Extra Flugzeugproduktions- und Vertriebs- GmbH Airworthiness Directives

20 ADs indexed for Extra Flugzeugproduktions- und Vertriebs- GmbH aircraft.

Models

Recent ADs

2026-04-12

final rule

Airworthiness Directives; Extra Aerobatic Aircraft GmbH Airplanes

Unsafe Condition: reports of the canopy opening or detaching in flight because of a partially or improperly locked canopy

Effective: Apr 21, 2026 Category: aircraft Compliance: Within 3 months or 25 hours time-in-service, whichever occurs first after the effective date of t...

Why matched: Airworthiness Directives; Extra Aerobatic Aircraft GmbH Airplanes

2022-03-15

final rule

Airworthiness Directives; Various Airplanes

Unsafe Condition: The displayed fuel quantity can have an error as much as four gallons/fuel tank with the display indicating four gallons with an empty tank. In the context of this event, the end level effect is th...

Effective: Mar 21, 2022 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Various Airplanes

Technical illustration of an aircraft fuel pump, filter, valve, and lines
Problem area Fuel system

2010-04-11

final rule

Airworthiness Directives; Extra Flugzeugproduktions- und Vertriebs- GmbH Models EA-300/200 and EA-300/L Airplanes

Unsafe Condition: The combination of a redesigned tail spring support with a stiffer tail spring and rough field operations has led to cracks in the tail spring support mounting base. Cracks have also been reported ...

Effective: Mar 30, 2010 Category: aircraft Compliance: Before further flight after March 30, 2010, and repetitively thereafter at intervals not to excee...

Why matched: Airworthiness Directives; Extra Flugzeugproduktions- und Vertriebs- GmbH Models EA-300/200 and EA-300/L Airplanes

2007-02-11

final rule

Airworthiness Directives; EXTRA Flugzeugproduktions-und Vertriebs-GmbH Models EA-300, EA-300S, EA-300L, and EA-300/200 Airplanes

Unsafe Condition: Cracks in the upper longeron at the horizontal stabilizer attachment could result in structural failure of the aft fuselage, leading to loss of control.

Effective: Feb 28, 2007 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; EXTRA Flugzeugproduktions-und Vertriebs-GmbH Models EA-300, EA-300S, EA-300L, and EA-300/200 Airplanes

Technical illustration of a riveted aircraft structural panel and frame
Problem area Airframe structure

2005-11-07

final rule

Airworthiness Directives; Extra Flugzeugproduktions-und Vertriebs-GmbH Models EA-300, EA-300S, EA-300L, and EA-300/200 Airplanes

Unsafe Condition: Fuel from a leaking gascolator could flow behind the firewall through the non-sealed connections between the firewall and the bottom fuselage cover (belly fairing), potentially resulting in an in-f...

Effective: Jul 18, 2005 Category: aircraft Compliance: Within the next 50 hours time-in-service (TIS) or 3 calendar months after July 18, 2005, whicheve...

Why matched: Airworthiness Directives; Extra Flugzeugproduktions-und Vertriebs-GmbH Models EA-300, EA-300S, EA-300L, and EA-300/200 Airplanes

2005-01-17

final rule

Airworthiness Directives; EXTRA Flugzeugbau GmbH Model EA-300 and EA-300/S Airplanes

Unsafe Condition: Cracks in the upper longeron cutout-bridge could cause the upper longeron cutout-bridge to fail, resulting in structural damage to the fuselage and potentially leading to loss of control of the air...

Effective: Feb 28, 2005 Category: aircraft Compliance: Within 50 flight hours after the effective date of this AD.

Why matched: Airworthiness Directives; EXTRA Flugzeugbau GmbH Model EA-300 and EA-300/S Airplanes

Technical illustration of a riveted aircraft structural panel and frame
Problem area Airframe structure

2005-01-19

final rule

Airworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders

Unsafe Condition: The GTX 33/33D/330/330D Mode S transponders may detect the S1 (suppression) interrogating pulse below the minimum trigger level (MTL) and, in some circumstances, not reply. This could lead to inacc...

Effective: Feb 23, 2005 Category: aircraft Compliance: Within 12 months of the effective date (February 23, 2005).

Why matched: Airworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders

2003-17-02

final rule

Airworthiness Directives; EXTRA Flugzeugbau GmbH Models EA-300/200, EA-300L, and EA-300S Airplanes

Unsafe Condition: Fuel leakage in the wings due to incorrect operation of the fuel selector valve, caused by deterioration of the 'O'-ring in the valve, which could lead to structural damage of the wings and reduced...

Effective: Oct 10, 2003 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; EXTRA Flugzeugbau GmbH Models EA-300/ 200, EA-300L, and EA-300S Airplanes

2002-21-11

final rule

Airworthiness Directives; EXTRA Flugzeugbau GmbH Model EA-300S Airplanes

Unsafe Condition: Fatigue cracks at the horizontal stabilizer attachment, which could result in structural failure of the aft fuselage with consequent loss of control of the airplane.

Effective: Dec 17, 2002 Category: aircraft Compliance: Before further flight for airplanes with less than 200 hours time-in-service; otherwise, within a...

