N548UA

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,048 hrs · 24,589 cycles

AFT PIT, BILGE AREA, FRAME CORROSION STATION 1300, STRINGER 30L. REMOVED DAMAGE & INSTALL REPAIR IAW REO-G18514 REV A & ECRA 5310-06329.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,048 hrs · 24,589 cycles

AFT PIT FRAME HAS EXFOLIATION CORROSION STATION 1480, STRINGER 25 - 26R. REMOVED DAMAGED SECTION OF RIB STATION 1480, STRINGER 26 - 25R. INSTALLED NEW SECTION IAW SRM 530-00 -07 REPAIR 5. SPLICE PLATES & J ANGLE REPAIR.

Part: NUT — SPLIT (MLG WHEEL) · airframe 84,849 hrs · 24,296 cycles

NUMBER 1 MLG TIRE TIE BOLT NUT SPLIT. REPLACED WHEEL & TIRE IAW AMM 32-45-01 PG 406.

Part: O-RING — DAMAGED (AILERON ACTUATOR) · airframe 84,528 hrs · 24,221 cycles

HYDRAULIC QTY DECREASED TO 047. QTY STABLE WITH PUMPS OFF RT SYS FIM 29-11-00 FIG 107. REPLACED O RING ON LT AILERON ACTUATOR PLUG FOUND LEAKING.

Part: STARTER — FAULTED (APU) · airframe 84,087 hrs · 24,119 cycles

APU FAULT ON START UP. R & R APU STARTER MOTOR IAW AMM 49-41-0. ALSO REPLACED APU CRANK CONTACTOR RELAY IAW AMM 49-41-05. APU START & OPERATION ALL NORMAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 77,872 hrs · 22,532 cycles

EXTERNAL FUSELAGE SKIN DENTED BS 734, STRINGER 21L - STRINGER 22L. CUT OUT DAMAGE, FABRICATED & INSTALLED A REPAIR DOUBLER BTW BS 727 & 737, STRINGER 21L TO STRINGER 22L.

Part: MOUNT BRACKET — DAMAGED (TE FLAP) · airframe 83,986 hrs · 24,091 cycles

LEFT WING INBD FLAP, OTBD AFT FAIRING, FWD INBD MOUNT BRACKET HAS PULLED RIVETS & ELONGATED HOLE. EIGHT EACH LOCK FASTENERS R & R IN TRANSITION FIT HOLES IAW REO G15089 REV C NR 36137.

Part: ENGINE — OIL CONSUMPTION (NR 2) · airframe 83,502 hrs · 23,964 cycles

NR 2 ENG HIGH OIL CONSUMPTION EXCEEDS LIMITS. ACFT TO BE REMOVED FROM ETOPS OPERATION UNTIL A POSITIVE FIX IS FOUND & OIL CONSUMPTION RETURNS TO NORMAL LIMITS.

Part: SENSOR — FAULTY (AC BAY) · airframe 83,124 hrs · 23,875 cycles

FWD CABIN COLDER THAN SELECTED WITH SWITCH ON & TEMP CONTROL IN AUTO. REPLACED COMP OUTLET SENSOR NR 2 ON PACK 2. OPERATIONS CHECKED OK. ALSO CLEANED COCKPIT TEMP SENSOR, FWD & AFT. RAN PACK & HAD CONTROL THRU OUT CABIN. DEF TEMP CONTROL.

Part: STARTER — FAULTY (APU) · airframe 83,072 hrs · 23,866 cycles

APU INOPERATIVE 2 ATTEMPTS. SHOWS STARTER ON BITE CHECK. INSPECTED STARTER & FOUND BURNED OUT NEEDS MR49408. REPLACED APU STARTER MOTOR IAW AMM-49-41-01, OPERATIONS CHECKED OK.

Part: SEAT — UNSECURE (CABIN) · airframe 82,923 hrs · 23,831 cycles

SEATS 22DEF NOT SECURED TO FLOOR. SECURED SEATS IAW MM.

Part: LIGHT — DETACHED (CABIN) · airframe 82,840 hrs · 23,810 cycles

EMERGENCY LIGHT STRIP 9ABC NEEDS RE ATTACHED. SECURED EMERGENCY EXIT LIGHT STRIP.

Part: HYDRAULIC LINE — LEAKING (RT MLG) · airframe 82,791 hrs · 23,793 cycles

WHILE PERFORMING NR 1 SVC WALK AROUND FOUND A HYD LEAK AT RT MAIN GEAR BETWEEN STRUT DOOR & STRUT RETURN LINE FOR TILT ACT. REMOVED 2 LINES AT LOCATION FOR REPLACEMENT, ON AOG. REPLACED LINES & LEAK CHECKED.

Part: SPAR — CORRODED (RT WING) · airframe 82,788 hrs · 23,792 cycles

RT WING REAR SPAR EXFOLIATED BELOW RT AFT FUEL PUMP HOUSING ADJACENT TO LOWER BONDING STRAP. IAW AVO2569 NEED TO COMPLETE STEPS 4 THRU 6. STEPS 1 THRU 3. ACCOMPLISHED STEP 4, NEED TO COMPLETE STEPS 5 & 6. ACCOMPLISHED STEPS 5 & 6.

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS) · airframe 82,788 hrs · 23,792 cycles

NR 1 ENG HPSOV HAS NO BLEED SHIFT. HPSOV LOCKED OUT IAW MEL & CANNON PLUG SECURED. REPLACED HPSOV, OPERATIONS CHECKED GOOD.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 82,784 hrs · 23,791 cycles

AUTO PRESSURIZATION CONTROLLER SELECTOR NR 1 & NR 2 INOPERATIVE, FLT DIVERTED. ACCOMPLISHED VAC PRESS RELIEF VLV TEST. REPLACED NR 1 AUTO PRESSURIZATION CONTROLLER IAW MM.

Part: PUMP — FAULTY (FUEL SYSTEM) · airframe 82,788 hrs · 23,792 cycles

RT AFT FUEL PUMP CB POPS WITH FUEL PUMP SELECTED ON. RT AFT BOOST PUMP REPLACED. UNABLE TO CONTINUE TO OPERATIONAL CHECK DUE TO FAILED RESISTANCE CHECK. AFT SPAR EXFOLIATING AT LOWER BONDING ATTACH POINT PUMP ON MR28705-4, PUMP OFF MR28216 & SN 049111949A.

Part: STARTER — MAKING METAL (NR 2 ENGINE) · airframe 82,788 hrs · 23,792 cycles

NR 2 ENG, SILVERS METAL IN PNEUMATIC STARTER CHIP DETECTOR. REPLACED NR 2 ENG PNEUMATIC STARTER, OPERATIONS CHECKED GOOD.

Part: STARTER — FAILED (APU) · airframe 82,736 hrs · 23,777 cycles

THREE FAILED APU ATTEMPTS. APU CONTROL UNIT SHOWING MINI FLAG 35, STARTER FAILED. R & R APU STARTER IAW AMM, STARTED APU TWICE, STARTS NORMAL.

Part: CONTROLLER — FAULTY (APU) · airframe 82,729 hrs · 23,775 cycles

APU WOULD NOT START ON TAXI IN APU FAULT EICAS. REPLACED APUC, OPERATIONS CHECKED GOOD.

Part: NUT — LOOSE (ELEVATOR PCU) · airframe 82,714 hrs · 23,771 cycles

RF ON CTR HYD 65 QUANTITY. FLANGE NUT ON RT INBD ELEVATOR PCU LEAKING. TIGHTENED FLANGE NUT LEAK, CHECKED GOOD.

Part: COVER — BROKEN (CABIN) · airframe 82,377 hrs · 23,692 cycles

FLOOR EMERGENCY EXIT LIGHT STRIP REMOVED FOR MAINT AT SEAT ROWS 8ABC THRU 12ABC. REPLACED BROKEN EMERGENCY EXIT LIGHTS & EMERGENCY EXIT LIGHT COVER, OPERATIONS CHECKED GOOD. INSPECTED EMERGENCY EXIT LIGHTS, REPLACED BETWEEN ROWS 8-12. FOUND IN AIRWORTHY CONDITION.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 82,377 hrs · 23,692 cycles

ROW 12 FLOOR IS WEAK, REPLACED CENTER AISLE FLOOR PANEL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,184 hrs · 23,637 cycles

WHITE EMERGENCY LIGHT AT SEAT 12 DEF WILL NOT ILLUMINATE, RELAMPED. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,184 hrs · 23,637 cycles

WHITE EMERGENCY LIGHT AT SEAT EF WILL NOT ILLUMINATE, RELAMPED. OPERATIONS CHECKED OKAY.

Part: JACK — FAULTY (NLG) · airframe 82,178 hrs · 23,635 cycles

FLIGHT INTERPHONE DOES NOT WORK.. AT DEPARTURE NO TIME TO WORK, COMPLIED WITH MEL. REPLACED FLIGHT INTERPHONE JACK ON NOSE GEAR, OPERATIONS CHECKED GOOD.

Part: LIGHT — UNSECURE (CABIN) · airframe 81,770 hrs · 23,536 cycles

EMERGENCY LIGHT AT BULLNOSE SEAT 12D INOPERATIVE. SECURED LAP AT BULLNOSE, OPERATION CHECKED NORMAL.

Part: MODULE — MALFUNCTIONED (APU) · airframe 81,759 hrs · 23,534 cycles

APU BLEED WILL NOT OPEN. APU BLEED OPERATED NORMAL FOR ABOUT 20 MINUTES (33-34PSI) THEN SURGE VALVE DUMPING AIR OVERBOARD. STARTED NR 2 ENGINE OK PRESSURE NORMAL TRIED TO START NR 1, PRESSURE DROPPED TO 9PSI THEN SLOW TO RISE TO 30 PSI. APU BLEED VALVE MUST REMAIN IN OFF POSITION. INSTALLED APU FLOW SENSING MODULE IAW AMM, OPERATIONS CHECKED NORMAL.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 81,615 hrs · 23,506 cycles

MANUAL PRESSURIZATION SWITCH WILL NOT OPERATE OUTFLOW VALVE. R & R CABIN PRESSURE OUTFLOW VALVE IAW MM 21-31-03 AND 21-31-04. OPS CKS NORMAL.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 81,554 hrs · 23,490 cycles

EMERGENCY LIGHT COVER AT SEAT 40C CRACKED. REPLACED COVER.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 81,554 hrs · 23,490 cycles

EMERGENCY LIGHT COVER AT SEAT 21C CRACKED. REPLACED COVER.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 81,554 hrs · 23,490 cycles

EMERGENCY LIGHT COVER MISSING AT SEAT 8C. REPLACED COVER.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 81,554 hrs · 23,490 cycles

EMERGENCY LIGHT COVER AT SEAT 24C CRACKED. REPLACED COVER.

Part: IGNITER — INOPERATIVE (RT ENGINE) · airframe 81,474 hrs · 23,470 cycles

RIGHT ENGINE NR 1 IGNITION SYS, INOPERATIVE. RT ENGINE NO START IN NR 1 IGNITION. OK USING BOTH. REPLACED IGNITER PLUG IAW AMM AND TESTED IGNITION SYS IAW AMM.

Part: EEC — DAMAGED (NR 2) · airframe 81,422 hrs · 23,457 cycles

DURING RT ENGINE ECC REMOVAL, FOUND EEC VENT FITTING JAMMED BETWEEN ECC AND ENGINE FAN CASE. CAUSED EEC DAMAGE (2" HOLE ON EEC), AND SOME WEAR ON FAN CASE. REPLACED EEC IAW AMM.

Part: FLOOR PANEL — GOUGED (CARGO BAY) · airframe 81,360 hrs · 23,443 cycles

AFT CARGO BAY HAS A 2.5" GASH IN METAL CARGO FLOOR DIRECTLY IN FRONT OF CARGO DOOR, 15" INTO CENTER OF PANEL. ACCOMPLISHED INTERIM REPAIR IAW GPM 1-0-1-102.

Part: PNEUMATIC SYSTEM — MALFUNCTIONED (APU) · airframe 81,277 hrs · 23,424 cycles

APU SHUTOFF VALVE SHOWS OPEN BUT VERY LITTLE INCREASE IN DUCT PRESSURE. REPLACED PNEUMATIC CLUSTER.

Part: UNKNOWN — UNKNOWN (PNEUMATIC SYS) · airframe 81,277 hrs · 23,424 cycles

AFTER APU RESTART, NO PNEUMATIC DUCT PRESSURE WITH APU BLEED VALVE SHOWING OPEN.

Part: LIGHT — UNSECURE (CABIN) · airframe 81,249 hrs · 23,416 cycles

EMERGENCY LIGHT LOOSE AT L2 DOOR. SECURED LIGHT.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 81,218 hrs · 23,410 cycles

EMERGENCY LIGHT DAMAGED NEAR L2 DOOR FOUND COVER BROKEN AND LOOSE. REPLACED DAMAGE COVER AND SECURED.

Part: COMPUTER — FAILED (RT FCC) · airframe 81,216 hrs · 23,409 cycles

CREW REPORTED ELECTRICAL ODOR IN COCKPIT AND MID CABIN. TURNED OFF RIGHT RECIRCULATION FAN AND HAD F/A'S TURN OFF GALLEY POWER. ODOR DID DISSIPATE, SHORTLY THEREAFTER, LOST F/O FLIGHT DIRECTOR BARS AND RECEIVED A NO LAND III ASA. FOUND FCC BOX BURNED. RAN PACKS. NO ODOR OF SMOKE NOTED. ACFT OK FOR SERVICE.

Part: ACTUATOR — FAULTY (APU DOOR) · airframe 81,147 hrs · 23,390 cycles

APU DOOR STATUS MESSAGE, APU FAULTED. FOUND APU INLET ACTUATOR CIRCUIT BREAKER IN AFT BAY OPEN, RESET, OPENED APU DOOR FULLY. APU OIL LEVEL GOOD, 1 QT ADDED. CIRCUIT BREAKER TRIPPED TWICE ON SHUTDOWN WHEN DOOR CLOSING. SUSPECT ACTUATOR, REPLACED APU DOOR ACTUATOR.

