AD 92-15-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Fokker | F28 0100 | Airworthiness Directives; FOKKER Model F28 Mark 0100 Series Airplanes |
Unsafe Condition
Fatigue damage and subsequent reduced structural capability of the horizontal stabilizer attachment.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Remove the normal maximum (second) detent for the reverse thrust control and install a modified detent in accordance with Fokker Service Bulletin SBF100-76-008. An alternative method of compliance or adjustment of the compliance time may be used if approved by the FAA.
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Compliance Time
Within 7 months after the effective date of this AD
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Affected Aircraft
FOKKER Model F28 Mark 0100 series airplanes; serial numbers 11244 through 11308, inclusive; 11310, and 11312 through 11314, inclusive; certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Horizontal Stabilizer Attachment
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_92-15-08.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 92-15-08 Document Type: AD Final Rules Docket Number: 92-NM-47-AD Subject Heading: Airworthiness Directives; FOKKER Model F28 Mark 0100 Series Airplanes Subject: Horizontal Stabilizer Attachment Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 09/08/1992 Make: Model: F.28 Mark 0100 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 92-15-08 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 92-NM-47-AD AMENDMENT: 39-8302 AD NUMBER: 92-15-08 SUBJECT HEADING: Airworthiness Directives; FOKKER Model F28 Mark 0100 Series Airplanes ACTION: SUMMARY: DATES: Effective on September 8, 1992. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 92-15-08 FOKKER: Amendment 39-8302. Docket No. 92-NM-47-AD. Applicability: Model F28 Mark 0100 series airplanes; serial numbers 11244 through 11308, inclusive; 11310, and 11312 through 11314, inclusive; certificated in any category. Compliance: Required as indicated, unless accomplished previously. To prevent fatigue damage and subsequent reduced structural capability of the horizontal stabilizer attachment, accomplish the following: (a) Within 7 months after the effective date of this AD, remove the normal maximum (second) detent for the reverse thrust control and install a modified detent, in accordance with Fokker Service Bulletin SBF100-76-008, dated May 8, 1991. (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, Standardization Branch, FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Standardization Branch. NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Standardization Branch. (c) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished. (d) The removal and installment shall be done in accordance with Fokker Service Bulletin SBF100-76-008, dated May 8, 1991. 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 Fokker Aircraft USA, Inc., 1199 North Fairfax Street, Alexandria, Virginia 22314. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington; or at the Office of the Federal Register, 1100 L Street NW., Room 8401, Washington, DC. (e) This amendment becomes effective on September 8, 1992. FOOTER:
Document Text
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AD Final Rules - DRS_92-15-08.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 92-15-08 Document Type: AD Final Rules Docket Number: 92-NM-47-AD Subject Heading: Airworthiness Directives; FOKKER Model F28 Mark 0100 Series Airplanes Subject: Horizontal Stabilizer Attachment Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 09/08/1992 Make: Model: F.28 Mark 0100 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 92-15-08 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 92-NM-47-AD AMENDMENT: 39-8302 AD NUMBER: 92-15-08 SUBJECT HEADING: Airworthiness Directives; FOKKER Model F28 Mark 0100 Series Airplanes ACTION: SUMMARY: DATES: Effective on September 8, 1992. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 92-15-08 FOKKER: Amendment 39-8302. Docket No. 92-NM-47-AD. Applicability: Model F28 Mark 0100 series airplanes; serial numbers 11244 through 11308, inclusive; 11310, and 11312 through 11314, inclusive; certificated in any category. Compliance: Required as indicated, unless accomplished previously. To prevent fatigue damage and subsequent reduced structural capability of the horizontal stabilizer attachment, accomplish the following: (a) Within 7 months after the effective date of this AD, remove the normal maximum (second) detent for the reverse thrust control and install a modified detent, in accordance with Fokker Service Bulletin SBF100-76-008, dated May 8, 1991. (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, Standardization Branch, FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Standardization Branch. NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Standardization Branch. (c) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished. (d) The removal and installment shall be done in accordance with Fokker Service Bulletin SBF100-76-008, dated May 8, 1991. 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 Fokker Aircraft USA, Inc., 1199 North Fairfax Street, Alexandria, Virginia 22314. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington; or at the Office of the Federal Register, 1100 L Street NW., Room 8401, Washington, DC. (e) This amendment becomes effective on September 8, 1992. FOOTER:
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Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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