N155DL

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 122,303 hrs · 21,990 cycles

LEFT & RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. DURING FUNCTIONAL CHECK FLIGHT. FOUND BLOWN FUSES AND REPLACED.

Part: SKIN — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

AFT CARGO COMP INTERNAL SKIN IS CORRODED BETWEEN STA 1197+22- STA 1197+44 S36R AFT OF REPAIR DOUBLER BLENDED AREA OF CORROSION REMOVED .045 MATERIAL, REMAINING THICKNESS .075 OUT OF POSSINBLE .120. FOUND TO BE OUT OF LIMITS. C/W SRM 53-00-01.

Part: SHEAR TIE — CORRODED (BS 1351) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

SHEAR TIE CORRODED ON SHORT FRAME JUST FWD OF RIGHT SIDE BS 1351 ON FWD SIDE. REPLACED SHEAR TIE.

Part: SKIN — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

AFT CARGO COMP INTERNAL SKIN IS CORRODED BETWEEN BS 1197+22 - 1197+44, S36R AFT OF REPAIR DOUBLER. C/W SRM 53-00-01.

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 AFT CARGO COMP SHEAR TIE IS CORRODED AT STA 1197+22, S36R- S37R. CORRSION OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1379215)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 SHEAR TIE AT STA.1197+44 BETWEEN S35R AND 36R CORRODED AND OUT OF LIMITS. SHEAR TIE REPLACED. (LP 1379216)

Part: FLOORBEAM — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 CORROSION UNDER NUTPLATES ON FLOOR BEAM AT STA.1197 LBL 28 TO LBL41. REMOVED AND REPLACED BEAM. (LP 1375178)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 AFT CARGO COMP SHEAR TIE IS CORRODED AT STA 1197+66, S35R - S36R. CORRISION IS OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1371360)

Part: FLOORBEAM — CORRODED (BS 654) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 FLC LOWER FLOOR BEAM UPPER CHORD IS CORRODED AROUND NUTPLATE AT STA 654+121, BL25REMOVED CORROSION 100% MAT. LOSS FOUND TO BE OUT OF LIMITS. EPLACED WITH NEW "J" CHORD. (LP 1369739)

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 HORZ STAB BOX HAS CORR ON TOP SKIN JUST ABOVE PANEL 341AZ CORROSION OUT OF LIMITS. C/W ERA 582917-14. (LP 1369339)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 SHEAR TIE AT STA.1197+44 BETWEEN S38R AND 39R CORRODED. REPLACED SHEAR TIE (LP 1366670)

Part: SHEAR TIE — CORRODED (BS 1175) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 AFT CARGO COMP SHEAR TIE IS CORRODED AT STA 1175, S35R-S36R. REPLACED SHEAR TIE. (LP 1367311)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 AFT CARGO COMP SHEAR TIE IS CORRODED AT STA 1197,S36R-S37R. REPLACED SHEAR TIE. (LP1367317)

Part: STRINGER — CORRODED (BS 420) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 STRINGER 36R CORRODED AT STA 420. REPLACED STRINGER. (LP 1365388)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 AFT CARGO COMP SHEAR TIE IS CORRODED AT STA 1197+44, S37L-S38L. REMOVED SHEAR TIE (LP 1366696)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 AFT CARGO COMP SHEAR TIE IS CORRODED AT STA 1197+66, S39L - S39R. CORROSION OUT OF LIMITS AND REPLACED SHEAR TIE. (LP 1365174)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 AFT CARGO COMP SHEAR TIE IS CORRODED AT STA 1197+88, S39L - S39R. CORROSION OUT OF LIMITS. SHEAR TIE REPLACED. (LP 1366691)

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 SHEAR TIE FOUND TO BE OUT OF LIMITS. REPLACED SHEAR TIE (LP 1362637)

Part: SHEAR TIE — CORRODED (BS 1175) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

LEVEL 2 CORRISION AFT CARGO COMPARTENT SHEAR TIE IS CORRODED AT STA 1175, S37R-38R. FOUND OUT OF LIMITS. SHEAR TIE REPLACED. (LP 1362596)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

AFT CARGO COMP SHEAR TIE IS CORRODED AT STA 1197+66, S37T-S38R BLEND CHECK LIMITS, FOUND CORROSION OUT OF LIMITS. (LP 1362622)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 AFT CARGO COMP SHEAR TIE IS CORRODED AT STA 1197+132, S37R - S38R. CORRISION OUT OF LIMITS. SHEAR TIE REPLACED. (LP 1369345)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 AFT CARGO COMP SHEAR TIE IS CORRODED AT STA 1197 + 22, S38R-S39R. CORRISION OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1362609)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

AFT CARGO COMP SHEAR TIE IS CORRODED AT STA 1197+66, S36R-S37R BLEND CHECK LIMITS. CORROSION OUT OF LIMITS. SHEAR TIE REPLACED. (LP 1362626)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

LEVEL 2 CORROSION AFT CARGO COMP SHEAR TIE IS CORRODED AT STA 1197+66, S38R-S39R . CORROSION FOUND OUT OF LIMITS. REPLACED SHEAR TIE (LP 1362615)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

LEVEL 2 CORROSION AFT CARGO COMP SHEAR TIE IS CORRODED AT STA 1197 + 22, S39L-S39R . CORRISION FOUND OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1362603)

Part: SHEAR TIE — CORRODED (BS 1329) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 CORRODED SHEAR TIE, JUST AFT OF FRAME 1329, BTW STR36L AND STR3 REPLACED SHEAR TIE(LP136096)

Part: SHEAR TIE — CORRODED (BS 1285) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 CORRODED SHEAR TIE, JUST AFT OF FRAME 1285, BTW STR39R AND STR38R, REPLACED SHEAR TIE. (LP 1360437)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2AFT CARGO COMP SHEAR TIE IS CORRODED AT STA 1197+132, S37L-S38L. CORROSION OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1361603)

Part: SHEAR TIE — CORRODED (BS 1241) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 CORRODED SHEAR TIE, JUST AFT OF FRAME 1241, BTW STR39L AND STR39R. REPLACED SHEAR TIE. (LP 1360429)

Part: SHEAR TIE — CORRODED (BS 1285) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 CORRODED SHEAR TIE, JUST AFT OF FRAME 1285, BTW STR37L AND STR38L. REPLACED SHEAR TIE (LP 1360431)

