N202UW

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,196 hrs · 26,886 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS O/H BIN SEAT 33C AND 37C EMERGENCY BULLNOSE LIGHT INOP. DOOR 1R EXIT IDENTIFIER INOP. OVERHEAD BIN SEAT 1C EMERGENCY BULLNOSE LIGHT INOP. OVERHEAD BIN SEAT 3C EMERGENCY BULLNOSE LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK OK.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 78,716 hrs · 26,738 cycles

AIRCRAFT WAS GROUNDED: FLIGHT DECK FIRST OFFICERS #1 WINDSHIELD IS CRACKED. REPLACED WINDSHIELD PER AMM 56-11-01.

Part: BOTTLE — LOW PRESSURE (L3 DOOR SLIDE) · airframe 77,675 hrs · 26,491 cycles

AIRCRAFT WAS NOT GROUNDED: L3 EMERGENCY EXIT SLIDE LOW PRESSURE. MAINTENANCE REPLACED L3 EMERGENCY EXIT SLIDE PER JOB CARD 19L83525001 AND C/W EA295021.

Part: UNKNOWN — MALFUNCTIONED (HF COMM) · airframe 77,353 hrs · 26,420 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS A/C SUFFERED FROM A DUAL HF RADIO FAILURE VERY SHORTLY AFTER CROSSING INTO ETOPS AIRSPACE. THE MESSAGE WAS RELAYED TO THE CONTROLLING DISPATCHER THROUGH SFO VIA VHF RELAY THROUGH ANOTHER AIRLINE ON 123.4. AFTER REVIEWING THE ETOPS SYSTEMS FAILURE CHECKLIST THE CAPTAIN AND THE DISPATCHER WERE BOTH IN CONCURRENCE THAT IT WAS SAFE TO CONTINUE. AIR TRAFFIC CONTROL CENTER WAS NOTIFIED AT 0831Z THROUGH SFO. NO LOST COMMS PROCEDURES WERE ENACTED AND NO EMERGENCY WAS DECLARED. MAINTENANCE TESTED THE HF SYSTEM IAW AMM 23-11-00-732-014. OPS CHECK WAS GOOD. NO 30 DAY HISTORY.

Part: FRAME — CORRODED (BS 1540) · corrosion level 2 · airframe 77,001 hrs · 26,333 cycles

CORROSION FOUND ON THE FRAME WEB, BS 1540, BETWEEN STRINGERS 28L & 29L. REPAIRED THE FRAME WEB IAW EA 291597.

Part: SHEAR TIE — CORRODED (BS 1540) · corrosion level 2 · airframe 77,001 hrs · 26,333 cycles

CORROSION FOUND ON THE SHEAR TIE AT BS 1540, BETWEEN STRINGER 28L & 29L. REPLACED THE SHEAR TIE IAW SRM 53-60-07-01-1, AND SRM 51-40-02.

Part: PLATE — INOPERATIVE (LIGHT SWITCH) · airframe 76,691 hrs · 26,252 cycles

EMERGENCY LIGHT SWITCH LIGHT PLATE WAS INOPERATIVE ON THE COCKPIT OVERHEAD PANEL. REPLACED THE EMERGENCY LIGHT SWITCH LIGHT PLATE IAW AIPC 33-13-01-02, AND AMM 33-13-01-401. PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 33-13-01-404-006, SUBTASK 714-009.

Part: SKIN — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 77,001 hrs · 26,333 cycles

CORROSION FOUND ON THE FUSELAGE SKIN AT BS 1540, STRINGERS 28L - 29L. REPAIRED THE SKIN IAW SRM 53-00-01-2R-3, REPAIR 3.

Part: OVEN — ODOR (GALLEY) · airframe 76,691 hrs · 26,252 cycles

HAD A TRANSIENT BURNING ODOR JUST AFTER TAKEOFF, SIMILAR TO OVEN TURNING ON. DISSIPATED AFTER A FEW MINUTES. PERFORMED JC 19L00021001 IAW TSI 0081377. REPLACED THE NR 2 FORWARD GALLEY OVEN IAW AMM 25-31-05. OPS CHECKED GOOD. NO ABNORMAL ODOR NOTED AT THIS TIME.

Part: SKIN — CORRODED (LT WING TE FLAP) · airframe 75,818 hrs · 26,041 cycles

CORROSION FOUND ON THE LEFT WING INBOARD TRAILING EDGE FLAP UPPER SURFACE. THE AIRCRAFT WAS GROUNDED. REPAIRED THE FLAP IAW EA 284911.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 75,818 hrs · 26,040 cycles

EXTERIOR EMERGENCY LIGHT, R1 DOOR, WOULDN'T ILLUMINATE DURNING TEST. MAINTENANCE REPLACED M730 AND M735 POWER SUPPLIES AND PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 31-51-00.

Part: SENSOR — OUT OF ADJUST (MLG) · airframe 72,866 hrs · 25,385 cycles

LANDING GEAR DISAGREE LIGHT INBOUND. WHEN GEAR HANDLE WAS PUT TO OFF, GEAR DISAGREE LIGHT WENT OUT AND STAYED OUT WHEN HANDLE WAS PUT BACK TO UP. REMOVED AND REPLACED NOSE LANDING GEAR LOCK ACTUATOR AND LOCK ACTUATOR BOLT IAW AMM 32-34-02. ADJUSTED THE GAPS ON THE NOSE LANDING GEAR UPLOCK & DOWNLOCK SENSORS IAW AMM 32-61-03. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: ACTUATOR — MALFUNCTIONED (MLG) · airframe 72,866 hrs · 25,385 cycles

LANDING GEAR DISAGREE LIGHT INBOUND. WHEN GEAR HANDLE WAS PUT TO OFF, GEAR DISAGREE LIGHT WENT OUT AND STAYED OUT WHEN HANDLE WAS PUT BACK TO UP. REMOVED AND REPLACED NOSE LANDING GEAR LOCK ACTUATOR AND LOCK ACTUATOR BOLT IAW AMM 32-34-02. ADJUSTED THE GAPS ON THE NOSE LANDING GEAR UPLOCK & DOWNLOCK SENSORS IAW AMM 32-61-03. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: BOLT — DAMAGED (MLG) · airframe 72,866 hrs · 25,385 cycles

LANDING GEAR DISAGREE LIGHT INBOUND. WHEN GEAR HANDLE WAS PUT TO OFF, GEAR DISAGREE LIGHT WENT OUT AND STAYED OUT WHEN HANDLE WAS PUT BACK TO UP. REMOVED AND REPLACED NOSE LANDING GEAR LOCK ACTUATOR AND LOCK ACTUATOR BOLT IAW AMM 32-34-02. ADJUSTED THE GAPS ON THE NOSE LANDING GEAR UPLOCK & DOWNLOCK SENSORS IAW AMM 32-61-03. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 72,723 hrs · 25,351 cycles

AIRCRAFT WAS NOT GROUNDED. L1 DOOR EMERGENCY EVACUATION SLIDE PRESSURE IS LOW. REMOVED AND REPLACED SLIDE PER JOB CARD 19L8002502. OPERATIONAL CHECK GOOD.

