N864DA

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 84,416 hrs · 10,049 cycles

THERE IS NO COVER FOR THE EXIT SIGN LEAVING THE UPPER CREW REST. SECURED SIGN.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 84,200 hrs · 10,027 cycles

LEFT ASILE CEILING EMERGENCY LIGHT LENS MISSING AT ROW 34-35. INSTALLED MISSING LENS AS NEEDED.

Part: HANDLE — LACK OF LUBE (R1 DOOR) · airframe 82,450 hrs · 9,842 cycles

(AIRCRAFT 7005, L/P 5333138) 1 RIGHT DOOR EXTERIOR DOOR HANDLE WILL OPEN OR CLOSE PASSENGER DOOR FROM OUTSIDE OF A/C. EXERCISED AND LUBED 1 RIGHT DOOR HANDLE SPINDLE, NOWS OPS NORMAL. (SUSPECT DOOR HANDLE ROLLERS FROZEN ON DOOR INTERIOR ) OUTSIDE TEMP -15 F.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 79,508 hrs · 9,542 cycles

ON TAXI OUT FLIGHT ATTENDANT NOTICED THE EMERGENCY LIGHTS IN THE AFT 1ST CLASS SECTION DID NOT WORK AGAIN. AS PREVIOUSLY WRITTEN UP. T/S PER SEAT CMM 25-24-61 FIG 2016 SHT 4 AND WDM 33-51-58 SHT 1 FOUND C/P J1 DISCONNECTED AND J2 C/P BROKEN AT SEAT 12C. RECONNECTED J1 REMOVED AND REPLACED J2 CONNECTOR PER WDM 33-51. OPS CHECK GOOD OK FOR SERVICE.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 79,488 hrs · 9,540 cycles

EMERGENCY LIGHT BULBS OUT 3C, ROW 10 THRU 12 EMERGENCY LIGHTS OUT. TROUBLESHOOTING PERFORMED IAW FIM 33-51-00-810-803, FOUND POWER SUPPLY M33098 FAULTY. R&R POWER SUPPLY IAW AMM 33-51-06-960-803, R&R BATTERY PACK IAW AMM 33-51-06-960-802. FOUND POWER SUPPLY FROM DL STOCK BFS. FOUND FUSE INOP, NEW FUSE INSTALLED. BATTERY PACK LOAN PART FROM AF. BATTERY PACK CHANGED POS 33097 PRECAUTIONARY. NEW FUSE INSTALLED ON POS. 33097. TEST SATISFACTORY. A/C OK FOR SERVICE.

Part: INDICATION SYS — MALFUNCTIONED (CABIN) · airframe 79,488 hrs · 9,540 cycles

OCCASIONAL ERRONEOUS READINGS ON FLT ATT MAIN PANEL DOORS SHOWING ARMED WHEN DISARMED. T/S IAW FIM 52-11-00 -810-802 PED FLC TEST NO FAULTS OPERATIONAL CK OF ARM/DISARM LIGHT OK FOR SVC.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,211 hrs · 9,513 cycles

EMERGENCY LIGHTS CHARGING UNIT M33098 INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY POWER CHARGER AND BATTERY PACK IAW AMM 33-51.

Part: FUSE — BLOWN (CHARGER) · airframe 79,055 hrs · 9,497 cycles

FOUND EMERGENCY LIGHTS OUT ROWS 10, 11, 12. REPLACED FUSE F2 ON CHARGER M33098 PER AIM 33-51. EMERGENCY LIGHTS OPS CK GOOD.

