Airworthiness Directives - Airframe (Page 1 of 1) Manufacturer: Piper

Transcription

1 Airworthiness Directives - Airframe (Page 1 of 1) Manufacturer: Piper Model: PA18A-150 Serial #: Total Time Airframe: Control Stick Previously Complied With. Inspection revealed that AN3 bolts Attachment installed per AD Fuel-Hydraulic N/A by aircraft Model & Serial numbers. Lines Brake Line Cover N/A by aircraft serial number. Plate Gas Tank Cap Vent Previously Complied With. Inspection revealed vented fuel caps in compliance with the AD intent. Positive Detent Operated fuel valve and found it to operate in compliance with the AD Engagement of Fuel Valve Marking plate markings align with valve detents. 4/1/12 Tach+100 hrs Sleeves - Control Inspection revealed sleeves are in compliance with AC and are Cables considered in compliance the AD Rudder Cable Inspection revealed that welds are in compliance with the AD. Attachment Lug Exhaust Mufflers Inspection at Tach. Time = , Total Time = revealed that See Eng. Tach= hrs. the muffler was in compliance with the AD. Next inspection due at Log Entry TTAF= Tach. Time = =394.44, Total Time = hrs. 3/6/ Wing Lift Struts Superseded by AD Fuel Venting Previously Complied With. Inspection revealed vented fuel caps in compliance with the AD intent Fuel Tank Placard per AD in place on LH side of cockpit Wing Lift Struts Superseded by AD Wing Lift Struts Previously Complied With. Forks replaced with roll threaded forks Wing struts replaced I.A.W as noted in logbook entry dated 8/20/93 and considered terminating action per the AD.

2 Airworthiness Directives - Engine (Page 1 of 3) Manufacturer: Lycoming Model: O-320 Serial #: L Time SMOH: Engine Accessory Previously Complied With (PCW). See Mattituck logbook entry dated Drive Adaptor Gasket February Baffle Clamps Inspection revealed that the baffle clamps have been replaced with baffle retainers and hooks in compliance with the AD. Exhaust Valve Stem PCW. See Mattituck logbook entry dated 15 February Also, visual with Camshaft inspection revealed that the 7/16 valves have been replaced with ½ Assembly valves Oil Seal Failure Not Applicable (N/A). No fuel pump installed on this engine/aircraft Oil Filter Adapter PCW. See Mattituck logbook entry dated 15 February Gasket Piston Pin Recall PCW. See Mattituck logbook entry dated 15 February Oil Pump Drive PCW. See Mattituck logbook entry dated 15 February Shaft Oil Filler Extension PCW. See Mattituck logbook entry dated 15 February Rocker Box Covers, N/A. Applies only to O-320-H series engines Arms, Fulcrums, Spacer Washers Oil Pump N/A. Applies only to O-320-H series engines Crankshaft N/A. Applies only to O-320-H series engines. Assembly Fuel Injector Center N/A. No fuel injector installed on this engine. Body Bellows Seal Fuel Injector N/A. No fuel injector installed on this engine Regulator Diaphragm Aircraft Mounting N/A. Applies only to O-320-H series engines Bracket Attaching R2 Bolts

3 Airworthiness Directives - Engine (Page 2 of 3) Manufacturer: Lycoming Model: O-320 Serial #: L Total Time: Exhaust Hydraulic N/A. Applies only to O-320-H series engines Lifters and Upper R2 Exhaust Valve Upper Exhaust N/A. Applies only to O-320-H series engines Valve Spring Seats R R1 Superseded by Rocker Arm PCW. See Mattituck logbook entry dated 15 February Assemblies Rear Mounted N/A. No propeller governor installed on this engine/aircraft Propeller Governor R1 & External Oil Line Fuel Pump N/A. Applies only to engines with turbo chargers. No turbo charger Diaphragm and Vent Fitting installed on this engine/aircraft Superseded by AD Piston Pin Recall N/A by dates of overhaul and when piston pins were supplied and by engine serial numbers listed in Lycoming S/B 501 B. Low Pressure N/A. No fuel pump installed on this engine/aircraft Diaphragm Fuel Pump Low Octane Engine N/A by engine model number and aircraft ID (N) numbers listed in AD. Damage Engine Oil Pump N/A. Oil pump gears replaced. See engine logbook entry dated 7/17/2001. Impeller Superseded by AD Piston Pin Recall N/A. No cylinder work since 1988 overhaul.

4 Airworthiness Directives - Engine (Page 3 of 3) Manufacturer: Lycoming Model: O-320 Serial #: L Time (SMOH): Corrosion Pits in N/A. Only applicable to 160 HP engines. I.D. of Crankshaft Crankshaft Cracks N/A. No work on crankshaft noted in engine logbook between 2/1/95 & 12/31/ Superseded by AD Oil Filter Converter N/A by engine model number Plate Gasket Corrected by AD C Crankshaft Gear and N/A. Applies only to engines that have experienced sudden stoppage. No C1 Gear Retaining Bolt such event as described in the AD has occurred with this engine ECI Cylinder Superseded by AD Cracks ECI Cylinder N/A. ECI Cylinders not installed on this engine/aircraft Cracks Superior Air Parts Revised by AD R1. N/A. Superior Air Parts not installed Cylinder Head Fatigue Failure Superior Air Parts N/A. Superior Air Parts not installed Cylinder Head 19R1 Fatigue Failure Engine N/A. Engine Components, Inc. cylinders not installed Components, Inc (ECI) Cylinder Head Failure

5 Manufacturer: Piper Model: PA18A-150 Serial #: Total Time Airframe: Airworthiness Directives Engine Accessories & Miscellaneous (Page 1 of 1) Bendix (Magneto) Functional test of ground. Functionally tested magneto switch per AD Switches instructions and found it to be airworthy Induction Air Filters P.C.W. See logbook entry of July 17, 2001 Tach: 770 4/1/12 Paper Air Filters or 7/7/06 ACS Products N/A. Bendix ignition switch installed Company Ignition Switches Precision Airmotive (formerly Facet, N/A. Applies only to carburetors overhauled between 11/1/91 & 7/15/92. Carburetor installed overhauled by Mattituck in 1988 See engine logbook Marvel Schebler) MA-4 Series Carburetors entry dated 15 Feb Brackett Aircraft Specialties, Inc. Filter Assemblies w/neoprene Gasket Bendix Magnetos Impulse Coupling Assemblies Precision Airmotive (Formerly Facet, Marvel Shebler) MA-4 Series Carburetors 2 Piece Venturi Bendix Magnetos Riveted or Snap Ring Impulse Coupling Assemblies N/A. Brackett Aircraft filter not installed on this aircraft. Superseded by Inspected impulse coupling in accordance with AD and found it to be airworthy. N/A. V stamped on the data plate indicates that the carburetor has a 1- piece venturi. Logbook entry dated 5/11/94 indicates that a 1-piece venturi was installed. N/A. Applies only to Lycoming 540 series engines.

6 Airworthiness Directives - Propeller (Page 1 of 1) Manufacturer: Sensenich Corp. Model: M74D Series Propeller Serial: A52599 Installed New on Feb. 25, 1988 Tach. Time 4191 Serial #: Total Time Airframe: Cracked Hubs N/A. Applies to B series engines only Mid-Blade Propeller N/A. No mid-blade decals installed on this propeller. Decals Maintenance Repair N/A. No record of maintenance or repair by T&W Propellers, Inc by T & W Propellers, Inc. Return to Service by N/A. No record of return to service by Southern California Propeller Southern California Propeller Service Service.