N547UA

Part: CIRCUIT CARD — FAULTY (FIRE WARNING) · airframe 83,733 hrs · 24,187 cycles

STATUS MSG RT ENG FIRE LP 2. CLEANED ALL FIRE LOOP CONNECTORS & CHECKED LOOPS FOR ANY WIRE DISCREPANCIES, NONE NOTED. REPLACED CARD M684 IAW AMM 26 -10-01. OPERATIONS CHECKED OK. TOTAL RESISTANCE CHECK FROM P54 PIN 19 TO PIN 20 WITHIN LIMITS 1509 OHMS.

Part: NUT — CRACKED (MLG) · airframe 83,710 hrs · 24,181 cycles

NUMBER 3 MLG TIRE TIE BOLT NUT CRACKED. R & R NR 3 MLG TIRE IAW AMM 32-45-01.

Part: GROUND WIRE — DAMAGED (EXTERIOR LIGHT) · airframe 83,573 hrs · 24,143 cycles

TEST FLT 2186 OVERWING RT SIDE EXTERNAL EMER LIGHTS INOPERATIVE. REPAIRED GND WIRE RT OVERWING EMER LIGHT IAW BSWPM 20-10-11, OPERATIONS CHECKED GOOD.

Part: FEEDER CABLE — DAMAGED (CABIN) · airframe 83,573 hrs · 24,143 cycles

LEFT EEL FEEDER CABLES DAMAGED. R & R EEL FEEDER CABLES IAW MM 31-51-96. OPERATIONS CHECKED GOOD IAW MM 33-51-00.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 83,573 hrs · 24,143 cycles

EEL INVERTER INOPERATIVE. R & R EEL INVERTER AT ROW 23 IAW WDM 33-51-21. OPERATIONS CHECKED GOOD IAW MM 33-51-00.

Part: CARRIER ASSY — LACK OF LUBE (EVAC SLIDE) · airframe 83,573 hrs · 24,143 cycles

LEFT OFF WING SLIDE PNEUMATIC DEPLOYMENT CARD CHECKED CARD 5R25I1356 FAILED AT STEP 8. CARRIER DID NOT TURN OUT OF SLIDE COMPARTMENT. LUBED LT OFF WING SLIDE COMPARTMENT DOOR & SLIDE CARRIER IAW MM 25-65-00, STEP 8. OPERATIONAL CHECK GOOD IAW MM 25-65-00.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 76,629 hrs · 22,361 cycles

EXTERIOR UPPER FUSELAGE STATION 700, BETWEEN STATION 3L & 4L HAS A DEEP BLENDED OUT AREA. CUT OUT DAMAGED SKIN, HFEC CUT SKIN & SURROUNDING HOLES. INSTALLED REPAIR DOUBLERS & FILLER IAW ECRA 5531-01609. PLANNING TO CONTACT ENGINEERING AFTER 22 MONTHS BUT BEFORE 23 MONTH TO ACCOMPLISH PERM REPAIR AT 24 MONTHS. REV A MF2188 TO TRACK INSPECTION IAW PART 2 STEP 1 REPEAT EVERY 12000C. CF9087 CREATED FOR ONE TIME CHECK IAW PART 2 STEP 2 AFTER 30000C BUT BEFORE 36000PTC CHANGED LIMIT CF9082 TO 44300PTC FOR RECHECK PT 2 STEP 3. ACCOMPLISHED MF2188 AT HMV4 ON NR40553 MAY 7 2014. ACCOMPLISHED HFEC OF REPAIR WITH NO CRACK INDICATIONS NOTED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,573 hrs · 24,143 cycles

AFT GALLEY FLOOR SUPPORT CORRODED AT STATION 1681 FWD OF RT OTBD GALLEY MOUNT. NEW DOUBLER INSTALLED IAW ECRA 5 330-04259 REV. PERFORMED HFEC IAW NDT51-00-19. ALODINED, PRIMED & TOP COATED IAW SRM 51-20-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,573 hrs · 24,143 cycles

MAIN CABIN FLOORBEAM UPPER CAP FASTENER HOLES CORRODED BS 365 - BS 365, RBL 40.00. R & R NEW T CAP AT EXISTING REPAIR IAW ECRA 5310-05536. REINSTALLED UPPER T CAP STRAP, SPLICE PLATE, FLOOR SUPPORT, SCUFF PLATE SUPPORT & FLOOR DRAIN IAW SRM 51-40-02.

Part: DOUBLER — CRACKED (R2 DOOR) · airframe 83,573 hrs · 24,143 cycles

MED DOOR R2 UPPER HINGE CUT OUT FWD EDGE PREVIOUS REPAIR DOUBLER CRACKED. REMOVED PREVIOUS REPAIR, HFEC CUT OUT & FASTENER HOLES COMMON TO THE REPAIR, NO CRACK FOUND. FABRICATED & INSTALLED NEW REPAIR DOUBLER IAW SRM 52-10-02 REPAIR 1. THIS IS A CAT B REPAIR. INSPECTION THRESHOLD IS 5,800 DOOR FLIGHT CYCLE AFTER REPAIR INSTALLATION & AT 5,800 DOOR FC INTERVAL THEREAFTER IAW SRM 52-10-02 REPAIR 1 TABLE 202 ON PAGE 209. CF CREATED TO ACCOUNT FOR RE INSPECTION THRESHOLD. MF 4148 CREATED TO MONITOR, MF4148 ADDED TO MONITOR.

Part: DOUBLER — CRACKED (R2 DOOR) · airframe 83,573 hrs · 24,143 cycles

MED DOOR R2 UPPER HINGE CUT OUT FWD EDGE PREVIOUS REPAIR DOUBLER CRACKED. REMOVED PREVIOUS REPAIR, HFEC CUT OUT & FASTENER HOLES COMMON TO THE REPAIR, NO CRACK FOUND. FABRICATED & INSTALLED NEW REPAIR DOUBLER IAW SRM 52-10-02 REPAIR 1. THIS IS A CAT B REPAIR. INSP THRESHOLD IS 5,800 DOOR FLIGHT CYCLE AFTER REPAIR INSTALLATION & AT 5,800 DOOR FLIGHT CYCLE INTERVAL THEREAFTER IAW SRM 52-10-02 RPR 1 TABLE 202 ON PAGE 209.

Part: GATE — CORRODED (R2 DOOR) · corrosion level 2 · airframe 83,573 hrs · 24,143 cycles

NR 2R MED DOOR LOWER GATE FOUND CORRODED. R & R R2 MED DOOR LOWER GATE IAW SM-09-13-25-10-JD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 76,629 hrs · 22,361 cycles

EXTERIOR UPPER FUSELAGE STATION 700, BETWEEN STRINGER 3L & 4L HAS A DEEP BLENDED OUT AREA. CUT OUT DAMAGED SKIN, HFEC CUT SKIN & SURROUNDING HOLES. INSTALLED REPAIR DOUBLERS & FILLER.

Part: LENS — UNSECURE (CABIN) · airframe 82,674 hrs · 23,936 cycles

EXIT LIGHT STRIP RIPPED FROM FLOOR IN LAST ROW. SECURED EMERGENCY EXIT LIGHT LENS.

Part: UNKNOWN — MALFUNCTIONED (HYDRAULIC SYS) · airframe 82,683 hrs · 23,939 cycles

FLIGHT DIVERTING TO SFO DUE TO A CTR HYD SYS QTY AT ZERO.

Part: ANTENNA — FAULTY (ATC TRANSPONDER) · airframe 82,402 hrs · 23,877 cycles

ATC FAULT LIGHT ON, FOUND LT ATC TRANSPONDER FAILING UPPER & LOWER ANT & RT TRANSPONDER FAILING LOWER ANT.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 82,305 hrs · 23,852 cycles

EXTERNAL FUSELAGE SKIN EXTERNAL SURFACE HAS LIGHTNING STRIKE AT STATION 745 BETWEEN STRINGER 23R & 24R. REPAIRED IAW SRM 53-00-01 ALLOWABLE DAMAGE 1, DETAIL 1.

Part: LINK — OBSTRUCTED (GIRT BAR) · airframe 82,074 hrs · 23,801 cycles

2L DOOR HARD TO OPEN, FROST ON DOOR. REPLACED 2L FWD GIRT BAR LINK & AFT RADIUS ROD.

Part: GIRT BAR — BROKEN (L2 DOOR) · airframe 82,074 hrs · 23,801 cycles

DOOR GIRT FOOT LIFTING MECHANISM BOTTOM HALF BROKEN OFF & MISSING. REPLACED L2 DOOR FWD LIFTING FITTING LINK.

Part: STUD — DEFECTIVE (CABIN) · airframe 81,986 hrs · 23,781 cycles

SEAT 25 DEF FWD AISLE LEG LOCK LOOSE. LOCK NUT SPINNING IN LEG ASSEMBLY. REPLACED STUD & ANTI RATTLE NUT, SEAT SECURED.

Part: VALVE — LEAKING (NR 1 ENGINE) · airframe 81,882 hrs · 23,756 cycles

NR 1 ENG FUEL DISTRIBUTION VLV LEAKING FROM TOP SURFACE OF UNIT AT 6 O`CLOCK POSITION. REPLACED FUEL DISTRIBUTION VLV, ABOVE NO HELP STILL LEAKING. REPLACED FUEL DISTRIBUTION VLV FOR THE SECOND TIME, NO HELP STILL LEAKS AFTER ENG SHUT DOWN. REMOVED OLD UNIT MR73518-9 INSTALLED MR73151-02. NEED LEAK CHECKED & IDLE RUN. ACCOMPLISHED IDLE LEAK CHECK OF FUEL DISTRIBUTION VLV AFTER EEC REPLACEMENT, LEAK CHECKED GOOD.

Part: VALVE — LEAKING (FUEL SYSTEM) · airframe 81,882 hrs · 23,756 cycles

NR 1 ENG FUEL DISTRIBUTION VLV LEAKING FROM TOP SURFACE OF UNIT, AT 6 O'CLOCK POSITION. REPLACED FUEL DISTRIBUTION VLV.

Part: UNKNOWN — INTERMITTENT (RT ENGINE) · airframe 81,702 hrs · 23,707 cycles

RT ENG EEC ALTERNATOR CHECK. 2 ESN 717972 HAS INTERMITTENT SEC CONT FAULT WITH EPCS MESSAGES 274-18.

Part: FLUID — LEAKING (LAVATORY SERVICE) · airframe 81,633 hrs · 23,690 cycles

WHILE PRESSURIZING AC THE MID LAVATORY WAS LEAKING FLUID FROM THE SERVICE PORT.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 81,380 hrs · 23,622 cycles

EMEGENCY LIGHT LENS FOUND CRACKED FROM SEATS 8 TO 14. REPLACED CRACKED SECTION OF CLEAR LENS.

Part: BOTTLE — FAULTY (EVAC SLIDE) · airframe 81,370 hrs · 23,620 cycles

EMERGENCY ESCAPE SLIDE SQUIB TEST 2R BULB DOES NOT ILLUMINATE. DUE BOTTLE PRESSURE NOT WITHIN SERVICEABLE LIMITS. JUMPED BOTTLE PRESSURE SW CONN D5542 PINS A-C & TEST 2 CHECKED GOOD. SSM 25-65-01. NEED TO REPLACE RT OFF WING SLIDE BOTTLE & NEC TO DISARM OFF WING SYSTEM AS APPLICABLE. REPLACED RT OFF WING SLIDE BOTTLE.

