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2022-14-11

final rule

Airworthiness Directives; Stemme AG (Type Certificate Previously Held by Stemme GmbH & Co. KG) Gliders

Unsafe Condition: A deviation in the construction of the connection of the inner wing to the outer wing, resulting in a wrong positioning of the glass-fiber reinforced plastic (GFRP) blocks.

Effective: Jul 26, 2022 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Stemme AG (Type Certificate Previously Held by Stemme GmbH & Co. KG) Gliders

2017-10-11

final rule

Airworthiness Directives; Stemme AG Gliders

Unsafe Condition: Certain propeller front transmission gear wheels have insufficient material strength due to improper heat treatment during manufacturing.

Effective: Jun 15, 2017 Category: propeller Compliance: Before further flight

Why matched: Airworthiness Directives; Stemme AG Gliders

2012-24-02

final rule

Airworthiness Directives; Stemme GmbH & Co. KG Powered Sailplanes

Unsafe Condition: Unapproved rubber hoses installed in the engine fuel, oil, and cooling systems could lead to a system leak and result in an engine fire.

Effective: Jan 7, 2013 Category: engine Compliance: Before further flight after January 7, 2013

Why matched: Airworthiness Directives; Stemme GmbH & Co. KG Powered Sailplanes

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2010-11-08

final rule

Airworthiness Directives; Stemme GmbH & Co. KG Model S10-VT Powered Sailplanes

Unsafe Condition: Fuel leakage in the gear compartment in front of the engine, potentially caused by deformation of fuel hoses by originally installed clamps, preventing new clamps from being sufficiently tightened.

Effective: Jul 6, 2010 Category: aircraft Compliance: Within 12 months of the effective date of the AD.

Why matched: Airworthiness Directives; Stemme GmbH & Co. KG Model S10-VT Powered Sailplanes

2008-23-05

final rule

Airworthiness Directives; Stemme GmbH & Co. KG Models S10 and S10-V Gliders

Unsafe Condition: Fuel lines fabricated between March 2008 and May 2008, after the introduction of a new pressing tool, present a manufacturing defect which could lead to the puncture of the fuel lines.

Effective: Nov 26, 2008 Category: aircraft Compliance: Before further flight if leakage is found or within 25 days after the effective date of this AD.

Why matched: Airworthiness Directives; Stemme GmbH & Co. KG Models S10 and S10-V Gliders

2008-11-20

final rule

Airworthiness Directives; Stemme GmbH & Co. KG Model S10-VT Powered Sailplanes

Unsafe Condition: unsafe condition on an aviation product.

Effective: Jun 23, 2008 Category: aircraft

Why matched: Airworthiness Directives; Stemme GmbH & Co. KG Model S10-VT Powered Sailplanes

2008-03-06

final rule

Airworthiness Directives; Stemme GmbH & Co. KG Model S10-VT Powered Sailplanes

Unsafe Condition: unsafe condition on an aviation product.

Effective: Feb 20, 2008 Category: aircraft

Why matched: Airworthiness Directives; Stemme GmbH & Co. KG Model S10-VT Powered Sailplanes

2007-21-09

final rule

Airworthiness Directives; Stemme GmbH & Co. KG Model S10-VT Gliders

Unsafe Condition: Fuel leak through the air pressure line into the airbox, with fuel escaping through the drainage tubes. The possibility of a leak to the engine compartment cannot be excluded.

Effective: Nov 1, 2007 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Stemme GmbH & Co. KG Model S10-VT Gliders

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

2007-15-03

final rule

Airworthiness Directives; Stemme GmbH & Co. KG Model S10-V and S10-VT Powered Sailplanes

Unsafe Condition: The connection screw of the propeller blade follower type 10AP-VM may break, and the main part of the blade follower can be lost in flight. This could lead to high vibration during powered flight a...

Effective: Aug 28, 2007 Category: aircraft Compliance: Within 25 engine operating hours or 90 days after August 28, 2007, whichever occurs first.

