Federal Register / Vol. 70, No. 197 / Thursday, October 13, 2005 / Rules and Regulations 59647 

by adding the following new 

airworthiness directive (AD): 

2005–20–41 Boeing: Amendment 39–14338. 

Docket No. FAA–2005–20137; 

Directorate Identifier 2004–NM–96–AD. 

Effective Date 

(a) This AD becomes effective November 

17, 2005. 

Affected ADs 

(b) None. 

Applicability 

(c) This AD applies to Boeing Model 757–

200, –200PF, and –300 series airplanes; 

certificated in any category; powered by Pratt 

& Whitney PW2000 series engines. 

Unsafe Condition 

(d) This AD was prompted by reports of 

damage and subsequent failure of the support 

brackets and associated fasteners for the 

hydraulic lines located internal to the upper 

fairing cavity of the nacelle struts. We are 

issuing this AD to prevent such failure, 

which, in conjunction with sparking of 

electrical wires, failure of seals that would 

allow flammable fluids to migrate to 

compartments with ignition sources, or 

overheating of the pneumatic ducts beyond 

auto-ignition temperatures, could result in an 

uncontained fire. 

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. 

Repetitive Inspections 

(f) Within 6,000 flight hours or 24 months 

after the effective date of this AD, whichever 

is first: Do a detailed inspection for loose or 

damaged components of the support brackets 

and associated fasteners for the hydraulic 

lines located in the nacelle struts by 

accomplishing all of the actions specified in 

Part 1, Part 2, and Part 3 of the 

Accomplishment Instructions of Boeing 

Service Bulletin 757–29–0064 (for Model 

757–200 and –200PF series airplanes) or 

Boeing Service Bulletin 757–29–0065 (for 

Model 757–300 series airplanes), both dated 

February 29, 2004; as applicable. Repeat the 

inspection thereafter at intervals not to 

exceed 6,000 flight hours or 24 months, 

whichever is first. 

Note 1: For the purposes of this AD, a 

detailed inspection is defined as: ‘‘An 

intensive visual examination of a specific 

structural area, system, installation, or 

assembly to detect damage, failure, or 

irregularity. Available lighting is normally 

supplemented with a direct source of good 

lighting at intensity deemed appropriate by 

the inspector. Inspection aids such as mirror, 

magnifying lenses, etc., may be used. Surface 

cleaning and elaborate access procedures 

may be required.’’

Concurrent Service Bulletin 

(g) Prior to or concurrently with the 

accomplishment of paragraph (f) of this AD: 

Accomplish all of the actions specified in the 

Accomplishment Instructions of Boeing 

Service Bulletin 757–29–0043, dated June 21, 

1990. 

Note 2: The part numbers identified in 

Boeing Service Bulletins 757–29–0064 or 

757–29–0065, both dated February 29, 2004; 

or Boeing Service Bulletin 757–29–0043, 

dated June 21, 1990; are acceptable 

configurations and fully comply with the AD 

requirements for the actions required by 

paragraphs (f) and (g) of this AD. 

Related Investigative and Corrective Actions 

(h) Except as required by paragraph (i) of 

this AD: If any loose or damaged part is 

found during any inspection required by 

paragraph (f) of this AD, before further flight, 

do all of the related investigative and 

corrective actions specified in Part 1 and Part 

2 of the Accomplishment Instructions of 

Boeing Service Bulletin 757–29–0064, or 

Boeing Service Bulletin 757–29–0065, both 

dated February 29, 2004; as applicable. 

Repair Information 

(i) If any damage is found during any 

inspection required by this AD, and the 

service bulletin specifies contacting Boeing 

for appropriate action: Before further flight, 

repair per a method approved by the 

Manager, Seattle Aircraft Certification Office 

(ACO), FAA. For a repair method to be 

approved, the approval letter must 

specifically refer to this AD. 

Note 3: There is no terminating action 

currently available for the repetitive 

inspections required by paragraph (f) of this 

AD. 

Alternative Methods of Compliance 

(AMOCs) 

(j)(1) The Manager, Seattle ACO, 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. 

