N552UA

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 82,450 hrs · 23,734 cycles

IN UNDER 2 HR FUEL IN LT TANK UP BY 1500 LBS. IAW FUEL IMBALANCE, FUEL EVEN USING CTR PUMPS. 1:50 AFTER TANK TO ENG LT TANK 1500 LBS ABOVE RT. LT ENG BURN 100 PPH MORE THAN RT ENG IAW SEQ 4502010, 4502009, 4502007 & 4502002. COMPLETED FUEL TRANSFERS WAS UNABLE TO DUPLICATE ANY TRANSFER OF FUEL IAW ABOVE SEQ NR.

Part: GENERATOR — LEAKING (APU) · airframe 82,445 hrs · 23,733 cycles

APU NO START AFTER LANDING FAULT INDICATION. FOUND LOW OIL QTY, ECU SHOWED LOW OIL PRESS. CLEARED ECU, SERVICED & RAN APU, FOUND GEN CASE LEAKING OIL, NEEDS GENERATOR. REPLACED APU GEN IAW MM 24-21-01, OPERATIONS & LEAK CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (PARKING BRAKE) · airframe 82,297 hrs · 23,702 cycles

WHEN SETTING PARKING BRAKE, NO PARK BRAKE LIGHT & NO EICAS PARKING BRAKE.

Part: VSI — INOPERATIVE (COCKPIT) · airframe 82,260 hrs · 23,694 cycles

LIGHT ON FIRST OFFICER`S VSI OUT. REPLACED FIRST OFFICER`S VSI INDICATOR IAW MM, CHECKED GOOD.

Part: HYDRAULIC LINE — LEAKING (RT MLG) · airframe 81,909 hrs · 23,611 cycles

HYD LEAK RT MLG STRUT AREA. REPLACED HYD LINE IAW IPC 32-41-51-025, ITEM 265 (170-5876) & BLEED RT MLG TRUCK POSITIONER ACTUATOR IAW AMM, NO LEAKS. SERVICED HYD RESERVOIRS TO FULL.

Part: DUCT — CONTAMINATED (COCKPIT) · airframe 81,865 hrs · 23,599 cycles

LOOSE OBJECT IN DUCTING FWD OF FIRST OFFICER'S INSTRUMENT PANEL. NOISE IN CKPT AIR DUCT. REMOVED CLAMPS ON CKPT AC DUCT BELOW FLOOR IN FWD EE BAY & FOUND WASHER & BROKEN TIE WRAP. REMOVED ITEMS & ASSEMBLED DUCTING, NOISE WENT AWAY.

Part: BATTERY — DISCHARGED (MAIN) · airframe 81,821 hrs · 23,586 cycles

MAIN SHIP'S BATTERY IS DEAD. REPLACED BATTERY IAW AMM.

Part: SEAL — LEAKING (NR 1 ENGINE) · airframe 81,788 hrs · 23,575 cycles

NR 1 ENG OIL CONSUMPTION HAS REACHED AMBER LEVEL. FOUND STARTER DRIVE PAD SEAL LEAKING. REPLACED PAD SEAL IAW 72-61-02, NO LEAKS NOTED. REPLACED NR 1 ENG STARTER PRECAUTIONARY.

Part: EEC — FAILED (LT ENGINE) · airframe 81,772 hrs · 23,567 cycles

LEFT ENGINE EEC MALFUNCTIONED. REPLACED EEC IAW MM 73-21-04 AND ACCOMPLISHED NR 1 ENGINE RUN. NO STATUS MESSAGE ON SHUTDOWN.

Part: COVER — DAMAGED (EMERGENCY LIGHTS) · airframe 81,749 hrs · 23,558 cycles

EMERGENCY FLOOR LIGHT COVER IS DAMAGED FROM ROWS 37ABC- 40ABC. REPLACED LIGHT COVER.

Part: COVER — DAMAGED (EMERGENCY LIGHTS) · airframe 81,749 hrs · 23,558 cycles

EMERGENCY FLOOR LIGHT COVER IS DAMAGED FROM ROWS 8ABC - 14ABC. REPLACED LIGHT COVER.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 81,749 hrs · 23,558 cycles

EMERGENCY FLOOR LIGHT COVER IS DAMAGED AT ROW 29ABC. REPLACED & SECURED COVER, OPERATION CHECKED GOOD.

Part: WIRE — CHAFED (NR 1 ENGINE) · airframe 81,749 hrs · 23,558 cycles

WHILE ACCOMPLISHING LM7397, FOUND 1 BROKEN & 1 CHAFFED WIRE ON HARNESS TO PMA STATOR. ON NR 1 ENG REPLACED WIRE FROM CONNECTOR D4856 OF NR 1 EEC TO CONNECTOR D4858 OF THE PMA IAW WDM.

Part: EEC — FAULTY (LT ENGINE) · airframe 81,749 hrs · 23,558 cycles

LT ENG EEC REPLACEMENT DUE TO REPEAT LT ENG REV CONTROL STATUS MESSAGE WITH EPCS PAGE MESSAGE 274-18. REPLACED EEC MR73237 DASH NR 96 IAW AMM 73-21-04 401. REPLACED NR 1 EEC IAW MM 73 -21-04. CYCLED REVERSER SEVERAL TIMES NO FAULTS OR MESSAGE.

Part: ACTUATOR — LEAKING (NLG STEERING) · airframe 80,699 hrs · 23,292 cycles

LEFT NOSE STEERING CYLINDER ACTUATOR HAS FLUID LEAKING FROM ROD END, ONE DROP PER MINUTE.

Part: LANYARD — UNSECURE (L2 DOOR SLIDE) · airframe 80,649 hrs · 23,282 cycles

LANYARD HANGING FROM SLIDE PACK AT DOOR 2L. STOWED LANYARD AT SLIDE PACK AT DOOR 2L.

Part: SIGNAL COND UNIT — FAULTY (ENG VIBRATION) · airframe 80,649 hrs · 23,282 cycles

RIGHT ENGINE VIBRATION INDICATION READS HIGH, LOW, ZERO, BLANK, FLUCTUATES OR INOPERATIVE. NO ABNORMAL VIBRATION PERCEIVED. OTHER ENGINE PARAMETERS NORMAL. REPLACED AIRBORNE VIBRATION MONITOR SIGNAL CONDITIONER IAW AMM.

Part: MODULE — FAULTY (SWITCH) · airframe 80,636 hrs · 23,278 cycles

FUEL CONTROL PANEL ASSY SWITCH S5 FAILED. CMM 28-41-71, PG 1005, FUNCTIONAL TEST STAT 48 AND 51. RESISTANCE TOO HIGH. REF COA 507225, STEP 1A2-4. R & R S5 SWITCH MASTER MODULE. ACCOMPLISHED FUNCTIONAL TEST IAW CMM, CHECKS GOOD.

Part: PANEL — WEAK (1ST OFFICER'S) · airframe 80,598 hrs · 23,269 cycles

F/O RADIO VOLUME WEAK ALL CHANNELS. R & R F/O AUDIO CONTROL PANEL IAW AMM, OPS CHECK NORMAL.

Part: STRAP — LOOSE (L2 DOOR) · airframe 80,550 hrs · 23,258 cycles

DOOR 2L SLIDE RESTRAINING STRAP CAME LOOSE. COULD NOT ARM DOOR. RE-ROUTED SLIDE STATIC LINE.

Part: STRAP — OUT OF POSITION (L2 DOOR) · airframe 80,548 hrs · 23,257 cycles

DOOR 2L DOES NOT CLOSE PROPERLY. FOUND "D" RING STRAP HANGING DOWN. REPOSITIONED STRAP IAW AMM 25-60-00. DOOR CLOSES PROPERLY.

Part: UNKNOWN — LEAKING (NR 2 ENGINE) · airframe 80,540 hrs · 23,253 cycles

NR 2 ENG HAS EXCESSIVE OIL DRIPPING FROM FAN COWL. PERFORMED AMM 71-71-00 INSP FOR LEAKS FOUND ACCUMULATION JUST AFT OF TOWER SHAFT. SUSPECT BREATHER AIR BUILD-UP, NO LEAKS FOUND.

Part: BOLT — WORN (TE FLAP) · airframe 80,537 hrs · 23,251 cycles

LT INBD AFT FLAP, INSTALLATION BOLTS FOR AFT FLAP PUSH RODS AND SUPPORT TRACKS ARE WORN REPLACE AS REQUIRED. REPLACED HARDWARE AND TRACK. VERIFIED NEW HARDWARE AND SUPPORT TRACKS INSTALLED IAW AMM AND IPC 27-51-02-010C.

Part: PUSHROD — WORN (TE FLAP) · airframe 80,537 hrs · 23,251 cycles

LT INBD AFT FLAP, CENTER UPPER AND LOWER PUSH ROD ENDS WORN. REPLACED ROD AND HARDWARE. VERIFIED NEW ROD AND HARDWARE ARE IN PLACE IAW IPC 27-51-02-010C.

Part: FLAP TRACK — WORN (TE FLAPS) · airframe 80,537 hrs · 23,251 cycles

FOUR LEFT OTBD AFT FLAP SUPPORT TRACKS WORN FROM ROLLERS AND BEARINGS LOOSE AND ATTACHING HARDWARE WORN. REPLACED SUPPORT TRACKS AND ATTACHING HARDWARE.

Part: BOLT — SCORED (LT AILERON) · airframe 80,537 hrs · 23,251 cycles

LEFT AILERON ATTACH BOLTS SCORED. REPLACED DAMAGED BOLTS IAW MM.

Part: INDICATOR — DAMAGED (RT FUEL SYS) · airframe 80,370 hrs · 23,207 cycles

LEFT MAIN FUEL INDICATOR HAS MISSING SEGMENTS ON THE REFUELING PANEL. REPLACED INDICATOR, TEST OK.

Part: PRESSURE SWITCH — FAILED (LT HYD SYSTEM) · airframe 80,384 hrs · 23,211 cycles

LEFT ENGINE HYDRAULIC PRESSURE LIGHT DOES NOT ILLUMINATE WITH ENGINE OFF. REPLACED EDP HYDRAULIC PUMP PRESSURE SWITCH IAW AMM 29-11-17. MOTORED ENGINE AND PUMP AND INDICATOR LIGHT WORKS NORMAL.

Part: COMPUTER — FAILED (NR 2) · airframe 80,227 hrs · 23,158 cycles

BURNING ODOR IN COCKPIT & FIRST OFFICER`S EADI IS BLANK. FOUND EHSI BURNED AND REPLACED RIGHT EHSI AND SYMBOL GENERATOR AGAIN. RESTORED OPERATIONS.

Part: FRAME — DENTED (BS 640 S23L) · airframe 64,163 hrs · 18,463 cycles

FWD CARGO BAY FRAME DENTED BS 640 S23L. CUTOUT DAMAGED SECTION OF FLANGE AND FABRICATED A REPAIR ANGLE AND INSTALLED PER SRM 53-00 -07, REPAIR 5. MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 620 S24L) · airframe 64,163 hrs · 18,463 cycles

FORWARD CARGO BAY FRAME DENTED BS 620 S24L. CUT OUT DAMAGED SECTION OF FLANGE AND FABRICATED A REPAIR ANGLE AND INSTALLED PER SRM 53-00 -07, REPAIR 5 TABLE II, ZONE 1. MAJOR REPAIR.

Part: FRAME — DENTED (BS 1480, S26L) · airframe 64,163 hrs · 18,463 cycles

AFT CARGO BAY FRAME BS 1480, S26L DENTED. CUT OUT DAMAGED SECTION OF FLANGE & FABRICATED A 'J-ANGLE' REPAIR AND INSTALLED PER SRM 53- 00-07, REPAIR 5 ON NON ROUTINE 44405. PER SRM 53-00-07, REPAIR 5, TABLE II, ZONE 1. MAJOR REPAIR.

Part: FRAME — DENTED (BS 1420 S26L) · airframe 64,163 hrs · 18,463 cycles

FRAME DENTED BS 1420, S26L. CUT OUT DAMAGED SECTION OF FLANGE AND FABRICATED A J-ANGLE REPAIR PER SRM 53-00-07, REPAIR 5. PER SRM 53-00-07, REPAIR 5 , TABLE II, ZONE 3. MAJOR REPAIR.

Part: ACTUATOR — FAILED (LT WING SLAT) · airframe 80,123 hrs · 23,130 cycles

LEFT WING LEADING EDGE SLAT ROTARY ACTUATORS NR 2 AND NR 8 HAVE OVERLOAD SPRINGS BAD. REMOVED AND REPLACED NR 2 ROTARY ACTUATOR IAW MM 27-81-18.

Part: FSEU — NO TEST (NR 3) · airframe 80,123 hrs · 23,130 cycles

NR 3 FLAP/SLAT ELECTRICAL UNIT BITE TEST FAILED. REPLACED NR 3 FSEU.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 79,937 hrs · 23,088 cycles

AUTOPILOT DISC LIGHT ON & EICAS MESSAGE 'AUTOPILOT DISC' DISPLAYED WITH 2 AUTOPILOT SYSTEM ENGAGED IN COMMAND. AT CRUISE 380 M.80 CTR A-P DISCONNECTED. TRIMMED AND TRIED AGAIN, NO GO, LEFT AND RIGHT AUTOPILOT SYS OK. FOUND FAULT FCC-C. REPLACED CENTER FCC PER MM AND ACCOMPLISHED CATIII CHECK PER MM, OPS NORMAL.

