N1607B

Part: SLIDE — DEPARTED (OVERWING) · airframe 86,583 hrs · 11,143 cycles

AFTER GEAR EXTENSION INTO BOS, FLIGHT ATTENDANTS HEAR AND ABNORMAL LOUD THUD. UPON AIRCRAFT INSPECTION FOUND SLIDE/RAFT RIGHT OVER WING MISSING. REPLACED SLIDE, DOOR ACTUATOR, EVACUATION CYLINDER, SLIDE DOOR ACTUATORS, SLIDE INFLATION BOTTLE AND ADJUSTED OVER WING SLIDE SYSTEM. LP 6346164

Part: COMPRESSOR — FAILED (WATER SYSTEM) · airframe 86,434 hrs · 11,123 cycles

ELECTRICAL ODOR ROW 39. AFTER INVESTIGATION FOUND WATER COMPRESSOR FAIL. HOT SMOKE COMING OUT. WATER SYSTEM AIR COMPRESSOR DEACTIVATED PULLED AND COLLARED CB H6 PANEL P33. DISCONNECTED PLUG FROM WATER COMPRESSOR. REPLACED POTABLE WATER COMPRESSOR AND CHECK VALVE. SYSTEM OPERATION NORMAL.

Part: SKIN PANEL — CRACKED (LT WING) · airframe 81,520 hrs · 10,623 cycles

LT WING FIXED LEADING EDGE SKIN PANEL LOWER EDGE BETWEEN ISS 285.23 AND ISS 345.50 FOUND 01EA HOLE CRACK REPAIRED PER SRM 51-70-08. (LP 0787937)

Part: SKIN — DELAMINATED (LE SLAT) · airframe 81,486 hrs · 10,618 cycles

NR 10 SLAT EXTERNAL SURFACE O/B UP CORNER FOUND DELAMINATION REPAIRED PER SRM 57-43-02.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 81,486 hrs · 10,618 cycles

NR 5 SLAT O/B UPPER CORNER OUTER SURFACE 2" FROM T/E 5" FROM O/B EDGE SUSPECT DELAMINATION. REPAIRED PER SRM 57-43-02.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 81,486 hrs · 10,618 cycles

LT WING NR 1 SLAT UPPER SURFACE 2 IN FROM T/E 24 IN FROM I/B EDGE DELAMINATION REPAIRED PER SRM 57-43-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,486 hrs · 10,618 cycles

CORRROSION LEVEL 2: BULK CARGO COMPARTMENT SHEAR TIE FOUND CORROSION AT BS1562 S-39L SND S-39R. REPAIRED PER ER/A 571857-14. (LP 077849)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,486 hrs · 10,618 cycles

CORROSION LEVEL: 2 SEAT TRACK-CABIN SEAT TRACKS FOUND SURFACE CORROSION AT RBL 11 BETWEEN STA 929 TO STA998 FOUND ALL OUT OF LIMIT. REPLACED CORRODED SEAT. (LP 0776266)

Part: FAILSAFE — CORRODED (BS 1562) · corrosion level 2 · airframe 81,651 hrs · 10,635 cycles

CORROSION WAS NOTED ON THE FAIL SAFE IN THE BULK CARGO, BS 1562, STRINGERS 37L - 37R. REPAIRED IAW ER/A 571857-14AD.

Part: FLOOR SUPPORT — CORRODED (BS 966-977) · corrosion level 2 · airframe 81,486 hrs · 10,618 cycles

CORROSION LEVEL: 2 CABIN FLOOR BEAM UPPER CHORD FOUND SURFACE CORROSION AT LBL11 BETWEEN STA933 TO STA977 & #65292 REPAIRED PER SRM 53-00-41. (LP 0758013)

Part: SKIN — CRACKED (BS 1662) · airframe 81,486 hrs · 10,618 cycles

HFEC INSPECTION FOUND 01EA CRACK AT STA1662 S-13AR APPROX 1/4 INCH MARKED THE CRACKED AREA OF SKIN AS MARKED AT STA1662 S13AR CUT SRM53-80-01 THE REPAIR PARTS MADE FROM 7075T6-0.056" CLAD & 7075-T6-0.063" CLAD AND DRILLED FASTENER HOLES AND INSTALLED PER SRM 53-80-01. (LP 0756793)

Part: SKIN — CRACKED (BS 1660) · airframe 81,486 hrs · 10,618 cycles

HFEC INSPECTION FOUND 01EA CRACK AT STA1660 S-13AL APPROX 3.3 INCH MARKED THE REPAIR PARTS MADE FROM 7075T6-0.056" CLAD & 7075-T6-0.063" CLAD AND DRILLED FASTENER HOLES AND THE REPAIRED PARTS INASTALLED AS PER SRM 53-80-01. (LP 0756775)

