AD 75-23-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aer-Pegaso S.p.A. | Societe C.A.R.M.A.M. | M-100 S | Airworthiness Directives; Aer Pegaso M100S and Carmam M200 Gliders |
| aircraft | Aer-Pegaso S.p.A. | Societe C.A.R.M.A.M. | M-200 | Airworthiness Directives; Aer Pegaso M100S and Carmam M200 Gliders |
Unsafe Condition
Possible structural failure of aileron spars due to cracks in the spar to the right of the central hinge.
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Required Actions
Within 10 hours' time in service after the effective date, inspect aileron spar to the right of the central hinge for cracks every 20 hours' time in service. If cracks are found, reinforce with 1.5 mm thick birch plywood plates per Carmam Drawing dated April 12, 1968, before further flight.
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Compliance Time
Within the Next 10 hours' time in service after the effective date, and thereafter at intervals not to exceed 20 hours' time in service from the last inspection
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Affected Aircraft
Aer-Pegaso S.p.A. M-100 S gliders, all serial numbers; Carmam M-200 gliders except serial number 45 and subsequent
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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