N805NW

Part: LIGHT — DAMAGED (ZONE 200) · airframe 95,915 hrs · 12,496 cycles

SHIP 3305 33H & 58H EMER LIGHT HOUSING DAMAGED UNDER SEAT. REPLACED HOUSING PER A330 AMM 33-51. OK FOR SERVICE. (7921595)

Part: ENGINE — FAILED (NR 1) · airframe 94,557 hrs · 12,325 cycles

SHIP 3305 #1 ENG FAIL AT FL380 MACH 0.82 SMOOTH AIR. CHANGED ENGINE #1 IAW A330 AMDS JIC 7100-9901-01. (7314738).

Part: ENGINE — STALLED (LEFT) · airframe 94,557 hrs · 12,325 cycles

SHIP 3305 -DIV/IFSD- DIVERTED TO TER DUE TO LEFT ENGINE FAILED DURING CRUISE. CORRECTIVE ACTION: LEFT ENGINE EXPERIENCED A STALL WITH AN EGT OVER LIMIT, ENGINE WAS SHUTDOWN. ENGINE CHANGE DUE TO EGT EXCEEDANCE OF 751C FOR 120 SECONDS. ESN 733547 CSR 1044 TSR 8083 NO PRIOR HISTORY OF ENGINE ISSUES, TREND DATA REVIEWED, NO SHIFTS IN ANY PARAMETERS PRIOR TO EVENT. REPLACED ENGINE PER A330 AMM 71-00-00-000-803.

Part: SKIN — DAMAGED (ZONE 300) · airframe 93,943 hrs · 12,251 cycles

SHIP 3305 TOOLING DAMAGE FOUND ON R/H HORIZONTAL STAB UPPER SURFACE. APPROX 48" FROM LEADING EDGE AND 4" OUTBOARD OF SEAL. CORRECTIVE ACTION: REPAIRED DAMAGE PER A330 SRM 55-11-11-283-012. (0983935)

Part: SKIN — DAMAGED (ZONE 300) · airframe 94,557 hrs · 12,325 cycles

SHIP 3305 TOOLING DAMAGE FOUND ON R/H HORIZONTAL STAB UPPER SURFACE. APPROX 48" FROM LEADING EDGE AND 4" OUTBOARD OF SLIGING SEAL. EVALUATED AND REPAIRED DAMAGE PER A330 SRM 55-11-11-283-012. (0983934).

Part: ENGINE — FAILED (RIGHT) · airframe 91,684 hrs · 11,955 cycles

-ATO- DISCONTINUED TAKEOFF AT 25 KNOTS DUE TO RIGHT ENGINE FAILURE ALONG WITH FIRE INDICATION WARNING IN THE FLIGHT DECK. RIGHT ENGINE FIRE BOTTLES DISCHARGED. CORRECTIVE ACTION: FOUND METAL IN THE 2.5 AND 2.9 BLEED PORTS, ENGINE CHANGE REQUIRED. R/R RIGHT ENGINE #1 FIRE BOTTLE AND R/R RIGHT ENGINE PER AMDS W/C 7100-9901. OPS CHECK GOOD. OK FOR SERVICE. (5808846)

Part: ENGINE — MAKING METAL (RIGHT) · airframe 91,678 hrs · 11,952 cycles

SHIP 3305 -ATO- DISCONTINUED TAKEOFF AT 25 KNOTS DUE TO RIGHT ENGINE FAILURE ALONG WITH FIRE INDICATION WARNING IN THE FLIGHT DECK. RIGHT ENGINE FIRE BOTTLES DISCHARGED. CORRECTIVE ACTION: FOUND METAL IN THE 2.5 AND 2.9 BLEED PORTS, ENGINE CHANGE REQUIRED. MAINTENANCE IN PROGRESS.

Part: SKIN — GOUGED (L4 DOOR) · airframe 91,549 hrs · 11,937 cycles

SHIP 3305 A GOUGE WAS FOUND ON DOOR 4L AFT LOWER CORNER. CORRECTIVE ACTION: COMPLIED WITH ERA 621514-14. (0614825)

Part: SKIN — DAMAGED (ZONE 100) · airframe 91,549 hrs · 11,937 cycles

SHIP 3305 DAMAGE AROUND AFT CARGO DOOR. CORRECTIVE ACTION: COMPLIED WITH ERA 620921-14 REV.A. (0613444)

Part: SKIN — DAMAGED (ZONE 200) · airframe 91,549 hrs · 11,937 cycles

SHIP 3305 FUSELAGE UPPER SKIN FOUND TOOL MARK BETWEEN STR P'3 AND STR P'2 FROM STA C53.7 TO C53.8. CORRECTIVE ACTION: COMPLIED WITH ERA 621544-14 REV.0. (0612948)

Part: SKIN — DAMAGED (ZONE 200) · airframe 91,549 hrs · 11,937 cycles

SHIP 3305 FUSELAGE UPPER SKIN FOUND TOOL MARK BETWEEN STR P3 AND STR P2 FROM STA C53.6 TO C53.7. CORRECTIVE ACTION: COMPLIED WITH ERA 621544-14 REV.0. (0612944)

Part: SKIN — DAMAGED (ZONE 200) · airframe 91,549 hrs · 11,937 cycles

SHIP 3305 FUSELAGE UPPER SKIN FOUND TOOL MARK BETWEEN STR P'3 AND STR P'2 FROM STA C53.6 TO C53.7. CORRECTIVE ACTION: COMPLIED WITH ERA 621544-14 REV.0. (0612936)

Part: SKIN — DAMAGED (ZONE 200) · airframe 91,549 hrs · 11,937 cycles

SHIP 3305 FUSELAGE UPPER SKIN FOUND TOOL MARK BETWEEN STR P3 AND STR P2 FROM STA C53.7 TO C53.8. CORRECTIVE ACTION: COMPLIED WITH ERA 621544-14 REV.0. (0612957)

Part: SKIN — GROUND DAMAGE (ZONE 100) · airframe 91,549 hrs · 11,937 cycles

SHIP 3305 AFT CARGO DOOR SURROUND / C59A & STR-40RH TO STR-42RH / GROUND DAMAGE. CORRECTIVE ACTION: COMPLIED WITH ERA 620921-14, REV B. (0611670)

Part: SKIN — GOUGED (ZONE 200) · airframe 91,549 hrs · 11,937 cycles

SHIP 3305 GOUGES WERE FOUND ON THE FUSELAGE SKIN BETWEEN FR 53.6 AND FR 53.7, STR 2R TO STR 2L. CORRECTIVE ACTION: COMPLIED WITH ERA 621544-14. (0611415)

Part: LEVER — OUT OF RIG (L4 DOOR) · airframe 91,433 hrs · 11,922 cycles

SHIP 3305 DEVELOPING HISTORY OF 4L DOOR INDICATION. CORRECTIVE ACTION: RIGGED OUTSIDE DOOR LEVER. OK TO CONTINUE. (0561236)

Part: SKIN — DAMAGED (ZONE 100) · airframe 91,464 hrs · 11,926 cycles

SHIP 3305 FOA AFT CARGO, FWD SIDE OF AFT CARGO DOOR SURROUNDING SKIN. 3X DAMAGE AT FR59 / STRINGER 40RH UNTIL 42RH. 2X OLD DAMAGE IN SAME AREA. CORRECTIVE ACTION: COMPLIED WITH ERA 620921-14. (6345402)

Part: TURNBUCKLE — OUT OF ADJUST (ZONE 700) · airframe 91,312 hrs · 11,906 cycles

SHIP 3305 - ATB - DUE TO L/G ECAM FAULT AND GEAR NOT RETRACTING WHEN SELECTED UP. CORRECTIVE ACTION: ADJUSTED LT MLG SHORTENING MECHANISM TURNBUCKLE. PERFORMED GEAR SWING. NO FAULTS. ALL GEAR RETRACT PROPERLY. (5890558)

Part: HOUSING — BROKEN (EMERGENCY LIGHT) · airframe 91,312 hrs · 11,906 cycles

SHIP 3305 EMERGENCY LIGHT HOUSING BROKEN ON SEAT 41H. CORRECTIVE ACTION: REPLACED LIGHT ASSY. OPS GOOD. (5890566)

Part: DOOR — FOD (R4) · airframe 90,791 hrs · 11,832 cycles

SHIP 3305 4R DOOR FAILED TO ARM. CORRECTIVE ACTION: REMOVED FOD PER A330 AMM 52-12. OPS CHECK GOOD. (6098718)

Part: OXYGEN MASK — UNWANTED DEPLOY (ZONE 200) · airframe 90,706 hrs · 11,820 cycles

SHIP 3305 4L FLIGHT ATTENDANT MASK DEPLOYED IN FLIGHT. CORRECTIVE ACTION: R/R OXYGEN CONTAINER ASSY. IN REF. TO A330 AMM 35-21. PERFORMED MASK DROP TEST AND OPS CHECK NORMAL. (5911473)

Part: STRUCTURE — CRACKED (L4 DOOR) · airframe 90,312 hrs · 11,767 cycles

FOUND INDENTATION ON DOOR 4L LOWER AFT CORNER EDGE. REPAIRED PER A330 SRM 52-10-00-283-001.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 88,369 hrs · 11,520 cycles

SHIP 3305 UPON ARRIVAL AT GATE ALL CABIN PRESSURE DOOR LIGHTS WERE FLASHING. AIRCRAFT WAS DEPRESSURIZED. CORRECTIVE ACTION: REPLACED CONTROLLER AND PROX SWITCH PER A330 AMM 52-71. (5426150)

Part: LIGHT — BROKEN (SEAT 58 AB) · airframe 88,267 hrs · 11,506 cycles

SHIP 3305 SEAT 58AB EMERGENCY LIGHT INOP. CORRECTIVE ACTION: INSTALLED NEW LIGHT ASSY PER A330 AWM 33-51. (4354097)

Part: LIGHT — BROKEN (EMERGENCY LIGHT) · airframe 88,267 hrs · 11,506 cycles

SHIP 3305 SEAT 46AB EMERGENCY LIGHT INOP. CORRECTIVE ACTION: INSTALLED NEW LIGHT ASSY PER A330 AWM 33-51. (4354096)

Part: INDICATION SYS — FALSE INDICATION (L4 DOOR) · airframe 88,198 hrs · 11,497 cycles

SHIP 3305 4L DOOR SLIDE INDICATES ARMED WHEN DISARMED. CORRECTIVE ACTION: DOOR WAY 4L CLEANED. OPS SLIDE SEVERAL TIMES, INDICATION ON FAP. (4354076)

Part: PROXIMITY SENSOR — OUT OF ADJUST (L4 DOOR) · airframe 88,231 hrs · 11,501 cycles

DOOR 4L SLIDE ARMED IND IN FLT DECK FA VERIFIED. CORRECTIVE ACTION: DEFERRED. (0157647) ADJUSTED PROXIMITY SENSOR 37MJ, REF A330 AMM 52-71-11. DOOR PROXIMITY SENSOR FOR SLIDE OPS CHECKS GOOD.

