N589UA

Part: COFFEEMAKER — LEAKING (GALLEY) · airframe 82,527 hrs · 21,209 cycles

WATER LEAKING FROM MID GALLEY COFFEE MAKER. WOULD NOT STOP WITH SHUTOFF VALVE IN OFF REPLACED COFFEE REPLACED COFFEE MAKER.OPS GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1118399 SN OFF 0340 COFFEEMAKER, IN OFF 31-2534-9-0001 0340 ON 31-2534-9-0001 1504

Part: SPRING — DIRTY (R2 DOOR) · airframe 81,657 hrs · 21,039 cycles

DOOR-MOUNTED ESCAPE SYSTEM DOOR 2R - A EVACUATION SLIDE PROBLEM WAS ENCOUNTERED WHICH IS NOT COVERED IN THE FAULT CODE DIAGRAMS SLIDE PLACARD 2R STAYS FLUSH WITH DOOR WHEN ARMED. SLIDE LIGHT ON GIRT BAR ENGAGED FOUND DOOR ARMED IDENTIFIER SPRING DIRTY WITH DEBRIS, CLEANED AND LUBED, DOOR ARMS AND DISARMS NORMAL, LIGHT WORKS NORMAL AND GIRT BAR ENGAGES NORMAL. OPS CHECKED NORMAL.

Part: UNKNOWN — MALFUNCTIONED (R2 DOOR) · airframe 81,572 hrs · 21,022 cycles

DOOR-MOUNTED ESCAPE SYSTEM DOOR 2R - A EVACUATION SLIDE PROBLEM WAS ENCOUNTERED WHICH IS NOT COVERED IN THE FAULT CODE DIAGRAMS KNUCKLE KNOCKER IS STICKING IN THE RETRACTED POSITION WHEN DOOR IS ARMED. OPS CHECKED DOOR 2R KNUCKLE KNOCKER. COULD NOT DUPLICATE ANY STICKING KNOCKER EXTENDS AND RETRACTS WHEN ARMING AND DISARMING. OPS CHECK GOOD.

Part: SEAL — MISSING (TE FLAP) · airframe 80,519 hrs · 20,814 cycles

PDA 2. REF L/P 3347020, SEAL FROM LT O/B FLAP I/B SEAL MISSING. REF IPC 57-53-10-51 ITEM 100. SEAL REPLACED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 79,820 hrs · 20,681 cycles

FUSELAGE EXTERIOR SKIN APU AIR INLET DOOR AFT LOWER CORNER HAS EVIDENCE OD DELAMINATION REF AAR N/R 9888901 CUT OUT DAMAGED AREA AT STA 1825 FABRICATED AND INSTALLED REPAIR DOUBLER AND STRAP PER REF SRM 53-80-15 REPAIR 1 REMOVED AND REPLACED ANGLES AT STR 3R AND STR 6R AND STRAP AT STA 1787.45 REF DWG 148N3105 AND SRM 51-40-2.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 79,820 hrs · 20,681 cycles

FUSELAGE BODY FAIRING SUPPORT BRACKET HAS 1IN CRACK AT BS 1300 STR 21L REF N/R 9889215 CUTOUT DAMAGED AREA FABRICATED AND INSTALLED REPAIR PARTS REF SRM 53-60-71 FIG 201.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 79,820 hrs · 20,681 cycles

AFT LOWER LOBE INTERNAL AREA WASTE TANK SERVICE PANEL BOX TOP AFT I/B RIB HAS EVIDENCE OF SURFACE CORROSION REF N/R 9889039 INSTALLED A NEW PANEL BOX TOP AFT I/B RIB PREVIOUSLY REMOVED SINCE IT HAD EVIDENCE OF CORROSION REF SRM 51-40-02 AND DWG 146N3650.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 79,820 hrs · 20,681 cycles

(B757-53-3-6620) FUSELAGE BODY FAIRING SUPPORT BRACKET HAS 1" CRACK AT BS 1300 STR 25L (51-006). REF NR 9889216. CUTOUT CRACK DAMAGE AND FABRICATED REPAIR ANGLE AT FAIRING SUPPORT BRACKET ON STA 1300 STR 25L IN REF SRM 53-60-71. REF NR 9889216.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 79,820 hrs · 20,681 cycles

(B757-53-3-6620) 1" CRACK ON FUSELAGE BODY FAIRING SUPPORT BRACKET AT BS 1300 STR 21R (51-004). REF AAR NR 9889214 CUT OUT CRACK DAMAGED AND INSTALLED ANGLE REPAIR AT FAIRING SUPPORT BRACKET ON BS 1300 STR 21R IN REF SRM 53-60-71. REF NR 9889214.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 79,820 hrs · 20,681 cycles

(B757-53-3-6620) FUSELAGE BODY FAIRING SUPPORT BRACKET HAS 1" CRACK AT BS 1300 STR 25R (51-003). REF NR 9889213. CUT OUT CRACK DAMAGE AREA AND FABRICATED REPAIR ANGLE AT FAIRING SUPPORT BRACKET AT BS 1300 STR 25R REF SRM 53-60-71 AND INSTALLED. REF NR 9889213.

Part: SLIDER — LACK OF LUBE (L2 GIRT BAR) · airframe 76,537 hrs · 20,053 cycles

ARM/DISARM LEVER FOR THE L2 DOOR IS VERY DIFFICULT TO MOVE. LUBRICATED THE L2 DOOR GIRT BAR SLIDER FITTINGS IAW AMM 12-21-99 -640-801C1. LEVER MOVES SMOOTHLY.

Part: LINE — KINKED (STANDBY AIRSPEED) · airframe 75,987 hrs · 19,950 cycles

STANDBY AIRSPEED INDCATOR STUCK ON ZERO, DURING TAKEOFF. REJECT AT ABOUT 105KTS. REMOVED THE STANDBY AIRSPEED INDICATOR IAW AMM 34-13-05-004-004. FOUND KINKED PITOT LINE BEHIND INSTRUMENT PANEL. BOTH NEW & OLD INDICATORS ARE IN COCKPIT. REMOVED THE FLEX LINE AND INSTALLED A NEW FLEX LINE IAW AMM 20-10-10. PERFORMED A LOW RANGE LEAK TEST IAW AMM 34-11-00/501. NO LEAKS NOTED. INSPECTED LOW RANGE LEAK TEST AND FOUND IT TO BE IN COMPIANCE WITH AMM 34-11-00/501. REMOVED AND REPLACED STANDBY AIRSPEED INDICATOR IAW AMM 34-13-05. OPS AND LEAK CHECKED GOOD.

Part: STRAP — BROKEN (L1 DOOR SLIDE) · airframe 75,402 hrs · 19,837 cycles

THE ORANGE SLIDE ARMED STRAP ON THE L1 DOOR IS BROKEN. REPLACED THE STRAP

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 75,350 hrs · 19,827 cycles

R1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. SECURED A LOOSE CONNECTOR. CHECKED OK.

Part: TARGET — FAULTY (L2 DOOR) · airframe 75,236 hrs · 19,806 cycles

2L SLIDE LIGHT WENT OUT IN FLIGHT. R&R GIRT BAR ACTUATOR TARGET OPS CHECK NORMAL PER AMM 25-66-11.

Part: SLIDE — LOW PRESSURE (R4 DOOR) · airframe 75,215 hrs · 19,802 cycles

R4 DOOR SLIDE GUAGE IN THE RED. REMOVED AND REPLACED SLIDE IAW AMM 25-66-00, OPS CHECKED GOOD.

Part: PROXIMITY SENSOR — DIRTY (L2 DOOR) · airframe 75,174 hrs · 19,794 cycles

SLIDE LIGHT INOP AT DOOR 2L. CLEANED GIRT BAR PROX SENSORS, SLIDE LIGHT WORKED NORMALLY AT 2L WHEN ARMED OR DIS-ARMED

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 75,127 hrs · 19,785 cycles

L1 DOOR EMERGENCY GROUND SERVICE LIGHT INOPERATIVE. REPLACED THE EMERGENCY LIGHT LAMP. OPS CHECKED GOOD.

Part: SENSOR — DIRTY (L2 DOOR SLIDE) · airframe 75,022 hrs · 19,764 cycles

L2 SLIDE OFF LGHT NOT ON WHEN DOOR ARMED. WHEN DISARMING DOOR, THE LIGHT FLASHED AND THEN STAYED ON. CLEANED DEBRIS FROM DOOR SLIDE ARM SENSOR, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (DOOR SLIDE IND) · airframe 75,022 hrs · 19,764 cycles

L1 DOOR SLIDE ARM LIGHT DOES NOT COME ON WHEN DOOR IS ARMED. REMOVED AND REPLACED THE BULBS IN THE L1 DOOR SLIDE LIGHT. OPS CHECKED GOOD

Part: TARGET — DIRTY (L2 DOOR SLIDE) · airframe 75,022 hrs · 19,764 cycles

L2 DOOR SLIDE LIGHT WILL NOT SHOW ARMED. THE ARMED LIGHT FLICKER ON AND THEN GOES OUT. CLEANED THE TARGET. OPS CHECKED GOOD. OK TO CONTINUE.

Part: SLIDE — OBSTRUCTED (L2 DOOR) · airframe 75,022 hrs · 19,764 cycles

L2 DOOR UNABLE TO ARM, MX REPOSITIONED EXCESS FLAP HANGING FROM UNDER SLIDE PACK AT THE L2 DOOR AND ENTRY DOOR CLOSES AND ARM & DISARM NORMALLY. OPS CHECKED GOOD.

Part: WARNING LIGHT — EXTINGUISHED (L2 DOOR SLIDE) · airframe 75,022 hrs · 19,764 cycles

AFTER TAKEOFF, THE L2 DOOR SLIDE ARM LIGHT WENT OUT. RAN DOOR THROUGH SEVERAL 'ARM & DISARM CYCLES, OPS CHECKED GOOD

Part: SWITCH — OUT OF ADJUST (L2 GIRT BAR) · airframe 75,022 hrs · 19,764 cycles

AFTER TAKEOFF, THE L2 DOOR SLIDE LIGHT WENT OUT FOR SEVERAL MINUTES AND CAME ON AND STAYED ON. ADJUSTED L2 DOOR GIRT BAR PROXIMITY SWITCH. NOW OPS NORMAL IAW MM 25-66-11-822-011.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 74,809 hrs · 19,722 cycles

TRAILING EDGE FLAP SYSTEM EICAS MESSAGE TE FLAP DISAGREE WHEN TE FLAP POSITION SELECTED. FLAPS FAILED TO MOVE TO SELECTED POSIT ION TE FLAPS DISAGREE ON FINAL. LANDED FLAPS 20 USING ALTERNATE FLAPS. EMERGENCY DECLARED. ON INITIAL VISIT TO COCKPIT FOUND NO EICAS MESSAGE PERFORMED TEST OF TE FLAP SYS TASK 27-51-00-715-001 AND PERFORMED FSEU (-1,-2) BITE TEST , FOUND FLAP LD RELIEF MESSAGE WHICH IS NORMAL OPERATION WHEN MET WITH EXTREME AIR LOADS. FLAP TE FLAP SYS IS GOOD ALL CHECKS PASSED.

Part: SWITCH — OBSTRUCTED (R1 DOOR) · airframe 73,343 hrs · 19,438 cycles

1R DOOR SLIDE LIGHT INOP. REMOVED DEBRIS AND CYCLED DOOR ARM SWITCH SEVERAL TIMES. ALL OPS ON DOOR LIGHT OK AT THIS TIME.

Part: LATCH — DIRTY (GIRT BAR) · airframe 73,204 hrs · 19,411 cycles

DOOR 2L WILL NOT ARM. CLEANED DOOR SLIDE AREA, CYCLED DOOR AND ARMED SEVERAL TIMES. NO DEFECTS NOTED, OK TO CONTINUE.

Part: FRAME — GOUGED (BS 1520) · airframe 72,779 hrs · 19,327 cycles

SCREW GOUGING J SECTION OF FRAME AT BS 1520 AND STRINGER 26R. FOUND TO BE OUT OF LIMITS IAW SRM 53 -00-07, FIG 101, SHT 1-4. PERFORMED REPAIR ON FRAME IAW SRM 53-00-07, REPAIR 5, FIG 201, DETAIL 1.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 71,678 hrs · 19,113 cycles

ELECTRIC BURNING ODOR NEAR OVERWING EXIT. DISSIPATED RAPIDLY. FOUND EMERGENCY EXIT LEFT SIDE SIDE WALL LIGHTS BLACK AT THE END. REPLACED LT EMERGENCY EXIT SIDE WALL LIGHTS IAS AMM 33-21-30

Part: CARBON SEAL — NOT REPORTED (RT ENGINE) · airframe 69,778 hrs · 18,740 cycles

RIGHT ENG SHUTDOWN ON TAXI OUT. NR 2 ENG EEC STATOR, ROTOR & PMA CARBON SEAL REPLACED. RAN ENG IAW AMM 71-00-59 TABLE V & TEST 3. OPERATIONS CHECKED OK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 69,679 hrs · 18,721 cycles

EXTERIOR EMER EXIT LIGHT AFT OF DOOR 3 RT INOPERATIVE. RELAMPED & OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 69,679 hrs · 18,721 cycles

EXTERIOR EMER EXIT LIGHT AFT OF DOOR 2 LT INOPERATIVE. RELAMPED & OPERATIONS CHECKED NORMAL.

