N865DA

Part: RIB — CRACKED (VERTICAL STAB) · airframe 87,164 hrs · 10,443 cycles

(AIRCRAFT 7006, L/P 1392582) OPEN HOLE HFEC INSPECTION SHOWS 7 EA CRACK INDICATIONS AT RIB ISS196 (2ND RIB O/B). 1 EA HOLE HAS CRACK APPROX. 1.25". OTHER 6 CRACKS ARE APPROX. 0.5".*MARKED*. CORRECTIVE ACTION: REPAIRED PER B777 SRM 57-43-01.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 83,344 hrs · 10,056 cycles

SEVERAL EMERGENCY PATH LIGHTING COVERS MISSING. CORRECTIVE ACTION: INSTALLED NEW COVERS. CKS OK.

Part: FLOOR SUPPORT — DENTED (BS 1944) · airframe 82,599 hrs · 9,975 cycles

(AIRCRAFT 7006, L/P 0864004) MTC TASK - BULK CARGO STA 1944 RBL 16.5 ATTACHED FLOOR STRINGER SURFACE FOUND DENT. MTC TASK - BULK CARGO AT STA 1942 - STA 1944.5 RBL 16.5 FLOOR STRINGER REPAIRED AS PER B777-200 SRM 53-70-53 FIG 202 REPAIR 2.

Part: FLOOR SUPPORT — DENTED (BS 1944) · airframe 82,599 hrs · 9,975 cycles

(AIRCRAFT 7006, L/P 0864018) MTC TASK - BULK CARGO STA 1944 RBL 16.5 ATTACHED FLOOR STRINGER SURFACE FOUND DENT. MTC TASK - BULK CARGO AT STA 1942 - STA 1944.5 RBL 16.5 FLOOR STRINGER REPAIRED AS PER B777-200 SRM 53-70-53 FIG 202 REPAIR 2.

Part: FLOOR SUPPORT — DENTED (BS 1991) · airframe 82,599 hrs · 9,975 cycles

(AIRCRAFT 7006, L/P 0864010) MTC TASK - BULK CARGO STA 1991 LBL 8.5 ATTACHED FLOOR STRINGER SURFACE FOUND DENT. MTC TASK - BULK CARGO AT STA 1990 - STA 1993 LBL 8.5 FLOOR STRINGER REPAIRED AS PER B777-200 SRM 53-70-53 FIG 202 REPAIR 2.

Part: FLOOR SUPPORT — DENTED (BS 1895) · airframe 82,599 hrs · 9,975 cycles

(AIRCRAFT 7006, L/P 0864025) MTC TASK - BULK CARGO STA 1895 RB 16.5 ATTACHED FLOOR STRINGER SURFACE FOUND DENT. MTC TASK - BULK CARGO AT STA 1895 RBL 16.5 FLOOR STRINGER SURFACE DENT MEASURED AND FOUND WITHIN LIMIT AS PER B777-200 SRM. MORE THAN 20.

Part: LIGHT — DAMAGED (SEAT 51D) · airframe 82,504 hrs · 9,963 cycles

(AIRCRAFT 7006, L/P 5115673) UNDER SEAT EMERGENCY LIGHT AT 51D DAMAGED. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT ASSY. PER B777 AMM 33-51-05.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 82,358 hrs · 9,947 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:38D. SECURED LIGHT CONNECTION.

Part: POWERPACK — INOPERATIVE (CABIN) · airframe 82,323 hrs · 9,943 cycles

(AIRCRAFT 7006, L/P 4361533) EMERGENCY LIGHTS INOP ON SEVICE CHECK ZONE 3. REMOVED AND REPLACED POWER PACK AND BATTERY IAW WDM 33-51-14 AT LOCATION M33404.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 78,724 hrs · 9,580 cycles

