ATR72 DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY
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1 DGCA/ATR 72/1 DGCA/ATR 72/2 TO ENSURE THAT FLIGHT CREWS ACTIVATE THE WING & TAIL PNEUMATIC DEICING BOOTS TO PREVENT FATIGUE CRACKING OF THE FUSELAGE & THE PAX. & SERVICE DOORS FAA AD FAA AD DGCA/ATR 72/3 LANDING GEARS- INSTALL MODIFIED UPLOCK BOXES DGAC AD (B) DGCA/ATR 72/4 FIRE PROTECTION - FIRE HANDLES DGAC AD (B)R1 DGCA/ATR 72/5 DGCA/ATR 72/6 SEVER ICING CONDITIONS -IMPLEMENT AIRCRAFT DESIGN ENHANCEMENTS ENGINE CONTROLS - FLIGHT MANUAL PROCEDURE ASSOCIATED WITH REVERSE APPLICATION DGAC AD (B) R1 DGAC AD (B) DGCA/ATR 72/7 TIME LIMITS DGAC AD (B) R1 DGCA/ATR 72/8 TAKE-OFF AFTER USE OF TYPE II OR IV FLUIDS - APPENDIX TO THE FLIGHT MANUAL DGCA/ATR 72/9 CANCELLED IN VIEW OF DGCA/ATR 72/01 VIDE LETTER NO 9-752/03 DATED 04/10/05 DGCA/ATR 72/10 ELECTRICAL CIRCUIT - WIRING CONDUIT BETWEEN FRAME 28 & 28A DGAC AD (B) R2 DGAC AD (B) DGCA/ATR 72/11 STRUCTURE - RESULT OF FATIGUE TESTS DGAC AD (B) DGCA/ATR 72/12 PROPELLER FEATHERING- ATPCS TEST SELECTOR SWITCH DGAC AD (B) DGCA/ATR 72/13 HAMILTON STANDARD 247F PROPELLERS-BLADE ROOT (ATA 61) DGAC AD (B) R1 DGCA/ATR 72/14 HYDRAULIC PUMP POWER SUPPLY CABLES ROUTING DGAC AD (B) DGCA/ATR 72/15 MAIN LANDING GEAR- SWINGING LEVER SPACER DGAC AD (B) DGCA/ATR 72/16 THERMAL ACCOUSTICAL INSULATION MATERIALS DGAC AD (B) DGCA/ATR 72/17 ENGINES-HP OIL PUMP-(PRV) DGAC AD (B)R1 DGCA/ATR 72/18 PROPELLERS-PITCH CHANGE SYSTEM COMPONENT DGAC AD (B)R2
2 DGCA/ATR 72/19 DGCA/ATR 72/20 ELECTRICAL RACK 90VU-WIRE BUNDLE ROUTING ON 93,94 AND 95 VU CARBON SHELVES CANCELLED VIDE LETTER NO 9-752/03 AI(2) DATED 19/10/06, IN VIEW OF DGCA/ATR 72/26R1 DGAC AD (B) DGCA/ATR 72/21 FORWARD ATTENDANT SEAT DGAC AD (B) DGCA/ATR 72/22 FLIGHT CONTROL-STANSBY PITCH TRIM SWITCH DGAC AD (B) R1 DGCA/ATR 72/23 ICING CONDITIONS - REVISE THE AIRPLANE FLIGHT MANUAL ( AFM ) DGCA/ATR 72/24 EQUIPMENT & FURNISHINGS -- THERMAL / ACOUSTIC INSULATION BLANKETS --- REPLACEMENT/REMOVAL DGCA/ATR 72/25(R1) LANDING GEAR, MAIN LANDING GEAR SECONDARY SIDE BRACE DGCA/ATR 72/26(R1) STABILIZERS- VERTICAL STABILIZER FIN TIP - / REPAIR / MODIFICATION DGAC AD R2 EASA AD SUPERSEDES DGAC AD F DGAC AD F , ORGINAL AD IS CANCELLED EASA AD (EASA AD SUPERSEDES DGAC AD (B)R1 AND DGAC AD F ) DGCA/ATR 72/27 FUEL QUANTITY INDICATORS DGAC AD F DGCA/ATR 72/28R1 DGCA/ATR 72/29 DGCA/ATR 72/30R1 FUEL- FUEL TANK SYSTEM WIRING & SENSORS - MODIFICATION /REPLACEMENT FUEL TANK SAFETY MAIN LANDING GEAR- SHOCK ABSORBER- CROSS LOCKING BOLT OF THE ATTACHMENT PIN TIME LIMITS / MAINTENANCE CHECKS --- CERTIFICATION MAINTENANCE REQUIREMENTS & CRITICAL DESIGN CONFIGURATION CONTROL LIMITATIONS ( FUEL TANK SAFETY) DGCA/ATR 72/31 ELECTRICAL POWER VU ELECTRICAL HARNESS - DGCA/ATR 72/32 FLIGHT CONTROLS - AILERON TAB BELLCRANK ASSEMBLY - EASA AD R1 EASA AD E EASA AD EASA AD EASA AD
