DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY TURBINE (IPT) AND INTERMEDIATE PRESSURE COMPRESSOR (IPC) SHAFT SPLINE FLANK WEAR
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1 DGCA/RR RB 211-TRENT 700/800 SERIES/01 DGCA/RR RB 211-TRENT 700/800 SERIES/02 DGCA/RR RB 211-TRENT 700/800 SERIES/03 TO PREVENT THRUST REVERSER HINGE FAILURE TO PREVENT INTERMEDIATE PRESSURE TURBINE (IPT) AND INTERMEDIATE PRESSURE COMPRESSOR (IPC) SHAFT SPLINE FLANK WEAR TO DETECT CRACKING, LOOSE RIVETS, AND MISSING RIVETS ON COMMON NOZZLE ASSEMBLY P/N FK OR FK DGCA/RR RB 211-TRENT 700/800 SERIES/04 ENGINE - GROUP A (CRITICAL) PARTS - FOCUSED S DGCA/RR RB 211-TRENT 700/800 SERIES/05 ENGINE - HP COMPRESSOR - TEST/MODIFICATION DGCA/RR RB 211-TRENT 700/800 SERIES/06 DGCA/RR RB 211-TRENT 700/800 SERIES/07 DGCA/RR RB 211-TRENT 700/800 SERIES/08 ENGINE - HP/IP TURBINE BEARING OIL VENT TUBES - / CLEANING / TO PREVENT POSSIBLE MULTIPLE LPC FAN BLADE FAILURE ENGINE - IP TURBINE BEARING OIL VENT & SCAVENGE TUBE - /MODIFICATION DGCA/RR RB 211-TRENT 700/800 SERIES/09 ENGINE OIL TANK - OIL FILLER CAP ASSEMBLY - / DGCA/RR RB 211-TRENT 700/800 SERIES/10 DGCA/RR RB 211-TRENT 700/800 SERIES/11 DGCA/RR RB 211-TRENT 700/800 SERIES/12R6 ENGINE - IP TURBINE BEARING/ OIL FEED TUBE FRETTAGE - ENGINE - LP COMPRESSOR - BLADE ANNULUS FILLER REVISED LIVES ATA-72- ENGINE --- INTERMEDIATE PRESSURE COMPRESSOR ROTOR SHAFT AND BALANCE FAA AD FAA AD FAA AD UK CAA AD G EASA AD EASA AD FAA AD EASA AD EASA AD EASA AD EASA AD EASA AD R1 REVISED EASA AD 2014-
2 WEIGHTS ---- /MODIFICATION DGCA/RR RB 211-TRENT 700/800 SERIES/13 ENGINE --- IP COMPRESSOR SHAFT ---- DGCA/RR RB 211-TRENT 700/800 SERIES/14 ENGINE -- ENGINE ELECTRONIC CONTROLLER ( EEC ) --- DGCA/RR RB 211-TRENT 700/800 SERIES/15 DGCA/RR RB 211-TRENT 700/800 SERIES/16 DGCA/RR RB 211-TRENT 700/800 SERIES/17R2 ENGINE - HP/IP TURBINE BEARING OIL VENT TUBE RESTRICTOR - / CLEANING / ENGINE - INTERMEDIATE PRESSURE (IP) TURBINE DISC ---- IDENTIFICATION/REMOVAL ENGINE -- HIGH PRESSURE COMPRESSOR STAGE 1-4 SHAFT --- LIFE LIMIT REDUCTION DGCA/RR RB 211-TRENT 700/800 SERIES/18 ENGINE -- IP AND HP COMPRESSOR SHAFTS --- DGCA/RR RB 211-TRENT 700/800 SERIES/19R2 ENGINE -- HIGH PRESSURE COMPRESSOR ROTOR DISCS & ROTOR SHAFTS --- / DGCA/RR RB 211-TRENT 700/800 SERIES/20 ENGINE -- HIGH PRESSURE (HP) / INTERMEDIATE PRESSURE (IP) TURBINE BEARING OIL VENT TUBE --- /CLEANING / DGCA/RR RB 211-TRENT 700/800 SERIES/21 DGCA/RR RB 211-TRENT 700/800 SERIES/22R1 ENGINE -- FUEL SYSTEM,FUEL TO OIL HEAT EXCHANGER (FOHE) --- ENGINE --- FRONT COMBUSTION LINER HEAD SECTION --- / 0152 SUPER EASA AD EASA AD R1 EASA AD R1 - CN(THIS AD HAS BEEN CANCELLED FOR RB 211 TRENT 700 SERIES ENGINE) EASA AD EASA AD E - CN EASA AD EASA AD EASA AD EASA AD EASA AD EASA AD R2 DGCA/RR RB 211-TRENT 700/800 SERIES/23 THRUST REVERSER --- C ---DUCT --- EASA AD CN
