N196DN

Part: SWITCH — INOPERATIVE (ZONE 200) · airframe 120,179 hrs · 17,851 cycles

EMERGENCY LIGHT S/W FWD INOP. REMOVED & REPLACED S//W S'1 IAW B767 AMM / WD 33-51-11 OPS CHK OK. A/C OK FOR SVC (7880350)

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 118,736 hrs · 17,594 cycles

RIGHT OVERWING AFT EMERGENCY EXIT ESCAPE LIGHT INOPERATIVE. R & R THE AFT RT OVERWING EXIT SIGN LIGHT ASSY IAW AMM 33-51. OPS CHECKED GOOD. MEL CLEARED. (7070197)

Part: SKIN — CRACKED (ZONE 400) · airframe 118,665 hrs · 17,580 cycles

CRACK ON #1 PYLON SKIN, STARTING ON AFT BOTTOM CORNER OF ACCESS 436BR. REMOVED CRACKED EXISTING #1 ENGINE STRUT SIDE SKIN CUTOUT AT AFT TRAPEZOIDAL ACCESS DOOR REPAIR DOUBLER AND INSTALLED REPLACEMENT REPAIR DOUBLER IAW B767 SRM 54-53-01-2R-7 STEPS 5-17. (1158031)

Part: STRAP — CRACKED (ZONE 100) · airframe 118,660 hrs · 17,579 cycles

STRAP CRACKED AT FS325, RBL12, WL192.5. C/W ER/A 628614-14 REV ORIGINAL (1154135)

Part: LENS — DIRTY (ZONE 200) · airframe 118,322 hrs · 17,529 cycles

SHIP 0196 2L DOOR REMAINS ARMED WITH ARM LIGHT AND SLIDE LIGHT AFTER DOOR IS DISARMED. CORRECTIVE ACTION: CLEANED LIGHT LENS SIDES NOW OPS CK GOOD REF 67AMM 52-11. (7049949).

Part: INDICATOR — FAULTED (ZONE 200) · airframe 117,388 hrs · 17,388 cycles

SHIP 0196 -DIV- FLIGHT DIVERTED TO JFK DUE TO F/O ELECTRIC ALTIMETER FLAG IN VIEW. CORRECTIVE ACTION: REPLACED INDICATOR. (LP 7079394)

Part: CONTROL PANEL — MALFUNCTIONED (ZONE 200) · airframe 117,060 hrs · 17,322 cycles

THE CABIN EMERGENCY LIGHTS WON'T TURN OFF AT AFT FLIGHT ATTENDENT PANEL. MAINTENANCE HAD TO RESET FLIGHT ATTENDENT LIGHT CONTROL PANELS PER B767-300 FIM 24-00. CABIN EMERGENCY LIGHTS NOW OPERATE AS NORMAL AT THIS TIME. (LP #6763931)

Part: BULB — MISSING (ZONE 200) · airframe 115,614 hrs · 17,040 cycles

SHIP 196 ROW 34 RT SEAT EMER LIGHT MISSING BULBS. CORRECTIVE ACTION: REMOVED AND REPLACED ROW 34 RT SIDE SEATS ESCAPE PATH LIGHT ASSEMBLY PER B767 AMM 33-51-10. OP'S TEST GOOD. (6459560)

Part: LIGHT — DAMAGED (ZONE 200) · airframe 114,859 hrs · 16,932 cycles

SHIP 196 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:32F. CORRECTIVE ACTION: RESECURED LIGHT ASSY AT SEAT 32F,OPS CKS NML. (0528243)

Part: DOOR — OUT OF RIG (L1) · airframe 113,843 hrs · 16,784 cycles

SHIP 0196 -ATO- @ 50-55 KNOTS DUE TO LT FWD (L1) ENTRY DOOR INDICATION. CORRECTIVE ACTION: JFK MTC RIGGED DOOR. A/C RTS. (LP 533088)

Part: MECHANISM — FOD (R1 DOOR) · airframe 113,391 hrs · 16,720 cycles

SHIP 196 F/A REPORTED R1 DOOR WAS UNABLE TO BE ARMED, HANDLE WAS STUCK. CORRECTIVE ACTION: PERFORMED OPS CHECK PER B767 AMM 52-11. FOUND DEBRIS ON LOWER DOOR MECHANISM. OPS NML. OK FOR SVC. (5928404)

Part: LIGHT — DAMAGED (CABIN) · airframe 112,555 hrs · 16,598 cycles

SHIP 196 48F EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. CORRECTIVE ACTION: SECURED 48F FLOOR PROX EMERGENCY LIGHT ASSY AND CHKED NML PER B767 AMM 33-51 (5292705)

Part: WARNING LIGHT — NO INDICATION (R1 DOOR) · airframe 112,149 hrs · 16,530 cycles

SHIP 196 1R ENTRY DOOR NOT SHOWING ARMED LIGHT ILLUMINATED ON FWD FLIGHT ATTENDANT PANEL OR ON DOOR ITSELF. CORRECTIVE ACTION: PERFOMED INSPECTION OF VISUAL INDICATION OF THE SLIDE GIRT BAR OF DOOR 1R. YELLOW INDICATION ITS OK. (5037894)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 112,038 hrs · 16,511 cycles

SHIP 196 SEAT 51GF EMERGENCY LIGHT BROKEN. CORRECTIVE ACTION: REPLACED EMERGENCY LIGHT SHROUD AT SEAT 51GFIAW B767 AMM 33-51- 10. OPS CHECK OK (5037816)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 111,940 hrs · 16,494 cycles

SHIP 196 1R DOOR SLIDE ARMED LIGHT INOP. CORRECTIVE ACTION: FOUND CONNECTOR UNATTACHED. RESECURED, OPS NML B767-300 AMM 52- 73. (5036464)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 111,165 hrs · 16,371 cycles

SHIP 196 DOOR 1R ARMING LEVER IS EXTREMELY HARD TO ARM. CORRECTIVE ACTION: CLENING DOOR FRAME OUTLINE . CHECKED AND TESTED IAW B767/300 AMM 25-66-01 SATISF OK . REV 138.02 . CKD OK (6742319)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 111,145 hrs · 16,368 cycles

2L DOOR HANDLE DISARMED BUT ARMED LIGHT ILLUMINATED. FA FORWARD PANEL SHOWS ARMED. DEFER TO MEL 52-11-01. PLCD INST. 'M' PROC C/W. (6742309)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 111,076 hrs · 16,353 cycles

SHIP 196 RH WING FIXED LEADIND EDGE AIRLOAD RIB AFT FITTING AT OSS 664.58 FOUND CRACK. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767 SRM 51-40. (2989325)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 111,076 hrs · 16,353 cycles

SHIP 196 FOUND LH SIDE LOWER SKIN PANEL IN SECTION 48 UNDER PANEL 313CLX FRONT CORNER,BETWEEN STA1725.5 AND 1746.125. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767 SRM 53-80-01. (2989311)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 111,076 hrs · 16,353 cycles

