[Federal Register Volume 60, Number 181 (Tuesday, September 19, 1995)]
[Proposed Rules]
[Pages 48428-48429]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 95-23123]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 95-SW-19-AD]
Airworthiness Directives; Flight Trails Helicopters, Inc.,
Hardpoint Assemblies Installed on McDonnell Douglas Helicopter Systems
Model 369D, 369E, 369F, 369FF, and 500N Helicopters
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 Flight Trails Helicopters, Inc.
hardpoint assemblies, installed in accordance with Supplemental Type
Certificate (STC) No. SH6080NM, or in accordance with Federal Aviation
Administration (FAA) Form 337, ``Major Repair and Alteration,''
approved on McDonnell Douglas Helicopter Systems (MDHS) Model 369D,
369E, 369F, 369FF, and 500N helicopters. This proposal would require
removing any Flight Trails Helicopters, Inc. hardpoint assembly not
identified by part number (P/N) and serial number (S/N). This proposal
is prompted by two incidents in which the hardpoint assembly used to
support a search light or night vision system reportedly failed. The
actions specified by the proposed AD are intended to prevent failure of
the hardpoint assembly, separation of the hardpoint assembly from the
helicopter, and subsequent contact between the hardpoint assembly and
the fuselage or rotor system of the helicopter.
DATES: Comments must be received by November 20, 1995.
ADDRESSES: Submit comments in triplicate to the FAA, Office of the
Assistant Chief Counsel, Attention: Rules Docket No. 95-SW-19-AD, 2601
Meacham Blvd., Room 663, Fort Worth, Texas 76137. 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: Mr. James Wang, Aerospace Engineer,
FAA, Los Angeles Aircraft Certification Office, 3960 Paramount Blvd.,
Lakewood, California 90712, telephone (310) 627-5232, fax (310) 627-
5210.
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 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,
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 No. 95-SW-19-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, Office of the Assistant Chief Counsel, Attention: Rules
Docket No. 95-SW-19-AD, 2601 Meacham Blvd., Room 663, Fort Worth, Texas
76137.
Discussion
This document proposes the adoption of a new AD that is applicable
to Flight Trails Helicopters, Inc. hardpoint assemblies installed in
accordance with STC No. SH6080NM, or in accordance with FAA Form 337,
``Major Repair and Alteration,'' approved on MDHS Model 369D, 369E,
369F, 369FF, and 500N helicopters. Two incidents have occurred in which
the hardpoint assembly reportedly failed at its installation weld. The
hardpoint assembly is used to attach equipment such as a search light
or night vision
[[Page 48429]]
system to the helicopter's fuselage. In the first incident, a failure
occurred in the hardpoint installation weld area due to a fatigue
crack. The discovery of a crack in the hardpoint assembly installation
weld on a second helicopter occurred during a visual ground check. This
condition, if not corrected, could result in failure of the hardpoint
assembly, separation of the hardpoint assembly from the helicopter, and
subsequent contact between the hardpoint assembly and the fuselage or
rotor system of the helicopter.
Since an unsafe condition has been identified that is likely to
exist or develop on other Flight Trails Helicopters, Inc. hardpoint
assemblies installed on MDHS Model 369D, 369E, 369F, 369FF, and 500N
helicopters of the same type design, the proposed AD would require,
before further flight, removing the hardpoint assembly that secures a
searchlight or night vision system to the helicopter.
The FAA estimates that 59 helicopters of U.S. registry would be
affected by this proposed AD, that it would take approximately 1 work
hour per helicopter to accomplish the proposed actions, and that the
average labor rate is $60 per work hour. Based on these figures, the
total cost impact of the proposed AD on U.S. operators is estimated to
be $3,540.
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), 40101, 40113, 44701.
Sec. 39.13 [Amended]
2. Section 39.13 is amended by adding a new airworthiness directive
to read as follows:
Flight Trails Helicopters, Inc.: Docket No. 95-SW-19-AD.
Applicability: McDonnell Douglas Helicopters Systems (MDHS)
Model 369D, 369E, 369F, 369FF, and 500N helicopters, that have been
modified in accordance with Supplemental Type Certificate (STC) No.
SH6080NM, or in accordance with a Federal Aviation Administration
(FAA) Form 337, ``Major Repair and Alteration,'' using Flight Trails
Helicopters, Inc. hardpoint assemblies, certificated in any
category.
Note 1: This AD applies to each helicopter 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 helicopters that have been modified,
altered, or repaired so that the performance of the requirements of
this AD is affected, the owner/operator must use the authority
provided in paragraph (b) to request approval from the FAA. This
approval may address either no action, if the current configuration
eliminates the unsafe condition, or different actions necessary to
address the unsafe condition described in this AD. Such a request
should include an assessment of the effect of the changed
configuration on the unsafe condition addressed by this AD. In no
case does the presence of any modification, alteration, or repair
remove any helicopter from the applicability of this AD.
Note 2: Information concerning the hardpoint assemblies may be
obtained from Flight Trails Helicopters, Inc., ATTN: Mr. Larry
Anderson, 4805 Falcon Drive, Mesa, Arizona, 85205, telephone (602)
396-8242.
Compliance: Required as indicated, unless accomplished
previously. To prevent failure of the hardpoint assembly, separation
of the hardpoint assembly from the helicopter, and subsequent
contact between the hardpoint assembly and the fuselage or rotor
system of the helicopter, accomplish the following:
(a) Before further flight, remove from the helicopter any Flight
Trails Helicopters, Inc. hardpoint assembly not marked with a part
number (P/N) and serial number (S/N) by removing the NAS 1351-3 cap
screw that secures the hardpoint assembly to the jacking fitting, P/
N 369H2521, and slipping the hardpoint assembly out of the step
mount.
The only Flight Trails Helicopters, Inc. hardpoint assemblies
that are considered airworthy and eligible for installation are
those hardpoint assemblies marked with a serial number and either P/
N FTH 105 LH Mod 1, for a hardpoint assembly mounted on the left
side of the helicopter, or P/N FTH 105 RH Mod 1, for a hardpoint
assembly mounted on the right side.
(b) An alternative method of compliance or adjustment of the
compliance time that provides an acceptable level of safety may be
used when approved by the Manager, Los Angeles Aircraft
Certification Office, FAA. Operators shall submit their requests
through an FAA Principal Maintenance Inspector, who may concur or
comment and then send it to the Manager, Los Angeles Aircraft
Certification Office.
Note 2: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be
obtained from the Los Angeles Aircraft Certification Office.
(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 helicopter to a location where
the requirements of this AD can be accomplished.
Issued in Fort Worth, Texas, on September 11, 1995.
Eric Bries,
Acting Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. 95-23123 Filed 9-18-95; 8:45 am]
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