Part: SHEAR TIE — CORRODED (BS 1329) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 CORRODED SHEAR TIE, JUST AFT OF FRAME 1329, BTW STR39L AND STR39R. CORROSION OUT OF LIMITS. SHEAR TIE REPLACED (LP 1361584)

Part: SHEAR TIE — CORRODED (BS 1285) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 CORRODED SHEAR TIE, JUST AFT OF FRAME 1285, BTW STR36L AND STR37L. REPLACED SHEAR TIE. (LP 1360433)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 AFT CARGO COMP SHEAR TIE IS CORRODED AT STA 1197+132, S35R-S36R. CORROSION OUT OF LIMITS. SHEAR TIE REPLACED. (LP1361602)

Part: SHEAR TIE — CORRODED (BS 1329) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 CORRODED SHEAR TIE, JUST AFT OF FRAME 1329, BTW STR37L AND STR38L. REPLACED SHEAR TIE (LP 1360956)

Part: SHEAR TIE — CORRODED (BS 1502) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 BULK CARGO - SHEAR TIE AT STA.1502 CORRODED BETWEEN STRINGERS 39L AND 39R CORRODED OUT OF LIMITSSHEAR TIE REPLACED. (LP 1361577)

Part: SHEAR TIE — CORRODED (BS 1241) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 CORRODED SHEAR TIE, JUST AFT OF FRAME 1241, BTW STR38L AND STR39L. CORRISION FOUND OUT OF LIMITS. SHEAR TIE REPLACED. (LP 1360438)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 AFT CARGO COMP SHEAR TIE IS CORRODED AT STA 1197+132, S36R - S37R. REPLACED SHEARTIE (LP1360202)

Part: STRINGER CLIP — CORRODED (BS 1395) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 FRAME TO STRINGER ATTACH CLIP AT STA.1395 AT S39L CORRODED BLENDED FRAME TO STRINGER CLIP AT STA 1395 S-39L, 0.030 REMAINING OF 0.040, FOUND TO BE OUT OF LIMITS. REPLACED CLIP. (LP 1359982)

Part: SKIN — CRACKED (BS 1702) · airframe 122,247 hrs · 21,981 cycles

LEFT AFT FUSELAGE STA 1702 JUST BELOW STRINGER 6L EXTERIOR SKIN IS CRACKED EXTENDING AFT FROM RIVET HEAD. REPAIRED PER SRM 53-80-01. (LP 1359045)

Part: FLOOR SUPPORT — CORRODED (BS 1153-1175) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 FLOOR PANEL ATTACH ANGLE AT STA.1153 - 1175 RBL 44 HAS SMALL AREA OF CORROSION FORMING ON TOP SURFACE OUT OF LIMITS. REPLACED ANGLE. (LP 1351902)

Part: STRINGER CLIP — CORRODED (BS 1351) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 CLIP SHOWS SIGN OF CORROSION ON FWD SIDE OF SHORT FRAME, JUST FWD OF STA1351 RIGHT SIDE. REPLACED STRINGER CLIP. (LP 1351895)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 SHEAR TIE AT STA.1197+110 BETWEEN S39L AND 39R CORRODED. REPLACED SHEAR TIE.

Part: ANGLE — CRACKED (CLOSEOUT PANEL) · airframe 122,247 hrs · 21,981 cycles

CLOSE OUT ANGLE CRACKED AT INBD UPPER AREA IN PYLON AS SEEN THROUGH PANEL 436AL. REPLACED PYLON CLOSE OUT ANGLE (LP 1351374)

Part: SHEAR TIE — CORRODED (BS 1439) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 BULK CARGO - SHEAR TIE AT STA.1439 CORRODED BETWEEN STRINGERS 39L AND 39R. SHEAR TIE REPLACED. (LP 1350445)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 SHEAR TIE AT STA.1197+132 BETWEEN S36L AND 37L CORRODED FOUND OUT OF LIMITS AND REPLACED. (LP 1350442)

Part: SHEAR TIE — CORRODED (BS 1540) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 BULK CARGO - SHEAR TIE AT STA.1540 CORRODED BETWEEN STRINGERS 39L AND 39R. FOUND TO BE OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1350465)

Part: SHEAR TIE — CORRODED (BS 1219) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 SHEAR TIE AT STA.1219 BETWEEN S38L AND 39L CORRODED AND OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1348972)

Part: SHEAR TIE — CORRODED (BS 1285) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 FAA FINDING SHEAR TIE CORRODED AT STA 1285 AT S39L-S38L. FOUND TO BE OUT OF LIMITS. REPLACED SHEAR TIE. (LP 135077)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 SHEAR TIE AT STA.1197+44 BETWEEN S36R AND 37R CORRODED FOUND TO BE OUT OF LIMITS. REOKACED SHEAR TIE. (LP 1350061)

Part: SHEAR TIE — CORRODED (BS 1480) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 BULK CARGO - SHEAR TIE AT STA.1480 HAS CORROSION FORMING BETWEEN STRINGERS 39L AND 39R BLENDED SHEAR TIE AT STA 1480 BETWEEN S-39L-39R, 0.040 REMAINING OF 0.050, FOUND TO BE OUT OF LIMIT. REPLACED SHEAR TIE. (LP 1350072)

Part: SEAT TRACK — CORRODED (BS 1210) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 UPPER CABIN SEAT TRACK RBL 88 STA 1210 CORRODED. REPLACED SEATTRACK UPPER CABIN STA 1209-1429 RBL88 (1350197)

Part: SHEAR TIE — CORRODED (BS 1219) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 SHEAR TIE AT STA.1219 BETWEEN S35R AND 36R CORRODED AND FOUND OUT OF LIMITS. REPLACED NEW SHEAR TIE. (LP 1348974)

Part: SHEAR TIE — CORRODED (BS 1219) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 SHEAR TIE AT STA.1219 BETWEEN S39L AND 39R CORRODED. FOUND OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1348975)

Part: SHEAR TIE — CORRODED (BS 1307) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 SHEAR TIE AT STA.1307 BETWEEN S39L AND 39R CORRODED. REPLACED SHEAR TIE. (LP 1350066)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 SHEAR TIE AT STA.1197+88 BETWEEN S37R AND 38R CORRODED. FOUND OUT OF LIMITS REPLACED SHEAR TIE. (LP 1349635)

