Airworthiness Directive

AD 98-08-25 R1 63 FR 54347 Active

Federal Aviation Administration · 14 CFR part 39

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…

FR document
98-26974
Amendment
39-10821
Published
1998-10-09
Effective
1999-01-05
Models covered
1

Last live check: 2026-08-19

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.
AD

98-08-25 R1

FR doc 98-26974 · 63 FR 54347

AD 98-08-25 R1Published 1998-10-09Effective 1999-01-05

Revises 98-08-25

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

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 on certain Twin Commander Aircraft Corporation (Twin Commander) 500, 680, 690, and 695 series airplanes; 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.

Full official abstract

This amendment revises Airworthiness Directive (AD) 98-08-25, which currently 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 on certain Twin Commander Aircraft Corporation (Twin Commander) 500, 680, 690, and 695 series airplanes; 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. The FAA inadvertently transposed the serial numbers of the 4 affected Model 695A airplanes. This AD retains the same actions of AD 98-08-25, and corrects the serial numbers of these 4 airplanes. Three of the four airplanes are not on the U.S. Register and the other one is already in compliance with the actions of AD 98-08-25. The actions specified in this AD are intended to continue 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.

More directives for Twin Commander (Aero Commander)

  1. AD 2013-09-05 Airworthiness Directives; Twin Commander Aircraft LLC Airplanes Effective 2013-05-29
  2. AD 2009-25-02 Airworthiness Directives; Twin Commander Aircraft LLC Models 690, 690A, ... Effective 2010-01-08
  3. AD 2006-15-01 Airworthiness Directives; Twin Commander Aircraft Corporation Models 690... Effective 2006-08-21
  4. AD 2003-07-03 Airworthiness Directives; Twin Commander Aircraft Corporation Models 690... Effective 2003-05-16
  5. AD 2000-02-30 Airworthiness Directives; Twin Commander Aircraft Corporation 600 Series... Effective 2000-03-24

All Twin Commander (Aero Commander) directives

Applies to 1 model in our index