AD 2001-07-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna | 750 | Airworthiness Directives; Cessna Model 750 Airplanes |
Unsafe Condition
Jamming of the roll control system (ailerons and spoilers) due to inadequate clearance between the control cable and the web, which could result in reduced controllability of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the bulkhead web for an existing round bulkhead web doubler with part number 6711093-38 and remove it if found. Install new left and right bulkhead web doublers with part numbers 6791213-3 and 6791213-4, respectively, and enlarge the lightening holes as specified in Cessna Service Bulletin SB750-53-19.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 200 flight hours or 180 days after the effective date of the AD, whichever occurs first.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Cessna Model 750 airplanes, serial numbers -0001 through -0102 inclusive, certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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