airbus a318,a319,a320,a321

24
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.

Upload: voduong

Post on 10-Feb-2017

527 views

Category:

Documents


6 download

TRANSCRIPT

Page 1: airbus a318,a319,a320,a321

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.

Page 2: airbus a318,a319,a320,a321

DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320 family/18 WIRE LOOM CHAFING AT RACEWAY/CONDUIT EXITS. BVAD 91-182-020(B) R2; FAA

AD 96-25-04 AND SB A320-24-1044 R2 & ìR3 A320-24-1045 R1, R2 & R3.

AS IN AD AND SB.

AS IN AD AND SB.

DGCA/A320 family/19R2 ATA 34, NAVIGATION – AIRSPEED PITOT PROBES – REPLACEMENT

EASA AD 2014-0237R1 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

DGAC AD 2002-531(B) AS IN & SB. AS IN AD & SB.

DGCA/A320 family/27 INSPECTION OE FUSELAGE PRESSURE FLOOR BETWEEN FRAMES 42 & 43.

BVAD NO. 92-205-033(B)R2 FAAD 93-14-04 ì& SB A320-53-1023 R3.

AS IN AD & SB.

AS IN AD & SB.

DGCA/A320 family/28 TRIMMABLE HORIZONTAL STABLIZER ACTUATOR (THS).

BVAD NO. 92-211-036(B) R1 AND AIRBUS SB A320-27-1045.

AS IN AD & SB.

AS IN AD & SB.

DGCA/A320 family/29 MODIFICATION OF APU'S TO AVOID SEPERATION OF APU TIESHAETS.

FAA AD 92-21-05 & SB GTCP 36-49-A6642 SB GTCP ì36-49-A6653.

AS IN AD & SB.

AS IN AD & SB.

Page 3: airbus a318,a319,a320,a321

DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320 family/30 CONNECTION OF FUEL RETURN LINE IN PYLON

CHECK OF SEALANT IN ìPYLON. BVAD 92-228-037(B) & AIRBUS INDUSTRIE AOT 28-04 REV.1 ìFAAD93-01-25.

AS IN AD & AOT.

AS IN AD & SB.

DGCA/A320 family/31 LAVAOTRY SMOKE DETECTION. BVAD 92-236-038(B) & AIRBUS INDUSTRIE AOT 28-04 REV.1 FAAD ì93-01-21.

AS IN ADS & AOT.

AS IN ADS & AOT.

DGCA/A320 family/32 ELECTRIC TERMINAL BLOCKS. BVAD 92-271-039(B) R3 & A320 AOT 24-02 DT. DEC 21 1992.

AS IN ADS & AOT.

AS IN ADS & AOT.

DGCA/A320 family/33 CANCELLED VIDE LETTER NO 9-412/05 DATED 01-04-05 IN VIEW OF DGCA/A320/120

DGCA/A320 family/34 BF GOODRICH CARBON BRAKES REDUCTION OF BRAKING PERFORMANCES.

BVAD NO. 93-056-040 (B) R3 AIRBUS SB A320-32-1090 & FAAD 93-15-05 ìAIRBUS SD A320-32-1114.

AS IN ADS & SB'S.

AS IN AD'S & SB'S.

DGCA/A320 family/35 CHECK FOR RAM AIR TURBINE BALL BEARING INTEGRITY.

BVAD NO. 93-057-041 (B)R2 AND AIRBUS SB A320-29-1061 & ìA320-29-1065 FAAAD 94-01-11.

AS IN AD'S & SB'S.

DGCA/A320 family/36 SEAT TRACK JOINTS AT FRAME 64. BVAD NO. 93-081-042(B) AND AIRBUS AOT A320 53-01 DT AUG 27, 1992.

AS IN AD & AOT.

AS IN AD & AOT.

DGCA/A320 family/37 MODIFICATION OF THE INNER REAR SPAR WEB OF THE MAIN LANDING GEAR.

FAAD 93-08-15 & AIRBUS SB A320-57-1040RI DT. SEPT 24,1992.

AS IN AD & SB.

AS IN AD & SB.

DGCA/A320 family/38 FUSELAGE - MODIFICATION REINFORCEMENT OF FRAME 20.

BVAD 93-107-045(B)& AIRBUS SB A320-53-1017.

AS IN AD & SB.

AS IN AD & SB.

DGCA/A320 family/39 TRIMMABLE HORIZONTAL STABLIZER LIGHTNING STRIKE PROTECTION ìIMPROVEMENT.

BVAD 93-123-046(B)R1 AND SB A320-27-1041R1 & A320-29-1058R1 ìAOT29-10 ORIGINAL ISSUE R-1 & 2.

AS IN AD & SB.

AS IN AD & SB.

DGCA/A320 family/40 NOSE WHEEL STEERING CONTROL. BVAD 92-117-025(B)R1 AND AIRBUS SB A320-32-1094 & A320-32-1100.

AS IN AD & SB.

AS IN AD & SB.

Page 4: airbus a318,a319,a320,a321

DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320 family/41 BRAKING SYSTEM- REPLACEMENT OF RELAYS 24GG

& 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.

Page 5: airbus a318,a319,a320,a321

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.

FAAD 94-14-17 & AIRBUS A320-025-1109.

AS IN AD & SB.

AS IN AD & SB.

DGCA/A320 family/54R1 INDICATING & RECORDING SYSTEMS --- FLIGHT WARNING COMPUTERS ---- REPLACEMENT

EASA AD 2011 -0001R1 AS IN AD AS IN AD

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)

FAAD 97-02-04. AS IN AD. AS IN AD.

DGCA/A320 family/59 JAMMING OF PASSENGER DOORS. BVAD 95-004-062(B)R1 A320/AOT 52-07 SB A320-52-1064 & ìA320-52-1066.

AS IN AD & SB.

AS IN AD & SB.

DGCA/A320 family/60 MAIN LANDING GEAR SHOCK ABSORBER UPPER BEARING DOWEL RETENTION.

BVAD 95-016-063(B) AIRBUS INDUSTRIE SB A320-32-1144.

AS IN AD & SB.

AS IN AD & SB.

