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2000-03-19 REM

final rule

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Unsafe Condition: Failure to activate the airframe pneumatic deicing boots at the first signs of ice build-up could result in reduced control of the aircraft due to adverse aerodynamic effects of ice adhering to the...

Effective: Jan 2, 2001 Category: aircraft

Why matched: Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

2000-07-11 Recurring

final rule

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Unsafe Condition: Brake hydraulic fluid leakage due to brake assembly rods contacting brake valve tubing, which could result in the inability to adequately stop the airplane during ground operations.

Effective: May 29, 2000 Category: aircraft Compliance: Within 150 hours time-in-service after the effective date

Why matched: Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

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

2000-03-19

final rule

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Unsafe Condition: Reports of in-flight incidents and an accident in icing conditions where the airframe pneumatic deicing boots were not activated, leading to reduced controllability due to ice accumulation.

Effective: Apr 7, 2000 Category: aircraft Compliance: Before further flight.

Why matched: Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

99-11-06

final rule

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Unsafe Condition: Thermal expansion causing leakage of the environmental control system bleed tube due to improper installation, which could result in deterioration of the electrical wiring and surrounding structure.

Effective: Jul 5, 1999 Category: aircraft Compliance: Within 100 hours time-in-service after the effective date

Why matched: Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

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

Amdt-39-11176

final rule

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Unsafe Condition: Improper installation of environmental control system bleed tubes may cause thermal expansion, leading to leakage and potential deterioration of electrical wiring and surrounding structures.

Effective: Jul 5, 1999 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

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

99-07-10

final rule

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Unsafe Condition: The accumulation of loose particles on the engine inlet screen caused by film delamination could result in reduced engine power and possible loss of airplane control.

Effective: May 10, 1999 Category: aircraft Compliance: Within 6 calendar months after the effective date

Why matched: Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Amdt-39-11095

final rule

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Unsafe Condition: Delamination of the inner film on the upper and lower engine nacelle inner panels could lead to the accumulation of loose particles on the engine inlet screen, potentially causing reduced engine po...

Effective: May 10, 1999 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

98-23-14

final rule

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Unsafe Condition: The retaining pins for elevator and aileron controls may be improperly installed or damaged, which could interfere with flight control elements and result in loss of cable retaining function and co...

Effective: Dec 18, 1998 Category: aircraft Compliance: Within the next 100 hours time-in-service after the effective date of this AD (December 18, 1998).

Why matched: Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

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

Amdt-39-10881

final rule

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Unsafe Condition: Improperly installed or damaged elevator and aileron control retaining pins could interfere with flight control elements, leading to loss of cable retaining function and consequent loss of control ...

Effective: Dec 18, 1998 Category: aircraft Compliance: Not specified in the source.

Why matched: Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

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

Amdt-39-10595

final rule

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes.

Unsafe Condition: Water leakage from the lavatory water duct system could collect in the fuselage, freeze in cold weather conditions, and cause the rudder control system to jam.

Effective: Aug 1, 1998 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes.

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

98-13-07

final rule

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes.

Unsafe Condition: Water leakage from the lavatory water duct system could collect in the fuselage, freeze in cold weather conditions, and cause the rudder control system to jam.

Effective: Aug 1, 1998 Category: aircraft Compliance: Within the next 3 calendar months after the effective date of this AD

Why matched: Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes.

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

98-12-13

final rule

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes.

Unsafe Condition: Low pitch stop switch support displacement could result in an improper cockpit indication that the propeller is in the Beta range and cause loss of control of the airplane.

Effective: Jul 18, 1998 Category: aircraft Compliance: within the next 150 hours time-in-service (TIS) after the effective date of this AD, unless alrea...

Why matched: Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes.

Technical illustration of an aircraft propeller assembly
Problem area Propeller

Amdt-39-10569

final rule

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Unsafe Condition: Displacement of the low pitch stop switch support could result in improper cockpit indication that the propeller is in the Beta range and cause loss of control of the airplane.

Effective: Jul 18, 1998 Category: propeller Compliance: Before further flight

Why matched: Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Technical illustration of an aircraft propeller assembly
Problem area Propeller

98-08-05

final rule

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes.

Unsafe Condition: Interference between the main landing gear (MLG) drag brace link and the MLG retraction actuator could cause MLG failure, resulting in loss of control during landing operations.

Effective: May 26, 1998 Category: aircraft Compliance: Within the next 100 hours time-in-service after the effective date of this AD

Why matched: Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes.

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

Amdt-39-10454

final rule

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Unsafe Condition: Interference between the main landing gear (MLG) drag brace link and the MLG retraction actuator could cause MLG failure.

