AD 75-26-09
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | SOCATA | MS 892A-150 | Airworthiness Directives; Morane Saulnier Models MS892.A-150, MS893-A, and MS894-A Airplanes |
| aircraft | SOCATA | MS 893A | Airworthiness Directives; Morane Saulnier Models MS892.A-150, MS893-A, and MS894-A Airplanes |
| aircraft | SOCATA | MS 894A | Airworthiness Directives; Morane Saulnier Models MS892.A-150, MS893-A, and MS894-A Airplanes |
Unsafe Condition
A distorted or bent elevator bellcrank could lead to loss of pitch-up control.
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Required Actions
Within 10 hours' time in service after the effective date, and every 100 hours thereafter, visually inspect the elevator bellcrank per Socata Service Bulletin No. 89 GR 27.07. If a bent or distorted bellcrank is found, replace it with reinforced part No. 880-27.0.371.0 before further flight.
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Compliance Time
Within the next 10 hours' time in service after the effective date of this AD, and thereafter at intervals not to exceed 100 hours' time in service from the last inspection
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Affected Aircraft
Morane Saulnier (SOCATA) Models MS892.A-150, MS893-A, and MS894-A airplanes, serial numbers 1873 and below
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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