Centrair Airworthiness Directives

15 ADs indexed for Centrair aircraft.

Models

Recent ADs

2014-07-08

final rule

Airworthiness Directives; Centrair Gliders

Unsafe Condition: Structural damage to the fuselage, which could lead to reduced structural integrity of the glider.

Effective: May 27, 2014 Category: aircraft Compliance: Within 25 days after May 27, 2014, and repetitively thereafter at intervals not to exceed every 1...

Why matched: Airworthiness Directives; Centrair Gliders

2010-24-10

final rule

Airworthiness Directives; CENTRAIR Models 101, 101A, 101P, and 101AP Gliders

Unsafe Condition: Damages to the rudder bar locking adjustment tube of a non-reinforced version have been reported. In case of tube breaking in flight, it might interfere with the rudder pedals, leading to rudder ja...

Effective: Jan 5, 2011 Category: aircraft Compliance: Within 30 days after January 5, 2011, for inspection. Replacement actions must be completed at th...

Why matched: Airworthiness Directives; CENTRAIR Models 101, 101A, 101P, and 101AP Gliders

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

2005-24-01

final rule

Airworthiness Directives; CENTRAIR 101 Series Gliders

Unsafe Condition: Conflicting information concerning the structural life limit in the Limitations Section of the CENTRAIR Model 101AP glider maintenance manual could lead to non-adherence to the published life limit...

Effective: Jan 3, 2006 Category: aircraft Compliance: Within the next 30 days after January 3, 2006

Why matched: Airworthiness Directives; CENTRAIR 101 Series Gliders

2005-08-12

final rule

Airworthiness Directives; CENTRAIR 101 Series Gliders

Unsafe Condition: Cracks or poorly repaired cracks at the weld seam between the hinge tube and the vertical tube of the rudder pedal could lead to failure of the rudder controls, resulting in loss of directional con...

Effective: Jun 6, 2005 Category: aircraft Compliance: Within the next 25 hours time-in-service (TIS) after June 6, 2005, unless already done.

Why matched: Airworthiness Directives; CENTRAIR 101 Series Gliders

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

2005-08-06

final rule

Airworthiness Directives; CENTRAIR 101 Series Gliders

Unsafe Condition: Incorrectly heat-treated elevator or aileron hinge pins could result in failure of the elevator or ailerons, leading to loss of glider control during takeoff, landing, or flight operations.

Effective: Jun 2, 2005 Category: aircraft Compliance: Within the next 25 hours time-in-service (TIS) after June 2, 2005, unless already done.

Why matched: Airworthiness Directives; CENTRAIR 101 Series Gliders

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

2000-24-22

final rule

Airworthiness Directives; S.N. CENTRAIR Model 201B Gliders

Unsafe Condition: The rear canopy retaining strap may not release properly during the emergency egress procedure due to the current design of the rear canopy emergency release system, potentially preventing the rear...

Effective: Jan 27, 2001 Category: aircraft Compliance: Within the next 3 months after the effective date of this AD (January 27, 2001).

Why matched: Airworthiness Directives; S.N. CENTRAIR Model 201B Gliders

2000-24-23

final rule

Airworthiness Directives; S.N. CENTRAIR 101 Series Gliders

Unsafe Condition: Cracks could occur in the welded parts of airbrake arms, potentially preventing the pilot from using the airbrake system.

Effective: Jan 27, 2001 Category: aircraft Compliance: Within 60 calendar days after January 27, 2001, and then every 12 calendar months for repetitive ...

Why matched: Airworthiness Directives; S.N. CENTRAIR 101 Series Gliders

Amdt-39-11140

final rule

Airworthiness Directives; S.N. CENTRAIR 101 Series Gliders

Unsafe Condition: An unsecured battery discharge warning device could cause elevator flight control interference, potentially leading to reduced or loss of glider control.

Effective: Jun 7, 1999 Category: aircraft Compliance: Before further flight.

99-09-07

final rule

Airworthiness Directives; S.N. CENTRAIR 101 Series Gliders

Unsafe Condition: Elevator flight control interference caused by an unsecured battery discharge warning device, which could result in reduced or loss of glider control.

Effective: Jun 7, 1999 Category: aircraft Compliance: Within the next 3 calendar months after the effective date of this AD (June 7, 1999)

Why matched: Airworthiness Directives; S.N. CENTRAIR 101 Series Gliders

Amdt-39-10755

final rule

Airworthiness Directives; S.N. Centrair 101 Series Sailplanes

Unsafe Condition: Cracks in the original design airbrake control system could result in loss of the airbrake control system.

Effective: Nov 9, 1998 Category: aircraft Compliance: Before further flight

98-19-14

final rule

Airworthiness Directives; S.N. Centrair 101 Series Sailplanes

Unsafe Condition: Cracks in the original design airbrake control system could cause loss of the system, leading to inadvertent forced landing with sailplane damage and/or passenger injury.

Effective: Nov 9, 1998 Category: aircraft Compliance: Within the next 3 calendar months after the effective date of this AD, and thereafter at interval...

Why matched: Airworthiness Directives; S.N. Centrair 101 Series Sailplanes

97-08-06 R1

final rule

Airworthiness Directives; Louis L'Hotellier, S.A., Ball and Swivel Joint Quick Connectors

Unsafe Condition: The L'Hotellier ball and swivel joint quick connectors can become inadvertently disconnected, which could result in loss of control of the sailplane or glider.

Effective: Aug 1, 1997 Category: appliance Compliance: within the next 30 calendar days after the effective date of this AD or upon installation of the ...

Why matched: Airworthiness Directives; Louis L'Hotellier, S.A., Ball and Swivel Joint Quick Connectors

96-02-01

final rule

Airworthiness Directives; S.N. CentrAir Model 201 (all types) Sailplanes

Unsafe Condition: Incorrect fastening of the aileron balancing mass could cause aileron failure and flutter, resulting in loss of control of the sailplane.

Effective: Feb 29, 1996 Category: aircraft Compliance: Required prior to further flight after the effective date of this AD

Why matched: Airworthiness Directives; S.N. CentrAir Model 201 (all types) Sailplanes

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

90-13-11

final rule

Airworthiness Directives S.N. CENTRAIR Model 201B Gliders

Unsafe Condition: Distortion, cracks, or inadequate thickness of the rear cockpit airbrake handle lower arm could result in failure of the airbrake system, compromising flight control.

Effective: Jul 17, 1990 Category: aircraft Compliance: within the next 50 hours time-in-service after the effective date of this AD, unless already acco...

Why matched: Airworthiness Directives S.N. CENTRAIR Model 201B Gliders

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

86-02-04

final rule

Airworthiness Directives; CENTRAIR SAILPLANES Model 101, 101A, 101P and 101AP Gliders

Unsafe Condition: Incorrect installation of the tow release cable guide on the front of the bulkhead could cause unintended release of the tow cable hook during takeoff.

Effective: Jan 14, 1986 Category: aircraft Compliance: within 30 days after the effective date of this AD, unless already accomplished

Why matched: Airworthiness Directives; CENTRAIR SAILPLANES Model 101, 101A, 101P and 101AP Gliders

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

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