Part: SLIDE — FALSE INDICATION (L4 DOOR) · airframe 88,198 hrs · 11,497 cycles

SHIP 3305 DOOR 4L SHOWING SLIDE ARMED IN COCKPIT BUT FA'S CONFIRMED DISARMED WITH PIN IN PLACE. CORRECTIVE ACTION: CYCLED 4L DOOR ARM/DISARM HANDLE. NO FAULTS NOTED + ALL INDICATIONS ON FAP MATCH. ALL OPS CHECK GOOD. (4354049)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,733 hrs · 11,438 cycles

SHIP 3305 EMERGENCY LIGHTS AT SEAT ROWS 43HJ, 44HJ, 45HJ, AND 46HJ. CORRECTIVE ACTION: REPINNED CONNECTOR. (0107751)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,721 hrs · 11,436 cycles

SHIP 3305 AT SHUTDOWN 4L SLIDE SHOWED INTERMITTENT ARMED WITH HANDLE DISARMED. CORRECTIVE ACTION: OPERATED ARMING HANDLE SEVERAL TIMES. DOORS ARMS / DISARMS AS IT SHOULD. (5487775)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,265 hrs · 11,378 cycles

SHIP 3305 - MISC/DE - DUE TO LOSS OF THE GREEN HYDRAULIC SYSTEM. CORRECTIVE ACTION: REPLACED #1 ENG GREEN HYD PUMP. (4373328)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,250 hrs · 11,376 cycles

SHIP 3305 4L DOOR DIFFICULT TO DISSARM AT GATE. CORRECTIVE ACTION: CYCLED 4L DOOR ARM/DISSARM HANDLE, COULD NOT DUPLICATE FAULT. OPS CHK NML. (4373320)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,096 hrs · 11,356 cycles

SHIP 3305 CARGO LOADER CONTACTED AIRCRAFT NEAR FWD CARGO DOOR. CORRECTIVE ACTION: PERFORMED ALL REPAIRS AND INSPECTIONS PER PRI 612078-14. SPLICED IN NEW SECTION OF FRAME 25. (4467222)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,096 hrs · 11,356 cycles

SHIP 3305 ROW 50JH EMERGENCY PATH LIGHT INOP. CORRECTIVE ACTION: REMOVED AND REPLACED EMERGENCY PATH LIGHT AT 50 JH. (0002387)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,621 hrs · 11,299 cycles

SHIP 3305 EXIT SIGN ABOVE 4R DOESN'T ILLUMINATE. CORRECTIVE ACTION: AFTER CIDS RESET, FOUND ALL EXIT SIGNS ILLUMINATED. TESTED EMERGENCY EXIT LIGHTS. (4391602)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,111 hrs · 11,237 cycles

AIRCRAFT 3305, EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:107. CORRECTIVE ACTION: FOUND LENS AND INSTALLED, OK FOR SVC. (LP 2838450)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,802 hrs · 11,199 cycles

SHIP 3305 AFTER PARKING SEA (ENGS SHUT DOWN) ALL DOORS SHOWED RED CABIN PRESS LIGHT. DIFF PRESS WAS 0 AT THE TIME. CORRECTIVE ACTION: T/S. NO ASSOCIATED DIFF CABIN PRESSURE MSGS. (4730770)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,736 hrs · 11,191 cycles

SHIP 3305 EXIT SIGN AT 4R NOT ILLUMINATED. CORRECTIVE ACTION: EXIT SIGN TESTED ON GROUND OPS CHECK GOOD. (4730752)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,718 hrs · 11,189 cycles

SHIP 3305 EXIT LITE BURNT OUT DOOR 4R. CORRECTIVE ACTION: OPS CHECK GOOD, NO DEFECT NOTED. (4730728)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,541 hrs · 11,168 cycles

SHIP 3305 AFTER ENGINE SHUTDOWN, CABIN ALTITUDE IN THE COCKPIT SHOWED THE LANDING ALTITUDE, BUT FLIGHT ATTENDANTS REPORTED THE DOOR FLASHING THE PRESSURIZED LIGHTS. CORRECTIVE ACTION: PERFORMED TSM TASK. PFR READOUT SHOWS NO CORRELATED MESSAGE, NO FURTHER ACTION REQUIRED PER TSM. (4694274)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,533 hrs · 11,167 cycles

SHIP 3305 DTA ER/A 603846-14 REV A MONITOR INSPECTION LOG REFERENCE REQUIRES 3RD STAGE DTA APPROVAL ON OR BEFORE 1ST OF 82300 CYC OR 219700 HRS AFTER SECT I. CORRECTIVE ACTION: REF ER/A 603846-14. (2774517)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,507 hrs · 11,164 cycles

SHIP 3305 DOOR POS DET 1 AND 2 FAULT FLASHED 3-4 TIMES PRIOR TO PUSH BACK, CLEARED ON ITS OWN. CORRECTIVE ACTION: PERFORMED BITE TEST. TEST OK. (4694248)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,344 hrs · 11,145 cycles

SHIP 3305 CABIN DOOR L2 WOULD NOT SHOW CLOSED. CORRECTIVE ACTION: CYCLED DOOR AND IT HAD CLOSED INDICATION. OK TO CONTINUE IN SERVICE. (4674978)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,622 hrs · 11,057 cycles

SHIP 3305 - ATB - DUE TO VISIBLE SPARKS FROM THE TOP OF THE COCKPIT DOOR WHEN OPENING AND CLOSING DOOR. CORRECTIVE ACTION: FOUND BARE WIRES CONTACTING DOOR STRUCTURE. SPLICED IN 6 FT OF NEW WIRING. C/W NO-GO PROCEDURES. (4147036)

Part: UNKNOWN — UNKNOWN · airframe 84,600 hrs · 11,054 cycles

SHIP 3305 SPARKS FLY FROM KEYPAD AREA 1 UPPER STRIKE WHEN CLOSING COCKPIT DOOR. CORRECTIVE ACTION: REMOVED & REPLACED COCKPIT DOOR KEYPAD. (4147025)

Part: NONE — NONE · airframe 84,250 hrs · 11,014 cycles

SHIP 3305 1ST OBSERVERS O2 MASK FAILS TO TEST. CORRECTIVE ACTION: REMOVED AND REPLACED O2 MASK STORAGE BOX PER A330 35-12. (4187534)

Part: JACK — SPARKS (SEAT 20J AUDIO) · airframe 84,009 hrs · 10,984 cycles

AUDIO JACK SPARKS AND SHORTS OUT AT SEAT 20J. FAULT NOT CONFIRMED. OPS CK GOOD.

Part: ANTI-ICE VALVE — FAULTED (NR 1 ENGINE) · airframe 83,835 hrs · 10,961 cycles

SHIP 3305 -DIV- TO MAD DUE TO NBR 1 ENGINE ANTI ICE VALVE FAILED CLOSED. CORRECTIVE ACTION: REPLACED VALVE AND SWAPPED SOLENOID WITH NACELLE COOLING VALVE SOLENOID. (4048020)

Part: DOOR — UNKNOWN (L4) · airframe 83,827 hrs · 10,960 cycles

L4 DOOR WILL NOT DISARM ON ARRIVAL. R/R CNTRL UNIT IAW A330 AMM 30-46. (4048006)

Part: GIRT BAR — FROZEN (L4 DOOR) · airframe 83,800 hrs · 10,956 cycles

4L DOOR SLIDE WILL NOT DISARM. 4L DOOR DISARMED AND FOUND WATER AND ICE IN GIRT BAR AREA. AREA CLEANED DOOR FUNCTIONED SEVERAL TIMES, ALL OPS AND INDICATIONS NORMAL.

