AD 46-13-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | DC3-G102 | DOUGLAS Model DC3 Aircraft |
| aircraft | The Boeing Company | DC3-G102A | DOUGLAS Model DC3 Aircraft |
| aircraft | The Boeing Company | DC3-G103A | DOUGLAS Model DC3 Aircraft |
| aircraft | The Boeing Company | DC3-G202A | DOUGLAS Model DC3 Aircraft |
| aircraft | The Boeing Company | DC3A-S1C3G | DOUGLAS Model DC3 Aircraft |
| aircraft | The Boeing Company | DC3A-S1CG | DOUGLAS Model DC3 Aircraft |
| aircraft | The Boeing Company | DC3A-S4C4G | DOUGLAS Model DC3 Aircraft |
| aircraft | The Boeing Company | DC3A-SC3G | DOUGLAS Model DC3 Aircraft |
| aircraft | The Boeing Company | DC3A-SCG | DOUGLAS Model DC3 Aircraft |
| aircraft | The Boeing Company | DC3C-R-1830-90C | DOUGLAS Model DC3 Aircraft |
Unsafe Condition
Canvas control boot assemblies may deteriorate, leading to loss of control column movement restriction and potential uncommanded control movement.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace canvas control boot assemblies with specified rubber assemblies per Douglas Service Bulletin No. 231 or approved alternatives from Thompson Co. or American Airlines. Inspect canvas boots before each flight until replaced.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
not later than April 1, 1947
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
The Boeing Company DC3-G102, DC3-G102A, DC3-G103A, DC3-G202A, DC3A-S1C3G, DC3A-S1CG, DC3A-S4C4G, DC3A-SC3G, DC3, and other listed models
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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