N182DN

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 135,065 hrs · 19,691 cycles

SHIP 0182 -ATO- DUE TO LEFT FUEL QUANTITY AND TOTALIZER WENT BLANK. CORRECTIVE ACTION: FOUND FAULT OF FQIS FOR TU14 SHORTED IN TANK. REPLACED TU14. (0082496)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 134,928 hrs · 19,652 cycles

SHIP 182 EMERGENCY LIGHTS ROW 13-19 INOP. CORRECTIVE ACTION: R/R BATTERY PACK (M9011) PER B767 AMM 33-51. OPS CHK NORMAL. (4346866)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 134,156 hrs · 19,486 cycles

SHIP 182 AFT SIDE OF OVERHEAD EXIT SIGN COVER MISSING FOR AILE BETWEEN 13 B&C A/C LEFT. CORRECTIVE ACTION: FOUND EXIT LENS AND REINSTALLED PER B767-300 AMM 33-51. OK TO CONTINUE. (4925392)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 133,856 hrs · 19,437 cycles

SHIP 0182 -DIV- TO AMS DUE TO FIRE WARNING BELL ALERT WITH NO OTHER INDICATIONS AND UNABLE TO SILENCE. CORRECTIVE ACTION: RESET WEU. AURAL WARNING AND FIRE WARNING SYSTEMS TEST NML IN AIR AND GROUND MODE. R/R WARN ELEX BELL/CHIME MODULE, BOTH WARN ELEX POWER SUPPLIES AND FIRE OVERHEAT DETECTION CARD. C/W OVERWEIGHT LANDING INSP. A/C RTS.(4692466)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 133,447 hrs · 19,377 cycles

AIRCRAFT 0182, DOOR 1L EXIT SIGN OVER DOOR HANDLE BROKEN . CORRECTIVE ACTION: SECURED EXIT SIGN COVER PER AMM 33-22. (LP 4973106)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 133,137 hrs · 19,332 cycles

SHIP 182 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:13B. CORRECTIVE ACTION: NO FAULT FOUND @ 13B LENS COVER OK FOR SVC. REF B767 AMM 33-51 (2809808)

Part: UNKNOWN — UNKNOWN · airframe 132,097 hrs · 19,138 cycles

SHIP 182 DR 1L & 1R EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: R/R BATTERY PACK & CHARGER M1208 REF B767-300 AMM 33-51. OPS CK GOOD. (9448222)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 132,117 hrs · 19,144 cycles

SHIP 182 DOOR 1L WILL NOT ARM. CORRECTIVE ACTION: RE-SEQUENCED DOOR ARMING LEVER - NOW DOOR CHKS NRML IAW B767 AMM 52-10 - OK TO CONTINUE (9448224)

Part: UNKNOWN — UNKNOWN · airframe 132,066 hrs · 19,119 cycles

SHIP 0182 - DIV - TO SJU DUE TO AIRSPEED DISAGREE AND ASSOCIATED STATUS MESSAGES. CORRECTIVE ACTION: FOUND TAT PROBE NOT HEATING AND LEFT ADC FAULT. REPLACED TAT PROBE AND ADC. OPS NORMAL.(9894596)

Part: NONE — NONE · airframe 132,040 hrs · 19,113 cycles

SHIP 182 ON SVC CHK FOUND RT WING PANEL 521ACB MISSING. CORRECITVE ACTION: INSTALLED NEW PANEL PN. 114T2401-10 PER B767-300 AMM 57-41. OK FOR SVC. (9894564)

Part: NOT ENTERED — NOT ENTERED (NOT ENTERED) · airframe 131,709 hrs · 19,053 cycles

SHIP 182 OVHD EMERGENCY LT LENS MISSING AT SEATS 5D AND 26F. CORRECTIVE ACTION: OK TO DEFER PER MEL 33-51-01A. LTS OPERATING NORMAL. (9463557)

Part: NOT ENTERED — NOT ENTERED (NOT ENTERED) · airframe 131,709 hrs · 19,053 cycles

SHIP 182 LLCR LWR FWD BUNK EMER LT INOP. CORRECTIVE ACTION: DURING SVC CHECK FOUND LWR BUNK EMER LT INOP. PER CMM 25-29-02, REPLACED EMER LT ASSY, OPS CHECK NORMAL. OK FOR SVC. (9463556)

Part: SUPPORT RIB — CRACKED · airframe 131,337 hrs · 18,978 cycles

SHIP 182 LH WING LE NOSE FORMER ACTUATOR SUPPORT RIB AT LES 648 CRACK. CORRECTIVE ACTION: ACCOMPLISHED REPAIRED THE DENT AREA AS PER ER/A 14-604624AD (2556507)

Part: SLAT — DENTED · airframe 131,337 hrs · 18,978 cycles

SHIP 182 FOUND LHW SLAT NO.5 EDGE DENT, CORRECTIVE ACTION: ACCOMPLISHED REPAIRED THE DENT AREA AS PER SRM 51-70-10 (2555113)

Part: SLAT — CRACKED · airframe 131,337 hrs · 18,978 cycles

SHIP 182 FOUND LHW SLAT NO.4 T/E WEDGE AFT EDGE CRACK. CORRECTIVE ACTION: ACCOMPLISHED REPAIRED THE DAMAGED AREA AS PER B767-300 SRM 57-43-02-2R-1 (2555604)

Part: SKIN — CRACKED · airframe 131,337 hrs · 18,978 cycles

SHIP 182 EO TASK - DURING PERFORM W/C 5310-01376-0703 STEP 2, OPEN HOLE HFEC INSPECTION FOUND 01 CRACK IN SKIN AT FORWARD ROW SECOND FASTENER COUNT FROM TOP . CRACKING MUST BE REPAIRED PRIOR TO FURTHER FLIGHT. CORRECTIVE ACTION: ACCOMPLISHED REPAIRED THE DAMAGED AREA AS PER ER/A604629-14AD (2555476)

Part: SKIN — NONE · airframe 131,337 hrs · 18,978 cycles

SHIP 182 ERA 604629-14AD ISSUED FOR REPAIR TO STA 1809.5 SKIN NEAR S12AL. FOLLOW ON ACTION IS REQUIRED, DTA DTE REQUIRED, CORRECTIVE ACTION: DTA DTE DAMAGE TOLERANCE ANALYSIS IS DUE NO LATER THAN 12000 FC OR 2191 DAYS, FIRST TO OCCUR, AFTER SECTION I (2555195)

Part: STRUCTURE — CRACKED · airframe 131,337 hrs · 18,978 cycles

SHIP 182 DURING PERFORM W/C 5310-01376-0703 STEP 3 , HFEC INSPECTION FOUND 01 CRACK IN REMOVED CHORD AND THE CRACK IS FROM THE SEVENTH FASTENER COUNT FROM TOP. CORRECTIVE ACTION: ACCOMPLISHED REPAIRED THE DAMAGED AREA AS PER AMDS W/C 5310-01376-0705. (2554266)

Part: FASTENER — CRACKED · airframe 131,337 hrs · 18,978 cycles

SHIP 182 EO TASK - BY STEP 3 LFEC INSPECTION FOUND 02EA FASTENERS CRACKED ON THE LOWERMOST ROW OF INSPECTION AREA 2,ACCOMPLISH SECTION 07(LH) PRIOR TO FURHER FLIGHT. CORRECTIVE ACTION: ACCOMPLISHED REPAIRED THE DAMAGED AREA AS PER AMDS W/C: 5310-01376-0705 (2554261)

