subject reference compliance applicabilitydgca.nic.in/mandmod/aircraft/airbus 330.pdf · easa ad...

DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY

DGCA/A 330/01 AFT ATTACHMENT TRACK 2 TO 5 OF INBOARD /OUTBOARD FLAP (LH/RH) GUIDE BUSHES

DGAC AD F-1995-124-012 (B) AS IN AD AS IN AD

DGCA/A 330/02 REAR TRACKS TO WING ATTACHMENT AT TRACKS 2 TO 5 OF TRAILING EDGES (LH/RH) SPHERICAL WASHERS


DGCA/A 330/03 THOMSON LOW RANGE RADIO ALTIMETER (LRRA) DGAC AD F-1995-271-025 R2 (B) AS IN AD AS IN AD

DGCA/A 330/04 FUSELAGE - REINFORCEMENT OF JOINT AT FRAMES 48 TO 53.2 BETWEEN STRINGERS 24 TO 26

DGAC AD F-1996-006-024 R1 (B) AS IN AD AS IN AD

DGCA/A 330/05 AFT CARGO COMPARTMENT DOOR DGAC AD F-1996-106-030 (B) AS IN AD AS IN AD

DGCA/A 330/06 OVERRIDE MECHANISM OF TRIMMABLE HORIZONTAL STABILIZER


DGCA/A 330/07R2 EXHAUST – THRUST REVERSER OPENING MECHANISM – INSPECTION

EASA AD 2010-0187R1 AS IN AD AS IN AD

DGCA/A 330/08 FWD FLAP TRACK ATTACHMENTS 3 THRU 5 OF INBOARD/OUTBOARD FLAP


DGCA/A 330/09 REAR FUSELAGE - FRAME 73A INSPECTION DGAC AD F-1997-270-055 (B) AS IN AD AS IN AD

DGCA/A 330/10 ALTERNATE BRAKING SYSTEM CHECK DGAC AD F-1998-264-075 R4 (B) AS IN AD AS IN AD

DGCA/A 330/11 MAIN LANDING GEAR - DOORS DGAC AD F-1998-268-073 R3 (B) AS IN AD AS IN AD

DGCA/A 330/12 PRATT & WHITNEY PW4164, PW4168 AND PW4168A ENGINES - REPLACEMENT OF CASCADE AFT SUPPORTS


DGCA/A 330/13 FUEL TRIM TRANSFER - INSPECTION OF THE TRIM TRANSFER LINE BETWEEN FRAMES FR77 AND FR86 AND ASSOCIATED FLIGHT OPERATIONAL PROCEDURE


DGCA/A 330/14 INSPECTION OF "MOOG" AILERON SERVO-CONTROLS DGAC AD F-2000-014-108 (B) AS IN AD AS IN AD

DGCA/A 330/15 WING - REPLACEMENT OF CLEARANCE FIT BOLTS BY INTERFERENCE BOLTS AT RIBS 2 AND 7


DGCA/A 330/16 WING - REPLACEMENT OF EXISTING INTERFERENCE FIT BOLTS AT RIBS 9 AND 11


DGCA/A 330/17 FUSELAGE - INSPECTION OF FR73A AT DOOR STOP FITTING DGAC AD F-2000-126-114 (B) AS IN AD AS IN AD


NO. 5

DGCA/A 330/18 WINGS - TRAILING EDGE - DRAIN HOLE IN SKIN PANEL 3 (BOTTOM)


