N319US

Part: PROXIMITY SWITCH — OUT OF RIG (ZONE 800) · airframe 94,433 hrs · 44,184 cycles

- ATO - AT 45KTS DUE TO FWD CARGO DOOR OPEN INDICATION. DEFERRED FWD CARGO INDICATION TO MEL AND CONTINUED. (LP: 6571856)

Part: BOTTLE — LOW PRESSURE (1R DOOR) · airframe 94,373 hrs · 44,155 cycles

SHIP 3219 DISC: 1R DOOR ASSIST BOTTLE FOUND LOW. C/A: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 022-0001:0514-2000/010 00065 REFILLED DOOR ASSIST BOTTLE REF. A320 AMM 52-10-00. (LLP: 0685108)

Part: BOTTLE — LOW PRESSURE (1L DOOR) · airframe 94,373 hrs · 44,155 cycles

SHIP 219 DISC: 1L DOOR ASSIST BOTTLE FOUND LOW. C/A: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 022-0001:0514-2000/012 00067 REFILLED DOOR ASSIST BOTTLE REF. A320 AMM 52-10-00. (LP: 0685106)

Part: BOTTLE — LOW PRESSURE (2R DOOR) · airframe 94,373 hrs · 44,155 cycles

SHIP 3219 DISC: 2R DOOR ASSIST BOTTLE FOUND LOW. C/A: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 022-0001:0514-2000/011 00066 REFILLED DOOR ASSIST BOTTLE REF. A320 AMM 52-10-00. (LP: 0685107)

Part: BOTTLE — LOW PRESSURE (2L DOOR) · airframe 94,373 hrs · 44,155 cycles

SHIP 3219 DISC: 2L DOOR ASSIST BOTTLE FOUND LOW. C/A: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 022-0001:0514-2000/013 00068 REFILLED DOOR ASSIST BOTTLE REF. A320 AMM 52-10-00. (LP: 0685103)

Part: A/C PACK — INOPERATIVE · airframe 93,473 hrs · 43,680 cycles

SHUP 3219 DISC: SINGLE PACK WAS UNABLE TO KEEP THE CABIN COOL. FA AND PASSENGERS COMPLAINED. 1 PASSENGER GOT SICK. C/A: REF LOG PAGE #6091206 FOR CORRECTION OF RT PACK. (LP: 6191210)

Part: SKIN — CORRODED (NOSE) · airframe 93,010 hrs · 43,396 cycles

SHIP 3219 DISC: ER/A 607913-14 HAS BEEN REVISED TO 'B'. FOLLOW ON ACTION IS REQU IRED. C/A: NOSE FWD FUSELAGE/ LOWER CENTER SKIN PANEL AND REINFORCEMENT /CORRODED. PERFORM SECTION II EVERY 16000FC AFTER SECTION I. ASSOCIATED ER/A 14-607913 ADDED FOR AC 3219. (LP: 0364760)

Part: PANEL — CORRODED (NLG WW) · airframe 92,888 hrs · 43,328 cycles

SHIP 3219 DISC: DURING CCK AND WHILE INSPECTING PER 522877-14,REV E (LP 1869716) CORROSION WAS FOUND AT SEVERAL LOCATIONS ON THE RHS NLG LATERAL PANEL (P/N D53113475202). PANEL REPLACEMENT REQUIRED. AT REV A DTE IS COMPLETE FOR THE SECTION I REPAIR. C/A: PER SECTION II OF 607700-14, REV A, ACCOMPLISH SECITON II INITIAL INSPECTION WITHIN 63,068 FC TOTAL FROM A/C FIRST FLIGHT. OR WITHIN 19,747 FC FROM 14MAY24. REPEAT SECTION II INSPECTION WITHIN EVERY 7,045 FC AFTER INITIAL INSPECTION. ASSOCIATED ER/A 32-607700 ADDED FOR AC 3219. (LP: 0342451)

Part: SKIN — CORRODED (FUSELAGE) · airframe 92,926 hrs · 43,347 cycles

SHIP 3219 DISC: DURING CCK AND WHILE INSPECTING PER ER/A 522877-14,REV E CORROSION FOUND ON SEVERAL LOCATIONS OF RHS NLG LATERL PANEL AND LWR CENTER SKIN PANEL AND REINFORCEMENT.PANEL REPLACEMENT NEEDED AT REV A DTE IS COMPLETED,ICA'S INCORPORATE. 197334 S PER SECTION II OF 607090-14, REV A ACCOMPLISH SECTION II INITIAL INSPECTION WITHIN 63,068 FC TOTAL FROM A/C FIRST FLIGHT, OR WITH IN 19,747 FC FROM 14MAY24. REPEAT SECTION II INSPECTION WITHIN EVERY 7,045 FC AFTER INITIAL INSPECTION. ASSOCIATED ER/A 32-607090 ADDED FOR AC 3219. (LP: 0342585)

Part: BULKHEAD — CORRODED (FRM 20) · airframe 92,888 hrs · 43,328 cycles

SHIP 3219 DISC: DURING CCK AND WHILE ACCOMPLISHING REPETITIVE INSPECTIONS PER ER /A 522877-14, REV E, CORROSION WAS FOUND ON THE LWR EDGE OF FR20 BULKHEAD BETWEEN LWR STRGR AND Y=520, RHS. AT REV A, FINAL DTE COMPLETE. C/A: PER SECTION II OF 608253-14,REV A, ACCOMPLISH SECTION II INITIAL INSPECTION WITHIN 45,601 FC - TOTAL FROM A/C FIRST FLIGHT, OR WITHIN 2,282 FC FROM 14MAY24. REPEAT SECITON II INSPECITON WITH IN EVERY 3,670 FC AFTER INITIAL INSPECTION. (LP: 0342084)

Part: HOUSING — BROKEN (EMERGENCY LIGHT) · airframe 92,087 hrs · 42,894 cycles

SHIP 3219 DISC: DURING WAKE-UP EMERGENCY LGT @ 23D HOUSING BROKEN. C/A: RPLCD P/N 1013436-015KA06. (LP: 5007668)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,772 hrs · 42,731 cycles

SHIP 3219 DISC: AFTER STARTING ENGINE #2, FLIGHT DECK HAD DIRTY SOCK SMELL. CAPT WAS LIGHT HEADED, FO GOT A HEADACHE RAN PARTIAL SMOKE/FUMES CHECK. DONNED OXYGEN MASKS AND FELT BETTER. RETURNED TO GATE. FLIGHT ATTENDANTS AND PASSENGERS SMELLED ODOR AS WELL. SOME COMPLAINED OF DIZZINESS. C/A: AFTER STARTING ENGINE #2, FLIGHT DECK HAD DIRTY SOCK SMELL. CAPT WAS LIGHT HEADED, FO GOT A HEADACHE RAN PARTIAL SMOKE/FUMES CHECK. DONNED OXYGEN MASKS AND FELT BETTER. RETURNED TO GATE. FLIGHT ATTENDANTS AND PASSENGERS SMELLED ODOR AS WELL. SOME COMPLAINED OF DIZZINESS. (LP: 4337374)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,772 hrs · 42,731 cycles

