N588HA

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 56,372 hrs · 10,296 cycles

APU FAULT WHEN ATTEMPTING TO START AFTER LANDING NO START. ACCOMPLISHED BITE OF APU ECU NO MINI FLAGS OK ON LAST TEST END. ACCOMPLISHED FIM 49-11-FAULT TREE 987, ALL OK. ACCOMPLISHED FIM 26-15-00/101 NO FAULTS, STARTED APU AND RAN ALL ELECTRICS AND PACKS. ALL OK ON 1ST START.

Part: START VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 56,268 hrs · 10,271 cycles

ETOPS SIGNIFICANT SYSTEM - #1 ENGINE START VALVE FAILED TO OPEN DURING ENGINE START.// REPLACED #1 ENGINE START VALVE PER AMM 80-11-02,OPS CHECK GOOD. OK TO CONTINUE.

Part: EEC — MALFUNCTIONED (RT ENGINE) · airframe 55,908 hrs · 10,192 cycles

AFTER 3 MINUTES AT CRUISE, 11,000' MSL. RT ENGINE HAD APPROX 5 SURGES WITH ASSOCIATED HPSOV CYCLING, WHEN ADDITIONAL THRUST APPLIED, DUE TO LOSS OF AIRSPEED. RT ENGINE UNABLE TO ACHIEVE MORE THAN 2,600 LBS FUEL FLOW, NO EPR/N1/N2 RESPONSE. AFTER APPROX 30 SECONDS, RT ENGINE OPERATED NORMALLY. ACCOMPLISHED FIM 73-21 FAULT TREE 804. PIMU BITE GAVE "EEC CHB REVERSER RNG FAIL, EEC CHA/B REVR CR-CK FAIL, AND EEC CH-B FAULT CAT2. ACCOMPLISHED FIM 71-01, 71-01 809, 71-01 848, AND 71-01 864. SIM BOX PROC GAVE PROBLEM WITH LVDT. PERFORMED RESISTANCE CHECK FROM T/R LVTD TO EEC WIRING HARNESS. RESISTANCE CHECK GOOD, PER FIM 71-01 864. REMOVED AND REPLACED #2 ENG EEC PER AMM 73-21-04, OPS CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 55,743 hrs · 10,155 cycles

AFTER TAKEOFF, RECEIVED AN EXTREME AIR NOISE FOR ABOUT 20 SECONDS, MUCH MORE THEN JUST PACK HIGH FLOW. AT THE SAME TIME, THE F/A'S REPORTED A ELECTRICAL BURNING ODOR IN FORWARD GALLEY, ODOR WENT AWAY AS SOON AS FLOW STOPPED. IAW FAULT ISOLATION MANUAL, PERFORMED AMM PAGE BLOCK 21-23-07/801 AND INSPECTED ALL DUCTS SURROUNDING THE FORWARD GALLEY CABIN CEILING, CABIN FLOOR AND FOUND NO LEAKS OR ABNORMAL ISSUES. OPERATED PACKS AND FOUND NO ISSUES AT THIS TIME.

Part: ADC — MALFUNCTIONED · airframe 55,340 hrs · 10,073 cycles

AT 1842Z FL360 CAUTION LTS AND EICAS "LE SLATS ASYM" ACCOMPANIED BY FLAP INDICATION GYRATING BETWEEN UP AND 1. F/O A/S INDICATOR INDICATED FLAP OVER SPEED WHILE CA A/S INDICATOR DID NOT. ALL INDICATIONS NORMAL FOR REMAINDER OF FLIGHT. T/S PER FIM 32-09-T803. FOUND BAD PSEU. REMOVED AND REPLACED PSEU PER AMM 32-09-04. PSEU OPS CK GOOD. T/S PER AMM 34-12-00. & FIM 34-12-T822. FOUND BAD "L" ADC. REMOVED AND REPLACED "L" ADC PER AMM 34-12-01. PILOT OVERSPEED WARNING OPS CHK GOOD. OK TO CONTINUE.

Part: A/C PACK — NOISY · airframe 55,282 hrs · 10,059 cycles

ETOPS SIGNIFICANT SYSTEM - ON TAXI IN PACS/RECIRCS GOT SO LOUD- EXCESSIVELY HI FLOW 30 PSI DUCT PRESS. WE COULDN'T COMMUNICATE W/ATC OR EACH OTHER. OPERATED BOTH PACK IAW AMM 21-51-00 WITH ENGINES RUNNING. COULD NOT DUPLICATE. OPS CHECK NORMAL. OK FOR SERVICE.

Part: INDICATOR — FAILED (TCAS) · airframe 103,972 hrs · 18,666 cycles

ELECTRICAL SMOKE FROM FORWARD CENTER CONSOLE IN THE COCKPIT. CIRCUIT BREAKER E-12 TRIPPED. SMOKE SUBSIDED AND CLEARED. REMOVED AND REPLACED TCAS INDICATOR ASSY. OPS CHECKED GOOD IAW MM 36-45-00. OK FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (FUEL SPAR VALVE) · airframe 55,121 hrs · 10,020 cycles

ON STARTING THE NR 2 ENGINE, FUEL SPAR VALVE LIGHT STAYED ON DURING START. START WENT TO 50% N2, THEN STARTED TO SPOOL DOWN, FUEL CONTROL SWITCH TO CUT OUT AT ABOUT 43% N2. PERFORMED AN OPS CHECK OF THE NR 2 ENGINE IAW AMM 71-00-00. OPS CHECKED GOOD. OK FOR SERVICE. PERFORMED BITE TEST OF THE RT PIMU IAW FIM 71-01 TREE 803 AND NO FAULTS FOUND. NO ISSUES ON FUEL SPAR VALVE LIGHT.

Part: ACTUATOR — INOPERATIVE (RUDDER) · airframe 54,918 hrs · 9,975 cycles

RUDDER TRIM WILL NOT MOVE. REMOVED & REPLACED RUDDER TRIM ACTUATOR IAW AMM 27-21-11. OPS & SECURITY CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (GPWS) · airframe 56,163 hrs · 10,331 cycles

ETOPS SIGNIFICANT SYSTEM, TERRAIN INOP ABOVE 5000AGL, PARTIAL DISPLAY BELOW 5000FT AGL. OPS NORMAL BELOW 2000 AGL BOTH DISPLAY. RESET GND PROX CB AND GPWS OPS TEST GOOD PER AMM 34-46-00-00-715-001-003. NO FAULT NOTED. OK FOR SVC.

Part: SWITCH — MALFUNCTIONED (LAV CALL LIGHT) · airframe 54,631 hrs · 9,913 cycles

LAVATORY D EMERGENCY CALL LIGHT DOES NOT TURN OFF. EXERCISED SWITCH. OPS CK OK

Part: INDICATOR — MALFUNCTIONED (FUEL PUMP) · airframe 54,574 hrs · 9,899 cycles

CENTER FUEL PUMP INDICATOR IS BEGINNING TO BUBBLE BUT PRESENTLY READABLE. MAINTENANCE COMPLIED WITH THE FAULT ISOLATION MANUAL 28-41 FAULT TREE 859 FUEL QUANTITY TEST AND ALL DISPLAYS INDICATION NORMAL OK TO CONTINUE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 54,125 hrs · 9,810 cycles

FAINT BURNING OR ELECTRICAL ODOR SMELLED IN COCKPIT INTERMITTENTLY FOR APPROXIMATELY TWO HOURS DURING CRUISE FLIGHT. PERFORM ENGINE RUN PER AMM 71-00-00/201. FOUND NO SMELL OF SMOKE OR FUMES IN COCKPIT AND CABIN PER FIM 21-00 TASK 1-4. OPS CHECKS GOOD ON GROUND. OK FOR SVC

Part: PUMP — MALFUNCTIONED (FUEL BOOST) · airframe 53,526 hrs · 9,704 cycles

DURING LANDING ROLL OUT, LEFT FUEL PUMP EICAS MESSAGE ILLUMINATED WITH PRESSURE LIGHT. REMOVED THE LT AFT BOOST PUMP IAW AMM 28-22-03. REMOVED AND INSTALLED THE BOOST PUMP IAW AMM 28-22-03. OPS CHECKED OK. OK FOR SERVICE.

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 53,500 hrs · 9,699 cycles

ETOPS SIGNIFICANT SYSTEM - L AFT FUEL PUMP EICAS MESSAGE AFTER PUSH RETURN TO GATE. FOUND LT AFT FUEL PUMP BREAKER OUT, RESET AND OPS CK OK, PUMP PRESS OK AND BREAKER STAYED SET OK TO CONT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,844 hrs · 9,576 cycles

EMERGENCY EXIT ROW LIGHT INOP FROM EAT 1A TO 24 A. REMOVED & REPLACED POWER SUPPLY ASSY M1557 & M1558 PER AMM 33-51-07. OPERATIONAL CHECK OK.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 53,953 hrs · 9,880 cycles

ETOPS SIGNIFICANT SYSTEM, AFTER PARKING CHECK, NOTICED STATUS MSG ON EICAS LT ENGINE FIRE LP 1. T/S MSG LT ENGINE FIRE LP 1 REF FIM 26-11, FAULT TREE 804 TO BLOCK 111 MSG CLEARED AND SYS TEST NORMAL.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 53,953 hrs · 9,880 cycles

ETOPS SIGNIFICANT SYSTEM, AFTER PARKING CHECK, NOTICED STATUS MSG ON EICAS LT ENGINE FIRE LP 1. T/S MSG LT ENGINE FIRE LP 1 REF FIM 26-11, FAULT TREE 804 TO BLOCK 111 MSG CLEARED AND SYSTEM TEST NORMAL.

Part: FAN — MALFUNCTIONED (LEFT) · airframe 52,040 hrs · 9,410 cycles

ODOR OF SMOKE THROUGHOUT THE CABIN AND COCKPIT, LT RECIRCULATION FAN ILLUMINATED ON EICAS AFTER ODOR OF SMOKE. ODOR WENT AWAY AFTER RUNNING QRH . R & R LT RECIRC FAN IAW AMM 21-25-01, OPS CHECK OK.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 51,847 hrs · 9,369 cycles

ETOPS SIGNIFICANT SYSTEM, STATUS MESSAGE WEATHER RADAR SYS DISPLAYED. TROUBLESHOOT IAW FIM 34-43, TASK 801. PERFORMED MAINTENANCE MESSAGE ERASE PROCEDURE IAW AMM 31-41-00-912-009. WEATHER RADAR SYS MESSAGE CLEARED. NO ASSOCIATED FAULTS OR MESSAGES. SYSTEM OK FOR SERVICE IAW FIM.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 51,688 hrs · 9,337 cycles

EICAS MESSAGE "TCAS". RESET TCAS C/B, PERFORMED TCAS SYS CK IAW AMM 34-45-00. TCAS SYS TEST OK. EICAS MESSAGE EXTINGUISHED. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (WX SYS) · airframe 51,304 hrs · 9,263 cycles

STATUS MESSAGE WEATHER SYS. PERFORMED WEATHER OPS TEST IAW AMM 34-43-00 TEST OK. ACFT OK FOR SERVICE.

