[Federal Register: May 11, 2005 (Volume 70, Number 90)]
[Proposed Rules]
[Page 24731-24734]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr11my05-10]
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Proposed Rules
Federal Register
________________________________________________________________________
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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[[Page 24731]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-20440; Directorate Identifier 2005-CE-05-AD]
RIN 2120-AA64
Airworthiness Directives; Aero Advantage ADV200 Series (Part
Numbers ADVPL211CC and ADVPL212CW) Vacuum Pumps
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for all airplanes equipped with Aero Advantage ADV200 series (part
numbers ADVPL211CC and ADVPL212CW) vacuum pumps installed under
supplemental type certificate number SA10126SC, through field approval,
or other methods. This proposed AD would require you to remove any
affected vacuum pump and related monitor system, remove the applicable
airplane flight manual supplement (AFMS) and placard, and install an
FAA-approved vacuum pump other than the affected part numbers. This
proposed AD results from several reports of pump chamber failure. We
are issuing this proposed AD to correct problems with the vacuum pump
before failure or malfunction during instrument flight rules (IFR)
flight that can lead to loss of flight instruments critical for flight.
The loss of flight instruments could cause pilot disorientation and
loss of control of the aircraft.
DATES: We must receive any comments on this proposed AD by July 11,
2005.
ADDRESSES: Use one of the following to submit comments on this proposed
AD:
DOT Docket Web site: Go to http://dms.dot.gov and follow
the instructions for sending your comments electronically.
Government-wide rulemaking Web site: Go to http://www.regulations.gov
and follow the instructions for sending your
comments electronically.
Mail: Docket Management Facility; U.S. Department of
Transportation, 400 Seventh Street, SW., Nassif Building, Room PL-401,
Washington, DC 20590-001.
Fax: 1-202-493-2251.
Hand Delivery: Room PL-401 on the plaza level of the
Nassif Building, 400 Seventh Street, SW., Washington, DC, between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
To view the comments to this proposed AD, go to http://dms.dot.gov.
The docket number is FAA-2005-20440; Directorate Identifier 2005-CE-05-
AD.
FOR FURTHER INFORMATION CONTACT: Peter Hakala, Aerospace Engineer,
Special Certification Office, Rotorcraft Directorate, FAA, 2601 Meacham
Boulevard, Fort Worth, Texas 76193-0190; telephone: (817) 222-5145;
facsimile: (817) 222-5785.
SUPPLEMENTARY INFORMATION:
Comments Invited
How do I comment on this proposed AD? We invite you to submit any
written relevant data, views, or arguments regarding this proposal.
Send your comments to an address listed under ADDRESSES. Include the
docket number, ``FAA-2005-20440; Directorate Identifier 2005-CE-05-AD''
at the beginning of your comments. We will post all comments we
receive, without change, to http://dms.dot.gov, including any personal
information you provide. We will also post a report summarizing each
substantive verbal contact with FAA personnel concerning this proposed
rulemaking. Using the search function of our docket Web site, anyone
can find and read the comments received into any of our dockets,
including the name of the individual who sent the comment (or signed
the comment on behalf of an association, business, labor union, etc.).
This is docket number FAA-2005-20440; Directorate Identifier 2005-CE-
05-AD. You may review the DOT's complete Privacy Act Statement in the
Federal Register published on April 11, 2000 (65 FR 19477-78) or you
may visit http: //dms.dot.gov.
Are there any specific portions of this proposed AD I should pay
attention to? We specifically invite comments on the overall
regulatory, economic, environmental, and energy aspects of this
proposed AD. If you contact us through a nonwritten communication and
that contact relates to a substantive part of this proposed AD, we will
summarize the contact and place the summary in the docket. We will
consider all comments received by the closing date and may amend this
proposed AD in light of those comments and contacts.
Docket Information
Where can I go to view the docket information? You may view the AD
docket that contains the proposal, any comments received, and any final
disposition in person at the DMS Docket Offices between 9 a.m. and 5
p.m. (eastern standard time), Monday through Friday, except Federal
holidays. The Docket Office (telephone 1-800-647-5227) is located on
the plaza level of the Department of Transportation NASSIF Building at
the street address stated in ADDRESSES. You may also view the AD docket
on the Internet at http://dms.dot.gov. The comments will be available
in the AD docket shortly after the DMS receives them.