SHIP 3219 DISC: AFTER T/O IN MSP WE AND FLIGHT ATTENDANTS COULD. SMELL AN ORDER THAT WAS UNUSUAL. AS WE CLIMB IT WENT AWAY ON THE FLT DECK THE FLIGHT ATTENDENTS SAID IT STILL SMELLED DURING CRUISE AND THEY FELT LIGHTHEADED. C/A: FOUND CONTAMINATION IN BOTH PACK BAYS. CLEANED BOTH PACK BAY, L&R OZONE CONV. FILTERS. REPLACED. R/R DAMAGED HYDRAULIC LINE. LEAK CHECK GOOD. FORWARD CARGO DOOAR OPS CHECK GOOD. CLEANED FWD CARGO AFT BULKHEAD. NO FURHTER SMEL C/W RECIRC FILTERS CHANGED. INSTALLED REMOVED BELLY FAIRING. (LP: 4337364)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,769 hrs · 42,729 cycles

SHIP 3219 DISC: APU AUTO-SHUTDOWN AT GATE, FOLLOWED HAZE AND DIRTY SOCK SMELL IN THE CABIN. C/A: PERFORMED GVI OF APU WHILE APU RUNNING FOUND OIL LEAKING @ STARTER V-BAND CLAMP INLET & APU BAY CONTAMINATED WITH OIL J.S. 781335. CLEANED APU BAY AND PLACED APU ON MEL REF LOG 4337353. PERFORMED DUCT BURN OUT AND DECONTIMINATION OF ECS SYSTEM PER W/ C 2100-2005. NO FURTHER DIRTY SOCK SMELL OR FURTHER DEFECTS NOTED. C/W NO GO ODI REF LOG 0094427. A/C OK FOR SVC. R/R DAMAGED HYDRAULIC LINE. LEAK CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,682 hrs · 42,691 cycles

SHIP 3219 - PRES - DUE TO LOSS OF CABIN PRESSURE, EMERGENCY DESCENT FROM 35K TO 10K. CORRECTIVE ACTION: FOUND LEAK COMING FROM THE LH ENGINE BLEED AIR DUCT, R/R SEAL. R/R SKIN AIR OUTLET VENT VALVE. LEAK CHECK PNEUMATIC DUCTING. OK FOR SERVICE. (4426790)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,261 hrs · 41,931 cycles

SHIP 3219 PERFORM DRILL HOLES ON FITTING (2 E/A) AT NLG AREA LATERAL SKIN PANEL RH SIDE P/N D53113475202 AND ER/A 607090-14. CORRECTIVE ACTION: COMPLIED WITH. (2790561)

Part: NONE — NONE (NONE) · airframe 90,261 hrs · 41,931 cycles

SHIP 3219 NEED TO PERFORM ER/A 608253-14 REV. ORIGINAL. CORRECTIVE ACTION: COMPLIED WITH. (2790157)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 90,261 hrs · 41,931 cycles

SHIP 3219 NEED TO ACCOMPLISH ER/A 607913-14 REV. ORIGINAL LOC. ON LOWER CENTER SKIN PANEL BTW FR13 TO FR20 RH SIDE NOSE FWD FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH. (2790107)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,261 hrs · 41,931 cycles

SHIP 3219 NEED TO FABRICATE CROSSBEAM P/N D5311345620200 FR 15 LOC AT LEVEL UPPER SURFACE NLG AND ER/A 607090-14. CORRECTIVE ACTION: FABRICATED. OK FOR SERVICE. (2790616)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 90,261 hrs · 41,931 cycles

SHIP 3219 NEED TO PERFORM ER/A 522877-14 REV F. CORRECTIVE ACTION: COMPLIED WITH. (2790089)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,261 hrs · 41,931 cycles

SHIP 3219 NEED TO ACCOMPLISH ER/A 607090-14 REV. ORIGINAL LOC ON RH-NLG BAY BTW FR9 TO FR20 LATERAL SKIN PANEL. CORRECTIVE ACTION: COMPLIED WITH. (2790035)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,261 hrs · 41,931 cycles

SHIP 3219 NEED TO ACCOMPLISH ER/A 607094-14 REV. ORIGINAL. CORRECTIVE ACTION: COMPLIED WITH. (2790130)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,261 hrs · 41,931 cycles

SHIP 3219 CRACKED CROSSBEAM FR 15 LOC AT LEVEL UPPER SURFACE NLG. CORRECTIVE ACTION: REPLACED PER A320 SRM 51-42-11. OK FOR SERVICE. (2787557)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,261 hrs · 41,931 cycles

SHIP 3219 DETERIORATED PASSENGER CREW DOOR 832 BONDED BUSHINGS UPPER AND LOWER CONNECTION LINK. CORRECTIVE ACTION: REPLACED BUSHINGS. OK FOR SERVICE. (2786506)

Part: NONE — NONE (NONE) · airframe 92,888 hrs · 43,328 cycles

SHIP 3219 DISC: ER/A 607913-14 REV(A) REQUIRES DAMAGE TOLERANCE ANALYSIS. C/A: *DTA TO BE COMPLETED WITH IN 12 MONTHS OF SECTION I* ASSOCIATED ER/A 32-607913 ADDED FOR AC 3219. (LP: 2784815)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,261 hrs · 41,931 cycles

SHIP 3219 CRACK ON LOWER FLANGE FR 19 AT LEVEL STR 40 RH ON NLG AREA. CORRECTIVE ACTION: REPAIRED PER A320 SRM 51-72-11. (2774693)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,261 hrs · 41,931 cycles

SHIP 3219 CORROSION WAS FOUND AT SEVERAL LOCATIONS ON THE RHS NLG LATERAL PANEL AND LWR CENTER SKIN PANEL AND REINFORCEMENT.THE DAMAGE REQIURES PANEL REPLACEMENT. CORRECTIVE ACTION: COMPLIED WITH ERA 522877-14. (2773483)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,261 hrs · 41,931 cycles

SHIP 3219 CORROSION WAS FOUND AT SEVERAL LOCATIONS ON THE RHS NLG LATERAL PANEL (P/N D53113475202). THE CORROSION WAS SEVERE ENOUGH TO REQUIRE PANEL REPLACEMENT. CORRECTIVE ACTION: COMPLIED WITH ERA 607700-32. (2770088)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,261 hrs · 41,931 cycles

SHIP 3219 CORROSION WAS FOUND ON THE LWR EDGE OF FR20 BULKHEAD BETWEEN LWR STRGR AND Y=520, RHS. CORRECTIVE ACTION: COMPLIED WITH ERA 608253-14. (2760920)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,261 hrs · 41,931 cycles

SHIP 3219 DETERIORATED PASSENGER CREW DOOR 831 LOWER ROLLER ON FWD AND AFT POSITION OF THE DOOR. CORRECTIVE ACTION: REPLACED ROLLERS. OK FOR SERVICE. (2759544)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,261 hrs · 41,931 cycles

SHIP 3219 PASSENGER CREW DOOR 831 DAMPER AT FWD GALLEY AREA WEAK. CORRECTIVE ACTION: REPLACED DAMPER. OK FOR SERVICE. (2672815)

Part: NONE — NONE · airframe 90,261 hrs · 41,931 cycles

SHIP 3219 PASSENGER CREW DOOR 831 DAMPER WEAK. CORRECTIVE ACTION: REPLACED DAMPER PER A320 AMM 52-11-14. OK FOR SERVICE. (2663542)

Part: NONE — NONE · airframe 90,261 hrs · 41,931 cycles

SHIP 3219 CREW DOOR 831 INTERLOCK MECHANISM NOT WORKING CORRECTLY. CORRECTIVE ACTION: CLEANED AND LUBRICATED DOOR LOCKING MECHANISM. OK FOR SERVICE. (2644848)

Part: NONE — NONE · airframe 90,261 hrs · 41,931 cycles

SHIP 3219 PASSENGER CREW DOOR 842 LOAD TO RELEASE THE DOOR FROM SUPPORT ARM TEST FAILED. CORRECTIVE ACTION: ADJUSTED DOOR PER A320 AMM 52-12. OK FOR SERVICE. (2638890)

