[Federal Register Volume 64, Number 220 (Tuesday, November 16, 1999)]
[Proposed Rules]
[Pages 62129-62131]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 99-29828]
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Proposed Rules
Federal Register
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This section of the FEDERAL REGISTER contains notices to the public of
the proposed issuance of rules and regulations. The purpose of these
notices is to give interested persons an opportunity to participate in
the rule making prior to the adoption of the final rules.
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Federal Register / Vol. 64, No. 220 / Tuesday, November 16, 1999 /
Proposed Rules
[[Page 62129]]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 99-NM-160-AD]
RIN 2120-AA64
Airworthiness Directives; Raytheon Model Hawker 800 and 1000
Airplanes and Model DH.125, HS.125, BH.125, and BAe.125 Series
Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Raytheon Model Hawker 800
and 1000 airplanes and Model DH.125, HS.125, BH.125, and BAe.125 series
airplanes. This proposal would require replacement of cadmium plated
fittings and cone caps in the oxygen system plumbing with improved
fittings and cone caps, a detailed visual inspection of the oxygen
system plumbing in the area of the replaced parts, and corrective
actions, if necessary. This proposal is prompted by reports indicating
that a field survey of the affected parts revealed that a reaction
process was occurring, which resulted in cadmium flaking. The actions
specified by the proposed AD are intended to prevent flaking of cadmium
from certain oxygen system plumbing fittings and cone caps from
blocking the valves and impairing the function of the oxygen system,
which could deprive the crew and passengers of necessary oxygen during
an emergency that requires oxygen.
DATES: Comments must be received by January 3, 2000.
ADDRESSES: Submit comments in triplicate to the Federal Aviation
Administration (FAA), Transport Airplane Directorate, ANM-114,
Attention: Rules Docket No. 99-NM-160-AD, 1601 Lind Avenue, SW.,
Renton, Washington 98055-4056. Comments may be inspected at this
location between 9:00 a.m. and 3:00 p.m., Monday through Friday, except
Federal holidays.
The service information referenced in the proposed rule may be
obtained from Raytheon Aircraft Company, Manager Service Engineering,
Hawker Customer Support Department, P.O. Box 85, Wichita, Kansas 67201-
0085. This information may be examined at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Small
Airplane Directorate, Wichita Aircraft Certification Office, 1801
Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas 67209.
FOR FURTHER INFORMATION CONTACT: Paul C. DeVore, Aerospace Engineer,
Systems and Propulsion Branch, ACE-116W, FAA, Small Airplane
Directorate, Wichita Aircraft Certification Office, 1801 Airport Road,
Room 100, Mid-Continent Airport, Wichita, Kansas 67209; telephone (316)
946-4142; fax (316) 946-4407.
SUPPLEMENTARY INFORMATION:
Comments Invited
Interested persons are invited to participate in the making of the
proposed rule by submitting such written data, views, or arguments as
they may desire. Communications shall identify the Rules Docket number
and be submitted in triplicate to the address specified above. All
communications received on or before the closing date for comments,
specified above, will be considered before taking action on the
proposed rule. The proposals contained in this notice may be changed in
light of the comments received.
Comments are specifically invited on the overall regulatory,
economic, environmental, and energy aspects of the proposed rule. All
comments submitted will be available, both before and after the closing
date for comments, in the Rules Docket for examination by interested
persons. A report summarizing each FAA-public contact concerned with
the substance of this proposal will be filed in the Rules Docket.
Commenters wishing the FAA to acknowledge receipt of their comments
submitted in response to this notice must submit a self-addressed,
stamped postcard on which the following statement is made: ``Comments
to Docket Number 99-NM-160-AD.'' The postcard will be date stamped and
returned to the commenter.
Availability of NPRMs
Any person may obtain a copy of this NPRM by submitting a request
to the FAA, Transport Airplane Directorate, ANM-114, Attention: Rules
Docket No. 99-NM-160-AD, 1601 Lind Avenue, SW., Renton, Washington
98055-4056.
Discussion
The FAA has received reports indicating that, during a field survey
of two Raytheon Model DH.125, HS.125, BH.125 series 400A/400B airplanes
equipped with cadmium plated cone caps, a reaction process occurred,
which resulted in cadmium flaking. The cause of the flaking has been
attributed to the cone caps being made of mild steel with cadmium
plating, which may decompose and flake when exposed to oxygen. Flaking
of cadmium from oxygen system plumbing fittings and cone caps can block
valves and impair the function of the oxygen system. This condition, if
not corrected, could result in depriving the crew and passengers of
necessary oxygen during an emergency that requires oxygen.
Cone caps and oxygen system plumbing fittings on Raytheon Model
Hawker 800 and 1000 airplanes and Model DH.125, HS.125, BH.125, and
BAe.125 series airplanes are similar to those on the affected Model
DH.125, HS.125, BH.125 series 400A/400B airplanes. Therefore, all of
these models may be subject to the same unsafe condition.
