DCA/CESS402/5 - Main Landing Gear Fork Bolts - Replacement 4 <applicability> <applicability> <p> <span> All model 402 Series All S/N’s</span> </p> </applicability> </applicability>
2018-0203 - Pilot Collective Stick Assembly <applicability> <applicability> <p> <span> AW169 helicopters, all S/N fitted with a Pilot Collective Stick Assembly P/N 6F6711A07832, or P/N 6F6711A07831.</span> </p> </applicability> </applicability>
DCA/LYC/166 - FAA AD 79-21-08 &amp; 79-26-03 Bendix Fuel Injection Regulator - Inspection <applicability> <applicability> <p> <span> Bendix fuel injection systems models RSA-5AB1, RSA-5AD1, RSA-7AA1, RSA-7DA1, RSA-1OAD1, RSA-1ODB1, RSA-1ODB2, RSA-1OED1, and RSA-1OED2 with parts list numbers detailed in Bendix SB's RS-68, RS-69 and RS-70 installed on, but not limited to, IO-320, AIO-32...
DCA/PROCTMK1/6 - Fuel Tank Gauze Filter - Modification <applicability> <applicability> <p> <span> All Proctor Mark 1 aircraft fitted with GSM prefixed S/N fuel tanks.</span> </p> </applicability> </applicability>
DCA/PROCTMK1/5 - Manifold Drain - Modification <applicability> <applicability> <p> <span> All Proctor Mark 1 aircraft.</span> </p> </applicability> </applicability>
You are here Home Aircraft Airworthiness Type acceptance reports Schleicher ASW 28-18 E Schleicher ASW 28-18 E
DCA/CESS402/18 - Fuel, Oil or Hydraulic Hose - Removal 9 <applicability> <applicability> <p> <span> All model 402 series, all S/Ns.</span> </p> </applicability> </applicability>
DCA/LYC/154 - FAA AD 75-09-15 Bendix Fuel Injector Flow Divider Cover Gasket - Modification <applicability> <applicability> <p> <span> All Lycoming model IO-320, AIO-320, IO-360, LIO-360, HIO-360-C, IVO-360, TIO-360, AIO-360, IGO-380, IO-540, TIO-540, IVO-540, IGO-540, and IO-720 series engines equipped with Bendix fuel injector flow divider part numbers listed in Lycoming SB 382.</span&g...
DCA/PROCTMK1/7 - Battery Master Switch - Modification <applicability> <applicability> <p> <span> All Proctor Mark 1 aircraft.</span> </p> </applicability> </applicability>
2018-0197 - Emergency Exit Windows <applicability> <applicability> <p> <span> AW169 helicopters, all S/N and AW189 helicopters, all S/N, except those helicopters fitted with emergency exit windows with strap P/N A487A003A, or helicopters with bubble windows P/N 8G5620F00112.</span> </p> </applicability>...
DCA/BELL222/20 - Tail Rotor Pitch Change Mechanism - Rework. 11 <applicability> <applicability> <p> <span> Models 222 aircraft, S/N 47006 through to 47089</span> </p> <p> <span>Model 222B aircraft, S/N 47131 through to 47156</span> </p> <p> <span>Model 222U aircraft...
2017-0155 - Emergency Exit Windows <applicability> <applicability> <p> <span> Leonardo AW169 helicopters, S/N 69007, 69009, 69011 through to 69019 inclusive, 69021 through to 69024 inclusive, 69027, 69032, 69033, 69041, 69045 and 69051.</span> </p> </applicability> </applicability>
DCA/LYC/150 - FAA AD 73-23-01 Piston Pins - Inspection. 4 <applicability> <applicability> <p> <span> As detailed</span> </p> </applicability> </applicability>
2015-07-03 - Engine Mount Beams <applicability> <applicability> <p> <span>Cessna 402C aircraft, S/N 402C0001 through to 402C1020.</span> </p> <p> <span>Cessna 414A aircraft, S/N 414A0001 through to 414A1212.</span> </p> </applicability> </applic...
You are here Home Aircraft Airworthiness Type acceptance reports Kubicek Balloons - Revision 1 Kubicek Balloons - Revision 1
2012-23-01 - Flap System <applicability> <applicability> <p> <span>Cessna 402C aircraft, all S/N embodied with Supplemental Type Certificate (STC) SA927NW and</span> </p> <p> <span>Cessna model 414A aircraft, all S/N embodied with STC SA892NW.</span> </p>...
DCA/GD/2 - Engine Studs - Inspection. 3 <applicability> <applicability> <p> <span> Model</span> <span>DG-1000 aircraft, S/N 10-1 through to 10-109.</span> </p> </applicability> </applicability>
DCA/LYC/222 - FAA AD 2012-03-06 AVStar Fuel Servos <applicability> <applicability> <p> <span> All Lycoming fuel injected engines fitted with a AVStar Fuel Systems, Inc. (AFS) fuel servo diaphragm P/N AV2541801 or P/N AV2541803.</span> </p> </applicability> </applicability>