N760NA

Part: CONTACT — WRONG PART (EMERGENCY LIGHT) · airframe 80,705 hrs · 13,487 cycles

FIRST TWO SECTIONS OF LT SIDE FLOOR PATH LIGHTING INOPERATIVE. R & R INCORRECT CONTACTS ON FLOOR PATH LIGHTS IAW SWPM 20-60-02, RELAMPED AND TESTED GOOD IAW 33-51-00.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 80,705 hrs · 13,487 cycles

EXTERIOR EMERGENCY EXIT LIGHT AT R4 DOOR INOPERATIVE. REPLACED TERMINAL OF WIRE IAW SWPM 20-30-11.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 80,640 hrs · 13,474 cycles

F/A FLASHLIGHT BY R2 DOOR INOPERATIVE. REPLACED FLASHLIGHT BATTERY, OPS CHECKED NORMAL IAW MM 25-54-00.

Part: PRESSURE SWITCH — DAMAGED (BLEED AIR SYS)

A/C HAD AN AIRTURN BACK DUE TO EICAS RT ENGINE PRESSURE REGULATOR VALVE DISPLAYED BLEED LIGHT ON, DUCT PRESS NORMAL. REMOVED AND REPLACED NR 2 ENGINE PRV IAW AMM 36-11-18 VALVE FAULT PER FIM 36-10-00, REMOVED AND REPLACED RT BLEED AIR CONTROL CARD M860 IAW AMM 36-11-12 AND REMOVED AND REPLACED OVER PRESSURE SWITCH S735 IAW AMM 36-21-03 A/C RELEASED FOR FLIGHT. A/C HAD A 2ND AIRTURN BACK (INBD WRITE UP) RT ENG PRV EICAS ACCOMPANIED WITH RT ENG BLEED OFF LIGHT. REMOVED AND REPLACED PRESSURE REG CONTROLLER IAW AMM 36-11-19 OHMD OUT WIRING 36-11-62 36-11-52 FOUND WIRE OPEN BETWEEN PIN 1 PRV TO LOGIC CARD PIN 18, REPAIRED WIRE AT D4252 ENGINE RUNS AS PER AMM 71-00-00 OPS CHECK GOOD (ITEM CLOSED). PARTS REPLACED PRESSURE REG VALVE P/N 802170-10 S/N 200103117 BLEED CONTROL CARD P/N 285T1115-15 S/N D1045 PRESSURE REG CONTROLER P/N 792755-15 S/N 9789143

Part: BATTERY PACK — DISCHARGED (EVAC SLIDE)

FORWARD DOOR RIGHT SLIDE GND ILLUM LIGHT INOP AT STA 357. REMOVED AND REPLACED BATTERY PACK ASSY M731. P/N OFF 2013-1A S/N OFF 52653 P/N ON 2013-1A S/N ON 30297.

Part: BATTERY PACK — DISCHARGED (EVAC SLIDE)

MID DOOR RIGHT SLIDE GND ILLUM LIGHT AT STA 654+36 INOP. REPLACED BATTERY PACK. P/N OFF 2013-1A S/N OFF 52653, P/N ON 2013-1A S/N ON 30297.

Part: LIGHT — INOPERATIVE (CABIN)

FWD CTR ELECTRO LUMINESCENT CROSS AISLE EMERGENCY LIGHT INOP AT STA 315. REPLACED LIGHT ASSY. P/N S417T510-11

Part: MOUNT — CORRODED (NR 2 ENGINE) · corrosion level 2

NR 2 ENGINE FWD ENGINE MOUNT HAS AREAS OF PITTING ON UPPER SURFACE. REMOVED AND REPLACED NR 2 FWD ENGINE MOUNT IAW AMM 71-21-01.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY PATH LIGHTING INOP FROM ROW 1 ECD TO 10ECD RIGHT SIDE. ACCOMPLISHED FIM 33-51-00, REMOVED AND REPLACED RIGHT FWD POWER SUPPLY AT STATION 401 PER MM 33-51-07, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR)

EXTERIOR EMERGENCY LIGHT FWD OF AFT CARGO DOOR INOP. RELAMPED EXTERIOR EMERGENCY LIGHT AS PER MM 33-51-06, OPS CHECK GOOD.