Part: GUST LOCK — INOPERATIVE (L2 DOOR) · airframe 83,800 hrs · 10,956 cycles

GUST LOCK BUTTON ON 2L DOESNT WORK. DOOR 2L GUST LOCK CHECKS NORMAL.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 83,732 hrs · 10,948 cycles

DOOR 1L EXIT LIGHT INOP. REMOVED EXIT LIGHT FOUND GRND WIRE BROKEN . DURING REMOVAL 5.6V WIRE ALSO BROKE. RE TERMINATED GRND WIRE 1L DOOR EXIT LIGHT NOW NORMAL.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 83,732 hrs · 10,948 cycles

SHIP 3305 4L OVERHEAD EMERGENCY LIGHTING INOP. OVHD EMERGENCY LIGHT COVER MISSING. CORRECTIVE ACTION: INSTALLED NEW LIGHT COVER PER A330 AMM 33-51. (2563944)

Part: NONE — NONE (NONE) · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR 30 TO FR31 BTW STR1L TO STR1R ON UPPER FUSELAGE. CORRECTIVE ACTION: EXISTING ALTERATION INSTALLED PER 2325-01059-03. STC IS APPROVED FOR DAMAGE TOLERANCEIN ACCORDANCE WITH FAR 25.47 AND 25.571. AS PER ER/A #603078-14. (2533312)

Part: FRAME — CRACKED (FRM 40) · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 CRACK FRAME 40 RH SIDE VERTICAL WEB ABOVE THE CENTER WING BOX LOWER PANEL AT HOLE H263, CRACK DIRECTION IS 6 OCLOCK, AA 5716-01017, SB A330- 57-3115 REV 02, AD 2019-16-07, IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR ON HOLE H263RH LOCATED ON FR40 RH SIDE VERTICAL WEB ABOVE THE CENTER WING BOX LOWER PANEL AS PER ER/A 603575-14AD. (2533233)

Part: SKIN — NOT REPORTED (FRMS 30-31) · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR.30 TO FR.31 BTW STR1L TO STR1R ON UPPER FUSELAGE. CORRECTIVE ACTION: EXISTING ALTERATION INSTALLED PER 2325-01059-03. INSTALLATION IS APPROVED BY STC . STC IS APPROVED FOR DAMAGE TOLERANCEIN ACCORDANCE WITH FAR 25.47 AND 25.571. AS PER ER/A #603078-14 JOB COMPLETE. (2533320)

Part: FRAME — CRACKED (FRM 40) · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 CRACK FRAME 40 RH SIDE VERTICAL WEB ABOVE THE CENTER WING BOX LOWER PANEL AT HOLE H260, CRACK DIRECTIONS ARE 7 AND 10 OCLOCK, AA 5716-01017, SB A330-57-3115 REV 02, AD 2019-16-07, IN FWD CARGO COMPARTMENT (2 EA). CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR ON HOLE H260 LOCATED ON FR40 RH SIDE VERTICAL WEB ABOVE THE CENTER WING BOX LOWER PANEL AS PER ER/A603575-14AD HAS BEEN COMPLIED WITH AND ER/A 603575-14AD REV-ORIGINAL MATCHES. (2533140)

Part: NONE — NONE (NONE) · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR OUTBOARD SIDE LOCATED EXTERNAL SKIN BTW RIB 8 TO RIB9 ON RH PYLON. CORREECTIVE ACTION: EXISTING REPAIR INSTALLED PER ER/A 582864-14AD AND A330 SRM 54-51-00-300-006. AS PER ER/A 603078-14 PRI REV-0 HAS BEEN COMPLIED WITH. (2533420)

Part: NONE — NONE (NONE) · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR.66 BTW STR50R TO STR56R AT LOWER FUSELAGE. CORRECTIVE ACTION: EXISTING REPAIR INSTALLED PER ER/A 523233-14 AND A330 SRM 53-41-11-300- 017. AS PER ER/A 603078-14 PRI REV-0 HAS BEEN COMPLIED WITH. (2533432)

Part: NONE — NONE (NONE) · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR PASSENGER CREW DOOR 834 LOCATED LOWER AFT CORNER IN PASSENGER CABIN. CORRECTIVE ACTION: EXISTING REPAIR INSTALLED PER A330 SRM 52-13-00-300-013, WHICH IS A CATEGORY (B), AS PER ER/A 603078-14 PRI REV-0 HAS BEEN COMPLIED WITH AND ER/A 603078-14 REV-ORIGINAL MATCHES JOB COMPLETE. (2533424)

Part: NONE — NONE (NONE) · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL STRUCTURE ON STRINGER 56R LOCATED FR70 IN AFT CARGO COMPARTMENT. CORRETIVE ACTION: EXISTING REPAIR INSTALLED PER ER/A 590986-14 AND A330 SRM 53-00-13-300-001, APPROVED AS A CATEGORY (A). AS PER ER/A 603078-14 PRI REV-0 HAS BEEN COMPLIED WITH. (2533377)

Part: NONE — NONE (NONE) · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 EXISTING ALTERATION INSTALLED PER 5320-01135. INSTALLATION IS APPROVED BY STC ST02455LA. STC IS APPROVED FOR DAMAGE TOLERANCE INACCORDANCE WITH FAR 25.47 AND 25.571. AS PER ER/A 603078-14. CORRECTIVE ACTION: EXISTING ALTERATION INSTALLED PER 5320-01135. INSTALLATION IS APPROVED BY STC ST02455LA. STC IS APPROVED FOR DAMAGE TOLERANCE INACCORDANCE WITH FAR 25.47 AND 25.571. AS PER ER/A #603078-14. (2533326)

Part: NONE — NONE (NONE) · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR DOOR INNER SKIN AT FR23 TO FR23A IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: EXISTING REPAIR INSTALLED PER ER/A 539577-14. AS PER ER/A603078-14 PRI REV-0 HAS BEEN COMPLIED WITH AND ER/A 603078-14 REV-ORIGINAL MATCHES JOB COMPLETE. (2533400)

Part: NONE — NONE (NONE) · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR DOOR LOCATED INTERNAL AREA AT LEVEL FR62 TO FR63 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: EXISTING REPAIR WAS REMOVED SINCE IT WAS DAMAGE. INSPECTION WERE EXECUTED WITH NIL FINDINGS AND A NEW REPAIR INSTALLED AS PER ER/A 539576-14 WITHOUT DEVIATIONS. SINCE ALL OF THE REQUIREMENTS WERE KEPT WITHOUT DEVIATION, REPAIR IS STILL CONSIDERED ASCATEGORY (A). ER/A 603078-14 PRI REV-0 HAS BEEN COMPLIED WITH. (2533446)

Part: NONE — NONE (NONE) · airframe 83,460 hrs · 10,915 cycles

SHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FUEL TANK LOCATED RIB 6 AFT ON RH WING. CORRECTIVE ACTION: EXISTING REPAIR INSTALLED PER EM 5720-01066-03B AND AIRBUS REPAIR DRAWING R57257026. REPAIR IS APPROVED PER AIRBUS REPAIR DRAWING R57257026 ACCORDING TO FAA AD 2006-22-14 PARA (K) GUIDELINES EM 5720-01066-06B. AS PER ER/A 603078-14 JOB COMPLETE. (2533370)

Part: NONE — NONE (NONE) · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FUEL TANK LOCATED RIB6 AFT ON LH WING. CORRECTIVE ACTION: EXISTING REPAIR INSTALLED. REPAIR IS APPROVED PER AIRBUS REPAIR DRAWING R57257026 ACCORDING TO FAA AD 2006-22-14, PARA. (K) GUIDELINES. AS PER ER/A 603078-14 JOB COMPLETE. (2533366)

Part: NONE — NONE (NONE) · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR.53 TO FR.54 BTW STR1L TO STR1R ON UPPER FUSELAGE. CORRECTIVE ACTION: EXISTING ALTERATION INSTALLED PER 2330-01325-01C. INSTALLATION IS APPROVED BY STC. STC ARE APPROVED FORDAMAGE TOLERANCE IN ACCORDANCE WITH FAR 25.47 AND 25.571. AS PER ER/A 603078-14 PRI REV-0 HAS BEEN COMPLIED WITH. (2533295)

Part: NONE — NONE (NONE) · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED SLAT 5 ON LH WING. CORRECTIVE ACTION: EXISTING REPAIR INSTALLED PER NWA EA 33-214642 REV-A, APPROVED. AS PER ER/A603078-14 HAS BEEN COMPLIED WITH AND ER/A 603078-14. ( 2533436)

Part: NONE — NONE (NONE) · airframe 83,460 hrs · 10,915 cycles

CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR DOOR LOCATED INTERNAL AREA FR63 TO FR63A IN AFT CARGO COMPARTMENT. REF ER/A 603078-14.

Part: CROSSBEAM — CRACKED (FRM 74) · airframe 83,455 hrs · 10,913 cycles

CRACK CROSSBEAM AT LEVEL STR 26R LOC -YB AT AFT GALLEY. ACCOMPLISHED PERMANENT REPAIR LOC. ON CROSSBEAM OF FR74 AT LEVEL STR26R -YB AT AFT GALLEY AREA AS PER ER/A #603503-14. (2531834)

Part: CROSSBEAM — CRACKED (FRM 74) · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 CRACK CROSSBEAM LOCATED FR74 AT LEVEL STRINGER 26L AND YB AT AFT GALLEY AREA. CORRECTIVE ACTION: COMPLETED WITH ER/A 603503-14 REV. ORIGINAL MATCHES WITH ALL STEPS ON PRI #603503-14 REV.0 AND REV.1 IT IS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTION AT REAR FUSELAGE/FLOOR STRUCTURE AT GALLEY AREA/CROSSBEAM FR74 AT LEVEL STRINGER 26L AND YB AT AFT GALLEY AREA. (2531852)

Part: NOT REPORTED — CRACKED (NOT REPORTED) · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 DURING HCK AND DURING ACCOMPLISHMENT OF EM 5716 -01017, HOLE 260 R/H WAS FOUND CRACKED. A REPAIR WAS ACCOMPLISHE D PER SECT I OF ERA 603575-14AD. CORRECTIVE ACTION: DEFERRED. (2530149)

Part: NOT REPORTED — CRACKED (NOT REPORTED) · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 DURING HCK AND DURING INSPECTION PER EM 5716-01 017, HOLE 263 RH WAS FOUND CRACKED. A REPAIR WAS ACCOMPLISHED PE R SECT II OF ERA 603575-14AD. CORRECTIVE ACTION: DEFERRED. (2530151)

Part: STRINGER — DAMAGED (FRM 53 S5L) · airframe 83,455 hrs · 10,913 cycles

ELONGATED HOLE G4 LOC. AT LEVEL STRGR 5 AND BTW FR53.6 AND FR53.7 LH SIDE UPPER FUSELAGE. ACCOMPLISHED PERMANENT REPAIR ON HOLE G4 LOCATED BTW FR 53.6 TO FR 53.7 AT LEVEL STR 5L AS PER ER/A 603846-14AD MATCHES WITH ALL STEPS ON PRI # 603846-14AD REV. 0 IT IS BEEN VALIDATED. PERFORMED REPAIR INSTRUCCION ON FUSELAGE SKIN CIRCUMFERENTIAL JOINT MOD BETWEEN FR 53.6-FR 53.7 AT STGR 5 LH.