Material Incorporated by Reference 

(k) You must use Boeing Service Bulletin 

757–29–0064, dated February 29, 2004, or 

Boeing Service Bulletin 757–29–0065, dated 

February 29, 2004; and Boeing Service 

Bulletin 757–29–0043, dated June 21, 1990; 

as applicable, 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 Boeing Commercial Airplanes, P.O. 

Box 3707, Seattle, Washington 98124–2207, 

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. 

Issued in Renton, Washington, on 

September 30, 2005. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 05–20264 Filed 10–12–05; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. 2001–NE–50–AD; Amendment 

39–14306; AD 2005–20–12] 

RIN 2120–AA64 

Airworthiness Directives; Dowty 

Aerospace Propellers Type R321/4–82–

F/8, R324/4–82–F/9, R333/4–82–F/12, 

and R334/4–82–F/13 Propeller 

Assemblies 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: The FAA is superseding an 

existing airworthiness directive (AD) for 

Type R321/4–82–F/8, R324/4–82–F/9, 

R333/4–82–F/12, and R334/4–82–F/13 

propeller assemblies. That AD currently 

requires initial and repetitive ultrasonic 

inspections of propeller hubs, part 

number (P/N) 660709201. This AD 

requires the same initial and repetitive 

ultrasonic inspections, but reduces the 

initial and repetitive compliance times 

for Type R334/4–82–F/13 propeller 

assemblies when used on 

Construcciones Aeronauticas, S.A. 

(CASA) 212 airplanes. This AD results 

from a report of a hub separation on a 

CASA 212 airplane. We are issuing this 

AD to prevent propeller hub failure due 

to cracks in the hub, which could result 

in loss of control of the airplane. 

DATES: Effective October 28, 2005. The 

Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in the 

regulations as of October 28, 2005. The 

Director of the Federal Register 

previously approved the incorporation 

by reference of certain publications as 

listed in the regulations as of July 27, 

2004 (69 FR 34560, June 22, 2004). 

We must receive any comments on 

this AD by December 12, 2005. 

ADDRESSES: 

Use one of the following addresses to 

comment on this AD: 

• By mail: Federal Aviation 

Administration (FAA), New England 

59648 Federal Register / Vol. 70, No. 197 / Thursday, October 13, 2005 / Rules and Regulations 

Region, Office of the Regional Counsel, 

Attention: Rules Docket No. 2001–NE–

50–AD, 12 New England Executive Park, 

Burlington, MA 01803–5299. 

• By fax: (781) 238–7055. 

• By e-mail: 9–ane– 

adcomment@faa.gov. 

You can get the service information 

referenced in this AD from Dowty 

Aerospace Propellers, Anson Business 

Park, Cheltenham Road East, Gloucester 

GL 29QN, UK; telephone 44 (0) 1452 

716000; fax 44 (0) 1452 716001. 

You may examine the AD docket at 

the FAA, New England Region, Office of 

the Regional Counsel, 12 New England 

Executive Park, Burlington, MA. 

FOR FURTHER INFORMATION CONTACT: 

Terry Fahr, Aerospace Engineer, Boston 

Aircraft Certification Office, FAA, 

Engine and Propeller Directorate, 12 

New England Executive Park, 

Burlington, MA 01803–5299; telephone 

(781) 238–7116; fax (781) 238–7155. 

SUPPLEMENTARY INFORMATION: June 10, 

2004, the FAA issued AD 2004–13–01, 

Amendment 39–13681 (69 FR 34560, 

June 22, 2004). That AD requires initial 

and repetitive ultrasonic inspections of 

propeller hubs, P/N 660709201, 

installed on airplanes, and for hubs and 

propellers in storage, initial ultrasonic 

inspection of propeller hubs before 

placing in service. That AD was the 

result of the manufacturer’s reevaluation 

of potential hub failure on Type R321/ 

4–82–F/8, R324/4–82–F/9, R333/4–82–

F/12, and R334/4–82–F/13 propeller 

assemblies. That condition, if not 

corrected, could result in propeller hub 

failure due to cracks in the hub, which 

could result in loss of control of the 

airplane. 