Part: PRESSURE SWITCH — FAULTY (HYD SYSTEM) · airframe 79,899 hrs · 23,078 cycles

LEFT ELECTRIC HYDRAULIC PUMP PRESSURE LIGHT DOES NOT ILLUMINATE WITH SWITCH OFF. PUMP OPERATES NORMALLY. PUMP OPERATES NORMALLY, ASSOCIATED LOW SYSTEM PRESSURE LIGHT OPERATES NORMALLY, REPLACED PRESSURE SWITCH. OPS CHECKED NORMAL, NO LEAKS.

Part: WARNING MESSAGE — FALSE ACTIVATION (FLAP/SLAT SYS) · airframe 79,847 hrs · 23,061 cycles

FLAP/SLAT STATUS MESSAGE DISPLAYED AND WILL NOT ERASE. RESET FLAP UNIT BITE, SYSTEM OPERATES NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,839 hrs · 23,058 cycles

FOUND LT WING OFF WING SLIDE EMERGENCY LIGHT INOP. RELAMPED PER MM, OPS CHECKED NORMAL

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 79,839 hrs · 23,058 cycles

FOUND EMERGENCY LIGHT LENS CRACK AFT OF LEFT WING. REPLACED LENS. OPS CHECKED OKAY.

Part: FCU — FAULTY (APU) · airframe 79,818 hrs · 23,050 cycles

REPLACED APU FLOW SENSING MODULE REF DF676 APU AUTO SHUTDOWN. REPLACED FLOW SENSING MODULE, NO HELP ACC. APU DEEP BITE TEST FAULTS SHOW DELTA P, FUEL CONTROL UNIT, DE-OILER SOLENOID, HOT SENSOR AND P2 SENSOR

Part: APU — FAILED (APU BAY) · airframe 79,817 hrs · 23,049 cycles

APU INOPERATIVE. REPLACED SURGE VALVE, BATTERY AND STARTER. APU STILL HANGS AT 30 TO 40 PERCENT. SWAPPED ECU AND BATTERY CHARGER, NO HELP. INSTALLED OLD CHARGER AND ECU. REPLACED APU.

Part: SLAT SYSTEM — MALFUNCTIONED (POSIT 2) · airframe 79,817 hrs · 23,049 cycles

WHEN FLAPS SELECTED TO POS 1, RECEIVED A LEADING EDGE SLAT DISAGREE EICAS AND FLAP INDICATION SHOW FLAP BETWEEN UP AND POS 1. TRIED TO MOVE FLAPS WITHIN ALTERNATE WITH BOTH LEADING AND TRAILING EDGE FLAPS SELECTED, NO MOVEMENT OCCURED. RECEIVED A LEADING EDGE FLAP DISAGREE EICAS AGAIN. NO EICAS MESSAGE DISPLAYED. PER FIM 27-81-00 FIG 104 BLOCK 1 FSEU BITE ON NR 2 FSEU FAULT BALL LATCHED SLAT PDU TRANSMITTER NOT IN POSITION. OPERATED FLAPS AND SLATS BOTH ON HYDRAULICS AND ELECTRICALLY IN ALTERNATE. SLATS BOTH ON HYDRAULICS AND ELECTRICALLY IN ALTERNATE, NO FAULTS NO EICAS MESSAGE. INSPECTED SLATS. NO FAULTS FOUND. REPLACED NR 2 FSEU PRECAUTIONARY PER AMM.

Part: EXCITER — FAILED (APU) · airframe 79,817 hrs · 23,049 cycles

APU NO START. REPLACED EXCITER, LEAD AND IGNITER PLUG. OPS NORMAL.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 79,678 hrs · 23,009 cycles

ON APU SHUTDOWN, BLACK SMOKE BELLOWED OUT OF TAIL PIPE. INSPECTED APU TAIL PIPE. NO DISCREPANCIES NOTED. FOUND APU OIL OVERSERVICED. NO FAULTS PRESENT ON ECS. RAN APU PER JRH 2-5-15, AND FOUND APU OPERATION NORMAL.

Part: ENGINE — SHUTDOWN (LEFT) · airframe 79,566 hrs · 22,973 cycles

AIRCRAFT RETURN TO GATE, PER CREW, AFTER NORMAL LEFT ENGINE STARTED AND STARTED RIGHT ENGINE. CREW NOTICE LEFT GENERATOR TRIPPED AND SAW THAT LEFT ENGINE AUTO-SHUT DOWN BY ITSELF. CHECKED EPCS PAGE, NO FAULTS DISPLAYED. NO FAULTS FOUND ON EICAS. NO ENGINE EXCEEDANCE FAULTS. CREW NO UNUSUAL ENGINE PARAMETERS. DRY MOTORED ENGINE PER JRH 2-5-9 ALL INDICATIONS NORMAL. RAN ENGINE PER JRH 2-5-1. RAN FOR APPROX 5 MINS WITH BLD AND PACKS ON, GENERATOR PWR'G ACFT. ALL NORMAL NO FAULTS.

Part: COMPRESSOR — LEAKING (POTABLE WATER) · airframe 79,527 hrs · 22,960 cycles

WATER LEAK IN AFT BELLY AREA. WATER LEAKING FROM BELLY DRAIN LOCATED BELOW AFT CARGO DOOR. DRAINED WATER TANK, WATER STILL DRAINING FROM BELLY BUT AT SLOWER RATE. SERVICED WATER TO THREE QUARTER FILL. DURING THE SERVICE PROCESS THE VOLUME OF WATER COMING FROM THE BELLY DRAIN INCREASED. THE WATER TANK HAS BEEN DRAINED. AFTER REMOVAL OF PIT FLOOR PANEL FOUND WATER IN CENTER LINE STRUCT. FOUND OVERFILL HOSE MISSING, THERE WAS A CAP ON TANK AND CAP ON VALVE NO HOSE. REPLACED H2O COMPRESSOR.

Part: GATE — UNSECURE · airframe 79,402 hrs · 22,922 cycles

TOP LATCH ON SECURITY GATE DOES NOT STAY LATCHED. SECURED WITH TY WRAPS IN STOWED POSITION. REPLACED SECONDARY BARRIER GATE.

Part: FCU — FAILED (APU) · airframe 79,374 hrs · 22,913 cycles

UNABLE TO START APU AT GATE. REPLACED APU FUEL CONTROL UNIT PER AMM. OPS CHECKED APU START PER JRH, OPS OK.

Part: FCU — MALFUNCTIONED (APU) · airframe 79,383 hrs · 22,915 cycles

APU WILL NOT START AND MM REPORTING THEY REPLACED FUEL CONTROL UNIT. APU ALTITUDE START REQUIRED DUE TO FUEL CONTROL REPLACEMENT. REF PTT NR 3832002 APU COLD SOAK REQUIREMENT WAS SUCCESSFUL.

Part: FCU — FAILED (APU) · airframe 79,374 hrs · 22,913 cycles

APU AUTO SHUTDOWN. REPLACED THE APU FUEL CONTROL UNIT. SYSTEM OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,367 hrs · 22,912 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT L1 DOOR ON OUTSIDE OF AIRPLANE. REPLACED LAMP.

Part: CONTROL VALVE — FAILED (ENGINE STARTER) · airframe 79,277 hrs · 22,882 cycles

RIGHT ENGINE STARTER FAILURE. NR 2 ENGINE STARTER CONTROL VALVE, GROUND CHECKED NORMAL.

Part: AUDIO PANEL — FAULTY (CABIN) · airframe 79,062 hrs · 22,825 cycles

PA VERY SCRATCHY WHEN TRANSMITTING FROM F/O AUDIO PANEL. REPLACED AUDIO SELECTOR PANEL, OPS CHECK OK.

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS) · airframe 78,942 hrs · 22,794 cycles

LEFT ENGINE BLD OFF LIGHT ON WHEN LEFT ENG HEAT SWITCHED TO ON POSITION. REPLACED PRSOV PER MM AND AIR SUPPLY OVERTEMP SWITCH.

Part: LANYARD — UNSECURE (L2 DOOR) · airframe 78,819 hrs · 22,756 cycles

DOOR 2L GIRT BAR LANYARD HANGING. SECURED LANYARD.

Part: LENS — DETACHED (EXIT SIGN) · airframe 78,664 hrs · 22,712 cycles

FLT ATTENDANTS REPORT AN EXIT SIGN HAS DETACHED AT OVERWING. RE-ATTACHED EXIT LENS TO FWD OVERWING EXIT LENS, ACFT LEFT.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 78,475 hrs · 22,664 cycles

DOOR 2R SLIDE EXIT LIGHT INOPERATIVE. UPON ARRIVAL AT LAX 1 F/A STATED THAT DOOR 2R SLIDE LIGHT WAS OK, INCORRECT DOOR LOCATION. DOOR 1R SLIDE EXIT LIGHT INOP. CLEANED GIRT BAR AREA FOR DOOR 1R. RELAMPED DOOR 1R SLIDE ARMED INDICATOR LIGHT. CHECK OKAY.

Part: LIGHT — INOPERATIVE (L1 DOORS) · airframe 78,442 hrs · 22,657 cycles

ARM LIGHTS DOORS 1L AND 1R INOPERATIVE. RELAMPED 1L AND 1R ARM LIGHTS, CYCLED DOORS LIGHTS CHECK NORMALLY.

Part: SMOKE GOGGLES — DAMAGED (COCKPIT) · airframe 78,430 hrs · 22,654 cycles

OBSERVER SMOKE MASK ELASTIC ALL STRETCHED OUT. REPLACED GOGGLES WITH A NEW UNIT.

Part: AILERON — DAMAGED (LT WING) · airframe 78,414 hrs · 22,648 cycles

HEAVY LIGHTNING DAMAGE TO LEFT WING OUTBOARD AILERON. REMOVED LEFT WING OUTBOARD AILERON. INSTALLED LEFT AILERON TO STEP 3G10 OF MM 27-11-21 PAGE 406.

Part: AILERON — DAMAGED (LT WING) · airframe 78,414 hrs · 22,648 cycles

HEAVY LIGHTNING DAMAGE TO LEFT WING OUTBOARD AILERON. REMOVED AILERON AND SENT TO SHOP. INSTALLED LEFT AILERON TO STEP 3G10 OF MM 27-11-21 PAGE 406. COMPLETED INSTALLATION OF LEFT O/B AILERON.

Part: LIGHT — INOPERATIVE (R2 DOOR) · airframe 78,398 hrs · 22,645 cycles

DOOR 2R WILL NOT ARM. RELAMPED DOOR ARMED LIGHT. OPS CHECKS GOOD.

Part: HYDRAULIC LINE — DAMAGED (RT AILERON) · airframe 78,347 hrs · 22,632 cycles

RIGHT WING INBOARD AIL PCU RETURN LINE DAMAGED. LINE REMOVED AND SENT TO SHOP FOR REMAKE, FITTINGS CAPPED. REPLACED RT WING INBD AIL PCU RETURN LINE. LEAK CHECK GOOD. SYS OP CKS GOOD.

Part: SELECTOR PANEL — FAULTY (COCKPIT) · airframe 78,228 hrs · 22,594 cycles

F/O AUDIO SEL PANEL WILL NOT SELECT NR 1 COMM MOVED PANEL TO OBS POS AND PLACARD OBS SEAT INOP. REPLACED OBSERVER'S AUDIO SELECTOR PANEL.

Part: SEAL — NOT SEATED (FUEL TANK) · airframe 78,228 hrs · 22,594 cycles

RUNNING FUEL LEAK AT RIGHT WING TANK OUTBOARD LOWER PRESSURE RELIEF PLATE. LEAK IS JUST OUTBOARD OF SURGE TANK SUMP DRAIN. SUSPECT PLATE NEEDS PACKING REPLACED. REMOVED PRESSURE RELIEF SURGE TANK ACCESS DOOR 643AB - RESEATED SEAL, NO LEAK NOTED.

Part: SKIN — DENTED (BS 760 S16L) · airframe 78,224 hrs · 22,593 cycles

SKIN DENTED BS 760 ABOVE S16L. INSTALLED REPAIR IAW ECRA 5531-01630.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,224 hrs · 22,593 cycles

NEED TO INITIATE A CF PER ECRA 5330-04323 FOR FUSELAGE SKIN INTERIM REPAIR BETWEEN BS 564-585 BETWEEN S26R TO S28L.

