N543UA

Part: COVER — UNSECURE (CABIN) · airframe 90,440 hrs · 25,891 cycles

EMERGENCY LIGHTING STRIP AT SEAT ROWS 32 - 34 INOPERATIVE. SECURED COVER TESTED LIGHT IAW 33-51-96-0401.

Part: PCA — FAULTED (SPOILER) · airframe 89,843 hrs · 25,727 cycles

SPOILERS MSG ON UPPER EICAS INFLIGHT WHEN EXTENDING FULL FLAPS SET AT 15 DEG. REF WD 27-61-13 TO 18 SPOILERS PCA'S RESISTANCE CHECK OK. PER PREVIOUS PCA NR 2 FAULTED. ACCOMPLISHED SPOILERS PCA NR 2 & 11 RVDT PHASE SYNC VOLTMETER IAW MM 27- 61-00 P 500 PROCEDURE 5 READS OK. CONFIRMED WITH LINE MX CONTROLLER IF ITS HIT AGAIN NEED TO REPLACE PCA 2 & 11.

Part: SKIN — PUNCTURED (L4 DOOR) · airframe 86,049 hrs · 24,776 cycles

L4 DOOR INNER SKIN HAS PUNCTURE AT UPPER HINGE. CUT OUT DAMAGE MADE FILLER & DOUBLER & INSTALLED IAW ECRA 5210-02509 & REO M18051. NDT INSPECTED IAW NTM 51-00-19 PART 6 NO CRACKS FOUND, ALSO ACCOMPLISHED INSURANCE CUT OF .040.

Part: SKIN — TORN (L4 DOOR) · airframe 86,049 hrs · 24,776 cycles

L4 DOOR ASSEMBLY INNER SKIN TORN AFT SIDE AT SECOND FROM BOTTOM LIGHTING HOLE. REMOVED & REPAIRED L4 DOOR ASSEMBLY INNER SKIN AFT SIDE FROM BOTTOM LIGHTING HOLE.

Part: PLATE — CORRODED (FUSELAGE) · airframe 86,049 hrs · 24,776 cycles

MAIN CABIN BS 1039 STRINGER 17R RBL 64 CREASE BEAM ATTACH PLATE CORRODED. REMOVED ATTACH PLATE. FABRICATED & INSTALLED NEW PARTS IAW SRM 51-30-01.

Part: SKIN — BENT (CARGO DOOR) · airframe 86,049 hrs · 24,776 cycles

FORWARD CARGO DOOR EXT SKIN BENT AT AFT LOWER CORNER. REMOVED DAMAGE. HFEC. FABRICATED & INSTALLED REPAIR PARTS IAW SRM 52-31-01 REPAIR 4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 86,049 hrs · 24,776 cycles

STATION 365.25 CABIN FLOORBEAM CORROSION RBL 11. REMOVED DAMAGE. HFEC. FABRICATED & INSTALLED REPAIR PARTS IAW ECRA 5310-05536.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 86,049 hrs · 24,776 cycles

MAIN CABIN BS 1028 - 1032 LBL 63 CORROSION ON L ANGLE. REMOVED DAMAGE. HFEC. FABRICATED & INSTALLED REPAIR PARTS IAW ECRA 5300-01416.

Part: PLATE — CORRODED (FUSELAGE) · airframe 86,049 hrs · 24,776 cycles

CORROSION ON FRAME CREASE BEAM ATTACH PLATE BS 1078, LBL 6 4 IN MAIN CABIN. REMOVED DAMAGE. FABRICATED & INSTALLED NEW WEB ATTACH PLATE PN 1445211-20 IAW DWG 144N5211 & SRM 51-40-05.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 86,049 hrs · 24,776 cycles

FLOORBEAM DOUBLER AT BS 365, RBL 45 HAS TWO EACH DAMAGED HOLES. HFEC VERIFIED, CRACK INDICATIONS FOUND. R & R DOUBLER AT BS 365, RBL 45 IAW SRM 51-40-02, PAR 7 FIG 12 & PAR 4B.

Part: PLATE — CRACKED (FUSELAGE) · airframe 86,049 hrs · 24,776 cycles

CORROSION ON FRAME CREASE BEAM ATTACH PLATE AT BS 1178, LBL 64 IN MAIN CABIN. R & R CREASE BEAM ATTACH PLATE AT BS 1178, LBL 64 IN MAIN CABIN.

Part: APU — LEAKING (APU BAY) · airframe 85,706 hrs · 24,691 cycles

APU OIL CONSUMPTION ABOVE LIMIT, LEAK CHECKED APU FOUND OIL COMING OUT FROM THE DRAIN FOR THE BEARING CAVITY SEAL., OIL CONSUMPTION RATE IS MORE THAN LIMIT. APU CONTROL UNIT IS -20. START TO LOOK AT FIM49-11-00.

Part: ACOUSTIC PANEL — DELAMINATED (THRUST REVERSER) · airframe 84,909 hrs · 24,502 cycles

NR 2 ENG RT THRUST REVERSER ACOUSTIC PANEL AT 12:00 POSITION DELAMINATED IN CTR. INSTALLED REPAIR DOUBLERS TO THE UPPER BIFURCATION PANEL IAW AMM 78-31-93.

Part: SHUTOFF VALVE — INOPERATIVE (APU) · airframe 84,154 hrs · 24,329 cycles

APU BLEED INOPERATIVE. REPLACED APU SOV IAW AMM.

Part: CRANK ASSY — OBSTRUCTED (RUDDER PEDAL) · airframe 83,966 hrs · 24,282 cycles

CAPTAIN`S RUDDER PEDALS ADJUSTING CRANK BINDS. CLEANED DEBRIS FROM ADJUSTING CRANK, OPERATIONS NORMAL.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 83,948 hrs · 24,277 cycles

APU FAULT IN FLT, RTFL.

Part: APU — SHUTDOWN (APU BAY) · airframe 83,945 hrs · 24,276 cycles

APU AUTO SHUT DOWN. ECU FAULTS GEN FILTERS, REPLACED BOTH FILTERS & REPLACED ECU, NO HELP. DELTAP NOT POPPED & CHIP DETECTOR CLEAN, APU SHUT DOWN AFTER 6 MINUTES WITH NO LOAD APPLIED, REINSTALLED ORIGINAL ECU.

Part: APU — FAULTED · airframe 83,923 hrs · 24,271 cycles

APU SHUTDOWN, FAULT LIGHT ILLUMINATED & EICAS MESSAGE, APU FAULT DISPLAYED. RESTARTED APU APPLIED ELECTRICAL & PNEUMATICS, WORKED OK, RAN FOR 30 MINUTES WITH NO PROBLEMS.

Part: STRUCTURE — DAMAGED (CARGO BAY) · airframe 83,887 hrs · 24,261 cycles

FWD CARGO FLOOR HAS CORROSION AT TIE DOWN BS 622, LBL 25. REMOVED DAMAGED AREA, INSTALLED REPAIR FILLER.

Part: FUEL CONTROL — MALFUNCTIONED (LT ENGINE) · airframe 83,802 hrs · 24,240 cycles

LT ENG FLUCTUATES BETWEEN 1.11-1.23 EPR AT CRUISE ALT. RT ENG STABLE AT 1.17. A-T ON OR OFF. FLUX RANGE IS OUT OF ALLOWABLE LIMITS OF SVC TIP 73- 21-04 PG 400A. REPLACED FUEL CONTROL UNIT IAW AMM 73-21-01 & FUEL PUMP IAW AMM 73-11-01 IAW ABOVE DIRECTIVE. ACP IDLE LEAK CHECKED GOOD, ALL IDLE PARAMETERS NORMAL.

Part: SERVO VALVE — LEAKING (LT SPOILER) · airframe 83,606 hrs · 24,185 cycles

FLUID APPEARS TO BE LEAKING FROM THE SPOILER ACTUATOR ON THE 3RD ONE IN FROM THE LT WINGTIP. REPLACED ELECTROHYDRAULIC SERVOVALVE ON NR 3 SPOILER PCA IAW MM. OPERATIONS & LEAK CHECKED GOOD.

Part: SEAL — BROKEN (CABIN) · airframe 83,456 hrs · 24,142 cycles

LIFE VEST COMPARTMENT SEALS BROKEN 1EF, 2AB, 3EF, 4EF, 5EF & 6AB. LIFE VEST COMPARTMENTS INSPECTION CHECKED NORMAL & RESEALED 1EF, 2AB, 3EF, 4EF, 5EF & 6AB.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 83,438 hrs · 24,137 cycles

EMERGENCY LIGHT ON FLOOR OF AFT LAVATORY INOPERATIVE. RECONNECTED THE LIGHT ASSEMBLY AT AFT LAVATORY IAW AMM. OPERATIONS CHECKED NORMAL. OPERATIONS CHECKED LIGHT IAW IDT LIST.

Part: RELAY — FAULTY (ELECTRICAL SYS) · airframe 83,250 hrs · 24,087 cycles

AFT CARGO COMPARTMENT LIGHTS DO NOT REMAIN ILLUMINATED WHEN APU POWER IS ON. WORKS OK ON EXTERIOR. COMPLIED IAW MEL. LIGHTS WORKS NORMAL WITH GROUND POWER NOT WITH APU POWER. APU ELECTRICAL INOPERATIVE. REPLACED RELAY K101, IAW AMM 24-51-01-401. GROUND BUSSES POWER NORMALLY FOR EXTERNAL & APU SOURCES. CARGO PITS POWERED WITH APU ON & EXTERIOR POWER DISCONNECTED.

Part: CONTROL UNIT — FAULTY (SLAT SYSTEM) · airframe 82,926 hrs · 24,009 cycles

DURING DESCENT, WHILE USING SPOILERS, SPOILER EICAS ILLUMINATED. ALSO SPOILER FAULT WHEN SPOILER STOWED. ACCOMPLISHED RESISTANCE CHECK REF FIM 27-09-806, PAGE 126 ON SPOILERS NR 3 AND NR 10, NR 3-PIN 1 & 3, 519.9, PIN 8 & 9, 78.3, PIN 5 & 7, 342.4. FOUND WITHIN LIMITS NR 10-PIN 1 & 3, 501.4 PIN 8 & 9, 78.5 PIN 5 & 7, 338.7. FOUND 10379 WITHIN LIMITS. REPLACED 2R SCM 27-09-00, CHECKED OK, OPS NORMAL WITH NO FAULTS OR MESSAGES.

Part: SPOILER — FAULTED (NR 3) · airframe 82,825 hrs · 23,982 cycles

DURING SPOILER PCA TESTS. NR 4 & NR 9 SPOILERS RETRACTED WHILE COMMANDED IN UP POSITION. NR 3R SPOILER CONT MODULE FAULTED AND EICAS MAINT MESSAGE CAME INTO VIEW.

Part: WARNING LIGHT — ILLUMINATED (ANTI ICE VALVE) · airframe 82,823 hrs · 23,981 cycles

LEFT WING ANTI-ICE VALVE LIGHT ON, ON GROUND. VALVE SECURED CLOSED.

Part: CONNECTOR — BURNED (NR 2 OVEN) · airframe 82,467 hrs · 23,892 cycles

SMOKE REPORTED IN CABIN. WHILE TROUBLESHOOTING LOG 1 FOUND GALLEY 1 ANR 2 OVEN CONNECTOR YSAD2 POS 3 BURNED. REPLACED NR 2 OVEN.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 82,305 hrs · 23,851 cycles

BULLNOSE EMERGENCY LIGHT AT SEAT 4AB, PLASTIC LENS COVER IS MISSING. NEW LENS INSTALLED.

Part: CONTROL PANEL — INOPERATIVE (COCKPIT) · airframe 82,246 hrs · 23,836 cycles

FIRST OBSERVER SEAT INOPERATIVE DUE TO AUDIO CONTROL PANEL INOPERATIVE. REPLACED FIRST OBSERVER AUDIO CONTROL PANEL.

Part: HYDRAULIC LINE — LEAKING (NLG) · airframe 82,112 hrs · 23,797 cycles

NOSE STEERING LINE LEAKING TOP OF NLG. LINE WAS LEAKING FROM FITTING WHERE LINE IS SWEDGED ONTO THE LINE. REPLACED HYD LINE WITH INTERIM REPAIR HOSE IAW EC-RA ;3234-01006. LEAK CHECKED AND SERVICED HYD SYS.

Part: DUCT — OBSTRUCTED (COCKPIT AIR) · airframe 81,799 hrs · 23,710 cycles

CAPTAIN`S AIR OUTLET HAS VERY LOW AIRFLOW. BLEW OUT DUCTING WITH REVERSE FLOW. REMOVED DEBRIS. AIRFLOW NORMAL.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 81,555 hrs · 23,654 cycles

CREW REPORT: RT ENGINE REV CONT STATUS MESSAGE AFTER ENGINE START.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 81,555 hrs · 23,654 cycles

RIGHT ELECTRIC DRIVEN HYD PUMP IS LEAKING. REMOVED AND REPLACED RT ELECT DRIVEN HYD PUMP AND PRESS 2 CASE DRAIN FILTERS OPS AND LEAK CHECKS NORMAL PER B757 MM 29-11-01 AND 29-11-18.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 81,544 hrs · 23,651 cycles

OVERBOARD EX VAL TEST STATUS MESSAGE WILL NOT CLEAR, HAD HARD FAULT THAT WOULD NOT CLEAR. REPLACED OVERBOARD EXHAUST VALVE AND AIR FILTER ASSY. OPS CHECKS GOOD. FAULTS CLEARED.

