AD 94-09-11 R1

final rule

Airworthiness Directives; Raytheon Model BAe.125 Series 1000A Airplanes and Model Hawker 1000 Airplanes

AD Number
94-09-11 R1
Status
final_rule
Effective Date
Product Category
aircraft
Docket
97-NM-313-AD
FR Citation
Federal Register: September 3, 2002 (Volume 67, Number 170)

Applicability

TypeManufacturerModelDetails
aircraft Raytheon Various Airworthiness Directives; Raytheon Model BAe.125 Series 1000A Airplanes and Model Hawker 1000 Airplanes

Unsafe Condition

Thrust Reverser System

Affected Aircraft

Raytheon Model BAe.125 Series 1000A and Model Hawker 1000 airplanes

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

Thrust Reverser System

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - 940911Res.pdf
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DetailsAttachments/Public Comments
AD Number:
94-09-11 R1
Document Type:
AD Final Rules
Docket Number:
97-NM-313-AD
Subject Heading:
Airworthiness Directives; Raytheon Model BAe.125 Series 1000A Airplanes and Model Hawker 1000 Airplanes
Subject:
Thrust Reverser System
Status:
Current
Citation:
Federal Register: September 3, 2002 (Volume 67, Number 170)
Citation Publish Date:
09/03/2002
Effective Date:
09/03/2002
Make:
Model:
BAe.125 Series 1000A | Hawker 1000
Product Type:
Aircraft
Product Subtype:
Large Airplane
Affected AD:
Superseded AD:
94-09-11
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
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[Federal Register: September 3, 2002 (Volume 67, Number 170)]


[Rules and Regulations]


[Page 56218-56219]


From the Federal Register Online via GPO Access [wais.access.gpo.gov]


[DOCID:fr03se02-2]


–––––––––––––––––––––––––––––––––––


DEPARTMENT OF TRANSPORTATION


Federal Aviation Administration


14 CFR Part 39


[Docket No. 97-NM-313-AD; Amendment 39-12875; AD 94-09-11 R1]


RIN 2120-AA64


Airworthiness Directives; Raytheon Model BAe.125 Series 1000A Airplanes and Model


Hawker 1000 Airplanes


AGENCY:
 
Federal Aviation Administration, DOT.


ACTION:
 
Final rule; rescission.


–––––––––––––––––––––––––––––––––––


SUMMARY:
 
This amendment rescinds an existing airworthiness directive (AD), applicable to


certain Raytheon Model BAe.125 Series 1000A Airplanes and Model Hawker 1000 airplanes. That


AD currently requires inspections of the thrust reverser system for integrity, and correction of any


discrepancy found. The requirements of that AD were intended to prevent a significant reduction in


the controllability of the airplane due to an in-flight deployment of a thrust reverser. Since the


issuance of that AD, the FAA has issued a separate AD that requires the accomplishment of


modifications that terminate the requirements of the existing AD.


DATES:
 
Effective September 3, 2002.


FOR FURTHER INFORMATION CONTACT:
 
Jeff Pretz, Aerospace Engineer, Systems and


Propulsion Branch, ACE-116W, FAA, Wichita Aircraft Certification Office, 1801 Airport Road,


Room 100, Mid-Continent Airport, Wichita, Kansas 67209; telephone (316) 946-4153; fax (316)


946-4407.


SUPPLEMENTARY INFORMATION:
 
A proposal to amend part 39 of the Federal Aviation


Regulations (14 CFR part 39) to rescind an airworthiness directive (AD) that is applicable to certain


Raytheon Model BAe.125 Series 1000A and Hawker 1000 series airplanes was published in the


Federal Register on September 10, 1999 (64 FR 49112). That action proposed the rescission of AD


94-09-11, amendment 39-8900 (59 FR 22125, April 29, 1994), in order to prevent operators from


performing an unnecessary action.
2


Comments


Interested persons have been afforded an opportunity to participate in the making of this


amendment. No comments were received in response to the proposal.


Conclusion


After careful review of the available data, the FAA has determined that air safety and the public


interest require the rescission of the rule as proposed, with the exception of the change to


applicability.