Part: FAILSAFE — CRACKED (BS 955) · airframe 81,486 hrs · 10,618 cycles

UT INSPECTION ON RH 955 FAIL-SAFE STRAP FOUND CRACK INDICATION SEE W/C 5312-01170-10B. (LP 0755314)

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 81,486 hrs · 10,618 cycles

CORROSION LEVEL: 2 SEAT TRACK-CABIN SEAT TRACK FOUND SURFACE CORROSION AT RBL88.5 BETWEEN STA1098 AND STA1197+33 FOUND ALL OUT OF LIMIT PER B767-300 SRM53-00-52 ALLOWABLE DAMAGE (LP 0754088)

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 81,486 hrs · 10,618 cycles

CORROSION LEVEL: 2 SEAT TRACK- CABIN SEAT TRACK FOUND SURFACE CORROSION AT RBL11 BETWEEN STA1197+33 AND STA1230 THE ALLOWABLE DAMAGE IS ALL OUT OF LIMITS THE REPAIR PARTS AND NEW SPLICE INSTALLED (LP 0754071)

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 81,486 hrs · 10,618 cycles

CORROSION LEVEL: 2 SEAT TRACK- CABIN SEAT TRACK FOUND SURFACE CORROSION AT LBL88.5 BETWEEN STA1362 TO STA1428 THE ALLOWABLE DAMAGE IS 0.030? AND FOUND ALL OUT OF LIMITS. THE CORRODED SEAT TRACK WAS REPLACED. (LP 0753849)

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 81,486 hrs · 10,618 cycles

CORROSION LEVEL: 2 SEAT TRACK-CABIN SEAT TRACK FOUND SURFACE CORROSION AT LBL88.5 BETWEEN STA966 AND STA1098 FOUND ALLOWABLE DAMAGE OUT OF LIMITS THE REPAIR PARTS AND NEW SPLICE INSTALLED. (LP 0754073)

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 81,486 hrs · 10,618 cycles

CORROSION LEVEL: 2 SEAT TRACK- CABIN SEAT TRACK FOUND SURFACE CORROSION AT LBL88.5 BETWEEN STA1197+33 AND STA1230 THE ALLOWABLE DAMAGE FOUND OUT OF LIMITS. THE REPAIR AND NEW SLICE WAS INSTALLED. (LP 0754078)

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 81,486 hrs · 10,618 cycles

CORROSION LEVEL: 2 SEAT TRACK- CABIN SEAT TRACK FOUND SURFACE CORROSION AT RBL88.5 BETWEEN STA1208 AND STA1428 FOUND ALL OUT OF ALLOWABLE LIMITS AND REPLACED. (LP 0753847)

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 81,486 hrs · 10,618 cycles

CORROSION LEVEL: 2SEAT TRACK-CABIN SEAT TRACK FOUND SURFACE CORROSION AT RBL88.5 BETWEEN STA966 AND STA1098 FOUND ALL OUT OF LIMIT PER B767-300 SRM53-00-52. REPAIRED PARTS AND NEW SPLICE INSTALLED (LP0754083)

Part: B-NUT — LOOSE (CREW OXYGEN) · airframe 78,601 hrs · 10,321 cycles

DIVERTED DUE TO OXYGEN PRESSURE AT ZERO DURING NORMAL INSTRUMENT SCAN DURING CRUISE. CREW OXYGEN BOTTLE REPLACED AND A LEAK CHECK PERFORMED. FOUND A LOOSE B-NUT BEHIND SECOND OBSERVER`S SEAT.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 78,131 hrs · 10,274 cycles

FOUND SEAT 19AB EMERGENCY FLOOR PATH LIGHT WON'T TURN ON UPON SERVICE CHECK. FOUND BROKEN CONNECTOR AND REPLACED EMERGENCY PATH LIGHT PLUG AND CONNECTOR. SYSTEM OPERATION IS NORMAL.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 78,131 hrs · 10,274 cycles

EMERGENCY LIGHTS AT SEAT 1,2,3 RIGHT SIDE ARE INOPERATIVE. FOUND BATTERY PACK F1 FUSE OPEN AND REPLACED FUSE. SYSTEM OPERATION IS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,884 hrs · 10,131 cycles

ON SERVICE CHECK, FOUND THE EMERGENCY LIGHTS INOPERATIVE AT ROWS 24G -34G. REPLACED BATTERY PACK AND CHARGER. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,559 hrs · 10,091 cycles

EMERGENCY LIGHTS AT SEAT 18 RIGHT ROW FROM AFT SIDE INOPERATIVE. REPLACED BATTERY OF M732 POWER SUPPLY. SYSTEM OPERATION IS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,387 hrs · 10,066 cycles

EMERGENCY LIGHTS ARE INOPERATIVE AT 24FG-32FG. REPLACED BATTERY PACK CHARGER AT 24FG. SYSTEM OPERATION IS NORMAL.