Part: DOUBLER — DAMAGED (L2 DOOR) · airframe 68,929 hrs · 18,575 cycles

L2 REPAIR DOUBLER AT UPPER HINGE CUT OUT DAMAGED. REMOVED EXISTING DAMAGED DOUBLER, AT UPPER HINGE CUT OUT ON FWD FRAME. FORMED A REPAIR ANGLE & INSTALLED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,411 hrs · 18,089 cycles

CORROSION AT AFT CARGO COMPARTMENT FRAME AT BS 1460, STRINGER 25R. R & R FRAME AT BS 1460, STRINGER 25R IAW SRM 51-40-02 PAR 7 FIG 12.

Part: UNKNOWN — MALFUNCTIONED (L1 DOOR) · airframe 62,530 hrs · 17,348 cycles

DOOR 1L WILL NOT ARM, RESET DOOR & CHECKED OK.

Part: COVER — MISSING (L4 DOOR) · airframe 62,353 hrs · 17,315 cycles

4L CABIN ENTRY DOOR FWD GIRT BAR SWITCH SENSOR COVER MISSING. ACP INTERIM SWITCH COVER IAW ECRA 2566-01098.

Part: COVER — UNSECURE (L3 DOOR) · airframe 61,907 hrs · 17,230 cycles

PART DETACHED FROM DOOR 3L, 3L SENSOR TARGET BROKE OFF. SECURED GIRT BAR TARGET COVER WITH ADHESIVE BOND.

Part: SHAFT — FAULTY (R4 DOOR) · airframe 61,838 hrs · 17,217 cycles

AT DOOR 4R UNABLE TO OPEN OR CLOSE DOOR USING OUTSIDE HANDLE. REPLACED SHAFT ITEM 110 SPRING ITEM 120 DEPRESSOR ITEM 125 & COLLAR CLUTCH ITEM 105 IPC IAW 52-11-13-001D, IAW AMM 52-11-13. OPERATIONS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (HYDRAULIC SYS) · airframe 61,652 hrs · 17,181 cycles

LT HYD SYSTEM MESSAGE, FLIGHT DIVERTED. PULLED HYD PAGE ON EICAS & NOTICED LT SYSTEM PRESS 1810 PSI QUANTITY NORMAL, JUST PRESS. RAN ENG ISOLATED LT ENG DRIVEN PUMP ALL INDICATES NORMAL 3000 PSI. REPLACED LT HYD PRESSURE TRANSMITTER IAW AMM, PRECAUTIONARY. OPERATIONS CHECKED NORMAL, NO LEAKS, ALL INDICATES NORMAL.

Part: CONTROLLER — INOPERATIVE (TEMP CONTROL) · airframe 61,572 hrs · 17,165 cycles

COMPARTMENT TEMP INOPERATIVE LIGHT ALL 3. REPLACED ZONE TEMP CONTROLLER & OPERATIONS CHECKED GOOD.

Part: FITTING — LACK OF LUBE (L4 DOOR) · airframe 61,540 hrs · 17,159 cycles

4L STILL STICKING WHEN ARMING. REMOVED MED 4L SLIDE PACK & LUBED ALL FITTINGS IAW AMM 52-11-20. RE-INSTALLED SAME SLIDE PACK. ARM DIS-ARM FUNCTION CHECKED NORMAL. SLIDE PACK R & R IAW AMM.

Part: HOUR METER — FAULTY (APU) · airframe 61,502 hrs · 17,152 cycles

APU HOC ADVISORY. REPLACED APU HOUR METER IAW AMM, OPERATIONS CHECKED OKAY.

Part: UNKNOWN — MALFUNCTIONED (COMM SYSTEM) · airframe 61,502 hrs · 17,152 cycles

FIRST OFFICER COMM PANEL HAS FEEDBACK & SQUEAL. ACCOMPLISHED CHECK OF COMM PANEL, FOUND NO ABNORMALITIES. SYSTEMS OPERATIONS CHECKED OKAY.

Part: GIRT BAR — DIRTY (L4 DOOR) · airframe 61,258 hrs · 17,105 cycles

L4 DOOR SLIDE ARM LIGHT INTERMITTENT. DOOR GIRT BARS TRAVEL GOOD. CLEANED AND LUBED GIRT BAR FLOOR FITTINGS.

Part: COVER — BROKEN (ESCAPE ROPE) · airframe 61,153 hrs · 17,084 cycles

EMERGENCY ESCAPE ROPE COVER OVER CAP SIDE BROKEN. FIXED & REINSTALLED ESCAPE ROPE COVER.

Part: STRIP — TORN (R1 DOOR) · airframe 61,050 hrs · 17,063 cycles

R1 DOOR BUSSEL FOR SLIDE HAS RUBBER STRIP ON LOWER EDGE OF BUSSEL TORN LOOSE.

Part: WARNING MESSAGE — ILLUMINATED (RT ENGINE) · airframe 60,928 hrs · 17,038 cycles

RIGHT ENGINE SEC CONT STATUS MESSAGE.

Part: WINDOW SHADE — BROKEN (SEAT 7 A) · airframe 60,628 hrs · 16,975 cycles

7A WINDOW SHADE ASSY BROKEN.

Part: CAM — OUT OF ADJUST (L1 DOOR HANDLE) · airframe 60,560 hrs · 16,958 cycles

L1 DOOR HANDLE MOVED UP IN FLIGHT, UP TO DOOR ARM WEDGE. TROUBLESHOT IAW AMM 52-11-00, ADJUSTED UPPER FWD LATCH CAM IAW AMM 52-11-00-401. OPS CHECKED OK.

Part: WIRE — MISINSTALLED (BUSS) · airframe 60,554 hrs · 16,955 cycles

UTILITY BUSS SWITCH FAILED TO TURN OFF UTILITY BUSS, UTIL BUSS OFF DID NOT DISPLAY OR OFF LIGHT ILLUMINATE. FOUND WIRES ON CIRCUIT BREAKER C9042 GOING TO GALLEY G2B RED AND BLUE IN WRONG POSITION AND WIRES ON TERMINAL BLOCK TB5031 TO CIRCUIT BREAKER C9041 RED AND BLUE IN WRONG POSITION, CORRECTED WIRING IAW WDM 24-21-14 AND DWG NR B11630 1-001, UTLITY BUSS AND LT BUSS, OPS CHECKED GOOD.

Part: GROUND WIRE — UNSECURE (EMERGENCY LIGHT) · airframe 60,551 hrs · 16,954 cycles

EMERGENCY TEST LIGHT SWITCH ABOVE DOOR NR 1 LT DOES NOT WORK. FOUND GROUND WIRE AT STUD GD1420D NOT SECURED. SECURED WIRE AND SWITCH TESTED GOOD.

Part: PANEL — OUT OF POSITION (SLIDE) · airframe 60,551 hrs · 16,954 cycles

P61 SQUIB TEST PANEL, ON TEST NR 1 EMERGENCY ESCAPE LIGHT BOTH LT AND RT FAILED TEST, TEST NR 2 TESTED OK. FOUND OVERWING EMERGENCY EXIT HATCH DISABLE PANEL P78 INSTALLED IN PLACE OF P79 SO DISABLE HANDLE INDICATED ARMED WHEN DISARMED. REINSTALLED P78 AND P79 TO CORRECT SIDES IAW 25-65-00 PG 109. FINAL SQUIB TEST SATISFACTORY.

Part: WINDOW — OUT OF ADJUST (COCKPIT) · airframe 60,551 hrs · 16,954 cycles

CAPTAIN`S WINDOW WILL NOT CLOSE ALL THE WAY. ADJUSTED WINDOW ASSY.

Part: GCU — FAULTY (LEFT) · airframe 60,550 hrs · 16,953 cycles

LEFT AC BUSS INOPERATIVE LIGHT ON WITH LT UTILITY BUSS, BUSS POWER ON. LEFT GCU REPLACED IAW AMM, GROUND TESTED OK.

Part: SKIN — CRACKED (L2 DOOR) · airframe 60,545 hrs · 16,951 cycles

L2 DOOR UPPER HINGE CUTOUT CRACKED. R & R L2 DOOR UPPER HINGE CUTOUT REPAIR DOUBLER IAW ECRA5211-01345. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 60,545 hrs · 16,951 cycles

FLOORBEAM BS 365 IS CORRODED FOR BL 0 TO RBL 60. REPAIRED FLOORBEAM LBL 12 TO RBL 70 IAW ECRA 5310-0536. MAJOR REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,545 hrs · 16,951 cycles

CLASS "B" REPAIR INSTALLED FUS STA 1707 BETWEEN STR 22L & 23L. REPAIR INSTALLED IAW SRM 53-00-01, FIG 201 REP 3.

Part: WEDGE — DENTED (NR 5 SLAT) · airframe 60,545 hrs · 16,951 cycles

NR 5 SLAT DENTED ON UPPER SURFACE T/E WEDGE. REPAIRED WEDGE BY FABRICATING FILLER DOUBLER AND CORE SECTION IAW SRM 57-43-02 AND 51-70-10 WORK PERFORMED.

Part: SKIN — DENTED (BS 1707) · airframe 60,545 hrs · 16,951 cycles

LOWER AFT SKIN DENTED BS 1707 BETWEEN S22-23L. INSTALLED REPAIR DOUBLER IAW SRM 53-00-10 FIG 201 REPAIR 3. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 60,545 hrs · 16,951 cycles

CORROSION ON AFT CABIN FLOORBEAM AT BS 1640, RBL 52. REPLACED FLOORBEAM UPPER TEE LBL10 TO RBL 72 IAW ECRA 5365-01076 NDT INSPECTION IAW NTM PART6 51-00-16. NO DEFECTS NOTED. MAJOR REPAIR.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,545 hrs · 16,951 cycles

CORROSION ON L4 DOOR BELOW SILL PLATE AROUND SEVEN NUT PLATES, FOUND OUT OF LIMITS. R & R SILL PLATE IAW SRM 51-40-02, PARA 4 &7, FIG 3, 8 & 12.

Part: INTERCOSTAL — MISINSTALLED (BS 1640-1660) · airframe 60,545 hrs · 16,951 cycles

BS 1640-1660, RBL 37 INTERCOSTAL, HAS LESS THAN MINIMUM ED ON HOLES. FABRICATED INTERCOSTAL, SHIM AND INSTALLED IAW ECRA 5365-01075. MAJOR REPAIR

Part: NOSE COWL — DENTED (NR 2 NACELLE) · airframe 60,545 hrs · 16,951 cycles

NR 2 ENGINE NOSE COWL L/E HAS A DENT APPROXIMATELY ONE O'CLOCK POSITION. INSTALLED DOUBLER REPAIR ON NOSE COWL L/E IAW SRM 54-11-01, FIG 201, REPAIR 1. MAJOR REPAIR.

Part: ATTACH FITTING — CORRODED (BS 365) · corrosion level 2 · airframe 60,545 hrs · 16,951 cycles

SEAT TRACK ATTACH PLATE AT BS 365 RBL 25 IS CORRODED. REMOVED CORROSION, FOUND OUT OF LIMITS. FABRICATED, TREATED AND PRIMED NEW DOUBLER IAW US MM 53-20-98, FIG 801.

Part: CHANNEL — CORRODED (BS 324-345) · corrosion level 2 · airframe 60,545 hrs · 16,951 cycles

CORROSION ON TOP SURFACE OF HAT CHANNEL AT R1 DOOR BS 324-345 RBL 60. CORROSION REMOVED IAW SRM 51-10-01, FIG 1. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04, FIG 101. REMOVED AND REPLACED HAT CHANNEL IAW SRM 51-40-02, FIG 12. MAJOR REPAIR.

Part: CHANNEL — CORRODED (BS 336) · airframe 60,545 hrs · 16,951 cycles

HAT CHANNEL AT RBL 34 BS 336 HAS CORROSION ON UPPER SURFACE. FABRICATED AND INSTALLED NEW HAT CHANNEL IAW SRM. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 60,527 hrs · 16,945 cycles

AFT CARGO FLOOR HAS A HOLE. FOUND HOLE ON RT SIDE FRAME, 10 FEET AFT OF CARGO DOOR. HOLE MEASURES 3-4 INCHES LONG BY 1-2 INCHES WIDE. PERFORMED INTERIM REPAIR REF PER GNMM 1-0-1-102.

Part: SMOKE DETECTOR — INOPERATIVE (FWD CARGO) · airframe 60,515 hrs · 16,941 cycles

EICAS STATUS MESSAGE FWD CARGO SMOKE DETECTOR NR 1. FWD CARGO NR 1 SMOKE DETECTOR INOPERATIVE. REPLACED NR 1 SMOKE DETECTOR.

Part: ANTENNA — FAILED (HF SYSTEM) · airframe 60,445 hrs · 16,921 cycles

LEFT HF INOPERATIVE. SWAP OF TRANSCEIVERS, NO HELP. INSTALLED BACK TO ORIGINAL POSITIONS. REPLACED LEFT HF COUPLER ANTENNA PER MM, OP CHECKED OK.

Part: ATTACH BRACKET — MISSING (OXYGEN BOTTLE) · airframe 60,354 hrs · 16,892 cycles

AFT GALLEY OXYGEN BOTTLE BRACKET LATCH MISSING. REPLACED BRACKET AND WALK AROUND O2 BOTTLE.

Part: LIGHT — DAMAGED (SEATS 11-12 ABC) · airframe 60,219 hrs · 16,848 cycles

EMERGENCY LIGHT SEATS 11-12 ABC RAISED & BOWED. SECURED LIGHT, OPS CHECKED NORMAL.

Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 60,197 hrs · 16,841 cycles

RIGHT REVERSER FILTER HOUSING LEAKING FROM TOP FRONT. LEAKS WHEN RIGHT SYSTEM PRESS WITH RIGHT REVERSER HANDLE DEPLOYED. REPLACED O-RINGS ON AFT DPI INDICATOR ON RIGHT ENG EDP CASE DRAIN, PRESS FILTER PRESS MODULE. OPERATIONAL AND LEAK CHECK GOOD.