Part: SHEAR TIE — CORRODED (BS 1219) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2SHEAR TIE AT STA.1219 BETWEEN S36L AND 37L CORRODED. FOUND OUT LIMITS. REPLACED SHEAR TIE. (LP 1348978)

Part: SHEAR TIE — CORRODED (BS 1219) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2SHEAR TIE AT STA.1219 BETWEEN S37L AND 38L CORRODED. FOUND OUT OF LIMITS AND REPLACED SEAT TRACK. (LP 1348976)

Part: SHEAR TIE — CORRODED (BS 1219) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 ALC - SHEAR TIE AT STA. 1219 BETWEEN S38R AND 39R CORRODED BLENDED SHEAR TIE AT STA 1219 BETWEEN S-38R-S-39R, FOUND TO BE OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1347419)

Part: SHEAR TIE — CORRODED (BS 1219) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 SHEAR TIE AT STA.1219 BETWEEN S36R AND 37R CORRODED BLENDED SHEAR TIE AT STA 1219 BETWEEN STRS 37R-36R, 0.008 REMOVED FROM 0.050 FOUND TO BE OUT OF LIMITS. REPLACED SHEAR TIE. (LP1347415)

Part: SHEAR TIE — CORRODED (BS 1219) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 SHEAR TIE AT STA.1219 BETWEEN S37R AND 38R CORRODED BLENDED SHEAR TIE AT STA 1219 BETWEEN S 37R-S38R, 0.010 REMOVED FROM 0.050, FOUND TO BE OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1347418)

Part: SHEAR TIE — CORRODED (BS 1417) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 BULK CARGO - SHEAR TIE AT STA.1417 CORRODED BETWEEN STRINGERS 39L AND 39R SHEAR TIE AT STA 1417 BETWEEN STRINGERS 39L-39R FOUND TO BE 100% MATERIAL LOSS REMOVED AND REPLACED SHEAR TIE. (LP 13473210)

Part: SHEAR TIE — CORRODED (BS 1540) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 BULK CARGO - SHEAR TIE AT STA.1540 CORRODED BETWEEN STRINGERS 38L AND 39L. FOUND CORROSION OUT OF LIMITS AND REPLACED. (LP 1345707)

Part: SHEAR TIE — CORRODED (BS 1540) · corrosion level 2 · airframe 122,247 hrs · 21,981 cycles

CORROSION LEVEL: 2 BULK CARGO - SHEAR TIE AT STA.1540 CORRODED BETWEEN STRINGERS 38R AND 39R ON AFT SIDE OF FRAME. CORROSION OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1345712)

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 121,520 hrs · 21,891 cycles

EMERGENCY LIGHTS A SEAT 40FG ARE INOPERATIVE. FOUND DISCONNECTED EMERGENCY LIGHT WIRE BEHIND SIDEWALL AND RE-CONNECTED. SYSTEM OPERATION IS NORMAL. MCO/PLAC REMOVED.

Part: ACCESS DOOR — MISSING (RT WING) · airframe 120,763 hrs · 21,799 cycles

FOUND ON PDC INSPECTION, RIGHT WING LEADING EDGE SLAT #3 AFT OF. LUBRICATION ACE DOOR MISSING. INSTALLED RT WING #3 L/E SLAT MECHANISM LUBRICATION ACCESS DOOR. MCO/PLAC REMOVED. (LP 4212496)

Part: WIRE — PULLED (CABIN) · airframe 119,266 hrs · 21,597 cycles

EMERGENCY LIGHTS AT SEAT 40F AND 31 F INOPERATIVE. FOUND WIRES PULLED OUT OF PLUG AT SIDE WALL UNDER THE SEATS. REPAIRED WIRES. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 118,875 hrs · 21,543 cycles

EMERGENCY PATH LIGHTS AT SEATS 26AB ARE INOPERATIVE. FOUND CONNECTOR ON 26A NEXT TO SIDEWALL SEAT FRAME UNDERNEATH WIRE PULLED OUT OF PIN. REPLACED CONNECTOR AT SEAT FRAME. MCO/PLAC REMOVED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 116,605 hrs · 21,243 cycles

WHILE PERFORMING PDC, FOUND EMERGENCY LIGHT RIGHT SIDE NOT TESTING. REPLACED THE BATTERY PACK AND CHARGER. SYSTEM OPS NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 115,822 hrs · 21,149 cycles

DAMAGE FOUND ON RIGHT NOSE OF AIRCRAFT APPROXIMATELY STA 196-220 STR 30R. REPAIRED PER ERA 569261-14.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 115,059 hrs · 21,046 cycles

SEAT 31B WHITE EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE FOUND A CONNECTOR DISCONNECTED AND CONNECTED . SYSTEM OPS NORMAL.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 114,392 hrs · 20,940 cycles

UT INSP ON LT STA955 FAIL-SAFE STRAP FOUND CRACK AND REPAIRED.

Part: PANEL — DAMAGED (NOT REPORTED) · airframe 114,392 hrs · 20,940 cycles

FOUND MID BALL TRANSFER PANEL REPAIR DOUBLER DAMAGED. REPLACED THE REPAIR IAW SRM 53-00-53, REPAIR 4, AND INSTALLED IAW SRM 51-40-02.

Part: FRAME — CRACKED (BS 1809) · airframe 114,392 hrs · 20,940 cycles

DURING HFEC INSPECTION, BS 1809.5 BULKHEAD OUTER FRAME RT SIDE FOUND CRACKED, .5 INCHES IN LENGTH. REPAIRED THE FRAME.

Part: SEAT TRACK — CORRODED (BS 754-1098) · corrosion level 2 · airframe 114,392 hrs · 20,940 cycles

FOUND CORROSION ON THE CABIN SEAT TRACK RBL 88.5, BS 754 TO 1098. FOUND TO BE OUT OF LIMIT IAW SRM 53-00-52. REPAIRED THE SEAT TRACK.