Explanation of Relevant Service Information
The FAA has reviewed and approved Raytheon Service Bulletins SB 35-
3034, SB 35-3167, SB 35-3168, SB 35-3169, SB 35-3171, and SB 35-3170,
all dated September 1998. These service bulletins describe procedures
for replacement of cadmium plated fittings and cone caps in the oxygen
system plumbing with improved fittings and cone caps; and a detailed
visual inspection of the oxygen system plumbing in the area of the
replaced parts, and corrective actions, if necessary. The corrective
actions include cleaning affected areas and performing a flow check of
the oxygen system. Accomplishment of the actions specified in the
service bulletins is
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intended to adequately address the identified unsafe condition.
Explanation of Requirements of Proposed Rule
Since an unsafe condition has been identified that is likely to
exist or develop on other products of this same type design, the
proposed AD would require accomplishment of the actions specified in
the service bulletins described previously, except as discussed below.
Differences Between Proposed Rule and Service Bulletin
Operators should note that, although the service bulletin specifies
that the manufacturer may be contacted for disposition of certain
repair conditions, this proposal would require the repair of those
conditions to be accomplished in accordance with a method approved by
the FAA.
Cost Impact
There are approximately 724 airplanes of the affected design in the
worldwide fleet. The FAA estimates that 481 airplanes of U.S. registry
would be affected by this proposed AD.
For Model DH.125, HS.125, BH.125 series 1A/1B, 3A/3B, 400A, 400B,
401B, 403A, 403B, 600A, 600B, 700A, 700B airplanes (236 airplanes of
U.S. registry), it would take approximately 7 work hours per airplane
to accomplish the proposed actions, at an average labor rate of $60 per
work hour. Required parts would cost approximately between $28 and $79
per airplane. Based on these figures, the cost impact of the proposed
AD on U.S. operators of these airplanes is estimated to be between
$105,728, and $117,764, or between $448 and $499 per airplane.
For Model BAe.125 series 800A (C-29A) airplanes (6 airplanes of
U.S. registry), it would take approximately 3 work hours per airplane
to accomplish the proposed actions, at an average labor rate of $60 per
work hour. Required parts would cost approximately $61 per airplane.
Based on these figures, the cost impact of the proposed AD on U.S.
operators of these airplanes is estimated to be $1,446, or $241 per
airplane.
For Model BAe.125 series 800A, and 800B airplanes, and Model Hawker
800 airplanes (202 airplanes of U.S. registry), it would take
approximately 10 work hours per airplane to accomplish the proposed
actions, at an average labor rate of $60 per work hour. Required parts
would cost approximately between $16 and $22 per airplane. Based on
these figures, the cost impact of the proposed AD on U.S. operators of
these airplanes is estimated to be between $124,432 and $125,644, or
between $616 and $622 per airplane.
For Model BAe.125 series 1000A and 1000B airplanes, and Model
Hawker 1000 airplanes (37 airplanes of U.S. registry), it would take
approximately 6 work hours per airplane to accomplish the proposed
actions, at an average labor rate of $60 per work hour. Required parts
would cost approximately between $66 and $122 per airplane. Based on
these figures, the cost impact of the proposed AD on U.S. operators of
these airplanes is estimated to be between $15,762 and $17,834, or
between $426 and $482 per airplane.
The cost impact figures discussed above are based on assumptions
that no operator has yet accomplished any of the proposed requirements
of this AD action, and that no operator would accomplish those actions
in the future if this AD were not adopted. However, the FAA has been
advised that manufacturer warranty remedies are available for some
labor costs associated with accomplishing the actions required by this
proposed AD. Therefore, the future economic cost impact of this rule on
U.S. operators may be less than the cost impact figures indicated
above.
Regulatory Impact
The regulations proposed herein would not have substantial direct
effects 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. Therefore, in
accordance with Executive Order 12612, it is determined that this
proposal would not have sufficient federalism implications to warrant
the preparation of a Federalism Assessment.
For the reasons discussed above, I certify that this proposed
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) if promulgated, 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. A copy of the draft
regulatory evaluation prepared for this action is contained in the
Rules Docket. A copy of it may be obtained by contacting the Rules
Docket at the location provided under the caption ADDRESSES.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Safety.
The Proposed Amendment
Accordingly, pursuant to the authority delegated to me by the
Administrator, the Federal Aviation Administration proposes to amend
part 39 of the Federal Aviation Regulations (14 CFR part 39) as
follows:
PART 39--AIRWORTHINESS DIRECTIVES
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]
2. Section 39.13 is amended by adding the following new
airworthiness directive:
Raytheon Aircraft Company (Formerly Beech): Docket 99-NM-160-AD.
Applicability: Models and series of airplanes as listed in the
applicable service bulletin(s) specified in Table 1 of this AD,
certificated in any category:
Table 1
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Raytheon service Date of service
Model of airplane bulletin bulletin
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DH.125, HS.125, BH.125 series SB 35-3169...... September 1998.
1A, 1B, 3A, 3B, 400A, 400B,
401B, 403A, 403B, 600A, 600B,
700A, and 700B airplanes.