Part: PIN — BACKED OUT (POWER CABLE)

FLOOR EMERGENCY LIGHT AT 5FG-6FG INOP. FOUND PIN PUSHED BACK IN CABLE STRIP, REPOSITION PIN PER SWPM 20-82-11, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

E-PATH LIGHT FROM SEAT 11 TO 30 RIGHT INOP. REPLACED BATTERY PACK FOR E-PATH LIGHT SEAT 11 TO 30 RIGHT AND TEST NORMAL AS PER B767 33-51-07.

Part: BATTERY PACK — DISCHARGED (CABIN)

SEATS 34, 35, 37 RIGHT EMERGENCY LIGHT INOP. REPLACED BATTERY PACK FOR RIGHT EMERGENCY LIGHT SEAT 34, 35, 37 & TEST NORMAL AS PER B767 33-51-07.

Part: BATTERY PACK — DISCHARGED (CABIN)

LAST DOOR RIGHT INTERIOR EMERGENCY LIGHT INOP. REPLACED BATTERY PACK FOR LAST DOOR RIGHT AND TEST NORMAL PER B767 33-51-07.

Part: BATTERY PACK — DISCHARGED (CABIN)

LAST 2 DOOR EXTERIOR EMERGENCY LIGHTS INOP AT RIGHT AND LEFT. REPLACED TWO BATTERY PACK FOR R4 AND L4 EMERGENCY LIGHT & TEST OK AS PER B767 33-51-07.

Part: LIGHT — INOPERATIVE (EXTERIOR)

EXTERIOR EMERGENCY LIGHT AFT OF LEFT WING INOP. RELAMPED EXTERIOR EMERGENCY LIGHT AS PER MM 33-51-06, OPS CHECK GOOD.

Part: FITTING — CRACKED (NR 2 PYLON)

DURING ACCOMPLISHMENT OF EO 767-54-002 FOUND CRACK INDICATION OF NR 2 ENGINE UPPER OUTBOARD PYLON MID SPAR FITTING, CONFIRMED CRACK ON SECOND FASTENER HOLE (FROM AFT TO FWD POSITION) INBOARD ROW. REMOVED AND REPLACED PYLON O/B MIDSPAR FITTING IAW SB 767-54-0081. INSTALLED FITTING P/N 311T2151-20, S/N 1178, P/N OFF IS UNREADABLE, S/N OFF 620.

Part: LIGHT — INOPERATIVE (EXTERIOR)

EXTERIOR EMERGENCY LIGHT INOP AT DOOR L4. RELAMPED LIGHT AT L4 DOOR AS PER MM 33-51-00, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR)

EXTERIOR EMERGENCY LIGHT INOP AT R2 DOOR. RECONNECTED EMERGENCY LIGHT AT R2 DOOR AS PER MM 33-51-00, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR)

EXTERIOR EMERGENCY LIGHT INOP AT R4 DOOR. RELAMPED EMERGENCY LIGHT AT R4 DOOR AS PER MM 33-51-00, OPS CHECK GOOD.

Part: HEAT SHIELD — CONTAMINATED (LT MLG)

GROUND REPORTED SMOKING GEAR ON LEFT SIDE REAR NR 6 TIRE AND WHEEL LEJ FIRE DEPARTEMENT DISPATCHED. INSPECTED WHEEL AND BRAKE ASSY PEM MM 32-41-08 NO LEAKS OR DEFECTS NOTED REMOVED GREASE FROM HEAT SHIELD NOTED PER FIRE DEPARTMENT BLOCK TEMP 300 DEG 'C' NO FIRE OBSERVED.

Part: LIGHT — OUT OF POSITION (CABIN)

SEAT 21 AND 22 RIGHT SIDE FLOOR EMERGENCY PATH LIGHTS INOP. REPOSITIONED LIGHTS OPS CHECK GOOD AS PER MM 33-51-05.