Part: NONE — NONE (NONE) · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR PASSENGER CREW DOOR 4L L OCATED LOWER AFT CORNER IN PASSENGER CABIN. ACCOMPLISHED DETAIL VISUAL INSPECTION ON REPAIR DOUBLER LOC. ON EXTERNAL SKIN AT DOOR AS REQUIRED PER AND ER/A 603078-14 AND NOT FOUND EVIDENCE OF DEGRADATION OR DAMAGE AND GENERAL VISUAL INSPECTION ON EXTERNAL DOUBLER REPAIR ON DOOR 4L AND REPAIR FOUND ON THE AIRCRAFT MATCHES THE DESCRIPTION DETAIL IN THE COMMENTS SECTION OF THIS ITEM. IAW SRM 52-13-00-300-013.

Part: SKIN — DAMAGED (FR 30-31 S26-27L) · airframe 83,455 hrs · 10,913 cycles

DURING AN H CHECK, A DENT AND SCRATCH WAS FOUND AT FR 30 -31, S26-27L. THE DAMAGE WAS REWORKED IAW SECT III OF ERA 580319-14, REV B. FOLLOW ON MAINTENANCE/INSPECTION REF ER/A 580319-14. (2525918)

Part: CROSSBEAM — CRACKED (FRM 74) · airframe 83,455 hrs · 10,913 cycles

DURING AN H-CHECK, FR74 CROSSBEAM WAS CRACKED AT YB AND Y-B. A REPAIR WAS ACCOMPLISHED PER SECT I OF ERA 603503-1 4.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,533 hrs · 11,167 cycles

SUPPLEMENTAL INFORMATION SHIP 3305 DURING HCK AND DURING ACCOMPLISHMENT OF EM 5310 -01461-01, AN OVERSIZED HOLE WAS FOUND AT FR 53.6, STR 5L. A REPAIR WAS ACCOMPLISHED PER SECT I OF ERA 603846-14AD. CORRECTIVE ACTION: ER/A 603846-14 REV A CANCELS THIS LOG PAGE. ALL FOLLOW-ON WORK IS ON LOG PAGE 2774517. OK TO CANCEL THIS LOG PAGE. (2525897)

Part: NONE — NONE (NONE) · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 IN PREPARATION FOR ACCOMPLISHMENT OF 5310-01461-01, IT WAS IDENTIFIED THAT THE CAPITAL TOOL KIT CALLED OUT IN THE WORK INSTRUCTIONS, P/N FTIA330533273-1, FOR COLD WORKING DOES NOT ALIGN WITH THE DAL ATICTS TOOLING P/N. THE CAPITAL KIT CONTAINS STANDARD TOOLING THAT IS REUSABLE AND OWNED BY DAL / READILY AVAILABLE TO BE PULLED VIA ATICTS FOR DAL MTC. VA 99359MA ADDRESSES THIS DIFFERENCE IN WHAT S OBTAINABLE VIA ATICTS VS. WHAT IS CALLED OUT IN THE SECTION 01 WORK CARD BY SPECIFICALLY CALLING OUT USE OF DAL P/N S LB-20 (PULLER) AND FT-20 (POWER PACK) IN ADDITION TO THE OVERALL KIT PART NUMBER THESE PULLER AND POWER PACK PART NUMBERS MAKE UP THE NECESSARY PIECES OF CAPITAL KIT, P/N FTIA330533273-1, FOR ACCOMPLISHMENT OF 5310-01461-01. CORRECTIVE ACTION: ACCOMPLISHED VA NUMBER 99359MA. (2509082)

Part: FLOOR SUPPORT — CORRODED (FRMS 75-80) · corrosion level 2 · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 CORROSION FLOOR BEAM -Y450 LOCATED FR75A TO FR80 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y450 LOCATED BTW FR75 TO FR80 IN AFT GALLEY AREA AS PER SRM A330 51-42-11, A330 SRM 51-72-11 AND DWGF53478040 RII INSPECTION COMPLETE. (2506939)

Part: FLOOR SUPPORT — CORRODED (FRMS 75-78) · corrosion level 2 · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 CORROSION FLOOR BEAM LOCATED FR75 TO FR78 BTW -Y450 TO Y0 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM LOC FR75 TO FR78 BTW -Y450 TO Y0 AT AFT GALLEY AREA AS PER A330 SRM 51-42-11-801 AND A330 SRM51-72-11-911-001 AND DWG F53478040. (2506561)

Part: FLOOR SUPPORT — CORRODED (FRMS 75-80) · corrosion level 2 · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 CORROSION FLOOR BEAM LOCATED Y0 TO Y450 BTW FR75 TO FR78 AT AFT GALLE Y AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM(Y381.0) LOC. BTW Y0 TO Y450 AND BTW FR75 TO FR78 AT AFT GALLEY AREA ASPER SRM A330 51-42-11-801, SRM A33051-72-11-911 AND DRAWING F53478040. (2506539)

Part: FLOOR SUPPORT — CORRODED (FRMS 37) · corrosion level 2 · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 CORROSION FLOOR +Y2462 LOCATED FR 37 TO FR 37.4 PLUS 10 INCHES IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM Y2462 LOC. BTW FR37 TO FR37.4 IN PASSENGER CABIN AS PER SRM A330 51-42-11-801, SRM A330 51-72-11-911 AND DRAWING F53278800. (2506500)

Part: FLOOR SUPPORT — CORRODED (FRSM 33-37) · corrosion level 2 · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 CORROSION FLOOR BEAM +Y953 LOCATED FR33 TO FR37.1 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM Y953 LOC. BTW FR33 TO FR37.1 IN PASSENGER CABIN AS PER SRM A330 51-42-11-801, SRM A330 51-72-11-911 AND DRAWING F53276401. (2506573)

Part: FLOOR SUPPORT — CORRODED (FRMS 71-74) · corrosion level 2 · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 CORROSION FLOOR BEAM -Y450 LOCATED FR71 TO FR74 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y450 LOCATED ON BTW FR71 TO FR74 ON PASSENGER CABIN AT AFT GALLEY AREA AS PER A330 SRM 51-72-11-911 AND DWGF53478650, DWG F53478040. (2506579)

Part: FLOOR SUPPORT — CORRODED (FRMS 78-79) · corrosion level 2 · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 CORROSION FLOOR BEAM Y0 LOCATED FR78 TO FR79 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM Y0 LOC. BTW FR78 TO FR79 AT AFT GALLEY AREA ASPER SRM A330 51-42-11-801, SRM A330 51-72-11-911 AND DWGF53478040. (2506550)

Part: FLOOR SUPPORT — CORRODED (FRMS 35-36) · corrosion level 2 · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 CORROSION FLOOR BEAM LOCATED Y1456 FR35 TO FR36 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM LOCATED Y1456 FR35 TO FR36 IN PASSENGER CABIN (SSI 532134) AS PER A330 SRM 51-42-11-801 AND A330 SRM 51-72-11-911 AND DWG F53276401. (2506568)

Part: NONE — NONE (NONE) · airframe 83,455 hrs · 10,913 cycles

DURING ACCOMPLISHMENT OF THE MODIFICATION REQUIRED PER FAA AD 2019-19-09 AND SB A330-53-3273 REV. 2 VIA WORK CARD 5310-01461- 01, MTC HAS REPORTED AN ERROR REFERENCING AN INCORRECT FIGURE VIEW WITHIN THE WORK STEPS. CORRECTIVE ACTION: ACCOMPLISHED VA NUMBER 99370MA.

Part: NONE — NONE (NONE) · airframe 83,455 hrs · 10,913 cycles

DURING ACCOMPLISHMENT OF THE MODIFICATION REQUIRED PER FAA AD 2019-19-09 AND SB A330-53-3273 REV. 2 VIA WORK CARD 5310-01461- 01, MTC HAS REPORTED THAT WORK COULD BE ACCOMPLISHED MORE EFFICIENTLY IF CERTAIN STEPS THAT ACCOMPLISH THE MODIFICATION OF DIFFERENT AREAS WERE PERFORMED SIMULTANEOUSLY. ACCOMPLISHED VA NUMBER 99369MA.

Part: NONE — NONE (NONE) · airframe 83,455 hrs · 10,913 cycles

SHIP 3305 EM 5716-01017 WAS WRITTEN TO PERFORM THE ACTIONS REQUIRED BY AD 2019-16-07. DURING ACCOMPLISHMENT OF EM -01 AND -02 WORK CARDS, WHICH INCLUDE SB A330-57-3115 (INSP) AND SB A330-57-3131 (MOD) INSTRUCTIONS, CERTAIN STEPS FROM THE MODIFICATION SB WERE FOUND TO HAVE AN IMPROPER N/A SIGN OFF STEP (REFERENCE STEP 32 OF THE WORK CARDS). CORRECTIVE ACTION: ACCOMPLISHED VA NUMBER 99350MA. (2500568)

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 83,455 hrs · 10,913 cycles

AIRCRAFT 3305, CORROSION FLOOR BEAM +Y1959 LOCATED FR 37 TO FR 37.4 PLUS 10 INCHES IN PASSENGER CABIN (SSI 533170-01-2). CORRECTIVE ACTION: REPLACED FLOOR BEAM Y1959 LOC. BTW FR37 TO FR37.4 IN PASSENGER CABIN AS PER SRM A330 51-42-11-801 AND SRM A330 51-72-11-911 AND DWG F53278800, DWG F53279681 AND DWG F53328090. LP2498285

Part: FLOOR SUPPORT — CORRODED (FRMS 33-38) · corrosion level 2 · airframe 83,455 hrs · 10,913 cycles

AIRCRAFT 3305, CORROSION FLOOR BEAM -Y1959 LOCATED FR33 TO FR38 IN PASSENGER CABIN (SSI 532134-01-2). CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y1959 LOC. BTW FR30 TO FR37 IN PASSENGER CABIN AS PER DWG F532 76401, A330 SRM 51-72-11 AND A330 SRM51-42-11. LP 2498292