Part: DOOR — BROKEN (RAM AIR EXHAUST) · airframe 81,101 hrs · 23,378 cycles

FLT DIVERTED. AIRFRAME VIBRATION CAN BE FELT THROUGHOUT THE CABIN AND IN FLT DECK ESPECIALLY AT FLOOR AREA. CHANGING AIRSPEED AND ALTITUDE-NO HELP. FEELS LIKE CONTINUAL LIGHT TURBULENCE WITH NONE REPORTED IN AREA, F/A REPORTS NORMAL WING APPEC. FELT MORE PROMINENT FWD OF THE WINGS. VIBRATION STOPPED DESCENDING THRU 21,000'. FOUND OUTLET ASSY RAM AIR EXHAUST DOOR BROKEN ON RIGHT PACK. REPLACED OUTLET ASSY RAM AIR EXHAUST.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 81,048 hrs · 23,366 cycles

EMERGENCY LIGHT COVER MISSING APPROX 5 FT BEHIND L2 DOOR. APPROXIMATELY 6-8 INCHES MISSING LEAVING EXPOSED STRIP. REPLACED EMERGENCY LIGHT CLEAR COVER AS REQUIRED.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 81,048 hrs · 23,366 cycles

EMERGENCY LIGHT COVER MISSING APPROX 5 FT BEHIND L2 DOOR. APPROX 6-8 INCHES MISSING LEAVING EXPOSED STRIP. REPLACED EMERGENCY LIGHT CLEAR STRIP AS REQUIRED.

Part: PSU — DAMAGED (CREW REST) · airframe 80,997 hrs · 23,351 cycles

PSU PANEL ABOVE 2L CREW SEAT DAMAGED. REPLACED PANEL ASSY.

Part: CONTROL UNIT — MALFUNCTIONED (GALLEY ELECTRIC) · airframe 80,912 hrs · 23,330 cycles

GALLEY ELCU TRIPS WHEN LOAD IS APPLIED BY EITHER HIGH TECH CARTS OR CHILLER. REPLACED ELCU REF CMM 25- 30-72 PG 117, 118 WIRING DIAGRAM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 80,892 hrs · 23,324 cycles

EMERGENCY LIGHT BETWEEN ROWS 22ABC AND 23 ABC INOPERATIVE. REPLACED LAMPS, OPS CHECKED GOOD.

Part: INDICATOR — FAULTY (AIRSPEED) · airframe 80,566 hrs · 23,243 cycles

CAPTAIN`S AIRSPEED INDICATOR ORANGE COMMAND BUG INOPERATIVE FLAG IN VIEW. REPLACED CAPTAIN'S MACH AIRSPEED INDICATOR PER AMM. OPS CHECKED GOOD.

Part: TRANSCEIVER — FAILED (NR 2 HF SYS) · airframe 80,490 hrs · 23,226 cycles

NR 2 HF WON`T TUNE ANY FREQ NR 2 HF FAILED PRIOR TO DEPARTURE, DD REFUSAL. REPLACED HF TRANSCEIVER PER AMM.

Part: LIGHT — INOPERATIVE (SEAT ROW 34) · airframe 80,467 hrs · 23,220 cycles

EMERGENCY LIGHT INOPERATIVE ADJACENT TO SEAT ROW 34. REPLACED EMERGENCY LIGHT. OP CHECKED GOOD.

Part: LIGHT — DIM (SEAT ROW 23) · airframe 80,467 hrs · 23,220 cycles

EMERGENCY LIGHT INTENSITY LOW, ADJACENT TO SEAT ROW 23. REPLACED EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 80,467 hrs · 23,220 cycles

EMERGENCY LIGHT COVER END CAP IS MISSING, ADJACENT TO SEAT ROW 8. REPLACED END CAP. INSPECTED INSTALLATION.

Part: LATCH — BROKEN (R4 SLIDE COVER) · airframe 80,382 hrs · 23,197 cycles

R4 DOOR SLIDE COVER HAS A BROKEN LATCH. REPLACED SLIDE COVER.

Part: MODULE — DAMAGED (START VALVE) · airframe 80,238 hrs · 23,159 cycles

RT ENGINE START VALVE LIGHT INOPERATIVE. SPRING IN LIGHT ASSY WEAK. REPLACED MASTER MODULE, TESTED OK ON ENGINE START.

Part: LINER — PUNCTURED (R1 DOOR) · airframe 80,159 hrs · 23,139 cycles

R1 DOOR UPPER LINING HAS A PUNCTURE. NO DAMAGE NOTED BEHIND UPPER LINING. FILLED HOLE AND SANDED SMOOTH.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 80,159 hrs · 23,139 cycles

EMERGENCY LIGHT COVER DAMAGE BY 8C. REPLACED COVER.

Part: ACCUMULATOR — LEAKING (BRAKE SYS) · airframe 79,647 hrs · 23,009 cycles

BRAKE PRESSURE FLUCUTATION , FLT DIVERTED. FOUND BRAKE ACCUMULATOR LEAKING ON NITROGEN SIDE. REPLACED PER MM.

Part: ACTUATOR — FAILED (INLET DOOR) · airframe 79,620 hrs · 23,000 cycles

APU FAILED AT GATE. APU INOPERATIVE. APU FAILED AT PUSHBACK. ACP BITE OF ECU FOUND INLET DOOR FAULT. ACP VISUAL AND AUDIBLE CK OF ACTUATOR AND CHECKED SECURITY OF DOOR OPEN SWITCH. STARTED APU SEVERAL TIMES AND LOADED APU. OPERATION NORMAL IAW AMM.

Part: BOLT — LOOSE (SEAT) · airframe 79,596 hrs · 22,992 cycles

LOOSE BOLT THAT SECURES SEAT 28DEF TO FLOOR. REMOVED SEAT ROW FROM TRACKS. INBOARD SEAT TRACK DAMAGED. INSTALLED NEW NUT AND STUD, RE-INSTALLED SEATS.

Part: TRANSCEIVER — FAULTED (WX RADAR) · airframe 79,570 hrs · 22,987 cycles

WEATHER RADAR OPS NORMAL BUT HAS RETURN AT 7 MILES THAT IS AN ARC THAT SHOWS IN ANY TILT CLEANED CONNECTOR ON WEATHER RADAR CONTROL PANEL, AND WEATHER RADAR ANTENNA. CHECKED FLAT PLATE, AND COMPONENTS. NO UNUSUAL DISCREPANCIES NOTED. CHECKED RADOME FOR ANY DELAMINATION, AND FOUND NONE PRESENT. RE-RACKED RADAR TRANSCEIVER. TESTED SYSTEM PER 757 AMM 34-43-00-501. SYSTEM OPERATED NORMAL.

Part: ISOLATION VALVE — FAULTY (BLEED) · airframe 79,525 hrs · 22,976 cycles

BLEED ISOLATION VALVE EICAS WHEN ISOLATION VALVE CLOSED. REPLACED ISOLATION VALVE, MM REF 36-11-04. ALSO AIR SUPPLY ISOLATION VALVE OPEN AND CLOSED RELAY K22 AND K21. ISOLATION VALVE OPS CHECKED NORMAL. REPLACED OVERHEAD ISOLATION BLEED SW CAP, MODULE AND CIRCUIT REF SSM.

Part: MICROPHONE — INOPERATIVE (O2 MASK) · airframe 79,454 hrs · 22,955 cycles

F/O O2 MASK MICROPHONE DOES NOT TRANSMIT TO F/O SPEAKER. REMOVED AND REPLACED RNP. OPS CHECKED GOOD. O2 MASK TRANSMITS NORMALLY.

Part: B-NUT — LOOSE (RUDDER) · airframe 79,046 hrs · 22,848 cycles

ON WALK AROUND, NOTICED HYD FLUID LEAKING FROM AFT END OF RUDDER. DURING ACCOMPLISHMENT OF SVC TIP FOUND B-NUT LOOSE, AND DRIPPING HYD FLUID ON RT YAW DAMP SERVO. TIGHTENED B-NUT, RAN RUDDER SEVERAL TIMES, NO NEW LEAKS NOTED. REF SVC TIP 22-21-02. ALSO RAN RUDDER WITH NORMAL HYD SYSTEM, NO LEAKS NOTED.

Part: STRUCTURE — LEAKING (FUEL TANK) · airframe 79,034 hrs · 22,844 cycles

WHILE PERFORMING ETOPS PDSC FOUND FUEL LEAKING FROM RT AC BAY, OPENED AC BAY ACCESS FOUND RT SIDE OF CENTER TANK BY AFT BULKHEAD LEAKING FUEL APPROX 60 DPM. APPLIED SEALANT TO AFT RT CORNER OF CENTER TANK CENTER BOX.AND APPLIED SEALANT TO O/B SIDE OF AFT CENTER BOX REF GPM 6-0-02-009. STILL NEEDS LEAK CHECK. ACP LEAK CHECK, NO LEAKS NOTED.

Part: CIRCUIT CARD — FAULTY (NR 2) · airframe 78,723 hrs · 22,756 cycles

LEFT ENGINE OVHT NR 2 LOOP, RTFL. ACCOMPLISHED HIGH POWER RUN, AFTER 3-5 MIN GOT STATUS MSG LEFT ENGINE OVERHEAT LP2, NO OVERHEAT LIGHT ON PANEL, MSG WENT OUT WHEN BLEED TURNED OFF, OR WHEN THROTTLE PULLED BACK TO APPROX 70 PERCENT N1. MAINT TEXT: SHOULD READ MSG LEFT ENGINE FIRE LP2 NO FIRE LIGHTS. REPLACED NR 1 ENGINE, UPPER CORE LOOP (#2) REF MM26-11-01-0401. NO HELP. MSG RETURNED DURING PWR RUN.

Part: CIRCUIT CARD — FAILED (BLEED SYS) · airframe 78,613 hrs · 22,728 cycles

BOTH PRSOV VALVES FAILED TO CLOSED. PERFORMED TEST. REPLACED NR 1 AND NR 2 ECS BLEED CARDS.

Part: CIRCUIT CARD — FAULTY (FIRE WARNING) · airframe 78,554 hrs · 22,716 cycles

STATUS MSG LEFT ENGINE FIRE LP2. REPLACED CARD M682, OPS CHECK OK PER MM 26-10-01.

Part: GENERATOR — FAULTY (APU) · airframe 78,554 hrs · 22,716 cycles

APU ELECTRICS DROPS OFF-LINE WITH LOAD. APU DROPS OFF LINE. REPLACED APU GENERATOR PER AMM, OPS CHECK GOOD. RAN APU WITH ALL HYDRAULIC, ALL PACKS ON. STARTED ENGINE AT GATE RAN APU FOR ONE HOUR. OPS CHECK GOOD.

Part: PCA — FAULTY (LT ELEVATOR) · airframe 78,296 hrs · 22,645 cycles

STATUS MSG L ELEV PCU AFTER LANDING. COMPLIED WITH SINGLE SYSTEM HYD TEST PER MEL 2721D. ACP BREAKOUT OF EACH PCA, FOUND LEFT INBOARD PCA BAD. NO PCA IN STOCK DEN. REPLACED LEFT INBOARD ELEVATOR PCA, OPS CHECK, LEAK OKAY.

Part: ELEVATOR — DAMAGED (RIGHT) · airframe 78,273 hrs · 22,638 cycles

OUTBOARD EDGE OF RIGHT ELEVATOR DAMAGED. REPLACED RIGHT ELEVATOR PER MM.

Part: CONTROL PANEL — FAULTY (AUTOPILOT) · airframe 78,076 hrs · 22,587 cycles

CENTER AUTOPILOT ENGAGED LIGHT ON WITH NO AUTOPILOT ENGAGED. REPLACED MODE CONTROL PANEL PER AMM, OPS CHECKED GOOD.

Part: FMC — FAULTY (LEFT) · airframe 78,012 hrs · 22,573 cycles

FMC & LOC DISAGREE, FLIGHT DIVERTED. REPLACED LEFT FMC COMPUTER, CROSSLOADED DATA, GND CHECK.

Part: LAVATORY — INOPERATIVE · airframe 77,998 hrs · 22,570 cycles

LAVATORY 132 AT DOOR 2L DOES NOT HOLD WATER. TOILET TANK DOES NOT HOLD PRECHARGE. TANK DRAINED AND DEACTIVATED. LAVATORY NOT USEABLE. LAVATORY TANK SERVICED FULL, DUMPED, AND SERVICED FULL AGAIN, HOLDS BLUE WATER, FLUSHES NORMALLY.

Part: CIRCUIT CARD — WRONG PART · airframe 77,903 hrs · 22,540 cycles

GENERATOR DRIVE DISCONNECT LIGHTS ON OVERHEAD PANEL ARE ILLUMINATED DIMLY, BUT GENS WORK NORMALLY. FOUND WRONG CIRCUIT CARDS INSTALLED ON DRIVE LIGHT SWITCHES (S1 AND S2). INSTALLED CORRECT (LED) CIRCUIT CARDS. DIM LIGHT WITH ENGINES RUNNING PROBLEM IS CORRECTED.

Part: CIRCUIT CARD — WRONG PART (GEN DRIVE) · airframe 77,903 hrs · 22,540 cycles

GEN DRIVE DISC LIGHTS ON OVERHEAD PANEL ARE ILLUMINATED DIMLY, BUT GENS WORK NORMALLY. FOUND WRONG CIRCUIT CARDS INSTALLED ON DRIVE LIGHT SWITCHES (S1&S2). INSTALLED CORRECT (LED) CIRCUIT CARDS. DIM LIGHT WITH ENGINES RUNNING PROBLEM IS CORRECTED.

Part: CONTROL HEAD — FAILED (ACARS) · airframe 77,872 hrs · 22,532 cycles

ACARS CONTROL HEAD ON PEDESTAL FAILS TO DIM BRIGHT CORRECTLY. REPLACED CONTROL HEAD PER AMM. OPS CHECKED GOOD.

Part: FRAME — CORRODED (BS 1400) · airframe 77,872 hrs · 22,532 cycles

AFT CARGO BAY LOWER BILGE STRUCTURE, FWD FACE OF FRAME EXFOLIATED BS 1400, BL 0 - RBL 24. REPAIRED BS 1400 FRAME WEB, BETWEEN S27R-S30 IAW REO-G15110 REV C & ECRA 5362-01022.

Part: FRAME — DAMAGED (BS 1400) · airframe 77,872 hrs · 22,532 cycles

AFT CARGO COMPARTMENT LOWER BILGE STRUCTURE, FWD FACE OF FRAME EXFOLIATED BS 1400, RBL 0-RBL 24. ACCOMPLISHED INTERIM REPAIR PER TIMCO REO-G15110 REV C AND ECRA 5362-01022. REPAIR BS 1400 FRAME WEB, BTWN S27R-S30 MUST RECEIVE NEW ACCOMPLISHED ON NR 40369. PLANNING-ECRA IS BEING EVALUATED FOR DMG TOLERANCE AND WILL LIKELY BE MADE PERMANENT WITH RPT INSP'S CONTACT EG AFTER 27JAN14, BUT BEFORE 27APR14.

