AD 91-09-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 757-200 Series | Airworthiness Directives; BOEING Model 757 Series Airplanes |
| aircraft | The Boeing Company | 757-200CB Series | Airworthiness Directives; BOEING Model 757 Series Airplanes |
| aircraft | The Boeing Company | 757-200PF Series | Airworthiness Directives; BOEING Model 757 Series Airplanes |
| aircraft | The Boeing Company | 757-300 Series | Airworthiness Directives; BOEING Model 757 Series Airplanes |
Unsafe Condition
Chafing of the thrust control cable assemblies, wire bundle clamps, and wire bundles.
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Required Actions
Inspect thrust control cable assemblies for damage and replace any damaged ones prior to further flight; inspect wire bundles for chafing and repair any chafed ones prior to further flight; modify the wire bundles in accordance with Boeing Service Bulletin 757-76-0008.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within the next 3,000 hours time-in-service after the effective date of this AD, unless previously accomplished
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Affected Aircraft
BOEING Model 757 series airplanes equipped with Rolls Royce RB211-535 engines, as listed in Boeing Service Bulletin 757-76-0008 dated March 22, 1990.
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Federal Register Abstract
Wire Bundles
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_91-09-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 91-09-02 Document Type: AD Final Rules Docket Number: 90-NM-269-AD Subject Heading: Airworthiness Directives; BOEING Model 757 Series Airplanes Subject: Wire Bundles Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 05/28/1991 Make: The Boeing Company Model: 757-200 Series | 757-200CB Series | 757-200PF Series | 757-300 Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 91-09-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 90-NM-269-AD AMENDMENT: 39-6983 AD NUMBER: 91-09-02 SUBJECT HEADING: Airworthiness Directives; BOEING Model 757 Series Airplanes ACTION: SUMMARY: DATES: Effective May 28, 1991. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 91-09-02 BOEING: Amendment 39-6983. Docket No. 90-NM-269-AD. Applicability: Model 757 series airplanes, equipped with Rolls Royce RB211-535 engines; as listed in Boeing Service Bulletin 757-76-0008, dated March 22, 1990; certificated in any category. Compliance: Required within the next 3,000 hours time-in-service after the effective date of this AD, unless previously accomplished. To prevent chafing of the thrust control cable assemblies, wire bundle clamps, and wire bundles, accomplish the following: A. Accomplish the following in accordance with Boeing Service Bulletin 757-76- 0008, dated March 22, 1990: 1. Inspect thrust control cable assemblies for damage, and replace any damaged thrust control cable assemblies prior to further flight; 2. Inspect the wire bundles for evidence of chafing, and repair any chafed wire bundles prior to further flight; and 3. Modify the wire bundles. B. An alternative method of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Seattle Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate. NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Seattle ACO. 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 Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington. This amendment (39-6983, AD 91-09-02) becomes effective on May 28, 1991. FOOTER:
Document Text
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AD Final Rules - DRS_91-09-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 91-09-02 Document Type: AD Final Rules Docket Number: 90-NM-269-AD Subject Heading: Airworthiness Directives; BOEING Model 757 Series Airplanes Subject: Wire Bundles Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 05/28/1991 Make: The Boeing Company Model: 757-200 Series | 757-200CB Series | 757-200PF Series | 757-300 Series 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: 91-09-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 90-NM-269-AD AMENDMENT: 39-6983 AD NUMBER: 91-09-02 SUBJECT HEADING: Airworthiness Directives; BOEING Model 757 Series Airplanes ACTION: SUMMARY: DATES: Effective May 28, 1991. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 91-09-02 BOEING: Amendment 39-6983. Docket No. 90-NM-269-AD. Applicability: Model 757 series airplanes, equipped with Rolls Royce RB211-535 engines; as listed in Boeing Service Bulletin 757-76-0008, dated March 22, 1990; certificated in any category. Compliance: Required within the next 3,000 hours time-in-service after the effective date of this AD, unless previously accomplished. To prevent chafing of the thrust control cable assemblies, wire bundle clamps, and wire bundles, accomplish the following: A. Accomplish the following in accordance with Boeing Service Bulletin 757-76- 0008, dated March 22, 1990: 1. Inspect thrust control cable assemblies for damage, and replace any damaged thrust control cable assemblies prior to further flight; 2. Inspect the wire bundles for evidence of chafing, and repair any chafed wire bundles prior to further flight; and 3. Modify the wire bundles. B. An alternative method of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Seattle Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate. NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Seattle ACO. 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 Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington. This amendment (39-6983, AD 91-09-02) becomes effective on May 28, 1991. FOOTER:
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