Part: SEQUENCE VALVE — FAULTY (NLG)

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. NOSE LANDING GEAR LIGHT DISAGREES WITH HANDLES. ALTERNATE GEAR EXTENSION SUCCESSFUL. LANDING UNEVENTFUL. REMOVED AND REPLACED NOSE LANDING GEAR SEQUENCE VALVE PER AMM 32-34-00. OPERATIONAL CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 71,763 hrs · 25,150 cycles

L2 DOOR EMERGENCY POWER RESERVOIR PRESSURE IS LOW. REMOVED AND REPLACED THE BOTTLE IAW AMM 52-11-30. OPERATIONAL CHECKED GOOD.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 71,708 hrs · 25,134 cycles

RIGHT ELEVATOR HAS A TWO INCH CRACK IN THE LOWER INBOARD CORNER AT ES 48, 50 INCHES FROM TRAILING EDGE. REPAIRED IAW SRM 51-70-04-0G, PARAGRAPH 4, AND SRM 55-20-01-2R-1, TABLE II.

Part: POWER SUPPLY — FAILED (CABIN)

AIRCRAFT WAS IN BASE MAINTENANCE. L4 DOOR EMERGENCY ESCAPE SLIDE LIGHT AND EMERGENCY EXIT SIGN FAILED CHECK. REMOVED AND REPLACED POWER SUPPLY M737 IAW AMM 33-51-07-902-001. OPERATIONAL CHECK GOOD..

Part: SKIN PANEL — DELAMINATED (VERTICAL STAB) · airframe 71,708 hrs · 25,134 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATION ON RIGHT VERTICAL STABILIZER FORWARD TORQUE BOX 82 INCHES FROM BOTTOM AND 24 INCHES FROM LEADING EDGE PANEL. REMOVED AND REPLACED PANEL IAW SRM 51-40-02-OG.

Part: ANGLE — CORRODED (BS 1360-1380) · airframe 71,708 hrs · 25,134 cycles

CORROSION ON AFT CARGO INTERCOSTAL UPPER ANGLE AT NUTPLATE ATTACHMENT POINTS, BETWEEN BS 1360 AND 1380, STRINGER 27R. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02-OG

Part: FLOOR SUPPORT — CRACKED (BS 1494) · airframe 71,708 hrs · 25,134 cycles

CRACK IN AFT CARGO FLOOR SUPPORT, BS 1494, LBL 16. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-OG.

Part: LIGHT — UNSECURE (ROWS 11-12) · airframe 71,435 hrs · 25,033 cycles

EMERGENCY LIGHT DETACHING FROM THE FLOOR AT ROW 11 AND 12. MAINTENANCE SECURED THE LIGHT AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — LOOSE (CABIN) · airframe 69,972 hrs · 24,625 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY FLOOR LIGHTING AT SEAT ROW 12 IS COMING LOOSE. SECURED EMERGENCY FLOOR LIGHTING AT SEAT ROW 12.

Part: COVER — LOOSE (R4 DOOR SLIDE) · airframe 69,661 hrs · 24,550 cycles

R4 DOOR SLIDE ARMING MECHANISM BINDING BETWEEN ARMED & UNARMED. PARTS AT FLOOR ARE MISALIGNED. MAINTENANCE FOUND THE ESCAPE SLIDE COVER LOOSE, INSTALLED THE ESCAPE SLIDE COVER IAW AMM 52-11-02-904 AND ACCOMPLISHED A SATISFACTORY OPS CHECK.

Part: GIRT BAR — OBSTRUCTED (R4 DOOR) · airframe 69,632 hrs · 24,546 cycles

R4 DOOR WILL NOT ARM. REMOVED DEBRIS FROM FORWARD SIDE OF GIRT BAR HOLD DOWN POINT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE DOOR ARMING SYSTEM.

Part: OVEN — DIRTY (GALLEY) · airframe 68,716 hrs · 24,325 cycles

AIRCRAFT WAS NOT GNDED. AFT GALLEY NR 1 OVEN SMOKED BADLY WHEN USED. BACK HEATING ELEMENT APPEARS TO NEED TO BE CLEANED. R & R OVEN OPERATIONAL CHECKED GOOD.

Part: LINE — EXPOSED (EVAC SLIDE) · airframe 68,450 hrs · 24,251 cycles

AIRCRAFT WAS NOT GNDED. R1 DOOR SLIDE MOORING LINE PARTIALLY EXPOSED. RE-INSTALLED & SECURED THE R1 DOOR SLIDE MOORING LINE & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — LOOSE (CABIN) · airframe 68,063 hrs · 24,146 cycles

AIRCRAFT WAS NOT GNDED. FLOOR MOUNTED EXIT LIGHTING STRIP AT SEAT 11D NEEDS REPAIR. SECURED LIGHT STRIP & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 67,951 hrs · 24,117 cycles

CATERING REPORTED GIRT BAR HANGING FROM SLIDE ON R1 DOOR. REPLACED GIRT BAR IAW AMM TASK 25-66-10-002-001 ON R1 DOOR. PERFORMED PAX DOOR ESCAPE SYS CHECK TASK 25-66-01-206-041.

Part: LIGHT — UNSECURE (CABIN) · airframe 67,906 hrs · 24,105 cycles

AIRCRAFT WAS NOT GNDED. 18C FLOOR LEVEL EMER LIGHT STRIP PEELING OFF FLOOR. SECURED LIGHT STRIP AT 18C FLOOR.

