5162 Federal Register / Vol. 71, No. 21 / Wednesday, February 1, 2006 / Rules and Regulations 

TABLE 3.—REQUIRED ACTIONS—Continued 

For— Required actions 

(3) Model Falcon 2000EX airplanes, serial number 6 and 28 through 64 

inclusive.

Drill holes in the cockpit protector located between the headline and 

the skin, and clamp the feeder cables coming from the essential, A1, 

and A2 buses. 

(4) All Model Falcon 2000 airplanes and for Model Falcon 2000EX airplanes, serial numbers 1 through 5 inclusive and 7 through 27 inclusive.Re-route the wiring on the cockpit protector, and bond the applicable 

supports with epoxy resin. 

(5) All airplanes ........................................................................................ Install a protective plate on the feeder cables. 

Note 1: For the purposes of this AD, a 

general visual inspection is: ‘‘A visual 

examination of an interior or exterior area, 

installation, or assembly to detect obvious 

damage, failure, or irregularity. This level of 

inspection is made from within touching 

distance unless otherwise specified. A mirror 

may be necessary to ensure visual access to 

all surfaces in the inspection area. This level 

of inspection is made under normally 

available lighting conditions such as 

daylight, hangar lighting, flashlight, or 

droplight and may require removal or 

opening of access panels or doors. Stands, 

ladders, or platforms may be required to gain 

proximity to the area being checked.’’

Corrective Actions 

(h) If any damaged feeder cable is detected 

during the inspection required by paragraph 

(g)(2) of this AD, before further flight, do the 

applicable corrective actions in accordance 

with the service bulletin. 

No Reporting 

(i) Although the service bulletins 

referenced in this AD specifies to submit 

certain information to the manufacturer, this 

AD does not include that requirement. 

Alternative Methods of Compliance 

(AMOCs) 

(j)(1) The Manager, International Branch, 

ANM–116, Transport Airplane Directorate, 

FAA, has the authority to approve AMOCs 

for this AD, if requested in accordance with 

the procedures found in 14 CFR 39.19. 

(2) Before using any AMOC approved in 

accordance with § 39.19 on any airplane to 

which the AMOC applies, notify the 

appropriate principal inspector in the FAA 

Flight Standards Certificate Holding District 

Office. 

Related Information 

(k) The European Aviation Safety Agency’s 

emergency airworthiness directive 2006–

0003, dated January 5, 2006, also addresses 

the subject of this AD. 

Material Incorporated by Reference 

(l) You must use the applicable service 

bulletin in Table 4 of this AD to perform the 

actions that are required by this AD, unless 

the AD specifies otherwise. The Director of 

the Federal Register approved the 

incorporation by reference of these 

documents in accordance with 5 U.S.C. 

552(a) and 1 CFR part 51. Contact Dassault 

Falcon Jet, P.O. Box 2000, South Hackensack, 

New Jersey 07606, for a copy of this service 

information. You may review copies at the 

Docket Management Facility, U.S. 

Department of Transportation, 400 Seventh 

Street SW., Room PL–401, Nassif Building, 

Washington, DC; on the Internet at http:// 

dms.dot.gov; or at the National Archives and 

Records Administration (NARA). For 

information on the availability of this 

material at the NARA, call (202) 741–6030, 

or go to http://www.archives.gov/ 

federal_register/code_of_federal_regulations/

ibr_locations.html. 

TABLE 4.—MATERIAL INCORPORATED

BY REFERENCE

Dassault service bulletin— Dated—

(1) F2000–332 .......... December 22, 2005. 

(2) F2000EX–92 ........ December 22, 2005. 

Issued in Renton, Washington, on January 

23, 2006. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 06–824 Filed 1–31–06; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2005–23031; Directorate 

Identifier 2005–NE–41–AD; Amendment 39–

14467; AD 2006–03–03] 

RIN 2120–AA64 

Airworthiness Directives; Rolls-Royce 

plc RB211 Trent 553–61, 553A2–61, 

556–61, 556A2–61, 556B–61, 556B2–61, 

560–61, and 560A2–61 Turbofan 

Engines 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule; request for 

comments. 

