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2016-05-04

final rule

Airworthiness Directives; Dowty Propellers Constant Speed Propellers

Unsafe Condition: Reports of dowel hole cracks in the face of the rear hub half.

Effective: Apr 15, 2016 Category: propeller Compliance: At the next removal of the propeller from the airplane, after the effective date of this AD.

Why matched: Airworthiness Directives; Dowty Propellers Constant Speed Propellers

Amdt-39-18007 Recurring

final rule

Airworthiness Directives; Dowty Propellers Constant Speed Propellers

Unsafe Condition: Failure of the propeller de-ice bus bar due to friction or contact between the bus bar and the backplate assembly, consequent intermittent short circuit, and possible double generator failure.

Effective: Jan 6, 2015 Category: propeller Compliance: Within 5,000 flight-hours after September 27, 2010, or within 100 flight-hours after the effectiv...

2010-17-11R2

final rule

Airworthiness Directives; Dowty Propellers Constant Speed Propellers

Unsafe Condition: Failure of the propeller de-ice bus bar due to friction or contact between the bus bar and the backplate assembly, consequent intermittent short circuit, and possible double generator failure.

Effective: Jan 6, 2015 Category: propeller Compliance: before further flight

Why matched: Airworthiness Directives; Dowty Propellers Constant Speed Propellers

2008-21-07R1

final rule

Airworthiness Directives; Dowty Propellers Propellers

Unsafe Condition: Loss of the bonded metallic leading edge (L/E) guard of the propeller, which could result in damage to the propeller or to the airplane, or injury to personnel.

Effective: Jul 15, 2014 Category: propeller Compliance: Effective July 15, 2014.

Why matched: Airworthiness Directives; Dowty Propellers Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

Amdt-39-17831 Recurring

final rule

Airworthiness Directives; Dowty Propellers Propellers

Unsafe Condition: The loss of the bonded metallic leading edge (L/E) guard of the propeller, which could result in damage to the propeller or to the airplane, or injury to personnel.

Effective: Jul 15, 2014 Category: propeller Compliance: Within the next 50 flight hours (FH) or within 30 days after the effective date of this AD, which...
Technical illustration of an aircraft propeller assembly
Problem area Propeller

Amdt-39-17481 Recurring

final rule

Airworthiness Directives; Dowty Propellers Propellers

Unsafe Condition: In-flight double generator failure, which could result in reduced control of the airplane.

Effective: Aug 14, 2013 Category: aircraft Compliance: Within 5,000 flight hours after September 27, 2010, or within 100 flight hours from the effective...
Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

2011-19-02

final rule

Airworthiness Directives; Dowty Propellers Type R212/4-30-4/22 and R251/4-30-4/49 Propeller Assemblies

Unsafe Condition: Reports of cracks in the propeller hub port buttress threads of R212 and R251 propellers, affecting hubs with over 6,000 flight hours. This could lead to propeller blade separation, potentially cau...

Effective: Nov 9, 2011 Category: propeller Compliance: Within 500 flight hours after the effective date

Why matched: Airworthiness Directives; Dowty Propellers Type R212/4-30-4/22 and R251/4-30-4/49 Propeller Assemblies

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2005-25-10R1

final rule

Airworthiness Directives; Dowty Propellers Type R321/4-82-F/8, R324/4-82-F/9, R333/4-82-F/12, and R334/4-82-F/13 Propeller Assemblies

Unsafe Condition: Propeller hub failure due to cracks in the hub, which could result in loss of control of the airplane.

Effective: Oct 11, 2011 Category: propeller Compliance: Effective October 11, 2011.

Why matched: Airworthiness Directives; Dowty Propellers Type R321/4-82-F/8, R324/4-82-F/9, R333/4-82-F/12, and R334/4-82-F/13 Propeller Assemblies

Technical illustration of an aircraft propeller assembly
Problem area Propeller

Amdt-39-16788 Recurring

final rule

Airworthiness Directives; Dowty Propellers Type R321/4-82-F/8, R324/4-82-F/9, R333/4-82-F/12, and R334/4-82-F/13 Propeller Assemblies

Unsafe Condition: Propeller hub failure due to cracks in the hub, which could result in loss of control of the airplane.

Effective: Oct 11, 2011 Category: propeller Compliance: Within the compliance times specified in Table 1 of the AD, unless already done.
Technical illustration of an aircraft propeller assembly
Problem area Propeller

2010-17-11

final rule

Airworthiness Directives; Dowty Propellers R408/6-123-F/17 Model Propellers

Unsafe Condition: Friction or contact between a propeller de-ice bus bar and the backplate assembly can cause failure of the bus bar and a consequent intermittent short circuit. Such a short circuit can cause a dual...