Part: NONE — NONE · airframe 131,334 hrs · 18,977 cycles

SHIP 182 DURING LAST C-CHECK (02JAN2019) AT STAG, ER/A 574076-14AD SECT. I REPAIR WAS ACCOMPLISHED ON A/C 182. CORRECTIVE ACTION: ACCOMPLISH ER/A 574076-14AD REV. A SECTION III EXTERNAL HFEC INSPECTION AT AREA 'A' AND AREA 'B' PRIOR TO 6,000 CYCLES OR 18,000 FLIGHT HOURS AFTER SECTION I REPAIR (2538698)

Part: NONE — NONE (NONE) · airframe 131,003 hrs · 18,911 cycles

DURING LAST H-CHECK (03JAN2019) AT STAG, ER/A 574045-14AD SECT. I REPAIR WAS ACCOMPLISHED ON A/C 0182. ACCOMPLISH ER/A 574045-14AD REV. A SECTION III PRIOR TO 6,000 CYCLES OR 18,000 FLIGHT HOURS AFTER SECTION I REPAIR.

Part: NONE — NONE · airframe 130,569 hrs · 18,837 cycles

SHIP 182 EMERGENCY EXIT SIGNS INOPERATIVE / LOCATIONS:603, CORRECTIVE ACTION: RE-SECURED EMERGENCY EXIT SIGNAT LOC 603 EXIT SIGN CHKS GOOD REF B767 AMM 33-51. (2388071)

Part: NONE — NONE · airframe 130,435 hrs · 18,814 cycles

AIRCRAFT 182, LT OVERHEAD EXIT SIGN AFT OF FIRST CLASS MISSING. CORRECTIVE ACTION: INSTALLED NEW EXIT SIGN PEER B767-300 AMM 25-63. LOG 6024593

Part: WARNING LIGHT — FALSE INDICATION · airframe 129,691 hrs · 18,692 cycles

SHIP 182 FA REPORTS 1L FA PANEL THAT 1R DOOR ARM LIGHT NO LONGER ILLUMINATION EVEN THOUGH DOOR IS ARMED, CORRECTIVE ACTION: COULD NOT DUPLICATE FAULT OPS NORMAL REF B767 AMM 52-73. OK FOR SVC NO 90 DAY HISTORY (7301610)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 127,331 hrs · 18,146 cycles

SHIP 182 DURING SERVICE CHECK FOUND SEVERAL CEILING EMERGENCY LIGHTS INOPERATIVE. CORRECTIVE ACTION: RELAMPED CABIN CEILING EMERGENCY LIGHTS. SYSTEM OPERATION IS NORMAL. (LP 7832241)

Part: PIN — BROKEN (OVERWING SLIDE) · airframe 126,845 hrs · 18,046 cycles

SHIP 182 DURING RIGHT OVER-WING SLIDE REPLACEMENT FOUND ALIGNMENT PINS BROKEN ON INSIDE OF THE SLIDE PACK DOOR. CORRECTIVE ACTION: REPLACED REALIGNMENT PINS AND INSTALLED ORIGINAL SLIDE. (LP 7477078)

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 126,490 hrs · 17,980 cycles

SHIP 182 MAINTENANCE FOUND FLIGHT DECK EXIT SIGN LENS DAMAGE BY FLIGHT DECK DOOR. CORRECTIVE ACTION: REPLACED FLIGHT EXIT SIGN LENS. (LP 7477006)

Part: STIFFENER — CRACKED (RT WING LE BEAM) · airframe 125,928 hrs · 17,838 cycles

DURING INSPECTION MAINTENANCE FOUND RIGHT WING FIXED LEADING EDGE NOSE BEAM STIFFENER LOCATED AT OFSS 525 IN CRACKED AT TOP EDGE. (JUST O/B OF NO. 8 TRACK.) C/W ERA 590241-14. (LP 1740139)

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 125,877 hrs · 17,821 cycles

SHIP 182 EMERGENCY LIGHTS AT 41 F INOPERATIVE. MAINTENANCE FOUND PUSHED PIN AT CONNECTOR NEAR SIDEWALL AND REPAIRED. SYSTEM OPERATION IS NORMAL. (LP 6994288)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 125,380 hrs · 17,673 cycles

EMERGENCY PATH LIGHT BATTERY INOPERATIVE AT 39J. CORRECTIVE ACTION: REPLACED BATTERY PACK AT 39J SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 125,377 hrs · 17,672 cycles

FLIGHT DECK OVER DOOR EMERGENCY EXIT LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY AND BATTERIES. SYSTEM OPERATION IS GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 125,276 hrs · 17,649 cycles

DURING SERVICE CHECK FOUND A SEGMENT OF EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER M737. SYSTEM OPERATION IS NORMAL.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 123,933 hrs · 17,453 cycles

EMERGENCY LIGHTS FROM ROW 5A TO 20B ARE INOPERATIVE. REPAIRED WIRE SPLICE AT SEAT 16B AND REPLACED BATTERY PACK CHARGER ABOVE CEILING PANEL. SYSTEM OPEARATION IS NORMAL.

Part: ACCESS PANEL — MISSING (NR 2 PYLON) · airframe 123,687 hrs · 17,417 cycles

ON WALK AROUND FOUND ACCESS PANEL MISSING ON #2 ENGINE PYLON INBOARD SIDE. REQUIRES MPN 311T3065-503. REF IPC 54-53-01-01. FIG. 01 ITEM 525 . NIS DTWFWD TO CDL 54-53-02. INSTALLED NEW PANEL PER B767 AMM 54-33 PLAC RMVD. (LP6130411)

Part: SOCKET — UNSECURE (CABIN) · airframe 123,615 hrs · 17,407 cycles

EMERGENCY LIGHTS AT SEAT 30B ARE INOPERATIVE. SECURED LIGHT SOCKET. SYSTEM OPERATION IS NORMAL.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 122,174 hrs · 17,218 cycles

EMERGENCY LIGHTS AFT OF RIGHT OF LAV 203 ARE INOPERATIVE. FOUND WIRE BROKEN UNDER CARPET AND REPAIRED. SYSTEM OPERATION IS NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 121,157 hrs · 17,068 cycles

EMERGENCY FLOOR LIGHT AT SEAT 24AB IS INOPERATIVE. REPAIRED BROKEN WIRE. SYSTEM OPERATION IS NORMAL.

