AD 89-23-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 737-300 Series | Airworthiness Directives; BOEING Model 737-300 and -400 Series Airplanes |
| aircraft | The Boeing Company | 737-400 Series | Airworthiness Directives; BOEING Model 737-300 and -400 Series Airplanes |
Unsafe Condition
Engine ice ingestion jeopardizing continued safe flight and landing.
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Required Actions
Incorporate Boeing Operations Manual Bulletin 737-300-89-1 or 737-400-89-1 into the Airplane Operations Manual. An alternate means of compliance or adjustment may be used if approved by the FAA Manager, Seattle Aircraft Certification Office.
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Compliance Time
within 10 days after the effective date of this AD
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Affected Aircraft
BOEING Model 737-300 and -400 Series airplanes, certificated in any category.
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Federal Register Abstract
Engine Ice Ingestion
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_89-23-10.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 89-23-10 Document Type: AD Final Rules Docket Number: 88-NM-212-AD Subject Heading: Airworthiness Directives; BOEING Model 737-300 and -400 Series Airplanes Subject: Engine Ice Ingestion Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/04/1989 Make: The Boeing Company Model: 737-300 Series | 737-400 Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 89-23-10 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 88-NM-212-AD AMENDMENT: 39-6375 AD NUMBER: 89-23-10 SUBJECT HEADING: Airworthiness Directives; BOEING Model 737-300 and -400 Series Airplanes ACTION: SUMMARY: DATES: Effective December 4, 1989. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 89-23-10 BOEING: Amendment 39-6375. Docket No. 88-NM-212-AD. Applicability: Model 737-300 and -400 series airplanes, certificated in any category. Compliance: Required within 10 days after the effective date of this AD, unless previously accomplished. To reduce the risk of jeopardizing continued safe flight and landing due to engine ice ingestion, accomplish the following: A. Incorporate Boeing Operations Manual Bulletin 737-300-89-1 or 737-400-89-1, both dated February 14, 1989, as appropriate, into the Airplane Operations Manual. 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, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. NOTE: The request should be forwarded through an FAA Principal Operations Inspector (POI), who will either concur or comment and then send it to the Manager, Seattle Aircraft Certification Office. 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 Airplanes, P.O. Box 3707, Seattle, Washington 98124. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. This amendment (39-6375, AD 89-23-10) becomes effective on December 4, 1989. FOOTER:
Document Text
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AD Final Rules - DRS_89-23-10.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 89-23-10 Document Type: AD Final Rules Docket Number: 88-NM-212-AD Subject Heading: Airworthiness Directives; BOEING Model 737-300 and -400 Series Airplanes Subject: Engine Ice Ingestion Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/04/1989 Make: The Boeing Company Model: 737-300 Series | 737-400 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: 89-23-10 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 88-NM-212-AD AMENDMENT: 39-6375 AD NUMBER: 89-23-10 SUBJECT HEADING: Airworthiness Directives; BOEING Model 737-300 and -400 Series Airplanes ACTION: SUMMARY: DATES: Effective December 4, 1989. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 89-23-10 BOEING: Amendment 39-6375. Docket No. 88-NM-212-AD. Applicability: Model 737-300 and -400 series airplanes, certificated in any category. Compliance: Required within 10 days after the effective date of this AD, unless previously accomplished. To reduce the risk of jeopardizing continued safe flight and landing due to engine ice ingestion, accomplish the following: A. Incorporate Boeing Operations Manual Bulletin 737-300-89-1 or 737-400-89-1, both dated February 14, 1989, as appropriate, into the Airplane Operations Manual. 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, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. NOTE: The request should be forwarded through an FAA Principal Operations Inspector (POI), who will either concur or comment and then send it to the Manager, Seattle Aircraft Certification Office. 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 Airplanes, P.O. Box 3707, Seattle, Washington 98124. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. This amendment (39-6375, AD 89-23-10) becomes effective on December 4, 1989. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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