FR Doc E7-10035

[Federal Register: May 25, 2007 (Volume 72, Number 101)]
[Rules and Regulations]
[Page 29239-29241]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr25my07-2]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2007-27016; Directorate Identifier 2006-NM-176-AD;
Amendment 39-15066; AD 2007-11-09]
RIN 2120-AA64

Airworthiness Directives; Bombardier Model DHC-8-400 Series
Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).

ACTION: Final rule.

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SUMMARY: The FAA is superseding an existing airworthiness directive
(AD), which applies to certain Bombardier Model DHC-8-400 series
airplanes. That AD currently requires inspecting the electrical
connectors of the fire bottles for the forward and aft baggage
compartments and for the auxiliary power unit (APU) and engine nacelles
to determine if they are connected correctly, and doing related
investigative and corrective actions if necessary. This new AD adds a
requirement to install/modify lanyards, mounts, and clamps to the
forward and aft baggage compartment, APU, and engine nacelle fire
extinguishing systems. This new AD also requires revising the aircraft
maintenance manual to incorporate installation and removal procedures
for certain fire bottles and fire extinguisher cartridges. This new AD
also adds two airplanes to the applicability. This AD results from
reports of the electrical connectors for the fire bottles in the
forward and aft baggage compartments, APU, and engine nacelle being
cross-connected. We are issuing this AD to detect and correct cross-
connection of the fire bottles and to prevent cross-connection, which
could result in failure of the fire bottles to discharge and consequent
inability to extinguish a fire in the affected areas.

DATES: This AD becomes effective June 29, 2007.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in the AD as of June 29, 2007.
On July 5, 2005 (70 FR 35172, June 17, 2005), the Director of the
Federal Register approved the incorporation by reference of Bombardier
Alert Service Bulletin A84-26-06, dated May 12, 2005.

ADDRESSES: You may examine the AD docket on the Internet at http://dms.dot.gov
or in person at the Docket Management Facility, U.S.

Department of Transportation, 400 Seventh Street, SW., Nassif Building,
Room PL-401, Washington, DC.
Contact Bombardier, Inc., Bombardier Regional Aircraft Division,
123 Garratt Boulevard, Downsview, Ontario M3K 1Y5, Canada, for service
information identified in this AD.

FOR FURTHER INFORMATION CONTACT: Ezra Sasson, Aerospace Engineer,
Systems and Flight Test Branch, ANE-172, FAA, New York Aircraft
Certification Office, 1600 Stewart Avenue, Suite 410, Westbury, New
York 11590; telephone (516) 228-7320; fax (516) 794-5531.

SUPPLEMENTARY INFORMATION:

Examining the Docket

You may examine the airworthiness directive (AD) docket on the
Internet at http://dms.dot.gov or in person at the Docket Management

Facility office between 9 a.m. and 5 p.m., Monday through Friday,
except Federal holidays. The Docket Management Facility office
(telephone (800) 647-5227) is located on the plaza level of the Nassif
Building at the street address stated in the ADDRESSES section.

Discussion

The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to include an AD that supersedes AD 2005-12-17, amendment
39-14133 (70 FR 35172, June 17, 2005). The existing AD applies to
certain Bombardier Model DHC-8-400 series airplanes. That NPRM was
published in the Federal Register on January 26, 2007 (72 FR 3756).
That NPRM proposed to require inspecting the electrical connectors of
the fire bottles for the forward and aft baggage compartments and for
the auxiliary power unit (APU) and engine nacelles to determine if they
are connected correctly; and doing related investigative and corrective
actions, if necessary. That NPRM proposed to add a requirement to
install/modify lanyards, mounts, and clamps to the forward and aft
baggage compartment, APU, and engine nacelle fire extinguishing
systems. That NPRM also proposed to require installation and removal
procedures for certain fire bottles and fire extinguisher cartridges.
That NPRM also proposed to add two airplanes to the applicability.

Comments

We provided the public the opportunity to participate in the
development of this AD. No comments have been received on the NPRM or
on the determination of the cost to the public.

