AD 65-28-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Augustair, Inc. | 2150 | Airworthiness Directives; Morrisey Models 2150 and 2150A Airplanes |
| aircraft | Augustair, Inc. | 2150A | Airworthiness Directives; Morrisey Models 2150 and 2150A Airplanes |
Unsafe Condition
Cracking in the weldments of strut assemblies, part numbers MO-11000 and MO-11002, where the scissor assemblies are attached to the main landing gear oleos.
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Required Actions
Visually inspect the upper and lower scissors attachment fittings for cracks within 25 hours' time in service after the effective date and at intervals not exceeding 25 hours' time in service. If cracks are found, reinforce with 4130 steel plates as per Figure 1 or an equivalent repair approved by the FAA before further flight.
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Compliance Time
Within 25 hours' time in service after the effective date of this AD and at intervals not to exceed 25 hours' time in service from the last inspection
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Affected Aircraft
Augustair, Inc. Models 2150 and 2150A airplanes with main landing gear oleos using strut assemblies part numbers MO-11000 and MO-11002.
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Federal Register Abstract
Main Landing Gear Oleos
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_65-28-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 65-28-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Morrisey Models 2150 and 2150A Airplanes Subject: Main Landing Gear Oleos Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/21/1965 Make: Augustair, Inc. Model: 2150 | 2150A Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 65-28-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-171 AD NUMBER: 65-28-05 SUBJECT HEADING: Airworthiness Directives; Morrisey Models 2150 and 2150A Airplanes ACTION: SUMMARY: DATES: Effective December 21, 1965. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 65-28-05 MORRISEY: Amdt. 39-171 Part 39 Federal Register December 21, 1965. Applies to Models 2150 and 2150A Airplanes. Compliance required as indicated, unless already accomplished. To detect cracking in the weldments of strut assemblies, P/N's MO-11000 and MO-11002, for both the right and left oleos of the main landing gear where the scissor assemblies are attached, accomplish the following: (a) Within 25 hours' time in service after the effeactive date of this AD and at intervals not to exceed 25 hours' time in service from the last inspection, visually inspect for cracks the upper and lower scissors attachment fittings of the main landing gear until accomplishment of (c). (b) If cracks are found, reinforce in accordance with (c) before further flight. (c) Reinforce upper and lower scissors attachment fittings by the addition of 4130 steel plates at three locations described in Figure 1 or accomplish an equivalent repair approved by the Chief, Aircraft Engineering Division, FAA Western Region. This directive effective December 21, 1965. FOOTER:
Document Text
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AD Final Rules - DRS_65-28-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 65-28-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Morrisey Models 2150 and 2150A Airplanes Subject: Main Landing Gear Oleos Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/21/1965 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: 65-28-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-171 AD NUMBER: 65-28-05 SUBJECT HEADING: Airworthiness Directives; Morrisey Models 2150 and 2150A Airplanes ACTION: SUMMARY: DATES: Effective December 21, 1965. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 65-28-05 MORRISEY: Amdt. 39-171 Part 39 Federal Register December 21, 1965. Applies to Models 2150 and 2150A Airplanes. Compliance required as indicated, unless already accomplished. To detect cracking in the weldments of strut assemblies, P/N's MO-11000 and MO-11002, for both the right and left oleos of the main landing gear where the scissor assemblies are attached, accomplish the following: (a) Within 25 hours' time in service after the effeactive date of this AD and at intervals not to exceed 25 hours' time in service from the last inspection, visually inspect for cracks the upper and lower scissors attachment fittings of the main landing gear until accomplishment of (c). (b) If cracks are found, reinforce in accordance with (c) before further flight. (c) Reinforce upper and lower scissors attachment fittings by the addition of 4130 steel plates at three locations described in Figure 1 or accomplish an equivalent repair approved by the Chief, Aircraft Engineering Division, FAA Western Region. This directive effective December 21, 1965. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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