Part: BULKHEAD — CORRODED (RT MLG WW) · corrosion level 2 · airframe 120,653 hrs · 16,996 cycles

CORROSION LEVEL: 2 TO REMOVE SEALANT AT RT MLG WHEEL WELL. REAR SPAR BULKHEAD NEAR PICKLE C/W ERA 573860-14. (LP 0913752)

Part: FRAME — CRACKED (FUSELAGE) · airframe 120,653 hrs · 16,996 cycles

HFEC INSPECTION FOUND 01 EA CRACK ON RH BS 883.5 FRAME INNER CHORD TRANSITION RADIUS. REPAIRED. (LP 0912493)

Part: FRAME — CRACKED (FUSELAGE) · airframe 120,653 hrs · 16,996 cycles

HFEC INSPECTION FOUND 01 EA CRACK ON RT BS 859.5 FRAME INNER CHORD TRANSITION RADIUS. CRACK REPAIRED. (LP 0912491)

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,653 hrs · 16,996 cycles

CORROSION LEVEL: 2 CORROSION FOUND ON STRINGER LOWER FLANGE.STA 1197+132 . S-19L. REPAIRED PER SRM 53-00-03. (LP 0912488)

Part: SKIN — CORRODED (BS 1175-1197) · corrosion level 2 · airframe 120,751 hrs · 17,014 cycles

CORROSION LEVEL 2 DURING HCK, CORROSION WAS NOTED ON THE LOWER FUSELAGE SKIN BETWEEN STA 1175-1197, S-36L. C/W ER/A 574289-14. (LP 0911289)

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 120,652 hrs · 16,995 cycles

FOUND TWO CRACK IN THE FWD CHORD AT BS1809.5 BULKHEAD OUTER RIGHT AND REPAIRED. (LP 0904639)

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

AFT CARGO COMPARTMENT FOUND FUSELAGE SKIN INERIOR CORROSION AT STA 1175 TO STA1197 S-36L. REPAIRED PER ERA 74289-14. (LP 0904784)

Part: FASTENER — LOOSE (NR 1 PYLON) · airframe 120,652 hrs · 16,995 cycles

NR 1 STRUT AFT FAIRING LOWER PANEL FASTENER FOUND LOOSEN. C/W ERA 396620-14. (LP 0904654)

Part: DOOR — GOUGED (R2) · airframe 120,652 hrs · 16,995 cycles

RE- EVALATE R2 DOOR AFT/ LOWER CORNER GOUGE. REPAIRED PER SRM 52-10-01. (LP 0904772)

Part: FASTENER — LOOSE (NR 1 PYLON) · airframe 120,652 hrs · 16,995 cycles

NR 1 STRUT AFT FAIRING LOWER PANEL FASTENER FOUND LOOSE. REPAIRED PER ERA 396620-14. (LP 0904670)

Part: FAILSAFE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,872 hrs · 17,028 cycles

CORROSION LEVEL 2 DURING HCK AT STAG, CORROSION WAS NOTED ON THE FAIL SAFE CHORD, STA 1562, S37L-37R C/W ERA 574252-14.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 02EA SHEAR TIE SURFACE CORROSION AT STA 1219. BETWEEN S-39R AND S-37R. REPLACED SHEAR TIE. (LP 0911364)

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 ANGLE ATTACHED TO FRAME ALONG S-17R, CORRODED AT STA 1362, STA 1329. STA 1307, STA 1285, STA 1274. C/W 574258-14. (LP 0912555)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 06EA SHEAR TIE SURFACE CORROSION AT STA 1219. BETWEEN S-39R AND S-34L. SHEAR TIE REPLACED. (LP 0911354)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPATMENT FOUND 03EA SHEAR TIE SURFACE CORROSION AT STA 1241. BETWEEN S-39R AND S-37L. REPLACED SHEAR TIE. (LP 0911268)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 03 EA SHEAR TIE SURFACE CORROSION AT STA 1197+132. BETWEEN S-38L AND S-35L. REPLACED SHEAR TIE (LP 0911292)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 BULK CARGO COMPARMTN FOUND 02EA SHEAR TIE SURFACE CORROSION AT STA 1540 BETWEEN S-39R AND S-38L. REPLACED SHEAR TIE. (LP 0911305)

Part: STRUCTURE — CRACKED (WING) · airframe 120,652 hrs · 16,995 cycles

AFTER HFEC FASTENER HOLES (NR 1 AND NR 2) WERE FOUND WITH CRACK INDICATIONS AND THE NR 4 NR 5 NR 6 NR 7 HOLE DIMETER CANNOT BE SATISFACTORILY .THE HOLE SIZE 0.325. C/W ERA 574045-14. (LP 0899037)

Part: STRUCTURE — CRACKED (WING) · airframe 120,652 hrs · 16,995 cycles

THE NR 1 HOLE FOUND CRACK. REAM THE HOLE TO 0.5755". C/W ERA 574045-14. (LP 0899020)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 120,652 hrs · 16,995 cycles

HFEC INSPECTION FOUND 01EA CRACK ON STA1809 BULKHEAD RIGHT FORWARD OUTER CHORD AT STRINGER 5R AS MARK. CRACK REPAIRED PER SRM 53-80-08. (LP 0899442)

Part: STRUCTURE — CRACKED (WING) · airframe 120,652 hrs · 16,995 cycles

THE FASTENER CODE A LOCATION .NR 1 HOLE FOUND CRACK, REAMED THE HOLE SIZE TO 0.5760. HOLE REPAIRED PER ERA 574076-14. (LP 0898989)

Part: SKIN — DEFECTIVE (WING) · airframe 120,652 hrs · 16,995 cycles

THE NEW STRINGER FOUND THE NR 66 HOLE LOOSEN AND NR 29 FASTENER THE DEFECT ON THE LT LOWER SKIN STRINGER REPAIRED PER ERA 574076-14. (LP 0899008)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 BULK CARGO COMPARTMENT FOUND 01 EA SHEAR TIE CORROSION AT 1562. BETWEEN S-39R AND S-39L. REPLACED SHEAR TIE. (LP 0899304)

Part: STRUCTURE — DAMAGED (WING) · airframe 120,652 hrs · 16,995 cycles

FASTENER CODE B LOCATION .THE NR 2 HOLE DIMETER :0.3460" IS GREATEER THAN 0.3185. REPAIRED PER ERA 574045-14. (LP 0899030)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,653 hrs · 16,996 cycles

CORROSION LEVEL: 2CORROSION FOUND ON SHAR TIE ON STA 1351. STR-16R. SHEAR TIE REPLACED. (LP 0912564)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1241. BETWEEN S-35R AND S-36R. SHEAR TIE REPLACED. (LP 0899329)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,653 hrs · 16,996 cycles

CORROSION LEVEL: 2 CORROSION FOUND ON SHEAR TIE, STA 1329, BTW S-16L TO S-17. REPLACED SHEAR TIE. (LP 0912653)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,653 hrs · 16,996 cycles

CORROSION LEVEL 2 :SEAT TRACK- CORROSION FOUND ON SEAT TRACK AROUND STA 753 TO STA 1048, RBL 88.5EL: 2. REPAIRED PER SRM 53-00-52. (LP 0912595)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,653 hrs · 16,996 cycles

CORROSION LEVEL: 2SEAT TRACK- CORROSION FOUND ON SEAT TRACK AROUND STA 753 TO STA 1098, LBL88.5. REPAIRED PER SRM 53-00-52. (LP 0912637)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1197+110. BETWEEN S-36L AND S-37L. CORROSION REPLACED. (LP 0905775)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1197+66. BETWEEN S-35L AND S-36L. REPLACED SHEAR TIE. (LP 0905746)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1197+22. BETWEEN S-39R AND S-38R. REPLACED SHEAR TIE. (LP 0905896)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1197. BETWEEN S-37R AND S-36R. REPLACED SHEAR TIE. (LP 0905789)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1197+110. BETWEEN S-39R AND S-38R AND REPLACED. (LP 0905812)

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 STRINGER (RT) LOWER FLAGE AT S-19R. STA 1197+24 FOUND CORRODED. REPAIRED PER SRM53-00-03. (LP 0912606)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1197. BETWEEN S-36R AND S-35R. REPLACED SHEAR TIE. (LP 0905730)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1197. BETWEEN S-36L AND S-37L AND REPLACED. (LP 0905905)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1197+132. BETWEEN S-39R AND S-38R AND REPLACED. (LP 0905888)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1219. BETWEEN S-36R AND S-35R. REPLACED SHEAR TIE. (LP 0905805)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1285. BETWEEN S-36L AND S-37L AND REPLACED. (LP 0905800)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1197+66. BETWEEN S-39R AND S-38R . SHEAR TIE REPLACED. (LP 0905818)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1263. BETWEEN S-36L AND S-37L. REPLACED SHEAR TIE. (LP 0905912)

Part: SKIN — CRACKED (RT WING) · airframe 131,334 hrs · 18,977 cycles

DURING AN H-CHECK AND DURING EM 5724-01010-44B, DISCREPANCY'S WERE NOTED DURING THE L-9.5 STRINGER ON THE RT WING LOWER WING SKIN. ER/A 574077-14AD SECT I ACCOMPLISHED.

