Published 2000-05-26 · Federal Register document 00-12813
Airworthiness Directives; Israel Aircraft Industries, Ltd., Model 1125 Westwind Astra and Astra SPX Series Airplanes
Publication summary
This amendment adopts a new airworthiness directive (AD), applicable to certain Israel Aircraft Industries, Ltd., Model 1125 Westwind Astra and Astra SPX series airplanes, that requires replacement of the existing pneumatic de-icing boot pressure indicator switch with a newly designed switch. This amendment is prompted by an occurrence on a similar airplane model in which the pneumatic de-icing boot indication light may have provided the flightcrew with misleading information as to the proper functioning of the de-icing boots. The actions specified by this AD are intended to prevent ice accumulation on the airplane leading edges, which could result in reduced controllability of the airplane.
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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.
- Source revision
- federal_register_ad_metadata_2000-18aee3630151116d
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- 18aee3630151116d2fb3a6893673332fd0937cde18bc691722f3a802a62279eb
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2000-10-19
- Effective date printed in this edition
- 2000-06-30
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Read 2 complete recorded clauses
Applicability wording · Applicability
Applicability: Model 1125 Westwind Astra and Astra SPX series
airplanes, serial numbers 004 through 115 inclusive; 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.
Exact source excerpt. Text positions 6981–7880, end exclusive, in the original decoded publication. SHA-256: 6fc61d6f0b05e2d0455085cde10eed8e03b9bb8e3f7ca1d89c074440b203413d
Compliance and requirements
Compliance: Required as indicated, unless accomplished
previously.
To prevent ice accumulation on the airplane leading edges, which
could result in reduced controllability of the airplane, accomplish
the following:
Modification
(a) Within 1 year after the effective date of this AD, replace
the pneumatic de-icing boot pressure indicator switch with a switch
that activates the flight deck indicator light at 15 pounds per
square inch gage, in accordance with Astra Alert Service Bulletin
1125-30A-199, dated April 17, 2000, or in accordance with a method
approved by the Manager, International Branch, ANM-116, FAA,
Transport Airplane Directorate.
Alternative Methods of Compliance
(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, International Branch, ANM-116.
Operators shall submit their requests through an appropriate FAA
Principal Maintenance Inspector, who may add comments and then send
it to the Manager, International Branch, ANM-116.
Note 2: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be
obtained from the International Branch, ANM-116.
Special Flight Permits
(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.
Incorporation by Reference
(d) Except as provided by paragraph (a) of this AD, the actions
shall be done in accordance with Astra Alert Service Bulletin 1125-
30A-199, dated April 17, 2000. 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
Galaxy Aerospace Corporation, One Galaxy Way, Fort Worth Alliance
Airport, Fort Worth, Texas 76177. Copies may be inspected at the
FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton,
Washington; or at the Office of the Federal Register, 800 North
Capitol Street, NW., suite 700, Washington, DC.
Note 3: The subject of this AD is addressed in Israeli
airworthiness directive 30-00-02-05, dated February 24, 2000.
(e) This amendment becomes effective on June 30, 2000.
Exact source excerpt. Text positions 7880–10288, end exclusive, in the original decoded publication. SHA-256: 78a335f771632040b049050756ed760defa814b9fb825d1d657fc21fe5f5a3f8
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 2000-10-19 · 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.
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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: 0012fa1ad0643f21dbd4aea36dc39da7889cbe570a60b003f376a790a7ba969b. Source manifest: 157782d64cdb6856706edd47c3976ce6b4c8f066317798690d13d32bc3fbfd24.
Official source · 2000-05-26
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 65, Number 103 (Friday, May 26, 2000)]
[Rules and Regulations]
[Pages 34054-34055]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 00-12813]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 99-NM-360-AD; Amendment 39-11743; AD 2000-10-19]
RIN 2120-AA64
Airworthiness Directives; Israel Aircraft Industries, Ltd., Model
1125 Westwind Astra and Astra SPX Series Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: This amendment adopts a new airworthiness directive (AD),
applicable to certain Israel Aircraft Industries, Ltd., Model 1125
Westwind Astra and Astra SPX series airplanes, that requires
replacement of the existing pneumatic de-icing boot pressure indicator
switch with a newly designed switch. This amendment is prompted by an
occurrence on a similar airplane model in which the pneumatic de-icing
boot indication light may have provided the flightcrew with misleading
information as to the proper functioning of the de-icing boots. The
actions specified by this AD are intended to prevent ice accumulation
on the airplane leading edges, which could result in reduced
controllability of the airplane.
DATES: Effective June 30, 2000.
The incorporation by reference of certain publications listed in
the regulations is approved by the Director of the Federal Register as
of June 30, 2000.