Part: SELECTOR — MALFUNCTIONED (CABIN PRESSURE) · airframe 81,531 hrs · 23,646 cycles

STATUS MSG CABIN ALT AUTO 1 WILL NOT CLEAR. PLEASE TROUBLESHOOT TO CONFIRM NEED. REF FIM 21-30-00 PG 111 FIG 104 FOR TROUBLESHOOTING. RPL- :4 HITS ON BITE TEST OF AUTO 1 PRESS CONTROLLER FOR SELECTOR, REPLACED SELECTOR AND TESTED PER MM, CHECKS GOOD.

Part: UNKNOWN — UNKNOWN (LAVATORY) · airframe 81,491 hrs · 23,634 cycles

LAVATORY AND POTABLE WATER ISSUE, FLIGHT DIVERTED.

Part: PCU — FAILED (LT ELEVATOR) · airframe 81,424 hrs · 23,614 cycles

LEFT ELEVATOR PCU MAINT MESSAGE. REMOVED AND REPLACED LEFT OUTBOARD ELEVATOR PCU PER MM.

Part: FSEU — FAULTED (FLAP SYS) · airframe 81,331 hrs · 23,591 cycles

FLAP SLAT ELEC AND WARN FLEX STATUS MESSAGE. FSEU UNIT NR 2 REF MM 27-51- 01. ALL GROUND CHECKS GOOD.

Part: ALTIMETER — FAILED (COCKPIT) · airframe 81,267 hrs · 23,571 cycles

CREW REPORTS: CAPT ALTIMETER FAILED FOR SEVERAL MINUTES WITH OFF FLAG TAPS WITH A KNUCKLE BROUGHT IT BACK. REMOVED AND REPLACED CAPTAIN'S ALTIMETER AS OUTLINED IN AMM. ALTIMETER TEST, TESTS NORMAL.

Part: ENGINE — MAKING METAL (NR 2) · airframe 81,126 hrs · 23,537 cycles

DUE TO METAL DEBRIS FOUND ON MAIN GEARBOX AND MAIN OIL FILTER, ENGINE MUST BE REPLACED PRIOR TO NEXT DEPARTURE. REPLACED NR 2 ENGINE PER MM. ENGINE S/N OFF 726665 S/N ON 727132.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 81,077 hrs · 23,527 cycles

EMERGENCY LIGHT JUST INBOARD OF FIRST CLASS CLOSET INOPERATIVE. ALL OTHER LIGHTS WORK OKAY. SECURED CONNECTOR D6644 IAW W-D 33-51-21 PAGE 2 AND EMERGENCY LIGHT OPS CHECKED OK.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 81,077 hrs · 23,527 cycles

EMERGENCY LIGHT JUST INBOARD OF FIRST CLASS CLOSET INOPERATIVE. SECURED CONNECTOR IAW W-D 33-51-21 PAGE 2 AND EMERGENCY LIGHT OPS CHECKED OK.

Part: LUG — BROKEN (MLG WHEEL) · airframe 80,999 hrs · 23,507 cycles

LUG CRACKED ON LEFT REAR OUTBOARD MAIN TIRE. REPLACED 1 AFT MLG TIRE.

Part: ACTUATOR — FAILED (APU DOORS) · airframe 80,917 hrs · 23,486 cycles

STATUS MESSAGE FOR APU DOOR. REPLACED DOOR ACTUATOR.

Part: GIRT BAR — OBSTRUCTED (R4 DOOR) · airframe 80,804 hrs · 23,462 cycles

UNABLE TO ARM R4 DOOR. CLEANED DEBRIS FROM GIRT BAR AREA.

Part: ARM — DIRTY (L1 DOOR) · airframe 80,758 hrs · 23,450 cycles

L1 DOOR WILL NOT ARM. CLEANED DEBRIS FROM DOOR CELL PER AMM.

Part: SPRING — BROKEN (DISARM LEVER) · airframe 80,733 hrs · 23,444 cycles

L4 DOOR ARM DISARM LEVER COVER, HINGE SPRING BROKEN. REPLACED DISARM LEVER COVER.

Part: WINDSHIELD — INOPERATIVE (COCKPIT) · airframe 80,682 hrs · 23,430 cycles

WINDOW HEAT INOPERATIVE LIGHT ILLUMINATED. REPLACED NR 3 RT WINDOW PER MM, HEAT OPS CHECKED OK.

Part: TIRE — UNKNOWN (MLG) · airframe 80,658 hrs · 23,422 cycles

NR 2 WHEEL LUG NUT BROKEN AT 2 O'CLOCK POSITION. NR 2 FORWARD TIRE IS PROBLEM. REPLACED NR 2 MLG TIRE PER AMM.

Part: B-NUT — LOOSE (APU) · airframe 80,644 hrs · 23,418 cycles

APU AUTO SHUTDOWN. FOUND LOOSE B-NUT. SECURED FITTING. SERVICE OIL TO FULL.

Part: REGULATOR — FAULTY (BLEED AIR SYS) · airframe 80,353 hrs · 23,344 cycles

LEFT DUCT PRESSURE FLUCTUATING FROM 25 - 45 PSI AT 41000 FEET CRUISE ALTITUDE. REPLACED LT ENGINE PRSOV REGULATOR IAW AMM. CHECK PNEU BLEED LINE TO PRSOV AND REV FLOW VALVE AND PRSOV REG ALL LINE ARE SECURED AND TIGHT. ACP'D ENGINE RUN WAS GOOD LT AND RT PNEU BLEED PSI WERE MATCHED WITH NO FLUCTUATIONS.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 80,322 hrs · 23,338 cycles

PRIOR TO DEPARTURE, FWD CARGO DET2 MSG DISPLAYD UNABLE TO CLEAR. FIRE TEST, NO HELP. PER MEL TEST VERIFIED OTHER DETECTOR OK. REPLACED SMOKE DETECTOR 2 PER AMM, OPS CHECKED OK. MESSAGE WENT AWAY.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 80,308 hrs · 23,335 cycles

FWD CARGO DET 2. PRIOR TO DEPARTURE, FWD CARGO DET2 MSG DISPLAYED UNABLE TO CLEAR, FIRE TEST NO HELP. PER MEL TEST VERIFIED OTHER DETECTOR OK. REPLACED SMOKE DETECTOR 2 PER AMM, OPS CHECKED OK. MESSAGE WENT AWAY.

Part: ROTOR — FAULTY (NR 2 ENGINE) · airframe 80,273 hrs · 23,328 cycles

RIGHT ENGINE OIL PRESS DURING TAXI IN. COMPLETED SHEET 1 AND 2 PER FIM 73-21-00-FIG 103. FOUND PMA FAULT ON EPCS PAGE, REPLACED PMA STATOR AND ROTOR.

Part: AUDIO PANEL — FAULTY (COCKPIT) · airframe 80,043 hrs · 23,261 cycles

F/O RIGHT RADIO AUDIO CONTROL DOES NOT COMPLETELY SILENCE RADIO. REMOVED AND REPLACED F/O AUDIO SELECT PANEL IAW AMM, OPS CHECK GOOD.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 79,950 hrs · 23,235 cycles

CABIN TEMP HOT WITH APU BLEED AND PACKS ON. MANUALLY LOCKED OUT FLOW CONTROL VALVE. AIR COND PACK HAS BEEN DEFERRED PER MEL 21250. REPLACE- :RIGHT PACK TEMP CONTROL VALVE PER MM.

Part: ENGINE — FLAMED OUT (NR 2) · airframe 79,617 hrs · 23,141 cycles

NR 2 ENGINE FLAMEOUT WITH NO DEFINITIVE CAUSE FOUND. NR 2 ENGINE FMU CHANGE. REPLACE FUEL CONTROL UNIT MR73233 PCN 621-9037. REPLACED EEC PCN 481-9246 MR73237 PER MM (P/N 1B7486 - SERIAL# 67 - POSIT #2). REPLACE ENGINE FUEL PUMP PCN 615-9007 MR73150 PER MM. TAG ALL THREE REMOVED ITEMS WITH EG ALERT TAGS FOR FOLLOW-UP BY ENGINEERING. REPLACED FCU AND THE MAIN FUEL PUMP PER AMM. ON TAXI RIGHT ENGINE SHUTDOWN. ALSO IDG TRIPPED OFF. NR 2 ENGINE LEAKING FUEL FROM B-NUT CONNECTION AT FUEL CONTROL REF IPC 71-00-01-529 ITEM 680. PCN 230-0126. REPLACED FUEL LINE LOWER SECTION BETWEEN FMU AND SVA ACTUATOR. LEAK CHECK OK.

Part: IDG — FAILED (NR 2 GENERATOR) · airframe 79,326 hrs · 23,071 cycles

RECEIVED A RIGHT GENERATOR OFF. CYCLED THE GENERATOR CONTROL SWITCH AND THE RIGHT GENERATOR RECOVERED MOMENTARILY THEN WENT OFF AGAIN. RAN ENGINE. GENERATOR WENT OFFLINE. REPLACED RT IDG PER MM.

Part: UNKNOWN — ODOR (CABIN) · airframe 79,325 hrs · 23,070 cycles

FLIGHT ATTENDANT REPORTED DETECTING STRONG BURNING ODOR AT ROWS 2 AND 3. UNABLE TO DUPLICATE ODOR.

Part: CONNECTOR — FAULTY (D13) · airframe 79,293 hrs · 23,061 cycles

TRIED NEW DFDR, DFDAU BOTH NO HELP. FOLLOWED FIM 31-31-00-PG 107-110 REPLACED K206 RELAY, NO HELP. FOUND 115VAC AT PIN 9 OF K206. RANG WIRING FROM RELAY TO DFDR AND HAD CONTINUITY. PER FIM, WHEN AIR GRD SYS 2 CIRCUIT BREAKER PULLED FLT REC 'OFF' LIGHT DOES NOT EXTINGUISH. TRIED NEW FLT REC CTRL PNL, NO HELP. ALL ORIGINAL UNITS REINSTALLED. TRIED KNOWN GOOD "DFDR" AND "DFDAU" -- STILL NO HELP. NEED CONTINUE FIM 31-31-00 BLOCK-3 PG 109. REPLACED FLT DATA RECORDER, NO HELP. TROUBLE SHOOTING TREE MM31-31-00-0101 PAGES 107-110. SYSTEM FAULTS ON FACE OF DFDR OR DFDAU. FOUND PIN NR 23 AT CONN D13 A IS INTERMITTENT, NEED PIN REPLACEMENT WDM 31-31-01, PG1A. REPLACED CONNECTOR D13, INSTALLED DATA RECORDER M200 PER MM, TESTS OKAY.

Part: TARGET — OUT OF POSITION (LT NLG) · airframe 79,293 hrs · 23,061 cycles

LANDING GEAR MONITOR STATUS MESSAGE. REPLACED TARGET ON LEFT NOSE GEAR. PERFORMED LANDING GEAR POSITION TEST, OPS CHECKED GOOD.

Part: SLAT — CRACKED (LE SLAT) · airframe 79,234 hrs · 23,046 cycles

RIGHT WING LEADING EDGE SLAT NR 8 CRACKED APPROX 69" O/B OF NR 7 LEADING EDGE SLAT AND 16" FWD OF WING TRAILING EDGE. INSTALLED A PERM REPAIR DOUBLER PER ECRA 5750-04472.

Part: SKIN — CRACKED (NR 2 SLAT) · airframe 79,234 hrs · 23,046 cycles

NR 3 L/E SLAT NOSE SKIN CRACKED APPROX 23 INCHES FROM OTBD EDGE AND 6 FT FROM TOP WEDGE. INSTALLED PERMANENT REPAIR DOUBLER.

Part: SKIN — DENTED (BS 1410) · airframe 79,234 hrs · 23,046 cycles

FUSELAGE DENTED AT STA 1410 OTBD OF S-29R. INSTALLED INTERIM REPAIR PER ECRA 5330-04281.

Part: LINER — DELAMINATED (THRUST REVERSER) · airframe 79,234 hrs · 23,046 cycles

NR 2 ENGINE RT THRUST REVERSER ACOUSTIC PANEL AT 12:00 POSITION DELAMINATED IN CENTER. INSTALLED REPAIR DOUBLERS TO THE UPPER BIFURCATION PANEL PER AMM.

Part: FORK — BENT (R1 DOOR) · airframe 79,234 hrs · 23,046 cycles

R1 DOOR UPPER HINGE TRIGGER FORK IS BENT. ACCOMPLISHED REPLACEMENT OF R1 TRIGGER FORK.

Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 79,234 hrs · 23,046 cycles

BS 1681 FLOORBEAM HAS CORROSION OUT OF SRM LIMITSACCOMPLISH RII INSPECTION OF AMIS ITEM 2342115. ACCOMPLISHED FLOORBEAM UPPER TEE REPLACEMENT IN REF TO ECRA 5310-05557.

Part: FLOORBEAM — CORRODED (BS 1600) · airframe 79,234 hrs · 23,046 cycles

BS 1600 FLOORBEAM HAS CORROSION OUT OF SRM LIMITS. REPAIRED FLOORBEAM UPPER TEE BETWEEN BL 0 AND RBL 11 IAW ECRA 5310-05556. ACCOMPLISHED REPAIR, RII INSPECTED.

Part: PRESSURE DECK — CORRODED (BS 1681) · corrosion level 2 · airframe 79,234 hrs · 23,046 cycles

BS 1681 AFT PRESSURE DECK WEB HAS CORROSION OUT OF LIMITS. PRESSURE DECK REPAIRED.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 79,234 hrs · 23,046 cycles

BS 1640 FLOORBEAM HAS CORROSION, OUT OF SRM LIMITS IAW SCAL LP 9974488. ACCOMPLISHED UPPER CHORD REPLACEMENT IAW ECRA 5310-05536 REPAIR 5.

Part: FRAME — CORRODED (BS 1480) · corrosion level 2 · airframe 79,234 hrs · 23,046 cycles

AFT CARGO FRAME HAS CORROSION ON UPPER CAP BS 1480 JUST OB OF RT TRANS PANEL. ACCOMPLISH RII INSPECTION OF AMIS ITEM 2342111. INSTALLED INTERIM RPR PER ECRA 5310-05555.

Part: FLOORBEAM — CORRODED (BS 1661) · corrosion level 2 · airframe 79,234 hrs · 23,046 cycles

STA 1661 FLOORBEAM HAS CORROSION OUT OF SRM LIMITS IAW SCAL LP 9974514. FLOORBEAM UPPER CHORD REPLACEMENT IN REF TO ECRA 5310-05536 REPAIR 4. ACCOMPLISHED REPAIR, RII INSPECTED.

Part: FRAME — CORRODED (BS 1400) · corrosion level 2 · airframe 79,234 hrs · 23,046 cycles

AFT CARGO, FRAME BS 1460 HAS CORROSION ON FWD SIDE AT LWR ATTACH POINT FOR THE SHEAR TIE BETWEEN BL 0 AND RBL 4. ACCOMPLISH RII INSPECTION OF AMIS ITEM 2342110. INSTALLED INTERIM REPAIR PER ECRA 5310-05547.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 79,234 hrs · 23,046 cycles

RIGHT HORIZONTAL STAB SKIN AT HSBL 229 ABOVE THE REAR SPAR HAS CORROSION OUT OF SRM LIMITS. ACCOMPLISH RII INSPECTION OF AMIS ITEM 2342112. INSTALLED INTERIM REPAIR PER ECRA 5510-02241.

Part: DOOR FRAME — CORRODED (BS 1681) · corrosion level 2 · airframe 79,234 hrs · 23,046 cycles

BS 1681 R4 DOOR FRAME HAS CORROSION OUT OF SRM LIMITS. ACCOMPLISH RII INSPECTION OF AMIS ITEM 2342114. INSTALLED INTERIM REPAIR IN REF TO ECRA 5310-05554.

Part: FLOORBEAM — CORRODED (BS 1600) · corrosion level 2 · airframe 79,234 hrs · 23,046 cycles

BS 1600 FLOORBEAM HAS CORROSION OUT OF SRM LIMITS. ACCOMPLISHED FLOORBEAM UPPER TEE REPAIR BETWEEN BL 0 AND RBL 11 IAW ECRA 5310-05556.

Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 79,234 hrs · 23,046 cycles

BS 1681 FLOORBEAM HAS CORROSION OUT OF SRM LIMITS. ACCOMPLISHED FLOORBEAM UPPER TEE REPLACEMENT IAW ECRA 5310-05557.

Part: DOOR FRAME — CORRODED (BS 1681) · airframe 79,234 hrs · 23,046 cycles

BS 1681 R4 DOOR FRAME HAS CORROSION OUT OF SRM LIMITS. INSTALLED INTERIM REPAIR IN REF TO ECRA 5310-05554.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 79,234 hrs · 23,046 cycles

BS 1640 FLOORBEAM HAS CORROSION OUT OF SRM LIMITS. ACCOMPLISHED UPPER TEE REPLACEMENT IAW ECRA 5310-05536 REPAIR 5.

Part: FLOORBEAM — CORRODED (BS 1661) · corrosion level 2 · airframe 79,234 hrs · 23,046 cycles

BS 1661 FLOORBEAM HAS CORROSION OUT OF SRM LIMITS. ACCOMPLISHED FLOORBEAM UPPER TEE REPLACEMENT IAW ECRA 5310-05536 REPAIR 4.

Part: PRESSURE PANEL — CORRODED (BS 1681) · corrosion level 2 · airframe 79,234 hrs · 23,046 cycles

BS 1681 RBL 33 AFT PRESSURE DECK WEB HAS CORROSION OUT OF SRM LIMITS. ACCOMPLISHED PRESSURE DECK REPAIR IAW ECRA 5330-04259.

Part: FRAME — CORRODED (BS 1681) · corrosion level 2 · airframe 79,234 hrs · 23,046 cycles

BS 1681 FRAME LOWER SECTION HAS CORROSION OUT OF SRM LIMITS IAW SCAL LP 9974494. INSTALLED PERMANENT REPAIR.

Part: FRAME — CORRODED (BS 1460) · corrosion level 2 · airframe 79,234 hrs · 23,046 cycles

AFT CARGO LWR LOBE FRAME STA 1460 HAS CORROSION ON FWD SIDE AT LWR ATTACH POINT FOR THE SHEAR CLIP BTWN BL- 0 AND RBL-4. INSTALLED PERMANENT REPAIR.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 79,234 hrs · 23,046 cycles

RT HORIZONTAL STAB SKIN AT HSBL 229 ABOVE THE REAR SPAR HAS CORROSION OUT OF SRM LIMITS. ACCOMPLISHED A PERMANENT REPAIR.

Part: FRAME — CORRODED (BS 1480) · corrosion level 2 · airframe 79,234 hrs · 23,046 cycles

AFT CARGO FRAME HAS CORROSION ON UPPER CAP STA 1480 JUST OUTBOARD OF RT TRANS PANEL. INSTALLED PERMANENT REPAIR.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 79,234 hrs · 23,046 cycles

BS 365 FLOORBEAM HAS CORROSION OUT OF SRM LIMITS REF SCAL LP 9974291. CUT OUT THE DAMAGED SECTION OF THE UPPER CHORD AND INSTALLED A REPAIR SECTION. REF SRM 53- 10-08 REPAIR NR 3. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 324) · corrosion level 2 · airframe 79,234 hrs · 23,046 cycles

BS 324 FLOORBEAM HAS CORROSION OUT OF SRM LIMITS REF SCAL LP 9974293. CUT OUT DAMAGED SECTION OF UPPER TEE AND INSTALLED A NEW REPAIR SECTION. REF SRM 53-10-08 REPAIR NR 1. MAJOR REPAIR.

Part: DOOR — STUCK (RT OVERWING) · airframe 79,234 hrs · 23,046 cycles

RT OVERWING EMERGENCY SLIDE DOOR WOULD NOT OPEN WITH MANUAL HANDLE. FOUND DOOR WAS SEALED WITH OVER SPRAYED PAINT, PAINT WAS FOUND BETWEEN DOOR SEAL AND DOOR, LWR FWD LOCATION. REMOVED OLD GREASE FROM DOOR LATCH TUBE AND RE-LUBED. PERFORMED MANUAL AND PNEUMATIC DEPLOYMENT SYSTEM OPS TEST. OPS CHECKED GOOD.

Part: CONTROLLER — FAILED (NR 2 ENGINE) · airframe 79,234 hrs · 23,046 cycles

NR 2 ENGINE 14TH STAGE HPC UNIT FAILED TEST. REMOVED AND REPLACED NEW SERVICEABLE HPC FOR NR 2 ENGINE ON NR 9975046.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 79,234 hrs · 23,046 cycles

LEFT AC ELECTRIC HYDRAULIC PUMP FAIL, THE RECEPTACLE PIN DIAMETER CHECK PER CARD WORK INSTRUCTIONS. REMOVED AND REPLACED LT HYD PUMP PER AMM.

Part: SCUFF PLATE — DAMAGED (FUSELAGE) · airframe 79,160 hrs · 23,027 cycles

CREW REPORT: DOOR 4R SQUEALING FOR HALF OF FLIGHT. HANDLE IS LOOSE ALSO MAINT TEXT: LOWER SCUFF PLATES HAVE VOIDS ON INTERIOR THROUGH EXTERIOR .5 X .375 PIECE OF SCUFF PLATE MISSING RESULTING IN AIR LEAK. HANDLE IS OKAY. REPAIRED SCUFF PLATE PER AMM 801.

Part: O-RING — LEAKING (SPOILER ACTUATOR) · airframe 78,932 hrs · 22,961 cycles

ON WALK AROUND, NOTICED HYD FLUID ON BOTTOM OF LEFT WING. FOUND NR 2 SPOILER ACTUATOR LEAKING AT HYD 'B' NUT TO SPOILER ACTUATOR AT ONE DROP A MINUTE. CLEANED AREA REPAIR WITHIN 75 FLIGHT HOURS.

Part: BLEED VALVE — STICKING (APU) · airframe 78,911 hrs · 22,956 cycles

APU NOT PUTTING OUT AIR PRESSURE. APU AIR PRESSURE NORMAL, NO PACKS ON 32 PSI, 2 PACKS ON 28 PSI, MOTOR 1 ENG, DIPS TO 25 PSI RECOVERS TO 32 PSI. SUSPECT STICKING APU BLEED VALVE.

Part: SWITCH — FAULTY (HYD PUMP) · airframe 78,692 hrs · 22,888 cycles

LEFT ELECTRICAL HYD SWITCH DOES NOT SHUT SYSTEM OFF. REPLACED LT HYD PUMP SWITCH CAP AND MASTER MODULE. PRESSURE LIGHT IS NOW SOLID AND PUMP OPERATION AND INDICATIONS ARE ALL CORRECT.

Part: PCU — FAULTY (LT ELEVATOR) · airframe 78,547 hrs · 22,846 cycles

LEFT ELEVATOR PCU STATUS MESSAGE WILL NOT CLEAR. REPLACED LEFT OUTBOARD PCU PER MM, NO FAULTS ON TEST.

Part: WINDOW — ARCED (COCKPIT) · airframe 78,492 hrs · 22,829 cycles

NR 1 ON WINDOW HEAT INTERMITTENTLY INOPERATIVE, FOUND EVIDENCE OF DISCOLORATION AND ARCHING ON LOWER LT SIDE OF F/O'S FORWARD WINDSHIELD. REPLACED RT NR 1 WINDOW AND ACP COA 507402.

Part: DRIVE ASSY — FAILED (WX RADAR SYS) · airframe 78,460 hrs · 22,818 cycles

WEATHER RADAR MADE GRINDING SOUNDS DURING CLIMB. RADAR DISPLAYED IS NOT ACCURATE. REPLACED WEATHER RADAR DRIVE UNIT. OPS CHECKED AT GATE SHOWS NORMAL TEST DISPLAY AND NO GRINDING NOISE WHEN OPERATING TILT FUNCTION.

Part: SHUTOFF VALVE — FAULTY (FUEL SYSTEM) · airframe 78,155 hrs · 22,733 cycles

DURING ENG START FOR THE LEFT ENG, THE SPAR VLV LIGHT ILLUMINATED AND GOT EICAS MSG ENG SHUT DOWN. RESTART ATTEMPTED, AND WAS SUCCESSFUL, BUT THIS IS THE SECOND HIT, SEE HISTORY PTT 0472009. REPLACED LEFT ENGINE FUEL SHUTOFF VALVE PER MM.

Part: WINDOW — DELAMINATED (R2 DOOR) · airframe 78,152 hrs · 22,732 cycles

F/A REPORTS IN THE AIR IN BRIGHT SUNLITE DOOR 2R 3L OUTER WINDOWS DELAMINATED-VISUAL GLAZE. DEBRIEFED CREW, VISIBILITY WITHIN LIMITS PER MM 56-31-02 AT DOOR 3L. CREW WANTED 2R REPLACED. REFERENCE SEQUENCE 1522001 FOR 2R REPLACEMENT. REPLACED DOOR 2R WINDOW PER MM.

