DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320 family/1 RIGGING/ADJUSTMENT OF THE RAM AIR TURBINE DOORS. BVAD 89-160-003(B) R2 & AIRBUS SB A320-29-1030. AS IN AD AND SB. AS IN AD AND SB. DGCA/A320 family/2 STANDBY GENERATOR CONTROL UNIT. BVAD 89-198-004(B) R1 AS IN AD AS IN AD DGCA/A320 family/3 REPLACEMENT OF STANDBY TRANSFORMER/RECTIFIER. FAA AD 90-02-15 AS IN AD AS IN AD DGCA/A320 family/4 FUEL PROBES. BVAD 90-017-005(B) & AIRBUS SB A320-28-1024. AS IN AD AND SB. AS IN AD AND SB. DGCA/A320 family/5 ANGLE OF ATTACK SENSORS SIMULTANEOUS POSITIONING AT HIGH ANGLE. BVAD 90-018-006(B) R2 & AIRBUS SB A320-34-1012 AND AIRBUS SB ìA320-34- 1013. AS IN AD AND SB. AS IN AD AND SB. DGCA/A320 family/6 INTERRUPTION OF LANDING GEAR RETRACTION. BVAD 90-026-007(B) R2 AS IN AD. AS IN AD. DGCA/A320family/7 PASSENGER ADDRESS SYSTEM - CIDS. BVAD 90-076-008(B) R1 AS IN AD. AS IN AD. DGCA/A320 family/8 AIR CONDITIONING - IMPROVE ADIRU DRAINAGE. AIRBUS SB A320-21-1023. AS IN SB. AS IN SB. DGCA/A320 family/9 AUXILIARY POWER UNIT NOTE: SINCE THE REQUIREMENTS OF THE FAA AD ARE MORE STRINGENT ìTHESE ARE TO BE FOLLOWED. FAA AD 92-27-14 & BVAD T90-102-011(B) R1 AND GARRETT GTCP ì36-49-6549 DT. FEB. 28 '1992. AS IN AD AND SB. AS IN AD AND SB. DGCA/A320 family/10 CANCELLED ACCORDING TO BVAD 90-107-013(B) R4. DGCA/A320 family/11 EMERGENCY OXYGEN CONTAINERS. BVAD 90-108-012(B) R1 & AIRBUS SB A320-35-1002 R1 AS IN AD. AS IN AD. DGCA/A320 family/12 TRIMMABLE HORIZONTAL STABILIZER (THS) ACTUATOR CONTROL JAMMING. BVAD 90-138-014(B) R1 & AIRBUS SB A320-27-1031 & AIRBUS SB ìA320-27-1032. AS IN AD & SB. AS IN AD & SB. DGCA/A320 family/13 LOW PRESSURE FIRE FUEL SHUT-OFF VALVE. BVAD 90-190-015(B) AS IN AD. AS IN AD. DGCA/A320 family/14 AUTOMATIC LANDING. BVAD 91-061-016(B0 R2 AND A320-22-1018 R1 ; FAA AD 92-19-13; BVAD ì93-203- 049(B); SB A320-34-1008. AS IN ADs AND SBs. AS IN ADs AND SBs. DGCA/A320 family/15 TRIMMABLE HORIZONTAL SURFACE RALAY 36 CE 3 BVAD 91-119-017(B) R1. AS IN AD. AS IN AD. DGCA/A320 family/16 HYDRAULIC FIRE SHUTOFF VALVE. BVAD 91-152-019(B) AOT 29- 04.JUNE 1, 1991. AS IN AD. AS IN AD. DGCA/A320 family/17 OVERWING ESACPE SLIDE. BVAD 91-153-018(B) AS IN AD. AS IN AD.
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DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320 family/1 RIGGING/ADJUSTMENT OF THE RAM AIR TURBINE
DOORS. BVAD 89-160-003(B) R2 & AIRBUS SB A320-29-1030.
AS IN AD AND SB.
AS IN AD AND SB.
DGCA/A320 family/2 STANDBY GENERATOR CONTROL UNIT. BVAD 89-198-004(B) R1 AS IN AD AS IN AD DGCA/A320 family/3 REPLACEMENT OF STANDBY
TRANSFORMER/RECTIFIER. FAA AD 90-02-15 AS IN AD AS IN AD
DGCA/A320 family/4 FUEL PROBES. BVAD 90-017-005(B) & AIRBUS SB A320-28-1024.
