Burkhart Grob Luft-Und Airworthiness Directives

51 ADs indexed for Burkhart Grob Luft-Und aircraft.

Models

Recent ADs

2025-20-07 Recurring

final rule

Airworthiness Directives; Fiberglas-Technik Rudolf Lindner GmbH & Co. KG (Type Certificate Previously Held by GROB Aircraft AG, Grob Aerospace GmbH i.l., Grob Aerospace GmbH, Burkhart Grob Luft- und Raumfahrt GmbH & Co. KG) Gliders

Unsafe Condition: Corrosion on the inner sides of the welded steel rudder drive plate could affect the structural integrity of the rudder drive plate and lead to reduced control or loss of control of the glider.

Effective: Oct 17, 2025 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Fiberglas-Technik Rudolf Lindner GmbH & Co. KG (Type Certificate Previously Held by GROB Aircraft AG, Grob Aerospace GmbH i.l., Grob Aerospace GmbH, Burkhart Grob Luft- und Raumfahrt GmbH & Co. KG) Gliders

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

2022-03-08

final rule

Airworthiness Directives; Fiberglas-Technik Rudolf Lindner GmbH & Co. KG (Type Certificate Previously Held by GROB Aircraft AG, Grob Aerospace GmbH i.l., Grob Aerospace GmbH, Burkhart Grob Luft-und Raumfahrt GmbH & Co. KG) Gliders

Unsafe Condition: corrosion on the elevator control pushrod

Effective: Mar 17, 2022 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Fiberglas-Technik Rudolf Lindner GmbH & Co. KG (Type Certificate Previously Held by GROB Aircraft AG, Grob Aerospace GmbH i.l., Grob Aerospace GmbH, Burkhart Grob Luft-und Raumfahrt GmbH & Co. KG) Gliders

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

2012-26-09

final rule

Airworthiness Directives; Burkhart GROB Luft- und Raumfahrt GmbH Sailplanes

Unsafe Condition: Corrosion and/or cracking of the elevator control rod that could lead to failure of the elevator control rod with consequent loss of control.

Effective: Feb 13, 2013 Category: aircraft Compliance: Within 25 hours time-in-service (TIS) or 60 days after February 13, 2013, whichever occurs first,...

Why matched: Airworthiness Directives; Burkhart GROB Luft- und Raumfahrt GmbH Sailplanes

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

2012-10-11

final rule

Airworthiness Directives; Burkhart GROB Luft- und Raumfahrt GmbH Powered Sailplanes

Unsafe Condition: Excessive corrosion on the nose plate (part number 109-2160.01) in the vertical stabilizer, which could cause the vertical stabilizer nose plate to fail and result in loss of control of the sailplane.

Effective: Jul 9, 2012 Category: aircraft Compliance: Within 3 months after July 9, 2012

Why matched: Airworthiness Directives; Burkhart GROB Luft- und Raumfahrt GmbH Powered Sailplanes

2011-09-19

final rule

Airworthiness Directives; BURKHART GROB LUFT-UND Model G 103 C Twin III SL Gliders

Unsafe Condition: The in-flight loss of a propeller and pulley wheel from the engine of a Grob G 103 C Twin III SL powered sailplane has been reported. Grob Aircraft AG suspects that the possible reasons for this lo...

Effective: Jun 15, 2011 Category: aircraft Compliance: Within 30 days after the effective date of this AD (June 15, 2011).

Why matched: Airworthiness Directives; BURKHART GROB LUFT-UND Model G 103 C Twin III SL Gliders

2010-20-06

final rule

Airworthiness Directives; GROB-WERKE (Type Certificate Previously Held by BURKHART GROB Luft- und Raumfahrt) Models G115C, G115D and G115D2 Airplanes

Unsafe Condition: A failed canopy jettison test during maintenance revealed that a cable shroud of the jettison system protruded the canopy structure, potentially causing inability to jettison the canopy in flight.

Effective: Nov 1, 2010 Category: aircraft Compliance: Before further flight after November 1, 2010, for the placard installation and aerobatic flight p...