OXYGEN PANEL MASK DEPLOYED. DOOR FELL OPEN BUT GENERATOR DID NOT ACTIVATED. INSPECTED PASSENGER OXYGEN SYSTEM NO DEFECTS. CHECKED AFFECTED MASK COMPARTMENT AND FOUND OK. REPOSITIONED AND SECURED THE OXYGEN MASKS. PERFORMED SECURITY CHECK AND AMM 35-21. ACFT OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 78,462 hrs · 9,555 cycles

EMERGENCY LIGHTS INOP AT3L DOOR. NEED BATTERY PACKS AT LOCATION M33406 AND 33405. FOUND BAD BATTERY CHARGER, REPLACED. ALSO REPLACED 4 EACH BATTERIES. ALL EMERGENCY LIGHTS OPN NORMAL.

Part: NONE — NONE (L2 DOOR) · airframe 78,340 hrs · 9,542 cycles

SHIP 7006 2L DOOR WILL NOT CLOSE PROPERLY. CORRECTIVE ACTION: RE-CYCLED DOOR SEVERAL TIMES. OPS CK GOOD (4016484).

Part: BEARING — OUT OF POSITION (FLAP TRACK) · airframe 78,216 hrs · 9,530 cycles

ON THE LEFT WING, THE NUMBER 3 FLAP TRACK, FLAP MOTOR CARRIAGE MOUNT, UPPER INBOARD ATTACH BOLT IS RUSTY AND THE BEARING HAS PULLED OUT OF STRUCTURE. INSTALLED NR 3 FLAP I/B UNDER WING ACTUATOR SUPPORT LINK REF AMM 27-51-14. REPLACED LINK ASSY PER BAC DWG 113W1342.

Part: DOOR — OUT OF SEQUENCE (CABIN) · airframe 78,037 hrs · 9,512 cycles

2L DOOR WILL NOT CLOSE. FOUND DOOR 2L OUT OF SEQUENCE. REMOVED ACCESS COVER TO PUT INSIDE HANDLE IN OPEN POSITION. CLOSED AND OPENED DOOR IAW AMM 52-00 OPS CKD OK. ACCESS COVER REINSTALLED.

Part: WIRE — SHORTED (CABIN) · airframe 77,691 hrs · 9,471 cycles

DOING SERVICE CHECK FOUND EMERGENCY LIGHTS INOP SEATS 29 DEF TO 43 DEF AND EXIT IDENTIFIERS INOP AT AISLES DOOR 3. REPAIRED SHORTED WIRES ABOVE DOOR 3 LEFT TO RIGHT PARTITION PER SSM 33-51-14 AND SWPM 20-10. REPLACED FUSE IN PWR SUPPLY M33401 PER AMM 33-51-06. OPS GOOD. OK FOR SERVICE.

Part: SEAT TRACK — CRACKED (BS 1860) · airframe 75,265 hrs · 9,202 cycles

DURNING CRV, FOUND SEAT 53JHG LOOSE AND THE TRACK CRACKED. THE DAMAGED SEAT TRACK IS AT BS 1860 LBL 108. RELACED THE SEAT TRACK SECTION IAW DRAWING 151W7285, SHT 2.

Part: LENS — MISSING (CABIN) · airframe 75,125 hrs · 9,188 cycles

EMERGENCY LENS MISSING AT 3L/R CROSS AISLE. INSTALLED NEW EMER LIGHT LENS PER AMM 33-51.

Part: BATTERY — INOPERATIVE (R1 EPAS) · airframe 74,965 hrs · 9,174 cycles

DURING A SERVICE CHECK, FOUND THE R1 DOOR EPAS GREEN LIGHT INOPERATIVE. REPLACED EPAS 9 VOLT BACK-UP BATTERY IAW AMM 52-11.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 74,645 hrs · 9,144 cycles

EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED SEAT 55D. THE LENS WAS REPLACED. OPS CHECKED NORMAL IAW CMM 25-27-89.

