[Federal Register Volume 63, Number 68 (Thursday, April 9, 1998)]
[Proposed Rules]
[Pages 17346-17348]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 98-9339]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 97-NM-71-AD]
RIN 2120-AA64
Airworthiness Directives; Mitsubishi Heavy Industries Ltd. Model
YS-11 and YS-11A 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 all Mitsubishi Model YS-11 and YS-
11A series airplanes. This proposal would require revising the airplane
flight manual (AFM) to prohibit positioning the power levers below the
flight idle stop. This proposal is a result of incidents and accidents
involving airplanes equipped with turboprop engines in which the
propeller beta was used improperly during flight. The actions specified
by the proposed AD are intended to prevent loss of airplane
controllability or engine overspeed with consequent loss of engine
power caused by the power levers being positioned below the flight idle
stop while the airplane is in flight.
DATES: Comments must be received by May 26, 1998.
ADDRESSES: Submit comments in triplicate to the Federal Aviation
Administration (FAA), Transport Airplane Directorate, ANM-103,
Attention: Rules Docket No. 97-NM-71-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.
FOR FURTHER INFORMATION CONTACT: Mark Quam, Aerospace Engineer,
Standardization Branch, ANM-113; FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-2145; fax (425) 227-1149.
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 97-NM-71-AD.'' The postcard will be date stamped and
returned to the commenter.
[[Page 17347]]
Availability of NPRMs
Any person may obtain a copy of this NPRM by submitting a request
to the FAA, Transport Airplane Directorate, ANM-103, Attention: Rules
Docket No. 97-NM-71-AD, 1601 Lind Avenue, SW., Renton, Washington
98055-4056.
Discussion
In recent years, the FAA has received reports of 14 incidents and/
or accidents on airplanes equipped with turboprop engines in which
intentional or inadvertent operation of the propellers in the beta
range occurred during flight. (For the purposes of this proposal, beta
is the range of propeller operation intended for use during taxi,
ground idle, or reverse operations as controlled by the power lever
settings aft of the flight idle stop.)
Five of the 14 in-flight beta occurrences were classified as
accidents. In each of these five cases, operation of the propellers in
the beta range occurred during flight. Operation of the propellers in
the beta range during flight, if not prevented, could result in loss of
airplane controllability, or engine overspeed with consequent loss of
engine power.
Communication between the FAA and the public during a meeting held
on June 11-12, 1996, in Seattle, Washington, revealed a lack of
consistency of the information on in-flight beta operation contained in
the FAA-approved airplane flight manual (AFM) for airplanes not
certificated for in-flight operation with the power levers below the
flight idle stop. (Airplanes that are certificated for this type of
operation are not affected by the above-referenced conditions.)
U.S. Type Certification of the Airplane
This airplane model is manufactured in Japan and is type
certificated for operation in the United States under the provisions of
Section 21.29 of the Federal Aviation Regulations and the applicable
bilateral airworthiness agreement. The FAA has reviewed all available
information, and determined that AD action is necessary for products of
this type design that are certificated for operation in the United
States.
The FAA's Determination
The FAA has examined the circumstances and reviewed all available
information related to the incidents and accidents described
previously. The FAA finds that the Limitations Section of the AFM's for
certain airplanes must be revised to prohibit positioning the power
levers below the flight idle stop while the airplane is in flight, and
to provide a statement of the consequences of positioning the power
levers below the flight idle stop. The FAA has determined that the
affected airplanes include those that are equipped with turboprop
engines and that are not certificated for in-flight operation with the
power levers below the flight idle stop. Since Mitsubishi Model YS-11
and YS-11A series airplanes meet these criteria, the FAA finds that the
AFM's for these airplanes must be revised to include the limitation and
statement of consequences described previously.
Explanation of the Requirements of the Proposed AD
Since an unsafe condition has been identified that is likely to
exist or develop in Mitsubishi Model YS-11 and YS-11A series airplanes
of the same type design, the proposed AD would require revising the
Limitations Section of the AFM to prohibit the positioning of the power
levers below the flight idle stop while the airplane is in flight, and
to add a statement of the consequences of positioning the power levers
below the flight idle stop while the airplane is in flight.
Interim Action
This is considered interim action until final action is identified,
at which time the FAA may consider further rulemaking.
Cost Impact
The FAA estimates that 10 Mitsubishi Model YS-11 and YS-11A series
airplanes of U.S. registry would be affected by this proposed AD, that
it would take approximately 1 work hour per airplane to accomplish the
proposed actions, and that the average labor rate is $60 per work hour.
Based on these figures, the cost impact of the proposed AD on U.S.
operators is estimated to be $600, or $60 per airplane.
The cost impact figure discussed above is 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.
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:
Mitsubishi Heavy Industries, Ltd. [Formerly Nihon Aeroplane
Manufacturing Company (NMAC)]: Docket 97-NM-71-AD.
Applicability: All Model YS-11 and YS-11A -200, -300, -500, and
-600 series airplanes; certificated in any category.
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 (b) 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.
[[Page 17348]]
To prevent loss of airplane controllability or engine overspeed
with consequent loss of engine power caused by the power levers
being positioned below the flight idle stop while the airplane is in
flight, accomplish the following:
(a) Within 30 days after the effective date of this AD, revise
the Limitations Section of the FAA-approved Airplane Flight Manual
(AFM) to include the following statements. This action may be
accomplished by inserting a copy of this AD into the AFM.
Warning: While the airplane is airborne, the LOW STOP lever (flight
fine pitch stop) should not be placed in the GROUND position for any
reason. Placing the LOW STOP lever in the GROUND position in flight
may lead to loss of airplane control or may result in an engine
overspeed condition and consequent loss of engine power.
(b) 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, Standardization Branch, ANM-113;
FAA, Transport Airplane Directorate. Operators shall submit their
requests through an appropriate FAA Principal Operations Inspector,
who may add comments and then send it to the Manager,
Standardization Branch, ANM-113.
Note 2: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be
obtained from the Standardization Branch, ANM-113.
(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.
Issued in Renton, Washington, on April 3, 1998.
S.R. Miller,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 98-9339 Filed 4-8-98; 8:45 am]
BILLING CODE 4910-13-U