DGCA/A 330/19R1 DOORS - PAX/CREW AND EMERGENCY EXIT DOORS - GIRT BAR SLIDER MECHANISM -- FUNCTIONAL CHECK & LUBRICATION

EASA AD 2010 - 0135 AS IN AD AS IN AD

DGCA/A 330/20 AIRSPEED INDICATION - AIRSPEED FLUCTUATIONS IN ICING CONDITIONS

DGAC AD F-2001-069 (B) AS IN AD AS IN AD

DGCA/A 330/21 AFT CARGO COMPARTMENT DOOR INSPECTION DGAC AD F-2001-126 (B) AS IN AD AS IN AD

DGCA/A 330/22R2 WINGS - INNER REAR SPAR UPPER BUILD SLOT - INSPECTION / MODIFICATION

EASA AD 2013-0101 AS IN AD AS IN AD

DGCA/A 330/23 ENGINE - ROLLS-ROYCE ENGINE STALL AND SHUT DOWN DURING ACCELERATION FROM IDLE

DGAC AD F-2001-383 R3 (B) AS IN AD AS IN AD

DGCA/A 330/24 INSPECTION OF LOWER FLANGE AND RADIUS OF FLOOR BEAM BETWEEN FR47 AND FR48


DGCA/A 330/25R1 EXHAUST - THRUST REVERSERS - C-DUCTS - LIFE LIMITS EASA AD 2011-0018 AS IN AD AS IN AD

DGCA/A 330/26R4 TIME LIMITS AND MAINTENANCE CHECKS - AGEING SYSTEMS MAINTENANCE - ALS PART 4 - AMENDMENT

EASA AD 2017-0228 SUPERSEDED EASA AD 2016-0011

AS IN AD AS IN AD



DGCA/A 330/28 GE POWERPLANT - FORWARD MOUNT BOLTS DGAC AD F-2001-556 (B) AS IN AD AS IN AD

DGCA/A 330/29 WINGS - REAR SPAR - WIRE HARNESS SLOT DGAC AD F-2001-578 (B) AS IN AD AS IN AD

DGCA/A 330/30R3 ATA 27, FLIGHT CONTROLS – TRIMMABLE HORIZONTAL STABILIZER ACTUATOR –INSPECTION / MODIFICATION




DGCA/A 330/32 FORWARD FUSELAGE - INSPECTION OF FRAME 12A DGAC AD F-2003-205 (B) AS IN AD AS IN AD


STIFFENER

DGCA/A 330/33 FUEL - INSPECTION FOR CORRECT CLOSURE OF THE LOW PRESSURE SHUT-OFF VALVE


DGCA/A 330/34(R2) FUSELAGE - FRAME 53.3 CIRCUMFERENTIAL JOINT -REINFORCEMENT


DGCA/A 330/35 WINGS - OUTBOARD FLAP - INSPECTION AND MODIFICATION OF SENSOR STRUT AT FLAP TRACK 4


DGCA/A 330/36 LANDING GEAR - NOSE WHEEL STEERING LIMITS DGAC AD F-2003-433 R1 (B) AS IN AD AS IN AD

DGCA/A 330/37(R1) FLIGHT CONTROLS - ELEVATOR SERVO CONTROLS -MODE SELECTOR VALVE POSITION TRANSDUCER


DGCA/A 330/38 NACELLES/PYLONS - PW 4000 ENGINES PYLONS - INSPECTION OF THE LOWER AFT PYLON FAIRING


DGCA/A 330/39 LANDING GEAR - INSPECTION OF MAIN LANDING GEAR RETRACTION ACTUATOR LOWER PIN (P-PIN)


DGCA/A 330/40 EQUIPMENT/FURNISHINGS - SLIDE RAFTS AND SLIDES FITTED ON TYPE A PASSENGER/CREW DOORS AND TYPE 1 EMERGENCY DOORS - MODIFICATION OF THE VESPEL PISTON OF REGULATOR VALVE


DGCA /A 330 /41R1 STABILIZERS - ELEVATORS - INSPECTION EASA AD 2009 - 0255 AS IN AD AS IN AD

DGCA/A 330/42 WINGS - WINGBOX - INSPECTION OF THE JETTISON VALVES AND MODIFICATION OF MOUNTING HOLES


DGCA/A 330/43R2 FLIGHT CONTROLS – ELEVATOR SERVO CONTROL SOLENOID VALVE O-RING SEALS – REPLACEMENT & AIRPLANE FLIGHT MANUAL / MASTER MEL – TEMPORARY REVISION & ELEVATOR SERVO CONTROLS – MODIFICATION & PRIMARY AND SECONDARY COMPUTERS – MODIFICATION