Part: SKIN — CRACKED (LT WING) · airframe 131,334 hrs · 18,977 cycles

DURING AN H-CHECK AND DURING EM 5724-01010-44A, CRACK INDICATIONS WERE NOTED ON THE LT WING LOWER SKIN. REPAIRED IAW ER/A 574076-14AD SECT I..

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 SEAT TRACK- CORROSION FOUND ON SEAT TRACK AROUND STA 1428.45 TO STA 1444, RBL88.5 C/W 574079-14. (LP 0912543)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 SEAT TRACK- CORROSION FOND ON SEAT TRACK AROUND STA 1428 TO STA 1444, LBL88.5. C/W ERA 574079-14. (LP 0912550)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1285 .BETWEEN S-39R AND S-38R. REPLACED SHEAR TIE. (LP 0905677)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 BULK CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1461. BETWEEN S-30R AND S-31R AND REPLACED. (LP 0905719)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1197+132 .BETWEEN S-35R AND S-36R . REPLACED SHEAR TIE. (LP 0905688)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1197+44. BETWEEN S-36R AND S-35R. REPLACED SHEAR TIE. (LP 0905707)

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 BULK COPARTMENT FOUND 01EA SPLICE UPER SURFACE CORROSION AT ST 1502. S-32R AND REPLACED. (LP 0904389)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1241. BETWEEN S-39R AND S-38R. REPLACED SHEAR TIE. (LP 0905697)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA1197+22. BETWEEN S-39R AND S-39L AND REPLACED. (LP 0897950)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA1197+66. BETWEEN S-39R AND S-39L. SHEAR TIE REPLACED. (LP 0899316)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA1197+132. BETWEEN S-39R AND S-39L. SHEAR TIE REPLACED. (LP 0899333)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA1197+88. BETWEEN S-39R AND S-39L. REPLACED SHEAR TIE. (LP 0897957)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1197+44. BETWEEN S-39R AND S-39L OUT OF LIMITS AND REPLACED. (LP 0898006)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1307. BETWEEN S-36L AND S-37L. REPLACED SHEAR TIE. (LP 0904397)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT SAT 1197+110. BETWEEN S-39R AND S-39L. REPLACED SHEAR TIE. (LP 0899360)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 SEAT TRACK- CORROSION FOUND ON SEAT TRACK AROUND STA 1208.45 TO STA 1428.45, RBL 88.5. REPLACED SEAT TRACK. (LP 0912578)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1285. BETWEEN S-37L AND S-38L. SHEAR TIE REPLACED. (LP 0904393)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,652 hrs · 16,995 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA1197+132. BETWEEN S-39L AND S-38L OUT OF LIMITS. SHEAR TIE REPLACED. (LP 0897922)

Part: WIRE — DAMAGED (CABIN) · airframe 120,515 hrs · 16,977 cycles

EMERGENCY LIGHTS AT 27AB ARE INOPERATIVE. MAINTENANCE FOUND WIRE DAMAGED AND REPAIRED. SYSTEM OPERATION IS NORMAL.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 116,629 hrs · 16,482 cycles

COCKPIT EXIT SIGN ASSEMBLY INOPERATIVE DURING SERVICE CHECK. REPLACED THE SIGN.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 102,961 hrs · 14,760 cycles

EMERGENCY LIGHTS AT SEAT 35AB ARE INOPERATIVE. MAINTENANCE REPLACED THE CONNECTOR. SYSTEM OPEATION IS NORMAL.

Part: SPAR — CRACKED (NR 1 PYLON) · airframe 102,547 hrs · 14,713 cycles

NR 1 PYLON, FWD UPPER SPAR WEB, CRACKS AT FUEL LINE PASS-THROUGH C/W ERA 530931-14.

Part: SKIN — CRACKED (RT WING) · airframe 102,547 hrs · 14,713 cycles

CRACK INDICATION IN RT WING LOWER SKIN. REPAIRED IAW ERA 530845-14.

Part: STRAP — NOT REPORTED (FUSELAGE) · airframe 102,636 hrs · 14,723 cycles

STA 955 FAILSAFE STRAP REPAIRED IAW 5312-01170SECT 10 / 

Part: SKIN — CRACKED (WING) · airframe 102,547 hrs · 14,713 cycles

WING SKIN CRACKED. REPAIRED IAW ERA 530749-14.

Part: SKIN — CRACKED (FUSELAGE) · airframe 102,547 hrs · 14,713 cycles

SKIN CRACKED AT FWD BLOWER OUTLET FOR LAVATORY SYS. REPAIRED IAW ERA 531019-14, REV 1.

Part: SKIN — CRACKED (RT WING) · airframe 121,089 hrs · 17,054 cycles

WING RIGHT LOWER INSPAR SKIN RIB 31 STR L-9.5 CRACKS C/W ER/A 530845-14. (LP 1713342)

Part: SKIN — CRACKED (BS 1582) · airframe 101,834 hrs · 14,622 cycles

FOUND A CRACK ON SKIN BS 1582 GOING FWD .3750 INCHES LT SIDE BEHIND LAV BLOWER VENTS AT PRODUCTION BREAK REPAIRED IAW ERA 529163-14.

Part: SKIN — CRACKED (BS 1582) · airframe 101,834 hrs · 14,622 cycles

FOUND A CRACK ON SKIN BS 1582 GOING FWD .3750 LT SIDE BEHIND LAV BLOWER VENTS AT PRODUCTION BREAK. PERMANENT REPAIR IAW ERA 529163-14.

Part: TIRE — FAILED (MLG) · airframe 98,417 hrs · 14,206 cycles

LOUD BANG AND VIBRATION AT ROTATION C AND RT HYD FAIL GEAR DID NOT RETRACT NR 8 MAIN TIRE EXPLODED ON ROLLOUT, DAMAGING STRUCTURE AND SEVERING HYDRAULIC LINES.

Part: LINER — PUNCTURED (NR 1 NACELLE) · airframe 98,434 hrs · 14,208 cycles

TWO SMALL PUNCTURES ON NR 1 ENGINE INNER LINER AT 10 O`CLOCK POSITION, REPAIRED IAW SRM 54-00-01.

Part: BEAM — DAMAGED (RT WING SPOILER) · airframe 98,417 hrs · 14,206 cycles

RIGHT WING SPOILER BEAM SURROUND STRUCTURE DAMAGED AFTER NR 8 TIRE. REPLACED UPPER AND LOWER RT WING SPOILER BEAM SURROUND STRUCTURE.

