Index of Airworthiness Directives issued from January 01, 1996 to December 31, 1997

AD Number

Subject aircraft/engine/propeller/appliance

CAA AD-4-001/95

EXTRA 300, Rudder Pedal Safety Control Stop Inspection

CAA AD-1-001/96

SAAB SF340A, 340B, 2000, Check of the Pitch Trim System

CAA AD-1-002/96

L 13SW, Air Brakes Control Cable Inspection

CAA AD-1-003/96

LYCOMING, Time Between Overhaul Change

CAA AD-1-004/96

SAAB SF340A, 340B, 2000, Anti Skid System - Hubcap Coupling

CAA AD-1-005/96

LYCOMING O-235, Push Rods No.73806 - Check

CAA AD-1-006/96

ROBINSON R22, Tail Rotor Gearboxes - Check

CAA AD-1-007/96

ROBINSON R22,Rotorcraft Flight Manual-Change

CAA AD-1-008/96

ROBINSON R44,Rotorcraft Flight Manual-Change

CAA AD-1-009/96

BEECH 400,Flightcrew Seat - Reinforcement

CAA AD-1-010/96

BEECH F90, 99, 99A, +, Landing Gear Leg Lock Link - Inspection

CAA AD-1-011/96

PIPER PA28-140, PA28-150, +, Oil Cooler Hose Assemblies - Inspection

CAA AD-2-012/96

ZLIN 242L, Oil System Service at Low Temperature.

