Published 2004-04-28 · Federal Register document 04-9377
Airworthiness Directives; HPH s. r. o. Models Glasflügel 304CZ, 304CZ-17, and 304C Sailplanes
Publication summary
The FAA adopts a new airworthiness directive (AD) for certain HPH s. r. o. (HPH) Models Glasfl[uuml]gel 304CZ, 304CZ-17, and 304C sailplanes. This AD requires you to inspect to determine the airbrake handle attachment rivet material. This AD also requires you to replace any non-steel rivet with a steel rivet. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for the Czech Republic. We are issuing this AD to prevent the airbrake handle from becoming loose, which could result in failure of the airbrake control. This failure could lead to loss of control of the sailplane.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:13.905821+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2004-cb1e1f18d61cac01
- Source row
- results[191]
- Raw source SHA-256
- cb1e1f18d61cac01616802134d899b0c8ce1a9f79716b5ee037f78e4cb53a00a
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2004-09-03
- Effective date printed in this edition
- Unknown
Read 8 complete recorded clauses
When Does This AD Become Effective?
When Does This AD Become Effective?
(a) This AD becomes effective on June 11, 2004.
Exact source excerpt. Text positions 8530–8620, end exclusive, in the original decoded publication. SHA-256: 839f156f4dd86aaf50b85dba52922fdaf7351a5d899131c26c65842c03d8df00
What Other ADs Are Affected by This Action?
What Other ADs Are Affected by This Action?
(b) None.
Exact source excerpt. Text positions 8620–8680, end exclusive, in the original decoded publication. SHA-256: 07ddca3e2ddd18af7ec96332163aefb7f30c8d066e5f6fc3b158d5fa460e1365
What Sailplanes Are Affected by This AD?
What Sailplanes Are Affected by This AD?
(c) This AD affects Models Glasfl[uuml]gel 304CZ, 304CZ-17, and
304C sailplanes, serial numbers 1 through 60-17, that are
certificated in any category.
Exact source excerpt. Text positions 8680–8881, end exclusive, in the original decoded publication. SHA-256: 737eceb9e7354d0971ae1a0cc9efd45e9ac4ccfd34119f9a32cd6400b01799f9
What Is the Unsafe Condition Presented in This AD?
What Is the Unsafe Condition Presented in This AD?
(d) This AD is the result of mandatory continuing airworthiness
information (MCAI) issued by the airworthiness authority for the
Czech Republic. The actions specified in this AD are intended to
prevent the airbrake handle from becoming loose, which could result
in failure of the airbrake control. This failure could lead to loss
of control of the sailplane.
Exact source excerpt. Text positions 8881–9302, end exclusive, in the original decoded publication. SHA-256: 2a5996590719bf16a95b040085c7da97016173458bfa8ec294a643c9b3876784
What Must I do To Address This Problem?
What Must I do To Address This Problem?
(e) To address this problem, you must do the following:
------------------------------------------------------------------------
Actions Compliance Procedures
------------------------------------------------------------------------
(1) Inspect to determine the Within the next 25 Follow HPH spol.s
airbrake handle attachment hours time-in- r.o. Mandatory
rivet material. service (TIS) Bulletin No.:
after June 11, G304CZ-05 a)
2004 (the G304CZ17-05 a),
effective date of dated March 26,
this AD). 2003.
(2) Replace any non-steel Before further Follow HPH spol.s
attachment rivet with a steel flight after the r.o. Mandatory
rivet. inspection Bulletin No.:
required in G304CZ-05 a)
paragraph (e)(1) G304CZ17-05 a),
of this AD. dated March 26,
2003.
------------------------------------------------------------------------
Exact source excerpt. Text positions 9302–10657, end exclusive, in the original decoded publication. SHA-256: a3e01a015a7cce14d88dfa044f5dc9e1fbda6154824a38c57cdf635d77a28274
May I Request an Alternative Method of Compliance?
May I Request an Alternative Method of Compliance?
(f) You may request a different method of compliance or a
different compliance time for this AD by following the procedures in
14 CFR 39.19. Unless FAA authorizes otherwise, send your request to
your principal inspector. The principal inspector may add comments
and will send your request to the Manager, Standards Office, Small
Airplane Directorate, FAA. For information on any already approved
alternative methods of compliance, contact Greg Davison, Aerospace
Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301,
Kansas City, Missouri 64106; telephone: (816) 329-4130; facsimile:
(816) 329-4090.
Exact source excerpt. Text positions 10657–11334, end exclusive, in the original decoded publication. SHA-256: d5786e8568a52ca6f110d7de31295c98fcac4cf0c6ac248ede05f3139903c867
Does This AD Incorporate Any Material by Reference?
Does This AD Incorporate Any Material by Reference?