Part: FIRE WARNING — FALSE ACTIVATION (CREW REST) · airframe 74,634 hrs · 9,848 cycles

AT 38000 FT ABOUT 3 HOURS INTO FLIGHT, RECEIVED A FIRE WARING BELL AND AFT CREW SMOKE DETECTOR LIGHT. F/A RESET THE SMOKE ALARM ON PANEL, NO HEAT OR SMOKE OBSERVED IN CREW REST COMPARTMENT. PERFORMED A SMOKE DECTECTOR TEST IAW AMM 26-14-04, TESTS OK CHECKED SECURITY OF PLASTIC SHIELDS ON CABIN TEST UNITS FOUND OK. A/C OK FOR SERVICE.

Part: FLAP — DAMAGED (RT WING) · airframe 74,511 hrs · 9,831 cycles

RIGHT O/B FLAP TRAILING EDGE DAMAGED I/B SIDE REPAIRED PER SRM 57-53-01.

Part: LAMP — INOPERATIVE (SLIDE INDICATOR) · airframe 73,680 hrs · 9,727 cycles

SLIDE INDICATOR LIGHT IS INOPERATIVE. REPLACED THE LAMP, SYSTEM OPERATION IS NORMAL.

Part: STRUCTURE — DAMAGED (RT WING TE FLAP) · airframe 62,170 hrs · 8,333 cycles

RT WING OTBD T/E FLAP L/E HAS BIRD STRIKE DAMAGE. REMOVED DAMAGE AND INSTALLED PERMANENT REPAIR IAW SRM 57-53-01.

Part: RELAY — FAILED (ESCAPE SLIDE) · airframe 57,063 hrs · 7,762 cycles

LEFT AND RT SLIDE AND LT AND RT SPOILER SQUIBS DONT TEST. R & R K838 AND K839 RELAY IN THE P-19 PANEL CHECKED GOOD AMM 25-65.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,372 hrs · 7,685 cycles

RT OVERWING SQUIB WILL NOT TEST. R & R RT OVERWING BATTERY PACK IAW AMM 25-65. LIGHT TESTED NORMAL,

Part: DOOR FRAME — DAMAGED (CARGO DOOR) · airframe 74,706 hrs · 9,858 cycles

FOUND SCRATCH ON LOWER FWD CORNER OF BULK CARGO DOOR FRAME AREA. BLENDED AND TREATED DAMAGE ON BULK CARGO FWD CORNER IAW SRM 53-00-01.

Part: BATTERY — INOPERATIVE (RT ESCAPE SLIDE) · airframe 55,738 hrs · 7,622 cycles

RT ESCAPE SLIDE SQUIB NOT TESTING. R & R RT ESCAPE SLIDE SQUIB BATTERY IAW AMM 52-21. OPS TEST OK.

Part: BOLT — WRONG PART (ENG LOAD FITTING) · airframe 55,349 hrs · 7,577 cycles

NR 1 ENGINE AFT PITCH LOAD FITTING FASTENER REMOVED FOUND TO BE DIFFERENT GRIP LENTH FROM THOSE STATED IN EA 01-451812-03, AD OPN 2801 TO VERIFY. EARN NR N1607B-0056 RAISED AND NR 1 ENGINE AFT PITCH LOAD FITTING INSTALLED IAW ERA 507119-14 AD, REV 0 SDR RAISED AND ATCL LOG PG 2050 RAISED IAW FINAL ERA 507119-14 AD REV ORIGINAL COMPLIED WITH.