Part: LIGHT — LOOSE (CABIN) · airframe 67,332 hrs · 23,949 cycles

AIRCRAFT WAS NOT GNDED. ILLUMINATED EMER STRIP ON FLOOR HAS SLID BEYOND ITS TRACK & PAX ARE TRIPPING ON IT. IT’S IN THE FWD GALLEY AREA. RE-ADHERED EMER STRIP IN FWD GALLEY AREA.

Part: SLIDE RAFT — LOW PRESSURE (R4 DOOR) · airframe 67,199 hrs · 23,913 cycles

DOOR R4 SLIDE RAFT LOW PRESS. REPLACED R4 DOOR SLIDE RAFT IAW TASK CARD 19L80025002.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 66,630 hrs · 23,753 cycles

C1 CHECK, R1 DOOR SURROUND EXIT SIGN & L1 DOOR OVERHEAD EXIT SIGN INOPERATIVE. R & R BATTERY CHARGER M731 IAW AMM 33-51-07. OPERATIONAL CHECKED GOOD IAW AMM 33-51-07.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,629 hrs · 23,752 cycles

C1 CHECK, FWD CARGO COMPARTMENT, FLOOR STRINGER AR, RBL 10.45 IS CORRODED AT FUSELAGE STATION 654. REPAIRED STRINGER IAW SRM 53-00-53-1A-1, DETAIL 3 & SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,629 hrs · 23,752 cycles

C1 CHECK, FWD CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT FS 839 IS CORRODED, BETWEEN LBL 25 & RBL 25. FABRICATED & INSTALLED REPLACEMENT ANGLE IAW SRM 53-00-53-1A-1 FIGURE 101 & SRM 51-40-02.

Part: BATTERY — DISCHARGED (CABIN) · airframe 66,629 hrs · 23,752 cycles

C1 CHECK, L3 DOOR EXIT SIGN INOPERATIVE. REPLACED POWER SUPPLY BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-07-201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,629 hrs · 23,752 cycles

C1 CHECK, FWD CARGO COMPARTMENT FLOOR STRINGER AT RBL 7.55 IS CORRODED AT FS 654. FABRICATED & INSTALLED REPLACEMENT STRINGER IAW SRM 53-00-53-1A-101 & SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,629 hrs · 23,752 cycles

C1 CHECK, FWD CARGO COMPARTMENT FLOOR STRINGER AT RBL 16.10 IS CORRODED AT FUSELAGE STATION 654. FABRICATED & INSTALLED REPLACEMENT STRINGER IAW SRM 53-00-53-1A-1, DETAIL 3 & SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,629 hrs · 23,752 cycles

C1 CHECK, FWD CARGO COMPARTMENT, FLOOR STRINGER AT RBL 2.90 IS CORRODED AT FUSELAGE STATION 654. FABRICATED & INSTALLED REPLACEMENT STRINGER IAW SRM 53-00-53-1A-1 DETAIL 3 & SRM 51-40-02.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 66,629 hrs · 23,752 cycles

C1 CHECK, FWD CARGO COMPARTMENT SIDE FLOOR PANEL IS CORRODED AT FUSELAGE STATION 622 & RBL 23. FABRICATED & INSTALLED REPLACEMENT PANEL IAW SRM 53-00-53-1A-1 DET III & SRM 51-40-02.

Part: HARNESS — DEFECTIVE (EVAC SLIDE) · airframe 66,629 hrs · 23,752 cycles

C1 CHECK, L1 DOOR EVACUATION SLIDE HARNESS INOPERATIVE, WILL NOT HOLD SLIDE. REPLACED SLIDE HARNESS IAW AMM 25-66-01-401.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,629 hrs · 23,752 cycles

C1 CHECK, FWD CARGO COMPARTMENT FLOOR STRINGER AT LBL 16.10 IS CORRODED AT FUSELAGE STATION 654. R & R STRINGER IAW SRM 53-00-53 & SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,629 hrs · 23,752 cycles

C1 CHECK, FWD CARGO COMPARTMENT FLOOR STRINGER AT LBL 10.45 IS CORRODED AT FUSELAGE STATION 654. R & R STRINGER IAW SRM 53-00-53 & SRM 51-40-02.

Part: SLIDE — UNSERVICEABLE (R4 DOOR) · airframe 66,629 hrs · 23,752 cycles

C1 CHECK, R4 DOOR EVACUATION SLIDE & RAFT SAFETY PIN ENGAGING BALL MISSING, PIN WILL NOT STAY IN. REPLACED R4 SLIDE & RAFT ON JC 19L80025002.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 66,579 hrs · 23,735 cycles

FLIGHT 743 EN-ROUTE, NR 2 ENG VIBRATION PEGGED AT 5.0, LIMIT GAUGE, CLIMBING THRU FL 280 WITH ENG ANTI-ICE ON IN PRECIPT, SULFUR SMELL. ALSO, COMPRESSOR STALL WITH EGT EXCEEDANCE 826 MAX FOR 3 MIN, DURING COMPRESSOR STALLS. EMER DECLARED, FLIGHT DIVERTED & LANDED WITHOUT FURTHER INCIDENT. ACCOMPLISHED FIM TASK 71-05-00-815-808-ROO, & FIM TASK 71-06-00-815-812-ROO. FOUND ALL PARAMETERS WITHIN LIMITS. ACFT OK FOR SERVICE.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 66,285 hrs · 23,659 cycles

LT OTBD TE FLAP, UPPER LE SKIN HAS A 10 SQUARE INCH AREA OF DAMAGE & MISSING COMPOSITE MATERIAL, LOCATED 110 INCHES FROM THE INBD END. R & R FLAP IAW JC 19L560287001.

Part: SWITCH — INOPERATIVE (CABIN) · airframe 62,916 hrs · 22,722 cycles

EMERGENCY LIGHT SWITCH S10295 ABOVE L4 DOOR INOPERATIVE. REPLACED SWITCH S10295.

Part: SWITCH — INOPERATIVE (CABIN) · airframe 62,801 hrs · 22,685 cycles

MID FWD EMER LIGHT TEST INOPERATIVE. R & R MID FWD EMER LIGHT TEST SWITCH.