Part: SIGN — DAMAGED (SEAT 43F) · airframe 79,055 hrs · 9,497 cycles

EMERGENCY LIGHT DAMAGED SEAT 43F. INSTALLED A NEW SIGN ASSY IAW AMM 33-51.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 1D) · airframe 78,485 hrs · 9,439 cycles

SEAT 1D OXYGEN MASK DROPPED ON DEPTATURE. PACKED THE MASK IAW AMM 35-21. OK FOR SERVICE.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 78,468 hrs · 9,437 cycles

FOUND THE EMERGENCY LIGHTS INOPERATIVE AT SEATS 10ABC, 11ABCD AND 12ABCD. FOUND THE FUSE BLOWN ON THE POWER SUPPLY. REPLACED THE FUSE IAW AMM 33-51. CHECKED OK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 78,102 hrs · 9,400 cycles

EMERGENCY LIGHT LENS MISSING. REPLACED THE LENS, OPS CHECKED GOOD IAW AMM 31-51.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 77,388 hrs · 9,326 cycles

AISLE LIGHT 10B LENS BROKEN. SECURED LENS. OK FOR SERVICE.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,290 hrs · 9,316 cycles

DURING A SERVICE CHECK, EMERGENCY SEAT LIGHTS WERE INOPERATIVE. TROUBLESHOT IAW SRM 33-51-13, REPLACED FUSE IN THE POWER SUPPLY M33098. OPS CHECKED GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 77,241 hrs · 9,311 cycles

EMERGENCY LIGHT BATTERY PACK FAILED AN EMERGENCY LIGHT FUNCTIONAL CHECK. REPLACED BATTERY PACK IAW AMM 33-51 .

Part: LIGHT — DETACHED (SEAT 36F) · airframe 77,150 hrs · 9,300 cycles

SEAT 36F EMERGENCY LIGHT DETACHED. REPLACED EMERGENCY LIGHT HOUSING. TESTED OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 77,150 hrs · 9,300 cycles

L2 DOOR AFT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMPS. TESTED OK.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 77,021 hrs · 9,285 cycles

DURING A SERVICE CHECK, FOUND EMERGENCY LIGHTS WOULD NOT ILLUMINATE IN BOTH AISLES FROM ROWS 10-12. REPLACED THE FUSE IN THE POWER SUPPLY IAW AMM 33-51, AND ASM 33-51.

Part: SKIN — DENTED (FUSELAGE) · airframe 82,273 hrs · 9,823 cycles

(AIRCRAFT 7005, L/P 9618172) REF LOG 9618169 FOR LT FUSELAGE DENT FOUND ON ARRIVAL. CORRECTIVE ACTION: FUSELAGE SKIN LT STA 424, STR 26 - STR 27L DENTED AREA PERFORMED REPAIR AS PER SRM 53-00-01 REPAIR NR 7 REV 76. RII COMPLETED.

Part: LENS — MISSING (CABIN) · airframe 76,181 hrs · 9,191 cycles

EMERGENCY FLOOR LIGHTING MISSING AT POSITION 4053. RE-INSTALLED LENS.

Part: LENS — MISSING (CABIN) · airframe 76,181 hrs · 9,191 cycles

EMERGENCY FLOOR LIGHTING LENS MISSING AT POSITION 406. INSTALLED LENS.

Part: FLAP — DENTED (RT WING) · airframe 74,755 hrs · 9,036 cycles

ON MX WALK AROUND FOUND DENT ON RIGHT OB TRAILING EDGE FLAP OUTBOARD 24" OF NR 7 FLAP SUPPORT CANOE + 14" FWD OF FLAP. REPAIRED DENT PER SRM 57-53-01. JOB COMPLETE.

Part: FLAP — DENTED (RT WING) · airframe 74,755 hrs · 9,036 cycles

ON MX WALK AROUND FOUND DENT ON RIGHT OB TRAILING EDGE FLAP. REPAIRED DENT PER SRM 57-53-01 JOB COMPLETE.

Part: WEB — NO TEST (RT NACELLE) · airframe 74,549 hrs · 9,017 cycles

RT PYLON AFT FAIRING LOWER WEB FAILED CONDUCTIVITY TEST AT NAC STA 450 (READING 35.4) REPLACED THE WEB IAW SRM 54-52-71.

Part: WEB — CORRODED (RT NACELLE) · airframe 74,549 hrs · 9,017 cycles

RT PYLON AFT WEB HAS CORROSION AT NAC 375 ON LOWER SURFACE. REPLACED THE WEB IAW SRM 54-52-71.