SHIP 196 WHEN PERFOREM DETAIL INSPECTION OF WORAKCARD 5300-0780 STEP15 REQUIRED , FOUND 01EA SHEAR TIE CORRODED AT STA 1540 STR39L AND 38L. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767 SRM 51-40. (2989389)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 111,076 hrs · 16,353 cycles

SHIP 196 FOUND LH SIDE FORWARD SKIN PANEL IN SECTION 48 UNDER PANEL 313CLX FRONT CORNER,BETWEEN STA1725.5 AND 1746.12 CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767 SRM 53-80-01. (2989273)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 111,076 hrs · 16,353 cycles

SHIP 196 FOUND RH SIDE LOWER SKIN PANEL IN SECTION 48 UNDER PANEL 314CRX FRONT CORNER,BETWEEN STA1725.5 AND 1746.125. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767 SRM 53-80-01. (2989301)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 111,076 hrs · 16,353 cycles

SHIP 196 FOUND RH SIDE FORWARD SKIN PANEL IN SECTION 48 UNDER PANEL 314CRX FRONT CORNER,BETWEEN STA1725.5 - 1746.125. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767 SRM 53-80-01. (2989287)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 111,076 hrs · 16,353 cycles

SHIP 196 DELAMINATION FOUND ON THE LH SIDE VERTICAL STABILIER EXTERNAL SKIN WHICH IS BETWEEN AUXLIARY SPAR AND FRONT SPAR FSS 39 TO FSS 92. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767 SRM 55-30-01-2R-1&SRM 51-70-10. (2987797)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 111,076 hrs · 16,353 cycles

SHIP 196 DELAMINATION FOUND ON THE LH SIDE VERTICAL STABILIER EXTERNAL SKIN WHICH IS BETWEEN AUXLIARY SPAR AND FRONT SPAR FSS 11 TO FSS 39. CORRECTIVE ACTION: 55-30-01-2R-1&SRM 51-70-10 (2987793)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 111,076 hrs · 16,353 cycles

SHIP 196 NBR 11 L/E SLAT MECHANISM LUBRICATION ONE ACCESS DOOR MISSING RT WING. CORRECTIVE ACTION: INSTALLED NBR 11 L/E SLAT MECHANISM LUBRICATION ONE ACCESS DOOR RT WING AS PER B767-300 AMM 20-11-00 (4461054)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 110,631 hrs · 16,279 cycles

SHIP 196 EXIT SIGN 1L FELL OFF. CORRECTIVE ACTION: SECURED EXIT SIGN COVER. CHECKS GOOD. REF B767 AMM 33-51. (4488928)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,945 hrs · 16,161 cycles

SHIP 196 EMERGENCY EXIT SIGNS INOPERATIVE / LOCATIONS:800 CORRECTIVE ACTION: REPLACED MISSING EXIT SIGN LENS. (2804962)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,604 hrs · 16,113 cycles

SHIP 0196 - ATB - DUE TO STANDBY ATTITUDE INDICATOR INOP. CORRECTIVE ACTION: C/W OVERWEIGHT LANDING INSP AND REPLACED THE STANDBY ATTITUDE INDICATOR AND STANDBY INVERTER / ILS PROCESSOR. (4671318)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,587 hrs · 16,110 cycles

SHIP 196 2L DOOR WILL NOT SHOW DISARMED ON FA PANEL. CORRECTIVE ACTION: ARMED AND DISARMED 2L DOOR PER TASK 52-73. OPS CHECK GOOD AT THIS TIME.A/C OK FOR SVC. (4671304)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,462 hrs · 16,092 cycles

SHIP 196 -RVSM- ALT DISAGREE EICAS ATL MCC, CORRECTIVE ACTION: DUE TO FIM PROCEDURE BY MCC REPLACED L ADC IAW AMM 34-12-01 REV 138.01 FUNCTIONAL TEST AND MCDP TEST PERFORMED SATISF . CKD OK . (4639468)

Part: NONE — NONE · airframe 108,819 hrs · 15,951 cycles

SHIP 196 - MISC/DE - DUE TO ANTI-SKID FAIL MESSAGE. CORRECTIVE ACTION: REPLACED #3 WHEEL SPEED TRANSDUCER. (9462552)

Part: NONE — NONE · airframe 108,787 hrs · 15,943 cycles

SHIP 196 UNABLE TO ARM DOOR 1R. CORRECTIVE ACTION: ARMED 1R DOOR (9449096)

Part: NONE — NONE · airframe 108,759 hrs · 15,939 cycles

SHIP 196 FOUND 40FG CEILING EMERGENCY LIGHT LENS MISSING. CORRECTIVE ACTION: FWD TO MEL 33-51-01A. NO MAINTENANCE ACTION REQUIRED. (9449072)

Part: NOT ENTERED — NOT ENTERED · airframe 108,581 hrs · 15,906 cycles

SHIP 196 R1 DOOR DIFFUCALT TO ARM. CORRECTIVE ACTION: OPEND AND CLOSED RQ DOOR, ARMED AND DISARMED PER B767 AMM52-11. (9449000)

Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 108,258 hrs · 15,840 cycles

FOUND RT CEILING EXIT SIGN MISSING. REPLACED EXIT SIGN IAW AMM 33-51.

Part: GIRT BAR — FOD (R1 DOOR) · airframe 108,258 hrs · 15,840 cycles

R1 DOOR HARD TO ARM. CORRECTIVE ACTION: REMOVED FOD AT GIRT BAR AREA. OPS CHECKED NORMAL. R1 DOOR ARMS NORMAL IAW AMM 52-00.

Part: TEST BUTTON — DAMAGED · airframe 107,768 hrs · 15,725 cycles

SHIP 196 ARM LENS DAMAGE ON LOC 101, CORRECTIVE ACTION: R/R ARMED TEST BUTTON LENS AT FA PNL. PER B767 AMM 25-20. (2469273)

Part: NONE — NONE · airframe 107,566 hrs · 15,694 cycles

SHIP 196 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. CORRECTIVE ACTION: POSITIONED ADJUSTED SECURED SAME OPS CK NRML (2440541)

Part: NONE — NONE · airframe 107,464 hrs · 15,680 cycles

SHIP 196 EMERGENCY EXIT SIGN AT DOOR 1L IS MISSING, CORRECTIVE ACTION: INSTALLED EMERGENCY EXIT SIGN LENS AT DOOR 1L IAW B767-300 AMM 33-51 (9551304)

Part: NONE — NONE · airframe 107,144 hrs · 15,626 cycles

SHIP 196 2L DOOR WILL NOT DISARM, CORRECTIVE ACTION: SLIDE LIGHT LENS HAD STICKY SUBSTANCE. REMOVED SUBSTANCE. LIGHT FUNCTIONAL NOW. OK FOR SVC (9048981)