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 83,455 hrs · 10,913 cycles

AIRCRAFT 3305, CORROSION FLOOR BEAM LOCATED Y1456 FR35 TO FR36 IN PASSENGER CABIN (SSI 532134-01-2). CORRECTIVE ACTION: REPLACED FLOOR BEAM LOCATED Y1456 FR35 TO FR36 IN PASSENGER CABIN (SSI 532134) AS PER A330 SRM 51-42-11-801 AND A330 SRM 51-72-11-911 AND DWG F53276401. LP 2498289

Part: FLOOR SUPPORT — CORRODED (FRM 37) · corrosion level 2 · airframe 83,455 hrs · 10,913 cycles

AIRCRAFT 3305, CORROSION FLOOR STRUCTURE -Y1959 BETWEEN FR37 TO FR37.4 PLUS 10 INCHES IN PASSENGER CABIN (SSI 533170-01-2). CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y1959 LOC BTW FR37.1 TO FR 37.4 IN PASSENGER CABIN AS PER A330 SRM 51-42-11-801 AND A330 SRM 51-72-11-911AND DWG F53328090 AND DWG F53278800. LP 2498275

Part: FLOOR SUPPORT — CORRODED (FRMS 53-54) · corrosion level 2 · airframe 83,455 hrs · 10,913 cycles

AICRAFT 3305, CORROSION FLOOR BEAM -Y1959 LOCATED FR53.5 TO FR54 IN PASSENGER CABIN (SSI 534159-01-2). CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y1959, LOC BTW FR53.2 TO FR54 IN PASSENGER CABIN A330 SRM 51-42-11-801 AND 51-72-11-911 AND DWG F53325686, DWG F53329385 AND F53326941. LP 2494969

Part: FLOOR SUPPORT — CORRODED (FRMS 33-36) · corrosion level 2 · airframe 83,455 hrs · 10,913 cycles

AIRCRAFT 3305, CORROSION FLOOR BEAM +Y450 LOCATED FR33 TO FR36 IN THE PASSENGER CABIN (S SI 532134-01-2). CORRECTIVE ACTION: REPLACED FLOOR BEAM Y450 IN PASSENGER CABIN (SSI 532134-01-2) AS PER A330 SRM 51-42-11-801, A330 SRM 51-72-11-911 AND DWGF53276401. LP 2494976

Part: NONE — NONE · airframe 82,570 hrs · 10,803 cycles

SHIP 3305 WHILE PERFORMING CID1 EPSU SYST TEST, FOUND FAULTS ESCAPE SLIDE LT SW DOOR 3, AND ESCAPE SLIDE DOOR 4L. CORRECTIVE ACTION: FOUND WIRING SWITCH NOT CORRECTLY ENGAGED, ENGAGED SWITCH ON DOOR 3RT AND TEST OK. REMOVED AND REPLACED EPSU. NO HELP, INSTALLED ORIGINAL EPSU. R&R 4L DOOR SLIDE, NO HELP. R&R LH DOOR PSU(17WL) AND BAT , NO HELP, FAIL "EXTERIOR LIGHT". FOUND WIRE 5021 AND 5023 AFTER PLUG 5171VC DAMAGED, REPAIRED BOTH WIRES. (9227581)

Part: NONE — NONE · airframe 82,570 hrs · 10,803 cycles

SUPPLEMENTAL INFORMATION SHIP 3305 SLIDE BTL 3R MSG ON CMS/PFR. CORRECTIVE ACTION: REMOVED AND REPLACED 3R DOOR SLIDE. (9227549)

Part: NONE — NONE · airframe 82,372 hrs · 10,778 cycles

SHIP 3305 EMERGENCY ESCAPE SLIDE WARNING. CORRECTIVE ACTION: COULD NOT DUPLICATE FAULT. OPERATIONAL CHECK OF EMERGENCY ESCAPE-SLIDE RELEASE WARNING SYSTEM PERFORMED AS PER A330 AMM 52-71. TEST OK. (2332765)

Part: IDG — READS HIGH · airframe 82,292 hrs · 10,768 cycles

SHIP 3305 - DIV- TO KEF DUE TO NO. 1 ENGINE IDG TEMPERATURE ABOVE LIMITS. CORRECTIVE ACTION: REPLACED NBR 1 IDG AND NBR 1 GCU. (9304378)

Part: RELAY — INOPERATIVE · airframe 81,797 hrs · 10,706 cycles

SHIP 3305 FOUND DURING SERVICE CHECK, EMER LIGHTS DO NOT ILLUM WHEN PRESSING EMER GEN TEST SWITCH. CORRECTIVE ACTION: T/S. REPLACED RELAY 26XE EMER CONFIG DET. EMERGENCY LIGHTS NOW ILLUM WHEN RE-PERFORMING SERVICE CHECK'S TEST WHEN PRESSING EMER GEN TEST SWITCH. (9259050)

Part: DOOR TRACK — DIRTY · airframe 81,667 hrs · 10,689 cycles

SHIP 3305 4L WONT ARM. CORRECTIVE ACTION: INSPECTED & FOUND DEBRIS IN DOOR TRACK. DEBRIS REMOVED & DOOR OPS CHECK PER A330-300 AMM 52-13. (8786262)

Part: NONE — NONE · corrosion level 2 · airframe 80,425 hrs · 10,519 cycles

SHIP 3305 CORROSION ON BUSHING ECCENTRIC PIN ON LH MAIN LANDING GEAR. CORRECTIVE ACTION: REPAIRED LUG OF ECCENTRIC PIN RIB 6 ON LH MAIN LANDING GEAR AS PER ER/A 597150-14. (2144413)

Part: NONE — NONE · corrosion level 2 · airframe 80,425 hrs · 10,519 cycles

SHIP 3305 RIB 6 FWD LUG WAS FOUND CORRODED AND AFT LUG FOUND ECENTRIC. CORRECTIVE ACTION: REPAIRED L/H MLG RIB 6 AS PER ER/A 597417-14AD. (2144045)

Part: WARNING MESSAGE — FALSE INDICATION (L4 DOOR) · airframe 80,089 hrs · 10,469 cycles

SHIP 3305 4L DOOR SHOWS ARMED ON SYS PAGE WHEN DOOR HAS ACTUALLY BEEN DISARMED. CORRECTIVE ACTION: CYCLED 4L DOOR ARM/DISARM AND VERIFIED SYS OPS CKS GOOD PER A330 AMM 52-71. (8211188)

Part: NONE — NONE · airframe 79,926 hrs · 10,448 cycles

SHIP 3305 2R DOOR BOTTLE INDICATION INOP. CORRECTIVE ACTION: REMOVED AND REPLACED DEU-B 300RH4 IAW A330 AMM 23-73. (8192193)

Part: NONE — NONE · airframe 79,926 hrs · 10,448 cycles

SHIP 3305 2R SLIDE BOTTLE PRESS INDICATION INOP. CORRECTIVE ACTION: REMOVED AND REPLACED DEU-B 300RH4 IAW A330 AMM 23-73. (8192192)

Part: NONE — NONE · airframe 79,460 hrs · 10,378 cycles

SHIP 3305 LED LIGHT UNIT FAULT STAY ON AFTER SELF TEST ON EPSU 13WL. CORRECTIVE ACTION: REPLACED EPSU 13WL. PERFORMED TEST BITE TEST. EPSU IS GOOD. (2023586)

Part: NONE — NONE · airframe 79,441 hrs · 10,373 cycles

SHIP 3305 TWO DENTS HAVE BEEN FOUND IN THE UPPER SURFACE OF THE FWD SIDE IN THE LH PYLON. DAMAGES HAS BEEN EVALUATED AS PER A330 SRM 54-50-00- 283-008, RESULTING IN AN OUT OF LIMITS SITUATION SINCE D IS LESS THAN 20XT. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR LOCATED BWT RIB 01 TO RIB J08 SECONDARY STRUCTURE UPPER SKIN PANEL ON THE FWD SIDE OF L/H PYLON AS PER ER/A 595384-14. (2020045)

Part: NONE — NONE · airframe 79,441 hrs · 10,373 cycles

SHIP 3305 ELONGATED HOLE ACCESS PANEL 453AR ON LH PYLON. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR INSTRUCTIONS ON HOLE LOCATED ON ACCESS PANEL 453AR INBOARD SIDE OF LH PYLON ON ENGINE#1 AS PER ER/A 595259-14. (2020248)

Part: NONE — NONE · airframe 79,441 hrs · 10,373 cycles

SHIP 3305 ACCESS PANELS 453AL IN THE LH PYLON WERE FOUND WITH ELONGATED HOLES. A330 SRM 54-57-11 DOES NOT PROVIDE ADL NOR REPAIR INSTRUCTIONS FOR THIS SCENARIO. CORRECTIVE ACTION: MAINTENANCE CORRECTIVE ACTION PERFORMED REF ER/A 595259-14. (2020216)

Part: NONE — NONE · airframe 79,441 hrs · 10,373 cycles

SHIP 3305 ELONGATED HOLE ACCESS PANEL 463AL ON RH PYLON 2 EA. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON HOLE ACCESS PANEL 463AL ON RH PYLON 2 EA SECTION I AS PER ER/A 595258-14. (2016047)

Part: NONE — NONE · airframe 79,441 hrs · 10,373 cycles

SHIP 3305 DON'T PASS TEST LOCKING MECHANISM ESCAPE SLIDE ICE PROTECTION 3DH IN FWD AVIONIC COMPARTMENT 1EA. CORRECTIVE ACTION: REPLACED SLIDE FITTING HEATER 7DH. PERFORMED OPERATIONAL TEST OF THE HEATED SLIDE FITTING GOOD. (2016573)

Part: NONE — NONE · airframe 79,441 hrs · 10,373 cycles

SHIP 3305 ELONGATED HOLE ACCESS PANEL 463AR ON RH PYLON. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON HOLE ACCESS PANEL 463AR ON RH PYLON AS PER SECTION I ER/A 595258-14. (2016049)