AS IN AD AND SB.
AS IN AD AND SB.
DGCA/A320 family/5 ANGLE OF ATTACK SENSORS SIMULTANEOUS POSITIONING AT HIGH ANGLE.
BVAD 90-018-006(B) R2 & AIRBUS SB A320-34-1012 AND AIRBUS SB ìA320-34-1013.
AS IN AD AND SB.
AS IN AD AND SB.
DGCA/A320 family/6 INTERRUPTION OF LANDING GEAR RETRACTION. BVAD 90-026-007(B) R2 AS IN AD. AS IN AD. DGCA/A320family/7 PASSENGER ADDRESS SYSTEM - CIDS. BVAD 90-076-008(B) R1 AS IN AD. AS IN AD. DGCA/A320 family/8 AIR CONDITIONING - IMPROVE ADIRU DRAINAGE. AIRBUS SB A320-21-1023. AS IN SB. AS IN SB. DGCA/A320 family/9 AUXILIARY POWER UNIT
NOTE: SINCE THE REQUIREMENTS OF THE FAA AD ARE MORE STRINGENT ìTHESE ARE TO BE FOLLOWED.
FAA AD 92-27-14 & BVAD T90-102-011(B) R1 AND GARRETT GTCP ì36-49-6549 DT. FEB. 28 '1992.
AS IN AD AND SB.
AS IN AD AND SB.
DGCA/A320 family/10 CANCELLED ACCORDING TO BVAD 90-107-013(B) R4.
DGCA/A320 family/12 TRIMMABLE HORIZONTAL STABILIZER (THS) ACTUATOR CONTROL JAMMING.
BVAD 90-138-014(B) R1 & AIRBUS SB A320-27-1031 & AIRBUS SB ìA320-27-1032.
AS IN AD & SB.
AS IN AD & SB.
DGCA/A320 family/13 LOW PRESSURE FIRE FUEL SHUT-OFF VALVE. BVAD 90-190-015(B) AS IN AD. AS IN AD. DGCA/A320 family/14 AUTOMATIC LANDING. BVAD 91-061-016(B0 R2 AND
A320-22-1018 R1 ; FAA AD 92-19-13; BVAD ì93-203-049(B); SB A320-34-1008.
AS IN ADs AND SBs.
AS IN ADs AND SBs.
DGCA/A320 family/15 TRIMMABLE HORIZONTAL SURFACE RALAY 36 CE 3 BVAD 91-119-017(B) R1. AS IN AD. AS IN AD. DGCA/A320 family/16 HYDRAULIC FIRE SHUTOFF VALVE. BVAD 91-152-019(B) AOT 29-
04.JUNE 1, 1991. AS IN AD. AS IN AD.
DGCA/A320 family/17 OVERWING ESACPE SLIDE. BVAD 91-153-018(B) AS IN AD. AS IN AD.
DGCA/A320 family/20 ELEVATOR SERVOCONTROLS. BVAD 91-272-023(B) R2 AND AIRBUS SB A320-27-1043 R1 AND ìA320-27-1048
AS IN AD AND SB.
AS IN AD AND SB
DGCA/A320family/21 INSTALLATION OF A NYLON INSULATION PLATE AND NEW SUPPORT BRACKET ìASSEMBLIES IN THE WING TANKS.
BVAD 92-048-024(B) AND FAA AD 93-10-03 AND AIRBUS A320-28-1040 R1 ìDT. 3/04/1992 REV. 3 DATED JAN. 15TH '1993
AS IN AD AND SBS.
AS IN ADS AND SBS.
DGCA/A320 family/22 AUTOAMATIC LANDING IN CATEGORY III CONDITIONS. BVAD 89-100-002(B) R1. AS IN AD. AS IN AD. DGCA/A320 family/23 REINFORCEMENT OF NOSE LANDING GEAR WHEELS. BVAD 92-164-026(B) AND SB
A320-32-1061 REV. 3 AND FAA 93-18-02
AS IN ADS AND SB
AS IN ADS AND SB.