Part: NONE — NONE · airframe 107,096 hrs · 15,619 cycles

SHIP 196 SLIDE INDICATOR LIGHT INOP OR DAMAGED, CORRECTIVE ACTION: SLIDE INDICATOR LIGHTS ON L2 AND R2 DOORS OPS CHK NORMAL. (2370380)

Part: SHUTOFF VALVE — INOPERATIVE · airframe 106,198 hrs · 15,453 cycles

SHIP 0196 -ATO- DUE TO LT PACK OFF DURING THROTTLE ADVANCE. CORRECTIVE ACTION: R/R LT PACK FLOW CONTROL SHUT OFF VALVE. A/C RTS. (2260661)

Part: SHROUD — DAMAGED · airframe 105,805 hrs · 15,387 cycles

SHIP 196 SEAT 38B LOWER EMERGENCY LIGHT SHROUD HAS DAMAGE. CORRECTIVE ACTION: SECURED LIGHT SHROUD PER B767 AMM 25-20 OK FOR SVC. (2202997)

Part: NONE — NONE · airframe 105,121 hrs · 15,260 cycles

SHIP 196 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS: 2R, CORRECTIVE ACTION: SECURED EXIT LENS AT DOOR 608. OK FOR SVC PER B767 MM 33-51. (2119932)

Part: NONE — NONE · airframe 104,816 hrs · 15,192 cycles

SHIP 196 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:101. CORRECTIVE ACTION: ALL OPS NML. OK FOR SVC (2076707)

Part: FAN — ODOR (CABIN) · airframe 104,280 hrs · 15,048 cycles

SHIP 196 F/A NOTIFIED US OF "LOUD FAN NOISE" AT THE BACK OF ACFT, AT 1000 FT FINAL APPROACH. AT THE GATE F/A REPORTED A STRANGE SMELL IN AFT CABIN. REPLACED INOPERATIVE FAN PER B767 AMM 21-26-06.

Part: COVER — DAMAGED (EMERGENCY SIGN) · airframe 103,986 hrs · 14,976 cycles

SHIP 196 EMERGENCY EXIT SIGN COVER DAMAGED. CORRECTIVE ACTION: REPLACED EXIT SIGN COVER. SYSTEM OPERATION IS NORMAL. (LP 1940339)

Part: FRAME — CORRODED (BS 1153 S36R) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01 EA FRAME WEB UPPER CHORD SURFACE CORROSION AT STA1153 S-36R. C/W ERA 593312-14. (LP 1923876)

Part: RIB — CRACKED (RT ELEVATOR) · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND RT O/B ELEVATOR RIB CRACK AT STA 258. CRACK REPAIRED PER SRM 55-20-02. (LP 1919849)

Part: SHEAR TIE — CORRODED (BS 1197 S38-39R) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1197 BETWEEN STR 38R AND 39R. REPLACED SHEAR TIE. (LP 1914575)

Part: ACCESS PANEL — CRACKED (NR 2 NACELLE) · airframe 103,853 hrs · 14,953 cycles

SHIP 196 MAINTENANCE FOUND NO.2 PYLON ACCESS PANEL 426BR CUT OUT CRACK. CORRECTIVE ACTION: REPAIRED PER SRM 54-53-01. (LP 1913825)

Part: SHEAR TIE — CORRODED (BS 742 S35-36R) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 FWD CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 742 BETWEEN S-35R AND S-36R. REPLACED SHEAR TIE. (LP 1911077)

Part: SHEAR TIE — CORRODED (BS 1175 S37-38R) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1175 BETWEEN STR 37R AND 38R. REPLACED SHEAR TIE. (LP 1911059)

Part: SHEAR TIE — CORRODED (BS 1307 S38-39L) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1307 BETWEEN STR 38L AND 39L. REPLACED SHEAR TIE. (LP 1911064)

Part: SHEAR TIE — CORRODED (BS 1373 S36-37L) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1373 BETWEEN STR 36L AND 37L. SHEAR TIE REPLACED. (LP 1911070)

Part: SHEAR TIE — CORRODED (BS 764 S36-37R) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AT STA 764 BETWEEN S-36R AND S-37R. SHEAR TIE REPLACED. (LP 1911074)

Part: SHEAR TIE — CORRODED (BS 1329 S39L-R) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1329 BETWEEN STR 39L AND 39R. REPLACED SHEAR TIE. (LP 1911058)

Part: SHEAR TIE — CORRODED (BS 1197 S37-38R) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1197 BETWEEN STR 37R AND 38R. SHEAR TIE REPLACED. (LP 1910104)

Part: FLOORBEAM — CORRODED (BS 347) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 CABIN COMPARTMENT FLOOR BEAM FOUND CORROSION AT BS 347, RBL54.75 TO 10 INCH. FLOOR BEAM REPAIRED PER SRM. (LP 1910098)

Part: SHEAR TIE — CORRODED (BS 654 S37-38L) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 FWD CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 654+88 BETWEEN S-37L AND S-38L. SHEAR TIE REPLACED. (LP 1910162)

Part: SHEAR TIE — CORRODED (BS 1175 S37-38L) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1175 BETWEEN STR 37L AND 38L. SHEAR TIE REPLACED. (LP 1910106)

Part: SHEAR TIE — CORRODED (BS 742 S35-36L) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 FWD CARGO COMPARTMENT FOUND 01 EA SHEAR TIE SURFACE CORROSION AT STA 742 BETWEEN S-35 L AND S-36L. REPLACED SHEAR TIE. (LP 1906407)

Part: SHEAR TIE — CORRODED (BS 1241 S38-39L) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01 EA SHEAR TIE SURFACE CORROSION AT STA 1241 BETWEEN STR 38L AND 39L. SHEAR TIE REPLACED. (LP 1906313)

Part: SHEAR TIE — CORRODED (BS 1241 S39L-R) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01 EA SHEAR TIE SURFACE CORROSION AT STA 1241 BETWEEN STR 39L AND 39R. REPLACED SHEAR TIE. (LP 1906309)

Part: SHEAR TIE — CORRODED (BS 742 S39L-R) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 FWD CARGO COMPARTMENT FOUND 01 EA SHEAR TIE SURFACE CORROSION AT STA742 BETWEEN STR S-39R AND S-39L. REPLACED SHEAR TIE. (LP 1906408)

Part: SHEAR TIE — CORRODED (BS 742 S37-38R) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 FWD CARGO COMPARTMENT FOUND 01 EA SHEAR TIE SURFACE CORROSION AT STA 742 BETWEEN STR S-37R AND S-38R. REPLACED SHEAR TIE. (LP 1906415)

Part: SHEAR TIE — CORRODED (BS 1307 S39L-R) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01 EA SHEAR TIE SURFACE CORROSION AT STA 1307 BETWEEN STR 39L AND 39R. REPLACED SHEAR TIE. (LP 1906421)

