Federal Register / Vol. 72, No. 70 / Thursday, April 12, 2007 / Rules and Regulations 18383 

Special Flight Permit 

(f) Under 14 CFR 39.23, we are allowing 

special flight permits for the purpose of 

compliance with this AD under the following 

conditions: Only operate under day visual 

flight rules (VFR). 

Alternative Methods of Compliance 

(AMOCs) 

(g) The Manager, Wichita Aircraft 

Certification Office (ACO), FAA, ATTN: 

Trenton Shepherd, Aerospace Engineer, 

Wichita ACO, 1801 Airport Road, Room 100, 

Wichita, Kansas 67209; telephone: (316) 946–

4143; fax: (316) 946–4107, has the authority 

to approve AMOCs for this AD, if requested 

using the procedures found in 14 CFR 39.19. 

Before using any approved AMOC on any 

airplane to which the AMOC applies, notify 

your appropriate principal inspector (PI) in 

the FAA Flight Standards District Office 

(FSDO), or lacking a PI, your local FSDO. 

(h) AMOCs approved for AD 2006–17–04 

are not approved for this AD. 

Material Incorporated by Reference 

(i) You must use Cessna Service Bulletin 

No. SB07–71–01, Revision 1, dated March 16, 

2007, to do the actions required by this AD, 

unless the AD specifies otherwise. 

(1) The Director of the Federal Register 

approved the incorporation by reference of 

this service information under 5 U.S.C. 

552(a) and 1 CFR part 51. 

(2) For service information identified in 

this AD, contact The Cessna Aircraft 

Company, Product Support, P.O. Box 7706, 

Wichita, Kansas 67277–7706; telephone: 

(316) 517–5800; facsimile: (316) 942–9006. 

(3) You may review copies at the FAA, 

Central Region, Office of the Regional 

Counsel, 901 Locust, Kansas City, Missouri 

64106; 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/ 

code_of_federal_regulations/ 

ibr_locations.html. 

Appendix to AD 2007–08–03—

Inspection Instructions—Cessna 

Aircraft Company Models 172R, 172S, 

182T, T182T, 206H, and T206H 

Airplanes 

1. Remove upper and side cowlings to 

perform torque procedure. 

2. Remove all signs of old torque putty or 

paint. 

3. Using a suitable tool loosen the hose end 

fitting of each joint, while using a suitable 

tool to restrain the other end fitting of the 

joint to preclude rotation. 

4. Using the applicable fitting torque from 

the table Torque Values for Hose End Fittings 

of this appendix to AD 2007–08–03, torque 

the hose end fitting to the proper torque, 

while using a suitable tool to restrain the 

other end fitting of the joint to preclude 

rotation. 

5. After proper torque has been applied to 

the hose end fitting, apply the applicable 

torque paint or putty to the hose end fitting 

joint. 

6. If during any torque procedure any of 

the non-hose end fittings rotate, stop the 

torque procedure. Totally disconnect the 

hose end joint and remove any fitting that 

has rotated. After the cleaning, visual 

examination, and/or replacement of the 

fitting and/or any seals or sealant, reinstall 

the fitting and torque it to the applicable 

requirement. Then reconnect the hose end 

fitting and repeat Step 4. of this appendix to 

AD 2007–08–03. 

7. Use the table below Torque Values for 

Hose End Fittings for the correct torque 

values to tighten the hose end fittings as 

required in paragraphs (e)(1) and (e)(2) of this 

AD: 

TORQUE VALUES FOR HOSE END FITTINGS

Flare hex sizes in fractions of an inch Hose size 

Correct torque in inch-pounds 

Minimum Maximum 

9⁄16 ................................................................................................................................................ ¥4 135 150 11⁄16 .............................................................................................................................................. ¥6 270 300 7⁄8 ................................................................................................................................................. ¥8 450 500 

Issued in Kansas City, Missouri, on April 

5, 2007. 

Kim Smith, 

Manager, Small Airplane Directorate, Aircraft 

Certification Service. 

[FR Doc. E7–6826 Filed 4–11–07; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No. FAA–2007–27110; Airspace 

Docket No. 07–AGL–1] 

Modification of Class E Airspace; Peru, 

IL 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Direct final rule; confirmation 

of effective date. 

SUMMARY: This document confirms the 

effective date of the direct final rule 

which revises Class E airspace at Peru, 

IL. 

EFFECTIVE DATE: 0901 UTC, May 10, 

2007. 

FOR FURTHER INFORMATION CONTACT: 

Grant Nichols, System Support, DOT 

Regional Headquarters Building, Federal 

Aviation Administration, 901 Locust, 

Kansas City, MO 64106; telephone (816) 

329–2522. 

SUPPLEMENTARY INFORMATION: The FAA 

published this direct final rule with a 

request for comments in the Federal 

Register on February 26, 2007 (72 FR 

8266). The FAA uses the direct final 

rulemaking procedures for a noncontroversial rule where the FAA 

believes that there will be no adverse 

public comment. This direct final rule 

advised the public that no adverse 

comments were anticipated, and that 

unless a written adverse comment, or a 

written notice of intent to submit such 

an adverse comment, were received 

within the comment period, the 

regulation would become effective on 

May 10, 2007. No adverse comments 

were received, and thus this notice 

confirms that this direct final rule will 

become effective on that date. 

Issued in Forth Worth, Texas, on March 21, 

2007. 

Ronnie L. Uhlenhaker, 

Manager, System Support Group, ATO 

Central Service Area. 

[FR Doc. 07–1803 Filed 4–11–07; 8:45 am] 

BILLING CODE 4910–13–M 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No. FAA–2006–25997; Airspace 

Docket No. 06–ANM–5] 

Revision of Class E Airspace; 

Redmond, OR 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: This action will revise the 

Class E airspace at Redmond, OR. 

Additional Class E airspace is necessary 

to accommodate aircraft using a new 

Area Navigation (RNAV) Global 

Positioning System (GPS) Standard 


rmajette on PROD1PC67 with RULES