FR Doc E8-27364

[Federal Register: November 25, 2008 (Volume 73, Number 228)]
[Rules and Regulations]
[Page 71539-71541]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr25no08-9]

[[Page 71539]]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2008-0892; Directorate Identifier 2008-CE-049-AD;
Amendment 39-15742; AD 2008-24-02]
RIN 2120-AA64

Airworthiness Directives; Maule Aerospace Technology, Inc. M-4,
M-5, M-6, and M-7 Series and Model M-8-235 Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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SUMMARY: The FAA adopts a new airworthiness directive (AD) for certain
Maule Aerospace Technology, Inc. M-4, M-5, M-6, and M-7 series and
Model M-8-235 airplanes. This AD requires you to paint the top of the
rear elevator control horn, the elevator control cable end attached to
the top of the rear control horn, the bottom of the forward elevator
control horn, and the elevator control cable end attached to the bottom
of the forward control horn. This AD also requires you to insert a
supplement into your maintenance program (maintenance manual). This AD
results from two reports of accidents where reversed elevator control
rigging was a factor. We are issuing this AD to reduce the likelihood
of a mechanic rigging the elevator controls backwards, which could
result in elevator movement in the opposite direction from control
input. This condition could lead to loss of control.

DATES: This AD becomes effective on December 30, 2008.
On December 30, 2008, the Director of the Federal Register approved
the incorporation by reference of certain publications listed in this
AD.

ADDRESSES: To get the service information identified in this AD,
contact Maule Aerospace Technology, Inc., 2099 Georgia Highway 133
South, Moultrie, Georgia 31788; telephone: (229) 985-2045; fax: (229)
985-2048; e-mail: engineering@mauleairinc.com; Internet: http://
www.mauleairinc.com/service_bulletins.htm.
To view the AD docket, go to U.S. Department of Transportation,
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200
New Jersey Avenue, SE., Washington, DC 20590, or on the Internet at
http://www.regulations.gov. The docket number is FAA-2008-0892;
Directorate Identifier 2008-CE-049-AD.

FOR FURTHER INFORMATION CONTACT: Cindy Lorenzen, Aerospace Engineer,
One Crown Center, 1895 Phoenix Blvd., Suite 450, Atlanta, Georgia
30349; telephone: (770) 703-6078; fax: (770) 703-6097; e-mail:
cindy.lorenzen@faa.gov; or
Gerald Avella, Aerospace Engineer, One Crown Center, 1895 Phoenix
Blvd., Suite 450, Atlanta, Georgia 30349; telephone: (770) 703-6066;
fax: (770) 703-6097; e-mail: gerald.avella@faa.gov.

SUPPLEMENTARY INFORMATION:

Discussion

On August 12, 2008, we issued a proposal to amend part 39 of the
Federal Aviation Regulations (14 CFR part 39) to include an AD that
would apply to certain Maule Aerospace Technology, Inc. M-4, M-5, M-6,
and M-7 series and Model M-8-235 airplanes. This proposal was published
in the Federal Register as a notice of proposed rulemaking (NPRM) on
August 19, 2008 (73 FR 48314). The NPRM proposed to require you to
paint the top of the rear elevator control horn, the elevator control
cable end attached to the top of the rear control horn, the bottom of
the forward elevator control horn, and the elevator control cable end
attached to the bottom of the forward control horn. The NPRM also
proposed to require you to insert a supplement into your maintenance
program (maintenance manual).

Comments

We provided the public the opportunity to participate in developing
this AD. The following presents the comments received on the proposal
and FAA's response to each comment:

Comment Issue No. 1: The AD Should Not Be Issued

An anonymous commenter suggests that the AD is unnecessary because
mechanics should already know to always check the rigging of the flight
controls anytime the cables have been disconnected and re-connected.
The commenter requests that we not issue the AD.
While we agree mechanics should always check the rigging of the
control cables for proper operation anytime the cables have been re-
connected to the airplane, there have been instances where this has not
happened and it has led to accidents. To minimize the possibility of
incorrect flight control system assembly, this AD requires color coding
the cables and control horns, which will provide a visual aid to the
mechanic during reassembly.
We are not changing the AD as a result of this comment.