Discussion
What events have caused this proposed AD? For the Aero Advantage
ADV200 series (part numbers (P/Ns) ADVPL211CC and ADVPL212CW) vacuum
pumps, FAA has received reports of 14 single shaft failures and 11 dual
shaft failures in a population of 285 pumps. Nine of the failures
occurred with less than 100 hours time-in-service. The failures are
concentrated on airplanes with the Lycoming Engines IO-540 series
engines.
In May 2004, Aero Advantage reported to FAA that they had stopped
production and sales of the pumps and that they were quitting the
business.
The Aero Advantage ADV200 series vacuum pumps are installed under
supplemental type certificate number SA10126SC, through field approval,
or other methods. The installation of the vacuum pump includes a
monitor system, airplane flight manual supplement (AFMS), and a
placard.
What is the potential impact if FAA took no action? Failure or
malfunction of the vacuum pump during instrument flight rules (IFR)
flight can lead to loss of flight instruments critical for flight.
[[Page 24732]]
The loss of flight instruments could cause pilot disorientation and
loss of control of the aircraft.
FAA's Determination and Requirements of This Proposed AD
What has FAA decided? We have evaluated all pertinent information
and identified an unsafe condition that is likely to exist or develop
on other products of this same type design. For this reason, we are
proposing AD action.
What would this proposed AD require? This proposed AD would require
you to remove any Aero Advantage ADV200 series (P/Ns ADVPL211CC and
ADVPL212CW) vacuum pump, the related monitor system, the applicable
AFMS and related placard installed under supplemental type certificate
number SA10126SC, through field approval, or other methods. It would
also require you to install an FAA-approved vacuum pump other than the
affected part numbers.
How does the revision to 14 CFR part 39 affect this proposed AD? On
July 10, 2002, we published a new version of 14 CFR part 39 (67 FR
47997, July 22, 2002), which governs FAA's AD system. This regulation
now includes material that relates to altered products, special flight
permits, and alternative methods of compliance. This material
previously was included in each individual AD. Since this material is
included in 14 CFR part 39, we will not include it in future AD
actions.
Costs of Compliance
How many airplanes would this proposed AD impact? We estimate that
this proposed AD could affect 285 airplanes in the U.S. registry.
What would be the cost impact of this proposed AD on owners/
operators of the affected airplanes? We estimate the following costs to
do this proposed removal and replacement. We have no way of determining
the exact number of airplanes that will need this removal and
replacement:
------------------------------------------------------------------------
Average parts Total cost per
Labor cost cost airplane
------------------------------------------------------------------------
3 work hours x $65 = $195......... $400 $595
------------------------------------------------------------------------
Authority for This Rulemaking
What authority does FAA have for issuing this rulemaking action?
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 AD.
Regulatory Findings
Would this proposed AD impact various entities? We have determined
that this proposed AD would not have federalism implications under
Executive Order 13132. This proposed AD would 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.
Would this proposed AD involve a significant rule or regulatory
action? For the reasons discussed above, I certify that this proposed
AD:
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 summary of the costs to comply with this proposed AD
(and other information as included in the Regulatory Evaluation) and
placed it in the AD Docket. You may get a copy of this summary by
sending a request to us at the address listed under ADDRESSES. Include
``AD Docket FAA-2005-20440; Directorate Identifier 2005-CE-05-AD'' in
your request.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Safety.
The Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the Federal Aviation Administration proposes to amend 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. The FAA amends Sec. 39.13 by adding the following new
airworthiness directive (AD):
Aero Advantage: Docket No. FAA-2005-20440; Directorate Identifier
2005-CE-05-AD.
When Is the Last Date I Can Submit Comments on This Proposed AD?
(a) We must receive comments on this proposed airworthiness
directive (AD) by July 11, 2005.
What Other ADs Are Affected by This Action?
(b) None.
What Airplanes Are Affected by This AD?
