N312US

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,638 hrs · 44,977 cycles

SHIP 3212 DISC: EMERG EXIT LTS AND SIGNSON AND OFF PERIODICALLYWITH NO INPUT. C/A: PERFORMED EMERGENCY LIGHT TEST IAW A320 AMM 33-51-00-710-001-A NO FAULTS WERE NOTED OKAY FOR SVC. (LP: 0125126)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,478 hrs · 43,839 cycles

SHIP 3212 BURNING SMELL FWD GALLEY ON DEPARTURE. DISSIPATED WHEN GALLEY POWER TURNED OFF. CORRECTIVE ACTION: R/R GALLEY PWR SPLY CONTACTOR PER A320 AMM 24-56-55 AND CABIN RECIRC FILTERS PER 21-21-41. OK FOR SVC. (9456522)

Part: DOOR SEAL — LEAKING (AFT CARGO) · airframe 94,033 hrs · 43,611 cycles

CABIN PRESSURIZATION ISSUES. REPLACED AFT CARGO DOOR SEAL IAW AMM 52-32-18. LEAK CHECKED GOOD.

Part: NONE — NONE · airframe 92,506 hrs · 42,690 cycles

SHIP 3212 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED AT SEAT 28D. CORRECTIVE ACTION: REPAIRED LIGHT ASSY AND REFASTENED PER A320 AMM 33-52. OPS CHECK GOOD. (2276331)

Part: NONE — NONE · airframe 91,614 hrs · 42,120 cycles

SHIP 3212 ON DESCENT THRU FL 220 1 EMERGENCY EXIT AFT ILLUMINATED. CORRECTIVE ACTION: FOUND DOOR PROX TARGET LOOSE ADJUSTED TARGET NO FAULTS NOTED AFTER ADJUSTMENT. (7999034)

Part: NONE — NONE · airframe 91,216 hrs · 41,890 cycles

SHIP 3212 EMERG PATH LIGHTING AT 10D WILL NOT STAY ATTACHED. CORRECTIVE ACTION: RESECURED PATH LIGHTING AT SEAT 10D. OK FOR SVC. (8296278)

Part: B-NUT — LEAKING (APU OIL SYSTEM) · airframe 90,510 hrs · 41,468 cycles

SHIP 3212 APU AUTO SHUTDOWN AT CRUISE DIVERTED TO CMH. AIR DIVERSION. CORRECTIVE ACTION: FOUND APU TO BE LOW 3 QTS FOUND B NUT ON OIL PUMP TUBE TO BE LOOSE TIGHTENED B NUT PER A320 AMM 49-91 PERFORMED LEAK CK . NO LEAKS NOTED OK FOR SVC. (8110164)

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 90,510 hrs · 41,468 cycles

SHIP 3212 F/A REPORTS CABIN EMERGENCY LIGHT TURN OFF AND ON RANDOMLY. CORRECTIVE ACTION: EMERG LTS OP NML UPON ARRIVAL RSW. BELIEVE TO BE ASSOCIATED WITH FAILURE OF NBR 1 ENG IDG. (8110158)

Part: PRIORITY VALVE — FAILED (NR 2 ENGINE) · airframe 89,639 hrs · 40,967 cycles

SHIP 3212 - ATB - DUE TO DUAL ENGINE BLEED ISSUES AND UNABLE TO PRESSURIZE CABIN. NO MASK DROP. CREW REPORTED BLEEDS AS INTERMITTENT. CORRECTIVE ACTION: REFERENCE LP 7383902 AND 7383906. ENG 2 PRV AND HP REPLACED, ENG 2 TCT PACKING REPLACED FOR LEAKS, AND ENG 1 PRV REPLACED.

Part: SOLENOID — FAILED (NR 1 THERMOSTAT) · airframe 89,628 hrs · 40,961 cycles

SHIP 3212 DURING CRUISE FLT AT 340 CABIN ALTITUDE CLIMBED TO A MAX OF 9000 ' AND DELTA P DROPPED TO 6.1 . DECENDED TO FL 260. CABIN REPRESSURIZED TO 3800' AND DELTA P 7.9. APPROX. 1 HOUR LATER CABIN UNCONTROLLED CLIMB AGAIN, DECENDED TO 15,000' AND CABIN ALT STABILIZED. CORRECTIVE ACTION: REPLACED #1 ENG THERMOSTAT 10HA1 SOLENOID AS PER A320 AMM 36-11- 55. REPLACED NBR 1 PRV VALVE PER A320 AMM 36-11. OPS CK GOOD. (7439096)

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 88,055 hrs · 40,161 cycles

CABIN EMERGENCY LIGHTS ARE "ON" AND WILL NOT RESET W/ COCKPIT OR CABIN SWITCH . CORRECTIVE ACTION: RESET A/X D/C PWR OPS CK OK

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 86,593 hrs · 39,450 cycles

EPSU L FW FAILED DURING EMERGENCY LIGHT TEST, REPLACED EPSU

Part: FRAME — CRACKED (FUSELAGE) · airframe 86,218 hrs · 39,267 cycles

CRACK INDICATION ON FRAME 36 RT SIDE IN HOLE 2"APPROX OTBD FROM -Y1292 OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX IN FWD CARGO COMPARTMENT (1 EA), PERFORMED REPAIR INSTRUCTION SECTION I ON FR36 RT SIDE OF THE PRESSURE DECK CENTER WING BOX AS PER PRI 580236-14 REV 0, REV 1, REV 2, REV 3 AND ER/A 580236-14 REV ORIGINAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 86,218 hrs · 39,267 cycles