CAA AD-2-013/96

BELL 206 L, Drain Tubes - Modification

CAA AD-2-014/96

PIPER PA28-140, PA28-250, +, Landing Light Support - Modification

CAA AD-2-015/96

ROBINSON R22, V-Belt Upper Sheave-Replacement

CAA AD-2-016/96

ZLIN 126,226,326,526,726, Main Wing Spar - Visual Check of Corrosion

CAA AD-3-017/96

Robinson Model R22, Throttle/Collective Governor

CAA AD-3-018/96

Robinson Model R44, Low-RPM Warning Unit Threshold

CAA AD-3-019/96

Bell Model 206L,206L-1,206L-3, Tailboom Failure

CAA AD-3-020/96

TCM & Rolls-Royce O-200A,O-200B, Engine Timing

CAA AD-3-021/96

Superior Air Parts, Inc. Engine Pistons

CAA AD-3-022/96

Brackett Air Filter Assemblies

CAA AD-3-023/96

Fokker F28 - Lapjoint at Stringer 16/17 and 58/59

CAA AD-3-024/96

Bell 206 - Tail Rotor Hub

CAA AD-3-025/96

AB Hot-Air Balloon - Tipping Frames of Balloon Basket

CAA AD-3-026/96

Piper PA-28, PA-32, + - Flap Lever

CAA AD-3-027/96

Bell 206, Fuel Cell Vent Decal

CAA AD-3-28/96

TCM( formerly Bendix) Ignition Systems Magnetos

CAA AD-3-29/96

Cessna Oil Filter Adapter Assemblies

CAA AD-4-030/96

Textron Lycoming O-235, O-290, O-.320, +, Oil Pump

CAA AD-4-031/96

Cessna, Survey FAA AD issued to December 31, 1995

CAA AD-4-032/96

Textron Lycoming IO-320, LIO-320, +, Pressure Fuel Pump

CAA AD-2-012 R1/96

Zlin 242L, Oil System Service at Low Temperature

CAA AD-4-032 R1/96

Textron Lycoming IO-320, LIO-320, +, Pressure Fuel Pump

CAA AD-4-033/96

McCauley C35, C72, C74, + Propeller Hub

CAA AD-1-001/97

JANAERO DEVICES, Combustion Heater Assemblies

CAA AD-4-032R2/92

TEXTRON LYCOMING IO-320, LIO-320, +, Pressure Fuel Pump

CAA AD-1-002/97

ROBINSON R44 - Gear Carrier Assembly

CAA AD-1-003/97

PIPER PA28R-180, PA28R-200, + - Landing Gear

CAA AD-1-004/97

PIPER, Survey FAA AD issued to December 31, 1995

CAA AD-1-005/97

BEECH, Survey FAA AD issued to December 31, 1995

CAA AD-1-006/97

ASW 19, Amendment of the MM and Inspection Program

CAA AD-1-007/97

CESSNA 150, 150A, 150B, +, Fuel, Oil, or Hydraulic Hose

CAA AD-1-008/97

ROBINSON Model R44 - Low RPM Warning Unit Threshold

CAA AD-1-009/97

Model R22 - Governor

CAA AD-1-010/97

ALLIED Signal TFE731-2, -2A, -3, +, Fan Rotor Disk

CAA AD-1-011/97

SUNDSTRAND AEROSPACE Models T-62T-40C, Compressor Wheel Assemblies

CAA AD-1-012/97

ROBINSON, Survey FAA AD issued to December 31, 1995

CAA AD-1-013/97

SAAB SF 340A, 340B, Landing Gear -Brakes

CAA AD-1-014/97

PRATT and WHITNEY PT6A, Bleed off Valve

CAA AD-2-015/97

Survey FAA AD issued on engines ALLISON 250 - C20 to December 31, 1995 installed on helicopter PZL Kania

CAA AD-2-016/97

BELL 206, Survey FAA AD and Transport Canada AD issued to December 31, 1995

CAA AD-2-017/97

WALTER M601D, - Turbine Blade

CAA AD-2-018/97

WALTER M601T, - Turbine Blade

CAA AD-2-019/97

SAAB SF340A a SAAB 340B, Survey AD issued Swedish LFV

CAA AD-2-020/97

SAAB SF340A a SAAB 340B, - Furnishing

CAA AD-2-021/97

TEXTRON LYCOMING O-320, O-360, +, Employing D-2000 or D-3000 TCM (Bendix) Dual Magnetos

CAA AD-2-022/97

LOUIS L´HOTELLIER, - Quick Connectors

CAA AD-2-023/97

SHEMPP-HIRTH, - Elevator Control System

CAA AD-2-024/97

BELL 206L, Main Rotor

CAA T AD-2-025/97

ZLIN 50LA,LS,LE,LX and M, Stabilizer - Hinge Point

CAA AD-2-26/97

Survey DGAC AD issued on helicopters AS 355 Ecureil and Survey FAA AD issued on engines Allison 250-C20 to December 31, 1995.

CAA AD-2-027/97

ALLISON 250, Visual Inspection of Engine Filters

CAA AD-2-028/97

BEECH C90A, Autopilot System

CAA AD-2-029/97

ZLIN 242L - Sludge Valve of the Oil System

CAA AD-2-030/97

HUGHES/SCHWEIZER , Survey FAA AD issued to December 31, 1995

CAA AD-2-031/97

GENERAL ELECTRIC CF34-1A,-3A a 3A2, Fan Disks

CAA AD-2-032/97

RAYETHON 90,99,100,200 and 1900, Pilot or Copilot Chair

CAA AD-2-033/97

GENERAL ELECTRIC CF34-1A,-3A a 3A2, - HPC Stage 1 Rotor Disks

CAA AD-2-035/97

ALLIED SIGNAL TFE731-2A,-3C,-3CR, LPT Seal Plates

CAA AD-2-036/97

BEECH 1900D, Stabilon Attachment Angles

CAA AD-2-037/97

PIPER PA23, PA31, PA31P, PA31T, PA42, Hydraulic Hoses

CAA AD-2-038/97

SENSENICH M76EMM, M76EMMS, 76EM8, 76EM8S, - Propeller Blade Tip Failures

CAA AD-2-039/97

SAAB 340A, 340B, Engine Controls - Installation of Flight Idle Stop

CAA AD-2-040/97

HARTZELL HC-A3VF-7, HC-B3TF-7, +, - Hub Replacement

CAA AD-2-041/97

TELEDYNE CONTINENTAL, ROLLS ROYCE C75, C85, +, - Rocker Shaft Bosses

CAA AD-2-042/97

AS-355 ECUREIL, MGB Suspension Bi-Directional Cross Beam

CAA AD-2-043/97

RAYETHON (formerly Beech) Model 400, 400A, MU-300-10, 2000, Model 200 and B200, Model 300 and B300, Outflow/Safety Valves

