77 FR 211 pgs. 65823-65824 - Control of Air Pollution From Aircraft and Aircraft Engines; Emission Standards and Test Procedures

Type: RULEVolume: 77Number: 211Pages: 65823 - 65824
Docket number: [EPA-HQ-OAR-2010-0687; FRL-9678-1]
FR document: [FR Doc. C1-2012-13828 Filed 10-30-12; 8:45 am]
Agency: Environmental Protection Agency
Official PDF Version:  PDF Version

ENVIRONMENTAL PROTECTION AGENCY

40 CFR Parts 87

[EPA-HQ-OAR-2010-0687; FRL-9678-1]

RIN 2060-AO70

Control of Air Pollution From Aircraft and Aircraft Engines; Emission Standards and Test Procedures

Correction

In rule document 2012-13828 appearing on pages 36341-36386 in the issue of Monday, June 18, 2012, make the following corrections:

§ 87.23 [Corrected]

1. On page 36382, in § 87.23, the table titled "Table 3 to § 87.23-Tier 6 NO X Standards for New Subsonic Turbofan or Turbojet Engines with Rated Output Above 26.7 kN" should read as set forth below:

If the rated pressure ratio is- and the rated output (in kN) is- The NO X emission standard (in g/kN rated output) is-
rPR = 30 26.7 < rO = 89 38.5486 + 1.6823·rPR - 0.2453·rO - 0.00308·rPR·rO
rO > 89 16.72 + 1.4080·rPR
30 < rPR < 82.6 26.7 < rO = 89 46.1600 + 1.4286·rPR - 0.5303·rO + 0.00642·rPR·rO
rO > 89 -1.04 + 2.0·rPR
rPR = 82.6 all 32 + 1.6·rPR

2. On page 36383, in § 87.23, the table titled "Table 4 to § 87.23-Tier 8 NO X Standards for New Subsonic Turbofan or Turbojet Engines with Rated Output Above 26.7 kN" should read as set forth below:

If the rated pressure ratio is- and the rated output (in kN) is- The NO X emission standard (in g/kN rated output) is-
rPR = 30 26.7 < rO = 89 40.052 + 1.5681·rPR - 0.3615·rO - 0.0018·rPR·rO
rO > 89 7.88 + 1.4080·rPR
30 < rPR < 104.7 26.7 < rO = 89 41.9435 + 1.505·rPR - 0.5823·rO + 0.005562·rPR·rO
rO > 89 -9.88 + 2.0·rPR
rPR = 104.7 all 32 + 1.6·rPR

[FR Doc. C1-2012-13828 Filed 10-30-12; 8:45 am]

BILLING CODE 1505-01-D