Actions Since AD 2004–13–01 Was 

Issued 

Since we issued AD 2004–13–01, the 

Civil Aviation Authority (CAA), which 

is the airworthiness authority for the 

United Kingdom (U.K.), recently 

notified the FAA that an unsafe 

condition might exist on Dowty 

Aerospace Propellers Type R334/4–82–

F/13 propeller assemblies installed on 

CASA 212 airplanes. The CAA advises 

that they have received a report of a hub 

separation of a Type R334/4–82–F/13 

propeller assembly installed on a CASA 

212 airplane. This AD requires the same 

initial and repetitive inspections as 

specified in AD 2004–13–01, but 

reduces the compliance intervals for the 

initial and repetitive inspections on 

Type R334/4–82–F/13 propeller 

assemblies installed on CASA 212 

airplanes. We intend the actions 

specified in this AD to prevent propeller 

hub failure due to cracks in the hub, 

which could result in loss of control of 

the airplane. 

Relevant Service Information 

We have reviewed and approved the 

technical contents of Dowty Aerospace 

Propellers Alert Mandatory Service 

Bulletin (MSB) No. 61–1119, Revision 4, 

dated September 14, 2005, that specifies 

initial and repetitive ultrasonic 

inspections of the rear wall of the rear 

half of the propeller hub for cracks on 

Type R334/4–82–F/13 propeller 

assemblies. The CAA classified this 

service bulletin as mandatory and 

issued CAA UK AD No. G–2005–0027, 

dated September 8, 2005, to assure the 

airworthiness of these Dowty Aerospace 

Propellers in the U.K. 

Differences Between This AD and the 

Manufacturer’s Service Information 

Although Appendix A of Alert MSB 

No. 61–1119, Revision 4, dated 

September 14, 2005, requires reporting 

the inspection data to Dowty Aerospace 

Propellers, this AD requires that you 

report the data to the Boston Aircraft 

Certification Office of the FAA. Also, 

the Accomplishment Instructions 

3.A.(1) of Alert MSB No. 61–1119, 

Revision 4, dated September 14, 2005, 

allows you to use Appendix A or 

Appendix D of that MSB, this AD 

requires that you use Appendix A of 

that MSB. 

Bilateral Airworthiness Agreement 

This propeller model is manufactured 

in the U.K. and is 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 has 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 

The unsafe condition described 

previously is likely to exist or develop 

on other Dowty Aerospace Propellers 

Type R321/4–82–F/8, R324/4–82–F/9, 

R333/4–82–F/12, and R334/4–82–F/13 

propeller assemblies of the same type 

design. We are issuing this AD to 

prevent propeller hub failure due to 

cracks in the hub, which could result in 

loss of control of the airplane. This AD 

requires: 

• Within 10 flight hours (FH) time-inservice (TIS) or 20 days after the 

effective date of this AD, whichever 

occurs earlier, performing an initial 

ultrasonic inspection of the rear halves 

of propeller hubs P/N 660709201, that 

are installed in Type R334/4–82–F/13 

propeller assemblies, and; 

• Within 50 FH TIS or 60 days after 

the effective date of this AD, whichever 

occurs earlier, performing an initial 

ultrasonic inspection of the rear halves 

of propeller hubs P/N 660709201, that 

are installed in Type R321/4–82–F/8, 

R324/4–82–F/9, and R333/4–82–F/12 

propeller assemblies, and; 

• Within 300 FH time-since-lastinspection (TSLI) performing a 

repetitive ultrasonic inspection of the 

rear halves of propeller hubs P/N 

660709201, that are installed in Type 

R334/4–82–F/13 propeller assemblies, 

and; 

• Within 1,000 FH TSLI performing a 

repetitive ultrasonic inspection of the 

rear halves of propeller hubs P/N 

660709201, that are installed in Type 

R321/4–82–F/8, R324/4–82–F/9, and 

R333/4–82–F/12 propeller assemblies, 

and; 

• If not already done, performing an 

ultrasonic inspection of the rear halves 

of propeller hubs P/N 660709201, that 

are installed in Type R321/4–82–F/8, 

R324/4–82–F/9, R333/4–82–F/12, and 

R334/4–82–F/13 propeller assemblies 

that are in storage before installing the 

propeller assembly onto an airplane. 

