AD 65-12-04

final rule

Airworthiness Directives; Morrisey Models 2150 and 2150A Aircraft

AD Number
65-12-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

Applicability

TypeManufacturerModelDetails
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.

AI-generated summary from the source AD text. Verify against the official source before acting.

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.

AI-generated summary from the source AD text. Verify against the official source before acting.

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

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Augustair, Inc. Models 2150 and 2150A Aircraft

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

Elevator Horn

Applicability Source Text

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AD Final Rules - DRS_65-12-04.html
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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Superseded AD: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Superseded By: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
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Document Versions
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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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