# [Corrected]
**Correction**
In rule document 2013-24712, appearing on pages 63015-63017 in the issue of Wednesday, October 23, 2013, make the following correction:
**14 CFR Part 34**
§ 34.23
On page 63017, in the Table titled “Tier 6 Oxides of Nitrogen Emission Standards for Subsonic Engines”, in the third column, in the last row, the entry “rO > 26.7” is corrected to read “rO *≥* 26.7”.