DGCA/A320 family/61R1` FUSELAGE -- CENTRE FUSELAGE TRANSITION AND PICK UP ANGLE -- INSPECTION / MODIFICATION

EASA AD 2013 - 0137 AS IN AD & SB.

AS IN AD & SB.

DGCA/A320 family/62R1 WING – CENTER WING / LOWER RIBS AT FRAME 36 JUNCTION – INSPECTION / REPAIR

EASA AD 2014-0053 AS IN AD & SB.

AS IN AD & SB.

DGCA/A320 family/63R2 WINGS --- CENTRE SECTION / PRESSURISED FLOOR FITTINGS AT FRAME NO.36 JUNCTION --- INSPECTION

EASA AD 2016-0181 SUPERSEDED EASA AD 2013-0226

AS IN AD & SB.

AS IN AD & SB.

DGCA/A320 family/64(R1) CENTRE WING BRACKET BETWEEN SHROUD BOX & FIXED SHROUD.

AD 95-100-068(B) & SB A320-57-1034 & SB A320-57-1035.FAA AD 96-25-05.

AS IN AD & SB.

AS IN AD & SB.

DGCA/A320 family/65(R1) CENTRE FUSELAGE-FRAME AND FRAME FEET WITH FRAMES AT FRAME NO. 37 THRU 41( ATA53).

DGAC 98-509-123 (B) SB A320-53-1128 & A320-53-1141.

AS IN AD & SB.

AS IN AD & SB.

DGCA/A320 family/66 HYDRAULIC FIRE SHUTOFF VALVE WESTLAND-SITEC P/N E0 3000.

BVAD 95-145-070(B) & AOT 29-15 DT.MAY 30, 1995 & WESTLAND-SITEC ìSERVICE BULLETIN EO1OWS-29-2.

AS IN AD AOT & SB..

AS IN AD AOT & SB.

Page 6: airbus a318,a319,a320,a321

DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320 family/67(R2) EQUIPMENT / FURNISHINGS --- OFF --- WING ESCAPE

SLIDE ENCLOSURES ---- MODIFICATION DGAC AD 2014-0025 AS IN AD. AS IN AD

DGCA/A320 family/68R2 CANCEL dated 22.05.2015

ATA- 27,FLIGHT CONTROLS – ELEVATOR AILERON COMPUTERS – REPLACEMENT / SOFTWARE UPDATE CANCELLED

EASA AD 2015-0088R1 REV AS IN BVAD & SB.

AS IN BVAD & SB.

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.

BVAD 96-009-074(B)R2 BVAD 97-315-109(B) & SB A320-53-1110 .

AS IN AD & SB.

AS IN AD & SDB.

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.

Page 7: airbus a318,a319,a320,a321

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.

BVAD 96-293(B) AS IN AD. AS IN AD.

DGCA/A320 family/87R2 FUSEALGE– REAR FUSEALGE FRAME 68 – INSPECTION / REPAIR

EASA AD 2015-0084 sup Correction 18.05.2015

AS IN AD. AS IN AD.

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

Page 8: airbus a318,a319,a320,a321

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/102 FUSELAGE-INSPECTION FRAME 46/STANGER 37 INTERSECTION

DGAC AD 2002-260(B) AS IN AD AS IN AD

DGCA/A320 family/103 WING INSPECTION CONNECTION OF FRAMES 43 & 44 WITH PRESSURE FLOOR

BVAD 97-316-110(B) AS IN AD AS IN AD

DGCA/A320 family/104 RELAY 11QG RELOCATION AND CONTACT INSPECTION

DGAC AD 2002-365(B) (DGAC AD 1999-263-134 IS CANCELLED)

AS IN AD. AS IN AD.

DGCA/A320 family/105 CANCELLED VIDE 9-413/03 AI(2) DATED 24-09-04 IN VIEW OF DGCA/A320/45 (R1)

DGCA/A320 family/106(R1) FUSELAGE REINFORCEMENT OF THE FRAME 35 BETWEEN STRINGER 30 & 31

DGAC AD 2002-032(B) AS IN AD AS IN AD

DGCA/A320 family/107 CANCELLED IN VIEW OF DGCA/A320/96 VIDE LETTER NO 9-412/98-AI(2) DATED 03-09-98

DGCA/A320 family/108 IMPROVEMENT OF AVIONIC PROTECTION FROM TRICKLING WATER

B.V.A.D.98-178-115 AS IN A.D. AS IN S.B.

DGCA/A320 family/109 CANCELLED IN VIEW OF DGCA/A320/79 VIDE LETTER NO 9-412/98-AI(2) DATED 03-09-98

DGCA/A320 family/110R3 ATA 32, LANDING GEAR – BRAKE DUAL DISTRIBUTION VALVE – MODIFICATION

EASA AD 2017-0119 SUPERSEDED EASA AD2014-0251R1 REVISION

AS IN AD AS IN SB

DGCA/A320 family/111 IAE FRONT ENGINE MOUNT MODIFICATION (ATA 71) DGAC FRANCE AD 98-293-118 (B)R1

AS IN AD AS IN AD

DGCA/A320 family/112 INSTALLATION OF CRADLES ON VERTICAL PARTITIONS

BVAD 98-176(AB) AS IN AD AS IN AD

Page 9: airbus a318,a319,a320,a321

DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320 family/113 IMPROVEMENT OF THE AIRBORNE GROUND CHECK

MODULE(AGCM) LOW PRESSURE CHECK VALVE (ATA29)

DGAC AD1998-537-124(B)R1 AS IN AD AS IN AD

DGCA/A320 family/114 COCKPIT-SLIDING TABLE/COCKPIT FOOTREST IMPROVEMENT

DGAC AD 2000-256-145(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

DGAC AD 1999-362-139(B) AS IN AD AS IN AD

DGCA/A320 family/123 (CN)

CANCELLED : EQUIPMENT / FURNISHINGS -- ESCAPE SLIDES & RAFTS --INSPECTION / REPLACEMENT / MODIFICATION

EASA AD 2012-0122-CN AS IN AD AS IN AD

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

Page 10: airbus a318,a319,a320,a321

DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320 family/131R1 INDICATING & RECORDING SYSTEMS --- FLIGHT