Part: BATTERY PACK — DISCHARGED (CABIN)

PHX EMERGENCY LIGHT ABOVE SEATS 3C. R & R BATTERY POWER SUPPLY.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 61,965 hrs · 22,478 cycles

C4 CHECK INTERLAYER CRACKS & MOISTURE INGRESS ON LT NR 1 FLIGHT COMPARTMENT WINDSHIELD AT BS 215, WL250. REPLACED LT NR 1 FLIGHT COMPARTMENT WINDSHIELD AMM 56-11-004-PB 401 & AMM 30-42-03 PB 401.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK CABIN FLOOR PRESS DECK PLATE CORRODED BETWEEN BS 1701 & BS 1720 FROM LBL 54 TO RBL 54. REPAIRED IAW SRM 53-60-51 FIG 201, SRM51-42-01 & EA 505977.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK, LEVEL 2 GALVANIC CORROSION ON L3 DOOR CUT OUT LOWER WEB BETWEEN BS 1320 & BS 1350 & STRINGER 17L. REPLACED L3 DOOR CUT OUT LOWER WEB BETWEEN BS 1320 & BS 1350 & STRINGER 17L IAW SRM 51-10-02, 51-40-02 & 53-60-15.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK, LEVEL 2 GALVANIC CORROSION ON R3 DOOR CUT OUT LOWER WEB BETWEEN BS 1320 & BS 1350 & STRINGER 17R. REPLACED R3 DOOR CUT OUT LOWER WEB BETWEEN BS 1320 & BS 1350 & STRINGER 17R IAW SRM 51-10-02, 51-40-02 & 53-60-15.

Part: SHEAR WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK, CORROSION FOUND ON SHEAR WEB AT BS 1681 & LBL 43. REPLACED SHEAR WEB AT BS 1681 & LBL 43 IAW SRM 51-40-02, FIG 8, 53-0051 & FIG 201.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK, LEVEL 2 GALVANIC CORROSION ON CREASE BEAM INNER CHORD BETWEEN BS 640 TO BS 660, LBL 58.22. REPAIRED CREASE BEAM INNER CHORD BETWEEN BS 640 TO BS 660, LBL 58.22 IAW EA 505975.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK, LEVEL 2 GALVANIC CORROSION ON AFT CABIN DECK PLATE BETWEEN BS 1681.8 TO BS 1720, LBL 50 TO RBL 50. REPAIRED AFT CABIN DECK PLATE BETWEEN BS 1681.8 TO BS 1720, LBL 50 TO RBL 50 IAW SRM 53-60-51, REPAIR 2, FIG 201, SHEET 1-5.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

SY6 C11 CHECK, LEVEL 2 GALVANIC CORROSION ON CREASE BEAM INNER CHORD BETWEEN BS 730 TO BS 760, LBL 63. REPAIRED CREASE BEAM INNER CHORD BETWEEN BS 730 TO BS 760, LBL 63 IAW SRM 53-30-1A-1, FIG 101, 51-40-02 & 51-20-01.

Part: FRAME — BUCKLED (FUSELAGE) · airframe 61,965 hrs · 22,478 cycles

C4 CHECK FRAME BUCKLED AT BS 1420 BETWEEN STRINGER 25L TO STRINGER 26L. REPAIRED FRAME SECTION AT BS 1420 BETWEEN STRINGER 25L TO STRINGER 26L IAW SRM 53-00-07-2R-5, FIG 201 & 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR BEAM UPPER SURFACE AT BS 345 AT RBL 13, 18 & 29. REPAIRED FLOOR BEAM UPPER SURFACE AT BS 345 AT RBL 13, 18 & 29 IAW SRM 51-10-02, 53-00-51-1A-1, FIG 1O1, 53-00-51 & 51-40-02.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN FLOOR ATTACH FITTING AT BS 328, RBL 41. REPLACED CABIN FLOOR ATTACH FITTING AT BS 328, RBL 41 IAW SRM 51-40-02 & 51-40-02-0G.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON R1 DOOR SCUFF PLATE SILL SUPPORT ANGLE BETWEEN BS 333.45 TO BS 365.25, STRINGER 17R. REPLACED R1 DOOR SCUFF PLATE SILL SUPPORT ANGLE BETWEEN BS 333.45 TO BS 365.25, STRINGER 17R IAW SRM 51-40-02, 53-10-15-1A-1, DETAIL 3, 4 & 6, 51-40-05.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON R1 DOOR SILL INBD SUPPORT STRUCTURE BETWEEN BS 324 TO BS 365.25, RBL 60. REPLACED R1 DOOR SILL INBD SUPPORT STRUCTURE BETWEEN BS 324 TO BS 365.25, RBL 60 IAW SRM 53-00-04-1A-1, FIG 101, DETAIL1, SECTION A A.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON SHEAR WEB AT BS 1681, LBL 10. REPLACED SHEAR WEB AT BS 1681, LBL 10 IAW SRM 53-00-51-1A-1, FIG 101, DETAIL 3, 51-40-05 & 51-20-01.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON CREASE BEAM WEB BETWEEN BS 1620 TO BS 1640, LBL 66. REPLACED CREASE BEAM WEB BETWEEN BS 1620 TO BS 1640, LBL 66 IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR BEAM AT BS 345.0, LBL 11. REPAIRED FLOOR BEAM AT BS 345.0, LBL 11 IAW SRM 53-00-51-2R-5 & 51-40-02.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN FLOOR FITTING BETWEEN BS 1250 TO BS 1320, LBL 24.75. REPLACED CABIN FLOOR FITTING BETWEEN BS 1250 TO BS 1320, LBL 24.75 IAW SRM 51-40-02.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FWD CABIN L1 DOOR CUT OUT LOWER SILL SCUFF PLATE SUPPORT ANGLES BETWEEN BS 333.5 TO BS 365.25, LBL 64. REPLACED SCUFF PLATE SUPPORT ANGLES BETWEEN BS 333.5 TO BS 365.25, LBL 64 IAW SRM 51-10-02, 53-10-15-1A-1 & 51-40-02.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 61,965 hrs · 22,478 cycles

C4 CHECK CRACK ON LONGERON AT BS 377, RBL 24.75. REPAIRED LONGERON AT BS 377, RBL 24.75 IAW SRM 51-40-02, 51-40-05, 51-20--01 & 51-21-15.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 61,965 hrs · 22,478 cycles

