EASA Regulations for Tecnam P2006T

8 airworthiness directives and regulations affecting Tecnam P2006T.

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New ADs and bulletins for Tecnam P2006T, summarized like the ones below, every Monday.

EASA AD 2026-0124

Jul 1, 2026

Flight Controls – Aileron Hinge / Cotter Pins – Inspection

EASA Airworthiness Directive 2026-0124 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Tecnam P2006T and P2006T NG aeroplanes. It mandates inspection of the aileron hinge assemblies and cotter pins to ensure their integrity and prevent potential detachment of the ailerons. This directive applies to specific serial numbers of these aircraft models and aims to maintain flight safety by addressing a critical flight control component issue.

Airworthiness Directive
  • Tecnam P2006T
  • Tecnam P2006T NG

EASA AD 2022-0167

Aug 11, 2022

Flight Controls — Aileron Control Rod / Cover Panel Screws — Inspection

EASA Airworthiness Directive 2022-0167 is an airworthiness directive addressing the inspection of aileron control rod assemblies and cover panel screws on Costruzioni Aeronautiche TECNAM P2006T aeroplanes, specifically those with serial numbers up to 345 inclusive and select additional serial numbers. The directive mandates detailed inspections to detect damage and verify screw lengths to prevent potential control rod blockage. This AD applies to aileron control assemblies with part number 26-9-1502-000.

Airworthiness Directive
  • Tecnam P2006T
  • Costruzioni Aeronautiche TECNAM P2006T

EASA AD 2022-0132

Jul 4, 2022

Flight Controls – Aileron Control Rod / Cover Panel Screws – Inspection

EASA Airworthiness Directive 2022-0132 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Costruzioni Aeronautiche TECNAM S.p.A. P2006T aeroplanes with serial numbers up to 345 inclusive. The directive addresses potential damage to the aileron control rod caused by screws of excessive length installed on the cabin ceiling panel covering the affected part. It mandates inspection and corrective actions to ensure flight control safety.

Airworthiness DirectiveSuperseded
  • Tecnam P2006T
  • Costruzioni Aeronautiche TECNAM P2006T

EASA AD 2019-0043

Mar 6, 2019

Landing Gear — Nose Landing Gear Piston Tube — Replacement

EASA Airworthiness Directive 2019-0043 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Costruzioni Aeronautiche TECNAM Srl P2006T aeroplanes. It addresses the replacement of nose landing gear piston tubes, specifically part number 26-8-1408-1, due to a manufacturing defect identified in a specific batch. The directive applies to all serial numbers of the P2006T model with affected parts installed.

Airworthiness Directive
  • Tecnam P2006T
  • Costruzioni Aeronautiche TECNAM P2006T

EASA AD 2018-0029

Jan 31, 2018

Flight Controls — Rudder Trim Actuator — Life Limit Implementation

EASA Airworthiness Directive 2018-0029 is an airworthiness directive affecting all serial numbers of Tecnam P2006T aeroplanes except those with modification 2006/322. It addresses an error in the Aircraft Maintenance Manual regarding the part number of the rudder trim actuator and mandates the implementation of a life limit for the rudder trim actuator part number B6-7T. This directive ensures the continued airworthiness and safety of the rudder control system on affected aircraft.

Airworthiness Directive
  • Tecnam P2006T

EASA SIB 2014-34

Dec 23, 2014

Possible Exceedance of Engine Temperature Limits of BRP-Powertrain Rotax 912 and 914 Engines

EASA Safety Information Bulletin 2014-34 addresses a possible exceedance of engine temperature limits in BRP-Powertrain Rotax 912 and 914 engines. The bulletin affects specific serial numbers of 912 A/F/S and 914 F engines and certain cylinder heads installed since January 2013. These engines are installed on various light aircraft models including Cessna 150 series, Diamond Aircraft DA20-A1, and Tecnam P2006T among others.

Safety Information Bulletin
  • Brp-Rotax Gmbh & Co Kg 912 A
  • Brp-Rotax Gmbh & Co Kg 912 F
  • Brp-Rotax Gmbh & Co Kg 912 S
  • Brp-Rotax Gmbh & Co Kg 914 F
  • Cessna 150
  • Diamond Aircraft DA20-A1
  • Tecnam P2006T

EASA SIB 2014-31

Nov 7, 2014

BRP-Powertrain Rotax 912 and 914 Engines Carburettor Float Non-Conformity

EASA Safety Information Bulletin SIB No. 2014-31 addresses a carburettor float non-conformity issue in BRP-Powertrain Rotax 912 and 914 engines. The affected carburettors and floats, identified by specific part numbers, are installed on various light aircraft including Cessna 150 series, Diamond Aircraft DA20-A1, and Tecnam P2006T among others. This bulletin informs operators and maintenance personnel about potential rough engine operation at low speeds caused by float buoyancy loss and fuel regulation issues.

Safety Information Bulletin
  • Brp-Rotax Gmbh & Co Kg 912 A
  • Brp-Rotax Gmbh & Co Kg 912 F
  • Brp-Rotax Gmbh & Co Kg 912 S
  • Brp-Rotax Gmbh & Co Kg 914 F
  • Cessna 150
  • Diamond Aircraft DA20-A1
  • Tecnam P2006T