Part: FITTING — DAMAGED (TE FLAP) · airframe 78,224 hrs · 22,593 cycles

NEED TO INITIATE A CF FOR ECRA 5750-04484 LEFT WING I/B MAIN FLAP I/B ATTACH FITTING.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,224 hrs · 22,593 cycles

NEED TO INITIATE A CF FOR ECRA 5330-04322 FUSELAGE SKIN INTERIM REPAIR BW BS 538 550 AND STRINGERS 27L BL 0.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,224 hrs · 22,593 cycles

NEED TO INITIATE A CF FOR ECRA 5331-01632 FUSELAGE SKIN INTERIM REPAIR BS 600-620 BETWEEN S27L 27R REF SCAL 9979840.

Part: SKIN — DENTED (FUSELAGE) · airframe 78,224 hrs · 22,593 cycles

FUSELAGE SKIN HAS DENT STA 605 AT S-29R. REPAIR DOUBLER INSTALLATION COMPLIED WITH PER ECRA 5331-01632.

Part: SKIN — DENTED (FUSELAGE) · airframe 78,224 hrs · 22,593 cycles

REF CF9025 FUSELAGE SKIN IS DENTED AT STA 1580 TO 1600 ABOVE S-20R. MAJOR REPAIR ACCOMPLISHED: REPAIR DOUBLER INSTALLATION AT STATION 1580-1600 AND S-19R TO S-21R WAS COMPLIED WITH PER ECRA 5330-04324 .

Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,224 hrs · 22,593 cycles

FUSELAGE SKIN HAS 2 EACH LIGHTNING STRIKES AT STA 543 OUTBOARD OF S-28L. REPAIR WAS COMPLIED WITH PER ECRA 5330-04322.

Part: SKIN — DENTED (FUSELAGE) · airframe 78,224 hrs · 22,593 cycles

FUSELAGE SKIN HAS A DENT STA 580 BETWEEN S -27R AND S-28R. REPAIR INSTALLATION AT FUSELAGE STA 564-585 BETWEEN S-26R TO S-26L WAS COMPLIED WITH PER ECRA 5330-04323.

Part: SKIN — DENTED (FUSELAGE) · airframe 78,224 hrs · 22,593 cycles

DENT REPORTED BY FLT CREW 12FT 4 INCHES AFT OF AFT CARGO PIT DOOR. DENTED FROM INSIDE. CHECKED FOR HIDDEN DAMAGE MEASURED DENT ON INSIDE AT 4 INCHES BY 1-32 DEEP WITHIN SRM 536-00-01 LIMITS DF9. INSTALLED REPAIR DOUBLER AT STA 1580-1600 AND S-19R TO S-21R PER ECRA 5330-04324.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,224 hrs · 22,593 cycles

CORROSION ON TOP OF FLOORBEAM STA 1640 FROM LBL 3 TO RBL 50. PERFORMED FLOORBEAM UPPER CHORD REPAIR BETWEEN LBL 33 AND RIGHT BODY FRAME.

Part: SKIN — DENTED (BS 760) · airframe 78,224 hrs · 22,593 cycles

SKIN DENTED BS 760 JUST ABOVE S16L. INSTALLED REPAIR BS 740-760 AND S15-17L IAW ECRA 5531-01630.

Part: SKIN — DENTED (FUSELAGE) · airframe 78,224 hrs · 22,593 cycles

FUSELAGE DENT AFT OF DOOR 2L AT STATION 760 BETWEEN STRINGERS 17 AND 18. DENT IS LOCATED AT STA 760 BETWEEN STR 15 LT AND 16 LT. ACP HFEC. DENT IS CRACK FREE AND WITHIN SRM 53-00-01 FIG 101 ITEM 1 LIMITS. NO FURTHER ACTION IS REQUIRED, ITEM ARCHIVED. REPAIR- :NEW DAMAGE AT THIS LOCATION REQUIRED A REPAIR DOUBLER TO BE INSTALLED PER ECRA 5331-01631.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,224 hrs · 22,593 cycles

FUSELAGE HAS LIGHTNING STRIKE DISCHARGE MARK AT ZONE 117 18 INCHES BELOW E&E COOLING FAN OUTLET LEFT SIDE OF FUSELAGE. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SKIN FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-00-01 REPAIR 3. C F9071 CREATED FOR REPEAT INSP REQ. REF SCAL LP 9979998. PER MM53-30-95 PAGE 602 ITEM 'B' OK TILL NEXT HMV. -INF- :TO BE RECHECKED AT C-CHECK AND REPAIRED AT NEXT HMV REF MM 53-3--95 PARAGRAPH 7. PER MM 53-30-5 PARAGRAPH 5 ARE WITH IN LIMITS.

Part: ACTUATOR — FAULTY (RUDDER) · airframe 78,224 hrs · 22,593 cycles

RUDDER RATIO CHANGER PART NUMBER 3800022-105 CURRENTLY INSTALLED AND REQUIRES REPLACEMENT PER WC 5R2717147 SEQ#448. REMOVED AND REPLACED RUDDER RATION ACTUATOR PER AMM. OPS, LEAK AND RIG CHECK GOOD.

Part: ACTUATOR — LEAKING (THRUST REVERSER) · airframe 78,224 hrs · 22,593 cycles

NR 1 ENGINE OUTBOARD T/R CENTER ACTUATOR LEAKING WHEN STOWED AFTER MOVEMENT. REMOVED AND REPLACED NR 1 ENGINE OUTBOARD T/R CENTER ACTUATOR PER AMM. REMOVED P/N 315A1801-24 - S/N 0677. INSTALLED P/N 315A1801-24; S/N 1189 MR78330.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 78,224 hrs · 22,593 cycles

EXTERIOR FUSELAGE BLEND OUT AT STA 324 & APPROX S-22R. REF SCAL LP 9979832. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER. REF SRM 53-00-01 REPAIR 3.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,224 hrs · 22,593 cycles

INSTALL REPAIR DOUBLER AT STA 1433 BETWEEN S- 30 AND S-29L. INSTALLED FUSELAGE REPAIR DOUBLER AT PREVIOUS AIRFONE ANTENNA LOCATION. REF SRM 53-00-01 REPAIR 3. ACCOMPLISH RII INSPECTION OF AMIS ITEM 2242054.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,224 hrs · 22,593 cycles

CORROSION ON FLOORBEAM STA 365 FROM RBL 6 TO RBL 42. PERFORMED UPPER T-CHORD REPLACEMENT PER REPAIR 3 OF ECRA 5310-05536.

Part: WIRE — DAMAGED (SHOULDER HEATER) · airframe 78,046 hrs · 22,536 cycles

CONNECTOR TO SHOULDER HEATER WIRED DAMAGED. REPLACED SHOULDER HEATER. REOPENED BY OPBLM MOGHADAM ON 24JUL12 FOR: ITEM STILL HAS PROBLEMS. WIRE W2064-0070-20 IS BURNED THROUGH 3 INCHES FROM CONNECTOR D1582. INSUFFICIENT WIRE FOR SIMPLE SPLICE REPAIR. NEEDS WIRE 560-4627. NON STOCK SEATTLE. OPENED LO CAPT AUX HEATER & HIGH CAPT AUX HEATER CB'S 94912ON P70 PANEL TO ISOLATE POWER TO WIRES. CAP & STOWED WIRE W2064 -0070-20. REF WD 21-45-11. -INF- :SHOULD READ OPEN & COLLARED CIRCUIT BREAKERS.PARTS: 560-4627 BMS13-48T10C1G20 WIRE. CUT OUT DAMAGED WIRE SECT, RETERMINATED CONNECTOR. CHECKS OKAY.

Part: BLADES — DAMAGED (NR 2 COMPRESSOR) · airframe 78,046 hrs · 22,536 cycles

NR 2 ENGINE FAN BLADES DAMAGED. REPLACED BLADE SET.

Part: B-NUT — LEAKING (FUEL LINE) · airframe 77,997 hrs · 22,516 cycles

LT ENGINE FCU SHOWS SIGNS OF FUEL LEAKAGE AT B-NUT FITTINGS ON LT SIDE OF FCU. REPLACED PACKINGS ON 3 AFT ADAPTERS AND RESECURED B-NUT'S. RAN ENGINE AND LINES LEAK CHECKED OKAY.

Part: DUCT — DAMAGED (PNEUMATIC SYS) · airframe 77,991 hrs · 22,512 cycles

UNUSUAL AIR HISSING NOISE COMING FROM NEAR FLOOR AIR VENT AT 39ABC. FOUND APU DUCT CRACKED AFT CARGO COMPARTMENT LT STA 540. CRACK ON UPPER SECTION OF DUCT APPROX 1 INCH LONG BY APPROX 1-4 INCH WIDE. APU BLEED INOPERATIVE. WHEN GND START INITIATED, NO HISSING SOUND HEARD FROM CRACKED DUCT. REPLACED DAMAGED APU PNEUMATIC DUCT IN AFT CARGO PIT SIDEWALL. LEAK CHECKED GOOD. NO HISSING NOISE NOTED.

Part: PSEU — FAULTY (MLG) · airframe 77,926 hrs · 22,493 cycles

EICAS GEAR DISAGREE ON FINAL WITH NORMAL GEAR DOWN GREEN LIGHTS ON. SECOND EXTENSION NORMAL. ACCOMPLISHED PSEU BITE. FAULTED 16 DIFFERENT SENSORS. GEAR DISAGREE MSG COMING FROM PSEU. REPLACED PSEU PER MM AND RELAY K10266 PER WDM. OPS CHECK GOOD. NO FAULTS OR EICAS MESSAGES.

Part: MODULE — CONTAMINATED (MLG) · airframe 77,832 hrs · 22,469 cycles

GEAR DISAGREE ON FINAL WITH THREE GREEN DISAPPEARED AFTER ABOUT 30 SECONDS. ACCOMPLISHED FIM 32-09-03 FIG 103. FOUND NO FAULTS WITH LANDING GEAR. FOUND HYDRAULIC FLUID RT MLG DOOR SENSORS AND CLEANED THEM. FOUND GAPPING PUDDY ON RIGHT MLG DOOR SENSORS AND REMOVED IT. LANDING GEAR HANDLE MODULE REPLACED.

Part: LINE — FAULTY (FUEL SYSTEM) · airframe 77,414 hrs · 22,343 cycles

FUELER REPORTS CTR TANK FUELING VALVES WILL NOT CLOSE WHEN SELECTED CLOSED OVERFUELED CTR TANK. REPLACED FUEL LINE P/N 344N2015 IAW MM.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 77,372 hrs · 22,329 cycles

CREW REPORTS LEFT ENG HYD PUMP FAILED AND LEFT SYSTEM FLUID QTY IS AT 65 PERCENT. REPLACED LEFT ENGINE DRIVEN PUMP PER AMM.

Part: CONNECTOR — DAMAGED (EEC) · airframe 77,359 hrs · 22,325 cycles

LEFT ENGINE ON GND UNABLE TO MANUALLY SELECT EEC SECONDARY CHANNEL FROM SECONDARY SELECT SWITCH AT P61 PANEL. FOUND CONTACT Y1 PUSHED BACK ON CONNECTOR D5860. SECURED CONTACT IN CONNECTOR. SECONDARY CONTROL MESSAGE SHOWS AND SEC CHANNEL SELECTED ON EPCS PAGE WHEN SELECTED ON P61 PANEL.

Part: EEC — FAULTY (LT ENGINE) · airframe 77,342 hrs · 22,319 cycles

LEFT ENGINE SEC CONT MESSAGE. CREW SHUTDOWN ENG, CLEARED MESSAGE AND PERFORMED RESTART. AT STARTER CUTOUT LT ENG SEC CONT MESSAGE RETURNED. PER FIM EPCS TROUBLESHOT FCU RESISTANCE, CHECKED OK. REPLACED NR 1 EEC PER MM. MESSAGE WENT AWAY AND REPLACED RELAY K10523 AND K10258.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 77,320 hrs · 22,312 cycles

CO-PILOTS FRONT WINDSHIELD MULTIPLE CRACKS. INSTALLED NEW WINDSHIELD PER AMM.

Part: WIRE — EXPOSED (EMERGENCY LIGHT) · airframe 77,055 hrs · 22,226 cycles

EMERGENCY LIGHT WIRING EXPOSED NEAR AFT LAVATORY. REPLACED END CAP AND SECTION OF COVER AND SECURED IN PLACE.

Part: WIRE — BROKEN (STICK SHAKER) · airframe 76,988 hrs · 22,204 cycles

STATUS MESSAGE WILL NOT CLEAR PRIOR TO START. FOUND WIRE BROKEN AT POS A OF D519 ON CAPTAIN'S STICK SHAKER. REPAIRED WIRE. REPLACED LEFT STALL WARNING MODULE PER MM. MESSAGE CLEARED. STALL WARNING SYS TEST OKAY.

Part: AUDIO PANEL — INOPERATIVE (HF SYSTEM) · airframe 76,931 hrs · 22,187 cycles

FIRST OFFICER CANNOT TRAMSMIT ON LEFT HF WITH EITHER BOOM OR HAND MIC. SWAPPED FIRST OBSERVER'S RADIO SELECT PANEL WITH THE FIRST OFFICERS PANEL. CHECKED L-HF RADIO ON THE FIRST OFFICER'S SIDE, OPS CHECKED NORMAL. CHECKED CAPTAINS LEFT HF AND RADIO WAS NORMAL. BOTH LT AND RT HF WORKING NORMAL.

