曝光台 注意防骗
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EASA AD 2006-0178 AS IN AD AS IN AD
208 DGCA/A310/208 TIME LIMITS / MAINTENANCE CHECKS ---
DAMAGE TOLERANT AIRWORTHINESS
LIMITATION ITEMS --- ALS PART 2 ---
AMENDMENT
EASA AD 2009 - 0155 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
SERIAL NO DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY
211 DGCA/A310/211 WINGS / MAIN LANDING GEAR (MLG)
ATTACHEMENT - INSPECTION
EASA AD 2007 - 0195 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
SERIAL NO DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY
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/A310/222 NACELLES/PYLONS --- PYLON SIDE PANELS AT
RIB 8 --- INSPECTION
EASA AD 2008-0181 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/A310/225 ENGINE EXHAUST --- CENTRE LATCH OF
THRUST REVERSER DOOR OPENING
MECHANISM --- REPLACEMENT / INSPECTION
EASA AD 2008 - 0226 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/A310/229 EQUIPMENT / FURNISHINGS --- PILOT & COPILOT
SEATS --- DEACTIVATION OF POWERED
MOVEMENT
EASA AD 2009 - 0084 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
SERIAL NO DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY
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
U.S. Department of Transportation
Federal Aviation Administration
Washington, D.C.
Master Minimum Equipment List
Revision: 21
Date: June 17, 2009
Airbus
A318/A319/A320/A321
Peter S. Neff, Chairman
Flight Operations Evaluation Board (FOEB)
Federal Aviation Administration
Aircraft Evaluation Group
1601 Lind Ave. S.W.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
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