CRACK INDICATION ON FRAME 36 LT SIDE IN HOLE LOCATED ABOVE + Y1523 OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX IN FWD CARGO COMPARTMENT (1 EA), PERFORMED REPAIR INSTRUCTION SECTION I ON FR36 LT SIDE AT THE PRESSURE DECK MEMBRANE TO CENTER WING BOX AS PER PRI 580236-14, REV 0, REV 1, REV 2, REV 3 AND ER/A 580236-14AD REV ORIGINAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 86,218 hrs · 39,267 cycles

CRACK INDICATION ON FRAME 36 RT SIDE IN HOLE LOCATED 2.920" APPROX AND OTBD FROM -Y1292 OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX IN FWD CARGO COMPARTMENT (1 EA), PERFORMED REPAIR INSTRUCTION SECTION 1 ON FRAME 36 RT SIDE OF THE PRESSURE DECK CENTER WING BOX AS PER PRI 580236-14 REV 0, REV 1, REV 2, REV 3 AND ER/A 580236-14AD REV ORIGINAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 86,218 hrs · 39,267 cycles

CRACK INDICATION ON FRAME 36 RT SIDE IN HOLE LOCATED 4.715" APPROX FR OM OTBD -Y1292 PRESSURE DECK MEMBRANE TO CENTER WING BOX IN FWD CARGO COMPARTMENT (1 EA), PERFORMED REPAIR INSTRUCTION SECTION 1 ON FR36 RT SIDE OF THE PRESSURE DECK CENTER WING BOX AS PER PRI 580236-14 REV 0, REV 1, REV 2, REV 3 AND ER/A 580236-14AD REV ORIGINAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 86,218 hrs · 39,267 cycles

CRACK INDICATION ON FRAME 36 RT SIDE IN HOLE LOCATED AT 3.835" APPROX OTBD FROM -Y1292 OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX IN FWD CARGO COMPARTMENT (1 EA), PERFORMED REPAIR INSTRUCTION SECTION I ON FR36 RT SIDE OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX AS PER PRI 580236-14 REV 0, REV 1, REV 2, REV 3 AND ER/A 580236-14AD REV ORIGINAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 86,218 hrs · 39,267 cycles

CRACK INDICATION ON FR36 LT SIDE OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX (8 E/A) "A CRACK THAT EXCEEDS THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE PANEL BTW FR 35 LT AND FR36 LT, PERFORMED REPAIR INSTRUCTION SECTION 1 ON FR36 LT SIDE OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX AS PER PRI 580236-14 REV 0, REV 1, REV 2, REV 3 AND ER/A 580236-14AD REV ORIGINAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 86,218 hrs · 39,267 cycles

CRACK INDICATION ON FRAME 36 RT SIDE IN HOLE LOCATED ABOVE - Y1523 OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX IN FWD CARGO COMPARTMENT (1 EA), PERFORMED REPAIR INSTRUCTION SECTION I ON FR36 RT SIDE OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX AS PER PRI 580264-14 REV 0, REV 1, REV 2, REV 3 AND ER/A 580236-14AD REV ORIGINAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 86,218 hrs · 39,267 cycles

CRACK INDICATION ON FRAME 36 RT SIDE OF THE PRESSURE DECK CENTER WING BOX (8EA) A CRACK THAT EXCEEDS THE AUTORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE PANEL BTW FR 35 RT AND 36RT, PERFORMED REPAIR INSTRUCTION SECTION I ON FR36 RT SIDE OF THE PRESSURE DECK CENTER WING BOX AS PER PRI 580236-14 REV 0, REV 1, REV 2, REV 3 AND ER/A 580236-14AD REV ORIGINAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 86,218 hrs · 39,267 cycles

CRACK INDICATION ON FRAME 36 RT SIDE IN HOLE LOCATED 1.800" APPROX INBD FROM -Y1523 OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX IN FWD CARGO COMPARTMENT (1 EA), PRESSURE DECK MEMBRANE TO CENTER WING BOX AS PER PRI 580236-14 REV 0, REV 1 , REV 2, REV 3 AND ER/A 580236-14AD REV ORIGINAL.

Part: WEB — CORRODED (FRAMES 50-51) · corrosion level 2 · airframe 86,218 hrs · 39,267 cycles

CORROSION INTERNAL STRUCTURE WEB FR 50 TO FR 51 AND STR 38R IN AFT CARGO COMPARTMENT, REPLACED INTERNAL STRUCTURE WEB FR 50 TO FR 51 AND STR 38R IN AFT CARGO COMPARTMENT (1EA) ASPER SRM A320 51-72-11 AND INSTALLED FASTENERS ASPER SRM A320 51-42-11 AND DRAWING # D53470320

Part: WEB — CORRODED (FRAMES 16-20) · corrosion level 2 · airframe 86,218 hrs · 39,267 cycles

CORROSION WEB LOCATED BTW FR 16 TO FR 17 AND FR 19 TO FR 20 LEVEL STR 28L IN LATERAL AVIONIC COMP LH (1 EA), REPLACED WEB LOCATED BTW FR 16 TO FR 20 AT LEVEL OF STR 28L IN LATERAL AVIONIC COMPARTMENT LH SIDE ASPER A320 SRM 51-72-11 AND DWG D53113501010 AND DWG D53118135000

Part: STRINGER — CORRODED (FRAMES 56-58) · corrosion level 2 · airframe 86,218 hrs · 39,267 cycles