You must use the service information 

described previously to perform the 

actions required by this AD. 

FAA’s Determination of the Effective 

Date 

Since an unsafe condition exists that 

requires the immediate adoption of this 

AD, we have found that notice and 

opportunity for public comment before 

issuing this AD are impracticable and 

that good cause exists for making this 

amendment effective in less than 30 

days. 

Comments Invited 

This AD is a final rule that involves 

requirements affecting flight safety. We 

did not precede it 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. 

2001–NE–50–AD’’ in the subject line of 

your comments. If you want us to 

acknowledge receipt of your mailed 

comments, send us a self-addressed, 

stamped postcard with the docket 

number written on it; we will dateVerDate Aug<31>2005 14:41 Oct 12, 2005 Jkt 208001 PO 00000 Frm 00028 Fmt 4700 Sfmt 4700 E:\FR\FM\13OCR1.SGM 13OCR1
Federal Register / Vol. 70, No. 197 / Thursday, October 13, 2005 / Rules and Regulations 59649 

stamp your postcard and mail it back to 

you. We specifically invite comments 

on the overall regulatory, economic, 

environmental, and energy aspects of 

the rule that might suggest a need to 

modify it. If a person contacts us 

verbally, and that contact relates to a 

substantive part of this AD, we will 

summarize the contact and place the 

summary in the docket. We will 

consider all comments received by the 

closing date and may amend the AD in 

light of those comments. 

Examining the AD Docket 

You may examine the AD Docket 

(including any comments and service 

information), by appointment, between 

8 a.m. and 4:30 p.m., Monday through 

Friday, except Federal holidays. See 

ADDRESSES for the location. 

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. 

Include ‘‘AD Docket No. 2001–NE–50–

AD’’ in your request. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

Adoption of the Amendment 

Accordingly, 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: 

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 

removing Amendment 39–13681 (69 FR 

34560, June 22, 2004), and by adding a 

new airworthiness directive, 

Amendment 39–14306, to read as 

follows: 

2005–20–12 Dowty Aerospace Propellers: 

Amendment 39–14306. Docket No. 

2001–NE–50–AD. 

Effective Date 

(a) This airworthiness directive (AD) 

becomes effective October 28, 2005. 

Affected ADs 

(b) This AD supersedes AD 2004–13–01, 

Amendment 39–13681. 

Applicability 

(c) This AD applies to Dowty Aerospace 

Propellers Type R321/4–82–F/8, R324/4–82–

F/9, R333/4–82–F/12, and R334/4–82–F/13 

propeller assemblies with propeller hubs part 

number (P/N) 660709201. These propeller 

assemblies are installed on, but not limited 

to, Construcciones Aeronauticas, S.A. 

(CASA) 212, British Aerospace Regional 

Aircraft Jetstream Models 3101 and 3201, 

Fairchild Aircraft, Inc., Merlin IIIC, and 

Merlin IVC/Metro III airplanes. 

Unsafe Condition 

(d) This AD results from a report of a hub 

separation on a CASA 212 airplane. We are 

issuing this AD to prevent propeller hub 

failure due to cracks in the hub, which could 

result in loss of control of 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 Ultrasonic Inspections 

(f) Perform an initial ultrasonic inspection 

of the rear wall of the rear half of the 

propeller hub for cracks within the 

compliance time specified in the following 

Table 1. Use Appendix A of the applicable 

Dowty Mandatory Service Bulletin (MSB) 

listed in Table 1 of this AD. 

TABLE 1.—APPLICABLE MSB FOR PROPELLER TYPE

Propeller assembly type Initial inspection within the earlier 

of . . . Repeat inspection within . . . Applicable MSB 

(1) R334/4–82–F/13 ....................... 10 flight hours (FH) time-in-service (TIS) or 20 days after the 

effective date of this AD.

300 FH time-since-last-inspection 

(TSLI).

Alert MSB No. 61–1119, Revision 

4, dated September 14, 2005. 

(2) R321/4–82–F/8 ......................... 50 FH TIS or 60 days after the effective date of this AD.1,000 FH TSLI .............................. MSB No. 61–1125, Revision 1, 

dated October 9, 2002. 

