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DGCA/ATR 42/1 FLIGHT CONTROLS-STANDBY PITCH TRIM SWITCH DGAC AD 2003-106(B) R1 DGCA/ATR 42/2 IPECO PILOT AND CO-PILOT SEATS DGAC AD 86-078-01(B)R1 DGCA/ATR 42/3 SOCEA CABIN ATTENDANT SEAT DGAC AD 86-079(B) DGCA/ATR 42/4 FLAPS -- USE OF THE 45DEGREE CONFIGURATION --- PROHIBITION/MODIFICATION EASA AD 2008-0124 DGCA/ATR 42/5 SPERRY AHRS DGAC AD 86-138-IMP(AB) & 87-046-005(B)R1 DGCA/ATR 42/6 AUTOMATIC STOP RECORDER DFDR/CVR DGAC AD 87-022-004(B) DGCA/ATR 42/7 SGU EFIS SPERRY DGAC AD 87-111-IMP(B) DGCA/ATR 42/8 ELEVATOR TRIM DGAC AD 87-155-007(B) DGCA/ATR 42/9 PROPELLER BRAKE CONTROL SYSTEM DGAC AD 87-156-008(B)R1 DGCA/ATR 42/10 AUTO PILOT ROLL ACTUATOR PROTECTION DGAC AD 87-173-009(B) DGCA/ATR 42/11 FUEL QUANTITY INDICATION DGAC AD 88-051-010(B)R2 DGCA/ATR 42/12 RUDDER CONTROL CHANNEL CABLES DGAC AD 88-070-011(B) DGCA/ATR 42/13 ENGINE AND PROPELLER FLEXIBLE CONTROL SHAFTS DGAC AD 88-080-012(B) DGCA/ATR 42/14 NAVIGATION ADC - SGU - AHRS DGAC AD 88-092-013(B) DGCA/ATR 42/15 PROPELLER BRAKE CONTROL PUSHBUTTON REPLACEMENT DGAC AD 88-147-015(B) DGCA/ATR 42/16 CARGO SMOKE DETECTOR TEST CIRCUIT DGAC AD 88-186-016(B)R1 DGCA/ATR 42/17 STRUCTURE MODIFICATIONS RESULTING FROM FATIGUE TESTS DGAC AD 89-017-017(B)R2 DGCA/ATR 42/18 PITCH TRIM DGAC AD 89-033-019(B)R1 DGCA/ATR 42/19 MLG RETRACTION JACKS FITTING BOLTS DGAC AD 89-067-020(B)R2 DGCA/ATR 42/20 AILERON TAB INBOARD HINGE PIN DGAC AD 89-077-021(B)R2 DGCA/ATR 42/21 COCKPIT VOICE RECORDER AUTOMATIC CUT OFF DGAC AD 89-093-022(B) DGCA/ATR 42/22 AHRS HONEYWELL AH600 DGAC AD 89-116-IMP(AB)R1 DGCA/ATR 42/23 ICING CONDITIONS PROCEDURES DGAC AD 89-120-023(B)R1

DGCA/ATR 42/24 PAX/CREW DOOR LIFTING DEVICE DGAC AD 89-138-024(B)R1 DGCA/ATR 42/25 ENGINE FIRE EXTINGUISHING SYSTEM DGAC AD 89-197-025(B)R1 DGCA/ATR 42/26 NOSE LANDING GEAR RETRACTING MECHANISM DGAC AD 90-028-026(B) DGCA/ATR 42/27 EMERGENCY LIGHTING DGAC AD 90-029-027(B) DGCA/ATR 42/28 PROPELLER BRAKE DGAC AD 90-030-028(B)R1 DGCA/ATR 42/29 MAIN FRAMES DGAC AD 90-109-029(B) DGCA/ATR 42/30 EMERGENCY OXYGEN SYSTEMOF THE CABIN ATTENDANTS DGAC AD 90-155-030(B)R1 DGCA/ATR 42/31 WHEEL WELL BAY DGAC AD 90-163-031(B) DGCA/ATR 42/32 HYDRAULIC SYSTEM LOW PRESSURE WARNING DGAC AD 90-193-032(B)R2 DGCA/ATR 42/33 FLIGHT CONTROL DGAC AD 90-201-033(B)R2 DGCA/ATR 42/34 FLIGHT CONTROLS DGAC AD 91-068-039(B) DGCA/ATR 42/35 TCAS COLLINS II (or 94) DGAC AD 91-131-IMP(AB)R1 DGCA/ATR 42/36 EROS OXYGEN MASKS DGAC AD 91-176(AB) DGCA/ATR 42/37 FLIGHT CONTROLS DGAC AD 91-214-042(B) DGCA/ATR 42/38 ENGINE AND PROPELLER FLEXIBLE CONTROLS DGAC AD 91-216-043(B)R1 DGCA/ATR 42/39 AUTO PILOT DGAC AD 91-237-044(B) DGCA/ATR 42/40 AFT RH SERVICE DOOR COMMERCIAL FURNISHINGS DGAC AD 92-043-045(B) DGCA/ATR 42/41 AERAZUR LIFE JACKETS PACKING POUCH DGAC AD 92-051(AB)R1 DGCA/ATR 42/42 ECE PUSH-BUTTON ASNE 0276C DGAC AD 92-122-047(B) DGCA/ATR 42/43 PITCH CONTROL DGAC AD 92-133-048(B)R1 DGCA/ATR 42/44 AUTO PILOT DGAC AD 92-197-049(B) DGCA/ATR 42/45 COLLINS VHF - 20B TRANCEIVER IDENTIFICATION PLATE DGAC AD 93-050(AB)R1 DGCA/ATR 42/46 COLLINS MODE 'S' ATC TRANSPONDER DGAC AD 93-054-IMP(AB) DGCA/ATR 42/47 OUTER WINGS DGAC AD 93-190-051(B) DGCA/ATR 42/48 PITCH TRIM CONTROLS DGAC AD 93-205-052(B)

