ATR 42 DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY
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1 DGCA/ATR 42/1 FLIGHT CONTROLS-STANDBY PITCH TRIM SWITCH DGAC AD (B) R1 DGCA/ATR 42/2 IPECO PILOT AND CO-PILOT SEATS DGAC AD (B)R1 DGCA/ATR 42/3 SOCEA CABIN ATTENDANT SEAT DGAC AD (B) DGCA/ATR 42/4 FLAPS -- USE OF THE 45DEGREE CONFIGURATION --- PROHIBITION/MODIFICATION EASA AD DGCA/ATR 42/5 SPERRY AHRS DGAC AD IMP(AB) & (B)R1 DGCA/ATR 42/6 AUTOMATIC STOP RECORDER DFDR/CVR DGAC AD (B) DGCA/ATR 42/7 SGU EFIS SPERRY DGAC AD IMP(B) DGCA/ATR 42/8 ELEVATOR TRIM DGAC AD (B) DGCA/ATR 42/9 PROPELLER BRAKE CONTROL SYSTEM DGAC AD (B)R1 DGCA/ATR 42/10 AUTO PILOT ROLL ACTUATOR PROTECTION DGAC AD (B) DGCA/ATR 42/11 FUEL QUANTITY INDICATION DGAC AD (B)R2 DGCA/ATR 42/12 RUDDER CONTROL CHANNEL CABLES DGAC AD (B) DGCA/ATR 42/13 ENGINE AND PROPELLER FLEXIBLE CONTROL SHAFTS DGAC AD (B) DGCA/ATR 42/14 NAVIGATION ADC - SGU - AHRS DGAC AD (B) DGCA/ATR 42/15 PROPELLER BRAKE CONTROL PUSHBUTTON REPLACEMENT DGAC AD (B) DGCA/ATR 42/16 CARGO SMOKE DETECTOR TEST CIRCUIT DGAC AD (B)R1 DGCA/ATR 42/17 STRUCTURE MODIFICATIONS RESULTING FROM FATIGUE TESTS DGAC AD (B)R2 DGCA/ATR 42/18 PITCH TRIM DGAC AD (B)R1 DGCA/ATR 42/19 MLG RETRACTION JACKS FITTING BOLTS DGAC AD (B)R2 DGCA/ATR 42/20 AILERON TAB INBOARD HINGE PIN DGAC AD (B)R2 DGCA/ATR 42/21 COCKPIT VOICE RECORDER AUTOMATIC CUT OFF DGAC AD (B) DGCA/ATR 42/22 AHRS HONEYWELL AH600 DGAC AD IMP(AB)R1 DGCA/ATR 42/23 ICING CONDITIONS PROCEDURES DGAC AD (B)R1
2 DGCA/ATR 42/24 PAX/CREW DOOR LIFTING DEVICE DGAC AD (B)R1 DGCA/ATR 42/25 ENGINE FIRE EXTINGUISHING SYSTEM DGAC AD (B)R1 DGCA/ATR 42/26 NOSE LANDING GEAR RETRACTING MECHANISM DGAC AD (B) DGCA/ATR 42/27 EMERGENCY LIGHTING DGAC AD (B) DGCA/ATR 42/28 PROPELLER BRAKE DGAC AD (B)R1 DGCA/ATR 42/29 MAIN FRAMES DGAC AD (B) DGCA/ATR 42/30 EMERGENCY OXYGEN SYSTEMOF THE CABIN ATTENDANTS DGAC AD (B)R1 DGCA/ATR 42/31 WHEEL WELL BAY DGAC AD (B) DGCA/ATR 42/32 HYDRAULIC SYSTEM LOW PRESSURE WARNING DGAC AD (B)R2 DGCA/ATR 42/33 FLIGHT CONTROL DGAC AD (B)R2 DGCA/ATR 42/34 FLIGHT CONTROLS DGAC AD (B) DGCA/ATR 42/35 TCAS COLLINS II (or 94) DGAC AD IMP(AB)R1 DGCA/ATR 42/36 EROS OXYGEN MASKS DGAC AD (AB) DGCA/ATR 42/37 FLIGHT CONTROLS DGAC AD (B) DGCA/ATR 42/38 ENGINE AND PROPELLER FLEXIBLE CONTROLS DGAC AD (B)R1 DGCA/ATR 42/39 AUTO PILOT DGAC AD (B) DGCA/ATR 42/40 AFT RH SERVICE DOOR