Part: SHEAR TIE — CORRODED (BS 1197 S39L-R) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01 EA SHEAR TIE SURFACE CORROSION AT STA 1197+110 BETWEEN STR 39L AND 39R. SHEAR TIE REPLACED. (LP 1906305)

Part: SHEAR TIE — CORRODED (BS 1197 S39L-R) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01 EA SHEAR TIE SURFACE CORROSION AT STA 1197 BETWEEN STR 39L AND 39R, SHEAR TIE REPLACED. (LP 1906383)

Part: SHEAR TIE — CORRODED (BS 1329 S37-38L) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01 EA SHEAR TIE SURFACE CORROSION AT STA 1329 BETWEEN STR 37L AND 38. REPLACED SHEAR TIE. (LP 1906418)

Part: SHEAR TIE — CORRODED (BS 742 S38-39L) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 FWD CARGO COMPARTMENT FOUND 01 EA SHEAR TIE SURFACE CORROSION AT STA 742 BETWEEN S-38L AND S-39L. SHEAR TIE REPLACED. (LP 1906393)

Part: SHEAR TIE — CORRODED (BS 1197 S39L-R) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01 EA SHEAR TIE SURFACE CORROSION AT STA 1197+88 BETWEEN STR 39L AND 39R. SHEAR TIE REPLACED. (LP 1906382)

Part: SEAT TRACK — CORRODED (BS 1417-1439) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

SHIP 196 DURING INSPECTION MAINTENANCE FOUND LEVEL 2 CORROSION ON SEAT TRACK-CABIN SEAT TRACK AT BS 1417 TO BS 1439 LBL 88.5 AREA. SEAT TRACK REPLACED. (LP 1898960)

Part: SKIN — CRACKED (LT WING) · airframe 103,853 hrs · 14,953 cycles

WHILE IN C CHECK DURING INSPECTION MAINTENANCE FOUND CRACK ON THE LH WING LOWER SKIN COMMON TO STRINGER L-9.5 BETWEEN WING STATIONS 962.2 AND 990.2. C/W ERA 573819-14. (LP 1897102)

Part: SEAT TRACK — CORRODED (BS 933-955) · corrosion level 2 · airframe 103,853 hrs · 14,953 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SEAT TRACK AT BS 933 TO BS 955.1 LBL 88.5 AREA. SEAT TRACK REPAIRED PER SRM. (LP 1895490)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 103,417 hrs · 14,841 cycles

DURING SERVICE CHECK MAINTENANCE FOUND OVERHEAD EMERGENCY LIGHTS FROM ROW 16-31 INOPERATIVE. CORRECTIVE ACTION: REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCYH LIGHT) · airframe 103,213 hrs · 14,800 cycles

OVER THE WING LEFT AISLE EMERGENCY LIGHT INOPERATIVE. CORRECTIVE ACTION: REPLACED POWER SUPPLY M737. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 103,162 hrs · 14,788 cycles

OVERHEAD EMERGENCY LIGHTS AT ROWS 16C THROUGH 31 ARE INOPERATIVE. CORRECTIVE ACTION: REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL.

Part: SHROUD — BROKEN (CABIN) · airframe 100,212 hrs · 14,377 cycles

SEAT EMERGENCY LIGHT SHROUD AT SEAT 41F IS BROKEN REPLACED EMERGENCY LIGHT SHROUD AND SECURED. SYSTEM OPERATION IS NORMAL.

Part: SHROUD — BROKEN (CABIN) · airframe 100,212 hrs · 14,377 cycles

SEAT EMERGENCY LIGHT SHROUD AT SEAT 38F IS BROKEN. REPLACED EMERGENCY LIGHT SHROUD AND SECURED. SYSTEM OPERATION IS NORMAL.

Part: CONTROL VALVE — WARNING MESSAGE (A/C PACK) · airframe 99,856 hrs · 14,324 cycles

ATO - AT 60KTS DUE RT PACK OFF LIGHT AND EICAS MSG DURING TO ROLL. REPLACED PACK FLOW CONTROL AND SHUTOFF VALVE.

Part: HOLDER — NOT REPORTED (CABIN) · airframe 99,353 hrs · 14,261 cycles

EMERGENCY SEAT MOUNTING AT SEAT 34F. REPLACED EMERGENCY SEAT MOUNTED LIGHT HOLDER. SYSTEM OPERATION.

Part: PROXIMITY SENSOR — FAILED (TE FLAPS) · airframe 98,251 hrs · 14,096 cycles

CREW REPORTED TO CONFIG FLAP WARNINGS DURING CLIMB OUT . ELECTED TO DIVERT. MTC FOUND FAILED K215 A/G RELAY AND S266 PROX SENSOR, AND HAS ALSO REPLACED TO CONFIG WARNING CARD. OPS CHECKS ARE NORMAL. NON-REV FCF SUCCESSFUL AND AIRCRAFT RTS.

Part: BATTERY — DISCHARGED (CABIN) · airframe 98,218 hrs · 14,091 cycles

ON SERVICE CHECK FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. REPLACED BATTERY ON CHARGER M1210. SYSTEM OPERATION IS NORMAL.

Part: SKIN — CRACKED (LT WING) · airframe 97,774 hrs · 14,034 cycles

CRACK INDICATION FROM BHEC AT STR L-6.5 FASTNER ZCB HOLE 5. HOLE SIZE 0.309" AND CRACK APPROX. 0.125" IN LENGTH PERMANENT REPAIR OF ERA 573937-14 (LP 0874912)

Part: SKIN — CRACKED (LT WING) · airframe 97,774 hrs · 14,034 cycles

HFEC INSP SHOWS CRACK AT LOWER WING SKIN AT STRINGER L-9.5 AT OUTBOARD MOST FASTENER IN INSPECTION AREA C/W PERMANENT REPAIR PER ERA 573819-14. (LP 0874908)

Part: SKIN — DAMAGED (WING) · airframe 97,774 hrs · 14,034 cycles

DISCOVERED (8) OVERSIZED HOLES IN LOWER WING SKIN ON I/B SIDE OF STRINGER 6.5. PERMANENT REPAIR PER ERA573998-14. (LP 0873389)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 111,076 hrs · 16,353 cycles

SHIP 196 ER/A 573998-14 REV ORIGINAL REPAIR TRACKING. CORRECTIVE ACTION: ASSOCIATED ER/A CHANGED FROM 00-573998 TO 14-573998 FOR AC 0196 PERFORMED EXTERNAL HFEC INSPECTION LH WING LOWER SKIN PER EM 5724-01010-42A AND INCLUDE THE REPAIRED LOCATION WITH THE FREEZE PLUG ALONG INBOARD STRINGER L-6.5 I.A.W ER/A 573998-14AD (0872592)

Part: SKIN — CRACKED (LT WING) · airframe 97,773 hrs · 14,033 cycles

CRACK ON LH WING LOWER SKIN STRINGER L-9.5 B/T WING STATIONS 962.2 AND 990.2, HOLE #66 C/W ERA 573819-14. (LP 0871400)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 111,076 hrs · 16,353 cycles

SHIP 196 ER/A 573891-14 REV ORIGINAL REPAIR TRACKING (RH WING LOWER SK FREEZE PLUG REPAIR). CORRECTIVE ACTION: ACCOMPLISHED EXTERNAL HFEC INSPECTION PER EM5724-01010-45B AND INCLUDE THE REPAIRED LOCATION WITH THE FREEZE PLUG ALONG INBOARD STRINGER-9.5 I.A.W ERA 573891-14AD (0873279)

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 94,848 hrs · 13,641 cycles

FORWARD MID LAVATORY EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED THE WIRE RUN FROM SIDEWALL TO RIGHT FORWARD MID LAVE FLOOR. SYSTEM OPERATION IS NORMAL.

