EASA Regulations for Daher Aerospace TB

4 airworthiness directives and regulations affecting Daher Aerospace TB.

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New ADs and bulletins for Daher Aerospace TB, summarized like the ones below, every Monday.

EASA AD 2025-0160

Jul 25, 2025

Flight Controls — Lower Rudder Hinge Fitting — Inspection

EASA Airworthiness Directive 2025-0160 is an official safety directive addressing the inspection of the lower rudder hinge fitting on DAHER Aerospace TB 9, TB 10, TB 200, TB 20, and TB 21 aeroplanes. This directive mandates repetitive visual inspections to detect potential cracks or failures in the lower rudder hinge fitting, a critical flight control component. The directive aims to prevent loss of control caused by separation between the rudder and its control linkage.

Airworthiness Directive
  • Daher Aerospace TB

EASA AD US-2024-14-03

Jul 22, 2024

Auto Flight - Garmin GFC 500 Autopilot System - Software Update

The Federal Aviation Administration's Airworthiness Directive 2024-14-03 addresses various airplanes equipped with the Garmin GFC 500 Autopilot System installed under Supplemental Type Certificate No. SA01866WI. This directive mandates a software update to the Garmin GFC 500 Autopilot System to prevent un-commanded automatic pitch trim runaway events. The affected aircraft include all models specified in the directive that have the optional GSA 28 pitch trim servo installed.

Airworthiness Directive
  • Commander (Cpac, Inc.) 112
  • Commander (Cpac, Inc.) 114
  • Daher Aerospace TB
  • Mooney International Corporation M20
  • Piper Aircraft PA-24 (Comanche)
  • Piper Aircraft PA-28 (Archer)
  • Piper Aircraft PA-28 (Cadet)
  • Piper Aircraft PA-28 (Cherokee)
  • Piper Aircraft PA-28 (Dakota)
  • Piper Aircraft PA-28 (Warrior)
  • Piper Aircraft PA-28R (Arrow)
  • Piper Aircraft PA-30 (Twin Comanche)
  • Piper Aircraft PA-32 (Cherokee Six)
  • Piper Aircraft PA-32 (Piper 6X)
  • Piper Aircraft PA-32 (Saratoga)
  • Piper Aircraft PA-32R (Lance)
  • Piper Aircraft PA-39 (Twin Comanche)
  • Textron Aviation 172 (Skyhawk)
  • Textron Aviation 172RG
  • Textron Aviation 177 (Cardinal)
  • Textron Aviation 177RG (Cardinal RG)
  • Textron Aviation 182 (Skylane)
  • Textron Aviation 19
  • Textron Aviation 206
  • Textron Aviation U206 (Super Skywagon)
  • Textron Aviation 206H (Stationair)
  • Textron Aviation 210 (Centurion)
  • Textron Aviation 23 (Musketeer)
  • Textron Aviation 24 (Sierra)
  • Textron Aviation 33 (Bonanza)
  • Textron Aviation 35 (Bonanza)
  • Textron Aviation 36 (Bonanza)
  • Textron Aviation F172
  • Textron Aviation F177RG
  • Textron Aviation F182
  • Textron Aviation FR172 (Reims Rocket)
  • Textron Aviation P172D
  • Textron Aviation P206
  • Textron Aviation TP206 (Super Skylane)
  • Textron Aviation R172 (Hawk XP)

EASA AD 2019-0274

Nov 6, 2019

Landing Gear — Main Landing Gear Leg — Inspection

EASA Airworthiness Directive 2019-0274 is an airworthiness directive issued by EASA concerning the inspection of the main landing gear legs on DAHER Aerospace TB 20 and TB 21 aeroplanes. It mandates repetitive detailed inspections using magnetic particle methods to detect cracks in the main landing gear leg areas. This directive applies to all serial numbers of these aircraft models to ensure continued airworthiness and safety.

Airworthiness Directive
  • Daher Aerospace TB
  • DAHER Aerospace TB 20
  • DAHER Aerospace TB 21

EASA AD 2018-0030R1

Jun 4, 2018

Wings — Wing Front Attachments — Inspection / Modification / Replacement

EASA Airworthiness Directive 2018-0030R1 addresses inspection, modification, and replacement requirements for wing front attachments on SOCATA TB 9, TB 10, and TB 200 aeroplanes. It mandates repetitive inspections and reinforcement of wing front attachments on both wing and fuselage sides to ensure structural integrity. The directive applies to all manufacturer serial numbers of these aircraft models.

Airworthiness Directive
  • Daher Aerospace TB
  • SOCATA TB 9
  • SOCATA TB 10
  • SOCATA TB 200