N563JB

Part: BLEED VALVE — UNKNOWN · airframe 79,586 hrs · 28,571 cycles

FLT#787, JFK-SXM. "DESCENDING THROUGH 10,000 INFLIGHT CALLED TO INFORM A DIRTY SOCK SMELLIN THE CABIN COMMING FROM ROW 16 TO THE FWD CABIN. CUSTOMERS ALSO NOTIFIED THE ODOR , INFLIGHT DESCROBED THE SMELL AS PERSISTANT AND SAID ODOR REMAINED TILL AFTER BLOCKING IN ( PACKS ); REF INFO NOTICE 2017-T015K REF TSN 05-50-00-810-831A IDENTIFIED SOURCE OF CABIN ODOR TO BE THE APU. PERFORMED PACK 1 AND 2 DECONTAMINATION IAW INFO NOTICE. BOTH PACKS #1 AND #2 OPS CHK OK FOR SERVICE. MDDR #564964 CLEARED MX-4 UPDATED, PLACARDS REMOVED, MCC NOTIFIED. '

Part: UNKNOWN — FUMES (ZONE 200) · airframe 79,002 hrs · 28,354 cycles

FLT#256, BZN-BOS. 'FUMES IN CABIN AT 1500` ON APPROACH. NO APU IN USE.' OPEN

Part: FRAME — CRACKED (FRM 66) · airframe 77,052 hrs · 27,566 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE UPPER INBOA RD AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION IS 12 OCLOCK, AT A FT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1254356 TASKCARD: NR-00013) REF AEROMAN NR 2023-741217 WO 2023 362/1 PERFORMED REPAIR ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE UPPER INBOARD AT DOOR STOP FITTING 7 POSITION AT AFT GALLEY AREA (1 EA) IAW A320 SRM 53-41-12-300-010. THIS REPAIR IS CLASSIFIED AS CATEGORY B , INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT AT 33,000 FC (FH NOT RELEVANT), SUBSEQUENT INSPECTION AT INTERVALS OF 10,700 FC (FH NOT RELEVANT), INSPECTION METHOD: HFEC AND ROTOTEST IAW A320 SRI 53-41-12-205-009 TABLE 001.

Part: FLANGE — CRACKED (FRM 68 S22L) · airframe 77,052 hrs · 27,566 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ONN FR68 LH SIDE HORIZONTAL FLANGE RADIUS AT STR 22LH, CRACK LENGTH .300 INSCH APPROX, AT AFT GALLEY AREA; REF AEM WO: 2023 362/1, NR 2023-741036. ACCOMPLISHED REPAIR ON RADIAL FLANGE STOP FITTING AT FR68,STR22L. PER JB EC A24-108-01 & AEM EA 53-0485-23.

Part: FRAME — CRACKED (FRM 66) · airframe 77,052 hrs · 27,566 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 2 POSITION, CRACK DIRECTION IS 6 OCLOCK, AT AF T GALLEY AREA (1 EA); (RESOLVED ON W/O: 1254356 TASKCARD: NR-00014) REF AEROMAN NR 2023-741218 WO 2023 362/1 PERFORMED REPAIR ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE LOWER INBOARD AT DOOR STOP FITTING 2 POSITION AT AFT GALLEY AREA (1 EA) IAW A320 SRM 53-41-12-300-010. THIS REPAIR IS CLASSIFIED AS CATEGORY B , INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT AT 33,000 FC (FH NOT RELEVANT) , SUBSEQUENT INSPECTION AT INTERVALS OF 10,700 FC (FH NOT RELEVANT), INSPECTION METHOD: HFEC AND ROTOTEST IAW A320 SRI 53-41-12-205-009 TABLE 001.

Part: FRAME — CRACKED (FRM 16) · airframe 77,052 hrs · 27,566 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH DOOR STOP Ñ7 HOLE H3 (LWR / INB), CRAC K DIRECTION AT 4 AND 6 O CLOCK. D= 0.150 INCH; REF AEROMAN NR 2023-741034 WO 2023 362/1 REMOVED AND REPLACED INTERCOSTAL FITTING BTW FR 15 LH TO FR 16 LH AT LEVEL DOOR STOP 7 IAW A320 SRM.