Part: NONE — NONE · airframe 90,261 hrs · 41,931 cycles

SHIP 3219 PASSENGER CREW DOOR 841 DAMPER WEAK. CORRECTIVE ACTION: REPLACED DAMPER. OK FOR SERVICE. (2634789)

Part: NONE — NONE · airframe 90,261 hrs · 41,931 cycles

SHIP 3219 DETERIORATED ROLLERS ON PASSENGER CREW DOOR 832 LOWER FROM FWD AND AFT SIDE OF THE DOOR. CORRECTIVE ACTION: REPLACED ROLLERS. OPS CHECK GOOD. (2633182)

Part: NONE — NONE · airframe 90,261 hrs · 41,931 cycles

SHIP 3219 PASSENGER CREW DOOR 831 OUT OF ADJ/HARD TO OPEN. CORRECTIVE ACTION: RIGGED DOOR PER A320 AMM 52-11-21. OK FOR SERVICE. (2629263)

Part: HINGE — DAMAGED (LT MLG DOOR) · airframe 90,214 hrs · 41,900 cycles

DAMAGE FOUND ON LT MAIN LANDING GEAR DOOR HINGE AND MOUNT FITTING. COMPLIED WITH ERA 605430-14AD REV. O.

Part: ATTACH FITTING — WORN (MLG DOOR) · airframe 90,214 hrs · 41,900 cycles

LOWER LT MLG DOOR ATTACH FITTING ON KEEL BEAM AT FR 43 INNER FLANGES WORN ON INNER FLANGE. COMPLIED WITH ERA 605430-14AD REV. O.

Part: ATTACH FITTING — WORN (MLG DOOR) · airframe 90,214 hrs · 41,900 cycles

LOWER LT MLG DOOR ATTACH FITTING ON KEEL BEAM AT FRAME 43, DAMAGE TO THE FWD FACE OF THE AFT FLANGE. COMPLIED WITH ERA 605430-14AD REV, 0, REV. 1, AND REV 2.

Part: PROXIMITY SWITCH — OUT OF ADJUST · airframe 89,574 hrs · 41,560 cycles

SHIP 3219 -ATO- AT 60KTS DUE TO A FWD CARGO DOOR OPEN MESSAGE. CORRECTIVE ACTION: DEFERRED FWD CARGO DOOR INDICATION SYSTEM PER MEL AND CONTINUED. FWD CARGO DOOR PROXIMITY SWITCH LATER ADJUSTED, AND MEL CLOSED. (9508346)

Part: FRAME — GOUGED · airframe 88,774 hrs · 41,088 cycles

SHIP 3219 FRAME 15 FWD RADIUS GOUGED ADJACENT TO DOOR STOP FITTING NUMBER 3 INTERCOSTAL. CORRECTIVE ACTION: COMPLIED WITH ERA 600572-14 REV B. OK FOR SERVICE. (2322443)

Part: NONE — NONE · airframe 88,701 hrs · 41,040 cycles

SHIP 3219 - ATO - DUE TO A TENDENCY TO PULL RIGHT AFTER THROTTLE UP. CORRECTIVE ACTION: REPLACED PARKING BRAKE ACCUMULATOR AND NORMAL BRAKE SERVO VALVE 16GG. OK FOR SERVICE. (8964650)

Part: NONE — NONE · airframe 88,224 hrs · 40,755 cycles

SHIP 3219 DECLARED EMERGENCY DIRTY SOCK SMELL IN COCKPIT. CORRECTIVE ACTION: REPLACED APU AND BURNED OUT DUCTS. OK FOR SERVICE. (2219652)

Part: ACCESS DOOR — MISSING · airframe 88,128 hrs · 40,686 cycles

SHIP 3219 ON ARRIVAL FOUND RT ENG STARTER VALVE ACCESS DOOR MISSING. CORRECTIVE ACTION: REPLACED DOOR PER A320 AMM 71-13. OK FOR SERVICE. (6183530)

Part: NONE — NONE · airframe 87,642 hrs · 40,404 cycles

SHIP 3219 LEFT HAND MAIN GEAR DOOR ACTUATOR FORWARD LUG SHOWING CRACK. CORRECTIVE ACTION: COMPLIED WITH ERA 597132-14AD REV A. (2121774)

Part: NONE — NONE · airframe 87,642 hrs · 40,404 cycles

SHIP 3219 RT MAIN GEAR DOOR ACTUATOR FORWARD AND AFT LUGS SHOWING CRACK. CORRECTIVE ACTION: COMPLIED WITH ERA 597133-14AD REV. ORIG. (2121482)

Part: NONE — NONE · airframe 87,642 hrs · 40,404 cycles

SHIP 3219 LT WING OB FLAP DENT IN UPPER SURFACE. CORRECTIVE ACTION: REPAIRED PER ERA 597124-14 REV ORIGINAL. OK FOR SERVICE. (2120736)

Part: NONE — NONE · airframe 87,642 hrs · 40,404 cycles

SHIP 3219 FRAME 43 LH CRACKED. CORRECTIVE ACTION: REPLACED FRAME 43 LH ON DELTA WC 5311-01239-02A JOB 47. ASSOCIATED AA 5311-01239. JOB COMPLETE. (2119646)

Part: LIGHT — INOPERATIVE (SEAT 12D) · airframe 86,255 hrs · 39,505 cycles

SHIP 3219 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:SEAT 12D. CORRECTIVE ACTION: SECURED LIGHT ASSY.OK FOR SVC. (1867455)

Part: FRAME — CRACKED (FRM 36) · airframe 85,014 hrs · 38,904 cycles

CRACK INDICATION ON FRAME 36 RT UPPER SURFACE PRESSURE DECK MEMBRANE. 4 INCHES OTBD OF -Y1292. CRACK AT 12 O`CLOCK IN THE FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTION ON THE FRAME IAW ER/A 584069-14AD, REV O, REV 1, REV 2, AND ER/A 584069-14AD, REV O.

Part: FRAME — CRACKED (FRM 36) · airframe 85,014 hrs · 38,904 cycles

CRACK INDICATION ON FRAME 36 LT UPPER SURFACE PRESSURE DECK MEMBRANE, 7.5 INCHES OTBD FROM Y1292, CRACK AT THE 9 O`CLOCK IN FWD CARGO COMPARTMENT, PERFORMED REPAIR INSTRUCTION ON FRAME 36 UPPER SURFACE PRESSURE DECK MEMBRANE IN FWD CARGO COMPARTMENT IAW ER/A 584069-14AD, REV 0, REV 1, REV 2 AND ER/A 584069-14AD, REV ORIGINAL.

Part: FRAME — CRACKED (FRM 36) · airframe 85,014 hrs · 38,904 cycles

CRACK INDICATION ON FRAME 36 RT UPPER SURFACE PRESSURE DECK MEMBRANE. 7.5 INCHES OTBD OF -Y1292, CRACK AT 7 O`CLOCK IN THE FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTION ON THE FRAME IAW ER/A 584069-14AD, REV O, REV 1, REV 2, AND ER/A 584069-14AD, REV O.

Part: FRAME — CRACKED (FRM 36) · airframe 85,014 hrs · 38,904 cycles

CRACK INDICATION ON FRAME 36 LT UPPER SURFACE PRESSURE DECK MEMBRANE, 8.25 INCHES OTBD OF Y1292. CRACK AT 12 O`CLOCK IN THE FWD CARGO COMPARTMENT, PERFORMED REPAIR INSTRUCTIONS ON THE FRAME IAW ER/A 584069-14AD, REV O, REV 1, REV 2, AND ER/A 584069-14AD, REV ORIGINAL.

