AD 60-03-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Lockheed Martin Corporation | 188A | LOCKHEED Model L-188 Aircraft |
| aircraft | Lockheed Martin Corporation | 188C | LOCKHEED Model L-188 Aircraft |
Unsafe Condition
Loss of the top cowl panel over the engine tail pipe has occurred in flight due to insecurity of the cowl latches.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace snap ring retention with clevis or shoulder pin design and safety in place on latch assemblies. Install position pins and locators to ensure proper alignment of the cowling with latches when closed.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
April 1, 1960
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Lockheed Model L-188 Aircraft, including 188A and 188C models, all serial numbers.
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.