Part: LANYARD — MISSING (CABIN) · airframe 81,091 hrs · 23,552 cycles

IAW FCD 2100-01378, CEILING STATION 1160 DIST. DUCT RT LANYARD IS MISSING. INSTALLED LANYARD IAW EC-RA 2100-01381.

Part: FASTENER — MISSING (LT WING) · airframe 77,455 hrs · 22,591 cycles

SCREW MISSING LT WING OUTBOARD OF MIDDLE FLAP CANOE NEXT TO DRAIN HOLE. REPLACED MISSING FASTENER.

Part: SIGN — UNSECURE (EMERGENCY LIGHTS) · airframe 80,371 hrs · 23,370 cycles

EXIT ROW 20F SIGN FALLING OFF. SECURED EXIT SIGN.

Part: MECHANISM — LACK OF LUBE (R1 DOOR ARMING) · airframe 79,621 hrs · 23,173 cycles

R1 DOOR ARMING LEVER DIFFICULT TO MOVE. LUBRICATED ARMING AND DISARMING MECHANISM.

Part: PROCESSOR — FAULTY (FUEL SYSTEM) · airframe 79,426 hrs · 23,119 cycles

FUEL QTY IND STATUS MESSAGE WITH RT FUEL IND BLANK MOMENTARILY TWICE DURING FLIGHT. REPLACED FQIS PROCESSOR REF TO AMM AND BITE TEST NO FAULT.

Part: TAB — BROKEN (DOOR HINGE) · airframe 79,421 hrs · 23,117 cycles

LEFT WING SLIDE SERVICE DOOR HAS TWO TABS BROKEN ON HINGE ALLOWING DOOR TO STICK OUT IN AIRSTREAM. INTERM REPAIR WITH 2 LAYERS OF TAPE WITH 2 INCH OVERLAP PER ECRA 5365-01073. REPLACED HINGE ASSY ON 195HL INSPECTED FOR DAMAGE ACCESS PANEL 195GL OR ACCESS DOOR 195HL, NO DEFECTS NOTED. ACP REPLACEMENT PER ECRA 5365-01073 PART 3 PERMANENT REPAIR GUIDELINES.

Part: SOCKET — ARCED (LAVATORY) · airframe 79,383 hrs · 23,107 cycles

F/A'S REPORT ODD ELECTRICAL TYPE ODOR IN AFT LAV. CONFIRMED DOME LIGHT IS OPERATIVE. MIRROR LIGHT BULBS REMOVED. FOUND LIGHT BULB SOCKET ARCHING. NOT TIME TO CHANGE. REMOVED BULBS.

Part: PITOT TUBE — FAILED (AUX) · airframe 79,337 hrs · 23,096 cycles

CREW REPORTS R AUX PIPOT EICAS ON TAXI OUT AFTER ENG START. REPLACED R AUX PITOT TUBE L. LEAKED AND OP CHECKED REF AMM. CHECKED OKAY.

Part: AMU — FAILED (NR 1) · airframe 79,337 hrs · 23,096 cycles

ACARS FAILED IN FLIGHT. REPLACED AMU PER MM, OPS CHECKED NORMAL.

Part: WINDSHIELD WIPER — BROKEN · airframe 79,325 hrs · 23,093 cycles

FIRST OFFICERS SIDE WIPER ARM IS BROKEN. REPLACED FIRST OFFICERS WIPER BLADE ASSY PER REF AMM.

Part: GROUND WIRE — UNSECURE (WING) · airframe 79,301 hrs · 23,083 cycles

GROUND WIRE HANGING OUT OF 1ST FLAP TRACK CANOE OUTBOARD OF LF ENG PYLON SECURED GROUND WIRE IN CANOE FAIRING.

Part: SPEAKER — INOPERATIVE (COCKPIT) · airframe 79,193 hrs · 23,052 cycles

CAPTAIN'S SPEAKER DOES NOT WORK (NO SOUND). REPLACED CAPT'S SPEAKER, OPS TEST NORMAL.

Part: BLADE — DAMAGED (LT ENGINE) · airframe 79,068 hrs · 23,016 cycles

BLADE FOD DAMAGE ON LEFT ENGINE NOTED ON SEVERAL BLADES 18 INCHES FROM BLADE TIP-SMALL NICKS. NICKS ARE WITHIN LIMITS PER MM. THE 18 INCHES FROM BLADE TIP IN (AREA 5) NICKS NEED TO BE BLENDED WITHIN 25 HOURS.

Part: SENSOR — OUT OF ADJUST (R2 DOOR GIRT BAR) · airframe 79,034 hrs · 23,004 cycles

R2 DOOR SLIDE LIGHT WENT OFF DURING TAKEOFF, CAME BACK ON IN FLT. CYCLED OFF AGAIN DURING LANDING. HANDLE IN ARM POSITION NOT MAKING FULL CONTACT. OK TO CONTINUE. ADJUSTED GIRT BAR PROXIMITY SENSORS FOR R2 DOOR.

Part: LIGHT — NO TEST (OVERHEAT SYS) · airframe 78,995 hrs · 22,990 cycles

RIGHT ENGINE OVERHEAT DOES NOT TEST, NO LIGHT. REPLACED RIGHT ENGINE OVERHEAT LIGHT ASSY BASE.

Part: PROBE — FAULTY (LT ENGINE) · airframe 78,953 hrs · 22,979 cycles

STATUS MSG LEFT ENGINE PROBE HEAT AFTER START. REPLACED LEFT ENGINE PROBE IAW AMM, TEST PASSED.

Part: GENERATOR — MALFUNCTIONED (NR 2) · airframe 78,810 hrs · 22,943 cycles

RIGHT ENGINE IDG LOW OIL PRESSURE LIGHT DOES NOT COME ON WITH ENGINE OFF, LIGHT TESTED OK. REPLACED NR 2 ENGINE GENERATOR. NR 2 ENGINE RAN PER JRH. NO LEAKS NOTED AND GENERATOR, OPS CHECKED NORMAL.

Part: HINGE — DAMAGED (EXT POWER DOOR) · airframe 78,365 hrs · 22,827 cycles

REPORTED EXTERNAL POWER ACCESS DOOR NOT FAIRED. REMOVED DOOR REF CDL -52L. NEEDS NEW HINGES AND LATCHES ACCOMPLISHED ADJUSTMENT AND RIG OF DOOR AND DOOR HINGE. FIT AND FARE ARCHIVED.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,359 hrs · 22,824 cycles

EXFOLIATION-CORROSION UNDERNEATH STIFFENING BRACKET. INSIDE APU INLET PLENUM ABOVE AFT CTR SUPPORT CASTING FOR ENGINE MOUNT (POPPED RIVET HEAD "MARKED"). CLEANED CORROSION AND REPAIRED STIFFENING BRACKET REF SRM.

Part: GIRT BAR — JAMMED (R1 DOOR) · airframe 78,294 hrs · 22,807 cycles

PRIOR TO DEPARTURE, 1R HARD TO ARM. UNJAMMED ARMING SLIDE ON GIRT BAR. OPS OK, SLIDE LIGHT OK.

Part: CONTROL PANEL — FAULTY (WEATHER RADAR) · airframe 78,280 hrs · 22,804 cycles

WX RETURNS ERRATIC ON WXR DISPLAY. CREW COMMENTS: FELT LIKE IT WAS MAGENTA TEST IS NORMAL PATTERN. REPLACED WEATHER RADAR TRANSCEIVER, AND TESTED PER AMM 34-43-01. REPLACED WEATHER RADAR CONTROL PANEL, AND TESTED PER AMM 34-43-02.

Part: COVER — UNSECURE (COCKPIT) · airframe 78,101 hrs · 22,756 cycles

F/O CENTER PEDESTAL SIDE COVER WILL NOT STAY ON, EXPOSED WIRES. SECURED PANEL.

Part: CONNECTOR — FAULTY (CABIN) · airframe 78,026 hrs · 22,734 cycles

SHORT TO GROUND IN W2070-0802-22 AND W2066-0805-22 PER 33-45-11 PAGE 1A. REF DF752 FOUND WIRE W2070-0802-22 TO BE THE PROBLEM. REMOVED WIRE FROM D3532 P23 ON M0071 LIGHT CTL PNL ON P5 PNL. WITH WIRE DISCONNECTED NORMAL OPS OF DIMMER & NO BLANKING OF CB PNL WHEN SELECTING LOGO LT SW TO ON. REF WDM 33-45 -11 P1A. DISCONNECTED WIRE FROM TB59 XA4 & CONFIRMED PROBLEM TO BE BETWEEN TB59 & D3532-P23. ISOLATED FAULT BETWEEN LOGO LIGHT CONN AND P11 PANEL. REPLACED CONN D03532. CB OVERHEAD PANEL WORKED OK WHEN LOGO LIGHT SWITCH TURNED ON.

Part: FILTER — FAULTY (EQUIP COOLING) · airframe 77,785 hrs · 22,674 cycles

EQUIP COOLING OVERHEAT LIGHTT ON AND OFF. REPLACED EQUIP COOLING FILTER.

Part: OXYGEN MASK — DEFECTIVE (COCKPIT) · airframe 77,646 hrs · 22,637 cycles

FLIGHT DECK OBSERVER O2 MASK IS DEFECTIVE. REPLACED O2 MASK. REMOVED AND INSTALLED PER AMM.

Part: OXYGEN BOTTLE — LOW PRESSURE (CABIN) · airframe 77,642 hrs · 22,636 cycles

O2 BOTTLE LOW LEFT SIDE OVERWING BOTTLE OUT OF SERVICE BAND. REPLACED O2 BOTTLE.

Part: MICROPHONE — STUCK (COCKPIT) · airframe 77,459 hrs · 22,592 cycles

F/O HAND MIKE STICKS. REPLACED MIKE, OPS CHECK OKAY.

Part: OIL SYSTEM — LOW (APU) · airframe 77,184 hrs · 22,516 cycles

APU FAULT DISPLAYED ON EICAS WITH APU FAULT LIGHT. APU AUTO SHUTDOWN AT FL360 4.5 INTO FLT. APU OIL PRESS FAULT FOUND ON ECU. SERVICED LOW OIL QUANTITY. WRENCH CHECKED ALL OIL PRESS LINES ACCESSIBLE ON APU AND FOUND SECURE. RAN APU FOR 1 HOUR AND RE-INSPECTED FOR LEAKS. NO LEAKS FOUND. OK FOR SERVICE.

Part: STARTER — FAULTY (APU) · airframe 77,177 hrs · 22,514 cycles

APU FAILS TO START. APU NO ROTATION AFTER SWITCH TURNED ON. REPLACED STARTER PER MM, OPS CHECKED OK.

Part: CONTROL UNIT — FAULTY (APU) · airframe 77,127 hrs · 22,504 cycles

APU RUN LIGHT ON WITH APU NOT ON AND THEN FAULT LT WHEN RUN LT OUT. REPLACED APU CONTROL UNIT. STARTED APU, BUT AUTO SHUTDOWN AT 95 PERCENT. APUC RECORDED "LOW OIL PRESS".

