- Model
- 202
- Data sheet
- TCDSA-795
- Product
- Aircraft · Large airplane
Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
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|---|---|---|---|
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On this page
The airworthiness directive
50-41-02 MARTIN: Applies to All Model 202 Aircraft.
Compliance required not later than December 1, 1950.
To maintain a sufficient hydraulic reservoir capacity for the operation of the hydraulic units in the event of failure in the emergency brake system, install a hydraulic fuse (Simmonds P/N G45-6E-402-80) or equivalent, adjacent to the main line tee in the emergency brake system between the main line and the emergency brake accumulator.
(Martin 202 Service Bulletin No. 105 covers this same subject.)
When the manually operated charging valve is installed in accordance with AD 51-11-01, this hydraulic fuse is no longer required.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.