Part: PANEL — CRACKED (RT PYLON) · airframe 94,123 hrs · 13,534 cycles

DURING PDC, FOUND ONE PANEL ON THE RT INBD PYLON CRACKED. COMPLIED WITH 566105-14.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,583 hrs · 13,310 cycles

EMERGENCY LIGHTS AT 1A-3A ARE INOPERATIVE. FOUND THE POWER SUPPLY INOPERATIVE. REPLACED THE POWER SUPPLY AND THE SYSTEM OPS NORMAL.

Part: RECEIVER — ODOR (ADF) · airframe 89,498 hrs · 12,835 cycles

CAPTAIN`S AND F/O`S YELLOW BAND DISPLAYED ON HSI'S. CIRCUIT BREAKER WAS RESET (A3) IAW MCC WITHIN 30 SEC STARTED TO SMELL BURNING ELECTRIC PLASTIC PULLED CIRCUIT BREAKER A3 AND ODOR DISSIPATED. FOUND ELECTRICAL ODOR FROM RADF RECEIVER, COMPLIED WITH ERA 555368-14. REPLACED RIGHT ADF RECEIVER SYSTEM OPERATION IS NORMAL.

Part: LINER — DENTED (LT ENGINE) · airframe 88,909 hrs · 12,739 cycles

LT ENG FAN CASE INTERIOR LINING BETWEEN FAN BLADES AND FAN EXHAUST GUIDE VANES FOUND 03EA DENTS AS MARKED. ERA 553433-14.

Part: SKIN — DAMAGED (LT WING) · airframe 88,909 hrs · 12,739 cycles

LT WING SKIN AT AFT PITCH LOAD FITTING O/B DAMAGED HOLE REPAIRED PER ERA 551291-14.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 88,896 hrs · 12,736 cycles

BULK CARGO SHEAR TIE AT STA 1417/S36R FOUND CORROSION AND REPLACED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 88,909 hrs · 12,739 cycles

AFT CARGO AT STA 1307 BETWEEN S-27L AND S-38L FOUND CORRODED SHEAR TIE AND WAS REMOVED AND REPLACED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 84,363 hrs · 12,069 cycles

EMERGENCY EXIT SIGN IN FLIGHT DECK IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 84,363 hrs · 12,069 cycles

EMERGENCY LIGHTS AT SEAT 33A ARE INOPERATIVE DUE TO BROKEN WALL TO SEAT CONNECTOR. MAINTENANCE REPLACED CONNECTOR. SYSTEM OPERATION IS NORMAL.

Part: STRINGER — CRACKED (LT WING) · airframe 82,439 hrs · 11,787 cycles

LEFT WING STRINGER L 6.5 HAS CRACK INDICATIONS IN HOLE NR 1 AND HOLE NR 2. REPAIRED IAW PRI 536622-14.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 82,351 hrs · 11,775 cycles

ENGINE NR 2 PYLON INBD SIDE ACCESS 446BL CUT OUT DOUBLER UPPER SIDE IS CRACKED. REPAIRED IAW SRM 54-53-01.

Part: SKIN — DAMAGED (WING) · airframe 72,819 hrs · 10,430 cycles

INSPECTED IAW SB 767-57-010, REV 9, PART 2. REPAIRED IAW SB 767-57-010, REV 9, PARTS 3 THRU 6 AND AA 5724-01010.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 73,855 hrs · 10,580 cycles

RT SIDE ROW 13 TO 20 EMERGENCY PATH LIGHTS DIM. FOUND AND REPLACED DAMAGED CONNECTOR AT 20 FC SIDEWALL PANEL SYS CHECKS NORMAL.

Part: LIGHT — MALFUNCTIONED (ESCAPE SLIDE) · airframe 73,104 hrs · 10,470 cycles

PILOT REPORTED LT FWD EMERGENCY DOOR LIGHT STAYED ILLUMINATED FROM AFTER TAKEOFF TO LANDING. MX ARMED AND DISARMED 1L DOOR SLIDE. SLIDE LIGHT OPERATION IS NORMAL. CYCLED EMERGENCY LIGHT. SYS OPERATION IS NORMAL.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 72,284 hrs · 10,347 cycles

EMERGENCY PATH LIGHTS ARE INOPERATIVE AT SEAT 22B. FOUND WIRE BEHIND THE SEAT DAMAGED AND REPAIRED.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 72,284 hrs · 10,347 cycles

EMERGENCY PATH LIGHTS AT SEAT 20B ARE INOPERATIVE. CONNECTED CONNECTOR SYS OPS NORMAL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 72,284 hrs · 10,347 cycles

EMERGENCY PATH LIGHTS AT SEAT 21B ARE INOPERATIVE. CONNECTED CONNECTOR. SYS OPS IS NORMAL.

Part: WIRE — OVERHEATED (CABIN LIGHTS) · airframe 71,625 hrs · 10,250 cycles

F/A SMELLED AN ODOR AT ROW 40CDE. ODOR DISAPATED AFTER SEVERAL MINUTES. REPAIRED WIRING AT ROW 15ABC INDIRECT LIGHT IAW SWPM 20-10-01, PG 298, INSPECTED ROW 40. NO TROUBLE FOUND. ALSO REF SAME LOG ITEM NR 009.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,364 hrs · 10,077 cycles

A ZONE LT OVERHEAD EMERGENCY LIGHTS CAME ON BUT WILL NOT TURN OFF. REMOVED AND REPLACED POWER SUPPLY & CHARGER M735 FOR FWD LEFT AISLE LIGHTS. SYSTEM OPERATION IS NORMAL.

Part: SOCKET — LOOSE (EMERGENCY LIGHT) · airframe 69,936 hrs · 10,020 cycles

EMERGENCY LIGHTS LEFT 3RD AND 4TH ARE INOPERATIVE. MAINTENANCE SECURED LAMP SOCKET AT BOTH POSITIONS. SYSTEM CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,872 hrs · 10,012 cycles

DURING DRC, FOUND EXTERIOR EMERGENCY LIGHT OUT OAT LET SIDE AFT OF TRAILING EDGE. THE POWER SUPPLY UNIT WAS REPLACED PER AMM. SYSTEM OPERATION IS NORMAL.