DGCA/ATR 42/49 FLIGHT CONTROL RODS DGAC AD 94-003-053(B) DGCA/ATR 42/50 AILERON TRIM CONTROL DGAC AD 94-004-054(B) DGCA/ATR 42/51 PURITAN BENNETT CREW MEMBER PROTECTIVE BREATHING EQUIPMENT NECK SEAL DGAC AD 94-028-IMP(AB) DGCA/ATR 42/52 NOSE LANDING GEAR NARDI HINGE PINS DGAC AD 94-005-055(B) DGCA/ATR 42/53 KARMAN WING FAIRINGS PANELS ATTACHMENT CLIPS DGAC AD 94-162-056(B) DGCA/ATR 42/54 ALLIED SIGNAL AEROSPACE CO (BENDIX / KING) TCAS II SYSTEMS DGAC AD 94-232-IMP(AB) DGCA/ATR 42/55 COLLINS TCAS II SYSTEMS DGAC AD 94-233-IMP(AB) DGCA/ATR 42/56 PROTECTION OF THE ELECTRICAL HARNESS IN FRONT AREA DGAC AD 95-103-059(B) DGCA/ATR 42/57 TIME LIMITS DGAC AD 95-104-060(B)R1 DGCA/ATR 42/58 WINDSHIELD, FRAME NODE 5 DGAC AD 95-126-061(B) DGCA/ATR 42/59 WINGS CORROSION ON REAR SPAR DGAC AD 95-127-062(B) DGCA/ATR 42/60 ENGINE NACELLE DRAIN SYSTEM DGAC AD 96-109-063(B) DGCA/ATR 42/61 FUSELAGE STRINGER 6, JUNCTION CLIPS TO FRAME 34 DGAC AD 96-132-065(B) DGCA/ATR 42/62 DE-ICING PROCEDURES AND PROTECTIONS IMPROVEMENT DGAC AD 96-208-067(B)R1 DGCA/ATR 42/63 STANDBY HORIZON POWER SUPPLY DGAC AD 96-230-066(B) DGCA/ATR 42/64 STICK SHAKER/PUSHER SYSTEM DGAC AD 96-256-068(B) DGCA/ATR 42/65 FORWARD CARGO COMPARTMENT NETS DGAC AD 96-289-069(B)R1 DGCA/ATR 42/66 AIR LIQUIDE - SMOKE HOOD TYPE 15-40F DGAC AD 97-088(AB)R1 DGCA/ATR 42/67 MLG ACTUATOR FITTING - FITTING BOLTS ON FUSELAGE DGAC AD 97-115-070(B)R1 DGCA/ATR 42/68 SICMA AEROSEAT - PASSENGER SEATS LEG COLLAR DGAC AD 97-134(AB) DGCA/ATR 42/69 KARMAN WING FAIRING PANELS FASTENERS DGAC AD 97-159-071(B) DGCA/ATR 42/70 FLIGHT CONTROLS - RUDDER DGAC AD 97-328-072(B)R1 DGCA/ATR 42/71 ENGINE MOUNT AND UPPER ENGINE FAIRING STIFFENER FOULING DGAC AD 98-069-073(B) DGCA/ATR 42/72 ROTRON RECIRCULATION FAN DGAC AD 98-070-074(B)