SUMMARY: The FAA is adopting a new 

airworthiness directive (AD) for certain 

Rolls-Royce plc (RR) RB211 Trent 553–

61, 553A2–61, 556–61, 556A2–61, 

556B–61, 556B2–61, 560–61, and 

560A2–61 turbofan engines. This AD 

requires initial and repetitive borescope 

inspections for missing HPT rear seal 

plate locking plugs and damaged 

locking plug retaining wires, and 

removal of the engine from service if 

necessary, based on inspection results. 

This AD results from two reports of 

missing HPT rear seal plate locking 

plugs, damage to the HPT disc, and 

damage to the remaining locking plug 

retaining wires. We are issuing this AD 

to prevent uncontained release of the 

HPT rear side plate and HPT disc, 

resulting in damage to the airplane. 

DATES: Effective February 16, 2006. The 

Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in the 

regulations as of February 16, 2006. 

We must receive any comments on 

this AD by April 3, 2006. 

ADDRESSES: Use one of the following 

addresses to comment on this AD: 

• DOT Docket Web site: Go to 

http://dms.dot.gov and follow the 

instructions for sending your comments 

electronically. 

• Government-wide rulemaking Web 

site: Go to http://www.regulations.gov 

and follow the instructions for sending 

your comments electronically. 

• Mail: Docket Management Facility; 

U.S. Department of Transportation, 400 

Seventh Street, SW., Nassif Building, 

Room PL–401, Washington, DC 20590–

0001. 

• Fax: (202) 493–2251. 

• Hand Delivery: Room PL–401 on 

the plaza level of the Nassif Building, 

400 Seventh Street, SW., Washington, 

DC, between 9 a.m. and 5 p.m., Monday 

through Friday, except Federal holidays. 

Contact Rolls-Royce plc, P.O. Box 31, 

Derby, DE248BJ; UK, telephone: 011–

44–1332–242424; fax: 011–44–1332–

249936, for the service information 

identified in this AD. 

FOR FURTHER INFORMATION CONTACT: 

Christopher Spinney, Aerospace 

Engineer, Engine Certification Office, 

FAA, Engine and Propeller Directorate, 

12 New England Executive Park; 

telephone (781) 238–7175; fax (781) 

238–7199. 

SUPPLEMENTARY INFORMATION: The Civil 

Aviation Authority (CAA), which is the 


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Federal Register / Vol. 71, No. 21 / Wednesday, February 1, 2006 / Rules and Regulations 5163 

airworthiness authority for the United 

Kingdom (U.K.), notified us that an 

unsafe condition may exist on RR 

RB211 Trent 500 series turbofan engines 

that have not incorporated RR Service 

Bulletin (SB) No. RB.211–72–E767. The 

CAA advises that during shop visit, 

some engines were noticed to be 

missing some of the HPT turbine rear 

seal plate locking plugs. This resulted in 

scoring of the HPT disc rear diaphragm 

and impact damage to the remaining 

locking plug retaining wires, and could 

have led to release of the HPT rear seal 

plate and reduced low-cycle-fatigue life 

of the HPT disc. 

Relevant Service Information 

We have reviewed and approved the 

technical contents of RR Alert SB No. 

RB.211–72–AE358, Revision 3, dated 

July 13, 2005, that describes procedures 

for borescope inspecting the HPT rear 

seal plate locking plugs and locking 

plug retaining wires. The CAA classified 

this as a mandatory SB and issued AD 

G–2005–0007 R1, dated July 11, 2005, in 

order to ensure the airworthiness of 

these RB211 Trent 500 series turbofan 

engines in the U.K. 

Bilateral Airworthiness Agreement 

These RB211 Trent 553–61, 553A2–

61, 556–61, 556A2–61, 556B–61, 

556B2–61, 560–61, and 560A2–61 series 

turbofan engines are manufactured in 

the U.K. and are type certificated for 

operation in the United States under the 

provisions of section 21.29 of the 

Federal Aviation Regulations (14 CFR 

21.29) and the applicable bilateral 

airworthiness agreement. Under this 

bilateral airworthiness agreement, the 

CAA kept the FAA informed of the 

situation described above. We have 

examined the findings of the CAA, 

reviewed all available information, and 

determined that AD action is necessary 

for products of this type design that are 

certificated for operation in the United 

States. 

