[Federal Register Volume 61, Number 182 (Wednesday, September 18, 1996)]
[Rules and Regulations]
[Pages 49053-49055]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 96-23715]
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DEPARTMENT OF TRANSPORTATION
14 CFR Part 39
[Docket No. 96-CE-42-AD; Amendment 39-9763; AD 96-16-06]
RIN 2120-AA64
Airworthiness Directives; Weatherly Aviation Company, Inc.,
Models 620A and 620B Airplanes
AGENCY: Federal Aviation Administration, DOT
.ACTION: Final rule; request for comments.
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SUMMARY: This document publishes in the Federal Register an amendment
adopting Airworthiness Directive (AD) 96-16-06, which was sent
previously to all known U.S. owners and operators of certain Weatherly
Aviation Company, Inc., (Weatherly) Models 620A and 620B airplanes.
This AD requires inspecting all wing hinge pins, part number (P/N)
40852-001, at the main wing-to-center section attachment (four per
airplane) for depth of the threaded ends, length of the pin, and
position of the pin; and replacing or repositioning any pin, as
necessary. A report received by the Federal Aviation Administration of
manufacturing deficiencies at the area of the main wing center section
attachment prompted the AD. The actions specified by this AD are
intended to prevent failure of the wing hinge pin, which could result
in the wing separating from the fuselage.
DATES: Effective October 6, 1996, to all persons except those to whom
it was made immediately effective by priority letter AD 96-16-06,
issued July 26, 1996, which contained the requirements of this
amendment.
The incorporation by reference of certain publications listed in
the regulations is approved by the Director of the Federal Register as
of October 6, 1996.
Comments for inclusion in the Rules Docket must be received on or
before November 18, 1996.
ADDRESSES: Submit comments in triplicate to the FAA, Central Region,
Office of the Assistant Chief Counsel, Attention: Rules Docket 96-CE-
42-AD, Room 1558, 601 E. 12th Street, Kansas City, Missouri 64106.
Service information that applies to this AD may be obtained from
the Weatherly Aviation Company, Inc., 2100 Flightline Drive, suite 1,
P.O. Box 68, Lincoln, California 95648. This information may also be
examined at the Rules Docket at the address above, or at the Office of
the Federal Register, 800 North Capitol Street NW., suite 700,
Washington, DC.
FOR FURTHER INFORMATION CONTACT: Mr. William Roberts, Aerospace
Engineer, Los Angeles ACO, FAA, 3960 Paramount Boulevard, Lakewood,
California 90712-4137; telephone (310) 627-5228.
SUPPLEMENTARY INFORMATION:
Events Leading to the AD
The FAA received a report of manufacturing deficiencies on certain
Weatherly Models 620A and 620B airplanes. In particular:
--the wing hinge pins, part number (P/N) 40852-001, at the main
wing spar wing-to-center section attachment could be too short and/or
misaligned, which could result in the pins not properly securing the
wing to the fuselage for ultimate airplane loads; and
--the threaded ends of the wing hinge pin retaining bolt holes could be
drilled too deep, which could result in excessive stress load on the
wing hinge pins with subsequent wing hinge pin failure.
Applicable Service Information
Weatherly Aviation Company, Inc., has issued Service Note No. 15,
dated July 17, 1996, which specifies procedures for inspecting the P/N
40852-001 wing hinge pins for depth of the threaded ends, overall
length, and pin position.
Explanation of the Provisions of This Action
Since an unsafe condition has been identified that is likely to
exist or develop in other Weatherly Models 620A and 620B airplanes of
the same type design that are equipped with at least one P/N 40852-001
hinge pin from a manufacturing lot that could have the above-referenced
quality control problems, the FAA issued priority letter AD 96-16-06 on
July 26, 1996, to prevent failure of the wing hinge pin. The AD
requires inspecting all wing hinge pins, P/N 40852-001, at the main
wing-to-center section attachment (four per airplane) for depth of the
threaded ends, length of the pin, and position of the pin; and
replacing or repositioning any pin, as necessary. Accomplishment of the
inspections is in accordance with the instructions in Weatherly
Aviation Company, Inc., Service Note No. 15, dated July 17, 1996. The
replacement or repositioning is accomplished in accordance with the
applicable maintenance manual.
Since it was found that immediate corrective action was required,
notice and opportunity for prior public comment thereon were
impracticable and contrary to the public interest, and good cause
existed to make the AD effective immediately by individual letters
issued on July 26, 1996 to all known U.S. operators of the following
Weatherly model and serial number airplanes:
------------------------------------------------------------------------
Model Serial Nos.
------------------------------------------------------------------------
620A...................................... 1520 through 1614.
620B...................................... 1616 through 1628.
------------------------------------------------------------------------
These conditions still exist, and the AD is hereby published in the
Federal Register as an amendment to section 39.13 of the Federal
Aviation Regulations (14 CFR 39.13) to make it effective as to all
persons.
Comments Invited
Although this action is in the form of a final rule that involves
requirements affecting immediate flight safety and, thus, was not
preceded by notice and opportunity to comment, comments are
[[Page 49054]]
invited on this rule. Interested persons are invited to comment on this
rule by submitting such written data, views, or arguments as they may
desire. Communications should 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 will
be considered, and this rule may be amended in light of the comments
received. Factual information that supports the commenter's ideas and
suggestions is extremely helpful in evaluating the effectiveness of the
AD action and determining whether additional rulemaking action would be
needed.