Part: CONTROL PANEL — INTERMITTENT (NR 1 AUDIO) · airframe 60,153 hrs · 16,829 cycles

NR 1 COMM VOLUME INTERMITTENT ON CAPTAINS AUDIO PANEL. REPLACED CAPTAIN'S AUDIO CONTROL PANEL, CHECKED OKAY.

Part: LINE — UNSECURE (HYD SYSTEM) · airframe 60,143 hrs · 16,827 cycles

HYDRAULIC FLUID SMEAR AFT OF LEFT PACK EXHAUST DOOR TO TAIL. SECURED LOOSE HYDRAULIC LINE IN WHEEL WELL.

Part: COUPLER — UNKNOWN (LT HF) · airframe 60,093 hrs · 16,812 cycles

LEFT HF COUPLER REPLACED. OPS CHECK REQUIRED OUTSIDE OF HANGER. ACCOMPLISHED TEST AND TESTED OKAY.

Part: COUPLER — FAULTY (HF COMM) · airframe 60,079 hrs · 16,809 cycles

LEFT HF RADIO UNABLE TO TRANSMIT. REPLACED LEFT HF COUPLER PER MM, OPS CHECK GOOD. TUNE FREQUENCY 6.640 TOOK BETWEEN 4 AND 7 SECONDS. RADIO TRANSMISSION MADE ON TUNED FREQUENCY TRANSMIT & RECEIVE VOICE COMMUNICATION.

Part: B-NUT — UNSECURE (HYDRAULIC SYS) · airframe 60,088 hrs · 16,811 cycles

APU FIRE BOTTLE ACCESS PANEL HAS FLUID ALONG BOTTOM. SECURED 'B' NUTS ON ELEVATOR FEEL COMPUTER. CLEANED UP FLUID ON APU DOOR AND FIRE BOTTLE ACCESS PANEL.

Part: TRANSCEIVER — FAULTY (HF COMM) · airframe 60,078 hrs · 16,808 cycles

SWAPPED HF TRANSCEIVERS FOR TROUBLESHOOTING. SWAPPED HF TRANSCEIVER FOR TROUBLESHOOTING, MR NUMBERS MR23173-199 IN POSITION NR 2 AND MR23173-98 IN POSITION NR 1.

Part: TRANSCEIVER — FAULTY (HF COMM) · airframe 60,078 hrs · 16,809 cycles

LEFT HF RADIO FAULTY, FLIGHT DIVERTED. AIRBORNE CLIMBING THROUGH FL190 LEFT HF RADIO TOOK 17 SECONDS TO AUTOTUNE AND WOULD NOT TSMT. REPLACED LEFT TRANSCEIVER AND CALLED SFO ON 6.640 KHZ, OPS CHECK OK. COUPLER TUNED IN 11 SECONDS. ALL WITHIN TOLERANCE OF AMM. DUE TO PREVIOUS GRIPES TOMC REQUEST LEFT HF COUPLER REPLACEMENT. REPLACED LEFT HF COUPLER PER MM, LEFT HF OPS CHECK TEST GOOD.

Part: OXYGEN MASK — FAULTY (COCKPIT) · airframe 60,073 hrs · 16,807 cycles

F/O OXYGEN MASK MICROPHONE VOLUME INAUDIBLE OUT OF F/O COCKPIT SPEAKER. REPLACED F/O OXYGEN MASK PER AMM, CHECK'S OKAY.

Part: STOWAGE BOX — FAULTY (COCKPIT) · airframe 60,073 hrs · 16,807 cycles

F/O OXYGEN MASK EXHALE VALVE DOES NOT OPEN PROPERLY WHEN F/O BREATHES. REPLACED CREW OXYGEN STOWAGE BOX PER AMM, CHECK'S OK.

Part: JACK — MALFUNCTIONED (INTERPHONE SYS) · airframe 60,063 hrs · 16,805 cycles

STATIC ON FLT INT THRU BOTH CAPT & F/O HEADSETS. REPLACED FLT INTERPHONE JACK D0043 IAW SSM23-51-01.

Part: SWITCH — STUCK (WHEEL MICROPHONE) · airframe 60,056 hrs · 16,802 cycles

CAPTAIN'S CONTROL WHEEL MICROPHONE SWITCH IS STUCK IN TRANSMIT POSITION. REPLACED CAPTAIN'S CONTROL WHEEL MICROPHONE SWITCH, OP CHECKED GOOD.

Part: COVER — LOOSE (L2 GIRT BAR) · airframe 59,844 hrs · 16,745 cycles

L2 DOOR WILL NOT ARM. FOUND COVER FOR DOOR AFT GIRT BAR SWITCH LOOSE. ATTACHED LOOSE AFT GIRT BAR SWITCH COVER IAW ECRA 2520-06109, PER STEP 3.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 59,582 hrs · 16,671 cycles

DUE TO REPORTED ELECRICAL ODOR IN CABIN, SMOKE ODOR IN CABIN. FLIGHT ATTENDANT TURNED OFF SIDEWALL LIGHTS AND ODOR DISSIPATED AND IS NO LONGER PRESENT. REPLACED LIGHT BALLAST AT ROW 14 D, E, F PER AMM. FOUND EVIDENCE OF ARCING, BURNED TERMINAL ENDS AND SOME MELTING OF THE OUTER PLASTIC CASING ON ONE END OF BALLAST.

Part: LIGHT — LOOSE (ROWS 11 & 12 ABC) · airframe 59,508 hrs · 16,651 cycles

FLOOR EMERGENCY LIGHTS AT 11 & 12 ABC ARE LOOSE. OPERATION NORMAL.

Part: FEEDER CABLE — FAULTY (CABIN) · airframe 59,424 hrs · 16,630 cycles

EMERGENCY EXIT FLOOR LIGHT STRIP IS INOP IN FIRST CLASS. REPLACED FEEDER CABLE SIDEWALL BATTERY PACK TO EEL STRIP AT ROW 2AB, CKS OK.

Part: CONNECTOR — DIRTY (CARGO DETECTOR) · airframe 59,095 hrs · 16,552 cycles

FWD CARGO DET 1 STATUS MSG NO CLEAR :NO TIME. CLEANED CONNECTOR AT FWD DETECTOR AND OPS NW NORMAL.

Part: PILOT VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 58,913 hrs · 16,496 cycles

CHRONIC: ON FINAL APPROACH RT DUCT PRESS CYCLES FM 20-35 PSI, LT STEADY AT 42. REPLACED HIGH STAGE PILOT VALVE PER MM. RAN ENGINE, OPS CHECK GOOD.

Part: SWITCH — FAULTY (L1 DOOR) · airframe 58,918 hrs · 16,498 cycles

DOOR 1L SLIDE ARM LIGHT NOT COMPLETELY EXTINGUISHED WHEN DOOR NOT ARMED. REPLACED SLIDE LIGHT SWITCH FOR DOOR 1L, TESTED GOOD.

Part: COWLING — DENTED (RT ENGINE) · airframe 58,422 hrs · 16,364 cycles

CREW REPORT: ON PUSHBACK GRD CREW NOTICED RIGHT ENGINE COWL LEADING EDGE SMALL DENT AT 6 O'CLOCK POSITION NO DOT. FBO REPORTS DENT MEASURES 6 IN LONG BY 1.125 WIDE BY .040 DEEP. BEYOND LIMITS PER SRM 54-11-01 PG 104. INSPECTED WITH HFEC NO CRACKS NOTED. NOSE PN 314N3080-1 SER #000700.

Part: COVER — LOOSE (CABIN) · airframe 58,402 hrs · 16,357 cycles

THE 12C FLOOR EMERGENCY LIGHT STRIP IS LOOSE. SECURED CLEAR PLASTIC EEL TRACK COVER.

Part: OXYGEN SYSTEM — LOW PRESSURE (COCKPIT) · airframe 58,313 hrs · 16,329 cycles

COCKPIT OXYGEN QTY LOW NEEDS SERVICING. SERVICED COCKPIT O2.

Part: COVER — UNSECURE (CABIN) · airframe 58,303 hrs · 16,326 cycles

FLOOR EVAC LIGHT STICKING UP AT 12C. SECURED LOOSE COVER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,303 hrs · 16,326 cycles

LAVATORY LIGHTS INOP AT DOOR 3L AFT CABIN FWD LAV. RELAMPED, OPS CHECK GOOD.

Part: ENGINE — DAMAGED (NR 2) · airframe 58,121 hrs · 16,277 cycles

NR 2 ENGINE HAS A NICK AND IS SLIGHTLY BENT. REPAIRED PER 72-31-02.

Part: GENERATOR — FAILED (APU) · airframe 58,057 hrs · 16,260 cycles

30 MINS PRIOR TO DEPARTURE, APU WILL NOT PICK UP ELECTRICAL LOAD. REPLACED APU GENERATOR PER MM.

Part: CONTROL VALVE — FAULTY (STARTER) · airframe 57,998 hrs · 16,239 cycles

RIGHT ENG STARTER EICAS DURING RIGHT ENGINE START. RT REPLACED STARTER CONTROL VALVE, CHECKED OKAY.

Part: DETECTOR — FAULTED (CARGO BAY) · airframe 57,919 hrs · 16,219 cycles

FWD CARGO DET 1 AND 2 BOTH LOOPS SHOW FAULT, CYC BREAKERS. NO MESSAGE .

Part: COVER — MISSING (WINDOW HANDLE) · airframe 57,860 hrs · 16,201 cycles

AT DEPARTURE, CAPTAIN REPORTED SLIDING WINDOW UNDERNEATH THE LOCK HANDLE TRACK COVER MISSING. REPLACED MISSING LOCK HANDLE TRACK COVER.

Part: EEC — FAILED (LT ENGINE) · airframe 57,787 hrs · 16,176 cycles

LEFT ENG THRUST REVERSER AND LT ENGINE SEC STATUS MESSAGE ON DESCENT. REPLACED LT ENGINE EEC AND ENGINE CONTROL HARNESS. ENGINE PARAMETERS NORMAL, NO FAULTS OR MESSAGE, REACTIVATED THRUST REVERSER, OP'S CHECKED NORMAL, NO FAULTS NOTED.

Part: CHILLER — NOISY (GALLEY) · airframe 57,689 hrs · 16,148 cycles

FLIGHT ATTENDANT AND PAX REPORTED NOISE COMING FROM OUTSIDE OF R1 DOOR TO SEAT 2B ON DESCENT. ODD NOISE WAS INTERMITTENT. MOST OF THE TIME CHILLER SOUNDED FINE THEN STARTED TO SOUND LIKE A HELICOPTER. REPLACED CHILLER, OP CHECKED GOOD.

Part: HANDSET — INTERMITTENT (INTERPHONE) · airframe 57,648 hrs · 16,137 cycles

FWD FLIGHT ATTENDANT HANDSET INTERMITTENT WHEN TRYING TO CALL COCKPIT AND SELECTING PA. REPLACED FLIGHT ATTENDANT HANDSET. RESTORED INTERPHONE SYSTEM OPERATIONAL .

Part: O-RING — LEAKING (NR 1 FMU) · airframe 57,596 hrs · 16,121 cycles

NR 1 ENGINE FMU LEAKING PROFUSELY AT BLUE END CAP. NOTED PACKING PROTRUDING. ORDERED NEW PACKING. RAN 5 MIN IDLE NO LEAKS NOTED. REPLACED LEAKING O-RING FUEL CONTROL WITH NEW.

Part: COUPLER — INOPERATIVE (HF RADIO SYS) · airframe 57,500 hrs · 16,098 cycles

NR 2 HF RADIO FREQUENCY DISPLAY INOPERATIVE. HF 2 COCKPIT BREAKER TRIPPED AND WOULD NOT RESET, REPLACED HF 2 ANTENNA COUPLER PER MM, OPS CHECKS OKAY.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 57,363 hrs · 16,060 cycles

EMERGENCY EXIT LIGHTS AT ROW 11 ARE LIFTING UP. REMOVED FORK FROM UNDER EEL LIGHT STRIP TRACK.

Part: CHILLER — SPARKS (GALLEY) · airframe 56,734 hrs · 15,872 cycles

GALLEY CHILLER HAS ELECTRICAL SPARKING AT GALLEY G4A. CHECKED ALL WIRING IN AND AROUND CHILLER, REMOVED CART CONTROLLERS AND CHECKED WIRING FOR ALL ARE GOOD. ALL WIRING FOR GALLEY CARTS INTACT. NO ODORS OR BURNED WIRING. REPLACED GALLEY AIR CHILLER PER MM. OPS CHECKED FOR 10 MINUTES, NORMAL

Part: CHILLER — SPARKS (GALLEY) · airframe 56,765 hrs · 15,881 cycles

GALLEY CHILLER HAS ELECTRICAL SPARKING AT GALLEY G4A. REPLACED GALLEY AIR CHILLER PER MM 25-33-98. OPS CHECKED FOR 10 MINS, NORMAL.

Part: ACTUATOR — FAULTY (SPAR VALVE) · airframe 56,724 hrs · 15,870 cycles

RT SPAR VALVE CAME ON DURING POWER TRANSFER -GRND TO APU. REPLACED RT SPAR VALVE ACTUATOR.

Part: LANYARD — LOOSE (R1 DOOR SLIDE) · airframe 56,707 hrs · 15,867 cycles

THE 1R WILL NOT ARM. FOUND RAFT LANYARD INTERFERING WITH GIRT MECHANISM. STOWED LANYARD. DOOR ARMS NORMALLY.

