AD 92-16-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna Aircraft Company | 441 | Airworthiness Directives; CESSNA Model 441 Airplanes |
Unsafe Condition
Loss of horizontal stabilizer front spar structural support caused by cracks in the fuselage bulkhead at Fuselage Station (FS) 387.22.
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Required Actions
Dye penetrant inspect the horizontal stabilizer forward attach bulkhead at FS 387.22 in accordance with Cessna Attachment to Service Bulletin CQB91-1R1. If cracks are found, replace the bulkhead and install Service Kit SK441-103A prior to further flight. The installation of SK441-103A terminates repetitive inspection requirements.
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Compliance Time
Initially upon the accumulation of 3,000 hours time-in-service (TIS) or within the next 200 hours TIS after the effective date of this AD, whichever occurs later, and thereafter at intervals not to exceed 2,000 hours TIS.
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Affected Aircraft
Cessna Model 441 airplanes (serial numbers 441-0001 through 441-0362), certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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