DGCA/A320 family/24 CANCELLED IN VIEW OF LETTER NO. 9-412/91-AI(2) DT. 12/02/93
DGCA/A320 family/25R1 FUSELAGE --- BELLY FAIRING AND KEEL BEAM SIDE PANEL ATTACHMENT ANGLES ---- INSPECTION / REPLACEMENT / REPAIR
EASA AD 2013-0122 AS IN AD AND SB.
AS IN AD AND SB.
DGCA/A320 family/26 WING-INSPECTION OF REAR SPAR BETWEEN RIBS 1&2
& 25GG. BVAD 93-163-043(B) & AIRBUS SB A320-32-1115.
AS IN AD & SB.
AS IN AD & SB.
DGCA/A320 family/42 FUEL SYSTEM ELECTRICAL WIRING ATTACHMENT CLIPS AT RIB 6.
BVAD 93-191-047(B) & AIRBUS SB A320-28-1052R2. FAA AD 96-18-12.
AS IN AD & SB.
AS IN AD & SB.
DGCA/A320 family/43 JAMMING OF PASSENGER DOORS. BVAD 93-207-048(B)R1 & AIRBUS SB A320-52-1027 A320-52-1047.
AS IN AD & SB.
AS IN AD & SB.
DGCA/A320 family/44 REPETITIVE INSPECTION OF RIVET HEADS AT SKIN TO FRAME JUNCTION OF ìTHE FUSELAGE AND REPLACEMENT OF DISCREPANT RIVETS WITH HIGH ìSTRENGTH BOLTS.
FAAD 94-03-04 & AIRBUS A320-53-1036 A320-53-1010R3.
AS IN AD & SB.
AS IN AD & SB.
DGCA/A320 family/45(R1) INSPECTION & MODIFICATION OF THE MLG FORWARD PINTLE PIN CROSS BOLT.
DGAC AD 2000-428-153(B)(R1)
AS IN AD & SB.
AS IN AD & SB.
DGCA/A320 family/46 THRUST REVERSER CHECK VALVE. BVAD 94-059-054(B) & AIRBUS SB A320-29-1048R1 OR ANY FURTHER ìAPPROVED REV.
AS IN AD & SB.
AS IN AD & SB.
DGCA/A320 family/47 CARGO FIRE EXTINGUISHER BOTTLE ELECTRICAL CONNECTIONS.
BVAD 94-056-051(B) & AIRBUS AOT 26-10 & SB A320-26-1020.
AS IN AD & SB.
AS IN AD & SB.
DGCA/A320 family/48 IAE V2500- AI ENGINE FIRE EXTINGUISHER DISTRIBUTION PIPE.
BVAD 94-058-053(B)R1 &AIRBUS AOT 26-11 AND AIRBUS SB ìA320-26-1032.
AS IN AD & SB.
AS IN AD & SB.
DGCA/A320 family/49 CANCELLED VIDE 9-413/03 AI(2) DATED 24-09-04 IN VIEW OF DGCA/A320/116R1
DGCA/A320 family/50 FUSELAGE INSPECTION -LOWER FORWARD FUSELAGE CORNER OF SLIDING ìWINDOW FRAME AT FRAME 4.
BVAD 94-166-056(B) & AIRBUS SB A320-53-1082;A320-53-1044.
AS IN AD & SB.
AS IN AD & SB.
DGDC/A320 family/51 SEALING OF FIRE WALL. BVAD 94-167-057(B) & AIRBUS SB A320-7B-1009.
AS IN AD & SB.
AS IN AD & SB.
DGCA/A320 family/52 SMOKE DETECTION IN LAVOTRIES. BVAD 94-168-058(B) & AIRBUS AOT 26-12. AND BVAD 96-007-073(B).
AS IN AD & AOT.
AS IN AD & AOT.
DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320 family/53 REMOVAL OF THE GIRTBAR VISUAL INDICATOR ON
PASSENGER EXIT DOORS ìOR MODIFICATION OF THE LANYARD CONNECTING THE SURVIVAL KIT TO THE ìSLIDE RAFT.
DGCA/A320 family/55 PASSENGER DOOR SAFETY PIN GREASING (ATA 52) DGAC AD 1999-148-130 (B) AS IN AD & SB AS IN AD & SB DGCA/A320 family/56 TO PREVENT A DELAY IN SENSING BY THE AIR-TO
GROUND LOGIC SYSTEM. FAAAD 94-23-06. AS IN AD AS IN AD.