DGCA/A 330/44 LOSS OF INTEGRATED STANDBY INSTRUMENT SYSTEM (ISIS) DGAC AD F-2004-167 (B) AS IN AD AS IN AD

DGCA/A 330/45 FUEL - THS FUEL TANKS - INTERTECHNIQUE OUTBOARD DGAC AD F-2005-003 (B) AS IN AD AS IN AD


VENT FLOAT VALVES LIFE LIMIT

DGCA/A 330/46 FUEL - THS FUEL TANKS - INSPECTION AND MODIFICATION OF THE ARGO-TECH OR INTERTECHNIQUE VENT FLOAT VALVES




DGCA/A 330/48 NOSE LANDING GEAR - MODIFICATION OF HYDRAULIC CONTROL BLOCK


DGCA/A 330/49 FIRE PROTECTION - INSPECTION FOR CLEANING OF THE FIRE EXTINGUISHING SYSTEM IN LDCC CARGO COMPARTMENT


DGCA/A 330/50 EQUIPMENT/FURNISHINGS - NON TEXTILE FLOOR (NTF) REPLACEMENT


DGCA/A 330/51 STABILIZERS - CARBON FIBER-REINFORCED PLASTIC (CFRP) RUDDER


DGCA/A 330/52 LEADING EDGE SLAT - INSPECTION AND REPLACEMENT OF ROTARY ACTUATOR TYPE A


DGCA/A 330/53 EQUIPMENT/FURNISHINGS - EMERGENCY ESCAPE SLIDES AND SLIDE RAFTS - INSPECTION OF ELECTRICAL HARNESS ROUTING


DGCA/A 330/54R2 LANDING GEAR - MAIN LANDING GEAR RETRACTION ACTUATOR PISTON ROD - INSPECTION /MODIFICATION


DGCA/A 330/55 EQUIPMENT/FURNISHINGS - COCKPIT SEATS ACTUATORS INSPECTION AND REPLACEMENT


DGCA/A 330/56 ENGINE FUEL AND CONTROL - FADEC 2000-10BP1 REPLACEMENT


DGCA/A 330/57 ELEVATOR SERVOCONTROLS - ADDITIONAL PERIODIC TEST OF THE SERVO-LOOPS


DGCA/A 330/58 FUEL - FUEL LEAK PROCEDURE DGAC AD F-2005-195 (B) AS IN AD AS IN AD


DGCA/A 330/59 NOSE LANDING GEAR - INSPECTION AND MODIFICATION OF THE NOSE WHEEL STEERING SYSTEM - ROTATING SLEEVE


DGCA/A 330/60 WING --- LH & RH WING RIB 6 ---INSPECTION / MODIFICATION

EASA AD 2007 -0148 AS IN AD AS IN AD

DGCA/A 330/61 EQUIPMENT/FURNISHINGS – COCKPIT INSTRUMENT PANEL -- INSPECTION / REPLACEMENT / MODIFICATION


DGCA/A 330/62 WINGS - LEADING EDGE - MODIFICATION OF BLOW-DOWN PANELS


DGCA/A 330/63 WINGS - WING SHROUD BOX BOTTOM PANEL - MODIFICATION


DGCA/A 330/64 STABILIZERS - CFRP (CARBON FIBRE REINFORCED PLASTIC) RUDDER - INSPECTION.


DGCA/A 330/65R3 ATA-05, TIME LIMITS & MAINTENANCE CHECKS -DAMAGE TOLERANT AIRWORTHINESS LIMITATIONS ITEMS --- ALS PART 2 --- IMPLEMENTATION


DGCA/A 330/66 TIME LIMITS - SAFE LIFE AIRWORTHINESS LIMITATION ITEMS – ALS PART 1

EASA AD 2007-0133(REVISION ONE)

AS IN AD AS IN AD

DGCA/A 330/67 AIR CONDITIONING - ZONAL DRYING SYSTEM DEACTIVATION EASA AD 2006-0140-E AS IN AD AS IN AD

DGCA/A 330/68R1 TIME LIMITS & MAINTENANCE CHECKS -- AGEING SYSTEMS MAINTENANCE --- ALS PART 4 --- AMENDMENT


DGCA/A 330/69R2 TIME LIMITS & MAINTENANCE CHECKS --- AIRWORTHINESS LIMITATIONS SECTION PART 5 --- FUEL AIRWORTHINESS LIMITATIONS --- AMENDMENT


AS IN AD AS IN AD

DGCA/A 330/70 INDICATING/RECORDING SYSTEMS - PERIODIC RESET AND MODIFICATION OF DISPLAY UNITS


DGCA/A 330/71(R2) TIME LIMITS & MAINTENANCE CHECKS --- AIRWORTHINESS LIMITATIONS SECTION PART 5 --- FUEL AIRWORTHINESS LIMITATIONS --- AMENDMENT


DGCA/A 330/72 ENGINE - ICING CONDITION DURING DESCENT - EASA AD 2007- 0215 AS IN AD AS IN AD


OPERATIONAL PROCEDURE AND DISPATCH RESTRICTION / MODIFICATION

DGCA/A 330/73R4 TIME LIMITS & MAINTENANCE CHECKS - CERTIFICATION MAINTENANCE REQUIREMENTS --- ALS PART 3 --- AMENDMENT

EASA AD 2016-0066 SUPERSEDED EASA AD 2013 - 0245

AS IN AD AS IN AD

DGCA/A 330/74 NAVIGATION – INERTIAL REFERENCE SYSTEMS EASA AD 2006-0232 AS IN AD AS IN AD

DGCA/A 330/75 FIRE PROTECTION - ENGINE FIRE EXTINGUISHING BOTTLE PIPE - INSPECTION


DGCA/A 330/76 TIME LIMITS / MAINTENANCE CHECKS -DAMAGE TOLERANT AIRWORTHINESS LIMITATIONS ITEMS --- ALS PART 2 --- AMENDMENT


DGCA/A 330/77 FLIGHT CONTROLS - BACK UP CONTROL MODULE (BCM) - OPERATIONAL TEST / REPLACEMENT


DGCA / A 330 / 78R3 WINGS - CENTRE WING BOX - KEEL BEAM FASTENER HOLES AT FRAME 40 - INSPECTION

EASA AD 2014-0010R1 REVISION AS IN AD AS IN AD



DGCA/A 330/80R2 TIME LIMITS/MAINTENANCE CHECKS --- SAFE LIFE AIRWORTHINESS LIMITATIONS ITEMS --- ALS PART 1 --- AMENDMENT


DGCA/A 330/81 FUSELAGE - SKIN - INSPECTION/ REPAIR EASA AD 2006-0332 AS IN AD AS IN AD

DGCA/A 330/82 EQUIPMENT/FURNISHINGS - SLIDE RAFTS FITTED ON TYPE A DOORS - MODIFICATION


DGCA/A 330/83R3 ATA--57,WINGS - MAIN LANDING GEAR RIB 6 AFT BEARING LUGS - INSPECTION /REPLACEMENT


DGCA/A 330/84(R1) ELECTRICAL POWER/AUXILLARY POWER UNIT---OIL PUMP MODULE---INSPECTION

EASA AD 2007-0080-R1 AS IN AD AS IN AD

DGCA/A 330/85R1 LANDING GEAR---NOSE WHEEL STEERING SYSTEM--- EASA AD 2007-0070R1 AS IN AD AS IN AD


ROTATING SLEEVE---INSPECTION/MODIFICATION

DGCA/A 330/86 FUSELAGE --- LONGITUDINAL JOINT AT STRINGER 28 RH BETWEEN FR 18 AND FR 19 -- INSPECTION


DGCA/A 330/87 EXHAUST -- THRUST REVERSER HINGE nº 5 -- SLEEVE & PIN REPLACEMENT


DGCA/A 330/88R1 ELECTRICAL POWER / AIRBORNE AUXILLARY POWER -- AUXILLARY POWER UNIT (APU) GENERATOR ---INSPECTION/MODIFICATION

