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Docket ID: [Docket No. 2002-NM-100-AD; Amendment 39-13070; AD 2003-04-21 R1]
RIN ID: RIN 2120-AA64
SUBJECT CATEGORY: Airworthiness Directives; Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes
The incorporation by reference of a certain publication, as listed in the regulations, was approved previously by the Director of the Federal Register as of April 4, 2003 (68 FR 9509, February 28, 2003).
DOCUMENT SUMMARY: This document corrects information in an existing airworthiness directive (AD) that applies to certain Bombardier Model CL6002B19 (Regional Jet Series 440) series airplanes. That AD currently requires replacement of the overwing emergency exit placards, door weight placards, and no baggage placards with new placards. This document corrects the applicability of AD 20030421 to identify affected model designations as published in the most recent type certificate data sheet. This correction is necessary to ensure that operators of all affected airplanes accomplish the requirements of this AD.
SUMMARY: Bombardier,
In the preamble of AD 20030421 under the heading ``Explanation of Change to Applicability,'' it states, ``[The FAA has] revised the applicability of the final rule to identify model designations as published in the most recent type certificate data sheet for the affected models.'' We revised the applicability of the final rule to include the parenthetical ``(Regional Jet Series 440).'' However, we inadvertently omitted Regional Jet Series ``100,'' which is specified on the type certificate data sheet. In addition, both of these airplane models were identified by serial numbers in the applicability. Therefore, the correct applicability of this AD is ``Bombardier Model CL6002B19 (Regional Jet Series 100 & 440) airplanes.''
We have determined that a correction to AD 20030421 is necessary. We have clarified the applicability of this AD by identifying the affected model designations as published in the most recent type certificate data sheet.
This document corrects the error and correctly adds the AD as an amendment to section 39.13 of the Federal Aviation Regulations (14 CFR 39.13).
The AD is reprinted in its entirety for the convenience of affected operators. The effective date of the AD remains April 4, 2003.
Since this action only corrects the applicability of AD 20030421 to identify affected model designations as published in the most recent type certificate data sheet, it has no adverse economic impact and imposes no additional burden on any person. Therefore, the FAA has determined that notice and public procedures are unnecessary. List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety.
Accordingly, pursuant to 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 39AIRWORTHINESS DIRECTIVES
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
2. Section 39.13 is amended by correctly adding the following airworthiness directive (AD):
20030421 R1 Bombardier, Inc. (Formerly Canadair): Amendment 39 13070. Docket 2002NM100AD.
Applicability: Model CL6002B19 (Regional Jet Series 100 & 440)
airplanes, certificated in any category, having the serial numbers listed in the following table:
TableSerial Numbers
Serial Nos.
7003 through 7434 inclusive.
7436 through 7442 inclusive.
7444 through 7452 inclusive.
7454 through 7458 inclusive.
7460 through 7497 inclusive.
Note 1: This AD applies to each airplane identified in the
preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the
requirements of this AD. For airplanes that have been modified,
altered, or repaired so that the performance of the requirements of
this AD is affected, the owner/operator must request approval for an
alternative method of compliance in accordance with paragraph (c) of
this AD. The request should include an assessment of the effect of
the modification, alteration, or repair on the unsafe condition
addressed by this AD; and, if the unsafe condition has not been
eliminated, the request should include specific proposed actions to address it.
Compliance: Required as indicated, unless accomplished previously.
To prevent the inability of a passenger to open and dispose of
the overwing emergency exit door during an emergency evacuation due to incorrect placards, accomplish the following:
Replacement of Placards
(a) Within 12 months after the effective date of this AD, replace the overwing emergency exit placards, door weight
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placards, and no baggage placards with new placards (including
cleaning of the applicable surface), as applicable, per Bombardier
Alert Service Bulletin A601R11077, Revision `A,' dated December
11, 2001, excluding Service Bulletin Comment SheetFacsimile Reply
Sheet and CRJ 100/200 Service Bulletin Compliance Facsimile Reply Sheet.
(b) Replacement accomplished before the effective date of this
AD per Bombardier Alert Service Bulletin A601R11077, dated July
12, 2001, is considered acceptable for compliance with the replacement specified in paragraph (a) of this AD.
Alternative Methods of Compliance
(c) 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, New York Aircraft Certification
Office (ACO), FAA. Operators shall submit their requests through an
appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, New York ACO.
Note 2: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be obtained from the New York ACO.
Special Flight Permits
(d) 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.
Incorporation by Reference
(e) Unless otherwise specified in this AD, the actions shall be
done in accordance with Bombardier Alert Service Bulletin A601R11
077, Revision `A,' dated December 11, 2001, excluding Service
Bulletin Comment SheetFacsimile Reply Sheet and CRJ 100/200 Service
Bulletin Compliance Facsimile Reply Sheet. This incorporation by
reference was approved previously by the Director of the Federal
Register as of April 4, 2003 (68 FR 9509, February 28, 2003). Copies
may be obtained from Bombardier, Inc., Canadair, Aerospace Group,
P.O. Box 6087, Station A, Montreal, Quebec H3C 3G9, Canada. Copies
may be inspected at the FAA, Transport Airplane Directorate, 1601
Lind Avenue, SW., Renton, Washington; or at the FAA, New York
Aircraft Certification Office, 10 Fifth Street, Third Floor, Valley
Stream, New York; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC.
Note 3: The subject of this AD is addressed in Canadian airworthiness directive CF200212, dated February 4, 2002.
Effective Date
(f) The effective date of this amendment remains April 4, 2003.
Issued in Renton, Washington, on March 17, 2003. Michael J. Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. 036992 Filed 32403; 8:45 am]
BILLING CODE 491013P
FOR FURTHER INFORMATION CONTACT Dan Parrillo, Aerospace Engineer, Systems and Flight Test Branch, ANE172, FAA, New York Aircraft Certification Office, 10 Fifth Street, Third Floor, Valley Stream, New York 11581; telephone (516) 2567505; fax (516) 5682716.
14 CFR Part 39 40 CFR Part 52 14 CFR Part 71 33 CFR Part 165 50 CFR Part 679 47 CFR Part 73 26 CFR Part 1 40 CFR Part 180 33 CFR Part 117 50 CFR Part 17 44 CFR Part 67 50 CFR Part 648 14 CFR Part 97 33 CFR Part 100 40 CFR Part 63 50 CFR Part 622 44 CFR Part 65 50 CFR Part 660 26 CFR Part 301 39 CFR Part 111 40 CFR Part 300 6 CFR Part 5 40 CFR Part 271 47 CFR Part 64 40 CFR Parts 52 and 81 50 CFR Part 665 44 CFR Part 64 10 CFR Part 50 49 CFR Part 571 47 CFR Part 76