COMMERCIAL FURNISHINGS DGAC AD (B) DGCA/ATR 42/41 AERAZUR LIFE JACKETS PACKING POUCH DGAC AD (AB)R1 DGCA/ATR 42/42 ECE PUSH-BUTTON ASNE 0276C DGAC AD (B) DGCA/ATR 42/43 PITCH CONTROL DGAC AD (B)R1 DGCA/ATR 42/44 AUTO PILOT DGAC AD (B) DGCA/ATR 42/45 COLLINS VHF - 20B TRANCEIVER IDENTIFICATION PLATE DGAC AD (AB)R1 DGCA/ATR 42/46 COLLINS MODE 'S' ATC TRANSPONDER DGAC AD IMP(AB) DGCA/ATR 42/47 OUTER WINGS DGAC AD (B) DGCA/ATR 42/48 PITCH TRIM CONTROLS DGAC AD (B)
3 DGCA/ATR 42/49 FLIGHT CONTROL RODS DGAC AD (B) DGCA/ATR 42/50 AILERON TRIM CONTROL DGAC AD (B) DGCA/ATR 42/51 PURITAN BENNETT CREW MEMBER PROTECTIVE BREATHING EQUIPMENT NECK SEAL DGAC AD IMP(AB) DGCA/ATR 42/52 NOSE LANDING GEAR NARDI HINGE PINS DGAC AD (B) DGCA/ATR 42/53 KARMAN WING FAIRINGS PANELS ATTACHMENT CLIPS DGAC AD (B) DGCA/ATR 42/54 ALLIED SIGNAL AEROSPACE CO (BENDIX / KING) TCAS II SYSTEMS DGAC AD IMP(AB) DGCA/ATR 42/55 COLLINS TCAS II SYSTEMS DGAC AD IMP(AB) DGCA/ATR 42/56 PROTECTION OF THE ELECTRICAL HARNESS IN FRONT AREA DGAC AD (B) DGCA/ATR 42/57 TIME LIMITS DGAC AD (B)R1 DGCA/ATR 42/58 WINDSHIELD, FRAME NODE 5 DGAC AD (B) DGCA/ATR 42/59 WINGS CORROSION ON REAR SPAR DGAC AD (B) DGCA/ATR 42/60 ENGINE NACELLE DRAIN SYSTEM DGAC AD (B) DGCA/ATR 42/61 FUSELAGE STRINGER 6, JUNCTION CLIPS TO FRAME 34 DGAC AD (B) DGCA/ATR 42/62 DE-ICING PROCEDURES AND PROTECTIONS IMPROVEMENT DGAC AD (B)R1 DGCA/ATR 42/63 STANDBY HORIZON POWER SUPPLY DGAC AD (B) DGCA/ATR 42/64 STICK SHAKER/PUSHER SYSTEM DGAC AD (B) DGCA/ATR 42/65 FORWARD CARGO COMPARTMENT NETS DGAC AD (B)R1 DGCA/ATR 42/66 AIR LIQUIDE - SMOKE HOOD TYPE 15-40F DGAC AD (AB)R1 DGCA/ATR 42/67 MLG ACTUATOR FITTING - FITTING BOLTS ON FUSELAGE DGAC AD (B)R1 DGCA/ATR 42/68 SICMA AEROSEAT - PASSENGER SEATS LEG COLLAR DGAC AD (AB) DGCA/ATR 42/69 KARMAN WING FAIRING PANELS FASTENERS DGAC AD (B) DGCA/ATR 42/70 FLIGHT CONTROLS - RUDDER DGAC AD (B)R1 DGCA/ATR 42/71 ENGINE MOUNT AND UPPER ENGINE FAIRING STIFFENER FOULING DGAC AD (B) DGCA/ATR 42/72 ROTRON RECIRCULATION FAN DGAC AD (B)
4 DGCA/ATR 42/73 EXTERNAL WINGS - INNER SKIN SURFACE / REAR SPAR JUNCTION DGAC AD (B) DGCA/ATR 42/74 GPS NAVIGATION SYSTEM DGAC AD (AB) DGCA/ATR 42/75 ICING CONDITIONS DGAC AD R2 DGCA/ATR 42/76 SEVERE ICING CONDITIONS DGAC AD (B)R1 DGCA/ATR 42/77 PURITAN BENNETT - PASSENGER MASKS DGAC AD IMP(AB) DGCA/ATR 42/78 STRUCTURE - RESULT OF FATIGUE TESTS DGAC AD (B) DGCA/ATR 