Part: SKIN — CRACKED (LT WING) · airframe 67,747 hrs · 9,728 cycles

LT WING LOWER SKIN AT AFT TENSION FITTING (PITCH LOAD) FWD I/B HOLE CRACKED. REAMED I/B HOLE TO .656. CRACK CONFIRMED. REMOVED BY NDI HFEC. ALL WORK DONE PER ER/A 500374-14 AD REV. PERMANENT REPAIR ACCOMPLISED.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 67,468 hrs · 9,688 cycles

CRACK FOUND IN RMLG FAILSAFE DURING ULTRA-SONIC INSPECTION PER SI 01-086393-12AD. REPAIRED PER ERA 499436-14AD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 66,876 hrs · 9,608 cycles

DURING LIGHTNING STRIKE INSP FOUND STRIKE AT STA 654+22 AT STR 32R TO BE OUT OF LIMITS. REPAIRED PER SRM 53-00-01 REPAIR NR 1. REPAIR WORKED ON NR 70. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: CHARGER — INOPERATIVE (CABIN) · airframe 66,184 hrs · 9,522 cycles

DURING DRC FOUND EMERGENCY LIGHTS INOP ROW 21-31AB. REMOVED AND REPLACED BATT CHARGER OPS CHECKED GOOD. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: WIRE — BROKEN (CABIN) · airframe 65,238 hrs · 9,401 cycles

EMERGENCY LIGHTS AT ROW 20AB ARE INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT SEAT QUICK DISCONNECT AND REPLACED IT. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 64,341 hrs · 9,282 cycles

EMERGENCY LIGHTS AT SEAT 23A ARE INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,341 hrs · 9,282 cycles

EMERGENCY LIGHTS AT SEATS 1AB ARE INOPERATIVE. MAINTENANCE SEATS. SYSTEM OPERATION IS NORMAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,238 hrs · 9,012 cycles

CABIN RT STA 903 BETWEEN S20R AND S21R FRAME INNER CHORD CRACK. REPAIR ACCOMPLISHED AS PER ER/A 485490-14AD (DL76L103230).

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,238 hrs · 9,012 cycles

CABIN LT STA 903 BETWEEN S20L AND S21L FRAME INNER CHORD CRACK. REPAIR ACCOMPLISHED AS PER ER/A 485489-14. (DL76L103229)

Part: CONNECTOR — LOOSE (CABIN) · airframe 61,193 hrs · 8,880 cycles

EMERGENCY LIGHTS AT SEAT 27AB ARE INOPERATIVE. MAINTENANCE RE-SECURED WIRE CONNECTOR SYSTEM OPERATION IS NORMAL (ODI 2010-D0924) BOS/704882 (DL76L102006).

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 60,946 hrs · 8,842 cycles

EMERGENCY LIGHTS AT SEAT 27AB ARE INOPERATIVE. MX SECURED THE WIRE CONNECTOR AND THE SYS OPERATED NORMALLY.

Part: PANEL — FIRE (SQUIB TEST) · airframe 60,688 hrs · 8,806 cycles

SQUIB TEST PANEL ON P61 PANEL HAD SMALL ELECTRICAL FIRE DURING PRE-FLIGHT. EXTINGUISHED WITH THE HALON FLIGHT DECK BOTTLECAP/ R & R SQUIB TEST PANEL 261001441/SYS TEST PNL 233T4239-26/ L ENG FIRE BTL 1 AND BTL 2 C/BS P6-1 H1/H2. INSPECTED ALL RELATED WIRING FOR VISIBLE SIGNS OF DAMAGE. NONE FOUND. PERFORMED ALL OPS GROUND CHECKS FOR ASSOCIATED PANELS IAW AMM REF 26-21-04/401. ALL CONDITIONS NORMAL. ACFT OK FOR SERVICE. (DL76L101514)

Part: STARTER — FAILED (NR 2 ENGINE) · airframe 58,275 hrs · 8,479 cycles

NR 2 ENG STARTER FAILED DURING ENG START RTB. REPLACED STARTER - STARTER CARBON SEAL AND STARTER DRIVE COUPL PER AMM. ENGINE STARTS NORMAL.

Part: SHAFT — LOOSE (PRV VALVE) · airframe 57,915 hrs · 8,425 cycles

RT PACK OFF LT ILLUMINATED RT ENG BLEED LT ILLUMINATED. T/S PER AMM R/R RT ENG PRV CONT FOUND RT ENG PRV VLV SHAF LOOSE R/R RT ENG PRV. PRV CONT AND VALVE NEEDS OPS CHECK. PERFORMED OPS CHECK PER AMM RT ENG RAN OPS CHECK NORMAL. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: VALVE — UNSERVICEABLE (BLEED AIR SYS) · airframe 57,913 hrs · 8,424 cycles

RT PACK OFF LT ILLUMINATED RT ENG BLEED LT ILLUMINATED. T/S PER AMM R/R RT ENG PRV CONT. FOUND RT ENG PRV SHAFT LOOSE R/R RT ENG PRV. PRV AND CONT AND VALVE NEEDS OPS CK. PERFORMED OPS CK PER AMM RT ENG RAN OPS CHECK NORMAL. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK.

Part: WIRE — BROKEN (CABIN) · airframe 56,833 hrs · 8,280 cycles

ON DRC - PASSENGER SEAT 39F EMERGENCY ESCAPE PATH LIGHT OUT. FWD TO MCO AND PLACARD PER MEL M33-51-03A. FOUND WIRE UNDER SEAT BROKEN.

Part: ENGINE — FAILED (NR 1) · airframe 56,490 hrs · 8,237 cycles

DESENDING THROUGH 22K NOTICED IDG DISCONNECTED AND THEN OIL PRESSURE IN THE RED. N1 AND N2 FAIL BELOW IDLE AND FF WAS LESS THAN 600LBS. TURNED FUEL CUTOFF SWITCH TO OFF. ENGINE SHOWED POSITIVE OIL PRESS THROUGHOUT THE REST OF THE DESCENTAND LANDING. EMERGENCY WAS DECLARED. R & R LT ENG PER TRANS 1T148 AD. ETOPS CATEGORY 'C': UNCOMMANDED PWR CHANGES,SURGES,OR STALLS

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,289 hrs · 8,214 cycles

ON TAXI OUT NR 1 ENGINE COULD NOT GENERATE ENOUGH PRESSURE TO START NR 2 ENGINE - 20 PSI AT 82 PERCENT N2. NO PSI FOR NR 2 ENGINE. SUSPECT DUCT LEAK. CHECKED ENG. NR 1 DUCTS FOR LEAK AND LT PACK. PERFORMED ENG. NO RUN BY CREW AND CROSSBLEED START NR 2 DUCT PRESS. AND INDICATIONS NORMAL. NOTHING ABNORMAL FOUND.

