AD 48-31-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Gulfstream American Corporation | G-44 | Airworthiness Directives; Grumman Model G-44 and G-44A Aircraft |
| aircraft | Gulfstream American Corporation | G-44A | Airworthiness Directives; Grumman Model G-44 and G-44A Aircraft |
Unsafe Condition
Cracks extending radially from the outside edge of the ears to the inside of the hole in the stabilizer strut upper terminal (P/N 17257-1).
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect upper terminal (P/N 17257-1) of stabilizer strut (P/N 17256) for cracks. Replace cracked terminals with steel terminals. Inspect all uncracked terminals every 100 hours.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
by September 15, 1948
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Grumman Model G-44 and G-44A 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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