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)

AS IN AD AS IN AD

DGCA/A320 family/141R2 ATA- 27,FLIGHT CONTROLS – ELEVATOR AILERON COMPUTERS – REPLACEMENT / SOFTWARE UPDATE

EASA AD2015-0088 R1REV AS IN AD AS IN AD

DGCA/A320 family/142 PAX DOOR; MODIFICATION OF THE UPPER SAFETY PIN

DGAC AD 2001-100(B) AS IN AD AS IN AD

DGCA/A320 family/143 NAVIGATION - NORTHROP - GRUMMAN (PREVIOUSLY LITTON) ADIRU - REPLACEMENT

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

Page 11: airbus a318,a319,a320,a321

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/148(R1) CANCELLED

GOODRICH CARBON BRAKE - REDUCTION OF PERFORMANCE

EASA Ad 2011-0188-CN AS IN AD AS IN AD

DGCA/A320 family/149R2 ATA 34, NAVIGATION – AIRSPEED PITOT PROBES – REPLACEMENT

EASA AD 2014-0237R1 REVISION

AS IN AD AS IN AD

DGCA/A320 family/150 OXYGEN SYSTEM-INPECTION OF OXYGEN PASSENGER CONTAINERS-(DRAEGER TYPE I AND II) (ATA 35)

DGAC AD 2001-363 (B) AS IN AD AS IN AD

DGCA/A320 family/151 YELLOW HYDERAULIC CIRCUIT-PARKING BRAKE OPERATED VALVE (PBOV) (ATA 32)

DGAC AD 2001-384 (B)R1 AS IN AD AS IN AD

DGCA/A320 family/152 IAE v2500 ENGINE-FAN COWL LATCH MODIFICATION (ATA 71)

DGAC AD 2001-381 (B) AS IN AD AS IN AD

DGCA/A320 family/153 PPG AEROSPACE WINDSHIELDS DGAC AD 2001-606(B) AS IN AD AS IN AD DGCA/A320 family/154 REAR PASSENGER DOOR FRAME - UPPER GUIDE

ROD FITTING DGAC AD 2001-634(B) AS IN AD AS IN AD

DGCA/A320 family/155 COCKPIT FIXED LATERAL WINDOWS OUTER PLY SEPARATION

DGAC AD 2001-632(B) AS IN AD AS IN AD

DGCA / A320 family /156(R3)

LANDING GEAR --- MAIN LANDING GEAR (MLG) SIDE-STAY CUFF LUG --- INSPECTION / REPAIR

EASA AD 2011 - 0024R1 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 2007-0163R1 AS IN AD AS IN AD

DGCA/A320 family/163R2 ATA 34, NAVIGATION – AIRSPEED PITOT PROBES – REPLACEMENT

EASA AD 2014-0237R1 AS IN AD AS IN AD

Page 12: airbus a318,a319,a320,a321

DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320 family/164 ELECTRICAL POWER-REPLACEMENT OF TRU

INSTALLED IN POSITION 2 (1PU2) DGAC AD 2002-554(B) AS IN AD AS IN AD

DGCA/A320 family/165(R2) TIME LIMITS AND MAINTENANCE CHECKS --- SAFE LIFE AIRWORTHINESS LIMITATIONS ITEMS --- (ALS) PART 1 ---- AMENDMENT

EASA AD 2012-0008 AS IN AD AS IN AD

DGCA/A320 family/166(R5) ATA -05, TIME LIMITS / MAINTENANCE CHECKS – ALS PART 2 - DAMAGE TOLERANT AIRWORTHINESS LIMITATION ITEMS – IMPLEMENTATION

EASA AD 2016-0239 AS IN AD AS IN AD

DGCA/A320 family/167(R1) FUEL LEAK PROCEDURE DGAC AD F 2005-165 ( DGAC AD 2003-119 IS CANCELLED)

AS IN AD AS IN AD

DGCA/A320 family/168(R2) ATA 53 - FUSELAGE - KEEL BEAM SIDE PANELS - INSPECTION

EASA AD 2015-0062 supersedure dated 22 april 2015

AS IN AD AS IN AD

DGCA/A320 family/169R2 AIRBORNE AUXILIARY POWER - AUXILIARY POWER UNIT EXHAUST TAILPIPE --- MODIFICATION

EASA AD 2013-0129 AS IN AD AS IN AD

DGCA/A320 family/170 NAVIGATION-INERTIAL REFERENCE SYSTEMS DGAC AD 2003-270-(B) AS IN AD AS IN AD DGCA/A320 family/171(R23)

INDICATING/RECORDING SYSTEMS- TEMPORARY LOSS OF ALL DISPLAY UNITS

EASA AD 2006-0108 (DGAC AD 2003-373(B) & 2004-104 R1 ARE CANCELLED)

AS IN AD AS IN AD

DGCA/A320 family/172 AUXILIARY POWER UNIT (APU) - HAMILTON SUNDSTRAND AC GENERATOR

DGAC AD 2004-019 AS IN AD AS IN AD

DGCA/A320 family/173(R1) MAIN LANDING GEAR ( MLG ) - SHOCK ABSORBER SLIDING TUBE CRACKS

DGAC AD F-2005-115 (DGAC AD F 2004-065, 2004-22 ARE CANCELLED)

AS IN AD AS IN AD

DGCA/A320 family/174R1 FUEL SYSTEM-ADDITIONAL CENTER TANKS MANHOLE COVER SEAL -- REPLACEMENT

EASA AD 2010-0177 AS IN AD A319, A320, A321

DGCA/A320 family/175 EQUIPMENT FURNISHINGS- PASSENGER DOOR EMERGENCY ESCAPE SLIDES

DGAC AD F-2004-072 AS IN AD,AS IN SB

ASIN AD, AS IN SB

DGCA/A320 family/176 FUEL- PREVENTION AGAINST EXPLOSION RISK- ADJACENT SYSTEMS

DGAC AD F-2004-073 AS IN AD,AS IN SB

AS IN AD, AS IN SB

DGCA/A320 family/177(R2) AIRCRAFT FLIGHT MANUAL - DISPLAY UNIT FAILURE - OPERATIONAL PROCEDURE

EASA AD 2011-0142 SUPERSEDES EASA AD 2006-0280 WHICH

AS IN AD AS IN AD

Page 13: airbus a318,a319,a320,a321

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

DGAC AD F 2004-146 AS IN AD AS IN AD

DGCA/A320 family/183 AUXILIARY HYDRAULIC POWER- AIRBORNE GROUND CHECK MODULE (AGCM)