Part: CYLINDER — SEPARATED (RT WING) · airframe 98,417 hrs · 14,206 cycles

RIGHT WING TRANSFER CYLINDER SEPARATED. INSTALLED TRANSFER CYLINDER.

Part: TIRE — FAILED (MLG) · airframe 98,407 hrs · 14,205 cycles

FLIGHT RETURNED TO DEPARTURE DUE TO A BLOWN TIRE ON TAKEOFF. AFTER ROTATION CREW HEARD LOUD BANG IN BACK OF THE ACFT FOLLOWED BY HEAVY VIBRATION. AT APPROX 1000 FEET, RECEIVED THE RT AND CENTER HYDRAULIC PRESSURE FAILURE INDICATION. COMPLETED QRH PROCEDURES AND DECLARED EMERGENCY. MULTIPLE AREAS OF DAMAGE TO THE ACFT. CURRENTLY.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 94,467 hrs · 13,677 cycles

EMERGENCY CEILING LIGHTS AT 31GF -41GF INOPERATIVE. R & R BATTERY CHARGER AND PACK M734 IAW AMM 33-50. OPS CHECKED NORMAL.

Part: TEE FITTING — DAMAGED (NR 1 PYLON) · airframe 93,519 hrs · 13,551 cycles

NR 1 PYLON UPPER LINK PITCH LOAD FITTING INBD TEE FITTING HAS SHORT EDGE MARGIN AND IS REPLACED IAW ERA 502733-14AD.

Part: SPLASH GUARD — CORRODED (FS 283 RBL 81) · airframe 93,519 hrs · 13,551 cycles

FS 283 RBL 81 CABIN LWR SILL SPLASH GUARD HAS DAMAGE TO THE VERTICAL LEG AND HAS BEEN REPAIRED IAW ERA 502729-14, REV ORG.

Part: FRAME — CORRODED (BS 1263 S19-20R) · airframe 93,519 hrs · 13,551 cycles

CABIN FRAME BS 1263, STRINGERS 19 TO 20R FOUND CORRODED. REPAIRED IAW ERA 502732-14 REV O.

Part: SKIN — CRACKED (RT WING) · airframe 93,519 hrs · 13,551 cycles

RIGHT WING AFT PITCH LOAD FITTING O/B FWD BOLT HOLE CRACKED. REPAIRED IAW ERA 502734-14._(ERA 502734-14)

Part: FLOORBEAM — CRACKED (BS 654) · airframe 93,519 hrs · 13,551 cycles

FWD CARGO BS 654+88 LBL 6 FLOORBEAM UPPER CHORD "J" SECTION UPPER FLANGE DAMAGED. REPAIRED IAW SRM 53-00-07, REPAIR 4, FIG 201, DETAIL V.

Part: FITTING — MISMANUFACTURED (RT WING) · airframe 93,519 hrs · 13,551 cycles

RT WING SIDE LINK FITTING FASTENER HOLES FOUND FOUND INTERFERING WITH RADIUS OF MILL STEP. SIDE LINK REWORKED IAW ERA 503735-16.

Part: FRAME — CRACKED (BS 903 S21R) · airframe 93,519 hrs · 13,551 cycles

BS 903 S21R FRAME INNER CHORD CRACKED. R & R IAW ERA 502725-14.

Part: FRAME — CRACKED (BS 883 S21L) · airframe 93,519 hrs · 13,551 cycles

BS 883, S21L FRAME INNER CHORD CRACKED. R & R IAW ERA 502724-14.

Part: FLOORBEAM — CORRODED (BS 1518) · airframe 93,519 hrs · 13,551 cycles

BS 1518, RBL 30-50 FLOORBEAM UPPER TEE CORRODED. REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201.

Part: BUSHING — LOOSE (NR 2 PYLON) · airframe 93,519 hrs · 13,551 cycles

NR 2 PYLON STRUT FWD UPPER SPAR FITTING BUSHING IS LOOSE AND IS REPAIRED IAW SRM 54-53-90, REPAIR 2.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 93,519 hrs · 13,551 cycles

RIGHT WING INBD MAIN FLAP OTBD L/E FAIRING IS DELAMINATED. REPAIRED IAW SRM 57-53-01, REPAIR 1, FIG 201 AND 51-70-05 FIG 5.

Part: BUSHING — WORN (NR 1 PYLON) · airframe 93,519 hrs · 13,551 cycles

NR 1 PYLON STRUT FWD UPPER SPAR FITTING BUSHING IS WORN AND REPLACED IAW SRM 54-53-90, REPAIR 2.

Part: BUSHING — MIGRATED (NR 1 PYLON) · airframe 93,519 hrs · 13,551 cycles

NR 1 STRUT LOWER SPAR FITTING BUSHING IS MIGRATED, REPAIRED IAW SRM 54-53-91, REPAIR 4.

Part: FLOORBEAM — CORRODED (FS 287 RBL 19) · airframe 93,519 hrs · 13,551 cycles

CABIN FLOORBEAM AT FS 287 RBL 19 IS CORRODED ON THE UPPER TEE. REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201.

Part: BUSHING — MIGRATED (NR 2 PYLON) · airframe 93,519 hrs · 13,551 cycles

NR 2 PYLON STRUT LOWER SPAR FITTING BUSHING IS MIGRATED, REPAIRED IAW SRM 54-53-90, REPAIR 4.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 93,519 hrs · 13,551 cycles

LEFT WING INBD MAIN FLAP OTBD L/E FAIRING IS DELAMINATED, REPAIRED IAW SRM 57-53-01, REPAIR 1, FIG 201 AND 51-70-05, FIG 5.

Part: SKIN — PUNCTURED (LT WING TE FLAP) · airframe 93,519 hrs · 13,551 cycles

LEFT WING INBD AFT FLAP UPPER SURFACE IS PUNCTURED AND REPAIRED IAW SRM 57-53-01 REPAIR 1, FIG 201 AND 51-70-10, REPAIR 4 FIG 201.

Part: FLOORBEAM — CORRODED (FS 346 RBL 45-47) · airframe 93,519 hrs · 13,551 cycles

CABIN FLOORBEAM FS 346 RBL 45-RBL 47 IS CORRODED AND REPAIRED IAW SRM 53-00-5 REPAIR 1, FIG 201.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,285 hrs · 13,382 cycles

SECTION OF EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE CHARGER BASE AT M7361P11/F2. OPS CHECKED GOOD.

Part: STRAP — CRACKED (FUSELAGE) · airframe 90,846 hrs · 13,191 cycles

FAIL SAFE STRAP FAILED U/T INSPECTION AT LT BS 955 REPAIR REQUIRED. BS 955 REAR SPAR BULKHEAD LT FAIL SAFE STRAP REPAIRED PER ERA 499093-14AD REV 0 09FEB2012 (ERA 499093-14AD).

Part: LIGHT — DAMAGED (CABIN) · airframe 89,376 hrs · 12,997 cycles

EMERGENCY LIGHT AT SEAT 4AB IS DAMAGED. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: CHILLER — MALFUNCTIONED (GALLEY) · airframe 86,906 hrs · 12,670 cycles

GALLEY AFT CHILLER C/B POPPED WITH AN ASSOCIATED ELECTRICAL SMELL. FORWARD TO NEF MAINTENANCE COULD NOT DUPLICATE FAULT. SYSTEM OPERATION IS GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 85,195 hrs · 12,452 cycles

EMERGENCY LIGHT MID GALLEY LEFT SIDE ON THE FLOOR INOPERATIVE. MAINTENANCE REPAIRED BROKE WIRE. SYSTEM OPERATION IS NORMAL. (2010-D1305) (DL76L103010).