CORROSION STRINGER 42L FR 56 TO FR 58 IN AFT CARGO COMPARTMENT (1 EA), PERFORMED REPAIR ON STRINGER 42L LOC FR 56 TO FR 58 IN AFT CARGO COMPARTMENT ASPER A320 SRM 53-00-13-300-001 AND DRAWING D53470345

Part: STRINGER — CORRODED (FRAMES 56-57) · corrosion level 2 · airframe 86,218 hrs · 39,267 cycles

CORROSION STRINGER 43L FR 56 TO FR 57 IN AFT CARGO COMPARTMENT (1 EA), PERFORMED REPAIR ON STRINGER 43L LOC FR 56 TO FR 58 IN AFT CARGO COMPARTMENT ASPER A320 SRM 53-00-13-300-001 AND DRAWING D53470345

Part: FRAME — CRACKED (FRM 16) · airframe 86,218 hrs · 39,267 cycles

CRACK INDICATION ON FRAME 16 LOWER INBD FASTENER HOLE OF DOOR STOP 7 A T RH SIDE, CRACK DIRECTION 8 OCLOCK AND DEPTH IS 0.130 INCH, REPLACED INTERCOSTAL LOC. FRAME 16 AT LEVEL DOOR STOP 7 RH SIDE AS PER A320 SRM 51-72-11 AND DRAWING #D53114223

Part: FRAME — CRACKED (FRM 16) · airframe 86,218 hrs · 39,267 cycles

CRACK INDICATION ON FRAME 16 UPPER INBD FASTENER HOLE AT DOOR STOP 7 R H SIDE. CRACK DIRECTION 8 OCLOCK AND DEPTH IS 0.165 INCH. WORK CARD 53 11-2031, SSI 531103. AT FWD GALLEY AREA (1 EA). REPLACED INTERCOSTAL LOC FRAME 16 AT LEVEL DOOR STOP 7,RH SIDE AS PER A320 SRM 51-72-11 AND DRAWING #D53114223.

Part: SEAT TRACK — CORRODED (FRAMES 47-64) · corrosion level 2 · airframe 86,218 hrs · 39,267 cycles

CORROSION LEVEL: 2. REPLACE SEAT TRACK -Y765 FROM FR47 TO FR64 PREVIOUSLY REWORKED AREA A ND EVALUATED WITH CARD 2500-2032-DE WAS FOUND OUT OF LIMITS MEASURES O F DEEPEST POINT IS: D=0.057'' W=0.382'' L=0.778'' IN PASSENGER CABIN. REPLACED SEAT TRACK -Y765 FROM FR47 TO FR64 AFT PASSENGER CABIN AS PER A320 SRM 51-72-11 AND DWG D53472000 RELEASE DATE:06-JAN- 03.

Part: SEAT TRACK — CORRODED (FRAMES 47-64) · corrosion level 2 · airframe 86,218 hrs · 39,267 cycles

CORROSION LEVEL: 2. REPLACE SEAT TRACK -Y765 FROM FR47 TO FR64 PREVIOUSLY REWORKED AREA AND EVALUATED WITH CARD 2500-2032-DE WAS FOUND OUT OF LIMITS MEASURES OF DEEPEST POINT IS: D=0.057'' W=0.382'' L=0.778 '' IN PASSENGER CABIN. REPLACED SEAT TRACK -Y765 FROM FR47 TO FR64 AFT PASSENGER CABIN AS PER A320 SRM 51-72-11 AND DWG D53472000.

Part: FRAME — CRACKED (FRM 16) · airframe 86,218 hrs · 39,267 cycles

CRACK INDICATION ON FRAME 16 LOWER INBD FASTENER HOLE AT DOOR STOP 1 RH SIDE, CRACK DIRECTION 6 AND 9 OCLOCK AND DEPTHS ARE 0.080 INCH AND 0.020 INCH WORK CARD 5311-2031, SSI 531103. AT FWD GALLEY AREA (2 EA). PERFORMED PERMANENT REPAIR ON HOLE #3 AT DOOR STOP #1 ON FR 16 R/H ASPER PRI 580094-14 REV 0 AND REV 1 AND ER/A #580094-14AD REV ORIGINAL.

Part: PLATE — CRACKED (SLAT TRACK) · airframe 86,218 hrs · 39,267 cycles

CRACK CLOSING PLATE SLAT TRACK 5 ON LH WING. REPLACED CLOSING PLATE SLAT TRACK 5 ON LH WING AS PER A320 FAM AMM 27-84-69-400-009-A.

Part: FRAME — CRACKED (FRM 16) · airframe 86,218 hrs · 39,267 cycles

CRACK INDICATION ON FRAME 16 UPPER INBD FASTENER HOLE AT DOOR STOP 7 L H SIDE, CRACK DIRECTION IS 5 OCLOCK AND DEPTH IS 0.150 INCH. WORK CARD 5311-2031, SSI 531103 AT FWD GALLEY AREA (1 EA). REPLACED INTERCOSTAL FITTING AND FASTENERS LOCATED ON FRAME 16 AT DOOR STOP 7LH SIDE AT FWD GALLEY AREA AS PER SRM A320 51-72-11 AND DRAWING D53114223.

Part: FRAME — CRACKED (FRM 66) · airframe 86,218 hrs · 39,267 cycles

CRACK INDICATION ON FRAME 66 IN OPEN LOWER INBOARD HOLE 4,DOOR STOP FITTING 2 RH SIDE ,AA 5311-01216, AD RELATED, ACTIONS REQUIRED PRIOR TO FURTHER FLIGHT AT AFT GALLEY AREA (1 EA) ( CRACK DIRECTION= 10 O'CLOCK APPROX, D1-D2= 0.150 INCH , (3.81MM) ). PERFORMED REPAIR INSTRUCTION ON LOWER I/B HOLE 4, DOOR STOP FITTING #2 RH SIDE ON FR 66 AT AFT GALLEY AREA ASPER A320 SRM 53-41-12-300-008 STEP 2A, FINAL DIAMETER AFTER REAMED ON HOLE 4 IS:0.4068" (10.333MM).