Part: GIRT BAR — DIRTY (R1 DOOR SLIDE) · airframe 56,689 hrs · 15,861 cycles

CANNOT ARM DOOR 1R. REMOVED DEBRIS IN THE AREA OF THE GIRT BAR, OPS CHECKED GOOD.

Part: LANYARD — LOOSE (R1 DOOR SLIDE) · airframe 56,635 hrs · 15,845 cycles

THE R1 DOOR ARM LEVER WON'T ENGAGE. OPENED DOOR. LANYARD HANGING DOWN FROM SLIDE PACK. STOWED LANYARD AND CLOSED AND ARMED DOOR.

Part: CONTROL UNIT — FAULTY (POSIT 1) · airframe 56,568 hrs · 15,823 cycles

CREW REPORTED AFTER TAKE OFF, RETURNED TO DEPARTURE. THE LEFT AND RIGHT UTILITY BUSSES DEPOWERED, AND WERE UNABLE TO RESET. FOUND REPLACE BPCU MESSAGE ON BPCU, REPLACED PER MM. RAN BOTH ENG PER JRH 2-5-5 AND BOTH UTILITY BUSSES RESET NORMAL.

Part: WIRE — FRAYED (COMM SYSTEM) · airframe 56,561 hrs · 15,821 cycles

CAPTAIN`S O2 MASK COMM WIRE FRAYED AT MASK. REPLACED CAPTAIN`S O2 MASK.

Part: SERVO VALVE — MALFUNCTIONED (YAW DAMPER) · airframe 56,506 hrs · 15,802 cycles

RIGHT YAW INOPERATIVE LIGHT ON DURING CLIMBOUT. SWITCH OFF PER CHECKLIST. ACCOMPLISHED YAW DAMPER SYSTEM BITE PER FIM, REF FIG 103A, SHEET 18, PG 123, BLOCK 130. REPLACED SERVO VALVE IAW MM.

Part: CLUTCH — FAILED (SPEED BRAKES) · airframe 56,517 hrs · 15,806 cycles

SPOILERS DEPLOY 1/2 WAY ON LANDING. FOUND BUSHING FOR SPEEDBRAKE ACTUATOR MOUNTING BOLT MISSING. INSTALLED BUSHING. PERFORMED AUTO SPEED BRAKE TEST. CHECK FAILED PER AMM. SPEED BRAKE LEVER VERY HARD TO MOVE OUT OF ARMED POSITION. NO BACK CLUTCH REPLACED PER MM 27-62-01, AS APPLICABLE, OPS CHECKED GOOD.

Part: SENSOR — FAULTED (RT ENGINE) · airframe 56,482 hrs · 15,793 cycles

CREW REPORTS AFTER ENGINE START RT ENG PROBE HEAT EICAS MSG DISPLAYED. DEFERRED PER SAMC. REPLACED RIGHT ENG P2-T2 SENSOR AND ACCOMPLISHED OPS CHECK, ALL TESTS PASS.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 56,451 hrs · 15,783 cycles

DOOR 1R WILL NOT ARM. OPENED DOOR - FOUND DEBRIS UNDER GIRT BAR ANCHOR POINT - CLOSED DOOR AND ARMING SEQUENCE OPERATED NORMAL.

Part: COVER — OUT OF POSITION (TOILET) · airframe 56,443 hrs · 15,781 cycles

FT AFT LAV TOILET SEAT COVER RIPPED OFF, CURRENTLY LOCATED BEHIND LAST ROW OF SEATS. SECURED LID, OPS NORMAL.

Part: SHAFT — BINDING (R3 DOOR) · airframe 56,310 hrs · 15,740 cycles

DOOR 3R OUTSIDE HANDLE INOP, WILL NOT STOW UPPER AND LOWER GATES. INNER SHAFT BINDING, DEBURRED SHAFT AND LUBED, DOOR HANDLE HAS TO BE PULLED OUT WITH FORCE TO CLOSE DOOR, NEEDS TROUBLESHOOTING. REPLACED ITEMS 125 AND 120 IN IPC 52-11-13-001A. REPLACED ITEMS 375 OUTER SHAFT, ITEM 135 SPRING AND ASSY 75 IPC 52-11-13-001A PG2, REF MM 52 -11-13. DOOR OP CHECKS OKAY.

Part: ACTUATOR — FAULTY (POSIT 1) · airframe 56,214 hrs · 15,710 cycles

TROUBLESHOT NR 1 ENGINE SEC CONT MESSAGE 5989-1 ESN 726585, REPLACED STATOR VANE ACTUATOR PER MM, ADJUSTED SVA PER MM. OPS AND LEAK CHECKED GOOD PER STATOR VANE ACT TEST. NO MESSAGES AFTER RUN.

Part: CONNECTOR — DIRTY (LT ENG EEC) · airframe 56,209 hrs · 15,709 cycles

LEFT ENGINE SEC CONT STATUS. CLEANED EEC CONNECTORS. CLEARED EICAS. PERFORMED IDLE RUN.

Part: LIGHT — DETACHED (CABIN) · airframe 56,192 hrs · 15,703 cycles

EXIT PATH LIGHTING BETWEEN 11C AND 12C DETACHED. RECONNECTED EMERGENCY LIGHT AT SEAT 11C. OP CHECKED OKAY. ACCOMPLISHED INSPECTION OF INSTALLED EMERGENCY LIGHT, OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: HANDLE — OUT OF ADJUST (RUDDER PEDAL) · airframe 55,504 hrs · 15,509 cycles

CAPTS RUDDER ADJUSTMENT CATCHES AT FULL FWD POSITION THEN MOVES OKAY. MAINT TEXT: PROBLEM HAPPENS AT FULL FORWARD ADJ WHEN TURNING TO BRING PEDALS AFT. ADJUSTED RUDDER PEDAL HANDLE, OPS CHECKS NORMAL.

Part: PAN — GOUGED (L2 DOOR) · airframe 55,172 hrs · 15,410 cycles

DOOR 2L HANDLE PAN GOUGED AROUND PERIMETER OF HANDLE CUTOUT. MAIN ENTRY DOOR 2 LEFT UPPER HINGE CUTOUT CRACKED. THE GOUGE COVERS APPROX 80-90 PERCENT OF CIRCULAR AREA OF HANDLE CUTOUT, APPROX .032 INCH DEEP. CRACK EXTENDS 18-32 OF AN INCH INTO THE PREVIOUS REPAIR. REPLACED CRACKED DOUBLER PER EVA UA-EVA-71536 ON SMB W-U W3014X. REPLACED PAN ON SMB W-U W3013X. AC RELEASE ON HOLD PENDING 8100-9 APROVAL. ORIGINAL EVA UA-EVA-71536 8100-9 APPROVAL STILL VALID.

Part: SLIDE — FAULTY (R1 DOOR) · airframe 55,172 hrs · 15,410 cycles

THE 1R SLIDE WAS REMOVED. REPLACED SLIDE.

Part: CONNECTOR — FAULTY (RUDDER TRIM ACT) · airframe 55,157 hrs · 15,406 cycles

RUDDER TRIM INDICATOR SHOWS NO MOVEMENT. RUDDER TRIM CIRCUIT BREAKER AT P11 C10 TRIPS WHEN TRYING TO TRIM RUDDER. REMOVED CONNECTOR D1746 AT RUDDER TRIM ACTUATOR AND CIRCUIT BREAKER P11 C10 STAYS IN.

Part: CONNECTOR — FAULTY (INTERPHONE) · airframe 55,144 hrs · 15,403 cycles

STATIC STILL PRESENT IN THE FLIGHT INTERFONE. REPLACED NLG FLIGHT INTERPHONE JACK. OP CHECKED PER MM, CHECKED GOOD.

Part: ACTUATOR — DEFECTIVE (SPEED BRAKE) · airframe 55,027 hrs · 15,372 cycles

ON LANDING AUTOSPEED BRAKES ONLY DEPLOYED PARTIALLY 50 PERCENT. NO TIME. REPLACED AUTOSPEED BRAKE ACTUATOR & K217 & K218 RELAYS. OPS CHECKS NORMAL.

Part: STOP PIN — OUT OF ADJUST (L1 DOOR) · airframe 54,999 hrs · 15,365 cycles

DOOR 1L HANDLE MOVES IN FLT. ADJUSTED DOOR STOP PINS PER MM. PRESSURIZED ACFT TO 4 PSI, DOOR 1L HANDLE STILL MOVES SLIGHTLY.

Part: LIGHT — DIRTY (SEAT 11ABC) · airframe 54,842 hrs · 15,319 cycles

EMERGENCY LIGHTING STRIP RAISED ABOVE IT'S RECESS AT 11ABC. REMOVED DEBRIS FROM UNDER EMERGENCY LIGHT STRIP.

Part: TIRE — OUT OF ROUND (NLG) · airframe 54,814 hrs · 15,310 cycles

NOSE WHEEL VIBRATES AT GEAR RETRACTION. NOSE WHEELS OUT OF ROUND. REPLACED LT AND RT NOSE TIRES PER AMM.

Part: PCU — FAULTY (ELEVATOR) · airframe 54,800 hrs · 15,304 cycles

LT ELEV PCU STATUS MSG. MSG WOULD NOT CLEAR, NO TIME TO TROUBLESHOOT. THE LEFT OUTBOARD PCA (RT HYD SYSTEM) FAILED FIM TEST WITH TEST BOX. NEED TO REPLACE THE LT OTBD PCA IAW MM. REPLACED LT OUTBOARD ELEV PCA PER MM, OPS CHK LEAK CHK RIG CHK OKAY.

Part: COVER — LOOSE (CABIN) · airframe 54,792 hrs · 15,301 cycles

EEL STRIP LOOSE ON FLOOR AT ROW 12. REPLACED COVER.

Part: COVER — OUT OF ADJUST (EMERGENCY LIGHT) · airframe 54,693 hrs · 15,266 cycles

EMERGENCY LIGHTS WOULD NOT ARM. ADJUSTED SWITCH COVER.

Part: PAN — GOUGED (R4 DOOR) · airframe 54,693 hrs · 15,266 cycles

DOOR 4 RIGHT DOOR HANDLE PAN HAS RADIAL GOUGE TWO PLACES AROUND HANDLE ROTATION POINT. DEEPEST AREA MEASURES .015 DEEP AND WITHIN .25 OF RADIUS. REMOVED DOOR 4R DOOR HANDLE PAN. COMPLETED INSTALLATION OF DOOR 4R DOOR HANDLE PAN REF DWG 146N6100.

Part: PRESSURE SWITCH — FAULTY (LT HYD PUMP) · airframe 54,681 hrs · 15,263 cycles

ENGINE DRIVEN PUMP (EDP) - HYDRAULIC LOW PRESS LIGHT DID NOT ILLUMINATE BUT EICAS MESSAGE ' HYD ENG PUMP' DID DISPLAY WITH ENGINE NOT RUNNING-LEFT SYSTEM. LEFT LOW PRESS LIGHT INOPERATIVE. PER CREW SHOULD READ LEFT ELECTRIC HYDRAULIC PUMP LOW PRESSURE LIGHT DID NOT ILLUMINATE WITH ENGINE NOT RUNNING. PER CREW SHOULD READ, LEFT ELECTRIC HYDRAULIC PUMP LOW PRESSURE LIGHT DID NOT ILLUMINATE WITH ENGINE NOT RUNNING. EICAS DISPLAYED. REPLACED PRESSURE SWITCH, OP CK GOOD.

Part: AUDIO PANEL — MALFUNCTIONED (COCKPIT) · airframe 54,657 hrs · 15,255 cycles

CAPTAIN'S AUDIO PANEL MALFUNCTION. OCCASIONAL NO SIDETONE, GARBLED RECEPTION & TONE DURING TRANSMIT. REPLACED CAPTAIN'S AUDIO PANEL.

Part: TRANSDUCER — FLUCTUATES (OXYGEN GAUGE) · airframe 54,273 hrs · 15,152 cycles

O2 GAUGE FLUCTUATES BETWEEN 0 AND 1400. OXYGEN READS 1500 AT BOTTLE. REPLACED PRESSURE TRANSDUCER. LEAK CHECKED AND VERIFIED PRESSURE ON EICAS.

Part: FIRE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 54,264 hrs · 15,148 cycles

FWD CARGO DET 1 AND 2 FAIL. MADE INPOERATIVE IAW MEL. PERFORMED LOWER CARGO BITE PROCEDURE PER MM. NO DEFECTS NOTED.

Part: RIVET — WORN (CABIN) · airframe 54,014 hrs · 15,083 cycles

ARMREST - CONSOLE LOOSE (ROCKS) AT 39C. AISLE ARMREST RIVETS SHEARED. SECURED ARMREST IN STATIONARY NORMAL POSITION. SEATS 39A, B, C NOT TO BE OCCUPIED. PLACARD WITH BLUE 'DO NOT OCCUPY COVERS'. SEATS IN UPRIGHT STOW POSITION. SEATS DO NOT INTERFERE WITH ROW 40 A, B, C ACCESS OR TRAY TABLE FUNCTIONS. REPLACED WORN OUT RIVETS WITH BLIND FASTERNERS.

Part: SUPPORT BRACKET — CRACKED (NACELLE) · airframe 53,933 hrs · 15,062 cycles

FOUND CRACKED HYD SUPPORT BRACKET AT NAC STA 180.8. REPLACED DAMAGED HYD SUPPORT BRACKET PER MM.