Part: BOLT — WRONG PART (2 ENG LOAD FIT) · airframe 55,349 hrs · 7,577 cycles

NR 2 ENGINE AFT PITCH LOAD FITTING FASTENER REMOVED. FOUND TO BE DIFFERENT GRIP LENGTH FRON THOSE STATED IN EA 01-451812-03AD, OPN 2801 TO VERIFY. EARN NR 1607B-0057 RAISED AND NR 2 ENG AFT PITCH LOAD FITTING INSTALLED IAW ERA 507119-14AD PRI REV 0 SDR RAISED AND ACTL LOG PAGE 2050 RAISED IAW FINAL ERA 507119-14AD REV ORIGINAL COMPLIED WITH ON NON ROUTINE 0669.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,231 hrs · 7,562 cycles

RIGHT AISLE EMERGENCY PATH LIGHTING INOPERATIVE IN MID CABIN. R & R EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51. OPS CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,040 hrs · 7,540 cycles

LT AND RT EMERGENCY OVERWING SQUIB LIGHTS INOPERATOVE. REPLACED BATTERY PACK IAW AMM 25-65. TESTED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,648 hrs · 7,490 cycles

DUE TO DELAY TAKEN FOR L AND R EMERGENCY ESCAPE SQUIB TEST 1 AND2 FAILING PLS RT AFT BATTERY PACK. REPLACED BATTERY PACK PER AMM 25-65 593110.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,642 hrs · 7,489 cycles

DURING ETOPS PDC SQUIP TEST FOR LT AND RT EMERGENCY ESCAPE LIGHT FAILED FOR BOTH TEST 1 AND TEST 2. FIM PROCEDURE B767 25-65-00 APPLIED. SQUIP TEST FOR EMERGENCY ESCAPE LIGHT NOW OK. BATTERY PACKS FOR LT AND RT SYS RECONNECTED EMERGENCY BATTERY FOR WING. REPLACED RT AFT BATTERY CHARGER SQUIP TEST OK.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 54,569 hrs · 7,480 cycles

DURING DRC, FOUND RIGHT EMERGENCY ESCAPE SQUIB TEST 1 WILL NOT TEST. TROUBLESHOT PER FIM 25-65. FOUND FAULTY BATTERY PACK. DISARMED OFFWING ESCAPE SYS IAW B767-300 AMM 25-65. REPLACED BATTERY CHARGER IAW AMM 25-65. REARMED OFF-WING ESCAPE SYSIAW AMM 25-65. OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (ESCAPE SYSTEM) · airframe 53,843 hrs · 7,385 cycles

POST SLIDE CHANGE FOUND LT AND RT OFF WING ESCAPE SYSTEM POWER SUPPLY BATTERIES DEAD. REMOVED AND REPLACED LT AND RT OFF WING ESCAPE SYSTEM POWER SUPPLIES PER AMM 25-65-17.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,667 hrs · 7,362 cycles

DURING PDC, FOUND EMERGENCY PATH LIGHTS 24GF-32GF INOPERATIVE. REMOVED AND REPLACED FUSE AT BATTERY CHARGER M732. INSTALLED BATTERY AND ALLOWED TO CHARGE. OPS CHECKED NORMAL. OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,243 hrs · 7,306 cycles

EMERGENCY PATH LIGHTS FROM 24-32 RIGHT SIDE ARE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 52,555 hrs · 7,217 cycles

DURING PDC SQUIB TEST BOTH EMER ESCAPE LT AND RT NOT ILLUMINATED WHEN TEST 1 S/W PRESSED. BOTH LT AND RT SPOILER NOT ILLUM WHEN TEST SW PRESSED. MAINTENANCE REPLACED BOTH LT AND RT OFF WING ESCAPE SYSTEM BATTERY PACK PER AMM. OPS TEST OK. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: UNKNOWN — ODOR (CABIN) · airframe 51,622 hrs · 7,115 cycles

EN ROUTE ELECTRICAL SMELL IN AFT GALLEY BY C/B PANEL LEFT OF OVENS. RAN BOTH PACKS AND BOTH GALLEY VENTS FANS NO ELECTRICAL SMELL. PULLED OUT BOTH AFT GALLEY CIRCUIT BREAKER PANELS. NO SMELL OR SIGNS OF ELECTRICAL BURNS. RAN ALL OVENS AND COFFEEMAKERS. WENT DOWN TO CREW REST AND INSPECTED CONNECTIONS AND VENT LINES. NO DEFECTS FOUND. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK

Part: FLAP — DENTED (LT WING) · airframe 51,387 hrs · 7,084 cycles

LT WING I/B MAIN FLAP LWR MID AREA IS DENTED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 FIG 201 AND SRM 51-70-10 REPAIR 4 FIG 201.