Part: O-RING — FAILED (HYD SYSTEM) · airframe 50,995 hrs · 9,205 cycles

AT 3:10 MIN INTO FLIGHT, C HYD QTY LIGHT ILLUMINATED ON EICAS. CHECKED STATUS PAGE CENTER HYD QTY 0.45RF. SHUTOFF ELEC AND HYD SYS C PUMPS. FOUND O-RING BLOWN ON NR 3 SPOILER PRESSURE LINE UNION. REPLACED O-RING, LEAK CHECK GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (EEC) · airframe 50,974 hrs · 9,201 cycles

STATUS LT ENGINE ELECTRONIC ENGINE CONTROL C1. PERFORM LT ELECTRONIC ENGINE CONTROL MAINT TEST ON GROUND, NO FAULTS NOTED MSG CLEARED.

Part: EEC — MALFUNCTIONED (LT ENGINE) · airframe 50,817 hrs · 9,172 cycles

STATUS MSG LT ENGINE, ELECTRONIC ENGINE CONTROL C1 ILLUMINATED ON DECENT. T/S IAW FIM 73-21 FAULT TREE 828. PIMU REPORTED TCC TRACK FAIL CH A AND CH B. AFTER RESET FOR PIMU IAW FIM 71-01-803, NO MORE MESSAGES PRESENT. NO PREVIOUS HISTORY, OK FOR SERVICE.

Part: STOP — INOPERATIVE (RUDDER TRIM) · airframe 50,790 hrs · 9,166 cycles

RUDDER TRIM STOPS WORKING INTERMITTENTLY. PERFORMED RUDDER TRIM AND RATE TEST IAW AMM 27-21-00. NO FAULTS NOTED, OPS CHECK OK.

Part: TRIM SYSTEM — MALFUNCTIONED (RUDDER) · airframe 50,622 hrs · 9,135 cycles

ON CLIMBOUT, RUDDER TRIM WAS INTERMITTENT, TOOK 2 OR 3 ATTEMPS TO GET INPUT, BOTH LT AND RT AFFECTED. OK TO CONTINUE IAW AMM 27-21-00. PERFORMED OPS TEST OF THE RUDDER AND RUDDER TRIM CONTROL SYSTEM. OPS CK AND TEST PASSED OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 50,281 hrs · 9,074 cycles

AFTER START OF DESCENT WHEN THRUST REDUCED TO IDLE, LT PACK TEMP. LT PACK OFF EICAS MSG DISPLAYED. PERFORMED QRH - STB "N" AND RESET PACK AFTER 5 MIN PACK RESTORED. PERFORMED LT PACK TEMP CONTROLLER BITE TEST, IAW AMM 21-51-14-705-035, NO FAULTS NOTED. RAN PACK .5 HR, OPS CKS NORMAL, OK TO CONTINUE.

Part: WARNING MESSAGE — FALSE ACTIVATION (IRS SYSTEM) · airframe 49,851 hrs · 8,996 cycles

AFTER LANDING RT IRS FAULT EICAS MESSAGE ILLUMINATED WITH RT FAULT LIGHT. RESET IRS OPS, TEST IAW AMM 34-21-00-715-038, NO FAULTS NOTED. PERFORMED MCDP TEST 30, TEST PASS, OK FOR CONTINUED SERVICE.

Part: PNEUMATIC SYSTEM — MALFUNCTIONED · airframe 49,856 hrs · 8,997 cycles

LT & RT DUCT PRESSURE DROPS TO 0 PSI MOMENTARILY THEN RETURNS TO 25 PSI. OPS CHECKED BLEED AIR SYS FOR APU, CKD GOOD. NO DEFECTS NOTED, OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 1 FIRE DETECT) · airframe 49,753 hrs · 8,976 cycles

EICAS MESSAGE FOR RT ENGINE LOOP 1. TROUBLESHOT IAW FIM 26-11-804, FIG 104, CLEANED LOOPS AND CONNECTORS. RT ENGINE SWAPPED ENGINE FIRE LOOP CARDS 1 AND 2. FIRE TEST GOOD. OK FOR SERVICE

Part: UNKNOWN — VIBRATION (FUSELAGE) · airframe 49,409 hrs · 8,913 cycles

UNUSUAL VIBRATION & NOISE UNDER MID GALLEY DECREASED WHEN FLAPS EXTENDED. ACFT WAS CLEAN CONFIGURATION WHEN VIB STARTED. INSPECTED ACFT IAW AMM 05-51-38, NO DEFECTS NOTED ALSO INSPECTED AIR CONDITION BATTERY, NO DEFECTS NOTED AND INSPECTED FWD CARGO RECIRCULATION FAN AND DUCTING NO DEFECTS NOTED, NO DEFECTS FOUND FROM MID GALLEY CHILLER OVEN. OK FOR SERVICE.

Part: ECU — MALFUNCTIONED (APU) · airframe 49,160 hrs · 8,865 cycles

APU "FAULT" LIGHT ON START. APU START FAILED. REPLACED APU ECU IAW AMM 49-61-05-404-008. GROUND CHECK OK. OK FOR SERVICE.

Part: IDG — FAILED (LEFT) · airframe 48,903 hrs · 8,808 cycles

AFTER ENGINE START, LT GENERATOR OFF LIGHT REMAINED ON. REMOVED AND INSTALLED THE LEFT IDG IAW 767-3-405001. OPS AND LEAK CHECKED GOOD.

Part: CONTROLLER — UNKNOWN (LT GENERATOR) · airframe 47,850 hrs · 8,778 cycles

LT GENERATOR OFF LIGHT ON TAXI OUT. OPENED LT ENGINE, CLEANED CONNECTIONS LT IDG. REPLACED IDG CONTROLLER. RAN LT ENGINE IDG, OPS NORMAL.

Part: PACKING — FAILED (HYD SYSTEM) · airframe 48,028 hrs · 8,625 cycles

ATB - LT HYD QTY .46, LANDED WITH .40. R & R PACKING FOR RUDDER HYD MANIFOLD, OPS CHECK, LEAK CHECK GOOD. OK FOR SERVICE, ACCOMPLISHED HYD SERVICING AMM12-12-01, OK FOR SERVICE.

Part: ACTUATOR — ACTIVATED (RT OVRWNG SLIDE) · airframe 47,914 hrs · 8,603 cycles

WHILE ARMING THE SLIDE SYSTEM BLEW RT OVERWING SLIDE ACTUATORS, SLIDE NOT DEPLOYED. R & R RT SPOILER OVERRIDE ACTUATOR SQUIB, R & R BOTH SLIDE COMPARTMENT DOOR OPEN ACTUATOR SQUIBS, R & R SLIDE COMPARTMENT DOOR LATCH OPENING ACTUATOR IAW AMM 25-65-09, 25-65-10, 25-65-19, AND 25-65-04.

Part: INTERCOSTAL — CRACKED (BS 1197) · airframe 47,845 hrs · 8,588 cycles

AT STA 1197+22 TO 1197+44 AT RBL 39.5, WATER LINE 200 INTERCOSTAL UPPER FLANGE HAS SEVERAL CRACKS. R & R INTERCOSTAL UPPER FLANGE AT STA 1197+22 TO 1197+44, RBL 39.9 IAW SRM 51-40-02-0G-0.

Part: INTERCOSTAL — CRACKED (BS 1241-1263) · airframe 47,845 hrs · 8,589 cycles

AT STA 1241 TO STA 1263, LBL 39.5, WATERLINE 200 INTERCOSTAL UPPER FLANGE CRACKED. R & R INTERCOSTAL FLANGE AT STA 1240 TO STA 1263, LBL 39.5, WATERLINE 200 IAW SRM 51-40-02-OG-O.

Part: INTERCOSTAL — CRACKED (BS 1087-1109) · airframe 47,845 hrs · 8,588 cycles

AT STA 1087 TO 1109 AT RBL 39.5, WATER LINE 200 INTERCOSTAL UPPER FLANGE HAS SEVERAL CRACKS. R & R INTERCOSTAL UPPER FLANGE AT STA 1087 TO 1109, IAW SRM 51-40-02-0G-O.

Part: GCU — MALFUNCTIONED (APU) · airframe 47,632 hrs · 8,549 cycles

FOUND RT ENGINE FIELD LIGHT ON. TROUBLESHOT DOWN TO GCU BY SWAPPING APU GCU AND NR 2 GCU LIGHT FOLLOWED TO APU AND NR 2 REMAINED OFF. REPLACED NR 2 ENG GCU IAW AMM 24-22-02/401. OPS CHECKED OK.

Part: O-RING — FAILED (HYD SYSTEM) · airframe 46,839 hrs · 8,400 cycles

CENTER HYD SYS QUANTITY DECREASED FROM 1.04 PRIOR TO DEPARTURE TO .66 IN CRUISE, RF DISPLAYED. QUANTITY CONTINUED TO DECREASE TO .46. R & R NR 10 SPOILER PCA FILTER O-RING IAW AMM 27-61-02. SERVICED CTR HYD SYS IAW AMM 12-12-01. OPS AND LEAK CHECKS OK.

Part: VALVE — MALFUNCTIONED (CABIN TEMP)

COULD NOT CONTROL CABIN TEMP IN ANY MODE AT FL 370. R & R LOW LIMIT VALVE ON THE LT PACK IAW AMM 21-51-11. LT PACK OUTLET TEMP WAS AT 60* ON ARRIVAL, AND FOUND LOW LIMIT VALVE OPEN.

Part: WARNING LIGHT — FALSE INDICATION (CONFIGURATION) · airframe 45,395 hrs · 8,129 cycles

LOW SPEED ABORT FOR CONFIGURATION RED INDICATION, EICAS INDICATES STABLIZER. SPEED LESS THAN 60 KTS. PERFORMED MCDP TEST 08, NO FAULTS NOTED, FIM 31-51 FAULT TREE 807, NO FAULTS NOTED.

Part: INDICATOR — MALFUNCTIONED (STAB TRIM) · airframe 45,395 hrs · 8,129 cycles

LOW SPEED ABORT FOR CONFIGURATION RED INDICATOR EICAS INDICATIES STABALIZER, SPEED LESS THAN 60 KTS. R & R STAB TRIM POSITION INDICATOR IAW AMM 27-48-01-024-001 & 27-48-01-434-053. PERFORMED MCDDP GROUND TEST 65 & 66. SYS OPS NORMAL. CONFIG TAKEOFF SYS TEST NORMAL IAW AMM 27-48-00-735-053. NO HIGH SPEED ABORT NO RTO CK REQUIRED.

Part: ACTUATOR — INOPERATIVE (OVERWING SLIDE) · airframe 44,889 hrs · 8,049 cycles

OVERWING SLIDE INOPERATIVE. FOUND RT FWD DOOR OPENING ACTUATOR BLOWN. R & R RT FWD DOOR OPENING ACTUATOR IAW AMM 25-65-10-004-001-001 AND AMM 25-65-10-404-016-001, TEST OK.

