AD 86-18-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Saab AB, Saab Aerosystems | 340A (SAAB SF340A) | Airworthiness Directives; SAAB-FAIRCHILD Model SF-340A Airplanes |
Unsafe Condition
Engine control cable freezing
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the engine control cable system in accordance with SAAB-Fairchild Service Bulletin SF340-76-007, Revision 3, dated August 14, 1985. An alternate means of compliance or adjustment of the compliance time may be used when approved by the FAA.
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Compliance Time
within 60 days after the effective date of this AD, unless previously accomplished
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Affected Aircraft
SAAB-FAIRCHILD Model SF-340A airplanes listed in SAAB-Fairchild Service Bulletin SF-340-76-007, Revision 3, dated August 14, 1985
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Federal Register Abstract
Engine Control Cable System
Applicability Source Text
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AD Final Rules - DRS_86-18-07.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 86-18-07 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; SAAB-FAIRCHILD Model SF-340A Airplanes Subject: Engine Control Cable System Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 09/11/1986 Make: Saab AB, Saab Aerosystems Model: 340A (SAAB SF340A) Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 86-18-07 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5387 AD NUMBER: 86-18-07 SUBJECT HEADING: Airworthiness Directives; SAAB-FAIRCHILD Model SF-340A Airplanes ACTION: SUMMARY: DATES: Effective September 11, 1986. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 86-18-07 SAAB-FAIRCHILD: Amendment 39-5387. Applies to Model SF-340A airplanes listed in SAAB-Fairchild Service Bulletin SF-340-76-007, Revision 3, dated August 14, 1985, certificated in any category. Compliance is required within 60 days after the effective date of this AD, unless previously accomplished. To prevent engine control cable freezing, accomplish the following: A. Modify the engine control cable system in accordance with SAAB-Fairchild Service Bulletin SF340-76-007, Revision 3, dated August 14, 1985. B. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Standardization Branch, ANM-113, FAA, Northwest Mountain Region. C. Special flight permits may be issued 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 document from the manufacturer, may obtain copies upon request to SAAB-Fairchild, Product Support, S-58188, Linkoping, Sweden. This document 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 September 11, 1986. FOOTER:
Document Text
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AD Final Rules - DRS_86-18-07.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 86-18-07 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; SAAB-FAIRCHILD Model SF-340A Airplanes Subject: Engine Control Cable System Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 09/11/1986 Make: Saab AB, Saab Aerosystems Model: 340A (SAAB SF340A) 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: 86-18-07 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5387 AD NUMBER: 86-18-07 SUBJECT HEADING: Airworthiness Directives; SAAB-FAIRCHILD Model SF-340A Airplanes ACTION: SUMMARY: DATES: Effective September 11, 1986. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 86-18-07 SAAB-FAIRCHILD: Amendment 39-5387. Applies to Model SF-340A airplanes listed in SAAB-Fairchild Service Bulletin SF-340-76-007, Revision 3, dated August 14, 1985, certificated in any category. Compliance is required within 60 days after the effective date of this AD, unless previously accomplished. To prevent engine control cable freezing, accomplish the following: A. Modify the engine control cable system in accordance with SAAB-Fairchild Service Bulletin SF340-76-007, Revision 3, dated August 14, 1985. B. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Standardization Branch, ANM-113, FAA, Northwest Mountain Region. C. Special flight permits may be issued 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 document from the manufacturer, may obtain copies upon request to SAAB-Fairchild, Product Support, S-58188, Linkoping, Sweden. This document 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 September 11, 1986. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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