Part: WEDGE — BULGED (LE SLAT) · airframe 51,387 hrs · 7,084 cycles

LT WING NR 2 SLAT T/E WEDGE UPPER SURFACE HAS A BULGE AND IS REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 FIG 201 AND SRM 51-70-10 REPAIR 4 FIG 201.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 51,387 hrs · 7,084 cycles

LT WING I/B MAIN FLAP LEADING EDGE O/B FAIRING IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 AND 51-70-05 PAR 5A(1) FIG 5.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 50,657 hrs · 6,992 cycles

MAINTENANCE FOUND EMERGENCY LIGHTS AT SEATS 24AB THROUGH 32AB INOPERATIVE. THE CHARGER WAS REPLACED. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 50,388 hrs · 6,952 cycles

EMERGENCY ESCAPE PATH LIGHTS AT SEAT 26AB ARE INOPERATIVE. MAINTENANCE FOUND THE CONNECTOR UNDER THE SEAT DISCONNECTED AND RECONNECTED IT. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,219 hrs · 6,927 cycles

DURING DRC MAINTENANCE FOUND EMERGENCY LIGHT AT 24AB TO BE DIM AND REPLACED THE BATTERY PACK. SYSTEM OPERATION IS NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 49,758 hrs · 6,869 cycles

DURING DAILY RELIABILITY CHECK, MAINTENANCE FOUND SEATS 24ABAND 32AB EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY CHARGER M11559 AT SEAT 34FG PER AMM. OPERATIONAL CHECK WAS NORMAL.

Part: BATTERY — DISCHARGED (ESCAPE SQUIB) · airframe 49,138 hrs · 6,795 cycles

EMERGENCY ESCAPE SQUIB FOR LEFT AND RIGHT WILL NOT TEST. MAINTENANCE FOUND BATTERY M961 LOW AND REPLACED THE BATTERY AND CHARGER. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — DISCONNECTED (LE SLAT) · airframe 46,041 hrs · 6,406 cycles

ON CLIMBOUT SLAT HANDLE IN FULL UP POSITION WITH 1 DISPLAYED ON INDICATOR. SLAT WOULD NOT RETRACT. L/E DISAGREE NOTED. QRH PROC ACCOMPLISHED. C/B 6F24 FOUND OUT. BIT PSEU/FSEU NO FAULTS. RESET C/B RAN FLAPS. FLAPS OK NO FAULTS OR MESSAGES. LUBRICATED OUTBOARD L/E SLATS AND CHECKS OK. FOUND INBOARD L/E FLAPS INOP IN ALT MODE. FOUND CONNECTOR OFF ELEC MOTOR. REINSTALLED CONNECTOR OPS CHECK GOOD (DL76G102017).

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,124 hrs · 6,309 cycles

SEAT MOUNTED EMERGENCY LIGHTS INOP LT AISLE 24-32. REPLACED THE PWR SUPPLY AT FIN NR M11559 AND REPLACED EMERGENCY SEAT HARNESS AT 31A-B.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,336 hrs · 6,226 cycles

EMERGENCY LIGHT ABOVE COCKPIT DOOR INOP. REPLACED BATTERYS. OP CKS GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 44,336 hrs · 6,226 cycles

SEAT 34F EMERGENCY EXIT LIGHT INOP. SPLICED BROKEN WIRE. LIGHT OP CKS GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,534 hrs · 6,147 cycles

FOUND ON LO CHECK SEATS 33 THRU 41 EMERGENCY LIGHTS INOP. R & R CHARGER AND BATTERY FOR EMERGENCY LIGHTS OPS CHECKS GOOD IAW MM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,097 hrs · 6,105 cycles

SEATS 33FG TO 41FG EMERGENCY PATH LIGHTS ARE INOP. REMOVED AND REPLACED E-PATH BATTERY CHARGER ASSY FOR SEATS 33-41 LOCATION STA 1384 IAW AMM. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: WIRE — BROKEN (CABIN) · airframe 42,752 hrs · 6,071 cycles

GALLEY 409 - MID RIGHT EMERGENCY LIGHT INOP. FOUND EMERGENCY LIGHT WIRE BROKEN. REPAIRED EMERGENCY LIGHT WIRE PER AMM AND PSM. OPS CHECK GOOD. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: IDG — FAILED (LT ENGINE) · airframe 42,269 hrs · 6,021 cycles

LEFT ENGINE GEN WOULD NOT COME ONLINE. BIT BPCU FOUND IDG/OIL IN OUT BULB WIRING. HIGH RISE. REPLACED GEN DIODE. GEN TRIP. T/S PER FIMM. REMOVED AND REPLACED GCU, NO HELP. REMOVED AND REPLACED LEFT ENG IDG PER MM. ALL NORMAL.

Part: PUMP — UNKNOWN (HYD SYSTEM) · airframe 34,603 hrs · 5,159 cycles

C HYD PUMP NR 1, RETURNED TO GATE, C1 ELECT HYD PUMP OPS OK AT GATE WITH ENGINES RUNNING SUSPECT ELECT LOAD SHED PROBLEM ALL OPS OK NOW.

