EADS SOCATA Airworthiness Directives

19 ADs indexed for EADS SOCATA aircraft.

Models

Recent ADs

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

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

2008-03-15

final rule

Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

Unsafe Condition: unsafe condition on an aviation product.

Effective: Mar 11, 2008 Category: aircraft

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

2007-23-07

final rule

Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

Unsafe Condition: Main landing gear wheel attaching nut partly unscrewed due to wheel axle machining issue, leading to loss of braking and potential wheel loss.

Effective: Nov 28, 2007 Category: aircraft Compliance: Before further flight after the effective date of this AD.

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

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

2007-21-10

final rule

Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

Unsafe Condition: Imperfect locking on ground of the upper access door opening interior handle, enabling its opening without actuating the unlocking knob, due to interference between the window trim panel and the ha...

Effective: Nov 21, 2007 Category: aircraft Compliance: Before each flight after November 21, 2007, until the required actions are completed.

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

2007-09-07

final rule

Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

Unsafe Condition: A Nose Landing Gear (NLG) hinge pin rupture that causes an uncommanded NLG retraction, resulting from an incomplete thermal treatment on three hinge pin batches, lowering their mechanical propertie...

Effective: Jun 4, 2007 Category: aircraft Compliance: Within 50 flight hours after the effective date of this AD.

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

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

2007-06-11

final rule

Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

Unsafe Condition: Cracks on a vertical stabilizer attachment fitting due to corrosion have been found on an aircraft in service.

Effective: Apr 20, 2007 Category: aircraft Compliance: Within the next 600 hours time-in-service (TIS) or the next 12 months, whichever occurs first, af...

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

2007-06-14

final rule

Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

Unsafe Condition: Discovery of propeller control cables with defective crimping. Two cable ends were found uncrimped at the factory after an engine run-up test, and one cable end was also found uncrimped on the firs...

Effective: Apr 20, 2007 Category: engine Compliance: Within the next 50 hours time-in-service (TIS) after April 20, 2007 (the effective date of this AD).

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

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2007-06-04

final rule

Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

Unsafe Condition: Fatigue failures of flap carriage rollpins occurred on in-service airplanes.

Effective: Apr 19, 2007 Category: aircraft Compliance: Before further flight

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

2007-05-18

final rule

Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

Unsafe Condition: Improper geometry of some pulley brackets, which can offset the cable in the sheave.

Effective: Apr 12, 2007 Category: aircraft Compliance: Before further flight.

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

2007-04-08

final rule

Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

Unsafe Condition: Incorrect length pilot door locking stop-fittings could result in depressurization of the airplane.

Effective: Mar 23, 2007 Category: aircraft Compliance: Before further flight.

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

2007-04-13

final rule

Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

Unsafe Condition: Cracks found on several main landing gear cylinders.

Effective: Mar 23, 2007 Category: aircraft Compliance: Before further flight.

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

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

2007-03-16

final rule

Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

Unsafe Condition: Excessive lateral play caused by a nonconforming washer that might lead to the deterioration of the elevator trim tab bearing fatigue resistance.

Effective: Mar 15, 2007 Category: aircraft Compliance: Before further flight

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

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

2007-03-17

final rule

Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

Unsafe Condition: Loose rivets on frames C18 BIS and C19, which could result in reduced structural integrity of the tail area.

Effective: Mar 15, 2007 Category: aircraft Compliance: Before further flight

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

2007-02-08

final rule

Airworthiness Directives; EADS SOCATA TBM 700 Airplanes

Unsafe Condition: Report of a master cylinder yoke failure.

Effective: Feb 26, 2007 Category: aircraft Compliance: Before further flight.

Why matched: Airworthiness Directives; EADS SOCATA TBM 700 Airplanes

2006-22-11

final rule

Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes

Unsafe Condition: Unsatisfactory initial elevator trim actuator greasing may lead to the icing of the elevator trim and generate an untrimmed nose-up attitude after an autopilot disconnection.

Effective: Dec 1, 2006 Category: aircraft Compliance: Within 25 hours time-in-service after December 1, 2006.

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

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

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