Part: STRUCTURE — CORRODED (LT NACELLE) · airframe 74,549 hrs · 9,017 cycles

LT PYLON INBD STRUCTURE CORRODED AT NAC STA 39, AND 405. REPAIRED IAW SRM 54-52-71.

Part: ANGLE — CORRODED (RT NACELLE) · airframe 74,549 hrs · 9,017 cycles

RT PYLON INBD ANGLE HAS CORROSION AT NAC STA 390, 405, AND 420. REPLACED THE ANGLE IAW SRM 54-52-71.

Part: CHANNEL — DAMAGED (RT NACELLE) · airframe 74,549 hrs · 9,017 cycles

RT PYLON AFT FAIRING U CHANNEL AT NAC STA 351 FAILED CONDUCTIVITY TEST (35.4 % IAC) REPLACED THE CHANNEL IAW SRM 54-52.

Part: BRACKET — CORRODED (RT NACELLE) · airframe 74,549 hrs · 9,017 cycles

RT PYLON AFT WEB BRACKET WORN INTO INBD STRUCTURE AT NAC STA 454. REPLACED THE BRACKET IAW SRM 54-52-71.

Part: BRACKET — WORN (RT NACELLE) · airframe 74,549 hrs · 9,017 cycles

RT PYLON AFT WEB BRACKET WORN INTO OTBD STRUCTURE AT NAC STA 454. REPLACED THE BRACKET IAW SRM 54-52-71.

Part: WEB — CORRODED (LT NACELLE) · airframe 74,549 hrs · 9,017 cycles

LT PYLON AFT WEB HAS CORROSION NAC STA 454. REPLACED THE WEB IAW SRM 54-52.

Part: ANGLE — CORRODED (RT NACELLE) · airframe 74,549 hrs · 9,017 cycles

RT PYLON OUT OTBD ANGLE HAS CORROSION AT NAC STA 390, 405, & 420. REPLACED THE ANGLE IAW SRM 54-52.

Part: WEB — DAMAGED (LT NACELLE) · airframe 74,549 hrs · 9,017 cycles

LT PYLON AFT WEB FAILED CONDUCTIVITY TEST AT NS 450. REMOVED AND REPLACED THE WEB IAW SRM 54-52-17.

Part: WEB — CORRODED (LT NACELLE) · airframe 74,549 hrs · 9,017 cycles

LEFT PYLON AFT WEB HAS CORROSION AT NAC STA 454. REPLACED THE WEB IAW SRM 54-52.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 74,526 hrs · 9,014 cycles

EMERGENCY LIGHT LENS DETACHED. INSTALLED THE LENS CHECKED GOOD.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 74,526 hrs · 9,014 cycles

EMERGENCY LIGHT LENS DETACHED. ATTACHED THE LENS.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,358 hrs · 9,000 cycles

FLOOR EMERGENCY LIGHTS INOPERATIVE FOR SEATS 10BC, 11BC & 12BC. INSPECTED & FOUND THE CHARGER DEFECTIVE. R & R THE CHARGER M33098 IAW AMM 33-51.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,258 hrs · 8,990 cycles

EMERGENCY LIGHT INOPERATIVE AT SEATS 10-12, BOTH SIDES. REPLACED THE FUSE IN THE POWER SUPPLY M33098 IAW AMM 33-51-06.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,175 hrs · 8,896 cycles

ONE EXIT DESIGNATOR AT THE L1 DOOR & ONE EXIT DESIGNATOR AT THE L4 DOOR FOUND INOPERATIVE. INSTALLED MISSING EMERGENCY LIGHTS.

Part: SHROUD — LOOSE (CABIN) · airframe 73,262 hrs · 8,904 cycles

FLOOR PROXIMITY LIGHTS AT 32D, 35D, 42D, 47D, 52D, 54D, 55D, 51F HAVE LOOSE HOUSINGS BUT OPERATE NORMALLY. REPLACED SHROUDS.

