AD Amdt-39-11226
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aviat | Various | Airworthiness Directives; deHavilland Inc. Models DHC-2 Mk. I, DHC-2 Mk. II, and DHC-2 Mk. III Airplanes |
Unsafe Condition
Cracking of the rear fuselage bulkhead at Station 228 could result in structural damage of the fuselage to the point of failure, leading to loss of airplane control.
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Required Actions
Repetitively inspect the rear fuselage bulkhead at Station 228 for cracks. Repair any crack found or replace any cracked rear fuselage bulkhead in accordance with a repair or replacement scheme obtained from the manufacturer through the FAA.
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Affected Aircraft
deHavilland Inc. Models DHC-2 Mk. I, DHC-2 Mk. II, and DHC-2 Mk. III airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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