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, 2015Category: propellerCompliance: Within 5,000 flight-hours after September 27, 2010, or within 100 flight-hours after the effectiv...
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, 2015Category: propellerCompliance: before further flight
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, 2014Category: propellerCompliance: Effective July 15, 2014.
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, 2014Category: propellerCompliance: Within the next 50 flight hours (FH) or within 30 days after the effective date of this AD, which...
Unsafe Condition: In-flight double generator failure, which could result in reduced control of the airplane.
Effective: Aug 14, 2013Category: aircraftCompliance: Within 5,000 flight hours after September 27, 2010, or within 100 flight hours from the effective...
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, 2011Category: propellerCompliance: 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
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, 2010Category: aircraftCompliance: 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
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, 2010Category: aircraftCompliance: Within 1,600 flight hours after the effective date or after any blade accumulates 15,000 flight h...
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, 2008Category: propellerCompliance: 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
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, 2006Category: aircraftCompliance: Before further flight
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, 2005Category: propellerCompliance: Within 10 flight hours or 20 days for Type R334/4-82-F/13, and within 50 flight hours or 60 days ...
Unsafe Condition: Possible loss of the propeller due to low torque or cracks in propeller retention bolts or hubs.
Effective: Oct 29, 1993Category: propellerCompliance: Within 500 hours time in service since last torque check and inspections under AD 87-21-51 (for m...
Unsafe Condition: Propeller hub failure due to cracks in the hub arm threads and subsequent loss of propeller blade retention.
Effective: Nov 15, 1984Category: propellerCompliance: 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
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, 1982Category: propellerCompliance: 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
Unsafe Condition: Propeller failure due to cracking of the propeller hub front wall to snout radius.
Effective: Jul 28, 1981Category: propellerCompliance: Compliance is required prior to accumulating specific operating hours as outlined: for hubs with ...
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, 1981Category: propellerCompliance: 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
Unsafe Condition: Cracks in the propeller pitch lock cylinder
Effective: Jul 28, 1981Category: propellerCompliance: Within the next 1,000 hours time in service after the effective date of this AD, or at the next p...
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, 1981Category: propellerCompliance: 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