Part: SIGN — OUT OF POSITION (CABIN) · airframe 73,581 hrs · 9,052 cycles

EXIT SIGN ABOVE DOOR 2L OFF OF BRACKET. REINSTALLED EXIT SIGN COVER. CONDITION CHECK NORMAL.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 69,680 hrs · 8,658 cycles

DURING SERVICE CHECK, FOUND DOOR 3L HORIZONTAL EXIT SIGN IS DIM. RELAMPED 8 LIGHT BULBS.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,305 hrs · 8,419 cycles

EMERGENCY AISLE LIGHTS INOPERATIVE BETWEEN SEATS 30A-J TO 41A-J. FOUND EMERGENCY LIGHT POWER SUPPLY AT DOOR 3R INOPERATIVE. R & R POWER SUPPLY AT DOOR 3R IAW AMM 33-51. LIGHTS CK OK. 6959159.

Part: FUSE — FAILED (EMERGENCY LIGHT) · airframe 61,917 hrs · 7,834 cycles

R2 DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPLACED POWER SUPPLY FUSE. CHECKED NORMAL IAW AMM 33-51. OK FOR SERVICE.

Part: LAMP — WRONG PART (EMERGENCY LIGHT) · airframe 61,787 hrs · 7,824 cycles

EMERGENCY PATH LIGHTS INOPERATIVE. FOUND INCORECT LAMPS. INSTALLED CORRECT LAMPS, REPLACED FUSE. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,539 hrs · 7,800 cycles

FLOOR EMERGENCY ESCAPE LIGHT INOPERATIVE ROW 10-14 ABCD. REMOVED AND REPLACED BATTERY PACK AND FUSE IN POWER SUPPLY IAW MM 33-51-06 OPS CHECKED GOOD. OK FOR SERVICE.

Part: BATTERY — INOPERATIVE (R4 DOOR) · airframe 57,724 hrs · 7,436 cycles

DURING SERVICE CK, FOUND 4R DOOR EPAS BATTERY INOPERATIVE. C/A R & R (2) 9V BATTERIES FOR 4R EPAS BACKUP BATTERIES IAW B777 52-11. OPS CHECK GOOD AT THIS TIME.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,446 hrs · 7,414 cycles

ROWS 31 THRU 41 SEAT MOUNTED PROXIMITY LIGHTS INOP. POWER SUPPLY M33404, FUSE 4 AND FUSE 3 TESTED BAD WIP(801167). REPLACED FUSE, CHECKED GOOD REF 33-51-00.

Part: SKIN — DENTED (NR 4 TE FLAP) · airframe 53,412 hrs · 7,031 cycles

NR 4 FLAP UPPER SURFACE DENTED. REPAIRED IAW SRM 57-53-01, AND SRM 51-70-04.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 52,721 hrs · 6,962 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY EXIT SIGN AT DOOR 3R WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. SYSTEM OPERATION WAS NORMAL AFTER THE POWER SUPPLY WAS REPLACED.

Part: FUSE — BROKEN (CABIN) · airframe 52,198 hrs · 6,913 cycles

DURING A MAINTENANCE VISIT, DOOR 2R SLIDE LIGHT AND FORWARD ZONE 2 EMERGENCY FLOOR PROX LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE FUSE 2 BROKEN AND REPLACED IT. MAINTENANCE ALSO REPLACED M33098 POWER SUPPLY. SYSTEM OPERATION WAS NORMAL AFTER THE FUSE AND POWER SUPPLY WERE REPLACED.

Part: SOCKET — SHORTED (CABIN) · airframe 50,188 hrs · 6,730 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY TRACK LIGHTS ALONG BUSINESS ELITE SEATS ROW 10-14 ON THE LEFT AND RIGHT AISLE WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE LEFT SOCKET AT SEAT 11B SHORTED AND BLOWING THE FUSES AND REPLACED IT. SYSTEM OPERATION WAS NORMAL AFTER THE SOCKET WAS REPLACED.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 45,683 hrs · 6,276 cycles

BATTERY PACK FAILS CAPACITY TEST. REPLACED 3 BATTERY PACKS FOR SEAT ROWS 10-41 OPS NOW CK NML.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 45,623 hrs · 6,271 cycles

EMERGENCY LIGHT AT SEAT31F INOP. REPAIRED BROKEN CONNECTOR OP CK GOOD.

