AD 92-14-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | ATR - GIE Avions de Transport R gional | ATR42-300 | Airworthiness Directives; AEROSPATIALE Model ATR42-300 Series Airplanes |
| aircraft | ATR - GIE Avions de Transport R gional | ATR42-320 | Airworthiness Directives; AEROSPATIALE Model ATR42-300 Series Airplanes |
Unsafe Condition
Malfunction of the engine and propeller controls due to lack of sealing sheath and protective sleeve on the engine and propeller push-pull control cables.
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Required Actions
Modify the engine and propeller push-pull control cables on left and right engines by adding a sealing sheath and protective sleeve per Aerospatiale Service Bulletin ATR42-76-0002, Revision 1. Submit requests for alternative methods of compliance through an FAA Principal Maintenance Inspector.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 60 days after February 3, 1989
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
AEROSPATIALE Model ATR42-300 series airplanes listed in Service Bulletin ATR42-76-0002, Revision 1, dated May 16, 1988.
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Federal Register Abstract
Thermostatic Element
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_92-14-08.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 92-14-08 Document Type: AD Final Rules Docket Number: 92-NM-118-AD Subject Heading: Airworthiness Directives; AEROSPATIALE Model ATR42-300 Series Airplanes Subject: Thermostatic Element Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 07/01/1992 Make: ATR - GIE Avions de Transport R gional Model: ATR42-300 | ATR42-320 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 92-14-08 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 92-NM-118-AD AMENDMENT: 39-8290 AD NUMBER: 92-14-08 SUBJECT HEADING: Airworthiness Directives; AEROSPATIALE Model ATR42-300 Series Airplanes ACTION: SUMMARY: DATES: Effective July 1, 1992. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 92-14-08 AEROSPATIALE: Amendment 39-8290. Docket No. 92-NM-118-AD. Supersedes AD 88-26-04, Amendment 39-6094. Applicability: Model ATR42-300 series airplanes; as listed in Aerospatiale Service Bulletins ATR42-76 0002, Revision 1, dated May 16, 1988; certificated in any category. Compliance: Required as indicated, unless accomplished previously. To prevent a malfunction of the engine and propeller controls, accomplish the following: (a) Within 60 days after February 3, 1989 (the effective date of AD 88-26-04, Amendment 39-6094), modify the engine and propeller push-pull control cables on the left and right engines by adding a sealing sheath and protective sleeve, in accordance with Aerospatiale Service Bulletin ATR42-76-0002, Revision 1, dated May 16, 1988. (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. 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 modification shall be done in accordance with Aerospatiale Service Bulletin ATR42-76-0002, Revision 1, dated May 16, 1988, which incorporates the following list of effective pages: Page Number Revision Level Date 1-3 1 May 16, 1988 4 Original January 18, 1988 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 Aerospatiale, 316 Route de Bayonne, 31060 Toulouse, Cedex 03, France. 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 July 1, 1992. FOOTER:
Document Text
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AD Final Rules - DRS_92-14-08.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 92-14-08 Document Type: AD Final Rules Docket Number: 92-NM-118-AD Subject Heading: Airworthiness Directives; AEROSPATIALE Model ATR42-300 Series Airplanes Subject: Thermostatic Element Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 07/01/1992 Make: ATR - GIE Avions de Transport R gional Model: ATR42-300 | ATR42-320 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: 92-14-08 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 92-NM-118-AD AMENDMENT: 39-8290 AD NUMBER: 92-14-08 SUBJECT HEADING: Airworthiness Directives; AEROSPATIALE Model ATR42-300 Series Airplanes ACTION: SUMMARY: DATES: Effective July 1, 1992. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 92-14-08 AEROSPATIALE: Amendment 39-8290. Docket No. 92-NM-118-AD. Supersedes AD 88-26-04, Amendment 39-6094. Applicability: Model ATR42-300 series airplanes; as listed in Aerospatiale Service Bulletins ATR42-76 0002, Revision 1, dated May 16, 1988; certificated in any category. Compliance: Required as indicated, unless accomplished previously. To prevent a malfunction of the engine and propeller controls, accomplish the following: (a) Within 60 days after February 3, 1989 (the effective date of AD 88-26-04, Amendment 39-6094), modify the engine and propeller push-pull control cables on the left and right engines by adding a sealing sheath and protective sleeve, in accordance with Aerospatiale Service Bulletin ATR42-76-0002, Revision 1, dated May 16, 1988. (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. 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 modification shall be done in accordance with Aerospatiale Service Bulletin ATR42-76-0002, Revision 1, dated May 16, 1988, which incorporates the following list of effective pages: Page Number Revision Level Date 1-3 1 May 16, 1988 4 Original January 18, 1988 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 Aerospatiale, 316 Route de Bayonne, 31060 Toulouse, Cedex 03, France. 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 July 1, 1992. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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