Part: LIGHT — INOPERATIVE (CABIN)

FOUND THE R2 DOOR EMERGENCY LIGHT INOP. RESEATED LAMP OPS GOOD PER MM 33-51-00.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY)

SMOKE DET L2 BATHROOM VENT WENT OFF IN FLIGHT. NO SMOKE IN LAV, GARBAGE DET NORMAL. L2 LAV SMOKE DET, OPS CHECK GOOD IAW AMM 26-13-00. NO FURTHER DEFECTS NOTED.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT)

EMERGENCY FLASHLIGHT ADJ TO COCKPIT DOOR INOP. REMOVED AND REPLACED FLASHLIGHT AND BATTERY AS PER MM 25-64-00, OPS CHECK GOOD.

Part: CONNECTOR — LOOSE (CABIN)

ALL CROSS AISLE EMRGENCY LIGHT INOP AT ROW 27CDE. TROUBLESHOT ALL CROSS AISLE EMERGENCY LIGHT AT ROW 27CDE AND FOUND LOOSE CONNECTOR. RECONNECTED THE LIGHTS AND PERFORMED LAMP TEST AS PER REF B767 33-51-00, TEST NORMAL.

Part: CONNECTOR — LOOSE (CABIN)

EMERGENCY LIGHTS FROM 23AB TO 26AB INOP. TROUBLESHOT EMERGENCY LIGHTS FROM 23AB TO 26AB AND FOUND LOOSE CONNECTORS. RECONNECTED MM THE LIGHT AND PERFORMED LAMP TEST AS PER REF B767 AMM 33-51-11, TEST NORMAL.

Part: LIGHT — DEFECTIVE (CABIN)

O/H EMERGENCY LIGHT AT 35GF IS DIM. RELAMPED EMERGENCY LIGHT LAMP AT SEAT ROW 35GF AND PERFORMED TEST, OPS CHECK NORMAL REF B767 AMM 33-51-04.

Part: LIGHT — INOPERATIVE (EXTERIOR)

EXTERIOR EMERGENCY LIGHT AT L1 DOOR INOP. PERFORMED OPS CHECK OF EMERGENCY LIGHTS AND FOUND L1 DOOR LIGHT NORMAL (OPERATING) IAW B767 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHTS AT LEFT OVER WING AREA INOP. PERFORMED OPS CHECK OF EMERGENCY LIGHTS AND FOUND LEFT OVERWING LIGHT NORMAL (OPERATING) IAW B767 AMM 33-51-0.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS BY 21AB THROUGH 26D INOP. REMOVED AND REPLACED BAT PACK ASSY IAW AMM 33-51-05, OPS CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHT BY L1 THROUGH 3AB INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK ASSY IAW AMM 33-51-05, OPS CHECK OK.

Part: PLUG — CRACKED (NR 2 EXHAUST)

EXHAUST PLUG CRACKED AT 5 OCLOCK POSITION AT END OF PLUG ON NR 2 ENGINE. WELDED, VISUAL INSPECTED AND DYE CHECKED REPAIR AREA PER CMM 314T43201, ATA 78-11-15 REPAIR 2-1, ALL WORK COMPLIED WITH ON DELTA SHOP ORDER EA 5673.

Part: DRAIN — OBSTRUCTED (FUSELAGE)

SOUND OF AIR ESCAPING FROM UNKNOWN SOURCE IN PROXIMITY OF SEATS 19 - 22 ON RIGHT SIDE OF ACFT. FOUND A NOTICEABLE LEAK. LEAK FOUND APPROXIMATELY BS 952 WL 188. FOUND FUSELAGE DRAIN PLUNGER NEAR SEAT 20 STUCK IN OPEN POSITION. REMOVED DEBRIS FROM PLUNGER AND REINSTALLED. PERFORMED 8 PRESSURIZATION CYCLES OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (CABIN)

EMERGENCY FLOOR LIGHT INOP FROM SEAT ROW 1EC TO ROW 9GF. REMOVED & REPLACED BATTERY CHARGER ASSEMBLY PER AMM 33-51-07, OPS CHECK NORMAL.

Part: ARMING LEVER — LOOSE (R1 DOOR)

R1 ENTRY DOOR SLIDE ARMING LEVER WOULD NOT ENGAGE. FOUND ARMING LEVER FOR R1 DOOR LOOSE BY ALLEN BOLT AT TOP OF LEVER. SECURED HANDLE IN THE PROPER POSITION PER MM 52-11-00 R1 ARMS AND DISARMS NORMAL.