Part: FILTER — TORN (COCKPIT) · airframe 78,070 hrs · 22,710 cycles

COCKPIT ENVIRONMENT, EXTREMELY LOUD AND NOISY-AIR CONDITIONING BLOWN THROUGH THE WINDSHIELD. WEAR EAR PLUGS - TURNING RIGHT RECIRC OFF PROVIDES NO HELP. CLEANED DUCTS FOUND RT REC FAN FILTER TORN AND IN DUCTS. CLEANED DUCTS, RPL'D REC FILTERS FOUND RT FILTER TORN. DB WITHIN LIMITS.

Part: BLADE — DENTED (NR 2 ENGINE) · airframe 78,051 hrs · 22,706 cycles

NR 2 ENGINE HAS ONE BLADE WITH LEADING EDGE DAMAGED. BLADE MARKED. BLENDED DENT IN BLADE MARKED NR 2 ENG PER MM, AREA 8.

Part: BLADE — NICKED (NR 1 ENGINE) · airframe 78,051 hrs · 22,706 cycles

NR 1 ENGINE BLADE 25 HAS LEADING EDGE DAMAGE. BLENDED NICK OF BLADE 25 NR 1 ENG (AREA 2). INSPECTED BLENDING PROCESS AND ACCOMPLISHED HFEC PER NDT MM. NO CRACKS.

Part: DUCT — CLOGGED (COCKPIT) · airframe 78,047 hrs · 22,702 cycles

UNABLE TO CONTROL FLT DECK TEMP DURING DESCENT TEMP GOT DOWN TO 65F. FLT DCK TEMP TOO COLD. FOUND COCKPIT DUCTING CLOGGED. REMOVED DEBRIS AND REPLACED LT PACK TEMP SENSOR AND RT PACK FLOW CONTROL VALVE.

Part: SWITCH — DIRTY (R4 DOOR) · airframe 78,008 hrs · 22,689 cycles

NO SLIDE LIGHT ON WITH DOOR ARMED AT DOOR 4R. CLEANED SWITCH, SLIDE LIGHT OPS NORMAL.

Part: BRACKET — WORN (TE FLAP) · airframe 78,004 hrs · 22,688 cycles

RIGHT TRAILING EDGE INBD FLAP DRIVE BRACKET FITTING IS WORN, BEARING MIGRATED, AND BOLT WORN. REPLACED BRACKET ASSY IAW AMM. OPS CHECK GOOD. NO ADJ NEEDED.

Part: BATTERY — FAULTY (AMIN) · airframe 78,004 hrs · 22,688 cycles

MAIN BATTERY FAILS TEST JOB CARD 5-5010-A STEP 22U. AMPS DO NOT DROP TO ZERO WITHIN ONE TO TWO SECONDS. REPLACED MAIN BATTERY.

Part: UNKNOWN — MALFUNCTIONED (LT ENGINE) · airframe 77,994 hrs · 22,684 cycles

ABORTED TAKEOFF AT 100 KNOTS FOR LT ENG & SLOW TO RUN UP AT BRAKE RELEASE. LEFT ENGINE SPOOLED UP SLOW ON T/O ROLL. REJECTED T/O AT 100 KTS. ACCOMPLISHED VISUAL INSPECTION OF SVA ACTUATOR, LINKAGE, RODS AND RUNNER BLOCKS, FAN BLADES & TAIL PIPE ALL CHECK GOOD. ACCOMPLISHED ACCELERATION TEST PER JRH 2-5-64. TESTS GOOD.

Part: ALTIMETER — FAULTY (COCKPIT) · airframe 77,804 hrs · 22,629 cycles

F/O ALTIMETER ISSUE. DUE TO HISTORY OF F/O ALTIMETER REPLACE PRECAUTIONARY (PCN 481-9023), CONFIRM EFFEC WITH ONLINE IPC. RPLD F/O ALTIMETER PER MM, WITH BORROWED PART S-N 82050288.

Part: SEAL — LEAKING (COCKPIT) · airframe 77,685 hrs · 22,595 cycles

LOUD HISS COMING FROM AFT PART OF F/O SIDE WINDOW. F/O SLIDING WINDOW BULB SEAL LEAKS ACCESSIVELY DURING PRESSURIZATION, BULB SEAL IS DEFORMED ALSO. RPLD F/O SLIDING WINDOW BULB SEAL. PRESSURIZED ACFT TO 4D PSI, STILL HAVE LEAKAGE AT FWD LWR PORTION OF WINDOW (MARKED) BUT NO NOISE NOTED.

Part: CIRCUIT CARD — FAULTY (RT ENGINE) · airframe 77,586 hrs · 22,567 cycles

R ENG BLEED OFF EICAS MSG ON TAKEOFF. REPLACE R ENGINE SPEED CARD. RAN ENGINE PER JRH, OPS CKS OKAY.

Part: LINKAGE — BROKEN (SEQUENCE VALVE) · airframe 77,550 hrs · 22,555 cycles

LEFT MLG DOOR SEQUENCE VALVE LINKAGE IS BROKEN AT LOWER BRKT ASSY, REPLACED DOOR SEQUENCE VALVE PER MM, OP CHECKED GOOD.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 77,550 hrs · 22,555 cycles

LEFT WING INBD FLAP LEADING EDGE GOUGED ON OUTBD END, APPROX 2.5 FT FROM END. GOUGE MEASURED .014, REPAIRED IAW SRM.

Part: HINGE — WORN (LT MLG DOOR) · airframe 77,550 hrs · 22,555 cycles

LEFT MLG DOOR IS LOOSE AT KEEL SUPPORT. THE CENTER AND AFT HINGE POINTS SHOW WEAR AT BOLTS CONNECTING THE HINGE TO THE FRAME. REMOVED LT MLG DOOR. INSTALLED NEW HARDWARE AND INSTALLED LEFT MLG DOOR PER MM. ACCOMPLISHED OP CHECK PER MM, DOOR CHECKED GOOD.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 77,550 hrs · 22,555 cycles

EMERGENCY LIGHTS INOPERATIVE. REPAIRED EMERGENCY LIGHT FEEDER CABLE AND LIGHTS CHECKED OKAY.

Part: THRESHOLD — DAMAGED (CARGO DOORWAY) · airframe 77,511 hrs · 22,543 cycles

CARGO DOOR SCUFF PLATE HAS DENT AND CRACK BETWEEN THE 5TH AND 6TH SCREW ATTACHMENT FROM FRONT OF AIRCRAFT AT TOP OF SCUFF PLATE. DENT IS 1. BY .50 WITH A CRACK IN THE DIAMETER OF THE DENT MEASURING .75 INCHES LONG. THRESHOLD REMOVED. TRANSFERRED ALL HOLES FROM OLD THRESHOLD TO NEW THRESHOLD, REPLACED THRESHOLD.

Part: MODULE — FAILED (FIRE DETECTION) · airframe 77,271 hrs · 22,473 cycles

NO SYS FAIL LIGHT DURING FIRE LIGHT CHECK. REPLACED MASTER MODULE AND CIRCUIT BOARD FOR FAIL SWITCH ON FIRE OVERHEAT PANEL, CHECKED OKAY.

Part: CONTROL MODULE — FAILED (SPOILERS) · airframe 76,939 hrs · 22,378 cycles

CHRONIC SPOILER MSG EICAS MESSAGE, ALSO DOES NOT PASS SPEED BRAKE TEST. REPLACED NR 3 SCM, SPOILER TEST GOOD.

Part: TURBINE CASE — CRACKED (NR 2 ENGINE) · airframe 76,872 hrs · 22,359 cycles

NR 2 ENGINE 3RD STAGE LPT HAS L/E CRACK THAT IS LESS THAN .125 IN LENGTH. REPLACED ENGINE.

Part: ACTUATOR — FAILED (APU INTAKE) · airframe 76,770 hrs · 22,331 cycles

AT GATE, APU FAILED WITH FAULT LIGHT. TRIED RESTART 3 TIMES, FAILED ALL 3 TIMES. REMOVED AND REPLACED APU INTAKE DOOR ACTUATOR IAW AMM. OPS CHECKED NORMAL.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT TEMP) · airframe 76,673 hrs · 22,298 cycles

FLT DECK AUTO TEMP CONTROLLER DOES NOT CONTROL TEMP. OVERHEATS, FLEW WITH TRIM AIR OFF. ACCOMPLISHED SERVICE TIP 21-61-00. NO FAULTS NOTED ON ZONE TEMP CONTROLLER BITE TEST. CLEANED TEMP SENSOR. OPS CHECKED NORMAL. PROBLEM RECURRED. UNABLE TO CONTROL COCKPIT TEMP. TEMP FULL COLD, TEMP 96. AUTO MODE AND STBY MODE OF LEFT PACK CREATED DUCT TEMP OVER 120 DEG WITH TEMP SET TO FULL COLD. F-D TRIM AIR VALVE INDICATED CLOSED ON ECS PAGE. SELECTED LEFT PACK OFF, WITH RT PACK ON DUCT TEMP DECREASED. LEFT PACK CONTROLLER NOT TESTING. LEFT PACK INOPERATIVE PER MEL. PERFORMED BITE TEST ON BOTH PACK CONTROLLERS, NO FAULTS FOUND. OPERATED PACKS, BOTH SYSTEMS NORMAL. TRIM VALVES MATCHED TEMP SELECTIONS.

Part: SHUTOFF VALVE — FAULTY (STARTER VALVE) · airframe 76,650 hrs · 22,291 cycles

LT STARTER CUTOUT EICAS MESSAGE DISPLAYED. START VALVE LIGHT ILLUMINATED ALONG WITH EICAS MESSAGE. MASTER CAUTION BOTH EXTINGUISHED AFTER 5 SECONDS. REPLACED STARTER SHUT-OFF VALVE AND OP CHECKED GOOD.

Part: SHUTOFF VALVE — STICKING (FLT CONTROLS) · airframe 76,630 hrs · 22,287 cycles

RIGHT FLIGHT CONTROL SHUTOFF VALVE STICKING. REPLACED RIGHT FLIGHT CONTROL SHUTOFF VALVE, OPS CHECKED GOOD.

Part: HANDLE — LACK OF LUBE (COCKPIT) · airframe 76,387 hrs · 22,210 cycles

FLAP HANDLE STIFF TO MOVE AFT OF POSITION 1. INSPECTED FLAP HANDLE AND PULLEYS NO DEFECTS NOTED. HANDLE NOT SMOOTH TO MOVE. FEELS LIKE FLAT SPOTS IN EITHER DIRECTION OF MOVEMENT. WORKED HANDLE SEVERAL TIMES. REMOVED TOP COVER TO INSPECT. FOUND NO DEFECTS. SPRAYED AND LUBED HANDLE. WORKED HANDLE AGAIN, HANDLE FELT FINE IN ALL SPOTS.

Part: LANYARD — LOOSE (EVAC SLIDE) · airframe 76,374 hrs · 22,204 cycles

STRING NEAR SLIDE PACK AND COVER AT 4R COMING LOOSE. SECURED LOOSE LANYARD.

Part: SWITCH — FAULTY (APU) · airframe 76,201 hrs · 22,152 cycles

APU HAD SHUTDOWN, FAULT LIGHT ILLUM AND EICAS MSG. APU FAULT DISPLAYED. CREW COMMENTS: APU AUTO SHUTDOWN TWICE. ACP MEL 4911E. REPLACE AS PER AMM T-S 49-11-00 PAGE 150 FIGURE 112, DPI WAS NOT POPPED, REPLACED DELTA-P SWITCH AS PER MM, RAN APU, LOADED IT UP ELECTRIC AND PNEUMATIC OPS OK.

Part: CONTROLLER — FAULTY (APU) · airframe 76,171 hrs · 22,140 cycles

APU AUTO SHUTDOWN AT GATE. NO TIME TO T-S INOP APU, NO MSG PRESENT. IF APU REPLACEMENT IS REQUIRED, PLEASE INSTALL S/N 61811 IF POSSIBLE. -INF- :AUTO SHUTDOWN WITH GEN FILTER ON BITE. -INF- :CHECK DPI AND FILTERS. NO DEFECTS FOUND. CHANGED APU CONTROLLER RAN APU. AFTER 20 MINUTES APU AUTO SHUTDOWN. NEED GEN DELTA P SWITCH (PCN 481-1503). RESET ECB AND OPERATED APU FOR OVER AN HOUR LOADED. CHECKS NORMAL.

Part: HINGE — BROKEN (RT WING SLIDE) · airframe 76,167 hrs · 22,139 cycles

RIGHT SIDE SLIDE SERVICE PANEL FOUND OPEN WHEN ACFT ARRIVED AT GATE. PANEL IS OFF WING ESCAPE SLIDE DISABLE PANEL FOR MAINT ONLY NO EFFECT ON PN SLIDE OPERATION, WILL OPS NORMAL. HINGE SPRINGS ARE BROKEN. REPLACED HINGE ASSY, OPS CHK OK.

Part: FLAPPER VALVE — FAULTY (LAVATORY) · airframe 76,115 hrs · 22,125 cycles

MOST AFT COACH LAV 136 FLAPPER IN BOWL WILL NOT CLOSE. ADJ AFT CABIN MOST AFT LAV TOILET FLAPPER.

