Airworthiness Directives; Twin Commander Aircraft Corporation 500, 680, 690, and 695 Series Airplanes
airworthiness · Rule · Direct final rule; confirmation of effective date. · Published 1999-01-05 · Effective 1999-01-05 · 64 FR 395
Document
Document number
99-45
Federal Register citation
64 FR 395
Type
Rule
Action
Direct final rule; confirmation of effective date.
Category
airworthiness
Manufacturer
Twin Commander
Publication date
1999-01-05
Effective date
1999-01-05
FAA docket
Docket No. 96-CE-54-AD
Abstract
This action confirms the effective date of Airworthiness Directive (AD) 98-08-25 R1, which applies to certain Twin Commander Aircraft Corporation (Twin Commander) 500, 680, 690, and 695 series airplanes. AD 98-08-25 R1 requires replacing the nose landing gear (NLG) drag link bolt with an approved heat-treated bolt that has the manufacturer's serial number, manufacture date, and the last three digits of the drawing number (055) on the bolt head; and changing the bolt part number (P/N) to be installed on Models 690D and 695A from P/N ED10055 to P/N 750076-1. This AD was the result of the FAA inadvertently transposing the serial numbers of the 4 affected Model 695A airplanes. The actions specified in this AD are intended to prevent the NLG from collapsing due to failure of a drag link bolt, which could result in loss of control of the airplane during landing operations.