Part: FRAME — CRACKED (FRM 16) · airframe 77,052 hrs · 27,566 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH, DOUBLE JOGGLE AREA, HOLE C. CRACK DI RECTION AT 9 O CLOCK. D= 0.150 INCH; REF AEROMAN NR 2023-741040 WO 2023 362/1 PERFORMED REPAIR ON HOLE C LOCATED ON FRAME 16 RH, DOUBLE JOGGLE AREA, IAW REPAIR INSTRUCTION R53113041.

Part: FRAME — CRACKED (FRM 16) · airframe 77,052 hrs · 27,566 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH, DOUBLE JOGGLE AREA, HOLE Ñ6. CRACK D IRECTION AT 1 O CLOCK. D= 0.130 INCH; REF AEROMAN NR 2023-741038 WO 2023 362/1 PERFORMED REPAIR ON HOLE #6 LOCATED ON FOR 16 RH, DOUBLE JOGGLE AREA, IAW REPAIR INSTRUCTION R53113041.

Part: FRAME — CRACKED (FRM 66) · airframe 77,052 hrs · 27,566 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 6 OCLOCK, AT AF T GALLEY AREA (1 EA); (RESOLVED ON W/O: 1254356 TASKCARD: NR-00015) REF AEROMAN NR 2023-741219 WO 2023 362/1 PERFORMED REPAIR ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE POWER INBOARD AT DOOR STOP FITTING 1 POSITION AT AFT GALLEY AREA (1 EA) IAW A320 SRM 53-41-12-300-011. THIS REPAIR IS CLASSIFIED AS CATEGORY B , INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT AT 31,600 FC (FH NOT RELEVANT), SUBSEQUENT INSPECTION AT INTERVALS OF 5,600 FC (FH NOT RELEVANT), INSPECTION METHOD: HFEC IAW A320 SRI 53-41-12-205-010 TABLE 001 (AREA 2).

Part: STOP FITTING — CRACKED (FRM 68 S22L) · airframe 77,052 hrs · 27,566 cycles

DURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR 68 LH & STR 22 / DOOR STOP FITTING #1 / RADIAL FLANGE FILLET RADIUS / CRACK DAMAGE - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)

Part: SKIN — CORRODED (LT WING) · airframe 77,052 hrs · 27,566 cycles

DURING HEAVY MAINTENANCE: CORROSION ON LH WING TOP SKIN LOWER SURFACE OVERHANG AT TRAILING EDGE AREA BTW RIB 6 AND RIB 7; ACCOMPLISHED THE REPAIR OF CORROSION ON LH WING TOP SKIN PANEL 2 FALSE REAR SPAR TE OVERHANG LOWER SURFACE BETWEEN WX3622-WX4013 IN ACCORDANCE WITH AEROMAN EA 57-0470-23 REV 0 (COVER) AND PART 1-5 AND AIRBUS RDAF 81324016/004/2023#A, & JB EC A24-100-01.

Part: FRAME — CRACKED (FRM 68) · airframe 77,052 hrs · 27,566 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTIONS ARE 3 AND 6 OCLOC K, AT AFT GALLEY AREA (2 EA); (RESOLVED ON W/O: 1254356 TASKCARD: NR-00016) REF AEROMAN NR 2023-741220 WO 2023 362/1 PERFORMED REPAIR ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOARD AT DOOR STOP FITTING 1 POSITION AT AFT GALLEY AREA (2 EA) IAW A320 SRM 53-41-12-300-011. THIS REPAIR IS CLASSIFIED AS CATEGORY B , INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT AT 37,900 FC (FH NOT RELEVANT) , SUBSEQUENT INSPECTION AT INTERVALS OF 5,300FC (FH NOT RELEVANT), INSPECTION METHOD: HFEC IAW SRI 53-41-12-205-010 TABLE 006 (AREA 2).