Why matched: Airworthiness Directives; GROB-WERKE (Type Certificate Previously Held by BURKHART GROB Luft- und Raumfahrt) Models G115C, G115D and G115D2 Airplanes

2009-04-08

final rule

Airworthiness Directives; BURKHART GROB LUFT-UND RAUMFAHRT GmbH & CO KG G103 Series Gliders

Unsafe Condition: A bolt in the airbrake control was found failed due to a double-sided fatigue crack, likely caused by mean stress and excessive bolt torque exceeding the limit.

Effective: Mar 31, 2009 Category: aircraft Compliance: Within 60 days after March 31, 2009

Why matched: Airworthiness Directives; BURKHART GROB LUFT--UND RAUMFAHRT GmbH & CO KG G103 Series Gliders

2006-08-01 Recurring

final rule

Airworthiness Directives; BURKHART GROB LUFT-UND-RAUMFAHRT GmbH & Co. KG, Model G 103 C Twin III SL Sailplanes

Unsafe Condition: Increased play of the propeller bearing and upper pulley wheel.

Effective: May 9, 2006 Category: propeller Compliance: Within 25 engine operating hours after May 9, 2006.

Why matched: Airworthiness Directives; BURKHART GROB LUFT-UND-RAUMFAHRT GmbH & Co. KG, Model G 103 C Twin III SL Sailplanes

2005-26-14

final rule

Airworthiness Directives; BURKHARDT GROB LUFT-UND RAUMFA HRT GmbH & CO KG Model G103 TWIN ASTIR Sailplanes

Unsafe Condition: Cracks in the elevator lever, part number 103-3521, could cause the elevator lever to fail, resulting in loss of control of the sailplane.

Effective: Feb 6, 2006 Category: aircraft Compliance: Within the next 25 hours time-in-service after February 6, 2006.

Why matched: Airworthiness Directives; BURKHARDT GROB LUFT-UND RAUMFAHRT GmbH & CO KG Model G103 TWIN ASTIR Sailplanes

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

2005-26-12

final rule

Airworthiness Directives; BURKHARDT GROB LUFT-UND RAUMFAHRT GmbH & CO KG Models G103 TWIN ASTIR, G103 TWIN II, G103A TWIN II ACRO, G103C TWIN III ACRO, and G 103 C Twin III SL Sailplanes

Unsafe Condition: Cracked center of gravity (CG) release hook attachment brackets could lead to abnormal or uncontrolled sailplane release, resulting in reduced or loss of sailplane control.

Effective: Feb 6, 2006 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; BURKHARDT GROB LUFT-UND RAUMFAHRT GmbH & CO KG Models G103 TWIN ASTIR, G103 TWIN II, G103A TWIN II ACRO, G103C TWIN III ACRO, and G 103 C Twin III SL Sailplanes

2003-19-14 R2

final rule

Airworthiness Directives; BURKHART GROB LUFT--UND RAUMFAHRT GmbH & CO KG Models G103 TWIN ASTIR, G103A TWIN II ACRO, and G103C TWIN III ACRO Sailplanes

Unsafe Condition: Damage to the fuselage during limit load flight could result in reduced structural integrity and loss of control of the sailplane.

Effective: Nov 30, 2005 Category: aircraft Compliance: before November 30, 2005

Why matched: Airworthiness Directives; BURKHART GROB LUFT--UND RAUMFAHRT GmbH & CO KG Models G103 TWIN ASTIR, G103A TWIN II ACRO, and G103C TWIN III ACRO Sailplanes

Amdt-39-14322

final rule

Airworthiness Directives; BURKHART GROB LUFT-UND RAUMFAHRT GmbH & CO KG Models G103 TWIN ASTIR, G103A TWIN II ACRO, and G103C TWIN III ACRO Sailplanes

Unsafe Condition: Damage to the fuselage during limit load flight, which could result in reduced structural integrity and lead to loss of control of the sailplane.

Effective: Nov 30, 2005 Category: aircraft Compliance: Within 12 months of the effective date (November 30, 2005).

Amdt-39-13676

final rule

Airworthiness Directives; BURKHART GROB LUFT-UND RAUMFAHRT GmbH & CO KG Models G103 TWIN ASTIR, G103A TWIN II ACRO, and G103C TWIN III ACRO Sailplanes

Unsafe Condition: The safety margins established in the design of the fuselage may not have been sufficient to sustain limit loads during certain maneuvers and during flight at certain speeds, potentially leading to...