Part: CHILLER — INOPERATIVE (AFT GALLEY) · airframe 45,542 hrs · 6,261 cycles

IR - MIDGALLEY AFT CHILLER INOPERATIVE. OVERHEAT LT ON WITH ELECTRICAL ODOR. C/BS PULLED AND COLLARED.

Part: VALVE — MALFUNCTIONED (FUEL SYSTEM) · airframe 44,902 hrs · 6,198 cycles

RTB DUE TO LT ENG SPAR VLV MSG. RESET MSG, CLEARED MSG LT ENG STARTED NORMAL. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: SHROUD — DAMAGED (NR 2 ENGINE) · airframe 44,674 hrs · 6,179 cycles

THE 1ST STG LPT OUTER SHROUD WAS BORESCOPED PER OPN 52140. DAMAGE WAS FOUND IN THE OUTER SHROUD. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: PRESSURE SWITCH — FAILED (NR 1 ENG FUEL) · airframe 43,499 hrs · 6,078 cycles

RTB DUE TO LT ENG FUEL FILTER WARN EICAS MSG/C FWD TO MCO PLACARD PER MEL 73-34-01A. R & R FUEL FILTER DIFFERENTIAL PRESSURE SWITCH IAW AMM. OPS CHECK OK. LEAK CHECK OK. MESSAGE DID NOT RETURN MCO AND PLACARD REMOVED. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: SKIN — DAMAGED (STA 424-455) · airframe 36,201 hrs · 5,504 cycles

FUSELAGE SKIN HAD LIGHTNING STRIKE DAMAGE AT STA 424 AND STA 455 AT S-10L. ALSO, THE S-10L STRINGER SUSTAINED TOOLING DAMAGE DURING ACCOMPLISHMENT OF THE SKIN REPAIRS. THE DAMAGED SKIN WAS CUT OUT AND REPAIR DOUBLERS WERE INSTALLED. THE DAMAGE IN THE STRINGER FLANGE WAS TRIMMED OUT AND A REPAIR ANGLE WAS INSTALLED.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 35,174 hrs · 5,407 cycles

EMERGENCY LIGHTS IN CABIN ILLUMINATED INTERMITTENTLY DURING CRUISE. PERFORM EMERGENCY LIGHTS DAILY OPERATIONAL TEST AND EMERGENCY LIGHTS OPERATIONAL TEST WITH CONTROL SWITCHES PER AMM 33-51-00-710-801 AND AMM 33-51-00-710-803. EMERGENCY LIGHTS CHK OK.

Part: NONE — NONE (NONE) · airframe 33,185 hrs · 5,230 cycles

WINDSHEAR MSG DISPLAYED. FWD WINDSHEAR TO MCO PER MEL 34-43-01D. NO FAULT HIST IN MAT. RAN WXR TEST NO FAULTS. MCO AND PLACARD REPLACED.

Part: ELECTRONIC UNIT — INOPERATIVE (3R DOOR O/H) · airframe 31,514 hrs · 5,050 cycles

WORK LIGHTS INOPERATIVE AT 3L/3R. OEU M23406 AT 3R DOOR FAILED ON CABIN ALL TEST. FOUND OEU SHOWS EVIDENCE OF BURN MARK. REMOVED AND REPLACED OEU. COULD NOT COMPLETE SOFTWARE UPLOAD. FWD OEU SOFTWARE LOAD TOMCO AND PLAC PER MEL 25-20-01I. LOADED CONFIG AND DATABASE SOFTWARE TO OEU LIGHTS OP NORMAL MCO AND PLACARD REMOVED.

