AD 99-01-07
final rule
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | British Aerospace Regional Aircraft | Jetstream Series 3101 | Airworthiness Directives: British Aerospace Jetstream Model 3101 Airplanes |
Unsafe Condition
A strength deficiency in the lower fuselage skin panels between the main and rear spar frames (Frame Stations 223 and 257.8) could result in reduced or loss of control of the airplane during maximum speed limit operations.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install additional stringers at the lower fuselage skin panels between the main and rear spar frames as per Jetstream Modification JM 7297 and British Aerospace Jetstream Service Bulletin 53-JM7297. Special flight permits may be obtained under 14 CFR 21.197 and 21.199 to operate to a location where the modification can be accomplished.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within the next 50 hours time-in-service (TIS) after the effective date of this AD, unless already accomplished
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Affected Aircraft
Jetstream Model 3101 airplanes, constructors numbers 601 through 607 and 609 through 619, certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Lower Fuselage Skin Panels
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_99-01-07.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 99-01-07 Document Type: AD Final Rules Docket Number: 98-CE-100-AD Subject Heading: Airworthiness Directives: British Aerospace Jetstream Model 3101 Airplanes Subject: Lower Fuselage Skin Panels Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 03/19/1999 Make: British Aerospace Regional Aircraft Model: Jetstream Series 3101 Product Type: Aircraft Product Subtype: Small/Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 [64 FR 9911 No. 39 03/01/1999] Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 99-01-07 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 98-CE-100-AD AMENDMENT: 39-10974 AD NUMBER: 99-01-07 SUBJECT HEADING: Airworthiness Directives: British Aerospace Jetstream Model 3101 Airplanes ACTION: Final rule SUMMARY: This action confirms the effective date of Airworthiness Directive (AD) 99-01-07, which applies to certain British Aerospace Jetstream Model 3101 airplanes. AD 99-01-07 requires installing additional stringers at the lower fuselage skin panels between the main and rear spar frames. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for the United Kingdom. The actions specified in this AD are intended to correct a strength deficiency in the area of the lower fuselage skin panels between the main rear spar frames, which, if not corrected, could result in reduced or loss of control of the airplane during maximum speed limit operations. DATES: Effective March 19, 1999. ADDRESSES: FOR FURTHER INFORMATION CONTACT: Mr. S.M. Nagarajan, Aerospace Engineer, FAA, Small Airplane Directorate, 1201 Walnut, suite 900, Kansas City, Missouri 64106; telephone: (816) 426-6932; facsimile: (816) 426-2169. SUPPLEMENTARY INFORMATION: The FAA published this direct final rule with request for comments in the Federal Register on December 31, 1998 (63 FR 72139). The FAA uses the direct final rulemaking procedure for a non-controversial rule where the FAA anticipates that there will be no adverse public comment. This direct final rule advised the public that no adverse comments were anticipated, and that unless a written adverse comment, or a written notice of intent to submit such an adverse comment, was received within the comment period, the regulation would become effective on March 19, 1999. No adverse comments were received, and thus this notice confirms that this final rule will become effective on that date. REGULATORY TEXT: 99-01-07 BRITISH AEROSPACE: Amendment 39-10974; Docket No. 98-CE-100-AD. Applicability: Jetstream Model 3101 airplanes, constructors numbers 601 through 607 and 609 through 619, 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 (c) 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 within the next 50 hours time-in-service (TIS) after the effective date of this AD, unless already accomplished. To correct a strength deficiency in the area of the lower fuselage skin panels between the main rear spar frames, which, if not corrected, could result in reduced or loss of control of the airplane during maximum speed limit operations, accomplish the following: (a) Incorporate Jetstream Modification JM 7297 by installing additional stringers at the lower fuselage skin panels between the main and rear spar frames (Frame Stations 223 and 257.8). Accomplish this modification in accordance with Part B of the Accomplishment Instructions in British Aerospace Jetstream Service Bulletin 53-JM7297, Original Issue: May 10, 1984. (b) 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. (c) An alternative method of compliance or adjustment of the compliance time that provides an equivalent level of safety may be used if approved by the Manager, Small Airplane Directorate, Aircraft Certification Service, 1201 Walnut, suite 900, Kansas City, Missouri 64106. The request shall be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and then send it to the Manager, Small Airplane Directorate. NOTE 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Small Airplane Directorate. (d) The modification required by this AD shall be done in accordance with British Aerospace Jetstream Service Bulletin 53-JM7297, Original Issue: May 10, 1984. 