AD Amdt-39-16179 - Airworthiness Directives; AVOX Systems and B/E Aerospace Oxygen Cylinder Asse...

Type	Manufacturer	Model	Details
aircraft	AVOX	Various	Airworthiness Directives; AVOX Systems and B/E Aerospace Oxygen Cylinder Assemblies, as Installed on Various Transport Airplanes

Unsafe Condition

Rupture of a high-pressure gaseous oxygen cylinder due to insufficient strength characteristics caused by improper heat treatment.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Remove certain oxygen cylinder assemblies from the airplane as specified in the AD.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Before further flight

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

AVOX Systems and B/E Aerospace oxygen cylinder assemblies, as installed on various transport airplanes, approved under United States Department of Transportation Regulations for Type 3HT cylinders, identified in Table 1 of the AD.

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

The FAA is revising an existing airworthiness directive (AD), which applies to certain AVOX Systems and B/E Aerospace oxygen cylinder assemblies, as installed on various transport airplanes. That AD currently requires removing certain oxygen cylinder assemblies from the airplane. This AD removes certain oxygen cylinder part numbers from the applicability. This AD was prompted by the reported rupture of a high- pressure gaseous oxygen cylinder, which had insufficient strength characteristics due to improper heat treatment. We are issuing this AD to prevent an oxygen cylinder from rupturing, which, depending on the location, could result in structural damage and rapid decompression of the airplane, damage to adjacent essential flight equipment, deprivation of the necessary oxygen supply for the flightcrew, and injury to cabin occupants or maintenance or other support personnel.

Document Text

Show stored source text (verify against official source)

[Federal Register Volume 75, Number 12 (Wednesday, January 20, 2010)]
[Rules and Regulations]
[Pages 3141-3143]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2010-937]

-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2010-0029; Directorate Identifier 2009-NM-262-AD;
Amendment 39-16179; AD 2009-21-10 R1]
RIN 2120-AA64

Airworthiness Directives; AVOX Systems and B/E Aerospace Oxygen
Cylinder Assemblies, as Installed on Various Transport Airplanes

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

ACTION: Final rule; request for comments.

-----------------------------------------------------------------------

SUMMARY: The FAA is revising an existing airworthiness directive (AD),
which applies to certain AVOX Systems and B/E Aerospace oxygen cylinder
assemblies, as installed on various transport airplanes. That AD
currently requires removing certain oxygen cylinder assemblies from the
airplane. This AD removes certain oxygen cylinder part numbers from the
applicability. This AD was prompted by the reported rupture of a high-
pressure gaseous oxygen cylinder, which had insufficient strength
characteristics due to improper heat treatment. We are issuing this AD
to prevent an oxygen cylinder from rupturing, which, depending on the
location, could result in structural damage and rapid decompression of
the airplane, damage to adjacent essential flight equipment,
deprivation of the necessary oxygen supply for the flightcrew, and
injury to cabin occupants or maintenance or other support personnel.

DATES: This AD is effective February 4, 2010.
We must receive any comments on this AD by March 8, 2010.

ADDRESSES: You may send comments by any of the following methods:
<bullet> Federal eRulemaking Portal: Go to <a href="http://www.regulations.gov">http://www.regulations.gov</a>. Follow the instructions for submitting comments.
<bullet> Fax: 202-493-2251.
<bullet> Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590.
<bullet> Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590, between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.

Examining the AD Docket

You may examine the AD docket on the Internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a>; or in person at the Docket Management Facility
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains this AD, the regulatory evaluation,
any comments received, and other information. The street address for
the Docket Office (telephone 800-647-5527) is in the ADDRESSES section.
Comments will be available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Nicholas Wilson, Aerospace Engineer,
Cabin Safety and Environmental Systems Branch, ANM-150S, Seattle
Aircraft Certification Office, FAA, 1601 Lind Avenue, SW., Renton,
Washington 98057-3356; telephone (425) 917-6476; fax (425) 917-6590.

