AD 81-15-51 R1

final rule
Data completeness: 70%

Airworthiness Directives; ROCKWELL Models NA-265-60 and NA-265-80 Airplanes

AD Number
81-15-51 R1
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Sabreliner Corporation NA-265-60 Airworthiness Directives; ROCKWELL Models NA-265-60 and NA-265-80 Airplanes
aircraft Sabreliner Corporation NA-265-80 Airworthiness Directives; ROCKWELL Models NA-265-60 and NA-265-80 Airplanes

Unsafe Condition

Improper flap motion caused by a failure in the flap actuation system.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Rework the power drive unit and flap jackscrew actuators per Service Bulletin 81-5. Replace any drive shaft (part No. 57400-1640) with an extra hole. Repetitively remove and replace the power drive unit and flap jackscrew actuators every 200 landings.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within the next 20 landings following the effective date of this AD, or prior to the accumulation of 200 landings after incorporation of STC SA687NW or STC SA847NW, whichever comes later.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Rockwell NA-265-60 airplanes modified with STC SA687NW and equipped with Lear Siegler Flap Actuation System; Rockwell NA-265-80 airplanes modified with STC SA847NW.

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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