Federal Register / Vol. 80, No. 79 / Friday, April 24, 2015 / Proposed Rules 22939 

DEPARTMENT OF ENERGY 

10 CFR Parts 429 and 431 

[Docket No. EERE–2013–BT–TP–0055] 

RIN 1905–AD50 

Energy Conservation Program: Test 

Procedure for Pumps; Correction 

AGENCY: Office of Energy Efficiency and 

Renewable Energy, Department of 

Energy. 

ACTION: Notice of proposed rulemaking 

and public meeting; correction. 

SUMMARY: On April 1, 2015, the U.S. 

Department of Energy (DOE) published 

in the Federal Register a notice of 

proposed rulemaking and public 

meeting for Energy Conservation 

Program: Test Procedure for Pumps. 

This document corrects terms in four 

equations. 

DATES: April 24, 2015. 

FOR FURTHER INFORMATION CONTACT: 

Ashley Armstrong, U.S. Department of 

Energy, Office of Energy Efficiency and 

Renewable Energy, Building 

Technologies Office, EE–5B, 1000 

Independence Avenue SW., 

Washington, DC 20585–0121. 

Telephone: (202) 586–6590. Email: 

ashley.armstrong@ee.doe.gov. 

Corrections 

In the Federal Register published on 

April 1, 2015, in FR Doc. 2015–06945, 

make the following corrections: 

1. On page 17604: Equation (6) is 

corrected by removing ‘‘13.46’’ and 

adding in its place ‘‘17.80’’. The 

corrected equation reads as follows: 

Appendix A to Subpart Y of Part 431— 

Uniform Test Method for the 

Measurement of Energy Consumption of 

Pumps. [Corrected] 

2. On page 17645: The equation in 

section II.B.1.1.1 is corrected by 

removing ‘‘13.46’’ and adding in its 

place ‘‘17.80’’. The corrected equation 

reads as follows: 

hpump,STD = ¥0.85 * In(Q100%)2 ¥ 0.38 * 

In(NS) * In(Q100%) ¥ 11.48 * In(NS)2

+ 17.80 * In(Q100%) + 179.80 * 

In(NS) ¥ (C ¥ 555.6) 

3. On page 17646: The equation in 

section III.D.1.2.1 is corrected by 

removing ‘‘MotorH’’ and adding in its 

place ‘‘MotorHP’’. The corrected 

equation reads as follows: 

4. On page 17648: The equation in 

section V.D.1.2.1 is corrected by 

removing ‘‘MotorHPMotorH’’ and 

adding in its place ‘‘MotorHP’’. The 

corrected equation reads as follows: 

Issued in Washington, DC, on April 20, 

2015. 

Kathleen B. Hogan, 

Deputy Assistant Secretary for Energy 

Efficiency, Energy Efficiency and Renewable 

Energy. 

[FR Doc. 2015–09566 Filed 4–23–15; 8:45 am] 

BILLING CODE 6450–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–0831; Directorate 

Identifier 2014–NM–061–AD] 

RIN 2120–AA64 

Airworthiness Directives; Airbus 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: We propose to adopt a new 

airworthiness directive (AD) for all 

Airbus Model A318, A319, A320, and 

A321 series airplanes. This proposed 

AD was prompted by a report of a 

rupture of a main landing gear (MLG) 

sliding tube axle. This proposed AD 

would require an inspection to identify 

the part number and serial number of 

the MLG sliding tubes installed on the 

airplane; and an inspection of the axle 

on certain MLG sliding tubes for burned 

areas, and replacement of the sliding 

tube if necessary. We are proposing this 

AD to detect and correct cracks in the 

axle and (partial) detachment of the axle 

and wheel from the sliding tube, which 

could result in failure of an MLG. 


tkelley on DSK3SPTVN1PROD with PROPOSALSEP24AP15.017</GPH> EP24AP15.001</GPH> EP24AP15.002</GPH>