SERIAL NO

DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY

1 DGCA/A310/1 NOSE LANDING GEAR - STRUT ATTACHMENT PIN PT.NO. A322-10001-002-01

B.V.A.D.NO. 86-72-73(B) AND AIRBUS S.B.NOS. A300-32-374, A300-32-6011 & A300-32-2023

AS IN A.D. AND S.B. AS IN A.D. AND S.B.

2 DGCA/A310/2(R1) AGEING SYSTEMS MAINTENANCE (ASM). EASA AD 2007-0092 AS IN A.D. AS IN A.D.

3 DGCA/A310/3 SUNSTRAND RAM AIR - TO PREVENT DIFFICULTIES IN EJECTING RAM AIR TURBINES.

B.V.A.D.NO. 85-111-68(B) REV.1 AND F.A.A.A.D.NO. 87-20-06

AS IN A.D. AS IN A.D.

4 DGCA/A310/4 EMERGENCY EXIT DOORS - OPENING MECHANISM.

B.V.A.D.NO. 86-28-72(B) AS IN A.D. AS IN A.D.

5 DGCA/A310/5 FUSELAGE -- REAR/AFT PRESSURE BULKHEAD ATTACHMENT ANGLES -- MODIFICATION AND INSPECTION PROGRAM

EASA AD 2007 -- 0297R1 AS IN A.D. AND S.B. AS IN A.D. AND S.B.

6 DGCA/A310/6 TO PRECLUDE THE POTENTIAL FOR SEPARATION OF THE FIRE EXTINGUISHER DISCHARGE OUTLET AND MISDIRECTION OF THE FIRE EXTINGUISHING AGENT.

F.A.A.A.D.NO. 86-19-03 AND AIRBUS S.B.NOS. A310-26-2003 & A310-26-2004

AS IN A.D. AND S.B. AS IN A.D. AND S.B.

7 DGCA/A310/7 NOSE LANDING GEAR BARREL UPPER PART INSPECTION.

B.V.A.D.NO. 87-100-080(B) AND AIRBUS S.B.NO. A310-32-2036 (MBH S.B.NO. 470-32-604)

AS IN A.D. AND S.B. AS IN A.D. AND S.B.

8 DGCA/A310/8 INSPECTION OF FRAME 73A R.H. & L.H. BETWEEN BEAMS 5 AND 7 FOR CRACKS.

B.V.A.D.NO. 88-061-083(B) AND AI S.B.NO. A300-53-2043

AS IN A.D. AND S.B. AS IN A.D. AND S.B.

9 DGCA/A310/9 REPLACEMENT OF VICKERS HYDRAULIC PUMPS B.V.A.D.NO. 88-060-085(B) AS IN A.D. AS IN A.D.

10 DGCA/A310/10 INSPECTION OF FORK END FITTING OF EMERGENCY EXIT DOORS LOCKING MECHANISM.

B.V.A.D. NO. 88-073-084(B) AND A.I.S.B. NOS. A310-52-2024 & A310-52-2026

AS IN A.D. AND S.B. AS IN A.D. AND S.B.

11 DGCA/A310/11 INSPECTION OF LOWER AREA OF THE NOSE LANDING GEAR BARREL FOR CRACKS.

B.V.A.D. NO. 88-143--088(B) AND AIRBUS S.B.NOs. A310-32-2040 AND A310-32-2041.

AS IN A.D. AND S.B. AS IN A.D. AND S.B.

12 DGCA/A310/12 INSPECTION OF ENGINE FIRE EXTINGUISHER BOTTLES EARTHING.

B.V.A.D.NO. 88-181-089(B) R1 AS IN A.D. AS IN A.D.

13 DGCA/A310/13 MODIFICATION OF NOSE LANDING GEAR BARREL BETWEEN ATTACHMENT CLEVIS OF THE

B.V.A.D. NO. 88-185-090(B) REV. 2 AS IN A.D. AS IN A.D.

TELESCOPIC STRUT AND THE UPPER BEARING OF THE SHOCK ABSORBER.

14 DGCA/A310/14 INCORPORATION OF NEW COOLING FAN ASSEMBLY WITH THE IMPROVED FAN CONTAINMENT HOUSING.

F.A.A. A.D.NO. 85-14-02 REV.2 AS IN A.D. AS IN A.D.

15 DGCA/A310/15 INSPECTION OF PASSENGER/CREW DOORS - DAMPER AND EMERGENCY OPERATION CYLINDER FOR CORROSION.

B.V.A.D. NO. 89-092-095(B) AND A.I.S.B. NOs. A310-52-2018 & A310-52-2020.

AS IN A.D. AND S.B. AS IN A.D. AND S.B.

16 DGCA/A310/16 INSPECTION/ REPLACEMENT OF PITCH TRIM ELECTRICAL SWITCHES.

FAA AD 89-23-04 AS IN AD AS IN AD

17 DGCA/A310/17 LITTON- INERTIAL REFERENCE UNITS LTN90 AND LTN90-100

BVAD 89-170-IMP(AB) REV. 1 & AIRBUS A300 SB A310-34-2053

AS IN AD AND SB AS IN AD & SB

18 DGCA/A310/18 EMERGENCY LIGHTING SYSTEM. BVAD 89-107-096(B) R4 & AIRBUS SB A310-33-2015 REV 5

AS IN AD AND SB AS IN AD & SB

19 DGCA/A310/19 MAIN LANDING GEAR BOGIE BEAM INSPECTION. BVAD 90-005-101(B) R2 & BVAD 90-149-115(B)

AS IN AD AS IN AD

20 DGCA/A310/20 FIRE SHUTOFF VALVE. BVAD 90-042-107(B) & LUCAS SB B38LC 15-29-05

AS IN AD & SB AS IN AD & SB

21 DGCA/A310/21 FLAP TRANSMISSION ASSEMBLIES- UNIVERSAL JOINT ASSEMBLIES

BVAD 90-092-109(B) R3 & AIRBUS SB A310-27-2054 REV. 2

AS IN AD & SB AS IN AD & SB

22 DGCA/A310/22 EMERGENCY OXYGEN SYSTEM. BVAD 90-135-113(B) R1 AND AIRBUS SB A310-35-2002 R2.

AS IN AD AND SB AS IN AD AND SB

23 DGCA/A310/23 GENERATOR CONTROL UNIT. BVAD 90-197-118(B) AS IN AD AS IN AD

24 DGCA/A310/24 SLIDES AND SLIDE RAFTS PIN LANYARD. BVAD 90-215-119(B) AS IN AD AS IN AD

25 DGCA/A310/25 EMERGENCY EVACUATION- ESCAPE SLIDES POSITION OF GIRT BAR.

BVAD 90-218-120(B) AS IN AD AS IN AD

26 DGCA/A310/26 CANCELLED DGAC AD 91-103-123(B)R2

27 DGCA/A310/27 DOOR SURROUNDINGS - CORROSION FATIGUE INSPECTION.

DGAC AD 91-132-124(B) R1 AS IN AD AS IN AD

28 DGCA/A310/28 ADJUSTMENT OF PILOT'S AND COPILOT'S SEAT ENDSTOP SWITCHES.

BVAD 91-155-125(B) AS IN AD AS IN AD

29 DGCA/A310/29 REAR ATTACHMENT OF THE MAIN LANDING GEAR BARREL. VISUAL INSPECTION FOR CRACK

BVAD 91-234-127(B) R1 AS IN AD AS IN AD

AND CHECK FOR PLAY.