Part: PULLEY BRACKET — CRACKED (ELEVATOR)

FUSELAGE STA 245 ELEVATOR - PULLEY BRACKET INBOARD AND OUTBOARD SIDE CRACKED. REMOVED INBOARD AND OUTBOARD BRACKETS INSPECTED AREA INSTALLED NEW BRACKETS AS PER BOEING 255T4418.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FLOOR SUPPORT ANGLE AND ATTACHING WEB CRACKED ON AFT SIDE OF COCKPIT FS 246 LBL 24. REMOVED DAMAGED AREA AS PER SRM 53-10-51. HFEC INSPECTION OF DAMAGE AREA OK TO INSTALL REPAIRED PARTS AS PER SRM 53-10-51.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

FLOOR SUPPORT WEB AT STA 1550 WL 200 BL 0 JUST BELOW AFT GALLEY FLOOR. REPAIRED FLOOR SUPPORT WEB AS PER SRM 51-70-03 AND EO 767-53-041.

Part: PULLEY BRACKET — CRACKED (CONTROL CABLE)

FWD SIDE OF STATION 246 CENTER CONTROL CABLE PULLEY BRACKET CRACKED. REMOVED CRACKED BRACKETS INSTALLED NEW BRACKETS AS PER BOEING DRAWING 255T4472.

Part: ANGLE — DAMAGED (FUSELAGE)

ANGLE FWD SIDE OF FLOORBEAM AT STA 246 LBL 14. REPLACED ANGLE AS PER BOEING DRAWING 141T5104.

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 74,194 hrs · 12,200 cycles

WHILE AT PSV IN ATL, MTC FOUND A 2.25 INCH CRACK IN THE RADIUS OF THE INBOARD SKATE ANGLE OF THE NR 2 AFT STRUT FAIRING. THE CRACK EXTENDS FORWARD FROM THE AFT EDGE OF THE PART. THE SKATE ANGLE IS MANUFACTURED FROM 0.125 INCH BARE 7075-T6 SHEET. CRACK REPAIRED PER ERA 492007-14AD.

Part: FLOORBEAM — CORRODED (BS 287) · airframe 74,194 hrs · 12,200 cycles

DURING C2 CHECK IN HANGER, CORROSION DAMAGE WAS DISCOVERED TO THE UPPER SURFACE OF THE UPPER CAP OF STA 287 FLOORBEAM AT LBL40. CORROSION REPAIRED PER ERA 492601-14.REV A.

Part: HYDRAULIC LINE — CRACKED (LT ENGINE)

AIRCRAFT HAD AN AIR RETURN TO LEJ DUE LT EDP HYD LOW PRESS & DEMAND PRESS LIGHTS ILLUMINATED AND EICAS MSG DISPLAYED LT HYD PRIM PUMP. UPON INVESTIGATION FOUND HYD LINE P/N 272T3100-193 IN LEFT ENG PYLON LEAKING REMOVED & REPLACED DAMAGED LEFT SYS EDP HYD LINE IN PYLON PER MM 20-10-09, REPLACED NR 1 ENGINE HYD PUMP PER MM 29-11-05. REPLACED LEFT ACMP PER MM 29-11-01. REPLACED EDP CASE DRAIN FILTERS PER MM 29-11-17. REPLACED ACMP CASE DRAIN FILTERS 29-11-18. ALL OPS CHECK AND LEAK CHECK ACCOMPLISHED CHECK GOOD.

Part: TURBINE BLADES — DAMAGED (NR 2 ENGINE)

FOUND NR 2 ENGINE LOWER PRESSURE TURBINE BLADE DAMAGED ON WALK AROUND. REPLACED NR 2 ENGINE AS PER JOB CARD 767-71-R07.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY)

L1 LAV SMOKE ALARM SOUNDED NO SMOKE, FIRE EXTINGUISHER DID NOT DISCHARGE. REMOVED AND REPLACED LAV SMOKE DETECTOR AS PER MM 26-13-01, OPS CHECK OK.

Part: SIGN — INOPERATIVE (CABIN)

R1 GALLEY EMERGENCY EXIT SIGN INOP. RELAMPED R1 GALLEY EMERGENCY EXIT SIGN AS PER MM 33-51-01, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

FLOOR EMERGENCY LIGHT INOP AT SEAT 29B. RELAMPED FLOOR EMERGENCY LIGHT AY SEAT 29B, OPS CHECK GOOD.