Part: SEAT TRACK — CORRODED (FRAMES 41-51) · corrosion level 2 · airframe 86,218 hrs · 39,267 cycles

CORROSION SEAT TRACK +Y1292 BTW FR 41 TO FR 47/51 PREVIOUSLY REWORKED AND EVALUATED WITH CARD 2500-2031-DE WAS FOUND OUT LIMITS, REPLACED SEAT TRACK +Y1292 BTW FR 41 TO FR47/51 IN PASSENGER CABIN ASPER A320 SRM 51-72-11 AND SRM 51-42-11 AND DRAWING #D53 370500

Part: SEAT TRACK — CORRODED (FRAMES 36-41) · corrosion level 2 · airframe 86,218 hrs · 39,267 cycles

CORROSION SEAT TRACK +Y1292 BTW FR 36 TO FR 41 PREVIOUSLY REWORKED AND E VALUATED WITH CARD 2500-2031-DE WAS FOUND OUT LIMITS, REPLACED SEAT TRACK +1292 LOC BTW FR 36 TO 41 IN PASSENGER CABIN ASPER A320 SRM 51-42-11 AND SRM 51-72-11 AND DWG #D5337-0500

Part: FRAME — CRACKED (FRM 68) · airframe 86,218 hrs · 39,267 cycles

CRACK INDICATION ON FRAME 68 IN OPEN LOWER INBOARD HOLE 4 , DOOR STOP FITTING 4 RH SIDE, AA 5311-01216, AD RELATED, ACTIONS REQUIRED PRIOR TO FURTHER FLIGHT AT AFT GALLEY AREA (1 EA) (CRACK DIRECTION= 7 O'CLOC K APPROX D1-D2= 0.140 INCH (3.56MM)). PERFORMED RAPAIR INSTRUCTION ON HOLE 4 LOWER 1/B, DOOR STOP FITTING #4 RH SIDE ON FR 68 AT AFT GALLEY AREA ASPER A320 SRM 53-41-12-300-008 STEP 2A, FINAL DIAMETER AFTER REAMED ON HOLE 4 15:0.4068" (10.333MM).

Part: SEAT TRACK — OUT OF LIMITS (FRAMES 47-64) · airframe 86,218 hrs · 39,267 cycles

SEAT TRACK +Y1292 FROM FR47 TO FR64 PREVIOUSLY REWORKED AREA A ND EVALUATED WITH CARD 2500-2032-DE WAS FOUND OUT OF LIMITS, REPLACED SEAT TRACK +Y1292 FROM FR47 TO FR64 ASPER A320 SRM 51- 72-11 AND DWG 534720000

Part: SEAT TRACK — CORRODED (FRAMES 47-64) · corrosion level 2 · airframe 86,218 hrs · 39,267 cycles

SEAT TRACK -Y1292 FROM FR47 TO FR64 PREVIOUSLY REWORKED AREA AND EVALUATED WITH CARD 2500-2032-DE WAS FOUND OUT OF LIMITS REPLACED SEAT TRACK 41292 LOC FROM FR47 TO FR64 IN PASSENGER CABIN ASPER A320 SRM 51-72-11 AND 51-42-11 AND DRAWING D53472000

Part: SEAT TRACK — OUT OF LIMITS (FRAMES 47-65) · corrosion level 2 · airframe 86,218 hrs · 39,267 cycles

SEAT TRACK +Y765 FROM FR47 TO FR64 PREVIOUSLY REWORKED AREA AN D EVALUATED WITH CARD 2500-2032-DE WAS FOUND OUT OF LIMITS, REPLACED SEAT TRACK +Y765 FROM FR 47 TO FR 64 ASPER SRM 51-72-11 AND DWG D53478000

Part: SLIDING WINDOW — CRACKED (COCKPIT) · airframe 86,218 hrs · 39,267 cycles

CRACK SLIDING WINDOW LOCATED ON COPILOTS UPPER CORNER IN COCKPIT (1 EA). REMOVED SLIDING WINDOW PANEL RH SIDE. REPLACED SLIDING WINDOW PANEL ON COPILOTS IN COCKPIT AS PER A320 FAM AMM 56-12-11-400-002-A.WINDOW, GLASS, OFF 00000 ON 32-5610-9-0008 61879

Part: FLOOR SUPPORT — CORRODED (FRAME 69) · corrosion level 2 · airframe 86,218 hrs · 39,267 cycles

CORROSION FLOOR BEAM -Y765 BTW FR 68 TO FR 69 AT AFT GALLEY AREA, REPLACED FLOOR BEAM -Y765 LOC.BTW FR 66 TO 70 AT AFT GALLEY AREA ASPER A320 SRM 51-72-11 AND DWG:D53472000

Part: FLOOR SUPPORT — CORRODED (FRAME 68) · corrosion level 2 · airframe 86,218 hrs · 39,267 cycles

CORROSION FLOOR BEAM -464.75 AT LEVEL FR 68 AT AFT GALLEY AREA, REPLACED FLOOR BEAM -Y464.75 AT LEVEL FR 68 TO FR 70 AFT GALLEY AREA ASPER A320 SRM 51-72-11 AND DRAWING D53472000

Part: LIGHT — BROKEN (SEAT 15D) · airframe 85,381 hrs · 38,819 cycles

15D EMERGENCY EXIT PATH LIGHT HOUSING BROKEN, REPLACED PATH LIGHT HOUSING ASSY

Part: BATTERY PACK — NOT REPORTED (CABIN) · airframe 84,369 hrs · 38,330 cycles

REPLACED EMERGENCY LIGHTING ESCAPE PATH LIGHTING BATTERY PACKS.