BAe.125 series 800A (C-29A) SB 35-3171...... September 1998.
airplanes.
BAe.125 series 800A and 800B SB 35-3034 and September 1998
airplanes, and Hawker 800 SB35-3170.
airplanes.
BAe.125 series 1000A and 1000B SB 35-3167 and September 1998.
airplanes, and Hawker 1000 SB 35-3168.
airplanes..
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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
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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 (f) 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 flaking of cadmium from certain oxygen system
plumbing fittings and cone caps from blocking the valves and
impairing the function of the oxygen system, which could deprive the
crew and passengers of necessary oxygen during an emergency that
requires oxygen, accomplish the following:
(a) For Model DH.125, HS.125, BH.125 series 1A, 1B, 3A, 3B,
400A, 400B, 401B, 403A, 403B, 600A, 600B, 700A and 700B airplanes:
Within 6 months after the effective date of this AD, replace the
cadmium plated cone caps in the oxygen system plumbing with improved
cone caps, and perform a detailed visual inspection of the removed
cone caps, tee-piece and sleeve for evidence of flaking or
corrosion; in accordance with Raytheon Service Bulletin SB 35-3169,
dated September 1998. If any flaking or corrosion is detected, prior
to further flight, clean the tee-piece and sleeve, and perform an
oxygen system flow check in accordance with the service bulletin. If
any discrepancy is found during the flow check, prior to further
flight, repair the oxygen system in accordance with the service
bulletin, except as required by paragraph (e) of this AD.
Note 2: For the purposes of this AD, a detailed visual
inspection is defined as: ``An intensive visual examination of a
specific structural area, system, installation, or assembly to
detect damage, failure, or irregularity. Available lighting is
normally supplemented with a direct source of good lighting at
intensity deemed appropriate by the inspector. Inspection aids such
as mirror, magnifying lenses, etc., may be used. Surface cleaning
and elaborate access procedures may be required.''
(b) For Model BAe.125 series 800A (C-29A) airplanes: Within 6
months after the effective date of this AD, replace the cadmium
plated cone caps in the oxygen system plumbing with improved cone
caps, and perform a detailed visual inspection of the removed cone
caps, tee-piece and sleeve for evidence of flaking or corrosion; in
accordance with Raytheon Service Bulletin SB 35-3171, dated
September 1998. If any flaking or corrosion is detected, prior to
further flight, clean the tee-piece and sleeve, and perform an
oxygen system flow check in accordance with the service bulletin. If
any discrepancy is found during the flow check, prior to further
flight, repair the oxygen system in accordance with the service
bulletin, except as required by paragraph (e) of this AD.
(c) For Model BAe.125 series 800A and 800B airplanes and Model
Hawker 800 airplanes: Within 6 months after the effective date of
this AD, replace the cadmium plated cone caps in the oxygen system
plumbing with improved cone caps, and perform a detailed visual
inspection of the removed cone caps, tee-piece and sleeve for
evidence of flaking or corrosion; in accordance with Raytheon
Service Bulletins SB35-3034 or SB 35-3170, both dated September
1998, as applicable. If any flaking or corrosion is detected, prior
to further flight, clean the tee-piece and sleeve, and perform an
oxygen system flow check in accordance with the service bulletin. If
any discrepancy is found during the flow check, prior to further
flight, repair the oxygen system in accordance with the service
bulletin, except as required by paragraph (e) of this AD.
(d) For Model BAe.125 series 1000A and 1000B airplanes and Model
Hawker 1000 series airplanes: Within 6 months after the effective
date of this AD, replace the cadmium plated fittings in the oxygen
system plumbing with improved fittings, and perform a detailed
visual inspection of the removed fittings and the pipe connections
for evidence of flaking or corrosion; in accordance with Raytheon
Service Bulletin SB 35-3167 or SB 35-3168, both dated September
1998, as applicable. If any flaking or corrosion is detected, prior
to further flight, clean the pipe connections, and perform an oxygen
system flow check in accordance with the service bulletin. If any
discrepancy is found during the flow check, prior to further flight,
repair the oxygen system in accordance with the service bulletin,
except as required by paragraph (e) of this AD.
(e) If any discrepancy is found during a flow check required by
paragraph (a), (b), (c), or (d) of this AD and the applicable
service bulletin specifies to contact the manufacturer for a repair
disposition, prior to further flight, repair the oxygen system in
accordance with a method approved by the Manager, Wichita Aircraft
Certification Office (ACO), FAA, Small Airplane Directorate.
Alternative Methods of Compliance
(f) 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, Wichita ACO, FAA, Small Airplane
Directorate. Operators shall submit their requests through an
appropriate FAA Principal Maintenance Inspector, who may add
comments and then send it to the Manager, Wichita ACO.
Note 3: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be
obtained from the Wichita ACO.
Special Flight Permits
(g) Special flight permits may be issued in accordance with
Secs. 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.
Issued in Renton, Washington, on November 9, 1999.
D.L. Riggin,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 99-29828 Filed 11-15-99; 8:45 am]
BILLING CODE 4910-13-U