Effective: May 26, 1998 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

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

Amdt-39-10382

final rule

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Unsafe Condition: Pilot difficulty in disengaging the autopilot during flight could result in pilot's lack of proper attention to critical flight tasks due to increased pilot workload and possible loss of airplane c...

Effective: Apr 2, 1998 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

98-06-05

final rule

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Unsafe Condition: Pilot difficulty in disengaging the autopilot during flight could result in increased pilot workload and possible loss of airplane controllability.

Effective: Apr 2, 1998 Category: aircraft Compliance: within the next 10 hours time-in-service (TIS) after the effective date of this AD or within the ...

Why matched: Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

97-22-11

final rule

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Rinaldo Piaggio S.p.A. Model P-180 Airplanes

Unsafe Condition: Positioning of power levers below the flight idle stop while the airplane is in flight may lead to loss of airplane control or may result in an overspeed condition and consequent loss of engine power.

Effective: Dec 5, 1997 Category: aircraft Compliance: within the next 30 days after the effective date of this AD

Why matched: Airworthiness Directives; Industrie Aeronautiche e Meccaniche Rinaldo Piaggio S.p.A. Model P-180 Airplanes

Amdt-39-10183

final rule

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Rinaldo Piaggio S.p.A. Model P-180 Airplanes

Unsafe Condition: Positioning the power levers below the flight idle stop during flight can cause loss of airplane control or engine overspeed with consequent loss of engine power.

Effective: Dec 5, 1997 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Industrie Aeronautiche e Meccaniche Rinaldo Piaggio S.p.A. Model P-180 Airplanes

Amdt-39-10088 Recurring

final rule

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Rinaldo Piaggio S.p.A. Model P-180 Airplanes

Unsafe Condition: Fatigue cracks around the vertical pin and torque tube bottom flange of the rudder, and the fasteners connecting the torque tube to the bottom flange.

Effective: Sep 19, 1997 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Industrie Aeronautiche e Meccaniche Rinaldo Piaggio S.p.A. Model P-180 Airplanes

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

97-15-14

final rule

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Rinaldo Piaggio S.p.A. Model P-180 Airplanes

Unsafe Condition: Fatigue cracks around the vertical pin and the torque tube bottom flange of the rudder, and in the fasteners connecting the torque tube to the bottom flange, which could result in loss of rudder co...

Effective: Sep 19, 1997 Category: aircraft Compliance: Within the next 100 hours time-in-service after the effective date of this AD (September 19, 1997...

Why matched: Airworthiness Directives; Industrie Aeronautiche e Meccaniche Rinaldo Piaggio S.p.A. Model P-180 Airplanes

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

Amdt-39-10072

final rule

Airworthiness Directives; Industrie Aeronautiche E Meccaniche Model Piaggio P-180 Airplanes

Unsafe Condition: Contact between the freon air inlet duct and electrical wiring could result in trim system malfunction, which could result in loss of control of the airplane.

Effective: Aug 29, 1997 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Industrie Aeronautiche E Meccaniche Model Piaggio P-180 Airplanes

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

97-14-14

final rule

Airworthiness Directives; Industrie Aeronautiche E Meccaniche Model Piaggio P-180 Airplanes

Unsafe Condition: Contact between the freon air inlet duct and electrical wiring could cause trim system malfunction, resulting in loss of control of the airplane.

Effective: Aug 29, 1997 Category: aircraft Compliance: within the next 100 hours time-in-service after the effective date of this AD

Why matched: Airworthiness Directives; Industrie Aeronautiche E Meccaniche Model Piaggio P-180 Airplanes

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

96-19-02

final rule

Airworthiness Directives; Industrie Aeronautiche E Meccaniche Model Piaggio P-180 Airplanes

Unsafe Condition: Interference between the passenger seat cushion trim and the emergency exit door handle could prevent the door from opening from the outside during an emergency evacuation, risking passenger injury.

Effective: Oct 28, 1996 Category: aircraft Compliance: within the next 100 hours time-in-service after the effective date of this AD, unless already acc...

Why matched: Airworthiness Directives; Industrie Aeronautiche E Meccaniche Model Piaggio P-180 Airplanes

64-03-04

final rule

Airworthiness Directives; PIAGGIO Model P.166 Aircraft

Unsafe Condition: Fatigue cracks have developed in service on nose landing gear steering control unit part numbers 4105.26 and 4105.31.

Effective: Feb 20, 1964 Category: aircraft Compliance: within the next 50 hours' time in service after the effective date of this AD

Why matched: Airworthiness Directives; PIAGGIO Model P.166 Aircraft

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