DGCA/A320 family/57 STANDS CANCELLED.
DGCA/A320 family/58 TO PREVENT LOSS OF BRAKE EFFECTIVENESS DURING A HIGH ENERGY ìREJECTED TAKE OFF.(RTO)
DGCA/A320 family/69 TO PREVENT FATIGUE RELATED CRACKING AT THE MOUNTING HINGE OF THE ìAILERON SUPPORT FRAMES OF THE WINGS WHICH COULD RESULT IN LOSS OF ìTHE AILERON CONTROL SURFACE.
FAA AD 95-24-07 & SB A320-57-1002 REV1, DATED MAY 12, 1993.
AS IN AD AND SB.
AS IN AD AND SB.
DGCA/A320 family/70 TO PREVENT INITIATION & PROPAGATION OF FATIGUE CRACKING IN THE ìPINTLE PINS OF MAIN LANDING GEAR WHICH COULD LEAD TO THE FAILURE ìOF THE PINTLE PINS.
FAA AD 95-22-10 & AI SB A320-32-1024 DATED JAN 29, 1990.
AS IN AD & SB.
AS IN AD & SB.
DGCA/A320 family/71 IMPROVEMENT OF AVIONIC PROTECTION FROM TRICKLING WATER HATCH DOOR ìSEALING.
BVAD 96-011-075(B) & AI SB A320-53-1070.
AS IN AD & SB.
AS IN AD & SB.
DGCA/A320 family/72 FUSELAGE REINFORCEMENT OF THE STRUCTURE AT SECTION 18.
DGCA/A320 family/73 IMPROVEMENT OF AVIONIC PROTECTION FROM TRICKLING WATER 90 & 91VUS ìPROTECTION.
BVAD 96-040-076(B) & SB A320-53-1110.
AS IN AD & SB.
AS IN AD & SB.
DGCA/A320 family/74 MAIN LANDING GEAR FREE FALL EXTENSION SYSTEM.
BVAD 96-053-077(B) & AOT 53-08.
AS IN AD & AOT.
AS IN AD & AOT.
DGCA/A320 family/75 TO PREVENT ELECTRICAL OVERVOLTAGE OF THE RELAYS WHICH COULD ìRESULT IN LOSS OF BRAKING /STEERING CONTROL UNIT.
FAA AD 96-04-06 & Airbus SB A320-32-1115R2 dtd Sept 21, 1994.
AS IN AD & SB.
AS IN AD & SB.
DGCA/A320 family/76 CANCELLED VIDE 9-413/03 AI(2) DATED 24-09-04 IN VIEW OF DGCA/A320/118
DGCA/A320 family/77 ACTIVATION OF THE SPOILER FUNCTION "PHASED LIFT DUMPING" (PLD).
BVAD 96-169-081(B). AS IN AD. AS IN AD.
DGCA/A320 family/78 FUEL PUMP STRAINER. BVAD 96-170-082(B). AS IN AD. AS IN AD. DGCA/A320 family/79 SLIDE/SLIDE RAFT RELEASE CABLE. BVAD 96-171-083(B). AS IN AD. AS IN AD. DGCA/A320 family/80 COLLINS RADIO-ALTIMETER ANTENNAS. BVAD 96-172-084(B). AS IN AD. AS IN AD.
DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320 family/81 CAPACITOR OF THE LANDING GEAR RETRACTION
CONTROL CIRCUIT. BVAD 96-187-085(B)R2. AS IN AD. AS IN AD.
DGCA/A320 family/82R1 INSPECTION OF GUSSET FRAME ATTACHMENT HOLES OF DOOR FRAME FR66
EASA AD 2017-0128 SUPERSEDED DGAC AD 1996-234-087(B)R1
AS IN AD. AS IN AD.
DGCA/A320 family/83 FUSELAGE INSPECTION LONITUDNAL FLOOR BEAMS AT FRAME 43.
BVAD 96-236-089(B). AS IN AD. AS IN AD.
DGCA/A320 family/84 FUSELAGE INSPECTION CONNECTING ANGLE BETWEEN FRAME 56 AND FRAME ìSUPPORT AT STRINGER 38.
BVAD 96-237-090(B). AS IN AD. AS IN AD.
DGCA/A320 family/85 FUSELAGE - INSPECTION OF FRAME 60 AND 62 AT BULK CARGO DOOR ìFRAME.