Part: FLANGE — CRACKED (FRM 68 S22R) · airframe 77,052 hrs · 27,566 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND AO FR 68RH HORIZONTAL FLANGE RADIUS AT STR22RH. CRACK LENGTH 300 INCH, AT AFT GALLEY AREA; REF AEM WO: 2023 362/1, NR 2023-741035. ACCOMPLISHED REPAIR ON HORIZONTAL FLANGE FR 68RH AT STR 22RH. PER JB EC: A24-111-01 & AEM EA 53-0483-23.

Part: FRAME — CRACKED (FRM 16) · airframe 77,052 hrs · 27,566 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH, DOUBLE JOGGLE AREA, HOLE C. CRACK DI RECTION AT 3 AND 10 O CLOCK. D= 0.110 INCH; REF AEROMAN NR 2023-741037 WO 2023 362/1 PERFORMED REPAIR ON HOLE C LOCATED ON FRAME 16 LH, DOUBLE JOGGLE AREA IAW REPAIR INSTRUCTION R53113041.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 77,052 hrs · 27,566 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT AREA CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.200 INCH APPROX, IN COCKPIT (1 EA); REFAEROMAN NR 2023-741053 REMOVED AND REPLACED CONTINUITY FITTINGS IAW REPAIR INSTRUCTION R53112919 AND R53113426 ON WINDSHIELD AREA AND A320 ARM 51-72-11.

Part: FRAME — CRACKED (FRM 16) · airframe 77,052 hrs · 27,566 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH, DOUBLE JOGGLE AREA, HOLE A. CRACK DI RECTION AT 9 O CLOCK. D= 0.160 INCH; REF AEROMAN NR 2023-741039 WO 2023 362/1 PERFORMED REPAIR ON HOLE #A LOCATED ON FOR 16 RH, DOUBLE JOGGLE AREA, IAW REPAIR INSTRUCTION R53113041.

Part: STOP FITTING — CRACKED (FRM 68 S22R) · airframe 77,052 hrs · 27,566 cycles

DURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR 68 RH & STR 22 / DOOR STOP FITTING #1 / RADIAL FLANGE FILLET RADIUS / CRACK DAMAGE - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 76,943 hrs · 27,529 cycles

FLT#1692, LIR-JFK. 'REF L/P 3757835 ITEM # 2 L2 DOOR EMERG. CONTROL HANDLE VERY STIFF WHEN MOVED TO ARM/DISARMED POSITIONS; RE-ADJUSTED AFT L2 DOOR SLIDE GIRT BAR PLACEMENT. REF AMM 25-62-44-420-065-A. ALL OPS NORMAL.'

Part: UNKNOWN — UNKNOWN · airframe 75,053 hrs · 26,813 cycles

FLT#2332, PUJ-SJU. 'BIRD STRIKE ON L.E OF LEFT WING JUST OUTBOARD OF ENG#1.' (SUPPLEMENTAL INFORMATION TO FOLLOW)

Part: CONTROL UNIT — FAILED (10GG) · airframe 74,166 hrs · 26,466 cycles

FLT#706, FLL-EWR. 'ON TAKE OFF AROUND 70KTS WE GOT A BRAKE AUTOBRAKE FAULT BRAKE RELEASED; AS PER TSM 32-42-00-810-819A. PERFORMED BITE TEST OF BSCU IAW AMM 32-46-00 AND FUNCTIONAL TEST OF #2 TACHOMETER IAW AMM 32-42-00-720-002. ALL CHECKS ARE GOOD, COULD NOT DUPLICATE FAULT. REMOVED AND REPLACED BSCU (10GG) IAW AMM 32-42-34. THE OPS CHECK IS GOOD. (BSCU (10GG) PLACED ON SOS).

Part: SELECTOR VALVE — ODOR (CARGO DOOR) · airframe 69,936 hrs · 24,884 cycles

FLT 152, LGA-DEN. CABIN ODOR DURING APPROACH AND LANDING BY FLIGHT ATTENDANTS AND PASSENGER LEVEL 2 PERSISTENT. FOUND AFT CARGO DOOR SELECTOR VALVE LEAKING HYD FLUID REPLACED SELECTOR VALVE AS PER AMM 53-36-00 REPLACED BOTH CABIN RECERC FILTERS ACCOMPLISHED PACK BURN AS PER IN REF 2017-T015I CHANGED BOTH OZONE FILTERS SEE LP 3242738 NO ODOR NOTED.