Part: FRAME — CRACKED (FRM 36) · airframe 85,014 hrs · 38,904 cycles

CRACK INDICATION ON FRAME 36 RT UPPER SURFACE PRESSURE DECK MEMBRANE. 4.75 INCHES OTBD OF -Y1292. CRACK AT 2 O`CLOCK IN FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTION ON THE FRAME IAW ER/A 584069-14AD, REV 0, REV 1, REV 2, AND ER/A 584069-14AD, REV O.

Part: FRAME — CRACKED (FRM 36) · airframe 85,014 hrs · 38,904 cycles

CRACK INDICATION ON FRAME 36 RT UPPER SURFACE PRESSURE DECK MEMBRANE. 3 INCHES OTBD OF -Y1292. CRACK AT 6 O`CLOCK IN THE FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTION ON THE FRAME IAW ER/A 584069-14AD, REV O, REV 1, REV 2, AND ER/A 584069-14AD, REV ORIGINAL.

Part: FRAME — CRACKED (FRM 36) · airframe 85,014 hrs · 38,904 cycles

CRACK INDICATION ON FRAME 36 LT UPPER SURFACE PRESSURE DECK MEMBRANE, 5.75 INCHES OTBD OF Y1292. CRACK AT 12 O`CLOCK IN FWD CARGO COMPARTMENT, PERFORMED REPAIR INSTRUCTIONS ON THE FRAME IAW ER/A 584069-14AD, REV 0, REV 1, REV 2, AND ER/A 584069-14AD, REV ORIGINAL.

Part: FRAME — CRACKED (FRM 36) · airframe 85,014 hrs · 38,904 cycles

CRACK INDICATION ON FRAME 36 RT UPPER SURFACE PRESSURE DECK MEMBRANE, 2 INCHES OTBD OF -Y1292. CRACK AT 12 O`CLOCK IN FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTION ON THE FRAME IAW ER/A 584069-14AD, REV O, REV 1, REV 2, AND ER/A 584069-14AD, REV ORIGINAL.

Part: FRAME — CRACKED (FRM 36) · airframe 85,014 hrs · 38,904 cycles

CRACK INDICATION ON FRAME 36 LT UPPER SURFACE PRESSURE DECK MEMBRANE AT 3 INCHES OTBD FROM Y1292, CRACK AT 4 O`CLOCK IN THE FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTIONS ON THE FRAME IAW ER/A 584069-14AD, REV O, REV 1, REV 2, AND ER/A 584069-14AD, REV ORIGINAL.

Part: FRAME — CRACKED (FRM 36) · airframe 85,014 hrs · 38,904 cycles

CRACK INDICATION ON FRAME 36 RT UPPER SURFACE PRESSURE DECK MEMBRANE. 6.5 INCHES OTBD OF -Y1292. CRACK AT 12 O`CLOCK IN THE FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTIONS ON THE FRAME IAW ER/A 584069-14AD, REV 0, REV 1, REV 2, AND ER/A 584069-14AD, REV ORIGINAL.

Part: FRAME — CRACKED (FRM 36) · airframe 85,014 hrs · 38,904 cycles

CRACK INDICATION ON FRAME 36 LT UPPER SURFACE PRESSURE DECK MEMBRANE, 4 INCHES OTBD OF Y1292, CRACK AT 4 O`CLOCK IN FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTIONS ON THE FRAME IAW ER/A 584069-14AD, REV O, REV 1, REV 2, AND ER/A 584069-14AD, REV ORIGINAL.

Part: FRAME — CRACKED (FRM 36) · airframe 85,014 hrs · 38,904 cycles

CRACK INDICATION ON FRAME 36 LT UPPER SURFACE PRESSURE DECK MEMBRANE, 4.75 INCHES OTBD OF Y1292, CRACK AT 12 O`CLOCK IN THE FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTIONS ON THE FRAME IAW ER/A 584069-14AD, REV O, REV 1, REV 2, AND ER/A 584069-14AD, REV ORIGINAL.

Part: FRAME — CRACKED (FRM 36) · airframe 85,014 hrs · 38,904 cycles

CRACK INDICATION ON FRAME 36 LT UPPER SURFACE PRESSURE DECK MEMBRANE, 6.5 INCHED OTBD OF Y1292, CRACK AT 4 O`CLOCK IN FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTION ON THE FRAME IAW ER/A 584069-14AD, REV O, REV 1, REV 2, AND ER/A 584069-14AD, REV ORIGINAL.

Part: FRAME — CRACKED (FRM 36) · airframe 85,014 hrs · 38,904 cycles

CRACK INDICATION ON FRAME 36 LH UPPER SURFACE PRESSURE DECK MEMBRANE AT 2 INCHES OTBD FROM Y1292. CRACK AT THE 12 O`CLOCK, IN THE FWD CARGO COMPARTMENT, PERFORMED REPAIR INSTRUCTIONS ON FRAME 36 IAW ER/A 584069-14AD, REV 0, REV 1, REV 2, AND ER/A 584069-14AD, REV ORIGINAL.

Part: FRAME — CRACKED · airframe 85,022 hrs · 38,909 cycles

CRACK INDICATION ON FRAME 2 INTERNAL SIDE UPPER BOLT VERTICAL FLANGE O F THE LOWER ATTACHMENT AREA OF THE WINDSHIELD CENTER POST LH SIDE. (L=0.500 INCH APPROX.) IN COCKPIT (1 EA), PERFORMED REPAIR INSTRUCTION ON FRAME 2 INTERNAL SIDE UPPER BOLT VERTICAL FLANGE OF THE LOWER ATTACHMENT AREA OF THE WINDSHIELD CENTER POST LH SIDE IN COCKPIT 1EA AS PER ERA 583911-14 REV 0 REV 1, REV 2, AND ERA 583911-14AD REV ORIGINAL

Part: FRAME — CRACKED (FRM 3) · airframe 85,014 hrs · 38,904 cycles

CRACK FRAME 3 RACK 10VU CENTER LUG IN COCKPIT WORK CARD 2511-01146-01, AD 2019-07-05, REPAIRED IN ACCORDANCE WITH AD 2019-07-05 AND AIRBUS SB A320-92-1087 REV.3 CRACK LENGTH 0.532

Part: SKIN — GOUGED (FRAME 21) · airframe 85,014 hrs · 38,904 cycles

GOUGE EXTERNAL SKIN LOC. FR 21+19 INCH BTW STR 41R TO STR42R AT LOWER FUSELAGE, PERFORMED REPAIR INSTRUCTION ON GOUGE EXTERNAL SKIN LOC. FR 21 + 19 INCH BTW STR 41R TO STR 42R AT LOWER FUSELAGE AS PER ER/A 584200-14, REV. ORIGINAL AND PRI 584200-14, REV.0

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 85,014 hrs · 38,904 cycles

CRACK INDICATION ON INTERCOSTAL FITTING IN UPPER INBOARD HOLE AT LEVEL DOOR STOP 7 FRAME 16 RH AT FWD GALLEY AREA (1 EA), REPLACED OLD INTERCOSTAL FITTING AND FASTENER ON UPPER LB HOLES AT LEVEL DOOR STOP #7 FR.16 RH FWD GALLEY AREA ASPER A320 SRM 51-42-11 AND 51-72-11 AND DWG D53114223