Part: ISOLATION VALVE — OPEN (BLEED AIR SYS) · airframe 34,163 hrs · 5,110 cycles

AIRCRAFT 1607 ON FLT 130/22 RTB DUE TO THE RT ISOLATION VALVE STUCK OPEN. REPLACED VALVE CKS OK.

Part: LINE — CLOGGED (LWR DRAIN) · airframe 32,943 hrs · 4,965 cycles

DRAIN AT L1 DOOR BLOCKED UP WASTE WATER FOUND ON DRIP PAN OVER EICAS COMPUTERS. ON INSPECTION, FOUND EXCESSIVE WASTE WATER ABOVE EICAS COMPUTER DRIP TRAY. TRACED BLOCKAGE TO DRAIN LINE ADJACENT TO FWD DRAIN MAST. REMOVED DEBRIS INCLUDING BOTTLE TOPS ETC. FLUSHED LINE, RETURNED A/C TO NML. OK FOR SVC.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 32,420 hrs · 4,900 cycles

CABIN ALT AUTO 1 AND AUTO 2 INOP. FOUND CONTROLLER FAULT. NO RESET. REPLACED NR 2 CABIN PRESS CONTROLLER. BITE CHECK GOOD.

Part: ADC — MALFUNCTIONED · airframe 31,860 hrs · 4,828 cycles

DURING TAKEOFF ROLL F/O AIRSPEED INDICATOR FROZEN AT ZERO WITH NO WARNING FLAGS OR EICAS LIGHTS. ONCE AIRBORNE A/S INDICATOR BEGAN TO MOVE AND PEGGED HIGH AT 400KTS. WITH ASSOCIATED IAS DISAGREE. RUDDER RATIO-AIL LOCKOUT AND L/R EEC MODE EICAS ILLUM. F/O SELECTED ALT AIR DATA AND A/S AND ALTIMETER RETURNED TO NORMAL. EICAS WARNS THE SAME EXCEPT FOR TAS DISAGREE OUT. REMOVED AND REPLACED RT ADC. PERFORMED TEST 30 CHKS OK. PERFORMED ADC TEST CHKS NORMAL. OK FOR SERVICE.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 30,932 hrs · 4,712 cycles

EMERGENCY LIGHTS INOP ROWS 27-32 RT SIDE. FOUND D23346 DISCONNECTED. SECURED SAME, CKS GOOD.

Part: FITTING — CRACKED (LT WING TE FLAP) · airframe 30,861 hrs · 4,703 cycles

LT IB FLAP AFT FLAP I/B FITTING CRACKED AT ATTACHING FASTENERS. REPAIRED PER SRM 57-53-02 FIG 201.

Part: INLET — DENTED (NR 2 ENGINE) · airframe 30,861 hrs · 4,703 cycles

NR 2 ENGINE INLET ACCOUSTIC LINER DENTED AT 6 O:CLOCK POSITION. REPAIRED PER SRM ROHR 54-12-01 REPAIR NR 3.

Part: RIB — GOUGED (NR 1 NACELLE) · airframe 30,861 hrs · 4,703 cycles

NR 1 ENGINE I/B CORE COWL AFT RIB IS GOUGED. REPAIRED PER ERA 458864-14 AND SRM 54-45-01 REPAIR 4.

Part: FRAME — CRACKED (NR 2 NACELLE) · airframe 30,861 hrs · 4,703 cycles

NR 2 ENGINE I/B CORE COWL AFT HAT FRAME IS CRACKED. FAB`D REPAIR DOUBLER PER ERA 458865-14. INSTALLED REPAIR PER SRM 51-40-02 PAGE 2 AND 3 SRM 54-45-01 REPAIR 4 PARA 4G AND 4H.

Part: ENGINE — VIBRATION (NR 2) · airframe 29,122 hrs · 4,496 cycles

REPLACED NR 2 ENGINE DUE TO HIGH N2 VIBS.

Part: BLEED VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 27,947 hrs · 4,359 cycles

RTB, AFTER ENG START RT ENG BLEED VALVE WOULD NOT OPEN OFF LIGHT ILLUMINATED. FWD TO MCO, A/C DISPATCHED ACC MEL 36-11-08C, ALL MAINT PROCEDURES C/OUT ACC MEL 36-11-08C.