Part: NONE — NONE · airframe 79,441 hrs · 10,373 cycles

SHIP 3305 MISSING 2EA PASSENGER CREW DOOR SAFETY PIN OF ESCAPE SLIDE AT DOOR 2L AND 4R IN PASSENGER CABIN. CORRECTIVE ACTION: INSTALLED THE SAFETY PIN ON ESCAPE SLIDE RAFT AT DOOR L2 AND R4. (2009561)

Part: NONE — NONE · airframe 79,441 hrs · 10,373 cycles

SHIP 3305 ACCOMPLISH VA 99605MA REV IR IN CONJUNCTION WITH AA 2337-01184. CORRECTIVE ACTION: ACCOMPLISH VA 99605MA REV A IN CONJUNCTION WITH AA 2337-01184. (2004621)

Part: NONE — NONE · airframe 79,283 hrs · 10,349 cycles

SHIP 3305 MULTIPLE LIGHTNING STRIKE DAMAGE #1 LT FWD FAN COWL 6 INCHES AFT OF FWD EDGE. CORRECTIVE ACTION: REPAIRED FAN COWL DAMAGE PER A330 SRM 51-77-12. (1973800)

Part: NONE — NONE · airframe 79,283 hrs · 10,349 cycles

SHIP 3305 FOUND MULTIPLE LIGHTNING STRIKE ON #1 LT THRUST REVERSER. CORRECTIVE ACTION: REPAIRED THRUST REVERSER TRAILING EDGE PER A330 SRM 51-77-12. (1973794)

Part: NONE — NONE · airframe 79,271 hrs · 10,347 cycles

SUPPLEMENTAL INFORMATION SHIP 3305 L3 SLIDE FAILED THE DEPLOYMENT TEST. CORRECTIVE ACTION: WORK CARD 2561-9703 HAS BEEN REVISED AND NO LONGER REQUIRES TO DEFER. (1968075)

Part: NONE — NONE · airframe 79,441 hrs · 10,373 cycles

SHIP 3305 ACCOMPLISH VA 99568MA REV IR IN CONJUNCTION WITH AA 2521-01731. CORRECTIVE ACTION: ACCOMPLISHED VA 99568MA REV IR IN CONJUNCTION WITH AA 2521-01731. (1949681)

Part: NONE — NONE · airframe 79,441 hrs · 10,373 cycles

SHIP 3305 ACCOMPLISH VA 99549MA REV IR IN CONJUNCTION WITH AA 2337-01184. CORRECTIVE ACTION: ACCOMPLISH VA 99549MA REV A. (1948421)

Part: COVER — DETACHED (R4 DOOR SLIDE) · airframe 78,604 hrs · 10,247 cycles

SHIP 3305 SLIDE COVER DOOR 4R CAME OFF. CORRECTIVE ACTION: INSPECTED SLIDE COVER 4R DOOR COVER WAS ALREADY SECURED TO DOOR WHEN INSPECTED DOOR. (8040045)

Part: GUST LOCK — BROKEN (R2 DOOR) · airframe 78,295 hrs · 10,205 cycles

SHIP 3305 GUST LOCK BUTTON DEPRESSED/BROKEN DOOR 2R WILL NOT LOCK AGAINST FUSELAGE. CORRECTIVE ACTION: GUST LOCK CKS GOOD AT LOC 2R. (1882451)

Part: SERVICE PANEL — DAMAGED (POTABLE WATER) · airframe 77,005 hrs · 10,022 cycles

SHIP 3305 DAMAGE OCCURRED TO A/C FUSELAGE APPROX. 6-9 INCHES INBD OF PAOTABLE WATER SVC PANEL. CORRECTIVE ACTION: CUT OUT DAMAGE SKIN AT STA FR70 BETWEEN STR57 AND STR56RT STR 56RT DAMAGED FR70 DURING REPAIR PROCEDURES IAW A330 SRM 53-41. C/W ERA 590986-14. (7448286)

Part: OXYGEN MASK — UNWANTED DEPLOY (CREW REST) · airframe 76,683 hrs · 9,947 cycles

SHIP 3305 O2 MASK IN CREW REST BUNK 5 FALLEN OUT. CORRECTIVE ACTION: O2 MASK STOWED. (1742125)

Part: STATUS MESSAGE — FALSE INDICATION (L4 DOOR ARMING) · airframe 75,805 hrs · 9,804 cycles

AFTER GATE ARRIVAL DOOR 4L WOULD NOT SHOW DISARMED ON S/D OR F/A PANEL. CORRECTIVE ACTION: CYCLED NO 4L DOOR ARMED AND DIS-ARMED SLIDE, PER A330 AMM 25-62. OPERATIONS CHECK NORMAL NO FAULT NOTED.

Part: SKIN — DAMAGED (RT NR 1 SLAT) · airframe 83,455 hrs · 10,913 cycles

FOUND A DENT AND GOUGE ON RT WING NR 1 SLAT INBD OF NR 3 TRACK. DENT MEASURES APPROX 3/4" IN DIA AND 1/16 DEEP. GOUGE IS 3 3/4 " IN LENGTH AND APPROX 1/32" DEEP. A PERMANENT REPAIR ON SLAT 1 RH WING IAW SRM 57-40-00-300-008, REPAIR ZONE 2. THIS REPAIR IS CONSIDERED AS CAT A AND FUTHER INSPECTION NOT IS REQUIRED.

Part: CONNECTOR — DETACHED (EMERGENCY LIGHTS) · airframe 75,200 hrs · 9,713 cycles

12JH ISEAT EMERGENCY ESCAPE PATH LIGHT INOP. CORRECTIVE ACTION: CONNECTOR AT SIDEWALL UNHOOKED. RECONNECTED 12JH. CKS GOOD.

Part: PROBE — MALFUNCTIONED (P2) · airframe 74,877 hrs · 9,671 cycles

ATB - RIGHT ENGINE HAD MEL 73-25-01B (LP 9793990) APPLIED FOR EPR CONTROL MODE AND AUTO THRUST FUNCTION. AFTER CLIMB OUT FLIGHT CREW WAS UNABLE TO MEET/COMPLY WITH MEL "O" PROCEDURES AND ELECTED TO RETURN TO AMS. P2/T2 PROBE REPLACED.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 73,402 hrs · 9,475 cycles

DURING C CHECK, FLOOR SUPPORT JUST AFT OF SEAT TRACK OF GALLEY G4 LEFT OF CENTER AT Y450 FOUND CORRODED. REPAIRED BEAM PER ER/A 582791-14. LP 1352536

Part: SEAT TRACK — CORRODED (FRAME 36) · airframe 73,402 hrs · 9,475 cycles

DURING C CHECK, SEAT TRACK AT GALLEY G2, FR 36, -Y1959 WAS FOUND CORRODED. REPAIRED SEAT TRACK PER ER/A 582777-14. LP 1350971

Part: PLATE — CORRODED (R4 DOOR SILL) · corrosion level 2 · airframe 73,402 hrs · 9,475 cycles

DURING C CHECK, DOOR 4R DOOR SILL PLATE FORWARD INBOARD CORNER FOUND CORRODED. REPLACED DOOR SILL PLATE PER SRM 53-42-17. LP 1350283

Part: SEAT TRACK — CORRODED (FRAME 73) · corrosion level 2 · airframe 73,402 hrs · 9,475 cycles

DURING C CHECK, SEAT TRACK AT FR 73, -YC FOUND CORRODED. REPLACED SEAT TRACK PER AIRBUS DRAWING FR 53478007. LP 1349660

Part: PLATE — CORRODED (L4 DOOR SILL) · corrosion level 2 · airframe 73,402 hrs · 9,475 cycles

DURING C CHECK, DOOR 4L DOOR SILL PLATE FOUND CORRODED. REPLACED DOOR SILL PLATE PER SRM 53-42-17. LP 1348921

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 73,402 hrs · 9,475 cycles

DURING C CHECK, DOOR 4L FLOORBOARD SUPPORT FULL LENGTH OF DOOR OPENING FOUND CORRODED. REPLACED FLOOR SUPPORT ASSEMBLY PER SRM 51-72-11. LP 1348357

Part: SUPPORT — CORRODED (L4 DOOR) · corrosion level 2 · airframe 73,402 hrs · 9,475 cycles

DURING C CHECK, DOOR 4L CROSS SUPPORT BETWEEN YA AND TB1 FOUND CORRODED. REPLACED CROSS BEAM ASSEMBLY PER SRM 51-72-11. LP 1348542

Part: FLOOR SUPPORT — CORRODED (FRAME 73) · corrosion level 2 · airframe 73,402 hrs · 9,475 cycles

DURING C CHECK, DOOR 4L CROSS SUPPORT BETWEEN YA, FORWARD OF FR 73 FOUND CORRODED. REPLACED YA FLOOR SUPPORT ASSEMBLY PER SRM 51-72-11. LP 1348362

Part: SEAT TRACK — CORRODED (FRAMES 34-37) · airframe 73,402 hrs · 9,475 cycles

DURING C CHECK, SEAT TRACK AT FR 34-37, -Y450 FOUND CORRODED. REPAIRED SEAT TRACK PER ERA 582777-14. LP 1348739

Part: BUTTON — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,110 hrs · 9,438 cycles

FAP PANEL EMERGENCY LIGHT BUTTON FOUND INOP DURING SERVICE CHECK. REPLACED FAP PANEL. LP 9599072

Part: COVER — MISSING (FLAP TRACK) · airframe 72,619 hrs · 9,380 cycles

DURING WALK AROUND, FOUND ONE COVER MISSING ON FLAP TRACK FIXED FAIRING 631AB. DEFERRED PER CDL 57-00-07 UNTIL COVER IS AVAILABLE TO REPLACED. LP 6091646.