ADDRESSES: The service information referenced in this AD may be
obtained from Galaxy Aerospace Corporation, One Galaxy Way, Fort Worth
Alliance Airport, Fort Worth, Texas 76177. This information may be
examined at the Federal Aviation Administration (FAA), Transport
Airplane Directorate, Rules Docket, 1601 Lind Avenue, SW., Renton,
Washington; or at the Office of the Federal Register, 800 North Capitol
Street, NW., suite 700, Washington, DC.
FOR FURTHER INFORMATION CONTACT: Norman B. Martenson, Manager,
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-2110; fax (425) 227-1149.
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 all Israel Aircraft Industries,
Ltd., Model 1125 Westwind Astra and Astra SPX series airplanes was
published in the Federal Register on January 24, 2000 (65 FR 3617).
That action proposed to require replacement of the existing pneumatic
de-icing boot pressure indicator switch with a newly designed switch.
Interested persons have been afforded an opportunity to participate
in the making of this amendment. No comments were submitted in response
to the proposal or the FAA's determination of the cost to the public.
Changes to the Proposed AD
Since issuance of the proposed AD, the manufacturer has issued
Astra Alert Service Bulletin 1125-30A-199, dated April 17, 2000, which
describes procedures for replacement of the wing and tail de-icing boot
pressure indicator switches with improved switches. The Civil Aviation
Administration of Israel (CAAI), which is the airworthiness authority
for Israel, classified this service bulletin as mandatory.
Additionally, the CAAI previously issued Israeli airworthiness
directive 30-00-02-05, dated February 24, 2000, in order to assure the
continued airworthiness of these airplanes in Israel.
The FAA has determined that the replacement described in the
service bulletin provides an adequate method of addressing the unsafe
condition identified in this AD. Paragraph (a) of the AD has been
revised to include that replacement as an acceptable means of
compliance to the requirements of the AD. The applicability of the AD
has also been revised to exclude airplanes having serial number 116 and
up, on which the replacement will be installed in production.
The FAA has also revised the ``Cost Impact'' section of the AD to
provide the estimated cost of the replacement in accordance with the
previously described service bulletin, and to revise the number of
affected airplanes of U.S. registry.
Conclusion
After careful review of the available data, the FAA has determined
that air safety and the public interest require the adoption of the
rule with the changes described previously. The FAA has determined that
these changes will neither increase the economic burden on any operator
nor increase the scope of the AD.
Cost Impact
The FAA estimates that 89 airplanes of U.S. registry will be
affected by this AD.
Should an operator elect to accomplish the replacement in
accordance with Astra Alert Service Bulletin 1125-30A-199, it will take
approximately 2 work hours per airplane to accomplish it, at an average
labor rate of $60 per work hour. Required parts may cost as much as
$1,455 per airplane. Based on these figures, the cost impact of the
replacement on U.S. operators is estimated to be as much as $1,575 per
airplane.
Regulatory Impact
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:
[[Page 34055]]
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:
2000-10-19 Israel Aircraft Industries, Ltd.: Amendment 39-11743.
Docket 99-NM-360-AD.
Applicability: Model 1125 Westwind Astra and Astra SPX series
airplanes, serial numbers 004 through 115 inclusive; 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.
To prevent ice accumulation on the airplane leading edges, which
could result in reduced controllability of the airplane, accomplish
the following:
Modification
(a) Within 1 year after the effective date of this AD, replace
the pneumatic de-icing boot pressure indicator switch with a switch
that activates the flight deck indicator light at 15 pounds per
square inch gage, in accordance with Astra Alert Service Bulletin
1125-30A-199, dated April 17, 2000, or in accordance with a method
approved by the Manager, International Branch, ANM-116, FAA,
Transport Airplane Directorate.
Alternative Methods of Compliance
(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, International Branch, ANM-116.
Operators shall submit their requests through an appropriate FAA
Principal Maintenance Inspector, who may add comments and then send
it to the Manager, International Branch, ANM-116.
Note 2: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be
obtained from the International Branch, ANM-116.
Special Flight Permits
(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.
Incorporation by Reference
(d) Except as provided by paragraph (a) of this AD, the actions
shall be done in accordance with Astra Alert Service Bulletin 1125-
30A-199, dated April 17, 2000. 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
Galaxy Aerospace Corporation, One Galaxy Way, Fort Worth Alliance
Airport, Fort Worth, Texas 76177. Copies may be inspected at the
FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton,
Washington; or at the Office of the Federal Register, 800 North
Capitol Street, NW., suite 700, Washington, DC.
Note 3: The subject of this AD is addressed in Israeli
airworthiness directive 30-00-02-05, dated February 24, 2000.
(e) This amendment becomes effective on June 30, 2000.
Issued in Renton, Washington, on May 16, 2000.
Donald L. Riggin,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 00-12813 Filed 5-25-00; 8:45 am]
BILLING CODE 4910-13-U
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