Part: CONTROL PANEL — FAULTY (WEATHER RADAR) · airframe 76,876 hrs · 22,171 cycles

RADAR TILT UNREALISTIC-5 UNITS UP PAINTS STRAIGHT DOWN. REPLACED WX CONTROL PANEL AND WX TR ALL TESTED.

Part: ENGINE — MAKING METAL (NR 2) · airframe 76,734 hrs · 22,128 cycles

METALLIC DEBRIS FOUND ON ENG NR 2 NR 5 BEARING SCAVENGE CHIP DETECTOR. METALLIC DEBRIS FOUND ON ENG NR 2 NR 5 BEARING SCAVENGE CHIP DETECTOR. REPLACED NR 2 ENGINE PER AMM. ACP'D FINAL INSTALL INSPECTION OF RPL'D NR 2 ENGINE PER AMM.

Part: LIGHT — INOPERATIVE (EVAC SLIDE) · airframe 76,724 hrs · 22,126 cycles

SLIDE PRESSURE LIGHT AT 4L IS OUT. RELAMPED SLIDE ARMED LIGHT ABOVE DOOR 4L, OPS CK GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 76,597 hrs · 22,088 cycles

DURING WALK AROUND FOUND 16 LIGHTNING STRIKE MARKS ON THE LEFT LOWER SIDE OF FUSELAGE, SECTION 41 & 43, FROM STRINGERS 30 THROUGH STRINGER 17. REPAIRED 15 LIGHTNING STRIKES PER SRM 53-00-01, SECTION I, PARAGRAPH 4 AND REPAIRED 1 LIGHTNING STRIKE WITH A SOLID RIVET ONE SIZE LARGER PER SRM 53-00-01 SECTION II , PARAGRAPH II. ALODINED AND PRIMED. ACCOMPLISHED HFEC PER NDT MM 51-00-01-6 NO DEFECTS NOTED

Part: MODULE — FAULTY (FIRE DETECTION) · airframe 76,365 hrs · 22,025 cycles

CARGO FIRE SYST FAIL LIGHT DOES NOT ILLUMINATE ON TEST. REPLACED SWITCH MASTER MODULE AND CARD M10427, TESTS OKAY.

Part: GCU — INOPERATIVE (RT GENERATOR) · airframe 76,333 hrs · 22,016 cycles

RIGHT GENERATOR CONTROL UNIT INOPERATIVE EICAS MESSAGE ILLUMINATED AFTER ENGINE START. REPLACED GENERATOR CONTROL UNIT PER MM AND RAN BOTH ENGINES PER JRH AND FOUND GENERATOR TO BE OPERATING NORMAL.

Part: IDG — DEFECTIVE (RIGHT) · airframe 76,312 hrs · 22,012 cycles

RIGHT GENERATOR TRIPPING ON ENGINE START. SEVERAL POWER LEADS FOUND SLIGHTLY LOOSE ON IDG. SECURED POWER LEADS PER AMM. ACP ENG RUN AT GATE. CKS OKAY. AIRCRAFT RETURN TO GATE. RIGHT ENGINE GENERATOR TRIPPING OFF LINE. REPLACED IDG PER AMM, OPS CK GOOD.

Part: CONNECTOR — DIRTY (LT EFIS) · airframe 76,265 hrs · 21,999 cycles

CAPT SIDE NO MAP DH FLAG AND TCAS FAIL. CLEANED CONNECTOR LT EFIS CONTROL PANEL, CHECKED OK.

Part: ACTUATOR — INOPERATIVE (LT MLG DOOR) · airframe 76,265 hrs · 21,999 cycles

LEFT MLG DOOR DOWN ON ARRIVAL AT GATE. DOOR LIGHT ON WHEN PARKING AT GATE. REMOVED & REPLACED LT MAIN GEAR DOOR ACTUATOR. OPS CHECKED GOOD.

Part: CONTROL UNIT — FAULTY (RUDDER) · airframe 76,184 hrs · 21,974 cycles

AC YAW AT HIGH SPEED. REPLACE RUDDER AND MONITOR PRINTED CIRCUIT UNIT CARD ASSY DUE TO BOTTOM RUDDER PCA FAILING TEST. RPLC'D CARD ASSY PER MM & TESTED SYSTEM. OPERATES PROPERLY. IN ADDITION, LOWER RUDDER PCU IS STILL NOT PASSING. CARD WAS CHANGED AS A PRECAUTION AND CARD SYSTEM OPERATES PROPERLY. SEE SMC30 FOR REPLACEMENT OF PCU. PERFORMED PCA PRESS. DIFF. SEN S. ISOL. TEST ITEM 'O' OF MM. TEST INDICATED FAULTY RUDDER PCA (BOTTOM), COMPLETE TEST FROM STEP 25 AFTER RUDDER PCA RPL. RMV'D LWR PCA FOUND ROD END ATTACH BOLT & BUSHING DAMAGED, HARDWARE ORDERED FROM JJ RMV'D PER MM. COMPLETED INSTALLATION OF BOTTOM RUDDER PCA AND COMPLETED THE PCA PRESS DIFF SENS ISOL. TEST OF MM "O" OPS CHECKS GOOD.

Part: UNKNOWN — DEFECTIVE (HF COMM) · airframe 76,184 hrs · 21,974 cycles

HF 1 RECEPTION IS INTERMITTANT. SEEMS TO TRANSMIT OKAY. SUSPECT COUPLER DUE TO NOT TUNING COMPLETELY SEEMS TO TUNE OFF FREQ.

Part: ENGINE — POWER LOSS (NR 1) · airframe 76,184 hrs · 21,974 cycles

ABORTED TAKEOFF AT 140 KIAS FOR NR 1 ENGINE ROLLBACK WITH FUEL FLOW FLUCTUATIONS. CAPTAIN NOTICED THE NR 1 FUEL FLOW DROPPING OFF JUST PRIOR TO PULLING THROTTLE BACK. DID NOT NOTICE ANY OTHER PARAMETER FLUCTUATION.

Part: TRANSCEIVER — FAULTY (LT HF SYSTEM) · airframe 76,144 hrs · 21,962 cycles

LEFT HF WORKS BUT FADES IN AND OUT AT TIMES COMPARED TO THE RIGHT HF. REPLACED LEFT HF TRANCEIVER, CHECKED OK.

Part: UNKNOWN — UNKNOWN (MLG) · airframe 75,966 hrs · 21,915 cycles

GEAR DOORS EICAS AND LIGHT ABOVE HANDLE. CREW REPORTED GEAR HANDLE PLACED IN UP POSITION PER QRH PROCEDURE,VIBRATION AND NOISE WENT AWAY AND "DOORS" LIGHT AND EICAS EXTINGUISHED. CREW COULD NOT PINPOINT AREA OF VIBE-NOISE, BUT SUSPECT COMING FROM MAINS. PERFORMED PSEU BITE TEST PER AMM, NO FAULTS NOTED. ACCOMPLISHED MLG EXTENSION AND RETRACTION TEST AS PER AMM, CHECKED GOOD. VERFIFIED MLG DOORS FLUSH AND FAIR.

Part: ENGINE — MAKING METAL (NR 2) · airframe 75,853 hrs · 21,880 cycles

NR 2 ENG RPL 5552-2 ESN 728701: DUE TO METAL FOUND ON THE ANGLE GEAR BOX CHIP DETECTOR AND THE MAIN OIL FILTER EXCEEDING MM LIMITS. REMOVED THE METAL FOUND ON THE AGB CHIP DETECTOR AND PUT INTO A PLASTIC BAG. CLEANED THE CHIP DETECTOR. RE-INSTALL THE AGB CHIP DETECTOR AND ATTACH BAG WITH METAL PARTICLES TO THE ANGLE GEARBOX FOR ENGINEERING INSPECTION WHEN ENGINE RETURNED TO SHOP. OIL FILTER RPL. OLD FILTER COLLECTED FOR ANALYSIS ALONG WITH METAL FLAKES FROM ANGLE GEARBOX AND SENT TO SFOEP HADI RASTROU. RE-INSTALLED THE OIL FILTER REMOVED FROM THIS ENGINE FOR INSPECTION. REPLACED THE NR 2 ENG.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 75,719 hrs · 21,840 cycles

EXT EVAC LT ON AFT CARGO DOOR INOP. RELAMPED CARGO LIGHT.

Part: SHUTOFF VALVE — LEAKING (HYDRAULIC SYS) · airframe 75,719 hrs · 21,840 cycles

LT W-W HMG SHUT OFF VLV IS LEAKING HYD FLUID FROM AROUND BACK SIDE OF VLV WITH HYD POWER ON SYSTEM. REMOVED SHUT-OFF VALVE MR29245 SN 5757. INSTALLED VLV MR29245-6638 PER MM.

Part: OIL SYSTEM — LOW (APU) · airframe 75,562 hrs · 21,796 cycles

APU FAULT AND SHUTDOWN TWICE AFTER LANDING. BITE CHECK ECU FAULTS GEN FILTER CLEANED PRESS SW, NO HELP. GEN FILTER DPI IS NOT POPPED. SEE HISTORY. FOUND OIL ONE QT LOW. ECU BITE HAD NO FAULTS RECORDED. START AND RUN FOUR TIMES FOR TOTAL OF ONE HOUR. APU RUNS NORMAL.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 75,358 hrs · 21,733 cycles

SOFT FLOOR PANEL IN AISLE AT ROW 33. FLOOR PANEL INSTALLED AT SEATS 39 & 40ABC REINSTALLED CARPET AND SEATS.

Part: LIGHT — INOPERATIVE (L3 DOOR) · airframe 75,358 hrs · 21,733 cycles

DOOR ARMED LIGHT INOPERATIVE AT DOOR 3L. NOTICED DURING CLIMBOUT. SECURED DOOR ARMED LIGHT ASSY, OPS GOOD.

Part: CONTROL PANEL — FAULTY (LT VHF) · airframe 75,353 hrs · 21,730 cycles

LEFT VHF COMMS AUDIO RECEPTION POOR AT 1 POSTITION. RECEPTION OK AT OTHER CREW POSITIONS. (01=CAPT POS'N, 02=1ST OFF POS'N, 03=OBS POS'N). CAPT'S SIDE TONE INEXPLICABLY INTERMITTENT ON VHF 1. REPLACED CAPT AUDIO CONTROL PANEL. CHECKED OKAY.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 75,341 hrs · 21,724 cycles

CREW REPORTS ON TAKEOFF ROLL AT 130 KIAS (ALL 3 GEAR STILL ON THE GROUND), CREW FELT A MOMENTARY JOLT-YAW-LATERAL MOVEMENT NOSE LEFT. CREW COUNTERED WITH SLIGHT RT RUDDER. CREW DID NOT FEEL ANY MOVEMENT IN RUDDER PEDALS PRIOR TO COUNTERING THE YAW. RUNWAY WAS CHECKED FOR BLOWN TIRE-NONE FOUND. NO REPORTED GUSTY WINDS. CREW ALSO REPORTS AIRCRAFT HANDLED NORMALLY IN CRZ AND CLIMB. INSPECTED LANDING GEAR, TIRES AND STRUTS, OPERATED FLIGHT CONTROLS, ACP WALK AROUND OF ACFT NO ABNORMALITIES FOUND.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 75,318 hrs · 21,716 cycles

NO BACKGROUND LIGHTING ON F/O'S MIC-AUDIO SELECTOR PANEL. REPLACED F/O'S AUDIO CONTROL PANEL, CHECKED OKAY.

Part: COUPLER — FAULTY (HF COMM) · airframe 75,234 hrs · 21,693 cycles

LEFT HF RADIO DOES NOT TRANSMIT. SAMC TEXT: PLZ ACP BITE PER FIM. NO PARTS OR EQUIPMENT IN OGG. PUT GOOD RECEIVER FROM ANOTHER A/C INTO POSITION, NO HELP. PUT ORIGINAL R-T BACK IN LEFT POSITION. REPLACED LEFT HF COUPLER PER MM. CO PART S/N 10360 INSTALLED AT PTT 7523404. REMOVED S/N 115823.

Part: GIRT BAR — OBSTRUCTED (L4 DOOR) · airframe 75,065 hrs · 21,645 cycles

DOOR 4L SLIDE ARMED LIGHT WENT OUT IN FLIGHT. REMOVED SWIZZLE STICK FROM DOOR GIRT BAR AREA. CLOSED AND ARMED DOOR. CHECKS OKAY.

Part: BATTERY — FAULTY (APU) · airframe 74,978 hrs · 21,620 cycles

APU WON'T START. REPLACED APU BATTERY PER AMM. APU STARTS GOOD AND SYSTEM CHARGING GOOD.

Part: SOCKET — DIRTY (L4 DOOR) · airframe 74,966 hrs · 21,616 cycles

THE 4L SLIDE LIGHT NOT ILLUMINATED. CLEANED LIGHT SOCKET AND LED MOD, OPS CHECKED OK. OPERATED DOOR 5 TIMES NO PROBLEMS.

