AD 65-12-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Augustair, Inc. | 2150 | Airworthiness Directives; Morrisey Models 2150 and 2150A Aircraft |
| aircraft | Augustair, Inc. | 2150A | Airworthiness Directives; Morrisey Models 2150 and 2150A Aircraft |
Unsafe Condition
Cracks in the elevator horn, P/N 6000-9, due to improper fabrication.
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Required Actions
Visually inspect the 180 degrees bend of the elevator horn, P/N 6000-9, for cracks within the next 25 hours' time in service after the effective date, and thereafter every 100 hours' time in service. Replace the elevator horn before further flight if cracks are found, using a new horn manufactured after February 1, 1965, or an equivalent approved by the FAA.
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Compliance Time
within the next 25 hours' time in service after the effective date of this AD, and thereafter at intervals not to exceed 100 hours' time in service from the last inspection
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Affected Aircraft
Augustair, Inc. Models 2150 and 2150A Aircraft
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Federal Register Abstract
Elevator Horn
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_65-12-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 65-12-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Morrisey Models 2150 and 2150A Aircraft Subject: Elevator Horn Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 06/02/1965 Make: Augustair, Inc. Model: 2150 | 2150A Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 65-12-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-76 AD NUMBER: 65-12-04 SUBJECT HEADING: Airworthiness Directives; Morrisey Models 2150 and 2150A Aircraft ACTION: SUMMARY: DATES: Effective June 2, 1965. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 65-12-04 MORRISEY: Amdt. 39-76 Part 39 Federal Register June 2, 1965. Applies to Models 2150 and 2150A Aircraft. Compliance required as indicated. To prevent further elevator horn cracks as a result of improper fabrication, accomplish the following: (a) Visually inspect the 180 degrees bend of the elevator horn, P/N 6000-9, for cracks within the next 25 hours' time in service after the effective date of this AD, and thereafter at intervals not to exceed 100 hours' time in service from the last inspection. (b) If cracks are found, replace the elevator horn before further flight with a new horn, P/N 6000-9, manufactured after February 1, 1965, or an equivalent approved by the Chief, Aircraft Engineering Division, FAA Western Region. (c) The repetitive inspections required by (a) may be discontinued when the elevator horn is replaced in accordance with (b). NOTE: Elevator horn, P/N 6000-9, may be obtained from Shinn Engineering, Inc., 320 Dyer Road, Santa Ana, California. This directive effective June 2, 1965. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_65-12-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 65-12-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Morrisey Models 2150 and 2150A Aircraft Subject: Elevator Horn Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 06/02/1965 Make: Augustair, Inc. Model: 2150 | 2150A Product Type: Aircraft Product Subtype: Small 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: 65-12-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-76 AD NUMBER: 65-12-04 SUBJECT HEADING: Airworthiness Directives; Morrisey Models 2150 and 2150A Aircraft ACTION: SUMMARY: DATES: Effective June 2, 1965. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 65-12-04 MORRISEY: Amdt. 39-76 Part 39 Federal Register June 2, 1965. Applies to Models 2150 and 2150A Aircraft. Compliance required as indicated. To prevent further elevator horn cracks as a result of improper fabrication, accomplish the following: (a) Visually inspect the 180 degrees bend of the elevator horn, P/N 6000-9, for cracks within the next 25 hours' time in service after the effective date of this AD, and thereafter at intervals not to exceed 100 hours' time in service from the last inspection. (b) If cracks are found, replace the elevator horn before further flight with a new horn, P/N 6000-9, manufactured after February 1, 1965, or an equivalent approved by the Chief, Aircraft Engineering Division, FAA Western Region. (c) The repetitive inspections required by (a) may be discontinued when the elevator horn is replaced in accordance with (b). NOTE: Elevator horn, P/N 6000-9, may be obtained from Shinn Engineering, Inc., 320 Dyer Road, Santa Ana, California. This directive effective June 2, 1965. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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