Part: SKIN — CORRODED (BS 1393 S29-30L) · corrosion level 2 · airframe 77,872 hrs · 22,532 cycles

FUSELAGE SKIN CORRODED AT BS 1393, BETWEEN S29 - 30L, ACCOMPLISHED SKIN REPAIR BS 1393-1401 STR 28L AND 29R PER REO-G15092 REV A AND UA ECRA 5360-01214.

Part: FLOORBEAM — CORRODED (BS 1680) · corrosion level 2 · airframe 77,872 hrs · 22,532 cycles

AFT CABIN FLOORBEAM HAS CORROSION BS 1680 BL 0 - RBL 30. REPAIRED FLOORBEAM PER REO-G15097 REVC AND ECRA 5365-01067.

Part: STRUCTURE — DAMAGED (LT WING TE FLAP) · airframe 77,872 hrs · 22,532 cycles

LEFT WING INBOARD FLAP, OUTBOARD AFT FAIRING, FWD INBOARD MOUNT BRACKET HAS PULLED RIVETS AND ELONGATED HOLE. REPAIRED.

Part: SPRING — BROKEN (R4 DOOR SLIDE) · airframe 77,872 hrs · 22,532 cycles

R-4 DOOR ESCAPE SLIDE UPPER AFT BAYONET STRING BROKEN. REMOVED AND REPLACED SLIDE PER MM.

Part: TRIGGER — FROZEN (R4 DOOR) · airframe 77,872 hrs · 22,532 cycles

MAIN CABIN R-4 DOOR TRIGGER FORK IS FROZEN. REMOVED AND REPLACED TRIGGER FORK PER MM AND OPS CHECKED GOOD.

Part: FORK — FROZEN (L4 DOOR) · airframe 77,872 hrs · 22,532 cycles

MAIN CABIN L4 TRIGGER FORK ASSY IS FROZEN. MAJOR REPAIR ACCOMPLISHED, REMOVED AND REPLACED MAIN CABIN L4 TRIGGER FORK ASSY PER MM AND OPS CHECKED GOOD.

Part: SHEAR TIE — CORRODED (BS 1460 S28-29L) · corrosion level 2 · airframe 77,872 hrs · 22,532 cycles

AFT PIT BILGE FRAME TO SKIN SHEAR TIE CORRODED BS 1460, STR 28 - 29L. REMOVED SHEAR TIE AND FABRICATED A NEW SHEAR TIE PER BAC DWG 140N2002 AND INSTALLED PER BAC DWG 146N1014, REV. D AND SRM51-40-2. MAJOR REPAIR.

Part: SKIN — DENTED (BS 600 S15-16L) · airframe 77,872 hrs · 22,532 cycles

SKIN AT BS 600 HAS A SHARP DENT WITH A CREASE BETWEEN STR 15L AND STR 16L. REPAIRED PER SB 757-53A0092.

Part: SKIN — DENTED (BS 600 S15-16L) · airframe 77,872 hrs · 22,532 cycles

FUSELAGE SKIN AT BS 600 HAS A SHARP DENT WITH A CREASE BETWEEN STR 15L AND STR 16L. REPAIRED WITH SKIN PANEL INSTALLATION -WEIGHT CHANGE FOR THIS REPAIR IS 9.64 LB INCREASE. SCRIBELINE INSPECTION ACCOMPLISHED, BTW BS 439 TO 661 LH BUTT JOINTS AND SKIN LAPS S-14L AND S-19L

Part: SKIN — DENTED (BS 734 S21-22L) · airframe 77,872 hrs · 22,532 cycles

FUSELAGE SKIN DENTED BS 734, STR 21-22L. CUT-OUT DAMAGE AND FABRICATED AND INSTALLED A REPAIR DOUBLER PER REO G15109, REV B AND EC-RA NR 5331-01613.

Part: SHEAR TIE — CORRODED (BS 1400, S28-29L) · corrosion level 2 · airframe 77,872 hrs · 22,532 cycles

AFT PIT BILGE FRAME TO SKIN SHEAR TIE CORRODED. BS1400, STR28L-STR29L. SUPPLEMENTAL DATA UPDATE, REMOVED SHEAR TIE, REMOVED CORROSION AND REMAINING MATERIAL AFTER CLEAN-UP WITHIN LIMITS OF SRM 53-00-07 AND DWG 146N1011, AND REINSTALLED SHEAR TIE. MAJOR REPAIR

Part: FLOORBEAM — CRACKED (BS 700) · airframe 77,872 hrs · 22,532 cycles

MAIN DECK FLOORBEAM UPPER TEE CRACKED, BS 700, LBL 45.50. CUT-OUT DAMAGED SECTION OF T-CAP, AND FABRICATED A REPLACEMENT UPPER CHORD SECTION BETWEEN LBL 45.50 AND LBL 24.75 PRODUCTION SPLICE DUE TO CRACKS AT BOTH LOCATIONS AND INSTALLED. MAJOR REPAIR.

Part: FLOORBEAM — CRACKED (BS 700 LBL 45.5) · airframe 77,872 hrs · 22,532 cycles

MAIN DECK FLOORBEAM UPPER CHORD CRACKED, STA 700, LBL 45.5. CUT-OUT DAMAGED SECTION OF TEE, AND FABRICATED A REPLACEMENT UPPER TEE SECTION BETWEEN LBL 45.50 AND LBL 24.75 PRODUCTION SPLICE DUE TO CRACKS AT BOTH LOCATIONS, AND INSTALLED.

Part: FLOORBEAM — CRACKED (BS 700) · airframe 77,872 hrs · 22,532 cycles

MAIN DECK FLOORBEAM UPPER TEE CRACKED, BS 700, LBL 24.75. CUT-OUT DAMAGED SECTION OF TEE, AND FABRICATED A REPLACEMENT UPPER CHORD SECTION BETWEEN LBL 24.75 AND 45 PRODUCTION SPLICE DUE TO CRACKS AT BOTH LOCATIONS, AND INSTALLED.

Part: FLOORBEAM — CORRODED (BS 365.25) · corrosion level 2 · airframe 77,872 hrs · 22,532 cycles

MAIN CABIN FLOORBEAM TEE CORRODED BS 365.25, BL 0-RBL 41. CUT-OUT DAMAGED SECTION OF TEE PER SRMI. FABRICATED TWO REPAIR ANGLES AND TWO REPAIR STRAPS AND REPAIR ANGLE AND INSTALLED PER SRM. MAJOR REPAIR.

Part: FITTING — GOUGED (R1 DOOR SLIDE) · airframe 77,872 hrs · 22,532 cycles

MAIN CABIN R1 DOOR INBOARD AREA OF SLIDE BAYONET FITTING GOUGED. REMOVED AND REPLACED MAIN CABIN R1 DOOR SLIDE ASSY IAW AMM 25-66-01, OPS CHECKED DOOR IAW AMM 52-11-00. DOOR OPS CHECKED NORMAL.

Part: BEARING — WORN (L1 DOOR) · airframe 77,872 hrs · 22,532 cycles

MAIN CABIN L1 DOOR UPPER INBOARD GUIDE BEARING WORN. REMOVED AND REPLACED BEARING IAW AMM 52-11-00.

Part: BEARING — WORN (L1 DOOR) · airframe 77,872 hrs · 22,532 cycles

MAIN CABIN L1 DOOR UPPER OUTBOARD GUIDE BEARING WORN. REMOVED AND REPLACED BEARING IAW AMM,.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 77,872 hrs · 22,532 cycles

AFT CABIN FLOORBEAM HAS CORROSION ON TEE BS 1640, BL 0-RBL 60. CUT-OUT DAMAGED SECTION OF TEE AND FABRICATED TWO REPAIR ANGLES, TWO STRAPS AND REPAIR ANGLE AND INSTALLED PER SRM, REPAIR 3, FIG 201.

Part: FLOORBEAM — CORRODED (BS 324) · corrosion level 2 · airframe 77,872 hrs · 22,532 cycles

MAIN CABIN BS 324 FLOORBEAM TEE HAS CORROSION BETWEEN RBL 35-RBL 62. CUT-OUT DAMAGED SECTION OF TEE AND FABRICATED A NEW TEE AND SPLICE PER DWG 141N2932 AND INSTALLED PER SRM. MAJOR REPAIR.

Part: SKIN — DENTED (BS 620, S22L) · airframe 77,872 hrs · 22,532 cycles

FUSELAGE SKIN DENTED AT BS 620, STR 22L. CUTOUT DAMAGE AND CAT B REPAIR DOUBLER AND FILLER INSTALLED AT FUSELAGE BS 620, STR 22L IAW SRM 53- 00-01, FIG 201, REPAIR 2, TABLE 5.

Part: SKIN — DAMAGED (BS 511 S24L) · airframe 77,872 hrs · 22,532 cycles

EXTERNAL FUSELAGE SKIN DAMAGED BS 511, STR 24L. CUT-OUT DAMAGED SKIN AND FABRICATED A DOUBLER AND FILLER AND INSTALLED PER SRM 53-00-01, REPAIR 2 PER SRM 53-00- 01, RPR 2, FIG. 201 AND TABLE V.

Part: CAM — CORRODED (R1 DOOR) · airframe 77,872 hrs · 22,532 cycles

MAIN CABIN R1 DOOR UPPER AND LOWER CAM PLATES ARE RUSTY. REMOVED DOOR AND CAM PLATES PER MM. PAINT STRIPPED AND CAD PLATE STRIPPED, CADMIUM PLATED, AND REINSTALLED CAM PLATES AND DOOR PER MM.

Part: FITTING — GOUGED (L2 DOOR) · airframe 77,872 hrs · 22,532 cycles

MAIN CABIN L2 DOOR MID FRAME OUTBOARD GUIDE FITTING GOUGED. MAJOR REPAIR ACCOMPLISHED, REMOVED AND REPLACED MAIN CABIN L2 DOOR FRAME OTBD GUIDE FITTING IAW AMM. DOOR OPS CHECK GOOD.

Part: MOUNT BRACKET — DAMAGED (LT WING) · airframe 77,872 hrs · 22,532 cycles

LEFT WING INB FLAP, OTBD AFT FAIRING, FWD INBD MOUNT BRACKET HAS PULLED RIVETS & ELONGATED HOLE. ACCOMPLISHED A FREEZE PLUG STRAP REPAIR. ACFT WILL BECOME NON-AIRWORTHY ON OR BEFORE 20JUL14 UNLESS NEW 8100-9 RECEIVED.

Part: FITTING — GOUGED (L1 DOOR SLIDE) · airframe 77,872 hrs · 22,532 cycles

MAIN CABIN L1 DOOR SLIDE OUTBOARD BAYONET FITTING AREA DEEPLY GOUGED. REMOVED AND REPLACED MAIN CABIN L-1 DOOR SLIDE ASSY PER MM.

Part: BOLT — UNSECURE (RESERVOIR CABLE) · airframe 77,872 hrs · 22,532 cycles

MAIN CABIN L1 DOOR EMERGENCY POWER ASSIST PRESSURE RESERVOIR CABLE HAS LOOSE BOLT AT BOTTLE. SUPPLEMENTAL DATA UPDATE, SECURED MAIN CABIN L1 DOOR EMERGENCY POWER ASSIST PRESS RESERVOIR CABLE AND BOTTLE BOLTS PER MM ON NON ROUTINE 40240.

Part: LOCK — FAULTY (L1 DOOR) · airframe 77,872 hrs · 22,532 cycles

MAIN CABIN L1 DOOR HOLD OPEN ASSEMBLY CLUTCH WORN. REMOVED AND REPLACED MAIN CABIN L1 DOOR HOLD OPEN LOCK ASSY PER MM 52-11-08 ON NON ROUTINE 40215.

Part: ACTUATOR — FAILED (AILERON TRIM) · airframe 77,678 hrs · 22,481 cycles

ON TAXI OUT FLT CONTROL CHECK, AILERON MOVEMENT IS ABNORMAL. APPEARS HARDER THAN NORMAL TO MOVE AND DOES NOT RETURN TO CENTER, FROM EITHER CAPTAIN OR FIRST OFFICER POSITION. REPLACED AILERON TRIM ACTUATOR PER AMM 27-11-14. ADJUSTED FEEL AND CENTERING MECHANISIM SPRING TENSION PER AMM 27-11-00 ITM 11 P521. OPS CHECKED GOOD.

Part: SWITCH — DAMAGED (FIRE DETECTION) · airframe 77,618 hrs · 22,464 cycles

LEFT ENGINE OVERHEAT LIGHT DOES NOT ILLUMINATE DURING FIRE TESTS. REPLACED LEFT ENGINE OVERHEAT SWITCH BASE, FIRE TEST AND LIGHT TEST OK.

Part: CIRCUIT CARD — MALFUNCTIONED (BLEED SYSTEM) · airframe 77,550 hrs · 22,443 cycles

LEFT ENGINE BLEED OFF LIGHT ILLUMINATED WITH LT ENG BLEED OFF EICAS MESSAGE WITH ENGINE RUNNING. CYCLED BLEED SWITCH SEVERAL TIMES AND ENGINE POWER INCREASED TO 50% N1 TWICE WITH NO HELP. RESEATED LEFT ECS ENGINE BLEED CARD. PERFORMED PNEU SYSTEM TEST PER JRH 2-5-16. FOUND SYS TO BE OPERATING NORMAL.

Part: OXYGEN MASK — RUPTURED (FIRST OFFICER) · airframe 77,390 hrs · 22,388 cycles

INFLATABLE HARNESS ON F/O'S O2 MASK HAS RUPTURED. REPLACED F/O MASK AY, REF MM 35-11-51.

Part: ACTUATOR — LEAKING (RUDDER) · airframe 76,746 hrs · 22,194 cycles

HYDRAULIC LEAK AT RUDDER RATIO CHANGER ACTUATOR ROD SHAFT RUNNING LEAK. REMOVED RRCA. NEED TO INSTALL NEW UNIT MR27214-121 (MRDATA ENTERED).

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,604 hrs · 22,152 cycles

STA 1680 BETWEEN STR S30 AND S29 FRAME IS CORRODED. MAJOR REPAIR ACCOMPLISHED. RPLC'D FRAME SECTION STA 1680 STR 25L-25R DRWG 146N1025.