3 DGCA/RR RB 211-TRENT 700/800 SERIES/24R3 DGCA/RR RB 211-TRENT 700/800 SERIES/25 DGCA/RR RB 211-TRENT 700/800 SERIES/26R1 DGCA/RR RB 211-TRENT 700/800 SERIES/27R2 DGCA/RR RB 211-TRENT 700/800 SERIES/28R1 DGCA/RR RB 211-TRENT 700/800 SERIES/29 DGCA/RR RB 211-TRENT 700/800 SERIES/30R2 DGCA/RR RB 211-TRENT 700/800 SERIES/31 DGCA/RR RB 211-TRENT 700/800 SERIES/32R6 OF REAR HINGE LUGS ENGINE --- FRONT COMBUSTION LINER INNER WALL --- ENGINE -- FUEL SYSTEM,FUEL TO OIL HEAT EXCHANGER (FOHE) --- ENGINE -- LOW PRESSURE COMPRESSOR FAN BLADES -- / ATA 73,ENGINE FAN CASE LOW PRESSURE FUEL TUBES AND CLIPS - / ENGINE -- FRONT COMBUSTION LINER HEAD SECTION -- / ATA 72 - ENGINE - CRITICAL PARTS - LIFE LIMIT REDUCTION ENGINE --- INTERMEDIATE PRESSURE (IP) TURBINE DISC ---- IDENTIFICATION// ENGINE -- HIGH / INTERMEDIATE PRESSURE TURBINE BEARING SUPPORT STRUCTURE --- /MODIFICATION ENGINE -- LOW PRESSURE COMPRESSOR BLADES -- / EASA AD R3 EASA AD EASA AD EASA AD R1 EASA AD R1 AS IN AD AS IN AD EASA AD EASA AD R1 AS IN AD AS IN AD EASA AD EASA AD R1 REVISED EASA AD SUPERSEDED EASA AD (CORRECTION: 20 JULY 2016) SUPERSEDED EASA AD
4 DGCA/RR RB 211-TRENT 700/800 SERIES/33 CANCELLED: ENGINE -- HIGH PRESSURE COMPRESSOR TO HIGH PRESSURE TURBINE JOINT BOLTS --- DGCA/RR RB 211-TRENT 700/800 SERIES/34R1 ENGINE -- AIR GUIDE TUBE / PHONIC RING -- DGCA/RR RB 211-TRENT 700/800 SERIES/35 DGCA/RR RB 211-TRENT 700/800 SERIES/36 DGCA/RR RB 211-TRENT 700/800 SERIES/37 DGCA/RR RB 211-TRENT 700/800 SERIES/38 DGCA/RR RB 211-TRENT 700/800 SERIES/39R4 DGCA/RR RB 211-TRENT 700/800 SERIES/40R2 DGCA/RR RB 211-TRENT 700/800 SERIES/41 DGCA/RR RB 211-TRENT 700/800 SERIES/42R1 ENGINE --- HIGH PRESSURE / INTERMEDIATE PRESSURE TURBINE DISCS --- IDENTIFICATION / ENGINE FUEL & CONTROL --- ENGINE ELECTRONIC CONTROL --- SOFTWARE UPDATE ENGINE -- LOW PRESSURE TURBINE BEARING SUPPORT AND EXHAUST CASE ASSEMBLY -- / ENGINE FUEL & CONTROL ENGINE ELECTRONIC CONTROL SOFTWARE UPDATE ATA 73, ENGINE FUEL AND CONTROL LOW PRESSURE FUEL TUBES AND CLIPS, FUEL OIL HEAT EXCHANGER MOUNTS / ATA 72,ENGINE HIGH / INTERMEDIATE PRESSURE TURBINE BEARING SUPPORT OIL FEED TUBE SEALING SLEEVE / ATA 72, ENGINE-HIGH PRESSURE COMPRESSOR STAGE 1-4 DRUM- ATA 72-ENGINE-UPPER BIFURCATION FAIRING SEAL FACE- EASA AD CN AS IN AD AS IN AD EASA AD E AS IN AD AS IN AD EASA AD AS IN AD AS IN AD EASA AD EASA AD EASA AD EASA AD SUPERSEDED EASA AD R1 corrction revision SUP EASA AD EASA AD R1 revision SUPER EASA AD EASA AD (CORRECTION: 27 APRIL 2016) EASA AD
5 DGCA/RR RB 211-TRENT 700/800 SERIES/43R1 ATA-72 ENGINE COMPRESSOR INTERMEDIATE CASE / REPAIR EASA AD DGCA/RR RB 211-TRENT 700/800 SERIES/44 ATA 72 ENGINE LOW PRESSURE EASA AD COMPRESSOR CASE A-FRAME HOLLOW LOCATING PINS DGCA/RR RB 211-TRENT 700/800 SERIES/45 ATA 72 ENGINE CRITICAL PARTS REDUCTION OF DECLARED SAFE CYCLIC LIFE EASA AD DGCA/RR RB 211-TRENT 700/800 SERIES/46 ATA 72-ENGINE-INTERMEDIATE PRESSURE EASA AD R1 COMPRESSOR ROTOR SHAFT AND BALANCE WEIGHTS-/MODIFICATION
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