Part: UNKNOWN — ODOR (CABIN) · airframe 31,437 hrs · 5,042 cycles

FLT ATTN OBL REPORTS ODOR AT FWD B/E CABIN LEFT SIDE. POSS BURNING SMELL. NO SMOKE OR FIRE NOTED. FLT ATTN OBL COULD NOT IDENTIFY SMELL OR SOURCE. OBL DID NOT KNOW IF IT WAS A BURNING SMELL OR NOT. FLT CREW DID NOT SMELL ANY UNUSUAL ODOR EN ROUTE. RAN PACKS AT FULL HOT AND NO ABNORMAL SMELL. NO UNUSUAL SMELL IN ENTIRE CABIN. IFE EQUIP ON AND NO SMELL NOTED. INSPECT E/E COMPARTMENT AND NO SMELL NOTED. FWD CARGO BIN NO SMELL NOTED.

Part: WEU — MALFUNCTIONED (COCKPIT) · airframe 29,892 hrs · 4,873 cycles

ON T/O PWR STABILIZER WARNING SOUNDED - T/O TRIM WAS NOT IN THE GREEN BAND. TRIM WAS IN THE GREEN BAND AT PUSH BACK. AWABS TRIM SETTING 2.5. CHECKED MAT FOR RELATED MSGS - NONE NOTED. RAMP HAD TO RELOAD A/C REAR TO FRONT. MAT TEST FAILS WEU REPLACED WEU RT LOADED OPS AND OPC SOFTWARE TO RT WEU PERFORMED SUCCESSFUL WEU TEST IAW MM. ETOPS CATEGORY (E): PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: VALVE — LEAKING (BLEED AIR SYS) · airframe 26,138 hrs · 4,457 cycles

AFTER T/O, LEFT ENG BLEED OFF EICAS MESSAGE. A/C RETURN TO ATL. MTC REPLACED HPSOV AND PNEU PRESSURE LINE FROM BRACKET DISCO, HPSOV NEED LEAK CHECK AND OP CHECK. PERFORMED LEAK CHECK, ENGINE AIR SUPPLY OP TEST PER MM 36-10-00-700-801. FOUND PNEUMATIC LINE TO PRSOV LEAKING WHILE PERFORMING LEAK CHECK. REPLACED UNION AT PRSOV AND RE-PERFORMED LEAK CHECK. LEAK PAST AND ENG AIR SUPPLY OP TEST PAST.

Part: CHILLER — ODOR (AFT GALLEY) · airframe 25,878 hrs · 4,426 cycles

ON PRE-FLIGHT, F/A REPORTED BURNING SMELL IN AFT GALLEY. FAULT LIGHT ON CHILLER. REPLACED CHILLER.

Part: GSSR — FAILED · airframe 25,732 hrs · 4,411 cycles

UNABLE TO PWR GROUND SERVICE BUSS CABIN LIGHTS OUT/GALLEY PWROUT/ENT SYSTEM OUT. NO LAND 3 IN FDE WAS ABLE TO RESTORE USING APU PWR HOWEVER COULD RESTORE BACK TO FLT CONFIG DUE TO GROUND SERVICE BUS NECESSARY FOR FLT CREW ELECTED TO RTN ATL. REPLACED GSSR.

Part: INSULATION — DAMAGED (NR 1 & 2 ENGINE) · airframe 25,039 hrs · 4,323 cycles

THRUST REVERSER INSULATION BLANKETS WERE FOUND DAMAGED. INSPECTED AND REPAIRED PER ER/A 451632-14AD REF AD 2005-07-24.

Part: A/C PACK — ODOR (NR 1 ENGINE) · airframe 24,008 hrs · 4,164 cycles

A/C HAS STRONG OIL SMELL. RAN PACKS FOR 1 HOUR. CHECKED A/C SYSTEMS. NTF.

