Search FAA Documents

46 results found (1334ms)

Sort by: Date AD Number

2020-19-06

final rule

Airworthiness Directives; McCauley Propeller Systems

Unsafe Condition: The non-conforming idler gear bearing could have also been included in the idler gear assembly (idler gear and bearing), P/N A-20107, or the governor overhaul kit, P/N PL-20233 or PL-20234. The non...

Effective: Nov 3, 2020 Category: propeller Compliance: Before further flight

Why matched: Airworthiness Directives; McCauley Propeller Systems

2010-23-06

final rule

Airworthiness Directives; McCauley Propeller Systems Five-Blade Propeller Assemblies

Unsafe Condition: A cracked propeller hub could cause failure of the propeller hub, blade separation, and loss of control of the airplane.

Effective: Dec 8, 2010 Category: propeller Compliance: Within 250 hours time-in-service after the effective date for hubs exceeding 6,000 hours TSN on t...

Why matched: Airworthiness Directives; McCauley Propeller Systems Five-Blade Propeller Assemblies

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2010-14-20

final rule

Airworthiness Directives; McCauley Propeller Systems Model 4HFR34C653/L106FA Propellers

Unsafe Condition: Reports of 10 hubs found cracked during propeller overhaul indicate a potential failure of the propeller hub, which could cause blade separation, damage to the airplane, and loss of control of the ...

Effective: Aug 17, 2010 Category: propeller Compliance: Within 100 operating hours time-in-service after the effective date for hubs with 6,000 or more o...

Why matched: Airworthiness Directives; McCauley Propeller Systems Model 4HFR34C653/L106FA Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2010-04-05 Recurring

final rule

Airworthiness Directives; McCauley Propeller Systems 1A103/TCM Series Propellers

Unsafe Condition: Propeller hubs found cracked, with cracks beginning at bolt holes and extending to the hub outer surface, leading to potential propeller separation due to hub fatigue cracking.

Effective: Mar 10, 2010 Category: propeller Compliance: Within the compliance times specified in the AD, unless actions have already been performed.

Why matched: Airworthiness Directives; McCauley Propeller Systems 1A103/TCM Series Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2009-19-04 Recurring

final rule

Airworthiness Directives; McCauley Propeller Systems Propeller Models B5JFR36C1101/114GCA-0, C5JFR36C1102/L114GCA-0, B5JFR36C1103/114HCA-0, and C5JFR36C1104/L114HCA-0

Unsafe Condition: Cracks in the propeller blade that could cause failure and separation of the propeller blade and loss of control of the airplane.

Effective: Oct 27, 2009 Category: propeller Compliance: Before further flight for blades with more than 10,000 operating hours TSN. Within a specified ti...

Why matched: Airworthiness Directives; McCauley Propeller Systems Propeller Models B5JFR36C1101/114GCA-0, C5JFR36C1102/L114GCA-0, B5JFR36C1103/ 114HCA-0, and C5JFR36C1104/L114HCA-0

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2008-08-01 Recurring

final rule

Airworthiness Directives; McCauley Propeller Systems Propeller Models B5JFR36C1101/114GCA-0, C5JFR36C1102/L114GCA-0, B5JFR36C1103/114HCA-0, and C5JFR36C1104/L114HCA-0

Unsafe Condition: Cracks in the propeller blades could cause failure and separation, leading to loss of control. Blunt leading edges due to erosion can degrade single engine climb performance and increase the risk o...

Effective: May 19, 2008 Category: engine Compliance: Extended compliance times and intervals are specified, but exact details are not provided in the ...
Technical illustration of an aircraft propeller assembly
Problem area Propeller

2007-08-04 Recurring

final rule

Airworthiness Directives; McCauley Propeller Systems Models 3A32C406/82NDB-X and D3A32C409/82NDB-X Propellers

Unsafe Condition: Stress conditions affecting the fatigue life and damage tolerance of McCauley Propeller Systems models 3A32C406/82NDB-X and D3A32C409/82NDB-X propellers, when installed on Teledyne Continental Moto...

Effective: May 17, 2007 Category: propeller Compliance: Within 12 months of the effective date (May 17, 2007)

Why matched: Airworthiness Directives; McCauley Propeller Systems Models 3A32C406/82NDB-X and D3A32C409/82NDB-X Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2006-15-13

final rule

Airworthiness Directives; McCauley Propeller Systems Propeller Models B5JFR36C1101/114GCA-0, C5JFR36C1102/L114GCA-0, B5JFR36C1103/114HCA-0, and C5JFR36C1104/L114HCA-0

Unsafe Condition: Cracks in the propeller blade retention groove, near the ledge where the split retainers seat and on or near the shot peened surface of the retention groove, could cause failure and separation of t...