Part: APU — ODOR · airframe 69,818 hrs · 24,844 cycles

FLT # 648, SLC-BOS. FA'S STATED THAT MUSTY FUMES WERE PRESENT IN THE MID TO AFT CABIN DURING LOW ALT DESCENT AND REMAINED UNTIL THE ENGINES WERE SHUT DOWN ; DETERMINED APU TO BE AT FAULT FOR CABIN ODOR. REFERENCE LP 3242713 ITEM 1 FOR APU DEFECT. DECONTAMINATION OF ECS PERFORMED PER TSM 05-50-00-810-831-A.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 69,528 hrs · 24,753 cycles

FLT 1460, FLL-BDL. GREEN HYD RSVR LOW LEVEL AFTER LANDING EXTENSION FOUND LEAK NEAR MAIN GEAR ON RIGHT SIDE POST RIGHT; R/R R/H GEAR DOOR ACTUATOR FWD BRAIDED HYD LINER IAW AMM 32-31-35 LEAK + OPS CHECKS GOOD. (AN EMERGENCY WAS DECLARED)

Part: APU — ODOR · airframe 69,438 hrs · 24,722 cycles

FLT 939, JFK-SJD. STRONG OIL ODOR ON A/C FIRST ASSITANCE FAS REPORTED SLIGHT ON DESCENT BUT EXTREMELY STRONG ON GROUND ( APU SYSTEM ); PERFORMED INFO NOTICE 2017-T015I AND PLACED APU ON MEL 49-10-01A CAT C.MX4 UPDATED.PLCARD INSTALLED. OPEN

Part: SHEAR PLATE — CRACKED (FRAMES 41-42) · airframe 67,896 hrs · 24,172 cycles

DURING HEAVY MAINTENANCE, FUSELAGE / CENTER FUSELAGE / WING TO FUSELAGE FAIRING RH SUPPORT STRUCTURE FR41-42 SHEAR PLATE / CRACK - PERMANENT REPAIR; THIS REPAIR IS CLASSIFIED AS MAJOR PER JETBLUE EC A21-228-01

Part: ANGLE — DAMAGED (WG-BDY FAIRING) · airframe 67,896 hrs · 24,172 cycles

DURING HEAVY MAINTENANCE, R/H TI ANGLE AT FR 40-41 HAS LWR AFT HOLE OUT OF ROUND; (REF FAS SO# N563JB-01-01 NR# 00283 FAS EO# 21018 & JB E# A321-226) ACCOMPLISHED REPAIR OF ELONGATED HOLE AT THE WING FUSELAGE FAIRING R/H SUPPORT STRUCTURE SHEAR WEB BETWEEN FR 40-41 IN ACCORDANCE WITH FLIGHTSTAR EA 21018 & AIRBUS RDAF 80887754/003/2021 ISSUE A.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,472 hrs · 23,272 cycles

DURING HEAVY MAINTENANCE, INOPERATIVE EPSU AT THE EMERGENCY EXIT LT IN PASSENGER CABIN. REPLACED THE EPSU IAW 33-51-38-400-001-A.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 64,518 hrs · 22,875 cycles

FT 1796, L1 DOOR EMERGENCY EXIT LIGHT COVER MISSING; RE-SECURED L1 DOOR THRESHOLD EMERGENCY EXIT LIGHT ASSY PER AMM. CHECKS OK.

