AD 89-14-07
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
Failure of the emergency exit frame
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Accomplish modification of the fuselage emergency exit frame in accordance with Aerospatiale Service Bulletin ATR42-53-0024, Revision 2. An alternate means of compliance or adjustment of the compliance time may be used if approved by the FAA.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to the accumulation of 12,000 landings or within 60 days after the effective date of this AD, whichever occurs later
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Affected Aircraft
AEROSPATIALE Model ATR42-300 series airplanes, Serial Numbers 003 through 052
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Fuselage Emergency Exit Frame
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_89-14-07.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 89-14-07 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; AEROSPATIALE Model ATR42-300 Series Airplanes Subject: Fuselage Emergency Exit Frame Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/07/1989 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de Transport R gional Model: ATR42-300 | ATR42-320 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 89-14-07 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-6257 AD NUMBER: 89-14-07 SUBJECT HEADING: Airworthiness Directives; AEROSPATIALE Model ATR42-300 Series Airplanes ACTION: SUMMARY: DATES: Effective on August 7, 1989. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 89-14-07 AEROSPATIALE: Amendment 39-6257. Applicability: Model ATR42-300 series airplanes, Serial Numbers 003 through 052, certificated in any category. Compliance: Required as indicated, unless previously accomplished. To prevent failure of the emergency exit frame, accomplish the following: A. Prior to the accumulation of 12,000 landings or within 60 days after the effective date of this AD, whichever occurs later, accomplish modification of the fuselage emergency exit frame in accordance with Aerospatiale Service Bulletin ATR42-53-0024, Revision 2, dated May 16, 1988. 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. NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who will either concur or comment and then send it to the Manager, Standardization Branch, ANM-113. C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of 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 Aerospatiale, 316 Route de Bayonne, 31060 Toulouse, Cedex 03, France. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or at the Standardization Branch, 9010 East Marginal Way South, Seattle, Washington. This amendment (39-6257, AD 89-14-07) becomes effective on August 7, 1989. FOOTER:
Document Text
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AD Final Rules - DRS_89-14-07.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 89-14-07 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; AEROSPATIALE Model ATR42-300 Series Airplanes Subject: Fuselage Emergency Exit Frame Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/07/1989 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: 89-14-07 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-6257 AD NUMBER: 89-14-07 SUBJECT HEADING: Airworthiness Directives; AEROSPATIALE Model ATR42-300 Series Airplanes ACTION: SUMMARY: DATES: Effective on August 7, 1989. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 89-14-07 AEROSPATIALE: Amendment 39-6257. Applicability: Model ATR42-300 series airplanes, Serial Numbers 003 through 052, certificated in any category. Compliance: Required as indicated, unless previously accomplished. To prevent failure of the emergency exit frame, accomplish the following: A. Prior to the accumulation of 12,000 landings or within 60 days after the effective date of this AD, whichever occurs later, accomplish modification of the fuselage emergency exit frame in accordance with Aerospatiale Service Bulletin ATR42-53-0024, Revision 2, dated May 16, 1988. 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. NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who will either concur or comment and then send it to the Manager, Standardization Branch, ANM-113. C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of 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 Aerospatiale, 316 Route de Bayonne, 31060 Toulouse, Cedex 03, France. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or at the Standardization Branch, 9010 East Marginal Way South, Seattle, Washington. This amendment (39-6257, AD 89-14-07) becomes effective on August 7, 1989. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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