Published 2000-03-01 · Federal Register document 00-4795
Airworthiness Directives; MD Helicopters Inc. Model MD600N Helicopters
Publication summary
This amendment adopts a new airworthiness directive (AD), applicable to MD Helicopters Inc. (MDHI) Model MD600N helicopters, that requires inspecting each internal fuel hose connection to verify proper installation. This amendment is prompted by the discovery that certain fuel hose connections between the fuel cells and the engine can be incorrectly installed. The actions specified by this AD are intended to prevent fuel starvation of the engine while the fuel gage indicates fuel remaining in the tank, engine flameout, and a subsequent forced landing.
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Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:00.616356+00:00. The title, summary and date are source facts.
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Final-rule publication
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- AD identifier printed in this edition
- 2000-04-21
- Effective date printed in this edition
- Unknown
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Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 1600c2ea576b73f170701589dfb43a78f2d5579d68e8ba531babbdb10a349407. Source manifest: 9001304700d56a0d4a63be488c2e538494387b6f4cc720087ebadc2d1b058505.
Official source · 2000-03-01
Publication text
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Read the complete official publication text
[Federal Register Volume 65, Number 41 (Wednesday, March 1, 2000)]
[Rules and Regulations]
[Pages 10938-10939]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 00-4795]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 99-SW-54-AD; Amendment 39-11604; AD 2000-04-21]
RIN 2120-AA64
Airworthiness Directives; MD Helicopters Inc. Model MD600N
Helicopters
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule.
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SUMMARY: This amendment adopts a new airworthiness directive (AD),
applicable to MD Helicopters Inc. (MDHI) Model MD600N helicopters, that
requires inspecting each internal fuel hose connection to verify proper
installation. This amendment is prompted by the discovery that certain
fuel hose connections between the fuel cells and the engine can be
incorrectly installed. The actions specified by this AD are intended to
prevent fuel starvation of the engine while the fuel gage indicates
fuel remaining in the
[[Page 10939]]
tank, engine flameout, and a subsequent forced landing.
DATES: Effective April 5, 2000.
The incorporation by reference of certain publications listed in
the regulations is approved by the Director of the Federal Register as
of April 5, 2000.
ADDRESSES: The service information referenced in this AD may be
obtained from MD Helicopters Inc., Attn: Customer Support Division,
5000 E. McDowell Rd., Mail Stop M615-GO48, Mesa, Arizona 85215-9797,
telephone 1-800-388-3378 or 480-891-6342, fax 480-891-6782. This
information may be examined at the FAA, Office of the Regional Counsel,
Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas; or
at the Office of the Federal Register, 800 North Capitol Street, NW.,
suite 700, Washington, DC.
FOR FURTHER INFORMATION CONTACT: Elizabeth Bumann, Aerospace Engineer,
FAA, Los Angeles Aircraft Certification Office, 3960 Paramount Blvd.,
Lakewood, California 90712-4137, telephone (310) 627-5265; fax (310)
627-5210.
SUPPLEMENTARY INFORMATION: A proposal to amend part 39 of the Federal
Aviation Regulations (14 CFR part 39) to include an airworthiness
directive (AD) that is applicable to MDHI Model MD600N helicopters was
published in the Federal Register on December 8, 1999 (64 FR 68646).
That action proposed to require inspecting each internal fuel hose
connection to verify proper installation.
Interested persons have been afforded an opportunity to participate
in the making of this amendment. No comments were received on the
proposal or the FAA's determination of the cost to the public. The FAA
has determined that air safety and the public interest require the
adoption of the rule as proposed.
The FAA estimates that 40 helicopters of U.S. registry will be
affected by this AD, that it will take approximately 8 work hours per
helicopter to accomplish the required actions, and that the average
labor rate is $60 per work hour. Based on these figures, the total cost
impact of the AD on U.S. operators is estimated to be $19,200.
The regulations adopted herein 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. Therefore, it
is determined that this final rule does not have federalism
implications under Executive Order 13132.
For the reasons discussed above, I certify that this action: (1) Is
not a ``significant regulatory action'' under Executive Order 12866;
(2) is not a ``significant rule'' under 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. A final evaluation has been prepared for this action
and it is contained in the Rules Docket. A copy of it 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 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
2. Section 39.13 is amended by adding a new airworthiness directive
to read as follows:
AD 2000-04-21 MD Helicopters, Inc.: Amendment 39-11604. Docket No.
99-SW-54-AD.
Applicability: Model MD600N helicopters, serial numbers with a
prefix of ``RN'' 003 through 045, certificated in any category.
Note 1: This AD applies to each helicopter identified in the
preceding applicability provision, regardless of whether it has been
otherwise 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 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.
To prevent fuel starvation of the engine while the fuel gage
indicates fuel remaining in the tank, engine flameout, and a
subsequent forced landing, accomplish the following:
(a) Within 100 hours time-in-service, verify that the internal
fuel hose connections have been properly installed in accordance
with either Method A or Method B of the Accomplishment Instructions
of MD Helicopters Service Bulletin SB 600N-025, dated July 2, 1999.
Prior to further flight, make any necessary corrections.
(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, Los Angeles Aircraft Certification
Office. 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.
(d) The inspections shall be done in accordance with either
Method A or Method B of the Accomplishment Instructions of MD
Helicopters Service Bulletin SB 600N-025, dated July 2, 1999. 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 MD Helicopters Inc., Attn: Customer
Support Division, 5000 E. McDowell Rd., Mail Stop M615-GO48, Mesa,
Arizona 85215-9797, telephone 1-800-388-3378 or 480-891-6342, fax
480-891-6782. Copies may be inspected at the FAA, Office of the
Regional Counsel, Southwest Region, 2601 Meacham Blvd., Room 663,
Fort Worth, Texas; or at the Office of the Federal Register, 800
North Capitol Street, NW., suite 700, Washington, DC.
(e) This amendment becomes effective on April 5, 2000.
Issued in Fort Worth, Texas, on February 22, 2000.
Henry A. Armstrong,
Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. 00-4795 Filed 2-29-00; 8:45 am]
BILLING CODE 4910-13-P
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These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
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