Part: PUMP — MALFUNCTIONED (FUEL BOOST) · airframe 44,424 hrs · 7,980 cycles

LEFT FWD FUEL PUMP EICAS MESSAGE AT TOP OF CLIMB. REPLACED LT FWD FUEL BOOST PUMP IAW AMM 28-22-03. OPS AND LEAK CHECKED GOOD.

Part: SENSOR — MALFUNCTIONED (OUTLET TEMP) · airframe 44,001 hrs · 7,923 cycles

LEFT PACK TEMP, LT PACK OFF ILLUMINATED, COOLED FIVE MINUTES THEN RESET. LEFT PACK TEMP, TEMP OFF ILLUMINATED AGAIN. R & R LT PACK COMPRESSOR OUTLET SENSOR IAW AMM 21-51-06. OPS CHECKED GOOD, OK FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (RAT) · airframe 43,904 hrs · 7,909 cycles

RAM AIR TURBINE "UNLOCK" LIGHT ON IN OVERHEAD PANEL RAT UNLOCKED CAS MESSAGE. PERFORMED TEST IAW FIM REF 29-21, FAULT TREE 808, TEST PASSED, OPS CHECKED GOOD.

Part: CONTROLLER — MALFUNCTIONED (HIGH PRESSURE) · airframe 43,447 hrs · 7,841 cycles

RIGHT ENGINE AT 77.0 N1, 101 EPR, IS CYCLING. AP BLEED, AT FLT IDLE, ITS NORMAL. SWING 20-40 ON INDICATOR. R & R HIGH PRESSURE CONTROLLER IAW AMM 36-11-08. OPS CHECK GOOD LEAK CHECK GOOD. ACCOMPLISHED AMM 36-0001.

Part: GCU — MALFUNCTIONED (RT GENERATOR) · airframe 42,978 hrs · 7,772 cycles

AFTER ENGINE START, RIGHT GENERATOR CONTROL TRIPPED OFF, ONE RESET DID NOT GET GENERATOR BACK ONLINE. REPLACED NR 2 ENG GENERATOR CONTROL UNIT IAW AMM 24-22-02 HISTORY: 0 EVENTS LAST 30 DAYS.

Part: IDG — FAILED (NR 2) · airframe 42,978 hrs · 7,772 cycles

AFTER ENGINE START RT GENERATOR CONTROL TRIPPED OFF, ONE RESET DID NOT GET GEN BACK ON LINE. REPLACED NR 2 GENERATOR CONTROL UNIT IAW AMM 24-22-02. CONDITION SAME. R & R 2 IDG IAW AMM 24-11-01. OPS CHECK OK.

Part: FILTER — FAILED (HYD SYSTEM) · airframe 41,084 hrs · 7,464 cycles

ON CLIMBOUT, LT HYD QTY EICAS MESSAGE DISPLAYED. STATUS PAGE SHOWED ZERO QTY. RAN QRH PROCEDURE AND RETURNED TO DEPARTURE. FOUND DPI FOR PRESSURE FILTER ON EDP (L) MODULE BLOWN. REPLACED DPI IAW AMM 29-11-17. REPLACED CASE DRAIN AND PRESSURE FILTERS ON EDP (L) MODULE IAW AMM 29-11-17. REPLACED CASE DAIN AND PRESSURE FILTERS ON ACMP MODULE IAW AMM 29-11-18. REPLACED RETURN FILTER ON RETURN FILTER MODULE IAW AMM 29-11-15. NO DEBRIS FOUND ON FILTERS. LEAK CHECK PENDING. SERVICE OF HYD FLUID PENDING. SERVICE AND LEAK CHECK OF LT HYD SYS. LEAK AND OPS CHECK GOOD. OK FOR SERVICE IAW AMM 29-11-17.

Part: WINDOW — FAILED (COCKPIT) · airframe 40,161 hrs · 7,325 cycles

RT FWD WINDOW ARCED IN UPPER LT CORNER AND BEGAN TO GLOW. TURNED OFF WINDOW HEAT. THE OUTER PANEL SHATTERED. RETURNED TO BASE, R & R RT FWD WINDOW IAW MM 56-11, PERFORMED INITIAL TORQUE, AND SECOND TORQUE IAW AMM 56-11 IAW AMM 56-11. DUE TO RT FWD WINDOW ARCHING AND SHATTERING. WINDOW HEAT CONTROLLER REPLACEMENT IS NECESSARY. R & R RT FWD WINDOW HEAT CONTROLLER UNIT IAW AMM 30-41-01, CHECKED GOOD.

Part: ATTACH FITTING — CORRODED (BS 911) · airframe 38,434 hrs · 7,051 cycles

CORROSION ON FLOOR ATTACH FITTINGS AND SEAT TRACK SECTIONS GALLEY/CABIN DIVIDER STA 911. SEAT TRACK SECTIONS REPLACED IAW SRM 51-40-02 REV 90 ATTACH FITTINGS REPLACED.

Part: HEAT SHIELD — CORRODED (NR 1 NACELLE) · airframe 38,434 hrs · 7,051 cycles

NR 1 ENGINE AFT FAIRING LOWER EXHAUST HEAT SHIELD CORROSION ON SPLICE PLATE. FABRICATED REPLACEMENT STRAP IAW 313T3380 AND INSTALLED IAW SRM 1-40-02, REV 90. REPLACED SOLID EXISTING FASTENERS AT 6 LOCATIONS WITH BLIND FASTENERS IAW AIR NZ TI 1901-54328-0001.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,216 hrs · 6,696 cycles

FOUND EXTERIOR EMERGENCY LIGHT AFT R1 DOOR INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51-07. OPS CHECKED GOOD.

Part: SYMBOL GENERATOR — FAILED · airframe 36,085 hrs · 6,673 cycles

CAPTAIN`S ADI AND HSI WENT BLANK WITH SG FAIL MESSAGE DISPLAYED IN BOTH INDICATORS. CYCLED "ALTN EFI" OPS RETURNED TO NORMAL/GOOD. R & R NR 1 SYMBOL GENERATOR, GROUND CHECKED OK IAW AMM 34-22-01, GROUND TEST 30 PASSED. ACFT REMAINS IN LAND 3 STATUS.

Part: CHARGER — FAILED (APU BATTERY) · airframe 35,853 hrs · 6,625 cycles

ETOPS SIGNIFICANT SYS - EICAS MESSAGE FOR APU BATTERY CHARGER DISPLAYED. R & R APU BATTERY CHARGER IAW AMM 24-31-05. EICAS MESSAGE EXTINGUISHED, SYS CHECKED OK.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 35,626 hrs · 6,584 cycles

ETOPS SIGNIFICANT SYS - SPEED LIM DISPLAYED ON F/O PFD. SELECTED BOTH ALTERNATE EFI AND ALTERNATE AIR DATA SWITCHES. SPEED LIM REMAINED. PERFORMED TROUBLESHOOTING IAW FIMS 27-32-00, FIG 103 AND 32-09-03, FIG 103. RESET SYS. ALL CHECKED ARE GOOD.

Part: CIRCUIT CARD — FAILED (STALL WARNING) · airframe 35,635 hrs · 6,585 cycles

ETOPS SIGNIFICANT SYS - WARN ELEX DISPLAYED ON STATUS PAGE. REPLACED RT STALL WARNING CARD. OPS CHECK OK IAW MM 27-32-01.

Part: CIRCUIT CARD — FAILED (STALL WARNING) · airframe 35,540 hrs · 6,572 cycles

ETOPS SIGNIFICANT SYS - WARNING ELEX EICAS MESSAGE. FIM 27-32-00/101 STALL WARN MODULE BITE TEST. R & R RT STALL WARNING CARD IAW AMM 27-32-01. OPS CK IAW AMM 27-32-00. OPS CHECK GOOD.

Part: OIL SYSTEM — LOW (NR 1 IDG) · airframe 35,504 hrs · 6,566 cycles

ETOPS SIGNIFICANT SYS - TOP OF DESCENT, LT GENERATOR DRIVE LIGHT FLICKERED WITH MOMENTARILY EICAS MESSAGE LT GENERATOR DRIVE. ON ACFT OVERNIGHT CHECK AFTER ARRIVAL, FOUND NR 1 ENGINE IDG OIL LEVEL TO BE LOW. SERVICED IDG GROUND IDLE ENGINE RUN CK GOOD. NO GENERATOR DRIVE LIGHT INDICATOR, OK FOR SVC.

Part: RADAR — WARNING LIGHT (WX SYSTEM) · airframe 35,504 hrs · 6,566 cycles

ETOPS SIGNIFICANT SYS - EICAS "WXR SYS" MESSAGE ON STATUS PAGE. PERFORMED BITE TEST ON TRANSCEIVER, PERFORMED OPS CHECK IAW AMM 34-43-00, CHECKED GOOD.

Part: WARNING LIGHT — FALSE INDICATION (WX RADAR SYS) · airframe 35,467 hrs · 6,560 cycles

ETOPS SIGNIFICANT SYS - WX RADAR SYS EICAS STATUS MESSAGE DISPLAYED. ACCOMPLISHED FIM 34-43-00 NO FAULTS NOTED, SYS OPS CHECKED GOOD AT GATE. EICAS MESSAGE WXR RADAR SYS EXINGUISHED, OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (WX RADAR SYS) · airframe 35,467 hrs · 6,560 cycles

ETOPS SIGNIFICANT SYSTEM - WX RADAR SYS EICAS STATUS MESSAGE DISPLAYED. ACCOMPLISHED FIM 34-43-00 NO FAULTS NOTED. SYSTEMS OPS CK GOOD AT GATE, EICAS MSG WXR RADAR SYS EXINGUISHED. OK FOR SERVICE.

Part: EEC — NONE (RT ENGINE) · airframe 35,276 hrs · 6,532 cycles

ETOPS SIGNIFICANT SYS - MX LEVEL EICAS MESSAGE RT ENGINE EEC C2 DISPLAYED. PERFORMED FIM 73-21-00, FIG 116 NO FAULTS NOTED IAW MEL 73-21-10, NOTE 2 RT ENGINE EEC C2 FAULTS ARE ALLOWED BY ENGINE TYPE CERTIFICATE, MEL DISPATCHED NOT NECESSARY OK FOR SERVICE.

Part: COMPUTER — MALFUNCTIONED (LT EICAS) · airframe 35,276 hrs · 6,532 cycles

ETOPS SIGNIFICANT SYS - MX LEVEL EICAS MESSAGE, EICAS BITE DISPLAYED NUMEROUS DATA FIELDS BLANK WITH LT EICAS SELECTED. OPS NORMAL ON RT EICAS COMPUTER.

Part: COMPUTER — FAULTED (LT EICAS) · airframe 35,276 hrs · 6,532 cycles

ETOPS SIGNIFICANT SYS - MX LEVEL EICAS MESSAGE BITE DISPLAYED NUMEROUS DATA FIELDS BLANK WITH LT EICAS SELECTED, OPS NORMAL ON RT EICAS COMPUTER. RERACKED LT ECIAS COMPUTER OPS CK OK IAW MM31-41-02.

