Partenavia Airworthiness Directives

24 ADs indexed for Partenavia aircraft.

Models

Recent ADs

2000-03-18

final rule

Airworthiness Directives; Partenavia Costruzioni Aeronauticas S.p.A. Models AP68TP 300 “Spartacus” and AP68TP 600 “Viator” 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; Partenavia Costruzioni Aeronauticas S.p.A. Models AP68TP 300 Spartacus" and AP68TP 600 "Viator" Airplanes

98-04-20

final rule

Airworthiness Directives; Partenavia Costruzioni Aeronauticas, S.p.A. Model P68, AP68TP 300, AP68TP 600 Airplanes

Unsafe Condition: The absence of adequate information in the Airplane Flight Manual (AFM) to determine when icing conditions exceed certification limits and the lack of procedures to exit such conditions presents an...

Effective: Mar 13, 1998 Category: aircraft

Why matched: Airworthiness Directives; Partenavia Costruzioni Aeronauticas, S.p.A. Model P68, AP68TP 300, AP68TP 600 Airplanes

Amdt-39-10332

final rule

Airworthiness Directives; Partenavia Costruzioni Aeronauticas, S.p.A. Model P68, AP68TP 300, AP68TP 600 Airplanes

Unsafe Condition: Operating in severe icing conditions without clear procedures and limitations may lead to adverse effects on flight control devices and airplane performance.

Effective: Mar 13, 1998 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Partenavia Costruzioni Aeronauticas, S.p.A. Model P68, AP68TP 300, AP68TP 600 Airplanes

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

Amdt-39-10182

final rule

Airworthiness Directives; Partenavia Costruzioni Aeronauticas, S.p.A. Models AP68TP 300 ``Spartacus'' and AP68TP 600 ``Viator'' Airplanes

Unsafe Condition: Improper utilization of propeller beta during flight leading to power levers positioned below the flight idle stop, causing loss of airplane control or engine overspeed with consequent loss of engi...

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

Why matched: Airworthiness Directives; Partenavia Costruzioni Aeronauticas, S.p.A. Models AP68TP 300 ``Spartacus'' and AP68TP 600 ``Viator'' Airplanes

Technical illustration of an aircraft propeller assembly
Problem area Propeller

97-22-10

final rule

Airworthiness Directives; Partenavia Costruzioni Aeronauticas, S.p.A. Models AP68TP 300 "Spartacus" and AP68TP 600 "Viator" 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; Partenavia Costruzioni Aeronauticas, S.p.A. Models AP68TP 300 "Spartacus" and AP68TP 600 "Viator" Airplanes

91-22-06

final rule

Airworthiness Directives; PARTENAVIA P-68 Series (not applicable to AP-68TP Series) airplanes (serial numbers 1 through 327), certificated in any category.

Unsafe Condition: Horizontal stabilator failure, which could result in loss of control of the airplane.

Effective: Nov 12, 1991 Category: aircraft Compliance: Within the next 10 hours time-in-service (TIS) after the effective date of this AD, and within th...

Why matched: Airworthiness Directives; PARTENAVIA P-68 Series (not applicable to AP-68TP Series) airplanes (serial numbers 1 through 327), certificated in any category.

91-11-14

final rule

Airworthiness Directives; PARTENAVIA COSTRUZIONI AERONAUTICHE Models P68C-TC airplanes (all serial numbers (S/N)), P68-OTC airplanes (S/N 344-01-OTC and 340-02-OTC), and P68C and P68 Observer airplanes (S/N 268 to 381), certificated in any category.

Unsafe Condition: Fuel leakage into the airplane cabin that could result in ignition and explosion of the airplane.

Effective: Jun 14, 1991 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; PARTENAVIA COSTRUZIONI AERONAUTICHE Models P68C-TC airplanes (all serial numbers (S/N)), P68-OTC airplanes (S/N 344-01-OTC and 340-02-OTC), and P68C and P68 Observer airplanes (S/N 268 to 381), certificated in any category.

89-03-03

final rule

Airworthiness Directives; Partenavia Model P 68, P 68B, P 68C, P 68TC, P 68 "Observer", and P 68TC "Observer" Series Airplanes

Unsafe Condition: Loss of structural integrity of the engine mounts due to cracks, circumferential scoring, corrosion, or absence of protective coating on the shank of the bolts.

Effective: Feb 16, 1989 Category: aircraft Compliance: within the next 25 hours time-in-service (TIS) after the effective date of this AD, unless alread...

Why matched: Airworthiness Directives; Partenavia Model P 68, P 68B, P 68C, P 68TC, P 68 "Observer", and P 68TC "Observer" Series Airplanes

88-21-04

final rule

Airworthiness Directives; Partenavia Model P 68 Series Airplanes

Unsafe Condition: Pitch instability due to potential damage to left and right stabilator trim tabs and stabilator rear spar.

Effective: Oct 27, 1988 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; Partenavia Model P 68 Series Airplanes

88-13-08

final rule

Airworthiness Directives; Partenavia Model P 68, P 68B, P 68C, P 68C-TC, P 68 "Observer", and P 68-TC "Observer" Series Airplanes

Unsafe Condition: Engine mount failure, whirl mode flutter, and structural failure of the wing.

