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(c) This AD applies to Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440)
airplanes, certificated in any category; as identified in Bombardier Alert Service Bulletin A601R-35-
014, dated September 25, 2003; and Bombardier Service Bulletin 601R-35-016, dated September 8,
2005.
Unsafe Condition
(d) This AD results from several incidents, on certain airplane models, of incorrect installation of
the release pin into the safety pin hole of the activation mechanism of the chemical oxygen generator;
this resulted in failure to activate the chemical oxygen generator when required. A separate incident
occurred on a different airplane model during deployment of the cabin oxygen system, and resulted in
failure of the release pin to activate the oxygen generator at a flight attendant station. We are issuing
this AD to prevent failure of the activation mechanism of the chemical oxygen generator, which
could result in the unavailability of supplemental oxygen and possible incapacitation of passengers
and cabin crew during an in-flight decompression.
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.
Inspections/Corrective Action
(f) Do the detailed inspections for discrepancies of certain chemical oxygen generators of each
flight attendant and lavatory oxygen panel, as applicable, and each passenger service unit of the
passenger oxygen system, as specified in paragraphs (f)(1) and (f)(2) of this AD, as applicable.
(1) For airplanes identified in paragraph 1.A. of Bombardier Alert Service Bulletin A601R-35-
014, dated September 25, 2003: Within 550 flight hours after the effective date of this AD, do a onetime
inspection for correct alignment and engagement of the release pin with the lanyard tube in the
mask container module of the activation (firing) mechanism in the chemical oxygen generator by
doing all the actions, including all applicable corrective actions, in accordance with the
2007-03-11 2
14 BW 2007-04
Accomplishment Instructions of Bombardier Alert Service Bulletin A601R-35-014, dated September
25, 2003. Do all applicable corrective actions before further flight.
(2) For airplanes identified in paragraph 1.A. of Bombardier Service Bulletin 601R-35-016,
dated September 8, 2005: Within 1,100 flight hours after the effective date of this AD; do a one-time
inspection for correct installation of the release pin of the activation mechanism of the chemical
oxygen generator, by doing all the actions, including all applicable corrective actions, in accordance
with the Accomplishment Instructions of Bombardier Service Bulletin 601R-35-016, dated
September 8, 2005. Do all applicable corrective actions before further flight.
Note 1: For the purposes of this AD, a detailed inspection is: “An intensive examination of a
specific item, installation, or assembly to detect damage, failure, or irregularity. Available lighting is
normally supplemented with a direct source of good lighting at an intensity deemed appropriate.
Inspection aids such as mirror, magnifying lenses, etc., may be necessary. Surface cleaning and
elaborate procedures may be required.”
Note 2: Bombardier Service Bulletin 601R-35-016, dated September 8, 2005, refers to B/E
Aerospace Service Bulletin 117003-35-4, dated March 29, 2001, as an additional source of service
information for accomplishing the inspection and corrective action specified in paragraph (f) of this
AD.
Alternative Methods of Compliance (AMOCs)
(g)(1) The Manager, New York Aircraft Certification Office, FAA, has the authority to approve
AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19.
(2) Before using any AMOC approved in accordance with § 39.19 on any airplane to which the
AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate
Holding District Office.
Related Information
(h) Canadian airworthiness directive CF-2006-11, dated May 31, 2006, also addresses the subject
of this AD.
Material Incorporated by Reference
(i) You must use Bombardier Alert Service Bulletin A601R-35-014, dated September 25, 2003;
and Bombardier Service Bulletin 601R-35-016, dated September 8, 2005; as applicable; to perform
the actions that are required by this AD, unless the AD specifies otherwise. The Director of the
Federal Register approved the incorporation by reference of these documents in accordance with 5
U.S.C. 552(a) and 1 CFR part 51. Contact Bombardier, Inc., Canadair, Aerospace Group, P.O. Box
6087, Station Centre-ville, Montreal, Quebec H3C 3G9, Canada, for a copy of this service
information. You may review copies at the Docket Management Facility, U.S. Department of
　
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