Adoption of the Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
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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]
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2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive (AD):
2018-20-11 Bombardier, Inc.: Amendment 39-19445; Docket No. FAA-
2018-0586; Product Identifier 2017-NM-151-AD.
(a) Effective Date
This AD is effective November 23, 2018.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc., Model DHC-8-301, -311, and
-315 airplanes, certificated in any category, serial numbers 100
through 672 inclusive.
(d) SubjectAir Transport Association (ATA) of America Code 52, Doors.
(e) Reason
This AD was prompted by reports indicating that the forward
right-hand type I emergency exit door could not be opened during
maintenance. An investigation determined that the exit door handle
was jammed due to corroded center and lower shaft ball bearings. We
are issuing this AD to address corrosion of the emergency exit door
ball bearings, which could result in the inability to open the
emergency exit door
[[Page 52756]]
during an emergency evacuation and consequently impede airplane
egress.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Revision of Maintenance or Inspection Program
Within 60 days after the effective date of this AD: Revise the
maintenance or inspection program, as applicable, to incorporate de
Havilland Inc. Dash 8 Series 300 Maintenance Task Card Task Number
5220/12 (``Servicing of Forward RH Emergency Exit Mechanisms''),
dated March 15, 2017; and Temporary Revision 54-042, dated April 10,
2018, to the DHC-8-300 Aircraft Maintenance Manual (AMM). The
initial compliance time for doing the task is at the time specified
in de Havilland Inc. Dash 8 Series 300 Maintenance Task Card Task
Number 5220/12 (``Servicing of Forward RH Emergency Exit
Mechanisms''), dated March 15, 2017, or within 60 days after the
effective date of this AD, whichever occurs later.
(h) Inspection and Replacement
Within 5,000 flight hours or 36 months, whichever occurs first,
after the effective date of this AD: Do a detailed inspection of all
ball bearings of the forward right-hand type I emergency exit for
corrosion, seal damage, and loss of lubricant; replace bearings as
applicable; and apply corrosion inhibiting compound (CIC); in
accordance with the Accomplishment Instructions of Bombardier
Service Bulletin 8-52-65, dated July 26, 2017. Do all applicable
replacements before further flight.
(i) No Alternative Actions or Intervals
After the maintenance or inspection program has been revised as
required by paragraph (g) of this AD, no alternative actions (e.g.,
inspections) or intervals may be used unless the actions and
intervals are approved as an alternative method of compliance (AMOC)
in accordance with the procedures specified in paragraph (j)(1) of
this AD.
(j) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, New
York ACO Branch, FAA, has the authority to approve AMOCs for this
AD, if requested using the procedures found in 14 CFR 39.19. In
accordance with 14 CFR 39.19, send your request to your principal
inspector orlocal Flight Standards District Office, as appropriate.
If sending information directly to the manager of the certification
office, send it to ATTN: Program Manager, Continuing Operational
Safety, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516-228-7300; fax 516-794-5531. Before
using any approved AMOC, notify your appropriate principal
inspector, or lacking a principal inspector, the manager of the
local flight standards district office/certificate holding district
office.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain corrective actions from a manufacturer, the action must be
accomplished using a method approved by the Manager, New York ACO
Branch, FAA; or Transport Canada Civil Aviation (TCCA); or
Bombardier, Inc.'s TCCA Design Approval Organization (DAO). If
approved by the DAO, the approval must include the DAO-authorized
signature.
(k)Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) Canadian Airworthiness Directive CF-2017-30, dated August 30,
2017, for related information. This MCAI may be found in the AD
docket on the internet at http://www.regulations.gov by searching
for and locating Docket No. FAA-2018-0586.
(2) For more information about this AD, contact Darren Gassetto,
Aerospace Engineer, Airframe and Propulsion Section, FAA, New York
ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone 516-228-7323; fax 516-794-5531; email
[email protected].
(l) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(i) Bombardier Service Bulletin 8-52-65, dated July 26, 2017.
(ii) de Havilland Inc. Dash 8 Series 300 Maintenance Task Card
Task Number 5220/12 (``Servicing of Forward RH Emergency Exit
Mechanisms''), dated March 15, 2017.
(iii) Temporary Revision (TR) 54-042, dated April 10, 2018, to
the DHC-8-300 Aircraft Maintenance Manual (AMM).
(3) For service information identified in this AD, contact
Bombardier, Inc., Q-Series Technical Help Desk, 123 Garratt
Boulevard, Toronto, Ontario M3K 1Y5, Canada; telephone 416-375-4000;
fax 416-375-4539; email
[email protected]; internet
http://www.bombardier.com.
(4) You may view this service information at the FAA, Transport
Standards Branch, 2200 South 216th St., Des Moines, WA. For
information on the availability of this material at the FAA, call
206-231-3195.
(5) You may view this service information that is incorporated
by reference 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.