BVAD 96-238-091(B). AS IN AD. AS IN AD.
DGCA/A320 family/86 A.P.I.C AUXILLARY POWER UNIT APIC APS 3200 SOFTWARE.
DGCA/A320 family/88 CANCELLED REFER DGCA AD 2002-340 (R1). DGAC AD 2002-340(R1) AS IN AD. AS IN AD. DGCA/A320 family/89 LORAL DFDR F800 DAMPING RACK INSTALLATION. BVAD 96-272-098(B)R1. AS IN AD. AS IN AD. DGCA/A320 family/90 CANCELLED VIDE 9-413/03 AI(2) DATED 24-09-04 IN
VIEW OF DGCA/A320/64R1
DGCA/A320 family/91 STANDS CANCELLED.
DGCA/A320 family/92 REINFORCEMENT OF TAIL SECTION OF FUSELAGE AT FRAMES 68&69
FAA AD 97-08-04 AS IN AD A S IN AD
DGCA/A320 family/93 AVOID POSSIBLE UNCOMMANDED RETRACTION OF SLATS & /ON FLAGS DUE TO ìCOMMANDED AND MULFUNCTION
BVAD 97-085-099(B) AS IN AD AS IN AD
DGCA/A320 family/94 TO DETECT FATIGUE CRACKS ON THE PRESSURIZED FLOOR PICH - UP ANGLE ìON REAR SPAN WHICH COULD AFFECT THE STRUCTURAL INTIGUTY OF ìAIRPLANE.
BVAD 97-004-097(B) AS IN AD AS IN AD
DGCA/A320 family/95 FLIGHT MANAGEMENT GUIDANCE SYSTEM (F M G S) INSTALLATION OF A NEW CALCULATOR
DGAC AD 1999-411-140(B)R1 AS IN AD AS IN AD
DGCA/A320 family/96 PROBE HEAT COMPUTER BVAD 97-203-102(R1) AS IN AD AS IN AD
DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320 family/97 TOILET RINSE VALUE BVAD 97-269-103(B) AS IN AD AS IN AD DGCA/A320 family/98R1 WINGS – CENTRE WING BOX LOWER SURFACE PANEL
– INSPECTION / REPAIR EASA AD 2014-0065 SUPERSEDURE
AS IN AD AS IN AD
DGCA/A320 family/99R2 WINGS – FRONT SPAR VERTICAL STRINGERS – INSPECTION
EASA AD 2017-0099 SUPERSEDED EASA AD 2014-0069
AS IN AD AS IN AD
DGCA/A320 family/100 FUSELAGE INSPECTION LONGITUDNAL LAP JOINTS BVAD 97-312-106(B) AS IN AD AS IN AD DGCA/A320 family/101 INSPECTION OF FASTENER HOLES AROUND
EMERGENCY EXIT DGAC AD 2002-259(B) AS IN AD AS IN AD
DGCA/A320 family/115 FLIGHT CONTROLS: STIFF RUDDER PEDAL(ATA 27) DGAC AD 2000-372-151(B) AS IN AD AS IN AD DGCA/A320 family/116(R1) INBOARD FLAP TRUNNION (ATA 27) DGAC AD 1996-271-092(B)R3 AS IN AD AS IN AD DGCA/A320 family/117 NOSE LANDING GEAR WHEEL ROTATION (ATA 32) DGAC AD 1999-124-129(B) AS IN AD AS IN AD DGCA/A320 family/118 PASSENGER DOOR AND EMERGENCY DOOR
ACTUATOR STRIKER MECHANISM (ATA 52) DGAC AD 1998-482-122(B) R1 AS IN AD AS IN AD
DGCA/A320 family/119 INSPECTION OF MLG SLIDING TUBE DGAC AD 1999-358-137(B)R1 AS IN AD AS IN AD DGCA/A320 family/120R1 ATA 57, WINGS – INNER REAR SPAR – MODIFICATION DGAC AD 2001-249(B) AS IN AD AS IN AD DGCA/A320 family/121R2 ATA 52, DOORS – MAIN LANDING GEAR DOOR
ACTUATOR FITTINGS – INSPECTION / REPLACEMENT
EASA AD 2016-0182 SUPERSEDED EASA AD 2014-0166
AS IN AD AS IN AD
DGCA/A320 family/122 INSPECTION & MODIFICATION OF SPOILER SERVO CONTROLS