Part: LOGIC CARD — FAULTY (FIRE WARNING)

AFTER LANDING EICAS FIRE/OVERHEAT LIGHT ILLUMINATED. REMOVED AND REPLACED LEFT ENGINE FIRE / OVERHEAT LOGIC CARD M10224 PER M/M 26-10-01, OPS TEST OK, OK FOR SERVICE.

Part: TRANSDUCER — MALFUNCTIONED (MLG ANTI SKID)

A/C 760 RETURNED TO HS69 DUE TO INTERMITTENT ANTI SKID EICAS MSG. MX FOUND THE NR 7 ANTI SKID TRANSDUCER FAULTED, MCC WOULD LIKE TO DISPATCH THE A/C USING MEL 32-42-1 DEACTIVATING NR 7 BRAKE USING METHOD "A" IN ACCORDANCE WITH MEL 32-41-1. MAINT HAS SECURED THE BRAKE TOOL AND ACCOMPLISHED A SUCCESSFUL LEAK CHECK. REMOVED AND REPLACED ANTI-SKID TRANSDUCER ON NR 7 MLG WHEEL AS PER AMM 32-42-04 OPS CHECK PER AMM 32-42-00-705 CHECKS OKAY.

Part: LOGIC CARD — FAULTY (FIRE WARNING)

LEFT ENGINE FIRE LOOP 1 STATUS MSG, LEFT ENG FIRE LOOP NR 2 STATUS MSG, DISCREET FIRE LIGHT. REMOVED AND REPLACED LEFT ENGINE FIRE / OVERHEAT LOGIC CARD M10224 PER M/M 26-10-01, OPS TEST OK, OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (FIRE HANDLE)

APU FIRE HANDLE DID NOT ILLUMINATE DURING TEST. RELAMPED FIRE HANDLE IAW AMM 33-16-02, OPS CHECK OK.

Part: CONNECTOR — LOOSE (CABIN)

EMERGENCY LIGHTS INOP FROM ROW 10AB TO 20AB [FLOOR LIGHTS]. FOUND LOOSE ELECTRICAL CONNECTOR AT SEAT ROW 19AB E-PATH LIGHT ASSY RE-SECURED SAME ELECTRICAL CONNECTOR AS PER AMM 33-51-00, OPS CHECK OK.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHT INOP AT 37B. REPLACED LIGHT AS PER MM 33-51-00.

Part: SIGN — INOPERATIVE (CABIN)

EMERGENCY EXIT SIGN AT L2 DIM. RELAMPED L2 EMERGENCY EXIT SIGN AS PER MM 33-51-00.

Part: CHARGER — INOPERATIVE (CABIN)

EMERGENCY EXIT SIGN AT L1 DOOR DIM. REPLACED BATTERY CHARGER AS PER MM 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHT INOP AT 28B. REPLACED LIGHT AS PER MM 33-51-00.

Part: ALTIMETER — MALFUNCTIONED (COCKPIT)

THE CAPT'S AND F/O ALTIMETER SPLIT AT FL 350 TO FL 390 AND AN AIR SPEED DIFFERENCE. SDR REMAINS OPEN - ALTITUDE- 39,000 - CAPTAINS INDICATOR- 39,000 - F/O INDICATOR- 38,820 - STANDBY INDICATOR- 39,350 - CAPT'S MACH INDICATOR- .818 - F/O MACH INDICATOR- .809. ACFT DIDN’T EXCEED 20KTS OVERSPEED. PERFORMED A/C INSPECTION IAW MM 05-51-04, NO DEFECTS. PERFORMED FIM 22-00-03 FIG 103 110A + 117. ALL TEST OK. SPEED WERE VERIFIED WITH FLIGHT CREW DEBRIEF F/O VERIFIED SPEEDS AT .85 M EXCEED BY 2 TO 3 KTS / PERHAPS BY .002 MACH.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHTS INOP BY SEAT 18HG THRU 21HG. REPLACED EMERGENCY LIGHT ASSY STRIP PER MM 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHTS INOP BY CEILING 33AB 1FG. REPLACED LIGHT AS PER MM 33-51-00.

