Date of issue: June 8, 1999

Applicability: Beech Models 58P, 300LW, B300, certificated in any category.

Reason: Specification of system issuing AD's by CAA CZ. This AD contains FAA AD issued by FAA to May 31, 1999.

Effective date: July 15, 1999.

Compliance : At the nearest year or 100 hours check. Upon receipt this AD you check, whether AD's contains in this AD are integrated into the Aircraft's Logbook.

Airframe,Beech,58P - 15 ADs.
Engine, Teledyne Continental, TSIO-520 - 37 ADs.
Propeller, Hartzell, PHC - 7 ADs.
Propeller, McCauley, 3A - 4 ADs.
* = Recurring AD     %=Superceded AD

68-08-01 - Propeller cylinder screws

68-13-02 - Possible blade shank failure * %

69-18-05 - Turbocharger oil scavenge pumps

70-13-03 - Balance tube assembly

71-09-03 - Fuel leakage *

72-24-03 - Oil filter adaptor *

75-09-13 - Turbocharger oil inlet adapters *

76-13-09 - Exhaust flange and elbow *

76-17-02 - Cabin window *

77-05-04 - Crankshaft failure *

77-08-04 - Engine mount fittings

77-12-06 - Prop blade *

77-13-08 - Right and left truss assembly *

77-13-17 - Blade actuating pin failures

77-13-22 - Crankcase cracks *

78-06-01 - Flexible intake elbow *

79-01-01 - Screws in control systém

79-05-09 - Oil pressure relief valve

80-01-04 - Cylinder holddown flanges

80-22-05 - Crankshaft front oil seal

81-24-06 - Fuel pump *

82-09-01 - Fuel pressure regulator leaks

83-13-06 - Counterweight bolts

84-19-04 - Engine driven fuel pump

84-25-05 - Turbochg oil scavenge reservoir *

85-11-04 - AFM placard - seats

85-14-10 R2 - Blade clamp assemblies *

86-08-07 - Engine driven fuel pump

86-13-04 R3 - Cylinder assemblies *

87-14-02 - Starter adaptor shaftgear

87-18-06 R1 - Seat recline actuator handle

88-03-06 - Oil filter

88-17-03 - Starter adapter shaftgea failure

88-21-02 - Seat tracks

89-14-01 - Crankshaft end play check *

87-23-08 - Crankshaft fatigue cracks * %

87-26-08 - Crankshaft and piston pins

89-22-05 - Propeller hub failure * %

89-24-01 R1 - Scavenge oil pump gears

89-24-03 - Turbocharger inlet assembly *

91-17-01 - Elevator trim tab actuators

91-18-19 - Shoulder harnesses

91-19-03 - Champion oil filter

92-23-04 - Engine control angle clips

93-08-17 - Incorrect oil pick-up tube

93-10-02 - Cylinder valve retainer

93-16-14 - Prop hub cracks * %

93-16-15 - Fuel pumps

94-14-12 - Low octane detonation %

94-17-13 - Prop hub failure *

95-21-15 - Engine teardown and analytical inspect.

95-24-05 R1 - Cracks in propeller hubs *

96-12-22 - Oil filter adapter *

97-09-09 - Cracks and missing rivets

97-14-15 - Door handle's lock release button

97-18-02 - Blades, hubs, & blade clamps *

97-25-01 - Outflow/safety valve

97-26-17 - Crankshaft fatigue cracks *

98-01-08 - PRIORITY LETTER - Exhaust roller rocker arms

98-04-24 - Severe Icing Conditions

98-17-11 - Crankshafts

99-05-13 - Lack of fuel flow to the engine

99-09-17 - PRIORITY LETTER - Crankshaft

Airframe, Beech, 300LW - 2 ADs.
Engine, Pratt & Whitney, PT6A-60A - 5 ADs.
Propeller, Hartzell, HC-B4 - 15 ADs.
* = Recurring AD     %=Superceded AD

72-08-04 - Blade cracks

74-14-01 - Blade inspection for cracks

75-11-04 - Power turbine shaft housing *

77-12-06 - Prop blade *

78-12-04 - Oil transfer tube assembly

78-17-07 - Bypass valve diaphragm

83-08-01 R1 - Propeller attach bolt failures

85-14-10 R2 - Blade clamp assemblies *

87-15-04 - Propellers

87-15-05 R1 - Prop mid-blade fail *

89-22-14 - Aileron

91-12-10 - Wing spar attachment

93-01-09 - Blade cracks * %

93-09-04 - Prop hub arm cracks *

93-12-01 - Hub arm fatigue cracks *

94-03-11 - Fatigue cracks

94-17-13 - Prop hub failure *

95-01-02 - Fatigue cracks *

95-03-03 - Hub arm cracks *

96-18-14 - Hub replacement

97-04-12 - Compressor BOV reidentification

Airframe, Beech, B300 - 17 ADs.
Engine, Pratt & Whitney, PT6A-60A - 5 ADs.
Propeller, Hartzell, HC-B4 - 15 ADs.
* = Recurring AD     %=Superceded AD

72-08-04 - Blade cracks

74-14-01 - Blade inspection for cracks

75-11-04 - Power turbine shaft housing *

77-12-06 - Prop blade *

78-12-04 - Oil transfer tube assembly

78-17-07 - Bypass valve diaphragm

83-08-01 R1 - Propeller attach bolt failures

85-14-10 R2 - Blade clamp assemblies *

87-15-04 - Propellers

87-15-05 R1 - Prop mid-blade fail *

89-22-14 - Aileron

91-20-14 R1 - Performance charts

92-06-11 - Erroneous attitude information

92-15-01 - Fail. of truss/firewall bolts

93-01-09 - Blade cracks * %

93-01-20 - Aft cowling door

93-09-04 - Prop hub arm cracks *

93-12-01 - Hub arm fatigue cracks *

93-25-07 - Fuselage stringers *

94-01-01 - Seat base cracks

94-03-11 - Fatigue cracks

94-17-13 - Prop hub failure *

95-01-02 - Fatigue cracks *

95-03-03 - Hub arm cracks *

96-17-10 - Outflow/safety valves %

96-18-14 - Hub replacement

97-04-12 - Compressor BOV reidentification

97-23-17 - Inspection of tubing

97-25-01 - Outflow/safety valve

97-25-03 - AFM Limitations Section

98-04-24 - Severe Icing Conditions

98-15-13 - Rubber fuel hose

98-21-35 - MLG actuator clevis assembly

99-02-16 - Jamming of the elevator trim tab actuator

99-09-10 - Landing gear hand pump

99-09-15 - Flight control mechanism