30 DGCA/A310/30 FLIGHT CONTROLS - SLAT/FLAP WING TIP BRAKE SOLENOIDS INSPECTION.

BVAD 92-010-129(B) AS IN AD AS IN AD

31 DGCA/A310/31R1 FUSELAGE / STABILISERS / WINGS ---- STRUCTURAL FATIGUE ---- INSPECTION / MODIFICATION

EASA AD 2007-0053R3 AS IN AD AS IN AD

32 DGCA/A310/32 FLIGHT MANUAL BVAD 92-156-133(B) AND FAA AD 92-25-12

AS IN AD AS IN AD

33 DGCA/A310/33 FIRE SHUT OFF VALVES OPERATIONAL TEST. BVAD 92-217-134(B) AND A.O.T 29/07 DT.28/08/92 AND FAA AD 93-09-02

AS IN ADs AND AOT. AS IN ADs AND AOT.

34 DGCA/A310/34 RAM AIR TURBINE-EXTENSION CONTROL CABLES. FAA AD 92-19-03 AND SB. A310-29-2030 R2

AS IN AD & SB. AS IN AD & SB.

35 DGCA/A310/35 GREEN HYDRAULIC DRAIN SYSTEM INSPECTION AND ENGINE ACCESSORY GEARBOX SEAL REPLACEMENT AT THE GREEN HYDRAULIC PUMP PAD.

BVAD 92-230-135(B) R1 AND SB A310-72-2020,2017 R3

AS IN AD & SB. AS IN AD & SB.

36 DGCA/A310/36R1 NACELLES/PYLONS --- PYLON LOWER SPAR BETWEEN RIBS 9 AND 10 --- INSPECTION.

EASA AD 2013-0014 AS IN AD & SBs. AS IN AD. & SBs.

37 DGCA/A310/37 INSPECTION OF 101VU RACK LOWER ATTACHMENTS.

BVAD 92-253-138(B) AND AOT 53-03 DT. NOV.1992 FAA AD 96-12-15 AND A310-53-2077.

AS IN AD & AOT& SBs.

AS IN AD & AOT & SBs.

38 DGCA/A310/38 NOSE LANDING GEAR - BOTTOM OF THE SHOCK ABSORBER.

BVAD 92-27-140(B) R1. AS IN AD. AS IN AD.

39 DGCA/A310/39 INSPECTION/REPLACEMENT SLAT TRANSMISSION SYSTEM- UNIVERSAL JOINT ASSEMBLIES.

BVAD 92-275-139(B)R1 AND A310-27-2061.

AS IN AD & SB. AS IN AD & SB.

40 DGCA/A310/40 MAIN LANDING GEAR- INSPECTION OF THE ATTACHMENT BETWEEN THE DRAG STRUT AND RETRACTION ACTUATOR.

BVAD 93-039-143(B) R1 AND MESSIER-BUGATTI 470-32-744 R1; 470-32-760.

AS IN AD & SB. AS IN AD & SB.

41 DGCA/A310/41 NOSE LANDING GEAR FREE FALL JAMMING. BVAD 93-063-145(B) AND AOT AIRBUS 32-06 DT. MARCH 03, 1993 AND FAA AD 93-15-06

AS IN ADs AND AOT. AS IN ADs AND AOT.

42 DGCA/A310/42 INSPECTION & MODIFICATION TO THE DGAC AD 2000-259-315(B) & FAA AD AS IN AD AND AOT. AS IN AD AND

DOWTY/SUNDSTRAND HAMILTON RAM AIR TURBINES

94-04-05. AOT.

43 DGCA/A310/43 AFT CARGO COMPARTMENT FORWARD CONTAINER LATCH.

TAD T97-129-226(B). AS IN AD & AOT. AS IN AD & AOT.

44 DGCA/A310/44 GENERATOR CONTROL UNIT- PROTECTIVE COVER.

FAA AD 93-22-06 AS IN AD. AS IN AD.

45 DGCA/A310/45 TO PREVENT STIFF OPERATION OF PITCH CONTROL AND LOSS OF RUDDER TRAVEL LIMITATION FUNCTION.

FAA AD 96-09-02 AND BVAD 93-202-153(B) AND AOT 27-14.

AS IN ADs AND AOT. AS IN ADs AND AOT.

46 DGCA/A310/46R1 NACELLES/ PYLONS - PYLON LOWER SPAR BETWEEN RIBS 6 AND 7 --- INSPECTION

EASA AD 2013 - 0167 AS IN AD AND SBs. AS IN AD AND SBs.

47 DGCA/A310/47 COCKPIT FIXED SIDE WINDOWS. BVAD 94-104-160(B) R2 AND FAA AD 94-10-51.

AS IN AD AND AOT AS IN AD AND AOT

48 DGCA/A310/48 SMOKE DETECTION IN LAVATORIES. BVAD 94-169-161(B) R1 AND BVAD 96-186-204(B)R1 AND FAAAD 94-10-51.

AS IN AD AND AOT. AS IN AD AND AOT.

49 DGCA/A310/49 CARBON FIBRE ELEVATOR. BVAD 94-184-157(B)R1. BVAD 95-206-189(B).

AS IN AD'S AND AOT. AS IN AD AND AOT.

50 DGCA/A310/50 CARGO COMPARTMENT FIRE PROTECTIVE PRESSURE VALVE OF FIRE EXTINGUISHING FLOW METERING SYSTEM.

BVAD 94-186-164(B) AND AIRBUS SB A310-22-2010; A310-22-6011.

AS IN AD AND SB'S. AS IN AD AND SB'S.

51 DGCA/A310/51 SOGERMA SOCEA - PILOT COCKPIT AND THIRD OCCUPANT SEATS BACK REST RECLINE LOCK ATTAACHMENT FITTINGS.

BVAD 94-188-162(B)R2 AND SOGERMA SOCEA SB 25-229 DATED 26 NOV 1993.

AS IN AD AND SB. AS IN AD AND SB.

52 DGCA/A310/52 AUTO PILOT OVERRIDING. BVAD 94-185-165(B)R2, FAAAD 96-08-07 AND BVAD97-373-237(B).

AS IN AD & SB. AS IN AD & SB.

53 DGCA/A310/53 CHAFING OF PANNEL 104 VU ELECTRICAL BUNDLE BY EXTENDING LADDER.

BVAD 94-187-163(B)R1 AS IN AD AND AOT. AS IN AD AND AOT.

54 DGCA/A310/54 STANDS CANCELLED.

55 DGCA/A310/55 CHECK OF FLC. BVAD 95-202-188(B). BVAD 94-046-156(B)R3.

AS IN AD AND SB. AS IN AD AND SB.

56 DGCA/A310/56 IMPROVEMENT OF FUEL SYSTEM ROUTE 2S DGAC AD 2002-578(B) AS IN AD. AS IN AD

57 DGCA/A310/57 COCKPIT SLIDING SIDE WINDOW (LH & RH). BVAD 94-285-173(B) & TELEGRAPHIC AS IN AD AND AOT. AS IN AD AND

AOT 95-01-11 & AOT 30-01 DT. DEC 22, 94.

AOT.

58 DGCA/A310/58 HARD OPENING OF EMERGENCY EXITS BVAD 94-270-172(B)R1 & BVAD 96-239-205(B).

AS IN AD. AS IN AD.

59 DGCA/A310/59 PASSENGER/CREW DOORS AND EMERGENCY EXITS-ESCAPE SLIDE GIRT BAR ATTACHMENTR FITTINGS

DGAC AD 2002-525(B) AS IN AD AND AOT. AS IN AD AND AOT.