Part: CONNECTOR — MISSING (EMERGENCY LIGHTS) · airframe 113,307 hrs · 20,772 cycles

FOUND EMERGENCY SEAT LIGHTS TO SIDEWALL WIRE CONNECTOR MISSING AT 38AB. REPLACED WIRE CONNECTOR. SYSTEM OPERATION IS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 113,289 hrs · 20,768 cycles

DURING SERVICE RIGHT EMERGENCY ESCAPE PATH LIGHTS ARE INOPERATIVE ROW 22 TO 32. REPLACED POWER SUPPLY. SYSTEM OPERATION IS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 113,307 hrs · 20,772 cycles

EMERGENCY LIGHTS BETWEEN SEATS 23 &24 ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY. SYSTEM OPERATION NORMAL.

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHTS) · airframe 112,905 hrs · 20,711 cycles

WHITE AISLE EMERGENCY LIGHTS AT 38B ARE INOPERATIVE. RESEATED LIGHT CONNECTOR. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 112,645 hrs · 20,671 cycles

DURING SERVICE CHECK FOUND RIGHT EMERGENCY ESCAPE PATH LIGHTS FROM ROWS 22 -32 INOPERATIVE. FOUND CONNECTOR AT SEAT 24 DISCONNECTED AND SECURED AND REPLACED CHARGERS AND BATTERY PACK M9009 & M737. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 111,160 hrs · 20,441 cycles

INTERMITTENT SLIDE LIGHTS DOOR 1L & 2L. RELAMPED AND CLEANED 1L AND 2L SLIDE LIGHT ASSY.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 110,833 hrs · 20,396 cycles

2R LAV SMOKE DETECTOR WENT OFF DURING FLIGHT. REPLACED SMOKE DETECTOR AT MID RIGHT LAV.

Part: WIRE — UNSECURE (EMERGENCY LIGHTS) · airframe 106,196 hrs · 19,667 cycles

EMERGENCY LIGHTS AT SEAT 21F ARE INOPERATIVE. MAINTENANCE FOUND WIRES DISCONNECTED FROM THE PLUG AND SECURED. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 103,756 hrs · 19,324 cycles

EMERGENCY LIGHT AT CEILING ABOVE SEAT 33C IS INOPERATIVE. RECONNECTED THE CONNECTOR. SYSTEM OPERATION IS NORMAL.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 96,844 hrs · 18,358 cycles

NR 1 PYLON O/B SKIN FOUND CRACKED AT PANEL 432AL CUTOUT. REPAIRED AS PER ERA 518683-14.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 96,844 hrs · 18,358 cycles

FWD CARGO DOOR AFT LOWER CORNER OUTER SKIN AND SEAL REATINER DAMAGED. REPAIRED PER ERA 493184-14.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 96,844 hrs · 18,358 cycles

C-1 CARGO DOOR LOWER AFT CORNER OUTER SKIN AND SEAL RETAINER DAMAGED. REPAIRED PER ERA 493184-14. (LP 1185544)

Part: SPAR — CRACKED (LT WING) · airframe 96,844 hrs · 18,358 cycles

LEFT WING FRONT SPAR 783 ONE TENSION BOLT HOLE FOUND CRACK AT 3RD LAYER COUNT FROM AFT AT 6'O CLOCK POS APPROX "1/16" IN DEPTH. TENSION BOLD HOLE FREEZE PLUG REPAIR ACCOMPLISHED PER ERA 520027-14AD (LP 1185286)

Part: FITTING — UNKNOWN (WING) · airframe 96,844 hrs · 18,358 cycles

BOTH LT & RT WING BATHUB FITTING AND UNDERWING LONGERON FITTING TENSION BOLT. ACCOMPLISHED PER ERA A518688-14AD. (LP 1185379)

Part: FITTING — CRACKED (RT WING LONGERON) · airframe 96,844 hrs · 18,358 cycles

RT WING UNDERWING LONGERON FITTING FOUND CRACKED AT RADIUS APPROX 1/2 INCH . FITTING REPLACED.

Part: SUPPORT — CRACKED (NR 2 PYLON) · airframe 96,844 hrs · 18,358 cycles

NR 2 PYLON TRAILING EDGE FAIRING SUPPORT I/B AFT SKATE ANGLE AFT END FOUND CRACKED. REPAIR ACCOMPLISH PER ERA 518682-14. (LP 1183889)

Part: FITTING — CRACKED (LONGERON) · airframe 96,844 hrs · 18,358 cycles

LONGERON FITTING FOUND CRACKED AT RADIUS APPROX 1/2 INCH. LONGERON FITTING REPLACED.

Part: FLOORBEAM — DAMAGED (BS 348) · corrosion level 2 · airframe 96,844 hrs · 18,358 cycles

BS 348 LBL 50 TO RBL 50 FLOORBEAM UPPER TEE DAMAGED. REPAIRED IAW SRM 53-00-51.

Part: FLOORBEAM — DAMAGED (BS 654) · airframe 96,826 hrs · 18,354 cycles

BS 654+88 RBL 22 FLOORBEAM WEB DAMAGED. REPAIRED IAW ERA 518672-14.

Part: FLOORBEAM — DAMAGED (BS 654) · airframe 96,826 hrs · 18,354 cycles

BS 654+88 RBL 22 FLOO BEAM WEB FOUND CRACKED. REPAIRED IAW ERA 518672-14.

Part: WEDGE — DEBONDED (NR 9 SLAT) · airframe 96,826 hrs · 18,354 cycles

RT WING NR 9 SLAT WEDGE UPPER SURFACE FOUND DEBOND. HOT BOND REPAIR PER SRM 57-43-02.

Part: WEDGE — DEBONDED (NR 2 SLAT) · airframe 96,826 hrs · 18,354 cycles

RT WING NR 12 SLAT WEDGE UPPER SKIN FOUND DEBONDED. HOT BOND REPAIRED IAW SRM 57-43-02.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 96,826 hrs · 18,354 cycles

SPAR BULKHEAD FITTING AREA THE LOWEST FASTENER FOUND CRACK AT FAILSAFE STRAP AT 5"0 CLOCK POSITION. REPAIRED IAW ERA 515823-14AD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 91,810 hrs · 17,710 cycles

EMERGENCY ESCAPE LIGHTS SEATS 32-39 FG INOPERATIVE. REPLACED BATTERY CHARGER ASSY POSITION M9010. OPS CHECKED GOOD IAW AMM 33-50 MFG 2012-1.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 91,546 hrs · 17,680 cycles

EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHT) · airframe 91,213 hrs · 17,638 cycles

COCKPIT EMERGENCY LIGHT SIGN BATTERY WEAK. REPLACED BATTERY PACK. CHECKED GOOD PER AMM 33-51.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 89,143 hrs · 17,404 cycles

EMERGENCY PATH LIGHTING AT SEAT 35F INOP. REPLACED M9010 BATTERY CHARGER PER B767-300 AMM 33-51, FOUND CONNECTOR AT SEAT BY SIDEWALL BROKEN REPAIRED PER BOEING SWPM 20-30.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 89,041 hrs · 17,391 cycles

EMERGENCY ESCAPE PATH LIGHTS AT SEAT 24F ARE INOPERATIVE. MAITENANCE RE-TERMINATED CONNECTOR. SYSTEM OPERATION IS NML.