Part: WARNING LIGHT — ILLUMINATED · airframe 27,813 hrs · 4,343 cycles

STBY BUSS OFF LT ILLUMINATED IN FLT. FLT DIVERTED TO MXP. T/S PER FIM 24-33-00 AND WDM 24-33-11, NO FAULTS. ON ARRIVAL AT A/C NO STATUS. MTC MSG-REF FIM 24-33-00 AND WDM 24-33-11. NO FAULTS IND. PERF STBY GEN LONG TEST REF 24-33-00-206-001. ALL PARAMETERS WITHIN REF LIMITS, CONFIRMED PARAMETERS WITH REPEAT CHKS-CURRENT VALUES AC-V 117 FREQ 39 DC-V 28 CHARGE CYCLE NML OK FOR SVC.

Part: PRESSURE SWITCH — DAMAGED (NR 2 ENGINE OIL) · airframe 27,670 hrs · 4,324 cycles

FLT REPORTED RT ENG SHUTDOWN DUE OIL QTY AT ZERO AND OIL PRESSURE RED FLT DIV TO BRU. NORMAL LANDING WITH NO PROBLEMS REPORTED. BRU MTC FOUND OIL TANK EMPTY AND ON INSPECTION FOUND THE OIL LINE TO THE LOW OIL PRESS SWITCH BROKEN. RE CF6-80C2 IPC 72-00-05-12 ITEM 275 P/N 1978M64G01. REPLACED LINE AND CLAMPS. LEAK CHECK PERFORMED. ALSO FOUND P CLAMP DAMAGED. REPLACED P CLAMP BY NEW. REMOVED MAIN FILTER FOUND CLEAN. REPLACED IT. PULLED ALL CHIP DETECTORS. FOUND SATISFACTORY.

Part: FIRE LOOP — FAILED (FIRE WARNING) · airframe 27,134 hrs · 4,254 cycles

RIGHT ENG FIRE LP1 AND LP2 STATUS MESSAGES ON EICAS. REPLACED LOWER AFT LP1 AND LP2 ASSY AND PRESS TO TEST SWITCH.

Part: WIRE — DAMAGED (FIRE WARNING) · airframe 27,120 hrs · 4,251 cycles

RIGHT ENG FIRE LOOP 1 FAULTED DURING CLIMBOUT FROM JFK, 1 PREV ITEM FOR EACH LOOP IN THE LAST 30 DAYS. APPROX 2 HRS LATER INTO FLIGHT AND IN THE TRACK, THE SECOND LOOP FAILED CAUSING FIRE/OVERHEAT SYS FAIL MESSAGE AND CAUTION LIGHT AND MESSAGE. DIVERTED TO ST JOHNS. REPAIRED WIRING TO LOOP TS683.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 21,580 hrs · 3,497 cycles

DURING SVC FOUND SEATS 1AB TO 3AB AND L1 CLOSET E-PATH LIGHTS INOP. REPLACED FUSE ON M730 AND REPLACED M736 AND BATTERY PACK OPS OK.

Part: OVEN — ODOR (FWD GALLEY) · airframe 21,119 hrs · 3,433 cycles

STRANGE ELECTRICAL SMELL FROM FWD GALLEY. ALSO STRANGE VIBRATION NOISE LIKE A LOOSE FAN POSSIBLY. DEPOWERED FWD GALLEY, NOISE AND SMELL STOPPED. FOUND NR 1 OVEN IN FWD GALLEY C/B POPPED. REPLACED SAME.

Part: CONTROLLER — MALFUNCTIONED (NR 1 ENGINE) · airframe 20,181 hrs · 3,296 cycles

LEFT ENG BLEED LIGHT, LT ENG COWL OPEN 605396. REACTIVATED LEFT ENG HPSOV AND REMOVED AND REPLACED LT ENG HP CONTROLLER AS PER AMM. REPLACED RELAY K650 IN PANEL P36. FOUND LOOSE LINE AT PRV VALVE TIGHTENED SAME. COWL CLOSED AND SECURED. BLEED OPS NORMAL ON HIGH PWR RUN UP.

Part: IDG — UNSERVICEABLE (NR 2 ENGINE) · airframe 19,985 hrs · 3,266 cycles

CREW REPORTS RIGHT IDG DRIVE LIGHT. LEFT HP VLV ALREADY ON MCO, DIVERTING TO JFK AS PRECAUTION. REPLACED RIGHT IDG, LEAK CHECKS AND OPS CHECKS GOOD.

Part: IDG — FAILED (#2 ENGINE) · airframe 19,985 hrs · 3,266 cycles

RIGHT GENERATOR DRIVE LIGHT ON, DISCONNECTED RIGHT GENERATOR. DIVERTED TO JFK. SWAPPED EQUIPMENT TO A/C 1521. REPLACED NR 2 IDG ON A/C 1607.