42/79 TRANSPONDER SYSTEM MODE A,C & S DGAC AD (B) DGCA/ATR 42/80 LANDING GEAR UPLOCK BOXES DGAC AD (B) DGCA/ATR 42/81 VIEW OF DGCA/NEW MISC/44 DGCA/ATR 42/82 FIRE PROTECTION- FIRE HANDLES DGAC AD (B)R1 DGCA/ATR 42/83 ENGINES CONTROL 'LOW PITCH' DGAC AD (B) DGCA/ATR 42/84 TAKE OFF FOLLOWING A/C DEICING BY DE-ICING FLUIDS DGAC AD (B)R2 DGCA/ATR 42/85 ELECTRICAL SYSTEM - ENGINE START SELECTOR DGAC AD (B) DGCA/ATR 42/86 NAVIGATION SYSTEMS FM IMMUNITY DGAC AD (AB)R2 DGCA/ATR 42/87 ICING CONDITIONS DGAC AD (B) DGCA/ATR 42/88 ATPCS TEST SELECTOR DGAC AD (B) DGCA/ATR 42/89 FLIGHT CONTROLS - NORMAL PITCH TRIM SWITCHES DGAC AD (B) DGCA/ATR 42/90 WING TO FUSELAGE FAIRING PANEL DGAC AD (B)R1 DGCA/ATR 42/91 WALTER KIDDE FIRE EXTINGUISHER BOTTLE OAS CARTRIDGES DGAC AD IMP(AB) DGCA/ATR 42/92 DGCA/ATR 42/93 DGCA/ATR 42/94 VIEW OF DGCA/NEW MISC/56 VIEW OF DGCA/NEW MISC/56 EQUIPMENTS & FURNISHINGS - THERMAL/ACOUSTIC INSULATION BLANKETS -- REPLACEMENT/REMOVAL EASA AD SUPERSEDES DGAC AD F 2005-
5 DGCA/ATR 42/95 ELECTRICAL RACK 90VU WIRE BUNDLE ROUTING ON 93,94,95VU SHELVES 211 DGAC AD (B) DGCA/ATR 42/96 MAIN LANDING GEAR BARREL/SWINGING LEVER HINGE DGAC AD (B)R4 DGCA/ATR 42/97 MLG SWINGING LEVER SPACER DGAC AD (B) DGCA/ATR 42/98 COLLINS ATC MODE S DGAC AD IMP(AB)R1 DGCA/ATR 42/99 FLIGHT CONTROLS-PITCH CONTROL INTERFERENCES DGAC AD (B) DGCA/ATR 42/100 DGCA/ATR 42/101 DGCA/ATR 42/102 VIEW OF DGCA/NEW MISC/44 VIEW OF DGCA/NEW MISC/64 CANCELLED VIDE LETTER NO 9-764/06 AI(2) DATED 19/10/06, IN VIEW OF DGCA/ATR 42/133R1 DGCA/ATR 42/103 FORWARD FLIGHT ATTENDANT SEAT DGAC AD (B) DGCA/ATR 42/104 VIEW OF DGCA/ATR 42/128 DGCA/ATR 42/105 ENGINE AIR CIRCUIT REGULATION DGAC AD IMP(B) DGCA/ATR 42/106 VIEW OF DGCA/PW121/01 DGCA/ATR 42/107 ENGINE OIL CIRCUIT MANIFOLD DGAC AD (B)R1 DGCA/ATR 42/108 DGCA/ATR 42/109 DGCA/ATR 42/110 DGCA/ATR 42/111 VIEW OF DGCA/PW121/02 VIEW OF DGCA/PW121/04 VIEW OF DGCA/PW121/03
6 DGCA/ATR 42/112 DGCA/ATR 42/113 DGCA/ATR 42/114 DGCA/ATR 42/115 DGCA/ATR 42/116 VIEW OF DGCA/PW121/05 VIEW OF DGCA/PW121/06 VIEW OF DGCA/PW121/07 ENGINES - HIGH PRESSURE OIL PUMP - PRESSURE REGULATING VALVE VIEW OF DGCA/PW121/08 VIEW OF DGCA/PW127/02 DGAC AD (B) DGCA/ATR 42/117 LORAL MAIN LANDING GEAR WHEELS DGAC AD (B)R1 DGCA/ATR 42/118 MAIN LANDING GEAR WHEEL ROLLER BEARING DGAC AD (B) DGCA/ATR 42/119 GOOD YEAR TYRES DGAC AD IMP(AB)R1 DGCA/ATR 42/120 NOSE LANDING GEAR DGAC