Change to Installation and Removal Requirement

We have revised the requirement specified in paragraph (h) of the
NPRM. Paragraph (h) of the NPRM specifies to do certain installations
and removals of the fire bottles and cartridges in accordance with a
method approved by the FAA or Transport Canada Civil Aviation (or its
delegated agent). Paragraph (h) of the NPRM also specifies that
Bombardier Dash 8 Series 400 Aircraft Maintenance Manual, Product
Support Manual (PSM) 1-84-2, Revision 22, dated June 5, 2006, is one
approved method.
We have determined that operators need to only revise the FAA-
approved maintenance program to incorporate the information for those
installations and removals of the fire bottles and cartridges specified
in Bombardier Dash 8 Series 400 Aircraft Maintenance Manual, Product
Support Manual (PSM) 1-84-2, Revision 22, dated June 5, 2006. This will
place less of a burden on operators because operators will not need to
make a maintenance log entry to show compliance every time one of the
installations or removals is done. We have revised paragraph (h) of
this AD accordingly.

Clarification of Alternative Method of Compliance (AMOC) Paragraph

We have revised this action to clarify the appropriate procedure
for notifying the principal inspector before using any approved AMOC on
any airplane to which the AMOC applies.

Conclusion

We have carefully reviewed the available data and determined that
air safety and the public interest require adopting the AD with the
changes described previously. We have determined that these changes
will neither increase the economic burden on any operator nor increase
the scope of the AD.

Costs of Compliance

The following table provides the estimated costs for U.S. operators
to comply with this AD.

[[Page 29240]]

Estimated Costs
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Number of U.S.-
Action Work hours Average labor Parts Cost per registered Fleet cost
rate per hour airplane airplanes
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Inspection (required by AD 2005-12- 2 $80 $0..................... $160 19 $3,040.
17).
Modification (new action)........... 4 80 Up to $200............. 520 21 Up to $10,920.
Revision............................ 1 80 0...................... 80 19 $1,520.
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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 this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866;
(2) Is not a ``significant rule'' under 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 regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD docket. See the ADDRESSES
section for a location to examine the regulatory evaluation.

List of Subjects in 14 CFR Part 39

Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.

Adoption of the Amendment

0
Accordingly, under the authority delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

Authority: 49 U.S.C. 106(g), 40113, 44701.

Sec. 39.13 [Amended]

0
2. The Federal Aviation Administration (FAA) amends Sec. 39.13 by
removing amendment 39-14133 (70 FR 35172, June 17, 2005) and by adding
the following new airworthiness directive (AD):

2007-11-09 Bombardier, Inc. (Formerly de Havilland, Inc.): Amendment
39-15066. Docket No. FAA-2007-27016; Directorate Identifier 2006-NM-
176-AD.

Effective Date

(a) This AD becomes effective June 29, 2007.

Affected ADs

(b) This AD supersedes AD 2005-12-17.

Applicability

(c) This AD applies to Bombardier Model DHC-8-400 series
airplanes, certificated in any category; serial numbers (S/Ns) 4001
through 4107 inclusive.

Unsafe Condition

(d) This AD results from reports of the electrical connectors
for the fire bottles in the forward and aft baggage compartments,
auxiliary power unit (APU), and engine nacelle being cross-
connected. We are issuing this AD to detect and correct cross-
connection of the fire bottles and to prevent cross-connection,
which could result in failure of the fire bottles to discharge and
consequent inability to extinguish a fire in the affected areas.

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.

Restatement of Requirements of AD 2005-12-17

Inspection and Corrective Action

(f) For airplanes having S/Ns 4001 through 4105 inclusive:
Within 14 days after July 5, 2005 (the effective date of AD 2005-12-
17), inspect the electrical connectors of the fire bottles for the
forward and aft baggage compartments and for the APU and engine
nacelles to determine if they are connected correctly; and, before
further flight, do the related investigative and corrective actions,
as applicable; by doing all of the applicable actions specified in
the Accomplishment Instructions of Bombardier Alert Service Bulletin
A84-26-06, dated May 12, 2005; or Revision `A,' dated June 6, 2005.
Although the service bulletins specify to submit certain information
to the manufacturer, this AD does not include that requirement.

New Requirements of This AD

Installation/Modification

(g) For all airplanes: Within 5,000 flight hours after the
effective date of this AD, install/modify lanyards, mounts, and
clamps to the forward and aft baggage compartment, APU, and engine
nacelle fire extinguishing systems by doing all the actions
specified in the Accomplishment Instructions of Bombardier Service
Bulletin 84-26-07, Revision `B,' dated November 1, 2006.