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 85,014 hrs · 38,904 cycles

CRACK INDICATION ON FRAME 66 OPEN FASTENER HOLE 4 ON DOOR STOP 2 AFT GALLEY AREA (1 EA) LH SIDE, REPAIRED OPEN HOLE 4 ON FRAME 66 DOOR STOP 2 LH SIDE ASPER A320 SRM 53-41-12-300-010

Part: STRAP — CORRODED (FUSELAGE) · airframe 85,014 hrs · 38,904 cycles

CORROSION LOWER CUTOUT STRAP BELOW THRESHOLD SHEET IN FWD CARGO COMPARTMENT, REPLACED LOWER CUT OUT STRAP BELOW THRESHOLD SHEET IN FWD CARGO COMPARTMENT ASPER SRM A320 51-72-11 AND DWG E53470500

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,014 hrs · 38,904 cycles

CORROSION LOWER SILL FR 68 AND AT LEVEL STR 23L AT AFT GALLEY AREA, REPLACED LOWER SILL LOC FR66 TO FR 68 AND AT LEVEL STR 23L AT AFT GALLEY AREA ASPER A320 SRM 51-72-11 AND DWG # D53480020

Part: SEAT TRACK — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 85,014 hrs · 38,904 cycles

SEAT TRACK -Y1292 PREVIOUSLY REWORKED AREA AND EVALUATED WITH CARD 2500-2031-DE WAS FOUND OUT LIMITS, REPLACED SEAT TRACK -Y1292 LOC. BTW FR36 TO FR41 IN PASSENGER CABIN AS PER A320 SRM 51-72-11 AND DWG D53371000

Part: SEAT TRACK — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 85,014 hrs · 38,904 cycles

SEAT TRACK -Y1292 PREVIOUSLY REWORKED AREA AND EVALUATED WITH CARD 2500-2031-DE WAS FOUND OUT LIMITS, REPLACED SEAT TRACK -Y1292 LOC FR41 TO FR47 IN PASSENGER CABIN AS PER A320 SRM 51-72-11 AND DWG D53371000

Part: DAMPER — FAILED (PAX DOOR) · airframe 85,014 hrs · 38,904 cycles

DONT PASS OPERATIONAL TEST PASSENGER CREW DOOR 841 DOOR DAMPER AT FWD GALLEY AREA, REPLACED PASSENGER CREW DOOR 841 DOOR DAMPER AT FWD GALLEY AREA.

Part: FITTING — CORRODED · corrosion level 2 · airframe 85,014 hrs · 38,904 cycles

CORROSION ON THE CENTER FITTING OF THE LOWER SILL AFT ENTRY DOOR AT LEVEL STRINGER 23L IN THE AFT GALLEY AREA , REPLACED THE CENTER FITTING IAW SRM 51-72-11, AND DWG D53480048.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 85,014 hrs · 38,904 cycles

CORRODED FLOOR SUPPORT -Y1292 BETWEEN FRAMES 12 - 24 IN THE FWD GALLEY AREA, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112812.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · corrosion level 2 · airframe 85,014 hrs · 38,904 cycles

CORRODED FLOOR SUPPORT, +Y1162.5 BETWEEN FRAMES 68 AND 69 IN THE AFT GALLEY AREA, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53472800.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 85,014 hrs · 38,904 cycles

CORRODED FLOOR SUPPORT, -Y1227 BETWEEN FRAMES 66 AND 68 IN THE AFT GALLEY AREA, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DWG D53472800, AND D53472000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · corrosion level 2 · airframe 85,014 hrs · 38,904 cycles

CORRODED FLOOR SUPPORT, -Y1162.5 BETWEEN FRAMES 68 AND 69 IN THE AFT GALLEY AREA, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DWG D53472089, AND D53472089.

Part: DAMPER — FAILED (PAX DOOR) · airframe 85,014 hrs · 38,904 cycles

DONT PASS OPERATIONAL TEST DAMPER PASSENGER CREW DOOR 842 AT AFT GALLEY AREA, REPLACED PASSENGER CREW DOOR 842 AT AFT GALLEY AREA.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 85,014 hrs · 38,904 cycles

CORROSION FLOOR BEAM -Y765 LOCATED BTW FR 12 TO FR 24 AT FWD GALLEY AREA, REPLACED FLOOR BEAM -Y765 LOCATED BTW FR 12 TO FR 24 AT FWD GALLEY AREA AS PER A320 SRM 51-42-11 AND DWG D53918123 AND SRM A320 51-72-11

Part: SUPPORT — CORRODED (FRAMES 69-70) · corrosion level 2 · airframe 85,014 hrs · 38,904 cycles

CORROSION FRAME SUPPORT LOCATED AT LEVEL STR 23R BETWEEN FRAMES 69 AND 70 IN THE AFT GALLEY AREA, REPLACED THE FRAME SUPPORT IAW SRM 51-72-11, AND DWG D53470100.

Part: SUPPORT FRAME — CRACKED (FRAME 68) · airframe 85,014 hrs · 38,904 cycles

CRACKED SUPPORT FRAME, FRAME 68 UNDER STRINGER 23L IN THE AFT GALLEY AREA, REPLACED SUPPORT FRAME IAW SRM 51-72-11, AND DWG D53470150.

Part: DUMMY RAIL — CORRODED (FRAMES 12-21) · corrosion level 2 · airframe 85,014 hrs · 38,904 cycles

CORROSION RAIL DUMMY Y503.2 LOCATED BTW FR 12 TO FR 21 AT FWD GALLEY AREA, REPLACED RAIL DUMMY Y503.2 LOC. BTW FR 12 TO FR 21 AT FWD GALLEY AREA AS PER A320 SRM 51-42-11 AND SRM 51-72-11 AND DWG #D53112825 AND DWG #D53110984

Part: FITTING — CRACKED · airframe 85,014 hrs · 38,904 cycles

CRACK INDICATION ON INTERCOSTAL FITTING ON UPPER AND LOWER INBOARD HOLES AT LEVEL DOOR STOP 7 LT, FRAME 16 AT FWD GALLEY AREA (2EA), REPLACED INTERCOSTAL FITTING ON UPPER AND LOWER INBOARD HOLES AT LEVEL DOOR STOP 7 LT FRAME 16 AT FWD GALLEY AREA AS PER A320 SRM 51-72-11 DWG D53114223

Part: WEB — CRACKED (MLG WW) · airframe 80,284 hrs · 36,619 cycles

CRACK INDICATION ON WEB AT OPEN FASTENER HOLE COMMON TO AFT RT TEE ANGLE, IN THE MAIN WHEEL WELL, PERFORMED A PERMANENT REPAIR IAW PRI 567031-14, REVISION 0, AND ER/A 567031-14AD, REVISION ORIGINAL.

Part: SKIN — SCRATCHED (FRAME 29) · airframe 84,653 hrs · 38,716 cycles

SCRATCH ON EXTERNAL SKIN FR 29 BTW STR 27L TO STR 28L ON LOWER FUSELGE, PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN FR 29BTW STR 27L TO STR28L ON LOWER FUSELAGE AS PER SRM A320 53-00-11 REPAIR INSTRUCTION 1(A) TO (U) FIG 20140, MEASURES OF CUT OUT IS L:5.645" W=2.624"

Part: SKIN — CORRODED (FRAMES 69-70) · airframe 74,754 hrs · 33,917 cycles

CORROSION FOUND ON AFT FUSELAGE SKIN AND INTERNAL DOUBLER BETWEEN STR 31R-STR 32R AND FRAME 69 - FRAME 70. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN AT LOWER FUSELAGE FROM FRAME 69 TO FRAME 70 BETWEEN STR 31R TO STR 32R IAW PRI 544954-14, REV 0, 1, 2.