Part: CIRCUIT CARD — FALSE ACTIVATION (FIRE LOOP) · airframe 53,918 hrs · 15,059 cycles

AFTER ENG START RECEIVED A RT ENGINE FIRE LOOP 1 STATUS MESSAGE. REPLACED FIRE DETECTION CARD M683 PER MM, NO STATUS MESSAGE.

Part: CHARGER — FAULTED (MASTER BATTERY) · airframe 53,860 hrs · 15,036 cycles

MAIN BATTERY CHARGER AMPS BOUNCE BACK TO 1 5 AFTER CHARGING. REPLACED BATTERY CHARGER PER MM. ALSO REPLACED MAIN BATTERY PER MM.

Part: FAN — INOPERATIVE (WX RADAR TR TRAY) · airframe 53,750 hrs · 14,998 cycles

WEATHER RADAR FAILED ON PRE FLIGHT. REPLACED WEATHER RADAR TRANSCEIVER. OPS CHECKED GOOD. BITE TEST FAILURE MESSAGE WAS "RT". NOTED SEVERAL RECENT HISTORIES WITH TRANSCEIVER AND CONTROL PANEL REPLACED. TRANSCEIVER BOX WAS VERY WARM. SUSPECT COOLING FAN IN TRAY MAY BE INOP.ERATIVE. REMOVED WEATHER RADAR TRANSCEIVER IN ORDER TO INVESTIGATE LOG 1 (LACK OF COOLING IN E&E). FOUND NO AIR FLOW FROM MOUNTING TRAY. REINSTALLED WEATHER RADAR TRANSCEIVER AND CHECKED FOR FAN OPERATION, NO JOY. . REPLACED THE WEATHER TRANCEIVER COOLING FAN. FAN OPERATION CHECKED GOOD. ACCOMPLISHED OPERATIONAL TEST AND BITE TEST AT TRANCEIVER UNIT. TESTED OK.

Part: TRANSCEIVER — FAILED (RADAR) · airframe 53,704 hrs · 14,988 cycles

RADAR FAILURE. REPLACED TRX UNIT WITH JAL BP. JAL RETURN BOX IN HOLD BIN.

Part: VALVE — FAULTY (LEFT) · airframe 53,578 hrs · 14,944 cycles

NO LAND 3 ON BOTH AUTOLAND STATUS INDICATORS. MAINT TEXT: MCDP LAST LEG FAULT WAS "ILS CP-ILS L" AND "AIL SER VO-FCC L". MCDP TEST 7 INTERMITTANTLY FAILS "AIL SRVO R". SOME MCDP HISTORY FOR THIS FAULT SEVERAL LEGS AGO. DUE TO FAULTS ON BOTH SIDES A-C WAS TAKEN OUT OF SERVICE FOR MORE TS... MCDP TEST FAULT "NO LAND 3 AIL SRVO-FCC L" CODES 111461. REPLACED AP LATERAL CONT ALCS ELEC SERVO VALVE PER MM, OPS CHECKED GOOD. RIGHT AIL 112884 SRVO OK NOW, NO FAULTS. PERFORMED AUTOPILOT CAT-III AUTOLAND TEST PER MM. ILS OPS CHECK PER MM. TEST OKAY. AIRCRAFT OK TO CAT-III STATUS.

Part: EXCITER — FAILED (APU) · airframe 53,443 hrs · 14,908 cycles

APU FAILED TO START. BITE CHECK SHOWS IGN. NEED IGN UNIT EXCITER PER 757AMM. APU STARTED NORMALLY.

Part: LINE — CRACKED (HYD SYSTEM) · airframe 53,055 hrs · 14,803 cycles

HYDRAULIC RETURN LINE CRACKED AT UPPER RT LANDING GEAR. REPLACED RETURN LINE. PRESSURIZED NO LEAKS NOTED.

Part: WIRE — FAILED (RT ENGINE) · airframe 52,621 hrs · 14,680 cycles

RT ENG HYD PUMP FAILED DURING GEAR RETRACTION. REPAIRED WIRE W3486-1030-18 IN UPPER STRUT. MOTORED NR 2 ENGINE-HYD PRESS AND LOW PRESSURE LIGHT OPERATION OKAY.

Part: CONNECTOR — DIRTY (RT ENG HYD) · airframe 52,368 hrs · 14,617 cycles

AFTER ENG START, RT ENG HYD LOW PRESSURE LIGHT AND EICAS. COMPLIED WITH MEL CARD. CLEANED CONNECTOR. RAN ENG TWICE, OPS CKS GOOD.

Part: WIRE — BURNED (CABIN LIGHTS) · airframe 52,257 hrs · 14,590 cycles

ALL LAV OVERHEAD LIGHTS FAILED AND ELEC BURNING ODOR IN LAV 134 OVHD PANEL. UTIL BUSSES SECURED. ALL WIRING BURNED AT FWD AFT LAV DOOR SWITCH. SMOOTHED OUT WIRING CONDUIT, REPLACED ALL WIRING AT DOOR SWITCH AND REPLACED DOOR SWITCH. OPS CHECKED NORMAL.

Part: REGULATOR — FAILED (BLEED SYSTEM) · airframe 52,193 hrs · 14,570 cycles

WITH NR 2 ENGINE RUNNING DESELECTING BLEED SWITCH WOULD NOT TURN OFF PNEUMATIC SUPPLY (VALVE DID CLOSE WHEN ENGINE SHUTDOWN). INDICATIONS NORMAL. RAN NR 2 ENGINE APU BLEED OFF AND ISOLATED. HAD 15PSI DUCT PSI. HPSOV, PRSOV STILL OPEN, SWITCH OFF LIGHT OUT. SUSPECT CLOSE RELAY K10204. REPLACED RELAY AND PRSOV REGULATOR IAW MM, OPS CHECKED NORMAL.

Part: SHUTOFF VALVE — FAULTY (NR 2) · airframe 52,058 hrs · 14,530 cycles

RT ENG BLEED WILL NOT CLOSE WITH SWITCH OFF AND ISOLATION VALVE XSED. ALONG WITH ABOVE PROBLEM, WITH APU SUPPLYING AIR, ENG OFF, RT ENG BLEED OFF LIGHT EXTINGUISHES, APU BLEED VALVE LIGHT ILLUMINATES, DUCT PRESSURE DROPS, THEN APU BLEED VALVE LIGHT EXTINGUISHES. WHEN PRESSURE GETS TO ABOUT 5 PSI, APU BLD VALVE LIGHT FLASHES OFF AND ON, DUCT PRESSURE RISES AND RT ENG BLEED LIGHT ON. FOUND RIGHT ENG PRSOV OPENING WITH ANY BLEED SOURCE. REPLACED REVERSE FLOW CONTROL. NO HELP REPLACED RT PRSOV. BLEED OPERATES NORMAL.

Part: CIRCUIT CARD — MALFUNCTIONED (FIRE DECTECTION) · airframe 51,997 hrs · 14,514 cycles

RT ENG NR 1 FIRE LOOP STATUS MESSAGE DISPLAYED ON EICAS. REPLACED AFOLTS CARD M10274 AND FIRE CONTROL CARD M683 R ENG FIRE LOOP 1 PER MM. CHECKED OKAY. CLEANED RT ENGINE FIRE LOOP 1 CONNECTIONS. FIRE TEST CK OK AND OPERATED ENGINE AND TAXIED ACFT. CHECKED OKAY.

Part: BLEED VALVE — MALFUNCTIONED (RT ENGINE) · airframe 51,891 hrs · 14,483 cycles

RT ENGINE BLEED VALVE CYCLING OPEN WITH RT ENGINE SHUTDOWN AND APU SUPPLYING AIR TO THE PACK. REPLACED PRSOV REGULATOR. OPS NORMAL.

Part: LEAD — UNKNOWN (RAT) · airframe 51,882 hrs · 14,481 cycles

RAT POWER AND CONTROL CB TRIPPED. INITIAL REVIEW OF WDM 29-21-31 SHOWS CB LEADS TO RAT SOL ACTUATOR M10407.

Part: SHUTOFF VALVE — FAULTY (RT BLEED SYS) · airframe 51,882 hrs · 14,481 cycles

RT BLEED CYCLES. VALVE IS MALFUNCTIONING. REPLACED NR 2 ENGINE PRSOV. IDLE RUN OPS CHECK OKAY.

Part: ENGINE — FLUCTUATES (RIGHT) · airframe 51,760 hrs · 14,445 cycles

RT ENG DUCT PRESSURE FLUCTUATES. FLUCTUATES BETWEEN 20-40 PSI ALSO VARIES W PACK OFF. PER FLIGHT CREW FLUCTUATION AT CRUISE AND DESCENT RIGHT DUCT PRESS NEVER EXCEEDED LEFT SIDE, RIGHT OFF LIGHT ON AND OFF ON DESCENT. ENGINE WAS REPLACED. ACCOMPLISHED PNEUMATIC SYSTEM TEST PER JRH. ALL BLEED PARAMETERS NORMAL, NO FLUCTUATIONS NOTED.

Part: PIN — FAULTY (TE FLAPS) · airframe 51,717 hrs · 14,434 cycles

FLAPS 1 OVERSPEED 260 KTS, 20KTS OVER LIMIT. SUPPLEMENTAL DATA UPDATE ACP INSP ON LEFT AND RIGHT HAND OB FLAP TRACK FUSE PINS AND ALSO ACP INSP ON BOTH IB FLAP IB SUPPORT BOLTS. CHECKS GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 51,400 hrs · 14,340 cycles

FWD CARGO DET 2 STATUS MESSAGE AFTER FIRE-OVHT TEST ENG APU CARGO. REPLACED NR 2 FWD CARGO SMOKE DETECTOR PER MM.

Part: ISOLATION VALVE — FAULTY (POSITION 1) · airframe 50,801 hrs · 14,161 cycles

DUE TO REPORTS OF ISOLATION VALVE WOULD NOT OPEN (POPPED CB). REPLACED VALVE REF AMM, OPS CHECKS OK. CONNECTOR INSP AND PIN RETENTION CHECK OK, REMOVED RELAYS AND OVERHEAD PANEL AND MEGGERED WIRING, NO FAULTS FOUND.

Part: ISOLATION VALVE — FAULTY (POSITION 1) · airframe 50,780 hrs · 14,155 cycles

ISOLATION VALVE WILL NOT CLOSE. FOUND VALVE NOT FULLY FUNCTIONAL. REPLACED ISOLATION VALVE, OPS CHECKS OK.

Part: CIRCUIT CARD — FAULTY (FIRE DETECTION) · airframe 50,653 hrs · 14,119 cycles

CREW REPORTS LT ENGINE FIRE LP 2 STATUS MESSAGE DISPLAYED. ACCOMPLISHED FIM 26-11-00. LT ENGINE FIRE TEST CHECKS OK. IAW CREW MESSAGE WENT AWAY DURING FLIGHT. FOUND NO ACTIVE MSGS. REPLACED M682 LOOP 2 LT FIRE DET CARD AND OP-CHECK SATISFACTORY IAW MM AS PRECAUTIONARY.

Part: O-RING — LEAKING (FUEL CELL) · airframe 50,616 hrs · 14,106 cycles

LEFT SIDE CENTER FUEL TANK FILL VALVE LEAKING FROM MANUAL OVERRIDE KNOB ON CONTROL UNIT. REPLACED O-RINGS ON FILL VALVE CONTROL UNIT. PRESSURIZED FUELING MANIFOLD FOR 20 MINS. NO LEAKS NOTED.

Part: CAM — OUT OF ADJUST (R3 DOOR) · airframe 50,379 hrs · 14,037 cycles

DOOR 3R HANDLE MOVED OUT OF THE LOCKED POSITION ON LANDING UNCOMMANDED. EICAS R AFT DOOR. ADJUSTED UPPER AND LOWER LATCH CAMS IAW MM. INSPECTED LATCH ROLLER CRANK AND COCKING ROLLER CRANK LINKAGE. ALSO INSPECTED DOOR HANDLE MECHANISM. OPS CHECKS NORMAL.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 50,349 hrs · 14,029 cycles

EICAS SHOWS L ELEV PCU MSG. MSG ERASED, BUT RETURNS. TROUBLESHOT PER FIM MM. OPS CHECKED IT SEVERAL TIMES, UNABLE TO DUPLICATE MSG. REPLACED PCU MONITOR MODULE M10481 FOR PRECAUTION, OPS CHECKED GOOD.

Part: VALVE — FAILED (IDG) · airframe 50,187 hrs · 13,977 cycles

EICAS MSG LT GEN DRIVE DISPLAYED.GEN DRIVE LIGHT ILLUMINATED. GEN DRIVE DISCONNECTED. FOUND IDG TO BE LOW ON OIL. HAS HISTORY. IDG REPLACED 2 TIMES. FUEL OIL COOLER 1 TIME. LEFT IDG TOOK 64 STROKES UNTIL OIL OVERFLOWED INTO DRAIN BOTTLE. OPENED REVERSER AND CHECKED FOR EVIDENCE OF EXTERNAL LEAKS FROM AIR OIL COOLER ON DOWN AND NONE FOUND. SUSPECT INTERNAL LEAKAGE OF FUEL OIL COOLER BYPASS VALVE. REPLACED FUEL OIL COOLER BYPASS VALVE PER MM. RAN ENGINE FOR 10 MINUTES WITH AC ELECT ON LEFT IDG. NO LEAKS OR ABNORMAL INDICATIONS NOTED. RESERVICED IDG AFTER LEAK CHECK. REPLACED THE AIR-OIL HEAT EXCHANGER (PRECAUTIONARY).

