AD 71-24-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | FH1100 Manufacturing Corporation | FH-1100 | Airworthiness Directives; Fairchild Hiller Model FH-1100 Helicopters |
Unsafe Condition
Failure of the landing gear torque tube P/N 24-43041 at the skid support attachments.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect and replace if necessary torque tube P/N 24-43041 in accordance with Fairchild Hiller Service Letter SL FH1100-43-1 or FAA-approved revision. Initial inspection within 50 hours in service after the effective date, followed by inspections every 100 hours in service thereafter.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 50 hours in service after the effective date, unless already accomplished within the last 50 hours in service. Subsequent inspections every 100 hours in service thereafter.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
FH1100 Manufacturing Corporation Model FH-1100 helicopters certificated in all categories.
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.