(3) R324/4–82–F/9 ......................... 50 FH TIS or 60 days after the effective date of this AD.1,000 FH TSLI .............................. MSB No. 61–1126, Revision 1, 

dated October 9, 2002. 

(4) R333/4–82–F/12 ....................... 50 FH TIS or 60 days after the effective date of this AD.1,000 FH TSLI .............................. MSB No. 61–1124, Revision 1, 

dated October 8, 2002. 

(g) For hubs and propellers in storage, 

perform an initial ultrasonic inspection of the 

rear wall of the rear half of the propeller hub 

for cracks, before placing in service. Use 

Appendix A of the applicable Dowty MSB 

listed in Table 1 of this AD. 

(h) Propeller hubs, P/N 660709201, already 

inspected using a Dowty MSB listed in Table 

1 or earlier issue of those MSBs, comply with 

paragraph (f) of this AD. 

59650 Federal Register / Vol. 70, No. 197 / Thursday, October 13, 2005 / Rules and Regulations 

Repetitive Ultrasonic Inspections 

(i) Thereafter, perform a repetitive 

ultrasonic inspection of the rear wall of the 

rear half of the propeller hub for cracks 

within the compliance time specified in 

Table 1 of this AD. Use Appendix A of the 

applicable Dowty Mandatory Service Bulletin 

(MSB) listed in Table 1 of this AD. 

Inspection Reporting Requirements 

(j) Within 10 days after each inspection, 

record the inspection data on a copy of 

Appendix B of the applicable MSB listed in 

Table 1 of this AD. Report the findings to the 

Manager, Boston Aircraft Certification Office, 

FAA, Engine and Propeller Directorate, 12 

New England Executive Park, Burlington, 

MA 01803–5299. The Office of Management 

and Budget (OMB) approved the reporting 

requirements and assigned OMB control 

number 2120–0056. 

Alternative Methods of Compliance 

(k) The Manager, Boston 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. 

Special Flight Permits 

(l) Special flight permits may be issued in 

accordance with §§ 21.197 and 21.199 of the 

Federal Aviation Regulations (14 CFR 21.197 

and 21.199) to operate the airplane to a 

location where the requirements of this AD 

can be done. 

Documents That Have Been Incorporated by 

Reference 

(m) You must use the service information 

specified in Table 2 to perform the 

inspections required by this AD. The Director 

of the Federal Register approved the 

incorporation by reference of Dowty Alert 

Mandatory Service Bulletin (MSB) No. 61–

1119, Revision 4, Dated September 14, 2005, 

listed in Table 2 of this AD, in accordance 

with 5 U.S.C. 552(a) and 1 CFR part 51. The 

Director of the Federal Register previously 

approved the incorporation by reference of 

MSB No. 61–1124, Revision 1, Dated October 

8, 2002, and MSB No. 61–1125, Revision 1, 

Dated October 9, 2002, and MSB 61–1126, 

Revision 1, Dated October 9, 2002 (69 FR 

34560, June 22, 2004). Contact Dowty 

Propellers, Anson Business Park, Cheltenham 

Road East, Gloucester GL 29QN, UK; 

telephone 44 (0) 1452 716000; fax 44 (0) 1452 

716001 for a copy of this service information. 

You may review copies at the FAA, New 

England Region, Office of the Regional 

Counsel, 12 New England Executive Park, 

Burlington, MA; 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/ibr-locations.html. 

TABLE 2.—INCORPORATION BY REFERENCE

Service Bulletin No. Page Revision Date 

Alert MSB No. 61–1119 ...................................................... All ......................................... 4 ........................................... September 14, 2005. 

Appendix A ......................................................................... 1 ........................................... 1 ........................................... November 27, 2001. 

2 ........................................... Original ................................. November 1, 2001. 

3–6 ....................................... 1 ........................................... November 27, 2001. 

Appendix B ......................................................................... 1 ........................................... Original ................................. November 1, 2001. 

Appendix C ......................................................................... All ......................................... Original ................................. November 27, 2001. 

Appendix D ......................................................................... All ......................................... Original ................................. December 6, 2001. 

Total pages .................................................................. 30 ......................................... ..............................................

