{"title":"S10 Airworthiness Directives","description":"","products":[{"product_id":"faa-ad-2018-03-16","title":"S10\/12 FAA AD Front Gear Wheel","description":"\u003cp\u003eDocket No. FAA-2017-0952; Product Identifier 2017-CE-028-AD; Amendment 39-19189; AD 2018-03-16\u003c\/p\u003e\n\u003cp\u003eWe are superseding Airworthiness Directive (AD) 2017-10-11 for Stemme AG Model Stemme S10-VT gliders (type certificate previously held by Stemme GmbH \u0026amp; Co. KG). This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and address an unsafe condition on an aviation product. The MCAI describes the unsafe condition as certain propeller front transmission gear wheels having insufficient material strength because of improper heat treatment during manufacturing. We are issuing this AD to require actions to address the unsafe condition on these products and to add Stemme AG Model Stemme S 12 gliders to the Applicability section.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39763960004704,"sku":"2018-03-16","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/2018-03-16-1.jpg?v=1693508899"},{"product_id":"faa-ad-2012-24-02","title":"S10 FAA AD Hose Inspection","description":"\u003cp\u003eDocket No. FAA-2012-0982; Directorate Identifier 2012-CE-035-AD; Amendment 39-17272; AD 2012-24-02\u003c\/p\u003e\n\u003cp\u003eWe are adopting a new airworthiness directive (AD) for all Stemme GmbH \u0026amp; Co. KG\u003cbr\u003eModels S10, S10-V, and S10-VT powered sailplanes. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as unapproved rubber hoses installed in the engine fuel, oil, and cooling systems, which could lead to a system leak and result in an engine fire. We are issuing this AD to require actions to address the unsafe condition on these products.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39763960135776,"sku":"2012-24-02","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/2012-24-02-1.jpg?v=1693509051"},{"product_id":"faa-ad-2010-11-08","title":"S10 FAA AD Fuel Connector Replacement","description":"\u003cp\u003eDocket No. FAA-2008-0788; Directorate Identifier 2008-CE-039-AD; Amendment 39-16313; AD 2010-11-08]\u003c\/p\u003e\n\u003cp\u003eWe are superseding an existing airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as: AD 2007-0315-E was issued to address a possible fuel leakage in the gear compartment in front of the engine and mandated inspections and replacement of fuel plastic-made connectors by connectors made of metal. Since its publication, another fuel leakage has been reported on a S10-VT which had implemented the STEMME Service Bulletin (SB) A31-10-082 as required by AD 2007-0315-E. It has been determined that the fuel leak may have been caused by the deformation that the originally installed clamps created on the fuel hoses and thus preventing the new clamps from being sufficiently pinched to perform a correct tightening.\u003cbr\u003eWe are issuing this AD to require actions to correct the unsafe condition on these products.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39763960365152,"sku":"2010-11-08","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/2010-11-08-1.jpg?v=1693509189"},{"product_id":"faa-ad-2008-23-05","title":"S10 FAA AD Fuel Leak Inspection","description":"\u003cp\u003eDocket No. FAA-2008-1161; Directorate Identifier 2008-CE-067-AD; Amendment 39-15726; AD 2008-23-05\u003c\/p\u003e\n\u003cp\u003eWe are adopting a new airworthiness directive (AD) for the products listed above. This\u003cbr\u003eAD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as: Investigations performed following a report about a fuel leakage in a Stemme S10-V powered-sailplane revealed that some 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. This AD requires actions that are intended to address the unsafe condition described in the MCAI.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39763960725600,"sku":"2008-23-05","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/2008-23-05-1.jpg?v=1693509319"},{"product_id":"faa-ad-2007-21-09","title":"S10 FAA AD Pressure Sensor Inspection","description":"\u003cp\u003eDocket No. FAA-2007-28958; Directorate Identifier 2007-CE-070-AD; Amendment 39-15227; AD 2007-21-09\u003c\/p\u003e\n\u003cp\u003eWe are adopting a new airworthiness directive (AD) for the products listed above. This\u003cbr\u003eAD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as: As a result of a fault report from a Stemme S10-VT operator, an investigation of the differential fuel pressure sensor 11AB-K01 was performed. The fault report describes a fuel leak through the air pressure line into the airbox. The fuel escaped through the drainage tubes. As a result of this investigation, the possibility of a leak to the engine compartment cannot be excluded. This AD requires actions that are intended to address the unsafe condition described in the MCAI.