Part: SEAT TRACK — CHAFED (BS 951) · airframe 69,984 hrs · 8,574 cycles

CABIN SEAT TRACK AT BS 951, RBL 11 FOUND CHAFED. REPAIRED IAW SRM 53-00-52, FIG 202. REPAIR 1 AND ER/A 543536-14, PRI REV 0.

Part: SEAT TRACK — CORRODED (BS 1480-1567) · airframe 69,983 hrs · 8,573 cycles

SEAT TRACK BETWEEN BS 1480 - 1567, LBL 74 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 AND FOUND OUT OF LIMITS IAW SRM 53-00-52, FIG 102. REPAIRED IAW SRM 53-00-52, FIG 102, REPAIR 1 AND ER/A 543536-14, PRI REV 0.

Part: SEAT TRACK — CORRODED (BS 1434-1444) · airframe 69,984 hrs · 8,574 cycles

CABIN SEAT TRACK AT BETWEEN BS 1434 TO 1444, LBL 11 FOUND CORRODED. SEAT TRACK REPAIRED IAW SRM 53-00-52, FIG 202. REPAIR 1 AND ER/A 543536-14, PRI REV 0.

Part: SEAT TRACK — CORRODED (BS 1480-1567) · airframe 69,984 hrs · 8,574 cycles

CABIN SEAT TRACK BETWEEN BS 1480 TO BS 1567, LBL 74 FOUND CORROSION AT SEVERAL LOCATIONS. REPAIRED IAW SRM 53-00-52, FIG 202, REPAIR 3 AND ER/A 543536-14 PRI REV 0.

Part: TIRE — DEPARTED (MLG) · airframe 68,503 hrs · 8,426 cycles

DURING TAKEOFF, THE NR 8 TIRE DEPARTED THE ACFT. DISPATCHED NOTIFIED THE CREW WHILE ENROUTE. CREW REF PROCEDURES IN MANUALS AND A NORMAL APPROACH, LANDING, AND TAXI WAS MADE. MAINTENANCE REPLACED THE NR 8 TIRE, BRAKE, CENTER AXLE, AND AXLE NUT. ALSO, REPLACED THE NR 4, NR 7 AND NR 12 TIRES, NR 8 HUBCAP AND ANTI-SKID TRANDUCER AND REPAIRED RT WING INBD FLAP IAW ER/A 540151-14.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,341 hrs · 8,093 cycles

SEAT ROW 12-15 LT AND RT EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY UNIT IAW AMM 33-51-07.

Part: COVER — MISINSTALLED (LAVATORY DOOR) · corrosion level 3 · airframe 58,844 hrs · 7,370 cycles

LAVATORY DOOR HARD TO OPEN OR CLOSE. LOWER COVER WAS STRAIGHT AFTER REMOVAL, CORRECTLY INSTALLED AND DOOR CHECKED NORMAL TO OPEN & CLOSE IAW AMM 52-53-01.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 57,465 hrs · 7,260 cycles

EMERGENCY LIGHTS AT ROWS 10 THROUGH 14 LT AND RT SIDE ARE INOPERATIVE. TROUBLESHOT IAW WDM 33-51-58, FOUND BLOWN FUSE AT M33098 EMERGENCY POWER SUPPLY, REPLACED FUSE, OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,207 hrs · 7,149 cycles

EMERGENCY LIGHTS ROW 10-14 INOPERATIVE. R & R EMERGENCY LIGHT BATTERY CHARGER IAW AMM 33-51, CHECKED GOOD.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 55,786 hrs · 7,102 cycles

EMERGENCY LIGHT INOPERATIVE. REPLACED TWO BLOWN FUSES IN POWER SUPPLY. OPS CHECKED NORMAL IAW AMM 33-51-06. OK FOR SERVICE.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 55,786 hrs · 7,102 cycles

OUTSIDE DOOR EMERGENCY LIGHT. REPLACED BLOWN FUSES. OPS CHECKED OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,637 hrs · 7,008 cycles

EMERGENCY PATH LIGHTS ROWS 31 THRU 42 INOP. REPLACED POWER SUPPLY AT DOOR 3R PER MM33-51-06. OPS CHECK GOOD.