Part: BATTERY — FAILED (APU) · airframe 74,800 hrs · 21,572 cycles

APU FAILED TO START. FAULT LGT ILLUM AND EICAS MSG. APU FAULT DISPLAYED. SECOND ATTEMPT INDICATES (SLOW ACCEL, HUNG START). CREW COMMENTS: APU FAULT AFTER LANDING. APU BAT VOLTS AT 15V. REPLACED APU BATTERY PER MM, GROUND CHECKED NORMAL.

Part: UNKNOWN — MALFUNCTIONED (L4 DOOR) · airframe 74,804 hrs · 21,573 cycles

DOOR 4L SLIDE LIGHT INOPERATIVE. CHECKED DOOR 4L GIRT BAR AREA FOR DEBRIS. NONE FOUND. ARMED DOOR 4L SEVERAL TIMES WITH NO DEFECTS WITH SLIDE LIGHT. CHECK OK.

Part: CHARGER — FAULTY (APU BATTERY) · airframe 74,596 hrs · 21,515 cycles

APU BATTERY CHARGER NOT CHARGING. APU BAT AT 25VDC NOT CHARGING. NEEDS 560-9015, BATTERY CHARGER FOR APU. DEACTIVATED CHARGER REF. RPL APU BATTERY CHARGER PER MM.

Part: SEAT — LOOSE (29 ABC) · airframe 74,261 hrs · 21,417 cycles

SEAT ASSY LOOSE 29ABC. REPLACED RT FRONT MOUNT STUD AND ANTI RATTLE NUT IAW MM.

Part: OXYGEN MASK — DAMAGED (COCKPIT) · airframe 73,884 hrs · 21,303 cycles

CAPTS O2 MASK "NORM"-"COMF" LEVER BROKE OFF. REPLACED CAPTS O2 MASK.

Part: FITTING — LEAKING (HYD SYSTEM) · airframe 73,855 hrs · 21,291 cycles

HYDRAULIC LEAK NR 2 ENG PYLON, CASE DRAIN FILTER MODULE DELTA P INDICATOR. REPLACED DELTA P INDICATOR. MOTOR ENG NO LEAKS.

Part: LANYARD — OUT OF POSITION (EVAC SLIDE) · airframe 73,743 hrs · 21,255 cycles

LANYARD HANGING FROM SLIDE PACK. REPLACED LANYARD.

Part: IDG — FAULTY (NR 1) · airframe 73,708 hrs · 21,246 cycles

CREW REPORTED LEFT GEN DRIVE LIGHT ILLUMINATED DURING FLT. GENERATOR DISCONNECTED IAW FLT MANUAL PROCEDURES. HAS BEEN SERVICED AND SIGNED OFF 3 TIMES. REPLACED IDG ON NR 1 ENG IAW MM. OPS CHECKED IAW MM. OPS AND LEAK CHECKED GOOD. NO FAULTS NOTED.

Part: FAN — FAULTY (COCKPIT) · airframe 73,551 hrs · 21,203 cycles

UNCOMFORTABLE, AFFECT PILOTS-ATC COMMUNICATIONS TURNING R RECIRC FAN OFF PROVEN LITTLE HELP. RECIRC FAN IS OLD STYLE WITHOUT BAFFLE. PER SERVICE TIP OK TO DEFER FOR FAN REPLACEMENT. NEED FAN PCN 564-0211. REPLACED RIGHT RECIRC FAN, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (MID LAV) · airframe 73,437 hrs · 21,164 cycles

EMERGENCY LIGHT LOCATIONED AT MID LAV BURNT OUT. REPLACED EMERGENCY LIGHT, OPS CHECK GOOD.

Part: HANDLE — FAULTY (L1 DOOR) · airframe 73,196 hrs · 21,091 cycles

2ND RETURN TO GATE DUE TO DOOR 1L HANDLE REPORTEDLY POPPING OPEN WHILE TAXIING AROUND. TAXI'D A-C TO HANGAR. WHILE UNDER WAY PRESSURIZED A/C SLIGHTLY AND THEN UN-PRESSURIZED. THE PLANE WAS BOUNCING PRETTY GOOD GOING OVER 9R DOOR HANDLE DID NOT POP. TRIED PRESSURIZING AGAIN HANDLE DIDN'T MOVE. NOTICED DOOR ASSIST ACTUATOR A LITTLE WEAK. DOOR HARD TO CLOSE. MIGHT BE NORMAL. CREW DID NOT GET DOOR WARNING WHEN ALLEGED HANDLE POPPED. CHECKED 1L DOOR STOPS WITH MORTITE. ADJUSTED AFT DOOR FRAME STOPS. RE-ATTACHED 2 AFT SIDE STOP PADS WITH SEALANT. DOOR HANDLE AND ARM LEVER OPS NORMAL.

Part: SHUTOFF VALVE — FAULTY (FUEL SYSTEM) · airframe 73,193 hrs · 21,090 cycles

RT ENG FUEL SHUTOFF VLV WOULD NOT OPEN FOR ENG RUN. REPLACED FUEL SHUT-OFF VALVE PER MM. OPS CHECK NORMAL.

Part: LANYARD — UNSECURE (L2 DOOR) · airframe 73,149 hrs · 21,076 cycles

CREW REPORT: DOOR 2L SLIDE STRINGS HANGING OUT OF COVER. RE-SECURED LANYARD STRING.

Part: PROXIMITY SWITCH — WEAK (L2 DOOR SLIDE) · airframe 73,131 hrs · 21,070 cycles

2L SLIDE LIGHT NOT ON. APPLIED MEL2566S. REF TO WD 25-66-11, FOUND GIRT BAR PROX S108218 WEAK. REPLACED PROX SWITCH. OPS CHECKED OKAY.

Part: CONTROL PANEL — FAULTY (RUDDER TRIM) · airframe 72,998 hrs · 21,028 cycles

RUDDER TRIM INTERMITTANTLY INOP IN RIGHT DIRECTION. LEFT WORKS OKAY. REPLACED RUDDER AILERON TRIM PANEL PER MM AND GROUND TEST GOOD.

Part: FUEL LINE — KINKED (APU) · airframe 72,850 hrs · 20,984 cycles

APU FUEL SUPPLY LINE IN KINKED THAT GOES FROM FCU TO FIREWALL. REPLACED FUEL LINE, LEAK CHECKED GOOD.

Part: APU — OIL CONSUMPTION · airframe 72,602 hrs · 20,911 cycles

APU OIL CONSUMPTION ABOVE LIMIT. REPLACED APU ASSY IAW MM, ALL CHECKED OK.

Part: BATTERY — FAULTY (APU) · airframe 72,601 hrs · 20,910 cycles

APU DID NOT START, TRIED 3 TIMES. 2 MORE ATTEMPTS. EGT 770, RPM 20. NO LRU'S FAULTED ON APU CONTROLLER. ACFT REROUTED NON-ETOPS TO BASE FOR FIX. REPLACED APU BATTERY AND APU BATTERY CHARGER IAW MM.

Part: O-RING — LEAKING (SPOILER ACTUATOR) · airframe 72,553 hrs · 20,894 cycles

FOUND NR1 SPOILER POWER CONTROL ACTUATOR, LEAKING HYD FLUIDS. REPLACED LEAKING O-RING ON ACTUATOR PLUG-BLEEDER.

Part: O-RING — LEAKING (SPOILER ACTUATOR) · airframe 72,553 hrs · 20,894 cycles

L/E SLATS WILL NOT REACTIVATE. FOUND NR1 SPOILER POWER CONTROL ACTUATOR LEAKING HYD FLUIDS. REPLACED LEAKING O-RING ON ACTUATOR PLUG-BLEEDER. L/E SLAT BYPASS VALVE RED LEVER WHEN MOVED OUT OF POSITION (2) DOES NOT RETURN ELECTRICALLY TO ORIGINAL POSITION. REPLACED VALVE ASSY IAW MM, CHECKS GOOD.

Part: SWITCH — FAILED (APU DOOR CONTROL) · airframe 72,434 hrs · 20,861 cycles

APU NO START ON THE GROUND. APU FAILED TO START SEVERAL TIMES. BIT OF ECU SHOWS CURRENT LAST RUN, RUN ABORTED "AC START CIRCUIT". APU DOOR CONTROL SWITCH REPLACED. RAN APU FOR 2 HOURS AND PERFORMED MULTIPLE APU STARTS. APU CHECKED GOOD, NO FAULTS.

Part: STRAP — OUT OF POSITION (L3 DOOR) · airframe 72,433 hrs · 20,860 cycles

CAN'T ARM DOOR 3L. REPOSITIONED STRAP. OPS NORMAL.

Part: CHARGER — FAULTED (APU STARTER) · airframe 72,411 hrs · 20,855 cycles

APU FAILED TO START. FAULT LIGHT ILLUMINATED AND EICAS MESSAGE. APU FAULT DISPLAYED. REPLACED APU. AFTER APU REPLACEMENT STILL UNABLE TO START, FOUND BATTERY VOLTAGE DURING CRANK CYCLE AT 8VDC. REPLACED APU BATTERY AND CHARGER PER MM. OPS CKS NORMAL.

Part: ACTUATOR — FAULTY (APU) · airframe 72,361 hrs · 20,832 cycles

APU FAULT DURING SHUTDOWN. FAULT LGT ILLUM AND EICAS MSG APU FAULT DISPLAYED. REPLACED VALVE ACTUATOR IAW AMM, OPS GOOD.

Part: DOOR ACTUATOR — FAULTY (APU BAY) · airframe 72,352 hrs · 20,829 cycles

APU DOOR STATUS MESSAGE. REPLACED APU DOOR INLET ACTUATOR. OPERATED SEVERAL TIMES, APU WORKS FINE. NEEDS ALITITUDE START TO VERIFY DOOR OPERATIONS. CREW SAID START NORMAL AT FLIGHT LEVEL 390.

Part: ACTUATOR — FAULTY (FUEL SHUTOFF) · airframe 72,303 hrs · 20,812 cycles

APU FUEL SHUTOFF VALVE INOP. DUE HISTORY AND ETOPS SENSITIVE, VALVE MADE INOPERATIVE IN CLOSED POSITION IAW MEL PROCEDURES. REPLACED APU FUEL SHUTOFF VALVE ACTUATOR IAW MM, OPS CHECK GOOD.

Part: RELAY — FAULTY (APU ENGINE INLET) · airframe 72,273 hrs · 20,800 cycles

APU WOULD NOT START IN FLT. REPLACED APU INLET DOOR RELAY (K176). OPERATED INLET DOOR NUMEROUS TIMES WITH NO DISCREPANCIES & INSP. INLET DOOR FAIRING AND LINKAGE. RECOMMEND REPLACING ECU BOX (PRECAUTIONARY). REPLACED APU CONTROLLER, OPS CHECK OK.

Part: ACTUATOR — FAULTY (APU DOOR) · airframe 72,240 hrs · 20,789 cycles

APU DOOR WILL NOT OPEN. REPLACED APU DOOR ACTUATOR, OPS CHECKS NORMAL.

Part: SELECTOR — MALFUNCTIONED (CABIN PRESSURE) · airframe 72,240 hrs · 20,789 cycles

CABIN ALTITUDE CONTROL SELECTOR SPINS BUT WON'T ACTUALLY CHANGE LANDING ALTITTUDE. REPLACED PANEL, GROUND CHECKED OK.

Part: FAN — NOISY (COCKPIT) · airframe 72,230 hrs · 20,787 cycles

COCKPIT NOISE LEVEL VERY HIGH. RT RECIRCULATION FAN LOUD. REPLACED RT RECIRCULATION FAN, OPS CHECKS GOOD.

Part: SERVO — MALFUNCTIONED (AUTOTHROTTLES) · airframe 7,656 hrs · 20,630 cycles

ON TAKE OFF RT THROTTLE, STOPPED AT 1.33 EPR HAD TO FORCE THROTTLE TO T/O EPR. CONSULTED WITH ENG CONTROLLER, ADVISED TO DEFER AUTOTHROTTLE SYS. OPERATED THROTTLES TO FIREWALL, NO BINDING FELT. FOUND THRUST REVERSER INTERLOCK ACTUATOR IN EXTENDED POSITION, REPLACED IAW AMM. ALSO REPLACED AUTOTHROTTLE SERVO IAW AMM.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 71,624 hrs · 20,619 cycles

OBSERVERS O2 MASK LEAKS AT HARNESS. NO PARTS NEED MASK ASSY. OBSERVERS SEAT INOPERATIVE. REPLACED OBSERVERS OXYGEN MASK.

Part: ROD — OUT OF ADJUST (RUDDER TCS) · airframe 71,487 hrs · 20,571 cycles

RUDDER TRIM ISSUE. REQUIRES 3.5 UNITS OF LT RUDDER TO FLY STRAIGHT AND LEVEL. RUDDER PCA'S RIG COMPLETE, NOW ADJUSTING RUDDER RATIO INPUT RODS. ADJUSTED RUDDER AND RUDDER TRIM CONTROL SYSTEM, OPS CHECKED GOOD.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 71,463 hrs · 20,563 cycles

CAP O2 MASK LEAKS AT HOSE CONNECTION. REPLACED MASK ASSY.