Explanation of Change to Applicability


The FAA has revised the applicability of this final rule to identify model designations as


published in the most recent type certificate data sheet for the affected models.


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, Safety.


The Rescission


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 removing amendment 39-8900.

Document Text

Show stored source text (verify against official source)
AD Final Rules - 940911Res.pdf
Copy URL
Document Versions
 Feedback
DetailsAttachments/Public Comments
AD Number:
94-09-11 R1
Document Type:
AD Final Rules
Docket Number:
97-NM-313-AD
Subject Heading:
Airworthiness Directives; Raytheon Model BAe.125 Series 1000A Airplanes and Model Hawker 1000 Airplanes
Subject:
Thrust Reverser System
Status:
Current
Citation:
Federal Register: September 3, 2002 (Volume 67, Number 170)
Citation Publish Date:
09/03/2002
Effective Date:
09/03/2002
Make:
Model:
BAe.125 Series 1000A | Hawker 1000
Product Type:
Aircraft
Product Subtype:
Large Airplane
Affected AD:
Superseded AD:
94-09-11
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
Automatic Zoom
Actual Size
Page Fit
Page Width
⁨50⁩%
⁨75⁩%
⁨100⁩%
⁨125⁩%
⁨150⁩%
⁨200⁩%
⁨300⁩%
⁨400⁩%
125%
of ⁨3⁩
1


[Federal Register: September 3, 2002 (Volume 67, Number 170)]


[Rules and Regulations]


[Page 56218-56219]


From the Federal Register Online via GPO Access [wais.access.gpo.gov]


[DOCID:fr03se02-2]


–––––––––––––––––––––––––––––––––––


DEPARTMENT OF TRANSPORTATION


Federal Aviation Administration


14 CFR Part 39


[Docket No. 97-NM-313-AD; Amendment 39-12875; AD 94-09-11 R1]


RIN 2120-AA64


Airworthiness Directives; Raytheon Model BAe.125 Series 1000A Airplanes and Model


Hawker 1000 Airplanes


AGENCY:
 
Federal Aviation Administration, DOT.


ACTION:
 
Final rule; rescission.


–––––––––––––––––––––––––––––––––––


SUMMARY:
 
This amendment rescinds an existing airworthiness directive (AD), applicable to


certain Raytheon Model BAe.125 Series 1000A Airplanes and Model Hawker 1000 airplanes. That


AD currently requires inspections of the thrust reverser system for integrity, and correction of any


discrepancy found. The requirements of that AD were intended to prevent a significant reduction in


the controllability of the airplane due to an in-flight deployment of a thrust reverser. Since the


issuance of that AD, the FAA has issued a separate AD that requires the accomplishment of


modifications that terminate the requirements of the existing AD.


DATES:
 
Effective September 3, 2002.


FOR FURTHER INFORMATION CONTACT:
 
Jeff Pretz, Aerospace Engineer, Systems and


Propulsion Branch, ACE-116W, FAA, Wichita Aircraft Certification Office, 1801 Airport Road,


Room 100, Mid-Continent Airport, Wichita, Kansas 67209; telephone (316) 946-4153; fax (316)


946-4407.


SUPPLEMENTARY INFORMATION:
 
A proposal to amend part 39 of the Federal Aviation


Regulations (14 CFR part 39) to rescind an airworthiness directive (AD) that is applicable to certain


Raytheon Model BAe.125 Series 1000A and Hawker 1000 series airplanes was published in the


Federal Register on September 10, 1999 (64 FR 49112). That action proposed the rescission of AD


94-09-11, amendment 39-8900 (59 FR 22125, April 29, 1994), in order to prevent operators from


performing an unnecessary action.
2


Comments


Interested persons have been afforded an opportunity to participate in the making of this


amendment. No comments were received in response to the proposal.


Conclusion


After careful review of the available data, the FAA has determined that air safety and the public


interest require the rescission of the rule as proposed, with the exception of the change to


applicability.


Explanation of Change to Applicability


The FAA has revised the applicability of this final rule to identify model designations as


published in the most recent type certificate data sheet for the affected models.


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, Safety.


The Rescission


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 removing amendment 39-8900.

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.