DGCA/A320 family/124 LITTON GPSSU DGAC AD 1999-361-138(B) AS IN AD AS IN AD DGCA/A320 family/125 TO PREVENT UNCOMMANDED NOSE LANDING GEAR
WHEEL ROTATION FAA AD 99-23-09 AS IN AD AS IN AD
DGCA/A320 family/126 TO PREVENT THERMAL OXIDATION OF THE MAIN BRAKE ASSEMBLIES OF THE MLG
FAA AD 99-25-07 AS IN AD AS IN AD
DGCA/A320 family/127 ROCKWELL COLLINS RADIO ALTIMETER SOFTWARE ANOMALIES
DGAC AD 2000-004-142(B) AS IN AD AS IN AD
DGCA/A320 family/128 FMU COMMON FLOW STANDARDIZATION DGAC AD 2000-005-143(B)R1 AS IN AD AS IN AD DGCA/A320 family/129 ADDITIONAL ELECTRICAL BONDING IN FUEL TANKS DGAC AD2002-202(B) & 2002-
476 R1 AS IN AD AS IN AD
DGCA/A320 family/130(R1) VERTICAL STABILIZER SPAR BOX DGAC AD 2000-520-159(B) AS IN AD AS IN AD
WARNING COMPUTERS ---- REPLACEMENT EASA AD 2011-0001R1 AS IN AD AS IN AD
DGCA/A320 family/132 WING FUEL TANK PUMPS WIRING SHORT CIRCUIT DGAC AD 2002-221 (B) AS IN AD AS IN AD DGCA/A320 family/133(R2) FUEL SYSTEM WIRING CABLE SEGREGATION
AROUND RACK 90VU DGAC AD F 2004-129(ORG AD 2000-407-150, 2004-044 IS REPLACED)
AS IN AD AS IN AD
DGCA/A320 family/134(R2) KEEL BEAM-MAIN LANDING GEAR DOOR ACTUATOR FITTING
DGAC AD F 2004-189 R1 (ORG DGAC AD 2000-521-160(B) IS REPLACED)
AS IN AD AS IN AD
DGCA/A320 family/135 PASSENGER DOOR OUTER HANDLE MECHANISM DGAC AD 2000-519-158(B) AS IN AD AS IN AD DGCA/A320 family/136 WINDOWS: INSPECTION OF THE COCKPIT SLIDING
WINDOW LOWER MECHANISM DGAC AD 2000-518-157(B) AS IN AD AS IN AD
DGCA/A320 family/137 FLIGHT CREW SEATS DGAC AD 2000-524(B) AS IN AD AS IN AD DGCA/A320 family/138R1 FUSELAGE - FRAME 36 - INSPECTION OF THE
LONGITUDINAL BEAMS OF THE PRESSURE PANEL EASA AD 2016-0206(CORRECTION: 14 OCTOBER 2016)
AS IN AD AS IN AD
DGCA/A320 family/139R1 STABILIZERS --- ELEVATOR --- INSPECTION EASA AD 2014-0014 AS IN AD AS IN AD DGCA/A320 family/140(R1) PASSENGER DOOR-SLIDE RAFT TELESCOPIC GIRT
BAR DGAC AD 2001-063(B) & 2005-057 (ADs REPLACED ARE 2001-165(B) R1, 2001-275(B) & 2002-637(B) R1)
EASA AD 2007 - 0217 AS IN AD A318, A319, A-320, A-321
DGCA/A320 family/144 CREW OXYGEN SUPPLY(ATA 35) DGAC AD 2001-237(B)R1 AS IN AD AS IN AD DGCA/A320 family/145 RAT ACTUATOR(ATA 29) DGAC AD 2001-236(B)R1 &
2002-640(R1) AS IN AD AS IN AD
DGCA/A320 family/146 FUSELAGE-OVERWING EMERGENCY EXIT DOOR FRAME CORNERS
DGAC AD 2003-147(B)R1(DGAC AD 2001-241 IS CANCELLED)
AS IN AD AS IN AD
DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320 family/147 LOSS OF FUEL QUANTITY INDICATION ON CENTER
TANK (ATA 28) DGCA AD 2001-271(B) AS IN AD AS IN AD
