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Airworthiness directives › 2017-07-01

AD 2017-07-01 Airworthiness Directives; M7 Aerospace LLC Models Airplanes

2017-05-05
2017-03-31
39-18839
FAA-2016-9531
Airframe
—

Applicability*9

This AD applies to M7 Aerospace LLC SA226-T, SA226-AT, SA226-T(B), SA226-TC, SA227-AC (C-26A), SA227-AT, SA227-BC (C-26A), SA227-CC, SA227-DC (C-26B), and SA227-TT airplanes; all serial numbers, certificated in any category.

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

Use the applicable service bulletins as listed in paragraph (g)(1), (2), or (3) of this AD as reference to complete the actions in paragraph (i)(1) or (2) of this AD: (1) M7 Aerospace LLC SA226 Series Service Bulletin 226-76-012, dated March 17, 2015; (2) M7 Aerospace LLC SA227 Series Service Bulletin 227-76-007, dated March 17, 2015; or (3) M7Aerospace LLC SA227 Series Commuter Category Service Bulletin CC7-76-004, dated March 17, 2015.

Unsafe condition

This AD was prompted by detachment of the power lever linkage to the TPE331 engine propeller pitch control (PPC). We are issuing this AD to prevent detachment of the power lever linkage to the TPE331 engine PPC, which could result in uncommanded change to the engine power settings with consequent loss of control.

Affected ADs

None.

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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1