EASA AD 2008 - 0173R1 AS IN AD AS IN AD

DGCA/A 330/89 FUEL -- ENGINE FEED LINE --- OPERATIONAL PROCEDURE EASA AD 2007- 0216 - E AS IN AD AS IN AD


EASA AD 2013- 0268 AS IN AD AS IN AD

DGCA/A 330/91 FUEL --- REFUEL ISOLATION VALVE --- REPLACEMENT EASA AD 2007 - 0239 AS IN AD AS IN AD

DGCA/A 330/92 FLIGHT CONTROLS ---- RUDDER CONTROL ROD ---- INSPECTION/REPLACEMENT


DGCA/A 330/93R1 FUSELAGE --- CONE/REAR FUSELAGE --- SECTION 19 ---INSPECTION /MODIFICATION


DGCA/A 330/94R2 FUSELAGE -- LONGITUDINAL DOUBLER AT VERTICAL TAIL PLANE ATTACHMENT CUT OUT --- INSPECTION / MODIFICATION


DGCA/A 330/95 FUSELAGE -- FORWARD FUSELAGE -- FRAME 12 -- INSPECTION/REPAIR


DGCA/A 330/96(R5) ATA 32 - LANDING GEAR -- MAIN LANDING GEAR BOGIE BEAM --- INSPECTION/REPAIR/MODIFICATION

EASA AD 2013-0267R1 CORRECTION

AS IN AD AS IN AD

DGCA/A 330/97 STABILIZERS -- CARBON FIBER REINFORCED PLASTIC (CFRP) RUDDER -- INSPECTION/REPAIR


DGCA/A 330/98R2 ATA 27- FLIGHT CONTROLS -- FLIGHT CONTROL PRIMARY COMPUTER (FCPC) -- DISPATCH RESTRICTION & OPERATIONAL TEST

EASA AD 2010 - 0109 R1 AS IN AD AS IN AD


DGCA/A 330/99 POWERPLANT --- ENGINE MOUNT LINK PIN RETENTION BOLTS --- INSPECTION/REPLACEMENT


DGCA/A 330/100 ENGINE/ENGINE FUEL & CONTROL ---- INTERMEDIATE PRESSURE TURBINE OVER SPEED (IPTOS) PROTECTION --- FUNCTION ACTIVATION


DGCA/A 330/101R2 FLIGHT CONTROLS – FLIGHT CONTROL PRIMARY COMPUTER (FCPC) – PRIM 3 DISPATCH RESTRICTION / MODIFICATION


DGCA/A 330/102 ELECTRICAL/ELECTRONIC SYSTEMS -- PASSENGER COMPARTMENT ELECTRICAL HARNESS --- MODIFICATION




DGCA/A 330/104 WINGS --- MOVABLE FLAP TRACK FAIRING NO 3 --- MODIFICATION/ REPLACEMENT


DGCA/A 330/105 FIRE PROTECTION --- ENGINE FIRE EXTINGUISHER BOTTLE CONNECTION --- INSPECTION/REPLACEMENT


DGCA/A 330/106 NAVIGATION --- AIR DATA INERTIAL REFERENCE UNIT (ADIRU) --- OPERATIONAL PROCEDURE

EASA AD 2009 - 0012 -E AS IN AD AS IN AD

DGCA/A- 330/107R1 FUEL -- FUEL PUMP NON RETURN VALVE(NRV)---OPERATIONAL TEST

EASA AD 2010 - 0083 - CN STANDS CANCELLED

DGCA/A 330/108R1 FUSELAGE -- CENTRE FUSELAGE -- FR 40 KEEL BEAM FLANGE -- INSPECTION /REPAIR


DGCA/A 330/109R4 ATA-32, LANDING GEAR – MAIN LANDING GEAR BOGIE BEAM – INSPECTION / REPAIR

AS IN AD AS IN AD

DGCA/A 330/110 WINGS --- CENTRE WING --- FRAME (FR) 40 REAR FITTING WEB --- INSPECTION


DGCA/A 330/111 FIRE PROTECTION --- FIRE EXTINGUISHING SYSTEM --- REPLACEMENT/MODIFICATION


DGCA/A 330/112 ELECTRIC & ELECTRONIC COMMON INSTALLATION --- HAT- RACK CONNECTORS --- MODIFICATION



DGCA/A 330/113 ELECTRIC & ELECTRONIC COMMON INSTALLATION --- ROUTING --- INSTALLATION / MODIFICATION






DGCA / A 330 / 116R1

STABILIZERS --- RUDDER SIDE SHELL SKIN --- INSPECTION EASA AD 2010 - 0021 AS IN AD AS IN AD

DGCA/A 330/117R5 TIME LIMITS AND MAINTENANCE CHECKS - SAFE LIFE AIRWORTHINESS LIMITATION ITEMS --- ALS PART 1 --- AMENDMENT