MSB No. 61–1124 .............................................................. 1 ........................................... 1 ........................................... October 8, 2002. 

2–3 ....................................... Original ................................. May 7, 2002. 

Appendix A ......................................................................... All ......................................... Original ................................. May 7, 2002. 

Appendix B ......................................................................... All ......................................... Original ................................. May 7, 2002. 

Appendix C ......................................................................... All ......................................... Original ................................. May 7, 2002. 

Appendix D ......................................................................... All ......................................... Original ................................. May 7, 2002. 

Total pages .................................................................. 30 ......................................... ..............................................

MSB No. 61–1125 .............................................................. 1 ........................................... 1 ........................................... October 9, 2002. 

2–3 ....................................... Original ................................. May 7, 2002. 

Appendix A ......................................................................... All ......................................... Original ................................. May 7, 2002. 

Appendix B ......................................................................... All ......................................... Original ................................. May 7, 2002. 

Appendix C ......................................................................... All ......................................... Original ................................. May 7, 2002. 

Appendix D ......................................................................... All ......................................... Original ................................. May 7, 2002. 

Total pages .................................................................. 30 ......................................... ..............................................

MSB No. 61–1126 .............................................................. 1 ........................................... 1 ........................................... October 9, 2002. 

2–3 ....................................... Original ................................. May 7, 2002. 

Appendix A ......................................................................... All ......................................... Original ................................. May 7, 2002. 

Appendix B ......................................................................... All ......................................... Original ................................. May 7, 2002. 

Appendix C ......................................................................... All ......................................... Original ................................. May 7, 2002. 

Appendix D ......................................................................... All ......................................... Original ................................. May 7, 2002. 

Total pages .................................................................. 30 ......................................... ..............................................

Federal Register / Vol. 70, No. 197 / Thursday, October 13, 2005 / Rules and Regulations 59651 

Related Information 

(n) United Kingdom (U.K.) Civil Aviation 

Authority (CAA) airworthiness directives No. 

G–2006–0027, dated September 8, 2005; CAA 

UK AD No. 009–05–2002, dated April 15, 

2003; CAA UK AD No. 010–05–2002, dated 

April 15, 2003; and CAA UK AD No. 011–

05–2002, dated April 15, 2003, also addresses 

the subject of this AD. 

Issued in Burlington, Massachusetts, on 

September 26, 2005. 

Francis A. Favara, 

Acting Manager, Engine and Propeller 

Directorate, Aircraft Certification Service. 

[FR Doc. 05–20170 Filed 10–12–05; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No. FAA–2005–21873; Airspace 

Docket No. 05–ACE–27] 

Modification of Class D and Class E 

Airspace; Salina Municipal Airport, KS; 

Correction 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Direct final rule; request for 

comments; correction. 

SUMMARY: This action corrects errors in 

the legal description of Class D airspace 

in a direct final rule, request for 

comments that was published in the 

Federal Register on Friday July 29, 2005 

(70 FR 43742). 

DATES: This direct final rule is effective 

on 0901 UTC, October 27, 2005. 

FOR FURTHER INFORMATION CONTACT: 

Brenda Mumper, Air Traffic Division, 

Airspace Branch, ACE–520A, DOT 

Regional Headquarters Building, Federal 

Aviation Administration, 901 Locust, 

Kansas City, MO 64106; telephone: 

(816) 329–2524. 

SUPPLEMENTARY INFORMATION: 

History 

Federal Register Document 2005–

21873 published on Friday July 29, 2005 

(70 FR 43742), modified Class D and 

Class E Airspace at Salina Municipal 

Airport, KS. The legal descriptions of 

these airspace areas used outdated and 

incorrect information. This action 

corrects those errors. 

■ Accordingly, pursuant to the authority 

delegated to me, the errors in the legal 

descriptions of airspace at Salina 

Municipal Airport, KS as published in 

the Federal Register Friday July 29, 

2005 (70 FR 43742), (FR Doc. 2005–

21873), are corrected as follows: 

§ 71.1 [Amended] 

■ 2. The incorporation by reference in 

14 CFR 71.1 of Federal Aviation 

Administration Order 7400.9N, dated 

September 1, 2005, and effective 

September 15, 2005, is amended as 

follows: 

Paragraph 5000 Class D Airspace. 