Part: STOP FITTING — CRACKED (FRAME 68) · airframe 74,747 hrs · 33,915 cycles

CRACK INDICATION ON FRAME 68 COMMON TO STOP DOOR FITTING AT STR 22R LOWER INBD HOLE AT AFT GALLEY AREA . PERFORMED PERMANENT REPAIR ON FRAME 68 AT STR 22 LOWER INBD HOLE IAW SRM 53-41-12, PARA 5E, PAGE 220.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 74,164 hrs · 33,647 cycles

SEAT 1B FWD EMEGENCY LIGHT, WHITE, INOPERATIVE. REPLACED PIG TAIL AT SEAT 1B.

Part: STRINGER — CORRODED (FRAMES 55-58) · airframe 73,976 hrs · 33,557 cycles

CORROSION ON STR 43L BETWEEN FRAMES 55 TO 58, INSTALLED NEW STRINGER 43L, PN D53479420202.

Part: STRINGER — CORRODED (FRAMES 56-57) · airframe 73,976 hrs · 33,557 cycles

CORROSION ON STR 42L BETWEEN FRAMES 56-57, REMOVED STR 42L BETWEEN FRAMES 57 AND 58 FABRICATED NEW STRINGER AND COUPLINGS IAW SRM 53-00-13, FIG 201 J.

Part: SKIN — CORRODED (FRAMES 56-57) · airframe 73,976 hrs · 33,557 cycles

CORROSION ON INNER SKIN SURFACE OTBD OF STR S42L BETWEEN FRAMES 56-57, REMOVAL OF CORROSION AND BLEND OUT AT INNER SKIN OTBD OF STR 42L BETWEEN FRAMES 56 AND 57 IAW PRI 542225-14, REV STEP 1 TREATED BARE METAL AREAS AND PRIMERED, REF PRI, ERA 542225-14, REV 2.

Part: SIGN — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 73,976 hrs · 33,557 cycles

RED EMERGENCY EXIT SIGNS AT THE AFR CABIN AND BY DOORS 2L AND 2R WILL NOT ILLUMINATE WHEN THE LANDING GEAR IS EXTENDED WITH THE, NO SMOKING SWITCH POSITIONED TO AUTO, REPLACED EPSU.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,901 hrs · 33,520 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE AFT, REPLACED EMERGENCY LIGHT BATTERY ABOVE L2 DOOR.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,860 hrs · 33,500 cycles

EMERGENCY LIGHTS AT SEATS 11 THRU 14, 17, 18, 19, 21 THRU 26 INOPERATIVE. REPLACED EPSU.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,479 hrs · 33,280 cycles

NUMEROUS EMERGENCY LIGHTS INOPERATIVE ON AISLE SEATS. FOUND AFT UNIT PWR SUPPLY AT FAULT. R & R POWER SUPPLY.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 72,894 hrs · 32,963 cycles

AFT LT EPSU HAS UNIT FAULT. REPLACED AFT LT EPSU/BATTERY AND OPS CHECK WAS NORMAL.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 71,714 hrs · 32,406 cycles

DURING NON-ROUTINE CHECK, FOUND SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE AT ROW 7. FOUND 2 CONNECTORS PULLED APART. INSTALLED 2 NEW CONNECTORS. OPS CHECK WAS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,248 hrs · 32,195 cycles

DURING NON ROUTINE CHECK, FOUND FOUND ON SERVICE CHECK DURING EMERGENCY LIGHTS TEST, UNIT FWD LT FAULT. REPLACED FWD LT EPSU UNIT, 10WL, EMERGENCY LIGHTS AND FUNCTIONAL CHECK WAS NORMAL.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 76,373 hrs · 34,772 cycles

CORROSION WAS FOUND ON SKIN REINFORCEMENT DOUBLER AT RT NLG BAY ASSEMBLY. REPAIR ON INTERNAL FUSELAGE SKIN LOCATED BTW FR 17 TO FR 18 AND AT LEVEL STR 39R IN RT LATERAL AVIONIC COMPARTMENT AS PER ER/A N 524162-14 REV 0 REV A.

Part: PANEL — CORRODED (NLG WW) · airframe 74,747 hrs · 33,915 cycles

FOUND SEVERAL CORROSION SPOTS, 5 E/A ON DIFFERENT PARTS OF THE NLG BAY, SIDE PANEL. THE CORROSION REMOVED IAW SRM AND REPAIR ACCOMPLISHED IAW 522877-14, SECTION I.

Part: STRINGER — CORRODED (FRAMES 65-66) · airframe 68,859 hrs · 31,030 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 31R BETWEEN FRAMES 65-66 IN AFT BULKHEAD AREA. REPLACED STRINGER IAW SRM 51-72-11 AND DWG D53480019.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,859 hrs · 31,030 cycles

DURING NON ROUTINE CHECK, FOUND INOPERATIVE EPSU. MAINTENANCE REPLACED EPSU AFT LEFT EPSU AND FUNCTIONAL CHECKED NORMAL.

Part: FRAME — CORRODED (FRAME 19) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON LATERAL FRAME 19 IN RT AVIONIC BAY S39R. REPLACED FRAME IAW SRM 51-72-11 AND DWG D53114433, D53113542.

Part: SKIN — DENTED (FRAME 68) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND DENT ON EXTERNAL FUSELAGE, FRAME 68 AT S29L. REPAIRED IAW ER/A 522856-14, REV ORIGINAL AND PRI 522856-14, REV 0, 1, 2 .

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 76,373 hrs · 34,772 cycles

CORROSION ON FLOORBEAM -Y254 IN FWD PAX CABIN FLOOR STRUCTURE. LOC BTW FR 12 TO FR 24, REPAIR ON FLOORBEAM -Y254 IN FWD PAX CABIN FLOOR STRUCTURE LOC BTW FR 12 TO FR 24 AS PER ER/A 523452-14 REVISION 0 AND REVISION ORIGINAL.

Part: STRINGER — CORRODED (FRAMES 65-66) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 26R BETWEEN FRAMES 65-66. REPLACED STRINGER IAW SRM 51-72-11 AND DWG D53480019.

Part: STRINGER — CORRODED (FRAMES 65-66) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 25R BETWEEN FRAMES 65-66. REPLACED STRINGER IAW SRM 51-72-11 AND DWG D53480019.

Part: STRINGER — CORRODED (FRAMES 33-34) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 44 LOCATED BETWEEN FRAMES 33-34. REPAIRED STRINGER IAW SRM 53-00-39, PARA 4A, FIG 201, PAGES 201-212 AND DWG D532-10093.

Part: STRUCTURE — CORRODED (FRAME 20) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER SILL LOCATED AT FR 20 AT LEVEL STR 23LT FWD PAX CABIN. REPLACED LOWER SILL LOCATED ON FR 16 TO FR 20 FWD PAX CABIN IAW SRM 51-72-11 AND DWG D53110339.

Part: STRINGER — CORRODED (FRAMES 33-34) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 43L IN FWD CARGO BAY BETWEEN FRAMES 33 - 34. REPAIRED STRINGER IAW SRM 53-00-13.

Part: STRUCTURE — CRACKED (EMERGENCY EXIT) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CRACK LOCATED ON INTERNAL STRUCTURE OF EMERGENCY EXIT DOOR 844 LT AND TRANSMITTING PROFILE. REPLACED LOAD TRANSMITTING PROFILE LOCATED ON INTERNAL STRUCTURE OF EMERGENCY EXIT DOOR 844 LT IAW SRM A320 51-72-11 AND DWG N. D52279036.