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 84,241 hrs · 12,321 cycles

ON DRC CHECK, MX FOUND EMERGENCY LIGHTS AT 18FG INOPERATIVE. MX FOUND A BROKEN WIRE AT THE WALL CONNECTOR AND REPAIRED. SYS OPS ARE NORMAL.

Part: ENGINE — UNKNOWN (NR 2) · airframe 82,950 hrs · 12,157 cycles

REPLACED NR 2 ENGINE - DUE TO HISTORY OF OIL FILTER LIGHT. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 82,185 hrs · 12,059 cycles

DURING TAXI OUT GOT T/E FLAP DISAGREE EICAS INTERMITTENTLY WAS DISPLAYED. PERFORMED FSEU BITE NO FAULTS NOTED RAN FLAPS FROM UP TO 30 SEVERAL TIMES NO FAULTS NOTED. RAN FLAPS IN ATLN MODE NO FAULTS. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 81,868 hrs · 12,020 cycles

EMERGENCY EXIT PATH LIGHTS AT SEATS 31AB 32AB 33AB AND 38AB INOP FOUND BROKEN WIRE AT SPLICE FOR SEAT 33AB CONNECTOR. REPLACED CONNECTOR. LIGHT CHKS NML MCO AND PLAC REMOVED. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 81,837 hrs · 12,016 cycles

MX FOUND THE EMERGENCY ESCAPE PATH LIGHTING AT SEAT 38AB INOP. MX RELAMPED THE LIGHT AT 38AB, SECURED T32AB BUT HAD TO FORWARD 33AB TO MCO IAW MEL 33-51-03A BECAUSE TROUBLESHOOTING. THE LIGHTS THAT WERE REPAIRED OPERATED NORM WAS PERFORMED.

Part: IDG — FAILED (NR 2 ENGINE) · airframe 81,762 hrs · 12,007 cycles

RTB ON TAXI OUT RT ENG GEN OFF LIGHT ILLUMINATED 1 REST NO HELP. MX PLACED RT GEN ON MCO RELEASED IAW MEL 24-00-01 REPLACED R ENG IDG NEEDS OPS AND LEAK CHECK. 605370. OPS AND LEAK CHECK IAW AMM. IDG OK FOR SERVICE MCO AND PLACARD REMOVED.

Part: CONNECTOR — DIRTY (ACM) · airframe 80,623 hrs · 11,853 cycles

IRREG: PRIOR TO TAKEOFF RIGHT PACK OFF LIGHT ILLUM. RERACKED RT PACK CONTROLLER CLEANED ACM INLET SENSOR CONNECTOR RT PACK WORKS NORMAL. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED SYSTEM) · airframe 78,807 hrs · 11,629 cycles

ON TAXI OUT L HPSOV MESSAGE W/OVERHEAD BLEED LIGHT ON. PERFORMED QRH CYCLED BLEED MESSAGE AND LIGHT CAME BACK ON 2 TIMES. FWD TO MCO AND PLACARD IAW MEL 36-11-02 T/S IAW FIM REMOVED AND REPLACED LT HPC. PERFORMED BITE CK AND RAN ENG ALL CKD NML. REPLACED HPC IAW AMM. MCO/PLAC RMVD ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: MODULE — FAILED (NLG STEERING) · airframe 78,739 hrs · 11,621 cycles

ON TAXI OUT AIRCRAFT MADE UNCOMMANDED TURN. REPLACING STEERING BYPASS MODULE. REPLACED NOSE GEAR WHEEL STEERING METERING VALVE PER AMM OPS OK.

Part: SHUTOFF VALVE — MALFUNCTIONED (LT ENGINE) · airframe 78,639 hrs · 11,609 cycles

L ENG HPSOV ILLUMINATED DURING TAKEOFF ROLL FWD TP MCO PER MEL 36-11-02. HPSOV DEACTIVATED AND JUMPER INSTALLED PER MEL. REMOVED AND REPLACED LT ENG HPSOV PER AMM VALVE IS IN UNLOCKED POSITION ALSO T3 TERMINAL BROKEN AT VALVE 680596. RETERMINATED T3 WIRE IAW SWPM CONNECTED T1 T2 T3 TO HPSOV CONTINUED IN CLOSED LOCK POS.

Part: PITOT HEAD — UNSERVICEABLE (LT) · airframe 77,470 hrs · 11,459 cycles

UPON ENGINE START L AUX PITOT ILLUMINATED. REMOVED AND REPLACED LT AUX PITOT PROBE PER AMM. PERFORMED PITOT LEAK CHECK, OPS CHECK PER AMM, CHECKS NORMAL.

Part: PITOT HEAD — INOPERATIVE (LEFT AUX) · airframe 77,470 hrs · 11,459 cycles

LEFT AUX PITOT EICAS MESSAGE. REMOVED AND REPLACED LT AUX PITOT PROBE PER M/M. PERFORMED PITOT LEAK CHEAK A OPS CHECK PER AMM. CHECKS NORMAL.

Part: FUSE — LOOSE (CABIN) · airframe 77,147 hrs · 11,419 cycles

AFTER 6 HRS SMELLED BURNING ODOR IN THE AFT GALLEY. INSPECTED AFT GALLEY AREA, NO EVIDENCE OF BURNING OR SMOKE. INSPECTED ALL LIGHT FITTINGS AND FOUND INBOARD RIGHT AFT CEILING LIGHT INOP. RELAMPED, NO HELP. FOUND FUSE LOOSE AT M0065 CONNECTOR CAUSING INTERMITTENT OPN, DISCONNECTED M00655 AND FWD TO MCO AND PLAC PER MEL 33-21-01. ALSO INSPECTED BULK CARGO AREA, NO TROUBLE FOUND.

Part: FITTING — CLOGGED (GALLEY) · airframe 76,150 hrs · 11,300 cycles

A/C RTB DUE TO WATER COMING OUT OF AFT FLOOR DRAINS WHENEVER WATER IS POURED INTO AFT GALLEY DRAINS. ALSO HAD A PROBLEM WITH A WATER LEAK FROM A FWD GALLEY COFFEEMAKER. TURNED OFF WATER IN AFT GALLEY AND DEFERRED WATER PER MEL. PUT FWD COFFEEMAKER ON NEF. UNCLOGGED GALLEY DRAIN. FOUND CLOG IN Y-FITTING BY BULK CARGO AFT WALL. OK FOR SERVICE. MCO AND PLAC REMOVED.

Part: SKIN — CORRODED (FUSELAGE) · airframe 72,406 hrs · 10,834 cycles

CORROSION AND CRACKING OF SKIN AT FS 1219, S-37L. DAMAGE WAS CUT OUT AND REPAIR PARTS WERE INSTALLED.

Part: CONTROLLER — MALFUNCTIONED (ENGINE BLEED) · airframe 69,639 hrs · 10,503 cycles

AFTER ENG START L BLEED OFF MSG W/NO ENG A/I AVAILABLE. RETURNED TO GATE. SWAPPED L HPSOV/LPRV NO HELP. REPLACED PRV CONTROLLER. REACTIVATED L HPSOV. RAN ENGINE. BLEED SYSTEM OPERATES NORMALLY.