FAA’s Determination and Requirements 

of This AD 

Although no airplanes that are 

registered in the United States use these 

engines, the possibility exists that the 

engines could be used on airplanes that 

are registered in the United States in the 

future. The unsafe condition described 

previously is likely to exist or develop 

on other RR RB211 Trent 500 series 

turbofan engines of the same type 

design. We are issuing this AD to 

prevent uncontained release of the HPT 

rear side plate and HPT disc, resulting 

in damage to the airplane. This AD 

requires initial and repetitive borescope 

inspections for missing HPT rear seal 

plate locking plugs and damaged 

locking plug retaining wires. This AD 

also requires removing engines from 

service based on the number of HPT 

locking plugs with acceptable locking 

plug retaining wires installed. You must 

use the service information described 

previously to perform the actions 

required by this AD. 

FAA’s Determination of the Effective 

Date 

Since there are currently no domestic 

operators of this engine model, notice 

and opportunity for public comment 

before issuing this AD are unnecessary. 

A situation exists that allows the 

immediate adoption of this regulation. 

Comments Invited 

This AD is a final rule that involves 

requirements affecting flight safety and 

was not preceded by notice and an 

opportunity for public comment; 

however, we invite you to send us any 

written relevant data, views, or 

arguments regarding this AD. Send your 

comments to an address listed under 

ADDRESSES. Include ‘‘AD Docket No. 

FAA–2005–23031; Directorate Identifier 

2005–NE–41–AD’’ in the subject line of 

your comments. We specifically invite 

comments on the overall regulatory, 

economic, environmental, and energy 

aspects of the rule that might suggest a 

need to modify it. 

We will post all comments we 

receive, without change, to http:// 

dms.dot.gov, including any personal 

information you provide. We will also 

post a report summarizing each 

substantive verbal contact with FAA 

personnel concerning this AD. Using the 

search function of the DMS Web site, 

anyone can find and read the comments 

in any of our dockets, including the 

name of the individual who sent the 

comment (or signed the comment on 

behalf of an association, business, labor 

union, etc.). You may review the DOT’s 

complete Privacy Act Statement in the 

Federal Register published on April 11, 

2000 (65 FR 19477–78) or you may visit 

http://dms.dot.gov. 

Examining the AD Docket 

You may examine the docket that 

contains the AD, any comments 

received, and any final disposition in 

person at the Docket Management 

Facility Docket Office between 9 a.m. 

and 5 p.m., Monday through Friday, 

except Federal holidays. The Docket 

Office (telephone (800) 647–5227) is 

located on the plaza level of the 

Department of Transportation Nassif 

Building at the street address stated in 

ADDRESSES. Comments will be available 

in the AD docket shortly after the DMS 

receives them. 

Authority for This Rulemaking 

Title 49 of the United States Code 

specifies the FAA’s authority to issue 

rules on aviation safety. Subtitle I, 

section 106, describes the authority of 

the FAA Administrator. Subtitle VII, 

Aviation Programs, describes in more 

detail the scope of the Agency’s 

authority. 

We are issuing this rulemaking under 

the authority described in subtitle VII, 

part A, subpart III, section 44701, 

‘‘General requirements.’’ Under that 

section, Congress charges the FAA with 

promoting safe flight of civil aircraft in 

air commerce by prescribing regulations 

for practices, methods, and procedures 

the Administrator finds necessary for 

safety in air commerce. This regulation 

is within the scope of that authority 

because it addresses an unsafe condition 

that is likely to exist or develop on 

products identified in this rulemaking 

action. 

Regulatory Findings 

We have determined that this AD will 

not have federalism implications under 

Executive Order 13132. This AD will 

not have a substantial direct effect on 

the States, on the relationship between 

the National Government and the States, 

or on the distribution of power and 

responsibilities among the various 

levels of government. 

For the reasons discussed above, I 

certify that the regulation: 

1. Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866; 

2. Is not a ‘‘significant rule’’ under the 

DOT Regulatory Policies and Procedures 

(44 FR 11034, February 26, 1979); and 

3. Will not have a significant 

economic impact, positive or negative, 

on a substantial number of small entities 

under the criteria of the Regulatory 

Flexibility Act. 

We prepared a summary of the costs 

to comply with this AD and placed it in 

the AD Docket. You may get a copy of 

this summary by sending a request to us 

at the address listed under ADDRESSES. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

Adoption of the Amendment 

■ Under the authority delegated to me 

by the Administrator, the Federal 

Aviation Administration amends part 39 

of the Federal Aviation Regulations (14 

CFR part 39) as follows: 


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5164 Federal Register / Vol. 71, No. 21 / Wednesday, February 1, 2006 / Rules and Regulations 

PART 39—AIRWORTHINESS 

DIRECTIVES 

■ 1. The authority citation for part 39 

continues to read as follows: 

Authority: 49 U.S.C. 106(g), 40113, 44701. 