AD (B) DGCA/ATR 42/121 MAIN LANDING GEAR- SIDE BRACE LOWER ARM DGAC AD (B)R2 DGCA/ATR 42/122 MAIN LANDING GEAR- WHEEL AXLE DGAC AD (B)R1 DGCA/ATR 42/123 NOSE LANDING GEAR DGAC AD (B) DGCA/ATR 42/124 MAIN LANDING GEAR SIDE BRACE PIN DGAC AD (B) DGCA/ATR 42/125 MAIN LANDING GEAR- PINS MAGNAGHI DGAC AD (B) DGCA/ATR 42/126 PROPELLERS - PITCH CHANGE SYSTEM COMPONENT DGAC AD (B)R1 DGCA/ATR 42/127 ATTITUDE AND HEADING SYSTEM DGAC AD (B)R1 DGCA/ATR 42/128 OIL COOLING SYSTEM DGAC AD (B)R1 DGCA/ATR 42/129 MAIN LANDING GEAR SWINGING LEVER ( ATA 32 ) DGAC AD (B) DGCA/ATR 42/130(R2) LANDING GEAR - MAIN LANDING GEAR - SIDE BRACE ASSEMBLY DGAC AD F ( DGAC AD , AD & 2004-
7 DGCA/ATR 42/131 CANCELLED IN VIEW OF DGCA/ATR 42/ 130 R1 VIDE LETTER NO 9-764/03 AI(2) DATED ARE CANCELLED) DGCA/ATR 42/132R1 WINGS- OUTER WING BOXES- UPPER SKIN AND RIBS EASA AD SUPERSEDED DGAC AD F DGCA/ATR 42/133(R1) STABILIZERS- VERTICAL STABILIZER FIN TIP - INSPECTION / REPAIR / MODIFICATION EASA AD (EASA AD SUPERSEDES DGAC AD (B)R1 AND DGAC AD F ) DGCA/ATR 42/134 FUEL QUANTITY INDICATORS DGAC AD F DGCA/ATR 42/135(R1) FUEL- FUEL TANK SYSTEM WIRIING & SENSORS - MODIFICATION/REPLACEMENT - FUEL TANK SAFETY DGCA/ATR 42/136 MAIN LANDING GEAR- SHOCK ABSORBER- CROSS LOCKING BOLT OF THE ATTACHMENT PIN DGCA/ATR 42/137R1 TIME LIMITS / MAINTENANCE CHECKS --- CERTIFICATION MAINTENANCE REQUIREMENTS & CRITICAL DESIGN CONFIGURATION CONTROL LIMITATIONS ( FUEL TANK SAFETY) EASA AD R1 EASA AD E EASA AD DGCA/ATR 42/138 ELECTRICAL POWER VU ELECTRICAL HARNESS - INSPECTION EASA AD DGCA/ATR 42/139 FLIGHT CONTROLS - AILERON TAB BELLCRANK ASSEMBLY - INSPECTION DGCA/ATR 42/140 EQUIPMENT/FURNISHINGS --- THERMAL ---- ACOUSTICAL INSULATION BLANKETS ON FRAME REMOVAL DGCA/ATR 42/141 MAIN LANDING GEAR --- SIDE BRACE ASSEMBLY --- INSPECTION/MODIFICATION/REPLACEMENT DGCA/ATR 42/142 ICE & RAIN PROTECTION -- PITOT PROBE RESISTANCE & LOW CURRENT SENSOR --- INSPECTION/REPLACEMENT EASA AD EASA EAD E EASA AD EASA AD
8 DGCA/ATR 42/143 ELECTRICAL/ELECTRONIC --- REAR PRESSURE BULKHEAD AREA AND WIRE CHAFING ---INSPECTION/MODIFICATION DGCA/ATR 42/144 EQUIPMENT & FURNISHINGS --- PASSENGER SEATS --- INSPECTION/REPAIR/MODIFICATION DGCA/ATR 42/145 ELECTRICAL / ELECTRONIC --- WIRE BUNDLES IN THE REAR BAGGAGE ZONE --- PROTECTION & CLAMPING DGCA/ATR 42/146R1 WINDOWS --- COCKPIT FORWARD SIDE WINDOWS --- INSPECTIONS / REPLACEMENT DGCA/ATR 