Part: FORK — CRACKED (CARGO DOOR) · airframe 84,982 hrs · 38,629 cycles

AFT CARGO DOOR / FRAME FORKS / CRACKED AND OVERSIZED HOLES, REPAIRED PER ER/A 570297-14AD SECTION I. REPAIR INSTALLED OVERSIZED FASTENERS ON FR 54 AND FR54A AT FORK ENDS AND REPLACED FR53 FORK END ON AFT CARGO DOOR.

Part: NONE — NONE (NONE) · airframe 84,331 hrs · 38,310 cycles

(LP# 0674165) /ERA 570292-14AD HAS BEEN UPDATED TO REV A TO INCORPORATED NEW RDAS APPROVAL. PERMANENT WITH NO FOLLOW ON ACTION REQUIRED. . 28NOV CLOSED LOG AND REMOVED MONITOR.

Part: LENS — MISSING (RT OVRWG SLIDE) · airframe 80,384 hrs · 36,373 cycles

RT OVERWING SLIDE ARMED LIGHT LENS MISSING, INSTALLED A NEW LENS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,830 hrs · 36,108 cycles

FLOOR PROXIMITY EMERGENCY LIGHT INOP F/C BULKHEAD. REPLACED FLOOR PROX LIGHT ASSY.

Part: BOX BEAM — CRACKED (FRAME 43) · airframe 78,553 hrs · 35,509 cycles

ACCOMPLISHED SIDE BOX BEAM UPPER FLANGE AT FR 43 BETWEEN STRINGERS 5 AND 7L OPEN HOLE ET IAW AMDS 5310-01450-01 AND NTM 51-10-01. AFT 2 REMOVED FASTENER HOLES HAVE CRACK INDICATIONS. REPAIRED IAW AMDS 5310-01450-02 AND ERA 551398-14AD REV ORIGINAL,

Part: BOX BEAM — CRACKED (FRAME 43) · airframe 78,553 hrs · 35,509 cycles

ACCOMPLISHED SIDE BOX BEAM UPPER FLANGE AT FRAME 43 BETWEEN STRINGERS 5 AND 7R OPEN HOLE ET IAW AMDS 5310-01450-01 AND NTM 51-10-01. AFT 2 REMOVED FASTENER HOLES HAVE CRACK INDICATIONS, REPAIRED IAW AMDS 5310-01450-02 AND ERA 551398-14AD REV ORIGINAL,

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 86,218 hrs · 39,267 cycles

CRACK INDICATION DOOR STOP FITTING ON FRAME 68 LOC BTW STR 21R TO STR 22R CRACK DIRECTION: 6 O'CLOCK APPROX AT AFT GALLEY AREA, PERFORMED PERMANENT REPAIR ON DOOR STOP FITTING ON FR.68 LOC BTW STR.21R TO STR.22R AT AFT GALLEY AREA AS PER SRM 53-41-12 PARAGRAPH 5C AND 5E FIGURE 203 AND 204.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 86,218 hrs · 39,267 cycles

CRACK INDICATION DOOR STOP FITTING ON FRAME 68 LOC BTW STR 21L TO STR 22L CRACK DIRECTION: 6 O'CLOCK APPROX AT AFT GALLEY AREA, REPAIR ON DOOR STOP FITTING AND FRAME 68 LOC BTW STR.21L TO STR.22L AT AFT GALLEY AREA AS PER SRM 53-41-12 PARAGRAPH 5.C AND 5.E FIGURE 203 AND 204.

Part: ANGLE — NOT REPORTED · airframe 75,804 hrs · 34,142 cycles

REPLACED ANGLE ON INTERNAL STRUCTURE EXTERNAL BOTTOM SKIN OF KEELBEAM IN MAIN WHEEL ON STR 43R BETWEEN FRAME 45 TO FRAME 46 IAW SRM 51-72-11 AND DWG D53371804.

Part: ANGLE — NOT REPORTED · airframe 75,804 hrs · 34,142 cycles

REPLACED ANGLE ON INTERNAL STRUCTURE BOTTOM SKIN OF KEELBEAM IN MAIN WHEEL WELL ON STR 43L BETWEEEN FRAME 45 TO FRAME 46 IAW SRM 51-72-11 AND DWG D53371804.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 74,449 hrs · 33,432 cycles

DURING INSPECTION, FOUND FWD ATG 4 ANTENNA DOUBLER HAS DAMAGE WITHIN 10" CIRCUMFERENTILLY AND 20" LONGITUDINALLY. DENT IS .015 DEEP, 1" IN DIAMETER. C/W ERA 535856-14AD FWD ATG4 ANTENNA REPAIR DOUBLER.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 73,733 hrs · 33,117 cycles

DURING INSPECTION, FOUND ROW 22 EMERGENCY LIGHT INOPERATIVE. REPAIRED BROKEN WIRE AND FUNCTIONAL CHECKED NORMAL.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 71,484 hrs · 32,035 cycles

DURING SERVICE CHECK, EMERGENCY LIGHTS TEST FAILED. R & R BATTERY PACK AT LT OVERWING EXIT AND TESTED IAW AMM 33-51.