Effective: Sep 27, 2010 Category: aircraft Compliance: Within 5,000 flight hours after the effective date for initial sealant application, and every add...

Why matched: Airworthiness Directives; Dowty Propellers R408/6-123-F/17 Model Propellers

2010-10-23

final rule

Airworthiness Directives; Dowty Propellers R175/4-30-4/13; R175/4-30-4/13e; R184/4-30-4/50; R193/4-30-4/50; R193/4-30-4/61; R193/4-30-4/64; R193/4-30-4/65; R193/4-30-4/66; R.209/4-40-4.5/2; R212/4-30-4/22; R.245/4-40-4.5/13; R257/4-30-4/60; and R.259/4-40-4.5/17 Model Propellers

Unsafe Condition: could result in reduced controllability of the airplane.

Effective: Jun 25, 2010 Category: propeller

Why matched: Airworthiness Directives; Dowty Propellers R175/4-30-4/13; R175/ 4-30-4/13e; R184/4-30-4/50; R193/4-30- 4/50; R193/4-30-4/61; R193/4-30- 4/64; R193/4-30-4/65; R193/4-30-4/66; R.209/4-40-4.5/2; R212/4-30-4/22; R.245/4-40-4.5/13; R257/4-30-4/60; and R.259/4-40-4.5/17 Model Propellers

2010-05-09

final rule

Airworthiness Directives; Dowty Propellers Models R354/4-123-F/13, R354/4-123-F/20, R375/4-123-F/21, R389/4-123-F/25, R389/4-123-F/26, and R390/4-123-F/27 Propellers

Unsafe Condition: A number of propeller blade outer sleeves have been found with cracks since 1996. Testing has shown that blade retention integrity is not affected by this cracking. However, this condition, if not ...

Effective: Apr 7, 2010 Category: aircraft Compliance: Within 1,600 flight hours after the effective date or after any blade accumulates 15,000 flight h...

Why matched: Airworthiness Directives; Dowty Propellers Models R354/4-123-F/ 13, R354/4-123-F/20, R375/4-123-F/21, R389/4-123-F/25, R389/4-123-F/26, and R390/4-123-F/27 Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2008-21-07 Recurring

final rule

Airworthiness Directives; Dowty Propellers R408 Series Propellers

Unsafe Condition: Three in-service propellers have been found to have blades which have lost the bonded metallic leading edge guard. If the leading edge guard comes off as the propeller turns, it could cause seconda...

Effective: Oct 31, 2008 Category: propeller Compliance: Within 50 flight hours or within 1 month after the effective date of this AD, whichever occurs fi...

Why matched: Airworthiness Directives; Dowty Propellers R408 Series Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2006-23-10

final rule

Airworthiness Directives; Dowty Propellers R321/4-82-F/8; R324/4-82-F/9; R333/4-82-F/12; and R334/4-82-F/13 Propellers

Unsafe Condition: One propeller blade has been identified where the blade counterweight capscrew holes have not been correctly drilled. If the capscrew holes are not machined to their required depth, the counterweig...

Effective: Nov 24, 2006 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Dowty Propellers R321/4-82-F/8; R324/4- 82-F/9; R333/4-82-F/12; and R334/4-82-F/13 Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2005-25-10 Recurring

final rule

Airworthiness Directives; Dowty Propellers Type R321/4-82-F/8, R324/4-82-F/9, R333/4-82-F/12, and R334/4-82-F/13 Propeller Assemblies

Unsafe Condition: Propeller hub failure due to cracks in the hub, which could result in loss of control of the airplane.

Effective: Dec 27, 2005 Category: propeller Compliance: Within 10 flight hours or 20 days for Type R334/4-82-F/13, and within 50 flight hours or 60 days ...
Technical illustration of an aircraft propeller assembly
Problem area Propeller

2003-04-25

final rule

Airworthiness Directives; Dowty Aerospace Propellers, Models R354, R375, R389, and R390 Propellers

Unsafe Condition: Fretting on the joint mating faces of propeller hubs could lead to failure of the hub due to loose hub through bolts.

Effective: Apr 8, 2003 Category: propeller Compliance: Within 50 flight hours after the effective date of this AD.

Why matched: Airworthiness Directives; Dowty Aerospace Propellers, Models R354, R375, R389, and R390 Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

99-18-18 R1

final rule

Airworthiness Directives; Dowty Aerospace Propellers Model R381/6-123-F/5 Propellers

Unsafe Condition: Propeller blade cracks and propagation could result in propeller blade separation and possible aircraft loss of control.