Part: BLADE — DAMAGED (NR 2 ENGINE FAN) · airframe 35,239 hrs · 6,526 cycles

ETOPS SIGNIFICANT SYS - NR 2 ENGINE NR 1 FAN BLADE HAS SMALL NICK. BLENDED IAW AMM 72-31-02, NR2 ENG FAN BLADE NR1, PERFORMED EDDY CURRENT INSP, NO CRACK INDICATIONS NOTED. BLENDED IAW AMM 72-31-02, NR 2 ENG FAN BLADE NR 1, PERFORMED EDDY CURRENT INSP, NO CRACK INDICATIONS NOTED.

Part: BLADE — DAMAGED (NR 2 ENGINE FAN) · airframe 35,239 hrs · 6,526 cycles

ETOPS SIGNIFICANT SYS - NR 2 ENG NR 27 FAN BLADE HAS SMALL NICK. BLENDED FAN BLADE NR27 ON NR2 ENG IAW AMM 72-31-02, PERFORMED EDDY CURRENT INSP, NO CRACK INDICATIONS NOTED.

Part: COMPUTER — MALFUNCTIONED (EICAS) · airframe 34,771 hrs · 6,448 cycles

ETOPS SIGNIFICANT SYS - MX LEVEL EICAS MSG 'EICAS BITE' DISPLAYED. NUMEROUS DATA FIELDS BLANK W/EICAS IN AUTO. RT EICAS COMPUTER OPS NORMAL. INFO NOTED LT EICAS COMPUTER GROUND CHECKED OK IAW AMM 31-41-02, ACFT OK FOR SERVICE.

Part: MMR — INOPERATIVE · airframe 34,577 hrs · 6,421 cycles

ETOPS SIGNIFICANT SYS - ECIAS MSG APPEARED ON POS REF PAGE W/FMS IN IRS MODE RNP/ACTUAL NRS KEEP RUNNING UP TO 4.00 (NM). REPLACED NR1 MMR IAW AMM 34-31-01. OPS CHECKED OK IAW AMM34-21-00.

Part: RELAY — MALFUNCTIONED (PROBE HEAT) · airframe 34,458 hrs · 6,400 cycles

ETOPS SIGNIFICANT SYS - PROBE HEAT EICAS MESSAGE ILLUMINATED MOMENTARILY AFTER TAKEOFF. REMAINDER OF FLIGHT WAS NORMAL. REPLACED RELAYS K518 & K552. PROBE HEAT OPS CHECKED OK IAW AMM 30-31-00 AND 30-33-00.

Part: WARNING LIGHT — FALSE INDICATION (PITOT HEAT) · airframe 34,458 hrs · 6,400 cycles

ETOPS SIGNIFICANT SYS - ATB - EICAS MESSAGE "PROBE HEAT", LT AUX PITOT, F/O PITOT, TAT, LT EEC ALT LIGHTS ILLUMINATED. UNABLE TO DUPLICATE FAULTS ON GROUND. REPLACED RELAYS K514, K522,K528, K643, AND K645. OPS CHECK OF THE PITOT STATIC PROBE HEAT SYS AND TAT PROBE HEAT SYS, OPS CHECKED OK IAW AMM 30-31-00 AND 30-33-00.

Part: WARNING LIGHT — ILLUMINATED (PITOT HEAT) · airframe 34,134 hrs · 6,344 cycles

ETOPS SIGNIFICANT SYS - INFLT EICAS 'PROBE HEAT' MESSAGE ON; " LT AUX; FO PITOT;TAT;" LIGHTS ON OVERHEAD ADVISORY PANEL NO DIFFERENCES NOTED AND LATER RETURNED TO OPS NORMAL.

Part: TURBINE BLADES — DAMAGED (ENGINE) · airframe 33,487 hrs · 6,234 cycles

ETOPS SIGNIFICANT SYS - FOUND DURING BORO CARD 72-410-C1-2 2 HPT BLADES ON STAGE 2HPT DAMAGED IN AREA B L/E OUT OF LIMITS IAW TABLE 605, PG 65. ENG CHANGE REQUIRED. REMOVED NR 2 ENG IAW HAL M274-767 & INSTALLED NEW NR ENG IAW HAL M275-767.

Part: ENGINE — POWER LOSS (NR 2) · airframe 33,401 hrs · 6,219 cycles

NR 2 ENG RIGHT EPR CONSTANT FLUCTUATIONS IN CRUISE (1.28 TO 1.30 ) FUEL FLOW STABLE N1 > 85.7 TO 85.8 VIB NR 1 ENG > .9 NR 2 ENG 1.1 FL 390 N2 87 % STABLE. PERFORMED FIM 77 11 00 NO PIMU FAULTS CHECKED PT2 AND P5 SENSE LINES FOR LEAKS FOUND OK BLEW OUT PT2 AND P5 LINES REQUIRES RUN PERFORMED ENGINE RUN UP PER 71-00-00 /501 ALL EPR INDICATIONS NORMAL AND STEADY.

Part: DISPLAY — INTERMITTENT (COCKPIT) · airframe 33,160 hrs · 6,179 cycles

ETOPS SIGNIFICANT SYS - F/O ADI DISPLAY INTERMITTENT. R & R F/O'S EADI GROUND CHECKED OK IAW AMM 34-22-03 TESTED PASSED ACFT REMAINS IN LAND 3 STATUS.

Part: CONTROLLER — FAILED (DUCT PRESSURE) · airframe 33,020 hrs · 6,155 cycles

ETOPS SIGNIFICANT SYS - LEFT DUCT PRESSURE FLUCTUATES WITH ENGINE RUNNING AND BLEED AIR SWITCH ON. OPERATES NORMALLY IN CRUISE. WHEN POWER COMES BACK DURING DESCENT, RT PRESSURE STICKS AND LT FLUCTUATES. PRONOUNCED AIR SURGE SOUND THRU ACFT PACKS. REPLACED PRV CONTROLLER IAW MM 36-11-19. REPLACED PRSOV IAW MM 36-11-09.

Part: VALVE — MALFUNCTIONED (PNEUMATIC SYS) · airframe 33,020 hrs · 6,155 cycles

ETOPS SIGNIFICANT SYS, PNEUMATIC FLUCTUATIONS DURING CLIMB AND APPROACH MODES. RT BLEED SEEMS TO STICK AT 40 PSI UNTIL LEFT BLEED MODULATION COULD UNSTICK IT. BOTH PRSOV EXERCISED AND VISUALLY INSP AND EXERCISED PRSOV ALSO FUNCTION CHECKED OK. AS PER 36-11-00 AND ALSO HIGH POWER ENGINE RUN DUCT PRESSURE CHECKED NORMAL AND NO FOUND FLUCTUATE RT. PRESS ENG RUN BY FLT CREW. AMM 71-00-00 WITH BOTH ENG.

Part: PNEUMATIC SYSTEM — FLUCTUATES · airframe 33,007 hrs · 6,153 cycles

ETOPS SIGNIFICANT SYS - ON CLIMBOUT AND INITIAL DESCENT, LT PNUEMATIC DUCT PRESSURE FLUCUATED 10-15 PSI. CHECKED AND CLEANED FILTERS ON PRC REGULATOR AND FAN AIR CONTROL VALVE AND PRSOV IAW AMM 36-11-19-404-034 AND AMM 36-11-09-422-163, AMM 36-11-17. PERFORMED ENGINE RUN IAW AMM 71-00-00 DUCT PRESS STEADY 32 PSI IDLE, 38 PSI AT POWER COULD NOT DUPLICATE ON GROUND.

Part: MODULE — MALFUNCTIONED (AUTOPILOT) · airframe 32,596 hrs · 6,088 cycles

ETOPS SIGNIFICANT SYS - ATB - AT FL 370 A/P ON - ACFT DOVE 100' AND YAWED RT. OCCURRED 3 TIMES. DISENGAGED A/P - NORMAL OPERATION ON RETURN. BIT CHECK ALL SCM. FOUND FAULT ON 3 RT SCM BOX. SCM FAULT APL 767 SHELF. NO OTHER FAULTS ON THE REST OF BOXES. R & R SCM 3R IAW AMM27-09-00. OPS CHECK GOOD. OK FOR SERVICE.

Part: BLADE — NICKED (NR 1 ENGINE) · airframe 32,215 hrs · 6,026 cycles

UNDRESS NICK NOTED ON NR 1 ENGINE FAN BLADE. FOUND NR 1 ENGINE FOD ON NR 28 BLADE,REMOVED AND REPLACED BLADE 9 AND 28 PER AMM 72-31-404-021-400. ACCOMPLISHED VIBRATION CHECK PER AMM 71-00-00, OPS CHECK OK. OK FOR SERVICE.

Part: ALTIMETER — MALFUNCTIONED (1ST OFFICER) · airframe 31,518 hrs · 5,903 cycles

ETOPS SIGNIFICANT SYS - F/O ALTIMETER OFF FLAG IN VIEW AFTER TOP OF CLIMB, SELECTING F/O AIR DATA SWITCH TO ALTN CORRECTED FAULT. INTERMITTENT FAULT. ACCOMPLISHED OPS TEST OF THE RT AIR DATA SYS IAW AMM 34-12-00, NO DEFECT FOUND OPS CHECK OK. ACCOMPLISHED MCDP TEST 40 IAW AMM 22-00-02, ALL TEST 40 PASS. LMP REMAINS IN LAND 3.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 31,383 hrs · 5,878 cycles

ETOPS SIGNIFICANT SYSTEM - ON TOUCHDOWN IRS L 3.6 NM; ILS C 3.2 NM; ILS R 0.7 NM EXCESS OF 2.0 NM NORMAL LIMIT. WITH IN LIMITS REF FIM 34-21-00 FIG 107B OK FOR SERVICE.

Part: ALTIMETER — MALFUNCTIONED (COCKPIT) · airframe 31,362 hrs · 5,874 cycles

ETOPS SIGNIFICANT SYSTEM - FLAG ON F/O'S ALTIMETER. RESET F/O'S ALTIMETER C/B OPS CHECK GOOD PER AMM 34-13-01, NO FAULTS NOTED NO FLAG IN VIEW, OK FOR SERVICE.

Part: SHUTOFF VALVE — FAILED (A/C PACK) · airframe 31,291 hrs · 5,861 cycles

ETOPS SIGNIFICANT SYS - ATO - RT PACK OFF WITH RT ENG BLEED ON ICAS WHEN PWR ADVANCE FOR TAKE-OFF AT 80 KTS. ACCOMP FIM 36-10-00. REPLACED RT BLD AIR CTL CARD (M860). GRND OPS CK PEND. REPLACED RT PACK FLOW CNTL & SHUTOFF VLV IAW AMM 21-51-01. HIGH PWR RAN ENG. OPS CK GOOD. NO FAULTS NOTED OK FOR SVC.