Part: FAN — CONTAMINATED (ENGINE) · airframe 63,711 hrs · 22,601 cycles

FT # 1452, LEVEL 2 FUMES EVENT. ODER NOTICED AT CRUISE AND WAS SPORADIC DIRTY SOCK. ODER NOTIFIED IN COCKPIT AND FRONT GALLEY; EVIDENCE OF OIL FOUND IN THE INNER RIM OF FAN DISC CLEANED OIL AND RE-INSTALLED CONE AND FAIRING AS PER AMM 72-38-11-400-010-A. AS PER TSM 71-00-00-810-801-A LOW PRESSURE TURBINE SHAFT BLIND CAP SEAL NEEDS TO BE REPLACED. AS PER TSM 71-00-00-810-0801-A EXAMINED THE LPC IGV'S FOR OIL WETNESS /PUDDLE AT 6 O'CLOCK POSITION, NO OIL FOUND. PERFORMED BORESCOPE INSPECTION OF THE LPC AS PER AMM 72-00-00-200-017. NO OIL FOUND ALSO PERFORMED BORESCOPE OF THE HPC AS PER AMM 72-00-00-200-016. NO OIL FOUND. R & R ENG 1 LP TURBINE SHAFT BLIND CAP SEAL . REF MM 72-51-41. REF LP 2496658 ITEM 1 AND 2 REF LP 2496657 ITEM 1 AND 2. PERFORMED HIGH POWER ASSURANCE TEST. OPERATE ENGINES AT MULTIPLE POWER SETTING. NO ODOR FOUND. REF MM 71-00-00-710-013. COMPLIED WITH INFORMATION NOTICE 2017-T015D SECTION B. AIRCRAFT IS OK FOR SERVICE.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 62,719 hrs · 22,203 cycles

FT # 319, FLL-SLC. RETURNED TO FIELD. CABIN PRESSURE CONTROL 1+2 FAIL. AIR RETURN; R & R OUTFLOW VALVE IAW AMM 21-31-51.

Part: FLOOR SUPPORT — CORRODED (FRAME 18) · corrosion level 2 · airframe 59,319 hrs · 20,908 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FWD CABIN FLOOR SUPPORT AT Y-254, REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, AND 51-42-11.

Part: DOOR SILL — CORRODED (L2) · corrosion level 2 · airframe 59,319 hrs · 20,908 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE L2 DOOR SILL. REMOVED AND REPLACED THE DOOR SILL IAW AMM SRM 51-71-11, AND 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 18) · corrosion level 2 · airframe 59,319 hrs · 20,908 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FWD CABIN SEAT TRACK Y1292. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 52-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · corrosion level 2 · airframe 59,319 hrs · 20,908 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOOR SUPPORT, -Y1292, FRAMES 68-69. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, PARA 2D.

Part: FLOOR SUPPORT — CORRODED (FRAME 66) · corrosion level 2 · airframe 59,319 hrs · 20,908 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE AFT CABIN FLOOR SUPPORT -765, 2 INCHES FORWARD OF FRAME 66. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, PAR 2D.

Part: DOOR SILL — CORRODED (FRAME 65) · corrosion level 2 · airframe 59,319 hrs · 20,908 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE R2 DOOR SILL FWD OF FRAME 66. REMOVED THE DOOR SILL. FABRICATED TWO ANGLES AND ONE FILLER. TREATED, PRIMED, AND TOP COATED THE REPAIR. INSTALLED IAW SRM 53-41-14-300-001, FIG 001, SHT 5 , REPAIR PRICIPAL 9.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,319 hrs · 20,908 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM -Y1292 HAS CORROSION AT FRAME 66 + 2" FORWARD OF BEAM REF NR 440458-30599, REMOVED AND REPLACED FLOORBEAM -Y1292 FRAME 66 IAW SRM 51-72-11 PARA 2D REF SCR 884892-00018.

Part: FLOOR SUPPORT — CORRODED (FRAME 15) · corrosion level 2 · airframe 59,319 hrs · 20,908 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FWD CABIN FLOOR SUPPORT, INBD OF THE SEAT TRACK, Y504, FRAME 15. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.

Part: DOOR SILL — CORRODED (FRAME 66) · corrosion level 2 · airframe 59,319 hrs · 20,908 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE L2 DOOR SILL. REMOVED AND REPLACED THE DOOR SILL IAW AMM SRM 51-71-11, AND 51-42-11.

Part: DOOR SILL — CORRODED (FRAME 66) · corrosion level 2 · airframe 59,319 hrs · 20,908 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE L2 DOOR SILL. REMOVED AND REPLACED THE DOOR SILL IAW AMM SRM 51-71-11, AND 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 20) · corrosion level 2 · airframe 59,319 hrs · 20,908 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN SEAT TRACK, Y-765, AT FRAME 20. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-72-11, PARA 2D.