Comment Issue No. 2: Removal of the Word ``Horn'' From Paragraph
(e)(1)(iii)

Mr. Geoffrey Sharp comments that the word ``horn'' does not make
sense in the painting instruction requiring painting of ``the bottom of
the forward elevator control horn.'' We infer that he is requesting
that we remove the word ``horn'' from paragraph (e)(1)(iii) of the AD.
We do not agree with the comment. The instructions to paint the
elevator control horn are correct. The horn is the connecting piece for
the control cables. However, upon review we noticed that the word horn
was omitted from paragraph (e)(1)(iv) of the proposed AD.
We are changing paragraph (e)(1)(iv) of this AD by adding the word
``horn'' to the end of the sentence. We have also made this change in
the Summary and Discussion sections of this AD.

Conclusion

We have carefully reviewed the available data and determined that
air safety and the public interest require adopting the AD as proposed
except for the changes previously discussed and minor editorial
corrections. We have determined that these minor corrections:
Are consistent with the intent that was proposed in the
NPRM for correcting the unsafe condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM.

Costs of Compliance

We estimate that this AD affects 1,765 airplanes in the U.S.
registry.
We estimate the following costs to do the modification:

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Total cost per Total cost on
Labor cost Parts cost airplane U.S. operators
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1 work-hour x $80 per hour = $80............................. $20 $100 $176,500
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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 AD.

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 this 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 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 ``Docket
No. FAA-2008-0892; Directorate Identifier 2008-CE-049-AD'' in your
request.

List of Subjects in 14 CFR Part 39

Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.

Adoption of the Amendment

0
Accordingly, under the authority delegated to me by the Administrator,
the Federal Aviation Administration 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. FAA amends Sec. 39.13 by adding a new AD to read as follows:

2008-24-02 Maule Aerospace Technology, Inc.: Amendment 39-15742;
Docket No. FAA-2008-0892; Directorate Identifier 2008-CE-049-AD.

Effective Date

(a) This AD becomes effective on December 30, 2008.

Affected ADs

(b) None.

Applicability

------------------------------------------------------------------------
Model Serial Nos.
------------------------------------------------------------------------
Bee Dee M-4............................... All serial numbers.
M-4....................................... All serial numbers.
M-4-180C.................................. All serial numbers.
M-4-180V.................................. 47001T through 47014T.
M-4-210................................... All serial numbers.
M-4-210C.................................. All serial numbers.
M-4-210S.................................. All serial numbers.
M-4-220C.................................. All serial numbers.
M-4-220S.................................. All serial numbers.
M-4C...................................... All serial numbers.
M-4S...................................... All serial numbers.
M-4T...................................... All serial numbers.
M-5-180C.................................. All serial numbers.
M-5-200................................... All serial numbers.
M-5-210C.................................. All serial numbers.
M-5-210TC................................. All serial numbers.
M-5-220C.................................. All serial numbers.
M-5-235C.................................. All serial numbers.
M-6-180................................... 8020C, 8043C, 8065C through
8067C.
M-6-235................................... 7249C, 7356C, 7379C through
7444C, 7446C through 7450C,
7452C through 7459C, 7461C
through 7466C, 7468C,
7469C, 7471C through 7475C,
7488C through 7514C, 7516C
through 7522C.
M-7-235................................... 4001C through 4132C, 12001C,
12002C.
M-7-235A.................................. 24001C.
M-7-235B.................................. 23001C through 23105C.
M-7-235C.................................. 25001C through 25106C.
M-7-260................................... 26001C through 26021C.
M-7-260C.................................. 30001C through 30040C.
M-7-420A.................................. 35001C.
M-7-420AC................................. 29001C, 29003C through
29007C.
M-8-235................................... 15001C through 15006C.
MT-7-235.................................. 18001C through 18097C,
18099C, 18100C.
MT-7-260.................................. 27001C through 27014C.
MT-7-420.................................. 51001C, 51002C.
MX-7-160.................................. 19001C through 19046C.
MX-7-160C................................. 34001C.
MX-7-180.................................. 11001C through 11097C.
MX-7-180A................................. 20001C through 20064C.
MX-7-180AC................................ 33001C through 33010C.