Part: CAP — MISSING (CABIN) · airframe 76,523 hrs · 22,129 cycles

EMERGENCY ESCAPE PATH LIGHTING STRIP END CAP MISSING 1L CLOSET & SEATS 6B, 8C & 40C. REPLACED LIGHTING STRIP END CAPS AT DOOR 1L CLOSET STRIP, 6B, 8C, AND 40C LOCATIONS. EMERGENCY PATH LIGHTS CK OK.

Part: FEEDER CABLE — DEFECTIVE (CABIN) · airframe 76,375 hrs · 22,084 cycles

EEL LTS FROM ROW 22 TO ROW 34 ARE INTERMITTENT. TAPPING ON THE EEL COVER WHERE POWER FEEDER CROSSES THE EEL BASE WILL CAUSE THIS SECTION TO FAIL. EQUIP CHANGE FOR THIS PROBLEM. REPLACED EEL LIGHT POWER FEEDER AT ROW 22, OPS CHECK OKAY.

Part: FEEDER CABLE — DAMAGED (CABIN) · airframe 76,375 hrs · 22,084 cycles

EEL LIGHT INOP AT LAV 2L DOOR. REPAIRED POWER FEEDER AND RE-INSTALLED EEL STRIP IN FRONT OF MID LAV DOOR. LIGHT CHECKS GOOD.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 76,357 hrs · 22,080 cycles

EEL LIGHT STRIP ADJACENT TO FIRST CLASS CLOSET IS DISCONNECTED. SECURED LIGHT STRIP CONNECTION AND COVER ADJACENT TO FIRST CLASS CLOSET. CKS OKAY. FOUND STRIP SECURE AND FUNCTIONING OKAY.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 76,093 hrs · 22,010 cycles

EMERGENCY LIGHTS INOPERATIVE. SPLICED FEEDER CABLE AND SECURED. OPS CHECKED OKAY.

Part: MODULATING VALVE — INOPERATIVE (CABIN TEMP) · airframe 75,857 hrs · 21,942 cycles

AFT CABIN TEMP INOPERATIVE IN AUTO. VERIFIED VALVE CLOSE BY PROCEDURE ONE (1). FAULT SHOWS AFT ZONE VALVE. REPLACED AFT CABIN MODULATING TRIM AIR VALVE PER AMM. OPS CHECKED NORMAL.

Part: SKIN — DENTED (RT WING LE) · airframe 75,743 hrs · 21,906 cycles

ON INSPECTION OF FIXED LEADING EDGE, UNDER RT INBOARD SLAT NR 6 FOUND DAMAGED. TWO, SIX INCH OVAL DENTS MEASURING 1-4 INCH DEEP IN COMPOSITE STRUCTURE. REPAIRED PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 75,743 hrs · 21,906 cycles

CREW REPORT: SKIN DELAMINATION ON RT INBD SLAT. ABOUT 12 INCH PIECE CAME OFF DURING CLMB. NO ADVRS CNTR. SAMC TEXT: CREW REPORTS NO VIBRATION FELT AND NO AIRCRAFT TRIM NEEDED. MAINT TEXT: RT INBOARD LEADING EDGE SLAT HAS A LARGE AREA AT THE TRAILING EDGE OF SLAT MISSING AND DELAMINATED. REMOVED INBD RT SLAT. TWO 6 IN OVAL DENTS MEASURING 1-4 IN DEEP IN COMPOSITE STRUCTURE. ACCOMPLISHED ALL REPAIRS PER SRM. ACCOMPLISHING RPR F-N 119069, F-N 118471, AND F-N 105607. INSTALLED NEW SLAT.

Part: SENSOR — OBSTRUCTED (R4 DOOR) · airframe 75,713 hrs · 21,896 cycles

DOOR 4R 'ARMED' LIGHT INOP. CLEANED DEBRIS FROM GIRT BAR SENSORS, OPS CHECKS GOOD.

Part: CARBON SEAL — LEAKING (NR 1 ENGINE) · airframe 75,698 hrs · 21,891 cycles

NR 1 ENG FUEL PUMP CARBON SEAL LEAKING OIL OUT OF DRAIN. REPLACED CARBON SEAL PER MM.

Part: LANYARD — LOOSE (GIRT BAR) · airframe 75,623 hrs · 21,869 cycles

UNABLE TO ARM 4R. SECURED LOOSE GIRT BAR CORD.

Part: EXHAUST VALVE — FAULTY (NR 1) · airframe 75,566 hrs · 21,850 cycles

OVBD EXHAUST VALVE TEST STATUS MSG ON. REPLACED OVBD EXHAUST VALVE, CHECKS OKAY.

Part: ACTUATOR — NO TEST (FUEL SYSTEM) · airframe 75,556 hrs · 21,846 cycles

AFT CROSSFEED VALVE WILL NOT TEST OPEN. CLEANED AND SECURED CONNECTOR AND GROUND CHECK NORMAL. CREW REPORT: AFT FUEL XFEED INOP REPEAT WRITEUP. VALVE SECURED IN CLOSED POSITION. -INF- :REPLACED RELAY K10714, NO HELP. XFEED ACTUATOR HAS STRIPPED SCREW. COULDN'T REMOVE. NEEDS ACTUATOR. REPLACED AFT XFEED ACTUATOR PER MM, OPS CHECK GOOD.

Part: LEVER — FAULTY (RUDDER PEDAL) · airframe 75,531 hrs · 21,840 cycles

CAPT RUDDER ADJ KNOB SLIPS WHEN APPLYING PRESSURE. REPLACED RUDDER PEDAL CRANK LEVER.

Part: FILTER — ODOR (CABIN) · airframe 75,441 hrs · 21,817 cycles

BAD ODOR OVER ENTIRE CABIN AND COCKPIT, DURING FLT AND ON GROUND. REPLACED RECIRCULATION FILTER IAW AMM.

Part: CIRCUIT BREAKER — FAULTED (FUEL SYSTEM) · airframe 75,395 hrs · 21,801 cycles

FUEL CROSSFEED LIGHT REMAINED ON WHEN OPEN-CLOSE SELECTED. RESET BREAKER AND RECONNECTED CONNECTOR TO AFT FUEL CROSSFEED ACTUATOR, AFT FUEL CROSSFEED CHECKED OKAY PER MM.

Part: COMPRESSOR BLADE — BENT (RT ENGINE) · airframe 75,381 hrs · 21,795 cycles

INGESTED RED TAIL HAWK IN RT ENGINE. DURING INSPECTION BIRD STRIKE OF RT ENG FOUND ONE FAN BLADE TIP BENT OUT OF LIMITS. REMOVED DAMAGED BLADE AND 2 OTHERS TO FACILITATE REPAIR TO ACOUSTIC LINING BEHIND FAN BLADES. REPLACED DAMAGED BLADE AND OPPOSITE AND RE-INSTALLED 2EA REMOVED BLADES.

Part: SHOULDER BELT — FRAYED (COCKPIT) · airframe 75,353 hrs · 21,785 cycles

CAPTAIN'S RT SHOULDER HARNESS BEGINNING TO FRAY. REPLACED CAPTAIN'S SEAT INERTIA REEL.

Part: DOOR — CORRODED (MID LAV SERVICE) · corrosion level 2 · airframe 75,366 hrs · 21,790 cycles

MID LAV SERVICE PANEL DOOR HAS 1.5 INCH CORROSION BLISTER ON BOTTOM EDGE. DOOR IS INTACT AND CLOSED PROPERLY AND LATCHED. PANEL HAS EXTENSIVE CORROSION. REPLACED DOOR ASSY AND INSTALLED 143N3417-2 BRACKET AND PLACARDS.

Part: DUCT — CRACKED (RT A/C PACK) · airframe 75,303 hrs · 21,772 cycles

DURING TROUBLE SHOOTING OF LEFT & RIGHT PACK ISSUES FOUND REHEATER INLET DUCT ASSY CRACKED AT WELD. REMOVED CRACKED DUCT AT FWD END OF RT SECONDARY HEAT EXCHANGER TO REHEATER. INSTALLED DUCT. OPS CHECK OF PACK GOOD.

Part: ACTUATOR — FAULTY (ELEVATOR) · airframe 75,245 hrs · 21,754 cycles

ON FINAL APPROACH, STATUS MESSAGE FORELEVATOR ASYMETRY. ACCOMPLISHED FIM TSK 27-09-00 PG 161, BOTH SAMS SHOW YELLOW FAULT BALL AFTER THEIR RESPECTIVE TESTS. REPLACED ELEVATOR ASYMMETRY LIMITER ACTUATOR PER MM.

Part: LANYARD — DAMAGED (L1 DOOR) · airframe 74,953 hrs · 21,672 cycles

DOOR 1L WILL NOT ARM. REPAIRED SLIDE COVER LANYARD.

Part: CONTROL VALVE — FAULTY (TE FLAP) · airframe 74,829 hrs · 21,637 cycles

T/E FLAP VIBRATION. VIBRATES FROM 5 TO 1 DEG. REPLACED TRAILING EDGE PDU CONTROL VALVE (P/N S251N404-2; S/N 88), BYPASS VALVE, SHUTOFF VALVE, NO HELP. TE FLAP POWER DRIVE UNIT REPLACED (P/N S251N404-2 - DASH# 88) AND TE PDU CONTROL VLV, BYPASS VLV SHUTOFF VLV REPLACED, FLAPS OPERATE NORMAL WITH NO VIBRATION OR HUM.

Part: LEVER — BINDING (R4 DOOR) · airframe 74,560 hrs · 21,552 cycles

DOOR 4R WILL NOT ARM. FOUND DOOR ARMING LEVER BINDING. REMOVED SLIDE AND LUBED ALL HINGE POINTS AND PUSHRODS. REINSTALLED SLIDE, OPS CHECKED GOOD.

Part: DUCT — DAMAGED (CABIN) · airframe 74,479 hrs · 21,523 cycles

FLT ATTENDANT REPORTED LOUD NOISE AT ROW 11. FOUND OVERHEAD DISTRIBUTION DUCT DAMAGED AND CRACKED AT PREVIOUS REPAIR. REPLACED CRACKED VENT AND REPAIRED DAMAGE TO DUCT NOZZLE ATTACH POINTS. RAN PACKS AFTER REPAIRED & NO LOUD NOISES HEARD.

Part: D-RING — UNSECURE (EVAC SLIDE) · airframe 74,328 hrs · 21,477 cycles

DOOR 1L SLIDE PACK D-RING NOT VISIBLE. SECURED D-RING AND SLIDE COVER.

Part: TRANSCEIVER — FAULTY (WEATHER RADAR) · airframe 74,171 hrs · 21,434 cycles

WX RADAR DOES NOT PAINT ON THE 10 20 40 MILE SCALES, TEST OKAY. REPLACED W-R TR PER MM, GROUND WEATHER RADAR INDICATIONS NORMAL.

Part: UNKNOWN — VIBRATION (TE FLAP) · airframe 74,071 hrs · 21,410 cycles

VERY HEAVY VIBRATION ON FLAP RETRACTION AT FLAPS 1 COMING THROUGH HANDLE.

Part: CIRCUIT CARD — FAULTY (STARTING SYS) · airframe 74,066 hrs · 21,408 cycles

LEFT ENG STARTER WILL NOT HOLD IN GND. LT START HOLD-CUTOUT START SYSTEM INOP. MANUAL HOLD PROCEDURES APPLY. INSTALLED NEW LEFT ENGINE SPEED CARD M10298 PER MM. ACCOMPLISHED LT ENG START AFTER SPEED CARD REPLACEMENT. START HOLD FUNCTION CHECK TESTED GOOD.

Part: ACTUATOR — INOPERATIVE (FUEL SYSTEM) · airframe 73,742 hrs · 21,301 cycles

AFT (UPPER) FUEL XFEED SWITCH 'VALVE' LIGHT INOPERATIVE. MM COMMENTS: TOP FUEL CROSSFEED VALVE LIGHT DOES NOT COME ON WHEN ACTUATED. LIGHT INOP, CONFIRMED OPERATION PER MEL. FOUND WRONG SWITCH INSTALLED. NEEDS LENS CAP 563-3644, MASTER MODULE 563-3385 & CIRCUIT CARD 563-3969. LENS CAP NON STOCK SEATTLE. POST COA 505010. FWD CROSS FEED VALVE LIGHT IS INTERMITTENT. NEEDS SAME PARTS AS AFT CROSSFEED VALVE. LENS CAP NON-STOCK SEATTLE. VERIFIED BOTH CROSSFEED VALVES OPERATE PER MEL. REPLACED ACT PER MM. LIGHT AND ACT OPS CHECK OK NOW.

Part: PRESSURE SWITCH — FAULTY (HYDRAULIC SYS) · airframe 73,734 hrs · 21,301 cycles

LEFT ELECTRIC HYDRAULIC LOW PRESSURE LIGHT DOES NOT ILLUMINATE WITH SWITCH OFF. LIGHT TESTS OKAY. VERIFIED SYS LOW PRESS INDICATIONS ARE GOOD AND HYD PAGE SHOWS 3000 LBS PRESS WITH LEFT ELEC PUMP ON PER MEL. NEED LEFT SYSTEM LOW PRESS SW. (NON STOCK LAX). REPLACED PRESS SWITCH PER MM, OPS CHECK OKAY.

Part: HEAT EXCHANGER — DAMAGED (AC PACK) · airframe 73,461 hrs · 21,221 cycles

PRIMARY HEAT EXCHANGER IS DAMAGED AT INTAKE DUCT, HAS DENT POSSIBLE CRACK. THE COOLING FINS HAVE HEAT DAMAGE & EXFOLIATION. SOME FINS APPEAR TO BE WELDED TOGETHER. ACCOMPLISHED REMOVAL OF PRIMARY AND SECONDARY HEAT EXCHANGER PER MM. REPLACED PRI & SEC HEAT XCH PER AMM DUE TO CRACKED HEAT XCHG. RAN RT PACK, OPS CHK NORMAL

Part: HEAT EXCHANGER — CRACKED (AC PACK) · airframe 73,461 hrs · 21,221 cycles

RIGHT PACK SECONDARY HEAT EXCHANGER IS CRACKED OPEN ON TOP SIDE. ACCOMPLISHED REMOVAL OF PRIMARY AND SECONDARY HEAT EXCHANGER PER MM. REPLACED PRI & SEC HEAT XCH PER AMM DUE TO CRACKED HEAT XCHG. RAN RT PACK, OPS CHK NORMAL

Part: IDG — FAULTY (RIGHT) · airframe 73,424 hrs · 21,209 cycles

R GEN TRIPPED OFF AFTER LANDING. FOUND RT IDG OVERSERVICED AND REPLACED RT GCU. REACTIVATED PER MEL RAN ENG SYS. OPERATED NORMALLY.

