Airworthiness Directives (ADs)
87-F28-045A
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
- 1999/07/22
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Applicability
- F28 Mark 0070 and Mark 0100 series
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Model Number
- F28
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CAA AD Number
- 87-F28-045A
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 99-09-18
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Effective Date
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Subject
- To prevent leakage of hot air from the corrujoint seals of the low- and high-pressure check valves located in the stubwings, and subsequent heat damage of fuselage skin and stubwing structure adjacent to bleed air system components in the stubwings, which could result in reduced structural integrity of the airplane.
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Reference Publications (Revision/ATA/SB)
- AD 98-08-01,SB SBF100-53-087, SBF100-36-027, SBF100-53-084, SBF100-36-026R1
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Remarks
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Download
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