Part: FRAME — CRACKED (68) · airframe 70,079 hrs · 31,342 cycles

DURING INSPECTION, FOUND TWO CRACKS ON THE WEB FILLET RAD II OF FRAME 68 AND IN THE NEAREST FASTENER HOLE. CRACK FOUND DURING A NDT INSPECTION. REPAIRED IAW 520115-14, SECTION I. ERA SECT.II.

Part: STRINGER — CORRODED (44 LEFT) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 44L FWD CARGO BAY. REPAIRED STRINGER IAW SRM 53-00-13 FIGURE 201 (SHEET 2) PAGE 211/212.

Part: STRINGER — CORRODED (CARGO BAY) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 43L LOCATED FWD CARGO BAY BETWEEN FRAMES 32 AND 33. REPAIRED STRINGER IAW SRM 53-00-13 PARAGRAPH 4.A FIGURE 201 SHEET 3 PAG.213/214.

Part: HINGE FITTING — WORN (ELEVATOR) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND WEAR ON PLAIN BUSHING OUTBOARD OF HINGE FITTING NR 5 RT AT ELEVATOR SIDE. REPAIRED HINGE FITTING IAW SRM 55-26-41.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND WEAR ON PLAIN BUSHING INBOARD OF HINGE FITTING NR 5 RT ELEVATOR SIDE. REPAIRED HINGE FITTING IAW SRM 55-26-41.

Part: FITTING — CORRODED (ELEVATOR ACT) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON O/B ACTUATOR FITTING FOR RIGHT ELEVATOR. REPAIRED ACTUATOR FITTING IAW SRM 55-26-47 STEP 5.B AND PERFORMED HFEC INSPECTION ON BORE CRACK AND CORROSION INDICATION NOT FOUND.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON PAX CABIN FLOOR SUPPORT. REPLACED FLOOR SUPPORT IAW SRM A320 51-72-11 AND DWG D53472000.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND WEAR ON PLAIN BUSHING INBOARD OF HINGE NR 1 RT AT ELEVATOR SIDE. REPAIRED HINGE FITTING IAW SRM 55-26-41.

Part: FITTING — CORRODED (ELEVATOR ACT) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON I/B ACTUATOR FITTING AT RIGHT ELEVATOR. REPAIRED ACTUATOR FITTING IAW SRM 55-26-47 ITEM5.B.

Part: HINGE FITTING — WORN (ELEVATOR) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND WEAR ON PLAIN BUSHING OUTBOARD OF HINGE FITTING NR 1 RT AT ELEVATOR SIDE. REPAIRED HINGE FITTING IAW SRM 55-26-41.

Part: PROFILE — CRACKED (FUSELAGE) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND A CRACK ON LT LOAD TRANSMITTING PROFILE. REPLACED LOAD TRANSMITTING PROFILE IAW SRM A320 51-72-11 AND DRAWING D52279020.

Part: FLOOR SUPPORT — CORRODED (PAX CABIN) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON PAX CABIN FLOOR SUPPORT -Y1162 BETWEEN FRAMES 67+15 AND 69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D534-72000.

Part: ATTACH FITTING — CORRODED (CABIN) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON SECTION CONNECTING AT STR.27L FRAME 67. REPLACED SECTION CONNECTING IAW SRM 51-72-11 AND DRAWING D53480505.

Part: STRINGER — CORRODED (AFT CARGO) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 25R IN AFT CARGO BAY FRAMES 64 TO 65. REPLACED STRINGER IAW SRM 51-72-11 AND DRAWING D534-80009.

Part: FLOOR SUPPORT — CORRODED (PAX CABIN) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON PAX CABIN FLOOR SUPPORT -Y1292 AND -Y1162 FRAMES 66+6 AND 67+13. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53472000.

Part: FLOOR SUPPORT — CORRODED (PAX CABIN) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON PAX CABIN FLOOR SUPPORT -Y1292 AND FRAME. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53472000.

Part: RECEPTACLE — CORRODED (LT NACELLE) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON LT PYLON SPIGOT RECEPTACLE FITTING. REPLACED LT PYLON SPIGOT RECEPTACLE IAW SRM 54-51-12 PARAGRAPH 5.A FIG 201, DWG R54612042, & R54612043.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON FUEL TANK ACCESS PANEL 540PB OF LEFT WING. FOUND BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 57-27-11 PARAGRAPH 4.B (4) AND REPLACED ACCESS PANEL IAW AMM 57-27-11-400-002-A STEP 4.B(3).

Part: SEAT TRACK — CORRODED (PAX CABIN) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK +Y1292 FRAME 35+7. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53370000.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON PAX CABIN LOWER FLOOR SUPPORT LOCATED FRAMES 66 AND 68. REPLACED LOWER FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53480505.

Part: STRUCTURE — CORRODED (CABIN) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON PAX CABIN AFT LOWER STRUCTURE FRAME 68 STRINGER 23L. REPLACED STRUCTURE IAW SRM A320 51-72-11 AND DWG D53480505.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON PAX CABIN FLOOR SUPPORT Y1162 BETWEEN FRAMES 68 AND 69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: STRUCTURE — CORRODED (CABIN) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER SILL LOCATED FRAMES 66 AND 68. REPLACED LOWER SILL IAW SRM 51-72-11 AND DWGS D53480505, D53474250 AND D53480076.