DGAC AD F 2004-150 AS IN AD AS IN AD

DGCA/A320 family/ 184 (R1)

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

DGAC AD F 2005-040 AS IN AD AS IN AD

Page 14: airbus a318,a319,a320,a321

DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320 family/193R1 EQUIPMENT & FURNISHINGS --- DASELL LAVATORY

WALLS ---INSPECTION/REPAIR EASA AD 2010-0148 AS IN AD AS IN AD

DGCA/A320 family /194R1 FLIGHT CONTROLS- TRIMMABLE HORIZONTAL STABILIZER ACTUATOR --- INSPECTION

EASA AD 2014 - 0147 SUPERSEDURE PREV

AS IN AD A318, A319, A-320, A-321

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

DGCA/A320 family/199(R1) LANDING GEAR- MAIN LANDING GEAR (MLG) AXLE NUT SEPERATION

DGAC AD F 2005-128 ( DGAC AD UF 2005-120 IS CANCELLED)

AS IN AD AS IN AD

DGCA/A320 family/200 (R2)

FUEL, WINGS- FUEL SYSTEM- LABELS IN FUEL TANKS EASA AD 2006-0236R1 (SUPERSEDES DGAC AD F 2005-121)

AS IN AD AS IN AD

DGCA/A320 family/201R1 FLIGHT CONTROLS / WINGS --- INBOARD FLAP TRUNNION AND SLIDING PANEL --- INSPECTION

EASA AD 2010-0209 AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/202 EQUIPMENT/ FURNISHINGS- COCKPIT SEATS ACTUATORS INSPECTION AND REPLACEMENT

DGAC AD F 2005-164 AS IN AD AS IN AD

DGCA/A320 family/203 FUEL SYSTEM-PREVENTION AGAINST EXPLOSION RISKS- DRY RUNNING FUEL PUMP

DGAC AD F 2005-173 AS IN AD AS IN AD

DGCA/A320 family/204 FUEL SYSTEM- TWIN MOTOR LOW PRESSURE VALVE ACTUATOR

DGAC AD F 2005-189 AS IN AD AS IN AD

DGCA/A320 family/205(R3) ATA-32, LANDING GEAR - NOSE LANDING GEAR / BRAKING AND STEERING CONTROL UNIT - INSPECTION / REPLACEMENT

EASA AD 2011-0201R1 AS IN AD AS IN AD

DGCA/A320 family/ 206(CN)

CANCELLED: EQUIPMENT/FURNISHINGS -- ESCAPE SLIDES & RAFTS --- INSPECTION / REPLACEMENT / MODIFICATION

EASA AD 2012-0122-CN AS IN AD AS IN AD

DGCA/A320 family/ 207 RAM AIR TURBINE (RAT)- CARBON BLADE DGAC AD F 2005-212 AS IN AD AS IN AD

Page 15: airbus a318,a319,a320,a321

DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320 family/ 208 (R2)

NACELLES/PYLONS- ENGINE PYLON SPAR BOX RIBS EASA AD 2006-0136 (DGAC AD F 2006-011(R1)IS CANCELLED)

AS IN AD AS IN AD

DGCA/A320 family/209R2 FUEL- MAIN FUEL PUMP SYSTEM/ FUEL PUMPS -- AIRWORTHINESS LIMITATIONS / INSPECTION /REPLACEMENT

EASA AD 2007- 0218R2 revision

AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/210R3 LANDING GEAR- MAIN LANDING GEAR DOOR ACTUATOR - MONITORING / INSPECTION / REPLACEMENT / MODIFICATION

EASA AD 2013 - 0288 AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/211 HYDRAULIC POWER- RAT (RAM AIR TURBINE)- SPEED LIMITATION WHEN RAT DEPLOYED

EASA AD 2006-0135 AS IN AD AS IN AD

DGCA/A320 family/212R2 ATA-49, AIRBORNE AUXILIARY POWER-AUXILIARY POWER UNIT STARTER MOTOR AND AIR INTAKE SYSTEM- INSPECTION/CLEANING

EASA AD 2016-0176 SUPERSEDED EASA AD 2016-0159

AS IN AD AS IN AD

DGCA/A320 family/213 R1 EQUIPMENT / FURNISHINGS - CARGO LOADING SYSTEM FIXED YZ LATCHES ATTACHMENT POINTS - MODIFICATION

EASA AD 2011-0077 AS IN AD AS IN AD

DGCA/A320 family/214R5 ATA 05, TIME LIMITS / MAINTENANCE CHECKS – AIRWORTHINESS LIMITATIONS SECTION (ALS) PART 5 FUEL AIRWORTHINESS LIMITATIONS – AMENDMENT

EASA AD 2017-0169 SUPERSEDED EASA AD 2014-0260

AS IN AD AS IN AD

DGCA/A320 family/215 STABILIZERS - RUDDER ACTUATOR FITTINGS - REPLACEMENTS

EASA AD 2006-0262 AS IN AD AS IN AD

DGCA/A320 family/216 POWERPLANT---FORWARDBENGINE MOUNT BOLTS----INSPECTION/REPLACEMENT/RETORQUE

EASA AD 2007-0036R1 AS IN AD AS IN AD

DGCA/A320 family/217 WINGS---CENTRE AND OUTER WING BOX AT LEVEL OF RIB 1 JUNCTION----INSPECTION

EASA AD 2007-0067R1 AS IN AD AS IN AD

DGCA/A320 family/218R2 LANDING GEAR --- EXTENSION AND RETRACTION SELECTOR VALVES --- INSPECTION / REPLACEMENT

EASA AD 2007-0065R2 CORRECTED ON 22/03/2011

AS IN AD AS IN AD

DGCA/A320 family/219 WING----DRY BAY SKIN-----INSPECTION EASA AD 2007-0064R1 AS IN AD A319, A-320, A-321

DGCA/A320 family/220R1 FUSELAGE -CENTRE FUSELAGE -MAIN LANDING GEAR DOOR KEEL BEAM HINGE AND ACTUATOR FITTING - INSPECTION