Part: SKIN — DENTED (FRMS 30-31) · airframe 83,460 hrs · 10,915 cycles

MTC REPORTED A DENT COMMON TO THE LT FUSELAGE SKIN, JUST BELOW THE LT WING ILLUMINATION LIGHT BETWEEN FRAMES 30-31, STR 26-27L. THE DENT MEASURED 4 IN LENGTH FWD/AFT, 1.5 IN LENGTH UP/DWN AND 0.062 AT THE DEEPEST POINT. ALTHOUGH THE DENT IS WITHIN SRM ALLOWABLE FOR DEPTH, LENGTH AND PROXIMITY TO NEARBY FASTENERS IT IS INSIDE THE EXCLUDED SECTION IAW SRM 53-21-11-283-006. ACCOMPLISHED PERMANENT REPAIR AND BLENDED AREA IAW ERA 580319-14, PERFORMED DVI INTERNAL AND EXTERNAL SKIN ON REPAIR AREA AND FOUND NO ADDITIONAL DAMAGE.

Part: COVER — MISSING (TE FLAP) · airframe 71,170 hrs · 9,209 cycles

RIGHT WING FLAP TRACK FAIRING NR 5 ACCESS COVER 634CL MISSING. REPLACED ACCESS COVER 634CL. LP 6262250

Part: LENS — MISSING (CABIN) · airframe 68,604 hrs · 8,891 cycles

EMERGENCY EXIT COVER DIFFUSER LENS MISSING AT LOCATION 606. INSTALLED NEW LENS.

Part: LIGHT — BROKEN (CABIN) · airframe 68,339 hrs · 8,858 cycles

WIRE BUNDLE HANGING BELOW SEAT 15B. FOUND EMERGENCY LIGHT ASSEMBLY BROKEN OFF THE SEAT. REPLACED EMERGENCY LIGHT ASSEMBLY.

Part: EPSU — FAILED (CABIN) · airframe 68,102 hrs · 8,828 cycles

DURING EPSU TEST DOOR 4 17WL FAILED. REPLACED 17WL EMERGENCY POWER SUPPLY UNIT.

Part: LENS — UNSECURE (CABIN) · airframe 62,039 hrs · 8,054 cycles

EMERGENCY EXIT LIGHT FELL OFF DURING LANDING AT 3L. SECURED LENS. OK FOR SVC.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 60,948 hrs · 7,919 cycles

DURING A EMERGENCY LIGHTS TEST, A FAULTED 17WC BATTERY WAS FOUND. REPLACED THE BATTERY.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 60,288 hrs · 7,837 cycles

EMERGENCY LIGHT LENS MISSING AT CEILING ABOVE SEAT 7G. REPLACED EMERGENCY LIGHT LENS.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 54,522 hrs · 7,091 cycles

DURING M-CHECK, FOUND THE AFT CARGO DOOR INNER SKIN AT FRAME 23-23A, BEAM 4-5 WORN. CUTOUT DAMAGED AREA AND INSTALLED FILLERS AND DOUBLERS IAW ER/A 53-9577-14.

Part: SKIN — WORN (FRAME 62) · airframe 54,522 hrs · 7,091 cycles

DURING M-CHECK, FOUND AFT CARGO DOOR INNER SKIN AT FRAME 62-62A, BEAM 4-5 WORN. REMOVED DAMAGED AREA AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW ER/A 539576-14.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 54,522 hrs · 7,091 cycles

DURING M-CHECK, FOUND REPAIR DAMAGED ON AFT CARGO DOOR INNER SKIN PANEL AT FRAME 63, BEAM 5. REMOVED DAMAGED AREA AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW ER/A 539574-14.

Part: SEAT TRACK — CORRODED (FRAMES 35-36) · airframe 54,522 hrs · 7,091 cycles

DURING M-CHECK, FOUND SEAT TRACK CORRODED, FRAMES 35-36, -Y2462. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAMES 35-36) · airframe 54,522 hrs · 7,091 cycles

DURING M-CHECK, FOUND SEAT TRACK CORRODED AT CABIN ZONE 240, FR 35-36, -Y1959. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAMES 33-34) · airframe 54,522 hrs · 7,091 cycles

DURING M-CHECK, FOUND SEAT TRACK CORRODED AT FRME 33-34, Y1959. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAMES 15-17) · airframe 54,522 hrs · 7,091 cycles

DURING M-CHECK, FOUND SEAT TRACK CORRODED AT FRAME 15-17, -Y1456. REPLACED SEAT TRACK.

Part: FLOOR SUPPORT — CORRODED (FRAMES 74-75) · airframe 54,522 hrs · 7,091 cycles

DURING M CHECK, FRAMES 74-75, -Y450 FOUND FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FRAMES 73-74) · airframe 54,522 hrs · 7,091 cycles

DURING M-CHECK, FRAMES 73-74 FLOOR SUPPORT FOUND CORRODED. REPLACED THE FLOOR SUPPORT.

Part: SEAT TRACK — CORRODED (FRAMES 73-74) · airframe 54,522 hrs · 7,091 cycles

DURING M-CHECK, FRAMES 73-74, FOUND ADAPTER SEAT TRACK CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK CORRODED Y450, FRAMES 53.8-54. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAMES 38-39) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK CORRODED Y2462, FRAMES 38-39. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK CORRODED -Y450, FRAMES 53-54. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAMES 59-61) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK CORRODED -Y1959 FRAMES 59-61. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAMES 47-75) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK CORRODED -Y14 FRAMES 47.8-75. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAME 53) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK CORRODED -Y2462, FRAME 53-53.1. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAME 37) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK CORRODED -Y1959, FRAME 37.2-37.3. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAME 37) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK CORRODED Y450, FRAME 37.2-37.3. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAMES 36-37) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK CORRODED AT Y1459, FRAMES 36-37. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAMES 68-69) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK, Y450 FOUND CORRODED FRAMES 68-69. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 101. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 53) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK Y1959 FOUND CORRODED FRAME 53.4-53.9. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 50-53) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK Y2462 FOUND CORRODED FRAMES 50 - 53.1. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS SRM 53-31-15, FIG 101. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 57-58) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK Y450 FOUND CORRODED FRAMES 57.3-58. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 38-39) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK -Y1959 FOUND CORRODED AT FRAMES 38 - 39. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-31-15, FIG 101. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 40-42) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK Y2462 FOUND CORRODED FRAMES 40.2-42. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-31-15 FIG 101. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 56-57) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK Y1959 FOUND CORRODED FRAMES 56-57.3. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 35-36) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK Y1959 FOUND CORRODED FRAMES 35-36. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-31-15, FIG 101. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 33) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK Y1456 FOUND CORRODED FRAME 33. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK REMOVED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 74) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK -YB FOUND CORRODED FRAME 74. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 34) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK Y2462 FOUND CORRODED FRAME 34. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00- 15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 73) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK FOUND CORRODED FRAME 73. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-41-14, FIG 103. R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 75) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK Y1447.8 FOUND CORRODED FRAME 75. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-41-14, FIG 103. R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 43-45) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK -Y1959 FOUND CORRODED FRAMES 43-45. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-31-15 FIG101. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 44-46) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK Y450 FOUND CORRODED FRAMES 44-46. CORROSION REMOVED SRM 51-74-00 AND FOUND OUT OF LIMITS SRM 53-31-15, FIG 101. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 36-37) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK Y450 FOUND CORRODED FRAMES 36-37. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 42-46) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK -Y450 FOUND CORRODED FRAME 42-46. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-31-15, FIG 101. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 75-78) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK -Y400 , FOUND CORRODED FRAMES 75-78. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-41-14, FIG 103. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 39) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK Y450 FOUND CORRODED FRAME 39.1-.2. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-31-15, FIG 101, SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 73) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK FOUND CORRODED AT FRAME 73. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-41-14, FIG 103. R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 73) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK FOUND CORRODED AT FRAME 73. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 63-69) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK -Y2462 FOUND CORRODED FRAMES 63-69 . CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-31-15, FIG 101. SEAT TRACK R & R IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 73) · airframe 45,958 hrs · 6,017 cycles

FLOOR SUPPORT FOUND CORRODED AT FRAME 73. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-41-14, FIG 103. FLOOR SUPPORT R & R AS IAW SRM 51-42-11.

Part: INTERCOSTAL — CORRODED (FRAME 73) · airframe 45,958 hrs · 6,017 cycles

INTERCOSTAL FOUND CORRODED AT FRAME 73. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-41-14, FIG 103. R & R IAW SRM 51-42-11.

Part: PROFILE — CORRODED (FRAME 76) · airframe 45,958 hrs · 6,017 cycles

ZEE PROFILE FOUND CORRODED AT FRAME 76. CORROSION REMOVED IAW SRM 51-74- 00. FOUND OUT OF LIMITS IAW SRM 53-41-14. PROFILE REMOVED & REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 70-71) · airframe 45,958 hrs · 6,017 cycles

CORROSION ON SEAT TRACK Y450, FRAMES 70-71. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 33) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK FOUND CORRODED Y1552.5, FRAME 33. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 56-58) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK -Y450 FOUND CORRODED AT FRAMES 56-58. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15. REMOVED & REPLACED SEAT TRACK IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 50-51) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK -Y1959 FOUND CORRODED FRAMES 50-51. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 34-35) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK Y1959 FOUND CORROSION AT FRAMES 34-35. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15. SEAT TRACK REMOVED & REPLACED WITH NEW SEAT TRACK IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 78) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK FOUND CORRODED AT FRAME 78. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-41-14, FIG 103. R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 60-63) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK -Y953 FOUND CORRODED FRAMES 60-63. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK REMOVED IAW SRM 51-42-11. SEAT TRACK REWORKED IAW DWG F53477233, ISSUE A AND INSTALLED IAW SRM 51-42-11.

Part: INTERCOSTAL — CORRODED (FRAME 73) · airframe 45,958 hrs · 6,017 cycles

INTERCOSTAL FOUND CORRODED AT FRAME 73. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-41-14, FIG 103. R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES51-53) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK Y450 FOUND CORROSION AT FRAMES 51-53.1. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMIT IAW SRM 53-31-15, FIG 101. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 64-66) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK -Y450 FOUND CORROSION AT FRAMES 64 - 66. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG101. REMOVED & REPLACED SEAT TRACK IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 74) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK FOUND CORRODED AT FRAME 74. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. R & R SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 55-57) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK Y2642 FOUND CORRODED AT FRAMES 55-57.2. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 74) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK FOUND CORRODED AT FRAME 74. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 64-69) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK Y1959 FOUND CORRODED FRAMES 64-69. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102 . SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 75-78) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK Y400 FOUND CORRODED FRAMES 75-78. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-41-14, FIG 103. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 60-61) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK Y2462 FOUND CORRODED AT FRAMES 60-61. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53 -00-15, FIG102. SEAT TRACK REMOVED & REPLACED IAW SRM 51-42-11.