DGCA/ATR 42/73 EXTERNAL WINGS - INNER SKIN SURFACE / REAR SPAR JUNCTION DGAC AD 98-147-075(B) DGCA/ATR 42/74 GPS NAVIGATION SYSTEM DGAC AD 99-258(AB) DGCA/ATR 42/75 ICING CONDITIONS DGAC AD 99-014-076 R2 DGCA/ATR 42/76 SEVERE ICING CONDITIONS DGAC AD 99-165-077(B)R1 DGCA/ATR 42/77 PURITAN BENNETT - PASSENGER MASKS DGAC AD 99-234-IMP(AB) DGCA/ATR 42/78 STRUCTURE - RESULT OF FATIGUE TESTS DGAC AD 2000-337-079(B) DGCA/ATR 42/79 TRANSPONDER SYSTEM MODE A,C & S DGAC AD 2000-080(B) DGCA/ATR 42/80 LANDING GEAR UPLOCK BOXES DGAC AD 2000-189-078(B) DGCA/ATR 42/81 VIEW OF DGCA/NEW MISC/44 DGCA/ATR 42/82 FIRE PROTECTION- FIRE HANDLES DGAC AD 2000-281-078(B)R1 DGCA/ATR 42/83 ENGINES CONTROL 'LOW PITCH' DGAC AD 2000-436-080 (B) DGCA/ATR 42/84 TAKE OFF FOLLOWING A/C DEICING BY DE-ICING FLUIDS DGAC AD 2000-449-082(B)R2 DGCA/ATR 42/85 ELECTRICAL SYSTEM - ENGINE START SELECTOR DGAC AD 2000-454-081(B) DGCA/ATR 42/86 NAVIGATION SYSTEMS FM IMMUNITY DGAC AD 2001-023(AB)R2 DGCA/ATR 42/87 ICING CONDITIONS DGAC AD 2001-044-083(B) DGCA/ATR 42/88 ATPCS TEST SELECTOR DGAC AD 2001-214-084(B) DGCA/ATR 42/89 FLIGHT CONTROLS - NORMAL PITCH TRIM SWITCHES DGAC AD 2001-387-085(B) DGCA/ATR 42/90 WING TO FUSELAGE FAIRING PANEL DGAC AD 2001-554-087(B)R1 DGCA/ATR 42/91 WALTER KIDDE FIRE EXTINGUISHER BOTTLE OAS CARTRIDGES DGAC AD 2001-569-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 2007-0164 SUPERSEDES DGAC AD F 2005-

DGCA/ATR 42/95 ELECTRICAL RACK 90VU WIRE BUNDLE ROUTING ON 93,94,95VU SHELVES 211 DGAC AD 2002-090-092(B) DGCA/ATR 42/96 MAIN LANDING GEAR BARREL/SWINGING LEVER HINGE DGAC AD 96-294(B)R4 DGCA/ATR 42/97 MLG SWINGING LEVER SPACER DGAC AD 2001-614-089(B) DGCA/ATR 42/98 COLLINS ATC MODE S DGAC AD 2002-275-IMP(AB)R1 DGCA/ATR 42/99 FLIGHT CONTROLS-PITCH CONTROL INTERFERENCES DGAC AD 2002-431(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 2002-539(B) DGCA/ATR 42/104 VIEW OF DGCA/ATR 42/128 DGCA/ATR 42/105 ENGINE AIR CIRCUIT REGULATION DGAC AD 89-011-IMP(B) DGCA/ATR 42/106 VIEW OF DGCA/PW121/01 DGCA/ATR 42/107 ENGINE OIL CIRCUIT MANIFOLD DGAC AD 89-042-018(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