DGCA/A320 family/157 MODIFICATION OF FUEL PROBES (ATA 28) DGAC AD 2002-220(B)R1 AS IN AD AS IN AD DGCA/A320 family/158 THALES AVIONICS DDRMI FAILURE (ATA 34) DGAC AD 2002-458(B)R2
(DGAC AD 2002-150 IS CANCELLED)
AS IN AD AS IN AD
DGCA/A320 family/159 CENTER WING BOX-INSPECTION OF UPPER STRINGERS
DGAC AD 2002-341(B) AS IN AD AS IN AD
DGCA/A320 family/160 THRUST REVERSER-PISTON ROD CHROME PLATING DGAC AD 2002-337(B)R1 AS IN AD AS IN AD DGCA/A320 family/161 CANCELLED DGAC AD F 2002-418 R1 DATED 09 JUNE
2004 DGAC AD 2002-418(B) R1 AS IN AD AS IN AD
DGCA/A320 family/162R1 FLIGHT CONTROL-- ELEVATOR BACKLASH -- INSPECTIONS
EASA AD 2011-0142 SUPERSEDES EASA AD 2006-0280 WHICH
AS IN AD AS IN AD
DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY
SUPERSEDES DGAC AD F-2004-074)
DGCA/A320 family/178 FUEL SYSTEM- AIR RELEASE VALVE(ARV) DGAC AD F-2004-120 AS IN AD AS IN AD DGCA/A320 family/179(R1) LIGHTS-EMERGENCY ESCAPE PATH MARKING BRUCE
FPEEPMS DGAC AD F-2004-121(R1) AS IN AD AS IN AD
DGCA/A320 family/180 FLIGHT CONTROLS- SPOILER ACTUATORS DGAC AD F-2004-122 AS IN AD AS IN AD DGCA/A320 family/181(R1) ENVIRONMENTAL/ AIR CONDITIONING- CARGO
COMPARTMENT- HEATING TEMPERATURE SENSOR DGAC AD F-2004-123(R1) AS IN AD AS IN AD
DGCA/A320 family/182 WING- INSPECTION OF BOTTOM SKIN PANEL BETWEEN RIBS 13 AND 22
INDICATING/RECORDING SYSTEMS- LOSS OF INTEGRATED STANDBY INSTRUMENT SYSTEM (ISIS) (ATA34)
DGAC AD F 2004-168 (R1) AS IN AD AS IN AD
DGCA/A320 family/185(R1) FIRE PROTECTION- CARGO COMPARTMENT WATER DRAIN VALVES
DGAC AD F 2004-172(R1) AS IN AD AS IN AD
DGCA/A320 family/186R2 FUEL / ELECTRICAL POWER --- PREVENTION OF FUEL TANK EXPLOSION RISKS - ELECTRICAL CABLES -- MODIFICATION
EASA AD 2008 - 0051R1 AS IN AD A318, A319, A-320, A-321
DGCA/A320 family/187 LANDING GEAR- PARKING BRAKE SYSTEM. DGAC AD F 2004-137 AS IN AD AS IN AD DGCA/A320 family/188 FLIGHT CONTROLS- ELAC 1 COMPUTER DGAC AD F 2005-013 AS IN AD AS IN AD DGCA/A320 family/189(R3) FUEL SYSTEM-PREVENTION AGAINST EXPLOSION
RISKS- IN TANK BONDING EASA AD 2006-0176, DGAC AD 2005-058 ( DGAC AD 2005-056, DGAC AD F 2005-028 ARE CANCEELED)
AS IN AD AS IN AD
DGCA/A320 family/190 FUEL SYSTEM-FUEL PUMPS-PREVENTION AGAINST EXPLOSION RISKS
DGAC AD F 2005-031 AS IN AD AS IN AD
DGCA/A320 family/191R2 WINGS - OUTER WING MAIN LANDING GEAR SUPPORT RIB 5 FITTING -- INSPECTION/MODIFICATION
EASA AD 2012 - 0032 AS IN AD A-318,A319, A-320, A-321
DGCA/A320 family/192 EQUIPMENT/ FURNISHINGS- NON TEXTILE FLOOR (NTF) REPLACEMENT
DGCA/A320 family/195 EQUIPMENT/ FURNISHINGS - 103 VU BOX - HINGE PIN STOPPER - MODIFICATION
EASA AD 2007 - 0214 AS IN AD A318, A319, A-320, A-321