Part: COUPLING — LEAKING (NR 2 IDG) · airframe 18,496 hrs · 3,049 cycles

RIGHT GENERATOR DRIVE ILLUMINATED. COMPLIED WITH QRH. BPCU BITE OK, SERVICE IDG, IDG OVERFLOW PORT LEAKING. REPLACED OVERFLOW COUPLING FILTER AND CHECKED CHIP DET DRAINED AND RESERVICED IDG. RAN ENG FOR 20 MIN, OPS CHECK/LEAK CHECK OK.

Part: NUT — MISSING (MLG WHEEL) · airframe 17,698 hrs · 2,938 cycles

ON WALKAROUND FOUND TIE NUT MISSING FROM NR 3 MAIN LANDING WHEEL ASSEMBLY. REPLACED MLG TIRE ASSY IAW MM.

Part: IDG — FAILED (NR 2 ENGINE) · airframe 17,576 hrs · 2,917 cycles

ON TAXI IN ATL, SHUT DOWN LT ENG AFTER COOLING. AFTER POWER TRANSFER, POWER STARTED TO TURN ON AND OFF APPROX THREE TIMES. FLIGHT ATTENDANT REPORTED SMOKE AND BURNING IN MAIN CABIN ALONG WITH FLICKERING LIGHTS. DOWN LOADED UTILITY BUSSES AND LT GEN CONTROL SWITCH. STARTED APU AND PROBLEM STOPPED, HAVE NOT RESET THE UTILITY BUSSES. RANG OUT FIELD WIRES AND ALL RESISTANCES WERE WITHIN LIMIT. REMOVED AND REPLACED NR 2 GCU, NO HELP. FOUND NO ELECTRICAL ODOR THROUGH OUT CABIN. REMOVED AND REPLACED RT IDG, OPS OK.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 13,350 hrs · 2,230 cycles

APPROXIMATELY 6 HOURS AND 50 MINS INTO FLIGHT RIGHT VSI CB POPPED AND RIGHT GEN TRIPPED OFF SIMULTANEOUSLY. A SLIGHT ELECTRICAL SMELL WAS NOTED IN THE FLIGHT STATION. THIS DISSIPATED RAPIDLY. GEN WAS RESET SUCCESSFULLY AS PER THE QRH PROCEDURE. RIGHT VSI CB NOT RESET. VERIFIED ELECTRICAL ODOR FROM RT VSI. REPLACED VSI, RESET CB AND OPS CHECK NORMAL. PERFORMED BITE CHECK OF BPCU RT GEN FAULTS DP TRIP IDG RISE TEMP GEN/FDR MAIN BUS/OVERLAP ZONE. PER FIM24-20-00 CHECK FDRS FOR SHORTS, ALL OK. IDG SERVICED PER PDC. REPLACED RT GCU, RUN UP CHECK NORMAL.

Part: WINDOW — CRACKED (COCKPIT) · airframe 6,150 hrs · 1,006 cycles

F/O RT WINDOW CRACKED ON LANDING. REPLACED SAME.

Part: VALVE — FAILED (RT WING) · airframe 5,623 hrs · 929 cycles

T/O DISCONTINUED. RT WING ANTI-ICE VALVE ILLUMINATED, APPROX 100 KNOTS. REMOVED AND REPLACED WING TAI VALVE. OPS CKS OK. PERFORMED ENG RUN VALVE LIGHT REMAINED OFF. CK OK PER M/M.

Part: WIRE — CHAFED (E/E BAY) · airframe 3,558 hrs · 604 cycles

WHILE INVESTIGATING ITEM 001 FOUND WIRE NR W230 OFF OF GND SERVICE SELECT RELAY DAMAGED FROM AVIONICS EQUIP ACCESS DOOR. WDM24-51-52 PAGE 12 SH 1 WIRE W230-011-8. REPAIRED WIRING PER PS SECURED WIRING TO PREVENT FURTHER CHAFING. ASSOCIATED SYSTEM CKS OK.

Part: UNKNOWN — ODOR (CABIN) · airframe 402 hrs · 80 cycles

ODOR WAS EVIDENT THROUGHOUT CABIN AND COCKPIT. ENTERTAINMENT SYSTEMS WAS TURNED OFF. ODOR SEEMED TO DISSIPATE. UTILITY BUSSES TURNED OFF EQUIPMENT COOLING TO OVERRIDE AND RECIRC FANS TURNED OFF. IN CONJUNCTION WITH TWO R/C REPS AND TWO DAL MECHANICS NO ODOR COULD BE DETECTED. SYSTEM OPS CHECK NORMAL. NO OVERHEATING DETECTED. ALL POWER TO IFE WAS TURNED BACK ON.