Comments are specifically invited on the overall regulatory,
economic, environmental, and energy aspects of the rule that might
suggest a need to modify the 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 that
summarizes each FAA-public contact concerned with the substance of this
AD will be filed in the Rules Docket.
Commenters wishing the FAA to acknowledge receipt of their comments
submitted in response to this rule must submit a self-addressed,
stamped postcard on which the following statement is made: ``Comments
to Docket No. 96-CE-42-AD.'' The postcard will be date stamped and
returned to the commenter.
Regulatory Impact
The regulations adopted herein will 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 final
rule does not have sufficient federalism implications to warrant the
preparation of a Federalism Assessment.
The FAA has determined that this regulation is an emergency
regulation that must be issued immediately to correct an unsafe
condition in aircraft, and is not a ``significant regulatory action''
under Executive Order 12866. It has been determined further that this
action involves an emergency regulation under DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979). If it is determined
that this emergency regulation otherwise would be significant under DOT
Regulatory Policies and Procedures, a final regulatory evaluation will
be prepared and placed in the Rules Docket. A copy of it, if filed, may
be obtained from the Rules Docket at the location provided under the
caption ADDRESSES.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
Accordingly, pursuant to 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
1. The authority citation for part 39 continues to read as follows:
Authority: 49 USC 106(g), 40113, 44701.
Sec. 39.13 [AMENDED]
2. Section 39.13 is amended by adding a new airworthiness directive
(AD) to read as follows:
96-16-06 Weatherly Aviation Company, Inc.: Amendment 39-9763;
Docket No. 96-CE-42-AD.
Applicability: The following model and serial number airplanes,
certificated in any category, that are equipped with at least one
part number (P/N) 40852-001 hinge pin:
------------------------------------------------------------------------
Model Serial Nos.
------------------------------------------------------------------------
620A...................................... 1520 through 1614.
620B...................................... 1616 through 1628.
------------------------------------------------------------------------
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 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 (d) 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 prior to further flight after the effective
date of this AD, unless already accomplished, except to those
operators receiving this action by priority letter issued July 26,
1996, which made these actions effective immediately upon receipt.
To prevent failure of the wing hinge pin, which could result in
the wing separating from the fuselage, accomplish the following:
(a) Inspect the wing hinge pins, P/N 40852-001, at the main spar
wing-to-center section attachment (four per airplane) for the
following in accordance with the instructions in Weatherly Aviation
Company, Inc., Service Note No. 15, dated July 17, 1996:
(1) Inspect for the depth of the threaded ends per figure 1 of
Weatherly Aviation Company, Inc., Service Note No. 15, dated July
17, 1996. If the depth exceeds .84 inches, prior to further flight,
replace the pin in accordance with the applicable maintenance
manual.
(2) Inspect for the overall length per figure 1 of Weatherly
Aviation Company, Inc., Service Note No. 15, dated July 17, 1996. If
the length is less than 3.06 inches, prior to further flight,
replace the pin in accordance with the applicable maintenance
manual.
(3) Inspect the position of the pin to ensure it is centered in
the spar hinges. If the pin position is not centered in the spar
hinges, prior to further flight, center the pin and tighten the cap
retainer bolts evenly as specified in Weatherly Aviation Company,
Inc., Service Note No. 15, dated July 17, 1996, and in accordance
with the applicable maintenance manual.
Note 2: Although not required by this AD, it is encouraged that
all pins that require replacement be returned to the Weatherly
Aviation Company, Inc., 2100 Flightline Drive, suite 1, P.O. Box 68,
Lincoln, California 95648.
(b) Send the results of the inspection required by paragraph (a)
of this AD within 10 calendar days after the inspection to the
Manager, Los Angeles Aircraft Certification Office (ACO), Attention:
W. Roberts, FAA, 3960 Paramount Boulevard, Lakewood, California
90712-4137. Include the airplane serial number, and the condition
and number of hours time-in-service of each deficient wing hinge pin
at the time of inspection. (Reporting approved by the Office of
Management and Budget under OMB no. 2120-0056.)
(c) Special flight permits may be issued in accordance with
sections 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. The hopper must be
empty during this flight.
(d) An alternative method of compliance or adjustment of the
compliance time that provides an equivalent level of safety may be
approved by the Manager, Los Angeles ACO, at the address specified
in paragraph (b) of this AD. The request shall be forwarded through
an appropriate FAA Maintenance Inspector, who may add comments and
then send it to the Manager, Los Angeles ACO.
Note 3: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be
obtained from the Los Angeles ACO.
(e) The inspections required by this AD shall be done in
accordance with Weatherly Aviation Company, Inc., Service Note No.
15, dated July 17, 1996. This incorporation by reference was
approved by the Director of the Federal Register in accordance with
5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from the
Weatherly Aviation Company, Inc., 2100 Flightline Drive, suite 1,
P.O. Box 68, Lincoln, California 95648. Copies may be inspected at
the FAA, Central Region, Office of the Assistant Chief Counsel, Room
1558, 601 E. 12th Street, Kansas City, Missouri, or at the Office of
the Federal
[[Page 49055]]
Register, 800 North Capitol Street, NW, suite 700, Washington, DC.
(f) This amendment (39-9763) becomes effective on October 6,
1996, to all persons except those persons to whom it was made
immediately effective by priority letter AD 96-16-06, issued July
26, 1996, which contained the requirements of this amendment.
Issued in Kansas City, Missouri, on September 10, 1996.
Henry A. Armstrong,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 96-23715 Filed 9-17-96; 8:45 am]
BILLING CODE 4910-13-U