Part: FUEL SYS — LEAKING · airframe 58,670 hrs · 20,653 cycles

EMERGENCY DECLARED, DIVERTED PASSING FL 240 AND APPROX 330 KTS, AIRCRAFT BEGAN A SIGNIFICANT VIBRATION. AIRCRAFT WAS SLOWED, AND VIBRATION CEASED AT APPROX 290 KTS. PASSING FL 240, RECEIVED FUEL AUTO FEED FAULT. FUEL PAGE SHOWED 12,000 LBS LEFT INNER TANK, 9,200 IN RT INNER TANK AND QUICKLY DROPPING. RAN FUEL LEAK QRH. WHEN THE NR 2 ENGINE SHUTDOWN, LEAK STOPPED. FOUND MULTIPLE BODY PANEL FASTENERS LOOSE OR MISSING. REPLACED FASTENERS IAW AMM 53-55-00. PERFORMED INSPECTION OF AIRCRAFT FUSELAGE, NO DEFECTS NOTED IAW AMM 53-10-00. INSPECTED THE NR 2 ENGINE, AND NO FUEL LEAK NOTED . ACCOMPLISHED A NR 2 ENGINE WINDMILLING IAW AMM 72-00-00. NO DEFECT NOTED. ALSO ACCOMPLISHED TEST NR 3 IAW AMM 71-00-00. NO LEAKS NOTED. ALL OPS CHECKED OK. ACCOMPLISHED TEST NR 11 HIGH POWER INSURANCE TEST IAW AMM 71-00-00 ON BOTH ENGINES. FUEL CONSUMPTION WAS ON TARGET ON BOTH ENGINES AND ALL OPS CHECKED OK. NO DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: ENGINE — FAILED (NR 2) · airframe 58,174 hrs · 20,464 cycles

REJECTED TAKE-OFF. NR 2 ENGINE FAIL ECAM AT 80 KTS. PERFORMED 05-51-26 INSPECTION IAW AMM 05-51-26 PB 601, NO DISCREPANCY. R & R THE 2 ENGINE.

Part: COFFEEMAKER — FAILED (GALLEY) · airframe 54,639 hrs · 19,146 cycles

PILOT REPORTED AN ELECTRICAL BURNING ODOR WHEN FRONT COFFEE POTS WERE ON. ODOR DISAPPEARED WHEN COFFEE POTS WERE DEACTIVATED. R & R FWD GALLEY NR 1 COFFEEMAKER IAW AMM 25-35-15. PERFORMED OPS TEST. OPS TEST PASSED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,273 hrs · 18,655 cycles

AFT CABIN FLOORBEAM, Y1292 CORRODED AT FRAME 67 + 18". REPLACED BEAM IAW SRM REF 51-42-11 REF NR 440322-32197.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,273 hrs · 18,655 cycles

L2 DOOR SILL CORRODED AROUND FASTENER HOLES FWD OF FRAME 66. REPAIRED IAW SRM REF 53-41-14, INSTALLED 2EA ANGLES REF NR 440322-32242.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,273 hrs · 18,655 cycles

AFT CABIN FLOORBEAM CORRODED AT FRAME 67 AND 67+10 ; Y765. REPLACED BEAM IAW SRM REF 51-72-11, REF NR 440322-32199.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,273 hrs · 18,655 cycles

L2 DOOR SILL CORRODED AROUND FASTENER HOLE FRAME 68. REPAIRED SILL IAW SRM REF 53-41-14 REF NR 440322-32194.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,273 hrs · 18,655 cycles

AFT CABIN RT SIDE FLOORBEAM -Y765 CORRODED AT FR 66+14". REPLACED BEAM IAW SRM REF 51-72-11, REF NR 440322-32200.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,273 hrs · 18,655 cycles

AFT CABIN FLOORBEAM Y1292, CORRODED AT FRAME 67. REPLACED BEAM IAW SRM REF 51-42-11, REF NR 44322-32196.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,273 hrs · 18,655 cycles

AFT CABIN FLOORBEAM Y1291, CORRODED AT FRAME 66. REPLACED BEAM IAW SRM REF 51-42-11, REF NR 440322-32195.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,273 hrs · 18,655 cycles

LT FLOORBEAM CORRODED AT FRAME 66; STR 23L. REPLACED FLOORBEAM IAW SRM REF 51-42-11 REF NR 440322-32307.