Part: STRUCTURE — CORRODED (CABIN) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON PAX CABIN AFT LOWER STARUCTURE FRAME 68. REPLACED STRUCTURE IAW SRM 51-72-11 AND DWG D53480505.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON PAX CABIN FLOOR SUPPORT BETWEEN Y1292 AND Y1162 FRAMES 66+5 AND 67+15. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53472000.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT FRAME 20 AND -Y1292. REPLACED FLOOR SUPPORT BETWEEN FRAMES 12 - 24, IAW SRM 51-72-11 AND DWG D53112812.

Part: FITTING — CORRODED (CABIN) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON PAX CABIN CENTER FITTING FRAME 67+15. REPLACED CENTER FITTINGIAW SRM 51-72-11 AND DWG D53480305.

Part: FITTING — CORRODED (FUSELAGE) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON CORNER FITTING LOCATED FRAME 20. REPLACED FITTING IAW SRM 51-72-11 AND DWG D53112225.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON STRUCTURE. REPLACED STRUCTURE IAW SRM A320 51-72-11 AND DRAWING D53480009.

Part: FITTING — CORRODED (FUSELAGE) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON CENTER FITTING FRAMES 16 - 20. REPLACED CENTER FITTING IAW SRM 51-72-11 AND DRAWING D53112109.

Part: FITTING — CORRODED (FUSELAGE) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON CENTER FITTING LOCATED BETWEEN FRAMES 16 & 20. REPLACED CENTER FITTING IAW SRM 51-72-11 AND DRAWING D53112198.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON SECTION CONNECTING AT STRINGER 29L FRAME 67. REPLACED STRUCTURE IAW SRM 51-72-11 AND DRAWING D53480009.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT FRAME 20 -Y765. REPLACED FLOOR SUPPORT BETWEEN FRAMES 12 TO 24 IAW SRM 51-72-11 AND DWG D53112812.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON PAX CABIN FLOOR SUPPORT -Y308 FRAME 66+5. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472305.

Part: FITTING — CORRODED (CABIN) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON CORNER FITTING LOCATED ON FRAME 16 STRINGER 23R. REPLACED CORNER FITTING AND FASTENERS IAW SRM 51-72-11 AND DWG D53112109.

Part: FLOOR SUPPORT — CORRODED (PAX CABIN) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON PAX CABIN FLOOR SUPPORT Y765 FRAME 66. REPLACED FLOOR SUPPORT BETWEEN FRAMES 64 TO 66 IAW SRM 51-72-11 AND DWG D53472090 AND D53472000.

Part: FLOOR SUPPORT — CORRODED (MAIN CABIN) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON PAX CABIN FLOOR SUPPORT -Y160 FRAME 69+18. REPLACED FLOORBEAM FRAMES 68 TO 70 IN PAX CABIN IAW SRM 51-72-11 AND DWG D53472458.

Part: FLOOR SUPPORT — CORRODED (PAX CABIN) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON PAX CABIN FLOOR SUPPORT Y765 FRAME 68. REPLACED FLOOR SUPPORT FRAMES 67 TO 70 IAW A320 51-72-11 AND DWG 53472000 AND 53472092.

Part: FLOOR SUPPORT — CORRODED (FWD CABIN) · airframe 70,046 hrs · 31,326 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT LOCATED BETWEEN FRAMES 20 TO 22 -Y189 FWD PAX CABIN. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112834.

Part: PANEL — DELAMINATED (CARGO BAY) · airframe 5,681 hrs · 2,550 cycles

DURING NON ROUTINE CHECK, FOUND FORWARD CARGO SLOPING PANEL 131BF DELAMINATED. FABRICATED ON STAM TRAVELER# T12/913531 PER DWG 3D25-37705 FROM FR 24 TO FR 28 STRINGER 34L TO 38L. REPLACED PANEL 131BF IAW A320 AMM 53-22-14.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 5,681 hrs · 2,550 cycles

DURING NON ROUTINE CHECK, MAINTENANCE FOUND RT AFT OVERWING EMERGENCY DOOR RT PROFILE CRACKED. REMOVED DAMAGE SEGMENT ANGLE AND INSTALLED FABRICATED SEGMENT ANGLE FROM MATERIAL 2024-0.050C. BATCH 0001942011 PER A320 SRM 52-21-00 & HEAT TREATED BY STAM TRAVELER# T12/913706. INSTALLED REPAIR IAW A320 SRM 51-42-11 DIM.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 5,681 hrs · 2,550 cycles

DURING NON ROUTINE CHECK, MAINTENANCE REMOVED AFT CARGO FLOOR PANEL 151PF DUE DELAMINATION. FABRICATED AFT CARGO FLOOR PANEL 151PF ON STAM TRAVELER # T12/913710 IAW DRAWING 3D25-37705 MATERIAL A402AB-60X144 BATCH# 2105510. DAMAGE DIM. L=42" W=21". INSTALLED FLOOR PANEL 151PF IAW A320 AMM 53-42-14-400-001.

Part: SKIN — DENTED (FUSELAGE) · airframe 5,681 hrs · 2,550 cycles

DURING NON ROUTINE CHECK, FOUND LOWER FWD FUSELAGE EXTERNAL SKIN AT FR 26, BTW STR 42R - 43R DENTED. PERFORMED A DETAILED VISUAL INSP ON EXTERNAL SKIN AND NO CRACKS NOTED. ACCOMPLISHED PERMANENT REPAIR IAW A320 SRM 53-21-11 FIG 216.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 59,567 hrs · 26,362 cycles

DURING NON ROUTINE CHECK, THE EMERGENCY PATH LIGHT AT SEAT 1A-B, ROW 1L WAS INOPERATIVE. MX REPAIRED WIRE AT AFT OTBD SEAT LEG AND OPS CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.