EASA AD 2012-0118 AS IN AD AS IN AD

Page 16: airbus a318,a319,a320,a321

DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320 family/221 FLIGHT CONTROLS --- TRIMMABLE HORIZONTAL

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/A320 family/232 INSTRUMENTS --- ELECTRONIC INSTRUMENT SYSTEM (EIS) DISPLAY MANAGEMENT COMPUTER (DMC) SOFTWARE UPDATE ----INTRODUCTION

EASA AD 2008 - 0198 AS IN AD A319, A-320, A-321

DGCA/A320 family/233 ENGINE --- HIGH PRESSURE COMPRESSOR (HPC) STALL EVENT --- INSPECTION/REPLACEMENT

EASA AD 2008 - 0228 - E AS IN AD A318, A319, A-320, A-321

Page 17: airbus a318,a319,a320,a321

DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320 family/234 WINGS ---- FLAP TRACK NO 1 PENDULUM ASSEMBLY --

- INSPECTION/REPLACEMENT EASA AD 2009 - 0025 AS IN AD A318, A319, A-

320, A-321 DGCA/A320 family/235R1 STABILIZERS --- RUDDER SIDE SHELL SKIN ---

INSPECTION EASA AD 2010 - 0164 AS IN AD A318, A319, A-

320, A-321 DGCA/A320 family/236 ELECTRICAL POWER --- AC & DC ESS BUS POWER

SUPPLY --- MODIFICATION EASA AD 2009 - 0235 AS IN AD A318, A319, A-

320, A-321 DGCA/A320 family/237 SSAD AS IN AD A318, A319, A-

320, A-321 DGCA/A320 family/238R1 HYDRAULIC POWER --- HAMILTON SUNDSTRAND RAM

AIR TURBINE WEIGHT SCREWS --- INSPECTION / REPLACEMENT

EASA AD 2010-0120 AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/239 FUEL --- FUEL TANK HARNESS RING TAGS --- INSPECTION

EASA AD 2010 -0027 AS IN AD A-321

DGCA/A320 family/240R2 STABILIZERS --- ELEVATORS ---- INSPECTION EASA AD 2014 -0014 AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/241 FLIGHT CONTROLS --- ELEVATOR AILERON COMPUTER (ELAC) SYSTEM POWER SUPPLY --- MODIFICATION

EASA AD 2010-0149 AS IN AD A - 320

DGCA/A320 family / 242R2 (CANCELLED)

OXYGEN SYSTEM --- PASSENGER OXYGEN MASKS --- IDENTIFICATION / MODIFICATION / REPLACEMENT

EASA AD 2010-0165R1 CORRECTED ON 31ST JANUARY 2011 HAS BEEN CANCELLED

AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/243R2 EQUIPMENT / FURNISHINGS --- OFF -- WING ESCAPE SLIDE ENCLOSURE --- MODIFICATION

EASA AD 2014-0025R1 REVISION

AS IN AD A318, A319, A-320,

DGCA/A320 family/244 FUSELAGE -- EMERGENCY OFF - WING EXIT ESCAPE SLIDE RELEASE CABLES -- REPLACEMENT

EASA AD 2011-0015 AS IN AD A318, A319, A-320,

DGCA/A320 family/245 WINGS --- CENTRE WING BOX LOWER PANEL --- INSPECTION

EASA AD 2011-0035 AS IN AD A-321

DGCA/A320 family/246R2 WINGS --- OUTER WING REFUELLING APERTURE ELECTRICAL BONDING --- INSPECTION / MODIFICATION

EASA AD 2013-0277R1 AS IN AD A319, A-320, A-321

DGCA/A320 family/247 ELECTRIC & ELECTRONIC COMMON INSTALLATION --- TERMINAL MODULES --- IDENTIFICATION / REPLACEMENT

EASA AD 2011 -0054 AS IN AD A318, A319, A-320, A-321

Page 18: airbus a318,a319,a320,a321

DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320 family/248(R1) ATA 57 - WINGS - NUTS- INSPECTION / REPLACEMENT EASA AD 2011-0121R1

REVISES EASA AD 2011-0121 AS IN AD A318, A319, A-

320, A-321 DGCA/A320 family/249(R1) ATA 53 - FUSELAGE - NUTS- INSPECTION /

REPLACEMENT EASA AD 2011-0120(R1) REVISES EASA AD 2011-0120

AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/250R1 ATA 25 - EQUIPMENT/FURNISHINGS- PASSENGER COMPARTMENT CLASS DIVIDER / GAS SPRING DAMPER - INSPECTION / REPLACEMENT

EASA AD 2011-0137R1 AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/251R3 ATA 25 - EQUIPMENT/FURNISHINGS - ESCAPE SLIDE RAFT- MODIFICATION/REPLACEMENT

EASA AD 2016-0043 AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/252R2 ATA 35 , OXYGEN - CHEMICAL EMERGENCY OXYGEN CONTAINERS - MODIFICATION

EASA AD 2014-0208 AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/253 ATA 53 - FUSELAGE - FORWARD FUSELAGE FRAME (FR) 35 CIRCUMFERENTIAL JUNCTION – INSPECTION / REPAIR

EASA AD 2011-0176 AS IN AD A-320

DGCA/A320 family/254R1 LANDING GEAR --- LANDING GEAR CONTROL AND INTERFACE UNIT WIRING --- MODIFICATION

EASA AD 2013-0202 AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/255R4 ATA-34,NAVIGATION --- ANGLE OF ATTACK (AOA) SENSORS --- REPLACEMENT

EASA AD 2015--0135 sup AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/256 FUSELAGE --- FORWARD FUSELAGE FRAME (FR) 24 ---- INSPECTION / REPAIR

