EADS CASA Airworthiness Directives

89 ADs indexed for EADS CASA aircraft.

Models

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

2014-13-15 Recurring

final rule

Airworthiness Directives; EADS CASA (Type Certificate Previously Held by Construcciones Aeronauticas, S.A.) Airplanes

Unsafe Condition: Reduced thickness of the center fuselage lower skin panel between Frame FR13 and FR21, and from Stringer STR24 LH to STR24 RH, which could result in reduced fatigue and damage tolerant characterist...

Effective: Aug 19, 2014 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; EADS CASA (Type Certificate Previously Held by Construcciones Aeronauticas, S.A.) Airplanes

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

2013-24-09

final rule

Airworthiness Directives; EADS CASA (Type Certificate Previously Held by Construcciones Aeronáuticas, S.A.) Airplanes

Unsafe Condition: Propeller pitch control (PPC) lever becoming disconnected from the engine due to a missing bolt, which fixes the clamp that joins the PPC lever to the PPC rod.

Effective: Jan 21, 2014 Category: engine Compliance: Within 24 months after the effective date of this AD.

Why matched: Airworthiness Directives; EADS CASA (Type Certificate Previously Held by Construcciones Aeron[aacute]uticas, S.A.) Airplanes

2013-23-02

final rule

Airworthiness Directives; EADS CASA (Type Certificate Previously Held by Construcciones Aeronauticas, S.A.) Airplanes

Unsafe Condition: Damage to the feeder cables of certain fuel booster pumps, including signs of electrical arcing and fuel leaks, which could create an ignition source in the fuel tank vapor space, potentially leadi...

Effective: Dec 2, 2013 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; EADS CASA (Type Certificate Previously Held by Construcciones Aeronauticas, S.A.) Airplanes

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

2013-02-12

final rule

Airworthiness Directives; EADS CASA (Type Certificate Previously Held by Construcciones Aeronáuticas, S.A.) Airplanes

Unsafe Condition: Incorrect electrical polarity connections on engine fire extinguishing discharge cartridges could prevent the actuation of the discharge cartridge in case of automatic fire detection or manual init...

Effective: Mar 8, 2013 Category: engine Compliance: Within 30 days after the effective date of this AD.

Why matched: Airworthiness Directives; EADS CASA (Type Certificate Previously Held by Construcciones Aeronáuticas, S.A.) Airplanes

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2012-01-04 Recurring

final rule

Airworthiness Directives; EADS CASA (Type Certificate Previously Held by Construcciones Aeronauticas, S.A.) Airplanes

Unsafe Condition: Failure of the engine condition control cable, specifically part number 35-56382-0003, due to a fracture in the area of the pulley MS 20219-1, caused by an unsuitable ratio between the diameter of ...

Effective: Mar 13, 2012 Category: engine Compliance: Within 9 months or 300 flight hours, whichever occurs first, after the effective date of the AD.

Why matched: Airworthiness Directives; EADS CASA (Type Certificate Previously Held by Construcciones Aeronauticas, S.A.) Airplanes

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

2010-23-05

final rule

Airworthiness Directives; EADS CASA (Type Certificate Previously Held by Construcciones Aeronauticas, S.A.) Model CN-235, CN-235-100, CN-235-200, and CN-235-300 Airplanes, and Model C-295 Airplanes

Unsafe Condition: Failure modes associated with an `unsafe condition' in fuel tank systems, which could lead to an unacceptable probability of ignition risk if specific tasks and/or practices are not performed in ac...

Effective: Dec 10, 2010 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; EADS CASA (Type Certificate Previously Held by Construcciones Aeronauticas, S.A.) Model CN-235, CN-235-100, CN-235-200, and CN-235-300 Airplanes, and Model C-295 Airplanes

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

2009-26-14

final rule

Airworthiness Directives; Construcciones Aeronauticas, S.A. (CASA), Model CN-235, CN-235-100, CN-235-200, and CN-235-300 Airplanes

Unsafe Condition: Fatigue cracking of the rear internal support fittings and longerons of the outer flap structure could result in failure of the outer flaps, and consequent reduced controllability of the airplane.

Effective: Feb 4, 2010 Category: aircraft Compliance: Within 12 months of the effective date (February 4, 2010).

Why matched: Airworthiness Directives; Construcciones Aeronauticas, S.A. (CASA), Model CN-235, CN-235-100, CN-235-200, and CN-235-300 Airplanes

2009-20-10

final rule

Airworthiness Directives; Construcciones Aeronauticas, S.A. (CASA), Model C-212-CB, C-212-CC, C-212-CD, and C-212-CE Airplanes

Unsafe Condition: Failure of the servo-motors, which could result in roll oscillations or possible hard-over failures when the autopilot is engaged.

Effective: Nov 17, 2009 Category: aircraft Compliance: Within 2 months after the effective date of this AD.

Why matched: Airworthiness Directives; Construcciones Aeronauticas, S.A. (CASA), Model C-212-CB, C-212-CC, C-212-CD, and C-212-CE Airplanes

2009-18-06

final rule

Airworthiness Directives; Construcciones Aeronauticas, S.A. (CASA), Model CN-235, CN-235-100, CN-235-200, and CN-235-300 Airplanes

Unsafe Condition: During operation in icing conditions, an asymmetric configuration of the de-icing boots was detected, occurring during the inflation and deflation check of the de-icing system. This was found to be...

