Federal Register / Vol. 67, No. 174 / Monday, September 9, 2002 / Rules and Regulations 57145

§ 996.73 Verification of reports. 

For the purpose of checking and 

verifying reports filed by handlers and 

importers and the operation of handlers 

and importers under the provisions of 

this Part, the officers, employees or duly 

authorized agents of USDA shall have 

access to any premises where peanuts 

may be held and at any time during 

reasonable business hours and shall be 

permitted to inspect any peanuts so 

held by such handler or importer and 

any and all records of such handler with 

respect to the acquisition, holding, or 

disposition of all peanuts which may be 

held or which may have been disposed 

by the handler.

§ 996.74 Compliance. 

(a) A handler or importer shall be 

subject to withdrawal of inspection 

services, for a period of time to be 

determined by USDA, if the handler or 

importer: 

(1) Acquires farmers stock peanuts 

without official incoming inspection, 

pursuant to § 996.30; 

(2) Fails to obtain outgoing inspection 

on shelled or cleaned-inshell peanuts, 

pursuant to § 996.31, and ships such 

peanuts for human consumption use; 

(3) Ships failing quality peanuts, 

pursuant to § 996.31, for human 

consumption use; 

(4) Commingles failing quality 

peanuts with certified edible quality 

peanuts and ships the commingled lot 

for human consumption use; 

(5) Fails to maintain positive lot 

identification, pursuant to § 996.40(a), 

on peanut lots certified for human 

consumption use; 

(6) Fails to maintain and provide 

access to records, pursuant to § 996.71, 

on the reconditioning or disposition of 

peanuts acquired by such handler or 

importer; or 

(7) Otherwise violates any provision 

of section 1308 of the Act or any 

provision of this part. 

(b) Any peanut lot which fails to meet 

the Outgoing quality standards specified 

in § 996.31, and is not reconditioned to 

meet such standards, or is not disposed 

to non-human consumption outlets as 

specified in § 996.50, shall be reported 

by USDA to the Food and Drug 

Administration and listed on an 

Agricultural Marketing Service Web 

site.

§ 996.75 Effective time. 

The provisions of this part, as well as 

any amendments, shall apply to the 

remainder of the 2002 crop year peanuts 

and subsequent crop year peanuts, to 

2001 crop year peanuts not yet 

inspected, and to 2001 crop year failing 

peanuts that have not met disposition 

standards, and shall continue in force 

and effect until modified, suspended, or 

terminated. Indemnification payments 

for the 2001 crop peanuts will continue 

through December 31, 2002, under the 

terms and conditions of 7 CFR part 998.

PART 997—[REMOVED] 

2. Part 997 is removed.

PART 998—[REMOVED] 

3. Part 998 is removed, effective 

January 1, 2003.

PART 999—SPECIALTY CROPS; 

IMPORT REGULATIONS 

4. The authority citation for part 999 

continues to read as follows:

Authority: 7 U.S.C. 601–674; 7 U.S.C. 

1445c–3, and 7 U.S.C. 7271.

§999.600 [Removed] 

5. Section 999.600 is removed.

Dated: September 3, 2002. 

A.J. Yates, 

Administrator, Agricultural Marketing 

Service.

[FR Doc. 02–22700 Filed 9–6–02; 8:45 am] 

BILLING CODE 3410–02–P

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. 98–ANE–48–AD; Amendment 

39–12867; AD 2002–17–02] 

RIN 2120–AA64 

Airworthiness Directives; Pratt & 

Whitney JT8D Series Turbofan 

Engines; Correction

AGENCY: Federal Aviation 

Administration, DOT.

ACTION: Final rule; correction.

SUMMARY: This document makes a 

correction to Airworthiness Directive 

(AD) 2002–17–02 applicable to Pratt & 

Whitney JT8D series turbofan engines 

that was published in the Federal 

Register on August 28, 2002 (67 FR 

55108). The first sentence in the 

amendatory language that states ‘‘2. 

Section 39.13 is amended by removing 

Amendment 39–11940 (65 FR 65731, 

November 2, 2000) and by adding a new 

airworthiness directive to read as 

follows:’’ is incorrect. This document 

corrects that sentence. In all other 

respects, the original document remains 

the same.

EFFECTIVE DATE: August 28, 2002.

FOR FURTHER INFORMATION CONTACT:

Christopher Spinney, Aerospace 

Engineer, Engine Certification Office, 

FAA, Engine and Propeller Directorate, 

12 New England Executive Park; 

Burlington, MA 01803–5299; telephone 

(781) 238–7175; fax (781) 238–7199.

