AD 65-28-05

final rule

Airworthiness Directives; Morrisey Models 2150 and 2150A Airplanes

AD Number
65-28-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

Applicability

TypeManufacturerModelDetails
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.

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

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.

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

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

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

Affected Aircraft

Augustair, Inc. Models 2150 and 2150A airplanes with main landing gear oleos using strut assemblies part numbers MO-11000 and MO-11002.

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

Federal Register Abstract

Main Landing Gear Oleos

Applicability Source Text

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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Superseded AD: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Superseded By: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

Show stored source text (verify against official source)
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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