Part: EXCITER — FAULTY (APU ENGINE) · airframe 75,914 hrs · 22,065 cycles

APU FAULT ON START. BITE APU BOX, 2 MSG LATCHED, NO FLAME LIGHT-OFF, CLEARED MSG AND TRY RESTART, NO JOY. GOT 30 PERCENT THEN APU FAULT STATUS MSG. EXCITER FAULTY.

Part: LANYARD — OUT OF POSITION (GIRT BAR) · airframe 75,618 hrs · 21,971 cycles

DOOR 3R WILL NOT ARM. LANYARD UNDER GIRT BAR REPOSITIONED. DOOR ARMS GOOD.

Part: ATTACH FITTING — LOOSE (R3 DOOR) · airframe 75,485 hrs · 21,933 cycles

SLIDE LIGHT DOOR 3R INOPERATIVE. FOUND FLOOR FITTING ATTACH SCREWS NOT SCREWED DOWN ALL THE WAY PREVENTING DOOR FROM ARMING. SECURED SCREWS. DOOR ARMING OPERATION NORMAL.

Part: PCU — FAULTY (LT ELEVATOR) · airframe 75,301 hrs · 21,876 cycles

STATUS MESSAGE L ELEV PCU WILL NOT ERASE. MESSAGE ERASES WITH NO HYD POWER APPLIED. RETURNS WITH HYD POWER APPLIED. DF'D REF MEL COMPLIED WITH MEL. 2721D. SAM NOTIFIED OF STATUS PER MEL. FOUND THE MOST INNER PDU INBD TO BE THE CAUSE OF MESSAGE. FOUND THE MOST INNER PCU TO BE THE CAUSE OF MESSAGE. REPLACED THE PCU.

Part: IDG — FAULTY (POSITION 1) · airframe 74,507 hrs · 21,649 cycles

NR 1 IDG TEMP SENSOR MESSAGE INTERMITTENTLY ON. NO TIME TO T/S, HAS HISTORY. REPLACED NR 1 IDG, OPS GOOD.

Part: TRANSCEIVER — OUT OF TOLERANCE (ELT) · airframe 74,325 hrs · 21,595 cycles

BOTH ELTS ARE OUT OF TOLERANCE. REPLACED AFT ELT & FWD ELT TRANSMITTERS.

Part: PILOT VALVE — FAILED (NR 2 ENGINE) · airframe 74,077 hrs · 21,524 cycles

AT CRUISE LEFT DUCT PRES 26 RT 42 PSI. THEN BOTH AT 26. ACP TROUBLESHOOTING IAW SERVICE TIP. REPLACED HIGH STAGE PILOT ON NR 2 ENG IAW MM. ACCOMPLISHED PNEUMATIC HEALTH CHECK OF HPSOV AND HIGH PRESSURE CONTROLLER IAW MM. SYS OPS CHECKED GOOD.

Part: BAFFLE — UNSECURE (CABIN AIR) · airframe 74,061 hrs · 21,517 cycles

LOUD AIR FLOW FROM CTR AISLE AIR DISTRIBUTION DUCT ROW 12 AND STUFFY AND LOW FLOW AFT CABIN. RESECURED LOOSE AIR BAFFLE ON CTR OVERHEAD AIR DISTRIBUTION DUCT NEAR SEAT ROW 21.

Part: SHUTOFF VALVE — BINDING (NR 2 ENGINE) · airframe 74,061 hrs · 21,517 cycles

RIGHT HIGH STAGE VALVE NOT OPENING. IN FLT, RT DUCT PRESSURE READS ABOUT 10 PSI LOW AND SUSPECTED HIGH STAGE SYS. AT ARRIVAL, IT APPEARED TO WORK OK. DUE HISTORY ON NR 2 ENG BLEED SYS. REPLACED NR 2 ENG HPSOV DUE TO FAILED HEALTH CHECK. ACCOMPLISHED PNEUMATIC HEALTH CHECK ON NR 2 ENG IAW MM. . HPSOV FAILED PNEUMATIC HEALTH CHECK DUE TO IT BINDING.

Part: PRESSURE SWITCH — FAULTY (HYD SYSTEM) · airframe 74,009 hrs · 21,500 cycles

LT HYD RSV PRESS ON EICAS AND OVHD PANEL ON TAXI IN. REPLACED RESEVOIR PRESSURE SWITCH AND RESERVOIR DEPRESSURIZATION VALVE. OPS CHECKED FOR 10 MINUTES, CHECKED OK.

Part: BLEED VALVE — FAULTY (RT ENGINE) · airframe 73,940 hrs · 21,477 cycles

RT ENG BLEED VALVE OFF LIGHT NOT ILLUMINATING. FOUND RT ENG PRSOV NOT FULLY CLOSING WITH NO AIR APPLIED, REPLACED RT-ENG PRSOV IAW MM. NO LEAKS WITH APU BLEED ON, CKD NORMAL ON ENG RUN, NO FAULTS.

Part: BUSS — FAULTED (LEFT) · airframe 73,888 hrs · 21,461 cycles

LEFT BUSS PROBLEM, RTFL. AFTER ACFT PARKED RESET THE C-B & DID NOT TRIP, INSPECTED ALL WIRING RELATED TO THE SYS IN P6 PANELS, NO LOOSE OR OVERHEATED CONNECTIONS NOTED, REPLACED C/B C326,TRANSFORMER T10040 AND RELAY K10566. RUN BOTH ENG WITH HEAVY ELC LOAD,TESTED HMG, BPCU HAS NO RELATED FAULT HISTORY.

Part: SENSOR — MALFUNCTIONED (BLEED SYS) · airframe 73,888 hrs · 21,460 cycles

ON SHUTDOWN RT ENGINE BLEED DID NOT CLOSE AND APU VALVE DID NOT OPEN. REPLACED K10201. DRY MOTORED ENGINE. CHECKED OK.

Part: FITTING — OUT OF ADJUST (R3 DOOR) · airframe 73,798 hrs · 21,436 cycles

DOOR 3R WILL NOT ARM. DOOR ARMS BUT SLIDE LIGHT IS NOT COMING ON WHEN DOOR IS ARMED. COMPLIED WITH MEL CARD. TRIED NEW LED LIGHT, NO HELP. FOUND SLIDE LIGHT WOULD ILLUM WHEN ARM HANDLE FULLY SET TO ARM. ADJUSTED PROX SW FLOOR FITTINGS AND SECURED LANYARDS THAT WERE BINDING GIRT BAR. SLIDE LIGHT AND DOOR ARMS OKAY.

Part: PITOT TUBE — SHORTED (RIGHT) · airframe 73,732 hrs · 21,421 cycles

FIRST OFFICER PITOT TUBE GLOWING RED HOT ON GROUND. FOUND RIGHT AUX PITOT TUBE HEATER SHORTED TO CASING. REPLACED RIGHT AUX PITOT TUBE, HEATER CIRCUITS TEST OKAY.

Part: SWITCH — FAULTY (HYD SYSTEM) · airframe 73,654 hrs · 21,401 cycles

LEFT RESERVOIR LIGHT ON OVERHEAD ILLUMINATED. LOW PSI RESERVOIR LIGHT ON AFTER TURNING ON AND OFF ELEC PUMPS, RAN LEFT ENG AND THE LOW PSI RESERVOIR LIGHT STAYED OUT. WRENCH CHECKED LINES AND FOUND NO LEAKS. INSPECTED PLUMBING AND B-NUTS, NO LEAKS FOUND. REPLACED RESERVOIR PRESSURE SWITCH PER MM. LIGHT REMAINED OUT USING APU WITH PUMP, PACKS AND EAI'S SELECTED ON. OPS CHECKS OKAY.

Part: ACTUATOR — MALFUNCTIONED (NR 7 SPOILERS) · airframe 73,556 hrs · 21,368 cycles

SPOILERS EICAS MESSAGE ON DESCENT WHEN SPOILER HANDLE IN USE INFLIGHT. FOUND "PCA 7 FAULT" DISPLAYED ON 3 LT SPOILER CONTROL MODULE M532, TYPE: INTERMIT, PHASE: DESCENT. DID NOT CLEAR MODULE MEMORY. SPOILER 6 AND 7 ARE LOCKED OUT IN THE DOWN POSITION. PERFORMED TEST OF THE NR 7 SPOILER. FOUND RESISTANCE AT ALL PIN LOCATIONS AND CORROSION AT CONNECTOR ON PCA. REPLACED NR 7 PCA REF MM AND OP AND LEAK CHECKED GOOD.

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 73,391 hrs · 21,324 cycles

NR 2 ENG PYLON ENG HYD MODULE, FWD MOST HYD UNION IS LEAKING 20 DPM WITH ENGINE RUNNING. REPLACED O-RING ON LEAKING UNION. SECURED ALL HYD LINES. BOLTS ON HYD MODULE NEED TO BE REINSTALLED AND CONNECTOR PLUG INSTALLED. REINSTALLED BOLTS AND RAN ENGINE, NO LEAKS NOTED.

Part: CONNECTOR — LEAKING (HYD SYSTEM) · airframe 73,391 hrs · 21,324 cycles

NR2 ENG HYD PUMP PRESS SWITCH SW 10541 CONNECTOR PLUG D6242 IS CONTAMINATED FROM LEAK ON MODULE. REPLACED CONNECTOR. NO LEAKS DETECTED.

Part: IDG — LEAKING (NR 2) · airframe 73,391 hrs · 21,324 cycles

NR 2 ENG IDG LEAKING OIL FROM POWER FEEDER CABLE TERMINALS. REPLACED NR 2 ENG IDG PER MM. OPS NORMAL.

Part: MODULE — FAULTY (STALL WARNING) · airframe 73,200 hrs · 21,270 cycles

RT STALL WARNING INOP. REPLACED BITE MODULE.

Part: ACTUATOR — FAULTY (SPOILERS) · airframe 73,196 hrs · 21,268 cycles

SPOILERS EICAS AND OVERHEAD LIGHT ON. SPOILER CONTROL MODULE 3L HAS PCA FAULT, SPOILERS NR 4 AND NR 9 PER FIM. COMPLIED WITH MEL 2761A, DL8057 CREATED TO MONITOR. REPLACED NR 4 GRD SPOILER ACTUATOR PER MM, OPS TEST GOOD.

Part: VALVE — FAILED (HYD SYSTEM) · airframe 73,094 hrs · 21,237 cycles

AIRCRAFT BELLY SATURATED WITH HYDRAULIC FLUID FROM MLG TO TAIL. FOUND SLAT BYPASS VALVE SPRAYING FLUID WHEN SLATS ARE OPERATED. REPLACED VALVE WITH BORROWED PART. PART COMPATIBLE PER OLIPC. REPLACED AND OPS CK GOOD PER MM.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 73,076 hrs · 21,232 cycles

SMOKE TYPE VAPOR EXITING AROUND RT PACK EXHAUST VENTS. FOUND HYD LEAK JUST FWD OF LEFT AIR COND BAY. TIGHTNED LOOSE CONNECTION AND CHECKED ALL OTHER HYD LINES IN AREA. LEAK STOPPED, CLEANED AREA OF ACCESS LIQUID USING RAGS. NO FUMES NOTED IN AIR CONDITIONING SYSTEM. SYSTEMS LEAK CHECK OKAY.

Part: CONTROL MODULE — FAULTY (POS 3L) · airframe 72,988 hrs · 21,202 cycles

EICAS MESSAGE 'SPOILERS' DISPLAYED. SPOILERS LIGHT ILLUMINATED WITH SPEEDBRAKE LEVER SELECTED TO UP. SPOILER EICAS ON DESCENT. FEELS LIKE THEY ARE WORKING. ONLY FAULT DETECTED WAS AN SCM OR WIRING FAULT FOR THE -200 TYPE MODULE IN POS 3L. REPLACED SCM AT POS 3L WITH -100 TYPE. SYSTEM TEST REF THE MM SHOWED NO FAULTS OR MESSAGES.

Part: ACTUATOR — LEAKING (MLG) · airframe 72,925 hrs · 21,184 cycles

FLUID NOTICED BENEATH RT MAIN TRUCK UNDER 30 DROPS IAW MIN. UPON ARRIVAL TO GATE, NO LEAKS NOTED. RT TILT ACTUATOR HAS SOME SIGNS OF MINOR LEAKAGE, BUT NO LEAKAGE NOTED AT GATE. REPLACED TILT ACTUATOR, OPS CHECKS GOOD.

Part: CONTROL UNIT — WRONG PART (SPOILERS) · airframe 73,218 hrs · 21,274 cycles

EICAS MESSAGE 'SPOILERS' DISPLAYED. SPOILERS LIGHT ILLUMINATED WITH SPEEDBRAKE LEVER SELECTED TO DOWN. ACCOMPLISHED CHRONIC REVIEW. REPLACED SPOILER CONTROL MODULE PER AMM. FOUND -100 SERIES INSTALLED; INSTALLED -200 SERIES PER AMM.