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MX-7-180B................................. 22001C through 22025C,
22027C.
MX-7-180C................................. 28001C through 28027C.
MX-7-235.................................. 10001C through 10122C.
MX-7-420.................................. 13001C through 13003C.
MXT-7-160................................. 17001C through 17008C.
MXT-7-180................................. 14000C through 14125C.
MXT-7-180A................................ 21001C through 21096C.
------------------------------------------------------------------------

Unsafe Condition

(d) This AD results from two reports of accidents where reversed
elevator control rigging was a factor. We are issuing this AD to
reduce the likelihood of a mechanic rigging the elevator controls
backwards, which could result in elevator movement in the opposite
direction from control input. This failure could lead to loss of
control.

Compliance

(e) To address this problem, you must do the following, unless
already done:

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Actions Compliance Procedures
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(1) Using yellow enamel paint, color Before the next time the elevator Follow Maule Aerospace Technology,
code the following: control cable is disconnected for Inc. Mandatory Service Bulletin No.
(i) the top of the rear elevator any reason or within the next 12 30, dated March 4, 2008.
control horn; calendar months after December 30,
(ii) the elevator control cable end 2008 (the effective date of this
attached to the top of the rear AD), whichever occurs first.
control horn;
(iii) the bottom of the forward
elevator control horn; and
(iv) the elevator control cable end
attached to the bottom of the
forward control horn
(2) Insert the following text into Before the next time the elevator Follow Maule Aerospace Technology,
the rigging procedure section of control cable is disconnected for Inc. Mandatory Service Bulletin No.
your FAA-approved maintenance any reason or within the next 12 30, dated March 4, 2008. You may
program (e.g. maintenance manual): calendar months after December 30, insert a copy of this AD or you may
``CAUTION--BEFORE FLIGHT WHENEVER 2008 (the effective date of this insert the text located on the
ELEVATOR CABLES ARE RECONNECTED OR AD), whichever occurs first. bottom of page 3 of Maule Aerospace
NEW CABLES INSTALLED: Always check Technology, Inc. Mandatory Service
operation of elevators after a Bulletin No. 30, dated March 4,
cable reconnect by pulling back on 2008, into the FAA-approved
the control and ascertain that the maintenance program (e.g., 1
elevators are in the UP position.'' maintenance manual).
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Alternative Methods of Compliance (AMOCs)

(f) The Manager, Atlanta Aircraft Certification Office (ACO),
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: Gerald Avella, Aerospace Engineer, One Crown Center, 1895
Phoenix Blvd., Suite 450, Atlanta, Georgia 30349; telephone: (770)
703-6066; fax: (770) 703-6097; e-mail: gerald.avella@faa.gov. Before
using any approved AMOC on any airplane to which the AMOC applies,
notify your appropriate principal inspector (PI) in the FAA Flight
Standards District Office (FSDO), or lacking a PI, your local FSDO.

Material Incorporated by Reference

(g) You must use Maule Aerospace Technology, Inc. Mandatory
Service Bulletin No. 30, dated March 4, 2008, to do the actions
required by this AD, unless the AD specifies otherwise.
(1) The Director of the Federal Register approved the
incorporation by reference of this service information under 5
U.S.C. 552(a) and 1 CFR part 51.
(2) For service information identified in this AD, contact Maule
Aerospace Technology, Inc., 2099 Georgia Highway 133 South,
Moultrie, Georgia 31788; telephone: (229) 985-2045; fax: (229) 985-
2048; e-mail: engineering@mauleairinc.com; Internet: http://
www.mauleairinc.com.
(3) You may review copies at the FAA, Central Region, Office of
the Regional Counsel, 901 Locust, Kansas City, Missouri 64106; or 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/code_
of_federal_regulations/ibr_locations.html.

Issued in Kansas City, Missouri, on November 10, 2008.
James E. Jackson,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E8-27364 Filed 11-24-08; 8:45 am]

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