(g) You must do the actions required by this AD following the
instructions in HPH spol.s r.o. Mandatory Bulletin No.: G304CZ-05 a)
G304CZ17-05 a), dated March 26, 2003. The Director of the Federal
Register approved the incorporation by reference of this service
bulletin in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. You
may get a copy from HPH spol.s r.o., C[aacute]slavsk[aacute] 126,
P.O. Box 112, CZ284 01 Kutn[aacute] Hora, Czech Republic; telephone:
011-42-327 513441; e-mail: [email protected]. You may review copies at FAA,
Central Region, Office of the Regional Counsel, 901 Locust, Room
506, Kansas City, Missouri 64106; or at the Office of the Federal
Register, 800 North Capitol Street, NW., suite 700, Washington, DC.
Exact source excerpt. Text positions 11334–12141, end exclusive, in the original decoded publication. SHA-256: 94e099c0eb7c70d1f003a78429c6319402d67eac6c7b0dc183506ec4976c6ef5
Is There Other Information That Relates to This Subject?
Is There Other Information That Relates to This Subject?
(h) Czech Republic AD Number CAA-AD-040/2003, dated May 6, 2003,
also addresses the subject of this AD.
Exact source excerpt. Text positions 12141–12308, end exclusive, in the original decoded publication. SHA-256: 9563a1e1cd296ce70c21f42d8e7c24e3f62cc9cce273a911864e54d8d9ffdfed
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2004-09-03 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 489ceaf95f3e07af87416b1753a4ac41bb4409e70888d3ea42eb1f949081e357. Source manifest: 714760d5a5bb74657cfa93e7cece7e63be5e4aa6156d397e361db0ae4c769d0d.
Official source · 2004-04-28
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 69, Number 82 (Wednesday, April 28, 2004)]
[Rules and Regulations]
[Pages 23099-23101]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 04-9377]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2003-CE-63-AD; Amendment 39-13592; AD 2004-09-03]
RIN 2120-AA64
Airworthiness Directives; HPH s. r. o. Models Glasfl[uuml]gel
304CZ, 304CZ-17, and 304C Sailplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA adopts a new airworthiness directive (AD) for certain
HPH s. r. o. (HPH) Models Glasfl[uuml]gel 304CZ, 304CZ-17, and 304C
sailplanes. This AD requires you to inspect to determine the airbrake
handle attachment rivet material. This AD also
[[Page 23100]]
requires you to replace any non-steel rivet with a steel rivet. This AD
is the result of mandatory continuing airworthiness information (MCAI)
issued by the airworthiness authority for the Czech Republic. We are
issuing this AD to prevent the airbrake handle from becoming loose,
which could result in failure of the airbrake control. This failure
could lead to loss of control of the sailplane.
DATES: This AD becomes effective on June 11, 2004.
As of June 11, 2004, the Director of the Federal Register approved
the incorporation by reference of certain publications listed in the
regulation.
ADDRESSES: You may get the service information identified in this AD
from HPH spol.s r.o., C[aacute]slavsk[aacute] 126, P.O. Box 112, CZ284
01 Kutn[aacute] Hora, Czech Republic; telephone: 011-42-327 513441; e-
mail: [email protected].
You may view the AD docket at FAA, Central Region, Office of the
Regional Counsel, Attention: Rules Docket No. 2003-CE-63-AD, 901
Locust, Room 506, Kansas City, Missouri 64106. Office hours are 8 a.m.
to 4 p.m., Monday through Friday, except Federal holidays.
FOR FURTHER INFORMATION CONTACT: Greg Davison, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329-4130; facsimile: (816) 329-4090.
SUPPLEMENTARY INFORMATION:
Discussion
What events have caused this AD? The Civil Aviation Authority
(CAA), which is the airworthiness authority for the Czech Republic,
recently notified FAA that an unsafe condition may exist on certain HPH
Models Glasfl[uuml]gel 304CZ, 304CZ-17, and 304C sailplanes. The CAA
reports that excessive free play in the airbrake handle was found
during a pre-flight check on a Glasfl[uuml]gel 304CZ sailplane.
A non-steel (duralumin) rivet connecting the airbrake handle to the
pushrod had become loose.
What is the potential impact if FAA took no action? If not
corrected, a loose airbrake handle could result in failure of airbrake
control. This failure could lead to loss of control of the sailplane.
Has FAA taken any action to this point? 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 HPH Models Glasfl[uuml]gel
304CZ, 304CZ-17, and 304C sailplanes. This proposal was published in
the Federal Register as a notice of proposed rulemaking (NPRM) on
February 4, 2004 (69 FR 5302). The NPRM proposed to require you to
inspect to determine the airbrake handle attachment rivet material and
replace any non-steel rivet with a steel rivet.
Comments
Was the public invited to comment? We provided the public the
opportunity to participate in developing this AD. We received no
comments on the proposal or on the determination of the cost to the
public.
Conclusion
What is FAA's final determination on this issue? We have carefully
reviewed the available data and determined that air safety and the
public interest require adopting the AD as proposed except for 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.