Part: VALVE — FAULTY (BLEED AIR SYS) · airframe 73,328 hrs · 21,177 cycles

ENG DUCT PRESSURES SPLIT DURING CRUISE WITH ISOL VLV CLOSED & BLEED SW SELECTED ON. RECORD DUCT PRESSURES. CREW COMMENTS: LEFT 45 PSI RIGHT 30 PSI CRUISE AT 26000FT. APPLIED MEL 3611A. REPLACED HIGH STAGE PILOT VALVE PER AMM. RAN ENGINE AT HIGH POWER PER JRH. VALVE CHECKS NORMAL AND ALL INDICATIONS OKAY.

Part: GCU — FAULTY (LT GENERATOR) · airframe 73,159 hrs · 21,126 cycles

LEFT GEN DRIVE LIGHT ON OVHD PANEL NOT ILLUMINATED. NO AMIS HISTORY. BPCU FAULT WAS "REPLACE L ENG GCU". REPLACED LT ENG GCU. RAN ENG AT GATE AND DRIVE LIGHT OPERATION WAS NOW NORMAL WITH NO OTHER FAULTS NOTED.

Part: UNKNOWN — NOISY (COCKPIT) · airframe 72,969 hrs · 21,072 cycles

COCKPIT EXTREMELY LOUD WITH OR W/O RT REC FAN ON. TOO MUCH AIRFLOW FROM VENTS ABOVE WINDOWS. COMPARED FLIGHT DECK NOISE TO OTHER ACFT ON THE FIELD, SOUND LEVEL VERY COMPARABLE, ALSO FLIGHT DECK NOISE LEVEL IS REDUCED WITH RT RECRIC FAN OFF. CLEANED CABIN DUCTS. INBOUND DECIBLE READINGS 73 WITH RT FAN OFF 76 WITH BOTH FANS AFTER CLEANING 71 RT FAN OFF 73 BOTH FANS ON.

Part: START VALVE — INOPERATIVE (NR 2 ENGINE) · airframe 72,545 hrs · 20,954 cycles

CREW REPORTED NR 2 ENG DOES NOT ROTATE WHEN START VALVE IS OPENED. START VALVE LIGHT CAME ON AND WENT OUT, BUT NO ROTATION. OPERATED START VALVE MANUALLY. REPLACED START VALVE.

Part: DRAIN — CLOGGED (WASTE WATER) · airframe 72,500 hrs · 20,941 cycles

ICE FOUND IN THE LOWER E/E AND NOSE TUNNEL BILGE AREA. GRAY WATER HAS BEEN SUCTIONED OUT AND DRIED. ALSO, DRAIN LINE HAS BEEN UNCLOGGED.

Part: SELECTOR PANEL — FAILED (AUDIO) · airframe 72,276 hrs · 20,878 cycles

NR5 YOKE & GLARESHIELD PUSH-TO-TALK SW ARE DEFECTIVE BUT ASSOC AUDIO SEL PNL PUSH-TO-TALK SW IS OK. (04=CAPT, 05=1ST OFF). CREW COMMENTS: F/O NO SIDETONE ON PA. VHF NORMAL. REPLACED F/O AUDIO SELECTOR PANEL. FOUND PA AUDIO WORKING NORMALLY AT SPEAKER AND MINITEL BUT REPLACED AS A PRECAUTION. CHECKS OK.

Part: GCU — FAILED (LEFT) · airframe 72,263 hrs · 20,873 cycles

LEFT GEN DRIVE LIGHT NOT ILLUMINATED. LIGHT TESTS GOOD. REPLACED LT GCU.

Part: PCA — MALFUNCTIONED (SPOILERS) · airframe 72,244 hrs · 20,868 cycles

SPOILERS EICAS MSG FAULT IS HITTING PCA FOR MOD 1R. REPLACED SCM. NO HELP STILL HITTING PCA ON 1R SUSPECT THE PCA ON RT SIDE AS WHEN DOING OPS CHECK ALWAYS FAILS WHEN TURNING CONTROL WHEEL TO RT SIDE. REINSTALLED OLD SCM FAULT IS ON FLT SPOILERS 2 OR 11. REPLACED NR11 SPOILER PCA IAW MM, OPS CK OK. NO SPOILER LIGHT, NO EICAS MESSAGES & NO FAULT BALLS.

Part: ACTUATOR — FAULTY (STAB TRIM) · airframe 72,019 hrs · 20,800 cycles

STABILIZER TRIM BALLSCREW ACTUATOR NEEDS TO BE REPLACED. REMOVED OLD ACTUATOR. TRANSFERRED HYD MOTORS FROM OLD ACTUATOR TO NEW REF AMM. TRANSFERRED SECONDARY BRAKES FROM OLD ACTUATOR TO NEW REF AMM.

Part: MODULE — FAULTY (STAB) · airframe 72,019 hrs · 20,800 cycles

FOUND RIGHT STABILIZER POSITION MODULE BAD. PART ON ORDER REF OSTF U5770. COMING FROM ORD 22NOV 10. REPLACED RT 'STCM' PER MM. LEAK AND OPS CKD PER ITM 3H. STAB TRIM STILL SLOW WITH EICAS MSG 'STAB TRIM' 2 UNITS NOSE DOWN USING PICKLE SW'S. SINGLE SYS INOP IN RT MODE (CNTR CUTOUT). SAME COND AS LOG 1. ALL OTHER OPS AND LK CKS GOOD ON STCM INSTALLATION MM.

Part: SWITCH — DIRTY (CABIN) · airframe 72,019 hrs · 20,800 cycles

RT RECIRCULATION FAN MUST BE TURNED OFF TO COMMUNICATE AND HEAR THE RADIOS. ACP SERVICE TIP MM FAILED STEP 6. FLOW WAS 480 CFM SHOULD BE LESS THEN 375 CFM. VELOCITY WAS 5500 FPM SHOULD BE 3430 FPM. CLEANED DUCTS AFTER ALT SWITCH REPLACED. RAN TEST READINGS CFM 363 AND FPM 3347 DECIBEL READING WITHIN LIMITS, OK FOR SERVICE. REPLACED LT FCV, COCKPIT STILL NOISY. PRIOR TO CHANGING ALT SWITCH, ACCOMPLISHED TEST OF BOTH PACK CONTROLLERS PER MM. NO FAULTS FOUND. REPLACED LT ALT SWITCH PER MM. ACCOMPLISHED TEST, NO FAULTS FOUND. CLEANED DUCTS AFTER ALT SWITCH REPLACED. RAN TEST READINGS CFM 363 AND FPM 3347 DECIBEL READING WITHIN LIMITS. OKAY FOR SERVICE.

Part: VALVE — ACTIVATED (WARMER) · airframe 72,019 hrs · 20,800 cycles

FLIGHT DECK WARMER THAN SELECTED WITH SWITCH ON AND TEMP CONTROL IN AUTO INOP, LIGHT EXTINGUISHING. PRESS ECS REC BUTTON AND RECORD ZONE TEMPS. NEED FURTHER TROUBLESHOOTING USED PROCEDURE 1 PER MEL 2161E TRIM VALVE CLOSED ON EICAS. REPLACED FLIGHT DECK TRIM AIR MODULATING VALVE, OPS CHECK OKAY.

Part: ACCESS PANEL — DAMAGED (CARGO BAY) · airframe 71,734 hrs · 20,720 cycles

AFT CARGO BAY SMOKE DETECTOR ACCESS PANEL DAMAGED BY NESTING SYS. REPAIRED, STRAIGHTENED PANEL AND RESECURED AND RETAPED.

Part: RADAR — FAILED (WX SYSTEM) · airframe 71,725 hrs · 20,718 cycles

WEATHER RADAR FAIL DISPLAYED ON HSD DURING TAXI BUT TESTED OKAY DURING PREFLIGHT. WX RADAR FOUND FAULTY. REPLACED RIGHT UNIT PER MM. OPS NORMAL.

Part: TURBINE BLADES — CRACKED (STAGE 3) · airframe 71,609 hrs · 20,683 cycles

NR2 ENG STAGE 3 LPT HAS 1 EACH BLADE WITH SULFIDATION AND CRACKED BLADE AT SULFIDATION AREA. CRACK LOCATED ON CONCLAVE SIDE OF BLADE. ENG NOT SERVICEABLE IAW MM. R & R ESN 726686 WITH ESN 726538 IN POS 02 IAW AMM.

Part: ACTUATOR — LEAKING (NR 6 SPOILER) · airframe 71,439 hrs · 20,633 cycles

HYD LEAK FOUND ON ARRIVAL, FOUND NR6 SPOILER LEAKING STEADY STREAM WHEN IN THE DOWN POSITION. R & R NR6 SPOILER ACTUATOR AND ALL OPERATIONS NORMAL AND ADJUSTMENTS COMPLETED.

Part: VALVE — FAULTY (HYD SYSTEM) · airframe 71,429 hrs · 20,631 cycles

ON TAXI OUT, HAD INTERMITTENT C FLT CONT HYD EICAS MESSAGE. SECURED VALVE OPEN IAW MEL. OFF LIGHT ON C FLT CONTROL SWITCH LIGHT INOP. REPLACED CENTER VALVE. OPS NORMAL.

Part: START VALVE — FAILED (NR 1 ENGINE) · airframe 71,280 hrs · 20,577 cycles

NUMBER 1 ENGINE FAILED TO START, NO N2 ROTATION WITH START VALVE LIGHT ILLUMINATED. REPLACED NR 1 ENG STARTER CONTROL VALVE. OPS AND LEAK CHECK GOOD.

Part: ACTUATOR — READS HIGH · airframe 71,276 hrs · 20,576 cycles

TOTAL FUEL DIFFERS FROM FMC QTY WITH NORMAL FLOW. RT FUEL QTY GAUGE READS 1500 LBS HIGH AT QTYS LESS THAN 28000 LBS TOTAL. AFT CROSSFEED VALVE ACTUATOR RUNS BUT WILL NOT DRIVE VALVE. WILL NEED ACTUATOR. EXISTING ACTUATOR, DATA PLATE FELL OFF (PN S343T003-14) (SN N82284). REPLACED AFT CROSSFEED ACTUATOR AND CHECKS OK. REPLACED FUEL QTY IND ASSY FUEL QTY SYS. TESTED NORMAL. REQUEST OUT-BOUND CREW COMMENT. REOPENED BY OPBLM ON 14SEP10 FOR: PROBLEM STILL THERE. BITE CHECK FUEL QTY PROCESSOR AND FOUND RT MAIN TANK COMP OPEN LO Z OR HI Z WIRE. FAULT ACTIVE. WILL NEED TANK ENTRY. REPLACED FUEL QTY PROCESSOR IAW MM. FUELING PANEL INDICATORS AND FLIGHT DECK CHECK OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LGIHT) · airframe 71,120 hrs · 20,526 cycles

DOOR 3L EMERGENCY EXIT LIGHT OUT. ACTUAL POSITION IS ABOVE DOOR 4L. FOUND DEAD BATTERY PACK AND REPLACED BATTERY PACK, OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,120 hrs · 20,526 cycles

AFT GALLEY AREA, 2 EACH VERTICAL FLUORESCENT EXIT SIGNS, 1 EA AT DOOR 4L AND 4R, INOP. REPLACED BATTERY PACK ON NON ROUTINE 2224N0037 AND OPS CHECK GOOD IAW MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,120 hrs · 20,526 cycles

CENTER GALLEY EMERGENCY EXIT LIGHT INOP. IAW CREW, THE EXIT LIGHT IS AT THE AFT GALLEY AREA, OVERHEAD CEILING, CENTER AISLE. REPLACED BATTERY PACK AND OPS CHECK IS GOOD AND INSPECTED.

Part: LIGHT — MISINSTALLED (CABIN) · airframe 71,119 hrs · 20,525 cycles

MAIN CABIN EMERGENCY LIGHTING ORANGE STRIP IS IN WRONG POSITION. SHOULD BE BETWEEN SEAT 14 AND 15ABC AISLE FWD OVERWING EXIT. ACP SMC003 ON NR CARD 5R53 I8040 BY EMP 600428. REPOSITIONED ORANGE STRIP BETWEEN SEATS 14 AND 15 ABC AISLE FWD OVERWING EXIT.

Part: LIGHT — MISSING (CABIN) · airframe 71,119 hrs · 20,525 cycles

MAIN CABIN EMERGENCY LIGHTING ORANGE STRIP MISSING AT AFT LT OVERWING EXIT AISLE BETWEEN SEAT 15-16ABC. ACCOMPLISHED SMC004 ON NR CARD 5R53 I8040. REPLACED EMERGENCY LIGHTING ORANGE STRAP AT AFT LT OVERWING EXIT AISLE BETWEEN SEAT 15 AND 16 ABC.

Part: HEAT EXCHANGER — FAULTY (LT A/C PACK) · airframe 71,119 hrs · 20,525 cycles

LEFT PACK HEAT EXCHANGERS FAULTY - REMOVED AND REPLACED LT PACK HEAT EXCHANGERS.

Part: VALVE — OUT OF TOLERANCE (LEFT RECIRC FAN) · airframe 71,109 hrs · 20,520 cycles

THE RT RECIRCULATION FAN IS PARTICULARLY LOUD ON THIS AIRPLANE. REF SERVICE TIP MM, ACCOMPLISHED STEP 6. TEST FAILED. REF STEPS 1 THRU 5 OF SERVICE TIP. ALREADY ACCOMPLISHED. ACCOMPLISHED DUCT CLEANING. DECIBEL READING WITHIN LIMITS. CFM 370 AND FPM 3357 WITHIN LIMITS AT THIS TIME. REPLACED LT FLOW CONTROL VALVE AND RECIRCULATION FILTERS.