Part: PRESSURE SWITCH — FAULTY (APU OIL SYS) · airframe 77,127 hrs · 22,504 cycles

REPLACED APUC AND STARTED APU, BUT AUTO SHUTDOWN FOR LOW OIL PRESSURE. REPLACED LOW OIL PRESSURE SWITCH AND RESTORED APU OPERATIONS.

Part: MODULE — FAULTED (RIGHT) · airframe 77,011 hrs · 22,474 cycles

STABILIZER TRIM EICAS ILLUMINATED ON SHORT FINAL WENT OUT ON TAXI IN WITH CENTER STABILIZER SWITCH IN CUTOUT. MOVING THE STABILIZER USING THE RIGHT HYDRAULIC SYSTEM STABILIZER TRIM LIGHT ILLUMINATES. PERFORMED FIM 27-09-00 FIG 103. NO MSG PER SHEET 8 BLOCK 6. THE CSEU SYSTEM IS OK PERFORMED AUTO STAB TRIM OPS TEST PER MM, (MCDP TEST 65) CHECKED OK. COULD NOT DUPLICATE PROBLEM. NEED MORE TIME TO ISOLATE AND FIX PROBLEM. RIGHT SAM MODULE M525, SHOWS A FAULT BALL FOR STCM. RESET IT.IT COMES BACK. REMOVED AND REPLACED STABILIZER TRIM CONTROL MODULE.

Part: CONTROL ROD — OUT OF ADJUST (RT ELEVATOR) · airframe 76,919 hrs · 22,447 cycles

DURING CONTROL CHECK, ELEVATORS SPLIT AND NOT NEUTRAL. FOUND RT ELEVATOR RIG PIN ES T9 UNABLE TO FREELY PUT IN MIDDLE PCA AND RT ELEVATOR TRAILING EDGE .25 INCH FROM LOCATING HOLE ON INDEX PLATE. ADJUSTED RT ELEVATOR PCA INPUT CONTROL ROD AND POWER CONTROL ACTUATORS REF AMM. PERFORMED ELEVATOR CONTROL SYSTEM, OPS TESTED. ADJUSTMENT & OPS CHECKED OKAY.

Part: GATE — CORRODED (R4 DOOR) · corrosion level 2 · airframe 76,629 hrs · 22,361 cycles

R4 DOOR LOWER GATE HAS CORROSION ON BOTTOM LIP. INSTALLED LOWER GATE.

Part: GATE — CORRODED (L1 DOOR) · corrosion level 2 · airframe 76,629 hrs · 22,361 cycles

L1 LOWER GATE CORRODED. INSTALLED LOWER GATE REF MM 52-11-38 STEP 3,D 5-7.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 76,629 hrs · 22,361 cycles

EXTERIOR UPPER FUSELAGE STA 700, BETWEEN STA 3L AND 4L HAS A DEEP BLENDED OUT AREA. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SKIN, HFEC CUT SKIN AND SURROUNDING HOLES, INSTALLED REPAIR DOUBLERS AND FILLER PER ECRA 5531-01609.

Part: TORQUE TUBE — CORRODED (LT WING TE FLAPS) · corrosion level 2 · airframe 76,629 hrs · 22,361 cycles

LEFT INBD MAIN FLAP TORQUE TUBE FAILSAFE SHOWS SIGNS OF CORROSION. REPAIRED THE FAILSAFE TORQUE TUBE PER CMM 57-53-43, REFERENCE R03846, 8130-3, 016-A004726 49. WORK WAS ACCOMPLISHED AT SFO.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,629 hrs · 22,361 cycles

AFT CARGO FRAME HAS CORROSION AT STA 1440 AND RBL4. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION, JUST OUT OF SRM LIMITS, TREATED, PRIMED, INSTALLED REPAIR DOUBLER PER ECRA 5360-01209.

Part: TORQUE TUBE — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 76,629 hrs · 22,361 cycles

RT MAIN FLAP FAILSAFE TORQUE TUBE SHOWS SIGNS OF CORROSION. REPAIRED RT WING FAILSAFE TORQUE TUBE PER CMM 57-53-43.

Part: FLOORBEAM — CORRODED (BS 1380) · corrosion level 2 · airframe 76,629 hrs · 22,361 cycles

AFT CARGO BAY FLOOR STRUCTURE, AFT SIDE OF FRAME AT BS 1380 HAS CORROSION FROM RBL 13 TO RBL 17. REMOVED CORROSION OUT OF SRM LIMITS ON THE END OF FRAME. HFEC INSPECTION SURROUNDING FASTENER HOLES AND REWORKED AREA, TREATED, PRIMED, INSTALLED FASTENERS PER ECRA 5360-01208

Part: SKIN — DAMAGED (FUSELAGE) · airframe 76,629 hrs · 22,361 cycles

EXTERIOR UPPER FUSELAGE STA 1450 SPLICE BETWEEN STR 3L AND 4L HAS A BLENDED OUT AREA. MAJOR REPAIR ACCOMPLISHED. TRIMMED OUT AREA, INSTALLED REPAIR DOUBLERS AND FILLERS.

Part: SKIN — DAMAGED (BS 1450 S3-4L) · airframe 76,629 hrs · 22,361 cycles

EXTERIOR UPPER FUSELAGE BS 1450 SPLICE BETWEEN STR 3L AND 4L HAS A BLENDED OUT AREA. TRIMMED OUT DAMAGED SKIN. HFEC INSPECTED SURROUNDING FASTENER HOLES AND TRIMMED OUT AREA. INSTALLED REPAIR DOUBLERS AND FILLERS. PLANNING TO CONTACT ENGINEERING AFTER 30000 TOTAL CY, BUT BEFORE 32000 CY TO ACCOMPLISH INSPECTION BEFORE 36000 CYCLES.

Part: SKIN — DENTED (FUSELAGE) · airframe 30,029 hrs · 9,207 cycles

RIGHT FUSELAGE DENTED AT STA 1390 BETWEEN STR 22R AND 23R. INSPECTED AREA WITH HFEC AND FOUND TO BE CRACK FREE. DENT IS WITHIN LIMITS OF SRM. DURING HEAVY CHECK, FOUND PREVIOUSLY REPAIRED.

Part: SKIN — DENTED (BS 740 S25-26L) · airframe 76,629 hrs · 22,361 cycles

LEFT FUSELAGE SKIN IS DENTED AT BS 740 BETWEEN STR 25L AND 26L. DENT WAS INSPECTED WITH HFEC AND FOUND TO BE CRACK FREE. DENT IS WITHIN LIMITS OF SRM 53-00-01 FOR CONTINUED SERVICE.

Part: GATE — GOUGED (R1 DOOR LOWER) · airframe 76,629 hrs · 22,361 cycles

R1 DOOR LOWER GATE HAS A DEEP GOUGE. INSTALLED NEW R1 LOWER GATE ASSY.

Part: GATE — GOUGED (R1 DOOR) · airframe 76,629 hrs · 22,361 cycles

R-1 DOOR LOWER GATE HAS A DEEP GOUGE. INSTALLED NEW R-1 LOWER GATE ASSY. WORK PERFORMED ON SCAL. NEW GATE INSTALLED PER SC AL NR AND RII INSPECTED.

Part: GATE — CORRODED (R1 DOOR) · airframe 76,629 hrs · 22,361 cycles

NR 1 DOOR UPPER GATE HAS EVIDENCE OF CORROSION AT LEVELING COMPOUND AREA. RIGHT DOOR UPPER GATE HAS EVIDENCE OF CORROSION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 76,629 hrs · 22,361 cycles

AIRPHONE ANTENNA DOUBLERS AT STA 1393 AND STA 1433 INSTALLED DURING SCAL C6 CHECK ON LP 9972327. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLERS AT STA 1393 AND STA 1433 REF SRM 53-00-01 REPAIR 3. ACCOMPLISHED ON SCAL LP 9972327.

Part: SWITCH — BROKEN (CABIN) · airframe 76,622 hrs · 22,358 cycles

DOOR 2L EMERGENCY LIGHT TEST SWITCH INOPERATIVE. FOUND TERMINAL BLADE BROKEN OFF OF SWITCH S10293 REF WDM 33-51-13 (PCN 564-0147) REPLACED SWITCH. FOUND WIRE TERMINAL SPADE CRACKED. REPLACED TERMINAL (PCN 562 -1675) REF SWPM20-30-15. TESTED EMERGENCY LIGHTING USING TEST SWITCH AND NORMAL OPERATION OBSERVED.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 76,622 hrs · 22,358 cycles

EEL PATH LIGHT AND STOWBIN EMERGENCY LIGHT INOPERATIVE ROW 25 TO 35. FOUND BATTERY AT POS M735 BAD REPLACED PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 76,622 hrs · 22,358 cycles

EMERGENCY LIGHT IN STOW BIN AT SEAT 30C INOPERATIVE. RELAMPED 1317 BULB. TESTED USING AFT FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH. NORMAL OPERATION OBSERVED.

Part: INDICATOR — FAULTY (CABIN TEMP) · airframe 76,250 hrs · 22,237 cycles

CABIN TEMP INDICATOR LIGHTS VERY DIM, DIFFICULT TO READ. INDICATIONS ARE READABLE.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 75,805 hrs · 22,109 cycles

SIDE WINDOW LEFT AND AFT OF CAPTAIN DELAMINATED. CAPTAIN'S NR 3 WINDOW HAS SMALL DELAM 7" AFT OF LOWER FWD CORNER, DELAM MEASURES APPROX 3.5" BY .75", AND MEETS VISUAL QUALITY PARAMETERS FOR CONTINUED SERVICE. NO EVIDENCE OF ARCING OR BUSBAR DISCOLORATION. WINDOW TO BE REPLACED AT NEXT OVERNIGHT MAINT OPPORTUNITY WHERE REPLACEMENT WINDOW IS AVAILABLE.

Part: ACM — FAULTY (AC BAY) · airframe 75,790 hrs · 22,106 cycles

ACRID SMELL IN COCKPIT, ABORTED T/O. WT 221K SPEED 125 KNOTS; ACCOMPANIED BY GRINDING NOISE. ACCOMPLISHED WHEEL AND BRAKE INSPECTION CHECK. HIGH ENERGY STOP INSPECTION 'CAUTION RANGE', CKS OK PER AMM. SMELL IN COCKPIT AND GRINDING NOISE COVERED IN LOG 2. COCKPIT GOT VERY HOT. L PACK INOP. SHUT OFF PACK AND TEMP RETURNED NORMAL. REPLACED LEFT ACM PER MM, OPS CHECK NORMAL.

Part: APU — SHUTDOWN · airframe 75,746 hrs · 22,092 cycles

APU AUTO SHUTDOWN AT GATE WHILE POWERING A-C. STARTED APU. APPLIED LOAD, OPS CHECKS NORMAL.

Part: GIRT BAR — OBSTRUCTED (L4 DOOR) · airframe 75,690 hrs · 22,074 cycles

THE 4L WILL NOT ARM. REMOVED A PLASTIC GLASS UNDER GIRT BAR.

Part: LAMP — INOPERATIVE (L2 DOOR SLIDE) · airframe 75,533 hrs · 22,029 cycles

DOOR 2L SLIDE ARMED LIGHT IS INOPERATIVE. RELAMPED INDICATOR. OP'S CHECKED GOOD.