Changes to 14 CFR Part 39--Effect on the AD
How does the revision to 14 CFR part 39 affect this AD? On July 10,
2002, the FAA published a new version of 14 CFR part 39 (67 FR 47997,
July 22, 2002), which governs the FAA's AD system. This regulation now
includes material that relates to altered products, special flight
permits, and alternative methods of compliance. This material
previously was included in each individual AD. Since this material is
included in 14 CFR part 39, we will not include it in future AD
actions.
Costs of Compliance
How many sailplanes does this AD impact? We estimate that this AD
affects 12 sailplanes in the U.S. registry.
What is the cost impact of this AD on owners/operators of the
affected sailplanes? We estimate the following costs to accomplish the
inspection:
----------------------------------------------------------------------------------------------------------------
Total Cost Per Total Cost on U.S.
Labor Cost Parts Cost Sailplane Operators
----------------------------------------------------------------------------------------------------------------
1 workhour x $65 per hour = $65...... Not applicable......... $65.................... $65 x 12 = $780.
----------------------------------------------------------------------------------------------------------------
We estimate the following costs to accomplish any necessary
replacements that will be required based on the results of this
inspection. We have no way of determining the number of sailplanes that
may need this replacement:
------------------------------------------------------------------------
Total Cost Per
Labor Cost Parts Cost Sailplane Airbrake
Handle
------------------------------------------------------------------------
1 workhour x $65 per hour = $65. $10 for each $65 + $30 (to
rivet. 3 rivets replace all 3
on each airbrake rivets) = $95.
handle.
------------------------------------------------------------------------
Regulatory Findings
Will this AD impact various entities? 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.
Will this AD involve a significant rule or regulatory action? 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
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
``AD Docket No. 2003-CE-63-AD'' in your request.
[[Page 23101]]
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:
2004-09-03 HPH s. r. o.: Amendment 39-13592; Docket No. 2003-CE-63-
AD.
When Does This AD Become Effective?
(a) This AD becomes effective on June 11, 2004.
What Other ADs Are Affected by This Action?
(b) None.
What Sailplanes Are Affected by This AD?
(c) This AD affects Models Glasfl[uuml]gel 304CZ, 304CZ-17, and
304C sailplanes, serial numbers 1 through 60-17, that are
certificated in any category.
What Is the Unsafe Condition Presented in This AD?
(d) This AD is the result of mandatory continuing airworthiness
information (MCAI) issued by the airworthiness authority for the
Czech Republic. The actions specified in this AD are intended to
prevent the airbrake handle from becoming loose, which could result
in failure of the airbrake control. This failure could lead to loss
of control of the sailplane.
What Must I do To Address This Problem?
(e) To address this problem, you must do the following:
------------------------------------------------------------------------
Actions Compliance Procedures
------------------------------------------------------------------------
(1) Inspect to determine the Within the next 25 Follow HPH spol.s
airbrake handle attachment hours time-in- r.o. Mandatory
rivet material. service (TIS) Bulletin No.:
after June 11, G304CZ-05 a)
2004 (the G304CZ17-05 a),
effective date of dated March 26,
this AD). 2003.
(2) Replace any non-steel Before further Follow HPH spol.s
attachment rivet with a steel flight after the r.o. Mandatory
rivet. inspection Bulletin No.:
required in G304CZ-05 a)
paragraph (e)(1) G304CZ17-05 a),
of this AD. dated March 26,
2003.
------------------------------------------------------------------------
May I Request an Alternative Method of Compliance?
(f) You may request a different method of compliance or a
different compliance time for this AD by following the procedures in
14 CFR 39.19. Unless FAA authorizes otherwise, send your request to
your principal inspector. The principal inspector may add comments
and will send your request to the Manager, Standards Office, Small
Airplane Directorate, FAA. For information on any already approved
alternative methods of compliance, contact Greg Davison, Aerospace
Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301,
Kansas City, Missouri 64106; telephone: (816) 329-4130; facsimile:
(816) 329-4090.
Does This AD Incorporate Any Material by Reference?
(g) You must do the actions required by this AD following the
instructions in HPH spol.s r.o. Mandatory Bulletin No.: G304CZ-05 a)
G304CZ17-05 a), dated March 26, 2003. The Director of the Federal
Register approved the incorporation by reference of this service
bulletin in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. You
may get a copy from HPH spol.s r.o., C[aacute]slavsk[aacute] 126,
P.O. Box 112, CZ284 01 Kutn[aacute] Hora, Czech Republic; telephone:
011-42-327 513441; e-mail: [email protected]. You may review copies at FAA,
Central Region, Office of the Regional Counsel, 901 Locust, Room
506, Kansas City, Missouri 64106; or at the Office of the Federal
Register, 800 North Capitol Street, NW., suite 700, Washington, DC.
Is There Other Information That Relates to This Subject?
(h) Czech Republic AD Number CAA-AD-040/2003, dated May 6, 2003,
also addresses the subject of this AD.
Issued in Kansas City, Missouri, on April 19, 2004.
Dorenda D. Baker,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 04-9377 Filed 4-27-04; 8:45 am]
BILLING CODE 4910-13-P
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