Revision of Aircraft Maintenance Manual

(h) For airplanes having S/Ns 4001 through 4105 inclusive:
Within 30 days after the effective date of this AD, incorporate the
information in the page blocks of Bombardier Dash 8 Series 400
Aircraft Maintenance Manual (AMM), Product Support Manual (PSM) 1-
84-2, Revision 22, dated June 5, 2006, specified in paragraphs
(h)(1), (h)(2), (h)(3), (h)(4), (h)(5), (h)(6), and (h)(7) of this
AD, into the FAA-approved maintenance program to specify an
installation and removal of nacelle fire bottles, an installation of
aft high-rate fire bottles, an installation of forward high-rate
fire bottles, an installation and removal of low-rate fire bottles,
an installation of APU fire bottles, an installation and removal of
low-rate fire extinguisher cartridges, and an installation and
removal of nacelle fire extinguisher cartridges, in accordance with
a method approved by either the Manager, New York Aircraft
Certification Office (ACO), FAA; or Transport Canada Civil Aviation
(or its delegated agent). The page blocks of the Bombardier Dash 8
Series 400 AMM specified in paragraphs (h)(1), (h)(2), (h)(3),
(h)(4), (h)(5), (h)(6), and (h)(7) of this AD, are one approved
method for the actions required by this paragraph.
(1) Chapter 26-21-01, Page Block 401, dated December 5, 2005.
(2) Chapter 26-21-06, Page Block 401, dated December 5, 2005.
(3) Chapter 26-22-02, Page Block 401, dated December 5, 2005.

[[Page 29241]]

(4) Chapter 26-22-03, Page Block 401, dated December 5, 2005.
(5) Chapter 26-22-11, Page Block 401, dated December 5, 2005.
(6) Chapter 26-22-16, Page Block 401, dated December 5, 2005.
(7) Chapter 26-23-01, Page Block 401, dated December 5, 2005.

Actions Accomplished According to Previous Issue of Service Bulletin

(i) Actions accomplished before the effective date of this AD in
accordance with Bombardier Service Bulletin 84-26-07, dated June 15,
2005; and Revision `A,' dated February 21, 2006; are considered
acceptable for compliance with the corresponding action specified in
paragraph (g) of this AD, provided the intended restriction of the
connectors was done as specified in Bombardier Service Bulletin 84-
26-07, Revision `B,' dated November 1, 2006.

Alternative Methods of Compliance (AMOCs)

(j)(1) The Manager, New York ACO, FAA, has the authority to
approve AMOCs for this AD, if requested in accordance with the
procedures found in 14 CFR 39.19.
(2) To request a different method of compliance or a different
compliance time for this AD, follow the procedures 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.

Related Information

(k) Canadian airworthiness directive CF-2005-14R1, dated May 8,
2006, also addresses the subject of this AD.

Material Incorporated by Reference

(l) You must use the service information identified in Table 1
of this AD to perform the actions that are required by this AD,
unless the AD specifies otherwise.

Table 1.--All Material Incorporated by Reference
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Bombardier Service Bulletin Revision level Date
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A84-26-06..................... Original...... May 12, 2005.
A84-26-06..................... `A'........... June 6, 2005.
84-26-07...................... `B'........... November 1, 2006.
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(1) The Director of the Federal Register approved the
incorporation by reference of Bombardier Alert Service Bulletin A84-
26-06, Revision `A,' dated June 6, 2005; and Bombardier Service
Bulletin 84-26-07, Revision `B,' dated November 1, 2006; in
accordance with 5 U.S.C. 552(a) and 1 CFR part 51.
(2) On July 5, 2005 (70 FR 35172, June 17, 2005), the Director
of the Federal Register approved the incorporation by reference of
Bombardier Alert Service Bulletin A84-26-06, dated May 12, 2005.
(3) Contact Bombardier, Inc., Bombardier Regional Aircraft
Division, 123 Garratt Boulevard, Downsview, Ontario M3K 1Y5, Canada,
for a copy of this service information. 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
.

Issued in Renton, Washington, on May 15, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E7-10035 Filed 5-24-07; 8:45 am]

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