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39763961184352,"sku":"2007-21-09","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/2007-21-09-1.jpg?v=1693509574"},{"product_id":"faa-ad-2007-15-03","title":"S10 FAA AD Propeller Follower","description":"\u003cp\u003eDocket No. FAA-2007-27431 Directorate Identifier 2007;-016-AD; Amendment 39-15132; AD 2007-15-03\u003c\/p\u003e\n\u003cp\u003eWe are adopting a new airworthiness directive (AD) for the products listed above. This\u003cbr\u003eAD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as: Service experience showed that 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 condition, if not corrected, could lead to high vibration during powered flight and consequently result in decreased control of the aircraft. We are issuing this AD to require actions to correct the unsafe condition on these products\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39763961643104,"sku":"2007-15-03","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/2007-15-03-1.jpg?v=1693509739"},{"product_id":"faa-ad-2007-01-03","title":"S10 FAA AD Evans Coolant","description":"\u003cp\u003eFAA-2006-26518; Directorate Identifier 2006-CE-84-AD; Amendment 39-14874;\u003cbr data-mce-fragment=\"1\"\u003eAD 2007-01-03\u003c\/p\u003e\n\u003cp\u003eWe are adopting a new airworthiness directive (AD) for the products listed above. This\u003cbr\u003eAD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as: During certification works it was found that the cooling liquid EVANS NPG+ is flammable. The liquid cooling circuit of the Stemme S10-VT is not designed to be filled with a flammable liquid without prior modifications. This AD requires actions that are intended to address the unsafe condition described in the MCAI.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39763961872480,"sku":"2007-01-03","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/2007-01-03-1.jpg?v=1693509848"},{"product_id":"faa-ad-2006-26-02","title":"S10 FAA AD Leaking Fuel Connector","description":"\u003cp\u003eFAA-2006-26557; Directorate Identifier 2006-CE-85-AD; Amendment 39-14860; AD 2006-26-02\u003c\/p\u003e\n\u003cp\u003eWe are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as: a leaking brass fuel connection (part no. 10AB-75) was found during maintenance check. This AD requires actions that are intended to address the unsafe condition described in the MCAI.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39763962560608,"sku":"2006-26-02","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/2006-26-02-1.jpg?v=1693510149"},{"product_id":"faa-ad-2006-24-06","title":"S10 FAA AD Ripped Pressure Lines","description":"\u003cp\u003eDocket No. FAA-2006-24956; Directorate Identifier 2006-CE-32-AD; Amendment 39-14835; AD 2006-24-06\u003c\/p\u003e\n\u003cp\u003eWe are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as ripped pressure lines between Airbox-Carburetor-Differential fuel pressure sensor. We are issuing this AD to require actions that are intended to address the unsafe condition described in the MCAI.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39763964723296,"sku":"2006-24-06","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/2006-24-06-1.jpg?v=1693510682"},{"product_id":"faa-ad-2006-19-08","title":"S10 FAA AD Exhaust Inspection","description":"\u003cp\u003eDocket No. FAA-2006-25689; Directorate Identifier 2006-CE-45-AD; Amendment 39-14765; AD 2006-19-08\u003c\/p\u003e\n\u003cp\u003eThe FAA is adopting a new airworthiness directive (AD) for certain Stemme GmbH \u0026amp;\u003cbr\u003eCo. KG Model STEMME S10-VT sailplanes. This AD requires you to do a one-time inspection of all exhaust bends (each cylinder 1 to 4) in the area of the curvature bend near the cylinder flange, replace any damaged exhaust pipes found, and recondition the heat protection wrapping. This AD results from deformations and cracks found at an exhaust bend during maintenance work. We are issuing this AD to detect and correct cracks in the exhaust pipes. Damaged exhaust pipes could cause exhaust gases to expand into the engine compartment and\/or carbon monoxide (CO) to leak into the cockpit section.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39763965378656,"sku":"2006-19-08","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/2006-19-08-1.jpg?v=1693511047"},{"product_id":"faa-ad-2006-17-03","title":"S10 FAA AD Push-Rod Inspection","description":"\u003cp\u003eDocket No. FAA-2006-24641; Directorate Identifier 2006-CE-27-AD; Amendment 39-14724; AD 2006-17-03\u003c\/p\u003e\n\u003cp\u003eThe FAA adopts a new airworthiness directive (AD) for certain Stemme GmbH \u0026amp; Co. KG (Stemme) Models S10, S10-V, and S10-VT sailplanes. This AD requires you to inspect the\u003cbr\u003econnection between the aileron push-rod and the connecting shaft to determine if a safety washer is installed. If there is no safety washer installed, this AD requires you to modify the aileron control assembly. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to prevent a loose bearing in the aileron control lever, which could result in separation of the aileron control system. Separation of the aileron control system could lead to loss of aileron control.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39763965870176,"sku":"2006-17-03","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/2006-17-03-1.jpg?v=1693511182"},{"product_id":"faa-ad-2004-14-21","title":"S10 FAA AD Driveshaft Inspection","description":"\u003cp\u003eDocket No. 2003-CE-58-AD; Amendment 39-13730; AD 2004-14-21\u003c\/p\u003e\n\u003cp\u003eThe FAA adopts a new airworthiness directive (AD) for all Stemme GmbH \u0026amp; Co.\u003cbr\u003eModels S10, S10-V, and S10-VT sailplanes. This AD requires you to remove the drive shaft\u003cbr\u003eassembly and ship it to the service department of Stemme GmbH \u0026amp; Co. The engine is mounted behind the two side-by-side seats. The engine combined with the carbon fiber drive shaft turn the centrifugally extended propeller. After an initial visual inspection, the service department will perform an operational check to determine whether the drive shaft can be further used or must be replaced. Once corrective action is identified, a drive shaft will be shipped to you for installation. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to detect and correct incorrectly glued drive shafts, which could result in drive shaft failure. During self-takeoff or critical periods of landing, failure of the drive shaft could lead to loss of control of the sailplane.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39763977797728,"sku":"2004-14-21","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/2004-14-21-1.jpg?v=1693511431"},{"product_id":"faa-ad-2003-20-09","title":"S10 FAA AD Placard Installation","description":"\u003cp\u003eDocket No. 2003-CE-36-AD; Amendment 39-13327; AD 2003-20-09\u003c\/p\u003e\n\u003cp\u003eThe FAA is adopting a new airworthiness directive (AD) for all Stemme GmbH \u0026amp; Co.\u003cbr\u003eKG Model STEMME S10-VT sailplanes that incorporate a certain gear box. This AD requires you to incorporate flight restrictions into the Limitations Section of the sailplane flight manual and fabricate and install a placard close to the throttle lever indicating these restrictions. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to prevent the potential for the lower cog wheel in the gear box to rupture, which could result in loss of power and possible loss of control of the sailplane.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39763986874464,"sku":"2003-20-09","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/2003-20-09-1.jpg?v=1693511790"},{"product_id":"faa-ad-2003-07-05","title":"S10 FAA AD Firewall Modification","description":"\u003cp\u003eDocket No. 2002-CE-52-AD; Amendment 39-13101; AD 2003-07-05\u003c\/p\u003e\n\u003cp\u003eThis amendment adopts a new airworthiness directive (AD) that applies to all Stemme\u003cbr\u003eGmbH \u0026amp; Co. KG (Stemme) Models S10 and S10-V sailplanes. This AD requires you to modify the engine compartment fuel and oil system and firewall. This AD is the result of FAA's determination that the actions required in AD 2002-22-04 should also be accomplished on other sailplanes of similar type design. The actions specified by this AD are intended to reduce the potential for a fire to ignite in the engine compartment and to increase the containment of an engine fire in the engine compartment. A fire in the engine compartment could lead to loss of control of the sailplane.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39763987595360,"sku":"2003-07-05","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/2003-07-05-1.jpg?v=1693511941"},{"product_id":"faa-ad-2002-22-04","title":"S10 FAA AD Firewall Modification","description":"\u003cp\u003eDocket No. 2002-CE-29-AD; Amendment 39-12928; AD 2002-22-04\u003c\/p\u003e\n\u003cp\u003eThis amendment adopts a new airworthiness directive (AD) that applies to certain\u003cbr\u003eStemme GmbH \u0026amp; Co. KG (Stemme) Model S10-VT sailplanes. This AD requires you to modify the engine compartment fuel and oil system and firewall. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to reduce the potential for a fire to ignite in the engine compartment and increase the containment of an engine fire in the engine compartment. A fire in the engine compartment could lead to loss of control of the sailplane.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39763989430368,"sku":"2002-22-04","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/2002-22-04-1.jpg?v=1693512046"},{"product_id":"faa-ad-2000-26-18","title":"S10 FAA AD Eyebolt Replacement","description":"\u003cp\u003e2000-CE-81-AD | 2000-26-18\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eThis amendment adopts a new airworthiness directive (AD) that applies to certain Stemme\u003cbr\u003eGmbH \u0026amp; Co. KG (Stemme) Models S10 and S10-V sailplanes. This AD requires you to replace the eyebolts on the airbrake, inspect the airbrake sheets for proper clearance and adjust as necessary, and inspect for damage to the landing gear doors and replace any damaged parts. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to prevent aerodynamic flutter of the upper covering straps on the airbrake\u003cbr\u003ecover caused by the current design airbrake eyebolts, which could result in damage to the airbrake system and landing gear doors. Continued operation with such damaged components could result in loss of control of the sailplane.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39764190429280,"sku":"2000-26-18","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/2000-26-18-1.jpg?v=1693571045"},{"product_id":"faa-ad-2000-15-03","title":"S10 FAA AD Propeller Fork Replacement","description":"\u003cp\u003e99-CE-25-AD | 2000-15-03\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eThis amendment adopts a new airworthiness directive (AD) that applies to Stemme GmbH \u0026amp; Co. KG (Stemme) Models S10-V and S10-VT sailplanes. This AD supersedes AD 98-15-24, which currently requires replacing the propeller blade suspension forks with parts of improved design on Stemme S10-V sailplanes. This AD requires you to remove the propeller blade suspension forks, exchange them with the manufacturer for improved design forks, and install the improved design propeller blade suspension forks. This AD is the result of analysis that shows that the existing propeller blade suspension forks are currently cracking more rapidly than originally projected. The actions specified by this AD are intended to prevent certain propeller blade suspension forks from cracking, which could result in the loss of a propeller blade during flight with possible lateral imbalance and loss of thrust.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39764190658656,"sku":"2000-15-03","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/2000-15-03-1.jpg?v=1693571164"},{"product_id":"faa-ad-99-15-03","title":"S10 FAA AD Wastegate Modification","description":"\u003cp\u003e99-CE-07-AD | 99-15-03\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eThis amendment adopts a new airworthiness directive (AD) that applies to certain Stemme\u003cbr\u003eGmbH \u0026amp; Co. KG (Stemme) Model S10-VT sailplanes. This AD requires modifying the wastegate control in order to eliminate heat damage. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to prevent the wastegate control from malfunctioning because of heat damage, which could result in loss of automatic manifold pressure control and engine damage.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39764192526432,"sku":"99-15-03","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/99-15-03-1.jpg?v=1693571345"},{"product_id":"faa-ad-98-24-30","title":"S10 FAA AD Flight Control Inspection","description":"\u003cp\u003e98-CE-106-AD | 98-24-30\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eThis amendment adopts a new airworthiness directive (AD) that applies to certain Stemme\u003cbr\u003eGmbH \u0026amp; Co. KG (Stemme) Models S10, S10-V, and S10-VT sailplanes. This AD requires inspecting certain areas in the flight control system for cracks; immediately replacing any cracked parts; and eventually replacing all longitudinal coupling with modified coupling regardless if found cracked. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to detect and correct cracks in certain areas of the flight control system, which could result in flight control system failure with consequent reduced or loss of\u003cbr\u003econtrol of the sailplane.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39764192559200,"sku":"98-24-30","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/98-24-30-1.jpg?v=1693571460"},{"product_id":"faa-ad-98-24-10","title":"S10 FAA AD Flap Rocker Replacement","description":"\u003cp\u003e98-CE-103-AD | 98-24-10\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eThis amendment adopts a new airworthiness directive (AD) that applies to certain Stemme\u003cbr\u003eGmbH \u0026amp; Co. KG (Stemme) Model S10 sailplanes. This AD requires replacing the flap drive rocker, part number (P\/N) 10SW-RMW, with a modified flap drive rocker. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to prevent failure of the flap drive rocker caused by the design of the original part, which could result in loss of lateral control and wing flap control with consequent reduced and\/or loss of\u003cbr\u003esailplane control.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39764198817888,"sku":"98-24-10","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/98-24-10-1.jpg?v=1693573387"},{"product_id":"faa-ad-98-19-01","title":"S10 FAA AD O-Ring Replacement","description":"\u003cp\u003e93-CE-24-AD | 98-19-01\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eThis amendment adopts a new airworthiness directive (AD) that applies to certain Stemme\u003cbr\u003eGmbH \u0026amp; Co. KG (Stemme) Model S10 sailplanes. This AD requires replacing the O-ring that is installed in the mounting part of the pitot tube (in the propeller dome) with one of improved design. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to prevent failure of the pitot tube O-ring caused by an ineffective design, which could result in the pitot tube falling out and the sailplane pilot losing airspeed\u003cbr\u003eindications.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39764207665248,"sku":"98-19-01","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/98-19-01-1.jpg?v=1693576207"},{"product_id":"faa-ad-98-15-24","title":"S10 FAA AD Propeller Forks","description":"\u003cp\u003e97-CE-128-AD | 98-15-24\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eThis amendment adopts a new airworthiness directive (AD) that applies to certain Stemme\u003cbr\u003eGmbH \u0026amp; Co. KG (Stemme) Model S10-V sailplanes. This AD requires replacing the propeller blade suspension forks with parts of improved design. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to prevent propeller suspension fork failure caused by design deficiency, which could result in loss of a propeller blade and loss of sailplane controllability\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39764207698016,"sku":"98-15-24","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/98-15-24-1.jpg?v=1693576275"},{"product_id":"faa-ad-98-12-06","title":"S10 FAA AD Fuel Filter Replacement","description":"\u003cp\u003e97-CE-129-AD |  98-12-06\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eThis amendment adopts a new airworthiness directive (AD) that applies to certain Stemme\u003cbr\u003eGmbH \u0026amp; Co. KG (Stemme) Models S10 and S10-V sailplanes. This AD requires replacing the fuel filter if it is contaminated, inserting a revision to the Limitations Section of the flight manual, and inspecting the engine valve shafts for brownish-black sticky residue. If a residue is found on the valve shafts, this action will require cleaning the engine. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to prevent engine valve malfunction, which could cause engine failure during flight and loss of control of the sailplane.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39764208484448,"sku":"98-12-06","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/98-12-06-1.jpg?v=1693576672"},{"product_id":"faa-ad-98-08-03","title":"S10 FAA AD Cracked Fittings","description":"\u003cp\u003e97-CE-127-AD | 98-08-03\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eThis amendment adopts a new airworthiness directive (AD) that applies to certain Stemme\u003cbr\u003eGmbH \u0026amp; Co. KG (Stemme) Models S10 and S10-V sailplanes. This AD requires replacing the horizontal stabilizer rear fittings with parts of improved design. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to prevent structural failure of the horizontal stabilizer caused by cracked rear fittings, which could result in loss of sailplane controllability.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39764208615520,"sku":"98-08-03","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/98-08-03-1.jpg?v=1693576751"},{"product_id":"faa-ad-95-17-08","title":"S10 FAA AD Rudder Cable","description":"\u003cp\u003e94-CE-32-AD |  95-17-08\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eThis amendment adopts a new airworthiness directive (AD) that applies to Stemme GmbH\u003cbr\u003e(Stemme) S10 gliders. This action requires modifying the rudder control cable system. Rupture of a turnbuckle eye bolt in the rudder control cable system on one of the affected gliders prompted this action. The actions specified by this AD are intended to prevent rudder control cable system failure caused by rupture of the turnbuckle eye bolt, which, if not detected and corrected, could result in loss of rudder control and eventual loss of control of the glider\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39764208975968,"sku":"95-17-08","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/95-17-08-1.jpg?v=1693577041"},{"product_id":"faa-ad-2023-02-3","title":"S10\/12 FAA AD Superseded","description":"\u003cp\u003eDocket No. FAA-2022-1421; Project Identifier MCAI-2022-01088-G; Amendment\u003cbr data-mce-fragment=\"1\"\u003e39-22310; AD 2023-02-03\u003c\/p\u003e\n\u003cp\u003eThe FAA is superseding Airworthiness Directive (AD) 2022-01-09 for certain Stemme AG Model Stemme S 10-VT and Model Stemme S 12 gliders. AD 2022-01-09 required removing the affected freewheel clutch from service and prohibited the installation of affected parts. Since the FAA issued AD 2022-01-09, the European Union Aviation Safety Agency (EASA) superseded its mandatory continuing airworthiness information (MCAI) to amend the definition of an affected part. This AD retains the requirements of AD 2022-01-09 for removing the affected freewheel clutch from service and continues to prohibit the installation of an affected part, and amends the definition of an affected part and clarifies the part installation prohibition. The FAA is issuing this AD to address the unsafe condition on these products.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39766042771552,"sku":"2023-02-03","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/2023-02-03-1.jpg?v=1693942840"},{"product_id":"easa-ad-2006-0316-r1","title":"S10 EASA AD Valve Tappet","description":"\u003cp\u003eMarch 13, 2008 | 2006-0316 R1\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eIn limited cases, increased wear of camshaft\/hydraulic valve tappet can occur. This may lead to improper engine operation, power loss or in-flight engine failure. To address and correct this problem, BRP-Rotax GmbH \u0026amp; Co. KG issued Alert Service Bulletins ASB-912-051 and ASB-914-034 which describe a special inspection for the affected engines. EASA issued Emergency AD 2006-0316-E to require the inspection of these engines as described in the referenced ASB’s. Since then, BRP-Rotax has introduced hydraulic valve tappet P\/N 854.095 on production engines and P\/N 881.831 as spare part, eliminating the need for these repetitive inspections. Consequently, this AD has been revised to limit the applicability to those engines that do not have this new hydraulic valve tappet installed.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39766615883872,"sku":"2006-03016 R1","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/EASA_AD_2006-0316R1_1-1.jpg?v=1694005599"},{"product_id":"easa-ad-2007-0025","title":"S10 EASA AD Crankcase Cracks","description":"\u003cp\u003eFebruary 1, 2007 | 2007-0025\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eThis Airworthiness Directive (AD) results from reports of cracks in the engine crankcase. Austro Control GmbH (ACG) addressed the problem by issuing AD No 107R3 which was superseded by ACG AD A-2004-01. The present AD supersedes the ACG AD A-2004-01. On one hand, introduction by Rotax of an optimized crankcase assembly has permitted to reduce applicability of the new AD, when based on engines’ serial numbers (s\/n). On the other hand, applicability is extended for some engines that may have been fitted with certain crankcase s\/n, supplied as spare parts.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39766617358432,"sku":"2007-0025","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/EASA_AD_2007-0025_1-1.jpg?v=1694006251"},{"product_id":"easa-ad-2007-0155","title":"S10 EASA AD Coolant Specification","description":"\u003cp\u003eMay 29, 2007 | 2007-0155\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eUnder certain powerplant installation and operating conditions, boiling of conventional coolant with a mixing ratio of 50% coolant and 50% water can occur before reaching maximum permissible cylinder head temperatures (CHT). This can lead to evaporation of the coolant and in consequences to loss of coolant in the coolant system, causing the engine to overheat. This condition, if not corrected could result in engine damage or an accident.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39766617653344,"sku":"2007-0155","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/EASA_AD_2007-0155_1-1.jpg?v=1694006474"},{"product_id":"easa-ad-2009-0149-cn","title":"S10 EASA AD Incorrect Venting","description":"\u003cp\u003eJuly 9, 2009 | 2009-0149-CN\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eTechnical investigation on Austro Control GmbH AD No. 113 R1 demonstrates the subject of incorrect venting not as root cause of the possibility of failure on the engine. Austro Control GmbH AD No. 116 dated 27 August 2003 with subject “Introduction of a new oil dipstick” substitutes the technical content of AD 113 R1. For the reasons described above, Austro Control AD No. 113 R1 is cancelled.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39766617817184,"sku":"2009-0149-CN","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/EASA_AD_2009-0149-CN_1-1.jpg?v=1694006660"},{"product_id":"easa-ad-2011-0082","title":"S10 EASA AD Fuel Regulator Threads","description":"\u003cp\u003eMay 10, 2011 | 2011-0082\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eIsolated manufacturing deviations have been reportedly found on the threads of a certain batch of Fuel pressure Regulators, Part Number (P\/N) 887130, installed on Rotax 914 F series engines. \u003cbr\u003eThis condition, if not corrected, could lead to a fuel leak and in-flight fire which would necessitate an engine shut-down, possibly resulting in a forced landing, with consequent damage to the aeroplane and injury to occupants. For the reasons describe above, this AD requires the replacement of all affected P\/N 887130 Fuel Pressure Regulators with serviceable parts.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39766617915488,"sku":"2011-0082","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/EASA_AD_2011-0082_1-1.jpg?v=1694006773"},{"product_id":"easa-ad-2012-0097r1","title":"S10 EASA AD Fuel Hose Replacement","description":"\u003cp\u003eJune 1, 2012 | 2012-0097R1\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eReports from the field confirmed a non-compliance of pressure side fuel hoses installed on certain P\/N 893114 fuel pumps, which may have resulted in a latent defect on a limited number of engines. The affected fuel hoses may not be fuel resistant in accordance with the specification.\u003cbr\u003eThis condition, if not corrected, could lead to detachment of particles from the fuel hose and irregularities in the carburetor function, possibly resulting in in-flight engine shutdown and forced landing, damage to the aeroplane and injury to occupants.\u003cbr\u003e\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39766618079328,"sku":"2012-0097R1","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/EASA_AD_2012-0097R1_1-1.jpg?v=1694006890"},{"product_id":"easa-ad-2012-0154","title":"S10 EASA AD Fuel Hose Inspection","description":"\u003cp\u003eAugust 17, 2012 | 2012-0154\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eAn occurrence has been reported of an engine fire during ground run of a S10-VT powered sailplane. The investigation results indicated that an unapproved fuel hose was installed in the engine fuel system of that aeroplane. Subsequent survey of some N-registered S 10 aeroplanes revealed more cases of installation of unapproved fuel, oil and cooling hoses on sailplanes engine systems.\u003cbr\u003eThis condition, if not detected and corrected, could lead to a system leak with subsequent engine fire, possibly resulting in damage to the sailplane and\/or injury of occupants.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39766620930144,"sku":"2012-0154","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/EASA_AD_2012-0154_2-1.jpg?v=1694007299"},{"product_id":"easa-ad-2021-0278r1","title":"S10\/12 EASA AD 12AK Clutch","description":"\u003cp\u003eAugust 11, 2022 | 2021-0278R1\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eOccurrences have been reported of unintended slipping of the freewheel clutch (P\/N 12AK) during operation and, subsequently, overheating (burnishing) of the friction pads inside of the clutch. This condition, if not corrected, could lead to total loss of thrust, possibly resulting in loss of control of the powered sailplane. Even after a successful implementation of the recommendations for safe operation of the clutch, published in Stemme AG Service Information P064-8900057\/01, it has been determined that loss of thrust could occur without signs in advance.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39766622371936,"sku":"2021-0278R1","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/EASA_AD_2021-0278R1_1-1.jpg?v=1694007447"},{"product_id":"easa-ad-d-2004-443","title":"S10 EASA AD Loose Bearings","description":"\u003cp\u003eSeptember 27, 2004 | D-2004-443\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eA control lever with a loose bearing was found during the production of the powered sailplane S10. The following inspection of other levers has shown that a bearing may become loose during the operation of the powered sailplane. Except for one connection, all the other connections between push-rods and levers are held in a fork-design that does not allow the joints to disengage due to a loose bearings It is normally possible to find a slack\u003cbr\u003ebearing during the scheduled maintenance of the aircraft. A typical indication for a slack bearing is that it sticks out of its supporting lever. The only joint which may completely disengage due to a loose bearing is the connection between the aileron control rod 10SQ-RMB and the connecting shaft 10SQ-RMW.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39766623256672,"sku":"D-2004-443","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/EASA_AD_D-2004-443_1-1.jpg?v=1694007574"},{"product_id":"easa-ad-d-2005-228","title":"S10 EASA AD Pressure Line Crack","description":"\u003cp\u003eJune 24, 2005 | D-2005-228\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eRipped pressure lines between Airbox-Carburator- Differential fuel pressure sensor were found during a requested maintenance event after engine trouble in the range between maximum continuous power and take off power. The cracks can be a result of non complete temperature resistance. This type of pressure line was installed since July 27, 2004. It was used for serial production and for spare parts\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39766640459872,"sku":"D-2005-228","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/EASA_AD_D-2005-228_1-1.jpg?v=1694007862"},{"product_id":"easa-ad-2006-0311-e","title":"S10 EASA AD Coolant Replacement","description":"\u003cp\u003eOctober 11, 2006 | 2006-0311-E\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eDuring certification works it was found that the cooling liquid EVANS NPG+ is flammable. The liquid cooling circuit of the Stemme S10-VT is not designed to be filled with a flammable liquid without prior modifications. For that reason, this Emergency AD requires the replacement of the EVANS NPG+ cooling liquid. In addition, the operation limit of the cylinder head temperature must be temporary changed to 120°C \/ 248°F.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39766640689248,"sku":"2006-0311-E","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/EASA_EAD_2006-0311-E_1-1.jpg?v=1694007967"},{"product_id":"easa-ad-2007-0191-e","title":"S10 EASA AD Fuel Pressure Sensor","description":"\u003cp\u003eJuly 13, 2007 | 2007-0191-E\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eAs a result of a fault report from a Stemme S10-VT operator, an investigation of the differential fuel pressure sensor 11AB-K01 was performed. The fault report describes a fuel leak through the air pressure line into the airbox. The fuel escaped through the drainage tubes. As a result of this investigation, the possibility of a leak to the engine compartment cannot be excluded.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39766640853088,"sku":"2007-0191-E","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/EASA_EAD_2007-0191-E_1-1.jpg?v=1694008069"},{"product_id":"easa-ad-2007-0315-e","title":"S10 EASA AD Fuel Connector Superseded","description":"\u003cp\u003eDecember 21, 2007 | 2007-0315-E\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eA leakage in the area of a plastic T-connector was found during a daily pre-flight check. The investigation has shown a crack in the center part of this connector.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39766641541216,"sku":"2007-0315-E","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/EASA_EAD_2007-0315-E_1-1.jpg?v=1694008260"},{"product_id":"easa-ad-2008-0053-e","title":"S10 EASA AD Fuel Connector Replacement","description":"\u003cp\u003eMarch 5, 2008 | 2008-0053-E\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eAD 2007-0315-E was issued to address a possible fuel leakage in the gear compartment in front of the engine and mandated inspections and replacement of fuel plastic-made connectors by connectors made of metal. Since its publication, another fuel leakage has been reported on a S10-VT which had implemented the STEMME Service Bulletin (SB) A31-10-082 as required by AD 2007-0315-E.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39766664872032,"sku":"2008-0053-E","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/EASA_EAD_2008-0053-E_1-1.jpg?v=1694008367"},{"product_id":"easa-ad-2011-0222-e","title":"S10 EASA AD Crankshaft Defect Superseded","description":"\u003cp\u003eNovember 15, 2011 | 2011-0222-E\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eDuring a production process review, a deviation in the manufacturing process of certain Part Number (P\/N) 888164 crankshafts has been detected, which may have resulted in a latent defect.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39766674309216,"sku":"2011-0222-E","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/EASA_EAD_2011-0222-E_1-1.jpg?v=1694008468"},{"product_id":"easa-ad-2011-0224-e","title":"S10 EASA AD Crankshaft Cracking","description":"\u003cp\u003eNovember 24, 2011 | 2011-0224-E\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eDuring a production process review, a deviation (double side straightening) in the manufacturing process of certain Part Number (P\/N) 888164 crankshafts has been detected, which may have resulted in cracks on the surface of the crankshaft. Only a few crankshafts are suspected to have received this double side straightening treatment, but it has been impossible to identify these by individual serial number (s\/n). To address this safety concern, BRP-Powertrain issued Alert Service Bulletin ASB-912-059 and ASB-914-042 (single document) with instructions to identify and inspect the entire batch of crankshafts that could be affected. These crankshafts have been installed on a limited number of engines, but some crankshaft sets have also been shipped as spare parts.\u003cbr\u003e\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39766674571360,"sku":"2011-0224-E","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/EASA_EAD_2011-0224-E_1-1.jpg?v=1694008615"},{"product_id":"easa-ad-2012-0019-e","title":"S10 EASA AD Oil Pump Torque","description":"\u003cp\u003eJanuary 26, 2012 | 2012-0019-E\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eDuring a production quality review, a deviation in the assembly process of the oil pump attachment bolts has been detected, which may have resulted in a latent defect on a limited number of engines. The affected bolts may not have been tightened to the correct torque value, i.e. not in accordance with the specification.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39766674604128,"sku":"2012-0019-E","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/EASA_EAD_2012-0019-E_1-1.jpg?v=1694008695"},{"product_id":"easa-ad-2012-0093-e","title":"S10 EASA AD Fuel Pump Superseded","description":"\u003cp\u003eMay 26, 2012 | 2012-0093-E\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eReports from the field confirmed a non-compliance of the installed pressure\u003cbr\u003eside fuel hose part of fuel pump P\/N 893114 which may have resulted in a\u003cbr\u003elatent defect on a limited number of engines. The affected fuel hoses may not\u003cbr\u003ehave been fuel resistant in accordance with the specification.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39766674669664,"sku":"2012-0093-E","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/EASA_EAD_2012-0093-E_1-1.jpg?v=1694008721"},{"product_id":"easa-ad-2013-0055-e","title":"S10 EASA AD Cylinder Inspection Superseded","description":"\u003cp\u003eMarch 6, 2013 |  2013-0055-E\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eDuring a production test run, a non-compliance of the installed cylinder head assembly of cylinder no. 2 and 3 (2\/3) was detected, which may result in a latent defect on a limited number of engines. The affected cylinder heads may not have been manufactured in accordance with the specification.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39766675128416,"sku":"2013-0055-E","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/EASA_EAD_2013-0055-E_1-1.jpg?v=1694008851"},{"product_id":"easa-ad-2013-0117-e","title":"S10 EASA AD Cylinder Head Inspection","description":"\u003cp\u003eMay 30, 2013 | 2013-0117-E\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eDuring a production test run, a non-compliance of the installed cylinder head assembly of cylinder no. 2 and 3 (2\/3) was detected, which may result in a latent defect on a limited number of engines. The affected cylinder heads may not have been manufactured in accordance with the specification.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39766677946464,"sku":"2013-0117-E","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/EASA_EAD_2013-0117-E_1-1.jpg?v=1694008917"},{"product_id":"easa-ad-2017-0072-e","title":"MLG Door Pulley Wheel","description":"\u003cp\u003eApril 26, 2017 | 2017-0072-E\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eIt has been determined that, following improper heat treatment during manufacture, the material strength of an identified batch of propeller front transmission gear wheels is insufficient.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39766678372448,"sku":"2017-0072-E","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/EASA_EAD_2017-0072-E_1-1.jpg?v=1694008980"},{"product_id":"easa-ad-2014-34","title":"EASA AD Engine Temp Limit","description":"\u003cp\u003eDecember 23, 2014 | 2014-34\u003cbr\u003e\u003c\/p\u003e\n\u003cp\u003eThis SIB is issued to alert aircraft Type Certificate (TC) and Supplemental Type Certificate (STC) holders, owners, operators, repair facilities and engineers of possible service difficulties, including engine failures during flight, arising from unnoticed exceedances of approved engine coolant temperature limits due to installation of an unapproved design.\u003c\/p\u003e","brand":"Stemme USA","offers":[{"title":"Default Title","offer_id":39766678536288,"sku":"2014-34","price":2.0,"currency_code":"USD","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0253\/8350\/1920\/files\/EASA_SIB_2014-34_1-1.jpg?v=1694009048"}],"url":"https:\/\/www.stemmeusa.com\/collections\/s10-airworthiness-directives.oembed","provider":"Stemme USA","version":"1.0","type":"link"}