60 DGCA/A310/60 FLAP TRANSMISSION SYSTEM BEARING. BVAD 95-073-178(B)R1. AS IN AD. AS IN AD.

61 DGCA/A310/61 SLAT TRANSMISSION SYSTEM BEARING. BVAD 95-074-179(B). AS IN AD. AS IN AD.

62 DGCA/A310/62 TO PREVENT UNWANTED DEPRESSURISATION/ LOSS OF WING DEICING.

FAA AD 95-10-14. AS IN AD . AS IN AD.

63 DGCA/A310/63 RAM AIR TURBINE (RAT) UPLOCK PIN - CORROSION INSPECTION.

BVAD 95-163-182(B) R3 AS IN AD. AS IN AD.

64 DGCA/A310/64 RIGGING OF AUTOPILOT ACTUATORS. BVAD 95-164-183(B) & AOT 27-20 DT. DEC19, 1994.

AS IN AD & AOT. AS IN AD AND AOT.

65 DGCA/A310/65 APU - BLEED AIR DUCTS. BVAD 95-182-184(B). AS IN AD. AS IN AD.

66 DGCA/A310/66 REPLACEMENT OF MAGNETIC SEALS BETWEEN THE ACCESSORIES & THE GEARBOX.

BVAD 95-183-185 AS IN AD. AS IN AD

67 DGCA/A310/67 REPLACEMENT OF DRAIN MODULE. BVAD 95-183-185. AS IN AD. AS IN AD.

68 DGCA/A310/68 THS ACTUATOR HYDRAULIC MOTORS. TAD 96-01-52R3 & BVAD 96-001-194(B) R3 AND AOT 27-21 REV2 DT.10 JUNE 1996.

AS IN AD AS IN AD AND AOT.

69 DGCA/A310/69 LAVATORIES - SMOKE DETECTION SYSTEM. BVAD 95-243-190(B) & AOT 26-16. AS IN AD AS IN AD AND AOT.

70 DGCA/A310/70 MODIFICATION TO THE RUDDER TRIM CONTROL SWITCHES AND KNOBS.

BVAD 95-246-193(B). AS IN AD. AS IN AD.

71 DGCA/A310/71 FUSELAGE - WING ROOT CHAFING PLATES --- INSPECTION/REPAIR/REWORK.

EASA AD 2007 - 0292 AS IN AD AS IN AD & SB.

72 DGCA/A310/72 CHAFING OF THE ELECTRICAL WIRE BUNDLE. BVAD 96-021-196(B) & SB A320-24-2065.

AS IN AD AS IN AD & SB.

73 DGCA/A310/73 TO PREVENT AN OUT-OF-TRIM CONDITION BETWEEN THE TRIMMABLE HORIZONTAL

FAA AD 95-25-09. AS IN AD. AS IN AD.

STABLIZER & THE ELEVATOR.

74 DGCA/A310/74 NOSE LANDING GEAR FREE FALL EXTENSION MECHANISM.

BVAD 96-052-197(B) & AOT 32-11 REV1.

AS IN AD AS IN AD & AOT.

75 DGCA/A310/75 ATTACHMENT BRACKETS OF UPPER WING TO FUSELAGE FAIRINGS.

DGAC AD 97-175-228(B) AS IN AD. AS IN AD

76 DGCA/A310/76 FRAMES OF AFT DOORS - STRESS CORROSION. BVAD 96-135-199(B). AS IN AD. AS IN AD.

77 DGCA/A310/77 RUDDER SERVO CONTROL DE-SYNCHRONISATION.

BVAD 96-242-208(B)R2.R3, F 2004-092 R4

AS IN AD. AS IN AD.

78 DGCA/A310/78 PREVENT PRESENCE OF WATER IN THE ELEVATOR

FAA AD 96-22-15 AS IN AD. AS IN AD.

79 DGCA/A310/79 RUDDER TRIM SYSTEM CONTROL SWITCH AND CONTROL KNOB INSTALLATION.

BVAD 96-240-206(B)R1 & AOT 27-22R1

AS IN AD AS IN AD.

80 DGCA/A310/80 WINGS --- CENTRE WING BOTTOM SKIN AT RIB 1 --- INSPECTION.

EASA AD 2008 - 0208 R1 AS IN AD. AS IN AD.

81 DGCA/A310/81 TO DETECT & PREVENT DISBONDING, WHICH IF NOT CORRECTED COULD REDUCE THE STRUCTURAL INTEGRITY OF THE RUDDER.

FAA AD 97-04-07 AS IN AD. AS IN AD.

82 DGCA/A310/82 PAX.DOORS STRICKER MECHANISM OF PAX DOOR EMERGENCY ACTUATORS.

DGAC AD 1999-410-294(B) AS IN AD. AS IN AD.

83 DGCA/A310/83 MAIN FUEL SYSTEM MODIFICATION TO NON-RETURN VALVESINSTALLED IN INNER AND OUTER WING TANKS.

BVAD 97-082-215(B). AS IN AD. AS IN AD.

84 DGCA/A310/84 HYDRAULIC MOTORS OF HORIZONTAL STABLIZER ACTUATOR (HAS)

CdeN AD 97-081-217(B) AS IN AD. AS IN AD.

85 DGCA/A310/85(R1)

FUSELAGE - INSPECTION OF REAR PRESSURE BULKHEAD.

DGAC AD F 2004-193 ORG AD 97-061-212 IS REPLACED

AS IN AD. AS IN AD.

86 DGCA/A310/86 TO DETECT & CORRECT ANY WIRING INVERSIONS AT THE THREE AIR DATA STATIC LINES SUPPLYING STATIC LINES SUPPLYING STATIC PRESSURE DATA.

BVAD 97-098-216(B) AS IN AD. AS IN AD.

87 DGCA/A310/87 FUSELAGE --- PASSENGER DOOR STOP FITTINGS ---- INSPECTION

EASA AD 2007 -- 0154 AS IN AD. AS IN AD.

88 DGCA/A310/88 RUDDER TRIM CONTROL SWITCH BVAD 97-111-219(B) AS IN AD. AS IN AD.

89 DGCA/A310/89 LANDING GEAR FREE FALL EXTENSION. DGAC AD 1997-113-221(B)R3 AS IN AD AS IN AD.

90 DGCA/A310/90 NI (EPR) LIMIT SETTING ON TRP (THRUST RATING PANEL).

BAVD 97-110-218(B) AS IN AD. AS IN AD.

91 DGCA/A310/91 FUSELAGE - ARTICULATED SEAT & DUMMY TRACKS.

DGAC AD 1999-511-297(B)R2 AS IN AD. AS IN AD.

92 DGCA/A310/92 101VU PANEL WIRE BUNDLE WEAR DUE TO CHAFING.

BVAD 97-152-225(B). AS IN AD. AS IN AD.

93 DGCA/A310/93 WINGS -- WING-PYLON THRUST & SIDE LOAD FITTING (SPIGOT) --- INSPECTION/REPLACEMENT

EASA AD 2007 - 0243 AS IN AD. AS IN AD.

94 DGCA/A310/94 FIRE SHUT OFF VALVES. BVAD 97-384-241(B)R2 BVAD 98-356-259(B).

AS IN AD. AS IN AD.