Effective: Aug 10, 2006 Category: propeller Compliance: Within 100 operating hours time-in-service after the effective date of the AD, depending on the o...
Technical illustration of an aircraft propeller assembly
Problem area Propeller

2005-24-09

final rule

Airworthiness Directives; McCauley Propeller Systems Propeller Assemblies Models 2D34C53/74E-X; D2A34C58/90AT-X; 3AF32C87/82NC-X; D3AF32C87/82NC-X; D3A32C88/82NC-X; D3A32C90/82NC-X; and 3AF34C92/90LF-X.

Unsafe Condition: Propeller hubs with improperly machined socket retention threads could cause concentrated loading on the threads, resulting in cracking of the hub and blade separation, which could lead to failure ...

Effective: Dec 15, 2005 Category: propeller Compliance: Within 10 flight hours or 10 days after the effective date of this AD, whichever occurs first.

Why matched: Airworthiness Directives; McCauley Propeller Systems Propeller Assemblies Models 2D34C53/74E-X; D2A34C58/90AT-X; 3AF32C87/82NC-X; D3AF32C87/82NC-X; D3A32C88/82NC-X; D3A32C90/82NC-X; and 3AF34C92/90LF- X.

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2005-24-08

final rule

Airworthiness Directives; McCauley Propeller Systems Five-Blade Propeller Assemblies

Unsafe Condition: Cracked propeller hubs, which could cause failure of the propeller hub, blade separation, and loss of control of the airplane.

Effective: Dec 15, 2005 Category: propeller Compliance: Within 50 hours time-in-service after the effective date for hubs exceeding their life limit on t...
Technical illustration of an aircraft propeller assembly
Problem area Propeller

2005-18-20

final rule

Airworthiness Directives; Goodrich De-icing and Specialty Systems “FASTprop” Propeller De-icers

Unsafe Condition: Goodrich De-icing and Specialty Systems 'FASTprop' propeller de-icers becoming loose or debonded, and detaching from propeller blades during operation.

Effective: Oct 14, 2005 Category: propeller Compliance: Before further flight

Why matched: Airworthiness Directives; Goodrich De-icing and Specialty Systems "FASTprop" Propeller De-icers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2005-14-11

final rule

Airworthiness Directives; Hartzell Propeller, Inc., McCauley Propeller Systems, and Sensenich Propeller Manufacturing Company, Inc. Propellers

Unsafe Condition: Failed propeller blade leading to separation and potential loss of control of the airplane.

Effective: Aug 17, 2005 Category: propeller Compliance: Before further flight

Why matched: Airworthiness Directives; Hartzell Propeller, Inc., McCauley Propeller Systems, and Sensenich Propeller Manufacturing Company, Inc. Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2004-23-16

final rule

Airworthiness Directives; McCauley Propeller Systems Five-Blade Propeller Assemblies

Unsafe Condition: Cracked hubs in McCauley Propeller Systems propeller assemblies, which could cause failure of the propeller hub and loss of control of the airplane.

Effective: Dec 7, 2004 Category: propeller Compliance: Within 200 hours TSLI or 30 days after the effective date for propeller assemblies with more than...

Why matched: Airworthiness Directives; McCauley Propeller Systems Five-Blade Propeller Assemblies

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2003-17-10

final rule

Airworthiness Directives; McCauley Propeller Systems, Inc. Propeller Hub Models B5JFR36C1101, C5JFR36C1102, B5JFR36C1103, and C5JFR36C1104; Correction

Unsafe Condition: This document makes a correction to Airworthiness Directive (AD) 2003-17-10. That AD applies to McCauley Propeller Systems, Inc. Propeller Hub Models B5JFR36C1101, C5JFR36C1102, B5JFR36C1103, and C...

Effective: Sep 3, 2003 Category: propeller
Technical illustration of an aircraft propeller assembly
Problem area Propeller

2003-13-17

final rule

Airworthiness Directives; Hartzell Propeller, Inc., McCauley Propeller Systems, Sensenich Propeller Manufacturing Company, Inc., and Raytheon Aircraft Company Propellers

Unsafe Condition: Extensive corrosion in the internal bearing bore of the blade, absence of corrosion protection in the internal bearing bore area, cadmium plating on top of deep corrosion pits, poor cadmium plating...

Effective: Jul 18, 2003 Category: propeller Compliance: Before further flight

Why matched: Airworthiness Directives; Hartzell Propeller, Inc., McCauley Propeller Systems, Sensenich Propeller Manufacturing Company, Inc., and Raytheon Aircraft Company Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2003-15-01

final rule

Airworthiness Directives; McCauley Propeller Systems, Inc. Propeller Hub Models B5JFR36C1101, C5JFR36C1102, B5JFR36C1103, and C5JFR36C1104

Unsafe Condition: A significant crack in a propeller blade shank and two reports of cracks in the hubs of the same propeller model could cause a failure of the propeller blade and loss of control of the airplane.