Part: ADC — MALFUNCTIONED · airframe 55,746 hrs · 8,149 cycles

DIVERTING TO BGR FOR AIR DATA ISSUES. CAPT AIRSPEED WENT TO 400 KNOT AND ALTN STARTED TO DROP AT FL330. F/O SIDE WAS UNRELIABLE.

Part: ACTUATOR — MALFUNCTIONED (A/C PACK DOOR) · airframe 55,593 hrs · 8,128 cycles

LEFT PACK TEMP EICAS MESSAGE AND PACK TRIPPED OFF. PACK RESET AFTER FIVE MINUTES AND OPERATED IN STBY-N. SEVERAL MINUTES LATER PACK TRIPPED OFF AGAIN. REPLACED LEFT PACK INLET DOOR ACTUATOR.

Part: STARTER — INOPERATIVE (NR 2 ENGINE) · airframe 55,082 hrs · 8,059 cycles

NO N2 ROTATION DURING RIGHT ENGINE START UP. RT ENGINE STARTER WAS REPLACED IAW AMM 80-11-01-404-014-N00 80-11-01-404-014-N00. STARTER SERVICED IAW AMM 12-13-02 PB301. DRY MOTORING PERFORMED AMM 71-00-00/201 N2 UP TO 26 PERCENT. LEAK CHECK OK.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 54,270 hrs · 7,963 cycles

MID LAV 219 SMOKE ALARM SOUNDED. NO SMOKE OR BURNING ODOR NOTED. LAVATORY INSPECTED FOR BURNS OR DISCREPANCY NIL FOUND. LAVATORY WASTE FLAP AND LAVATORY FIRE EXTINGUISHER BOTTLE INSPECTED OK. SMOKE DETECTOR OPS CHECKED OK FOR SERVICE.

Part: BLEED VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 51,152 hrs · 7,583 cycles

RT ENG HPSOV MSG. FWD TO MCO PLAC PER MEL 36-11-02 RT ENG HP BLEED VALVE LOCKED OUT. NOTE: AIRCRAFT FLOWN TO ATL FOR EQUIP SUB DUE TO ADDITIONAL PROBLEM WITH THE LT ENG BLEED. CVG REPLACED LT HP CONTROLLER AND LOCK RT HP BLEED VALVE CLOSED. ATL MTC REPLACED RT ENG HP BLEED VALVE. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,220 hrs · 7,458 cycles

3 EXTERIOR EMERGENCY LIGHTS INOP, 2 AFT OF RIGHT WING AND R2 DOOR. REPLACED BATTERY PACK. OPS CK GOOD.

Part: TRANSCEIVER — FAILED (WEATHER RADAR) · airframe 48,970 hrs · 7,309 cycles

WX RADAR FAILED IN FLT WITH ANT FAULT. REPLACED TRANSCEIVER AND ANTENNA CHECKS OK.

Part: ANTENNA — FAILED (WEATHER RADAR) · airframe 48,970 hrs · 7,309 cycles

WX RADAR FAILED IN FLIGHT WITH ANT FAULT. REPLACED TRANSCEIVER AND ANTENNA. CKS OK.

Part: ENGINE — MAKING METAL (NR 2) · airframe 46,871 hrs · 7,052 cycles

METAL ON MASTER CHIP DETECTOR. REPLACED ENGINE PER ROUTINE TRANSMITTAL, RC CARDS 28-30.

Part: BEARING — FAILED (NR 2 ENGINE) · airframe 46,791 hrs · 7,042 cycles

N2 ENGINE INOP, AUTO-THROTTLES INOP-FADEC C1 MSG. FOUND N2 STATOR /ROTOR BEARING FAILED. FOUND EEC ALTERNATOR ROTOR/STATOR WORN AND EEC ALTERNATOR DR GEARSHAFT AFT BEARING DAMAGED. REPLACED EEC ALTERNATOR DRIVE GEARSHAFT AND BEARING ASSEMBLY AND ROTOR AND STATOR AS PER 72-61-14 AND 73-21-05. ACCOMPLISHED ENG RUN AT IDLE AUTHORITY PER TOPP 40-20-15 AND MCC NO FAULTS. NO MSGS.

Part: COFFEEMAKER — SMOKE (AFT GALLEY) · airframe 46,026 hrs · 6,950 cycles

AFT COFFEE MAKER ON CAPT'S SIDE PRODUCED SMOKE WHEN TURNED ON. SMOKE QUIT WHEN COFFEE MAKER WAS TURNED OFF. CB'S WERE PULLED. RESET C/B FOR AFT COFFEE MAKER. MADE A POT OF COFFEE FROM EACH. ALL CKS OK. NO SMOKE NOTED AT ANY TIME.

Part: IDG — UNKNOWN (RIGHT) · airframe 45,391 hrs · 6,870 cycles

RT GEN OFF ILLUMINATED. FOUND GEN DIODE FAULT ON BPCU-TRIED GCU NO HELP. REINSTALLED ORIG, REPLACED AND TESTED RT IDG PER MM ALL CHKS NORMAL.

Part: STARTER — UNSERVICEABLE (NR 1 ENGINE) · airframe 44,580 hrs · 6,772 cycles

NR 1 ENG WOULD NOT START NO ROTATION. FOUND NR 1 ENG STARTER AT FAULT. REPLACED STARTER, OPS CKS OK.

Part: DUCT — UNKNOWN (RIGHT) · airframe 39,628 hrs · 6,156 cycles

RT DUCT LEAK LP 1. RETURN TO BLOCK. TESTED DUCT LEAK. UNABLE TO DUPLICATE OR FIND FAULT.

Part: COMPUTER — FAILED (ADC) · airframe 38,771 hrs · 6,037 cycles

AT LEVEL OFF FL330 ALT DISAGREE EICAS LIGHT CAME ON. CAPT ALT READ 300 FEET DIFF FROM F/O ALT. AFTER DESCENT TO FL280 CAPT ALT READ 28010, F/O ALT READ 27760 STDBY READ 28350. PER FIM REPLACED F/O`S ADC AND CHECKS NORMAL. OPS OK PER M/M. ALSO REPLACED F/O`S ALT IND AS PRECAUTIONARY.

Part: IDG — FAILED (RIGHT) · airframe 38,130 hrs · 5,953 cycles

RIGHT IDG DROP OFFLINE AND WOULD NOT RESET. BPCU BITE CHECK FAULTS GEN DIODE. REPLACED GCU, NO HELP. REINSTALL ORIGINAL GCU. REMOVED AND REPLACED RIGHT IDG. OPS AND LEAK CHECK OK.