Why matched: Airworthiness Directives; Stemme GmbH & Co. KG Model S10-V and S10-VT Powered Sailplanes

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2007-01-03

final rule

Airworthiness Directives; Stemme GmbH & Co. KG Model S10-VT Gliders

Unsafe Condition: unsafe condition on an aviation product.

Effective: Jan 29, 2007 Category: aircraft

Why matched: Airworthiness Directives; Stemme GmbH & Co. KG Model S10-VT Gliders

2006-26-02

final rule

Airworthiness Directives; Stemme GmbH & Co. KG Model S10, S10-V, and S10-VT Gliders

Unsafe Condition: A leaking brass fuel connection (part no. 10AB-75) was found during maintenance check.

Effective: Jan 10, 2007 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Stemme GmbH & Co. KG Model S10, S10-V, and S10-VT Gliders

2006-24-06

final rule

Airworthiness Directives; Stemme GmbH & Co. AG Model STEMME S10-VT Sailplanes

Unsafe Condition: Ripped pressure lines between Airbox-Carburetor-Differential fuel pressure sensor, potentially caused by incomplete temperature resistance.

Effective: Jan 3, 2007 Category: aircraft Compliance: Within 30 days after the effective date of this AD.

Why matched: Airworthiness Directives; Stemme GmbH & Co. AG Model STEMME S10- VT Sailplanes

2006-19-08

final rule

Airworthiness Directives; Stemme GmbH & Co. KG Model STEMME S10-VT Sailplanes

Unsafe Condition: Deformations and cracks found at an exhaust bend during maintenance work, specifically in the curvature bend near the cylinder flange.

Effective: Oct 10, 2006 Category: engine Compliance: Within the next 10 hours time-in-service after October 10, 2006.

Why matched: Airworthiness Directives; Stemme GmbH & Co. KG Model STEMME S10- VT Sailplanes

2006-17-03

final rule

Airworthiness Directives; Stemme GmbH & Co. KG Models S10, S10-V, and S10-VT Sailplanes

Unsafe Condition: A loose bearing in the aileron control lever, which could result in separation of the aileron control system, leading to loss of aileron control.

Effective: Sep 22, 2006 Category: aircraft Compliance: Within the next 20 hours time-in-service after September 22, 2006.

Why matched: Airworthiness Directives; Stemme GmbH & Co. KG Models S10, S10-V, and S10-VT Sailplanes

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

2004-14-21

final rule

Airworthiness Directives; Stemme GmbH & Co. Models S10, S10-V, and S10-VT Sailplanes

Unsafe Condition: Incorrectly glued drive shafts, which could result in drive shaft failure. This failure could lead to loss of control of the sailplane.

Effective: Aug 21, 2004 Category: engine Compliance: Within 50 hours time-in-service after August 21, 2004.

Why matched: Airworthiness Directives; Stemme GmbH & Co. Models S10, S10-V, and S10-VT Sailplanes

2003-20-09

final rule

Airworthiness Directives; Stemme GmbH & Co. KG Model STEMME S10-VT Sailplanes

Unsafe Condition: The lower cog wheel in the gear box may rupture, which could result in loss of power and possible loss of control of the sailplane.

Effective: Oct 20, 2003 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Stemme GmbH & Co. KG Model STEMME S10-VT Sailplanes

2003-07-05

final rule

Airworthiness Directives; Stemme GmbH & Co. KG Models S10 and S10-V Sailplanes

Unsafe Condition: Potential for a fire to ignite in the engine compartment and propagate, leading to loss of control of the sailplane.

Effective: May 22, 2003 Category: engine Compliance: Not specified.

Why matched: Airworthiness Directives; Stemme GmbH & Co. KG Models S10 and S10-V Sailplanes

2002-22-04

final rule

Airworthiness Directives; Stemme GmbH & Co. KG Model S10-VT Sailplanes

Unsafe Condition: An in-flight fire incident revealed that the fire was not contained in the engine compartment, leading to a potential for a fire to ignite and spread into the cockpit, which could result in loss of...