SUPPLEMENTARY INFORMATION:

Discussion

On November 25, 2009, we issued AD 2009-21-10, amendment 39-16049
(74 FR 63063, December 2, 2009). That AD applies to certain AVOX
Systems and B/E Aerospace oxygen cylinder assemblies, as installed on
various transport airplanes. That AD requires removing certain oxygen
cylinder assemblies from the airplane. That AD was prompted by the
reported rupture of a high-pressure gaseous oxygen cylinder, which had
insufficient strength characteristics due to improper heat treatment.
The actions specified in that AD are intended to prevent an oxygen
cylinder from rupturing, which, depending on the location, could result
in structural damage and rapid decompression of the airplane, damage to
adjacent essential flight equipment, deprivation of the necessary
oxygen supply for the flightcrew, and injury to cabin occupants or
maintenance or other support personnel.

Actions Since AD Was Issued

Since we issued AD 2009-21-10, we have been notified that its
applicability (in paragraph (c)) erroneously includes oxygen cylinder
assemblies having part numbers B43570-3 and B43570-5. Those oxygen
cylinder assemblies are manufactured from composite material, instead
of steel, and the erroneous part numbers do not correspond to any
serial numbers listed in the AD. Composite oxygen tanks are not subject
to the identified unsafe condition. These part numbers have been
removed from Table 1 of this AD.
We have also been notified that serial numbers K617383 through
K617423 inclusive and K757064 through K757066 inclusive have been
withdrawn from service. These serial numbers have been removed from
Table 3 of this AD.

FAA's Determination and Requirements of This AD

Certain affected airplanes have been approved by the aviation
authorities of other countries, and are approved for operation in the
United States.
The unsafe condition described previously is likely to exist or
develop in other products of these same type designs. For this reason,
we are issuing this AD to revise AD 2009-21-10. This new AD retains the
requirements of the existing AD, but removes part numbers B43570-3 and
B43570-5 from the applicability of this AD, and removes certain serial
numbers from Table 3 of this AD.

Additional Change to AD

We have revised this AD to identify the legal name of certain
manufacturers as published in the most recent type certificate data
sheet for the affected airplane models.

FAA's Justification and Determination of the Effective Date

This AD addresses the consequences of the potential rupture of
certain oxygen cylinder assemblies. Because of our requirement to
promote safe flight of civil aircraft and thus the critical need to
ensure the proper functioning of the oxygen cylinders and the short
compliance time involved with this action, this AD must be issued
immediately.
Because an unsafe condition exists that requires the immediate
adoption of

[[Page 3142]]

this AD, we find that notice and opportunity for prior public comment
hereon are impracticable and that good cause exists for making this
amendment effective in less than 30 days.

Comments Invited

This AD is a final rule that involves requirements affecting flight
safety, and we did not provide you with notice and an opportunity to
provide your comments before it becomes effective. However, we invite
you to send any written data, views, or arguments about this AD. Send
your comments to an address listed under the ADDRESSES section. Include
``Docket No. FAA-2010-0029; Directorate Identifier 2009-NM-262-AD'' at
the beginning of your comments. We specifically invite comments on the
overall regulatory, economic, environmental, and energy aspects of this
AD. We will consider all comments received by the closing date and may
amend this AD because of those comments.
We will post all comments we receive, without change, to <a href="http://www.regulations.gov">http://www.regulations.gov</a>, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this AD.

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 the regulation:
1. Is not a ``significant regulatory action'' under Executive Order
12866;
2. Is not a ``significant rule'' under the 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, Safety.

Adoption of the Amendment

0
Accordingly, under the authority delegated to me by the Administrator,
the FAA amends part 39 of the Federal Aviation Regulations (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 FAA amends Sec. 39.13 by removing amendment 39-16049 (74 FR
63063, December 2, 2009) and adding the following new AD:

2009-21-10 R1 AVOX Systems and B/E Aerospace: Amendment 39-16179.
Docket No. FAA-2010-0029; Directorate Identifier 2009-NM-262-AD.