SUPPLEMENTARY INFORMATION: A final 

rule airworthiness directive FR Doc. 02–

21832 applicable to Pratt & Whitney 

JT8D series turbofan engines, was 

published in the Federal Register on 

August 28, 2002 (67 FR 55108). The 

following correction is needed:

§ 39.13 [Corrected] 

On page 55110, in the second column, 

the first sentence of the amendatory 

language is corrected to read: 

‘‘2. Section 39.13 is amended by 

removing Amendment 39–11940 (65 FR 

65731, November 2, 2000) and by 

adding a new airworthiness directive, 

Amendment 39–12867, to read as 

follows:’’

Issued in Burlington, MA, on August 30, 

2002. 

Francis Favara, 

Acting Manager, Engine and Propeller 

Directorate, Aircraft Certification Service.

[FR Doc. 02–22759 Filed 9–6–02; 8:45 am] 

BILLING CODE 4910–13–P

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. 2002–NE–08–AD; Amendment 

39–12865; AD 2002–16–26] 

RIN 2120–AA64 

Airworthiness Directives; BombardierRotax GmbH Type 912 F and 914 F 

Series Reciprocating Engines; 

Correction

AGENCY: Federal Aviation 

Administration, DOT.

ACTION: Final rule; request for 

comments, correction. 

SUMMARY: This document makes a 

correction to Airworthiness Directive 

(AD) 2002–16–26, applicable to 

Bombardier-Rotax GmbH type 912 F and 

914 F series reciprocating engines. AD 

2002–16–26 was published in the 

Federal Register on August 15, 2002 (67 

FR 53296). The effective date in the 

DATES: section is incorrect. This 

document corrects that date. In all other 

respects, the original document remains 

the same.

EFFECTIVE DATE: August 30, 2002.

FOR FURTHER INFORMATION CONTACT:

James Lawrence, Aerospace Engineer, 

57146 Federal Register / Vol. 67, No. 174 / Monday, September 9, 2002 / Rules and Regulations 

Engine Certification Office, FAA, Engine 

and Propeller Directorate, 12 New 

England Executive Park, Burlington, MA 

01803–5299; telephone (781) 238–7176; 

fax (781) 238–7199.

SUPPLEMENTARY INFORMATION: A final 

rule; request for comments 

airworthiness directive FR DOC. 02–

20679, applicable to Bombardier-Rotax 

GmbH type 912 F and 914 F series 

reciprocating engines, was published in 

the Federal Register on August 15, 2002 

(67 FR 53296). The following correction 

is needed: 

On page 53296, in the second column, 

in the DATES: section, ‘‘Effective 

September 16, 2002’’ is corrected to read 

‘‘Effective August 30, 2002’’.

Issued in Burlington, MA, on August 30, 

2002. 

Francis A. Favara, 

Acting Manager, Engine and Propeller 

Directorate, Aircraft Certification Service.

[FR Doc. 02–22760 Filed 9–6–02; 8:45 am] 

BILLING CODE 4910–13–P

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. 95–ANE–64–AD; Amendment 

39–12876; AD 97–09–02R1] 

RIN 2120–AA64 

Airworthiness Directives; CFM 

International CFM56 Series Turbofan 

Engines

AGENCY: Federal Aviation 

Administration, DOT.

ACTION: Final rule; request for 

comments. 

SUMMARY: This amendment revises an 

existing airworthiness directive (AD) 

that is applicable to CFM International 

(CFMI) CFM56–5C series turbofan 

engines. This action establishes new life 

limits for certain low pressure turbine 

rotor (LPTR) stage 3 disks and all high 

pressure turbine rotor (HPTR) disks 

listed in the existing AD. This 

amendment is prompted by the results 

of an extensive life management 

program performed by the 

manufacturer. The actions specified in 

this AD are intended to prevent lowcycle-fatigue (LCF) failure of certain 

HPTR front shafts, HPTR front air seals, 

HPTR disks, booster spools, and LPTR 

stage 3 disks, which could result in an 

uncontained engine failure and damage 

to the airplane.

DATES: Effective September 24, 2002. 

Comments for inclusion in the Rules 

Docket must be received on or before 

November 8, 2002.

ADDRESSES: Submit comments in 

triplicate to the Federal Aviation 

Administration (FAA), New England 

Region, Office of the Regional Counsel, 

Attention: Rules Docket No. 95–ANE–

64–AD, 12 New England Executive Park, 

Burlington, MA 01803–5299. Comments 

may be inspected at this location, by 

appointment, between 8 a.m. and 4:30 

p.m., Monday through Friday, except 

Federal holidays. Comments may also 

be sent via the Internet using the 

following address: ‘‘9-aneadcomment@faa.gov’’. Comments sent 

via the Internet must contain the docket 

number in the subject line.