Part: PRESSURE SWITCH — INOPERATIVE (APU)

APU FAILED TO START IN FLT ON 1ST ATTEMPT, 2ND ATTEMPT STARTED APU OK. BUT HAD AN AUTO SHUTDOWN AT FL 090 & FAULT LIGHT CAME ON. REPLACED APU ECU, PER AMM 49-61-05, LOADED APU TO 76 PERCENT OPS NORMAL STARTED AND RESTARTED 5 TIMES, OPS CHECK OK, AUTO SHUTDOWN RE-OCCURRED STARTED & OPS IAW 49-11-00. NO FAULTS, AUTO SHUTDOWN RE-OCCURRED REPLACED LT UPPER & LOWER THERMOCOUPLES IAW AMM 49-71-01. START & RUN CHECKS NORMAL, AUTO SHUTDOWN RE-OCCURRED BITE CHECK APU PER FIM 49-41-00, CHANGED FILTER, APU OPERATES NORMAL. APU FAULT ON INITIAL START OCCURRED, R & R APU OIL SOLENOID VALVE PER MM 49-27-08-004-001 LEAK CHECK OPS CHECK OK. AUTO SHUTDOWN RE-OCCURRED, DRAINED APE OIL PER MM 49-27-00-603-001, R & R SCAVENGE OIL FILTER PER MM 49-27-03, R & R OIL FILTER ELEMENT PER MM 49-27-03, R & R APU DIFFERENTIAL PRESSURE INDICATOR, LEAK & OPS CHECK OK. AUTO SHUTDOWN RE-OCCURRED, R & R APU GENERATOR FILTER DIFFERENTIAL PRESSURE SWITCH AS PER MM 49-27-15. OK FOR SERVICE. (ORIGINAL SUBMISSION: 2-8-2010)

Part: FIRE LOOP — MALFUNCTIONED (NR 1 ENGINE)

NR 1 ENG FIRE LP STATUS MESSAGE ON EICAS. COMPLIED WITH PL760-1001-03, REPLACED THE NR 1 ENGINE FIRE LOOP ELEMENT T50683 PER AMM 26-11-00, OPERATIONAL CHECK OK.

Part: LIGHT — BROKEN (CABIN)

EMERGENCY TRACK LIGHTING AT SEAT 5H BROKEN. REMOVED AND REPLACED EMERGENCY TRACK LIGHT ASSY AT 5HG PER AMM 33-51-10, OPS CHECK NORMAL.

Part: WIRE — BROKEN (CABIN)

AFT GALLEY PHOTO LUMINESCENT E-PATH LIGHT ON RIGHT SIDE HAS BROKEN WIRES. REMOVED AND REPLACED LIGHT ASSY AND OPS CHECKS NORMAL PER AMM 33-51-00. P/N 81000-22608

Part: REPAIR — CRACKED (LE SLAT)

RIB STIFFENER REPAIR IS CRACKED L/E STA 690 AT FWD END OF NR 10 SLAT. REPLACED ANGLE AS PER SRM 51-40-02.

Part: REPAIR — CRACKED (LE SLAT)

REPAIR ANGLE CRACKED L/E STA 690 AT INBOARD END OF NR 10 SLAT. REPLACED ANGLE AS PER SRM 51-40-02.

Part: FLAP — DENTED (LT WING)

LT INBOARD AFT FLAP HAS DENT WITH GOUGE APPROX 5FT FROM INBOARD END 8 INCHES LONG. REMOVED DAMAGED ON LT INBOARD AFT FLAP AND INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-70-10.

Part: STRUCTURE — CRACKED (NR 7 SLAT)

NR 7 L/E SLAT, INTERIOR (AFT SIDE) T/E STRUCTURE HAS TWO ANGLE CLIPS CRACKED, HAS APPROX 42 INCHES AND 52.5 INCHES I/B OF SLAT EDGE. MANUFACTURED ANGLES PER DRAWING 114T3166 AND INSTALLED ON SLAT.