C4 CHECK CRACK ON SHEAR TIE AT BS 333.5 TO BS 820 BETWEEN STRINGER 16L TO STRINGER 17L. REPLACED SHEAR TIE AT BS 333.5 TO BS 820 BETWEEN STRINGER 16L TO STRINGER 17L IAW SRM 51-40-02 & DWG 140N2002.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FWD CABIN FLOOR ATTACH FITTING AT BS 331.0, LBL 60. REPLACED FLOOR ATTACH FITTING AT BS 331.0, LBL 60 IAW SRM 51-10-02, 51-40-02-OG & 51-40-05.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK, LEVEL 2 GALVANIC CORROSION ON FITTING AT BS 336, LBL 20. REPLACED FITTING AT BS 336, LBL 20 IAW SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK, LEVEL 2 GALVANIC CORROSION ON FITTING AT BS 339, LBL40. REPLACED FITTING AT BS 339, LBL 40 IAW SRM 51-40-02.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK, LEVEL 2 GALVANIC CORROSION ON WEB BETWEEN BS 980 TO BS 1000, LBL 68. REPLACED WEB BETWEEN BS 980 TO BS 1000, LBL 68 IAW SRM 51-10-02, 53-40-13, 51-40-02, 51-40-05 & 51-21-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK, FLOOR SUPPORT CORRODED AT BS 365.25 & BL 0. R & R SUPPORT IAW SRM 51-10-02, 53-00-51-1A & 51-40-21.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK, LEVEL 2 GALVANIC CORROSION ON CHANNEL BETWEEN BS 1300 TO BS 1320, LBL 24.75. REPAIRED CHANNEL BETWEEN BS 130 TO BS 1320, LBL 24.75 IAW SRM 51-10-02, 53-00-04, 51-40-02, 51-40-05 & 51-21-01.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK, CREASE BEAM CHORD CORRODED AT BS 1340 & RBL 64. R & R CHORD IAW SRM 53-60-15-1A, 51-40-02 & 51-40-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK, FLOOR SUPPORT CORRODED BETWEEN BS 700 & BS 720 AT RBL 63. R & R SUPPORT IAW SRM 51-10-02, 53-00-51 & 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK, FLOOR SUPPORT CORRODED AT BS 399 & RBL 49. R & R SUPPORT IAW SRM 53-00-51, 51-40-02 & 51-30-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK, FLOOR SUPPORT CORRODED BETWEEN BS 1300 & BS 1320 AT LBL 22. R & R SUPPORT IAW SRM 53-00-04, 51-40-02 & 51-40-05.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK, CREASE BEAM CHORD CORRODED BETWEEN BS 1260 & BS 1280 AT STRINGER 17R. REPAIRED CREASE BEAM CHORD IAW SRM 51-10-02, 53-60-13, 51-40-02, 51-40-05 & 51-20-01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK, LEVEL 2 GALVANIC CORROSION ON INTERCOSTAL WEB BETWEEN BS 1661 TO BS 1680, RBL 10. REPLACED INTERCOSTAL IAW SRM 53-00-51-1A-1 DETAIL VI, FIG 101, 51-40-02 & 51-20-01.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK, LEVEL 2 GALVANIC CORROSION ON CREASE BEAM INBD CHORD AT BS 1320, LBL 60. REPLACED CREASE BEAM INBD CHORD AT BS 1320, LBL 60 IAW SRM 53-60-15, FIG 101, 51-40-05, 51-40-02 & 51-20-01.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK, LEVEL 2 GALVANIC CORROSION ON CREASE BEAM WEB BETWEEN BS 1350 TO BS 1360, STRINGER 17L. REPAIRED CREASE BEAM WEB BETWEEN BS 1350 TO BS 1360, STRINGER 17L IAW SRM 51-40-02 & DWG 146N8322.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,965 hrs · 22,478 cycles

C4 CHECK, LEVEL 2 GALVANIC CORROSION ON WEB BETWEEN BS 1300 TO BS 1320, RBL 64. REPLACED WEB BETWEEN BS 1300 TO BS 1320, RBL 64 IAW SRM 53-60-15-1A, 51-40-02, 51-40-05 & 51-020-01.

Part: BEARING — SEIZED (L2 DOOR) · airframe 61,502 hrs · 22,328 cycles

CLT L2 AX HANDLE DIFFICULT TO MOVE TO OPEN POSITION. R & R EXTERIOR HANDLE DUE TO BAD BEARING.

Part: COLLAR — DEFECTIVE (L2 DOOR) · airframe 61,489 hrs · 22,324 cycles

PHL L2 DOOR GUST LOCK INOPERATIVE. R&R L2 DOOR GUST HOLD OPEN LOCK COLLAR.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 60,838 hrs · 22,156 cycles

PHOTOLUMINESCENT STRIP AT ROW 26R DAMAGED. R & R STRIP.

Part: SHAFT SEAL — LEAKING (RT ENGINE) · airframe 59,957 hrs · 21,917 cycles

EN-ROUTE, DURING CRUISE FLIGHT, THE RT ENG OIL QTY DROPPED TO A "0" INDICATION. THE OIL TEMP REMAINED NORMAL, AND OIL PRESS FLUCTUATED BETWEEN GREEN AND AMBER. THE FLIGHT DIVERTED. THE RT ENG WAS AT IDLE FOR 1HR 40MINS. MX R & R THE ACCESSORY GEARBOX TOWER SHAFT SEAL. LEAK AND OPS CK GOOD.

Part: HANDLE — OUT OF ADJUST (L2 DOOR)

CLT - NUMBER 2L PAX DOOR OUTSIDE DOOR HANDLE NOT FLUSH WITH AIRCRAFT WHEN DOOR IS CLOSED. ADJUSTED & LUBED EXTERIOR HANDLES. OPS CHECK GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 58,736 hrs · 21,548 cycles

CLT - EMERGENCY LIGHT FLOOR STRIP BY ROW 12 A/C LEFT IS LOOSE. RE-SECURED FLOOR STRIP WITH CARPET TAPE.

Part: COVER — MISSING (CABIN) · airframe 57,882 hrs · 21,248 cycles

CLT - CLEAR PLASTIC STRIP COVERING FLOOR MOUNT GREEN FLUORESCENT EMERGLOW LEVEL LIGHTING IS MISSING A/C LEFT AT SEATS 8 THRU 10. REPLACED FLOOR ESCAPE PATH LIGHTING RACEWAY PLASTIC COVER ROW 8 THRU 10 L.