95 DGCA/A310/95 FRAMES OF AFT DOORS STRESS CORROSION. BVAD 97-135-199(B) R1 AS IN AD. AS IN AD.

96 DGCA/A310/96 FIRE SHUT OFF VALVES BVAD 97-884-241(B)R1 AS IN AD. AS IN AD.

97 DGCA/A310/97 ENGINE CONTROLS REPLACEMENT OF BEARING ON BOTH THROTTLE CONTROL LEVERS.

BVAD 96-270-209R1 AS IN AD. AS IN AD.

98 DGCA/A310/98 SLIDE AND SLIDE RAFTS MODIFICATION OF THE REGULATOR VALVE.

BVAD 98-122-244(B)R1 AS IN AD. AS IN AD.

99 DGCA/A310/99 FUEL TANKS BONDING LEADS. DGAC AD 1998-174-248(B)R1 AS IN AD. AS IN AD.

100 DGCA/A310/100 FLIGHT CONTROLRUDDER (ATA 27) BVAD 98-175-249(B) AS IN AD. AS IN AD.

101 DGCA/A310/101 RH & LH AFT ENGINE MOUNT LINKS ON CF 6-80A3 ENGINES

DGAC AD 2000-267-318(B) AS IN AD AS IN AD.

102 DGCA/A310/102 ALTERNATE BRAKING SYSTEM CHECK. DGAC AD 98-263-255(B)R3 AS IN AD. AS IN AD.

103 DGCA/A310/103 THS ACTUATOR HYDRAULIC MOTORS (ATA 27) BVAD 98-271-253(B) AS IN AD. AS IN AD

104 DGCA/A310/104 THRUST REVERSER CONTROL SYSTEM (ATA 78) DGAC AD 2000-352-319(B) AS IN AD. AS IN AD.

105 DGCA/A310/105 TRIM TANK MODIFICATION TO THE WATER SCAVENGE PUMPS (ATA 28)

BVAD 98-354-256(B). AS IN AD. AS IN AD.

106 DGCA/A310/106 EMERGENCY EXITS-REPLACEMENT OF THE BEARINGS OF THE EMERGENCY EXIT OPENING MECHANISM (ATA 52)

BVAD 98-340-254(B)R1 AS IN AD. AS IN AD.

107 DGCA/A310/107 APU FUEL FEEDLINE (ATA49) BVAD 98-480-269(B) AS IN AD AS IN AD

108 DGCA/A310/108 RH & LH AFT ENGINE MOUNT LINKS ON CF 6-80C2 ENGINES

DGAC AD's 98-504- 274(B) & 2000-165-307(B) R1

AS IN AD AS IN AD

109 DGCA/A310/109 P&W ENGINE MODIFICATION TO IGNITION SYSTEM POWER SUPPLY(ATA74)

BVAD 98-479-266(B) AS IN AD AS IN AD

110 DGCA/A310/110 SPOILER N3 ACTUATOR ATTACHMENT FITTING (ATA57)

DGAC AD 1998-483-271(B)R1 AS IN AD AS IN AD

111 DGCA/A310/111 MODIFICATION TO THE RAM AIR TURBINE UPLOCK UNIT (ATA 29)

DGAC AD 1999-006-263(B) AS IN AD AS IN AD

112 DGCA/A310/112 HIGH FREQUENCY EDDY CURRENT INSPECTION (HFEC)OF THE INNER FLANGE OF FRAME FR73A BETWEEN BEAMS 5&7

DGAC AD 1999-013-276 (B) AS IN AD AS IN AD

113 DGCA/A310/113 101VU PANEL- INSPECTION OF CONTACTORS 12XC & 15XE

DGAC AD's 1999-077-278 (B) R1 & 2000-145-306(B)

AS IN AD AS IN AD

114 DGCA/A310/114 THRUST REVERSER DIRECTIONAL PILOT VALVE DGAC AD 1999-242-289 R1 AS IN AD AS IN AD

115 DGCA/A310/115 CENTER TANK METALLIC VAPOR SEAL DGAC AD's 1999-180-282 (B) & 2000-336-311(B)

ASIN AD AS INAD

116 DGCA/A310/116 FIRE PROTECTION-ENGINE AND AUXILIARY POWER UNIT (APU) FIRE DETCTION SYSTEM-(ATA 26)

DGAC AD 1999-238-286 (B)R2 AS IN AD AS IN AD

117 DGCA/A310/117 FLIGHT CONTROLS-RUDDER SERVO CONTROL INPUT SPRING RODS

DGAC AD 1999-240-288 (B) R1 AS IN AD AS IN AD

118 DGCA/A310/118 ERRATIC RUDDER MOVEMENT DURING APPROACH

DGAC AD 1999-268-292 (B) AS IN AD AS IN AD

119 DGCA/A310/119 ELECTRICAL POWER - TRUs DGAC AD 1999-435-296 (B) & DGAC AD 2003-082 R1

AS IN AD AS IN AD

120 DGCA/A310/120(R1)

LOSS OF AUTOTRIM FUNCTION DGAC AD 2000-007-301 (B) & 2000-115-304 R5

AS IN AD AS IN AD

121 DGCA/A310/121 SLIDES AT TYPE A DOORS DGAC AD 2000-059-302(B) AS IN AD AS IN AD

122 DGCA/A310/122 FLIGHT CONTROLS- FLAP CONTROL SCREW JACK NO.1

DGAC AD 1999-510-299(B) AS IN AD AS IN AD

123 DGCA/A310/123 FUSELAGE - CENTRE SECTION PICK-UP ANGLE AT FRAME 40 - INSPECTION

EASA AD 2007 -- 0184 AS IN AD AS IN AD

124 DGCA/A310/124 FLIGHT CONTROL COMPUTERS (FCC) - INTRODUCTION OF A NEW STANDARD

DGAC AD 2000-137-305(B) AS IN AD AS IN AD

125 DGCA/A310/125 FUSELAGE NOSE SECTION - INSPECTION OF DGAC AD 2000-263-314(B) AS IN AD AS IN AD

UPPER FRAME SECTION OF LATERAL WINDOWS

126 DGCA/A310/126 FUSELAGE- BULK CARGO COMPARTMENT DOOR FRAMES

DGAC AD 2000-262-313(B) AS IN AD AS IN AD

127 DGCA/A310/127 HYDRAULIC POWER - RAM AIR TURBINE (RAT) EJECTION JACK REPLACEMENT

DGAC AD 2000-284-317(B) AS IN AD AS IN AD

128 DGCA/A310/128 WING TO FUSELAGE UPPER FAIRINGS DGAC AD 98-450-261(B) AS IN AD AS IN AD

129 DGCA/A310/129 INERTIAL REFERENCE SYSTEM - UNIT ALIGNMENT DGAC AD 2000-480-325(B) AS IN AD AS IN AD

130 DGCA/A310/130 FUEL TANKS - ELECTRICAL CONNECTIONS TO FUEL LEVEL SENSORS

DGAC AD 2000-481-324(B)R1 AS IN AD AS IN AD

131 DGCA/A310/131 FLIGHT CREW SEATS DGAC AD 2000-524(B) AS IN AD AS IN AD

132 DGCA/A310/132 THROTTLE CONTROL - INSPECTION & MODIFICATIONS

DGAC AD 2001-072(B) R2 AS IN AD AS IN AD

133 DGCA/A310/133(R1)

FUSELAGE - INSPECTION OF SKIN LAP JOINTS AT THE PASSENGER DOORS & BETWEEN FRAMES 56 AND 58 STRINGER 52.