Part: GENERATOR — CRACKED (APU) · airframe 31,263 hrs · 5,856 cycles

ETOPS SIGNIFICANT SYS - DURING OVERNIGHT CK NOTICED EVIDENCE OF OIL LEAK AT APU. RAN APU. FOUND OIL SPURTING FROM CRACK ON GENERATOR HOUSING. REPLACED APU GENERATOR IAW AMM 24-21-01. OPS NML. LEAK CK GOOD.

Part: STRUCTURE — DENTED (RT MLG DOOR) · airframe 31,241 hrs · 5,852 cycles

OPEN - DURING OVERNIGHT CHECK FOUND RT MLG TRUNNION DOOR DENTED LOWER EDGE (DOOR REMOVED). OK TO CONTINUE IAW L CDL32-12-1.

Part: CONTROL VALVE — MALFUNCTIONED (A/C PACK) · airframe 31,204 hrs · 5,846 cycles

ETOPS SIGNIFICANT SYS - BOTH PNEUMATIC PRESS DROPS EXCESSIVE WHEN LT & RT PACK SWITCHES ARE TURNED OFF USING BOTH APU OR ENG BLEED AIR (BLEED AIR DOES NOT RETURN TO NORMAL) REPLACED LT FLOW CONTROL VALVE IAW AMM21-51-01 TILL STEP 4A. OPS CK IAW AMM21-51-01 OK.

Part: A/C PACK — MALFUNCTIONED · airframe 31,204 hrs · 5,846 cycles

ETOPS SIGNIFICANT SYS - BOTH LT & RT PACK SWITCHES HAD TO BE TURNED OFF THEN BACK ON MORE THAN ONCE TO GET THE PACK OFF LIGHTS TO EXTINGUISH (EICAS MESSAGE WAS THE SAME THEY FOLLOWED THE PACK OFF LIGHTS. ACCOMPLISHED BITE LT & RT PACK TEMP CONTROLLER & AIR SUPPLY MODULE IAW AMM21-51-00 NO FAULTS NOTED OK TO CONTINUE SERVICE.

Part: CONNECTOR — DIRTY (ALTIMETER) · airframe 31,057 hrs · 5,821 cycles

ETOPS SIGNIFICANT SYS - F/O ALTIMETER SHOWED FLAG IN CRUISE FLT AT FL 360 SELECTED ALT AIR DATA FLAG WENT AWAY- RESELECTED NORMAL ON F/O AIR DATA SWITCH - NO FLAGS - F/O ALTIMETER OPS NORMAL FOR REST OF FLT. CLEANED CONNECTOR PLUG ON F/O ALTIMETER - REMOVED AND REINSTALLED F/O'S ALTIMETER IAW AMM 34-13-01 AND PERFORMED ALTIMETER TEST 34-13-01-864-020 ALL CHECKED GOOD -OK TO CONTINUE SERVICE.

Part: INDICATOR — INTERMITTENT (AIRSPEED) · airframe 30,696 hrs · 5,757 cycles

ETOPS SIGNIFICANT SYS - F/O MACH AIRSPEED INDICATOR INOP (INTERMITTENT). REPLACED F/O MACH A/S IND OPS CK OK IAW MM 34-13-02.

Part: ADI — MALFUNCTIONED (COCKPIT) · airframe 30,270 hrs · 5,685 cycles

ETOPS SIGNIFICANT SYS - CAPTS ADI & HSI WENT BLANK WITH SG FAIL MESSAGE DISPLAYED IN BOTH INDICATORS, SELECTING ALT EFI CORRECTED FAULT. AFTER A COUPLE OF MIN RESELECTED CAPTS EFI AND DISPLAY WAS NORMAL. PERFORMED EFIS SYMBOL GEN TEST IAW 34-22-01-864-015 PERFORMED EFIS BITE PROCEDURE IAW FIM 34-22-00/101 FIG 108 SHEET 1 ALL CHECKS ARE GOOD SYS OPERATES NORMAL.

Part: RADIO ALTIMETER — FAILED (CENTER) · airframe 29,682 hrs · 5,581 cycles

ETOPS SIGNIFICANT SYS - ON APPROACH 'NO LAND3' DISPLAYED ON ASA. CENTER RADIO. ALTIMETER FAIL. FLAG INTERMITTENTLY DISPLAYED. PERFORMED BITE TEST OF R/A LT,ST,RT. ALL CK NORMAL. C/W TEST 30. NO LAST FLT FAULTS. TEST PASS ACFT REMAINS LAND 3.

Part: SWITCH — MALFUNCTIONED (LT A/C PACK) · airframe 29,623 hrs · 5,570 cycles

ETOPS SIGNIFICANT SYS - AFTER LANDING LT PACK OFF ILLUMINATE RESET OPS OK. BITE CK LT PACK COMPENSATOR CONTROLLER NO FAULTS NOTED. BITE CK LT PACK STANDBY CONTROLLER NO FAULT NOTED. R & R LT PACK OVERHEAT SWITCH IAW AMM21-51-18. OPS CK GOOD NO FAULTS NOTED.

Part: CONTROL VALVE — INOPERATIVE (A/C PACK TEMP) · airframe 29,617 hrs · 5,569 cycles

ETOPS SIGNIFICANT SYS - LT PACK OFF LIGHT ILLUM EICAS MESSAGE LT PACK OFF DISPLAYED. LIGHT DID NOT EXTINGUISH WHEN STBY SELECTED AND RESET PUSHED. REPLACED TEMP CONTROL VALVE IAW MM 21-51-12. TEST OK, NO DEFECTS.

Part: WARNING LIGHT — ILLUMINATED (LT A/C PACK) · airframe 29,559 hrs · 5,558 cycles

ETOPS SIGNIFICANT SYS - LT PACK OFF LIGHT ILLUM. EICAS MESSAGE L PACK OFF DISPLAYED. LIGHT DID NOT EXTINGUISH WHEN STBY SELECTED AND RESET PUSHED. PERFORMED LT PACK BITE CHECK IAW FIM 21-51000/101, FIG 103. NO FAULT SHOW. CYCLED PACK LT, SEVERAL TIMES. LT PACK WORKED NORMAL. LIGHT EXTINGUISHED. EICAS MSG DID NOT REAPPEAR.

Part: PNEUMATIC SYSTEM — MALFUNCTIONED (APU) · airframe 29,328 hrs · 5,514 cycles

ETOPS SIGNIFICANT SYS - AFTER LANDING UNABLE TO GET PNUEMATIC AIR FROM APU. PROVIDED GROUND AIR & GROUND POWER. POWERED DOWN ACFT. SHUTDOWN APU & RESTARTED APU. TURNED ON ELECTRICAL & PNUEMATIC SYSTEMS IAW AMM 49-11-00-802-002. STANDARD PROCEDURES ALL APU ELECTRICAL & PNUEMATIC FUNCTIONS CKD OK.

Part: ECU — MALFUNCTIONED (APU) · airframe 28,963 hrs · 5,451 cycles

ETOPS SIGNIFICANT SYSTEM - FRM CODE 4911XA00 AFTER LANDING UNABLE TO START APU NO RPM RISE. NO OTHER FAULT INDICATIONS. ECU FAULT SHOWS ECU AND MINI FLAGS 30-32-39-48-55-105. REPLACED ECU PER TASK 49-61-05-404-008. STARTED BOTH ENGINES AND RAN PACKS AND ELECTRICAL LOAD FOR SEVERAL MINUTES. NO FAULTS, OK FOR SERVICE.

Part: APU — FAILED · airframe 28,785 hrs · 5,418 cycles

ETOPS SIGNIFICANT SYS - APU FAILED TO START AFTER LANDING. OIL QTY INITIALLY INDICATE .75 THEN AFTER SEVERAL MINUTES FULL. R & R APU IAW HAL M266-767 GND OPS CHECK & LEAK CHECKS OK.

Part: CONNECTOR — CONTAMINATED (APU) · airframe 28,687 hrs · 5,400 cycles

ETOPS SIGNIFICANT SYSTEM - APU FAULT AFTER LDG (ADD OIL). T/S PER FIM 49-11-22-00-116 PERFORMED ECU FAULT BITE WITH NO FAULTS DETECTED; CHECKED QTY FOUND FULL, NO EVIDENCE OF OIL LEAK. RAN APU UNDER LOAD NO PR'S NOTED. RE-INSPECTED APU FOR LEAKS. CLEANED OIL LEVEL SENSOR CONNECTOR. RE-INSTALLED, RAN OPS CHECK GOOD. OK FOR CONT SERVICE.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 28,647 hrs · 5,394 cycles

ETOPS SIGNIFICANT SYSTEM - "APU FAULT" EICAS MESSAGE AFTER APU START ATTEMPT ON GND, SECOND ATTEMPT SUCCESSFUL. PERFORMED APU BITE CHECK PER FIM 49-11-00 FIG 103, NO FAULTS FOUND. INSPECTED APU, NO LEAKS NOTED FOUND APU OVER SERVICED, DRAINED APU OIL TO PROPER LEVEL, APU STARTED AND OPS NORMAL ON FIRST ATTEMPT. OK FOR SERVICE.

Part: APU — SHUTDOWN · airframe 28,595 hrs · 5,386 cycles

ETOPS SIGNIFICANT SYSTEM, ON TAXI IN APU AUTOSHUT DOWN SUCCESSFULLY RESTARTED. CHECKED OIL QTY FOUND FULL, PERFORMED APU BIT CK ON ECU PER FIM 49-11-00-1 FIG 103. FOUND NO PREVIOUS FAULTS OR CURRENT FAULTS AND MINI FLAGS CK OK. STARTED APU SEVERAL TIMES, NO FAULTS. OK TO CONTINUE.

Part: CONNECTOR — DIRTY (APU ACU) · airframe 28,554 hrs · 5,380 cycles

ETOPS SIGNIFICANT SYSTEM - APU FAILED TO START TWO ATTEMPTS. BITE TEST DONE ON ECU SHOWING "LOW OIL PRESS" VIS CK APU OIL AT FULL. CLEANED ELECTRICAL PLUG OF LOW OIL TEMP SWITCH AND RERACKED APU ACU. RESTARTED, APU WORKS NORMALLY. ALL PARAMETERS NORMAL BITE TEST DONE. TEST OK. A/C OK FOR CONTINUE TO SERVICE REF AMM 49-61-00.

Part: SWITCH — MALFUNCTIONED · airframe 28,393 hrs · 5,350 cycles

ETOPS SIGNIFICANT SYSTEM - APU WILL NOT START GOT FAULT LT OIL QTY SHOWED, 25 AFTER SHUTDOWN. VISUALLY CHECKED APU OIL LEVEL, OIL LEVEL AT FULL, BITE CHK APU ECU LAST FLT LEG FAULTED LOW OIL PRESSURE. REMOVED AND REPLACED LOW OIL PRESSURE SWITCH IAW AMM RESTARTED APU ALL CHKS NORMAL, BITE CHK APU ECU ALL OK C/W TASK 49-94-04-206-007 OIL QTY XMTER INSP ALL CHK GOOD.