Effective: Oct 1, 2009 Category: aircraft Compliance: Within six months after the effective date of this AD.

Why matched: Airworthiness Directives; Construcciones Aeronauticas, S.A. (CASA), Model CN-235, CN-235-100, CN-235-200, and CN-235-300 Airplanes

2009-14-10

final rule

Airworthiness Directives; EADS-PZL “Warszawa-Okęcie” S.A. Model PZL-104 WILGA 80 Airplanes

Unsafe Condition: Severe corrosion of the steel front fuselage structural elements, which if left uncorrected, could lead to loss of strength of the structural front posts elements and consequent reduction of the st...

Effective: Aug 12, 2009 Category: aircraft Compliance: Within 12 years from date of manufacture or within the next 2 months after May 18, 2009, whicheve...

Why matched: Airworthiness Directives; EADS-PZL "Warszawa-Okecie'' S.A. Model PZL-104 WILGA 80 Airplanes

2009-12-04

final rule

Airworthiness Directives; Construcciones Aeronauticas, S.A. (CASA), Model C-212-CB, C-212-CC, C-212-CD, C-212-CE, C-212-CF, and C-212-DE Airplanes

Unsafe Condition: Cracks have been reported in the inner shell of pitot/static pressure heads, supplied by Thales Optronics, which could operate outside their voltage specification. This could lead to incorrect read...

Effective: Jul 16, 2009 Category: aircraft Compliance: Within 1 month or 300 flight hours after the effective date, whichever occurs first.

Why matched: Airworthiness Directives; Construcciones Aeronauticas, S.A. (CASA), Model C-212-CB, C-212-CC, C-212-CD, C-212-CE, C-212-CF, and C- 212-DE Airplanes

2009-08-09

final rule

Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

Unsafe Condition: A damaged wiring harness, resulting from chafed wires due to interference with under-floor attachment fittings of the cabin partition net caused by incorrect routing on the production line, which c...

Effective: May 20, 2009 Category: aircraft Compliance: Within 100 hours time-in-service or 12 months after May 20, 2009, whichever occurs first.

Why matched: Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

2009-09-04

final rule

Airworthiness Directives; EADS-PZL “Warszawa-Okęcie” S.A. Model PZL-104 WILGA 80 Airplanes

Unsafe Condition: Severe corrosion of the steel front fuselage structural elements, which if left uncorrected, could lead to loss of strength of the structural front posts elements and consequent reduction of the st...

Effective: May 18, 2009 Category: aircraft Compliance: Within 12 years from date of manufacture or within the next two months after May 18, 2009, whiche...

Why matched: Airworthiness Directives; EADS-PZL “Warszawa-Okęcie” S.A. Model PZL-104 WILGA 80 Airplanes

2009-02-01

final rule

Airworthiness Directives; Construcciones Aeronauticas, S.A. (CASA), Model C-212-DF Airplanes

Unsafe Condition: Cracks in outer to center wing attachment fittings caused by a defective manufacturing process, which could result in reduced structural integrity of the airplane.

Effective: Mar 9, 2009 Category: aircraft Compliance: Within 10 flight hours

Why matched: Airworthiness Directives; Construcciones Aeronauticas, S.A. (CASA), Model C-212-DF Airplanes

2008-19-10

final rule

Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

Unsafe Condition: A risk of mechanical interference exists in the movement of the emergency landing gear by-pass selector, due to an insufficient functional gap between a floor panel attachment lug and the landing g...

Effective: Oct 23, 2008 Category: aircraft Compliance: Before further flight after the effective date of this AD (October 23, 2008), or within 30 days a...

Why matched: Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

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

2008-19-06

final rule

Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

Unsafe Condition: Rupture of the alternator and vapor cycle cooling system pulley drive assembly, compressor drive shaft, and cracks on the standby-alternator and compressor support.

Effective: Oct 8, 2008 Category: aircraft Compliance: Within 100 flight hours after the effective date of this AD.

Why matched: Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

2008-17-09

final rule

Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

Unsafe Condition: A rupture of the alternator and vapour cycle cooling system pulley drive assembly has reportedly been found. Such a failure could lead to the loss of the alternator and vapour cycle cooling systems...

Effective: Sep 23, 2008 Category: aircraft Compliance: Before further flight if a leak is found; within 12 months of September 23, 2008 for the pulley d...

Why matched: Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

2008-10-13

final rule

Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

Unsafe Condition: unsafe condition on an aviation product.

Effective: May 29, 2008 Category: aircraft

Why matched: Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

2008-06-13

final rule

Airworthiness Directives; Construcciones Aeronauticas, S.A. (CASA), Model C-212 Airplanes

Unsafe Condition: unsafe condition on an aviation product.

Effective: Apr 17, 2008 Category: aircraft

Why matched: Airworthiness Directives; Construcciones Aeronauticas, S.A. (CASA), Model C-212 Airplanes

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