Effective: Apr 19, 2001 Category: propeller Compliance: Required as indicated, unless accomplished previously.

Why matched: Airworthiness Directives; Dowty Aerospace Propellers Model R381/6-123-F/5 Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

93-19-01

final rule

Dowty Rotol (now Dowty Aerospace Gloucester Ltd.) Models (c)R354/4-123-F/13, (c)R354/4-123-F/20, and (c)R375/4-123-F/21 Propellers

Unsafe Condition: Possible loss of the propeller due to low torque or cracks in propeller retention bolts or hubs.

Effective: Oct 29, 1993 Category: propeller Compliance: Within 500 hours time in service since last torque check and inspections under AD 87-21-51 (for m...

Why matched: Dowty Rotol (now Dowty Aerospace Gloucester Ltd.) Models (c)R354/4-123-F/13, (c)R354/4-123-F/20, and (c)R375/4-123-F/21 Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

78-16-02 R1

final rule

DOWTY ROTOL LTD Model R.209/4-40-4.5/2 Propellers

Unsafe Condition: Propeller hub failure due to cracks in the hub arm threads and subsequent loss of propeller blade retention.

Effective: Nov 15, 1984 Category: propeller Compliance: Within the next 1,000 flight cycles after the effective date of this AD or at a time not to excee...

Why matched: DOWTY ROTOL LTD Model R.209/4-40-4.5/2 Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

82-08-01

final rule

DOWTY ROTOL Models (c)R.209/4-40.5/2, (c)R.245/4-40.5/13, and (c)R.259/4-40-4.5/17 Propellers

Unsafe Condition: Loosening of the propeller blade groups due to separation of red line position markings by more than 0.100 inch or damaged lockpieces, set bolts, or shims affecting the locking mechanism of the bla...

Effective: Apr 12, 1982 Category: propeller Compliance: within the next 50 hours' time in service after the effective date, and thereafter at intervals n...

Why matched: DOWTY ROTOL Models (c)R.209/4-40.5/2, (c)R.245/4-40.5/13, and (c)R.259/4-40-4.5/17 Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

81-16-03

final rule

DOWTY ROTOL LTD. Models R175/4-30-4/13E Propellers

Unsafe Condition: Propeller failure due to cracking of the propeller hub front wall to snout radius.

Effective: Jul 28, 1981 Category: propeller Compliance: Compliance is required prior to accumulating specific operating hours as outlined: for hubs with ...

Why matched: DOWTY ROTOL LTD. Models R175/4-30-4/13E Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

81-13-05

final rule

DOWTY ROTOL Models (c)R.289/3-110-F/1 and (c)R.289/3-110-F/11 Propellers

Unsafe Condition: Cracks, scratches, pitting, nicks, dents, or gouges on the outer 15 inches of the leading edge of propeller blades, P/N 660705335, could lead to blade tip failures.

Effective: Jul 28, 1981 Category: propeller Compliance: Prior to each engine start or prior to accumulating 3 hours of engine/propeller operating time, w...

Why matched: DOWTY ROTOL Models (c)R.289/3-110-F/1 and (c)R.289/3-110-F/11 Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

81-16-02

final rule

DOWTY ROTOL, LTD. Propeller Types

Unsafe Condition: Cracks in the propeller pitch lock cylinder

Effective: Jul 28, 1981 Category: propeller Compliance: Within the next 1,000 hours time in service after the effective date of this AD, or at the next p...

Why matched: DOWTY ROTOL, LTD. Propeller Types

Technical illustration of an aircraft propeller assembly
Problem area Propeller

81-07-09

final rule

DOWTY ROTOL Models (c)R.289/3-110- F/1 and (c)R.289/3-110-F/11 Propellers

Unsafe Condition: Blade tip failures due to cyclic bending stresses from improper indexing of the propeller shaft to the engine crankshaft.

Effective: Apr 2, 1981 Category: propeller Compliance: Within the next 50 hours time in service after the effective date of this AD or by April 30, 1981...

Why matched: DOWTY ROTOL Models (c)R.289/3-110- F/1 and (c)R.289/3-110-F/11 Propellers

81-05-04

final rule

DOWTY ROTOL Models (c)R.289/3-110- F/1 and (c)R.289/3-110-F/11 Propellers

Unsafe Condition: Blade tip failures due to operation at manifold pressures above 26 inches Hg below 2000 RPM.

Effective: Apr 2, 1981 Category: propeller Compliance: Within the next 10 hours time in service after the effective date of this AD

Why matched: DOWTY ROTOL Models (c)R.289/3-110- F/1 and (c)R.289/3-110-F/11 Propellers