Effective: Jul 13, 1988 Category: aircraft Compliance: Initially within 6 calendar months after the effective date (July 13, 1988), and thereafter at in...

Why matched: Airworthiness Directives; Partenavia Model P 68, P 68B, P 68C, P 68C-TC, P 68 "Observer", and P 68-TC "Observer" Series Airplanes

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

87-10-12

final rule

Airworthiness Directives; Partenavia Model P 68, P 68B, P 68C Series Airplanes

Unsafe Condition: Cracking of composite leading edge wing ribs and debonding of composite wing leading edge from the ribs, which could lead to possible loss of control and structural failure.

Effective: Jun 1, 1987 Category: aircraft Compliance: Within the next 100 hours time-in-service after the effective date of this AD, and each 100 hours...

Why matched: Airworthiness Directives; Partenavia Model P 68, P 68B, P 68C Series Airplanes

87-04-20

final rule

Airworthiness Directives; Partenavia Models P-68, P-68B, P-68C, P-68C-TC, P68 "OBSERVER" and P68TC "OBSERVER" Series Airplanes

Unsafe Condition: Interference between the brake oil line and aileron control cable could cause loss of braking and/or loss of aileron control.

Effective: Mar 16, 1987 Category: aircraft Compliance: within 50 hours time-in-service (TIS) after the effective date of this AD

Why matched: Airworthiness Directives; Partenavia Models P-68, P-68B, P-68C, P-68C-TC, P68 "OBSERVER" and P68TC "OBSERVER" Series Airplanes

85-08-06

final rule

Airworthiness Directives; Partenavia Model P 68, P 68B, P 68C, P 68C-TC, and P 68 OBSERVER Series Airplanes

Unsafe Condition: Loss of aileron control due to aileron cable chain safety lock failure and wear caused by rubbing against the cable guard plates.

Effective: May 28, 1985 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; Partenavia Model P 68, P 68B, P 68C, P 68C-TC, and P 68 OBSERVER Series Airplanes

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

83-14-03

final rule

Airworthiness Directives; Partenavia Models P68 and P68B Series Airplanes

Unsafe Condition: Failure of the fin rear spar

Effective: Aug 19, 1983 Category: aircraft Compliance: within the next 100 hours after the effective date of this Airworthiness Directive (AD), unless a...

Why matched: Airworthiness Directives; Partenavia Models P68 and P68B Series Airplanes

83-07-22 R1

final rule

Airworthiness Directives; Partenavia Model P-68B, P-68C, and P-68C-TC Series Airplanes

Unsafe Condition: Unintentional return of flaps to the zero degree position due to flap selector switch failure.

Effective: Aug 9, 1983 Category: aircraft Compliance: within the next 100 hours time-in-service

Why matched: Airworthiness Directives; Partenavia Model P-68B, P-68C, and P-68C-TC Series Airplanes

83-15-04

final rule

Airworthiness Directives; Partenavia Model P68, P68B, P68C, P68C-TC and P68 Observer Series Airplanes

Unsafe Condition: Loosening of the stabilator support brackets due to insufficient torque on AN4-6A bolts attaching the horizontal stabilator torque tube support brackets to the fuselage frame.

Effective: Aug 4, 1983 Category: aircraft Compliance: within 50 hours time-in-service from the effective date of this AD

Why matched: Airworthiness Directives; Partenavia Model P68, P68B, P68C, P68C-TC and P68 Observer Series Airplanes

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

83-12-04

final rule

Airworthiness Directives; Partenavia Model P68, P68B, P68C, P68C-TC, and P68 Observer Series Airplanes

Unsafe Condition: Failure of the flap bellcrank attachment mounting brackets due to cracks in the area surrounding the pivot bolt hole.

Effective: Jun 23, 1983 Category: aircraft Compliance: Within the next 100 hours time-in-service from the effective date of this AD, or upon the accumul...

Why matched: Airworthiness Directives; Partenavia Model P68, P68B, P68C, P68C-TC, and P68 Observer Series Airplanes

83-07-17

final rule

Airworthiness Directives; Partenavia Model P68B and P68C Series Airplanes

Unsafe Condition: Failure of the stop tube for the fuel selector control system

Effective: Apr 14, 1983 Category: aircraft Compliance: within the next 100 hours time-in-service after the effective date of this AD

Why matched: Airworthiness Directives; Partenavia Model P68B and P68C Series Airplanes

83-05-07

final rule

Airworthiness Directives; Partenavia Model P68 and P68B Series Airplanes

Unsafe Condition: Failure of the engine oil cooler left-hand elbow fittings and oil cooler hoses

Effective: Mar 17, 1983 Category: aircraft Compliance: Within the next 50 hours time-in-service on airplanes having 500 or more hours time-in-service on...

Why matched: Airworthiness Directives; Partenavia Model P68 and P68B Series Airplanes

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

82-18-11

final rule

Airworthiness Directives; Partenavia Model P68 and P68B Series Airplanes

Unsafe Condition: Failure of the control wheel shaft universal joint due to cracks and interference.

Effective: Sep 13, 1982 Category: aircraft Compliance: Within the next 50 hours time-in-service after the effective date of this AD

Why matched: Airworthiness Directives; Partenavia Model P68 and P68B Series Airplanes

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

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