Part: PIN — DEFECTIVE (CABIN) · airframe 88,847 hrs · 17,369 cycles

EMERGENCY LIGHTS AT SEAT 26B ARE INOPERATIVE. MAINTENANCE REPLACED PIN. SYSTEM OPERATION IS NORMAL.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 88,014 hrs · 17,264 cycles

C-1 DOOR WAS DAMAGED IN THE LOWER AFT CORNER DUE TO CONTACT WITH GROUND SUPPORT EQUIPMENT. PERMANENT REPAIR PER ERA 493184-14 REV C.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 86,915 hrs · 17,141 cycles

EMERGENCY ESCAPE LIGHT AT 23F IS INOPERATIVE. MAINTENANCE RE-TERMINATED CONNECTOR AT SIDEWALL. SYSTEM OPERATION IS NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 86,896 hrs · 17,139 cycles

MAINTENANCE FOUND EMERGENCY LIGHTS INOPERATIVE AT SEATS 21 -29, RIGHT SIDE OF CABIN. MAINTENANCE REPLACED THE CHARGER ASSEMBLY AND THE OPERATIONAL CHECK WAS GOOD.

Part: LIGHT — MISINSTALLED (L1 DOOR SLIDE) · airframe 84,529 hrs · 16,858 cycles

SLIDE LIGHT AT L1 IS INOPERATIVE. MX FOUND HOLDER BACKWARDS AND REINSTALLED THE HOLDER. SYS OPS IS NORMAL.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 84,100 hrs · 16,804 cycles

EMERGENCY CEILING LIGHT AT SEAT 30AB ARE INOPERATIVE. MX REPLACED THE FUSE 2 AT M733 POWER SUPPLY. SYS OPS IS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 83,317 hrs · 16,711 cycles

EMERGENCY ESCAPE PATH LIGHTS AT SEAT 22GF ARE INOPERATIVE. THE LUMINATOR AND BATTERY CHARGER WAS REPLACED. SYSTEM OPS IS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,201 hrs · 16,698 cycles

MX INSPECTED THE VERTICAL EXIT EMERGENCY LIGHT AT R1 DOOR AND REPLACED THE EXIT IDENTIFIER LIGHT BASE. SYS OPS IS NOW NORMAL.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 81,433 hrs · 16,499 cycles

EMERGENCY SEAT LIGHTS AT 40 FIN OP CREW REST SEAT SECURED CONNECTION.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 81,414 hrs · 16,497 cycles

EMERGENCY SEAT LIGHTS AT 40FG INOP-SECURED CONNECTION. OP CKS GOOD LIGHT.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,379 hrs · 16,493 cycles

EMERGENCY LIGHTS ROW 32-40 GF ARE INOPERATIVE. MX REPLACED CHARGER ASSY M9010. SYS OPS IS NORMAL. (DL76G101416)

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 80,304 hrs · 16,363 cycles

DAMAGE OCCURRED TO LOWER SKIN CAUSING DELAMINATION TO EXTENT THAT LOWER SKIN AND SOME LOW DENSITY HONEYCOMB CORE REQUIRED REPLACEMENT. C/A: COMPLY WITH ER/A 480754-14.

Part: ENGINE — OVERTEMP (NR 2) · airframe 77,564 hrs · 16,021 cycles

RT ENGINE OVERTEMP DURING ENGINE START. EGT EXCEEDANCE CAT D OPENED ENGINE FOR BORO PER M/M 72-00-00-60 273001. C/W NR 2 ENG 695446 BOROSCOPE FOR HOT START ABOVE PER M/M 72-00-00-601. NO DAMAGE FOUND QC 1510. RE-INSTALLED BORO PLUGS AND CRANK PAD COVER. LEAK CHECK GOOD.

Part: ENGINE — LEAKING (NR 1) · airframe 77,393 hrs · 16,002 cycles

NR 1 ENGINE HIG OIL USAGE, OIL COMING OUT OF RECOUP DUCT. REPLACING NR 1 ENGINE.

Part: ISOLATION VALVE — INOPERATIVE · airframe 76,861 hrs · 15,942 cycles

ACFT RTB DUE TO RIGHT ISOLATION VALVE INOP. REMOVED AND REPLACED RT ISOLATION VALVE PER M/M.

Part: CONTROL VALVE — SLOW (APU BLEED) · airframe 75,779 hrs · 15,818 cycles

APU SHUTDOWN ON PUSHBACK WITH FAULT LIGHT. ECU FAULTED REV FLOW. REPLACED SURGE CONTROL VALVE. CKS GOOD MFG P/N 979806-12.

Part: INDICATOR — INOPERATIVE (STDBY ATTITUDE) · airframe 74,582 hrs · 15,678 cycles

STANDBY ATTITUDE INDICATOR INOP. REPLACED INDICATOR.

Part: RECEPTACLE — DAMAGED (AUDO SYSTEM) · airframe 74,269 hrs · 15,631 cycles

ACRID ODOR AY SEAT 2A AND 2B. FOUND AUDIO JACK AT SEAT 2B EXTREMELY HOT AND PARTIALLY MELTED. REPLACED AUDIO JACK, NO HEAT AND AUDIO OPS CK GOOD. AUDIO QUARANTINE PER TOPP 20-60-02.

Part: ELECTRICAL BOX — OVERHEATED (2 A/ 2B) · airframe 74,218 hrs · 15,619 cycles

DUE TO FUMES THE IFE SYSTEM WAS SHUTDOWN. REMOVED AND REPLACED DC SEB P/N RD-FA 3124-07. REMOVED AND REPLACED SPM P/N RD-FA 3621-01 AND R SAC CONTROL BOX P/N PS4-52222-52. ALL IFE AND SEAT FUNCTION OPS NORMAL AT 5 A/B.