Part: INTERCOSTAL — CORRODED (FRAME 73) · airframe 45,958 hrs · 6,017 cycles

CORROSION ON INTERCOSTAL BETWEEN YB AND YC, FRAME 73. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-41-14, FIG 103. INTERCOSTAL R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 75) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK FOUND CORRODED -Y400, FRAME 75. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-41-14, FIG 103 . SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 57) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK -Y1959 FOUND CORRODED AT FRAME 57.3-57.4. CORROSION REMOVED SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 31) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK FOUND CORRODED FRAME 37.1-37.3. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 61-66) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK FOUND CORRODED AT FRAMES 61 - 66. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 48-49) · airframe 45,958 hrs · 6,017 cycles

SEAT TRACK Y1959 FOUND CORRODED FRAMES 48-49. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-31-15, FIG 101. SEAT TRACK REMOVED AND INSTALLED WITH REWORKED NEW SEAT TRACK IAW DWG F533129522, ISSUE C AND SRM 51-42-11.

Part: WIRE — DAMAGED (CABIN) · airframe 33,229 hrs · 4,400 cycles

DURING EMERGENCY LIGHT TEST FOUND SEAT ROW 16J INOP. REPLACED CONNECTOR PIN REPAIRED WIRE AND TESTS OK.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 3,815 hrs · 488 cycles

BATTERY EPSU (13WL) DOOR 2 FAILED SYS CHECK, REPLACED BATTERY AND TESTS OK.

Part: LEVER — DISENGAGED (ASSIST BOTTLE) · airframe 31,907 hrs · 4,228 cycles

DURING INSP & ACCOMPLISHMENT OF AMDS WC NR5220-01026-01D, FOUND PERCUSSION LEVER ON DOOR ASSIST BOTTLE DISARMED POS: 4L ARMED AND SAFETIED PERCUSSION LEVER IAW STEP 9 OF AMDS WC NR5220-01026-01D. REQUIRED INSP COMPLETED.

Part: BATTERY — FAILED (CABIN) · airframe 31,209 hrs · 4,138 cycles

BATTERY EPSU (19WL) LDMCR FAILED SYSTEM CHECK. REPLACED BATTERY AND TESTS OK.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON FLOOR STRUCTURE AT PANEL 271NF AT FR76 & FR78. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 BETWEEN FR53-FR54. REPAIRED IAW SRM 53-31-01.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON PANEL 271KF UNDER FLOOR STRUCTURE AT FR76. REPAIRED IAW SRM 51-42-11.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON FLOOR STRUCTURE AT PANEL 271KF FR75-FR76. REPAIRED IAW 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y1456 FR19-FR21. REPAIRED IAW SRM 53-00-15.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON FLOOR STRUCTURE AT PANEL 272KF FR75-76. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 BETWEEN FR 53-54. REPAIRED IAW SRM 51-42-11 AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y2462 FR 57 TO FR 58. REPAIRED IAW ERA 479251-14.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON FLOOR STRUCTURE AT Y1959 FR 17. REPAIRED IAW ERA 478938-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 BETWEEN FR 37.3 AND FR 37.4. REPAIRED IAW SRM 53-31-15.

Part: FLOORBEAM — CORRODED (BS 950) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON FLOOR STRUCTURE AT Y950 FR 78. REPAIRED IAW SRM 51-42-11.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON FLOOR STRUCTURE AT Y450 FR 75. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 BETWEEN FR 67-68, FR 68-69 AND FR 70-71. REPAIRED IAW SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR 34 AND FR 37. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK Y1959 AT FR 61. REPAIRED IAW 53-00-15.

Part: FLOOR SUPPORT — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON FLOOR STRUCTURE AT Y1456 FR 15-16. REPAIRED IAW ERA 478937-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y1959 FR 65. REPAIRED IAW SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR 37. REPAIRED IAW SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-450 CORRODED BETWEEN FR59 AND 67. REPAIRED IAW SRM 53-00-15, AND REPLACEMENT ON NRC 005-260.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION IN SEAT TRACK AT Y450 FR48-53. REPAIRED IAW ERA 478940-14.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON FLOOR STRUCTURE AT PANEL 272KF. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y2462 FR 56 AND BETWEEN FR 57.4-58. REPAIRED IAW SRM 53-00-15.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON FLOOR STRUCTURE AT PANEL 272 JF. REPAIRED IAW SRM 53-41-14.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON FLOOR STRUCTURE AT PANEL 271MF. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR 48, FR 49-50, FR 51, FR52-53. REPAIRED IAW ERA 478941-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y2462 FR 33. REPAIRED IAW SRM 53-00-15.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON FLOORBEAM AT Y450 FR 73. REPAIRED IAW 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y1959 FR 36 AND FR 37. REPAIRED IAW SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 BETWEEN FR 59-60, FR 62-63, FR 63-64, FR 64-65, FR 66-67. REPAIRED IAW SRM 53-00-15.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON FLOORBEAM AT Y960 FR 16A. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y2462 FR 50. REPAIRED IAW ERA 478947-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y950 FR 17. REPAIRED IAW ERA 478936-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-950 CORRODED BETWEEN FR53 AND 55. REPAIRED IAW SRM 53-00-15, AND SRM 53-31-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK, FOUND SEAT TRACK Y-450 CORRODED BETWEEN FR38 AND 39. REPAIRED IAW SRM 53-31-15, SRM 51-42-11, AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-2462 CORRODED FR37. REPAIRED IAW SRM 53-00-15, AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-2462, BETWEEN FR 62-63, FR 65-66, AND FR71 CORRODED. REPAIRED IAW SRM 53-00-15, AND SA5100-01581-1 REV H.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y1456 BETWEEN FR 20 AND FR 21. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-450 CORRODED BETWEEN FR40 AND FR47. REPAIRED IAW SRM 53-31-15, SRM 51-42-11, AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK, FOUND SEAT TRACK Y-2462 CORRODED BETWEEN 63 AND 64, AND AT 65. REPAIRED IAW SRM 53-00-15, AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK, FOUND SEAT TRACK Y-2462, CORRODED AT FR59, AND BETWEEN FR 60-62. REPAIRED IAW SA5100-01581-1, SRM 53-00-15, SRM 51-42-11, AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y1959 FR 35. REPAIRED IAW SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-1959 CORRODED BETWEEN FR 62-63, FR 66-67, FR 68, AND FR 71. REPAIRED IAW SRM 53-00-15, AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK, FOUND SEAT TRACK Y-1959 CORRODED BETWEEN FR 32-34. REPAIRED IAW SRM 53-00-14, AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-450 CORRODED AT FR 69, AND BETWEEN FR 70-71. REPAIRED IAW SRM 53-00-15, AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FROM FR 55 TO FR 57. REPAIRED IAW SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-2462 CORRODED AT FR57. REPAIRED IAW SRM 53-00-15, AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR 40. REPAIRED PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-450 CORRODED BETWEEN FR72 AND 73. REPAIRED IAW SRM 53-31-15, AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-2462 CORRODED AT FR40, FR42, AND FR44. REPAIRED IAW SRM 53-31-15, AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,370 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-450 CORRODED AT FR 69 AND BETWEEN FR 70 AND 71. REPAIRED IAW SRM 53-00-15, AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-1456 CORRODED BETWEEN 21 AND 22. REPAIRED IAW SRM 53-00-15, AND REPLACEMENT ON NRC 160-230.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-1959 CORRODED AT FR59. REPAIRED IAW SRM 53-00-15, AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 BETWEEN FR 39 TO FR 39.2. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-450, BETWEEN FR73 AND 75 WAS CORRODED. REPAIRED IAW SRM 53-00-15, SRM 51-42-11, AND SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 BETWEEN FR 37.1 AND FR 37.2. REPAIRED PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y2462 FR 51-FR 53. REPAIRED IAW SRM 53-31-15 FIG 101.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND SEAT TRACK Y450 CORRODED AT FR54. REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND SEAT TRACK Y450 CORRODED AT FR58 AND FR59. REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,112 hrs · 3,730 cycles

DURING "H" CHECK FOUND SEAT TRACK Y450 CORRODED AT FR42, AND FR45. REPLACED IAW SRM 51-42-11.

Part: BATTERY — DISCHARGED (CABIN)

BATTERY EPSU (15WL) MESSAGE DURING TEST, REPLACED BATTERY AND TESTS, OK. (K)

Part: BATTERY — DISCHARGED (CABIN)

BATTERY EPSU (14WL) MESSAGE DURING TEST, REPLACED BATTERY AND TESTS, OK. (K)

Part: BATTERY — FAULTY (CABIN) · airframe 22,212 hrs · 2,947 cycles

PERFORMING EMERGENCY LIGHTS OPERATION CHECK, EPSU 12WL & 15 WL FAULTS BATTERY. REPLACED BATTERY OF EPSU 12WL & 15WL, TESTS OK (L/P 2908998, 2909005). (S)

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 21,633 hrs · 2,872 cycles

EPSU FAULT (17WC), REPLACED POWER SUPPLY (17WC) AND CHECKS GOOD. (A)

Part: VIDEO MONITOR — CONTAMINATED (CABIN) · airframe 13,723 hrs · 1,808 cycles

VIDEO MONITOR 24B STARTED EMITTING WHITE SMOKE. MONITOR WORKS OK AND NO EVIDENCE OF ELECTRICAL HEAT DAMAGE WAS FOUND. FOUND A MELTED CHOCOLATE AT THE BOTTOM AND BEHIND THE MONITOR. REMOVED AND REPLACED THE MONITOR AS A PRECAUTION AND CHECKS OK. Â