Part: FLOORBEAM — CORRODED (FRAME 24) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND BENT FLOORBEAM Y 254 AT LEVEL FR24 FWD PAX CABIN. REPAIRED FLOORBEAM IAW SRM 53-00-14 PARA 5.G, FIG 207, SHEET 1, PAGES 250/254.

Part: STRINGER SPLICE — CORRODED (FRAMES 30-31) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER SPLICE IN FWD CARGO BAY AT S43L AND BETWEEN FRAMES 30 - 31. REPLACED STRINGER SPLICE IAW SRM 51-72-11 AND DWG D53231626.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT LOCATED AT FRAME 20 S23R. REPLACED FLOOR SUPPORT FROM FRAMES 16 - 20 IAW SRM 51-72-11 AND DWG D53110339.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y765 BETWEEN FRAMES 66+ 5 AND 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: STRINGER — CORRODED (FRAMES 54-60) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 43L FRAMES 54-60 IN AFT CARGO BAY. REPLACED STRINGER IAW SRM 51-72-11 AND DWG D53470345.

Part: SUPPORT ANGLE — CORRODED (EMERGENCY EXIT) · airframe 76,373 hrs · 34,772 cycles

CORROSION ON SUPPORT ANGLE LOCATED LOWER POSITION OF EMERGENCY EXIT DOOR 834. REPLACED SUPPORT ANGLE PER SRM 51-72-11.

Part: SUPPORT ANGLE — CORRODED (EMERGENCY EXIT) · airframe 76,373 hrs · 34,772 cycles

CORROSION ON SUPPORT ANGLE LOCATED INTERNAL STRUCTURE EMERGENCY EXIT DOOR 843 LOWER POSITION. REPLACED SUPPORT ANGLE PER SRM 51-72-11 AND DRAWING D52279040.

Part: CROSSBEAM — CORRODED (FRAME 53) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON CROSSBEAM FITTING FRAME 53 STR 41. REPLACED CROSSBEAM IAW SRM A320 51-72-11 AND DWG D53470261.

Part: FLOOR SUPPORT — DAMAGED (FRAMES 64-66) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND ELONGATED HOLE ON FLOOR SUPPORT Y1292 BETWEEN FRAMES 64-66+5. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D534 72000.

Part: SUPPORT ANGLE — CORRODED (EMERGENCY EXIT) · airframe 76,373 hrs · 34,772 cycles

CORROSION ON SUPPORT ANGLE LOCATED INTERNAL STRUCTURE OF EMERGENCY EXIT DOOR 833 LOWER POSITION. REPLACED SUPPORT ANGLE PER SRM 51-72-11 AND DRAWING D52279040.

Part: STRUCTURE — CORRODED (FRAME 20) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER AFT CORNER AT FRAME 20 OF RT FWD PAX DOOR CUT OUT. REPLACED LOWER AFT CORNER FITTING IAW SRM 51-72-11 AND DWG D53112225.

Part: SPLICE — CORRODED (FRAMES 30-31) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON SPLICE LOCATED IN FWD CARGO BAY STRINGER 41L BETWEEN FRAMES 30 - 31. REPLACED SPLICE IAW SRM 51-72-11 AND DRAWING D53231586.

Part: STRINGER — CORRODED (FRAMES 30-31) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 41L BETWEEN FRAMES 30 - 31 IN FWD CARGO BAY. REPAIRED STRINGER IAW SRM 53-00-13, PARA 4.A, FIGURE 201.

Part: STRUCTURE — CORRODED (FRAME 20) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON AFT LOWER CORNER FRAME 20 OF LT FWD PAX DOOR CUTOUT. REPLACED IAW SRM 51-72-11 AND DWG D53112225.

Part: FITTING — CORRODED (FRAME 16) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON SCUFF PLATE FWD CORNER FITTING FRAME 16. REPLACED CORNER FITTING IAW SRM 51-72-11 AND DWG D53112225.

Part: SUPPORT ANGLE — CORRODED (EMERGENCY EXIT) · airframe 76,373 hrs · 34,772 cycles

CORROSION ON SUPPORT ANGLE LOCATED INTERNAL STRUCTURE OF EMERGENCY EXIT DOOR 844 LOWER POSITION. REPLACED SUPPORT ANGLE PER SRM 51-72-11 AND DRAWING D52279040.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-67) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1225 BETWEEN FRAMES 66+5 - 67+15. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472780.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-69) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1162 BETWEEN FRAMES 67 +15 - 69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472780.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y254 BETWEEN FRAMES 12-24. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112816.

Part: FITTING — CORRODED (FRAMES 16-20) · airframe 68,858 hrs · 31,029 cycles

DURING INPECTION, FOUND CORROSION ON CENTER FITTING FRAMES 16-20 STRINGER 23L PAX CABIN DOOR. REPLACED FITTING AT DOOR IAW SRM 51-72-11, DWG D53112225.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE LOCATED IN THE FWD CARGO BAY AT FRAME 31 BETWEEN STRINGERS 39-40R. REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53231623.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-69) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1162 BETWEEN FRAMES 67+15 - 69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: FLOOR SUPPORT — DAMAGED (FRAMES 64-66) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND ELONGATED HOLE ON FLOOR SUPPORT -Y1292 IN AFT PAX CABIN LOCATED BETWEEN FRAMES 64-66+5". REPLACED FLOOR SUPPORT IAW SRM A320 51-72-11 AND DWG D53472816.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-67) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECION, FOUND CORROSION ON FLOOR SUPPORT -Y1225 BETWEEN FRAMES 66+5 - 67+15. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53470150.

Part: SHEAR TIE — CORRODED (FRAME 30) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE, LOCATED IN THE FWD CARGO BAY AT FRAME 30 BETWEEN STRINGERS 41-42R. REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53231586.

Part: STRINGER SPLICE — CORRODED (FRAMES 30-31) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER SPLICE 41R BETWEEN FRAMES 30-31. REPLACED STRINGER SPLICE IAW SRM 51-72-11.

Part: WEB — CORRODED (FRAME 20) · airframe 68,858 hrs · 31,029 cycles

CORROSION ON WEB LOWER SURFACE Y1732 AT FRAME 20 IN FWD PAX CABIN. REPLACED WEB IAW SRM 51-72-11 AND DWG NR D53114392.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-70) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y465 BETWEEN FRAMES 67+10-70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG 53472000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 14-16) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y940 BETWEEN FRAMES 14-16. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112822.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y765 BETWEEN FRAMES 66+5-70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472816.

Part: STRUCTURE — CORRODED (FRAME 68) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON AFT LOWER CORNER AT FRAME 68 OF RT AFT PAX DOOR CUTOUT. REPLACED AFT LOWER CORNER IAW SRM 51-72-11 AND DWG D53480019.

Part: STRUCTURE — CORRODED (FRAME 68) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON AFT LOWER CORNER AT FRAME 68 OF LT AFT PAX DOOR CUTOUT. REPLACED AFT LOWER CORNER IAW SRM 51-72-11 AND DWG D53480019.

Part: SHEAR PLATE — CORRODED (FRAMES 69-70) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR PLATE FRAMES 69 - 70 S23L. REPLACED SHEAR PLATE IAW SRM 51-72-11 AND DWG D5347060.