Part: FILTER — TRIPPED (APU OIL SYS) · airframe 28,322 hrs · 5,340 cycles

ETOPS SIGNIFICANT SYSTEM - FRM 49110300 APU WILL NOT START APU FAULT ILLUMINATED. BITE CK ECU FOUND (LOW OIL PRESS FAULT) CK MAG PLUGS NO METAL NOTED. REPLACED LOW OIL PRESS SWITCH COND SAME FOUND OIL FILTER DETA "P" POPPED. REMOVED FILTER REF FOR S/W MM49-94-02. REPLACED APU OIL FILTER PER AMM49-27-03. OPS AND LEAK CK GOOD.

Part: WARNING MESSAGE — ILLUMINATED (BOOST PUMP) · airframe 27,777 hrs · 5,245 cycles

ETOPS SIGNIFICANT SYS - RT FWD BOOST PUMP LOW PRESS LIGHT ILLUM WITH SWITCH ON. EICAS MSG R FWD FUEL PUMP DISPLAYED. T/S IAW FIM 28-22-00/101 FIG 106 AND 106A. ALSO PERFORMED WIRE INSPECTION IAW AMM 28-22-15-206-001 NO TROUBLE FOUND OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (ENGINE) · airframe 27,307 hrs · 5,157 cycles

ETOPS SIGNIFICANT SYS - BTB: ON LT ENG START RECEIVED STATUS MSG "L ENG CONTROL" AND EICAS MSG "L ENG CONTROL". ENGINE STABILIZED AT 60 PERCENT N2; 32.5 PERCENT N1. ADVANCED THROTTLES N1 AND N2 RESPONDED BUT LIGHTS STILL ON. PERFORMED FIM 73-21-00 FIG 112 CLEARED MESSAGE IAW BLOCK 2 AND 21. RAN ENG, MESSAGE DID NOT RETURN.

Part: WARNING MESSAGE — FALSE ACTIVATION (ENGINE) · airframe 27,026 hrs · 5,106 cycles

ETOPS SIGNIFICANT SYS - BTB -ON ENGINE START L ENG CONTROL EICAS MESSAGE. BITE LT ENG PIMU IAW FIM 73-21-00 FIG 112 NO FAULTS. PIMU RESET. RAN LT ENG. NO FAULTS. MSG DID NOT RETURN ON ENG RUN.

Part: THROTTLE — OUT OF ADJUST · airframe 26,486 hrs · 5,009 cycles

ETOPS SIGNIFICANT SYS - ENG THRUST LEVERS MISALIGNED IN NORM MODE. RT THRUST LEVER LAGS 1/2 KNOB W/EPR MATCHED LT ENG N1-EGT-F/F HIGH AND N2 IS LOW 2 PERCENT. INSPECTED LINKAGES AND BRGS T/S IAW FIM 73-21-00. NO PIMU FAULTS. ADJUSTED THROTTLE LEVERS IAW AMM 73-21-11-825-002-N00. OPS CKD GOOD.

Part: SWITCH — FAILED (APU) · airframe 26,374 hrs · 4,987 cycles

ETOPS SIGNIFICANT SYS - APU AUTO SHUTDOWN AFTER BLOCK IN AT OGG. T/S IAW FIM 49-27-04 AND 49-11-00 REMOVED AND REPLACED DELTA P SWITCH. OPS CHECK GOOD IAW AMM 49-27-15 AND AMM 49-11-00. APU OIL LEVEL FULL, OK FOR SERVICE. ALL TEST ON GROUND NORMAL LEAK CK GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 26,276 hrs · 4,968 cycles

ETOPS SIGNIFICANT SYSTEM - FIM 31514300 CONFIG LGT ILLUM EICAS MSG "GEAR NOT DOWN" DISPLAYED APL INFLIGHT ABOVE 800 FT NOT IN LANDING CONFIGURATION. ALL 3 RADIO ALT T/R OPS CK OK PER MM34-33-00. ACCOMP FIM 31-51-00 FIG 109A NO DEFECTS NOTED OK FOR SVC.

Part: WARNING LIGHT — ILLUMINATED · airframe 26,249 hrs · 4,963 cycles

ETOPS SIGNIFICANT SYSTEM - AFTER ENG. START RT GEAR DRIVE LIGHT & EICAS MESS ILLUMINATED. INSP D R IDG, DELTA P BUTTON NO POPPED, SERVICED IDG FULL, RAN ENG FOR 5 MIN. CK'D IDG OIL QUANTITY AGAIN. REQUIRED NO MORE SERVICING. DURING ENG. RUN ALL PERAMETERS NORMAL . OK FOR SERVICE. IAW AMM 24-11-00.

Part: CONNECTOR — DIRTY (EEC) · airframe 26,229 hrs · 4,959 cycles

ETOPS SIGNIFICANT SYS - ON OVERNIGHT CHECK FOUND R PIMU MESSAGE ON ECS MSG PAGE EICAS. TROUBLESHOT IAW FAULT ISOLATION MANUAL CH 71. PIMU INDEX BITE OF PIMU REVEALS EEC CHA FAULT, CAT 2 EEC CH A,TCC FD-BK FAIL. EEC CH B FAULT CAT 2 AND EEC CH B BTCC FD-BK FAIL MESSAGES, FAULT NR 351-27. PERFORMED TS IAW FIM CLEANED AND INSPECTED CONNECTOR D90029 ON HARNESS W4P16 ON TCC VALVE M3107, OK FOR SVC.

Part: VALVE — MALFUNCTIONED (RT ENGINE) · airframe 26,190 hrs · 4,951 cycles

ETOPS SIGNIFICANT SYS - ON ENG SHUTDOWN RT ENGINE SPAR VALVE LT CAME ON W/EICAS MSG. PERFORMED OPS CK OF RT ENG SPAR VALVE IAW AMM 28-22-11-404-008. OPS CHECKED NORMAL. NO FAULTS NOTED.

Part: ECU — MALFUNCTIONED (APU) · airframe 26,019 hrs · 4,919 cycles

ETOPS SIGNIFICANT SYS - APU FAULT ILLUMINATED DURING 1ST START ATTEMPT AFTER LANDING CLEARED FAULT LT STARTED 2ND ATTEMPT OK. PERFORMED BITE OF ECU IAW FIM 49-11-00 FIG 103 FAULTS NOTED 132,133 MINI FLAG APU OPERATING NML OK FOR SERVICE, REPLACED ECU AS PRECAUTIONARY IAW AMM 49-61-05.

Part: APU — UNKNOWN · airframe 25,870 hrs · 4,891 cycles

ETOPS SIGNIFICANT SYSTEM, APU FAILED TO START. FAULT LIGHT ILLUM AND EICAS MSG APU FAULT DISPLAYED. SECOND ATTEMPT INDICATES EGT HIGH. PERFORMED BITE CHECK OF APU NO FAULTS, CHECKED CONDITION AND SECURITY OF APU, OIL QTY CHECK GOOD, PERFORMED SUCCESSFUL START OF APU AIR AND ELECTRIC, OPS CHECK GOOD REF AMM 49-11-00.

Part: CHARGER — INOPERATIVE (MASTER) · airframe 25,704 hrs · 4,861 cycles

ETOPS SIGNIFICANT SYSTEM - BTB: STATUS MESSAGE" MAIN BATT CHARGER". MX CONTROL REQUESTED RETURN TO RAMP. REPLACED MAIN BATTERY PER AMM 34-31-01. REPLACED MAIN BATTERY CHARGER PER AMM 24-31-02. OPS CHECK GOOD. OK FOR SERVICE.

Part: APU — SHUTDOWN · airframe 25,704 hrs · 4,860 cycles

APU AUTO SHUTDOWN AT ETP MID POINT APU START VERIFICATION UNSUCCESSFUL ON DESCENT. ATTEMPTED APU START APU REACHED 99PCT. THEN AUTOSHUTDOWN AGAIN. APU REMOVED AND REPLACED PER AMM TASK 49-11-01-004-116 AND TASK 49-11-01-404-153 AND C/W HAL M266-767.

Part: PUMP — LEAKING (APU OIL SYSTEM) · airframe 25,704 hrs · 4,860 cycles

APU START AT TOP OF DESCENT FAILED. GOT 100 PERCENT THEN AUTO SHUT DOWN. "APU FAULT" ON EICAS. ACCOMP BITE OF APU ECU FOUND LOW OIL PRESS. VISUAL CHECK APU OIL LEVEL, FOUND LOW, SERVICED APU W/8 PINTS OF OIL. STARTED APU. FOUND OIL LEAKING AT BASE OF LUBE PUMP. REMOVED AND REPLACED PACKINGS ON PUMP AND OIL TRANSFER TUBES PER AMM 49-27-01. LEAK CHECK PEND. RAN APU 4 HRS LEAK CHECK OK.

Part: OIL SYSTEM — LEAKING (APU) · airframe 25,700 hrs · 4,859 cycles

AFTER APU VERIFICATION TO ETP AT TOP OF DESCENT, APU STARTED NORMALLY AND ALL INDICATIONS NORMAL FOR .5 SECONDS THEN APU SHUT DOWN WITH ASSOCIATED "APU FAULT" ON EICAS. BIT OF ECU SHOWS LOW OIL PRESS. APU SHOWS SIGNS OF EXTERNAL LEAK, APU OIL QUANTITY INDICATION OUT OF SIGHT GAUGE. FILLED OIL TO FULL, CLEANED APU OFF, CHECKED EXHAUST AND T/S PER FIM 49-11-00. NO DISCREPANCIES NOTED. RAN APU UNDER LOAD FOR OVER 1HOUR. NO LEAKS NOTED APU QTY STAYED AT FULL.

Part: APU — MALFUNCTIONED · airframe 25,694 hrs · 4,858 cycles

APU AUTO SHUTDOWN WITH FAULT LIGHT ON ATTEMPTED ONE RESTART WHICH FAILED. FOUND UNDERSPEED AND MINI FLAGS 42 AND 66 ON APU BITE. FOUND NO LIGHT OFF ON SUBSEQUENT APU START TRIES ON APU BITE. REPLACED APU IGNITOR PLUG PER AMM 49-41-02. REPLACED APU IGNITION LEAD PER AMM 49-41-04. REPLACED APU EXCITOR BOX PER AMM 49-41-03. REPLACED INLET GUIDE VANE ACTUATOR PER AMM 49-52-02. INSTALLED FUEL INLET AND RETURN LINES. APU CHANGE REQUIRED. REMOVED AND REPLACED APU ASSY PER HAL-M266-767. OPS AND LEAK CHECK GOOD. OK FOR SERVICE.

Part: GARLOCK SEAL — LEAKING (NR 1 ENGINE) · airframe 25,661 hrs · 4,852 cycles

DURING ROUTINE OIL SERVICE NR 1 ENG TOOK 3 QUARTS. RAN ENG AT IDLE POWER FOUND PMA GARLOCK SEAL LEAKING. REPLACED PMA ROTOR ASSY PER AMM 72-61-00-400-001-0. REINSTALLED STATOR ASSY PER AMM 73-21-05-404-038, RAN TEST NR 6, CHECK GOOD, LEAK CHECK GOOD.