Part: FILTER — FAULTY (EQUIPMENT COOL) · airframe 71,118 hrs · 20,458 cycles

CREW REPORTS OFF THE BLOCKS. EQUIPT OVERHEAT EICAS ADVISORY MSG. NO ASSOCIATED MAINT MSG. OK IN ALTN. REPLACED EQUIPMENT COOLING FILTER, SYS OPS NORMAL.

Part: CONTROLLER — FAULTY (WHC M192) · airframe 70,953 hrs · 20,411 cycles

DURING BITE CHECK OF WHC M192, CONTROLLER FAIL LIGHT ILLUMINATED. CONTROLLER FOUND FAULTY. REPLACED WHC, OPS CK NORMAL.

Part: CONTROL UNIT — FAILED (WINDOW HEAT) · airframe 70,932 hrs · 20,406 cycles

L FWD WINDOW HEAT INOPERATIVE. REPLACED WHCU M191 IAW MM. SYS TESTED SATISFACTORY.

Part: CONTROL MODULE — FAULTY (SPOILER SYS) · airframe 70,888 hrs · 20,396 cycles

SPOILER MSG. UPON ARRIVAL, FOUND SPOILER CONTROL MODULE 1L HAD MODULE FAULT LIGHT. REPLACED SPOILER CONTROL MODULE. TESTS NORMAL. ALSO PUT SPOILER CONTROL MODULE IN POSITION.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 70,887 hrs · 20,395 cycles

LEFT OUTBOARD AFT FLAP DENTED AND POSSIBLE DELAMINATION. LOCATED INBOARD OF OUTBOARD CANOE NEAR TRAILING EDGE. REPAIRED AREA IAW SRM.

Part: BYPASS VALVE — FAILED (LE SLAT) · airframe 70,684 hrs · 20,339 cycles

L/E SLATS INOP IN ALTERNATE, L/E SLATS DISAGREE EICAS MESSAGE. TROUBLESHOT SYSTEM PER MM. NEEDS BYPASS VALVE V10059. VALVE REPLACED. ACP OP TEST PER MM, CHECKS OKAY. ACP'D OP TEST OF FLAP SLAT. ALT DRIVE SYS PER JIC, OP CHECK OKAY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,684 hrs · 20,339 cycles

NR 2 MED EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP, OPS GOOD.

Part: PUMP — FAULTY (HYDRAULIC SYS) · airframe 70,505 hrs · 20,290 cycles

AC MOTOR PUMP - WITH LOW PRESS LIGHT ILLUMINATED AND EICAS MESSAGE 'R HYD ELEC PUMP' DISPLAYED AND EICAS MESSAGE 'HYD SYS MAINT' WAS NOT DISPLAYED. CREW COMMENTS: PRESS LIGHT ALSO ON W-EICAS MSG. NOTICEABLE BUMP IN YOKE WHEN LIGHT GOES OUT. REPLACED RT ACMP AND PRESSURE AND CASE DRAIN FILTERS IAW AMM. RT ACMP IS CYCLING ON AND OFF WITH PUMP SWITCH IN 'ON' POSITION. REPLACED RELAY K10255 AND K10525 PER WDM. OPERATED PUMP FOR 15 MINUTES, PUMP NORMAL. FOUND PIN 8 AT ELCU CONNECTOR D3062 LOSING 28VDC SIGNAL AFTER 2 MINUTES OF OPS. PUMP RECOVERS AFTER 5 SECOND TIME DELAY. PUMP AND PRESSURE NOW NORMAL.

Part: SWITCH — BINDING (TEST PANEL) · airframe 70,308 hrs · 20,237 cycles

SQUIB TEST PANEL TEST SWITCH 2 DIFFICULT TO OPERATE. REPLACED MISSING LENS.

Part: CONTROLLER — FAULTY (A/C PACK) · airframe 70,164 hrs · 20,196 cycles

LT PACK LIGHT INOP ON WITH PACK IN AUTO. LT PACK INOP IN AUTO, STANDBY OK. REPLACED LT PACK TEMP CONTROLLER ACCT CONTROLLER FAULT MESSAGE ON LT PACK CONTROLLER. CKS OK.

Part: FSEU — FAULTY (TE FLAPS) · airframe 70,104 hrs · 20,172 cycles

T/E FLAP DISAGREE LIGHT ON WHEN FLAPS SELECTED TO 5. ONLY LT ENG RUNNING. TROUBLESHOT IAW FIM, ENDED UP AT BLOCK NR 53. REPLACED SOLENOID VALVE, NO HELP. STILL GET DISAGREE. TESTED DEPRESSURIZATION MODULE PRESSURE SWITCH FOUND OPEN WITH HYD SYS PRESSURIZED. SUSPECT BAD SWITCH. REPLACED PRESSURE SWITCH, NO HELP. NEEDS FURTHER TROUBLESHOOTING. NEED TO ACCOMPLISH OPERATIONAL TEST OF FLAP-SLAT SOLENOID VALVEON ACCOUNT OF REPLACEMENT. CKS OK. REPLACED FSEU-1. PLACED NR 2 FSEU (-40) IN NR1 POS IAW MM.

Part: BLADE — NICKED (NR 1 ENGINE) · airframe 69,886 hrs · 20,107 cycles

NR 1 ENGINE 3 BLADES HAVE SEVERAL NICKS. REPAIRED BLADE AREAS MARKED WITH WHITE DOTS, WILL NEED EDDY CURRENT CHECK. ACCOMPLISHED BLADE HFEC NDT PER MM. INDICATIONS NORMAL. BLADE REPAIRS WITHIN LIMITS.

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 69,254 hrs · 19,936 cycles

EXT EVAC LIGHT INOP AT DOOR 2 RT. RELAMPED EVAC LIGHT, CHECKS OK.

Part: LANYARD — EXPOSED (L2 DOOR SLIDE) · airframe 68,831 hrs · 19,806 cycles

DOOR 2L SLIDE STATIC COMING OUT OF SLIDE. REPORTED BY CREW AT DEPARTURE. REPOSITIONED STATIC CORD. SLIDE NOT REMOVED FROM DOOR. INSPECTED DOOR 2L SLIDE INSTALLATION. OK FOR SVC.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,770 hrs · 19,786 cycles

FOUND EMERGENCY LIGHTING NOT WORKING FWD OF AFT LAV DOOR. REPLACED EMERGENCY EGRESS LIGHTING FWD OF AFT LAV DOOR.

Part: RELAY — FAULTY (ANTI ICE SYS) · airframe 68,426 hrs · 19,691 cycles

RT/LT WING ANTI-ICE VLV IND, FLIGHT DIVERTED. WITH WING ANTI-ICE SW SELECTED ON, LT, RT VALVE LIGHTS REMAINED EXTINGUISHED. NO EICAS MESSAGE DISPLAYED. REPLACED K204 RELAY. ACP SYS OPS CK. OPS CK OK.

Part: COVER — UNSECURE (L2 DOOR) · airframe 68,314 hrs · 19,650 cycles

DANGLING CORD OFF OF SLIDE PACK DOOR 2L. SECURED SLIDE COVER.

Part: PANEL — LEAKING (FUEL SYSTEM) · airframe 67,930 hrs · 19,530 cycles

FUEL LEAKING FROM RT WING PYLON AREA. FUEL FOUND LEAKING FROM DRY BAY DRAIN. OPENED AND VENTED RT FUEL TANK AND INSTALLED DRY BAY POSITIVE PRESSURE EQUIPMENT. FOUND LEAK AT NR 2 ENG FUEL SUPPLY LINE FITTING. REMOVED DAMAGED SEALANT AND RESEALED. WILL NEED TO BE LEAK CHECKED AFTER 0300-04NOV. REMOVED LEAK TEST PANEL AND INSTALLED PNL 632CZ. LEAK CHECKED GOOD.

Part: TERMINAL — ARCED (WINDOW HEAT) · airframe 67,930 hrs · 19,530 cycles

ON CLIMBOUT AND INITIAL CRUISE GOT ELECTRICAL-ACRID SMELL IN COCKPIT. SUPPLEMENTAL DATA UPDATE FOUND THE CAPT'S WINDOW ARCING CAUSING THE PROBLEM. CAPT NR 1 WINDOW HAS A LOOSE POWER TERMINAL CONNECTION CAUSING ARCING AND BURN RESIDUE ON WINDOW. REPLACED WINDOW AND TERMINAL.NEEDS FINAL TORQUE AFTER 8AM. FINAL TORQUE ACCOMPLISHED.

Part: FAN — DIRTY (POS 1) · airframe 67,928 hrs · 19,529 cycles

ODOR FROM CAPT EYEBALL VENT, EGPWS WARNING, SELECTED LT RECIRC FAN OFF. WITH FAN OFF AND OVBD EXH VALVE OPEN, ODOR DISSIPATED. SELECTED R RECIRC FAN AND BOTH UTIL BUSSES OFF PRECAUTIONARY AS WELL AS TERR OVRRD, PER CREW. REPLACED BOTH PRIMARY NR 1 AND ALTERNATE NR 2 EQUIPMENT COOLING FANS. CHECKED BOTH RECIRC FANS FOR 3 PHASE. ALL INLET FILTERS CLEAN.

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT) · airframe 67,710 hrs · 19,463 cycles

ELECTRICAL ODOR IN COCKPIT, FLIGHT DIVERTED. CREW REPORTED ELEC ODOR ON CAPT SIDE AROUND THE AREA OF GLARE SHIELD. INSPECTED FWD AND CENTER E&E COMPARTMENTS. FOUND NO BREAKERS OUT OR ANY ELECTRICAL ODOR. REMOVED CAPT VOR CONTROL PANEL, HAD SLIGHT BURN ODOR. INBD CAPT AND F/O AGREED THAT THIS WAS THE BURN ODOR. REPLACED VOR CONTROL PANEL.

Part: TRANSMITTER — MALFUNCTIONED (TE FLAP) · airframe 67,691 hrs · 19,455 cycles

FLAPS FAIL TO MOVE. EICAS MESSAGE 'TE FLAP ASYM' DISPLAYED. REPLACED RIGHT TRAILING EDGE FLAP TRANSMITTER, CHECKS OKAY.

Part: ISOLATION VALVE — FAULTY (BLEED AIR SYS) · airframe 67,534 hrs · 19,416 cycles

FLT CREW REPORTS ISO VLV AMBER LIGHT ON. RECYCLE OF B2, B3 C/B'S, NO HELP. CYCLING BLEEDS ON-OFF, NO HELP ISO VLV APPEARS TO BE IN STUCK CLOSED POSITION. REPLACED VALVE, CHECKS OKAY.

Part: LINE — OUT OF POSITION (EVAC SLIDE) · airframe 67,534 hrs · 19,416 cycles

DOOR 1R WILL NOT ARM. FOUND SLIDE PACK STATIC LINE CAME PARTIALLY OUT OF ITS STOWAGE LOCATION, INTERFERING WITH GIRT BAR. INSPECTED LINE AN ATTACH POINTS, AND RESTOWED. CONFIRMED DOOR OPENS AND CLOSES NORMALLY, AND ARMS AND DISARMS NORMALLY.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 67,378 hrs · 19,371 cycles

FOUND FWD SECTION OF COACH SEAT EMERGENCY LIGHT IS NOT WORKING. REPAIRED PREVIOUSLY SPLICED SECTION OF THE RUNNER, OPS CHECK GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 66,961 hrs · 19,249 cycles

EMERGENCY FLOOR LIGHT STRIP PULLED UP, INOP. REPAIRED DAMAGED EEL STRIP AND RE-INSTALLED PLASTIC COVER. TESTED OKAY.

Part: LIGHT — DAMAGED (CABIN) · airframe 66,961 hrs · 19,249 cycles

EMERGENCY FLOOR LIGHT STRIP PULLED UP, INOP. REPAIRED DAMAGED EMERGENCY LIGHT STRIP AND RE-INSTALLED PLASTIC COVER. TESTED OKAY.

Part: PIN — DAMAGED (EXTINGUISHER) · airframe 66,628 hrs · 19,149 cycles

FIRE EXTINGUISHER IN LAST ROW OF FIRST CLASS HAS A DAMAGED PIN. REPLACED EXTINGUISHER.

Part: CONTROL VALVE — MALFUNCTIONED (LT A/C PACK) · airframe 65,459 hrs · 18,814 cycles

WITH LT PACK IN STANDBY, THE FLT DECK COMPT TEMP REGISTERS 64 DEG & COCKPIT IS COLD. BITE LT PACK TEMP CONT FAULT LT PACK TEMP CONTROL VALVE, REPLACED VALVE, REPLACED FLIGHT DECK TEMP FILTER, OPS AND LEAK CKS OK.

Part: FITTING — BROKEN (HYDRAULIC SYS) · airframe 65,096 hrs · 18,717 cycles

NR 1 ENG HYD PRESSURE HOSE IS CONTACTING HARD ON C-FLANGE OF ENG FAN CASE. REPLACED PRESS LINE FITTING DUE TO BEING BROKEN.