Part: FUSE — BLOWN (CABIN) · airframe 52,090 hrs · 6,753 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY ESCAPE PATH LIGHT AT ROWS 10-14 ABCD WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE FUSE ON THE BATTERY PACK. SYSTEM OPERATION WAS NORMAL AFTER THE FUSE WAS REPLACED.

Part: FUSE — BLOWN (CABIN) · airframe 52,018 hrs · 6,745 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY FLOOR PROXIMITY LIGHTS IN CABIN ZONE B WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK FUSES. SYSTEM OPERATION WAS NORMAL AFTER THE BATTERY PACK FUSES WERE REPLACED.

Part: WIRE HARNESS — DISCHARGED (CABIN) · airframe 49,914 hrs · 6,550 cycles

EMERGENCY LIGHTS AT SEAT 5C WAS FOUND TO BE INOPERATIVE. MAINTENANCE RE-CONNECTED THE HARNESS AND OPERATION RETURNED TO NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 49,560 hrs · 6,510 cycles

LIGHTNING STRIKE AT STA 236 AT 36R HAS 3 SPOTS THAT NEED TO BE REPAIRED. REPAIRED PER ERA 492206-14 REV B.

Part: SLAT TRACK — LOOSE · airframe 48,474 hrs · 6,394 cycles

DURING INSPECTION OF SLAT DOWNSTOPS IAW EA 11-469704-03 AD, ME 01 AND ME 02 FOUND NR 4 SLAT OTBD TRACK ALSO NR 5, SLAT OTBD TRACK AND NR 9 SLAT OTBD TRACK BOLT LOOSE. REPLACED FASTENERS IAW EA 11-469704-03, AD, ME 09 AND ME 10.

Part: EEC — UNSERVICEABLE (NR2 ENGINE) · airframe 44,249 hrs · 5,963 cycles

ENG EEC MODE RT ENGINE CONTROL STATUS AND CAUTION MSG REPLACED RT ENG POWER CONTROL UNIT IAW AMM. MFG PN PCU500MK5. MSG CLEARED. RAN ENG AT IDLE. CHECKS GOOD. ETOPS CATEGORY 'E': PROBLEMS WITH SYS CRITICAL TO ETOPS

Part: APU — UNSERVICEABLE (APU BAY) · airframe 43,598 hrs · 5,901 cycles

APU CHANGE. REMOVED AND REPLACED APU S/N ON P1314. IN FLT START REQUESTED.

Part: IDG — LEAKING (NR 1) · airframe 40,806 hrs · 5,675 cycles

ON ENG START THE LEFT GEN OFF AND LEFT GEN DRIVE LIGHT REMAINED ILLUMINATED. REPLACED LT IDG PER AMM ALL CKS GOOD MPN 764939B.

Part: GCU — FAILED (LEFT) · airframe 40,798 hrs · 5,674 cycles

DURING ENG START LEFT GEN OFF LIGHT NEVER EXTINGUISHED. ATTEMPTED RESET PER QRH. RESET FAILED. RETURNED TO GATE FWD TO MCO AND PLACARD PER 24-11-01 CAT B APPLIED. MAINTENANCE PROCEDURE CUT OUT AS PER MEL. TROUBLESHOOTING PER FIM FOUND L GCU BAD. REPLACED SAME, CHECKS OK. MCO/PLACARD REMOVED. MFN INSTALLED 756603E.

Part: SKIN — GOUGED (BS 677 S21R) · airframe 40,608 hrs · 5,658 cycles

A FAN BLADE FRAGMENT FROM THE NR 2 ENGINE GOUGED THE FUSELAGE SKIN AT STA 677 ABOVE S-21R. THE DAMAGED SKIN WAS CUTOUT AND AN EXTERNAL REPAIR DOUBLER WAS INSTALLED.

Part: ENGINE — MAKING METAL (NR 1) · airframe 36,818 hrs · 5,371 cycles

FOUND M50 BEARING MATERIAL ON MCD ENG REMOVED AND REPLACED ON LOGSHEET H124922 ITEM 010 MSU REMOVED.