Part: SKIN — DAMAGED (LT WING TE FLAP) · corrosion level 2 · airframe 58,684 hrs · 26,044 cycles

DURING "L" CHECK FOUND SKIN DAMAGED ON LT OTBD FLAP. REPAIRED IAW SRM 57-53-00.

Part: LIGHT — ODOR (CABIN) · airframe 56,813 hrs · 25,238 cycles

AFT FLIGHT ATTENDANTS REPORT FAINT ELECTRICAL ODOR ON INITIAL CLIMB THAT DISSIPATED IN CRUISE. AFTER GEAR DOWN, THE EMERGENCY EGRESS EXIT LIGHTS ILLUMINATED NORMALLY, FOLLOWED BY FAINT ELECTRICAL ODOR AND EMERGENCY EGRESS LIGHTING TURNING OFF IN REAR OF AIRCRAFT. REPLACED EPSU 13WL, CHECKS OK.

Part: LIGHT — NO TEST (CABIN) · airframe 56,771 hrs · 25,220 cycles

EMERGENCY EGRESS LIGHT TEST FAILS. REPLACED EPSU 13WL, CKS OK.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,470 hrs · 23,679 cycles

DURING "H" CHECK, FOUND SURFACE CORROSION ON AFT LT PASSENGER DOOR SILL AT FR 66. REPAIRED PER EA 32-212484.

Part: POWER SUPPLY — BURNED (EMERGENCY LIGHT) · airframe 45,433 hrs · 19,867 cycles

AFTER TAKEOFF, ALL CREW MEMBERS OBSERVED A BURNING ODOR. CABIN EMERGENCY LIGHTING CIRCUIT BREAKER TRIPPED. RETURNED TO DTW AND LANDED UNEVENTFULLY. REPLACED EMERGENCY LIGHT POWER SUPPLY AND TESTED OK. CHECKED WIRING FOR DAMAGE AND FOUND OK. AIRCRAFT RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,580 hrs · 14,142 cycles

DURING "L" CHECK FOUND CORROSION ON FLOORBEAMS IN AFT GALLEY AREA AT Y765 AND Y1162.5/Y1292. REPAIRED PER EA 32-181716.

Part: FLOORBEAM — CORRODED (BS 13-24)

DURING LINE CHECK, FOUND SOFT FLOOR IN FORWARD GALLEY AREA. FOUND CORROSION ON FLOORBEAMS AND SEAT TRACKS FROM FRAMES FS 13 TO 24. REPAIRED PER SRM 51-72-11 AND NW DWG SA 5346-01004-2.

Part: GUARD — MISSING (GALLEY OVEN)

DURING CLIMB, FLIGHT ATTENDANT REPORTED FIRE IN AFT GALLEY OVEN AND ECAM MESSAGE SMOKE LAVATORY SMOKE WAS RECEIVED. FIRE EXTINGUISHER WAS USED TO PUT OUT THE FIRE AND THE AIRCRAFT RETURNED TO ORIGINATING FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSTALLED MISSING GUARD IN OVEN, CHECKED OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING TEST OF EMERGENCY LIGHT SYSTEM, EXIT LIGHT ABOVE DOOR 2L WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY AND BATTERY PACK, OPERATIONAL CHECK OK.

Part: POWER SUPPLY — FAILED (CABIN)

DURING MAINTENANCE TEST OF EMERGENCY LIGHT SYSTEM, LEFT AFT EMERGENCY LIGHT FAULTED. REPLACED THE LEFT AFT EMERGENCY POWER SUPPLY UNIT, OPERATIONAL CHECK OK.

Part: WIRE — BROKEN (CABIN)

DURING LINE MAINTENANCE CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE AT SEATS 19, 20, 21, 22, 23, AND 24. REPAIRED BROKEN WIRE IN SEAT TRACK.

Part: WIRE — BROKEN (CABIN)

DURING LINE MAINTENANCE, FOUND THE FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE AT SEAT TRACK BETWEEN SEATS 1AB AND 2AB. OPERATIONAL CHECK OK.

Part: WINDSHIELD — SHATTERED (RT COCKPIT)

DURING CLIMB, THE FIRST OFFICER'S WINDSHIELD SHATTERED FOLLOWED BY AN ECAM WINDSHIELD HEAT MESSAGE. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED WINDSHIELD. OPERATIONAL CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (AVIONICS COMPT)

DURING CLIMBOUT, RECEIVED VENT AVIONICS SYS FAULT, FOLLOWED SHORTLY BY VENT EXTRACT FAULT. SEVERAL MINUTES LATER, RECEIVED AVIONICS SMOKE MESSAGE AND GEN 1 LINE SMOKE LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO CLE AND LANDED WITHOUT INCIDENT WITH EMERGENCY EQUIPMENT STANDING BY. MAINTENANCE REPLACED THE AVIONICS EQUIPMENT VENTILATION COMPUTER AND OPERATIONAL CHECK OK.

Part: HMU — MALFUNCTIONED (NR 1 ENGINE)

DURING CLIMBOUT, VIBRATION FROM NR 1 ENGINE WAS FELT THROUGHOUT THE AIRCRAFT ACCOMPANIED BY FLUCTUATIONS IN FUEL FLOW N1, AND THROTTLE POSITION ON ECAM INDICATION. POWER WAS REDUCED, BUT ENGINE PERFORMANCE WAS STILL ERRATIC. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. THE HMU WAS REPLACED AND POWER ASSURANCE CHECK PERFORMED AND THE AIRCRAFT WAS DEEMED OK FOR SERVICE.