AircraftDirectives
MembershipSign inCreate free account
Menu
Airworthiness Directive

AD 2002-07-01 67 FR 15714 Active

Federal Aviation Administration · 14 CFR part 39

FR document
02-7645
Amendment
39-12695
Published
2002-04-03
Effective
2002-05-13
Models covered
2
Last live check
2026-10-01

Printed from https://aircraftdirectives.com/ad/2002-07-01 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

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.

Opens your browser's print dialog. Choose “Save as PDF” to export a file. Keyboard: Ctrl+P or Cmd+P.

AD

2002-07-01

FR doc 02-7645 · 67 FR 15714

AD 2002-07-01Published 2002-04-03Effective 2002-05-13

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 you to visually inspect certain horizontal stabilizer attachment reinforcement brackets for the existence of seam welds and replace any reinforcement bracket found without seam welds.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Cessna Aircraft Company (Cessna) P206, TP206, TU206, U206, 207, T207, 210, P210, and T210 series airplanes. This AD requires you to visually inspect certain horizontal stabilizer attachment reinforcement brackets for the existence of seam welds and replace any reinforcement bracket found without seam welds. This AD authorizes the pilot to check the logbooks to determine whether one of the affected horizontal stabilizer attachment reinforcement brackets is installed. This AD is the result of a report that certain parts were manufactured without seam welds. The actions specified by this AD are intended to detect and replace structurally deficient horizontal stabilizer attachment brackets. Continued use of such brackets could result in structural failure of the horizontal stabilizer with reduced or loss of control of the airplane.

More directives for Cessna 206

  1. AD 2020-18-01 Airworthiness Directives; Textron Aviation Inc. Airplanes 2020-10-07
  2. AD 2013-11-11 Airworthiness Directives; Cessna Aircraft Company Airplanes 2013-06-27
  3. AD 2012-10-52 Airworthiness Directives; Hartzell Engine Technologies Turbochargers 2012-06-11
  4. AD 2011-10-09 Airworthiness Directives; Cessna Aircraft Company Models 150, 152, 170, ... 2011-05-13
  5. AD 2008-26-10 Airworthiness Directives; Cessna Aircraft Company 172, 175, 177, 180, 18... 2008-12-24

All Cessna 206 directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab)

Applies to 2 models in our index