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 2002-071-091(B) DGCA/ATR 42/117 LORAL MAIN LANDING GEAR WHEELS DGAC AD 87-091-006(B)R1 DGCA/ATR 42/118 MAIN LANDING GEAR WHEEL ROLLER BEARING DGAC AD 88-135-014(B) DGCA/ATR 42/119 GOOD YEAR TYRES DGAC AD 88-187-IMP(AB)R1 DGCA/ATR 42/120 NOSE LANDING GEAR DGAC AD 91-005-36(B) DGCA/ATR 42/121 MAIN LANDING GEAR- SIDE BRACE LOWER ARM DGAC AD 91-033-038(B)R2 DGCA/ATR 42/122 MAIN LANDING GEAR- WHEEL AXLE DGAC AD 91-081-040(B)R1 DGCA/ATR 42/123 NOSE LANDING GEAR DGAC AD 91-157-041(B) DGCA/ATR 42/124 MAIN LANDING GEAR SIDE BRACE PIN DGAC AD 95-051-058(B) DGCA/ATR 42/125 MAIN LANDING GEAR- PINS MAGNAGHI DGAC AD 96-131-064(B) DGCA/ATR 42/126 PROPELLERS - PITCH CHANGE SYSTEM COMPONENT DGAC AD 2002-070-090(B)R1 DGCA/ATR 42/127 ATTITUDE AND HEADING SYSTEM DGAC AD 1987-046-005(B)R1 DGCA/ATR 42/128 OIL COOLING SYSTEM DGAC AD 1986-085-002(B)R1 DGCA/ATR 42/129 MAIN LANDING GEAR SWINGING LEVER ( ATA 32 ) DGAC AD 2003-376(B) DGCA/ATR 42/130(R2) LANDING GEAR - MAIN LANDING GEAR - SIDE BRACE ASSEMBLY DGAC AD F 2005-106 ( DGAC AD 2005-054, AD 2004-006 & 2004-

DGCA/ATR 42/131 CANCELLED IN VIEW OF DGCA/ATR 42/ 130 R1 VIDE LETTER NO 9-764/03 AI(2) DATED 06-04-05 078 ARE CANCELLED) DGCA/ATR 42/132R1 WINGS- OUTER WING BOXES- UPPER SKIN AND RIBS EASA AD 2017-0244 SUPERSEDED DGAC AD F 2004-191 DGCA/ATR 42/133(R1) STABILIZERS- VERTICAL STABILIZER FIN TIP - INSPECTION / REPAIR / MODIFICATION EASA AD 2006-0303 (EASA AD SUPERSEDES DGAC AD 2002-506(B)R1 AND DGAC AD F 2005-059) DGCA/ATR 42/134 FUEL QUANTITY INDICATORS DGAC AD F 2005-160 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 2007-0226R1 EASA AD 2006-0216E EASA AD 2009-0242 DGCA/ATR 42/138 ELECTRICAL POWER - 120 VU ELECTRICAL HARNESS - INSPECTION EASA AD 2006-0283 DGCA/ATR 42/139 FLIGHT CONTROLS - AILERON TAB BELLCRANK ASSEMBLY - INSPECTION DGCA/ATR 42/140 EQUIPMENT/FURNISHINGS --- THERMAL ---- ACOUSTICAL INSULATION BLANKETS ON FRAME 24 ---- 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 2006-0376 EASA EAD 2007-0106 - E EASA AD 2007-0263 EASA AD 2007-0179

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 2008-0062 EASA AD 2008-0097 EASA AD 2008-0218 EASA AD 2013-0087 EASA AD 2009-0170 EASA AD 2010-0061 SUPERSEDED EASA AD 2009-0276R1 EASA AD 2010-0138 EASA AD 2012-0064 EASA AD 2012-0160 EASA AD 2012-0193 EASA AD 2013-0032 EASA AD 2015-0018 SUPER EASA AD 2013-0280 EASA AD 2015-0171 sup EASA AD 2014-0052R1

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 2014-0056 EASA AD 2016-0135 SUPERSEDED EASA AD 2014-0074 DGCA/ATR 42/158R1 ATA 28, FUEL FUEL PROBES INSPECTION / REPLACEMENT EASA AD 2014-0075R1 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 2014-0144R1 EASA AD 2015-0237R1 REVISED EASA AD 2015-0237 SUPERSEDED EASA AD 2015-0230 EASA AD 2016-0046 EASA AD 2016-0070 EASA AD 2018-0105 SUPERSEDED EASA AD 2017-0118 EASA AD 2018-0080 SUPERSEDED EASA AD 2017-0172 EASA AD 2017-0222R1 REVISED EASA AD 2017-0222 EASA AD 2017-0221R1 REVISED EASA AD 2017-0221

DGCA/ATR42/167 CANCELLED: ATA 05 AIRWORTHINESS LIMITATION ITEMS STRUCTURAL SIGNIFICANT ITEM TASKS AMENDMENTS. EASA AD 2012-0193-CN DGCA/ATR42/168 CANCELLED: ATA 05 - TIME LIMITS / MAINTENANCE CHECKS CERTIFICATION MAINTENANCE REQUIREMENTS AND CRITICAL DESIGN CONFIGURATION CONTROL LIMITATIONS [FUEL TANK SAFETY] EASA AD 2009-0242-CN