Part: LANYARD — OUT OF POSITION (R1 DOOR) · airframe 72,540 hrs · 21,062 cycles

DOOR 1R HARD TO ARM. FOUND LANYARD FOR SURVIVAL KIT HANGING OUT AND IN THE WAY OF ARMING MECHANISM. RESTOWED LANYARD - DOOR ARMS NORMALLY.

Part: TERMINAL BLOCK — LOOSE (COCKPIT WINDOW) · airframe 72,304 hrs · 20,984 cycles

FOUND TERMINAL BLOCK J1 LOOSE AT CAPT'S NR1 WINDOW. NEED TO REPLACE NR1 CAPT'S WINDOW. REMOVED WINDOW. REMOVED WINDOW. INSTALLED NEW CAPT'S NR 1 WINDOW, WINDOW HEAT OPS OK, COMPLETED 2ND TORQUE & SEALED, SEALANT CURED, REMOVED TAPE & REPOSITIONED WIPER BACK TO PARK.

Part: RELAY — FAULTED (PITOT SYSTEM) · airframe 72,233 hrs · 20,962 cycles

RIGHT AUX PITOT LIGHT & EICAS ON TOUCHDOWN. REPLACED RELAY K10847 AND RT AUX PITOT PROBE PER MM. OPS CHECK OK PER MM.

Part: INVERTER — FAILED (STATIC) · airframe 72,193 hrs · 20,948 cycles

STATIC INVERTER EICAS MESSAGE. REPLACED STATIC INVERTER, OPS CHECK GOOD.

Part: TRANSCEIVER — FAILED (WX RADAR SYS) · airframe 72,135 hrs · 20,928 cycles

WEATHER RADAR FAIL ON EFIS. FOUND DEFECTIVE TRANSCEIVER. REPLACED TRANSCEIVER PER MM. OPS ARE GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,953 hrs · 20,876 cycles

NR2 LT ENTRY DOOR EMERGENCY LIGHT IS INOP. REPLACED LAMP AND OPS CHECKED GOOD.

Part: EXCITER — FAILED (APU) · airframe 71,866 hrs · 20,853 cycles

ATTEMPTED TWO STARTS OF APU, NO LIGHT OFF AND FAULT LIGHT DISPLAYED. REPLACED EXCITER BOX. FL 340 APU RUNS NORMAL. CREW CONFIRMED APU OPERATED NORMAL.

Part: EXCITER — FAULTY (APU) · airframe 71,845 hrs · 20,848 cycles

APU FAULT ON START DURING TAXI IN. APU BITE INDICATES FAULTY IGNITION UNIT. NO TIME TO FURTHER TROUBLESHOOT. REPLACED IGNITER, CABLE AND BOX PER MM'S, OPS OKAY.

Part: FUEL CONTROL — LEAKING (APU) · airframe 71,816 hrs · 20,833 cycles

FUEL LEAKING FROM APU WHILE RUNNING: APPEARS TO BE COMING FROM FUEL CONTROL. REPLACED APU FUEL CONTROL. LEAK CKS OK, APU OPERATES NORMAL.

Part: SEAL — LEAKING (STARTER) · airframe 71,816 hrs · 20,833 cycles

NR 1 ENG HOC TROUBLE SHOOTING. DUE TO CONTINUED ABOVE NORMAL OIL USAGE NEED TO PERFORM HOC TROUBLESHOOTING. BAGGED AND HIGH POWER RAN. FOUND STARTER SEAL LEAKING, REPLACED STARTER SEAL AND CKD FOR LEAKS. NO LEAKS ON STARTER SEAL.

Part: SWITCH — FAULTY (POSITION A) · airframe 71,816 hrs · 20,833 cycles

APU INOPERATIVE. 'LOP' ON APU BITE WITH AUTO SHUTDOWN DURING START AT 95 PERCENT RPM (ECU DOES NOT MONITOR LOP UNTIL 95 PERCENT). WITH LOP FAULTS PRIOR TO APU RPLM'T 10JULY, ACP'D WIRING RING OUT BETWEEN LOP SWITCH, PIN 1 TO ECU BENCH PLUG, PIN C5 AND GRD IS AT LOP SW, PIN 2--ALL CHECKS OK. REPLACED PRESS AND GEN SCAV FILTERS REF MM (FILTERS WERE CLEAN). WITH DIRECT READING GAUGE AT LUBE PUMP TEST PORT, OIL PRESS IS 22 PSI (NORMAL IS 65+-5 PSI). REMOVED DEOIL SOLENOID TO VERIFY FULLY CLOSED, CHECKED OK. REINSTALLED DEOIL SOLENOID. VERIFIED GEN SCAV PUMP OPS NORMAL WITH APPROX 4-6 OZ'S OIL DRAINING OUT ON REMOVAL OF IT'S CHIP DETECTOR PLUG HOUSING. REPLACED APU FUEL CONTROL. LEAK CHECKS OK, APU OPERATES NORMAL

Part: CHARGER — FAULTY (APU BATTERY) · airframe 71,816 hrs · 20,833 cycles

APU BATTERY WILL NOT CHARGE. BATTERY CHARGER NOT OPERATIVE. REPLACED APU BATTERY CHARGER PER MM. OPS CK OKAY.

Part: SWITCH — FAULTED (APU) · airframe 71,669 hrs · 20,789 cycles

APU FAULT ON START. APU FAULT ON START. ECU BOX SHOWS LOP FAULT. CLEARED MSG, ATTEMPT TO START APU, FAULTS AT 89 PERCENT AND SHUTS DOWN. BITE FAULTS 'LOP'. ON START APU COMES UP TO APPROX 90 PERCENT THEN SHUTS DOWN. FAULT LIGHT AND "LOP" ON BITE. NO SWITCH IN STOCK DEN. REPLACED LOW OIL PRESSURE SWITCH. APU RAN FOR 30 MIN THEN AUTOSHUT DOWN. BITE SHOWS LOP. NEXT STEP IS CHANGE DE-OILER SOLENOID. REPLACED DE-OILER SOLENOID PER MM, NO HELP. T-S PER MM FOUND OIL FILTER DPI POPPED. REPLACED APU OIL FILTER PER MM, APU STARTED OK, NO LEAKS NOTED.

Part: CHARGER — FAULTY (APU) · airframe 71,643 hrs · 20,777 cycles

APU NO START 2 ATTEMPTS EGT 780 - RPM 20 PERCENT. STARTED APU, NOTED APU BAT VOLTS WENT TO 14 DURING START. SUGGEST REPLACING APU BAT AND CHARGER. BIT APU CONTROLLER, GOT LOP FAULT--LOW OIL PRESS. FOUND OIL QTY LOW--ADDED 1QT. APU STARTED NORMALLY.

Part: LINE — DAMAGED (LT DUCT) · airframe 71,516 hrs · 20,744 cycles

LT DUCT PRESS FLUCTUATES BY 20 TO 30 PSI DURING DESCENT. THROTTLES IDLE. REPLACED HI-STG VLV STILL FLUCTUATES 10-14 PSI. NEED FURTHER TROUBLESHOOTING. NEEDS NEW SUPPLY PRESS HOSE ASSY, B-NUT THREADS DAMAGED. REPLACED LINE, NO HELP. REPLACED HIGH STAGE VALVE, NO HELP. NEEDS FURTHER T.S. VALVE LOCK IAW MEL REPLACED NR1 ENGINE PRSOV VALVE (SN 1176) AND THE HIGH STAGE PILOT VALVE (PN 3399004, SN 162).

Part: REGULATOR — FAULTY (LT ENGINE) · airframe 71,460 hrs · 20,727 cycles

L ENG BLEED ON DURING CLIMB. REPLACED PRSOV. REPLACED REGULATOR & REPLACED HIGH STAGE PILOT (P/N 3399004-6U2 SERIAL 86). OPS CHECK WITH ENGINE RUN AND 3 MIN HIGH PWR IDLE RUN. NO FAULTS NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,324 hrs · 20,394 cycles

EMERGENCY LIGHT STRIP IN FRONT OF 1ST CLASS CLOSET IS INOP. ALL ADJACENT STRIPS WORK. RELAMPED, OPS CHK'D OKAY.

Part: VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 70,331 hrs · 20,396 cycles

RIGHT ENG HI STAGE LIGHT ILLUMINATED AS POWER WAS ADVANCED FOR TAKEOFF. CREW COMMENTS: RIGHT ENG HI STAGE LIGHT ILLUMINATED AS POWER WAS ADVANCED FOR TAKEOFF. VALVE LOCKED CLOSED PER MEL. REPLACED NR 2 ENGINE HIGH STAGE PILOT. ACCOMPLISHED TAKEOFF POWER CHECK FOR 5 MINUTES & PNEUMATIC SUPPLY TEST, CHECKS OKAY.

Part: RING — OUT OF POSITION (R2 DOOR) · airframe 68,702 hrs · 19,948 cycles

DOOR 2 RIGHT SLIDE ATTACHMENT RING OFF. REINSTALLED SLIDE ATTACH RING TO HOOK AND LOOP.

Part: LINE — DAMAGED (HIGH STAGE) · airframe 68,119 hrs · 19,776 cycles

ENG DUCT PRESSURES SPLIT DURING CRUISE WITH ISOL VLV CLOSED & BLEED SWITCH SELECTED ON. RECORD DUCT PRESSURES. LEFT 42 PSI. RIGHT 27 PSI. REPLACED HIGH STAGE PILOT CONTROL, DUE TO HIGH PRESSURE SENSE LINE UNION CROSS THREAD REPLACEMENT. PERFORMED RUN UP TO VERIFY DUCT PRESSURE NORMAL AT 26-29 PSI. ENGINE RUN OK PER CREW.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 68,105 hrs · 19,771 cycles

OXYGEN MASK DEFECTIVE AT1. (1=CAPT,2=1ST OFF,3=1ST OBS). CREW COMMENTS: CAPT O2 MASK LEAKS WHEN OUT OF STORAGE POSITION OK IN. REPLACED CAPT'S O-2 MASK.

Part: SHUTOFF VALVE — FAULTY (NR 1 ENGINE) · airframe 67,924 hrs · 19,719 cycles

ENG DUCT PRESSURES SPLIT DURING CRUISE WITH ISOL VALVE CLOSED & BLEED SWITCH SELECTED ON. RECORD DUCT PRESSURES. LT DUCT PRESS 40 PSI RT DUCT PRESS 30 PSI. REPLACED NR 1 ENGINE HIGH PRESSURE SHUTOFF VALVE.

Part: ACTUATOR — FAILED (AILERON TRIM) · airframe 67,532 hrs · 19,602 cycles

AILERON TRIM INOPERATIVE. REPLACED AILERON RUDDER TRIM PANEL RUDDER TRIM SYSTEM, OP CHECK OK, AILERON SYSTEM NO HELP. NEED AILERON TRIM ACTUATOR. AILERON TRIM ACTUATOR, OPS CHECKS GOOD.

Part: TRANSMITTER — FAULTY (NR 1 ENGINE) · airframe 67,352 hrs · 19,545 cycles

NR 1 ENGINE OIL PRESSURE INDICATION. REPLACING OIL PRESSURE XMITTER. DUE TO PREVIOUS HISTORY OF LOW OIL PRESS EICAS MSG LT ENG, REPLACING LOW OIL PRESSURE SWITCH. LEAK CHECKED & NO LEAKS NOTED.

Part: ANTI-ICE VALVE — FAILED (LT ENGINE) · airframe 67,276 hrs · 19,521 cycles

LEFT ENG ANTI-ICE EICAS AND VALVE LIGHT IN SWITCH WITH SWITCH IN OFF POSITION. VALVE OPERATED A COUPLE TIMES NORMAL, THEN IT STAYED IN THE OPEN POSITION, LOCKED OPEN PER MEL. REPLACED VALVE.

Part: VALVE — FAULTY (LE SLAT) · airframe 67,259 hrs · 19,514 cycles

ON AUTO SLAT EXTENSION TEST SLATS FAIL TO EXTEND SMOOTHLY. CHANGED SOL VLV ASSY BORROWED FROM NWA, NOW FLAPS WILL NOT EXTEND HYD FOUND INPUT SHAFT SHEARED FROM THE FLAP DRIVE UNIT TO THE PDU. WHEN ACP AUTO SLAT EXTENSION TEST, SLATS START, STOP, THEN CONTINUE TO FULL DOWN, INSTEAD OF ONE MOVEMENT. BOTH LEFT AND RIGHT STALL SYS. REPLACED T/E FLAP POWER DRIVE VALVE ASSY.

Part: PIN — BROKEN (CONNECTOR) · airframe 67,259 hrs · 19,514 cycles

FOUND FWD OF AFT LAV EMERGENCY EGRESS LIGHTING SM STRIP. PINS BROKEN AT END OF PLUG. REPLACED EEL LIGHTING STRIP IN FRONT OF AFT FWD LAV.