42/147 INDICATING / RECORDING SYSTEMS --- MULTI PURPOSE COMPUTER (MPC) WITH AIRCRAFT PERFORMANCE MONITORING (APM) FUNCTION -- INSTALLATION DGCA/ATR 42/148R2 FIRE PROTECTION --- HALON 1211 FIRE EXTINGUISHERS --- IDENTIFICATION / REPLACEMENT DGCA/ATR 42/149 DGCA/ATR 42/150 DGCA/ATR 42/151 DGCA/ATR 42/152 DGCA/ATR 42/153 STABILIZERS --- ELEVATOR INBOARD HINGE FITTING LOWER STOP ANGLES --- INSPECTION/REPLACEMENT FLIGHT CONTROLS --- RUDDER TAB,RUDDER PEDAL AND ELEVATOR CONTROL RODS --- INSPECTION/REPLACEMENT NACELLES / PYLONS --- ENGINE NACELLE LOWER FAIRING JUNCTION WITH UNDERWING BOX --- INSPECTION AIRWORTHINESS LIMITATION ITEMS --- STRUCTURAL SIGNIFICANT ITEM TASKS --- AMENDMENTS ICE AND RAIN PROTECTION --- PNEUMATIC ICE PROTECTION DUAL DISTRIBUTOR VALVES --- INSPECTION / REPLACEMENT DGCA/ATR 42/154R1 EQUIPMENT / FURNISHING --- TYPE III EMERGENCY EXIT DOOR --- INSPECTION / MODIFICATION DGCA/ATR 42/155R2 ELECTRICAL ROUTING ELECTRONIC RACK 90VU SHELF / ELECTRICAL HARNESS INSPECTION EASA AD EASA AD EASA AD EASA AD EASA AD EASA AD SUPERSEDED EASA AD R1 EASA AD EASA AD EASA AD EASA AD EASA AD EASA AD SUPER EASA AD EASA AD sup EASA AD R1
9 DGCA/ATR 42/156 ELECTRICAL ROUTING ELECTRONIC RACK 120VU SHELF / ELECTRICAL HARNESS INSPECTION / MODIFICATION DGCA/ATR 42/157R1 ATA 32, LANDING GEAR MAIN LANDING GEAR HINGE PIN INSPECTION / REPLACEMENT EASA AD EASA AD SUPERSEDED EASA AD DGCA/ATR 42/158R1 ATA 28, FUEL FUEL PROBES INSPECTION / REPLACEMENT EASA AD R1 DGCA/ATR 42/159 ATA 26, FIRE PROTECTION ENGINE FIRE EXTINGUISHING PIPE INSPECTION DGCA/ATR 42/160R2 ATA22, AUTO FLIGHT-AUTO PILOT AND YAW DAMPER-OPERATIONAL LIMITATIONS MASTER MINIMUM EQUIPMENT LIST-AMENDMENT DGCA/ATR42/161 DGCA/ATR42/162 DGCA/ATR42/163R1 ATA22, AUTO FLIGHT-AUTO PILOT AND YAW DAMPER-OPERATIONAL LIMITATIONS AIRCRAFT FLIGHT MANUAL-AMENDMENT ATA 33, LIGHTS-EMERGENCY EXIT-EMERGENCY POWER SUPPLY UNIT-INSPECTION/REPLACEMENT ATA-92, ELECTRIC / ELECTRONIC COMMON INSTALLATION WIRE CHAFING BEHIND CABIN SIDEWALL INSPECTION DGCA/ATR42/164R1 ATA-32, LANDING GEAR MAIN LANDING GEAR UNIVERSAL JOINT INSPECTION / REPLACEMENT DGCA/ATR42/165R1 DGCA/ATR42/166R1 ATA-05, TIME LIMITS/ MAINTENANCE CHECKS CERTIFICATION MAINTENANCE REQUIREMENTS AND AIRWORTHINESS LIMITATIONS AMENDMENTS. 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 EASA AD R1 REVISED EASA AD
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