DGAC AD 2002-639(R1) AS IN AD AS IN AD

134 DGCA/A310/134 AIRSPEED INDICATION - AIRSPEED FLUCTUATIONS IN ICING CONDITIONS

DGAC AD 2001-129(B) AS IN AD AS IN AD

135 DGCA/A310/135R1 NACELLES/ PYLON - PYLON LOWER SPAR BETWEEN RIBS 9 & 10 --- INSPECTION

EASA AD 2013 - 0014 AS IN AD AS IN AD

136 DGCA/A310/136 SLAT & FLAP POWER CONTROL UNITS- LIFE LIMITS OF THE PRESSURE OFF BRAKES (POBs) ATA 27

DGAC AD 2001-185(B) AS IN AD AS IN AD

137 DGCA/A310/137 THRUST REVERSER - "ENG REV UNLK" PROCEDURE ATA 78

DGAC AD 2001-186(B) AS IN AD AS IN AD

138 DGCA/A310/138 AUXILIARY HYDRAULIC POWER - OVERHAUL & MODIFICATION TO THE RAM AIR TURBINE

DGAC AD 2001-212(B) AS IN AD AS IN AD

139 DGCA/A310/139 APU-STARTER FEEDER LINE TERMINAL BLOCKS (ATA 24)

DGAC AD 2001-266(B) AS IN AD AS IN AD

140 DGCA/A310/140 NAVIGATION-PITOT PROBES (ATA 34) DGAC AD 2001-265(B)R2 & 2003-148(B)

AS IN AD AS IN AD

141 DGCA/A310/141 A310 AND A300-600 AIRCRAFT EQUPPED WITH PW 4000 ENGINES-PERFORMANCE DATA (ATA 72)

DGAC AD 2001-086(B)R2 AS IN AD AS IN AD

142 DGCA/A310/142(R1)

AGEING SYSTEMS MAINTENANCE (ASM) EASA AD 2007-0092 AS IN AD AS IN AD

143 DGCA/A310/143 NAVIGATION-INERTIAL REFERENCE UNITS (ATA 34)

DGAC AD 2001-303(B) AS IN AD AS IN AD

144 DGCA/A310/144 PRATT 7& WHITNEY FORWARD ENGINE MOUNT (ATA 10,71)

DGAC AD 2001-264(B) AS IN AD AS IN AD

145 DGCA/A310/145 CANCELLED IN VIEW OF DGCA/A 310/161 (R2) VIDE LETTER NO 9-411/05 AI(2) DATED 13-07-05

146 DGCA/A310/146 EFIS SYURBOOL GENERATOR UNIT (SGU) INTRODUCTION OF A NEW STANDARD

DGAC AD 2001-467(B) AS IN AD AS IN AD

147 DGCA/A310/147 VERTICAL STABILIZER AND RUDDER ATTACHMENT FITTINGS

DGAC AD 2001-560(B) AS IN AD AS IN AD

148 DGCA/A310/148 WING TO ENGINE PYLON INTERFACE DGAC AD 2001-555(B) AS IN AD AS IN AD

149 DGCA/A310/149 INSTALLATION OF CRADLES ON VERTICAL PARTIPIONS

DGAC AD 98-176 (AB)R1 AS IN AD AS IN AD

150 DGCA/A310/150 THRUST REVERESER DGAC AD 199-181-283(B)R1 & 2001-523 (B)

AS IN AD AS IN AD

151 DGCA/A310/151 PPG AEROSPACE WINDSHIELDS DGAC AD 2001-606(B) AS IN AD AS IN AD

152 DGCA/A310/152 LANDING GEAR NORMAL EXTENSION MODE- INSPECTION OF LANDING GEAR SELECTOR VALVES

DGAC AD 2001-603(B) AS IN AD AS IN AD

153 DGCA/A310/153 TO DETECT AND CORRECT REDUCED STRUCTURAL INTEGRITY OF THE AIRPLANE

FAA AD 2002-06-09 AS IN AD AS IN AD

154 DGCA/A310/154 INSPECTION OF THE SPACING BETWEEN FQI PROBES AND THE STRUCTURE

DGAC AD 2002-170(B) AS IN AD AS IN AD

155 DGCA/A310/155 PW 4000 ENGINE OIL CIRCUIT FLEXIBLE HOSE DGAC AD 2002-173(B) AS IN AD AS IN AD

156 DGCA/A310/156R2 FUEL --- ELECTRIC/ELECTRONIC COMMON INSTALLATION FUEL SYSTEM ROUTE 2S --- MODIFICATION

EASA AD 2012 - 0188 AS IN AD AS IN AD

157 DGCA/A310/157 INSPECTION OF FLIGHT CONTROL CABLES DGAC AD 2002-608(B)R1 AS IN AD AS IN AD

158 DGCA/A310/158 R.A.T. EJECTION JACK DGAC AD 2002-638(B)R1 AS IN AD AS IN AD

159 DGCA/A310/159 CABIN PRESSURIZATION CONTROL SYSTEM DGAC AD 2002-626(B)R1 AS IN AD AS IN AD

160 DGCA/A310/160 ENGINE VIBRATION INDICATION DGAC AD 2003-019(B) R1 AS IN AD AS IN AD

161 DGCA/A310/161(R2)

AUTO PILOT-NEW FLIGHT AUMENTATION COMPUTER (FAC) STANDARD

DGAC AD F2005-111 R1( AD 2003-165(B), 2003-243(R1), & 2003-110 ARE CANCELLED)

AS IN AD AS IN AD

162 DGCA/A310/162 WINGS -- HAMILTON SUNDSTRAND RAM AIR TURBINE (RAT) SWIVEL COUPLING YOKE FITTING- REPLACEMENT

EASA AD 2007 - 0273 AS IN AD AS IN AD

163 DGCA/A310/163 IMPROVVEMENT IN THE ELECTRICAL BONDING OF THE ADDITIONAL CENTER TANKS

DGAC AD 2003-161(B) AS IN AD AS IN AD

164 DGCA/A310/164 AFM - FUEL LEAK PROCEDURE ( ATA 28 ) DGAC AD 2003-319(B)R1 AS IN AD AS IN AD

165 DGCA/A310/165 CORROSION PREVENTION AT PRESSURE BULKHEADS / FRAMES 39 AND 54 ( ATA 21,53)

DGAC AD 2003-317(B) AS IN AD AS IN AD

166 DGCA/A310/166 RAT (RAM AIR TURBINE )EJECTION JACK GIMBALS ASSEMBLY (ATA 29,57 )

DGAC AD 2002-263(B) AS IN AD AS IN AD

167 DGCA/A310/167 (R1)

PASSENGER /CREW DOORS - ESCAPE SLIDE GIRT BAR ( ATA25 )

DGAC AD 2003-435(B) AS IN AD AS IN AD

168 DGCA/A310/168 YELLOW HYDERAULIC SYSTEM PARKING BRAKE OPERATED VALUE

DGAC AD 2001-510(B)R1 AS IN AD AS IN AD

169 DGCA/A310/169 (R1)

FUEL SYSTEM - PREVENTION AGAINST EXPLOSION RISKS - FQIS WIRING - MODIFICATION

EASA AD 2006-0291 (EASA AD REPLACES DGAC AD 2004-005)