3 DGCA/ATR 72/33 DGCA/ATR 72/34 ICE & RAIN PROTECTION -- PITOT PROBE RESISTANCE & LOW CURRENT SENSOR --- /REPLACEMENT ELECTRICAL/ELECTRONIC --- REAR PRESSURE BULKHEAD AREA AND WIRE CHAFING ---/MODIFICATION DGCA/ATR 72/35 EQUIPMENT & FURNISHINGS --- PASSENGER SEATS --- /REPAIR/MODIFICATION DGCA/ATR 72/36 DGCA/ATR 72/37 FLIGHT CONTROLS --- COTTER PINS & PITCH UNCOUPLING MECHANISM (PUM) -- /INSTALLATION ELECTRICAL / ELECTRONIC --- WIRE BUNDLES IN THE REAR BAGGAGE ZONE --- PROTECTION & CLAMPING DGCA/ATR 72/38R1 WINDOWS --- COCKPIT FORWARD SIDE WINDOWS --- S / REPLACEMENT DGCA/ATR 72/39 INDICATING / RECORDING SYSTEMS --- MULTI PURPOSE COMPUTER (MPC) WITH AIRCRAFT PERFORMANCE MONITORING (APM) FUNCTION -- INSTALLATION DGCA/ATR 72/40R2 FIRE PROTECTION --- HALON 1211 FIRE EXTINGUISHERS --- IDENTIFICATION / REPLACEMENT DGCA/ATR 72/41R1 DGCA/ATR 72/42 DGCA/ATR 72/43 DGCA/ATR 72/44 DGCA/ATR 72/45 FLIGHT CONTROLS --- RUDDER TAB,RUDDER PEDAL AND ELEVATOR CONTROL RODS --- /REPLACEMENT STABILIZERS --- ELEVATOR INBOARD HINGE FITTING LOWER STOP ANGLES --- / REPLACEMENT NACELLES / PYLONS --- ENGINE NACELLE LOWER FAIRING JUNCTION WITH UNDERWING BOX --- NACELLES & PYLONS --- ENGINE SHOCK MOUNT PICK UP FITTINGS --- /REPLACEMENT ICE AND RAIN PROTECTION --- PNEUMATIC ICE PROTECTION DUAL DISTRIBUTOR VALVES --- / REPLACEMENT EASA AD EASA AD EASA AD EASA AD E EASA AD EASA AD EASA AD EASA AD SUPERDEDED EASA AD R1 EASA AD EASA AD EASA AD EASA AD EASA AD
4 DGCA/ATR 72/46 FUEL --- FUEL INDICATING SYSTEM --- MODIFICATION EASA AD DGCA/ATR 72/47R1 EQUIPMENT / FURNISHING --- TYPE III EMERGENCY EXIT DOOR -- - / MODIFICATION DGCA/ATR 72/48R2 ELECTRICAL ROUTING ELECTRONIC RACK 90VU SHELF / ELECTRICAL HARNESS DGCA/ATR 72/49 ELECTRICAL ROUTING ELECTRONIC RACK 120VU SHELF / ELECTRICAL HARNESS / MODIFICATION DGCA/ATR 72/50R1 ATA 32, LANDING GEAR MAIN LANDING GEAR HINGE PIN / REPLACEMENT EASA AD SUPPER EASA AD EASA AD sup EASA AD R1 EASA AD EASA AD SUPERSEDED EASA AD DGCA/ATR 72/51R1 ATA 28, FUEL FUEL PROBES / REPLACEMENT EASA AD R1 DGCA/ATR 72/52 ATA 26, FIRE PROTECTION ENGINE FIRE EXTINGUISHING PIPE DGCA/ATR 72/53R2 DGCA/ATR72/54 DGCA/ATR72/55 ATA 22, AUTO FLIGHT-AUTO PILOT AND YAW DAMPER- OPERATIONAL LIMITATIONS MASTER MINIMUM EQUIPMENT LIST-AMENDMENT ATA22, AUTO FLIGHT-AUTO PILOT AND YAW DAMPER- OPERATIONAL LIMITATIONS AIRCRAFT FLIGHT MANUAL- AMENDMENTS ATA 33, LIGHTS-EMERGENCY EXIT-EMERGENCY POWER SUPPLY UNIT-/REPLACEMENT DGCA/ATR72/56R1 ATA-92, ELECTRIC / ELECTRONIC COMMON INSTALLATION WIRE CHAFING BEHIND CABIN SIDEWALL DGCA/ATR72/57R1 DGCA/ATR72/58R1 ATA-32, LANDING GEAR MAIN LANDING GEAR UNIVERSAL JOINT / REPLACEMENT ATA-05, TIME LIMITS/ MAINTENANCE CHECKS CERTIFICATION MAINTENANCE REQUIREMENTS AND AIRWORTHINESS LIMITATIONS AMENDMENTS. EASA AD R1 EASA AD R1(REVISED EASA AD , SUPERSEDED EASA AD ) EASA AD EASA AD EASA AD SUPERSEDED EASA AD EASA AD SUPERSEDED EASA AD EASA AD R1 REVISED EASA AD
5 DGCA/ATR72/59 CANCELLED: ATA 05 - TIME LIMITS / MAINTENANCE CHECKS CERTIFICATION MAINTENANCE REQUIREMENTS AND CRITICAL DESIGN CONFIGURATION CONTROL LIMITATIONS [FUEL TANK SAFETY] EASA AD CN
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