Airworthiness Directives; Schweizer Aircraft Corporation Model 269C-1 Helicopters
airworthiness · Rule · Final rule. · Published 1999-02-16 · 64 FR 7493
Document
Document number
99-3588
Federal Register citation
64 FR 7493
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Schweizer
Publication date
1999-02-16
FAA docket
Docket No. 98-SW-39-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to Schweizer Aircraft Corporation Model 269C-1 helicopters, that requires a visual inspection of the bond line between the main rotor blade (blade) abrasion strip (abrasion strip) and the blade for voids, separation, or lifting of the abrasion strip; a visual inspection of the adhesive bead around the perimeter of the abrasion strip for erosion, cracks, or blisters; a tap (ring) test of the abrasion strip for debonding or hidden corrosion voids; and removal of any blade with an unairworthy abrasion strip and replacement with an airworthy blade. This amendment is prompted by four reports that indicate that debonding and corrosion have occurred on certain blades where the abrasion strip attaches to the blade skin. The actions specified by this AD are intended to prevent loss of the abrasion strip from the blade and subsequent loss of control of the helicopter.