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.
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.
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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
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.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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