AD 73-14-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Commander Aircraft Corporation | 112 | Airworthiness Directives; Rockwell Commander Model 112 Airplanes |
Unsafe Condition
Cracks in the prop spinner bulkhead flange, radius between flange and web, or rear bulkhead and doublers near spinner dome attachments.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Remove the spinner dome, visually inspect front and rear bulkheads for cracks, replace defective parts with new or serviceable parts, reassemble spinner dome with fiber washers and torque screws to 20-25 in.lbs, and record compliance in Aircraft Log Book.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within the next 10 hours time in service after the effective date of this AD and every 10 hours time in service thereafter
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Rockwell Commander Model 112 airplanes Serial Number 3 and up equipped with Hartzell propeller spinner C-3533 or C-3533P
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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