Part: CONVERTER — FAILED (OZONE) · airframe 23,967 hrs · 4,152 cycles

STRONG OIL SMELL DURING FLT WORSE IN CLB/DESCENT AND PWR CHANGES. SUSPECT FROM PACK L/R. OVERWHELMING ODOR IN C/P ON DESCENT IRRITATED EYES. CHECKED EXH OF LT AND RT PACK. FOUND ODOR COMING FROM LT PACK. CHECKED INSIDE LP AND HP DUCTS LT ENG NO OIL RESIDUE FOUND. CHECKED ALL BLEED VLV EXITS LT ENG NO RESIDUE. CKD APU DUCT NO RESIDUE. RAN LT ENG NOTICED STRONG ODOR IN C/P DURING BLEED SHIFT. BORO LT ENG COMP NO OIL FOUND. PERFORMED CONTAMINATION REMOVAL PER AMM. REPLACED UPPER/LWR RECIRC FILTERS. REPLACED LT OZONE CONV PER AMM. NO FUMES AFTER OZONE CONV REPLACED.

Part: ODOR — DETECTED (CABIN) · airframe 23,967 hrs · 4,152 cycles

CHEMICAL/MUSTY SMELL 4 TIMES USUALLY WITH PWR REDUCTION ALSO NOTED IN AFT CABIN, CHKD PER FIM TASK 21-00-00-810-808. CHKD L ENG BLEED AIR FOR OIL CONTAM. CHKD PACKS FOR OIL CONTAM. CHKD HYD RES PRESS MODULES. CHKD RECIRC FANS AND CARGO COMPT. CHKD FOR HYD LEAKS INSP NO TROUBLE FOUND. CONTACTED MCC FOR MORE INFO, HAD CREW RUN ENGS NTF.

Part: FAN — FAILED (CABIN) · airframe 23,116 hrs · 4,036 cycles

RECIRC FAN STAUS MSG STRONG ELECTRICAL ODOR. REPLACED FAN.

Part: CASE — CRACKED (NR 2 ENG IDG) · airframe 21,187 hrs · 3,780 cycles

ELEC GEN OFF RIGHT EICAS MESSAGE IN FLIGHT WITH GEN DRIVE RIGHT EICAS MESSAGE. FOUND RT IDG CASE SHATTERED AND ZERO OIL. REPLACED IDG AND RAN ENG PER PFHB TEST 1 AND 2. ALL NORMAL.

Part: FUSE — BLOWN (BATTERY PACK) · airframe 16,415 hrs · 3,058 cycles

EMERGENCY CEILING LIGHT AT SEAT ROW 38 IS OUT. FOUND FUSE BLOWN IN BATTERY PACK. REPLACED FUSE EMERGENCY LIGHTS CHECKS GOOD.

Part: SLIDE — UNSERVICEABLE (L-2 DOOR) · airframe 16,061 hrs · 3,009 cycles

AT DEPARTURE L-2 DOOR SLIDE CAME OFF THE DOOR. REPLACED L2 DOOR SLIDE ASSEMBLY.

Part: FAN — FAILED (RIGHT) · airframe 15,427 hrs · 2,925 cycles

RT LOWER RECIRC FAN TRIPPED IN FLT HEAVY ELECTRICAL SMELL DETECTED PRIOR TO FAILURE. REMOVED AND REPLACED RECIRC FAN. SYSTEM OPS CHECK NORMAL.

Part: COFFEEMAKER — SPARKS (GALLEY) · airframe 13,611 hrs · 2,604 cycles

COFFEEMAKER AT 205 SPARKING TURNED OFF PWR PULLED C/B. REPLACED COFFEEMAKER.