Part: ELECTRICAL BOX — MALFUNCTIONED (CABIN) · airframe 74,209 hrs · 15,618 cycles

ELECTRICAL ODOR NEAR SEATS 2F/G. FOUND SEB AT 2A/B (NOT 2F/G) AT FAULT. MOVED SEB TO SEATS 5A/B. FWD TO MCO AND MEL PER 25-25-02A. SEATS 2A/B NOW GOOD. REMOVED AND REPLACED DC SEB P/N RD-FA 3124-07. REMOVED AND REPLACED SPM P/N RD-FA 3621-01 AND R SAC CONTROL BOX P/N PS4-52222-52. ALL IFE AND SEAT FUNCTION OPS NORMAL AT 5 A/B. REMOVED PLACARD.

Part: FLOORBEAM — CORRODED (FS 1480) · airframe 71,365 hrs · 15,303 cycles

DURING CURRENT HMV, HEAVY CORROSION WAS FOUND ON THE FS 1480 FLOORBEAM UPPER CHORD. ADDITIONAL INSPECTION REVEALED THAT THE CORROSION WAS ON AN EXISTING REPAIR (TEE REPAIR) BETWEEN LBL 73 AND LBL 44. THE EXISTING REPAIR WAS REMOVED AND A MODIFIED SRM REPAIR INSTALLED PER BOEING INSTRUCTIONS, AS DOCUMENTED IN ERA/ 466277-14

Part: FLOORBEAM — CORRODED (BS 287) · airframe 71,365 hrs · 15,303 cycles

CABIN FLOORBEAM STA 287 RBL 54-64 UPPER CORD FOUND CORRODED. REPAIRED ON NR AVM508026 PER SRM 53-00-51D FIGURE 201.

Part: FLOORBEAM — CORRODED (BS 1480) · airframe 71,365 hrs · 15,303 cycles

FLOORBEAM CORRODED AT STA 1480 RBL 32 TO BRL 48. BEAM REPAIRED ON NR AVM506152 PER SRM 53-00-51D FIGURE 201.

Part: FLOORBEAM — CORRODED (BS 1197) · airframe 71,365 hrs · 15,303 cycles

FLOORBEAM CORRODED AT STA 1197 RBL 34. BEAM REPAIRED ON NRAVM 523371 PER SRM 52-00-07 FIGURE 201 REPAIR 4 AT HMV3.

Part: SKIN — CORRODED (BS 1197 S36R) · airframe 71,365 hrs · 15,303 cycles

AFT CARGO STA 1197+12 TO 1197+26 AT STR 36R SKIN LAP INNER SKIN FOUND CORRODED AND SUBJECT SKIN REPAIR PER 53-00-01 FIGURE 201 REPAIR 12 TOTAL WEIGHT ADDED 14LBS. WORKED ON NR CARD AVM 510907.

Part: FLOORBEAM — CORRODED (BS 1197) · airframe 71,365 hrs · 15,303 cycles

FLOORBEAM CORRODED BOTTOM SIDE AT STA 1197+132 LBL40. REPAIRED ON NR AVM523900 PER 53-00-07 FIGURE 201 REPAIR 4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,365 hrs · 15,303 cycles

FLOORBEAM CORRODED AT STA 654+121 AT RBL 30 TO RBL 51. FLOORBEAM REPLACED PER 53-00-51D FIGURE 201 ON NR AVM511426.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,365 hrs · 15,303 cycles

FLOORBEAM CORRODED AT STA 654+66 AT LBL 18 TO LBL26. BEAM REPLACED PER 53-00-51D FIGURE 201 ON NR AVM511442.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,365 hrs · 15,303 cycles

FLOORBEAM CORRODED AT STA 654+88 AT RBL 22 TO RBL 29. BEAM REPLACED PER 53-00-51D FIGURE 201 ON NR CARD AVM511467.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,365 hrs · 15,303 cycles

FLOORBEAM CORRODED AT STA 654+110 RBL 22 TO RBL 29. BEAM REPLACED PER 53-00-51D FIGURE 201 ON NR AVM5111491.

Part: FLOORBEAM — CORRODED (BS 654) · airframe 71,365 hrs · 15,303 cycles

FLOORBEAM CORRODED AT STA 654+44 RBL 20 TO RBL 40. FLOORBEAM REPLACED PER 53-00-51D FIGURE 201 ON NR AVM529188.

Part: FLOORBEAM — CORRODED (BS 1480) · airframe 70,985 hrs · 15,262 cycles

FLOORBEAM CORRODED AT 1480 RBL 28 TO RBL56. REPAIRED ON AVM508455 PER SRM 53-00-51D FIGURE 201 AT HMV.

Part: ENGINE — HOT START (NR 2) · airframe 68,500 hrs · 14,973 cycles

PENDING HOT START IN STR. PRECAUTIONARY BORO SHOWED DAMAGE TO 10 BLADES OF HPC. CHANGED NR 2 ENGINE PER ROUTINE TRANSMITTAL 1T161.

Part: ACTUATOR — LEAKING (LT ELEVATOR) · airframe 67,068 hrs · 14,806 cycles

FLT 128/15 NOTIFIED MTC AT APPROX 2300E THAT RT SYS HYD WAS DOWN TO .43 AND FALLING. HAD CREW TURN OFF RT HYD AND FLUID LOSS STOPPED. CREW DECIDED TO DIVERT TO BOS. AFTER BOS MTC INSPECTED AIRCRAFT FOUND THE LEFT ELEVATOR-RT SYS PCA LEAKING HYD FLUID. REMOVED AND REPLACED LT ELEVATOR RT HYD SYS CTR POSITION PCA. OPS CHK AND LEAK CHK OK. ALL PER AMM. ALL RII REQUIREMENTS MET QC4021.

Part: FITTING — CORRODED (TE FLAPS) · airframe 66,218 hrs · 14,695 cycles

CORROSION WAS FOUND IN THE ATTACH HOLES OF THE LT AND RT INBOARD FLAP SUPPORT BEAMS. THE HOLES WERE OVERSIZED TO REMOVE THE CORROSION AND BUSHED.