Part: LIGHT — INOPERATIVE (L2 DOOR SLIDE) · airframe 43,921 hrs · 15,352 cycles

DURING MAINTENANCE CHECK, FOUND ESCAPE LIGHTING INOPERATIVE ON L2 SLIDE. TROUBLESHOT TO BAD EMERGENCY ESCAPE SLIDE LIGHT. R & R L2 SLIDE ASSY IAW AMM TASK 25-62-44. OPS CHECKED NORMAL.

Part: INTERFACE UNIT — FAILED (LANDING GEAR) · airframe 40,558 hrs · 14,324 cycles

ACFT DIVERTED DUE TO LGCIU FAULT ON ECAM. ON TAKEOFF 3 RED LIGHTS INDICATING GEAR UNLOCKED. ACCOMPLISHED TASK CARD 32-31-00 AND BITE CHECK OF LGCIU1&2. R & R NR 1 LGCIU IAW AMM TASK 32-31-71. ALSO REPLACED LANDING GEAR LEVER (6GA) AS PRECAUTIONARY IAW AMM 32-31-11. ACCOMPLISHED LANDING GEAR SWING IAW AMM 07-11-000. NO DEFECTS NOTED, ALL SYS NORMAL, ACFT OK FOR CONTINUED SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 26,387 hrs · 9,116 cycles

FLT 41 - JFK - MCO FLIGHT ATTENDANTS NOTICED ELECTRICAL ODOR COMING FROM SEAT 24B. LIVE TV SYSTEM WAS TURNED OFF AND THE ODOR WENT AWAY. PERFORMED TSM 24-00-00-810-823. CHECKED SEB AT 24B NO VISUAL DEFECTS NOTED. ACCOMPLISHED INSPECTION AS PER TSM 23-39-00-810-801. DID NOT FIND EVIDENCE OF ARCING, DISCOLORATION OR OVERHEATING. ACCOMPLISHED OPS CHECK.

Part: SEAT — UNSERVICEABLE (CO PILOT) · airframe 8,556 hrs · 2,994 cycles

APPROXIMATELY ONE HOUR INTO FLIGHT, AN ELECTRICAL OR METAL SMELL BECAME INCREASINGLY NOTICEABLE IN COCKPIT, ESPECIALLY ON F/O SIDE. THEN SEEMED TO COME AND GO. PERFORMED TSM TASK 24-00-00-810-823. FOUND F/O'S SEAT ASSY IS CAUSE OF SMELL. REPLACED F/O SEAT REF AMM 25-11-51.

Part: ELECTRICAL BOX — SMOKE (CABIN) · airframe 5,464 hrs · 1,921 cycles

ELECTRIC ODOR COMING FROM 26D. INFO NOTICE 2004-T023TR PERFORMED IN SAN AND FOUND SEB AT 26D WITH ELECTRICAL ODOR. LIVE TV PLACED ON MEL 25-22-03 CAT D, C/N L01825. REMOVED AND REPLACED SEB AT 26D IAW LTV MM 23-39-00, OPS CHECK NORMAL. MEL CLEARED.

Part: ELECTRICAL BOX — FAULTY (ENTERTAIN SYS) · airframe 2,984 hrs · 997 cycles

FLIGHT ATTENDANT REPORTED ELECTRICAL ODOR AROUND ROWS 12 & 13. INSPECTED ROWS 9 THRU 15 PER INFO NOTICE 2003-T050TRA, FOUND 12D VDU INOP, LIVE TV PLACED ON MEL PER 25-22-03, C/B'S ZN 1-3, ZN 1-4 OPENED. UPON ARRIVAL AT JFK PERFORMED INFORMATION NOTICE 2003-T050TRA LV TV SYS INTEGRITY CHECK CONCERNING ELEC ODOR. FOUND EVIDENCE OF ELECTRIC ODOR AND SPILL AT SEB 13R. REMOVED AND REPLACED SEB IAW LV TV AMM 23-39-00. SYSTEM CHECK OK.