EASA AD 2011-0229 AS IN AD A-320, A-321

DGCA/A320 family/257R1 TIME LIMITS & MAINTENANCE CHECKS --- DAMAGE TOLERANT AIRWORTHINESS LIMITATION ITEMS --- ALS PART 2 ---- AMENDMENT

EASA AD 2013-0147 AS IN AD A319, A-320, A-321

DGCA/A320 family/258R1 ATA 27 - FLIGHT CONTROLS - FLAP INTERCONNECTING STRUT - IDENTIFICATION / MODIFICATION / REPLACEMENT

EASA AD 2016-0113 AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/259R3 ATA 35 - OXYGEN --- CHEMICAL EMERGENCY OXYGEN CONTAINERS --- MODIFICATIONS

EASA AD 2014-0207 correction26/11/2014

AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/260R4 ATA 54 -- NACELLES/PYLONS --- AFT PYLON MOVEABLE FAIRING RIB 5 --- INSPECTION/REPAIR

EASA AD 2015-0051 supersedure

AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/261R1 ATA 53 -- FUSELAGE -- FORWARD FUSELAGE FRAME (FR) 24 CIRCUMFERENTIAL JUNCTION -- INSPECTION/REPAIR

EASA AD 2012-0132R1 AS IN AD A318, A319,

Page 19: airbus a318,a319,a320,a321

DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320 family/262R1 ATA 28,FUEL SYSTEM --- CENTRE TANK FUEL PUMP

CONTROL CIRCUIT --- MODIFICATION EASA AD 2012-0198R1 rev AS IN AD A318, A319, A-

320 DGCA/A320 family/263R2 ATA-27, FLIGHT CONTROLS --- TRIMMABLE

HORIZONTAL STABILIZER ACTUATOR BALL SCREW LOWER SPLINES ---- INSPECTION/REPLACEMENT

EASA AD 2012-0175R2 AS IN AD A318, A319, A-320

DGCA/A320 family/264 WINGS --- MAIN LANDING GEAR RETRACTION JACK ANCHORAGE FITTINGS ---- INSPECTION/REPLACEMENT

EASA AD 2012-0223 AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/265 STABILIZERS --- ELEVATORS ---- WEIGHT CHECK / RE-IDENTIFICATION

EASA AD 2012-0221 AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/266R3 ATA- 34, NAVIGATION – ANGLE OF ATTACK SENSORS – REPLACEMENT

EASA AD 2015-0135 sup AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/267 WINDOWS --- COCKPIT SLIDING WINDOW SEALS ---- INSPECTION/MODIFICATION

EASA AD 2013-0011 AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/268R4 ATA-71, POWERPLANT ---- AFT ENGINE MOUNT RETAINERS ---- INSPECTION / REPLACEMENT

EASA AD 2017-0138 SUPERSEDED EASA AD 2016-0010R1

AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/269R3 ATA 32, LANDING GEAR – MAIN LANDING GEAR DOOR ACTUATOR – MONITORING / INSPECTION / REPLACEMENT / MODIFICATION

EASA AD 2014-0021R1 AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/270R2 ATA-05, TIME LIMITS / MAINTENANCE CHECKS --- AIRWORTHINESS LIMITATIONS SECTION PART 4- SYSTEM MAINTENANCE REQUIREMENTS (SEMR)--IMPLEMENTATION

EASA AD 2017-0170 SUPERSEDED EASA AD 2016-0093

AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/271 WINGS --- CENTRE WING BOX STRUTS --- INSPECTION / REPAIR

EASA AD 2013-0149 AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/272R2 OXYGEN --- PASSENGER GASEOUS OXYGEN SYSTEM --- MODIFICATION

EASA AD 2014-0045 AS IN AD A319,

DGCA/A320 family/273 FUSELAGE ---- FRAME 47 SPLICE PLATE BUTT JOINT CROSSING AREA ---- INSPECTION/REPAIR

EASA AD 2013-0203 AS IN AD A320

DGCA/A320 family/274 FUSELAGE ---- SIDE BOX BEAM FLANGE IN FRAME 43 AREA ---- INSPECTION/REPAIR/MODIFICATION

EASA AD 2013-0261 AS IN AD A318, A319, A-320, A-321

Page 20: airbus a318,a319,a320,a321

DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320 family/275R1 OXYGEN ---- CREW OXYGEN / OXYGEN PIPE

CORROSION ---- INSPECTION EASA AD 2017-0150 SUPERSEDED EASA AD 2013-0278

AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/276R1 LANDING GEAR --- MAIN LANDING GEAR RETRACTION ACTUATOR ---- INSPECTION / REPLACEMENT

EASA AD 2013-0283R1 AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/277 STABILIZERS --- COMPOSITE RUDDER SIDE SHELL SANDWICH REPAIR --- INSPECTION

EASA AD 2013-0302 AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/278 FUSELAGE --- TACK AND RIVET HOLES IN FITTING BRACKETS AT FRAME 50 TO FRAME 63 --- INSPECTION / REPAIR

EASA AD 2013-0310 AS IN AD A319, A-320, A-321

DGCA/A320 family/279R2 FLIGHT CONTROLS ---- TRIMMABLE HORIZONTAL STABILIZE ACTUATOR ----- INSPECTION

EASA AD 2016-0184 SUPERSEDED EASA AD 2014-0011R1

AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/280 LANDING GEAR – MAIN LANDING GEAR SLIDING TUBE AXLES – INSPECTION

EASA AD 2014-0058 AS IN AD A318, A319, A-320, A-321

DGCA/A320 family/281 NACELLES / PYLONS – FORWARD CORNER FITTINGS OF PYLON AFT SECONDARY STRUCTURE – INSPECTION / REPLACEMENT