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 69,370 hrs · 10,470 cycles

DURING ACCOMPLISHMENT OF INSPECTIONS OF THE NR 2 PYLON MIDSPAR FITTINGS AND CLOSEOUT ANGLE PER OPN 5281AD (01-074944-12). THE CLOSEOUT ANGLE WAS FOUND CRACKED IN THE TYPICAL LOCATIONS AT THE FASTENERS COMMON TO THE MIDSPAR FITTINGS. THE MID SPAR FITTINGS WERE INSPECTIONS AND NO INDICAITONS WERE NOTED. THE CLOSEOUT ANGLE WAS REPLACED WITH A NEW PART PER INSTRUCTIONS CONTAINED IN ERA 461325-14AD.

Part: GCU — UNKNOWN (RIGHT) · airframe 68,328 hrs · 10,343 cycles

ON ENG START RT GEN CONT OFF LIGHT ILLUM FWD TO MCO AS PER MEL 24-00-01. PLACARD INSTALLED. PART NEEDED GCU MFG PN S281T001-40.

Part: SKIN — DENTED (BS 1373 S29R) · airframe 66,716 hrs · 10,151 cycles

DURING HMV A DENT WAS FOUND IN THE EXTERIOR SKIN IN THE AREA OF THE AFT CARGO DOOR CUTOUT. THE DENT IS LOCATED AT FS 1373 BETWEEN S-28R AND S-29R. THE DENT WAS INSPECTED AND PUT ON A REPETITIVE RE-INSPECTION PROGRAM PER ERA 457839-14.

Part: SLIDE — UNWANTED DEPLOY (CABIN) · airframe 66,578 hrs · 10,133 cycles

REFERENCE: NR1492, DURING SLIDE ARMING, RT OVERWING SLIDE SYSTEM INADVERTENTLY ACTUATED. REPLACED RT OVERWING SLIDE AND COMPONENTS IAW OPN 7838AD.

Part: FRAME — CRACKED (BS 500) · airframe 66,576 hrs · 10,132 cycles

A CRACK WAS FOUND ON THE INNER CHORD OF THE STA 500 LOWER FRAME SEGMENT IN THE FORWARD CARGO BAY AT APPROX LBL 60. THE DAMAGED AREA OF CHORD WAS REMOVED AND A REPAIR ANGLE WAS INSTALLED.

Part: BRAKE — SMOKE (MLG) · airframe 66,576 hrs · 10,132 cycles

NR 3 WHEEL BRAKE ASSY EXCESSIVE SMOKE DURING TAXI FOR FCF. TOWER STOPPED AIRCRAFT AND NOTIFIED FIRE CREW. AIRCRAFT RETUNED TO HANGER SAFE. WHEEL BRAKE PUCK FOUND LEAKING AND CARBON FIBER DISK ASSY DISINTEGRATED. WHEEL ASSY BRAKE REPLACED ON LOG ENTRY AND NR 1476/ HMV 2 AT ACTS.

Part: FRAME — CRACKED (BS 903) · airframe 66,575 hrs · 10,131 cycles

THE FUSELAGE FRAME, LOWER END HAS A CRACK, STA 903 LT SIDE. THE DAMAGED END OF THE FRAME WAS REMOVED AND A REPAIR ANGLE WAS INSTALLED.

Part: KEELBEAM — DAMAGED (BS 1192) · airframe 66,575 hrs · 10,131 cycles

NR1375 AND ERA 457835-14 KEELBEAM RT DAMAGED AT STA 1192+17 DUE TO SKIN REMOVAL ON NR 952. REPAIRED IAW PRODUCTION PERMIT B767-5326413PA, REF ERA 457835-14.

Part: STRINGER — GOUGED (BS 1219 S37R) · airframe 66,575 hrs · 10,131 cycles

FUELAGE EXTERIOR SURFACE FOUND GOUGED AT STRINGER 37R AT APPROX STA 1219. REPAIRED IAW SRM 53-00-01 FIG 201 REPAIR 1.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 65,104 hrs · 9,956 cycles

FOUND 1 LT AND 2 RT EXTERIOR EMERGENCY LIGHTS INOP. RELAMPED 1 LT EXTERIOR EMERGENCY LIGHT, 178821. RELAMPED 2 RT EXTERIOR EMERGENCY LIGHT. OPS CK GOOD.

Part: MONITOR — OVERHEATED (CABIN) · airframe 56,961 hrs · 8,861 cycles

DIVERTED TO YYT DUE TO REPORTED SMOKE FUMES IN THE CABIN. MTC FOUND AN OVERHEAD VIDEO MONITOR AT 18AB OVERHEATED. MTC FOUND ALL THREE COOLING HOLES OBSTRUCTED, TWO WERE BLOCKED BY SUPPORT BRACKETS AND THE REMAINING ONE BY DUST. ALSO FOUND AN AFT COFFEEMAKER ELEMENT LOOSE AND CONTACTING SOME OLD COFFEE GROUNDS.

Part: SKIN — LIGHTNING STRIKE (HORIZONTAL STAB) · airframe 54,554 hrs · 8,527 cycles

FOUND ON ARRIVAL LIGHTING STRIKE AND DAMAGE ON LT HORIZONTAL STAB, L1 DOOR AREA. REPAIRED SAME

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,366 hrs · 8,208 cycles

SEAT 6 F/G EMERGENCY ESCAPE PATH MARKING LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY AT 6F/G, OPS CHECKS GOOD.

Part: WINDOW — DAMAGED (COCKPIT) · airframe 49,123 hrs · 7,688 cycles

AT CRUISE AND NEAR MSP, CREW SMELLED AN ELECTRICAL ODOR. WENT TO STBY ON EQPT COOLING AND SHUTTING OFF GASPER AND RECIRC FANS. SMELL STARTED TO GO AWAY AND THEN CAME BACK FORA SPLIT SECOND AND THEN WENT AWAY AGAIN. SEEMED TO COME OUT FROM THE VENTS. MADE A PRECAUTIONARY LANDING INTO MSP. MTC IN PROGRESS REPLACING R1 WINDOW DUE TO TERMINAL BLOCK ATBOTTOM FOUND LOOSE AND ARCING. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: BALLAST — ODOR (CABIN) · airframe 49,120 hrs · 7,687 cycles

FLIGHT ATTENDANTS SMELLED AN ELECTRICAL ODOR NEAR ROW 21. CHECKED OVERHEAD FOR LIGHT BALLASTS. CHECKED MOVIE PROJECTOR CHECKED SEBS. UNABLE TO SMELL ELECTRICAL ODOR. OK FOR SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 48,001 hrs · 7,477 cycles

DURING ETOPS L/O CHECK, L1 AND OVERWING EXTERIOR EMERGENCY LIGHTS FOUND INOP. REPLACED POWER SUPPLY M736. OPS NOW OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,728 hrs · 7,436 cycles

ON ETOPS L/O CHECK, FOUND EXTERIOR EMERGENCY LIGHT BY 2L DOOR INOP. RELAMPED EXTERIOR LIGHT, OPERATION NOW NORMAL.

