AD 69-24-01
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 Model M.100S and Carmam Model M.200 Gliders |
| aircraft | Aer-Pegaso S.p.A. | Societe C.A.R.M.A.M. | M-200 | Airworthiness Directives; Aer-Pegaso Model M.100S and Carmam Model M.200 Gliders |
Unsafe Condition
Improper installation of the horizontal stabilizer to the glider.
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Required Actions
Install an inspection window on the left side of the dorsal fin and paint the elevator control transmission fork plates per Aer-Pegaso Technical Bulletin N.10/M-100S or FAA-approved equivalent. Install a placard in the cockpit instructing the pilot to visually confirm the elevator control lever engagement before first flight after tailplane rigging.
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Compliance Time
within the next 25 hours' time in service after the effective date of this AD
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Affected Aircraft
Aer-Pegaso Model M.100S and Carmam Model M.200 gliders
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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