Why matched: Airworthiness Directives; EXTRA Flugzeugbau GmbH Model EA-300S Airplanes

98-24-07

final rule

Airworthiness Directives; EXTRA Flugzeugbau GmbH Models EA-300, EA-300S, and EA-300L Airplanes

Unsafe Condition: Failure of the rudder pedal footrest caused by overloading the rudder pedal safety control stop, which could result in loss of directional control of the airplane.

Effective: Dec 28, 1998 Category: aircraft Compliance: Within the next 50 hours time-in-service after the effective date of this AD (December 28, 1998),...

Why matched: Airworthiness Directives; EXTRA Flugzeugbau GmbH Models EA-300, EA-300S, and EA-300L Airplanes

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

Amdt-39-10893 Recurring

final rule

Airworthiness Directives; EXTRA Flugzeugbau GmbH Models EA-300, EA-300S, and EA-300L Airplanes

Unsafe Condition: Failure of the rudder pedal footrest caused by overloading the rudder pedal safety control stop, which could result in loss of directional control of the airplane.

Effective: Dec 28, 1998 Category: aircraft Compliance: Not specified.

Why matched: Airworthiness Directives; EXTRA Flugzeugbau GmbH Models EA-300, EA-300S, and EA-300L Airplanes

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

Amdt-39-10490

final rule

Airworthiness Directives; EXTRA Flugzeugbau GmbH Models EA-300 and EA-300S Airplanes

Unsafe Condition: Control cable pulling through an incorrectly swaged Nicopress type sleeve, which could result in loss of rudder control with consequent loss of control of the airplane.

Effective: Jun 7, 1998 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; EXTRA Flugzeugbau GmbH Models EA-300 and EA-300S Airplanes

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

98-09-10

final rule

Airworthiness Directives; EXTRA Flugzeugbau GmbH Models EA-300 and EA-300S Airplanes.

Unsafe Condition: A control cable could pull through an incorrectly swaged sleeve, resulting in loss of rudder control with consequent loss of control of the airplane.

Effective: Jun 7, 1998 Category: aircraft Compliance: within the next 100 hours time-in-service after the effective date of this AD

Why matched: Airworthiness Directives; EXTRA Flugzeugbau GmbH Models EA-300 and EA-300S Airplanes.

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

98-06-03

final rule

Airworthiness Directives; EXTRA Flugzeugbau GmbH Model EA-300 Airplanes.

Unsafe Condition: Failure of the elevator mass balance assemblies could cause damage and possible jamming of the airplane’s control system, leading to loss of control.

Effective: Apr 24, 1998 Category: aircraft Compliance: within the next 50 hours time-in-service (TIS) after the effective date of this AD

Why matched: Airworthiness Directives; EXTRA Flugzeugbau GmbH Model EA-300 Airplanes.

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

Amdt-39-10381

final rule

Airworthiness Directives; EXTRA Flugzeugbau GmbH Model EA-300 Airplanes

Unsafe Condition: Damage and possible jamming of the airplane's control system due to insufficiently reinforced elevator mass balance assemblies.

Effective: Apr 24, 1998 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; EXTRA Flugzeugbau GmbH Model EA-300 Airplanes

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

98-04-01

final rule

Airworthiness Directives; EXTRA Flugzeugbau GmbH Model EA-300/S Airplanes

Unsafe Condition: Failure of the canopy while the airplane is in flight because of cracked canopy latches, which could result in loss of the canopy and possible loss of control of the airplane.

Effective: Mar 24, 1998 Category: aircraft Compliance: within the next 100 hours time-in-service (TIS) after the effective date of this AD, unless alrea...

Why matched: Airworthiness Directives; EXTRA Flugzeugbau GmbH Model EA-300/S Airplanes

Amdt-39-10314

final rule

Airworthiness Directives; EXTRA Flugzeugbau GmbH Model EA-300/S Airplanes

Unsafe Condition: Failure of the canopy while the airplane is in flight because of cracked canopy latches, which could result in loss of the canopy and possible loss of control of the airplane.

Effective: Mar 24, 1998 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; EXTRA Flugzeugbau GmbH Model EA-300/S Airplanes

Amdt-39-10307

final rule

Airworthiness Directives; EXTRA Flugzeugbau GmbH Models EA-300 and EA-300/S Airplanes

Unsafe Condition: Cracks in the upper longeron cutout bridge could result in loss of control of the airplane.

Effective: Mar 16, 1998 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; EXTRA Flugzeugbau GmbH Models EA-300 and EA-300/S Airplanes

Technical illustration of a riveted aircraft structural panel and frame
Problem area Airframe structure

Amdt-39-10174

final rule

Airworthiness Directives; Extra Flugzeugbau, GmbH. Model EA-300/ 200 Airplanes

Unsafe Condition: Seat belt falling into the rear rudder pedal controls, interfering with the rudder pedals and causing loss of directional control.

Effective: Nov 24, 1997 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Extra Flugzeugbau, GmbH. Model EA-300/ 200 Airplanes

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

97-22-03

final rule

Airworthiness Directives; Extra Flugzeugbau, GmbH. Model EA-300/200 Airplanes

Unsafe Condition: The pilot’s seat belt may fall into the rear rudder pedal controls, hampering rudder control and possibly causing loss of directional control.

Effective: Nov 24, 1997 Category: aircraft Compliance: within the next 5 hours time-in-service (TIS) after the effective date of this AD, unless already...

Why matched: Airworthiness Directives; Extra Flugzeugbau, GmbH. Model EA-300/200 Airplanes

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

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