FOR FURTHER INFORMATION CONTACT:

Glorianne Niebuhr, Aerospace Engineer, 

Engine Certification Office, FAA, Engine 

and Propeller Directorate, 12 New 

England Executive Park, Burlington, MA 

01803–5299; telephone (781) 238–7132; 

fax (781) 238–7199.

SUPPLEMENTARY INFORMATION: On April 

22, 1997, the FAA issued AD 97–09–02, 

Amendment 39–9998 (62 FR 23642), 

applicable to CFMI CFM56–5C series 

turbofan engines, to reduce the LCF 

retirement lives of certain HPTR front 

shafts, HPTR front air seals, booster 

spools, HPTR disks, and LPTR stage 3 

disks. That action was prompted by 

results of a refined life analysis 

performed by the manufacturer which 

revealed minimum calculated LCF lives 

lower than published LCF retirement 

lives. This condition could result in LCF 

failure of certain HPTR front shafts, 

HPTR front air seals, HPTR disks, 

booster spools, and LPTR stage 3 disks, 

which could result in an uncontained 

engine failure and damage to the 

airplane. Since AD 97–09–02 was 

issued, the manufacturer conducted an 

extensive life management program for 

the LPTR stage 3 disks installed in 

CFM56–5C2/G and –5C3/G engines and 

HPTR disks installed in all CFM56–5C 

series engines. This consisted of a 

mission cycle based on field data, an 

updated 2D heat transfer and stress 

analysis, and a 3D finite element 

analysis. The results indicated higher 

LCF retirement lives for certain LPTR 

stage 3 disks and all HPTR disks than 

the lives published in AD 97–09–02. 

Therefore, this revision establishes new 

life limits for LPTR stage 3 disks part 

numbers (P/N’s) 337–001–602–0 and 

337–001–605–0 installed in CFM56–

5C2/G and –5C3/G engines and HPTR 

disk P/N 1498M43P04 installed in all 

CFM56–5C series engines. Except for 

CFM56–5C4 engines, the LCF retirement 

lives for LPTR stage 3 disks part 

numbers (P/N’s) 337–001–602–0 and 

337–001–605–0 are now extended to 

20,000 cycles-since-new (CSN) in 

Chapter 05 of the CFM56–5C Engine 

Shop Manual, CFMI–TP.SM.8. The LCF 

retirement lives for HPTR disk part 

number 1498M43P04 are now extended 

to 7,800 cycles-since-new (CSN) in 

Chapter 05 of the CFM56–5C Engine 

Shop Manual, CFMI–TP.SM.8. The 

cyclic lives of these LPTR stage 3 disks 

installed in CFM56–5C4 engines, and 

the cyclic lives of HPTR front shafts P/

N’s 1498M40P03, 1498M40P05, and 

1498M40P06; HPTR front air seals, P/

N’s 1523M34P02 and 1523M34P03; and 

booster spools, P/N 337–005–210–0, 

remain unchanged. 

FAA’s Determination of an Unsafe 

Condition and Required Actions 

Although these affected engine 

models are not used on any airplanes 

that are registered in the United States, 

the possibility exists these engine 

models could be used on airplanes that 

are registered in the United States in the 

future. This AD establishes new life 

limits for certain LPTR stage 3 disks and 

all HPTR disks listed in the existing AD.

Immediate Adoption of This AD 

Since there are currently no domestic 

operators of CFM56–5C series turbofan 

engines, notice and opportunity for 

prior public comment are unnecessary. 

Therefore, a situation exists that allows 

the immediate adoption of this 

regulation. 

Comments Invited 

Although this action is in the form of 

a final rule that involves requirements 

affecting flight safety and, thus, was not 

preceded by notice and an opportunity 

for public comment, comments are 

invited on this rule. Interested persons 

are invited to comment on this rule by 

submitting such written data, views, or 

arguments as they may desire. 

Communications should identify the 

Rules Docket number and be submitted 

in triplicate to the address specified 

under the caption ADDRESSES. All 

communications received on or before 

the closing date for comments will be 

considered, and this rule may be 

amended in light of the comments 

received. Factual information that 

supports the commenter’s ideas and 

suggestions is extremely helpful in 

evaluating the effectiveness of the AD 

action and determining whether 

additional rulemaking action would be 

needed. 

Comments are specifically invited on 

the overall regulatory, economic, 

environmental, and energy aspects of 

the rule that might suggest a need to