Part: METERING VALVE — FAILED (CABIN PRESSURE) · airframe 57,852 hrs · 21,237 cycles

SJU - FLT 1072 EN ROUTE. EICAS MESSAGE FOR CABIN ALTITUDE. CABIN ALTITUDE PLUS CABIN ALTITUDE LIGHT ON. COULD NOT CONTROL CABIN PRESSURE IN MANUAL MODE. UNABLE TO CONTROL CABIN ALTITUDE IN ANY MODE. A GRADUAL DESCENT TO 10,000 FT WAS MADE. FLIGHT RETURNED TO FIELD. NO EMERGENCY DECLARED AND FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED CABIN PRESSURE SELECTOR PANEL ASSEMBLY. OPS CHECKED OK. INTERMITTENT OUTPUT. PRIMARY FAILURE WAS VALVE METER. CONTRIBUTING FAILURE WAS THE MODE SELECT SWITCH. REPLACED VALVE METER AND MODE SELECT SWITCH.

Part: STRUCTURE — DAMAGED (LT PYLON) · airframe 57,053 hrs · 20,985 cycles

C3 CHECK. LEFT PYLON INBOARD LOWER CHORD LOWER BOLT HOLE ELONGATED. REPAIRED CHORD IAW EA104119.

Part: SKIN — WORN (FUSELAGE) · airframe 57,053 hrs · 20,985 cycles

C3 CHECK - FUSELAGE SKIN WORN AT BS 1650, BL 0 (AFT WATER SERVICE PANEL AREA). REPAIRED SKIN IAW EA 104127.

Part: STRUCTURE — DAMAGED (LT PYLON) · airframe 57,053 hrs · 20,985 cycles

C3 CHECK - LEFT PYLON INBOARD LOWER CHORD UPPER BOLT HOLE ELONGATED. REPAIRED CHORD IAW EA 104119.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 57,053 hrs · 20,985 cycles

C3 CHECK - RIGHT INBOARD AFT FLAP TRAILING EDGE WEDGE UPPER SKIN DISBONDED AT INBOARD AFT CORNER. REPAIRED SKIN IAW EA 1041551 AND B757 SRM 57-53-01 REPAIR 1.

Part: MOUNT BRACKET — CRACKED (EVAC SLIDE) · airframe 57,053 hrs · 20,985 cycles

C3 CHECK - L3 DOOR ESCAPE SLIDE LOWER AFT MOUNT BRACKET CRACKED. REPLACED L3 DOOR ESCAPE SLIDE IAW JOB CARD 19C8352505.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,053 hrs · 20,985 cycles

C3 CHECK - EXFOLIATION CORROSION ON STRINGER SUPPORT AT BS 1470, LBL 77. REPAIRED STRINGER SUPPORT AT BS 1470, LBL 77 IAW B757 SRM 51-70-11.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,053 hrs · 20,985 cycles

C3 CHECK - EXFOLIATION CORROSION ON STRINGER SUPPORT AT BS 1470, LBL 3. REPAIRED STRINGER SUPPORT AT BS 1470, LBL 3 IAW B757 SRM 51-70-11.

Part: SKIN — WORN (TE FLAP) · airframe 57,053 hrs · 20,985 cycles

C3 - LEFT MAIN INBOARD FLAP TOP SURFACE HAS WORN AREA AT WING STA 204, 3.5 FEET FROM EDGE OF MID FLAP. REPAIRED LEFT MAIN INBOARD FLAP AT WING STA 204, 3.5 FEET FROM EDGE OF MID FLAP IAW B757 SRM 51-70-10, 57-53-01.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 57,053 hrs · 20,985 cycles

C3 CHECK - RIGHT ELEVATOR PREVIOUS SKIN REPAIR DELAMINATED FROM STA 241 TO 254 AT TRAILING EDGE. REMOVED AND REPLACED RIGHT ELEVATOR.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 57,053 hrs · 20,985 cycles

C3 CHECK - RIGHT ELEVATOR TRAILING EDGE WEDGE UPPER AND LOWER SKINS DISBONDED BETWEEN ES 241 AND ES 254. REPAIRED IAW CMM 55-20-15 REV 19.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,451 hrs · 20,805 cycles

EMERGENCY LIGHTS ROW 17 & 14L INOPERATIVE. MAINTENANCE REMOVED & REPLACED EMERGENCY LIGHT ASSEMBLY AT ROW 17, OPERATIONAL CHECK IS GOOD.

Part: GIRT BAR — DETACHED (L4 DOOR) · airframe 55,472 hrs · 20,492 cycles

AMS - CREW REPORTS NOT POSSIBLE TO DISARM AFT DOOR 4L. RE-ATTACHED GIRT BAR ON DOOR 4L.

Part: BOTTLE — LOW PRESSURE (L4 DOOR)

AMS - FOUND L4 DOOR ASSIST BOTTLE WITH LOW PRESSURE. REPLACED L4 DOOR ASSIST BOTTLE.

Part: MECHANISM — OUT OF ADJUST (L4 DOOR) · airframe 54,604 hrs · 20,255 cycles

CLT - 4L DOOR HANDLE DOES NOT MOVE TO THE DISARM MARK-DOES NOT ALIGN WITH DISARM. ACCOMPLISHED ADJUSTMENT OF GIRT BAR MECHANISM. SYS CHECK GOOD.

Part: OVEN — DEFECTIVE (GALLEY) · airframe 54,147 hrs · 20,133 cycles

PHX - FLT 1197 EN ROUTE PHL TO PHX. OVEN AT G1A DEFECTIVE, STRONG ELECTRICAL SMELL WHEN ATTEMPTING USE. MAINTENANCE ACTION WAS DEFERRED BY PLACING THE G1A GALLEY NR 1 OVEN ON MEL. MAINTENANCE REMOVED AND REPLACED G1A OVEN. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 53,711 hrs · 20,025 cycles

PHL - FLASHLIGHT NEEDS NEW BATTERY AFT GALLEY. REPLACED BATTERY AT AFT GALLEY, OPS CHECK OK.