AS IN AD AS IN AD

170 DGCA/A310/170 FUSELAGE - AFT PRESSURE BULKHEAD DGAC AD2004-004(B) AS IN AD AS IN AD

171 DGCA/A310/171(R2)

SAFETY SIGN - PASSENGER , EMERGENCY AND CARGO DOOR

DGAC AD 2004-003(R2) AS IN AD AS IN AD

172 DGCA/A310/172 NAVIGATION-THALES AVIONICS EQUIPMENT DGAC AD 2004-037 AS IN AD AS IN AD

173 DGCA/A310/173 ELECTRICAL POWER -- ENGINE FEEDER HARNESS --- INSPECTION & NACELLES/PYLONS -GE CF6 - 80C2 PYLON FORWARD PYRAMID -- INSPECTION

EASA AD 2009 - 0055R1 AS IN AD AS IN AD

174 DGCA/A310/174 LANDING GEAR ---NOSE LANDING GEAR SHOCK ABSORBER/ BARREL ATACHMENT BOLTS --- INSPECTION / RE-TORQUE / REPLACEMENT

EASA AD 2008 - 0052R1 AS IN AD AS IN AD

175 DGCA/A310/175 NAVIGATION- INERTIAL REFERENCE UNITS DGAC AD F 2004-093 AS IN AD AS IN AD

176 DGCA/A310/176(R1)

INSTRUMENTS / LIGHTING - STANDBY HORIZON INTEGRAL LIGHTING LOGIC - MODIFICATION / OPERATIONAL TEST

EASA AD 2006-0370 AS IN AD AS IN AD

177 DGCA/A310/177 CANCELLED VIDE LETTER NO 9-411/03 DATED 11-05-05

DGAC AD F 2004-102 (R1) AS IN AD AS IN AD

178 DGCA/A310/178 FUSELAGE -CABIN DOOR SURROUNDINGS - IMPROVING FATIGUE STRENGTH.

DGAC AD F 2004-103 AS IN AD AS IN AD

179 DGCA/A310/179 PW 4000 SERIES ENGINES- HPC DAMAGE AND SURGE

DGAC AD F 1990-141-114 R4 AS IN AD AS IN AD

180 DGCA/A310/180(R1)

THRUST REVERSER- IMPLEMENTATION OF A THIRD LINE OF DEFENSE

DGAC AD F 2001-523 R1& 2004-165 AS IN AD AS IN AD

181 DGCA/A310/181 FUEL SYSTEM- PREVENTION AGAINST EXPLOSION RISKS- INSPECTION OF CLEARANCE BETWEEN THE COMPENSATOR ON PROBE NO 1 AND THE GUIDE ASSEMBLY

DGAC AD F 2004-125 AS IN AD AS IN AD

182 DGCA/A310/182(R1)

FUEL SYSTEM- PREVENTION AGAINST EXPLOSION RISKS- APU BLEED AIR LEAK DETECTION LOOP

DGAC AD 2004-130(R1) AS IN AD AS IN AD

183 DGCA/A310/183(R1)

STABLIZERS - CARBON FIBRE ELEVATORS WITH GFRP / TEDLAR FILM AS EXTERNAL PROTECTION - INSPECTION

EASA AD 2006 0289 (EASA AD SUPERSEEDES DGAC AD F 2004-131)

AS IN AD AS IN AD

184 DGCA/A310/184 FUEL SYSTEM- AUXILIARY CENTRAL TANK (ACT) -MODIFICATION / RE - IDENTIFICATION (PREVENTION AGAINST FUEL TANK EXPLOSION RISKS)

EASA AD 2008 - 0207 AS IN AD AS IN AD

185 DGCA/A310/185 PRESSURISATION- AIR CONDITIONING- NEW CABIN ALTITUDE INDICATOR

DGAC AD F 2005-027 AS IN AD AS IN AD

186 DGCA/A310/186 EQUIPMENT/ FURNISHINGS- SOGERMA PILOT AND CO-PILOT SEATS

DGAC AD F 2005-038 AS IN AD AS IN AD

187 DGCA/A310/187 EQUIPMENT/ FURNISHINGS- NON TEXTILE FLOOR (NTF) REPLACEMENT

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

188 DGCA/A310/188 STABILIZERS- REINFORCED CARBON FIBER (CFRP) RUDDER

DGAC AD F 2005-048 AS IN AD AS IN AD

189 DGCA/A310/189(R1)

PROTECTION GRATING FOR OUTFLOW VALVE DGAC AD F 2005-061(R1) AS IN AD AS IN AD

190 DGCA/A310/190 FUSELAGE- UPPER FRAME BASES - TO - ARCHES JUNCTIONS FROM FR 43 TO FR 46 -- MODIFICATION

EASA AD 2008 - 0212 AS IN AD AS IN AD

191 DGCA/A310/191(R1)

INSPECTION OF FRAME 12A FLOOR/ FUSELAGE BEAM STIFFENER FITTINGS

DGAC AD F 2005-084(R1) AS IN AD AS IN AD

192 DGCA/A310/192(R2)

FUEL SYSTEM- PREVENTION OF RISKS OF EXPLOSION- WIRING OF ADJACENT SYSTEM AND FUEL PUMP

EASA AD 2006-0074 (DGAC AD F 2005-112(R1) IS CANCELLED)

AS IN AD AS IN AD

193 DGCA/A310/193 FLIGHT CONTROLS- LIMITATION- HIGH ALTITUDE PITCH OSCILLATIONS

DGAC AD F 2005-114 AS IN AD AS IN AD

194 DGCA/A310/194R1 TIME LIMITS & MAINTENANCE CHECKS --- CERTIFICATION MAINTENANCE REQUIREMENTS ---- ALS PART 3 --- AMENDMENT

EASA AD 2013-0072 AS IN AD AS IN AD

195 DGCA/A310/195 FUEL TANK OF TRIMMABLE HORIZONTAL STABILIZER (THS)- REPLACEMENT OF VENT FLOAT VALVE

DGAC AD F 2005-148 AS IN AD AS IN AD

196 DGCA/A310/196(R2)

TIME LIMITS & MAINTENANCE CHECKS --- AGEING SYSTEMS MAINTENANCE CHECKS --- AGEING SYSTEMS MAINTENANCE --- ALS PART 4 --- AMENDMENT

EASA AD 2013-0075 AS IN AD AS IN AD

197 DGCA/A310/197 TRANSFER CONTROL SYSTEM- CENTRE TANK- MODIFICATION TO THE NON-RETURN VALVE

DGAC AD F 2005-197 AS IN AD AS IN AD

198 DGCA/A310/198 CENTER TANK- DAMAGE TO FUEL PUMP CANISTER AND BODY

DGAC AD F 2005-199 AS IN AD AS IN AD

199 DGCA/A310/199 FUEL SYSTEM - PREVENTION AGAINST EXPLOSION RISKS - FUEL TANK ELECTRICAL BONDING - INSPECTION / MODIFICATION

EASA AD 2006-0325 R1 AS IN AD AS IN AD

200 DGCA/A310/200 STABILIZERS- VERTICAL STABILIZER & RUDDER STRUCTURE- INSPECTION/REPAIR

EASA AD 2007-0266 AS IN AD AS IN AD

201 DGCA/A310/201 FUEL - PREVENTION OF RISKS OF EXPLOSION- INSPECTION OF ELECTRICAL LINES IN THE WING LEADING AND TRAILING EDGES