EASA AD 2018-0034 SUPERSEDED EASA AD 2014 - 0009

AS IN AD AS IN AD

DGCA/A 330/118 NAVIGATION --- AIRSPEED PITOT PROBES --- REPLACEMENT EASA AD 2009 - 0195 AS IN AD AS IN AD

DGCA/A 330/119R2 ATA 34 - NAVIGATION --- PITOT PROBE QUICK --- DISCONNECT UNION --- TORQUE CHECK


DGCA/A 330/120R6 ATA 29, HYDRAULIC POWER – HIGH PRESSURE MANIFOLD CHECK VALVES – INSPECTION / MODIFICATION


DGCA/A 330/121R1 OXYGEN --- OXYGEN CONTAINERS --- INSPECTION EASA AD 2009 - 0237 -E CORRECTED ON 13TH JAN 2010

AS IN AD AS IN AD

DGCA/A 330/122 POWERPLANT --- FORWARD & AFTWARD MOUNT PYLON BOLTS --- INSPECTION/REPLACEMENT


DGCA/A 330/123 SSAD AS IN AD AS IN AD

DGCA/A 330 /124R1 HYDRAULIC POWER --- RAM AIR TURBINE (RAT) BALANCE WEIGHT SCREWS --- INSPECTION/REPLACEMENT

EASA AD 2009 -0260 CORRECTED ON 14TH DEC 2009

AS IN AD AS IN AD

DGCA/A -330 / 125R2

NAVIGATION --- ANGLE OF ATTACK SENSORS --- REPLACEMENT


DGCA/A 330/126 FUEL --- WING TANK FUEL PRESSURE SWITCH --- REPLACEMENT



DGCA/A 330/127R1 LANDING GEAR --- NOSE LANDING GEAR (NLG) MAIN FITTING AND SLIDING TUBE --- INSPECTION


DGCA/A 330/128R3 CANCELLED: FUEL ---MAIN FUEL PUMP SYSTEM WATER SCAVENGE SYSTEM --- DEACTIVATION

EASA AD 2010 -0132-CN AS IN AD AS IN AD

DGCA/A 330/129R1 ELECTRIC AND ELECTRONIC COMMON INSTALLATION --- HYDRAULIC PUMP ELECTRICAL MOTOR CONNECTORS --- MODIFICATION




DGCA/A 330/131R1 ELECTRIC AND ELECTRONIC COMMON INSTALLATION – CABLE LOOM INSTALLATION -- MODIFICATION


DGCA/A 330/132 STABILIZERS --- RUDDER SIDE SHELL SKIN --- INSPECTION EASA AD 2010 - 0127 AS IN AD AS IN AD

DGCA/A 330/133R1 FUSELAGE --- FUSELAGE INTERNAL STRUCTURE AT FRAME 39.1 --- INSPECTION




DGCA/A 330/135 FUSELAGE --- NUTS --- INSPECTION / REPLACEMENT EASA AD 2010 - 0252 AS IN AD AS IN AD

DGCA/A 330/136R1 FLIGHT CONTROLS -- WING TIP BRAKES (WTB)-- OPERATIONAL TEST/REPLACEMENT


DGCA/A 330/137 AUTO FLIGHT ---AUTO PILOT & AUTO THRUST DISCONNECT --- OPERATIONAL PROCEDURE


DGCA/A 330/138R1 DOORS --- FORWARD AND AFT CARGO COMPARTMENT DOORS --- INSPECTION


DGCA/A 330/139 LANDING GEAR --- NOSE LANDING GEAR (NLG) --- NLG MAIN FITTING --- MODIFICATION


DGCA/A 330/140R1 LANDING GEAR --- MAIN AND CENTER LANDING GEAR BOGIE PIVOT PINS --- INSPECTIONS



DGCA/A 330/141R2 ATA-71, POWERPLANT-- ENGINE AIR INTAKE COWL ASSEMBLY --- PICCOLO TUBE --- INSPECTION


DGCA/A 330/142 FIRE PROTECTION --- FIRE DETECTION UNIT (FDU) --- INSPECTION / REPLACEMENT


DGCA/A 330/143R2 TIME LIMITS AND MAINTENANCE CHECKS --- SAFE LIFE AIRWORTHINESS LIMITATION ITEMS --- ALS PART 1 --- AMENDMENT


AS IN AD AS IN AD

DGCA/A 330/144R2 ATA 32 - LANDING GEAR - MAIN LANDING GEAR (MLG) WHEEL AXLE - REDUCED LIFE LIMIT FOLLOWING REPAIR


AS IN AD AS IN AD

DGCA/A 330/145R1 ATA 53- FUSELAGE - FRAME (FR) 40 / FUSELAGE SKIN PANEL JUNCTION - INSPECTION


DGCA/A 330/146R1 ATA 71 - POWER PLANT - ENGINE AIR INLET COWL ACOUSTIC PANELS - INSPECTION


DGCA/A 330/147R1 ATA 52 - DOORS - FORWARD AND AFT CARGO DOORS – INSPECTION / REPLACEMENT

EASA AD 2011-0177 (CORRECTION: 28 SEPTEMBER 2011)

