Costruzioni Aeronautiche Tecnam srl Airworthiness Directives

41 ADs indexed for Costruzioni Aeronautiche Tecnam srl aircraft.

Models

Recent ADs

2026-07-05 Recurring

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Airworthiness Directives; Costruzioni Aeronautiche Tecnam S.P.A. Airplanes

Unsafe Condition: 95 percent blockage of the exhaust due to disconnection of the exhaust muffler flame tube, which could result in unrecoverable loss of engine power and loss of control of the airplane.

Effective: Apr 20, 2026 Category: engine Compliance: Within 25 hours time-in-service or 30 days, whichever occurs first after the effective date of th...

Why matched: Airworthiness Directives; Costruzioni Aeronautiche Tecnam S.P.A. Airplanes

2025-17-13 Recurring

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Airworthiness Directives; Costruzioni Aeronautiche Tecnam S.p.A. Airplanes

Unsafe Condition: Failure of the pilot seat locking mechanism, which could lead to the pilot seat unlocking during flight, possibly resulting in loss of control of the airplane.

Effective: Sep 26, 2025 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Costruzioni Aeronautiche Tecnam S.p.A. Airplanes

2025-03-09

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Airworthiness Directives; Costruzioni Aeronautiche Tecnam S.P.A Airplanes

Unsafe Condition: The disconnection of a rudder pedals torque tube from one of its hinges could cause the rudder pedals assembly to slip out of its housing resulting in the inability of the flightcrew to maintain th...

Effective: Mar 3, 2025 Category: aircraft Compliance: Within 25 hours time-in-service or 30 days, whichever occurs first after the effective date of th...

Why matched: Airworthiness Directives; Costruzioni Aeronautiche Tecnam S.P.A Airplanes

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

2023-09-09 Recurring

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Airworthiness Directives; Various Airplanes, Helicopters, and Engines

Unsafe Condition: Multiple failures of spot-welded, multi-segment v-band couplings at the tailpipe to the turbocharger exhaust housing flange.

Effective: Jul 17, 2023 Category: engine Compliance: Within 50 flight hours after the effective date of this AD.

Why matched: Airworthiness Directives; Various Airplanes, Helicopters, and Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2022-19-11

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Airworthiness Directives; Costruzioni Aeronautiche Tecnam S.P.A. Airplanes

Unsafe Condition: screws attaching the ceiling panel covering the aileron control assembly could be of excessive length and cause the aileron control rod to become blocked, cracked, or damaged.

Effective: Sep 30, 2022 Category: aircraft Compliance: before further flight

Why matched: Airworthiness Directives; Costruzioni Aeronautiche Tecnam S.P.A. Airplanes

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

2022-12-06 Recurring

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Airworthiness Directives; Costruzioni Aeronautiche Tecnam S.P.A. Airplanes

Unsafe Condition: free play in the trim tab actuator and trim tab surface, which could lead to a significant free play on the trim tab connection, with consequent increase in dynamic loads and vibrations, possibly r...

Effective: Jul 19, 2022 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Costruzioni Aeronautiche Tecnam S.P.A. Airplanes

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

2021-22-22

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Airworthiness Directives; Costruzioni Aeronautiche Tecnam S.P.A. Airplanes

Unsafe Condition: A manufacturing defect in the nose landing gear (NLG) piston tube, which could result in failure of the NLG upon or after landing.

Effective: Dec 3, 2021 Category: aircraft Compliance: Within 50 hours time-in-service after the effective date of this AD or within 2 months after the ...

Why matched: Airworthiness Directives; Costruzioni Aeronautiche Tecnam S.P.A. Airplanes

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

2018-15-07

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Airworthiness Directives; Costruzioni Aeronautiche Tecnam srl Airplanes

Unsafe Condition: an incorrect part number for the rudder trim actuator is referenced in the Airworthiness Limitations section of the FAA-approved maintenance program (e.g., maintenance manual), and the life limit f...

Effective: Sep 4, 2018 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Costruzioni Aeronautiche Tecnam srl Airplanes

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

2015-02-09

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Airworthiness Directives; Costruzioni Aeronautiche Tecnam srl Airplanes

Unsafe Condition: Cracking found in the engine exhaust pipe Part Number (P/N) 26-7-1800-1.

Effective: Mar 5, 2015 Category: engine Compliance: Within 25 hours time-in-service (TIS) after March 5, 2015, or within the next 30 days after March...

Why matched: Airworthiness Directives; Costruzioni Aeronautiche Tecnam srl Airplanes

2014-11-09

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Airworthiness Directives; Costruzioni Aeronautiche Tecnam srl Airplanes

Unsafe Condition: A cracked engine mount, specifically part number 26-7-1200-000, which could lead to engine damage, possibly resulting in damage to the airplane and injury to the occupants.

Effective: Jul 15, 2014 Category: engine Compliance: Within the next 25 hours time-in-service (TIS) after July 15, 2014, or within the next 30 days af...

Why matched: Airworthiness Directives; Costruzioni Aeronautiche Tecnam srl Airplanes

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2014-02-07

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Airworthiness Directives; Costruzioni Aeronautiche Tecnam srl Airplanes

Unsafe Condition: cracking of the nose landing gear (NLG) lower link

Effective: Mar 14, 2014 Category: aircraft Compliance: within the next 25 hours time-in-service (TIS) after March 14, 2014, or within the next 30 days a...