Part: GLOWSTRIP — UNSECURE (CABIN)

CLT - EXIT PATH LIGHT ROW 11 A/C L LIFTING UP. MAINTENANCE SECURED TRACK AS REQUIRED.

Part: DOOR SEAL — WORN (OVEN)

CLT FLT 1035 EN ROUTE SJU TO CLT. THE CABIN CREW REPORTED A MOMENTARY "BURNED RUBBER" ODOR IN THE AFT GALLEY OF THE AIRCRAFT. THE ODOR DISSIPATED ON ITS OWN. THE FLIGHT CONTINUED AND LANDED IN CLT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE DOOR SEAL ON THE NUMBER ONE AFT GALLEY OVEN WORN. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE AFT GALLEY OVEN.

Part: ELEVATOR — DELAMINATED (RIGHT) · airframe 52,091 hrs · 19,199 cycles

CLT - MAJOR REPAIR - C2 - RIGHT ELEVATOR HAS 7 INCH BY 1 INCH LONG AREA OF DELAMINATION AT TRAILING EDGE FROM ELEVATOR STATION 245 TO 252. ELEVATOR WAS REMOVED, SENT TO VENDOR REPAIRED, THEN RE-INSTALLED PER JOB CARD 19I33027002.

Part: ELEVATOR — DELAMINATED (ZONE 300) · airframe 52,091 hrs · 19,499 cycles

CLT - C2 - MAJOR REPAIR - DELAMINATION ON RIGHT ELEVATOR AT ELEV STA 245 TO 252. REMOVED ELEVATOR, SENT TO VENDOR FOR REPAIR & RE-INSTALLED SAME ELEVATOR IAW B757 SRM 55-20-01-2R01, 51-70-17 & JOB CARD 19I33027002.

Part: STRAP — CRACKED (FUSELAGE) · airframe 52,091 hrs · 19,499 cycles

CLT - C2 - MAJOR REPAIR - CRACK IN FLOOR SUPPORT STRAP AT BS 365, LBL 20. REPAIRED FLOOR SUPPORT STRAP AT BS 365, LBL 20 IAW TYPICAL REPAIR 53-35-01.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 52,091 hrs · 19,499 cycles

CLT - C2 - MAJOR REPAIR - DELAMINATION ON LOWER SIDE OF NR 5 SLAT WEDGE 16 INCHES OUTBOARD FROM INBOARD END. REPAIRED NR 5 SLAT WEDGE IAW B757 SRM 51-70-10.

Part: STOP FITTING — CRACKED (R4 DOOR) · airframe 52,091 hrs · 19,499 cycles

CLT - MAJOR REPAIR - C2 - CRACK ON R4 DOOR STOP TEE CLIP AT BS1681.8, STR 10R. REPLACED R4 DOOR STOP TEE CLIP AT BS 1681.8, STR 10R IAW ENGINEERING AUTHORIZATION 102346.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 52,091 hrs · 19,499 cycles

CLT - C2 - MAJOR REPAIR - CRACK IN R4 DOOR WAY AT NR 3 DOOR STOP TEE CLIP AT BS 1681.8, S10R. REPLACED R4 DOOR WAY AT NR 3 DOOR STOP TEE CLIP AT BS 1681.8, S10R IAW EA 102346.

Part: MOTOR — BURNED (SEAT)

FLT 750 WHILE EN-ROUTE, DURING FLIGHT, SEAT 3C MOTOR OVERHEATED. HOT ACRID SMELL FROM UNDER SEAT. SPARKS FROM AREA POWER DISCONNECTED. THE FLIGHT DIVERTED TO YJT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND VACUUM MOTOR FOR LUMBAR BAGS BURNT. REMOVED AND REPLACED VACUUM MOTOR. ALSO FOUND CHAFED WIRING HARNESS TO RIGHT SEAT. REMOVED AND REPLACED WIRING HARNESS.

Part: TRANSFORMER — FAULTY (TE FLAPS)

CLT FLT 1728 EN ROUTE MCO TO CLT. DURING APPROACH, TRAILING EDGE AND LEADING EDGE FLAPS FAILED TO EXTEND NORMALLY. LEADING EDGE EXTENDED BY ALTERNATE. TRAILING EDGE FLAPS NEVER INDICATED MOVEMENT, EVEN AT ALTERNATE 15 FLAP GAUGE NEVER MOVED. TRAILING EDGE ALTERNATE POSITION RESULTED IN LEADING EDGE DISAGREE. REMOVED AND REPLACED TRANSFORMER T10040 28AC TRANSFER BUSS LEFT TRANSFORMER.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 49,098 hrs · 18,646 cycles

PHX - B1 - MAJOR REPAIR - NR 5 SLAT T/E WEDGE SURFACE HAS 2 AREAS OF DELAMINATION FROM ISS104 TO ISS150. REPAIRED NR 5 SLAT T/E UPPER SURFACE IN BEND FROM ISS104 TO ISS150 IAW B757 SRM 51-70-10.

Part: SKIN — CORRODED (NR 2 NACELLE) · airframe 46,574 hrs · 18,056 cycles

CLT - C1 - MAJOR REPAIR - CRACK IN NR 2 ENGINE NACELLE STRUT AT 7 O'CLOCK POSITION IN ALUMINUM CHORD IN OUTBOARD AFT HINGE FITTING UPPER AFT FASTENER HOLE. REPAIRED NR 2 ENGINE NACELLE STRUT OUTBOARD AFT HINGE FITTING UPPER AFT FASTENER HOLE IAW US AIRWAYS EA 100950.

Part: LIGHT — INOPERATIVE (EVAC SLIDE)

PHL - THE R4 DOOR EMERGENCY ESCAPE SLIDE LIGHT WAS FOUND INOPERATIVE. MAINTENANCE RELAMPED THE R4 DOOR EMERGENCY ESCAPE SLIDE LIGHT.

Part: SLIDE — DEFECTIVE (R1 DOOR)

THE EVACUATION SLIDE ARMING LEVER WAS BINDING AT SERVICE DOOR 1R. MX REPLACED THE 1R DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERVICE.

Part: COUPLER — INOPERATIVE (HF ANTENNA)

DUB - FLT 723 EN ROUTE DUB TO PHL. BOTH HF RADIOS BECAME INOPERATIVE DURING THE FLIGHT. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT HF ANTENNA COUPLER. OPERATIONALLY CHECKS OK.