Part: IDG — FAULTY (POSITION 1) · airframe 50,140 hrs · 13,964 cycles

LEFT GEN DRIVE LIGHT ON GEN .DISCONNECTED APU POWERING BUSS. REPLACED LT IDG. REPLACED LEFT ENG GCU. RAN LEFT ENGINE, OPS CHK NORMAL, NO LEAKS.

Part: FUEL/OIL COOLER — FAULTY (LT ENGINE) · airframe 50,125 hrs · 13,961 cycles

LT GEN DROPPED OFF LINE AND APU POWERING LT BUSS HAD L IDG OIL LEVEL MESSAGE. SERVICED LT IDG WITH 2 QTS OIL. RECONNECTED AND RAN ENGINE. IDG OPS OK, HAS HISTORY OF OIL SERVICE. DRIVE LIGHT CAME ON THEN WE DISCONNECTED DRIVE. REPLACED LT ENGINE IDG FUEL OIL HEAT EXCHANGER, OPS CK'S AND LEAK CK GOOD. NO MSGS.

Part: CONTROL SYSTEM — MALFUNCTIONED (APU) · airframe 50,116 hrs · 13,959 cycles

APU FAILED TO START. FAULT LIGHT ILLUM AND EICAS MSG. APU FAULT DISPLAYED. SECOND ATTEMPT INDICATES (SLOW ACCEL, HUNG START). CREW COMMENTS: APU HUNG AT 44 PERCENT ON 3 ATTEMPTS APU INOP. RESET APU CONTROL AND START BREAKERS. STARTED APU SEVERAL TIMES, NO PROBLEMS.

Part: IDG — FAULTY (LT GENERATOR) · airframe 50,097 hrs · 13,952 cycles

L GEN DRIVE DISPLAYED. FAULT TRACED TO IDG. REPLACED LT IDG, ENG RUN CHECKS OKAY.

Part: CONTROL CABLE — MISROUTED (RT AILERON) · airframe 49,703 hrs · 13,843 cycles

FLIGHT CONTROLS STIFF IN PITCH AND ROLL ON GROUND AND IN AIR. HEAVY CONTROLS FELT ON BOTH CONTROL COLUMNS, AP'S DISENGAGED, HYD'S PRESS AND QTY'S NORMAL. CHECKED LT AND RIGHT AILERON PCU. COMPLETED SYSTEM TEST. SYSTEM WILL INCREASE WHEEL FORCE. HAD TO FLY APPROACH AND LANDING WITH 2 HANDS- VERY HEAVY AND STIFF. FOUND RT AILERON CABLES INCORRECTLY ROUTED. REF SMC3, ORDERED THE FOLLOWING PARTS AOG. BRACKET ASSY (251N6285-3) ITEM 345 AND PULLEYS 2EA PCN 170-3359. CABLE P/N: (BACC2C4C06369FG) 1EA ITM 60 OSTF W2649 AND ITEM 65 (BACC2C4C05722FG) 1EA OSTF Y6386. PARTS HAVE BEEN RECEIVED. PARTS IN R6 FOREMANS OFFICE. REROUTED CABLES AND RIGGED, OPS CHK SYSTEM NORMAL.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 49,611 hrs · 13,819 cycles

RT HYD ENG PUMP FAILED. PUMP LOW PRESS LIGHT ON WITH EICAS MSG, IAW CREW. REPLACED RT ENGINE DRIVEN HYD PUMP. OPS NORMAL.

Part: TRANSCEIVER — FAILED (HF SYSTEM) · airframe 49,272 hrs · 13,723 cycles

LEFT HF DOES NOT TRANSMIT. REPLACED LEFT TRANSCEIVER AND OPS CHECKED OK.

Part: PRESSURE SWITCH — FAULTED (HYD PUMP) · airframe 49,017 hrs · 13,651 cycles

ON LANDING RT ENG HYD PUMP ON EICAS. MOTORED ENGINE, PRESSURE CHECKS NORMAL. LOW PRESSURE LIGHTS OPS NORMAL. HAS HISTORY. PUMP, AND FILTERS REPLACED PREVIOUSLY. NEEDS FURTHER TROUBLESHOOTING. REMOVED AND REPLACED RT EDP PRESSURE SWITCH. OPS CHECK & LEAK CHECK GOOD ON GND TEST.

Part: CONTROLLER — FAULTY (FUEL SYSTEM) · airframe 48,918 hrs · 13,623 cycles

FOUND CENTER TANK RT FUEL FILL VALVE INOP. LT FILL VALVE OKAY. REPLACED CENTER RT FUEL FILL VALVE ACTUATOR - CONTROLLER PER MM, NO HELP. NEXT STEP TO REPLACE FUELING SHUTOFF VALVE. REQUIRES TANK ENTRY. REQUEST 3 SHIFT SLOT. FUEL TANK ENTRY REQUIRED. NEED TO REPLACE RIGHT CENTER TANK FUELING VALVE V10064 REF MM. REPLACED THE RT CENTER FUELING VALVE CONTROLLER. OPS CHECKED OF SYS IS GOOD AND LEAK CK GOOD. ALL FUELING SYS WORKING NORMAL. ALL LIGHTS WORKING.

Part: PCU — MALFUNCTIONED (ELEVATOR) · airframe 48,809 hrs · 13,591 cycles

L ELEV PCU STATUS. PERFORMED MAINT COMPLIANCE ITEMS FOR MEL 2721D. MSG WILL NOT CLEAR. NO HISTORY. REPLACED L ELEV CENTER PCU. OPS CHECK GOOD AND NO MSG.

Part: PUMP — FAULTY (NR 2 ENGINE) · airframe 48,774 hrs · 13,580 cycles

CREW REPORTS THE RIGHT ENG HYD PUMP LOW PRESSURE LIGHT CAME ON. CREW TURNED PUMP SW OFF IAW THE IRREG PROCEDURE. REPLACED RT EDP AND CASE DRAIN FILTERS.

Part: CONNECTOR — DAMAGED (OIL PRESSURE) · airframe 48,602 hrs · 13,529 cycles

L ENG OIL PRESS STATUS MSG. EXAMINE THE CIRCUIT FROM THE MAIN OIL PRES SURE TRANSMITTER, CONNECTOR D4794 TO THE LT EICAS COMPUTER CONNECTOR D319B PINS G1 &H2. BY- 107540 EXAMINED CIRCUIT FROM D479 4 PINS 2 &3 TO D319B PINS G1 &H2, NO DEFECTS FOUND. MEGGERED FROM D4794 PIN 2 TO D42362P PIN 34 AND D4794 PIN 3 TO D42362P PIN 35 NO DEFECTS NOTED. RETURNED CIRCUIT TO NORMAL. PROBLEM RECURRED DURING NEXT FLT SEGMENT. CHECKED OIL SYSTEM WIRING PER WDM. CLEANED CONNECTORS AND REPOSITIONED HARNESS. OPS CHECK PER OIL SYSTEM PRESS TEST. ALL INDICATIONS WITHIN LIMITS.

Part: OXYGEN MASK — LEAKING (FO'S) · airframe 48,502 hrs · 13,503 cycles

FIRST OFFICERS O2 MASK LEAKS. MASK LEAKS WHEN INFLATING HARNESS. SWAPPED MASK WITH OBSERVERS POSITION. NEED MASK ASSY, OUT OF STOCK SEATTLE. OBSERVERS SEAT CONSIDERED INOP. REPLACED OBSERVERS O2 MASK.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 48,440 hrs · 13,484 cycles

NR 2 ENG HYD PUMP HAS FAILED. INSTALLED NEW HYD PUMP AND REPLACED CASE DRAIN AND PRESS FILTERS. HYD LINES STILL NEED TO BE FLUSHED AND CONNECTED TO HYD PUMP. FLUSHED AND CONNECTED LINES. LEAK CK OF PUMP AND FILTERS WAS GOOD.

Part: IDG — FAULTY (LEFT) · airframe 48,400 hrs · 13,471 cycles

LEFT IDG ISSUE, FLT DIVERTED. HAD SECOND HIT, RTFL. SERVICED IDG. SUSPECT IDG OVERSERVICED. GROUND RUNUP CHECKS OK, VOLTS-FREQS NORMAL, BPCU BITE SHOWED LOW OIL PRESS-SERVICE IDG. SERVICED AS NEEDED. RTG FOR LT IDG SECOND HIT. BPCU BIT LT IDG,SERVICE IDG, IDG PRESS SW WIRING IDG, IDG NOT DISCONNECT. REMOVED LT IDG. NO EVIDENCE OF METAL FOUND IN SCAVENGE FILTER OR IDG CASE OIL. LT IDG OIL-IN LINE REMOVED FOR ACCESS. INSTALLED AND SAFETIED LINE. REPLACED LT IDG. LEAK CHECK OK. OPS CHECK OK.

Part: EXHAUST VALVE — FAULTY (EQ COOLING) · airframe 48,277 hrs · 13,430 cycles

OVERBOARD EXHAUST VALVE TEST STATUS MESSAGE. REPLACED EQUIPMENT COOLING OVERBOARD EXHAUST VALVE. OP CKS NORMAL.

Part: PDU — FAULTED (NR 2 ALTERNATOR) · airframe 48,277 hrs · 13,430 cycles

NR 2 ENG EICAS MSG ENG SEC CONT DISPLAYED. REPLACED NR 2 ENG EEC ALTERNATOR STATOR. MSG STILL RETURNS. WIRING CHECKED GOOD. REPLACED PDIU M10553 PER AMM. NO MESSAGES PRESENT.

Part: AILERON SYS — MALFUNCTIONED · airframe 48,153 hrs · 13,393 cycles

AILERON CONTROL ISSUE, FLIGHT DIVERTED. INSPECTED CABLES AND PULLEYS FROM WHEEL WELL TO AILERON PCU'S BOTH LT AND RT WING. ALSO CHECKED AILERON QUADRANTS AND COLD SOAKED QUADRANT BRGS IN WHEEL WELLS AND DAMPER UNDER COCKPIT PIT FLOOR FOR TROUBLESHOOTING. NO DISCREPENCIES NOTED. COULD NOT DUPLICATE HEAVY FORCES. ACP CONTROL WHEEL TORQUE CHECK. FEEL, CENTERING AND TRIM TEST. ALL CHECKS AND TEST WITHIN LIMITS. HAS DEAD SPOTS AT LWR SPEEDS- ALL MOVEMENT IS MUCH HEAVIER THAN NORMAL. LUBRICATED SYS AT ALL ACCESSIBLE POINTS. ADJUSTED FEEL AND CENTERING SPRINGS. REDUCING BREAK OUT FORCE. ALSO REPLACED LT OTBD PCA AND OPS CHECKED. NO LEAKS NOTED AND TOLERANCE AT .005.

Part: YOKE — OBSTRUCTED (COCKPIT) · airframe 48,149 hrs · 13,390 cycles

AILERON CONTROL STIFF IN FLT ABOVE 200 KTS. ACP TEST FLT. ACTUATE AILERONS IN ALL PHASES OF FLT ABOVE & BELOW 200 KTS. FOUND SPOILERS 4 & 9 EXTENDED & NOT ALIGNED WITH WING, 5 & 8 MEASURED 19 IN. INSTEAD OF 9.19 IN. & 6 & 7 MEASURED 15 IN. INSTEAD OF 7.05 IN. WITH SPEEDBRAKE LEVER UP, SPOILERS DON`T STOW WITH FULL CONTROL WHEEL DEFLECTION. ONLY 6 & 7 MOVED TO ALMOST FLUSH. 1, 2, 3, 5, 8, 10, 11, & 12 ALL REMAIN APPROX. 4.5 IN FROM FLUSH. FOUND YOKE PROTRACTOR CONTACTING YOKE & PREVENTING MAX DEFLECTION OF AILERONS. AFTER REMOVING, ALL CHECKED OK. TEST FLT, CREW REPORTS ROLL FORCED CHECKED NORMAL AT ALL SPEEDS UP TO 320 KIAS, ALL ROLL FORCES & ROLL RATES NORMAL. SUCCESSFUL TEST ACP.

Part: DOUBLER — DAMAGED (L2 DOOR) · airframe 47,951 hrs · 13,329 cycles

L2 REPAIR DOUBLER AT UPPER HINGE CUT OUT DAMAGED, WU 33083. REMOVED EXISTING DAMAGED DOUBLER AT UPPER HINGE CUT-OUT ON FORWARD FRAME. FORMED A REPAIR ANGLE & INSTALLED IAW REO G13168, REV. B & UAL EVA 73214. L2 DOOR UPPER HINGE CUTOUT AREA REMOVED & REPLACED DOUBLER ON NR40351 IAW ECRA521 1-01345.

Part: STRUCTURE — DAMAGED (HINGE CUTOUT) · airframe 47,951 hrs · 13,329 cycles

L-2 REPAIR DOUBLER AT UPPER HINGE CUTOUT DAMAGED. MAJOR REPAIR ACCOMPLISHED: REMOVED EXISTING DAMAGED DOUBLER AT UPPER HINGE CUTOUT ON FWD FRAME. FORMED A REPAIR ANGLE AND INSTALLED.

Part: CABLE — OUT OF ADJUST (DOOR EMER POWER) · airframe 47,951 hrs · 13,329 cycles

L2 DOOR EMERGENCY POWER ACTUATOR CABLE TRAVEL CHECK FAILED. ADJUSTED EMERGENCY POWER TRIGGER MECHANISM AND CABLE. OPS CHECK GOOD.

Part: SLIDE — UNSECURE (LT OVERWING) · airframe 47,951 hrs · 13,329 cycles

LT OVERWING EXIT SLIDE UNLACING. REMOVED AND REPLACED LT OVERWING SLIDE.

