AD 86-03-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Fokker Services | F.28 Mark 0070 | Airworthiness Directives; FOKKER B.V. Model F28 Airplanes |
| aircraft | Fokker Services | F.28 Mark 0100 | Airworthiness Directives; FOKKER B.V. Model F28 Airplanes |
| aircraft | Fokker Services | F.28 Mark 1000 | Airworthiness Directives; FOKKER B.V. Model F28 Airplanes |
| aircraft | Fokker Services | F.28 Mark 2000 | Airworthiness Directives; FOKKER B.V. Model F28 Airplanes |
| aircraft | Fokker Services | F.28 Mark 3000 | Airworthiness Directives; FOKKER B.V. Model F28 Airplanes |
| aircraft | Fokker Services | F.28 Mark 4000 | Airworthiness Directives; FOKKER B.V. Model F28 Airplanes |
Unsafe Condition
Failure of pilot and copilot restraint harnesses due to inertia reel spring and mounting collar degradation, and illegible instruction placards on the service/emergency door under emergency lighting conditions.
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Required Actions
Replace inertia reel springs and mounting collars per Fokker Service Bulletin F28/25-93 and Teleflex Morse Limited Service Bulletin 25-00-185429. Modify the emergency lighting system per Fokker Service Bulletin F28/33-32. Alternate means of compliance may be used if approved by the FAA.
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Compliance Time
within the next 120 days after the effective date of this airworthiness directive
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Affected Aircraft
Fokker B.V. Model F28 Mark 0070, 0100, 1000, 2000, 3000, 4000 airplanes as indicated in the applicability statement of each service bulletin listed in this AD.
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Federal Register Abstract
Pilots Restraint Harnesses & Emergency Lighting System
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_86-03-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 86-03-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; FOKKER B.V. Model F28 Airplanes Subject: Pilots Restraint Harnesses & Emergency Lighting System Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 02/28/1986 Make: Fokker Services Model: F.28 Mark 0070 | F.28 Mark 0100 | F.28 Mark 1000 | F.28 Mark 2000 | F.28 Mark 3000 | F.28 Mark 4000 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: 86-03-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5221 AD NUMBER: 86-03-02 SUBJECT HEADING: Airworthiness Directives; FOKKER B.V. Model F28 Airplanes ACTION: SUMMARY: DATES: Effective February 28, 1986. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 86-03-02 FOKKER B.V.: Amendment 39-5221. Applies to Model F28 airplanes as indicated in the applicability statement of each service bulletin listed below. Compliance is required within the next 120 days after the effective date of this airworthiness directive, unless already accomplished: A. To prevent loss of the pilot and copilot restraint function of the safety harnesses, replace the inertia reel springs and mounting collars in accordance with Fokker Service Bulletin F28/25-93, dated June 4, 1984, and Teleflex Morse Limited Service Bulletin 25-00-185429, Issue 2, dated September 1983. B. To ensure that instruction placards on the service/emergency door in emergency lighting conditions are legible, modify the emergency lighting system in accordance with Fokker Service Bulletin F28/33-32, dated September 17, 1984. C. Alternate means of compliance which provide an acceptable level of safety may be used when approved by the Manager, Standardization Branch, ANM-113, FAA, Northwest Mountain Region. D. Special flight permits may be used in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD. All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to the Manager, Maintenance and Engineering, Fokker B.V., Product Support, P.O. Box 7600, 11172J Schiphol Oost, The Netherlands. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. This amendment becomes effective February 28, 1986. FOOTER:
Document Text
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AD Final Rules - DRS_86-03-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 86-03-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; FOKKER B.V. Model F28 Airplanes Subject: Pilots Restraint Harnesses & Emergency Lighting System Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 02/28/1986 Make: Fokker Services Model: F.28 Mark 0070 | F.28 Mark 0100 | F.28 Mark 1000 | F.28 Mark 2000 | F.28 Mark 3000 | F.28 Mark 4000 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: 86-03-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5221 AD NUMBER: 86-03-02 SUBJECT HEADING: Airworthiness Directives; FOKKER B.V. Model F28 Airplanes ACTION: SUMMARY: DATES: Effective February 28, 1986. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 86-03-02 FOKKER B.V.: Amendment 39-5221. Applies to Model F28 airplanes as indicated in the applicability statement of each service bulletin listed below. Compliance is required within the next 120 days after the effective date of this airworthiness directive, unless already accomplished: A. To prevent loss of the pilot and copilot restraint function of the safety harnesses, replace the inertia reel springs and mounting collars in accordance with Fokker Service Bulletin F28/25-93, dated June 4, 1984, and Teleflex Morse Limited Service Bulletin 25-00-185429, Issue 2, dated September 1983. B. To ensure that instruction placards on the service/emergency door in emergency lighting conditions are legible, modify the emergency lighting system in accordance with Fokker Service Bulletin F28/33-32, dated September 17, 1984. C. Alternate means of compliance which provide an acceptable level of safety may be used when approved by the Manager, Standardization Branch, ANM-113, FAA, Northwest Mountain Region. D. Special flight permits may be used in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD. All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to the Manager, Maintenance and Engineering, Fokker B.V., Product Support, P.O. Box 7600, 11172J Schiphol Oost, The Netherlands. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. This amendment becomes effective February 28, 1986. FOOTER:
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Retrieved: Apr 8, 2026
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