Part: DUCT — DAMAGED (AIR DISTRIBUTION) · airframe 70,952 hrs · 20,475 cycles

OVAL AIR DISTRIBUTION DUCT HAS DAMAGE. SECTION OF OVAL AIR DISTRIBUTION DUCT REMOVED AND SENT TO SHOP FOR REPAIR. STARTED RE-INSTALLATION OF DUCT. INSTALLED 4 OF 4 MOUNTING BOLTS. INSTALLED 2EA VENT HOSES AND TAPED. DUCT SECTION READY FOR FIBERGLASS SPLICE REPAIR AT FWD AND AFT ENDS. SPLICE REPAIR COMPLETE. NEED LEAK CHK AFTER DUCTS INSTALLED. REPAIRED IAW MM.

Part: INSULATION — DAMAGED (BS 800) · airframe 70,952 hrs · 20,475 cycles

CROWN INSULATION WORN DAMAGED AT AREA OF BLOWN CEILING DUCT STA 800. REPLACED DAMAGED SECTION OF INSULATION.

Part: BATTERY — FAULTY (MASTER) · airframe 70,952 hrs · 20,475 cycles

MAIN BATTERY CHARGER STATUS MESSAGE UNABLE TO CLEAR. REPLACED MAIN BATTERY CHARGER. REPLACED MAIN BATTERY. TESTS OF CHARGER AND BATTERY ARE OK.

Part: FUEL CONTROL — LEAKING (NR 1 ENGINE) · airframe 70,797 hrs · 20,434 cycles

NR 1 ENG FUEL LEAKING FROM AFT OF FUEL CONTROL ON ENG RUN. REPLACED NR 1 ENG FCU, OPS AND LEAK CHECKS OKAY.

Part: VALVE — LEAKING (SLATS) · airframe 70,801 hrs · 20,435 cycles

HYD LEAK FROM L/E SLAT BYPASS VALVE JUST FWD OF THE LT PACK BAY. ACCOMPLISHED REMOVAL OF SLAT BYPASS VALVE IAW AMM. CONTINUE AT STEP 3 INSTALL THE BYPASS VALVE FOR THE L/E SLAT TO THE END. COMPLETED FROM STEP 3 TO COMPLETION. INSTALLED L/E SLAT BYPASS VALVE. LEAK CHECK AND OPS CHECK GOOD IAW MM.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 70,020 hrs · 20,227 cycles

SMOKE SMELL ON COFFEE MAKER AFT GALLEY LT SIDE UNIT SHUTOFF AND NO SMELL OR SMOKE. SAMC TEXT: CB FOR COFFEEMAKER WAS PULLED. CHILLER CBS WERE PULLED PRECAUTIONARY. REPLACED COFFEEMAKER POS M41 AND M42. F/A REPORTED SMOKE EMANATED FROM COFFEE MAKER AT POS M41. REPLACED BOTH M41 AND M42 AS PRECAUTION. INSPECTED WIRING BEHIND COFFEE MAKERS AND POWER PANEL FOR COFFEE MAKERS AND CHILLERS.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 69,827 hrs · 20,168 cycles

EMERGENCY LIGHT AT THE MID LAV INOPERATIVE. MADE PERMANENT REPAIR TO LIGHT ASSY PIGTAIL.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 69,827 hrs · 20,168 cycles

EMERGENCY LIGHT AT THE FWD AFT LAV INOPERATIVE. SECURED LIGHT CONNECTION.

Part: CONTROLLER — MALFUNCTIONED (APU) · airframe 68,989 hrs · 19,926 cycles

APU WOULD NOT START. CONTROLLER MALFUNCTIONED. REPLACED APU CONTROLLER, OPS CHECK OF APU OKAY.

Part: UNKNOWN — UNKNOWN (FUEL SYSTEM) · airframe 68,788 hrs · 19,867 cycles

FUEL OVERBURN IN EXCESS OF 4,200 POUNDS. WINDS WERE AS FORECAST. CONFERRED WITH ENGINE CONTROLLER. NO UNUSUAL FAULTS NOTED ON ECM. FUEL BURN AND VALVE OPERATION NORMAL. FLEET CONTROLLER AND DISPATCHER CONFERRED WITH. NO PRIOR HISTORY. CREW WILL SEND ABNORMAL FUEL BURNOUT REPORT. STUCK TANKS AFTER FUELING AND FUEL QTY ON STICKS READ WITHIN TOLERANCES.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 68,657 hrs · 19,825 cycles

FLOOR EMERGENCY LIGHT STRIP UNPLUGGED LAST ROW OF ECONOMY CABIN. FOUND PLUG UNSECURE. SECURED EMERGENCY LIGHT STRIP PLUG, OPS TEST OK.

Part: GIRT BAR — CLOGGED (R3 DOOR) · airframe 68,152 hrs · 19,686 cycles

AT GATE DOOR 3R WILL NOT DISARM. CLEANED PLASTIC WATER BOTTLE CAP OUT OF GIRT BAR SLIDE INTO ATTACHMENT POINT OF DOOR SILL. OPENED AND CLOSED DOOR A FEW TIMES AND ARMS AND DISARMS NORMAL NOW. LEFT IN DISARMED POSITION WHEN LEFT ACFT.

Part: ACTUATOR — LEAKING (FUEL SYSTEM) · airframe 67,330 hrs · 19,461 cycles

FUEL LEAKING FROM APU FUEL SHUTOFF VALVE IN LEFT MLG WHEEL WELL. REPLACED APU FUEL SHUT OFF VALVE. ALSO REPLACED APU FUEL SHUT OFF VALVE ACTUATOR.

Part: GENERATOR — MALFUNCTIONED (APU) · airframe 67,330 hrs · 19,461 cycles

APU GEN DROPS OFF LINE. APU GEN DROPS OFF LINE. REPLACED GENERATOR. OPS CHECKED OKAY.

Part: ADI — MALFUNCTIONED (COCKPIT) · airframe 67,213 hrs · 19,426 cycles

CAPTAIN'S ADI FAILED ACCOMPANIED BY ELEC BURNING ODOR. ADI RETURNED TO NORMAL AFTER 2 MINUTES. PULLED CAPT ADI CB AND REMOVED ADI. INBOUND CREW REPORTED, DID NOT CHANGE COLOR AT ANY TIME BEFORE THE TWO MINUTES IT WAS OUT OR AFTER IT CAME BACK ON, WAS OUT ON DESCENT FROM 10K TO 6K. FLT DECK HAD ELECTRICAL BURNT SMELL AT GATE WHEN SPOKE TO CREW. ADI ON AOG. CREW REPORTED HAD TCAS MSG WHEN ADI WAS OUT. REMOVED ADI. CREW DID NOT HAVE ANY FLIGHT DECK CBS POP. REPLACED CAPT EADI.

Part: SHUTOFF VALVE — FAILED (R ENG STARTER) · airframe 67,022 hrs · 19,367 cycles

START VALVE DOES NOT OPEN RT ENGINE. REPLACED START VALVE. ACP DRY MOTOR.

Part: PCU — FAULTED (NR 1) · airframe 67,004 hrs · 19,361 cycles

AILERONS HEAVY ON CONTROLS. REPLACED RIGHT & LEFT INBD AILERON PCA(S), LEAK AND OP CHECKED OKAY. ACCOMPLISHED RII INSPECTION OF RIGHT & LEFT INBD AILERON INSTALLATIONS. AIL FORCES STILL HIGHER THAN NORMAL. NO BINDING. MOST APPARENT BETWEEN 0 +-- 4 UNITS L OR R. EG CREW INDICATED THAT ALTITUDE (COLD SOAKING) HAD NO EFFECT ON FORCES. VERIFIED AND DUPLICATED ISSUE WITH EG TEST CREW PRESENT AFTER TEST FLIGHT TO DEN. FOUND AILERON FEEL, CENTERING AND TRIM MECHANISM FEEL SPRINGS WITH SEVERE EXCESSIVE FORCE. ACCOMPLISHED AILERON FEEL SPRINGS ADJUSTMENT TO THE LOWEST POSSIBLE VALUE ()THAT WILL ALLOW THE WHEEL TO MEET THE CENTERING REQUIREMENT OF THE 6-2 RETURN TO CENTER TEST. MAINTENANCE MANUAL SPECIFICALLY STATETO ADJUST TO LOWEST POSSIBLE VALUE TO MEET REQUIREMENTS. AILERON SYSTEM NOW SMOOTH AND FREE WITH NO BINDING.

Part: REGULATOR — FAULTY (LT ENGINE) · airframe 66,972 hrs · 19,351 cycles

L ENG BLEED WON'T CLOSE AFTER ENG START. REPLACED PRSOV REGULATOR, L ENG BLEED OFF LIGHT ILLUMINATED WITH PRSOV IN CLOSED POSITION.

Part: ARM — CLOGGED (DOOR 3R) · airframe 66,740 hrs · 19,284 cycles

DOOR 3R DIFFICULT ARMING. FOUND INSULATION FELL OUT OF CEILING. REMOVED INSULATION & REINSTALLED INSULATION IN CEILING. DOOR ARM AND DISARMED OKAY.

Part: IDG — FAULTY (LEFT) · airframe 66,678 hrs · 19,267 cycles

LEFT GENERATOR DRIVE LIGHT IS INOP. REPLACED NR 1 IDG, OPS CHECK OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,964 hrs · 18,783 cycles

LEFT NR 4 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LAMP, OPS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,964 hrs · 18,783 cycles

LT WING OVERWING EXIT ESCAPE PATH FWD LIGHT INOP. REPLACED LAMP, OPS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,964 hrs · 18,783 cycles

LT WING OVERWING EXIT ESCAPE PATH FWD LIGHT INOP. REPLACED LAMP, OPS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,964 hrs · 18,783 cycles

LEFT NR 4 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LAMP, OPS GOOD.

Part: FUEL CONTROL — FAULTY (LT ENGINE) · airframe 64,860 hrs · 18,756 cycles

LEFT ENG SHUTDOWN. LEFT ENG NOT RESPONDING TO THROTTLE MOVEMENT. RE-LIT ENGINE. EVERYTHING WAS NORMAL DURING FLIGHT. REPLACED FCU. EPCS PAGE SHOWS DUAL FAILURE P&S 351-23, S SVA, P&S FCU -EEC. ACP NR 1 ENGINE RUN REF JRH 2-5-64. ALL PARAMETERS AND ACCEL TIMES NORMAL. NO MESSAGES NOTED. ALL MESSAGES CLEARED. INSPECTED FCU FOR SAFETY & SECURITY.

Part: ENGINE — FAILED (RIGHT) · airframe 64,760 hrs · 18,728 cycles

NR 2 ENGINE FAILED BOROSCOPE LPT 3-RD STAGE INSPECTION.

Part: ACTUATOR — LEAKING (RT AILERON) · airframe 64,259 hrs · 18,606 cycles

RT AILERON HAS EXCESSIVE FLUID RUNNING OUT OF IT. REPLACED RT INBD AILERON PCA. OPS AND LEAK CHKS GOOD.

Part: ACTUATOR — FAULTY (ELEVATOR) · airframe 64,190 hrs · 18,587 cycles

EICAS MESSAGE 'ELEV ASYM' IS DISPLAYED. REPLACED ASSY LIMITER ACTUATOR. CHECKS OKAY.

Part: LIGHT — LOOSE (CABIN) · airframe 63,710 hrs · 18,455 cycles

EMERGENCY LIGHT STRIP IN FRONT OF F/C CLOSET IS LOOSE.

Part: LIGHT — LOOSE (CABIN) · airframe 63,710 hrs · 18,455 cycles

EMERGENCY LIGHT STRIP IN FRONT OF FC CLOSET IS LOOSE. SECURED LIGHT STRIP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,576 hrs · 18,416 cycles

DOOR 4R EMERGENCY LIGHT OUT, OUTSIDE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,576 hrs · 18,416 cycles

DOOR 4R EMERGENCY LIGHT OUT - OUTSIDE. RELAMPED EMERGENCY EXIT LIGHT AT R4 DOOR AND OPS CHECKED GOOD.

Part: O-RING — LEAKING (LIFE RAFT) · airframe 63,574 hrs · 18,415 cycles

LIFE RAFT AT AFT LOWERED CEILING PANEL, CYLINDER PRESSURE FAILED. LOW BOTTLE PRESSURE. LEAKING AT GAUGE TO VALVE O-RING. REMOVED & REPLACED O-RING.

Part: SWITCH — FAULTY (CABIN) · airframe 63,574 hrs · 18,415 cycles

INSTALL JIFFY SPLICES ON EMERGENCY EXIT SWITCH, FWD F/A CALL INDICATORS AND DOOR SLIDE LIGHTS. INSTALLED JIFFY SPLICES ALL LOCATIONS PER BOEING SWPM 20-90-14. FOUND SWITCH S10219 BAD, REPLACED PER AND TEST GOOD PER MM 25-66-11. FOUND MID CABIN EMERGENCY TEST SWITCH BAD, REPLACED AND OPS CHECKS GOOD PER B757 WDM 33-51-13.

Part: LOCK NUT — OUT OF ADJUST (L2 DOOR) · airframe 63,574 hrs · 18,415 cycles

DOOR 2L EMERGENCY POWER ASSIST PRESSURE RESERVOIR RED BAND ON EMERGENCY POWER SPRING CYLINDER ALIGNED PROPERLY. ADJUSTED CABLE TERMINAL LOCK NUT TO ACHIEVE DIMENSION PER FIG 401 A-A OF MM 52-11-33.

Part: SENSOR — FAULTY (EVAC SLIDE) · airframe 63,574 hrs · 18,415 cycles

DOOR 2R SLIDE ANNUNCIATOR ALWAYS ON EVEN WHEN DOOR NOT ARMED. REPLACED DOOR 2R GIRT BAR SENSOR S10220. OPS CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,574 hrs · 18,415 cycles

DURING EMERG LITE TEST, FOLLOWING BULLNOSE LIGHTS INOP, 4AB, 6AB, 10CD, 13 CD, 14 AB, 15 AB, 20 CD, 21 AB, 23 CD, 27 CD, AND 29 AB. LAMPED ALL LISTED LOCATIONS. ALSO REPLACED BATTERY PACK M10568, OPS CHECKS GOOD. INSTALLED JIFFY SPLICES ALL LOCATIONS. FOUND SWITCH S10219 BAD. REPLACED AND TEST GOOD. FOUND MID CABIN EMERGENCY TEST SWITCH BAD, REPLACED AND OPS CHECKS GOOD.