(c) This AD affects ADV200 series (part numbers (P/Ns)
ADVPL211CC and ADVPL212CW) vacuum pumps installed on, but not
limited to, the following aircraft that are certificated in any
category. These vacuum pumps can be installed under supplemental
type certificate number SA10126SC, through field approval, or other
methods:
------------------------------------------------------------------------
Make Model
------------------------------------------------------------------------
Alexandria Aircraft, LLC.................. 14-19, 14-19-2, 14-19-3, 17-
30, 17-31, 17-31TC, 17-30A,
17-31A, and 17-31ATC.
Alliance Aircraft Group, LLC.............. H-295 (USAF U10D).
American Champion Aircraft Corp........... 7AC, 7ECA, 7GC, 7GCA, 7GCAA,
7GCB, 7GCBC, 7HC, 7KC,
7KCAB, 8GCBC, and 8KCAB.
[[Page 24733]]
Cessna Aircraft Company, The.............. 172, 172A, 172B, 172C, 172D,
172E, 172F, 172G, 172H,
172I, 172K, 172L, 172M,
172N, 172P, 172Q, 182,
182A, 182B, 182C, 182D,
182E, 182F, 182G, 182H,
182J, 182K, 182L, 182M,
182N, 182P, 182Q, 182R,
R182, T182, TR182, 172RG,
R172E, R172F, R172H, R172J,
152, A152, 210, 210-5
(205), 210-5A (205A), 210A,
210B, 210C, 210D, 210E,
210F, 210G, 210H, 210J,
210K, 210L, 210M, 210N,
P210N, T210G, T210H, T210M,
T210N, T210R, 185, 185A,
185B, 185C, 185D, 185E,
180, 180A, 180B, 180C,
180D, 180E, 180F, 180G,
180H, 180J, 120, 140, 170,
170A, 170B, 177, 177A,
177B, 207, 207A, T207,
T207A, 177RG, 206, P206,
P206A, P206B, P206C, P206D,
P206E, TP206A, TP206B,
TP206C, TP206D, TP206E,
TU206A, TU206B, TU206C,
TU206D, TU206E, TU206F,
TU206G, U206, U206A, U206B,
U206C, U206D, U206E, U206F,
U206G, 188, 188A, 188B,
A188, A188A, and A188B.
Commander Aircraft Company................ 112, 112B, 112TC, 114, and
114A.
Dynac Aerospace Corporation............... Aero Commander 100.
Global Amphibians, LLC.................... Lake LA-4-200, Lake Model
250.
Maule Aerospace Technology, Inc........... M-4-210, M-4-220, M-5-180C,
M-5-200, M-5-235C, M-6-180,
and M-6-235.
Mooney Aircraft Corporation............... M20, M20A, M20B, M20C, M20D,
M20E, M20F, M20G, M20J,
M20K, M20M, and M22.
Navion Aircraft Company, Ltd.............. Navion G and Navion H.
Piper Aircraft, Inc., The New............. PA-23, PA-23-160, PA-23-235,
PA-23-250 (Navy UO-1), PA-
E23-250, PA-24, PA-24-250,
PA-24-260, PA-18, PA-18-105
(Special), PA-18-135, PA-18-
150, PA-20-115, PA-20-135,
PA-22-108, PA-22-135, PA-22-
150, PA-22-160, PA-25, PA-
25-235, PA-25-260, PA-28-
140, PA-28-150, PA-28-151,
PA-28-160, PA-28-161, PA-28-
180, PA-28-181, PA-28-201T,
PA-28-235, PA-28-236, PA-
28R-180, PA-28R-200, PA-28R-
201, PA-28R-201T, PA-28RT-
201, PA-28RT-201T, PA-25,
PA-25-235, PA-25-260, J5A-
80, J5A (Army L-4F), J5B
(Army L-4G), J5C, PA-12, PA-
36-285, PA-36-300, PA-36-
375, PA-38-112, PA-30, PA-
39, PA-40, PA-31, PA-31-
300, PA-31-325, PA-31-350,
PA-32-260, PA-32-300, PA-32-
301, PA-32-301T, PA-32R-
300, PA-32R-301 (HP), PA-
32R-301T, PA-32RT-300T, PA-
31P, and PA-36-300.