Part: SLIDE — FAULTY (RT OVERWING) · airframe 47,951 hrs · 13,329 cycles

RT OVERWING EXIT SLIDE UNLACING. REMOVED AND REPLACED RT OVERWING EXIT SLIDE PACK.

Part: CAM — FAULTY (R4 DOOR) · airframe 47,951 hrs · 13,329 cycles

DOOR 4R ARMING LEVER FAIL HALF WAY TEST. REMOVED AND REPLACED LOCKOUT CAM. OPS CHK'D GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,951 hrs · 13,329 cycles

EMERGENCY LIGHT L562 OVER LT WING IS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, CHARGER AND LAMP; OPS CHK OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,951 hrs · 13,329 cycles

EXT EMERGENCY EGRESS LIGHT L568 FWD OF DOOR 4L IS INOPERATIVE. RELAMPED DOOR 4L, FWD SIDE L568 LIGHT, OPS CHK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,951 hrs · 13,329 cycles

EMERGENCY LIGHT BATTERY PACK M10699 AT SEAT 23DEF IS INOP. REMOVED AND REPLACED BATTERY PACK, OPS CK OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,951 hrs · 13,329 cycles

F-C EMERGENCY LIGHT STRIP AT LAV S KICK STRIP IS INOP. REMOVED AND REPLACED LIGHTING STRIP. GROUND OPS CK GOOD.

Part: PAN — DAMAGED (DOOR) · airframe 47,951 hrs · 13,329 cycles

L2 DOOR PAN DENTED AND GOUGED OUTSIDE SURFACE. REMOVED AND REPLACED DOOR PAN. DOOR RIG IS WORKED IN CONJUNCTION WITH HK ROUTINE DOOR JC. PAN IS REPLACED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,951 hrs · 13,329 cycles

EXT EMERGENCY EGRESS LIGHT L41 AFT OF DOOR 2R AT STA 735 RBL 73 IS INOPERATIVE. RELAMPED R2 DOOR EGRESS LIGHT, OPS CHK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,951 hrs · 13,329 cycles

EMERGENCY LIGHT BATTERY PACK M735 LOCATED AT SEAT 23ABC IS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHK OKAY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,951 hrs · 13,329 cycles

EMERGENCY LIGHT BATTERY PACK M10568 AT SEAT 15DEF IS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND OPS CHK.

Part: FLOORBEAM — CORRODED (BS 324) · airframe 47,951 hrs · 13,329 cycles

MAIN CABIN FLOORBEAM CORRODED AT STA 324 FROM RBL 42 TO RBL 66, UPPER T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED: REPLACED DAMAGED FLOORBEAM. REINSTALLED ADJ INTERCOSTAL AND FASTENERS.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 47,951 hrs · 13,329 cycles

AFT GALLEY AREA, FLOORBEAM UPPER T-CAP HAS EXFOLIATION CORROSION AROUND FASTENER HOLES, TOP SURFACE IN SEVERAL AREAS, BS 1640.0, BL 0 TOP RBL 60. MAJOR REPAIR ACCOMPLISHED: REPLACED DAMAGED SECTION OF FLOORBEAM. REINSTALLED ADJ INTERCOSTALS AND FASTNENERS.

Part: FLOORBEAM — CORRODED (BS 365.25) · airframe 47,951 hrs · 13,329 cycles

MAIN CABIN FLOORBEAM CORRODED AT STA 365. 25 BETWEEN RBL 58 TO RBL 20. MAJOR REPAIR ACCOMPLISHED: DAMAGED FLOORBEAM. REINSTALL ADJ INTERCOSTAL AND FASTENERS.

Part: LIFE RAFT — READS LOW (CABIN) · airframe 47,951 hrs · 13,329 cycles

MAIN CABIN CEILING MOST AFT LIFE RAFT BOTTLE PRESSURE IS LOW. REMOVED AND REPLACED NR 2 POSITION LIFE RAFT.

Part: TURNBUCKLE — OUT OF ADJUST (DOOR 2L) · airframe 47,951 hrs · 13,329 cycles

DOOR 2L EMERGENCY POWER MECHANISM CABLE NOT ADJUSTED PROPERLY, RED BAND IS NOT VISIBLE. ADJUSTED SPRING CABLE TURNBUCKLE AND ALIGN RED BAND. OPS CHK GOOD. RED BAND IS VISIBLE.

Part: TURNBUCKLE — OUT OF ADJUST (DOOR 4R) · airframe 47,951 hrs · 13,329 cycles

4R DOOR EMERGENCY POWER MECHANISM CABLE NOT ADJUSTED PROPERLY, RED BAND NOT VISIBLE. ADJ SPRING CABLE TURNBUCKLE AND ALIGN RED BAND, OPS CHK GOOD, RED BAND IS VISIBLE.

Part: CYLINDER — OUT OF ADJUST (DOOR 1R) · airframe 47,951 hrs · 13,329 cycles

MAIN CABIN R-1 DOOR EMERGENCY POWER MECHANISM CABLE NOT ADJUSTED PROPERLY, RED NOT POSITIONED PROPERLY. ADJUSTED POWER SPRING CABLE CYLINDER. OPS CHECK GOOD, RED BAND IS VISIBLE.

Part: CYLINDER — OUT OF ADJUST (L1 DOOR) · airframe 47,951 hrs · 13,329 cycles

DOOR 1L EMERGENCY POWER MECHANISM CABLE NOT ADJUSTED PROPERLY, RED BAND NOT PROPERLY POSITIONED. ADJ POWER SPRING CYLINDER. OPS CHECKED GOOD, RED BAND IS VISIBLE.

Part: STOP FITTING — OUT OF TOLERANCE (DOOR) · airframe 47,951 hrs · 13,329 cycles

DOOR 4 LT & RT DOOR STOP TEE CLIP. ACCOMPLISED COA 506902 DOOR 4L AND 4R DOOR STOP TEE CLIP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,586 hrs · 13,238 cycles

EXTERIOR EVAC LIGHT INOP AT DOOR 2LT. RELAMPED EXTERIOR EVAC LIGHT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,586 hrs · 13,238 cycles

EXTERIOR EVAC LIGHT INOP AT DOOR 1RT. RELAMPED EXTERIOR EVAC LIGHT.

Part: GCU — MALFUNCTIONED (NR 1) · airframe 47,474 hrs · 13,202 cycles

AT ABOUT 500FT' ON FINAL APPROACH L GEN TRIPPED OFF LINE. BITE TEST OF BPCU SHOWED "IDG HIGH RISE TEMP" AND "RPL GCU (D9)". MSGS CALL FOR RPL OF GCU. REPLACED LEFT ENG GCU. IDG OIL LEVEL WAS OK. IDG ELEC CONNECTOR WAS CLEANED. BITE TEST WAS GOOD AND MSGS ERASED. RAN L ENG FOR 5 MIN AND SWAPPED POWER NUMEROUS TIMES. GEN TAKES THE LOAD AND ALL INDICATIONS ARE NORMAL.

Part: IDG — FAULTY (POSITION 1) · airframe 47,438 hrs · 13,189 cycles

ON TAXIOUT, THE LT GEN TRIPPED OFF LINE, DRIVE LITE ILLUMINATED. HAD CREW DISCONNECT IDG AND VERIFIED 0 VOLTS AND FREQS. SERVICED APU OIL PRIOR TO DEPT. SERVICED #1 IDG OIL FOUND FULL. RECONNECTED IDG, BUT STILL HAD DRIVE LIGHTS PRIOR TO ENG RUN FOR DEF. HAD FOLLOWING AUTO EVENTS DC-A= 22, DC-V=28, IDGOUT 90, IDG RISE 9. ON BPCU HAD DISCONNECT TRIP WITH NO OTHER FAULTS. REPLACED NR1 GCU NO HELP. REPLACED IDG, LEAK CHECKED ENG. ADJ IDG AND TESTED PER MM. CK'D OKAY.

Part: BATTERY — DISCHARGED (MAIN) · airframe 47,185 hrs · 13,107 cycles

APU FAILED TO START 3 TIMES, 1ST ATTEMPT WAS ABORTED DUE TO A STANDBY POWER CHECK. REPLACED APU BATTERY. APU CONTROLLER DISPLAYED SLOW STARTS AND ACCEL FAULTS. BATT VOLTAGE BELOW 13 VOLTS & NO CHARGE. ACP BATTERY & APU TESTS, BOTH OP CHECK NORMAL. FAULTS CLEARED, APU NOW OPERATIONAL.

Part: SHUTOFF VALVE — STUCK (APU) · airframe 46,518 hrs · 12,912 cycles

EICAS MSG 'APU BLEED VAL' DISPLAYED. APU BLEED AIR VALVE LIGHT ON. DUCT PRESSURE WAS ZERO. APU BLEED AIR VALVE LOCKED IN THE CLOSED POSITION. REPLACED APU SHUT-OFF VALVE. OPS CHECKED VALVE BY CYCLE OPEN AND CLOSE A COUPLE OF TIMES AND DRY MOTOR AN ENGINE. CHECKS GOOD.

Part: GUARD — DAMAGED (COCKPIT) · airframe 46,337 hrs · 12,856 cycles

UNABLE TO ARM EMERGENCY EXIT LIGHTS. REPAIRED COCKPIT EMERGENCY EXIT SWITCH GUARD, OPS CHECKS OKAY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,269 hrs · 12,832 cycles

NR 1 RT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP. REPLACED LAMP, OPS GOOD.

Part: SEALANT — DEFECTIVE (RT WING) · airframe 46,067 hrs · 12,769 cycles

LEFT WING DRY BAY NR 1 DRAIN HOLE & RIGHT WING DRY BAY NR 3 DRAIN HOLE LEAKING FUEL. BOROSCOPE INSPECTED LT DRY BAYS NR 1, 2 & 3. FOUND NR 1 DRY BAY LEAKING AT O/B AND AFT FIBERGLASS PNLS. INSP'D NR 1 RT DRY BAY, NO LEAK FOUND. NEED TO CONTINUE T/S ON RT NR 2 AND NR 3 DRY BAYS. PRESSURIZED FUEL SYSTEM FOR 1HR. NO LEAKS FOUND. REMOVED OLD BAD SEALANT FROM FIBERGLASS PNK 532HZ, CLEANED AND PREPARED TO SEAL. NEED TO INSPECT O/B PYLON FUEL PNL. NEW SEALANT IN FUEL OFFICE. INSPECTED O/B PYLON PNL AND APPLIED A B SEALANT AT 1300. LT & RT TANKS SEALED, CURE TIMES TO 0130 01JUN, THEN ACP LEAK CK.

Part: PUMP — FAULTY (RT ENGINE) · airframe 45,080 hrs · 12,497 cycles

ENGINE NR 2 LOW OIL PRESSURE EICAS MESSAGES. REPLACED PUMP ASSY.

Part: TRANSMITTER — FAULTY (OIL PRESSURE) · airframe 45,080 hrs · 12,497 cycles

ENGINE NR 2 LOW OIL PRESSURE EICAS MESSAGES. REPLACED PUMP ASSY. REPLACED OIL PRESSURE TRANSMITTER PER MM 79-32-01. OPS CHECK GOOD.

Part: PUMP — FAULTY (RT ENGINE) · airframe 45,080 hrs · 12,497 cycles

ENGINE NR 2 LOW OIL PRESSURE EICAS MESSAGES . REPLACED PUMP ASSY.

Part: TRANSMITTER — FAULTY (NR 2 ENGINE) · airframe 44,842 hrs · 12,431 cycles

NR 2 ENGINE OIL PRESSURE DISPLAY INTERMITTENT, QTY & TEMP NORMAL. REPLACED NR 2 OIL PRESSURE TRANSMITTER AND RAN ENGINE. OPS GOOD.

Part: START VALVE — FAILED (NR 1 ENGINE) · airframe 44,826 hrs · 12,424 cycles

NR 1 ENG WOULD NOT START, STARTER FAILED, NO OIL IN STARTER. REPLACED START VALVE. START VALVE WORKS GREAT.

Part: PRESSURE SWITCH — FAILED (NR 2 ENGINE) · airframe 44,623 hrs · 12,366 cycles

NR 2 ENGINE FUEL FILTER BYPASS MESSAGE ON EICAS. DIVERTING TO SLC. ACP WIRING CHECK, AND REPLACED NR 2 FUEL DIFFERENTIAL PRESSURE SWITCH. ACCMP'D DRY MOTOR AND CHECKED FOR LEAKS. ACCMP MOTOR AND LEAK CHECK. NO LEAKS NOTED.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 44,475 hrs · 12,327 cycles

SLIDE PACK FELL OUT DOOR 2L. REPLACED SLIDE ASSY.

Part: BYPASS VALVE — LEAKING (NR 1 ENGINE OIL) · airframe 44,287 hrs · 12,272 cycles

NR 1 ENGINE HOC. FOUND NR 1 ENG FUEL-OIL HEAT EXCHANGER LEAKING OIL- INTO FUEL. REPLACED NR 1 FOX & BYPASS VALVE ASSY. OP CHECKED GOOD ON HIGH POWER RUN, NO LEAKS NO FAULTS.

Part: COUPLER — FAULTY (RT HF SYS) · airframe 43,194 hrs · 11,981 cycles

RIGHT HF WILL NOT TRANSMIT. FOUND FAULTY HF. SUSPECT COUPLER. REPLACED RT HF COUPLER AND RT HF TRANSCEIVER.