Part: SENSOR — FAULTY (R2 DOOR) · airframe 63,574 hrs · 18,415 cycles

DOOR 2R SLIDE ANNUNCIATOR ALWAYS ON EVEN WHEN DOOR NOT ARMED. REPLACED DOOR 2R GIRT BAR SENSOR S10220. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,574 hrs · 18,415 cycles

DURING EMERGENCY LIGHT TEST, FOLLOWING BULLNOSE LIGHTS INOP, 4AB, 6AB, 10CD, 13 CD, 14 AB, 15 AB, 20 CD, 21 AB, 23 CD, 27 CD, AND 29 AB. RELAMPED ALL LISTED LOCATIONS. ALSO REPLACED BATTERY PACK M10568, OPS CHECKS GOOD REF MM 33-51-07 AND 33-51-05.

Part: SKIN — DEBONDED (TE FLAP) · airframe 63,574 hrs · 18,415 cycles

LEFT WING INBOARD FWD FLAP OUTBOARD END UPPER SKIN DISBONDED DOUBLER. REMOVED PREVIOUS REPAIR. BONDED ON NEW DOUBLER REF REO G12468 REV B.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 63,574 hrs · 18,415 cycles

BS 500 BETWEEN STR 25L & 26L HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED. REMOVED EXISTING REPAIR & INSTALLED NEW REPAIR PER EVA 72035.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,574 hrs · 18,415 cycles

LT OVERWING MANUAL BACKUP CABLE FAILS OPS CHECK. CUT OUT DAMAGED SKIN REF SRM 53-00-01 FIG 201. FAB FILLER AND DOUBLER REF BAC DWG 146N3750 AND SRM 53-00-01 FIG 201, AND INSTALLED.

Part: LOCK NUT — MISALIGNED (L2 DOOR) · airframe 63,574 hrs · 18,415 cycles

DOOR 2L EMERGENCY POWER ASSIST PRESSURE RESERVOIR RED BAND ON EMERGENCY POWER SPRING CYLINDER ALIGNED IMPROPERLY. ADJUSTED CABLE TERMINAL LOCK NUT TO ACHIEVE DIMENSION.

Part: CABLE — FAILED (CABIN) · airframe 63,574 hrs · 18,415 cycles

LT OVERWING MANUAL BACKUP CABLE FAILS OPS CHECK. REPLACED BACK-UP CABLE. OPS CHECKS GOOD.

Part: SKIN — CHAFED (FOREFLAP) · airframe 63,574 hrs · 18,415 cycles

RIGHT WING INBOARD FORE FLAP OUTBOARD END UPPER SURFACE HAS CHAFED REPAIR. REMOVED DAMAGED REPAIR AND BONDED ON NEW REPAIR REO G12468, REV B.

Part: FRAME — DENTED (FUSELAGE) · airframe 63,574 hrs · 18,415 cycles

FWD CARGO PIT FUSELAGE FRAME AT STA 660 IS DENTED IN UPPER FLANGE AT STR 24L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION & INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 63,574 hrs · 18,415 cycles

FWD CARGO PIT FUSELAGE FRAME AT STA 680 IS DENTED IN UPPER FLANGE BETWEEN STR 24L TO 25L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE SECTION OR RIB AND INSTALLED DOUBLER REPAIR.

Part: CYLINDER — MISALIGNED (L4 DOOR) · airframe 63,574 hrs · 18,415 cycles

DOOR 4L EMERGENCY POWER ASSIST RESERVOIR RED BAND ON EMERGENCY POWER SPRING CYLINDER NOT ALIGNED PROPERLY. ADJUSTED CHECK NUT TO ACHIEVE DIMENSIONS INDICATED ON FIG 401 VIEW A-A PAGE 402. CABLE TRAVEL CHECKED PER MM 52-11-36. CHECKED GOOD.

Part: FRAME — DENTED (FUSELAGE) · airframe 63,574 hrs · 18,415 cycles

FWD CARGO PIT FUSELAGE FRAME AT STA 600 DENTED IN UPPER FLANGE IN AREA BETWEEN STR 23L AND 24R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE & INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 63,574 hrs · 18,415 cycles

FWD PIT STA 660 FRAME DENTED ABOUT STR 245. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME & INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 63,574 hrs · 18,415 cycles

AFT PIT DENTED FRAME STA 1520 BETWEEN STR 24-25 LEFT. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION FOR FRAME AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 63,574 hrs · 18,415 cycles

AFT PIT FRAME DENTED STA 1420 AT STR 26L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 63,574 hrs · 18,415 cycles

MAIN CABIN FWD OF DOOR L2, STR WEB CRACKED HI-LOK, STA 675 AT STR 11L. MAJOR REPAIR ACCOMPLISHED. REMOVED CRACKED STRINGER WEB. FABRICATED & INSTALLED NEW WEB.

Part: SMOKE DETECTOR — CRACKED (LAVATORY) · airframe 63,574 hrs · 18,415 cycles

LAV A SMOKE DETECTOR CRACKED. REPLACED LAV A SMOKE DETECTOR.

Part: STRUCTURE — DAMAGED (R2 DOOR) · airframe 63,574 hrs · 18,415 cycles

NEED DOUBLER ON DOOR 2R FOR UPPER HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED. FABRICATED A REPAIR DOUBLER AND INSTALLED.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,574 hrs · 18,415 cycles

MAIN CABIN STA 1400-1420, STR 17R, WEB CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED WEB, FABRICATED & INSTALLED A NEW WEB.

Part: GATE — CORRODED (R4 DOOR) · airframe 63,574 hrs · 18,415 cycles

DOOR 4R, LWR GATE CORRODED. REPLACED LOWER GATE.

Part: STRUCTURE — DAMAGED (L2 DOOR) · airframe 63,574 hrs · 18,415 cycles

DOOR 2L REQUIRES REPAIR DOUBLER FOR UPPER HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED. FABRICATED A REPAIR DOUBLER AND INSTALLED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 63,574 hrs · 18,415 cycles

MAIN CABIN FWD OF L-2 DOOR, STRINGER WEB CRACKED AT BS 675 AND STR 21L. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED WEB.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,574 hrs · 18,415 cycles

MAIN CABIN STA 1380-14--, STR 17R WEB CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED WEB, FABRICATED & INSTALLED A NEW WEB.

Part: FRAME — GOUGED (R1 DOOR) · airframe 63,574 hrs · 18,415 cycles

DOOR R1, DEEP GOUGE UNDERNEATH UPPER HINGE ARM. MAJOR REPAIR ACCOMPLISHED. CUT AND REMOVED DAMAGED SECTION OF FRAME INNER DOUBLER. FABRICATED & INSTALLED A REPAIR DOUBLER.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 63,574 hrs · 18,415 cycles

CUSP WEB, STA 1020-1025, LBL 75, WL 208 CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED WEB, FABRICATED & INSTALLED A -4 WEB.

Part: BATTERY — FAULTY (MASTER) · airframe 63,470 hrs · 18,389 cycles

BATTERY CHARGER STATUS MESSAGE WILL NOT ERASE. REPLACED BATTERY. OPS GOOD. NO FAULTS.

Part: EXCITER — INOPERATIVE (NR 2 ENGINE) · airframe 62,911 hrs · 18,241 cycles

CREW REPORTS LEFT ENGINE NR 2 IGNITON IS INOP. *S/D* IGNITION EXCITOR IS INOP. REPLACED IGNITION EXCITOR, OPS CHECKED NORMAL.

Part: OXYGEN MASK — DEFECTIVE (CAPTAIN'S) · airframe 62,583 hrs · 18,151 cycles

OXYGEN MASK DEFECTIIVE AT1 (1=CAPT,2=1ST OFF,3=1ST OBS). CREW COMMENTS: CAPT O2 MASK EMERGENCY PRESS TO TEST BUTTON STICKS ON. DIRT ACCUMULATION IN SWITCH. REPLACED O2 MASK, OPS CHECKED GOOD.

Part: SENSOR — FAULTY (APU) · airframe 62,452 hrs · 18,114 cycles

APU FAILED 3 START ATTEMPTS AT FL360. APU 60189 HAS EXHIBITED STARTING ISSUES SINCE LATE MAY. PRIOR TO THIS EVENT ECU MR49613-127 WAS REPLACED WITH MR49613-40 ON 6/8/08. THE -127 UNIT TESTED WITH NO FAULT FOUND. INLET PRESSURE SENSOR MR49533-225 WAS REPLACED WITH MR49533-75 ON 6/18/08. THE -225 UNIT TESTED WITH NO FAULT FOUND. THE STARTING ISSUES CONTINUED SINCE THIS EVENT ON 6/18/2008.

Part: OIL COOLER — LEAKING (NR 2 ENGINE) · airframe 62,412 hrs · 18,101 cycles

RIGHT IDG DRIVE LIGHT CAME ON JUST AFTER T/O. FUEL OIL COOLER FAILURE CAUSING LOW OIL QTY IN IDG. IDG SHUTDOWN. REPLACED NR 2 ENG FUEL/OIL COOLER AND REPLACED BYPASS VALVE ON COOLER. ALL LEAK CHECKS PERFORMED.

Part: OIL SYSTEM — LOW (IDG) · airframe 62,352 hrs · 18,082 cycles

INOP APU AND ENGINE GENERATOR. AMBER ALERT DECLARED. UNEVENTFUL LANDING. *S/D* LOW OIL QTY IN IDG. SERVICED IDG, RAN ENGINES AT FULL ELECTRICAL LOAD, NO PROBLEMS.

Part: IDG — FAILED (RT ENGINE) · airframe 62,292 hrs · 18,065 cycles

RIGHT GENERATOR TRIPPED DURING CRUISE TWICE. NO SHOP DATA EXISTS FOR REPAIR. REPLACED IDG.

Part: GIRT BAR — FAULTY (R4 DOOR) · airframe 62,177 hrs · 18,031 cycles

FWD END GRIT BAR FALLING OFF WHEN DOOR 4R OPENS. ARM AND DISARM FEELS STIFF AND BINDING. REMOVED LINER & SLIDE & LUBED ARM-DISARM MECHANISM, ADJUST FWD & AFT LIFTER WITH SLIDE INSTALLED, ALL OPS ARE NOW NORMAL.

Part: BULB — INOPERATIVE (L3 SLIDE LIGHT) · airframe 61,965 hrs · 17,978 cycles

DR 3L SLIDE LIGHT OUT. FOUND INOPERATIVE BULB. REPLACED BULB. OPS CHECKED OK.

Part: SEAL — WORN (STARTER DRIVE) · airframe 61,915 hrs · 17,965 cycles

NR 1 ENGINE HIGH OIL CONSUMPTION. FOUND STARTER DRIVE SEAL DRAIN TUBE LEAKING. REPLACED STARTER DRIVE SEAL, LEAK CHECK WAS GOOD.

Part: OVERHEAT LOOP — WORN (LT NACELLE) · airframe 61,834 hrs · 17,942 cycles

"L ENG OVHT LOOP 1" STATUS MESSAGE ON EICAS. FOUND OVER HEAT LOOP 1 WORN. REPLACED OVERHEAT LOOP 1, OPS CHECKED OK.

Part: OXYGEN MASK — CRACKED (CAPTAIN'S) · airframe 61,585 hrs · 17,874 cycles

CAPTAIN'S OXYGEN MASK CRACKED. REPLACED MASK, OPS CHECKED NORMAL.

Part: GENERATOR — FAILED (APU) · airframe 61,568 hrs · 17,870 cycles

EICAS MSG APU GEN OFF DISPLAYED AND APU GEN OFF LIGHT ILLUM WITH APU RUNNING. APU FIELD OFF LIGHT ON. APU GEN FIELD WOULD NOT RESET, RESET THEN RETRIPPED. FOUND APU GENERATOR FAILED. REPLACED APU GEN, OPS CHECK GOOD.

Part: TRANSCEIVER — INTERMITTENT (LEFT HF) · airframe 61,318 hrs · 17,804 cycles

LEFT HF INTERMITTENT, PER CHIDD. PER IB CREW: TX AND RX VERY GARBLED. REPLACED LT HF TRANSCEIVER, OPS & SELCAL CHECKED OK.

Part: SWITCH — INTERMITTENT (PRESSURE TRANSMI) · airframe 61,044 hrs · 17,726 cycles

CENTER HYD "RSVR" LIGHT ILLUMINATED. PRESSURE TRANSMITTER SWITCH INTERMITTENT. REPLACED PRESSURE TRANSMITTER SWITCH, OPS CHECKS GOOD.

Part: DISPLAY — FAILED (COCKPIT) · airframe 60,158 hrs · 17,479 cycles

RTFL DUE TO A FAILED COMPUTER DISPLAY UNIT. HAD TO RESOLDER SEVERAL JOINTS AND A5 CARD WAS REPLACED DUE TO A BURNT CARD. REPLACED CAPT CDU

Part: SWITCH — LOOSE (COCKPIT) · airframe 60,074 hrs · 17,456 cycles

EMERGENCY EXIT SWITCH LOOSE. FOUND DAMAGE TO THE SWITCH ASSY BY IMPACT. SECURED THE SWITCH & INSTALLED A NEW SWITCH GUARD.

Part: GIRT BAR — DETACHED (L4 DOOR) · airframe 60,074 hrs · 17,456 cycles

THE 3R GIRT BAR INOP. ITEM ROLLED FORWARD. DOOR POSITION IS DOOR 4L, GIRT BAR IS DETACHED AND LAYING ON THE FLOOR. ONE SLIDER HAS SPRING CLIP BROKEN OFF. REINSTALLED GIRT BAR/CLIPS. NO REPEATS SINCE ORIGINAL.

Part: OXYGEN MASK — FAULTY (FIRST OFFICER'S) · airframe 59,595 hrs · 17,320 cycles

FIRST OFFICER'S O2 MASK RUNS CONTINUOUSLY.

Part: SKIN PANEL — DAMAGED (LT WING) · airframe 59,335 hrs · 17,233 cycles

LEFT WING IS DAMAGED. REMOVED UNDERWING SKIN PANEL FOR REPLACEMENT.

Part: UNKNOWN — UNKNOWN (CABIN PRESSURE) · airframe 58,910 hrs · 17,113 cycles

RTFL DUE TO A PRESSURIZATION PROBLEM.

Part: SEAL — LEAKING (NR 2 ENGINE) · airframe 57,960 hrs · 16,832 cycles

LOST BETWEEN 8-10 QTS OF OIL AT THE BEGINNING OF THE FLIGHT & BETWEEN 4-5 QTS THE LAST TWO HOURS OF THE FLIGHT. FOUND NR 2 ENG DEOILER OIL SEAL LEAKING. REPLACED DEOILER SEAL.