§ 39.13 [Amended] 

■ 2. The FAA amends § 39.13 by adding 

the following new airworthiness 

directive: 

2006–03–03 Rolls-Royce plc: Amendment 

39–14467. Docket No. FAA–2005–23031; 

Directorate Identifier 2005–NE–41–AD. 

Effective Date 

(a) This airworthiness directive (AD) 

becomes effective February 16, 2006. 

Affected ADs 

(b) None. 

Applicability 

(c) This AD applies to Rolls-Royce plc (RR) 

RB211 Trent 553–61, 553A2–61, 556–61, 

556A2–61, 556B–61, 556B2–61, 560–61, and 

560A2–61 turbofan engines that have not 

incorporated RR Service Bulletin (SB) No. 

RB.211–72–E767. These engines are installed 

on, but not limited to, Airbus A340–500 and 

–600 series airplanes. 

Unsafe Condition 

(d) This AD results from two reports of 

missing HPT rear seal plate locking plugs, 

damage to the HPT disc, and damage to the 

remaining locking plug retaining wires. We 

are issuing this AD to prevent uncontained 

release of the HPT rear side plate and HPT 

disc, resulting in damage to the airplane. 

Compliance 

(e) You are responsible for having the 

actions required by this AD performed within 

the compliance times specified unless the 

actions have already been done. 

Initial Borescope Inspection 

(f) Borescope-inspect for missing HPT rear 

seal plate locking plugs and damaged locking 

plug retaining wires, between 500 and 1,000 

cycles-since-new (CSN) or cycles-sinceoverhaul where the locking plug wires were 

replaced, or within 50 cycles after the 

effective date of this AD, whichever occurs 

later. 

(g) Use paragraphs 3.B.(1)(a) through 

3.B.(1)(k)(xi) of the Accomplishment 

Instructions of RR Alert Service Bulletin No. 

RB.211–72–AE358, Revision 3, dated July 13, 

2005, to do the inspection. 

Repetitive Borescope Inspections 

(h) Using the criteria and intervals in the 

following Table 1, repeat the borescope 

inspection and remove engines from service 

to inspect the HPT disc. 

TABLE 1.—ENGINE REMOVAL CRITERIA

If the number of HPT locking plugs with acceptable locking plug retaining wires installed, determined in paragraph (f) of this AD is: 

Then repeat the borescope inspection within: Remove the engine from service to inspect 

HPT disc: 

(1) Zero or one. .................................................. Not applicable .................................................. Before further flight. 

(2) Two ............................................................... Not applicable .................................................. Within 15 CSLI. 

(3) Three or four ................................................ 100 cycles-since-last-inspection (CSLI) intervals.Before accumulating 1,100 cycles-since-loss 

of locking plug(s) or 1,100 CSN, or 1,100 

cycles-since-last acceptable inspection, 

whichever occurs later. 

(4) Five ............................................................... 1,000 CSLI intervals ......................................... Not applicable. 

(i) Use paragraphs 3.B.(1)(a) through 

3.B.(1)(k)(xi) of the Accomplishment 

Instructions of RR Alert Service Bulletin No. 

RB.211–72–AE358, Revision 3, dated July 13, 

2005, to do the inspection. 

(j) For Table 1, item (3), if possible, 

determine when the loss of locking plug(s) 

occurred by reviewing the engine vibration 

history. If it is not possible to determine the 

point of locking plug release, use 1,100 CSN, 

or 1,100 cycles-since-last acceptable 

inspection, whichever occurs later. 

Alternative Methods of Compliance 

(k) The Manager, Engine Certification 

Office, has the authority to approve 

alternative methods of compliance for this 

AD if requested using the procedures found 

in 14 CFR 39.19. 

Related Information 

(l) United Kingdom Civil Aviation 

Authority airworthiness directive G–2005–

0007 R1, dated July 11, 2005, also addresses 

the subject of this AD. 