Part: FITTING — BROKEN (NR 1 ENGINE) · airframe 65,096 hrs · 18,717 cycles

NR 1 ENG HYD PRESSURE HOSE IS CONTACTING HARD ON C-FLANGE OF ENG FAN CASE. REPLACED PRESS LINE FITTING DUE TO BEING BROKEN.

Part: FITTING — BROKEN (NR 1 ENGINE) · airframe 65,096 hrs · 18,717 cycles

NR 1 ENG HYD PRESSURE HOSE IS CONTACTING HARD ON C-FLANGE OF ENG FAN CASE. REPLACED PRESS LINE FITTING DUE TO BEING BROKEN.

Part: SHUTOFF VALVE — FAULTY (LT ENGINE) · airframe 65,096 hrs · 18,717 cycles

RTO AT APPROX 70KTS DUE TO LEFT ENG HIGH STAGE LT ILLUMINATING. REPLACED LT ENGINE HPSOV AND HIGH STAGE PILOT VALVE, NO HELP. CONTINUING TO TROUBLESHOOT. NR 1 ENG READS 4 PSI, NO HIGH STAGE AFTER HIGH STAGE AND PILOT VALVE REPLACEMENT AT IDLE. BLEED LIGHT STAYS ON,1-12 FOUND K10197 LEFT PRSOV VALVE OFF RELAY INOP. REPLACED RELAY K10197. WILL REQUIRE TEST OF LEFT HIGH STAGE BLEED AIR. ACP'D PNEUMATIC HEALTH CHECK ON NR 1 ENG, ON THE FOLLOWING COMPONENTS, HPC, HPSOV, PRSOV, PRC, AND FAMV. ALL COMPONENTS PASSED. ACP'D PNEUMATIC SYS TEST ON NR 1 ENG. ALL PARAMETERS WITHIN LIMITS.

Part: VALVE — FAULTY (LT ENGINE) · airframe 65,096 hrs · 18,717 cycles

RTO AT APPROX 70KTS DUE TO LEFT ENG HIGH STAGE LIGHT ILLUMINATING. REPLACED LT ENGINE HPSOV AND HIGH STAGE PILOT VALVE, NO HELP. CONTINUING TO TROUBLESHOOT NR 1 ENG READS 4 PSI NO HIGH STAGE AFTER HIGH STAGE AND PILOT VALVE REPLACEMENT AT IDLE. BLEED LIGHT STAYS ON, 1-12 FOUND K10197 LEFT PRSOV VALVE OFF RELAY INOP. REPLACED RELAY K10197. WILL REQUIRE TEST OF LEFT HIGH STAGE BLEED AIR. ACP'D PNEUMATIC HEALTH CK ON NR 1 ENG, ON THE FOLLOWING COMPONENTS. HPC, HPSOV, PRSOV, PRC, AND FAMV. ALL COMPONENTS PASSED. ACP'D PNEUMATIC SYS TEST ON NR 1 ENG. ALL PARAMETERS WITHIN LIMITS.

Part: VALVE — FAULTY (LT ENGINE) · airframe 65,096 hrs · 18,717 cycles

RTO AT APPROX 70KTS DUE TO LEFT ENG HIGH STAGE LT ILLUMINATING. REPLACED LT ENGINE HPSOV AND HIGH STAGE PILOT VALVE, NO HELP. CONTINUING TO TROUBLESHOOT, NR 1 ENG READS 4 PSI, NO HIGH STAGE AFTER HIGH STAGE AND PILOT VALVE REPLACEMENT AT IDLE. BLEED LIGHT STAYS ON. 1-12 FOUND K10197 LEFT PRSOV VALVE OFF RELAY INOP. REPLACED RELAY K10197. WILL REQUIRE TEST OF LEFT HIGH STAGE BLEED AIR. ACP'D PNEUMATIC HEALTH CK ON NR 1 ENG, ON THE FOLLOWING COMPONENTS. HPC, HPSOV, PRSOV, PRC, AND FAMV. ALL COMPONENTS PASSED. ACP'D PNEUMATIC SYS TEST ON NR 1 ENG. ALL PARAMETERS WITHIN LIMITS.

Part: LIGHT — FAULTY (EVAC SLIDE) · airframe 64,823 hrs · 18,645 cycles

DOOR 1R SLIDE LIGHT ILLUMINATED WITH SLIDE DISARMED. VERIFIED PROPER OPERATION OF ARM AND DISARM FUNCTION. REPLACED LIGHT ASSY, OP CHECKED OKAY.

Part: APU — SMOKE · airframe 64,816 hrs · 18,640 cycles

EXCESSIVE SMOKE FROM APU TAILPIPE. REPLACED APU, OPS AND LEAK CHECKS NORMAL.

Part: APU — MALFUNCTIONED · airframe 64,816 hrs · 18,640 cycles

EXCESSIVE SMOKE FROM APU TAILPIPE.

Part: ACTUATOR — INOPERATIVE (RUDDER TRIM) · airframe 64,816 hrs · 18,640 cycles

RUDDER TRIM INOP. REPLACED RUDDER TRIM ACTUATOR.

Part: VALVE — MALFUNCTIONED (APU) · airframe 64,766 hrs · 18,623 cycles

RETURNED TO THE GATE 3 TIMES WITH AN APU FUEL PROBLEM. REACTIVATED APU. APU FUEL VLV REPLACED.

Part: EXCITER — INOPERATIVE (LT ENGINE) · airframe 64,721 hrs · 18,611 cycles

LEFT ENGINE WILL NOT START IN IGN SYSTEM NR 1. STARTS NORMAL IN BOTH. REPLACED EXCITER - IGNITER FOR SYSTEM 1.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 64,627 hrs · 18,590 cycles

EMERGENCY LIGHTS BAR CAME UNGLUED FROM FLOOR AT 2L. LOCATION IS NEXT TO FIRST CLASS CLOSET. SECURED WITH TAPE. SECURED EMERGENCY LIGHT NEXT TO FIRST CLASS CLOSET.

Part: FUEL CONTROL — FAILED (LT ENGINE) · airframe 64,246 hrs · 18,486 cycles

L ENG SEC CONT MSG DISPLAYED. REPLACED FCU. ACCMP TEST 2A IAW MM 71-00-59 ON NR 1 ENG FCU, NO LEAKS NOTED. ACCOMPLISHED ENGINE RUN PER JRH 2-95-1 AND 71-00-59, NO FAULTS NOTED.

Part: DOOR FRAME — DENTED (FWD CARGO DOOR) · airframe 64,163 hrs · 18,463 cycles

FWD CARGO DOOR DENTED, LOWER AFT INSIDE CORNER. MAJOR REPAIR ACCOMPLISHED. REPLACED LWR AFT CORNER FRAME P/N 143N6618-5.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 64,163 hrs · 18,463 cycles

G4B GALLEY PRESSURE DECK STA 1682-1720, RBL 53 UNDER WATER DRAIN CHANNEL HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION, TRIMMED OUT DAMAGED SKIN AND INSTALLED DOUBLER REPAIR.

Part: DOOR FRAME — GOUGED (FWD CARGO DOOR) · airframe 64,163 hrs · 18,463 cycles

FWD CARGO DOOR LOWER FWD FRAME CORNER GOUGED. MAJOR REPAIR ACCOMPLISHED. REMOVED CORNER SECTION OF FRAME AND INSTALLED NEW CORNER FRAME P/N 143N6618-6.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,163 hrs · 18,463 cycles

FWD PIT FRAME DENTED STA 520 AT STR 24L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED I/B FLANGE AND INSTALLED J-ANGLE REPAIR.

Part: STRUCTURE — DAMAGED (L2 DOOR) · airframe 64,163 hrs · 18,463 cycles

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

Part: FRAME — DENTED (FUSELAGE) · airframe 64,163 hrs · 18,463 cycles

DENT IN FUSELAGE FRAME AT STA 1420, STR 26L. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SECTION OF FLANGE AND FABRICATED A J-ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,163 hrs · 18,463 cycles

AFT PIT AT STA 1480, STR 26L FRAME DENTED AT INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SECTION OF FLANGE AND FABRICATED A J-ANGLE REPAIR AND INSTALLED.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,163 hrs · 18,463 cycles

FWD PIT FRAME DENTED AT BS 620 AND STR 24L. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SECTION OF FLANGE AND FABRICATED A REPAIR ANGLE AND INSTALLED.

Part: SKIN — DENTED (FUSELAGE) · airframe 64,163 hrs · 18,463 cycles

FUSELAGE SKIN DENT STA 760, AT STR 17L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,163 hrs · 18,463 cycles

MAIN CABIN FLOORBEAM STA 1640, RBL 57 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF T-CAP, RBL 0 TO RBL 64. FAB NEW SECTION AND SPLICES.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,163 hrs · 18,463 cycles

AFT PIT AT STA 1560, STR 26R, FRAME DENTED AT INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,163 hrs · 18,463 cycles

AFT PIT AT STA 1500, STR 26L FRAME DENTED AT INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,163 hrs · 18,463 cycles

AFT PIT AT STA 1520, STR 26L FRAME DENTED AT INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED FRAME SECTION AND INSTALLED DOUBLER REPAIR.

Part: VALVE — FAULTY (NR 2) · airframe 63,604 hrs · 18,315 cycles

SPLIT DUCTS AT 30000 RT 10 PSI HIGHER THAN LEFT AT CRUISE THRUST SMALLER SPLIT AT IDLE THRUST. NR 2 HIGH STAGE VALVE WEAK. REPLACED NR 2 HIGH STAGE VALVE. OPS CHECK ON GROUND RUN NORMAL.

Part: SENSOR — FAULTY (L2 SLIDE) · airframe 62,682 hrs · 18,059 cycles

2L SLIDE LIGHT DID NOT ILLUM. SENSOR SWITCH S10219 FAULTY. REPLACED SENSOR SWITCH 10219, OPS CHECKED GOOD.

Part: GIRT BAR — OBSTRUCTED (R4 DOOR) · airframe 62,526 hrs · 18,016 cycles

DOOR 4R ARMING LEVER OUT OF ADJUSTMENT. FOUND A PIECE OF SAFETY WIRE AT THE GIRT BAR MECHANISM PUSHROD, CAUSING ROD TO BIND. REPOSITIONED WIRE, AFTER RE-INSTALL, OPS CHECK OF DOOR EMERGENCY MECHANISM, NORMAL NO BINDING.

Part: BATTERY — FAILED (MAIN) · airframe 62,517 hrs · 18,014 cycles

AIRCRAFT WILL NOT ACCEPT POWER. MAIN BATTERY FAILURE. REPLACED MAIN AIRCRAFT BATTERY, CHECKS GOOD.

Part: COVER — BROKEN (CABIN) · airframe 62,480 hrs · 18,001 cycles

EMERGENCY LIGHT STRIP ROW 34 NEEDS REPAIR. REPLACED BROKEN STRIP COVER. EMERGENCY LIGHT CHECKS OK.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 62,123 hrs · 17,896 cycles

LT ENGINE OIL FILTER MSG ON START. FOUND GEARBOX BEARING FAILURE. REPLACED NR 1 ENGINE.

Part: STRUCTURE — DAMAGED (THRUST REVERSER) · airframe 61,930 hrs · 17,850 cycles

NR 1 ENGINE FOUND LT REVERSER HALF DAMAGED CONSISTENT WITH SERVICE TIP, LATCH ACCESS DOOR ALSO DAMAGED. REPLACED THRUST REVERSER HALF.

Part: CONTROLLER — FAILED (WINDOW HEAT) · airframe 60,810 hrs · 17,550 cycles

FWD RIGHT WINDOW EXTREMELY COLD DURING FLIGHT. RIGHT FWD HEAT INDICATES NORMAL. WINDOW FROZE UP ON FINAL. WINDOW HEAT CONTROLLER FAILURE. REPLACED RT WINDOW HEAT CONTROLLER, OPS CHECKED NORMAL.

Part: LIGHT — FAULTY (ROWS 23 AFT) · airframe 60,067 hrs · 17,329 cycles

FOUND EEL LIGHTS VERY DIM ROWS 23 AFT. REPLACED POWER STRIP AND ALL LAMPS FROM ROW 22 AFT.

Part: TRIM SYSTEM — FAILED (RUDDER) · airframe 60,010 hrs · 17,311 cycles

RUDDER TRIM FAILED ON APPROACH.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,632 hrs · 17,198 cycles

EXTERIOR EMERGENCY EXIT LIGHT AT DOOR 4R INOPERATIVE. RELAMPED EMERGENCY LIGHT.

Part: UNKNOWN — UNKNOWN · airframe 59,220 hrs · 17,083 cycles

FLIGHT DIVERTED DUE TO GEAR DOOR EICAS MESSAGE AND IRREGULAR FUEL BURN. INCREASE IN LOUD RUMBLE FROM MID CABIN AREA. SEVERAL MESSAGES ON GEAR DOOR WARNING. RH MAIN LANDING GEAR DOOR HANGS DURING GEAR SWING. SUSPECT SEQUNCE VALVE UPLOCK SEQUENCE VALVE MALFUNCTIONING.

