AD 50-41-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Martin-Marietta Corporation | 202 | Martin Model 202 Aircraft |
Unsafe Condition
Failure of the emergency brake system hydraulic fuse could result in insufficient hydraulic reservoir capacity for operation of hydraulic units.
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Required Actions
Install a Simmonds P/N G45-6E-402-80 hydraulic fuse or equivalent adjacent to the main line tee in the emergency brake system between the main line and the emergency brake accumulator. The fuse is no longer required if a manually operated charging valve is installed as per AD 51-11-01.
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Compliance Time
not later than December 1, 1950
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Affected Aircraft
Martin-Marietta Corporation Model 202 aircraft
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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