Effective Date

(a) This airworthiness directive (AD) is effective February 4,
2010.

Affected ADs

(b) This AD revises AD 2009-21-10, Amendment 39-16049.

Applicability

(c) This AD applies to the oxygen cylinder assemblies, approved
under United States Department of Transportation Regulations for
Type 3HT cylinders, identified in Table 1 of this AD. These oxygen
cylinder assemblies may be installed on various transport airplanes,
certificated in any category, identified in but not limited to the
airplanes included in Table 2 of this AD.

Table 1--Affected Oxygen Cylinder Assembly Part Numbers
------------------------------------------------------------------------
Manufacturer Part Nos.
------------------------------------------------------------------------
AVOX Systems........................... 6350A34 series*
800112-03
800112-10
800112-13
801293-03
801307-00
801307-01
801307-02
801307-03
801307-07
801307-09
801307-23
801307-24
801365-04
801365-14
801375-00
801977-05
8915 series*
B/E Aerospace.......................... 176018-115
176112-115
176177-115
176181-115
176529-97
------------------------------------------------------------------------
(*For example, 6350A34-X-X or 8915XX-XX, where ``X'' denotes a part
number digit.)

Table 2--Affected Airplanes
------------------------------------------------------------------------
Manufacturer Model
------------------------------------------------------------------------
Airbus....................... A300 B4-620, B4-622, B4-605R, and F4-605R
airplanes.
A310-203, -204, -221, -222, -304, and -
324 airplanes.
A318-111 and -112 airplanes.
A319-111, -112, -113, -114, -115, -131, -
132, and -133 airplanes.
A320-111, -211, -212, -214, -231, -232,
and -233 airplanes.
A321-111, -112, -131, -211, and -231
airplanes.
A330-301, -321, and -322 airplanes.
A340-211 and -212 airplanes.
A340-311 and -312 airplanes.

[[Page 3143]]

The Boeing Company........... 707-100 long body, -200, -100B long body,
and -100B short body series airplanes;
and 707-300, -300B, -300C, and -400
series airplanes.
727, 727C, 727-100, 727-100C, 727-200,
and 727-200F series airplanes.
737-100, -200, -200C, -300, -400, -500, -
600, -700, -700C, -800, -900, and -900ER
series airplanes.
747-100, 747-100B, 747-100B SUD, 747-
200B, 747-200C, 747-200F, 747-300, 747-
400, 747-400D, 747-400F, 747SR, and
747SP series airplanes.
757-200, -200PF, -200CB, and -300 series
airplanes.
767-200, -300, -300F, and -400ER series
airplanes.
777-200, -200LR, -300, -300ER, and 777F
series airplanes.
Gulfstream Aerospace G-IV airplanes.
Corporation.
McDonnell Douglas Corporation DC-8-11, DC-8-12, DC-8-21, DC-8-31, DC-8-
32, DC-8-33, DC-8-41, DC-8-42, DC-8-43,
DC-8-51, DC-8-52, DC-8-53, and DC-8-55
airplanes.
DC-9-11, DC-9-12, DC-9-13, DC-9-14, DC-9-
15, DC-9-15F, DC-9-21, DC-9-31, DC-9-32,
DC-9-32 (VC-9C), DC-9-32F, DC-9-32F (C-
9A, C-9B), DC-9-33F, DC-9-34, DC-9-34F,
DC-9-41, DC-9-51, DC-9-81 (MD-81), DC-9-
82 (MD-82), DC-9-83 (MD-83), and DC-9-87
(MD-87) airplanes.
DC-10-10, DC-10-10F, DC-10-15, DC-10-30,
DC-10-30F (KC-10A and KDC-10), and DC-10-
40 airplanes.
MD-10-10F and MD-10-30F airplanes.
MD-11 and MD-11F airplanes.
MD-88 airplanes.
MD-90-30 airplanes.
Short Brothers PLC........... SD3-30, SD3-SHERPA, and SD3-60 SHERPA
airplanes.
------------------------------------------------------------------------

Subject

(d) Air Transport Association (ATA) of America Code 35: Oxygen.

