DCA/AL-T/4E - Rotating Components - Life Limitations. 3 <applicability> <applicability> <p> <span> All Model LTS 101-600A-2, -600A-3, -650B-1, -650B-1A, -650C-2, -650C-3, -650C-3A, -750A-1, -750A-3, -750B-1, -750B-2, and -750C-1 turboshaft engines and LTP 101-600A-1A and -700A-1A turboprop engines.</span> </p> </applicability&g...
DCA/BELL212/27 - Swashplate Support - Inspection. 9 <applicability> <applicability> <p> <span> All model 212</span> </p> </applicability> </applicability>
DCA/BELL407/44 - Hydraulic Pump Driveshaft <applicability> <applicability> <p> <span>Model 407 aircraft, S/N 53000 through 53408 and 53421 through 53459.</span> </p> </applicability> </applicability>
DCA/R22/1 - Main Rotor Blades - Inspection. 3 <applicability> <applicability> <p> <span> All model R22 series</span> </p> </applicability> </applicability>
DCA/R22/45C - Door Hinge Security <applicability> <applicability> <p> <span> All model R22, R22 Alpha, R22 Beta, R22 Mariner aircraft.</span> </p> </applicability> </applicability>
DCA/AL-T/34 - Combustion Chamber Housings <applicability> <applicability> <p> <span> Model T5313B, T5317A, T5317A-1, T5317B and T5317BCV turboshaft engines fitted with combustion chamber housing P/N 1-130-610-05, 1-130-610-12 or 1-130-610-17.</span> </p> <p> <span>These engines are installed o...
DCA/BELL212/13A - Main Rotor Hub Strap Assemblies - Retirement 5 <applicability> <applicability> <p> <span> All model 212 with strap assembly P/N 204-012-122-001 or 204-012-122-005.</span> </p> </applicability> </applicability>
DCA/BELL212/21B - Fatigue Critical Components - Retirement 7 <applicability> <applicability> <p> <span> All model 212</span> </p> </applicability> </applicability>
DCA/BELL407/38 - Turbine Steady State Operation <applicability> <applicability> <p> <span> Model 407 aircraft, S/N 53000 through to 53644.</span> </p> </applicability> </applicability>
DCA/McC/132A - Hub - Inspection and Replacement 6 <applicability> <applicability> <p> <span> B2D34C53N/74E having hubs S/N 705516 through 705560 used on Lycoming O-360 or IO-360 series engines</span> </p> </applicability> </applicability>
DCA/R2000/12 - Fuel Fittings <applicability> <applicability> <p> <span> Model R2100, R2100A, R2112, R2120U, R2160, R2160D and R2160i aircraft, S/Ns 001 through 191.</span> </p> </applicability> </applicability>
DCA/R22/39 - Tail Rotor Pitch Control <applicability> <applicability> <p> <span> Model R22 helicopters, up to and including S/N 3328, except 3167, 3326, and 3327, with pitch control assembly, P/N A031-1, Revision J or prior.</span> </p> </applicability> </applicability>
DCA/McC/110 - Hub - Inspection and Replacement 4 <applicability> <applicability> <p> <span> D2A34C49 & C49-A/90A, D2A34C58 & C58-A/90A1, D2AF34C54 & C54-A/84HF, 2AF34C55 through C55-C/78FF model propellers</span> </p> </applicability> </applicability>
DCA/R22/22 - Tailcone Skin Doubler - Installation. 8 <applicability> <applicability> <p> <span> Model R22 series S/N 0002 through S/N 2060 and 2073 equipped with Tail Rotor Visual Warning Guards (with either two or three red stripes)</span> </p> </applicability> </applicability>
DCA/R22/37 - Sprag Clutch - Replacement 14 <applicability> <applicability> <p> <span> Model R22, S/N 0002 through 2862, inclusive, fitted with sprag clutch, P/N A188-2, S/N 3708 through 3757, 3808 through 3893, and 3908 through 4207.</span> </p> </applicability> </applicability>
DCA/R22/40A - Main Rotor Blades <applicability> <applicability> <div style="border:none;"> <p style="border:none;"> <span> All R22 series with main rotor blades P/N A016-1 or A016-2 installed.</span> </p> </div> </applicability> </applicabil...
DCA/AL-T/30 - Boost Pump Drive Shaft <applicability> <applicability> <p> <span> Model T53 series turbine engines.</span> </p> </applicability> </applicability>