Why matched: Airworthiness Directives; Costruzioni Aeronautiche Tecnam srl Airplanes

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

2013-04-09

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Airworthiness Directives; Costruzioni Aeronautiche Tecnam srl Airplanes

Unsafe Condition: Multiple cracks found on the outboard aileron hinge support, part number 26-1-1082-1/3, which could jeopardize wing structural integrity.

Effective: Apr 9, 2013 Category: aircraft Compliance: Within 30 days or 25 hours TIS after specified milestones, depending on time-in-service as of Apr...

Why matched: Airworthiness Directives; Costruzioni Aeronautiche Tecnam srl Airplanes

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

2012-18-04

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Airworthiness Directives; Costruzioni Aeronautiche Tecnam srl Airplanes

Unsafe Condition: Cracking, bulging, deformation, or oil leakage in the lower lid of the landing gear emergency accumulator, which could result in decreasing the airplane's structural integrity and jeopardizing the ...

Effective: Oct 22, 2012 Category: aircraft Compliance: Within 12 months of the effective date (October 22, 2012).

Why matched: Airworthiness Directives; Costruzioni Aeronautiche Tecnam srl Airplanes

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

2011-13-02

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Airworthiness Directives; Costruzioni Aeronautiche Tecnam srl Model P2006T Airplanes

Unsafe Condition: A loose Seeger ring was found on the nose landing gear hydraulic actuator cap, attributed to a design deficiency of the hydraulic actuator caps. This could lead to uncommanded and improper extensio...

Effective: Jul 22, 2011 Category: aircraft Compliance: Within 50 hours time-in-service after July 22, 2011, or within 60 days after July 22, 2011, which...

Why matched: Airworthiness Directives; Costruzioni Aeronautiche Tecnam srl Model P2006T Airplanes

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

2008-12-13

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Airworthiness Directives; GENERAL AVIA Costruzioni Aeronatiche Models F22B, F22C, and F22R Airplanes

Unsafe Condition: Cracks found in the Firewall-to-Engine mounting attachments, which could lead to detachment of the engine mounts from the structure.

Effective: Jul 23, 2008 Category: aircraft Compliance: Before further flight and repetitively thereafter at intervals not to exceed 100 hours TIS.

Why matched: Airworthiness Directives; GENERAL AVIA Costruzioni Aeronatiche Models F22B, F22C, and F22R Airplanes

2000-03-18

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Airworthiness Directives; Partenavia Costruzioni Aeronauticas S.p.A. Models AP68TP 300 “Spartacus” and AP68TP 600 “Viator” Airplanes

Unsafe Condition: Reports of in-flight incidents and an accident in icing conditions where the airframe pneumatic deicing boots were not activated, leading to reduced controllability due to ice accumulation.

Effective: Apr 7, 2000 Category: aircraft Compliance: Before further flight.

Why matched: Airworthiness Directives; Partenavia Costruzioni Aeronauticas S.p.A. Models AP68TP 300 Spartacus" and AP68TP 600 "Viator" Airplanes

98-04-20

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Airworthiness Directives; Partenavia Costruzioni Aeronauticas, S.p.A. Model P68, AP68TP 300, AP68TP 600 Airplanes

Unsafe Condition: The absence of adequate information in the Airplane Flight Manual (AFM) to determine when icing conditions exceed certification limits and the lack of procedures to exit such conditions presents an...

Effective: Mar 13, 1998 Category: aircraft

Why matched: Airworthiness Directives; Partenavia Costruzioni Aeronauticas, S.p.A. Model P68, AP68TP 300, AP68TP 600 Airplanes

Amdt-39-10332

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Airworthiness Directives; Partenavia Costruzioni Aeronauticas, S.p.A. Model P68, AP68TP 300, AP68TP 600 Airplanes

Unsafe Condition: Operating in severe icing conditions without clear procedures and limitations may lead to adverse effects on flight control devices and airplane performance.

Effective: Mar 13, 1998 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Partenavia Costruzioni Aeronauticas, S.p.A. Model P68, AP68TP 300, AP68TP 600 Airplanes

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

Amdt-39-10182

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Airworthiness Directives; Partenavia Costruzioni Aeronauticas, S.p.A. Models AP68TP 300 ``Spartacus'' and AP68TP 600 ``Viator'' Airplanes

Unsafe Condition: Improper utilization of propeller beta during flight leading to power levers positioned below the flight idle stop, causing loss of airplane control or engine overspeed with consequent loss of engi...

Effective: Dec 5, 1997 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Partenavia Costruzioni Aeronauticas, S.p.A. Models AP68TP 300 ``Spartacus'' and AP68TP 600 ``Viator'' Airplanes

Technical illustration of an aircraft propeller assembly
Problem area Propeller

97-22-10

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Airworthiness Directives; Partenavia Costruzioni Aeronauticas, S.p.A. Models AP68TP 300 "Spartacus" and AP68TP 600 "Viator" Airplanes

Unsafe Condition: Positioning of power levers below the flight idle stop while the airplane is in flight may lead to loss of airplane control or may result in an overspeed condition and consequent loss of engine power.

Effective: Dec 5, 1997 Category: aircraft Compliance: within the next 30 days after the effective date of this AD

Why matched: Airworthiness Directives; Partenavia Costruzioni Aeronauticas, S.p.A. Models AP68TP 300 "Spartacus" and AP68TP 600 "Viator" Airplanes

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