Pilots Instruments Air System - CANCELLED, 95, 10/2008, CASA, CESSNA400-095.pdf, CESSNA400, Aircraft below 5700 kg, UNDER, UNDER, 5079, Textron Aviation (Cessna) 400 Series Aeroplanes, AD/CESSNA 400/, 181.00
Auxiliary Fuel Pump Wiring Modification, 96, 12/1989, CASA, CESSNA400-096.pdf, CESSNA400, Aircraft below 5700 kg, UNDER, UNDER, 5080, Textron Aviation (Cessna) 400 Series Aeroplanes, AD/CESSNA 400/, 181.00
Wing Front Spar Under Cap, 97 Amdt 1, 1/1995, CASA, CESSNA400-097.pdf, CESSNA400, Aircraft below 5700 kg, UNDER, UNDER, 5081, Textron Aviation (Cessna) 400 Series Aeroplanes, AD/CESSNA 400/, 181.00
Horizontal Stabiliser Fwd Attach Bulkhead, 98, 5/1992, CASA, CESSNA400-098.pdf, CESSNA400, Aircraft below 5700 kg, UNDER, UNDER, 5082, Textron Aviation (Cessna) 400 Series Aeroplanes, AD/CESSNA 400/, 181.00
Elevator Front Spar - CANCELLED, 99, 5/1995, CASA, CESSNA400-099.pdf, CESSNA400, Aircraft below 5700 kg, UNDER, UNDER, 5083, Textron Aviation (Cessna) 400 Series Aeroplanes, AD/CESSNA 400/, 181.00
Inlet Fuel Valve Assembly, 100 Amdt 4, 7/1995, CASA, CESSNA400-100.pdf, CESSNA400, Aircraft below 5700 kg, UNDER, UNDER, 5084, Textron Aviation (Cessna) 400 Series Aeroplanes, AD/CESSNA 400/, 181.00
Seat Back Reinforcing Strap, 101 Amdt 1, 7/1994, CASA, CESSNA400-101.pdf, CESSNA400, Aircraft below 5700 kg, UNDER, UNDER, 5085, Textron Aviation (Cessna) 400 Series Aeroplanes, AD/CESSNA 400/, 181.00
Elevator Forward Spar, 102 Amdt 4, 10/2005, CASA, CESSNA400-102.pdf, CESSNA400, Aircraft below 5700 kg, UNDER, UNDER, 5086, Textron Aviation (Cessna) 400 Series Aeroplanes, AD/CESSNA 400/, 181.00
Elevator Bellcrank Support Structure - CANCELLED, 104, 10/2008, CASA, CESSNA400-104.pdf, CESSNA400, Aircraft below 5700 kg, UNDER, UNDER, 5088, Textron Aviation (Cessna) 400 Series Aeroplanes, AD/CESSNA 400/, 181.00
Main Landing Gear Wheel Bay Wing Rib and Wing Skin, 105 Amdt 1, 10/1995, CASA, CESSNA400-105.pdf, CESSNA400, Aircraft below 5700 kg, UNDER, UNDER, 5089, Textron Aviation (Cessna) 400 Series Aeroplanes, AD/CESSNA 400/, 181.00