Part: FITTING — CORRODED (FRAMES 66-68) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON CENTER FITTING BETWEEN FRAMES 66 - 68 AT S23R PAX ENTRY DOOR. REPLACED CENTER FITTING IAW SRM 51-72-11 AND DWG D53480019.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 76,373 hrs · 34,772 cycles

CORROSION ON SHEAR TIE LOCATED FWD CARGO COMPARTMENT BETWEEN STR 40R AND STR 41R AND AT LEVEL OF FR31. REPLACED SHEAR TIE LOCATED FWD CARGO COMPARTMENT PER SRM 51-72-11 AND DRAWING D53231586.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-16) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON JOINT COVER BETWEEN FRAMES 12 - 16 OF FLOOR SUPPORT Y-81. REPLACED JOINT COVER IAW SRM 51-72-11 AND DWG D53112620.

Part: STOP FITTING — CORRODED (PAX DOOR) · airframe 76,373 hrs · 34,772 cycles

CORROSION ON BOLT STOP DOOR OF THE RIGHT AFT PAX DOOR LOCATED AT FWD POSITIONS 3,4,5,6,7 AND AFT POSITIONS 1,2,3,4,5,6,7.MEASURES L= 0.300" W=0.150" D=0.001". REPLACED DOOR STOP OF THE RIGHT AFT PAX DOOR PER AMM 52-13-00.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 76,373 hrs · 34,772 cycles

CORROSION ON SHEAR TIE LOCATED FWD CARGO COMPARTMENT BETWEEN STR 40 R AND STR 41R AT LEVEL OF FR30. REPLACED SHEAR TIE LOCATED FWD CARGO COMPARTMENT PER SRM 51-72-11 AND D53231586.

Part: SHEAR TIE — CORRODED (FRAME 33) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE FRAME 33 S41-42R. REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53230830.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE FWD CARGO BAY AT FRAME 32 BETWEEN S42-43R. REPLACED SHEAR TIE IAW 51-72-11 AND DWG D53230812.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE, LOCATED FWD CARGO COMPARTMENT AT FRAME 32 AND BETWEEN S41-42L, REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53231626.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE LOCATED FWD CARGO COMPARTMENT AT LEVEL OF FR32 AND BETWEEN STRG 42L TO STRG 43L, INTERNAL STRUCTURE. REPLACED SHEAR TIE LOCATED FWD CARGO COMPARTMENT ON LEVEL OF FR 32 BETWEEN STR 42L TO STR 43L INTERNAL STRUCTURE IAW SRM 51-72-11 AND DWG D532 31626.

Part: FLOOR SUPPORT — CORRODED (FRAMES 69-70) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON WEB IN AFT PAX CABIN FLOOR SUPPORT BETWEEN FRAMES 69 TO 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53470100.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE LOCATED FWD CARGO COMPARTMENT AT LEVEL OF FR32 AND BETWEEN STRG 40R TO STRG 41R, INTERNAL AREA. REPLACED SHEAR TIE LOCATED ON FWD CARGO COMP AT LEVEL OF FR 32 BETWEEN STR 40R AND STR 41R INTERNAL AREA IAW SRM 51-72-11 AND DWG D53231586.

Part: SHEAR PLATE — CORRODED (FRAMES 69-70) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR PLATE IN AFT PAX CABIN FRAMES 69-70 S23R. REPLACED SHEAR PLATE IAW SRM 51-72-11 AND DWG D53470100.

Part: SUPPORT ANGLE — CRACKED (FRAME 54) · airframe 68,858 hrs · 31,029 cycles

DURING INSPECTION, FOUND A CRACK ON SUPPORT ANGLE AT AFT CARGO DOOR ATTACH ACTUATOR BRACKETS, FR 54 OTBD SIDE. REPLACED SUPPORT ANGLE IAW SRM 51-72-11 AND DWG D53472000.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,125 hrs · 30,127 cycles

DURING INSPECTION, FOUND EXT LOADS EMERGENCY RT MESSAGE ON SERVICE CHECK FOR EMERGENCY LIGHT TEST. MX REPLACED BATTERY PACK AND FUNCTIONAL CHECK WAS NORMAL. .

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,855 hrs · 29,452 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT TEST ON SERVICE CHECK FAULT'S INTERIOR AND EXTERIOR. MX REPLACED LT MID EPSU AND BATTERY. FUNCTIONAL CHECK WAS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,470 hrs · 28,770 cycles

DURING INSPECTION, FOUND FORWARD LIGHT BATTERY FAULTED ON CIDS. MAINTENANCE REPLACED BATTERY PACK FROM EPSU 10WL AND FUNCTIONAL CHECKED NORMAL.

Part: WIRE — DAMAGED (CABIN) · airframe 61,807 hrs · 27,517 cycles

DURING EMERGENCY LIGHT TEST FOUND ROW 5C PATH LIGHT INOPERATIVE. MAINTENANCE REPAIRED WIRE AT CONNECTOR AND TESTS OK.

Part: WIRE — DAMAGED (CABIN) · airframe 61,173 hrs · 27,194 cycles

DURING EMERGENCY LIGHT TEST FOUND ROW 4 PATH LIGHT INOP, REPAIRED WIRE AND TESTS OK.

Part: EPSU — FAULTED (CABIN) · airframe 60,237 hrs · 26,784 cycles

DURING EMERGENCY LIGHT TEST EPSU FAULTED, REPLACED EPSU AND TESTS OK. (2011-00084)

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE)

DURING CRUISE, RECEIVED CABIN PRESSURE SYS 1 AND 2 FAULT AND CABIN PRESSURE EXCESS CAB ALT MESSAGES WITH AUTOMATIC DROP OF OXYGEN MASKS. INITIATED RAPID DESCENT DUE TO A MODERATELY RAPID DECOMPRESSION. DIVERTED TO MCI AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NR 1 AND NR 2 CABIN PRESSURE CONTROLLERS AND THE OUTFLOW VALVE. SYSTEM OPERATIONAL CHECK NORMAL.

Part: PUMP — LEAKING (LT HYD SYST)

DURING CRUISE, RECEIVED HYD B RSVR LOW LEVEL MESSAGE. FLIGHT DIVERTED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING BLUE ELECTRIC HYDRAULIC PUMP. OPERATIONAL CHECK OK.

Part: SEAL — LEAKING (BLUE HYD SYST)

RECEIVED B-RSVR LO LVL MESSAGE DURING FLIGHT. CAT 3 LANDING NOT AUTHORIZED AT ORIGINAL DESTINATION DUE TO WEATHER CONDITIONS. AIRCRAFT DIVERTED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING SEAL ON THE BLUE HYDRAULIC SYSTEM LOW PRESSURE SWITCH, LEAK CHECK OK.

Part: ACTUATOR — MALFUNCTIONED (LT/RT LE SLATS)

EXPERIENCED F/CTL SLATS FAULT' ACCOMPANIED BY SLATS LOCKED DURING HEAVY ICING. AIRCRAFT DID NOT SWITCH TO ALTERNATE LAW. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOTH LEFT AND RIGHT WING NR 2 SLAT ACTUATOR TORQUE LIMITERS POPPED. REPLACED BOTH SLAT ACTUATORS, OPS CHECKED OK.

Part: PUMP — MAKING METAL (B HYD SYST)

DURING CLIMBOUT FROM DTW, RECEIVED 'HYD B SYS LO PR' MESSAGE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND PRESSURE RETURNED TO 1750 PSI. DECISION WAS MADE TO RETURN TO DTW WHERE AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE FOUND THE BLUE HYDRAULIC SYSTEM CASE DRAIN FILTER DIFFERENTIAL PRESSURE INDICATOR POPPED. REPLACED THE BLUE HYDRAULIC SYSTEM ELECTRIC PUMP. OPERATIONAL CHECK OK.