EASA AD 2006-0076 AS IN AD AS IN AD

202 DGCA/A310/202 LIGHTS- BRUCE FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM (FPEEPMS)

EASA AD 2006-0077 AS IN AD AS IN AD

203 DGCA/A310/203 FLIGHT CONTROLS- FLAPS- INSPECTION OF TRANSMISSION SHAFT

EASA AD 2006-0111 AS IN AD AS IN AD

204 DGCA/A310/204 HYDRAULIC POWER- RAT(RAM AIR TURBINE) - LIMITATION OF AIRCRAFT SPEED WITH RAT DEPLOYED

EASA AD 2006-0122 AS IN AD AS IN AD

205 DGCA/A310/205 EXHAUST- THRUST REVERSER- UPPER AND LOWER TRACK BEAM LUGS INSPECTION

EASA AD 2006-0161 AS IN AD AS IN AD

206 DGCA/A310/206 FUEL TANK SAFETY- ALS PART 5- FUEL AIRWORTHINESS LIMITATIONS (FAL)

EASA AD 2007-0096R1 (REVISION TWO)

AS IN AD AS IN AD

207 DGCA/A310/207 LANDING GEAR- PARKING EMERGENCY BRAKING EASA AD 2006-0178 AS IN AD AS IN AD

208 DGCA/A310/208R1 TIME LIMITS AND MAINTENANCE CHECKS --- DAMAGE TOLERANT AIRWORTHINESS LIMITATION ITEMS --- ALS PART 2 --- AMENDMENT

EASA AD 2011 - 0198 AS IN AD AS IN AD

209 DGCA/A310/209(R1)

ELECTRICAL POWER - PREVENTION AGAINST EXPLOSION RISK - FUEL PUMP WIRING - MODIFICATION

EASA AD 2006-0284R1 AS IN AD AS IN AD

210 DGCA/A310/210(R1)

AGEING TRANSPORT SYSTEMS RULEMAKING ADVISORY COMMITTEE (ATSRAC) AGED AIRCRAFT DESIGN IMPROVEMENTS AND INSPECTION AGAINST POTENTIAL UNSAFE CONDITIONS

EASA AD 2006-0285 R1 AS IN AD AS IN AD

211 DGCA/A310/211R1 WINGS / MAIN LANDING GEAR RIB 5 AFT BEARING FORWARD LUG BUSHES - INSPECTION/REPLACEMENT

EASA AD 2012 - 0176 CORRECTED 20TH SEPTEMBER 2012

AS IN AD AS IN AD

212 DGCA/A310/212 FUSELAGE - NOSE LANDING GEAR WELL STRUCTURE BETWEEN FRAME 11 AND 17 - REWORK

EASA AD 2006-0367 AS IN AD AS IN AD

213 DGCA/A310/213 STABILIZERS-TRIMMABLE HORIZONTAL STABILIZER(THS)METALLIC HOISTING LUG FITTINGS

EASA AD 2007-0024 AS IN AD AS IN AD

214 DGCA/A310/214 AIRCONDITIONING --- AIRPLANE FLIGHT MANUAL ---- EMEGENCY PROCEDURE

EASA AD 2007-0093R1 AS IN AD AS IN AD

215 DGCA/A310/215 TIME LIMITS/MAINTENANCE CHECKS - SAFE LIFE AIRWORTHINESS LIMITATION ITEMS - (ALS PART 1) IMPLEMENTATION

EASA AD 2007- 0293 AS IN AD AS IN AD

216 DGCA/A310/216 FUSELAGE - FRAME 55/58 BUTT JOINT - REINFORCEMENT

EASA AD 2007-0111 AS IN AD AS IN AD

217 DGCA/A310/217 LANDING GEAR --- PARKING BRAKE PRESSURE LIMITER -- REPLACEMENT

EASA AD 2007-0151 AS IN AD AS IN AD

218 DGCA/A310/218 FUSELAGE - FASTENERS AT AFT FUSELAGE FRAME 91 (FR 91) -- REPLACEMENT

EASA AD 2007-0173 AS IN AD AS IN AD

219 DGCA/A310/219 WINGS -- OUTER WINGS STRUCTURAL FATIGUE --- INSPECTION/MODIFICATION

EASA AD 2007-0242 AS IN AD AS IN AD

220 DGCA/A310/220 NACELLES/PYLONS --- PYLON BOX RIB 5 LOWER SIDE --- INSPECTION

EASA AD 2008-0066 AS IN AD AS IN AD

221 DGCA/A310/221 FIRE PROTECTION / HYDRAULIC POWER -- AIR PRESSURISATION CHECK VALVES --- IDENTIFICATION / REPLACEMENT

EASA AD 2008-0166 - CN AS IN AD AS IN AD

222 DGCA/A310/222R2 NACELLES/PYLONS --- PYLON SIDE PANELS AT RIB 8 --- INSPECTION

EASA AD 2013-0136R1 AS IN AD AS IN AD

223 DGCA/A310/223 WINGS --- CENTRE WING REAR SPAR INTERNAL ANGLE & TEE FITTING --- INSPECTION /MODIFICATION

EASA AD 2008-0187 AS IN AD AS IN AD

224 DGCA/A310/224 WINGS --- WING TOP SKIN PANELS 1 & 2 RIB 2 --- INSPECTION / REPAIR

EASA AD 2008 - 0211 AS IN AD AS IN AD

225 DGCA/A310/225R1 ENGINE EXHAUST --- CENTRE LATCH OF THRUST REVERSER DOOR OPENING MECHANISM --- REPLACEMENT / INSPECTION

EASA AD 2008 - 0226R1 AS IN AD AS IN AD

226 DGCA/A310/226 EQUIPMENTS / FURNISHINGS --- IPECO PILOT & CO PILOT SEATS --- INSPECTION/MODIFICATION/REPLACEMENT

EASA AD 2009 - 0045 AS IN AD AS IN AD

227 DGCA/A310/227 FUSELAGE --- AFT FUSELAGE LOWER TAIL PLANE CUT OUT --- INSPECTION

EASA AD 2009 - 0058 AS IN AD AS IN AD

228 DGCA/A310/228 WINGS --- CENTRE WING TRELLIS BOOM DRAINAGE HOLES & FRAME 40 UPPER CORNER FITTING --- INSPECTION/REPAIR

EASA AD 2009 - 0057 AS IN AD AS IN AD

229 DGCA/A310/229R1 EQUIPMENT / FURNISHINGS --- PILOT & CO-PILOT SEATS --- DEACTIVATION OF POWERED MOVEMENT - MODIFICATION

EASA AD 2010 - 0070 AS IN AD AS IN AD

230 DGCA/A310/230 FUSELAGE --- FRAME (FR) 15A NOSE LANDING GEAR (NLG) CROSSBEAM --- INSPECTION/REPAIR

EASA AD 2009 - 0165 AS IN AD AS IN AD

231 DGCA/A310/231 FIRE PROTECTION / HYDRAULIC POWER --- AIR PRESSURISATION CHECK VALVES --- IDENTIFICATION/REPLACEMENT

EASA AD 2009 - 0171 AS IN AD AS IN AD

232 DGCA/A310/232 WINGS --- WING TIP FENCES --- INSPECTION/REPAIR/REPLACEMENT

EASA AD 2009 - 0186 AS IN AD AS IN AD

233 DGCA/A310/233 SSAD AS IN AD AS IN AD

234 DGCA/A310/234 HYDRAULIC POWER --- RAM AIR TURBINE (RAT) BALANCE WEIGHT SCREWS --- INSPECTION / REPLACEMENT

EASA AD 2009 - 0258 AS IN AD AS IN AD

235 DGCA/A310/235 STABILIZERS --- RUDDER SIDE SHELL SKIN --- INSPECTION

EASA AD 2010 - 0002 AS IN AD AS IN AD

236 DGCA/A310/236R1 NACELLES/PYLONS --- FUEL DRAIN PIPE AND ATTACHMENT SCREWS --- INSPECTION / REPLACEMENT

EASA AD 2010 - 0085 AS IN AD AS IN AD

237 DGCA/A310/237 ENGINE MOUNT --- FORWARD ENGINE MOUNT CAST YOKE --- INSPECTION/REPLACEMENT

EASA AD 2010 - 0066 AS IN AD AS IN AD

238 DGCA/A310/238 FLIGHT CONTROLS --- TRIMMABLE HORIZONTAL STABILIZER ACTUATOR (THSA) UPPER ATTACHMENT GIMBAL --- INSPECTION