Unsafe Condition

(e) This AD was prompted by the reported rupture of a high-
pressure gaseous oxygen cylinder, which had insufficient strength
characteristics due to improper heat treatment. The Federal Aviation
Administration is issuing this AD to prevent an oxygen cylinder from
rupturing, which, depending on the location, could result in
structural damage and rapid decompression of the airplane, damage to
adjacent essential flight equipment, deprivation of the necessary
oxygen supply for the flightcrew, and injury to cabin occupants or
maintenance or other support personnel.

Compliance

(f) 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 2009-21-10, With Revised Serial
Numbers

Inspection

(g) Within 90 days after December 17, 2009 (the effective date
of AD 2009-21-10), inspect to determine the serial number of the
oxygen cylinder assemblies installed in the airplane. The serial
number is stamped into the steel cylinder near the neck. A review of
airplane records is acceptable in lieu of this inspection if the
serial numbers of the oxygen cylinder assemblies can be conclusively
determined from that review. For any oxygen cylinder assembly that
has a serial number identified in Table 3 of this AD: Remove it from
the airplane before further flight.

Table 3--Affected Oxygen Cylinder Assembly Serial Numbers
------------------------------------------------------------------------
Cylinder manufacturer Affected Serial Nos.
------------------------------------------------------------------------
AVOX Systems.......................... ST82307 through ST82309
inclusive.
ST82335 through ST82378
inclusive.
ST82385 through ST82506
inclusive, except for S/N
ST82498, which ruptured.
ST82550 through ST82606
inclusive.
ST82617 through ST82626
inclusive.
ST83896 through ST83905
inclusive.
ST84209 through ST84218
inclusive.
ST84224 through ST84236
inclusive.
ST86138.
ST86143.
ST86145.
ST86150.
ST86169.
ST86172.
ST86177.
ST86299 through ST86307
inclusive.
B/E Aerospace......................... K495120 through K495121
inclusive.
K629573 through K629577
inclusive.
K674451 through K674455
inclusive.
------------------------------------------------------------------------

Parts Installation

(h) As of December 17, 2009, no person may install, on any
airplane, a United States Department of Transportation Type 3HT
oxygen cylinder assembly that has a part number identified in Table
1 of this AD and a serial number identified in Table 3 of this AD.

Alternative Methods of Compliance (AMOCs)

(i)(1) The Manager, Seattle Aircraft Certification Office, FAA,
has the authority to approve AMOCs for this AD, if requested using
the procedures found in 14 CFR 39.19. Send information to Attn:
Nicholas Wilson, Aerospace Engineer, Cabin Safety and Environmental
Systems Branch, ANM-150S, Seattle Aircraft Certification Office,
FAA, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone
(425) 917-6476; fax (425) 917-6590. Or, e-mail information to <a href="/cdn-cgi/l/email-protection#635a4e222d2e4e30060217170f064e22202c4e222e2c204e3106121606101710230502024d040c15"><span class="__cf_email__" data-cfemail="20190d616e6d0d73454154544c450d61636f0d616d6f630d7245515545535453604641410e474f56">[email&#160;protected]</span></a>.
(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 principal maintenance inspector (PMI) or
principal avionics inspector (PAI), as appropriate, or lacking a
principal inspector, your local Flight Standards District Office.
The AMOC approval letter must specifically refer to this AD.

Material Incorporated by Reference

(j) None.

Issued in Renton, Washington, on January 8, 2010.
Stephen P. Boyd,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2010-937 Filed 1-19-10; 8:45 am]
BILLING CODE 4910-13-P

Airworthiness Directives; AVOX Systems and B/E Aerospace Oxygen Cylinder Assemblies, as Installed on Various Transport Airplanes

Applicability

Unsafe Condition

Required Actions

Compliance Time

Affected Aircraft

Federal Register Abstract

Document Text