Part: BATTERY — FAULTY (FLASHLIGHT) · airframe 58,690 hrs · 16,935 cycles

FOUND EMERGENCY FLASHLIGHT FAULTY. [07-24-07] REPLACED ALL EMERGENCY FLASHLIGHT BATTERIES.

Part: LIGHT — INOPERATIVE (R2 DOOR) · airframe 58,690 hrs · 16,935 cycles

DOOR 2R ARMING LIGHT INOPERATIVE. [06-20-07] REPLACED DOOR 2R PROX SENSOR.

Part: STRUCTURE — CRACKED (R2 DOOR) · airframe 58,690 hrs · 16,935 cycles

NR 2R MED CABIN DOOR UPPER HINGE CUTOUT CRACKED. [06-20-07] MAJOR REPAIR ACCOMPLISHED. REPAIRED 2R MAIN ENTRY CABIN DOOR UPPER HINGE CUT OUT PER UA ENGINEERING SPECIFICATIONS.

Part: CYLINDER — OUT OF TOLERANCE (LT OFFWING SLIDE) · airframe 58,690 hrs · 16,935 cycles

LEFT OFFWING SLIDE INFLATION CYLINDER EXCEEDS LIFE LIMIT. [06-20-07] REPLACED LT OFF WING SLIDE CYLINDER.

Part: TRANSMITTER — MALFUNCTIONED (ENGINE OIL SYS) · airframe 58,582 hrs · 16,910 cycles

FLUCTUATING OIL PRESSURE ON NR 1 ENGINE. WENT FROM 102 TO 180 SETTLING TO 160 IN CRUISE. FOUND LINE DISCONNECTED AT BOTTOM OF DEOILER. SECURED LINE. RAN ENGINE AT IDLE FOR 5 MIN. NO LEAKS FOUND. REPLACED NR 1 ENGINE OIL SCAVENGE VALVE AND OIL PRESSURE TRANSMITTER FOR PRESS FLUX.

Part: STRUCTURE — DELAMINATED (TE FLAPS) · airframe 55,210 hrs · 15,969 cycles

RETURNED TO ORD AND CANCELLED DUE TO FLAP DELAMINATION. MAJOR REPAIR ACCOMPLISHED. DETECTED FAILURE OF NR 6 LE SLAT. TE WEDGE REMOVED FOR INSPECTION. INSPECTED LH HORIZ STAB L.E. AND WING UPPER SURFACE AFT OF SLAT TO VERIFY NO DAMAGE TO THE LE HORIZONTAL STABILIZER. INSTALLED A NEW NR 6 SLAT. FIXED WING LE PANEL DIRECTLY AFT OF NR 7 SLAT HAS TWO AREAS OF DELAM MEASURING APPROX 8X8 AND 10X10. MOST LIKELY CAUSED BY SLAT FAILURE.ACCOMPLISHED OVERLAY REPAIR. LT WING TE FLAP HAS ONE SMALL DENT- PUNCTURE IN LOWER SURFACE APPROX. 6 INCHES IN FROM THE INBD. EDGE AND 7 INCHES IN FROM THE TE FOUND HONEYCOMB EXPOSED BUT NOT PUNCTURED. ACCOMPLISHED THE NECESSARY REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 53,676 hrs · 15,541 cycles

LEFT SIDE OF FUSELAGE FWD OF NR 2 MAIN ENTRY DOOR HAS A PUNCTURE & DENT.

Part: SKIN — DAMAGED (BS 600-620) · airframe 53,676 hrs · 15,541 cycles

THREE AREAS OF DAMAGE FOUND FROM STATIONS 600 TO 620 ON LEFT SIDE BETWEEN STRINGERS 15L AND 20L. CAUSE OF DAMAGE - AIRCRAFT IMPACTED BY JETWAY AT DOOR 2L. SKIN AND FRAME DAMAGE WERE CUT OUT AND DOUBLERS INSTALLED PER EVA-60167 AND EVA-60176.

Part: COMPUTER — FAILED (EICAS) · airframe 52,797 hrs · 15,294 cycles

RETURNED TO LAX DUE TO FAILED LEFT EICAS COMPUTER. THE LEFT EICAS COMPUTER WAS REPLACED AND THE FLIGHT DEPARTED. THE SHOP TESTED THE UNIT AND FOUND NO FAULT.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,381 hrs · 15,167 cycles

CABIN FLOORBEAM CRACKED UPPER FLANGE FWD SIDE, LBL 26.

Part: CONNECTOR — CONTAMINATED (RT ENGINE) · airframe 44,902 hrs · 13,036 cycles

RIGHT ENG PRI CONT AND AUTO THROTTLE EICAS STATUS MESSAGE. AFTER TROUBLESHOOTING THE ENTIRE WIRING SYSTEM, A SMALL WIRE-LIKE FILAMENT WAS FOUND CROSSED BETWEEN TWO PINS INSIDE AN EEC CONNTECTOR. UPON CLEANING THE CONNECTOR AND RE-POSITIONING THE PINS, TESTS WERE OK. EEC REMOVED AND SENT TO THE SHOP FOR TESTING. NO FAILURE RESULTS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,925 hrs · 11,977 cycles

STATION 1640, RBL 57 FLOORBEAM UPPER CAP CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIR ANGLE INSTALLED.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 40,925 hrs · 11,977 cycles

CABIN CREASE BEAM HAS CORROSION AT STATION 324 RBL 62. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPLACED INBOARD CREASE BEAM CHORD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,925 hrs · 11,977 cycles

FLOORBEAM UPPER T-CAP HAD EXCESS MATERIAL REMOVED DURING CORROSION CLEAN UP AT STA 365, RBL 42 AT STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR WITH TWO STRAPS UNDER FWD CAP AND TWO J-ANGLE PLATES ON AFT SIDE.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 40,925 hrs · 11,977 cycles

CABIN FLOOR SUPPORT CHANNEL HAS CORROSION STATION 310 TO STATION 324 RBL 41. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT CHANNEL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,925 hrs · 11,977 cycles

CABIN FLOORBEAM UPPER CHORD IS CORRODED BS 324, RBL 61, WL 208. MAJOR REPAIR ACCOMPLISHED. SPLICED CABIN FLOORBEAM UPPER CHORD.

Part: SHEAR TIE — CRACKED · airframe 40,925 hrs · 11,977 cycles

SHEAR TIE AT FRAME STATION 1560 BETWEEN STRINGER 25L AND 26L IS CRACKED IN RADIUS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE.

Part: WEB — CRACKED (FUSELAGE) · airframe 40,925 hrs · 11,977 cycles

RIGHT SIDE COCKPIT FLOOR WEB CRACKED THROUGH FASTENER HOLE STATION 210 ADJACENT TO SKIN ATTACH FLANGE. MAJOR REPAIR ACCOMPLISHED. FLOOR WEB REPLACED.

Part: FRAME — GOUGED · airframe 40,925 hrs · 11,977 cycles

STRAP AT ENTRY DOOR CUTOUT 1L EXTERIOR AT UPPER HINGE CUTOUT STATION 331. STRINGER 21L HAD GOUGE THAT EXCEEDED MATERIAL REMOVAL LIMIT. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.STRAP REPAIR INSTALLED.

Part: FRAME — CORRODED · airframe 40,925 hrs · 11,977 cycles

FRAME IN AT PIT AREA AT STATION 1480 HAD EXCESS MATERIAL REMOVED DURING CORROSION CLEANUP AND BETWEEN STRINGER 26R AND 27R AREA EFFECTED WAS UPPER INNER FLANGE OF FRAME. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR UNDER INNER FLANGE.

Part: CREASE BEAM — CORRODED · airframe 40,925 hrs · 11,977 cycles

CABIN RIGHT HAND CREASE BEAM WEB CORRODED AT OUTER CHORD AT BODY STATION 966 RBL 68". SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM.

Part: WEB — CORRODED · airframe 40,925 hrs · 11,977 cycles

CABIN, L.H. CREASE BEAM WEB AT STATION 996 TO 1020 HAD EXCESSIVE CORROSION ON UPPER SURFACE AT STRINGER 17R. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.MANUFACTURED AND INSTALLED WEB.

Part: WEB — CRACKED · airframe 40,925 hrs · 11,977 cycles

CABIN FLOOR SUPPORT INTERCOSTAL WEB CRACKED IN RADIUS ON FORWARD END STATION 661 LBL 44" STRINGER 17L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REMOVED AND INSTALLED NEW WEB.

Part: FASTENER — ELONGATED · airframe 40,925 hrs · 11,977 cycles

CABIN FLOOR SEAT TRACK FLANGE FASTENER HOLE FOR FLOOR BOARD ON INBD SIDE OF FLANGE ELONGATED LOCATED AT STA.572 LBL 44. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. L-ANGLE AND STRAP INSTALLED.

Part: FRAME — CORRODED · airframe 40,925 hrs · 11,977 cycles

FUSELAGE FRAME IN AFT PIT STATION 1500 UNDER FLOOR STRUCTURE BETWEEN RBL 3" AND 16" RBL HAD EXCESS MATERIAL REMOVED FROM UPPER FLANGE DURING CORROSION CLEAN-UP. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED STRAP.

Part: ACTUATOR — FAILED (RT MLG WW) · airframe 35,233 hrs · 10,410 cycles

AIRCRAFT ARRIVED AT GATE WITH RIGHT MLG WHEEL WELL DOOR IN OPEN POSITION AND A HYDRAULIC LEAK IN THE SAME WHEEL WELL. GEAR DOOR EICAS MESSAGE ILLUMINATED. *S/D* DOOR RELEASE INTERLOCK ACTUATOR FAILED. REPLACED ACTUATOR.

Part: ANTENNA — DEFECTIVE (VOR SYSTEM)

COPILOTS VARIABLE OMNI RANGE WILL NOT TEST. *S/D* THE VOR ANTENNA WAS FOUND DEFECTIVE. THE VOR ANTENNA WAS REPLACED.

Part: HOSE — RUPTURED (HYD SYSTEM) · airframe 31,191 hrs · 9,345 cycles

LANDED IN DEN UNDER AMBER ALERT DUE TO HYDRAULIC SYSTEM FAILURE. *S/D* AIRCRAFT EXPERIENCED A COMPLETE LEFT SYSTEM HYDRAULIC LOSS WHEN THE RT MLG PRESSURE HOSE FOR THE UPLOCK ACTUATOR RUPTURED. REPLACED HOSE.

Part: ACTUATOR — MALFUNCTIONED (SPOILER)

RETURNED TO FIELD AT LAX DUE TO FLOATING SPOILER PROBLEM. *S/D* CAUSE OF SPOILER EICAS MESSAGE WAS NOT FOUND AND COULD NOT BE DUPLICATED DURING TROUBLESHOOTING. SPOILER FLOAT WAS NOT VERIFIED. ALL OPERATIONAL AND VISUAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: AIR COMPRESSOR — FAILED (GALLEY)

RETURNED TO LAX DUE TO VIBRATION UNDER AFT GALLEY. *S/D* POTABLE WATER SYSTEM ELECTRIC AIR COMPRESSOR FAILED. COMPRESSOR WAS REPLACED AND AN OPERATIONAL CHECK WAS PERFORMED. COMPRESSOR CHECKED OUT OK.

Part: WIRE — LOOSE (CABIN)

EEL LIGHT STRIP IN FRONT OF FIRST CLASS CLOSET DOES NOT TEST. REINSTALLED END CAP WITH POWER SUPPLY CABLE THAT WAS KICKED LOOSE FROM STRIP.

Part: STRAP — MISSING (SLIDE RAFT)

DOOR 2-RIGHT D-RING SLIDE RAFT RESTRAINING STRAP MISSING. *S/D* D-RING AT THE END OF THE RESTRAINT STRAP ON SLIDE RAFT WAS FOUND MISSING. ENTIRE RESTRAINT STRAP ASSEMBLY WAS REPLACED.

Part: TUBE — RUPTURED (SLIDE RAFT)

THE LOWER TUBE RUPTURED AND FAILED ON A SLIDE RAFT DURING OVER-PRESSURE TESTING. THIS FAILURE OCCURRED AT THE RIGHT FORWARD SUPPLEMENTAL TUBE BULK HEAD SEAM. THE SLIDE RAFT WAS DISCARDED.

Part: DOOR WARNING — ACTIVATED (COCKPIT)

DOOR WARNING EICAS MESSAGES ACCESS DOORS, ENTRY DOORS, AND OVERHEAD LIGHT APPEARED DURING CRUISE. AS THE EICAS APPEARED THE AIRCRAFT YAWED SLIGHTLY. PRESSURIZATION REMAINED NORMAL. FUNCTIONAL CHECK OF THE DOOR INDICATION SYSTEM DID NOT SHOW ANY FINDINGS. CHECK OF THE YAW DAMPER SYSTEM WAS NORMAL.