Federal Register / Vol. 63, No. 85 / Monday, May 4, 1998 /Rules and Regulations 24389

(2) Revise the Limitations Section of the

FAA-approved Airplane Flight Manual

(AFM), in accordance with Note 1 of

Paragraph 1.C. of Shorts Service Bulletin

SD330–26–14, dated September 1994 (for

Shorts Model SD3–30 series airplanes), or

Shorts Service Bulletin SD360–26–11, dated

July 1994 (for Shorts Model SD3–60 series

airplanes), as applicable.

(c) For airplanes equipped with fire

extinguishers having part number (P/N)

BA51012SR–3 or BA51012SR: Within 6

months after the effective date of this AD,

accomplish either paragraph (c)(1) or (c)(2) of

this AD:

(1) Install a chamfered nozzle on the

discharge head assembly of each fire

extinguisher and add a new trigger by

replacing the discharge head assembly with

a new discharge head assembly, having P/N

BA22988–3, in accordance with Fire Fighting

Enterprises (U.K.) Ltd. Service Bulletin 26–

107, Revision 1, dated November 2, 1992.

Or

(2) Replace the trigger on the discharge

head assembly of each fire extinguisher with

a new trigger, in accordance with Fire

Fighting Enterprises (U.K.) Ltd. Service

Bulletin 26–108, dated September 1992. After

replacement, install a chamfered nozzle on

the discharge head assembly of each fire

extinguisher by reworking the discharge head

assembly in accordance with Fire Fighting

Enterprises (U.K.) Ltd. Service Bulletin 26–

107, Revision 1, dated November 2, 1992.

(d) An alternative method of compliance or

adjustment of the compliance time that

provides an acceptable level of safety may be

used if approved by the Manager,

International Branch, ANM–116, FAA,

Transport Airplane Directorate. Operators

shall submit their requests through an

appropriate FAA Principal Maintenance

Inspector, who may add comments and then

send it to the Manager, International Branch,

ANM–116.

Note 2: Information concerning the

existence of approved alternative methods of

compliance with this AD, if any, may be

obtained from the International Branch,

ANM–116.

(e) Special flight permits may be issued in

accordance with sections 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 accomplished.

(f) The actions shall be done in accordance

with Short Brothers Shorts Service Bulletin

SD330–26–14, dated September 1994; Short

Brothers Shorts Service Bulletin SD360–26–

11, dated July 1994; Fire Fighting Enterprises

(U.K.) Ltd. Service Bulletin 26–107, Revision

1, dated November 2, 1992; and Fire Fighting

Enterprises (U.K.) Ltd. Service Bulletin 26–

108, dated September 1992; as applicable.

This incorporation by reference was

approved by the Director of the Federal

Register in accordance with 5 U.S.C. 552(a)

and 1 CFR part 51. Copies may be obtained

from Short Brothers (USA), Inc., Civil

Technical Operations, P.O. Box 211 (Route

76 East), Bridgeport, West Virginia 26330.

Copies may be inspected at the FAA,

Transport Airplane Directorate, 1601 Lind

Avenue, SW., Renton, Washington; or at the

Office of the Federal Register, 800 North

Capitol Street, NW., suite 700, Washington,

DC.

(g) This amendment becomes effective on

June 8, 1998.

Issued in Renton, Washington, on April 22,

1998.

Gary L. Killion,

Acting Manager, Transport Airplane

Directorate, Aircraft Certification Service.

[FR Doc. 98–11302 Filed 5–1–98; 8:45 am]

BILLING CODE 4910–13–U

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 98–NM–05–AD; Amendment

39–10458]

RIN 2120–AA64

Airworthiness Directives; Bombardier

Model CL–215–1A10 and CL–215–6B11

Series Airplanes; Correction

AGENCY: Federal Aviation

Administration, DOT.

ACTION: Direct final rule; correction.

SUMMARY: This document corrects an

error that appeared in amendment 39–

10458 that was published in the Federal

Register on April 10, 1998 (63 FR

17672). The error resulted in the

inadvertent omission of the

applicability statement of the

amendment. This amendment is

applicable to certain Bombardier Model

CL–215–1A10 and CL–215–6B11 series

airplanes. This amendment requires

repetitive inspections to detect cracking

on certain wing to fuselage frameangles, and repair, if necessary.

DATES: Effective July 9, 1998.

The incorporation by reference of

certain publications listed in the

regulations was previously approved by

the Director of the Federal Register as

of July 9, 1998 (63 FR 17672, April 10,

1998).

FOR FURTHER INFORMATION CONTACT:

Serge Napoleon, Aerospace Engineer,

Airframe and Propulsion Branch, ANE–

171, FAA, Engine and Propeller

Directorate, New York Aircraft

Certification Office, 10 Fifth Street,

Third Floor, Valley Stream, New York

11581; telephone (516) 256–7512; fax

(516) 568–2716.

SUPPLEMENTARY INFORMATION:

Amendment 39–10458, applicable to

certain Bombardier Model CL–215–

1A10 and CL–215–6B11 series

airplanes, was published in the Federal

Register on April 10, 1998 (63 FR

17672). That amendment requires

repetitive inspections to detect cracking

on certain wing to fuselage frameangles, and repair, if necessary.

As published, the applicability

statement of the amendment was

omitted inadvertently. The FAA has

determined that this omission must be

corrected. In all other respects, the

original document is correct.

Since no other part of the regulatory

information has been changed, the

direct final rule is not being

republished.

The effective date of this amendment

remains July 9, 1998.

§ 39.13 [Corrected]

1. On page 17674, in the first column,

the airworthiness directive, amendment

39–10458, is corrected by adding the

applicability statement preceding Note 1

to read as follows:

* * * * *

Applicability: Model CL–215–1A10 and

CL–215–6B11 series airplanes, serial

numbers 1001 through 1125 inclusive,

certificated in any category.

* * * * *

Issued in Renton, Washington, on April 24,

1998.

Gary L. Killion,

Acting Manager, Transport Airplane

Directorate, Aircraft Certification Service.

[FR Doc. 98–11560 Filed 5–1–98; 8:45 am]

BILLING CODE 4910–13–U

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 71

[Airspace Docket No. 97–ANM–24]

Amendment of Class D Airspace; Twin

Falls, ID

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

published on February 25, 1998 (63 FR

9409) which changed the name of the

airport in the Twin Fall, ID, Class D

airspace legal description. During a

review of Idaho airspace, it was

discovered that the airport name needed

updating because it was changed from

Twin Falls-Sun Valley Regional, Joslin

Field to Joslin Field-Magic Valley

Regional. This rule also updated the

coordinates for the airport.

EFFECTIVE DATE: The direct final rule

published at 63 FR 9409 is effective

0910 UTC, May 26, 1998.

FOR FURTHER INFORMATION CONTACT: