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Models

F.260 1 AD F.260B 1 AD F.260C 1 AD F.260D 1 AD F.260E 1 AD F.260F 1 AD S.205 - 18/F 1 AD S.205 - 18/R 1 AD S.205 - 20/F 1 AD S.205 - 20/R 1 AD Dornier 228-100 1 AD Dornier 228-101 1 AD Dornier 228-200 1 AD Dornier 228-201 1 AD Dornier 228-202 1 AD Dornier 228-212 1 AD

Recent ADs

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**

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2021-19-06

final rule

Airworthiness Directives; RUAG Aerospace Services GmbH (Type Certificate Previously Held by Dornier Luftfahrt GmbH) Airplanes

Unsafe Condition: loose bolts and nuts on the landing gear carbon brake assembly

Effective: Oct 15, 2021 Category: aircraft Compliance: before further flight after the effective date of this AD

Why matched: Airworthiness Directives; RUAG Aerospace Services GmbH (Type Certificate Previously Held by Dornier Luftfahrt GmbH) Airplanes

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

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2016-17-05

final rule

Airworthiness Directives; RUAG Aerospace Services GmbH Airplanes

Unsafe Condition: Excessive wear on the guide pin of the power lever or condition lever, which could cause functional loss of the flight idle stop.

Effective: Sep 30, 2016 Category: aircraft Compliance: Within 9,600 flight hours or 9,600 flight cycles, whichever occurs first.

Why matched: Airworthiness Directives; RUAG Aerospace Services GmbH Airplanes

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