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 British Aerospace Regional Aircraft, Prestwick International Airport, Ayrshire, KA9 2RW, Scotland. Copies may be inspected at the FAA, Central Region, Office of the Regional Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri, 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 British Aerospace Jetstream Service Bulletin 53-JM7297, Original Issue: May 10, 1984. This service bulletin is classified as mandatory by the United Kingdom Civil Aviation Authority (CAA). (e) This amendment becomes effective on March 19, 1999. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_99-01-07.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 99-01-07 Document Type: AD Final Rules Docket Number: 98-CE-100-AD Subject Heading: Airworthiness Directives: British Aerospace Jetstream Model 3101 Airplanes Subject: Lower Fuselage Skin Panels Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 03/19/1999 Make: British Aerospace Regional Aircraft Model: Jetstream Series 3101 Product Type: Aircraft Product Subtype: Small/Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 [64 FR 9911 No. 39 03/01/1999] Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 99-01-07 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 98-CE-100-AD AMENDMENT: 39-10974 AD NUMBER: 99-01-07 SUBJECT HEADING: Airworthiness Directives: British Aerospace Jetstream Model 3101 Airplanes ACTION: Final rule SUMMARY: This action confirms the effective date of Airworthiness Directive (AD) 99-01-07, which applies to certain British Aerospace Jetstream Model 3101 airplanes. AD 99-01-07 requires installing additional stringers at the lower fuselage skin panels between the main and rear spar frames. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for the United Kingdom. The actions specified in this AD are intended to correct a strength deficiency in the area of the lower fuselage skin panels between the main rear spar frames, which, if not corrected, could result in reduced or loss of control of the airplane during maximum speed limit operations. DATES: Effective March 19, 1999. ADDRESSES: FOR FURTHER INFORMATION CONTACT: Mr. S.M. Nagarajan, Aerospace Engineer, FAA, Small Airplane Directorate, 1201 Walnut, suite 900, Kansas City, Missouri 64106; telephone: (816) 426-6932; facsimile: (816) 426-2169. SUPPLEMENTARY INFORMATION: The FAA published this direct final rule with request for comments in the Federal Register on December 31, 1998 (63 FR 72139). The FAA uses the direct final rulemaking procedure for a non-controversial rule where the FAA anticipates that there will be no adverse public comment. This direct final rule advised the public that no adverse comments were anticipated, and that unless a written adverse comment, or a written notice of intent to submit such an adverse comment, was received within the comment period, the regulation would become effective on March 19, 1999. No adverse comments were received, and thus this notice confirms that this final rule will become effective on that date. REGULATORY TEXT: 99-01-07 BRITISH AEROSPACE: Amendment 39-10974; Docket No. 98-CE-100-AD. Applicability: Jetstream Model 3101 airplanes, constructors numbers 601 through 607 and 609 through 619, 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 (c) 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 within the next 50 hours time-in-service (TIS) after the effective date of this AD, unless already accomplished. To correct a strength deficiency in the area of the lower fuselage skin panels between the main rear spar frames, which, if not corrected, could result in reduced or loss of control of the airplane during maximum speed limit operations, accomplish the following: (a) Incorporate Jetstream Modification JM 7297 by installing additional stringers at the lower fuselage skin panels between the main and rear spar frames (Frame Stations 223 and 257.8). Accomplish this modification in accordance with Part B of the Accomplishment Instructions in British Aerospace Jetstream Service Bulletin 53-JM7297, Original Issue: May 10, 1984. (b) 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. (c) An alternative method of compliance or adjustment of the compliance time that provides an equivalent level of safety may be used if approved by the Manager, Small Airplane Directorate, Aircraft Certification Service, 1201 Walnut, suite 900, Kansas City, Missouri 64106. The request shall be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and then send it to the Manager, Small Airplane Directorate. NOTE 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Small Airplane Directorate. (d) The modification required by this AD shall be done in accordance with British Aerospace Jetstream Service Bulletin 53-JM7297, Original Issue: May 10, 1984. 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 British Aerospace Regional Aircraft, Prestwick International Airport, Ayrshire, KA9 2RW, Scotland. Copies may be inspected at the FAA, Central Region, Office of the Regional Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri, 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 British Aerospace Jetstream Service Bulletin 53-JM7297, Original Issue: May 10, 1984. This service bulletin is classified as mandatory by the United Kingdom Civil Aviation Authority (CAA). (e) This amendment becomes effective on March 19, 1999. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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