Part: COUPLER — INOPERATIVE (HF ANTENNA)

DUB - FLT 723 EN ROUTE DUB TO PHL. BOTH HF RADIOS BECAME INOPERATIVE DURING THE FLIGHT. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT HF ANTENNA COUPLER. OPERATIONALLY CHECKS OK.

Part: TRANSCEIVER — INOPERATIVE (HF COMM)

DUB - FLT 723 EN ROUTE DUB TO PHL. BOTH HF RADIOS BECAME INOPERATIVE DURING THE FLIGHT. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT HF RADIO TRANSCEIVER. OPERATIONALLY CHECKS OK.

Part: TRANSCEIVER — INOPERATIVE (HF COMM)

DUB - FLT 723 EN ROUTE DUB TO PHL. BOTH HF RADIOS BECAME INOPERATIVE DURING THE FLIGHT. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT HF RADIO TRANSCEIVER. OPERATIONALLY CHECKS OK.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

MCO - THE FLASHLIGHT NEAR THE L2 DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT.

Part: PROXIMITY SWITCH — INOPERATIVE (L1 GIRT BAR) · airframe 42,778 hrs · 17,202 cycles

BFM - EES - C4 CHECK - SLIDE LIGHT INOPERATIVE ON ALL DOORS. REPLACED AND OPERATIONAL CHECKED THE L1 DOOR GIRT BAR PROXIMITY SWITCH IAW B757 AMM 25-66-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,778 hrs · 17,202 cycles

BFM - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT PRESSURE PLATE TIE DOWN FITTING, BS 1681. REPLACED CABIN FLOOR SUPPORT PRESSURE PLATE TIE DOWN FITTING, BS 1681 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,778 hrs · 17,202 cycles

BFM - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT WEB ANGLE, BS 1661 - BS 1682, RBL 12. REPLACED CABIN FLOOR SUPPORT WEB ANGLE, BS 1661 - BS 1682, RBL 12 IAW B757 SRM 51-40-02.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,778 hrs · 17,202 cycles

BFM - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR PRESS PLATE, BS 1681 - BS 1720, LBL 56 - RBL 56. REPAIRED CABIN FLOOR PRESS PLATE, BS 1681 - BS 1720, LBL 56 - RBL 56 IAW B757 SRM 53-60-51.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,778 hrs · 17,202 cycles

BFM - MAJOR REPAIR - C4 CHECK - NR 6040676, LEVEL 2 CORROSION ON FLOOR SUPPORT, BS 1681, RBL 56. REPLACED FLOOR SUPPORT, BS 1681, RBL 56 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,778 hrs · 17,202 cycles

BFM - MAJOR REPAIR - C4 CHECK - NR 6040672, LEVEL 2 CORROSION ON CABIN FLOOR STRUCTURE INTERCOSTAL, BS 1661 - BS 1682, RBL 56. REPLACED CABIN FLOOR STRUCTURE INTERCOSTAL, BS 1661 - BS 1682, RBL 56 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,778 hrs · 17,202 cycles

BFM - MAJOR REPAIR - C4 CHECK - NR 6040671, LEVEL 2 CORROSION ON CABIN FLOOR STRUCTURE INTERCOSTAL, BS 1641 - BS 1661, BL 56. REPLACED CABIN FLOOR STRUCTURE INTERCOSTAL, BS 1641 - BS 1661, BL 56 IAW B757 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,778 hrs · 17,202 cycles

BFM - MAJOR REPAIR - C4 CHECK - NR 6039970, LEVEL 2 CORROSION ON CABIN FLOORBEAM PREVIOUS REPAIR, BS 377.7, LBL 1 - LBL 20. REPLACED CABIN FLOORBEAM, BS 377.7, LBL 1 - LBL 20 IAW B757 SRM 53-15-01.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 42,778 hrs · 17,202 cycles

BFM - MAJOR REPAIR - C4 CHECK - NR 6039999, CORROSION ON CABIN FLOOR SUPPORT, BS 343- BS 365, RBL 62, WL 208. REPLACED CABIN FLOOR SUPPORT, BS 343- BS 365, RBL 62, WL 208 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 42,778 hrs · 17,202 cycles

BFM - MAJOR REPAIR - CORROSION ON CABIN FLOOR SUPPORT, BS 365 - BS 395, BL 0, WL 208. REPLACED CABIN FLOOR SUPPORT, BS 365 - BS 395, BL 0, WL 208 IAW B757 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,778 hrs · 17,202 cycles

BFM - MAJOR REPAIR - C4 CHECK - NR 6040679, LEVEL 2 CORROSION ON CABIN FLOORBEAM, BS 1640, BL 0. REPLACED CABIN FLOORBEAM, BS 1640, BL 0 IAW B757 SRM 53-15-01.

Part: SEAT TRACK — CORRODED (BS 1520-1640) · airframe 42,778 hrs · 17,202 cycles

BFM - MAJOR REPAIR - C4 CHECK, LEVEL 2 CORROSION ON CABIN SEAT TRACK, BS 1520 - BS 1640, BL 24.75. REPLACED CABIN SEAT TRACK, BS 1520 - BS 1640, BL 24.75 IAW B757 SRM 53-00-52.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 42,778 hrs · 17,202 cycles

BFM - MAJOR REPAIR - C4 CHECK - NR 6039997, CORROSION ON CABIN FLOOR SUPPORT, BS 343 - BS 365, RBL 45, WL 208. REPLACED CABIN FLOOR SUPPORT, IAW B757 SRM 51-40-02.

Part: CREASE BEAM — CORRODED (ZONE 200) · airframe 42,778 hrs · 17,202 cycles

BFM- MAJOR REPAIR - C4 CHECK - CORROSION ON CREASE BEAM, BS 324 - BS 377, RBL 62. REPLACED CABIN FLOOR SUPPORT, BS 324 - BS 377, RBL 62 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,778 hrs · 17,202 cycles

BFM - MAJOR REPAIR - C4 CHECK - NR 6040673, LEVEL 2 CORROSION ON INTERCOSTAL, BS 1640 - BS 1661, BL 0. REPLACED CABIN FLOOR SUPPORT, BS 324 - BS 377, RBL 62 IAW B757 SRM 51-40-02.