DGCA/A320 family/196R1 TIME LIMITS & MAINTENANCE CHECKS ---- CERTIFICATION MAINTENANCE REQUIREMENTS ---- ALS PART 3 ---- AMENDMENT
EASA AD 2013 - 0148 AS IN AD AS IN AD
DGCA/A320 family/197 ENGINE-FORWARD MOUNT BOLT DGAC AD F 2005-117 AS IN AD AS IN AD DGCA/A320 family/198R1 FUEL SYSTEM- MAGNETIC FUEL LEVEL INDICATORS -
INSPECTION/REPLACEMENT/REPAIR EASA AD 2012 - 0119 AS IN AD AS IN AD
STABILIZER ACTUATOR --- INSPECTION EASA AD 2007-0178 AS IN AD AS IN AD
DGCA/A320 family/222 FIRE PROTECTION --- CARGO COMPARTMENT FIRE EXTINGUISHING --- INSPECTION OF BOTTLE WIRING CONNECTION --- INSPECTION AND CONTINUITY CHECK
EASA AD 2007-0249 AS IN AD A318, A319, A-320, A-321
DGCA/A320 family/223 LIGHTS --- INSTRUMENT & PANEL INTEGRAL LIGHTING --- EMERGENCY LIGHTING FOR STAND --BY INSTRUMENTS ---MODIFICATION
EASA AD 2007-0286 AS IN AD A318, A319, A-320, A-321
DGCA/A320 family/224R3 EQUIPMENT/FURNISHING --- 80 VU RACK ATTACHMENTS --- INSPECTION/REPAIR/REPLACEMENT
EASA AD 2012-0134 AS IN AD A318, A319, A-320, A-321
DGCA/A320 family/225R1 HYDRAULIC POWER --- RAM AIR TURBINE (RAT) GEROTOR PUMP - REPLACEMENT
EASA AD 2008-0034R1 AS IN AD A318, A319, A-320, A-321
DGCA/A320 family/226 INSTALLATION OF THE IMPROVED EIS2 STANDARD S7 EASA AD 2008-0032 AS IN AD A318, A319, A-320, A-321
DGCA/A320 family/227 LANDING GEAR --- BRAKING & STEERING CONTROL UNIT (BSCU) --- MODIFICATION / REPLACEMENT
EASA AD 2008-0048 AS IN AD A319, A-320, A-321
DGCA/A320 family/228 EQUIPMENT/FURNISHINGS --- COCKPIT DOOR LATCH/STRIKER ASSEMBLY --- MODIFICATION/REPLACEMENT
EASA AD 2008-0151 AS IN AD A318, A319, A-320, A-321
DGCA/A320 family/229R6 FLIGHT CONTROLS --- ELEVATOR SERVO --- CONTROL ROD EYE -- ENDS --- INSPECTION/ REPLACEMENT
EASA AD 2014-0137 CORRECTION 30sept2014
AS IN AD A318, A319, A-320, A-321
DGCA/A320 family/230 POWER PLANT ---- REAR ENGINE MOUNT BARREL NUTS ---- INSPECTION/REPLACEMENT
EASA AD 2008 - 0191- E AS IN AD A319, A-320, A-321
DGCA/A320 family/231R1 HYDRAULIC POWER --- AUXILIARY HYDRAULIC POWER --- RAM AIR TURBINE (RAT) EJECTION JACK --- REPLACEMENT
EASA AD 2008 - 0199R1 AS IN AD A318, A319, A-320, A-321
DGCA/A320family/329 ATA-53, FUSELAGE-FRAME 35.2A-INSPECTION EASA AD 2016-0106 AS IN AD AS IN AD DGCA/A320family/330 ATA-52, DOOR-FORWARD AND AFT CARGO DOOR
FRAME FORKS-INSPECTION EASA AD 2016-0187 AS IN AD AS IN AD
DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320family/331R2 ATA-92 – ELECTRIC AND ELECTRONIC COMMON
INSTALLATION – BATTERY RETAINING ROD –INSPECTION
EASA AD 2017-0161R1 [Correction: 20 September 2017] REVISED EASA AD 2017-0161 SUPERSEDED EASA AD 2016-0204 [Correction: 19 October 2016]