Part: APU — UNKNOWN · airframe 66,051 hrs · 14,675 cycles

C HYD DEMAND DURING FLAP OPERATION, USING APU AIR, APU AIR FWD TO MCO 49-11-01C. CHECKED APU PRESS. PRESS SHOW 36PSI. RAN BOTH PACK PRESS OK. RAN ADP OPS OK. EXT RETRACT FLAPS NO MSG. MCO AND PLACARD REMOVED.

Part: COMPUTER — UNSERVICEABLE (LEFT EICAS) · airframe 65,642 hrs · 14,622 cycles

A/C RTO AT 125KTS DUE TO A INCORRECT EGT EXCEDANCE OF THE LT ENGINE. THE LT EICAS COMPUTER DISPLAYED A RED EGT BOX AT 831 DEGREES C DURING TO ROLL. THE EGT EXCEEDANCE PARAMETER IS ABOVE 960 FOR THE CF680C2. ETOPS CATEGORY (E): PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: IDG — FAILED (NR 2 ENGINE) · airframe 64,192 hrs · 14,441 cycles

RT AC BUSS FAILURE WITH RT BUSS TIE ISLN LIGHT ILLUMINATED. THIS OCCURRED 5 MIN AFTER RT ENG STARTED. REPLACED NR 2 ENG IDG AND FLUSHED LINES. SERVICED IDG. RAN ENG PER PFHB, VOLTS AND FREQS NORMAL. ISOLATION NORMAL. DISCONNECTED AND RECONNECTED IDG. OPS AND LEAK CHECK GOOD. CLOSED AND SECURED COWLING.

Part: SHUTOFF VALVE — MALFUNCTIONED (LT ENGINE) · airframe 61,899 hrs · 14,171 cycles

HPSOV EICAS MSG ON TAKEOFF ROLL, LEFT ENGINE. RETURNED TO GATE. FOUND LINE TO HPSOV NOT TIGHT. RE-TIGHTENED LINE. RE-ACTIVATED THR/REV FOR MAINT. FOUND TERMS 2 AND 3 ON HPSOV REVERSED. FOUND CONNECTION AT FIREWALL DISCONNECT LOOSE. TIGHTENED CONNECTION. REPLACED HPSOV AND HPC. CHECKED GND BACK TO E3 RACK. RAN ENGINE BLEED. SHIFT NORMAL.

Part: BRAKE — DAMAGED (LEFT MLG) · airframe 61,701 hrs · 14,148 cycles

NR 6 BRAKE CARBON STATOR BROKEN. LARGE PIECE MISSING AND PUCK LEAKING. REPLACED BRAKE ASSY, OPER/LEAK CK NORMAL.

Part: ENGINE — DAMAGED (NR 1) · airframe 59,944 hrs · 13,933 cycles

DAMAGED BRACKETS, VSV LEVER ARMS, AND HEAT SHIELDS ON NR 1 ENGINE. REPLACED ENGINE.

Part: OVEN — ODOR (AFT GALLEY) · airframe 59,122 hrs · 13,836 cycles

AFT GALLEY OVEN ELEC SMELL. REPLACED SAME.

Part: FUSE — FAILED (POWER SUPPLY) · airframe 57,576 hrs · 13,643 cycles

ON EMERGENCY LIGHT TEST, FWD CABIN EMERGENCY LIGHTS INOP ON BUSINESS ELITE SEATS. REPLACED FUSE IN POWER SUPPLY.

Part: CONTROL PANEL — FAILED (COCKPIT) · airframe 56,042 hrs · 13,418 cycles

CABIN AUTO INOP EICAS MSG CAME ON AS A/C WAS LEVELING OFF AT FL 370. CABIN ALT AUTO 2 AND CABIN ALT AUTO 2 STATUS MSG, AUTO INOP LIGHT ILLUMINATED ON PRESS CONTROL PANEL. REPLACED CABIN PRESSURE CONTROL PANEL.

Part: CONTROL PANEL — FAULTY (NR 2 ENG FUEL) · airframe 48,857 hrs · 12,324 cycles

RT ENGINE TOOK ONE MINUTE TO SHUTDOWN WHEN FUEL CONTROL SWITCH MOVED TO SHUTOFF. REPLACED FIRE CONTROL PANEL.

Part: FAN — SMOKE (CABIN) · airframe 48,328 hrs · 12,231 cycles

CREW REPORTS RT RECIRC FAN EICAS MSG WITH SMOKE ODOR. QRH PROCEDURES COMPLIED WITH ODOR DISSIPATED. REPLACED RT RECIRCULATION FAN.

Part: WIRE — CHAFED (CARGO BAY) · airframe 48,079 hrs · 12,188 cycles

DURING L/O SERVICE, OPERATIONAL CHECK OF FWD CARGO COMPARTMENT NOTICED SPARKS AT STATION 500 UNDER FLOOR MATT AND THE FOLLOWING C/BS POPPED AT P35 PNL C166, C168 AND C169. MAINTENANCE IN PROGRESS REPAIRING WIRING. DAMAGE TO WIRING CAUSED BY A SPARE CARGO LOCK FALLEN INTO THE BOTTOM OF THE CARGO COMPARTMENT AND CHAFING ON WIRING.

Part: GCU — FAULTY (RIGHT) · airframe 47,160 hrs · 11,999 cycles

R GEN OFF WITH SLIGHT ELECTRICAL SMELL INITIALLY. APU POWERING THE RIGHT BUS. NO SMELL NOW. BPCU SHOWS R GEN NO RESPONSE FROM CONTROL FAULT AND WILL NOT RESET. T/S PER FIM 24-20-00. ALL WIRING CHECKS OK PER TABLE PG 180Y. FOUND GEN MAIN WINDINGS OPEN TO NEUTRAL WINDING. REPLACED RT GCU AND RESET BPCU. REPLACED RT IDG PER MM. LEA CKS OK. FOUND PIN 5 ON D4266J SHORTED. REPLACED D4266J AND CHECK NOW OK. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: LINE — CHAFED (LINE) · airframe 43,832 hrs · 11,418 cycles

DURING HMV IT WAS FOUND THAT A C-2 CARGO COMPARTMENT FIRE EXTINGUISHER DISCHARGE LINE WAS CHAFING ON APU AIR SUPPLY DUCT. REPLACED LINE.