Part: SKIN — DENTED (BS 1640- 1650) · airframe 36,278 hrs · 5,331 cycles

FUSELAGE SKIN HAS TWO DENTS/GOUGES LOCATED BETWEEN STA 1630 AND 1650 AT S-32R. CUTOUT DAMAGED SKIN AND INSTALLED REPAIR.

Part: ENGINE — DAMAGED (NR 2) · airframe 35,325 hrs · 5,236 cycles

RTO FOR ENG EXCEEDENCE, ACFT QUARANTINED PENDING NTSB INVESTIGATION FOR POSSIBLE UNCONTAINED FAN SEPERATION NR 2 ENGINE REPLACED.

Part: GCU — MALFUNCTIONED (LEFT) · airframe 33,459 hrs · 5,058 cycles

RTB DUE TO LT ENG GEN CONTROL OFF LIGHT ON GROUND. REPLACED LT GCU.

Part: ANTENNA — INOPERATIVE (WX RADAR SYS) · airframe 32,985 hrs · 5,005 cycles

CREW REPORTED WEATHER RADAR PROBLEMS UNABLE TO USE WEATHER RADAR MEL. RETURNING TO GATE FOR REPAIRS. WXR ANTENNA DRIVE UNIT REPLACED IAW AMM 34-43-03-000-802. OP CKS OK, MFG P/N 622-5136-202.

Part: CONTROL PANEL — FAILED (WX RADAR) · airframe 32,795 hrs · 4,986 cycles

AFTER T/O WX RADAR FAIL MESSAGE. TRIED RECYCLING C/B FOR WX RADAR AND OTHER PROCEDURES. ALL NO HELP. RETURNED TO ATL. MTC IN PROGRESS TROUBLESHOOTING SYS. REPLACED WX RADAR CONTROL PANEL AND TRANSCEIVER XCVR P/N O 622-5132-633 LRU SYSTEM AND OPS CHECK ALL NORMAL.

Part: ANTI-ICE VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 31,367 hrs · 4,846 cycles

GOT ENG A/I R ON GRND WITH SWITCH TO ON POSITION. RTB, FWD TO MCO/PLAC 30-21-01B. VLV LOCKED IN OPEN POS. CONN REMOVED FROM CONTROLLER AND TIED BACK.

Part: WATER HEATER — OVERHEATED (AFT LAVATORY) · airframe 29,372 hrs · 4,641 cycles

AFT LEFT LAVATORY WATER HEATER OVERHEATED IN FLIGHT. STRONG ODOR, LAVATORY LOCKED OUT. HEATER DISABLED. ODOR PERSISTS. REPLACED LAVATORY WATER HEATER. OPS NORMAL. EXAMINED WIRING. NO FAULTS. AIRED LAVATORY AND ODOR MINIMIZED.

Part: ENGINE — LEAKING (NR 2) · airframe 28,917 hrs · 4,592 cycles

OIL LEAK LP TURBINE DRAIN. REPLACED NR 2 ENGINE IAW TRANS 11T003.

Part: INDICATION SYS — MALFUNCTIONED (STBY ATTITUDE) · airframe 28,052 hrs · 4,497 cycles

STANDBY ATT IND BLANK SAARU STATUS MSG AND ATT FLAG. REPLACED SAARU PER MM.

Part: SKIN — PUNCTURED (BS 157-164 S39R) · airframe 27,435 hrs · 4,425 cycles

THE FUSELAGE SKIN WAS PUNCTURED BY GROUND SUPPORT EQUIPMENT BETWEEN BS 157 AND 164.75 ABOVE S-39R. PUNCTURED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.

Part: APU — FIRE (APU BAY) · airframe 23,996 hrs · 3,990 cycles

APU TAILPIPE FIRE ON PUSHBACK. NO DAMGE TO AIRCRAFT. REPLACED APU.