* * * * * 

ACE KS D Salina, KS 

Salina Municipal Airport, KS 

(Lat. 38°47′27′′ N., long. 97°39′08′′ W.) 

That airspace extending upward from the 

surface to and including 3,800 feet MSL 

within a 5.4-mile radius of Salina Municipal 

Airport. This Class D airspace area is 

effective during the specific dates and times 

established in advance by a Notice to 

Airmen. The effective date and time will 

thereafter be continuously published in the 

Airport/Facility Directory. 

* * * * * 

Paragraph 6002 Class E Airspace 

Designated as Surface Areas. 

* * * * * 

ACE KS E2 Salina, KS 

Salina Municipal Airport, KS 

(Lat. 38°47′27′′ N., long. 97°39′08′′ W.) 

Airmen. The effective date and time will 

thereafter be continuously published in the 

Airport/Facility Directory. 

* * * * * 

Paragraph 6004 Class E Airspace 

Designated as an Extension to a Class D or 

Class E Surface Area. 

* * * * * 

ACE KS E4 Salina, KS 

Salina Municipal Airport, KS 

(Lat. 38°47′27′′ N., long. 97°39′08′′ W.) 

Salina VORTAC 

(Lat. 38°55′31′′ N., long. 97°37′17′′ W.) 

That airspace extending upward surface 

within 1.5 miles each side of the Salina 

VORTAC 190° radial extending from the 5.4- 

mile radius of Salina Municipal Airport to 2 

miles south of the VORTAC. 

* * * * * 

Paragraph 6005 Class E airspace areas 

extending upward from 700 feet or more 

above the surface of the earth. 

* * * * * 

ACE KS E5 Salina, KS 

Salina Municipal Airport, KS 

(Lat. 38°47′27′′ N., long. 97°39′08′′ W.) 

That airspace extending upward from 700 

feet above the surface within an 8.4-mile 

radius of Salina Municipal Airport. 

Issued in Kansas City, MO, on September 

20, 2005. 

Elizabeth S. Wallis, 

Acting Area Director, Western Flight Services 

Operations. 

[FR Doc. 05–20462 Filed 10–12–05; 8:45 am] 

BILLING CODE 4910–13–M 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket FAA 2005–21523; Airspace Docket 

No. 05–AWP–07] 

Establishment of Class E3 Airspace, 

Riverside March Field, CA 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: This action establishes a Class 

E3 airspace area at Riverside March 

Field, CA. 

EFFECTIVE DATE: 0901 UTC December 22, 

2005. 

FOR FURTHER INFORMATION CONTACT: 

Debra Trindle, Western Terminal 

Service Area, Airspace Specialist, 

AWP–520, Federal Aviation 

Administration, 15000 Aviation 

Boulevard, Lawndale, California 90261, 

telephone (310) 725–6613. 

SUPPLEMENTARY INFORMATION: 

History 

On August 2, 2005, the FAA proposed 

to establish Class E3 airspace at 

Riverside March Field, CA. Class E3 

airspace areas are designated as arrival 

extensions to a Class C surface area. 

Class E arrival extensions are primarily 

designated to provide additional 

controlled airspace ancillary to a surface 

area to protect instrument operations for 

the primary airport, without imposing 

additional communications burdens on 

airspace users. This action is necessary 

at Riverside March Field to provide 

controlled airspace for Category E 

aircraft conducting circling maneuvers 

in conjunction with published Standard 

Instrument Approach Procedures. 

Generally, Category E aircraft are very 

large and/or high performance. These 

aircraft require additional airspace 

when conducting circling maneuvers. 

This action will establish the Class E3 

airspace at Riverside March Field. 

Interested parties were invited to 

participate in this rule making 

proceeding by submitting written 

comments on the proposal to the FAA. 

No comments were received. Class E3 

airspace is published in Paragraph 6003 

of FAA Order 7400.9N dated September 

1, 2005, and effective September 16, 

2005, which is incorporated by 

reference in 14 CFR 71.1. The Class E 

Surface Area airspace designation listed 

in this document would be published 

subsequently in this Order.