AD 93-18-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Fokker | F28 0100 | Airworthiness Directives; FOKKER Model F28 Mark 0100 Series Airplanes |
Unsafe Condition
Inability to evacuate smoke from the cabin due to the HP bleed air shut-off valve circuit breakers not being modified.
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Required Actions
Modify the high pressure (HP) bleed air shut-off valve circuit breakers in accordance with Fokker Service Bulletin SBF100-24-024, Revision 1. Wires may be coiled and capped at both ends as per the Fokker F28 Maintenance Manual.
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Compliance Time
Within 6 months after the effective date of this AD
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Affected Aircraft
FOKKER Model F28 Mark 0100 series airplanes, serial numbers 11244 to 11371 inclusive
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Federal Register Abstract
Evacuation Of Cabin Smoke
Applicability Source Text
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AD Final Rules - DRS_93-18-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 93-18-06 Document Type: AD Final Rules Docket Number: 92-NM-113-AD Subject Heading: Airworthiness Directives; FOKKER Model F28 Mark 0100 Series Airplanes Subject: Evacuation Of Cabin Smoke Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 11/18/1993 Make: Model: F.28 Mark 0100 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 93-18-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 92-NM-113-AD AMENDMENT: 39-8691 AD NUMBER: 93-18-06 SUBJECT HEADING: Airworthiness Directives; FOKKER Model F28 Mark 0100 Series Airplanes ACTION: SUMMARY: DATES: Effective November 18, 1993. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 93-18-06 FOKKER: Amendment 39-8691. Docket 92-NM-113-AD. Applicability: Model F28 Mark 0100 series airplanes, serial numbers 11244 to 11371 inclusive, certificated in any category. Compliance: Required as indicated, unless accomplished previously. To prevent the inability to evacuate smoke from the cabin, accomplish the following: (a) Within 6 months after the effective date of this AD, modify the high pressure (HP) bleed air shut-off valve circuit breakers, in accordance with Fokker Service Bulletin SBF100-24-024, Revision 1, dated December 29, 1992. Wires may be coiled and capped at both ends in accordance with procedures described in the Fokker F28 Maintenance Manual in lieu of being removed and discarded, as specified in the service bulletin. (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, ANM-113, 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, ANM-113. NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Standardization Branch, ANM-113. (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 modification shall be done in accordance with Fokker Service Bulletin SBF100-24- 024, Revision 1, dated December 29, 1992. 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, 800 North Capitol Street, NW., suite 700, Washington, DC. (e) This amendment becomes effective on November 18, 1993. FOOTER:
Document Text
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AD Final Rules - DRS_93-18-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 93-18-06 Document Type: AD Final Rules Docket Number: 92-NM-113-AD Subject Heading: Airworthiness Directives; FOKKER Model F28 Mark 0100 Series Airplanes Subject: Evacuation Of Cabin Smoke Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 11/18/1993 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: 93-18-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 92-NM-113-AD AMENDMENT: 39-8691 AD NUMBER: 93-18-06 SUBJECT HEADING: Airworthiness Directives; FOKKER Model F28 Mark 0100 Series Airplanes ACTION: SUMMARY: DATES: Effective November 18, 1993. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 93-18-06 FOKKER: Amendment 39-8691. Docket 92-NM-113-AD. Applicability: Model F28 Mark 0100 series airplanes, serial numbers 11244 to 11371 inclusive, certificated in any category. Compliance: Required as indicated, unless accomplished previously. To prevent the inability to evacuate smoke from the cabin, accomplish the following: (a) Within 6 months after the effective date of this AD, modify the high pressure (HP) bleed air shut-off valve circuit breakers, in accordance with Fokker Service Bulletin SBF100-24-024, Revision 1, dated December 29, 1992. Wires may be coiled and capped at both ends in accordance with procedures described in the Fokker F28 Maintenance Manual in lieu of being removed and discarded, as specified in the service bulletin. (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, ANM-113, 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, ANM-113. NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Standardization Branch, ANM-113. (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 modification shall be done in accordance with Fokker Service Bulletin SBF100-24- 024, Revision 1, dated December 29, 1992. 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, 800 North Capitol Street, NW., suite 700, Washington, DC. (e) This amendment becomes effective on November 18, 1993. FOOTER:
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Retrieved: Apr 8, 2026
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