Part: FILTER — LEAKING (GENERATOR) · airframe 25,525 hrs · 4,829 cycles

AT TOP OF CLIMB RT GEN DRIVE LIGHT ILLUMINATED, DISCONNECTED AND DIVERTED TO LAX. PERFORMED BITE CHK ON BPCU RIGHT IDG SERVICING MESSAGE DISPLAYED, 2 QTS ADDED. DURING DRY MOTORING FOUND OIL LEAKING FROM BOTH FILL AND OVER FILL ADAPTERS. REPLACED FILL AND OVERFILL ADAPTERS. INSPECTED IDG FILTER, NO CONTAMINATION NOTED. REPLACED FILTER PER AMM 24-11-02. PERFORMED OPERATIONAL CHECK OF RIGHT IDG PER AMM 24-11-00. NO LEAKS NOTED, SYSTEM OPS NORMAL. OK FOR SERVICE. FILTER PN 2400599 , ADAPTERS PN 2404075 2404073.

Part: AUTOLAND SYS — MALFUNCTIONED · airframe 25,004 hrs · 4,734 cycles

ETOPS SIGNIFICANT SYSTEM, AUTOLAND STATUS INDICATOR SHOWS "NO LAND 3" WILL NOT RESET. YELLOW G/S AND LOC WARNINGS SHOW ON CAPT ADI. LAST FLIGHT FAULT ON MCDP SHOWS LEFT ILS. FOUND LEFT MMR WILL NOT TEST CYCLED LEFT MMR C/B NOW LEFT MMR BITE TEST PASS. ALL LEFT ILS AND G/S FLAGS NOW PULLED FROM VIEW. PERFORMED MCDP TEST 40 PER HAL M7-22-01. TEST PASS LMP STATUS SCREW REMAINS IN LAND 3 POSITION.

Part: INDICATOR — READS HIGH (ALTIMETER) · airframe 24,604 hrs · 4,664 cycles

ETOPS SIGNIFICANT SYSTEM, FO ALTIMETER READS 80 FT HIGHER THEN CAPTS ALTIMETER FL 370. REMOVED AND REPLACED F/O ALTIMETER IAW AMM 34-13-01, ALL CHKS OK.

Part: SEAT TRACK — CORRODED (BS 911) · corrosion level 2 · airframe 21,271 hrs · 4,062 cycles

LEVEL 2 CORROSION ON BOTH TRACK FITTINGS WHERE FEET OF STA 911 PARTITION ATTACHES TO FLOOR. BOTH TRACK FITTINGS REPLACED IAW 767-300 SRM 51-40-02 REV 76 AND DWG 145T5222.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 21,271 hrs · 4,062 cycles

LEVEL 2 CORROSION ON THE HORIZONTAL STAB CENTER SECTION, UPPER SURFACE SKIN, RBL 32.5, STR 7, AROUND 1 FASTENER. CORROSION REMOVED AND SURFACE FINISH RESTORED, IAW SRM 55-10-01, FIG 101, REV 76 AND ANZ T.I. 190114804-0001.

Part: SEAT TRACK — CORRODED (BS 911) · corrosion level 2 · airframe 21,271 hrs · 4,062 cycles

CORROSION ON BOTH TRACK FITTINGS WHERE FEET OF STA 911 PARTITION ATTACH TO FLOOR, LBL, RBL. BOTH TRACK FITTINGS REPLACED IAW 767-300 SRM 51-40-02 REV 76 AND DWR 145T522Z.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 21,271 hrs · 4,062 cycles

LEVEL 2 CORROSION ON THE HORIZONTAL STAB CENTER SECTION UPPER SURFACE SKIN AT RBL 13, STR 3, ON 2 FASTENERS. REWORKED PER SRM 55-10-01, FIG 101, REV 76.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 21,271 hrs · 4,062 cycles

LEVEL 2 CORROSION ON HORIZONTAL STAB CENTER SECTION UPPER SURFACE SKIN AT RBL 10, STR. 1, AROUND 2 FASTENERS. REWORKED PER SRM 55-10-01 FIG 101, REV 76.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 21,271 hrs · 4,062 cycles

LEVEL 2 CORROSION ON THE HORIZONTAL STAB CENTER SECTION UPPER SURFACE SKIN AT LBL 14, STR 3, AROUND 5 FASTENERS. REWORKED PER SRL 55-10-01 FIG 101, REV 76.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 21,271 hrs · 4,076 cycles

LEVEL 11 CORROSION ON THE HORIZONTAL STAB CENTER SECTION UPPER SURFACE SKIN AT LBL 1, STR 3, AROUND 2 FASTENERS. REMOVED CORROSION AND REPROTECTED SURFACE IAW SRM 55-10-01 FIG 101, REV 76.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 21,271 hrs · 4,062 cycles

LEVEL 2 CORROSION ON HORIZONTAL STAB CENTER SECTION UPPER SKIN AT LBL 33.5, STR 3, AROUND 7 FASTENERS. REMOVED CORROSION AND RESTORED TO ORIGINAL SURFACE FINISH, IAW SRM 55-10-01 FIG 101 REV 76 AND TI 190114804-0001.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 21,271 hrs · 4,062 cycles

LEVEL 2 CORROSION ON THE CENTER HORIZONTAL STAB UPPER SURFACE SKIN AT LBL 35 STR 10, AROUND 2 FASTENERS. REMOVED CORROSION IAW SRM 55-10-01, FIG 101 REV 76. REWORK APPROVED BY TI FILE NR 588030.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 21,271 hrs · 4,062 cycles

LEVEL 2 CORROSION ON THE HORIZONTAL STAB CENTER SECTION UPPER SKIN, RBL 29.5 AT STR. 8,ON THREE FASTENERS. REMOVED CORROSION AND RESTORED ORIGINAL SURFACE FINISH IAW SRM 55-10-01, FIG 101 REV 76 AND ANZ T1190114804-0001.

Part: FAN — OVERHEATED (NR 1) · airframe 21,271 hrs · 4,062 cycles

CONTROL RELAY TEST FAILED. NUMBER 1 FAN OVERHEATED AND STOPPED, DET FAN PRESSURE SWITCH HAD ALSO FAILED DUE TO A PIN BEING BENT ON THE PRESSURE SWITCH. REMOVED AND REPLACED FAN AND DET AIR PRESSURE SWITCH. OPS CHECK GOOD. OK FOR SERVICE.

Part: ATTACH FITTING — CORRODED (BS 911) · corrosion level 2 · airframe 21,271 hrs · 4,062 cycles

PARTITION AT STA 911 BOTH LOWER ATTACH FITTINGS CORRODED. CORRROSION BEYOND SRM LIMITS. NEW BRACKETS MANUFACTURED IAW DRW 413T2047.

Part: SELECTOR PANEL — FAILED (CABIN PRESSURE) · airframe 21,218 hrs · 4,054 cycles

ATB - BOTH CABIN PRESS AUTO SYSTEMS FAILED, MANUAL MODE OPERATED OK. PERFORMED FIM 21-31-00. REPLACED CABIN PRESSURE SELECTOR PANEL PER AMM21-31-01. CHECKED OK, NO DEFECTS NOTED.

Part: INDICATOR — MALFUNCTIONED (AIRSPEED) · airframe 21,087 hrs · 4,030 cycles

ETOPS SIGNIFICANT SYSTEM, CAPT AIRSPEED IND AIRSPEED FLAG INTERMITTENTLY IN VIEW. REPLACED CAPT'S A/S INDICATOR, GND CK OK PER MM 34-13-02.

Part: POWER STRIP — INOPERATIVE (CABIN) · airframe 21,066 hrs · 4,026 cycles

FLOOR EMERGENCY LIGHTS INOP ADJ TO LAV C. REPLACED POWER STRIP PER AMM 33 51 10, OPS CHECKS GOOD.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 20,957 hrs · 4,005 cycles

ETOPS SIGNIFICANT SYSTEM, CO PILOTS FMS COMPUTER INOP. PULLED C/B ON FMS COMPUTER RESET C/B FMS COMPUTER SYNC WITH OTHER COMPUTER. CHECKS OK PER MM 34-61-01-424-05.

Part: ADAPTER — DEFECTIVE (CABIN) · airframe 19,636 hrs · 3,761 cycles

EMERGENCY FLOOR LIGHTING EXTINGUISHED DURING TEST, BETWEEN SEAT 25AB TO 26 AB. REMOVED AND REPLACED LIGHTING STRIP ADAPTER, OPS CHK EMERGENCY LTS ALL CHK OK.

Part: OIL SYSTEM — LOW (APU) · airframe 19,631 hrs · 3,760 cycles

ETOPS SIGNIFICANT SYSTEM, UPON ARRIVAL, APU WOULD NOT START, OIL QUANT .75 QT. SERVICED APU OIL QTY (1 PINT) BITE CK. NO DEFECTS NOTED. LK CK OK. OPS CK GOOD.

Part: CONTROL MODULE — MALFUNCTIONED (DISPLAY) · airframe 19,350 hrs · 3,700 cycles

ETOPS SIGNIFICANT SYSTEM, CENTER ENGINE UPPER AND LOWER CRT'S FLASHED BLACK, THEN BACK ON AND NORMAL, 7+ TIMES DURING FLIGHT. ALL OTHER INDICATIONS NORMAL, BOTH FLASHED TOGETHER. T/S PER FIM 31-41-00 FIG 104, 105. REMOVED UPPER AND LOWER DU'S CHECK COOLING. NO FAULTS FOUND. AFTER T/S AND A/C POWER UP UPPER DU FAILED TO DISPLAY. FOUND BAD PIN ON UPPER DISPLAY SW MODULE M10417. REMOVED AND REPLACED DU'S PER AMM 31-41-01-004-001/404-002. REMOVED AND REPLACED CONTROL MODULE PER AMM 31-41-04-004-001/404-001. PRFD EICAS BITE OPS PIN CK OK.

Part: ACTUATOR — MALFUNCTIONED (RAM AIR DOOR) · airframe 18,978 hrs · 3,628 cycles

ATB - UNABLE TO KEEP CABIN TEMP REASONABLE W/R PACK IN STBY W. REMOVED AND REPLACED RT PACK RAM AIR INLET DOOR ACTUATOR. OPERATION OF RT PACK GOOD. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (SEAT 20H) · airframe 18,478 hrs · 3,537 cycles

FLOOR EMERGENCY LIGHTING INOP SEAT 20H TO AFT OF LAV D. REPLACED POWER STRIP AFT OF LAV D PER AMM 33-51-10, OPS CK GOOD.

Part: UNKNOWN — UNKNOWN (EICAS COMPUTER) · airframe 18,372 hrs · 3,519 cycles

ETOPS SIGNIFICANT SYSTEM, MX LEVEL EICAS MSG 'EICAS BITE' DISPLAYED. MULTIPLE DATA FIELDS BLANK W/RIGHT EICAS COMPUTER SELECTED. ACCOMPLISHED EICAS BITE TEST NO FAULTS NOTED. CKS NML PER MM 31-41-02.