Part: INVERTER — MISSING (EMERGENCY LIGHT) · airframe 43,161 hrs · 11,971 cycles

ROBBED EEL INVERTER FOR A-C 5596. INVERTER GOES ABOVE AFT GALLEY MAIN CEILING LIGHTS. TAPE IDENTIFIES THE 2 CONNECTOR HOOKUPS. HARDWARE IS ATTACHED TO TAPE. *S/D* REPLACED INVERTER. OP CHECK NORMAL.

Part: COUPLER — FAULTY (HF RADIO) · airframe 42,400 hrs · 11,761 cycles

R HF RADIO FAIL TO TRANSMIT BUT RECEPTION IS GOOD. COUPLER IS FAULTY. REPLACED COUPLER.

Part: VALVE — INOPERATIVE (RT FUEL TANK) · airframe 42,371 hrs · 11,750 cycles

CENTER TANK RIGHT FUEL VALVE WILL NOT OPEN.

Part: DOOR — MALFUNCTIONED (APU ACTUATOR) · airframe 42,348 hrs · 11,744 cycles

THREE TRIES APU WILL NOT START - STATUS MSG APU DOOR. RESET C/B FOR APU DOOR ACT. CYCLED DOOR 2 TIMES ON GROUND AND THEN STARTED 2 TIMES WITH AIR AND ELEC. LOAD ALL OPS GOOD.

Part: VALVE — FAILED (NLG) · airframe 42,289 hrs · 11,727 cycles

GEAR DISAGREE WARNING PROMPTED RTFL. FOUND NOSE GEAR SAFETY VALVE BY-PASSING, FAILING. REPLACED NOSE GEAR SAFETY VALVE, PERFORMED GEAR SWINGS, OPS CHECKED NORMAL.

Part: WIRE HARNESS — SHORTED (LT ENGINE) · airframe 42,154 hrs · 11,692 cycles

RECEIVED "L ENG SECONDARY CONTROL" EICAS STATUS MSG. WIRING HARNESS D42048 HAS SHORTED. REPAIRED HARNESS D42048, ALL CONT CHECKS ARE GOOD, ITEM HAS NOT REPEATED.

Part: UNKNOWN — MALFUNCTIONED (R1 DOOR) · airframe 42,105 hrs · 11,678 cycles

INBOARD CREW REPORTS DOOR 1 RIGHT HARD TO ARM.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 42,079 hrs · 11,669 cycles

L ENG SEC CONT STATUS MESSAGE. CHECKED FOR EPCS MESSAGES LISTED ON MM CHAPTER 71 EICAS AND EPCS MESSAGES SERVICE TIP, NO MESSAGES FOUND. ERASED STATUS MESSAGE. PUT EEC SWITCH ON P61 PANEL TO SEC POSITION, NO MESSAGES APPEARED. ACFT OK FOR SERVICE.

Part: EEC — ERRATIC (NR 1 ENGINE) · airframe 41,626 hrs · 11,535 cycles

NR 1 ENG EICAS MSG ENG SEC CONT DISPLAYED. REPLACED LEFT ENGINE EEC PER FIM 71-EPCS MSG INDEX S274-24. AND MM73-21-04. CHECKED ALL CONNECTORS ON EEC AND FIREWALL, FOUND OK. RAN ENGINE NO FAULTS.

Part: LANDING GEAR — MALFUNCTIONED · airframe 41,200 hrs · 11,413 cycles

UPON T/O, GEAR DISAGREE AND GEAR DOOR DISPLAYED FOR A SHORT PERIOD TIME DURING GEAR RETRACTION. AFTER A SHORT PERIOD TIME ALL MSG'S CLEARED. JACKED A/C AND SWUNG GEAR, ALL CHECKED NORMALLY. LUBED NOSE GEAR ASSY, SWUNG GEAR SEVERAL TIMES WITH NORMAL SWING TIMES. NO REPEATS SINCE ORIGINAL.

Part: IDG — FAULTY (LEFT) · airframe 40,895 hrs · 11,326 cycles

THE L BUSS TIE WILL NOT COME ON-LINE. LT (NR 1 ENG) IDG IS FAILING. REPLACED IDG, ALL TESTS NORMAL.

Part: IDG — FAILED · airframe 40,528 hrs · 11,226 cycles

RIGHT GENERATOR DRIVE LIGHT ILLUMINATED. IDG FAILED, SHOP FOUND 4 SUPPORT SCREWS HAD LOOSE INSERTS CAUSING FAILURE. REPLACED IDG. VERIFICATION FLIGHT ACCOMPLISHED, ALL NORMAL.

Part: COMPUTER — MALFUNCTIONED (FUEL QTY) · airframe 40,483 hrs · 11,217 cycles

LEFT FUEL QTY IND WAS DECREASING AT A RAPID RATE. BALANCED FUEL PER IRREGULAR CHECKLIST. FUEL DECREASE IN LEFT AND RIGHT FUEL TANKS NORMAL. FUEL IND AT TIME OF MSG: LT TANK 12.4 RT TANK 14.4 CTR 1.0 CHECKED FUEL PROCESSOR, NO FAULTS. RESET FUEL QTY BITE TESTED GOOD. NO HISTORY. NO REPEATS SINCE ORIGINAL.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 39,126 hrs · 10,804 cycles

RTFL DUE TO SHATTERING OF PILOT'S WINDSHIELD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,474 hrs · 10,632 cycles

EXTERIOR EMERGENCY EXIT LIGHT INOP AT DOOR 1R. [07-27-07] RELAMPED.

Part: PUMP — FAILED (LEFT) · airframe 38,041 hrs · 10,507 cycles

RTFL DUE TO LEFT AFT FUEL BOOST PUMP FAILURE. [06-20-07] LT AFT FUEL BOOST PUMP INOP. AFT FUEL BOOST PUMP PRESSURE SWITCH WAS REPLACED.PLAN TO LAND APPROX 10K OVERGROSS ON RETURN FOR FUEL BOOST PUMP FAILURE. ACCOMPLISHED PHASE 1 ACFT INSPECTION AND NO DAMAGE FOUND.

Part: RING — MISSING (L1 DOOR) · airframe 37,685 hrs · 10,407 cycles

DOOR 1L MISSING D RING. [06-14-07] FOUND LANYARD MISSING INSTALLED SERVICABLE LANYARD. INSTALLED. ()INSPECTED DOOR 3L AND D-RING IS INSTALLED. REPLACED LANYARD AT DOOR 1L.

Part: GEAR — FAILED (GEARBOX) · airframe 37,504 hrs · 10,355 cycles

APU HAD SHUTDOWN, FAULT LIGHT ILLUM AND EICAS MSG. APU FAULT DISPLAYED. APU REMOVED FROM AIRCRAFT FOR METAL ON CHIP DETECTOR. COMPOUND GEAR IN GEARBOX FAILED AND CAUSED AUTO SHUTDOWN. GEARBOX AND COOLING FAN TSHM=6337 HRS AND CSHM=8381.

Part: SILL — DIRTY (R1 DOOR) · airframe 36,866 hrs · 10,158 cycles

DOOR 1R DIFFICULT TO DISARM. LEVER DOESN'T ALWAYS MOVE COMPLETELY TO DISARM POSITION. CLEANED DOOR SILL AND THE LEVER MOVEMENT WAS RESTORED. NO COMPONENT NEEDED TO BE REPLACED.

Part: SLIDE — UNWANTED DEPLOY (RT OVERWING) · airframe 36,001 hrs · 9,910 cycles

AIRCRAFT ARRIVED FOR C-CHECK MAINTENANCE AND IT WAS FOUND TO HAVE THE RT OVERWING SLIDE PARTIALLY DEPLOYED. SLIDE STILL IN COMPARTMENT. SLIDE REPLACED.

Part: HEATER — OVERHEATED (OVERWING EXIT) · airframe 35,971 hrs · 9,902 cycles

SIDE WALL AT 15F VERY HOT, PLASTIC DEFORMED. RIGHT OVERWING FWD HATCH AFT PART OF DOOR FRAME HOT TO THE TOUCH, WILL BURN, STAYED HOT UNTIL ACFT LANDED. INSPECTED AREA, NO SIGN OF ANY DEFORMED PLASTIC. PERFORMED OVERWING EXIT HATCH HEATER TEST. CHECKED BOTH SIDES OF AIRCRAFT USING DIGITAL NON CONTACT THERMOMETER. BOTH SIDES CHECKED UNDER 90 DEGREES AFTER 10 MIN. AREA DID NOT FEEL HOT TO TOUCH.

Part: RADAR — FAILED (WX SYSTEM) · airframe 34,687 hrs · 9,549 cycles

UNPLANNED STOP DUE TO WEATHER RADAR FAILURE. WX RADAR FAILURE DISPLAYED ON HSI. WXR FAILED ANTENNA DISPLAYED ON HSI IN WXR TEST POS. REPLACED WEATHER RADAR SCANNER ASSY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,837 hrs · 9,327 cycles

EEL LIGHT STRIP OUT AT 15ABC. [06-29-07] REPLACED LIGHT STRIP.

Part: SLIDE — UNKNOWN (R1 DOOR) · airframe 33,570 hrs · 9,253 cycles

1R MED SLIDE RAFT PRESSURE GAUGE AT BOTTOM OF GREEN BAND AFTER 5 HOURS ON GROUND.

Part: SKIN — GOUGED (FUSELAGE) · airframe 31,788 hrs · 8,740 cycles

LEFTHAND FUSELAGE, AFT OF DOOR 2L, DENT AND GOUGED SKIN ON FRAME AT STA 760 AND S16. ACCOMPLISHED INTERIM RPR PER SRM53-00-01 RPR#2 PG.201-206. LFEC TO BE ACCOMPLISHED EVERY 3 000 CYCLES.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 31,582 hrs · 8,681 cycles

RETURNED TO SFO DUE TO NOSE GEAR RETRACTION PROBLEM. REPLACED NOSE LANDING GEAR LOCK ACTUATOR. OPS CHECK OK.

Part: FAN — FAILED (GALLEY) · airframe 30,545 hrs · 8,366 cycles

STRONG ELECTRICAL ODOR IN MID GALLEY. STRONG ELECTRICAL ODOR IN MID GALLEY AFTER APU GEN FIELD TRIP. REPLACED NR 1 FWD EQUIP SUPPLY FAN.

Part: PACKING — LEAKING (HYD PACK) · airframe 26,110 hrs · 7,114 cycles

LEFT HYDRAULIC QUANTITY STARTED DROPPING IN CRUISE. QUANTITY STABILIZED AT .25 PERCENT AFTER PUMPS SELECTED OFF. PACKING AT HYDRAULIC MOTOR GENERATOR SHUTOFF VALVE WAS LEAKING. REPLACED PACKING.

Part: PUMP — FAILED (LT ENGINE) · airframe 25,240 hrs · 6,868 cycles

LT ENGINE HYDRAULIC PUMP FAILED. HYDRAULIC ENGINE PUMP EICAS MESSAGE DISPLAYED. PUMP IS ENROUTE TO VENDOR FOR EVALUATION. REPLACED PUMP AND FILTERS. FLUSHED SYSTEM, LEAK AND OPERATIONAL CHECK.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 23,961 hrs · 6,502 cycles

ARCING ON EXTERNAL FUSELAGE SKIN AT STA 319.5, STR 2 RT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 23,961 hrs · 6,502 cycles

EXTERNAL FUSELAGE SKIN DENTED SEVERAL LOCATIONS FWD OF DOOR 2L AT APPROX BS 608-627 BETWEEN STR 15L AND 17L. MAJOR REPAIR ACCOMPLISHED. REPLACED EXISTING SMALL DOUBLER AND INCORPORATED INTO LARGE EXTERNAL DOUBLER.

Part: FRAME — DENTED (FUSELAGE) · airframe 23,961 hrs · 6,502 cycles

FRAME RETURN FLANGE HAD DENT DAMAGE 2 PLACES BS 1400 AND BS 1420, BETWEEN STRINGERS 25L-27L. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.

Part: CONTROLLER — FAILED (ENGINE) · airframe 20,992 hrs · 5,715 cycles

LEFT ENGINE BLEED PRESSURE REGULATING AND SHUTOFF VALVE FAILURE PRIOR TO ENTERING ETOPS ENVIRONMENT. SUPPLEMENTAL DATA UPDATE HIGH STAGE PILOT CONTROLLER FAILED. REPLACED HIGH STAGE PILOT CONTROLLER.

Part: SLIDE — DAMAGED (PAX DOOR) · airframe 10,534 hrs · 2,926 cycles

DOOR 1 SLIDE/RAFT DEVELOPED SEAM BLISTERS IN BOTH THE SLIDE/RAFT INFLATABLE DOOR SILL PILLOWS DURING SHOP OVERHAUL. THE CAUSE OF THE SEAM BLISTERS IS UNKNOWN. UNIT IS BEING SENT TO THE VENDOR FOR EVALUATION AND REPAIR.

Part: STATOR — FAILED (NR 1 ENGINE) · airframe 8,545 hrs · 2,375 cycles

THE NUMBER ONE ENGINE WAS SHUT DOWN SHORTLY AFTER TAKEOFF DUE TO A COMPRESSOR STALL. THE AIRCRAFT RETURNED TO DEN. *S/D* AFTER LANDING AT DEN METAL WAS FOUND IN THE TAILPIPE AND THE ENGINE WAS REMOVED AND SENT TO THE SHOP FOR INVESTIGATION AND REPAIR. THE SHOP DISASSEMBLY FINDINGS WERE A FAILED 10TH STAGE HPC STATOR. THIS IS AN INDUSTRY PROBLEM AND IS UNDER INVESTIGATION BY PWA.

Part: FAN — MALFUNCTIONED (LEFT)

DIVERTED TO HNL WITH A LEFT RECIRCULATION FAN PROBLEM.