Raytheon Aircraft Company................. 35-33, 35-A33, 35-B33, 35-
C33, 35-C33A, 36, A36,
A36TC, B36TC, E33, E33A,
E33C, F33, F33A, F33C, G33,
H35, J35, V35, V35A, V35B,
D45 (Military T-34B), 35,
35R, A35, B35, C35, D35,
E35, F35, G35, 19A, 23,
A23, A23A, A24, A24R, B19,
B23, B24R, C23, and C24R.
Rogers, Burl A............................ 15AC and S15AC.
SOCATA--Groupe Aerospatiale............... MS 885, MS 892A-150, MS 892E-
150, MS 893A, MS 893E,
Rallye 150 ST, Rallye 150
T, TB 10, TB 20, and TB 9.
Tiger Aircraft LLC........................ AA-1, AA-1A, AA-1B, AA-1C,
AA-5, AA-5A, and AA-5B.
------------------------------------------------------------------------
What Is the Unsafe Condition Presented in This AD?
(d) This AD is the result of several reports of pump chamber
failure. The actions specified in this AD are intended to correct
problems with the vacuum pump before failure or malfunction during
instrument flight rules (IFR) flight that can lead to loss of flight
instruments critical for flight. The loss of flight instruments
could cause pilot disorientation and loss of control of the
aircraft.
What Must I Do To Address This Problem?
(e) To address this problem, you must do the following:
----------------------------------------------------------------------------------------------------------------
Actions Compliance Procedures
----------------------------------------------------------------------------------------------------------------
(1) Remove any Aero Advantage ADV200 Within 100 hours time-in-service Not Applicable.
series (P/Ns ADVPL211CC and ADVPL212CW) (TIS) or the next 12 calendar
vacuum pump, and the related monitor months after the effective date
system and placard. of this AD, whichever occurs
first, unless already done.
[[Page 24734]]
(2) Remove the airplane flight manual As of the removal of any vacuum Not Applicable.
supplement for any Aero Advantage ADV200 pump per paragraph (e)(1) of
series (P/Ns ADVPL211CC and ADVPL212CW) this AD.
vacuum pump and monitor system from the
FAA-approved airplane flight manual
(AFM).
(i) The owner/operator holding at least a
private pilot certificate as authorized
by section 43.7 of the Federal Aviation
Regulations (14 CFR 43.7) may do the
flight manual changes requirement of
this AD.
(ii) Make an entry in the aircraft
records showing compliance with this
portion of the AD following section 43.9
of the Federal Aviation Regulations (14
CFR 43.9).
(3) Install an FAA-approved vacuum pump Before further flight after Not Applicable.
other than the affected part numbers. removing any Aero Advantage
ADV200 series (P/Ns ADVPL211CC
or ADVPL212CW) vacuum pump per
paragraph (e)(1) of this AD.
(4) Do not install any Aero Advantage As of the effective date of this Not Applicable.
ADV200 series (P/Ns ADVPL211CC and AD.
ADVPL212CW) vacuum pump.
----------------------------------------------------------------------------------------------------------------
May I Request an Alternative Method of Compliance?
(f) You may request a different method of compliance or a
different compliance time for this AD by following the procedures in
14 CFR 39.19. Unless FAA authorizes otherwise, send your request to
your principal inspector. The principal inspector may add comments
and will send your request to the Manager, Special Certification
Office, Rotorcraft Directorate, FAA. For information on any already
approved alternative methods of compliance, contact Peter Hakala,
Aerospace Engineer, Special Certification Office, Rotorcraft
Directorate, FAA, 2601 Meacham Boulevard, Fort Worth, Texas 76193-
0190; telephone: (817) 222-5145; facsimile: (817) 222-5785.
May I Get Copies of the Documents Referenced in This AD?
(g) To view the AD docket, go to the Docket Management Facility;
U.S. Department of Transportation, 400 Seventh Street, SW., Nassif
Building, Room PL-401, Washington, DC, or on the Internet at http://dms.dot.gov.
The docket number is Docket No. FAA-2005-20440;
Directorate Identifier 2005-CE-05-AD.
Issued in Kansas City, Missouri, on May 4, 2005.
Kim Smith,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-9366 Filed 5-10-05; 8:45 am]
BILLING CODE 4910-13-P