Effective: Dec 20, 2002 Category: engine Compliance: Within the next 50 hours time-in-service (TIS) or 3 months after the effective date of this AD, w...

Why matched: Airworthiness Directives; Stemme GmbH & Co. KG Model S10-VT Sailplanes

2000-26-18

final rule

Airworthiness Directives; Stemme GmbH & Co. KG Models S10 and S10-V Sailplanes

Unsafe Condition: Current design airbrake eyebolts could cause aerodynamic flutter of the upper airbrake straps at high airspeeds, leading to damage to the airbrake system and landing gear doors.

Effective: Feb 2, 2001 Category: aircraft Compliance: Within the next 5 flight hours or 30 days, whichever occurs first.

Why matched: Airworthiness Directives; Stemme GmbH & Co. KG Models S10 and S10-V Sailplanes

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

2000-15-03

final rule

Airworthiness Directives; Stemme GmbH & Co. KG Models S10-V and S10-VT Sailplanes

Unsafe Condition: The existing propeller blade suspension forks are cracking more rapidly than originally projected, which could result in the loss of a propeller blade during flight with possible lateral imbalance ...

Effective: Aug 4, 2000 Category: propeller Compliance: Before further flight

Why matched: Airworthiness Directives; Stemme GmbH & Co. KG Models S10-V and S10-VT Sailplanes

Technical illustration of an aircraft propeller assembly
Problem area Propeller

Amdt-39-11222

final rule

Airworthiness Directives; Stemme GmbH & Co. KG Model S10-VT Sailplanes

Unsafe Condition: Heat damage to the wastegate control could result in loss of automatic manifold pressure control and engine damage.

Effective: Aug 31, 1999 Category: engine Compliance: Before further flight.

99-15-03

final rule

Airworthiness Directives; Stemme GmbH & Co. KG Model S10-VT Sailplanes

Unsafe Condition: Heat damage to the wastegate control could result in loss of automatic manifold pressure control and engine damage.

Effective: Aug 31, 1999 Category: aircraft Compliance: Within the next 3 calendar months after the effective date of this AD

Why matched: Airworthiness Directives; Stemme GmbH & Co. KG Model S10-VT Sailplanes

Amdt-39-10917

final rule

Airworthiness Directives; Stemme GmbH & Co. KG Models S10, S10-V, and S10-VT Sailplanes

Unsafe Condition: Cracks in certain areas of the flight control system could result in flight control system failure, leading to reduced or loss of control of the sailplane.

Effective: Dec 18, 1998 Category: aircraft Compliance: Before further flight
Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

98-24-30

final rule

Airworthiness Directives; Stemme GmbH & Co. KG Models S10, S10-V, and S10-VT Sailplanes

Unsafe Condition: Cracks in the flight control longitudinal coupling, wing flap coupling (P/N 10SW-RVW), airbrake control coupling (P/N 10SB-RVW), flap drive rocker (P/N 10SW-RMW), and flap/aileron interference shaf...

Effective: Dec 18, 1998 Category: aircraft Compliance: Compliance required by whichever occurs first: 6 calendar months or 100 hours time-in-service.

Why matched: Airworthiness Directives; Stemme GmbH & Co. KG Models S10, S10-V, and S10-VT Sailplanes

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

98-24-10

final rule

Airworthiness Directives; Stemme GmbH & Co. KG Model S10 Sailplanes

Unsafe Condition: Failure of the flap drive rocker caused by fatigue due to the design of part number 10SW-RMW, which could result in loss of lateral control and wing flap control with consequent reduced or loss of ...

Effective: Dec 9, 1998 Category: aircraft Compliance: Prior to further flight after the effective date of this AD (December 9, 1998).

Why matched: Airworthiness Directives; Stemme GmbH & Co. KG Model S10 Sailplanes