Part: DISPLAY — INOPERATIVE (COCKPIT) · airframe 37,299 hrs · 5,831 cycles

F/O CDU DISPLAY BLANK. SELECTING ALT SOURCE DID NOT CORRECT THE PROBLEM. REPLACED F/O FMC CDU PER MM, GROUND TEST NORMAL.

Part: SMOKE — DETECTED (CABIN) · airframe 37,064 hrs · 5,800 cycles

FLIGHT ATTENDANTS REPORT ELEC SMOKE IN MID CABIN AFTER T/O. RETURN TO ATL. RAN BOTH ENG AT TAKEOFF POWER FOR 10 MINS. RAN PACKS AT FULL HOT, HAD CABIN / GALLEYS POWERED OPS CK IFE SYSTEM. NO ELEC SMOKE ODOR FOUND ANYWHERE ON A/C. A/C OK FOR SERVICE.

Part: PDU — SPARKS · airframe 35,513 hrs · 5,580 cycles

SPARKS COMING FROM PDU 9L IN AFT CARGO DURING LOADING. REPLACED RECEPTACLE.

Part: SENSOR — CONTAMINATED (LE SLAT) · airframe 33,729 hrs · 5,323 cycles

L/E SLAT ASSY LIGHT AFTER TAKEOFF. ATB INTO ATL. FOUND SENSORS CONTAMINATED WITH GREASE.

Part: BRAKE — FIRE (RT MLG) · airframe 33,507 hrs · 5,292 cycles

AT GATE ARRIVAL NR 3 BRAKE HAD A GREASE FIRE. EXTINGUISHED FIRE, REMOVED TIRE AND BRAKE ASSEMBLY, INSPECTED AXLE FOR HEAT DAMAGE, NONE FOUND. INSTALLED NEW BRAKE ASSEMBLY AND NEW WHEEL ASSEMBLY, OPS CHECK OK.

Part: START VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 31,311 hrs · 4,995 cycles

LEFT STARTER CUTOUT EICAS MSG AND VALVE LIGHT ILLUMINATED ON TAKEOFF. FOLLOWED QRH. START VALVE REPLACED.

Part: MONITOR — ODOR (SEAT 4B) · airframe 30,589 hrs · 4,888 cycles

DURING PDC, NOTICED ELEC ODOR IN AREA OF 4A AND B FOUND SEAT 4-B INSEAT MONITOR TO BE SOURCE OF ODOR. REPLACED MONITOR. MONITOR CHECKS OK.

Part: RIB — GOUGED (CENTER WING) · airframe 27,449 hrs · 4,400 cycles

LOWER STRUCTURAL DAMAGE REPAIR THE LOWER STRUCTURE OF THE LBL 62.05 LOWER BEAM OF THE CENTER WING WAS BADLY GOUGE TO A BLOWN DUCT FROM FS 915-919. THE DAMAGED SECTION OF CHORD WAS CUT AND REMOVED. A NEW SECTION OF STRUCTURE WAS SPLICED IN WITH STEEL REPAIR ANGLES IAW ER/A 385317-14, REV A.

Part: CONTROLLER — FAILED (RIGHT ENGINE) · airframe 26,084 hrs · 4,166 cycles

RIGHT PRV INOPERATIVE. SWAPPED HPSOV AND PRV. AFTER TAKEOFF RIGHT ENG BLEED FAILED. DUE TO FORECAST WEATHER IN JFK DECISION WAS MADE TO DIVERT TO FRA. FOUND PRV CONTROLLER AT FAULT. REPLACED PRV CONTROLLER, OPS CHECK ON R/U OK.

Part: BLADE — DENTED (NR 2 ENGINE) · airframe 26,026 hrs · 4,156 cycles

DURING T/O AT 110 KNTS BIRD INGESTION INTO NR 2 ENGINE WITH ENGINE SURGE DETECTED. ENGINE INDICATIONS NORMAL. REPORTED BY CREW 1 HR INTO FLT, NR 1 ENG GEN FAILED. A/C DIVERTED TO LGW. FOUND BIRD DEBRIS IN ENG 1, FAN BLADE DAMAGED OUT OF LIMITS. BOROSCOPE INSPECTION COMPLETED WITH NO FAULTS. FOUND DAMAGE TO FAN EXIT VANE. FAN BLADE TO BE REPLACED/ERA ISSUED FOR REPAIR TO VANE. IDG REPLACED. BIRD STRIKE INSPECTION COMPLETED.

Part: MONITOR — MALFUNCTIONED (CABIN) · airframe 24,137 hrs · 3,845 cycles

DURING PDC IFE CHECK WALL MOUNTED MONITOR IN FRONT OF SEATS 1A AND 1B EMITTING SMOKE. REPLACED WALL MOUNTED MONITOR AT SEAT 1A AND 1B, ADJUSTED SAME. OPS CHECK OK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,619 hrs · 3,561 cycles

TWO EXTERIOR EMERGENCY LIGHTS AFT OF LEFT WING INOP. RELAMPED SAME, OPS NORMAL.

Part: DAU — FAILED (E/E BAY) · airframe 19,166 hrs · 2,984 cycles

STATUS MSG IN-FLT, FLT DATA ACQ. PULLED C/B J7 AND J8. ELEC SMELL JUST PRIOR TO MESSAGE. REPLACED DFDAU AND FLT DATA REC PER MM. OPS NORMAL. MTC REPORTED DFDAU HAD STRONG ELEC SMELL.

Part: COFFEEMAKER — BURNED (AFT GALLEY) · airframe 15,791 hrs · 2,461 cycles

WHITE SMOKE AND ELECTRICAL SMELL IN AFT GALLEY. FOUND AFT LEFT COFFEE MAKER INTERNAL SEAL BURNED. DISCONNECTED COFFEE MAKER AND FWD TO MCO

Part: BULB — FAILED (GALLEY) · airframe 13,642 hrs · 2,111 cycles

ON DESCENT, SMOKE BEGAN TO COME FROM SPEAKER ON CAPT SIDE AFT GALLEY AREA ABOVE CENTER F/A JUMP SEAT. FOUND SHORTED LIGHT BULB IN DIRECT CEILING LIGHTS ABOVE F/A SEAT. REPLACED BULB, SYSTEM OPS CHECK NORMAL.

Part: DOOR WARNING — ACTIVATED (RT EMER EXIT)

ATB FIRST FLIGHT DELAY, RT FWD EMERGENCY DOOR MSG CAME ON DURING CLIMB, WENT OUT ON ROLLOUT. FWD TO MCO.

Part: BULB — FAILED (LT EMER EXIT)

DURING L/O, FOUND LT EXTERIOR OVERWING EMERGENCY LIGHTING AFT, TWO LIGHTS INOP.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

WHILE PERFORMING L/O CK, FOUND EMER LIGHTS FROM AISLE 25AB THRU 35AB INOP. REPLACED POWER SUPPLY M9009, SYSTEM OPS CHECKS GOOD.