Part: VALVE — FAILED (BLEED AIR SYS) · airframe 66,647 hrs · 19,342 cycles

IN CRUISE FL400 L BLEED PRESS FLUCTUATED DOWN 2 AROUND 24 PSI. THEN WENT DOWN AND STAYED AT 24 PSI MAINT TEXT: PER VERBAL FROM INBOARD CREW LT 24 PSI RT 42 PSI REMAINDER OF CRUISE FLT. REPLACED VALVE AND CONTROL PER MM 36-11-07 AND MM 36-11-08. ACCOMPLISHED NR 2 ENG PNEUMATIC SYSTEM CK ACCT HPSOV, PILOT VALVE AND DAMAGED SENSE LINE REPLACED. ACP RUN PER JRH WITH NO DEFECTS NOTED.

Part: ACM — FAULTY (AC BAY) · airframe 66,432 hrs · 19,280 cycles

RIGHT PACK INOP LIGHT ON AND EICAS MSG "RIGHT PACK TEMP". FLT DIVERTED. REPLACED RIGHT PACK ACM. OPS CHECK RIGHT PACK OKAY.

Part: TRANSCEIVER — FAILED (RT HF SYSTEM) · airframe 65,293 hrs · 18,962 cycles

RIGHT HF WILL RECEIVE BUT WILL NOT TRANSMIT. REPLACED NR 2 HF TRANSCEIVER.

Part: CONTROLLER — FAULTY (APU) · airframe 65,110 hrs · 18,914 cycles

APU INOP. CAUSE WAS FOUND TO BE THE APU CONTROLLER. THIS PART HAS BEEN CHRONIC AND HAS A LONG HISTORY OF NFF.

Part: BATTERY — FAULTY (FLASHLIGHT) · airframe 65,098 hrs · 18,910 cycles

FLASHLIGHT FWD GALLEY NEEDS BATTERIES REPLACED. REPLACED BATTERY AND RESEALED.

Part: ACTUATOR — UNKNOWN (NR 8 SPOILER) · airframe 65,041 hrs · 18,889 cycles

SCM 2L INDICATES PCA 8 FAULT. INSTALLED -200 SERIES SCM AT 2L. CLEANED CONNECTORS (D655 SPL 8 M313) AND (D649 SPL 5 M310). RANG WIRES FROM SCM 2L TO NR 5 & 8 PCA. RESISTANCE WITHIN LIMITS. SLUGGED GEARS TO PUT IN AIR MODE. ACP'D SYS TEST ON SCM 2L IN AIR AND GND MODE, SYS TEST GOOD. NO EXISTING FAULTS FOUND, NO FAULT BALLS SHOWING ON REMAINING -100 SERIES SCM'S. RERACKED SCM 2L. INTERROGATED SCM 2L HISTORY AND FOUND ONLY PCA 5 FAULT WHICH WAS REPLACED.

Part: ECU — FAULTY (APU) · airframe 65,041 hrs · 18,889 cycles

APU FAULT WILL NOT START. REPLACED ECU DUE TO NO RESPONSE. OP CHECKS NORMAL.

Part: WIRE — FAULTY (HYDRAULIC SYS) · airframe 64,954 hrs · 18,868 cycles

LT HYD QTY "LOW" PRESSURE DISPLAYED ON HYDRAULIC PAGE ALONG WITH OVERHEAD "RSVR" LIGHT ILLUMINATED. FOUND LEAKING CAP AT PRESSURIZATION MODULE. REPLACED CAP, LEAK CHECK GOOD WITH APU BLEED AND ENG BLEED. REPLACED LEFT SIDE HYDRAULIC RESERVOIR. OPS OKAY. FOUND WIRE WITH HIGH RESISTANCE. REMOVED & REPLACED WIRE. WILL NEED TO PRESSURIZE RESERVOIR TO CONFIRM FIX.

Part: WIRE — FAULTY (HYDRAULIC SYS) · airframe 64,954 hrs · 18,868 cycles

LT HYD QTY "LOW" PRESSURE DISPLAYED ON HYDRAULIC PAGE ALONG WITH OVERHEAD "RSVR" LIGHT ILLUMINATED. FOUND LEAKING CAP AT PRESSURIZATION MODULE. REPLACED CAP, LEAK CHECK GOOD WITH APU BLEED AND ENG BLEED. REPLACED LEFT SIDE HYDRAULIC RESERVOIR. OPS OKAY. FOUND WIRE WITH HIGH RESISTANCE. REMOVED & REPLACED WIRE. WILL NEED TO PRESSURIZE RESERVOIR TO CONFIRM FIX.

Part: GIRT BAR — UNSECURE (R1 DOOR) · airframe 64,728 hrs · 18,809 cycles

DOOR 1R WILL NOT ARM. FOUND GIRT BAR OFF DOOR. SECURED GIRT BAR. OPS CHECK GOOD.

Part: HOUSING — CRACKED (SAM MODULE) · airframe 64,477 hrs · 18,740 cycles

ELEV ASYM AND STAB TRIM EICAS MESSAGE ON LOWER EICAS ON TAKEOFF, REPEAT GRIPE. FOUND L SAM MODULE BAD, FOUND HOUSING BODY CORRODED AND CRACKED 360 DEGREES AROUND. REPLACED SAM MODULE, REPLACED ELEVATOR ASSYMETRY ACTUATOR, PERFORMED ELEVATOR ASYM TEST 85625 -GOOD STAB TRIM MODULE M524 OPS GOOD.

Part: WIRE — BROKEN (SLIDE) · airframe 64,474 hrs · 18,737 cycles

RT OVER WING SLIDE BOTTLE FAILS PRESSURE TEST. FOUND WIRE LEADING TO CONNECTOR DO5542 BROKEN. REPAIRED WIRE. OPS CHECKS GOOD.

Part: GAUGE — LEAKING (LIFE RAFT) · airframe 64,474 hrs · 18,737 cycles

AFT CABIN LIFE RAFT COMPT, 1 LIFE RAFT FAILED PRESSURE CHECK. LEAK FOUND AT GAUGE. REMOVED AND REPLACED GAUGE.

Part: GUARD — OUT OF POSITION (DOOR 1L) · airframe 64,474 hrs · 18,737 cycles

DOOR 1L CAN BE ARMED WITHOUT MOVING ARMING GUARD. REPOSITIONED THE GUARD TO PREVENT ARMING WITHOUT MOVING GUARD.

Part: STRUCTURE — DENTED (BS 605-625) · airframe 64,474 hrs · 18,737 cycles

EXTERNAL FUSELAGE BETWEEN BS 605 AND 625 AND BETWEEN STR 16L AND 17L, PREVIOUS REPAIR DOUBLER IS DENTED. MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGED DOUBLER AND INSTALLED SKIN DOUBLER REPAIR.

Part: FRAME — DAMAGED (BS 1520) · airframe 64,474 hrs · 18,737 cycles

AFT PIT FRAME AT STA 1520 (LEFT SIDE) IS DENTED AND HAS GOUGES AT LOWER SECTION. MAJOR REPAIR ACCOMPLISHED. REMOVED PRODUCTION SPLICE AND DAMAGED SECTION OF FRAME. INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (BS 1580) · airframe 64,474 hrs · 18,737 cycles

AFT PIT STA 1580, STR 25L, FRAME DENTED INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION AND INSTALLED DOUBLER FRAME REPAIR.

Part: FRAME — DENTED (BS 1540 S25L) · airframe 64,474 hrs · 18,737 cycles

AFT PIT STA 1540 FRAME DENTED AT STR 25L AT INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED FRAME SECTION AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (BS 1410) · airframe 64,474 hrs · 18,737 cycles

FRAME DENTED AFT PIT BS 1410 AND STR 26L - 25L. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (BS 1400) · airframe 64,474 hrs · 18,737 cycles

FRAME DENTED AFT PIT BS 1400 STR 26L-25L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR.

Part: SKIN — DENTED (LEFT WING) · airframe 64,474 hrs · 18,737 cycles

LEFT WING UPPER SURFACE SKIN DENTED OUTBOARD END BETWEEN WS 780 AND WS 810. *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE AND INSTALLED CORE DOUBLER REPAIR.

Part: SKIN — DAMAGED (L2 DOOR) · airframe 64,474 hrs · 18,737 cycles

L-2 DOOR UPPER HINGE CUTOUT REQUIRES A REPAIR DOUBLER PER MM 52-11-87. HFEC INSPECTION COMPLETE PER NDT 6- 51-00-19, AND NO CRACKS NOTED. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: SKIN — DAMAGED (R2 DOOR) · airframe 64,474 hrs · 18,737 cycles

R-2 DOOR UPPER HINGE CUTOUT REQUIRES REPAIR DOUBLER PER MM 52-11-87. HFEC INSPECTION COMPLETE PER NDT 6-51 -00-19 AND NO CRACKS NOTED. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: BLADE — DAMAGED (RAM AIR TURBINE) · airframe 64,474 hrs · 18,737 cycles

RAM AIR TURBINE BLADES DAMAGED. REPLACED AND OPS CHECKED THE RAM AIR TURBINE.

Part: FAN — SEIZED (EXHAUST) · airframe 63,926 hrs · 18,587 cycles

AFT EQ EXHAUST FAN 1 STATUS MSG. *S/D* AFT EQ EXHAUST FAN FAILURE, BEARING WEAR. REPLACED AFT EQ EXHAUST FAN 1, OPS CHECKED OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,793 hrs · 18,551 cycles

DOOR 1R & 2R EXTERIOR EMERGENCY LIGHTS INOP. *S/D* LAMPS ARE INOP. REPLACED LAMPS, OPS CHECKED GOOD.

Part: LIGHT — DISCONNECTED (ROWS 9 - 13) · airframe 63,114 hrs · 18,378 cycles

EEL LIGHTS INOP ROW 9 - 13. FOUND EEL SEGMENT DISCONNECTED RECONNECTED EEL SEGMENTS, OPS CHECKED GOOD.

Part: SOFTWARE — MALFUNCTIONED (EICAS) · airframe 62,997 hrs · 18,346 cycles

L EICAS STATUS MSG WILL NOT CLEAR. -L EICAS STATUS MSG WILL NOT CLEAR -L EICAS COMP REPLACED EARLIER TODAY. REPLACED L EICAS COMPUTER REF MM 31-41-02 AND LOADED OPS SOFTWARE REF MM31-41-02. MSGS HAVE CLEARED AND ALL DISPLAYS NORMAL

Part: WARNING MESSAGE — ILLUMINATED (ENGINE) · airframe 62,964 hrs · 18,336 cycles

EICAS MESSAGE 'R ENG PRI CONT' DISPLAYED. REPLACED THE NR 2 ENGINE PERFORMED ALL REQUIRED TESTS AND RUNS, PERFORMED A SATISFACTORY VERIFICATION FLIGHT. NO REPEATS.

Part: SEAL — LEAKING (NR 2 ENGINE) · airframe 62,827 hrs · 18,299 cycles

NR 2 ENGINE HIGH OIL CONSUMPTION EXCEEDS LIMIT. FOUND STARTER DRIVE SHAFT SEAL FAILED. REPLACED STARTER DRIVE SEAL, LEAK CHECKED GOOD.

Part: OXYGEN SYSTEM — LOW (CREW) · airframe 62,560 hrs · 18,224 cycles

CREW OXYGEN BELOW ETOPS MIN AT 1480 PSI. SERVICED CREW O2 TO FULL FOR ETOPS FLIGHT. NO LEAKS WERE NOTED AT TIME OF SERVICE.

Part: OXYGEN SYSTEM — LOW (CREW) · airframe 62,570 hrs · 18,226 cycles

OXYGEN QUANTITY READS 1660 PSI. SERVICED CREW O2 TO FULL, NO LEAKS NOTED AT TIME OF SERVICE.

Part: IDG — LACK OF LUBE · airframe 61,823 hrs · 18,022 cycles

IDG DISCONNECTED DURING APPROACH. FOUND IDG SHUTDOWN DUE TO LOW OIL QTY. UNKNOWN AS TO REASON OF OIL LOW QTY. SERVICED IDG TO FULL. NO REPEATS SINCE ORIGINAL.

Part: WARNING LIGHT — ILLUMINATED (MLG) · airframe 60,794 hrs · 17,741 cycles

ON GEAR EXT GOT GEAR DISAGREE EICAS & YELLOW GEAR LIGHT.

Part: UNKNOWN — ODOR · airframe 60,794 hrs · 17,741 cycles

ELECTRICAL ODOR UPON CLIMB OUT BY FLT CREW.

Part: UNKNOWN — ODOR · airframe 60,794 hrs · 17,741 cycles

FLIGHT DIVERTED DUE TO ELECTRICAL ODOR. 10-23-07 MANUAL TEST OF EQUIP COOLING SYSTEM USING TEST SWITCH ON P61 PANEL FOUND NO FAULTS. DID NOT DETECT ANY ODOR ON FURTHER INVESTIGATION. CAUSE OF DISCREPANCY COULD NOT BE ESTABLISHED.

Part: WARNING MESSAGE — ILLUMINATED (BATTERY CHARGER) · airframe 60,719 hrs · 17,720 cycles

BATTERY CHARGER STATUS MESSAGE. 10-9-07 INSTALLED NEW MAIN EQUIPMENT LOWER BATTERY.

