Federal Register / Vol. 72, No. 200 / Wednesday, October 17, 2007 / Rules and Regulations 58757 

(3) Applicable to airplane serial numbers 

003 thorough 599: Incorporate Modsum 

8Q101445 to rework the spoiler cable 

disconnect sensing circuit. Bombardier 

Service Bulletin 8–27–103, Revision ‘B,’

dated January 24, 2007, provides approved 

instructions for incorporating Modsum 

8Q101445. (See paragraph (f)(6) of this AD.) 

If Modsum 8Q100898 has not yet been 

incorporated, incorporate Modsum 8Q101445 

in conjunction with Modsum 8Q100898. 

Refer to paragraph (f)(1) or (f)(2) of this AD, 

as applicable. 

Note 1: The mandatory operational check 

requirement for the spoiler cable disconnect 

system (Modsum 8Q100898) is detailed in 

Task Number 2760/14, dated November 21, 

2003, of Part 2 of the applicable de Havilland 

Dash 8 Maintenance Program Manual (MPM), 

Airworthiness Limitations (AWL). It was 

introduced by de Havilland Dash 8 

Temporary Revisions AWL–88 (series 100), 

AWL 2–28 (series 200), and AWL 3–95 

(series 300), all dated August 5, 2004. 

Temporary Revision AWL–88 (Task Number 

2760/14) has since been incorporated in 

Revision 17, dated April 19, 2005, of Part 2 

of the AWLs of the MPM for Model DHC–8–

100 series airplanes. 

(4) Installation of Modsum 8Q100898, in 

accordance with Bombardier Service Bulletin 

8–27–89, dated January 31, 2002; Revision 

‘A,’ dated September 10, 2002; Revision ‘B,’

dated November 17, 2003; Revision ‘C,’ dated 

March 10, 2004; Revision ‘D,’ dated June 29, 

2004; Revision ‘E,’ dated January 27, 2005; or 

Revision ‘F,’ dated March 14, 2007; also 

meets the requirements of paragraphs (f)(1) 

and (f)(2) of this AD. 

(5) Installation of Modsum 8Q101443, 

in accordance with Bombardier Service 

Bulletin 8–27–89, Revision ‘C,’ dated 

March 10, 2004; Revision ‘D,’ dated June 

29, 2004; Revision ‘E,’ dated January 27, 

2005; or Revision ‘F,’ dated March 14, 

2007; also meets the requirements of 

paragraph (f)(2) of this AD for this 

particular Modsum. 

(6) Installation of Modsum 8Q101445, 

in accordance with Bombardier Service 

Bulletin 8–27–103, dated November 5, 

2003; or Revision ‘A,’ dated February 

12, 2004; also meets the requirements of 

paragraph (f)(3) of this AD. 

FAA AD Differences 

Note 2: This AD differs from the MCAI 

and/or service information as follows: No 

differences. 

Other FAA AD Provisions 

(g) The following provisions also 

apply to this AD: 

(1) Alternative Methods of 

Compliance (AMOCs): The Manager, 

New York Aircraft Certification Office 

(ACO), FAA, has the authority to 

approve AMOCs for this AD, if 

requested using the procedures found in 

14 CFR 39.19. Send information to 

ATTN: Ezra Sasson, Aerospace 

Engineer; New York ACO, FAA, 1600 

Stewart Avenue, Suite 410, Westbury, 

New York 11590; telephone (516) 228–

7320; fax (516) 794–5531. 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. 

(2) Airworthy Product: For any 

requirement in this AD to obtain 

corrective actions from a manufacturer 

or other source, use these actions if they 

are FAA-approved. Corrective actions 

are considered FAA-approved if they 

are approved by the State of Design 

Authority (or their delegated agent). You 

are required to assure the product is 

airworthy before it is returned to 

service. 

(3) Reporting Requirements: For any 

reporting requirement in this AD, under 

the provisions of the Paperwork 

Reduction Act, the Office of 

Management and Budget (OMB) has 

approved the information collection 

requirements and has assigned OMB 

Control Number 2120–0056. 

Related Information 

(h) Refer to MCAI Canadian 

Airworthiness Directive CF–2006–13, 

dated June 6, 2006; Bombardier Service 

Bulletin 8–27–89, Revision ‘G,’ dated 

April 12, 2007; and Bombardier Service 

Bulletin 8–27–103, Revision ‘B,’ dated 

January 24, 2007; for related 

information. 

Material Incorporated by Reference 

(i) You must use the service 

information specified in Table 1 of this 

AD 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 Bombardier, Inc., 

Bombardier Regional Aircraft Division, 

123 Garratt Boulevard, Downsview, 

Ontario M3K 1Y5, Canada. 

(3) You may review copies at the 

FAA, Transport Airplane Directorate, 

1601 Lind Avenue SW., Renton, 

Washington; 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 1.—MATERIAL INCORPORATED BY REFERENCE

Service bulletin Revision 

level Date 

Bombardier Service Bulletin 8–27–89 ............................................................................... ‘G’ April 12, 2007. 

Bombardier Service Bulletin 8–27–103 ............................................................................. ‘B’ January 24, 2007. 

Issued in Renton, Washington, on October 

9, 2007. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. E7–20217 Filed 10–16–07; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF COMMERCE 

Bureau of Industry and Security 

15 CFR Part 740 

License Exceptions 

CFR Correction 

In Title 15 of the Code of Federal 

Regulations, revised as of January 1, 

2007, on page 282, in Supplement No. 

1 To Part 740—Country Groups, in the 

table Country Group D, for the entry 

‘‘Korea, North,’’ the table is corrected by 

adding an X under the second column 

[D: 1] National Security. 

[FR Doc. 07–55513 Filed 10–16–07; 8:45 am] 

BILLING CODE 1505–01–D 


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