Part: GIRT BAR — FAULTY (L4 DOOR) · airframe 57,848 hrs · 16,795 cycles

SLIDE PACK NOT ATTACHED. DOOR 4L GIRT BAR SLIDER FELL OFF. [06-14-07] INSTALLED 2EA GIRT BAR SLIDERS ON DOOR 4L. OPS CHECK GOOD. TESTED AND CHECKED ADJUSTMENT

Part: STARTER — FAULTY (NR 2 ENGINE) · airframe 56,871 hrs · 16,497 cycles

ON STARTING R ENG N2, SPUN UP TO 19 PERCENT THEN DOWN TO 0 PUSH, CREW SAW SPARKS FRM CWL. REPLACED STARTER AND START VALVE ON NUMBER TWO ENGINE.

Part: FCU — FAILED (RT ENGINE) · airframe 56,092 hrs · 16,280 cycles

AIR TURNBACK DUE TO RIGHT ENGINE SURGING 0.1 - 0.2 EPR. ON CLIMBOUT CREW INDICATED RIGHT ENGINE EPR FLUX 0.10 - 0.05 SLIGHT YAW FELT IN AIRFRAME. REPLACED FUEL CONTROL UNIT AND ACCOMPLISHED ACCEL CHECK AND POWER ASSURANCE.

Part: HYDRAULIC SYSTEM — LOW (LEFT) · airframe 55,718 hrs · 16,174 cycles

IN CRUISE "LEFT" HYDRAULIC QTY DECREASED TO .48. FOLLOWED CHECK LIST AND TURNED OFF BOTH LEFT SYSTEM PUMPS. QTY CONTINUES TO DROP AND IS NOW AT 0.40. NEED TO TOW AIRCRAFT OFF OF RUNWAY IF PTU WILL NOT SUPPLY NOSE WHEEL STEERING. QTY NOW DOWN TO 0.27 AND DROPPING. REPLACED RUDDER RATIO CHANGER ACTUATOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,391 hrs · 15,819 cycles

FLOOR MOUNTED EEL STRIP AT MID LAV THRESHOLD INOP. REPLACED LAMP ASSY.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 54,392 hrs · 15,820 cycles

TAXIED OUT ON LEFT ENGINE. STARTED 2ND ENGINE. CAPTAIN SMELLED SMOKE. RETURNED TO GATE. BOTH ENG BLEED OFF. ALSO ISOLATED PACKS AND RECIR, NO SMELL OR SMOKE NOTED. ALL LIGHTS IN CABIN ON VIDEO ON, CHECKED ALL CARGO PITS AND E&E COMPARTMENT, NO SOURCES SMOKE OR SMELL. CAUSE OF SMELL NOT ESTABLISHED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 54,391 hrs · 15,819 cycles

EXTERIOR EMERGENCY EXIT LIGHT AT DOOR 4L INOP. REPLACED LAMP.

Part: WARNING LIGHT — INOPERATIVE (DOOR 2L GIRT BAR) · airframe 51,842 hrs · 15,102 cycles

ONE BULB OF GIRT BAR WARNING LIGHT WILL NOT ILLUMINATE. REPLACED LIGHT ASSY.

Part: LIGHT — INOPERATIVE (ROW 29-32) · airframe 51,420 hrs · 14,972 cycles

EMERGENCY AISLE LIGHTS FROM ROW 29 TO 32 ARE INOP. REMOVED AND REPLACED BATTERY.

Part: UNKNOWN — UNKNOWN (CONTROL COLUMN) · airframe 49,790 hrs · 14,476 cycles

RETURNED TO FIELD DUE TO A LOUD BANG IN THE CAPTAIN'S CONTROL COLUMN. THE SUBJECT DISCREPANCY WAS DUE TO A BROKEN SPRING RETAINER ON THE ELEVATOR TENSION REGULAR WHICH ALLOWED THE SUBJECT TENSION STRING TO BECOME DETACHED. THE SUBJECT TENSION REGULATOR WAS REMOVED AND REPLACED AND OPS CHECKED PER MM 27-31-12 AND 27-31-00. ALL OPS CHECKS WERE GOOD.

Part: O-RING — LEAKING (SLIDE BOTTLE)

DOOR 1 RIGHT SLIDE LOW BOTTLE PRESSURE. SUPPLEMENTAL DATA UPDATE FILLER VALVE O-RING LEAKING. REPLACED O-RING.

Part: SENSOR — FAILED (EQUIP COOLING) · airframe 47,685 hrs · 13,888 cycles

FORWARD EQUIPMENT SMOKE LIGHT ILLUMINATED. SUPPLEMENTAL DATA UPDATE, REPLACED FORWARD EQUIPMENT COOLING SMOKE SENSOR.

Part: SMOKE — DETECTED (COCKPIT) · airframe 47,346 hrs · 13,796 cycles

EICAS MESSAGE INDICATING SMOKE IN FORWARD EQUIPMENT COMPARTMENT. *S/D* CAUSE IS UNKNOWN. SINCE NO SMOKE SOURCE WAS FOUND (NO RELATED EQUIPMENT FAILURES), FWD EQUIPMENT COOLING FILTER WAS ALSO REPLACED.

Part: CLAMP — LOOSE (BLEED DUCT) · airframe 44,551 hrs · 13,034 cycles

UPON LEVEL OFF AT FL340 RECIEVED A RT BLEED DUCT LEAK EICAS MESSAGE. DUCT LEAK BITE PRODUCED STORED FAULT 64 (RT WING LEADING EDGE - BOTH LOOPS IN ZONE BAD) . ERASED CODE FROM MEMORY & CLEARED STATUS MSG. FOUND BLEED DUCT CLAMP IN THE RIGHT LEADING EDGE TO BE LEAKING. REPLACED CLAMP.

Part: WINDOW — UNSECURE (COCKPIT) · airframe 42,914 hrs · 12,570 cycles

FIRST OFFICER'S WINDOW SQUEAL ON FLIGHT DECK DURING CLIMB. ATTEMPTED TO OPEN AND CLOSE DURING CLIMBOUT. DISCOVERED A LOOSE SEAL COMING OUT OF TRACK WHICH PREVENTED THE WINDOW FROM CLOSING PROPERLY. SEAL WAS REINSTALLED IN TRACK AND WINDOW OPERATED NORMALLY.

Part: ACTUATOR — LEAKING (LT AILERON) · airframe 41,530 hrs · 12,207 cycles

CENTER HYDRAULIC SYSTEM QUANTITY EICAS MESSAGE. SYSTEM SECURED AT .23. EXCESSIVE HYDRAULIC LEAKAGE FROM LEFT AILERON POWER CONTROL ACTUATOR (PCA). REPLACED SUBJECT ACTUATOR WITH SERVICEABLE UNIT.

Part: IDG — FAILED (NR1 GENERATOR) · airframe 40,913 hrs · 12,058 cycles

NR 1 GENERATOR DRIVE LIGHT ILLUMINATED PRIOR TO ENTERING ETOPS. DISCONNECTED GENERATOR. APU SUPPLIED POWER. LEFT AC INTEGRATED DRIVE GENERATOR (IDG) FAILURE. REPLACED THE LEFT IDG. CARRIER SHAFT FROZEN. REPLACED THE SHAFT AND OVERHAULED THE IDG.

Part: CONTROLLER — MALFUNCTIONED (LT ENGINE) · airframe 40,271 hrs · 11,881 cycles

LT ENGINE HIGH STAGE CAUTION ON EICAS AND HIGH STAGE LIGHT ILLUMINATED AT APPROX 40 KTS. REPLACED LT ENGINE HIGH STAGE CONTROLLER.

Part: BEAM — CORRODED · airframe 40,256 hrs · 11,873 cycles

CABIN FLOOR BEAM T-CAP CORRODED. STA 324 RBL 38-61. MAJOR REPAIR ACCOMPLISHED.INSTALLED REPAIR ANGLE ON FLOOR BEAM SUPPORT.

Part: SKIN — DENTED · airframe 40,256 hrs · 11,873 cycles

AFT EXT FUSELAGE SKIN DENT OUT OF LIMITS AT STATION 1617 STRINGER 20L SKIN LAP AND PRODUCTION JOINT. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,256 hrs · 11,873 cycles

CABIN FLOORBEAM UPPER CAP EXCESSIVE MATERIAL REMOVED STATION 680 LBL 1 TO RBL 16. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE STRAP.

Part: FRAME — CORRODED · airframe 40,256 hrs · 11,873 cycles

AFT CABIN FLOOR SUPPORT UPPER FRAME SURFACE IS CORRODEDSTATION 1640 AND RBL 58. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIRED WITH REPLACEMENT CORD, REPAIR STRAP, REPAIR ANGLE AND SPLICE ANGLE.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 40,256 hrs · 11,873 cycles

LEFT HAND CREASE BEAM WEB AT STATION 970-976 EXCESSIVE MATERIAL REMOVED TO ELIMINATE CORROSION. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM WEB.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 40,256 hrs · 11,873 cycles

STATION 1681 LBL 12 CABIN PRESSURE FLOOR WEB CORRODED AROUND FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,256 hrs · 11,873 cycles

CABIN FLOOR SUPPORT T-CAP AT STATION 365, RBL 12-42, WL 208 CORRODED. MAJOR REPAIR ACCOMPLISHED. STRAP REPAIR INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,256 hrs · 11,873 cycles

CABIN FLOOR STRUCTURE AT STATION 333 LBL 45-55, WL 208 FLOOR SUPPORT T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED T-CAP STRAP REPAIR.

Part: NUT — LOOSE (GEARBOX) · airframe 37,461 hrs · 11,107 cycles

NUMBER 1 ENGINE OIL QUANTITY DECREASED TO ZERO. OIL TEMPERATURE INCREASING. BREATHER MANIFOLD CRACKED. THIS WAS THE SECOND TIME IN 30 DAYS THAT THE BREATHER MANIFOLD WAS FOUND CRACKED ON THIS ENGINE. ENGINE WAS REMOVED AND SENT TO THE OVERHAUL SHOP. SHOP FOUND THE LOWER OIL DUCT LOOSE IN THE ANGLE GEARBOX. THIS WAS A RESULT OF A LOOSE LOCK NUT. THE LOOSE DUCT WAS CAUSING VIBRATION TO BE TRANSFERRED INTO THE BREATHER MANIFOLD TUBE THUS CAUSING IT TO CRACK. THE LOWER OIL DUCT AND HARDWARE WAS REPLACED AND THE ENGINE WAS RETURNED TO SERVICE.

Part: LINE — LOOSE (LT ENGINE) · airframe 37,475 hrs · 11,110 cycles

LEFT ENGINE REQUIRED 12 QUARTS OF OIL. SUPPLEMENTAL DATA UPDATE FOUND OIL PRESSURE TRANSMITTER LINE B-NUT EXTREMLY LOOSE, AND OIL LEAKING FROM IT ON DRY MOTOR. SECURED LINE.

Part: VENT LINE — CRACKED (NR 1 ENGINE) · airframe 37,226 hrs · 11,037 cycles

NUMBER 1 ENGINE OIL QUANTITY WENT TO ZERO IN CRUISE. NUMBER 1 SCAVENGE BEARING MANIFOLD BREATHER VENT TUBE CRACKED.

Part: SKIN — DAMAGED (ELEVATOR) · airframe 36,300 hrs · 10,771 cycles

RIGHT ELEVATOR UPPER LEADING EDGE SKIN DAMAGED BY ELECTRO STATIC DISCHARGE 6 INCHES FROM TIP, HOLE DIA .25 INCH. MAJOR REPAIR ACCOMPLISHED. SEAL AND POT HOLE, OVERLAYED FIBERGLASS PLY, DRILLED FASTENER HOLE AND RESTORED FINISH.

Part: ENGINE — VIBRATION (NR 2) · airframe 35,931 hrs · 10,678 cycles

EXCESSIVE VIBRATION IN THE NUMBER 2 ENGINE.

Part: GUIDE — LOOSE (L2 DOOR) · airframe 34,079 hrs · 10,193 cycles

DOOR 2 LEFT IS HARD TO OPEN. *S/D* GUIDE ARM PIN WAS FOUND LOOSE DURING TROUBLESHOOTING. NEW GUIDE ARM WAS INSTALLED AND ADJUSTED.

Part: SLIDE — DEPLOYED (SERVICE DOOR) · airframe 31,892 hrs · 9,584 cycles

AFT GALLEY DOOR SLIDE WAS INADVERTENTLY DEPLOYED. *S/D* SLIDE INADVERTENTLY BLOWN BY CONTRACT CLEANERS.

Part: ENGINE — FLUCTUATES (NR 2) · airframe 31,182 hrs · 9,384 cycles

AIRCRAFT DIVERTED TO HNL, DUE TO NR 2 ENGINE POWER FLUCTUATIONS.

Part: ALTIMETER — INOPERATIVE (CAPTAIN) · airframe 30,996 hrs · 9,337 cycles

RETURNED TO THE FIELD AT LAX DUE TO A PROBLEM WITH THE CAPTAIN''S ALTIMETER. *S/D* CAPTAINS ALTIMETER FLAG IN VIEW AND NEEDLE STUCK. RESET CB, NO HELP. CAPTAIN''S ALTIMETER WAS REPLACED. NO ADDITIONAL ALTIMETER WRITE-UPS HAVE OCCURRED. SHOP ANALYSIS OF ALTIMETER RESULTED IN REPLACEMENT OF DRIVE MOTOR.

Part: SLIDE — DAMAGED (1 L DOOR)

DURING SHOP OVERHAUL OF SLIDE REMOVED FROM DOOR 1L FOR TIME EXPIRATION, A HOLE ON THE LOWER TUBE NEXT TO THE RELIEF VALVE WAS FOUND. SLIDE SENT TO THE VENDOR FOR REPAIR.

Part: ACTUATOR — FAILED (NR 9 SPOILER)

EICAS MESSAGE AND SPOILER LIGHT CAME ON DURING TAXI OUT. SPOILER ACTUATOR FAILED. REPLACED THE ACTUATOR. NO FURTHER PROBLEMS REPORTED.

Part: IDG — FAILED (NR 2)

GENERATOR DRIVE LIGHT ILLUMINATED IN FLIGHT APPROXIMATELY 30 MINUTES INTO FLIGHT. AIRCRAFT RETURNED TO FIELD. REPLACED NR 2 RIGHT INTEGRATED DRIVE GENERATOR (IDG) AND OPS CHECK GOOD.