AD 82-27-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Sabreliner Corporation | NA-265-65 | Airworthiness Directives; ROCKWELL INTERNATIONAL Model NA 265-65 Airplanes |
Unsafe Condition
Failure of the horizontal stabilizer trim actuator and loss of longitudinal trim capabilities.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Disconnect and remove the flexible shaft interconnect (S. S. White Part Number 16023Y3.12) between the horizontal stabilizer trim actuators. Place a dust cover over the flexible shaft holes. Visually inspect the actuator dust cover/non-rotational sleeve for leaking grease, bulging, or cracking; replace the actuator if any condition exists. Inspect the actuator in the fully retracted position for sleeve contact with the base; replace if contact occurs. Inspect and rework each actuator per Service Bulletin 82-3 within 200 flight hours or six months, whichever comes first. Allow Special Flight Permits under FAR 21.197 for moving the airplane to a location for AD compliance.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 25 flight hours, within the next 25 flight hours and every 25 flight hours thereafter, and within the next 200 flight hours or six months, whichever occurs first.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
ROCKWELL INTERNATIONAL Model NA 265-65, Serial Numbers 465-1 through 465-76 and 306-114, 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.