DCA/BELL407/2 - Tail Rotor Drive - Shimming. 3 <applicability> <applicability> <p> <span> Model 407 S/N 53000, 53002 through 53065, 53067, and 53069 through 53075.</span> </p> </applicability> </applicability>
DCA/BELL407/46 - Gas Producer RPM (NG) Limitation <applicability> <applicability> <p> <span> Model 407 aircraft, S/N 53000 through to 53862.</span> </p> </applicability> </applicability>
DCA/McC/140 - Propeller Hubs - Modification and Inspection. 10 <applicability> <applicability> <p> <span> Constant speed hub models 2D34C8-( ), 2D34C9-( ), 2D34C53-( ), B2D34C53-( ), D2A34C58-( ), F2A34C58-( ), 2A34C66-( ), E2A34C70-( ), E2A34C73-( ), D2A34C78-( ), D2A34C98-( ); and feathering hub models D2AF34C30-( ), 2AF34C55-( ), D2AF34C56-( ), D2AF34C61-( ),...
DCA/R22/3B - Main Gear Box Coupling - Inspection. 3 <applicability> <applicability> <p> <span> Model R22 S/N 0002 through 0107</span> </p> </applicability> </applicability>
DCA/AL-T/5 - Gas Producer Blades - Modification. 3 <applicability> <applicability> <p> <span> All model LTP101-600A-1A and -700A-1A turboprop and LTS101-600A-2 turboshaft engines</span> </p> </applicability> </applicability>
DCA/BELL212/28 - Transmission Planetary Spider Gear - Inspection. 9 <applicability> <applicability> <p> <span> All model 212 with main transmission lower planetary spider gear, P/N 204-040-785-003.</span> </p> </applicability> </applicability>
DCA/BELL407/1 - Airworthiness Directive Compliance at Initial C of A Issue. 3 <applicability> <applicability> <p> <span> Model 407 helicopters</span> </p> </applicability> </applicability>
DCA/BELL407/45 - Tailboom Skin <applicability> <applicability> <p> <span> Model 407 aircraft fitted with tailboom P/N 407-030-801-201, -203 or -205.</span> </p> </applicability> </applicability>
DCA/McC/139A - Blade <applicability> <applicability> <p> <span> Models 2A36C23/84B-0 and 2A36C82/84B-2 propellers installed on, but not limited to, Beech 35-C33A, A36, V35, and V35B aircraft.</span> </p> </applicability> </applicability>
DCA/R22/2 - Airframe Structure - Inspection. 3 <applicability> <applicability> <p> <span> Model R22 S/N 0002 through 0082</span> </p> </applicability> </applicability>
DCA/AL-T/20 - Power Turbine Rotors - Removal 7 <applicability> <applicability> <p> <span> Model LTS101 series and LTP101 series</span> </p> </applicability> </applicability>
DCA/BELL407/16 - Oil Cooler Blower Assembly <applicability> <applicability> <p> <span> Model 407 S/N 53000 through 5332.</span> </p> </applicability> </applicability>
DCA/McC/103 - Blade Ferrule - Inspection and Rework. 3 <applicability> <applicability> <p> <span> All 2A36C model blades</span> </p> </applicability> </applicability>
DCA/R22/17A - Main Rotor Spindle - Inspection and Modification. 6 <applicability> <applicability> <p> <span> All model R22 aircraft fitted with a main rotor spindle P/N A158-1 and journals P/N A106.</span> </p> </applicability> </applicability>
DCA/AL-T/7 - Gear Assemblies - Replacement 4 <applicability> <applicability> <p> <span> All model LTS101-600A-2 turboshaft engines</span> </p> </applicability> </applicability>
DCA/BELL212/30 - Main Rotor Yoke - Inspection. 10 <applicability> <applicability> <p> <span> All model 212</span> </p> </applicability> </applicability>
DCA/BELL407/47 - Anti-drive Link Assembly <applicability> <applicability> <p> <span> Model 407 aircraft, S/N 53000 through to 53887, 53890 through to 53916, 53918, 53920, 53921, 53923 through to 53926 and 53928 fitted with anti-drive link assembly P/N 406-010-432-101 with a S/N prefix TI or TIFS.</span> </p> </app...