Material Incorporated by Reference 

(m) You must use the Rolls-Royce plc Alert 

Service Bulletin and Appendices listed in 

Table 2 of this AD to perform the inspections 

required by this AD. The Director of the 

Federal Register approved the incorporation 

by reference of this service bulletin in 

accordance with 5 U.S.C. 552(a) and 1 CFR 

part 51. Contact Rolls-Royce plc, P.O. Box 31, 

Derby, DE248BJ; UK, telephone: 011–44–

1332–242424; fax: 011–44–1332–249936, for 

a copy of this service information. You may 

review copies at the Docket Management 

Facility; U.S. Department of Transportation, 

400 Seventh Street, SW., Nassif Building, 

Room PL–401, Washington, DC 20590–0001, 

on the Internet at http://dms.dot.gov; or at the 

National Archives and Records 

Administration (NARA). For information on 

the availability of this material at NARA, call 

202–741–6030, or go to: http:// 

www.archives.gov/federal-register/cfr/ibrlocations.html. 

TABLE 2.—INCORPORATION BY REFERENCE

Alert Service Bulletin No. Page Revision Date 

RB.211–72–AE358 ................................................................................................................................. ALL ........ 3 July 13, 2005. 

Total Pages: 16 

Appendix 1 to ASB No. RB.211–72–AE358 .......................................................................................... ALL ........ 3 July 13, 2005. 

Total Pages: 2 

Appendix 2 to ASB No. RB.211–72–AE358 .......................................................................................... ALL ........ 3 July 13, 2005. 

Total Pages: 2 


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Federal Register / Vol. 71, No. 21 / Wednesday, February 1, 2006 / Rules and Regulations 5165 

Issued in Burlington, Massachusetts, on 

January 24, 2006. 

Peter A. White, 

Acting Manager, Engine and Propeller 

Directorate, Aircraft Certification Service. 

[FR Doc. 06–826 Filed 1–31–06; 8:45 am] 

BILLING CODE 4910–13–P 

CONSUMER PRODUCT SAFETY 

COMMISSION 

16 CFR Part 1000 

Statement of Organization and 

Functions 

AGENCY: Consumer Product Safety 

Commission. 

ACTION: Final rule. 

SUMMARY: The Consumer Product Safety 

Commission (CPSC or Commission) is 

amending its statement of organization 

and functions to reflect changes in the 

Commission’s organization as well as 

editorial and address changes. 

DATES: Effective Date: February 1, 2006. 

ADDRESSES: Office of the Secretary, 

Consumer Product Safety Commission, 

4330 East West Highway, Bethesda, 

Maryland 20814. 

FOR FURTHER INFORMATION CONTACT: 

Hyun Sun Kim, Office of the General 

Counsel, Consumer Product Safety 

Commission, 4330 East West Highway, 

Bethesda, Maryland 20814; telephone 

(301) 504–7632. 

SUPPLEMENTARY INFORMATION: Section 

1000.19 describes the new Office of 

Financial Management, Planning and 

Evaluation. Section 1000.21 describes 

the new Office of Compliance and Field 

Operations. Section 1000.23 describes 

the new Office of Information and 

Technology Services. Section 1000.24 

describes the new Office of International 

Programs and Intergovernmental Affairs. 

The following offices and directorates 

have been incorporated into the new 

offices referenced above: the Office of 

the Secretary, the Office of the Budget, 

the Office of Planning and Evaluation, 

the Office of Compliance, the Office of 

Information Services, the Directorate for 

Administration and the Directorate for 

Field Operations. 

Section 1000.10 provides that the 

Commission will annually elect a vice 

chairman for a term beginning on June 

1 and running until such time as 

another vice chairman is elected. 

Editorial changes have also been made 

in various sections and the address of 

the Commission has been changed from 

‘‘Washington, DC 20207’’ to ‘‘4330 East 

West Highway, Bethesda, Maryland 

20814’’ to reflect the current address. 

Since this rule relates solely to 

internal agency management, pursuant 

to 5 U.S.C. 553(b), notice and other 

public procedures are not required and 

it is effective immediately upon 

publication in the Federal Register. 

Further this action is not a rule as 

defined in the Regulatory Flexibility 

Act, 5 U.S.C. 601–612, and thus, is 

exempt from the provisions of the Act. 

List of Subjects in 16 CFR Part 1000 

Organization and Functions 

(Government Agencies). 

■ Therefore, for the reasons set forth in 

the preamble, revise 16 CFR part 1000 

to read as follows: 

PART 1000—COMMISSION 

ORGANIZATION AND FUNCTIONS 

Sec. 

