曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
140 DGCA/A310/140 NAVIGATION-PITOT PROBES (ATA 34) DGAC AD 2001-265(B)R2 & 2003-148(B) AS IN AD AS IN AD
SERIAL NO DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY
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
SERIAL NO DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY
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 MODEINSPECTION
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/A310/156 FUEL --- ELECTRIC/ELECTRONIC COMMON
INSTALLATION FUEL SYSTEM ROUTE 2S ---
MODIFICATION
EASA AD 2007 - 0230 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
SERIAL NO DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY
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
SERIAL NO DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY
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
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