Part: A/C PACK — MALFUNCTIONED (A/C BAY) · airframe 41,345 hrs · 10,991 cycles

LEFT PACK PRODUCED EXCESSIVE ODOR. TURNED IT OFF. OPERATED LT PACK FOR 1 HR ON GROUND. NO ABNORMAL SMELL IN CABIN. CHECKED PACK INLET. FOUND OK.

Part: ENGINE — FAILED (#2 ENGINE) · airframe 40,846 hrs · 10,923 cycles

SHIP 1505 FLT 107/13 FRA/JFK AT FL4K CAPT ATTEMPTED A LVL CHANGE AT FL4K RT ENG DID NOT RESPOND. THROTTLE BACK TO IDLE THE EGT CONTINUED TO CLIMB TO 895 THE ENG WAS SHUT DOWN./C MTC FOUND METAL IN TAIL PIPE. /C REPLACED THE ENG. ETOPS CATEGORY 'A': ANY IN-FLIGHT SHUTDOWN

Part: STEP — MISSING (OVERWING DOOR) · airframe 38,730 hrs · 10,589 cycles

ON ARRIVAL IN CVG CREW REPORTED HEARING CLICKING NOISE AND POPPING SOUND ON LEFT SIDE OF AC. MTC FOUND THE OVERWING EXIT STEP MISSING WITH FAIRING DAMAGE AND MINOR SKIN DAMAGE. REPLACED STEP AND REPAIRED SKIN PER ERA.

Part: PROXIMITY SENSOR — FAILED (RT WING SLIDE) · airframe 38,710 hrs · 10,585 cycles

AIRCRAFT PERFORMED AN AIR TURN BACK DUE TO A RIGHT WING SLIDE LIGHT EICAS MESSAGE. FOUND PROXIMITY SENSOR S-219 AT FAULT REPOSITIONED SEAL BITE OK ON PSEU CHKS OK

Part: SKIN — DENTED (FUSELAGE) · airframe 36,874 hrs · 10,272 cycles

THE FUSELAGE SKIN WAS DENTED AT FS 1373 AND STRINGER 28R, JUST FWD OF A FLOOD LIGHT CUTOUT. THE DAMAGE WAS REMOVED WITH A 2 X 2 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 378056-14.

Part: WIRE — EXPOSED (OXYGEN MASK) · airframe 36,098 hrs · 10,136 cycles

CAPT O2 MASK HAS EXPOSED WIRING ON THE OUTSIDE UNDERNEATH THE O2 LINE. REPLACED CAPT O2 MASK, SYSTEMS OPS NORMAL.

Part: SPAR — CRACKED (NR 1 PYLON) · airframe 35,675 hrs · 10,068 cycles

THE FWD UPPER SPAR WEB OF THE NR 1 PYLON WAS FOUND WITH A .25 INCH TYPICAL CRACK IN THE AFT, O/B CORNER OF THE POWER FEEDER CABLE CUTOUT. THE CRACK IS TYPICAL OF BAC S/B 767-54-0090. THE CRACKED AREA WAS ROUTED OUT AND A REPAIR/MOD DOUBLER INSTALLED PER THE S/B AND ER/A 377069-14, REV A.

Part: CHILLER — OVERHEATED (MID GALLEY)

MID GALLEY AFT CHILLER FAULT LIGHT ILLUMINATED. SHORTLY THERE AFTER NOXIOUS PLASTIC SMELL CAME FROM VENT AREA BETWEEN THE OVEN AND THE FREEZER CHILLER. OVEN C/B PULLED, BOTH ITEMS PUT ON MCO 25-20-01.

Part: FAN — FAILED (CABIN)

ELECTRICAL ODOR APPARENTLY FROM ENTERTAINMENT SYSTEM. STOPPED WHEN UNIT TURNED OFF. REPLACED COOLING FAN.

Part: LIGHT CONTROL — FAILED (COCKPIT)

FIRST OFFICERS INSTRUMENT FLOOD LIGHT GAVE OFF STRONG BURNING ODOR. TURNED OFF SWITCH AND SMELL CEASED. FOUND FLOOD LIGHT CONTROL ON P7 PRODUCING BURNING SMELL. REPLACED DIMMER.

Part: RETRACT MECH — MALFUNCTIONED (LANDING GEAR)

ON ATTEMPTED GEAR RETRACTION GEAR HANDLE STUCK AT OFF POSITION,10-15 SEC LATER HEARD A RELAY CLICK AND THEN HANDLE WAS ABLE TO BE MOVED TO THE UP POSITION. GEAR THEN RETRACTED NORMALLY. WHEN GEAR HANDLE LOWERED TO DOWN POSITION, AT 200 KTS, NOSE AND RT EXTENDED NORMALLY. NO LEFT MAIN GREEN DOWN AND GEAR DISAGREE EICAS, 40-50 SEC LATER LEFT MAIN INDICATED DOWN AND GEAR DISAGREE EXTINGUISHED. NORMAL LANDING AT JFK.

Part: BATTERIES — DISCHARGED (CABIN)

LT SIDE CABIN EMERGENCY PATH LIGHTS WOULD NOT EXTINGUISH. REPLACED BATTERY RACK ASSY AND BATTERIES FOR FWD LEFT.

Part: LINE — LEAKING (LT HYD SYST)

LEFT HYDRAULIC QUANTITY DECREASING .01/10 MIN, PRESS 3000, TEMP 14, QTY .55. REPLACED NR 1 ENGINE SUPPLY LINE IN STRUT AREA. LEAK CHECK NORMAL.

Part: FIRE LOOP — MALFUNCTIONED (NR 2 ENGINE)

EICAS MSG RT ENG OH LOOP -1- ON AFTER T/O AND STAYED ON. MTC IN PROGRESS. PREV MTC ACTION 17FEB. REPLACED WIRES W5316-001R AND W5306-002R PINS AND TERMINALS. MSG STILL ON EICAS. REPLACED M690 LOOP -2- CARD, ALL CKS GOOD. RAN ENG, NO FAULTS NOTED. REMOVED MCO AND PLACARD.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FOUND ON O/W II F/C AND B/C SEAT TRACK LIGHTS INOP. REPLACED POWER SUPPLY AND BATTERY OPS CKS OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

F/C EMERGENCY TRACK LIGHTS INOP. REPLACED POWER SUPPLY SYS, CKS NML.