Part: CONTROL VALVE — FAILED (RT ENGINE STARTE) · airframe 75,535 hrs · 22,030 cycles

RIGHT ENGINE STARTER EICAS MESSAGE DURING START, ENGINE STARTED NORMALLY. REPLACED STARTER CONTROL VALVE, LEAK AND OPS CHECKED.

Part: RELAY — FAULTED (RT ENGINE STARTE) · airframe 75,525 hrs · 22,026 cycles

RIGHT ENGINE START VALVE LIGHT AND STARTER EICAS MESSAGE. ENGINE STARTED NORMAL AND LIGHT WENT OUT. REPLACED RT SPEED CARD PER MM 77-12-01 AND RT ENG START RELAY 2 (K10250) AND RELAY 3 (K10351) MOTORED RT ENGINE TWO TIMES AND STARTED ONCE, OKAY.

Part: SKATE ANGLE — CRACKED (NR 1 PYLON) · airframe 75,245 hrs · 21,953 cycles

NR 1 ENG PYLON SKATE ANGLES CRACKED. EG MANDATED SKATE ANGLE REPLACEMENT. PARTS IN HAND. IN FUEL TANK REMOVING ANGLES. REF SMC1, INBD AFT SKATE ANGLE REMOVED FOR REPLACEMENT. STARTED PICKING UP FASTENER HOLES & INSTALLING NUT PLATES. REPLACED SKATE ANGLE. COMPLETED INSTALLATION.

Part: UNKNOWN — ODOR (CABIN) · airframe 75,193 hrs · 21,937 cycles

FLIGHT ATTENDANT NOTIFIED COCKPIT OF A SMOKE ODOR BY DOOR 2, ODOR WENT AWAY AFTER 5 MINUTES. ODOR WAS AROUND THE OVERWING EXITS ROW 20. CHECKED CEILING, ENTRY AND WINDOW LIGHTS AROUND EXIT ALL WORKING NORMALLY. CHECKED READING/CALL LIGHTS AND OPERATED VIDEO SYSTEM ALL NORMAL. FOUND READING LIGHT INOPERATIVE AT SEAT 20D. DROPPED CEILING PANEL AND OPERATED PACKS LEFT RIGHT NO ODOR. UNABLE TO DUPLICATE.

Part: PRESSURE SWITCH — FAILED (HYD PUMP) · airframe 75,176 hrs · 21,930 cycles

AC MOTOR PUMP, WITH HYDRAULIC PUMP OFF. LOW PRESSURE LIGHT DID NOT ILLUMINATE OR EICAS MESSAGE DISPLAY, CENTER PUMP NUMBER 1. EICAS MESSAGE DISPLAYS CORRECTLY. REPLACED LOW PRESSURE SWITCH.

Part: BOLT — BROKEN (ENGINE MOUNT) · airframe 74,350 hrs · 21,697 cycles

NR 2 ENGINE UPPER FWD ENGINE MOUNT HAS A LOWER ISOLATOR BOLT BROKEN. REPLACED BOLT.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 74,148 hrs · 21,635 cycles

AUTOSPEED BRAKE ILLUMINATED EICAS AND OVERHEAD.

Part: SEAL — LEAKING (NLG STRUT) · airframe 74,092 hrs · 21,620 cycles

AT GATE, FOUND NLG STRUT LEAKING OIL & LOW, CLEANED, TOWED ACFT TO HANGAR, NLG STRUT CONTINUES TO LEAK OIL. REPLACED NLG STRUT SEALS PER MM. FOUND LEAKING TO CEASE WITH NO DECREASE TO DIMENSION X. CHECKED EXTENSION AND FOUND IT 1.5" LOW. SERVICED STRUT WITH NITROGEN REF MM. SEAL REPLACED. SERVICED STRUT PER MM. CHECKED STRUT PER MM 32-11-02P.208 ITEM 6D. TAXIED ACFT. NO LEAKS NOTED.

Part: CONTROLLER — FAULTY (APU) · airframe 73,719 hrs · 21,499 cycles

APU WILL NOT START. NEXT MAINTENANCE STATION, INTERROGATE APU CONTROL UNIT PER FIM AND UPDATE ITEM WITH FAULTS FOUND. INTERROGATED FADEC. LAST FAULT SHOWS ABORT START, FAULTY UNITS SPD SNR 31, SPD SNR NR 2. PREVIOUS 4 FAULTS SHOW SHUTDOWN AND NO DATA ON FAULTY UNIT. T/S PER MM AND WDM. WRANG WIRING FROM FIREWALL TO BOTH SENSORS. ALL OKAY. RMV'D BOTH SENSORS. INSP FOR DAMAGE, NONE FOUND. ACP BORO BOTH BEARINGS LOOK CLEAN. REPLACED NR 1 SPEED 107441TS8. REINSTALLED ORIGINAL NR 2 PER MM. REPLACED ECU PER MM. RAN WITH TESTER. COULD NOT GET FAULT; BOTH RPM READINGS GOOD ALL TIME.

Part: CHECK VALVE — LEAKING (HYDRAULIC SYS) · airframe 73,680 hrs · 21,485 cycles

HYD LEAK IN RIGHT WING ROOT COMING FROM RETURN LINE CHECK VALVE. LEAKING ONE DROP EVERY EIGHT SECS, BECAME STEADY STREAM WHEN B-NUT WAS TIGHTENED. CHECK VALVE REMOVED. REPLACEMENT WOULD NOT THREAD ONTO O/B LINE WITHOUT SEVERELY BINDING. OLD VALVE & MS CAP GOES ON EASILY BY HAND. AOG'D 2 MORE VALVES WHICH ARE NOW PLANESIDE. ALSO, I/B LINE CLAMP BLOCK HAS ITS 3 MOUNTING BOLTS LOOSENED TO FACILITATE. REPLACED CHECK VALVE AND REINSTALLED CLAMP BLOCK.

Part: CIRCUIT CARD — FAULTY (FIRE DETECTION) · airframe 73,475 hrs · 21,426 cycles

LEFT ENG FIRE LP 1 EICAS STATUS MESSAGE APPEARS INTERMITTENTLY. TROUBLE SHOT WITH FIM AND RERACKED CARD M681 IN P54 FILE CABINET, NO HELP. USE FIM 26- 11-00-0101. MESSAGE STILL LATCHED SUSPECT CARD IS BAD. PCN FOR CARD 481-0040. REPLACED AFOLTS CARD 1, FIRE-OVHT TEST PASS NO MSG ON EICAS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,446 hrs · 21,417 cycles

4 FT FWD OF DOOR 2L JUST ABOVE FLOOR LEVEL SKIN DAMAGED. DENT APPROX 4" LONG 2.5" WIDE .200 DEEP. GOUGE IN MIDDLE OF DENT IS APPROX .020 DEEP. BLENDED DAMAGE AREA. ACCOMPLISHED NDT INSPECTION ON DAMAGED AREA. NO CRACKS FOUND ON EXTERIOR AND INTERIOR OF FUSELAGE SKIN. DEPTH OF MATERIAL REMOVE .014. CUT-OUT DAMAGED AREA PER SRM. FABRICATED AND INSTALLED A DOUBLER & FILLER PER REO G13875, REV. B. ALSO FABRICATED AND INSTALLED 2 SHEAR TIES PER DWG 140N2002. PER UAL EVA 81307.

Part: METERING VALVE — MALFUNCTIONED (NLG STEERING) · airframe 73,248 hrs · 21,364 cycles

AFTER TAXI FROM GATE-NOSE WHEEL STEERING JAMMED THEN SNAPPED TO THE LEFT FOR TURN ON TO RUNWAY. REPLACED NLG STEERING METERING VALVE PER MM. TAXI CHECKED GOOD.

Part: HINGE — BROKEN (ACCESS PANEL) · airframe 73,067 hrs · 21,311 cycles

GROUND POWER ACCESS PANEL, ONE HINGE IS BROKEN. DOOR REMOVED AND PLACED IN THE LOB. DOOR REMOVED AND PARTS PLACED IN COCKPIT.

Part: HINGE — BROKEN (GROUND POWER) · airframe 73,067 hrs · 21,311 cycles

GROUND POWER ACCESS PANEL, ONE HINGE IS BROKEN. DOOR REMOVED AND PLACED IN THE LOB. DOOR REMOVED AND PARTS PLACED IN COCKPIT. INF- :HINGE PCN 170-0975 SEE IPC 52-49-01-001 ITEM #260. INF- :HINGE 170-0975 PLACED ON OSTF X2511. *OPBLMOH* CDL REF: 52L (PARTS: 170-0975 H854-5 HINGE *X2511*)

Part: IDG — FAULTY (RIGHT) · airframe 73,016 hrs · 21,296 cycles

CREW REPORTS DURING TAXI RT GENERATOR CONTROL OFF LIGHT CAME ON. RIGHT GEN FIELD OFF LIGHT WAS ALSO ON. FIELD OFF RESET OK, BUT GENERATOR CONTROL WILL NOT RESET. REPLACED RIGHT IDG PER MM. LEAK AND OPS CHK OF RIGHT IDG OKAY.

Part: TRANSCEIVER — INOPERATIVE (WEATHER RADAR) · airframe 73,016 hrs · 21,296 cycles

WX RADAR INOPERATIVE. REPLACED CONTROL PANEL (P/N 622-5129-107; SERIAL# 142) PER MM. REPLACED WX RADAR TRANSCEIVER PER MM. REPLACED RADAR DRIVE UNIT. GROUND TEST PER MM. TESTS OKAY.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 72,935 hrs · 21,272 cycles

EXIT SIGN LENS LOOSE AT 15A. SECURED LENS.

Part: SKIN — DELAMINATED (FAN COWLING) · airframe 72,806 hrs · 21,232 cycles

NR 1 ENG INBD-RT FAN COWL HAS OUTER SKIN AREA OF FROST 9" BY 8" DUE TO FROZEN WATER IN CORE AND INNER SKIN DELAMINATION 14" BY 13" 14 INCH ALONG FORWARD TAPER OF HONEY COMB CORE AND AFT UP TO 13 INCHES FROM L/E OF CORE TAPER AREA OUT OF LIMITS PER SRM. NOTE F1 INCH MAX AND BEYOND INTERIM REPAIR LIMIT AND WET LAYUP LIMIT. NEEDS 350 DEGREE REPAIR. DELAM IS 3 INCH AFT OF LEADING EDGE ON INNER SKIN AT EDGE OF CORE TAPER AND IS FROM 12 INCH UP FROM LOWER EDGE TO 26 INCHES UP FROM LOWER EDGE. RPLD NR 1 ENG RT INBD FAN COWL, NO SERIAL NUMBER. NO DEFECTS NOTED.

Part: CONTROL PANEL — FAILED (CABIN PRESSURE) · airframe 72,649 hrs · 21,179 cycles

ALTITUDE CONTROLLER HAS FROZEN DIGITS IN LANDING ALT WINDOW. REPLACED CABIN PRESSURE SELECTOR PANEL AND PERFORMED OPS CHECKED PER MM.

