AD 67-31-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna Aircraft Company | 150G | Airworthiness Directives; CESSNA Models 150G and 150H Airplanes |
| aircraft | Cessna Aircraft Company | 150H | Airworthiness Directives; CESSNA Models 150G and 150H Airplanes |
Unsafe Condition
Loss of longitudinal control due to the presence of the glove compartment
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Required Actions
Remove the glove compartment from the aircraft prior to further flight. Any modification to the removed compartment must be approved by the Chief, Engineering and Manufacturing Branch, FAA Central Region before reinstallation and return to service.
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Compliance Time
prior to further flight
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Affected Aircraft
Cessna Models 150G and 150H, Serial Numbers 15064533 through 15067891
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Federal Register Abstract
Removal Of Glove Compartment
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_67-31-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 67-31-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CESSNA Models 150G and 150H Airplanes Subject: Removal Of Glove Compartment Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 11/29/1967 Make: Cessna Aircraft Company Model: 150G | 150H Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 67-31-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-516 AD NUMBER: 67-31-04 SUBJECT HEADING: Airworthiness Directives; CESSNA Models 150G and 150H Airplanes ACTION: SUMMARY: DATES: Effective November 29, 1967. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 67-31-04 CESSNA: Amdt. 39-516, Part 39, Federal Register November 29, 1967. Applies to Models 150G and 150H Airplanes, Serial Numbers 15064533 through 15067891. To prevent loss of longitudinal control, unless already accomplished, prior to further flight, remove the glove compartment from the aircraft. If after it is removed the glove compartment is modified, the modification must be approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Central Region, before it is reinstalled in the aircraft and the aircraft returned to service. This amendment effective November 29, 1967, for all persons except those to whom it was made effective by air mail letter dated November 17, 1967. FOOTER:
Document Text
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AD Final Rules - DRS_67-31-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 67-31-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CESSNA Models 150G and 150H Airplanes Subject: Removal Of Glove Compartment Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 11/29/1967 Make: Cessna Aircraft Company Model: 150G | 150H 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: 67-31-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-516 AD NUMBER: 67-31-04 SUBJECT HEADING: Airworthiness Directives; CESSNA Models 150G and 150H Airplanes ACTION: SUMMARY: DATES: Effective November 29, 1967. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 67-31-04 CESSNA: Amdt. 39-516, Part 39, Federal Register November 29, 1967. Applies to Models 150G and 150H Airplanes, Serial Numbers 15064533 through 15067891. To prevent loss of longitudinal control, unless already accomplished, prior to further flight, remove the glove compartment from the aircraft. If after it is removed the glove compartment is modified, the modification must be approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Central Region, before it is reinstalled in the aircraft and the aircraft returned to service. This amendment effective November 29, 1967, for all persons except those to whom it was made effective by air mail letter dated November 17, 1967. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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