AD 47-33-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | DC3-G102 | DOUGLAS DC3 Series Aircraft. |
| aircraft | The Boeing Company | DC3-G102A | DOUGLAS DC3 Series Aircraft. |
| aircraft | The Boeing Company | DC3-G103A | DOUGLAS DC3 Series Aircraft. |
| aircraft | The Boeing Company | DC3-G202A | DOUGLAS DC3 Series Aircraft. |
| aircraft | The Boeing Company | DC3A-S1C3G | DOUGLAS DC3 Series Aircraft. |
| aircraft | The Boeing Company | DC3A-S1CG | DOUGLAS DC3 Series Aircraft. |
| aircraft | The Boeing Company | DC3A-S4C4G | DOUGLAS DC3 Series Aircraft. |
| aircraft | The Boeing Company | DC3A-SC3G | DOUGLAS DC3 Series Aircraft. |
| aircraft | The Boeing Company | DC3A-SCG | DOUGLAS DC3 Series Aircraft. |
| aircraft | The Boeing Company | DC3C-R-1830-90C | DOUGLAS DC3 Series Aircraft. |
Unsafe Condition
Cowl flap hydraulic line failures and possible subsequent fires
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace grommets and lines forward of the firewall with AN 833-4 elbows and AN 924-4 nuts, or equivalent, and install new fire resistant flexible hose assemblies of proper length.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
not later than the first engine change after September 1, 1947, but in any event not later than December 1, 1947
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All DC3 Series Aircraft
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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