AS IN AD AS IN AD



DGCA/A 330/149 HYDRAULIC POWER --- RAM AIR TURBINE (RAT) PUMP --- ANTI STALL DEVICE --- INSPECTION / REPLACEMENT


DGCA/A 330/150R1 HYDRAULIC POWER --- RAM AIR TURBINE ACTUATOR --- IDENTIFICATION / REPLACEMENT


DGCA/A 330/151R1 AUTO FLIGHT / FLIGHT CONTROLS --- FLIGHT CONTROL PRIMARY COMPUTER (FCPC) --- MODIFICATION / REPLACEMENT


DGCA/A 330/152R2 TIME LIMITS AND MAINTENANCE CHECKS --- SAFE LIFE AIRWORTHINESS LIMITATION ITEMS --- ALS PART 1 ---

EASA AD 2018-0034 SUPERSEDED EASA AD 2014-

AS IN AD AS IN AD


AMENDMENT 0009

DGCA/A 330/153R2 WINDOWS --- FIXED WINDOWS / WINDSHIELD HEATING CONNECTORS --- INSPECTION/REPLACEMENT


DGCA/A 330/154 FLIGHT CONTROLS --- SPOILER SERVO CONTROLS (SSC) --- IDENTIFICATION/ OPERATIONAL TEST


DGCA/A 330/155 FUSELAGE --- BELLY FAIRING RODS --- INSPECTION EASA AD 2012-0005 AS IN AD AS IN AD

DGCA/A 330/156 R1 LANDING GEAR --- NOSE LANDING GEAR (NLG) RETRACTION ACTUATOR OVERHAUL


DGCA/A 330/157 R1 FLIGHT CONTROLS --- TRIMMABLE HORIZONTAL STABILIZER ACTUATOR BALLSCREW LOWER SPLINES -- INSPECTION/ REPLACEMENT


DGCA/A 330/158 NAVIGATION --- RADIO ALTIMETER ERRONEOUS INDICATION --- OPERATIONAL PROCEDURE


DGCA/A 330/159 ENGINE --- FORWARD ENGINE MOUNT BOLTS --- TORQUE CHECK / REPLACEMENT


DGCA/A 330/160 AIR CONDITIONING --- BULK CARGO ISOLATION VALVE BONDING LEAD AND ROUTE 1M --- MODIFICATION


DGCA/A 330/161 ELECTRIC AND ELECTRONIC COMMON INSTALLATION --- HARNESS 5877VB IN SECTION 19.1 --- REPLACEMENT


DGCA/A 330/162 ATA 27 - FLIGHT CONTROLS - TRIMMABLE HORIZONTAL STABILIZER ACTUATOR (THSA) BALL SCREW - INTEGRITY CHECK


DGCA/A 330/163R2 NAVIGATION - ANGLE OF ATTACK PROBE CONIC PLATES --- OPERATIONAL PROCEDURE/REPLACEMENT


DGCA/A 330/164 AUTO FLIGHT / FLIGHT CONTROLS --- FLIGHT CONTROL PRIMARY COMPUTER --- MODIFICATION / REPLACEMENT


DGCA/A 330/165 DOORS --- FORWARD AND AFT CARGO COMPARTMENT DOORS --- INSPECTION / REPAIR



DGCA/A 330/166R1 FIRE PROTECTION / LIGHTS / PNEUMATIC / FUSELAGE --- PREVENTION AGAINST EXPLOSION RISKSSECTION 19 --- MODIFICATIONS

