AD 83-05-02

final rule
Data completeness: 70%

Airworthiness Directives; Pilatus BN-2A Islander and Model BN-2A MKIII Trislander Series Airplanes

AD Number
83-05-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft B-N Group Ltd. BN-2A Airworthiness Directives; Pilatus BN-2A Islander and Model BN-2A MKIII Trislander Series Airplanes
aircraft B-N Group Ltd. BN-2A-2 Airworthiness Directives; Pilatus BN-2A Islander and Model BN-2A MKIII Trislander Series Airplanes
aircraft B-N Group Ltd. BN-2A-20 Airworthiness Directives; Pilatus BN-2A Islander and Model BN-2A MKIII Trislander Series Airplanes
aircraft B-N Group Ltd. BN-2A-21 Airworthiness Directives; Pilatus BN-2A Islander and Model BN-2A MKIII Trislander Series Airplanes
aircraft B-N Group Ltd. BN-2A-26 Airworthiness Directives; Pilatus BN-2A Islander and Model BN-2A MKIII Trislander Series Airplanes
aircraft B-N Group Ltd. BN-2A-27 Airworthiness Directives; Pilatus BN-2A Islander and Model BN-2A MKIII Trislander Series Airplanes
aircraft B-N Group Ltd. BN-2A-3 Airworthiness Directives; Pilatus BN-2A Islander and Model BN-2A MKIII Trislander Series Airplanes
aircraft B-N Group Ltd. BN-2A-6 Airworthiness Directives; Pilatus BN-2A Islander and Model BN-2A MKIII Trislander Series Airplanes
aircraft B-N Group Ltd. BN-2A-8 Airworthiness Directives; Pilatus BN-2A Islander and Model BN-2A MKIII Trislander Series Airplanes
aircraft B-N Group Ltd. BN-2A-9 Airworthiness Directives; Pilatus BN-2A Islander and Model BN-2A MKIII Trislander Series Airplanes

Unsafe Condition

Failure of throttle, mixture, or propeller control due to cracking in the attachment brackets of the teleflex conduit swivel assemblies.

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

Required Actions

Inspect attachment brackets on teleflex conduit swivel assemblies for cracking using a 5-power glass per SB BN-2/SB.109, Issue 3. Replace cracked assemblies with serviceable parts (C.79412, C.79411, or C.79410) and install bracket reinforcement. Incorporate reinforcement even if no cracks are found.

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

Compliance Time

within 100 hours time-in-service

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

Affected Aircraft

Pilatus BN-2A Islander and Model BN-2A MKIII Trislander airplanes not modified per Modification No. NB/M/939 and NB/M/996

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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