AD 82-26-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Sabreliner Corporation | NA-265-60 | Airworthiness Directives; ROCKWELL INTERNATIONAL Models NA 265-65, and NA 265-60 Series Airplanes |
| aircraft | Sabreliner Corporation | NA-265-65 | Airworthiness Directives; ROCKWELL INTERNATIONAL Models NA 265-65, and NA 265-60 Series Airplanes |
Unsafe Condition
Possible inadvertent cabin pressure loss due to fatigue failure of interior pressure panel P/N 306-312005-3.
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Required Actions
Visually inspect the vertical floor panel P/N 306-312005-3 per SB 82-9. If cracks are found, replace the panel before next flight (except ferry flights per item C). If no cracks, repeat inspections after 50 and 100 flight hours and replace if required. Replace panel within 150 flight hours per SB 82-9.
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Compliance Time
Prior to the next flight for initial inspection and crack replacement. Within the next 150 flight hours for panel replacement. Ferry flights allowed under specified conditions.
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Affected Aircraft
ROCKWELL INTERNATIONAL Models NA 265-65 (serial 306-114) and NA 265-60 series (serials 306-1 through 306-141 except 306-114 and 306-136), 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 8, 2026
Rights: U.S. Government Public Domain
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