EASA AD 2014-0148 SUPERSEDURE

AS IN AD AS IN AD

DGCA/A 330/167R4 FUSELAGE --- TRIMMABLE HORIZONTAL STABILIZER SUPPORT STRUTS --- INSPECTION / REPLACEMENT

EASA AD 2014-0068R2 REVISED EASA AD 2014-0068 R1

AS IN AD AS IN AD

DGCA/A 330/168R1 POWERPLANT -- UPPER AFT MOUNT BOLTS -- INSPECTION / REPAIR

EASA AD 2015-0126 SUP AS IN AD AS IN AD

DGCA/A 330/169R3 FLIGHT CONTROLS --- TRIMMABLE HORIZONTAL STABILIZER ACTUATOR --- IDENTIFICATION/REPLACEMENT

EASA AD 2014-0257R1 revIsion AS IN AD AS IN AD

DGCA/A 330/170 ELECTRICAL POWER --- GENERATOR CONTROL UNIT --- INSPECTION


DGCA/A 330/171R1 ATA 92, ELECTRIC & ELECTRONIC COMMON INSTALLATION – HARNESS AT DOOR 3 AREA –MODIFICATION


DGCA/A 330/172 AIR CONDITIONING --- CABIN PRESSURE CONTROL SYSTEM SAFETY VALVE --- REPLACEMENT


DGCA/A 330/173 FUSELAGE --- CENTER LANDING GEAR DOOR / STRUCTURE --- JOINT AREA BETWEEN FRAME 49 & 53.2 --- INSPECTION


DGCA/A 330/174R2 ATA 26,FIRE PROTECTION – FIRE EXTINGUISHER HOSE ASSEMBLY – REPLACEMENT

EASA AD 2014-0248 SUPER AS IN AD AS IN AD

DGCA/A 330/175 FLIGHT CONTROLS --- SPOILER SERVO CONTROL / HYDRAULIC LOCKING FUNCTION --- OPERATIONAL TEST


DGCA/A 330/176R1 STABILIZERS --- RUDDER SIDE PANEL ALONG THE Z - PROFILE --- INSPECTION


DGCA/A 330/177 HYDRAULIC POWER --- RAM AIR TURBINE HYDRAULIC PUMPS --- IDENTIFICATION / REPLACEMENT


DGCA/A 330/178 FIRE PROTECTION --- EXTINGUISHING PIPE BETWEEN FRAME (FR) 34 AND FR 36 --- MODIFICATION


DGCA/A 330/179 STABILIZERS --- RUDDER SIDE SHELL SANDWICH REPAIR --- INSPECTION



DGCA/A 330/180R1 AUTO FLIGHT – AUTO PILOT / FLIGHT DIRECTOR TCAS FUNCTION – DE-ACTIVATION


DGCA/A 330/181 EXHAUST – THRUST REVERSER COWL DOOR HINGE SLEEVES –IDENTIFICATION / REPLACEMENT


DGCA/A 330/182R2 LANDING GEAR – MAIN LANDING GEAR SIDE STAY UPPER CARDAN PIN – INSPECTION

EASA AD 2014-0079 supersedure AS IN AD AS IN AD

DGCA/A 330/183 ATA 25,EQUIPMENT/FURNISHINGS – COCKPIT INSTRUMENT PANEL BRACKETS – INSPECTION / REPLACEMENT


DGCA/A 330/184R1 ATA 57,WINGS – CENTER WING BOX FASTENER HOLES AT FRAME 40 VERTICAL WEB – INSPECTION


DGCA/A-330/185R1 ATA 53, FUSELAGE – FRAME (FR) 40 / FUSELAGE SKIN PANEL JUNCTION – INSPECTION


DGCA/A-330/186 ATA 92, ELECTRIC / ELECTRONIC COMMON INSTALLATION – CONSTANT SPEED MOTOR / GENERATOR HARNESS – MODIFICATION


DGCA/A-330/187 ATA 53, FUSELAGE – FRAME / STRINGER ATTACHMENTS – INSPECTION / REPAIR


DGCA/A-330/188 ATA 32, LANDING GEAR – MAIN LANDING GEAR BOGIE BEAM BORE – INSPECTION


DGCA/A-330/189 ATA 52, DOORS – FORWARD CARGO DOOR BEAM 3 AREA – INSPECTION


DGCA/A-330/190R1 ATA 34, NAVIGATION – TERRAIN AWARENESS WARNING SYSTEM – POWER CYCLE (RESET)


DGCA/A-330/191 AIRPLANE FLIGHT MANUAL – UNDUE ACTIVATION OF ALPHA PROTECTION –EMERGENCY PROCEDURE

EASA AD 2014-0267-E AS IN AD AS IN AD

DGCA/A-330/192R2 ATA 35, OXYGEN – CHEMICAL OXYGEN GENERATORS – REPLACEMENT

EASA AD 2015-0119 (CORRECTION 12TH JAN 2016)

AS IN AD AS IN AD

DGCA/A-330/193R3 ATA 24, ELECTRICAL POWER – ALTERNATING CURRENT EMERGENCY GENERATION – OPERATIONAL PROCEDURE

EASA AD 2017-0105R2 REVISED EASA AD 2017-0105R1 REVISED

AS IN AD AS IN AD



DGCA/A-330/194 ATA 29, HYDRAULIC POWER – RAM AIR TURBINE ACTUATOR – IDENTIFICATION / MODIFICATION


DGCA/A-330/195R1 ATA 52, DOORS – POTABLE WATER SERVICE PANEL ACCESS DOOR LATCHING MECHANISM – MODIFICATION

EASA AD 2015-0028R1 rev AS IN AD AS IN AD

DGCA/A-330/196 ATA 25 EQUIPMENT / FURNISHINGS – COCKPIT DOOR – MODIFICATION


DGCA/A-330/197 ATA-71,POWER PLANT – AFT AND FORWARD ENGINE MOUNT BOLTS – TORQUE CHECK / REPLACEMENT


DGCA/A-330/198R1 ATA 34, NAVIGATION – ANGLE OF ATTACK SENSORS – REPLACEMENT


DGCA/A-330/199 ATA – 53, FUSELAGE – SKIN AND STRUCTURE / ALLOWABLE DAMAGE LIMITS – RECORDS CHECK / REPAIR


DGCA/A-330/200R3 ATA – 27, FLIGHT CONTROLS – FLIGHT CONTROL PRIMARY COMPUTERS – MODIFICATION / REPLACEMENT


DGCA/A-330/201 ATA – 92, ELECTRIC / ELECTRONIC COMMON INSTALLATION – FEEDER CABLE ROUTING ATTACHMENT – MODIFICATION

EASA AD2015-0142 AS IN AD AS IN AD

DGCA/A-330/202/R1 ATA-25,EQUIPMENT / FURNISHINGS – PASSENGER / CREW AND EMERGENCY EXIT DOOR SLIDE AND SLIDE RAFT ATTACHMENTS – INSPECTION