Effective: Aug 12, 2004 Category: aircraft Compliance: Within 12 months of the effective date (August 12, 2004)

2003-19-14

final rule

Airworthiness Directives; Burkhart Grob Luft-und Raumfahrt GmbH & CO KG Models G103 Twin Astir, G103 Twin II, G103A Twin II Acro, and G103C Twin III Acro Sailplanes

Unsafe Condition: The safety margins established into the design of the fuselage may not be sufficient to sustain limit loads during certain maneuvers and during flight at certain speeds, potentially leading to redu...

Effective: Oct 20, 2003 Category: aircraft Compliance: Within 10 hours time-in-service (TIS) after the effective date of this AD.

99-20-11

final rule

Airworthiness Directives; Burkhart Grob Luft - Und Raumfahrt GmbH & CO KG Models G103 TWIN II and G103A TWIN II ACRO Sailplanes

Unsafe Condition: Cracks in the fastening (knurled) nut at the rear control stick could result in loss of control of the sailplane during flight instruction operations because the instructor may lose the ability to ...

Effective: Oct 21, 1999 Category: aircraft Compliance: Within the next 4 calendar months after the effective date of this AD if no cracks are found duri...

Why matched: Airworthiness Directives; Burkhart Grob Luft - Und Raumfahrt GmbH & CO KG Models G103 TWIN II and G103A TWIN II ACRO Sailplanes

Amdt-39-11341

final rule

Airworthiness Directives; Burkhart Grob Luft-Und Raumfahrt GmbH & CO KG Models G103 TWIN II and G103A TWIN II ACRO Sailplanes

Unsafe Condition: Cracks in the fastening (knurled) nut at the rear control stick could lead to the inability to use the rear control stick, potentially resulting in loss of control during flight instruction operati...

Effective: Oct 21, 1999 Category: aircraft Compliance: Within a specified time period if no cracks are found during preflight checks; immediately if cra...

98-24-20

final rule

Airworthiness Directives; Grob Luft-und Raumfahrt, GmbH Models G 109 and G 109B Sailplanes

Unsafe Condition: Fatigue cracking of the landing gear legs could result in landing gear failure with consequent loss of control during landing operations.

Effective: Jan 9, 1999 Category: aircraft Compliance: Within the next 120 calendar days after the effective date of this AD for retaining bars inspecti...

Why matched: Airworthiness Directives; Grob Luft-und Raumfahrt, GmbH Models G 109 and G 109B Sailplanes

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

Amdt-39-10895

final rule

Airworthiness Directives; Burkhart GROB Luft-und Raumfahrt GmbH Model G 109B Gliders

Unsafe Condition: Water penetration into the elevator and trim tab due to inadequate drainage can lead to delamination of the structure, resulting in elevator imbalance and flutter.

Effective: Dec 28, 1998 Category: aircraft Compliance: Before further flight
Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

Amdt-39-10894

final rule

Airworthiness Directives; Burkhart Grob Luft-und Raumfahrt Models G115, G115A, G115B, G115C, G115C2, G115D, and G115D2 Airplanes

Unsafe Condition: Cracks in the elevator trim tab hinges could result in trim tab failure, leading to loss of control of the airplane.

Effective: Dec 28, 1998 Category: aircraft

Why matched: Airworthiness Directives; Burkhart Grob Luft-und Raumfahrt Models G115, G115A, G115B, G115C, G115C2, G115D, and G115D2 Airplanes

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

98-24-08

final rule

Airworthiness Directives; Burkhart Grob Luft-und Raumfahrt Models G115, G115A, G115B, G115C, G115C2, G115D, and G115D2 Airplanes

Unsafe Condition: Cracks in the elevator trim tab hinges could result in trim tab failure with consequent loss of 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 for inspection; prio...

Why matched: Airworthiness Directives; Burkhart Grob Luft-und Raumfahrt Models G115, G115A, G115B, G115C, G115C2, G115D, and G115D2 Airplanes

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

View all Burkhart Grob Luft-Und ADs →