1000.1 The Commission. 

1000.2 Laws administered. 

1000.3 Hotline. 

1000.4 Commission address. 

1000.5 Petitions. 

1000.6 Commission decisions and records. 

1000.7 Advisory opinions and 

interpretations of regulations. 

1000.8 Meetings and hearings; public 

notice. 

1000.9 Quorum. 

1000.10 The Chairman and Vice Chairman. 

1000.11 Delegation of functions. 

1000.12 Organizational structure. 

1000.13 Directives system. 

1000.14 Office of the General Counsel. 

1000.15 Office of Congressional Relations. 

1000.16 Office of the Inspector General. 

1000.17 Office of Equal Employment 

Opportunity and Minority Enterprise. 

1000.18 Office of Executive Director. 

1000.19 Office of Financial Management, 

Planning and Evaluation. 

1000.20 Office of Information and Public 

Affairs. 

1000.21 Office of Compliance and Field 

Operations. 

1000.22 Office of Human Resources 

Management. 

1000.23 Office of Information and 

Technology Services. 

1000.24 Office of International Programs 

and Intergovernmental Affairs. 

1000.25 Office of Hazard Identification and 

Reduction. 

1000.26 Directorate for Epidemiology. 

1000.27 Directorate for Health Sciences. 

1000.28 Directorate for Economic Analysis. 

1000.29 Directorate for Engineering 

Sciences. 

1000.30 Directorate for Laboratory Sciences. 

Authority: 5 U.S.C. 552(a). 

§ 1000.1 The Commission. 

(a) The Consumer Product Safety 

Commission is an independent 

regulatory agency formed on May 14, 

1973, under the provisions of the 

Consumer Product Safety Act (Pub. L. 

92–573, 86 Stat. 1207, as amended (15 

U.S.C. 2051, et seq.)). The purposes of 

the Commission under the CPSA are: 

(1) To protect the public against 

unreasonable risks of injury associated 

with consumer products; 

(2) To assist consumers in evaluating 

the comparative safety of consumer 

products; 

(3) To develop uniform safety 

standards for consumer products and to 

minimize conflicting State and local 

regulations; and 

(4) To promote research and 

investigation into the causes and 

prevention of product-related deaths, 

illnesses, and injuries. 

(b) The Commission is authorized to 

consist of five members appointed by 

the President, by and with the advice 

and consent of the Senate, for terms of 

seven years. However, the Departments 

of Veterans Affairs and Housing and 

Urban Development, and Independent 

Agencies Appropriations Act, 1993, 

Public Law 102–389, limited funding to 

that for three Commissioners for fiscal 

year 1993 and thereafter. 

§ 1000.2 Laws administered. 

The Commission administers five 

acts: 

(a) The Consumer Product Safety Act 

(Pub. L. 92–573, 86 Stat. 1207, as 

amended (15 U.S.C. 2051, et seq.)). 

(b) The Flammable Fabrics Act (Pub. 

L. 90–189, 67 Stat. 111, as amended (15 

U.S.C. 1191, et seq.)). 

(c) The Federal Hazardous Substances 

Act (Pub. L. 86–613, 74 Stat. 380, as 

amended (15 U.S.C. 1261, et seq.)). 

(d) The Poison Prevention Packaging 

Act of 1970 (Pub. L. 91–601, 84 Stat. 

1670, as amended (15 U.S.C. 1471, et 

seq.)). 

(e) The Refrigerator Safety Act of 1956 

(Pub. L. 84–930, 70 Stat. 953, (15 U.S.C. 

1211, et seq.)). 

§ 1000.3 Hotline. 

(a) The Commission operates a tollfree telephone Hotline by which the 

public can communicate with the 

Commission. The number for use in all 

50 states is 1–800–638–CPSC (1–800–

638–2772). 

(b) The Commission also operates a 

toll-free Hotline by which hearing or 

speech-impaired persons can 

communicate with the Commission by 

teletypewriter. The teletypewriter 

number for use in all states is 1–800–

638–8270. 

(c) The Commission also makes 

available to the public product recall 

information, its public calendar, and 

other information through its worldwide 

Web site at http://www.cpsc.gov. The 

public may also report product hazards 

or other information to the Commission 

at its e-mail address: info@cpsc.gov. 


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