EASA AD 2010 - 0092 AS IN AD AS IN AD

239 DGCA/A310/239 STABILIZERS --- RUDDER SIDE SHELL SKIN --- INSPECTION

EASA AD 2010 - 0144 AS IN AD AS IN AD

240 DGCA/A310/240R1 ELECTRICAL POWER --- WIRING INSTALLATION AT PYLON /WING INTERFACE --- MODIFICATION

EASA AD 2010 - 0178R1 AS IN AD AS IN AD

241 DGCA/A310/241 FUEL --- FUEL LEVEL SENSOR AMPLIFIER (FLSA) AND MULTI TANK INDICATOR (MTI) WIRING ---

EASA AD 2010 - 0175 AS IN AD AS IN AD

REPLACEMENT

242 DGCA/A310/242 FUEL SYSTEM – FUEL TANK ELECTRICAL BONDING – INSPECTION/MODIFICATION [FUEL TANK SAFETY]

EASA AD 2010 - 0199 AS IN AD AS IN AD

243 DGCA/A310/243 FLIGHT CONTROLS --- TRIMMABLE HORIZONTAL STABILIZER ACTUATOR (THSA) UPPER ATTACHMENT -- MODIFICATION

EASA AD 2010 - 0224 AS IN AD AS IN AD

244 DGCA/A310/244R1 WINGS --- MAIN LANDING GEAR (MLG) RIB 5 AFT BEARING FORWARD LUG BUSHES --- REPLACEMENT

EASA AD 2012 - 0176 AS IN AD AS IN AD

245 DGCA/A310/245 HYDRAULIC POWER --- HYDRAULIC ACCUMULATOR --- INSPECTION / REPLACEMENT / PLACARDS INSTALLATION

EASA AD 2011 - 0006 AS IN AD AS IN AD

246 DGCA/A310/246 HYDRAULIC POWER --- ELECTRICAL MOTOR PUMP FEEDER CABLES & PRESSURE HOSES --- INSPECTION / REPAIR / PLACARD INSTALLATION

EASA AD 2011 - 0071 AS IN AD AS IN AD

247 DGCA/A310/247 R2

DOORS --- FORWARD CARGO DOOR HIGH PRESSURE PIPE --- REPLACEMENT

EASA AD 2011 - 0085R1 CORRECTION :20 TH JULY 2012

AS IN AD AS IN AD

248 DGCA/A310/248R1 FUSELAGE -- CROSS BEAM AT JUNCTION WITH LOWER CARGO DOOR ACTUATOR BEAM --- INSPECTION/MODIFICATION

EASA AD 2011 - 0086R1 AS IN AD AS IN AD

249 DGCA/A310/249 ATA 28 - FUEL PUMP SYSTEM - FUEL PUMP CANISTER HOOD HALVES-INSPECTION / REPLACEMENT

EASA AD 2011-0124 AS IN AD AS IN AD

250 DGCA/A310/250 ATA 57 -WINGS - BOTTOM SKIN NO. 2 PANEL - INSPECTION

EASA AD 2011-0125 AS IN AD AS IN AD

251 DGCA/A310/251 ATA 74-IGNITION -IGNITION STARTING AND CONTINUOUS RELIGHT -AUTO-RELIGHT FUNCTION IMPLEMENTATION FOR CF6-80C2 ENGINES

EASA AD 2011-0113 AS IN AD AS IN AD

252 DGCA/A310/252 ATA 28- FUEL - FUEL QUANTITY INDICATION COMPUTER - MODIFICATION

EASA AD 2011-0186 AS IN AD AS IN AD

253 DGCA/A310/253 ATA 57 - WINGS - SLATS # 2 AND 3, EXTENSION EASA AD 2011-0187 AS IN AD AS IN AD

BOLTS AT TRACKS 4,5,6,7 AND 8 - REPLACEMENT

254 DGCA/A310/254 STABILIZERS --- VERTICAL STABILIZER / RUDDER --- REPLACEMENT

EASA AD 2012-0006 AS IN AD AS IN AD

255 DGCA/A310/255R1 WINGS --- FUEL ACCESS PANELS --- REPLACEMENT / MODIFICATION

EASA AD 2012-0016R1 AS IN AD AS IN AD

256 DGCA/A310/256 ATA 57 - WINGS --- SLAT EXTENSION ECCENTRIC BOLTS --- REPLACEMENT

EASA AD 2012-0042 AS IN AD AS IN AD

257 DGCA/A310/257 ATA 71 - ENGINE MOUNTS --- FORWARD ENGINE MOUNT BOLTS --- REPLACEMENT

EASA AD 2012-0056 AS IN AD AS IN AD

258 DGCA/A310/258 FUEL/MAIN TRANSFER SYSTEM --- INNER,CENTRE AND TRIM TANK FUEL PUMP CONTROL CIRCUIT --- MODIFICATION

EASA AD 2012-0091 AS IN AD AS IN AD

259 DGCA/A310/259 EQUIPMENT & FURNISHINGS --- POWERED PILOT & CO -PILOTS SEATS --- INSPECTION

EASA AD 2012-0102 AS IN AD AS IN AD

260 DGCA/A310/260 AUTO FLIGHT / INSTRUMENTS --- STOP RUDDER INPUTS WARNING (SRIW) DEVICE --- INSTALLATION / ACTIVATION

EASA AD 2012-0088 AS IN AD AS IN AD

261 DGCA/A310/261R1 EQUIPMENT / FURNISHINGS ---- PORTABLE OXYGEN CYLINDER IN OVERHEAD STOWAGE --- INSPECTION / REPLACEMENT

EASA AD 2012-0245-E AS IN AD AS IN AD

262 DGCA/A310/262 STABILIZERS --- RUDDER SIDE PANEL ALONG THE Z - PROFILE --- INSPECTION

EASA AD 2013-0039 AS IN AD AS IN AD

263 DGCA/A310/263 LANDING GEAR --- SEQUENCE VALVE & LEVER --- INSPECTION / REPLACEMENT

EASA AD 2013-0058 AS IN AD AS IN AD

264 DGCA/A310/264 LANDING GEAR --- NORMAL EXTENSION & RETRACTION UPLOCK SPRINGS --- INSPECTION / REPLACEMENT

EASA AD 2013-0150 AS IN AD AS IN AD

265 DGCA/A310/265 FUEL --- FUEL PUMPS / POWER SUPPLY CIRCUIT BREAKERS --- FUNCTIONAL TEST / REPLACEMENT

EASA AD 2013-0163 AS IN AD AS IN AD

266 DGCA/A310/266 HYDRAULIC POWER --- ELECTRICAL MOTOR PUMPELECTRICAL ROUTING AND HYDRAULIC PIPES --- MODIFICATION

EASA AD 2013-0165 AS IN AD AS IN AD