CAA AD-2-044/97

RAYETHON (formerly Beech) Model 1900D, Windshield Circuit Breakers

CAA AD-2-045/97

WALTER, M 462-RF, - Treaded Coupling in the Accessory Case

CAA AD-2-047/97

ALLIED SIGNAL TFE731-2,-2A,-3,-3R, - Fan Rotor Disks

CAA AD-2-048/97

DA 20 A1 KATANA, Battery Attachment Modification

CAA AD-2-049/97

TEXTRON LYCOMING O-320, IO-320, +, - Piston Pin

CAA AD-2-050/97

ALLIED SIGNAL TFE731-( ), - Fan Rotor Disk

CAA AD-2-051/97

McCAULEY 1A103/TCM, - Hub cracks

CAA AD-2-052/97

HARTZELL HC-B3TN, HC-B5MP, +, - Inspection for forging flaws or cracks

CAA AD-3-053/97

SAAB SF 340A, 340B Windshield Wipers

CAA AD-3-054/97

SAAB SF 340A, 340B, Power Control

CAA AD-3-055/97

EXTRA EA 300/200, Front Seat Belt Cover

CAA AD-2-042R1/97

AS-355, MGB Suspension Bi-Directional Cross Beam

CAA AD-3-056/97

CESSNA 650, Wire Bundle Assembly

CAA AD-3-057/97

RAYTHEON 1900, 1900C, 1900D, Flaps - Inspection

CAA AD-3-058/97

TELEDYNE CONTINENTAL E-165, E-185, E-225, +, - Cylinder, Piston Pin

CAA AD-3-059/97

SAAB SF 340A, 340B, Wings Flaps - Replacement of Support Strap

CAA T AD-3-060/97

RAPCO Inc., Appliance – Pressure Filter

CAA AD-3-061/97

RAYTHEON E33, F33, G33, +, Cabin Side Door Handle

CAA AD-3-062/97

RAYTHEON, 1900, 1900C, 1900D, Airstair Door Handle

CAA AD-3-063/97

AS-355, Tailboom – Attachment Screws

CAA AD-3-064/97

TEXTRON LYCOMING O320, IO-320, +, – Piston Pin

CAA AD-3-065/97

LOUIS L´HOTELLIER S.A., Quick Connectors

CAA AD-3-66/97

SAAB SF340A, SAAB 340B, Engine Air Intake

CAA AD-3-067/97

ROBINSON R-44, Up-Limit Switches and Clutch Assembly

CAA AD-4-068/97

GENERAL ELECTRIC CT7-5A2,-7A,-9B,-9C, – Forward Cooling Plate

CAA AD-4-069/97

GENERAL ELECTRIC CT7-5A2,-7A,-9B,-9C, – ECI for Cracks

CAA AD-4-070/97

PURITAN-BENNET, -Oxygen Masks

CAA AD-4-071/97

SAAB –340A, -340B, Horizontal Stabilizers

CAA AD-4-072/97

SAAB SF 340A, 340B, Survey SAD for Engines, Propellers and Other Vendor Equipment

CAA AD-4-073/97

HARTZELL PROPELLER HC-( ), HA-A2V20-1B, – Blades, Hubs and Blade Clamps

CAA AD-4-074/97

TELEDYNE CONTINENTAL E-165,E-185,E-225, +, – Cylinders and Piston Pins

CAA AD-4-075/97

DOWTY ROTOL AEROSPACE R354, R375, R389, R390, - Blade Pitch Seizure

CAA AD-3-053R1/97

SAAB SF 340A 340B, Windshield Wipers

CAA AD-4-076/97

Survey FAA AD issued till November 20, 1997 for aircraft Piper PA-44-180T

CAA AD-4-077/97

Survey DGAC AD issued for aircraft SOCATA TB-10 and Survey FAA AD issued for engines Textron Lycoming and propellers Hartzell till November 30, 1997

CAA AD-4-078/97

CANADAIR CL 600, 601, 601 3A/-3R, 604, Check Failure of the Pressure Bulkhead

CAA AD-4-079/97

PIPER PA-20, -23, -24, -25, - +, Install Placard on the Pilot´s Instrument Panel

CAA AD-4-080/97

SCHWEIZER 269A, A-1, B, C a TH-55A, Main Rotor Transmission Ring Gear