Search FAA Documents

10 results found (4203ms)

Sort by: Date AD Number

2024-12-03

final rule

Airworthiness Directives; CFE Company Engines

Unsafe Condition: Certain HPT stage 1 and HPT stage 2 disks were manufactured from powder metal material suspected to contain iron inclusion, which may cause reduced material properties and a lower fatigue life capa...

Effective: Aug 13, 2024 Category: aircraft Compliance: Within the compliance times specified in the AD: For HPT stage 1 disks, at the next piece-part ex...

Why matched: Airworthiness Directives; CFE Company Engines

2017-08-08

final rule

Airworthiness Directives; CFE Company Turbofan Engines

Unsafe Condition: Quality escape for high-pressure compressor (HPC) impellers made from forgings with nonconforming material grain size, which could lead to uncontained failure of the HPC impeller, damage to the eng...

Effective: May 31, 2017 Category: aircraft Compliance: Within the compliance times specified in the AD, unless already done.

Why matched: Airworthiness Directives; CFE Company Turbofan Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2005-25-15

final rule

Airworthiness Directives; Dassault Model Falcon 2000 Airplanes Equipped With CFE Company CFE738-1-1B Turbofan Engines

Unsafe Condition: Missing spherical bearing on the attachment fitting of the front engine mount, leading to damage and abnormal fatigue of the attachment fitting, which could result in reduced structural integrity o...

Effective: Jan 17, 2006 Category: engine Compliance: Varies based on engine total landings: before 880 total landings for engines with 850 or fewer la...

Why matched: Airworthiness Directives; Dassault Model Falcon 2000 Airplanes Equipped With CFE Company CFE738-1-1B Turbofan Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Amdt-39-12791

final rule

Airworthiness Directives; CFE Company Model CFE738-1-1B Turbofan Engines

Unsafe Condition: Stage 2 high pressure turbine (HPT) aft cooling plate failure, which could result in an uncontained engine failure and damage to the airplane.

Effective: Aug 2, 2002 Category: engine Compliance: Before further flight.

Why matched: Airworthiness Directives; CFE Company Model CFE738-1-1B Turbofan Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

99-27-16 R1

final rule

Airworthiness Directives; CFE Company Model CFE738-1-1B Turbofan Engines

Unsafe Condition: Stage 2 high pressure turbine (HPT) aft cooling plate failure could result in uncontained engine failure and damage to the airplane.

Effective: Aug 2, 2002 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; CFE Company Model CFE738-1-1B Turbofan Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2002-09-10

final rule

Airworthiness Directives; CFE Company Model CFE738-1-1B Turbofan Engines

Unsafe Condition: Failure of the high pressure turbine (HPT) stage 1 aft cooling plate and HPT stage 2 disk, which could result in an uncontained engine failure and damage to the airplane.

Effective: Jun 12, 2002 Category: engine Compliance: Not specified.

Why matched: Airworthiness Directives; CFE Company Model CFE738-1-1B Turbofan Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2001-26-06

final rule

Airworthiness Directives; CFE Company Model CFE738-1-1B Turbofan Engines

Unsafe Condition: Metallurgical inclusions (contaminants) in fan rotor disks part number 3050745-2, serial numbers 000322903511 through 000322903541, could lead to crack initiation and uncontained disk failure, resu...

Effective: Jan 7, 2002 Category: engine Compliance: Before further flight or within specified engine cycle schedules (10, 70, or 140 cycles) after th...

Why matched: Airworthiness Directives; CFE Company Model CFE738-1-1B Turbofan Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2000-23-12

final rule

Airworthiness Directives; CFE Company Model CFE738-1-1B Turbofan Engines

Unsafe Condition: Failure of certain high pressure compressor (HPC) rotor components, which could result in an uncontained engine failure and damage to the airplane.

Effective: Jan 16, 2001 Category: engine Compliance: Required as indicated, unless accomplished previously.

Why matched: Airworthiness Directives; CFE Company Model CFE738-1-1B Turbofan Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2000-21-10

final rule

Airworthiness Directives; CFE Company CFE738-1-1B Turbofan Engines

Unsafe Condition: Loss of seal retention that results in contact between the seal face and the stage 2 high pressure turbine (HPT) rotor disk, leading to wear and subsequent separation of the stage 2 HPT wheel rim, ...

Effective: Nov 8, 2000 Category: aircraft Compliance: Within the specified replacement interval for engines not previously borescope inspected; otherwi...

Why matched: Airworthiness Directives; CFE Company CFE738-1-1B Turbofan Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Amdt-39-11497

final rule

Airworthiness Directives; CFE Company Model CFE738-1-1B Turbofan Engines

Unsafe Condition: Stage 2 high pressure turbine (HPT) aft cooling plates dented during assembly due to raised metal on the Stage 2 HPT disk post aft mating surface, which could lead to cooling plate failure and unco...

Effective: Feb 10, 2000 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; CFE Company Model CFE738-1-1B Turbofan Engines

Technical illustration of an aircraft turbine engine assembly
Problem area Engine