AD 2007-16-15
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aviat | Various | Airworthiness Directives; Aerospatiale Model SN-601 (Corvette) Airplanes |
Unsafe Condition
Cracks have been evidenced on the nose landing gear LH (left-hand) and RH (right-hand) hinge fittings due to stress corrosion on in-service aircraft. If undetected, they could lead to complete rupture of one or two of the fittings.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the nose landing gear LH and RH hinge fittings for cracking within 200 flight hours or 6 months after the effective date, whichever occurs first. Replace the hinge fitting with a new fitting before further flight if cracks are found. Repeat inspections at intervals not to exceed 3,600 flight hours or 36 months, whichever occurs first.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 200 flight hours or 6 months after the effective date, whichever occurs first.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Aerospatiale Model SN-601 (Corvette) airplanes, all serial numbers; certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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