Part: VALVE — FAULTY (APU) · airframe 72,511 hrs · 21,139 cycles

WITH APU BLEED SW ON, ONLY SHOWING 10 PSI. APU BLEED VALVE MANUALLY CLOSED, BREAKERS Q22 & P11 OPEN. CHECKED OPERATION OF BLEED VLV PER MM. OPERATION GOOD NEVER HUNG UP RE-INSTALLED CONN D3576. HOOKED TESTER UP FOUND SV TM VOLT OUT OF TOL. REPLACED SURGE VALVE PER MM.

Part: DUCT — CRACKED (CUSTOMER AIR) · airframe 71,407 hrs · 20,809 cycles

COCKPIT TEMP UNCONTROLLABLE. DUCT ASSY CPRSR INLET CRACK AND FROZEN ACM. DUCT REMOVED TO BE WELDED. FUSION WELD REPAIR ACCOMPLISHED. REPLACED ACM. SUCCESSFULLY LEAK CHECKED.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 71,249 hrs · 20,769 cycles

EMERGENCY FLOOR LIGHTING STRIP LOOSE BY FIRST CLASS CLOSET. LIGHTING STRIP NOT LOOSE. PLASTIC END CAP CAME OFF. REINSTALLED END CAP.

Part: ACM — FROZEN (LEFT) · airframe 71,226 hrs · 20,759 cycles

LEFT PACK TEMP UNABLE TO CONTROL. FOUND ACM FROZEN. REPLACED IAW MM. OPS OK.

Part: SWITCH — INTERMITTENT (HYD PUMP) · airframe 71,230 hrs · 20,762 cycles

NR 1 CENTER ELECTRIC HYDRAULIC PUMP LOW PRESSURE LIGHT INTERMITTANT. LIGHT FOUND TO BE INTERMITTENT. DEFERRED PER MEL. PUMP VERIFIED TO OPERATE NORMALLY ON EICAS. REPLACED NR 1 CENTER PRESSURE SWITCH PER MM. OPS OKAY. LIGHTS OPERATE NORMALLY.

Part: SEAL — LEAKING (NR 1 SPOILER) · airframe 70,910 hrs · 20,670 cycles

HYD FLUID DRIPPING FROM FLAP FAIRING OUTBOARD LEFT MOTOR. NR 1 SPOILER ROD END SEAL LEAKING APPROX 1 TO 2 DROPS PER CYCLE. REPLACED ACTUATOR.

Part: IDG — FAULTY (LT GENERATOR) · airframe 70,256 hrs · 20,469 cycles

LT GEN DRIVE LIGHT INOP, WORKS WITH TEST. GEN DRIVE LIGHT INOPERATIVE. REPLACED LT IDG, OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (EVAC SLIDE) · airframe 70,027 hrs · 20,392 cycles

DOOR 2R SLIDE LIGHT NOT ON WITH DOOR ARMED. RELAMPED, OPS CHECK OKAY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,845 hrs · 20,335 cycles

LT FWD INTERIOR OVERWING EMERGENCY L560 LIGHT IS INOPERATIVE. R & R LAMP IAW MM 33-51-010 PERFORMED OPS CHECK GOOD IAW MM ON NON ROUTINE 2190N00036.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,845 hrs · 20,335 cycles

EMERGENCY LIGHTS INOP FROM ROW 16 TO ROW 22. REPAIRED EMERGENCY LIGHTS FROM ROW 16 TO ROW 22 IAW MM.

Part: FEEDER CABLE — DISCONNECTED (CABIN) · airframe 69,845 hrs · 20,335 cycles

LT AISLE EMERGENCY LIGHTS BETWEEN SEAT ROW 15-22 ARE INOPERATIVE. TROUBLESHOT FOUND FEEDER WIRE ROW 17 WAS NOT CONNECTED. RECONNECTED IAW B757 MM. PERFORMED OPS CHECK IAW MM.

Part: SOCKET — BURNED (SEAT ROW 16ABC) · airframe 69,725 hrs · 20,300 cycles

DEBRIEFED INBOUND CREW, SMELL PRESENT THROUGHOUT ACFT. IAW SAMC TURNED OFF BOTH RECIRC FANS AND UTILITY BUSSES SMELL DISSIPATED. OPERATED AUDIO SYS, VIDEO SYS, AIRFONE, ALL SIGNS AND LIGHTING. FOUND OVERHEAD FLUORESCENT LIGHT AT ROW 16 ABC INOPERATIVE, WITH SOCKET BURNED AND ELECTRICAL SMELL AT BALLAST. REPLACED SOCKET AND BALLAST. OPERATED PACKS USING BOTH APU AIR AND ENGINE AIR. NO FURTHER EVIDENCE OF ELECTRICAL SMELL.

Part: SMOKE DETECTOR — FAULTY (AFT CARGO BAY) · airframe 69,625 hrs · 20,272 cycles

AFT CARGO DET 1 STATUS MESSAGE. CYCLED DETECTOR ASSY. NO AFT CARGO DET MSG NOTED, SYSTEM OP CHECKS GOOD IAW MM.

Part: EEC — MALFUNCTIONED (LT ENGINE) · airframe 69,141 hrs · 20,142 cycles

LT ENG EGT FLUCTUATED ON CLIMB 15K TO 22K BETWEEN ALMOST 0 - 510, ALL OTHER IND'S STABLE. REPLACED EEC. NO FURTHER FAULTS NOTED AFTER HIGH POWER ENGINE RUN. GOOD FOR SERVICE.

Part: METERING VALVE — FAULTED (NLG STEERING) · airframe 68,932 hrs · 20,086 cycles

CREW REPORTED STARTING TO TAXI, HAD NO NOSE WHEEL STEERING. ACCOMPLISHED TROUBLESHOOTING IAW MM. FOUND STEERING METERING VLV PROBLEM. RECONNECTED SUMMING LEVER LT AND RT. ALL SECURE. REPLACED NOSE WHEEL STEERING METERING VALVE.

Part: OUTFLOW VALVE — LEAKING (CABIN PRESSURE) · airframe 68,844 hrs · 20,064 cycles

DOOR LEAK AT 3L-R ACCOMPANIED BY HIGH PITCHED SQUEAL. PRESSURIZED TO 4.0 AND ON DESCEND BETWEEN 3.5 TO 3.0 HAD LOUD SQUEAL FROM OUTFLOW VALVE AREA. AMT IN CABIN STATED NOISE WAS VERY LOUD. REPLACED OUTFLOW VALVE.

Part: SKIN — DAMAGED (BS 648.5 S4L) · airframe 68,819 hrs · 20,054 cycles

LIGHTING STRIKE BLENDED AT STR 4L AND STA 648.5 DAMAGE MEASURES .375 WIDE BY 1.687 INCH LONG. SKIN THICKNESS MEASURES .050 IN UNBLENDED AREA, BLENDED AREA REMAINING THICKNESS MEASURES .033, TOTAL OF .017 MATERIAL MISSING. DAMAGE IS .250 BELOW SKIN LAP. REPAIR ZONE 'C'. CUT OUT DAMAGE USING .5 IN RADIUS. WILL NEED TO CLEAN UP CUTOUT AND EDDY CURRENT OPENING. ALSO DRILLED OUT RIVETS IN SKIN LAP. REPAIR ZONE 'C'. CUT OUT DAMAGE. CLEANED UP CUTOUT AND EDDY CURRENT OPENING. ALSO DRILLED OUT RIVETS IN SKIN LAP. PERFORMED HFEC INSP OF CUTOUT NO DEFECTS NOTED. COMPLETED PATCH REF EVA UA-73738-B.

Part: STATOR — FAULTY (POSITION 2) · airframe 68,803 hrs · 20,047 cycles

RT ENGINE PRI CONT STATUS MSG. AUTO THRT DISCONNECTED SEVERAL TIMES AS REPR BLANKED. READ EPCS MESSAGES AND FOLLOW FIM 73-21-00 FIG 114. COPY FAXED TO OPS. EPCS MSGS ARE P PDIU EEC, S PDIU EEC AND S 274-18.CHECKED ENG NR 2 CLEARED MSGS, REPLACED PMA. REPLACED PDIU. RAN ENGINE IAW JRH. RAN ENGINE UP TO 80 PERCENT, N2 NO FAULTS WERE NOTED, NO MSG'S.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 68,785 hrs · 20,040 cycles

CTR HYD QTY LIGHT AND EICAS ILLUMINATED. CTR HYD FLUID IS LOW. FLUID LEAKING FROM PINHOLE LEAK ON ONE OF THE SUPPLY LINES ON THE ELEVATOR CONTROL VALVES ON THE ELEVATOR TORQUE BOX. LEAK WILL FUMIGATE TAIL AREA WITH JUST PRESSURE ON CTR HYD SYS. WITH NO MOVEMENT OF ELEVATOR. DID NOT DETERMINE YET WHICH LINE IS LEAKING. FOUND LINE. MFG NEW LINE AND PRESSURE TESTED. FOUND QTY NORMAL. NO QTY LIGHTS OR EICAS MESSAGE. ACCOMPLISHED EXTERNAL VISUAL CHK AND FOUND NO ACTIVE LEAK, CTR HYD RESERVOIR IS FULL. SUSPECT BAD EICAS INDICATION TRANSMITTER. COMPLIED WITH MEL CARD. SVC'D CTR HYD SYS TO FULL. LEAK CKD TAIL AREA, GEAR AREA. FOUND LT MLG DOOR ACTUATOR SEEPING. NO RUNNING LEAKS WERE NOTED.

Part: PCA — NO TEST (RT ELEVATOR) · airframe 68,701 hrs · 20,015 cycles

RT ELEV RT HYD PCA FAILS ELEV PCU MONITOR SYS TEST. REMOVED RT ELEVATOR RT HYD PCA. REPLACED RT ELEVATOR RT PCA, OPS CHECK AND LEAK CHECK OK.

Part: CONTROLLER — FAULTY (APU) · airframe 68,454 hrs · 19,946 cycles

NO PNEUMATIC PRESSURE WITH APU RUNNING AND VALVE OPEN. APU BLEED VALVE OPENS AND CLOSES NORMALLY. REPLACED APU CONTROLLER. CHECKS GOOD.

Part: COMPUTER — FAULTY (ELEVATOR FEEL) · airframe 68,035 hrs · 19,821 cycles

ON DEPARTURE, STATUS MSG ELEV FEEL CHRONIC. REPLACED ELEVATOR FEEL COMPUTER. LEAK CHECKED UNIT, NO LEAKS NOTED. CYCLED STAB, NORMAL.

Part: FUEL TANK — LEAKING (CENTER) · airframe 67,573 hrs · 19,688 cycles

FUEL LEAKING FROM LT WHEEL WELL FROM CTR TANK. FOUND LEAK IN CTR LT REAR SPAR LWR CORNER SEALANT REPAIRED W A-HALF AND B-HALF AT 1400HRS. NEEDS LEAK CHECK REPAIR. NO LEAKS FOUND.

Part: CONTROLLER — MALFUNCTIONED (FUEL SYS) · airframe 67,304 hrs · 19,608 cycles

FUEL DRIPPING OUT OF LEFT PACK EXHAUST. WHILE DEFUELING CENTER TANK THE LEFT CENTER TANK FUELING VALVE WAS LEAKING APPROX 25 DROPS A SECOND. REPLACED LEFT CENTER TANK FUELING VALVE. ACCOMPLISHED OPS AND LEAK CHECK OF CTR TANK CHECK VALVE LT.