DGCA/A-330/203 ATA-28-FUEL-FUEL PUMPS-INSPECTION/MODIFICATION EASA AD 2015-0194 AS IN AD AS IN AD

DGCA/A-330/204R1 ATA-52-DOORS-FORWARS AND AFT CARGO COMPARTMENT DOORS-INSPECTION

EASA AD 2016-0188 (CORRECTION: 22 SEPTEMBER 2016)

AS IN AD AS IN AD

DGCA/A-330/205 ATA-71-POWER PLANT-FORWARD ENGINE MOUNT BOLTS-TORQUE CHECK/REPLACEMENT


DGCA/A-330/206 ATA-25, DOORS-FORWARD AVIONICS DOOR CROSS- EASA AD 2015-0207 AS IN AD AS IN AD


MEMBERS-INSPECTION

DGCA/A-330/207 ATA-53, FUSELAGE-CABIN AND CARGO COMPARTMENTS PARTS-INSPECTION/REPLACEMENT


DGCA/A-330/208 ATA 53-FUSELAGE-CABIN AND CARGO COMPARTMENTS STRUCTURAL PARTS-INSPECTION


DGCA/A-330/209 ATA 05-FUEL-FUEL TANKS SAFETY-INSPECTION/MODIFICATION


DGCA/A-330/210R1 ATA 53- FUSELAGE-FUSELAGE BULK CARGO DOOR FRAMES-INSPECTION/REPAIR


AS IN AD AS IN AD

DGCA/A-330/211R1 ATA 29- HYDRAULIC POWER-HYDRAULIC RESERVOIR FLUID LEVEL-INSPECTION


AS IN AD AS IN AD

DGCA/A-330/212R1 ATA-25, EQUIPMENT/FURNISHINGS-EMERGENCY EXIT DOOR 3 TYPE 1 SLIDE -IDENTIFICATION/REPLACEMENT


DGCA/A-330/213R1 ATA-57, WINGS-INBOARD FLAP PARTS-IDENTIFICATION/INSPECTION


DGCA/A-330/214 ATA-53-FUSELAGE-STRUCTURAL PARTS/JOINTS-MODIFICATION/ REINFORCEMENT


DGCA/A-330/215R1 ATA-71-POWER PLANT-ENGINE HYDRAULIC DAMPER-REPLACEMENT (LIFE LIMIT)

EASA AD 2017-0041 (CORRECTION: 28 FEBRUARY 2017)

AS IN AD AS IN AD

DGCA/A-330/216 ATA-27, FLIGHT CONTROLS-TRIMMABLE HORIZONTAL STABILIZER ACTUATOR AND UPPER ATTACHMENT-INSPECTION


DGCA/A-330/217 ATA-57, WINGS-SLAT TRACK FRONT STOP ATTACHMENT-INSPECTION


DGCA/A-330/218 ATA 55 – STABILIZERS – HORIZONTAL STABILIZER / CENTER BOX TOP SKIN – INSPECTION / REPAIR



DGCA/A-330/219R2 ATA-34 –NAVIGATION –TRAFFIC COLLISION AVOIDANCE SYSTEM PROCESSOR –MODIFICATION (SOFTWARE UPDATE) / REPLACEMENT


DGCA/A-330/220 ATA-24 –ELECTRICAL POWER-ALTERNATING CURRENT EMERGENCY GENERATION-FLIGHT WARNING COMPUTER SOFTWARE


DGCA/A-330/221 ATA-32 – LANDING GEAR – PARTS WITH 300M MATERIAL PROPERTIES OUTSIDE OF SPECIFICATION REQUIREMENTS – IDENTIFICATION / REPLACEMENT [LIFE LIMIT]


DGCA/A-330/222 ATA-28 – FUEL – FUEL PUMP CAVITATION EROSION – INSPECTION.


DGCA/A-330/223 ATA-22 – AUTO FLIGHT – FLIGHT MANAGEMENT SYSTEM/ AIRCRAFT FLIGHT MANUAL –AMENDMENT/MODIFICATION.


DGCA/A-330/224 ATA-27 – FLIGHT CONTROLS – FLIGHT CONTROLS PRIMARY COMPUTER – MODIFICATION.


DGCA/A-330/225R1 ATA-27 – FLIGHT CONTROLS – LIMIT CONTROL PRIMARY COMPUTER – MODIFICATION / REPLACEMENT.

EASA AD 2017-0246R1 REVISED EASA AD 2017-0246

AS IN AD AS IN AD

DGCA/A-330/226 ATA 29 – HYDRAULIC POWER – RAM AIR TURBINE HYDRAULIC PUMPS – REPLACEMENT


DGCA/A-330/227 ATA 05 – TIME LIMITS / MAINTENANCE CHECKS – AIRWORTHINESS LIMITATIONS SECTION PART 2 – DAMAGE TOLERANT AIRWORTHINESS LIMITATION ITEMS – IMPLEMENTATION


subject reference compliance applicabilitydgca.nic.in/mandmod/aircraft/airbus 330.pdf · easa ad...

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