Part: IDG — INOPERATIVE (#2 ENGINE) · airframe 13,060 hrs · 2,505 cycles

RT IDG TRIPPED OFF SHORTLY AFTER TAKEOFF. ELECT SMELL IN CABIN. TRIED ONE RESET NO HELP. 0634/28JAN/ATL/ 456509 - PASSING 10000 FEET AFTER TAKE OFF ELEC GEN RT LIGHT ILLUM. TRIED 1 RESET PROCEDURE AND REMANED OFF. LANDED WITH 482000 LBS. 02 FWD RT ENG DRIVE GEN. TO MCO AND PLAC PER MEL 24-11-01. RT GENERATOR DISCONNECTED REPLACED RT IDG. OPS CHECK NORMAL. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK

Part: LINE — LEAKING (NR 2 ENGINE) · airframe 12,216 hrs · 2,350 cycles

OIL QUANTITY RT ENGINE DROPPED TO 1 DURING FLIGHT, ALL OTHER INDICATIONS WERE NORMAL. REPLACED OIL BEARING SUPPLY LINE.

Part: ENGINE — DAMAGED (NR 1) · airframe 11,521 hrs · 2,236 cycles

BOTH ENGINES CHANGED DUE TO FAILED BOROSCOPE. DUST CAP INSPECTED

Part: COFFEEMAKER — SPARKS (GALLEY) · airframe 10,332 hrs · 2,035 cycles

GALLEY 412 DURING FLIGHT, F/A OBSERVED SPARKS FROM COFFEEMAKER NR 2. DEPOWERED ALL 3 C/BS TO ALL 3 COFFEEMAKERS. REMOVED ALL COFFEEMAKERS OUT OF AFT GALLEY LEFT SIDE. INSPECTED ALL WIRES BEHIND COFFEMAKERS, FOUND NO DAMAGE. REINSTALLED ORIGINAL COFFEEMAKERS, ALL CHECK OK.

Part: CONNECTOR — BURNED (CABIN) · airframe 9,635 hrs · 1,905 cycles

ROCKWELL FOUND BURNT CONNECTOR AT VIDEO SCREEN SEAT 30G. DISCONNECTED SDU TO AVU CABLE FWD TO MCO.

Part: POWER SUPPLY — FAULTY (E/E BAY) · airframe 9,453 hrs · 1,870 cycles

STRONG BURNING SMELL IN CABIN, INFLIGHT. EMERGENCY DECLARED INTO ATL. REMOVED AND REPLACED POWER SUPPLY. UNIT SENT TO MANUFACTURER FOR ANALYSIS. SUSPECT FOREIGN RESIDUE MAY HAVE CONTRIBUTED TO THE FAILURE.

Part: STRUCTURE — VIBRATION (FUSELAGE) · airframe 4,711 hrs · 1,025 cycles

MODERATE VIBRATION REPORTED BY F/A ON T/O LOUD NOISE AT 2L/2R DOORS F/O CONFIRMED AT APPROX 10K FEET. STAB WAS 4.5 FOR T/O BUT REQUIRED SUBSTANTIAL FORCE FOR ROTATION. VIB DOES DECREASE AS DID NOISE WITH A/S INCREASE. INSPECTED ALL A/C COMPONENTS IN MID FUS AND RAM AIR DOOR HINGES, RAN ENGS TO T/O PWR AND PRESSURISED A/C. NO NOISE NOTED. A/C REQUIRES TEST FLT. NOTE: TEST FLT NTF.

Part: TRANSCEIVER — MALFUNCTIONED (E/E BAY) · airframe 2,866 hrs · 706 cycles

STATUS MSG WXR SYS AND NO WXR AVAILABLE. REPLACED TRANSCEIVER, OPS CHECK NORMAL.

Part: APU — MALFUNCTIONED (AFT) · airframe 2,689 hrs · 672 cycles

LT ENG GEN/IDG ON MCO-APU S/D GOING THROUGH 19K APU RE-START OK BUT CREW LOST CONFIDENCE IN THE APU FOR THE CROSSING. AIR TURNBACK, ELEC GEN OFF L EICAS ILLUMINATED, RESET AS PER CHECKLIST. EICAS RETURNED, NO HELP. REPLACED LT IDG PER MM ENG RUN ALL INDICATIONS NORMAL, NO LEAKS. REMOVED MCO AND PLACARD. APU FWD TO MCO MEL 49-11-01.