Part: BOTTLE — DEFECTIVE (OXYGEN SYSTEM) · airframe 67,173 hrs · 19,574 cycles

FWD CABIN O2 BOTTLE PRESSURE READS ZERO. REPLACED O2 BOTTLE.

Part: LEVER — OUT OF TOLERANCE (PAX DOOR SLIDE) · airframe 66,917 hrs · 19,498 cycles

PASSENGER ENTRY-SERVICE DOORS R AFT EVAC SLIDE ARM LEVER DIFFICULT TO POSITION. CLEANED AND LUBED LINKAGE, OPS CHECK GOOD.

Part: THRESHOLD — DAMAGED (FUSELAGE) · airframe 66,908 hrs · 19,495 cycles

PRESSURIZED DOOR 4R, FOUND LOWER FWD & AFT CORNERS OF DOOR FRAME MISSING REN WHERE THRESHOLD PLATE MEETS. APPLIED TAPE TO AREA, PRESSURIZED AIRCRAFT STILL LEAKS AT LOWER FWD AREA & THRESHOLD PLATE LOOKS DAMAGED WITH DENTS IN CORNER & CENTER SECTION OF THRESHOLD PLATE HAS TWO HOLES WHERE PREVIOUS WELDS WERE. SENT THRESHOLD TO SFO TO HAVE THEM REPAIR DAMAGE. INSTALLED REPAIRED THRESHOLD PLATES AND SEALED. INSTALLED GIRT BAR PLATES AND ADJUSTED, OP'S CHECKED GOOD. INSPECTED AS REQUIRED. OP CHECKS GOOD.

Part: PDU — MALFUNCTIONED (TE FLAP) · airframe 66,816 hrs · 19,468 cycles

UNABLE TO DROP TRAILING EDGE FLAP ELEC. REMOVED TRAILING EDGE POWER DRIVE UNIT. INSTALLED NEW ALT FLAP DRIVE MOTOR. ACCOMPLISHED FUNCTIONAL TEST WITH NO PROBLEMS.

Part: IDG — MALFUNCTIONED (LT GENERATOR) · airframe 66,500 hrs · 19,377 cycles

LEFT GENERATOR FIELD OFF LIGHT ON PANEL BEHIND F/O. REPLACED LT ENG GCU. SERVICED BOTH LT & RT IDG OIL LEVELS. BITE ON BCU SHOWS NO FAULTS. RESET OVERHEAD ENG GEN CONT SWITCHES. RAN ENGINE AND VOLTS AND FREQUENCIES NORMAL. SHUTDOWN ENGINE AND NO FIELD LIGHT. INSTALLED IDG. ACP RUN AND CHECKS BPCU CLEAN. ACCOMPLISHED BITE ON BPCU, HAD LT IDG SERVICE OIL. SERVICED IDG OIL. RAN ENGINE, HAD OIL LEAK FOR IDG FILL LINE AT IDG UNION. REPLACED UNION AND O-RING. SVC'D IDG AND RAN ENGINE. NO LEAKS AT THIS TIME. LT ENGINE IDG WORKED NORMAL DURING VERIFICATION FLIGHT.

Part: IDG — LEAKING (RT ENGINE) · airframe 66,078 hrs · 19,252 cycles

FLUID DRIPPING FROM RT ENG IDLE RUN ENG FOUND FLUID LEAKING FROM NR 1 DRAIN TUBE THERMAL RELIEF VENT. IDG WAS NOT OVER SERVICED AND NO FUEL PRESENT. REPLACED NR 2 IDG.

Part: CHARGER — FAILED (APU BATTERY) · airframe 65,521 hrs · 19,095 cycles

APU WILL NOT START. REPLACED BLOWN APU AIR SURGE DUCT & CLAMP. REPLACED APU BATTERY & BATTERY CHARGER.

Part: FMC — FAILED (LEFT) · airframe 65,429 hrs · 19,067 cycles

LEFT FMC FAILURE. RTFL. REPLACED LEFT FMC, CHECKS OKAY.

Part: IDG — MALFUNCTIONED (RIGHT) · airframe 65,419 hrs · 19,063 cycles

RT GENERATOR PROBLEM. RTFL. REPLACED RT ENGINE IDG.

Part: STARTER — FAULTY (APU) · airframe 65,028 hrs · 18,951 cycles

APU FAILED TO START. FAULT LGT ILLUM AND EICAS MSG. APU FAULT DISPLAYED. FOUND STARTER DRAGGING DOWN BATTERY VOLT AND GETTING HOT. REPLACED STARTER, OPS CHECK GOOD.

Part: ACTUATOR — FAULTY (CENTER TANK) · airframe 64,966 hrs · 18,931 cycles

FUELER UNABLE TO FUEL CTR TANK. FOUND LT CTR TANK FUELING ACTUATOR SHOWING OPEN BUT NOT OPEN. REPLACED ACTUATOR. BOTH FUELING VALVE OPERATE NORMAL.

Part: STARTER — FAULTY (APU) · airframe 64,928 hrs · 18,921 cycles

APU WILL NOT START. APU CHECK SHOWS BAD STARTER. REPLACED STARTER, NO HELP, NO START. APU BATTERY DROPS TO 12V ON START BUT NO RPM. TRIED TO SPIN TURBINE FROM EXHAUST WOULD ONLY MOVE AN INCH BACK AND FORTH, LOCKED UP. PULLED CHIP DETECTORS PER SAMC FOUND LOTS OF METAL SHAVINGS. REPLACED CHIP DETECTORS INTACT. TRIED TO TURN AT STARTER NO MOVEMENT, CLUTCH OK. CHECKED MAG CHIP DETECTORS THE 2 AT GEARBOX ARE FULL OF METAL, THE OTHER 2 OK. REPLACED APU.

Part: FUEL CONTROL — FAILED (APU) · airframe 63,524 hrs · 18,531 cycles

AIRCRAFT RTFL DUE TO APU NO START AT ALTITUDE. PILOT REPORTS: APU HUNG AT 27 PERCENT DURING ALTITUDE OF 34,000 MSL AND THEN FAULTED, SHUT DOWN. REPLACED APU FUEL CONTROL DUE TO FAULTY FUEL SOLENOID.

Part: ANTI-ICE VALVE — FAULTY (RT WING) · airframe 63,433 hrs · 18,507 cycles

AFTER HIGH POWER RUN FOUND RIGHT WING ANTI ICE VALVE FAILED TO OPEN CORRECTLY. REPLACED RT WING ANTI ICE VALVE.

Part: START VALVE — MALFUNCTIONED (LT ENGINE) · airframe 63,360 hrs · 18,487 cycles

L ENG STARTER EICAS WHEN START SELECTOR SWITCH PLACED INTO GND. REPLACED START VALVE AND CHECK OKAY.

Part: IDG — FAULTY (RT ENGINE) · airframe 63,094 hrs · 18,409 cycles

R GEN DRIVE FAULTY. REPLACED RIGHT ENGINE IDG. OPS CHECKED GOOD.

Part: PUMP — LEAKING (NR 1 ENGINE) · airframe 63,036 hrs · 18,393 cycles

LOSS OF HYDRAULICS. FLIGHT DIVERTED. INBD CREW REPORTS PTU FAILED TO ENGAGE UPON FLUID LOSS VIA NR1 ENG EDP. NEED TO PERFORM HYDRAULIC PTU OPERATIONAL TEST. ACCOMPLISHED OPERATIONAL TEST PER MM 29-22-00 PTU CHECKS OK. ENGINE DRIVEN PUMP (EDP) - HYDRAULIC LOW PRESS LIGHT ILLUMINATED. EICAS MESSAGE 'HYD ENG PUMP' DISPLAYED BUT EICAS MESSAGE 'HYD SYS MAINT' NOT DISPLAYED-LEFT SYSTEM. HYD FLUID RUNNING FROM NR 1 ENG HYD PUMP DRIVE PAD CAVITY DRAIN TUBE. REPLACED NR 1 CASE DRAIN FILTER & LEAK CHECKED DUE TO ENG DRIVEN PUMP LEAKING. REPLACED NR 1 ENG EDP AND APPLICABLE FILTERS. PER SFOLM LEFT ELECTRIC AC PUMP WILL NEED PRESSURE AND CASE DRAIN FILTERS REPLACED. REPLACED FILTER PER IPC 29 -11-18 AND LEAK CHECKED.

Part: HYDRAULIC SYSTEM — UNKNOWN · airframe 63,036 hrs · 18,393 cycles

LOSS OF HYDRAULICS. FLIGHT DIVERTED.

Part: IGNITER — FAULTY (RT ENGINE) · airframe 62,939 hrs · 18,364 cycles

RIGHT ENGINE DID NOT LIGHT OFF WITH IGNITION SELECTED TO NR 2 SYSTEM. LIGHT OFF OK IN "BOTH". DUE TO HISTORY REPLACED BOTH IGNITER PLUGS. REPLACED LEADS BOTH. REPLACED EXCITER BOX BOTH. TESTED GOOD.

Part: TARGET — CONTAMINATED (DOOR) · airframe 62,928 hrs · 18,362 cycles

LEFT WING SLIDE INDICATION. FLIGHT DIVERTED. MECHANICS STATED THAT THERE WERE PAINT OVER-SPRAY ON THE TARGET AND SWITCH. AFTER REMOVAL OF THE OVER-SPRAY, A SLIGHT ADJUSTMENT TO THE DOOR SWITCH TO ENSURE WITHIN LIMITS, AND OPS CHECKING THE DOOR SEVERAL TIME TO ENSURE THE MESSAGE WENT AWAY THIS ITEM HAS BEEN SIGNED OFF.

Part: SWITCH — FAULTY (FUEL SYSTEM) · airframe 62,786 hrs · 18,321 cycles

RIGHT CENTER FUEL PUMP PRESSURE LIGHT ON. SWITCH IS FAULTY. REPLACED THE RT CENTER PRESSURE PUMP SWITCH, OPS CHECKED NORMAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 62,751 hrs · 18,311 cycles

PREVIOUS REPAIR STA 610, STR 17L, EXT FUSELAGE HAS DENT. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER REPAIR.

Part: SKIN — CORRODED (RT WING) · airframe 62,751 hrs · 18,311 cycles

RIGHT WING, UPPER SKIN AT WBL 95, STA 970 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER REPAIR.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 62,751 hrs · 18,311 cycles

STRINGER 18L STA 610, SEVERAL HOLES PREVIOUSLY FREEZE PLUGGED. ACCOMPLISHED MAJOR REPAIR AT GSO.

Part: SKIN — DENTED (FUSELAGE) · airframe 62,751 hrs · 18,311 cycles

DENT IN CROWN SKIN STA 900, STR 2L TO 3L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER.

Part: COVER — CRACKED (EVAC SLIDE) · airframe 62,751 hrs · 18,311 cycles

EMERGENCY EVAC SLIDE 2R DOOR CARRIER BOX CRACKED AT SIDE. REPLACED SLIDE AT DOOR 2R.