Part: WARNING MESSAGE — UNKNOWN (MLG) · airframe 59,972 hrs · 17,511 cycles

GEAR DISAGREE EICAS MSG AND LIGHT ILLUMINATED UPON SELECTING GEAR HANDLE DOWN.

Part: BEARING — DRY (ARMING MECHANISM) · airframe 59,922 hrs · 17,496 cycles

DOOR 4R WILL NOT ARM. ARMING MECHANISM HAS DRY BEARINGS, FOUND MOVEMENT STIFF. REMOVED DOOR LINING AND SLIDE. LUBED ARMING MECHANISM AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: GIRT BAR — FAULTY (R1 DOOR) · airframe 59,846 hrs · 17,472 cycles

DOORS 1R AND 3R DIFFICULT TO DISARM. [08-08-07] REMOVED DEBRIS FROM 1R, 3R DOOR GIRT BARS & LUBED GIRT BAR FITTINGS.

Part: GIRT BAR — FAULTY (L AFT DOOR) · airframe 59,612 hrs · 17,407 cycles

LEFT AFT DOOR WILL NOT ARM. [08-07-07] REMOVED DOOR BUSTLE AND INSPECTED DOOR ARMING MECHANISM. NO FAULTS NOTED. LUBED ALL DOOR ARMING MECHANISM. NO PROBABLE CAUSE REPORTED.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 59,556 hrs · 17,393 cycles

GEAR DISAGREE LIGHT ON FINAL. RECYCLED GEAR AND GOT NORMAL INDICATIONS. [07-10-07] BITE TEST ON PSEU SHOWS 421, 422, 423, 424. REPLACED LANDING GEAR CONTROL HANDLE MODULE. OPS AND BITE TEST OKAY.

Part: CONTROL MODULE — OUT OF RIG (MLG) · airframe 59,161 hrs · 17,277 cycles

EXECUTED A GO AROUND DUE TO VERBAL TOO LOW/TERRAIN AND LANDING GEAR WARNING MESSAGES. ACCOMPLISHED TROUBLESHOOTING. NO FAULTS FOUND. FOUND GEAR HANDLE BINDING IN DOWN POSITION WHEN PULLING HANDLE OUT OF DETENT. BINDING IS WORSE WITH HYDRAULICS ON. REPLACED LANDING GEAR CONTROL LEVER MODULE, FOUND CABLES THAT RUN FROM CNLT HANDLE TO GEAR CNTL MODULE OUT OF RIG. RIGGED CABLES.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 58,649 hrs · 17,114 cycles

AFTER PUTTING GEAR DOWN GOT GEAR DISAGREE LIGHT & CORRESPONDING EICAS MSG. 4-17-07....SUP. TAPPED OR PUSHED DOWN ON THE LND GR CNTRL HANDLE EICAS MSG WENT AWAY AND DID NOT COME BACK, NO EICAS MSG RECORDED AGAIN. NO FAULTS FOUND ON PROX ELECT UNIT. DUE TO NO FAULTS ON PSEU ACCOMPLISHED GEAR SWING. NO FAULTS OR DISCREPANCIES RECORDED DURING SWING. BITE TEST PSEU OKAY, BUT LAST FLT FAULT BITE SHOWED FAULT CODE 421-424. FOUND CONTROL LEVEL IS BINDING AGAINS P3-1 PANEL LIGHT PLATE, AND NOT FULLY DOWN DETENT (CHRONICALLY). REPOSITION LIGHT PLATE. OPS CHECKED NORMAL.

Part: WARNING SYSTEM — MALFUNCTIONED (CABIN) · airframe 58,565 hrs · 17,092 cycles

EVAC ALARM HAS ACTIVATED AT ALL STATIONS ALL BY ITSELF. PRESSED HORN SHUTOFF, NO HELP. [SUP 06-14-07] TESTED EVAC SYSTEM PER UA ENGINEERING SPECIFICATIONS. SYSTEM TESTED GOOD. NO DEFECTS NOTED. UNABLE TO ESTABLISH ANY CAUSE FOR THIS IRREGULARITY EVENT.

Part: SKIN — DENTED (FUSELAGE) · airframe 58,477 hrs · 17,062 cycles

DENT IN FUSELAGE LEFT SIDE JUST FWD OF LAV SERVICE PANEL. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED & FABRICATED & INSTALLED REPAIR DOUBLER.

Part: BOTTLE — READS LOW (SLIDE/RAFT) · airframe 58,477 hrs · 17,062 cycles

TWO EACH CABIN LIFE RAFTS, CYLINDER PRESSURE GAUGE NEEDLES ARE IN RED BAND (LOW PRESSURE). [SUP 05-18-07] LOW BOTTLE PRESSURE ATTRIBUTED TO A LEAKING GAUGE O-RING, WHICH APPARENTLY FAILED TO SEAL. FILL VALVE WAS FOUND LOOSE. TIGHTENED VALVE AND RETESTED.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 58,477 hrs · 17,062 cycles

NR 2 PYLON INBOARD SIDE SKIN CRACKED AT FWD HOLE. MAJOR REPAIR ACCOMPLISHED: REPAIRED SIDE SKIN WITH 3 EACH REPAIR DOUBLERS.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 58,477 hrs · 17,062 cycles

NR 2 PYLON OUTBOARD SKIN IS CRACKED AT FWD HOLE. [SUP 4-24-07] MAJOR REPAIR ACCOMPLISHED. HFEC INSP AT END OF CRACK. INSTALLLED 301 HALF 0.050" DOUBLERS AS A UA APPROVED REPAIR.

Part: UNKNOWN — UNKNOWN (LT ENGINE) · airframe 55,427 hrs · 16,204 cycles

RETURN TO FIELD DUE TO LT ENGINE EPR FLUX. LT ENGINE EPR FLUCTUATED FROM 1.3 TO 1.55. FELT YAW. LINE ACCOMPLISHED VISUAL CHECK OF ENGINE INLET AND EXHAUST AND FOUND NO DAMAGE, ENGINE RUN ACCOMPLISHED AT 1.41 EPR, CYCLED PNEU. BLEED, ENGINE RUN PARAMETERS ALL NORMAL, NO FLUCTUATIONS NOTED, RETURNED THE ENGINE BACK TO SERVICE. ON JULY 15 CREW REPORTED NR 1 ENG SURGED TWICE JUST MOMENTARILY IN CLIMB APROX 300 FT. REPLACED EEC, FMU AND SVA WITHOUT ESTABLISHING ANY PART DIRECTLY RESPONSIBLE FOR THIS INCIDENT.

Part: GENERATOR — TRIPPED · airframe 53,581 hrs · 15,691 cycles

RETURN TO FIELD AFTER LEFT GENERATOR TRIPPED OFF. MAINTENANCE LOG INDICATED THAT THE LEFT INTEGRATED DRIVE GENERATOR (IDG) WAS REMOVED AND REPLACED. FURTHER TROUBLESHOOTING FOUND THAT IDG CONNECTOR D05132, PIN (2) WIRE W5608-3501B-18 WAS SHORTED TO THE SHIELD. REPAIRED WIRE PER BSWPM, OPERATIONAL CHECK PER AMM 24-11-00.

Part: ODOR — DETECTED (COCKPIT) · airframe 52,095 hrs · 15,240 cycles

ACRID OIL SMELL IN COCKPIT THROUGHOUT FLIGHT. ACCOMPLISHED ENGINE BURNOUT PROCEDURE PER MM21-00-01 PG210. SMELL DIMINISHED AFTER ENGINE RUN. RETURNED AIRCRAFT TO SERVICE.

Part: SKIN — DELAMINATED (TE FLAPS)

TRAILING EDGE FLAPS SKIN HAS DAMAGE AND IS DELAMINATED. REPLACED THE TRAILING EDGE WEDGE.

Part: FAN — BROKEN (AIR DISTRIBUTION) · airframe 44,997 hrs · 13,278 cycles

ELECTRICAL BURNING ODOR IN FORWARD CABIN AND FLIGHT DECK. THE EQUIPMENT COOLING FAN HAD A WORN SHAFT AND EXHIBITED SHAFT END PLAY, ALLOWING THE BLADES TO CONTACT THE HOUSING. THIS WAS THE ORIGINAL FAN INSTALLED. FAN REPLACED

Part: PUMP — FAILED (LT ENG HYD) · airframe 43,356 hrs · 12,820 cycles

LOST LEFT HYD SYSTEM PRESSURE AND FLUID. LT ENGINE DRIVEN PUMP FAILED RESULTING IN A LOSS OF HYDRAULIC FLUID AND SYSTEM PRESSURE. LEFT ENGINE DRIVEN PUMP WAS REPLACED AND THE HYDRAULIC SYSTEM WAS SERVICED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,453 hrs · 12,067 cycles

CABIN FLOOR SUPPORT CORRODED AT STATION 327 RBL 40-55. MAJOR REPAIR ACCOMPLISHED. REPAIRED WITH STRAP DOUBLER.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,453 hrs · 12,067 cycles

AFT PIT LEFT HAND SIDE STATION 1480 STRINGER 26 FRAME DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED EXTERNAL REPAIR DOUBLER.

Part: CREASE BEAM — CORRODED · airframe 40,453 hrs · 12,067 cycles

CABIN FLOOR STATION 773, RBL 62, INBOARD CREASE BEAM HAS CORROSION AT FLOOR BOARD FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. CORROSION CUT OUT AND DOUBLER INSTALLED.

Part: CREASE BEAM — CORRODED · airframe 40,453 hrs · 12,067 cycles

CABIN CREASE BEAM IB CHORD BODY STATION 734 TO BODY STATION 740 LBL 65 UPPER SURFACE HAS EXCESS MAT LOSS. MAJOR REPAIR ACCOMPLISHED.CREASE BEAM INNER CHORD REPLACED. PARTS SEALED AND FASTENERS INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,453 hrs · 12,067 cycles

FLOORBEAM FLANGE CORRODED STA 1640 RBL 53, WL 208. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 40,453 hrs · 12,067 cycles

FUSELAGE LEFT CREASE BEAM WEB UPPER SURFACE HAS CORROSION AROUND LIGHTNING HOLES STATION 964 AND 969. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED DAMAGED WEB.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,453 hrs · 12,067 cycles

AFT PIT STATION 1280 BL 0 FRAME CAP CORROSION. MAJOR REPAIR ACCOMPLISHED. FRAME CAP STRAP REPAIRED INSTALLED.

Part: FUEL LINE — CHAFED (RT MAIN TANK) · airframe 38,003 hrs · 11,393 cycles

UNWANTED FUEL TRANSFER FROM RIGHT FUEL TANK TO CENTER TANK. FOUND CHAFED WATER SCAVENGE FUEL LINE. DAMAGE CAUSED FROM COUPLING CONTACT ON ADJACENT FUEL LINE DUE TO INCORRECT CLAMPING. REPLACED WATER SCAVENGE FUEL LINE.

Part: HOSE — RUPTURED · airframe 36,209 hrs · 10,900 cycles

DURING CLIMBOUT PASSING 18000, L HYD QTY EICAS CAME ON. LEFT HYDRAULIC PUMPS WERE SHUTOFF. SUPPLEMENTAL DATA UPDATE LEFT GEAR DOWN LOCK ACTUATOR HOSE RUPTURED. REPLACED DOWN LOCK HOSE.

Part: SKIN — DENTED (FUSELAGE) · airframe 35,568 hrs

FUSELAGE SKIN DENTED STA 600 - 620 WL 207. MAJOR REPAIR ACCOMPLISHED. INSTALLED SKIN DOUBLER AND SPLICED CREASE BEAM.

Part: PUMP — FAILED (FUEL BOOST) · airframe 32,627 hrs · 9,963 cycles

RIGHT AFT BOOST PUMP LOW PRESS LIGHT ON, EICAS MESSAGE RIGHT AFT FUEL PUMP DISPLAYED. *S/D* REPLACED RIGHT AFT BOOST.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,938 hrs · 9,776 cycles

AFT MAIN ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. *S/D* RELAMPED ACCORDINGLY. OPERATIONAL CHECK SATISFACTORY.

Part: OVEN — DIRTY (GALLEY)

FOOD WRAPPER IN FORWARD OVEN CAUGHT FIRE. HALON EXTINGUISHER USED TO PUT FIRE OUT. *S/D* FOOD WRAPPER WAS NOT PROPERLY INSTALLED. REMOVED WRAPPER, CLEANED OVEN, OPS NORMAL.

Part: VALVE — DEFECTIVE (BOTTLE)

DURING ROUTINE SHOP MAINTENANCE, EVACUATION SLIDE FAILED TO INFLATE. UPON PARTIAL DISASSEMBLY OF THE BOTTLE VALVE BODY THE COUPLING PIN (P/N 10003-0005-293) WAS FOUND TO BE BADLY BENT AND SHAFT (P/N B18116-1) WAS SPREAD. THE BOTTLE VALVE WAS REPLACED.