Airworthiness Directives (ADs)
88-S76-034A
The aircraft owner or operator shall comply with Airworthiness Directives issued by the CAA or the aeronautics authority of the State of Design (SoD) of the aviation products, appliances and parts, and take all necessary actions thereto.
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Issue Date
- 1999/07/05
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Applicability
- S-76A
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Model Number
- S76
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CAA AD Number
- 88-S76-034A
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 99-11-04
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Effective Date
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Subject
- To reduce the published Category "A" maximum takeoff and landing gross weights and single-engine forward climb performance limitations of the Rotorcraft Flight Manual (RFM), when an AC generator interlock system is not installed.
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Reference Publications (Revision/ATA/SB)
- RFM, ASB 76-77-4A Revision A
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Remarks
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Download
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