Part: FRAME — DENTED (FUSELAGE) · airframe 62,751 hrs · 18,311 cycles

AFT PIT STA 1480 BETWEEN STR 25L AND 26L FRAME IS DENTED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FUSELAGE FRAME. INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 62,751 hrs · 18,311 cycles

AFT PIT STA 1540 FRAME DENTED BETWEEN STR 22L AND 23L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED FRAME SECTION AND INSTALLED DOUBLER REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,751 hrs · 18,311 cycles

MAIN CABIN T-CAP AT BS 1640, RBL 58 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF T-CAP FROM RBL 0 TO RBL 64. FABBED AND INSTALLED NEW SECTION.

Part: FRAME — DENTED (FUSELAGE) · airframe 62,751 hrs · 18,311 cycles

AFT PIT STA 1500 FRAME DENTED BETWEEN STR 24L AND 26L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER FRAME REPAIR.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 62,751 hrs · 18,311 cycles

STR 15L AT BS 645 IS CRACKED AT FASTENER HOLE, APPROX 3-16 INCHES IN LENGTH, MARKED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF STR 15L. INSTALLED SPLICE REPAIR.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 62,751 hrs · 18,311 cycles

MAIN CABIN T-CAP AT BS 365, RBL 10 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF T-CAP RBL 0 TO RBL 64. INSTALLED NEW SECTION.

Part: FRAME — DENTED (FUSELAGE) · airframe 62,751 hrs · 18,311 cycles

AFT PIT STA 1600 FRAME DENTED AT STR 22L TO 23L. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR.

Part: TRIGGER — FAULTY (EVAC SLIDE) · airframe 62,751 hrs · 18,311 cycles

RIGHT OVERWING SLIDE FAILS PNEUMATIC DEPLOY. TRIGGER IS FAULTY. REPLACED TRIGGER. OP CHECKS GOOD.

Part: RUB STRIP — CRACKED (R2 DOOR GATE) · airframe 62,751 hrs · 18,311 cycles

DOOR R2 LWR GATE LWR RUB STRIP CRACKED. FOUND CORROSION AND OVERSIZED HOLES FOR STRIP ATTACH. REPLACED GATE.

Part: FITTING — CORRODED (L4 DOOR) · airframe 62,751 hrs · 18,311 cycles

DOOR 4L LWR FWD LOCKING CRACK FITTING CORRODED BEYOND LIMITS. REPLACED THE CRANK FITTING. REPLACED THE CRANK FITTING.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 62,751 hrs · 18,311 cycles

R-2 DOOR REQUIRES A REPAIR DOUBLER AT THE UPPER HINGE CUT-OUT OF FRAME. MAJOR REPAIR ACCOMPLISHED, INSTALLED A FRAME DOUBLER REPAIR.

Part: FLOORBEAM — CORRODED (BS 324) · airframe 62,751 hrs · 18,311 cycles

MAIN CABIN T-CAP AT BS 324, RBL 58, IS CORRODED BEYOND LIMITS. *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF T-CAP. FABRICATED & INSTALLED A NEW REPAIR SECTION.

Part: IDG — INOPERATIVE (NR 2) · airframe 62,349 hrs · 18,202 cycles

RIGHT GENERATOR DROPPING OFF. *S/D* NO IDG HISTORY. REPLACED NR 2 ENG IDG -OPS AND LEAK CHECKED GOOD DURING RUNS, ALL GENERATION OUTPUT NORMAL.

Part: CONNECTOR — DIRTY (FIRE LOOP) · airframe 61,772 hrs · 18,048 cycles

EICAS MSG - LEFT ENGINE FIRE LOOP 1. DIRTY CONNECTION. CLEANED ALL FIRE LOOP CONNECTORS ON NUMBER 1 ENG, SYS OPS CHECKED OK.

Part: CONNECTOR — LOOSE (LT ENG FIRE LOOP) · airframe 61,503 hrs · 17,970 cycles

EICAS MSG - FIRE OVHT SYS-. FIRE OVHT TEST PANEL SYS FAIL LIGHT ON: EICAS MSG - L ENG FIRE LP 1 -. CREW COMMENTS: EICAS STATUS MESSAGE LENG FIRE LP 1. LOOSE CONNECTOR IN HOT SECTION. SECURED LOOSE CONNECTOR.

Part: FILTER — DIRTY (COOLING FAN) · airframe 61,484 hrs · 17,966 cycles

EQUIP COOLING OVHT LT ON OVH PANEL AND FWD EICAS ILLUM INTERMITTENT. SUPPLEMENTAL DATA UPDATE CAUSE, EQ COOLING FAN FILTER DIRTY. REPLACED EQ COOLING FAN FILTER, OPS ARE NORMAL.

Part: CONTROL SYSTEM — MALFUNCTIONED (CABIN TEMP) · airframe 61,354 hrs · 17,929 cycles

CAN'T CONTROL COCKPIT OR CABIN TEMP WITH OR WITHOUT TRIM AIR EITHER TO HOT OR TO COLD.

Part: LANYARD — UNSECURE (R4 DOOR SLIDE) · airframe 61,330 hrs · 17,922 cycles

DOOR 4R WILL NOT ARM. FOUND SLIDE LANYARD INTERFERING. SECURED LANYARD, OPS ARMS/DISARMS NORMALLY.

Part: WIRE — ARCED (GALLEY COFFEMAKE) · airframe 61,104 hrs · 17,861 cycles

SMOKE AND ARC'S IN FWD GALLEY PER CREW. FOUND WIRE ON TOP OF COFFEE MAKER M10 THAT HAD BEEN GROUNDED AND ARCING. REPLACED COFFEE MAKER M10-ALL OPS WERE GOOD

Part: SMOKE GOGGLES — CRACKED (1ST OFFICER'S) · airframe 61,050 hrs · 17,848 cycles

F/O SMOKE GOGGLES ARE CRACKED. REPLACED GOGGLES.

Part: LANYARD — OUT OF POSITION (R 1 DOOR) · airframe 60,975 hrs · 17,829 cycles

FLIGHT ATTENDANT COULD NOT ARM DOOR ONE RIGHT BEFORE PUSHBACK. FOUND LANYARD OUT OF POSITION, INTERFERING WITH MECHANSIM. RESTOWED LANYARD ROPE. DOOR 1R ARMS DISARMS OK.

Part: UNKNOWN — SMOKE (CABIN) · airframe 60,439 hrs · 17,672 cycles

RTFL WITH SMOKE IN THE CABIN. ODOR EMINATED FROM 1ST CLASS TOWARD BACK, TURNING VIDEO EQUIP OFF REDUCED THE ODOR FOR A WHILE, THEN RETURNED. LIGHT HAZE IN CABIN EVIDENT. RAN BOTH LT AND RT PACKS INDIVIDUALY NO SMOKE OR ODOR NOTICED. RAN ENTIRE VIDEO SYSTEM AND INSPECTED LIGHT BALLEST IN FWD CABIN NO SMOKE OR ODORS NOTICED. RAN ALL FWD AND MID GALLEY SYSTEMS NO DESCRIPANCIES. NEVER REPEATED.

Part: O-RING — OUT OF POSITION (DOOR 1R) · airframe 60,202 hrs · 17,610 cycles

DR 1R NO ARM AT DEPARTURE. FOUND O-RING IN THE WAY OF ARMING LEVER. REPOSITIONED O-RING, ARMS/DISARMS OK.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 59,196 hrs · 17,338 cycles

OVERHEAD EEL LIGHT OUT AT DOOR 2L.

Part: COUPLER — INOPERATIVE (HF SYSTEM) · airframe 59,170 hrs · 17,331 cycles

RIGHT HF INOPERATIVE IN TRANSMIT. TRIED NEW TRANCEIVER NO HELP. SWAPPED RADIO CONTROL PANELS, NO HELP. REPLACED RIGHT HF COUPLER, CHECKED OK.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 57,213 hrs · 16,740 cycles

NR 2 PYLON INBOARD SKIN IS CRACKED AT THE MOST FWD ACCESS HOLE, 2:00 O'CLOCK POSITION. [SUP 06-06-07] ACCOMPLISHED REPAIR WITH UA ENGINEERING SPECIFICATION.

Part: WIRE — BURNED (FWD CARGO BAY) · airframe 57,213 hrs · 16,740 cycles

FOUND BURNED WIRE BUNDLES & SHIELDED WIRES DAMAGED ALONG WITH INTERCOSTAL AND FLOOR STRUCT AT STA 680 FWD PIT CEILING. FOUND WIRES W4104-0082-20 & W4104-0090-20 SHORTED TO GROUND. RIGHT RECIRC FAN CIRCUIT BREAKER C337 ON P37 PANEL TRIPPED. PUSHING C/B IN ACFT RESULTED IN LOSS OF RT BUSS POWER. FOUND WIRES W4104-0082-20 & W4104-0090-20 SHORTED TO GRND. (350 OHMS & 1.26 KOHMS) ORDERED WTR HEATER TAPE (B118) GOES TO WIRE W4104-0090-20. STILL NEED TO ISOLATE WIRES FROM SPLICE (SP285)TO LOCATE PROBLEM WITH MID FWD TOILET DRAIN HTR GASKET (B10112) OR MID FWD DRAIN LINE HTR TAPE. FLOORBEAM SUPPORT MFG AND INSTD. RMVD DMG INTERCOSTAL. MAIN ACFT BATTERY MAIN POWER CONNECTOR SAFETIED WITH BREAK AWAY WIRE.

Part: WIRE — FAULTY (EMERGENCY LIGHT) · airframe 57,162 hrs · 16,724 cycles

A-ZONE FLOOR EEL INOP FROM SEAT 3 TO SEAT 6. REPAIRED CABLE. OPS CHECKED GOOD.

Part: GIRT BAR — OUT OF ADJUST (L3 DOOR) · airframe 57,098 hrs · 16,703 cycles

FOUND DOOR 3L HARD TO DISARM. SECURED LOWER LINER AND ADJUSTED SLIDE GIRT. OPS CHECKS OK. ACCOMPLISHED INSPECTION, DOOR ARMS AND DISARMS NORMALLY. SECURED LOWER LINER AND ADJUSTED SLIDE GIRT BAR. NO COMPONENTS REPLACED.

Part: EEC — FAULTY (NR 2 ENGINE) · airframe 56,094 hrs · 16,406 cycles

EN ROUTE TO HNL THE NR 2 ENGINE SHUT DOWN. *S/D* RIGHT ENG FLAMEOUT AT FL400. SUCCESSFUL RELIGHT AT FL300. REPLACED EEC, FMU AND PMA. ACCOMPLISHED ENGINE LEAK AND ACCEL-DECEL CHECKS.

Part: VALVE — UNSERVICEABLE (ESCAPE SLIDE) · airframe 55,712 hrs · 16,302 cycles

LOW BOTTLE PRESSURE. *S/D* FILL VALVE WAS LEAKING. REPLACED WITH A NEW FILL VALVE.