EASA AD 2014-0064 AS IN AD AS IN AD

DGCA/A320 family/282R1 ATA 53, FUSELAGE – POTABLE WATER AND WASTE WATER SERVICE PANELS – REINFORCEMENT

EASA AD 2017-0098 SUPERSEDED EASA AD 2014-0081

AS IN AD AS IN AD

DGCA/A320 family/283R1 ATA 52, DOORS – MAIN LANDING GEAR FIXED FAIRING ASSEMBLY – INSPECTION

EASA AD 2015-0001R1 AS IN AD AS IN AD

DGCA/A320 family/284 ATA 32, LANDING GEAR – MAIN LANDING GEAR UPPER CARDAN – LIFE LIMITATION

EASA AD 2014-0141 AS IN AD AS IN AD

DGCA/A320 family/285 ATA 53, FUSELAGE – FRAME 24 AT STRINGER 17/18 – INSPECTION

EASA AD 2014-0146 AS IN AD AS IN AD

DGCA/A320 family/286 ATA 54, NACELLES / PYLONS – PYLON AFT FIXED FAIRING -INSPECTION /REPAIR STRUCTURE – INSPECTION / REPLACEMENT

EASA AD 2014-0154 AS IN AD AS IN AD

DGCA/A320 family/287 ATA 34, NAVIGATION – TERRAIN AWARENESS WARNING SYSTEM – POWER CYCLE(RESET)

EASA AD 2014-0174 AS IN AD AS IN AD

DGCA/A320 family/288R1 ATA -53, FUSELAGE – EMERGENCY EXIT CUT-OUT AREA – MODIFICATION

EASA AD 2015-0085 AS IN AD AS IN AD

Page 21: airbus a318,a319,a320,a321

DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320 family/289 ATA 53, FUSELAGE – REAR FUSELAGE CLIPS, SHEAR

WEBS AND ANGLES –REPLACEMENT EASA AD 2014-0177 AS IN AD AS IN AD

DGCA/A320 family/290 ATA 53, FUSELAGE – PASSENGER DOOR GIRT BAR FITTINGS – INSPECTION

EASA AD 2014-0178 AS IN AD AS IN AD

DGCA/A320 family/291 ATA 27, FLIGHT CONTROLS – FLIGHT COMPUTERS AND SHARKLET COMMON GROUND CONNECTION – MODIFICATION

EASA AD 2014-0186

DGCA/A320 family/292 ATA 53, FUSELAGE – CENTRE FUSELAGE FORWARD PRESSURE BULKHEAD –REINFORCEMENT

EASA AD 2014-0209 AS IN AD AS IN AD

DGCA/A320 family/293R2 ATA 22, 31 ,AUTO FLIGHT / INSTRUMENTS – STOP RUDDER INPUT WARNING – INSTALLATION / ACTIVATION

EASA AD 2016-0132 (CORRECTION: 20 JULY 2016)

AS IN AD AS IN AD

DGCA/A320 family/294R3 ATA 28, FUEL – FUEL VENT PROTECTOR – INSPECTION / REPLACEMENT

EASA AD 2016-0114 AS IN AD AS IN AD

DGCA/A320 family/295 ATA 25, EQUIPMENT / FURNISHINGS – PASSENGER SERVICE UNIT JIFFY JOINT CONNECTORS – INSPECTION

EASA AD 2014-0256 AS IN AD AS IN AD

DGCA/A320 family/296 ATA 71, POWER PLANT – AFT ENGINE MOUNT BOLTS – RE-TORQUE

EASA AD 2014-0258 AS IN AD AS IN AD

DGCA/A320 family/297R2 ATA- 34, NAVIGATION – ANGLE OF ATTACK SENSORS – REPLACEMENT

EASA AD 2015-0135 SUP AS IN AD AS IN AD

DGCA/A320 family/298R3 ATA 57, WINGS – WING BOTTOM SKIN AT MAIN LANDING GEAR RIB 5 – INSPECTION

EASA AD 2015-0026R1(rev) SUPERSEDURE

AS IN AD AS IN AD

DGCA/A320 family/299 ATA 53, FUSELAGE – EXTERNAL FUSELAGE SKIN – INSPECTION

EASA AD 2014-0259 AS IN AD AS IN AD

DGCA/A320 family/300 ATA 71, POWER PLANT – FAN COWL DOOR HINGE NUTS – INSPECTION /REPLACEMENT

EASA AD 2014-0276 AS IN AD AS IN AD

DGCA/A320 family/301R3 ATA–35,OXYGEN – CHEMICAL OXYGEN GENERATORS – REPLACEMENT

EASA AD 2015-0117 supersedure correctio dated 19/08/2015

AS IN AD AS IN AD

DGCA/A320 family/302 ATA 53, FUSELAGE – SKIN ABOVE LAP JOINT – INSPECTION

EASA AD 2014-0278 AS IN AD AS IN AD

Page 22: airbus a318,a319,a320,a321

DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320 family/303 ATA 71, POWER PLANT – FORWARD ENGINE MOUNT

PIN – IDENTIFICATION / REPLACEMENT EASA AD 2015-0004 AS IN AD AS IN AD

DGCA/A320 family/304R1 ATA 53, FUSELAGE – FUSELAGE SKIN REPAIRS – INSPECTION

EASA AD 2015-0036R1 REVISION

AS IN AD AS IN AD

DGCA/A320 family/305R1 ATA 71,POWERPLANT – FORWARD ENGINE MOUNT – INSPECTION

EASA AD 2015-0038R1 REVISED EASA AD 2015-0038

AS IN AD AS IN AD

DGCA/A320 family/306 ATA 27,FLIGHT CONTROLS – TRIMMABLE HORIZONTAL STABILIZER ACTUATOR – IDENTIFICATION / REPLACEMENT

EASA AD 2015-0080 AS IN AD AS IN AD

DGCA/A320 family/307R1 ATA- 27,FLIGHT CONTROLS – ELEVATOR AILERON COMPUTERS – REPLACEMENT / SOFTWARE UPDATE

EASA AD 2015-0088R1 REV AS IN AD AS IN AD

DGCA/A320 family/308 ATA–25, EQUIPMENT / FURNISHINGS – OVERHEAD STOWAGE COMPARTMENT ATTACHMENTS – MODIFICATION

EASA AD 2015-0164 AS IN AD AS IN AD

DGCA/A320 family/309 ATA 92 ELECTRIC AND ELECTRONIC COMMON INSTALLATION – COCKPIT PANEL BRACKET – INSPECTION

EASA AD 2015-0170 AS IN AD AS IN AD

DGCA/A320 family/310 ATA- AIRPLANE FLIGHT MANUAL-SECTION NORMAL PROCEDURES/AFTER START-AMENDMENT

EASA AD 2015-0191 AS IN AD AS IN AD

DGCA/A320 family/311 ATA-34, NAVIGATION-AIRSPEED PILOT PROBES-REPLACEMENT

EASA AD 2015-0205 AS IN AD AS IN AD

DGCA/A320family/312 ATA-53, FUSELAGE-CABIN/CARGO COMPARTMENT PARTS-INSPECTION/REPLACEMENT (IMPROPER HEAT TREATMENT)