Part: ENGINE — MAKING METAL (NR 2) · airframe 20,788 hrs · 3,540 cycles

METAL DISCOVERED IN MCD AND SCAVAGE FILTER NR 2 ENGINE. REPLACED ENGINE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 18,913 hrs · 3,260 cycles

REPLACED FLASHLIGHT AT POS 2L FOR LOW BATTERY LIGHT.

Part: OVEN — ODOR (GALLEY) · airframe 15,141 hrs · 2,708 cycles

NR 2 OVEN MID GALLEY HAD ELECTRICAL ODOR. FWD TO MCO IAW MEL 25-20-01H.

Part: SEAT — MALFUNCTIONED (CABIN) · airframe 14,778 hrs · 2,656 cycles

SEAT 44D HEAT BUILD UP ON BOARD MECHANIC (DELTA) DISCONNECTED ELECTRONICS AT SEAT. REACTIVATED SEAT 44D. CHECKED ALL LIGHTS FANS/WATER/HEATERS IN AREA, NO SMOKE OR ODOR NOTICED SEAT 44D. NO EVIDENCE OF SMOKE OR OVERHEAT. DISCONNECTED AND STOWED 44D SEAT CONNECTIONS AND FWD IFES TO MCO/PLAC PRECAUTUONARY. MEL REF 25-25-02JC/BS PULLED/SECURED PER MEL ON P110/210 PANELS.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 14,637 hrs · 2,636 cycles

SEAT 44D EXPOSED SPARKING WIRES LEADING TO INSEAT TV MONITOR FWD TO MCO MEL 25-25-02J ENTIRE IFE INOP. ALSO DISCONNECTED C/P J1 AND J2 AT AVU UNDERSEAT 44D. REPLACED MONITOR HARNESS. CHECKS GOOD.

Part: MONITOR — UNSERVICEABLE (SEAT 30J) · airframe 11,890 hrs · 2,182 cycles

FRC-257-8930J PASSENGER SEAT 30J INSEAT VIDEO MONITOR INOP WONT TURN ON. REPLACED AVU AND LOADED SOFTWARE. CHECKS GOOD BUT VIDEO MONITOR IS INOP AND HAS A STRONG ELECTRICAL SMELL. REMOVED MONITOR. ALL MOUNTING HARWARE STILL PRESENT ON ARM. STOWED ARM AND LOCKED OUT. CONT ON MCO NEEDS MONITOR NIS ATL ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: COMPRESSOR — DAMAGED (NR 2 ENGINE) · airframe 10,741 hrs · 1,989 cycles

BOROSCOPE OF NR 2 ENGINE. FOUND 6TH STAGE HIGH PRESSURE COMPRESSOR DAMAGE BEYOND LIMITS. REPLACED ENGINE

Part: FLEX LINE — LEAKING (RT MLG STEERING) · airframe 10,160 hrs · 1,899 cycles

ATB CTR HYD SYS FAILED-MTC MSG 29-10150 CTR HYD QTY LOW FLEX LINE GOING TO THE RT MLG STEERING ACT LEAKING (P/N AS4568G0580SS)- REPLACED LINE.

Part: PIN — CORRODED (LT & RT MLG) · airframe 7,952 hrs · 1,489 cycles

CORROSION FOUND ON BOTH LT AND RT LANDING GEAR RETRACT ACTUATOR ATTACH PINS. REPLACED BOTH LEFT AND RIGHT HAND ACT PINS IAW M/M WITH NEW ONES.

Part: ODOR — DETECTED (AFT GALLEY) · airframe 6,070 hrs · 1,148 cycles

SULFER/ELECTRICAL SMELL AFT GALLEY TURNED OFF CHILLERS AND OTHER GALLEY ELEC EQUIP AND SMELL DISSIPATED. RAN GALLEY COMPONENTS AFT GALLEY, NO UNUSUAL SMELL NOTED.

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 2,150 hrs · 453 cycles

DURING LAYOVER FOUND 2L DOOR EXTERIOR EMERGENCY ESCAPE LIGHT INOP. RELAMPED 2L DOOR EXTERIOR EMERGENCY ESCAPE LIGHT. CHECKS GOOD.