Part: UNKNOWN — UNKNOWN (APU) · airframe 17,943 hrs · 3,353 cycles

ETOPS SIGNIFICANT SYSTEM, APU AUTO SHUT DOWN AS PACKS WERE TURN OFF FOR ENG START. PERFORMED FIM 49-11-00 FIG 103 APU BITE, NO FAULTS NOTED. OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (BLEED WARNING) · airframe 17,247 hrs · 3,310 cycles

ETOPS SIGNIFICANT SYSTEM, ON DESCENT LEFT ENG BLEED LIGHT ILLUMINATED AND L ENG PRV EICAS MSG ILLUMINATED. TURNED OFF LEFT ENG BLEED AIR SWITCH AND LEFT PACK CONTROL SELECTOR. PERFORMED TEST PER FIM 36-10-00 FIG 123. OPS CK'S NORMAL. NO FAULTS. NO MSG'S.

Part: LINE — LOOSE (ENGINE) · airframe 17,125 hrs · 3,290 cycles

ETOPS SIGNIFICANT SYSTEM, L ENG PRV WARNING CAME ON SEVERAL TIMES DURING DESCENT FRM FL 380. TROUBLESHOT PER FIM 36-10-00 FIG 123. FOUND LOOSE SENSE LINE TO PRE-COOLER. TIGHTENED LINE, RAN ENGINE AND PERFORMED OPERATIONAL TEST OF PRV PER AMM 36-11-18/501. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (LT PACK CONTROL) · airframe 17,114 hrs · 3,288 cycles

ETOPS SIGNIFICANT SYSTEM, LEFT PACK TEMP EICAS LIGHT CAME ON. SWITCHED TO STBY "N" LIGHT WENT OUT. PERFORMED BITE CK ON LT PACK TEMP CONTROLLER. FOUND INLET ACT FAULT, VERIFIED AND RESET, MSG CLD. OK FOR SERVICE PER FIM 21-51-00.

Part: UNKNOWN — UNKNOWN (LT ENGINE) · airframe 13,103 hrs · 3,286 cycles

ETOPS SIGNIFICANT SYSTEM, LT ENG PRV CAUTION EICAS DISPLAYED ON DESCENT DUCT PRESS NORMAL. T/S PER FIM 36-10-00 FIG 123 LT ENG PRV CHECKS GOOD. PERFORMED BITE CHECK OF AIR SYSTEM CONTROLLER. NO FAULTS NOTED. OK FOR CONTINUED SERVICE.

Part: BRAKE ASSY — HOT (MLG) · airframe 16,904 hrs · 3,247 cycles

UPON WALK AROUND, FOUND MAIN LANDING GEAR WHEEL BRAKES NR 3 RED HOT AND SMOKING MAIN LANDING GEAR MLG THERMALED WENT FLAT REQUIRE REPLACEMENT. REMOVED AND REPLACED NR 3 MLG AS PER MM TASK CARD 32-45-01-004-001 AMD TASK CARD 32-45-01-404-027.

Part: WHEEL — DAMAGED (MLG) · airframe 16,904 hrs · 3,247 cycles

NR 4 MLG WHEEL HOT THERMALED UPON ARRIVAL REQUIRES REPLACEMENT. REMOVED AND REPLACED NR 4 MLG WHEEL ASSY PER TASK CARD 32-45-01-004 AND 32-45-01-404-027.

Part: RIB — CRACKED (LT WING) · airframe 16,797 hrs · 3,227 cycles

LT WING FIXED LE BULLNOSE RIB IS CRACKED JUST I/B OF NR 4 I/B ROTARY ACTUATOR. REMOVED SLAT CURTAIN AT NR 4 SLAT I/B ROTARY ACT. REMOVED AND REPLACED BULLNOSE RIB AERO DYNAMIC FORMER (NOSE) REINSTALLED SLAT CURTAIN. ALL WORK DONE IAW SRM 51-40-02 PAR 4 AND 7 AND M/M 27-81-024-001 STEP 2 E (2) AND M/M 27-81-424-019 STEP 3 (6).

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,434 hrs · 3,158 cycles

FIRST CLASS A/C RIGHT EMERGENCY FLOOR LIGHT INOP. REPLACED LIGHT STRIP FIRST CLASS CABIN A/C RIGHT OK FOR SVC, OPS CHECK GOOD AMM 33-51-05.

Part: WARNING MESSAGE — ILLUMINATED · airframe 15,753 hrs · 3,029 cycles

ETOPS SIGNIFICANT SYSTEM - EICAS: L ENG PRV. PERFORMED FIM PROCEDURES 36-10-00. ALL INDICATIONS GOOD, NO FAULTS FOUND.

Part: WARNING MESSAGE — ILLUMINATED (COCKPIT) · airframe 15,524 hrs · 2,987 cycles

ETOPS SIGNIFICANT SYSTEM, EICAS MSG R IDG VALVE DISPLAYED. PERFORMED BIT ON BPCU NO FAULTS. MSG ERASED PER FIM 31-41-00 FIG 109. RAN RIGHT ENG. NO EICAS MSG. CHECK HISTORY, NO HISTORY.

Part: ENGINE — VIBRATION · airframe 15,524 hrs · 2,987 cycles

ETOPS SIGNIFICANT SYSTEM, IN CRUISE RESONATING VIBRATION CAUSED BY SLIGHT SPLIT IN ENGINE INDICATIONS. FL390 AUTOTHROTTLES ON EPR 1.33L AND R LN,87.8 RN, 88.5 LN2 - 89RN288 FFL4.9 R4.8. INSPECTED NR 1 AND NR 2 ENGINES, NO DEFECTS NOTED ON GRD, ALL PARAMETERS NORMAL. NO VIBRATIONS NOTED.

Part: CAUTION MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 15,493 hrs · 2,981 cycles

ETOPS SIGNIFICANT SYSTEM, ON DESCENT"L ENG PRV" MESSAGE. NO MSG ON EICAS ON ARRIVAL BITE CK AIR SUPPLY MODULE NO FAULT NOTED, PERFORMED GRD IDLE RUN A/C OK FOR SERVICE.

Part: VALVE — MALFUNCTIONED (RT NACELLE) · airframe 14,926 hrs · 2,875 cycles

ETOPS SIGNIFICANT SYSTEM, EICAS MX MSG R NAC VENT VAL DIS PLAYED. REPLACED RT NAC VENT VALVE PER M/M 75-23-02.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 14,762 hrs · 2,843 cycles

ETOPS SIGNIFICANT SYSTEM, FMC DISPLAYED ON EICAS WITH NO CORRESPONDING FMS MESSAGE. NO EICAS MESSAGE "FMC" DISPLAYED ON ARRIVAL. OPS CHECK OK PER MM 34-61-00.

Part: WARNING MESSAGE — ACTIVATED (COCKPIT) · airframe 14,621 hrs · 2,817 cycles

STATUS MESSAGE OF -CABIN ALT AUTO 2- DISPLAYED. PERFORMED FIM 21-31-00/101 FIG 103, NR 2 CABIN PRESSURE CONTROLLER SHOWED NO VERIFIED FAULTS. MESSAGE CLEARED. THE SYSTEM IS OK.

Part: FAIRING — BENT (T/R BLOCKER DOOR) · airframe 14,563 hrs · 2,806 cycles

PER MECH, FOUND ON WALK AROUND NR 2 ENG T/R BLOCKER DOOR AFT FAIRING AT 5 O'CLOCK POSITION BENT-UP. OK TO CONTINUE PER EVA 78-03-02. REMOVED FAIRING & SPEED TAPED AREA. NEED TO INSPECT SPEED TAPE AFTER EVERY FLIGHT. PLACARD & ENTERED ON MIC SHEET.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 14,454 hrs · 2,784 cycles

MAINT ENTRY: FOUND ON OVERNIGHT CHECK ROW 25AB & 26AB FLOOR EMERGENCY LIGHT STRIP INOP.//REPLACED BROKEN JUMPER CABLE AT ROW 25AB & 26AB. OPS CK OK PER M/M 33-51-10.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 14,380 hrs · 2,769 cycles

ETOPS SIGNIFICANT SYSTEM, EICAS MSG CABIN ALT AUTO 2 ILLUMINATED. R AND R ALT 2 OUTFLOW VLV PER FIM 21-31-00 BIT CK AND VERIFY NML, OPS CK OK.

Part: LIGHT — UNKNOWN · airframe 14,279 hrs · 2,752 cycles

FLT DECK EXIT SIGN/EMERGENCY LIGHT INOP IN AUTO MODE, MANUAL MODE GOOD. TESTED COCKPIT EMERG LT PER MM 33-51-00-715-227 AND 33-51-00-725-247, AUTO FUNCTION CHECKS NORMAL W/EMERG LTS ARMED OPEN C/B B-6 ON PILOTS OVHD P-11, EMERG CHGR PORTABLE, CLOSED C/B ALL OPS NORMAL.

Part: RADIO — MALFUNCTIONED (HF SYSTEM) · airframe 14,230 hrs · 2,742 cycles

ETOPS SIGNIFICANT SYSTEM, NR 1 HF RADIO WILL NOT TUNE. PERFORMED OPERATION CK OF NR 1 HF RADIO-SYS, OPS CK OK PER AMM 23-11-03.

Part: SCUFF PLATE — GROUND DAMAGE (AFT CARGO BAY) · airframe 13,781 hrs · 2,655 cycles

BULK CARGO DOOR DAMAGED BY GROUND SERVICE EQUIPMENT. BULK CARGO DOOR SCUFF PLATE REMOVED, NO DAMAGE NOTED TO AIRFRAME. REPAIR SCUFF PLATE DENT PER COLD WORK BAC5300 AND CRACK PER BAC5975 613. INSTALLED SCUFF PLATE PER AMM 53-13-02, SECURITY CONDITION GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 13,770 hrs · 2,653 cycles

ETOPS SIGNIFICANT SYSTEM - AFT CARGO AFT DETECTION FAN MESSAGE ON EICAS. OK TO CONTINUE PER MEL 21-51-01.

Part: ACCESS PANEL — MISSING (NR 1 PYLON) · airframe 13,597 hrs · 2,619 cycles

NR 1 ENG PYLON ACCESS PANEL I/B SIDE MISSING ON A/C ARRIVAL (PANEL 436AR). INSTALLED NR 1 PYLON ACCESS PANEL.

Part: GROUND WIRE — SHORTED (APU STARTER)

REMOVED AND REPLACED APU STARTER IAW AMM. DID NOT FIX DISCREPANCY. (LOANER STARTER FROM DELTA). TROUBLESHOT WIRING TO STARTER AND FOUND STARTER GROUND LEADS SHORTED AT TERMINAL/ AIRFRAME SIDE. REPAIRED, REPLACED GROUND LEADS AND TERMINAL ENDS, AND FABRICATED ATTACHING BRACKET IAW DWG AND SWPM. (K)