EASA AD 2015-0219 AS IN AD AS IN AD

DGCA/A320family/313 ATA-53, FUSELAGE-CABIN/CARGO COMPARTMENT PARTS-INSPECTION/REPLACEMENT (WRONG MATERIAL)

EASA AD 2015-0218 AS IN AD AS IN AD

DGCA/A320family/314 ATA-71, POWER PLANT-FORWARD ENGINE MOUNT BOLTS-INSPECTION/REPLACEMENT

EASA AD 2015-0229 AS IN AD AS IN AD

DGCA/A320family/315R1 (CANCELLED)

ATA-52, DOORS-MAIN LANDING GEAR DOOR TIE ROAD ASSEMBLY-INSPECTION

EASA AD 2015-0234-CN SUPERSEDED EASA AD 2015-0234

AS IN AD AS IN AD

Page 23: airbus a318,a319,a320,a321

DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/A320family/316 ATA-57, WINGS-OUTER WING MAIN LANDING GEAR

SUPPORT RIB 5 FITTING-INSPECTION/MODIFICATION EASA AD 2012-0032R1 AS IN AD AS IN AD

DGCA/A320family/317R1 ATA-53, FUSELAGE-DOOR STOP FITTING HOLES-INSPECTION/REPAIR

EASA AD 2016-0238 AS IN AD AS IN AD

DGCA/A320family/318R1 ATA-32, LANDING GEAR-MAIN LANDING GEAR SIDE STAY ASSEMBLIES-REPLACEMENT/ MODIFICATION

EASA AD 2016-0018R1 AS IN AD AS IN AD

DGCA/A320family/319 ATA-25, EQUIPMENT/FURNISHINGS-BUFFET AND GALLEY/TROLLEY COMPARTMENTS-MODIFICATION

EASA AD 2016-0040 AS IN AD AS IN AD

DGCA/A320family/320 ATA-71, POWER PLANT-FAN COWL DOOR LATCH WITH KEY AND FLAG, IAE ENGINES-MODIFICATION

EASA AD 2016-0053 AS IN AD AS IN AD

DGCA/A320family/321R1 ATA-78, EXHAUST-THRUST REVERSER PIVOT FITTING-INSPECTION

EASA AD 2016-0076 AS IN AD AS IN AD

DGCA/A320family/322R1 ATA-71, POWER PLANT-FAN COWL DOOR LATCH WITH KEY AND FLAG, CFM ENGINES-MODIFICATION

EASA AD 2016-0257 AS IN AD AS IN AD

DGCA/A320family/323 ATA-27, FLIGHT CONTROLS-SPOILER ELEVATOR COMPUTER SOFTWARE UPDATE

EASA AD 2016-0056 AS IN AD AS IN AD

DGCA/A320family/324 ATA-22, AUTO FLIGHT-FLIGHT MANAGEMENT AND GUIDANCE COMPUTER-REPLACEMENT

EASA AD 2016-0122 AS IN AD AS IN AD

DGCA/A320family/325 ATA-53, FUSELAGE-CROSSBEAM SPLICING AT FRAMES 16 AND 20 - INSPECTION

EASA AD 2016-0139 AS IN AD AS IN AD

DGCA/A320family/326 ATA-53, FUSELAGE-FRAMES 35/ SLIDEBOX JUNCTION - INSPECTION

EASA AD 2016-0146 AS IN AD AS IN AD

DGCA/A320family/327R1 ATA-05, TIME LIMITS/MAINTENANCE CHECKS-AIRWORTHINESS LIMITATIONS SECTION PART 3-CERTIFICATION MAINTENANCE REQUIREMENTS-IMPLEMENTATION

EASA AD 2017-0168 SUPERSEDED EASA AD 2016-0092

AS IN AD AS IN AD

DGCA/A320family/328 ATA-53, FUSELAGE-CABIN FLOOR BEAM JUNCTION-INSPECTION

EASA AD 2016-0105 AS IN AD AS IN AD

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

Page 24: airbus a318,a319,a320,a321

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]

AS IN AD AS IN AD

DGCA/A320family/332 AIRCRAFT FLIGHT MANUAL – SECTION LIMITATIONS / FUEL GRAVITY FEED PROCEDURE – AMENDMENT

EASA AD 2016-0205 AS IN AD AS IN AD

DGCA/A320family/333 ATA-53 – FUSELAGE – CENTRAL VERTICAL STRUT AT FRAME 65 – MODIFICATION

EASA AD 2016-0212 AS IN AD AS IN AD

DGCA/A320family/334 ATA-57 – WINGS – BOTTOM PANEL 2 AT RIB 2 INTERFACE – INSPECTION

EASA AD 2016-0222 AS IN AD AS IN AD

DGCA/A320family/335R2 ATA-34 –NAVIGATION –TRAFFIC COLLISION AVOIDANCE SYSTEM PROCESSOR –MODIFICATION (SOFTWARE UPDATE) / REPLACEMENT

EASA AD 2017-0091R2 AS IN AD AS IN AD

DGCA/A320family/336 ATA 57 – WING – STRINGER ATTACHMENTS AT RIB 2 TO RIB 7 – MODIFICATION

EASA AD 2017-0117 AS IN AD AS IN AD

DGCA/A320family/337 ATA 71 – ENGINE – FORWARD ENGINE MOUNT MAIN BEAM SNOUT – REPLACEMENT

EASA AD 2017-0132 AS IN AD AS IN AD

DGCA/A320family/338 ATA 71 – POWER PLANT – MONOLITHIC FAN COWL DOORS – MODIFICATION

EASA AD 2017-0178 AS IN AD AS IN AD