Part: ODOR — DETECTED (CABIN) · airframe 42,802 hrs · 6,581 cycles

ACRID SMELL IN BUSINESS CLASS, NO SMOKE OR BURNING WAS OBSERVED BY PASSENGERS OR CREW. OCCURRED 20 MINS AFTER T/O SMELL DECREASED AFTER 5 MINS AND GONE UPON LANDING. CHECKED SIDEWALL AND OVERHEAD LIGHTS AND SURROUNDING AREAS, CHECKED UNDER SEATS AND OPERATION OF SAME. CKD FOR POPPED C/B'S IN COCKPIT AND E/E AREA NONE POPPED RAN ENGS AND LOADED SYSTEMS. NO TROUBLE FOUND, A/C OK FOR SERVICE.

Part: ODOR — DETECTED (CABIN) · airframe 42,802 hrs · 6,581 cycles

ACFT DIVERTED TO BOS WITH FUMES IN CABIN. CHECKED COMPLETE CABIN, NO TROUBLES FOUND. CKD FOR POPPED C/BS IN COCKPIT AND E/E. NO DISCREPANCIES. RAN BOTH ENGINES AND LOADED SYSTEMS. NO TROUBLE FOUND.

Part: ODOR — DETECTED (COCKPIT) · airframe 42,704 hrs · 6,568 cycles

TWENTY MINUTES OUT OF ATL CREW BECAME AWARE OF SULFUR SMELL IN COCKPIT. MTC T/S FOUND NO DISCREPANCIES. A/C WAS RELEASED FOR FLIGHT.

Part: FAN — DEFECTIVE (CABIN) · airframe 41,280 hrs · 6,353 cycles

BURNING SMELL IN CABIN. AT DEPARTURE BURNING SMELL IN CABIN. 02 FAULT TRACED TO RT RECIRC FAN, CB PULLED, FWD TO MCO AND PLACARD PER MEL 21-25-01A.

Part: FAN — FAILED (E/E BAY) · airframe 40,044 hrs · 6,155 cycles

ACRID ODOR SMELLED, FAN NOISE HEARD. FORWARD EXHAUST EQ COOLING FAN CB POPPED AND FWD EQ EXH FAN EICAS MESSAGE. DISPATCHED PER MEL CB PULLED AND COLLARED.

Part: RHEOSTAT — FAILED (SWITCH PANEL) · airframe 38,454 hrs · 5,898 cycles

AFTER LANDING THERE WAS A BURNING ELECTRICAL SMELL IN COCKPIT COULD NOT TELL WHERE IT WAS COMING FROM. FOUND BURNING SMELL CAME FROM OUT OF F/O P7 PNL P7 SWITCH. SUSPECT INTERNAL ARCING IN RHEOSTAT WAS HOT. PULLED C/B P31 ON P11 PNL. FWD TO MCO AND PLACARD.

Part: BATTERY — FAILED (FLASHLIGHT) · airframe 38,254 hrs · 5,864 cycles

JUMP SEAT AFT CENTER RT FLASHLIGHT RED LIGHT NOT FLASHING. REPLACED BATTERY ASSY, CHECKS OK.

Part: BULB — INOPERATIVE (SLIDE LIGHT) · airframe 37,480 hrs · 5,727 cycles

L2 DOOR EMERGENCY SLIDE LIGHT INOP. RELAMPED, CHECKS GOOD.

Part: OVEN — SMOKE (GALLEY) · airframe 36,437 hrs · 5,536 cycles

AFT GALLEY TOP OVEN RT SIDE SMOKES IN FAN AREA WITH POWER ON, SMOKE DISSIPATES WITH POWER OFF. REPLACED OVEN.

Part: ENGINE — FAILED (NR 2)

AT APPROX 160-170 KTS DURING TAKEOFF, RT ENG OVERTEMPED WITH ASSOCIATED VIBRATIONS. RT ENG SUBSEQUENTLY SHUTDOWN PER CHECKLIST. LANDING WT APPROX 338K. TAKEOFF PWR WAS AT 35. FUEL DUMPING USED TO DECREASE LANDING WT. DUMPED APPROX 30K. MAINT IN PROGRESS, REPLACING ENGINE.

Part: SLIDE — INOPERATIVE (LT EMER EXIT)

LEFT WING SLIDE SQUIB FAILED TEST NR 1. REPLACED K1 RELAY.

Part: SLIDE — FAILED TEST (LT EMER EXIT)

ON ETOPS PDC LT OVERWING EXIT SLIDE SQUIB TEST INOP. CHECKED VOLTS AT PIN A OF SQUIB CONNECTOR, NO VOLTS. CHECKED BATTERY PACK WIRING AND CONNECTIONS ALL OK. RESET PLUGS AND RESET DISABLED SWITCHES AND ALL OPS NORMAL. TEST OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

LT OVERWING EMERG EXIT SPOILER AND SLIDE SQUIBS WON'T TEST. REPLACED PWR SUPPLY AND BATT PACK.

Part: BULB — FAILED (NLG LIGHT MODULE)

DURING APPROACH, NO GREEN NOSE GEAR DOWN INDICATION. GO-AROUND PERFORMED AND ALT GEAR EXTENSION PERFORMED AS PER POM PROCEDURE. LIGHT DID NOT TEST, BULBS WERE CHANGED WITH NO RESULT. REPLACED BULBS IN LIGHT MODULE. PERFORMED ALT GEAR EXT INSP PER MM 05-51-33-2, ALL CHECKS FOUND OK.

Part: BATTERY — DISCHARGED (CABIN)

ON L/O, FOUND LT AFT DOOR SLIDE AND LT AFT GROUND AREA SLIDE LIGHT INOP. REPLACED BATTERY.

Part: ENGINE — MALFUNCTIONED (NR 2)

NR 1 ENG PARAMETERS SHIFTED. REPLACED NR 1 ENGINE.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FOUND ON SERVICE CHECK, LEFT AFT EMERGENCY SLIDE LIGHT INOP. REPLACED PWR SUPPLY M738, EMERGENCY LIGHTS TEST OK PER MM.

Part: ENGINE — HIGH OIL CONSUMP (NR 2)

DUE TO HIGH OIL CONSUMPTION HISTORY, NR 2 ENGINE WAS REMOVED AND ROUTED TO SHOP.

Part: EEL BULB — FAILED (CABIN)

EMERGENCY FLOOR TRACK LIGHT TO SEAT 20F INOP. REPAIRED WIRING AND REPLACED BULB. OPS NOW NORMAL.

Part: EEL BULB — FAILED (CABIN)

AFT MOST FUSELAGE EMERGENCY LIGHT INOP ON LEFT SIDE. RELAMPED, OPS CHECK GOOD.

Part: CONTROLLER — MALFUNCTIONED (CABIN)

DURING CRUISE, COULD NOT CONTROL CABIN PRESSURE IN EITHER AUTO 1 OR AUTO 2, DIVERTED BOS. RAN BITE CHECK AS PER FIM, NUMBER 2 AC POWER FAULT, RESET, ALL CHECK NORMAL. REPLACED NUMBER 2 CONTROLLER AND ALT SELECT ON MODE CONTROL PANEL, UNRELIABLE TEST. REPLACED MODE SELECT PANEL, RAN BITE CHECK AS PER FIM, ALL OPERATION NORMAL AND RETURNED TO SERVICE.

Part: CDU — FAILED (RT FLT DECK)

DURING CRUISE, RIGHT FMC CDU WENT BLANK. DIVERTED TO JFK. REPLACED RT CDU, OPERATION NORMAL.