Part: GENERATOR — CRACKED (APU) · airframe 54,057 hrs · 15,840 cycles

APU FAULT LT ON AFTER 3 START ATTEMPTS NO START. FOUND NO OIL IN APU. FOUND CRACK ON TOP OF GEN AT 1200 POSITION APU GENERATOR SHARES THE OIL SYSTEM AND RESERVIOR WITH THE APU. THE LINE AND APU SHOP HAS HISTORY OF GENERATOR HOUSINGS CRACKING IN THE SAME FASHION AS THIS EXAMPLE. OIL LEAKS FROM THE GENERATOR CRACK, DEPLETING THE SUPPLY OF OIL OF THE APU. THE APU WILL HAVE A "LOW OIL PRESSURE" PROTECTIVE SHUTDOWN. SUBSEQUENT START ATTEMPTS WILL BE UNSUCCESSFUL UNTIL THE OIL SYSTEM IS SERVICED AND THE ECU (ELECTRONIC CONTROL UNIT) FAULTS ARE CLEARED. THEREFORE, WITHOUT OIL IN THE SYSTEM, ANY ATTEMPT TO START THE APU AT ALTITUDE WILL BE UNSUCCESSFUL.

Part: RELIEF VALVE — LEAKING (ESCAPE SLIDE)

EES WAS TEST FIRED AND PRESSURE RECORDED GOOD. HOWEVER, THE BOTTOM TUBE WENT FLAT WITHIN 5 MINUTES OF INFLATION PRESSURE RELIFE VALVE FOUND LEAKING. PRESSURE RELIEF VALVE ASSEMBLY WAS REPLACED.

Part: COMPRESSOR — SURGES (NR 2 ENGINE) · airframe 48,824 hrs · 14,296 cycles

DIVERTED TO HNL DUE TO NR 2 COMPRESSOR SURGE. FOUND VSV SYSTEM 0.125 INCHES OUT OF RIG, ALL OTHER CHECKS OKAY.

Part: WARNING LIGHT — ILLUMINATED (APU OIL SYS) · airframe 47,573 hrs · 13,941 cycles

APU SHUTDOWN IN DUE TO OIL QTY MESSAGE AND RIGHT GENERATOR OFF EICAS MESSAGE.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 45,446 hrs · 13,354 cycles

STA 590 AND BS 638.5 STR 14L -19L IS DENTED. INSTALLED DOUBLER REPAIR.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 45,446 hrs · 13,354 cycles

FRAME AT BS 1681 WL 208 IS DAMAGED. INSTALLED FRAME DOUBLER REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 45,446 hrs · 13,354 cycles

EXTERNAL FUSELAGE SKIN AT BS600 STR 16L - 19L IS DAMAGED. INSTALLED DOUBLER AND FILLER REPAIR.

Part: ENGINE — FLUCTUATES (NR 2) · airframe 48,628 hrs · 14,238 cycles

DIVERTED TO HNL DUE TO NR 2 ENGINE POWER FLUCTUATION. AS A PRECAUTIONARY MEASURE BOROSCOPED ENGINE TO CHECK COMPRESSOR HEALTH, RECHECKED CHIP DETECTORS AND OIL FILTER. ALSO REPLACED 10TH STAGE CHECK VALVE.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE)

LOW BOTTLE PRESSURE. CAUSE NOT FOUND. BOTTLE TOPPED OFF AND CHECKED FOR LEAKS. OSV, WINSLOW, HAS ADDED ULTRASONIC LEAK DETECTION TO BOTTLE INSPECTION PROCESS. THERE WAS NO FAULT FOUND.

Part: SKIN — CORRODED · airframe 39,976 hrs · 11,860 cycles

RH UPPER WING SURFACE CORRODED. WS 159, WBL 77.5 TO 79.5 BS 996 TO 1005, MAJOR REPAIR ACCOMPLISHED.INSTALLED REPAIR ANGLES ON STRINGERS AND ROTOPEEN SKIN.

Part: FRAME — CORRODED · airframe 39,976 hrs · 11,860 cycles

FRAME CORRODED. STA 1680, WL208-211, RBL 65. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER AND TRIPLER ANGLES.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,976 hrs · 11,860 cycles

CABIN FLOOR BEAM STATION 310 RBL 39 TO 42 MATERIAL REMOVED EXCEEDS LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED SUPPORT ANGLE-REINFORCEMENT STRAP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,976 hrs · 11,860 cycles

FORWARD GALLEY FLOOR BEAM UPPER CAP REPAIR PLATE IS CORRODED AT BODY STATION 365 FROM RBL 13 TO RBL 54. MAJOR REPAIR ACCOMPLISHED. INSTALLED SUPPORT ANGLE-REINFORCEMENT STRAP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,976 hrs · 11,860 cycles

CABIN STATION 640 FLOOR BEAM CAP CORRODED FROM LBL 43 TO RBL 23. MAJOR REPAIR ACCOMPLISHED. STRAP REPAIR INSTALLED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,976 hrs · 11,860 cycles

CABIN FLOOR SUPPORT UNDER DRAIN GUTTER AT STATION 1640 RBL 65 STRINGER 17R HAD EXCESSIVE MATERIAL REMOVED DURING CORROSION CLEANUP. MAJOR REPAIR ACCOMPLISHED. REMOVED AND INSTALLED NEW BOEING FLOOR SUPPORT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,976 hrs · 11,860 cycles

CABIN FLOORBEAM STATION 324 RBL 57 TO 61 MATERIAL REMOVED EXCEEDS LIMITS. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED MATERIAL AND INSTALLED T-CAP SPLICE REPAIR.

Part: CREASE BEAM — CORRODED · airframe 39,976 hrs · 11,860 cycles

RIGHT HAND AFT CABIN BETWEEN STATION 1500 TO 1600 CREASE BEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED DAMAGED SECTION AND INSTALLED DOUBLER AND TRIPLER.

Part: FRAME — DENTED · airframe 39,976 hrs · 11,860 cycles

FORWARD PIT FRAME STATION 600 LBL 35 DENTED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. DAMAGE REMOVED. INSTALLED DOUBLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,976 hrs · 11,860 cycles

CABIN FLOOR BEAM UPPER CAP HAD EXCESS MATERIAL REMOVED DURING CORROSION CLEAN UP AT STATION 680 RBL 5 TO RBL 12, TWO SPOTS STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR.

Part: STRINGER CLIP — CORRODED · airframe 39,976 hrs · 11,860 cycles

STA. 1480, STRINGER 27L ATTACHMENT CLIP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. STRINGER CLIP WAS REPLACED.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 39,976 hrs · 11,860 cycles

CREASE BEAM WEB AT STA 741-743, RBL 68, STRINGER 17 RT AT WATERLINE 208 NEEDS REPLACING. MAJOR REPAIR ACCOMPLISHED. MID CABIN RT CREASE BEAM WAS REPLACED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,846 hrs · 11,273 cycles

FLOOR EEL LIGHT STRIP AT SEAT 13 ABC WILL NOT ILLUMINATE. REPLACED FLOOR EEL LIGHT SEGMENT AT SEAT 13 ABC.

Part: VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 37,170 hrs · 11,092 cycles

NUMBER 1 ENGINE EGT REACHED 648 DEGREES ON CLIMBOUT. 14TH STAGE CONVERTER VALVE WAS REPLACED DUE TO MESSAGES. ON THE FOLLOWING FLIGHT THE ENGINE HAD HIGH EGT AT TAKEOFF AND RETURNED TO FIELD. CONVERTER VALVE AND THE 14TH STAGE BLEED VALVE (BEANPOT) WAS REPLACED. ENGINE CHECKED GOOD AFTER THIS. SHOP FINDINGS: SERVO VALVE ON CONVERTER VALVE FAILED. 14TH STAGE BLEED VALVE (BEANPOT) CHECKED GOOD.

Part: TRANSFORMER — FAILED (SPOILER SYS) · airframe 33,586 hrs · 10,154 cycles

SPOILER EICAS AND OVERHEAD LIGHTS ILLUMINATED. FLIGHT LEVEL 380. *S/D* FAULTY RVDT ON SPOILER PCA CAUSING EICAS MESSAGE. REPLACED ROTARY VARIABLE DIFFERENTIAL TRANSFORMER ON SPOILER PCA NR 6 AND NR 7.

Part: STRAP — MISSING (PAX DOOR SLIDE) · airframe 31,445 hrs · 9,588 cycles

NUMBER 3 MAIN ENTRY DOOR SLIDE MISSING D-RING AND STRAP. *S/D* FOUND D-RING BEHIND SHROUD, ATTACHED TO SIDE OF DOOR.

Part: GENERATOR — FAILED (LT ENGINE)

AIRCRAFT RETURNED TO ORD, DUE TO LEFT ENGINE GENERATOR PROBLEM. REPLACED LEFT (NR 1) INTEGRATED DRIVE GENERATOR (IDG). THE IDG HAD AN INTERNAL DIODE FAILURE.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EEL LIGHTING SECTION IS INOP AT STATION 1370 LEFT HAND SIDE. *S/D* REPLACED BATTERY PACK IN PASSENGER SERVICE UNIT STATION 1370, LEFT HAND SIDE.

Part: RESTRAINT STRAP — MISSING (DOOR 4L)

D-RING MISSING FROM SLIDE AT DOOR 4-LEFT. *S/D* D-RING AT THE END OF RESTRAINT STRAP ON SLIDE RAFT WAS FOUND MISSING. ENTIRE RESTRAINT STRAP ASSY WAS REPLACED.

Part: AIR DISTR — ODOR (CABIN)

HOT ELECTRICAL SMELL AFT CABIN AREA AND COCKPIT. FLIGHT DIVERTED TO DEN.

Part: COMPRESSOR — DAMAGED (APU)

REPORTED SMOKE IN CABIN. FLIGHT DIVERTED TO SPOKANE. FOREIGN OBJECT DAMAGE IN THE APU DRIVEN COMPRESSOR. REPLACED APU.

Part: ACTUATOR — WORN (RUDDER)

CREW REPORTED LEFT HYDRAULIC FLUID LEVEL WENT DOWN ON LANDING. FOUND HYDRAULIC FLUID LEAKING FROM TAIL OF AIRCRAFT. SUPPLEMENTAL DATA UPDATE: REPLACED RUDDER CENTER PCA. PCA WAS FOUND TO HAVE WORN PISTON ROD SEALS CAUSING THE LEAKAGE. OVERHAULED ACTUATOR WAS TESTED AND RETURNED TO SERVICEABLE CONDITION.

Part: FUEL PUMP — OIL LEAK (NR 2 ENGINE)

DIVERTED TO DEN UNDER AMBER ALERT WITH NR 2 ENGINE SHUTDOWN DUE TO OIL QUANTITY LOSS. OIL LEAK CAUSED BY FAULTY FUEL PUMP ALLOWING OIL TO LEAK THROUGH THE WET SPLINE AREA.

Part: FUEL RETURN LINE — CROSS THREADED (NR 2 ENGINE)

EXPERIENCED NR 2 ENGINE FIRE. SECURED ENGINE AND ACTIVATED FIRE EXTINGUISHERS. FOUND THE HPT CASE COOLING VALVE FUEL RETURN LINE CROSS THREADED AT THE 2.5 BLEED VALVE FUEL PRESSURE RETURN LINE.

Part: RSTRACT MECH — MALFUNCTIONED (TE FLAPS)

DURING APPROACH THE FLIGHT CREW WAS UNABLE TO EXTEND FLAPS FULLY. OP CHECKED FLAPS, BITE CHECKED FLAP SLAT ELECTRONIC UNIT, AND VISUALLY INSPECTED FLAPS. NO DEFECTS FOUND.