Effective: Jul 17, 2003 Category: propeller Compliance: Within 50 hours time-in-service (TIS) after the effective date of this AD, depending on the prope...
Technical illustration of an aircraft propeller assembly
Problem area Propeller

2003-12-05 Recurring

final rule

Airworthiness Directives; McCauley Propeller Systems 1A103/TCM Series Propellers

Unsafe Condition: Propeller separation due to hub fatigue cracking, which can result in loss of control of the airplane.

Effective: Jul 17, 2003 Category: propeller Compliance: Within 800 hours TIS or 12 calendar months, depending on the inspection interval.
Technical illustration of an aircraft propeller assembly
Problem area Propeller

2000-15-10 Recurring

final rule

Airworthiness Directives; McCauley Propeller Model 4HFR34C653/L106FA-0

Unsafe Condition: Crack on the camber side of the blade surface, which could cause failure of the propeller blade and result in loss of control of the airplane.

Effective: Aug 23, 2000 Category: propeller Compliance: Within 200 flight hours after the effective date of this AD or within 30 days after the effective...

Why matched: McCauley Propeller Model 4HFR34C653/L106FA-0

Technical illustration of an aircraft propeller assembly
Problem area Propeller

98-25-13

final rule

McCauley Propeller Systems Models 2A36C23/84B-0 and 2A36C82/84B-2 Propellers

Unsafe Condition: Cracks in the propeller blade threaded retention area could progress to blade separation, resulting in loss of aircraft control.

Effective: Jan 4, 1999 Category: propeller Compliance: Compliance is required within the next 200 hours, at the next annual inspection, or within 12 cal...

Why matched: McCauley Propeller Systems Models 2A36C23/84B-0 and 2A36C82/84B-2 Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

Amdt-39-10939

final rule

Airworthiness Directives; McCauley Propeller Systems Models 2A36C23/84B-0 and 2A36C82/84B-2 Propellers

Unsafe Condition: Cracks in the propeller blade threaded retention area may progress to blade separation, which can result in loss of aircraft control.

Effective: Jan 4, 1999 Category: propeller Compliance: Within 100 hours or one calendar month after the effective date of this AD, depending on the prop...

Why matched: Airworthiness Directives; McCauley Propeller Systems Models 2A36C23/84B-0 and 2A36C82/84B-2 Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

Amdt-39-9973 Recurring

final rule

Airworthiness Directives; McCauley Propeller Systems 1A103/TCM Series Propellers

Unsafe Condition: Propeller separation due to hub fatigue cracking

Effective: Apr 24, 1997 Category: propeller Compliance: Before further flight
Technical illustration of an aircraft propeller assembly
Problem area Propeller

95-24-05 R1

final rule

Airworthiness Directives; MCCAULEY ACCESSORY DIVISION, THE CESSNA AIRCRAFT COMPANY Model C35, C72, C74, C75, C80, C86, C87, C92, and C93 series propellers

Unsafe Condition: Propeller blade separation due to a cracked propeller hub, which could result in separation of the engine from the aircraft and subsequent loss of aircraft control.

Effective: Apr 12, 1996 Category: propeller Compliance: Within the next 25 hours time in service (TIS) after December 18, 1995, unless already accomplish...

Why matched: Airworthiness Directives; MCCAULEY ACCESSORY DIVISION, THE CESSNA AIRCRAFT COMPANY Model C35, C72, C74, C75, C80, C86, C87, C92, and C93 series propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

95-09-08

final rule

McCauley Model 2A37C223/90RB Propellers

Unsafe Condition: Cylinder screw failure due to fatigue could result in loss of propeller control and subsequent loss of aircraft control.

Effective: May 19, 1995 Category: propeller Compliance: Within the next 50 hours time in service (TIS), at the next annual inspection, or within 12 calen...

Why matched: McCauley Model 2A37C223/90RB Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

91-15-04

final rule

MCCAULEY ACCESSORY DIVISION, CESSNA AIRCRAFT COMPANY Model ( )2( )34C( )-( ) Series Propellers

Unsafe Condition: Possible blade separation due to cracks in the propeller blade threaded retention area, hub blade socket threads, retention nut threads, or ferrule threads.

Effective: Aug 7, 1991 Category: propeller Compliance: Within the next 100 hours, next annual inspection, or within 12 calendar months after the effecti...

Why matched: MCCAULEY ACCESSORY DIVISION, CESSNA AIRCRAFT COMPANY Model ( )2( )34C( )-( ) Series Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

89-26-10

final rule

McCAULEY ACCESSORY DIVISION Model 1A103/TCM6958 Propellers

Unsafe Condition: Fatigue cracks that can lead to blade separation near the hub, which could subsequently lead to engine separation and loss of aircraft control.

Effective: Jan 31, 1990 Category: propeller Compliance: within the next 100 hours time in service after the effective date of this AD, or before the accu...

Why matched: McCAULEY ACCESSORY DIVISION Model 1A103/TCM6958 Propellers