Part: LIGHT — INOPERATIVE (CABIN)

R3 DOOR LOWER EMERGENCY EXIT SIGN SEVERAL LIGHTS INOP. RELAMPED R3 DOOR LOWER EMERGENCY EXIT SIGN IAW AMM 33-51-01. OPS CHECK OK.

Part: WINDOW — CRACKED (COCKPIT)

A/C N760 DIVERTED TO OTP (BUCHAREST) DUE TO THE CAPTAINS NR 1 WINDOW CRACKED. A/C IS ON AOG IN OTP UNTIL WINDOW REPLACEMENT. BORROWED PARTS FROM DHL IN LEJ ARE WINDOW P/N 141T4800-13; S/N G4742. WINDOW HEAT CONTROLLER P/N 624066-5; S/N 029C-1364 WERE PLACED ONBOARD A/C N768 IN LEJ. MX TEC REQUESTED TO CONTINUE TO OTP ON N768. MX TEC REQUESTED TO JOIN A/C N768 IN KWI AND CONTINUE TO OTP. PARTS AND MAINTENANCE TEC'S WILL ARRIVE OTP ON FLT 7004 AT 0035L 07/04/09. BACK-UP PARTS WERE PLACED ONBOARD A/C N765 FLT 7005 DFW LEJ 07/03/09, ARRIVING LEJ AT 0855L 07/04/09.

Part: LIGHT — INOPERATIVE (EXTERIOR)

R2 EMERGENCY SLIDE EXIT LIGHT ON OUTSIDE INOP. REPLACED LAMP AS PER MM 33-51-06.

Part: LIGHT — INOPERATIVE (CABIN)

2AB EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY FLOOR LIGHT ASSY AT 2A. OPS CHECK OK.

Part: FIRE WARNING — MALFUNCTIONED (RT ENGINE)

R ENG OH LP 1 STATUS MESSAGE. PERFORMED OPERATION TEST OF THE ENGINE FIRE DETECTION SYSTEM PER M/M 26-11-00, OPS NORMAL.

Part: MOTOR — INOPERATIVE (BLOWER)

FWD DET FAN MESSAGE DISPLAYED ON EICAS MAINT PAGE. REMOVED AND REPLACED FWD CARGO SMOKE DETECTOR BLOWER NR 1 PER AMM 26-16-02. OPS CHECK GOOD.

Part: WINDOW — MALFUNCTIONED (COCKPIT)

ON TAKEOFF ROLL AT 70 KTS "R SIDE WINDOW" EICAS CAUTION MESSAGE DISPLAYED, ABORTED TAKEOFF. C/A: REMOVED AND REPLACED R 3 WINDOW IAW MM 56-11-10. OPS CHECK OK. (K)

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2

INSIDE BULK CARGO BELOW FLOOR AT HEATED DRAIN LINE BOX AREA BETWEEN STR 36R-35R AT STA 1417-1395 HAS LEVEL 2 CORROSION. REPLACED DRAIN MOUNT PLATES AND BRACKETS IAW 51-10-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

STA 1480 FLOORBEAM IS CORRODED THRU AT APPROXIMATELY RBL 54-60 AND VARIOUS SPOTS TO RBL 81. ACCOMPLISHED STA 1480 RIGHT O/B FLOORBEAM REPAIR IN ACCORDANCE WITH SRM 53-00-51.

Part: INTERCOSTAL — CRACKED (FUSELAGE)

INTERCOSTAL ANGLE CRACKED AT CABIN FLOOR SUPPORT STA 1395-1417 AT LBL 40 AROUND NUT PLATE. REPLACED INTERCOSTAL AS PER SRM 51-70-13.

Part: FRAME — CRACKED

AFT A FRAME LOWER CHANNEL CRACKED AT RIVET I/B FWD SIDE OF A FRAME BELOW DIAG BRACE AFT FITTING. REPLACED CRACKED C-CHANNEL IAW SRM 51-10-02.

Part: FITTING — CRACKED (LT FAN COWL)

FAN COWL SUPPORT BEAM FITTING ASSY IS CRACKED IN TWO PLACES LT SIDE. REPLACED COWL SUPPORT BEAM FITTING AND SHIMMED AS PER SRM 51-10-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE)

INTERCOSTAL ANGLE AT CEILING IS CRACKED AT 2EA AREAS AROUND FASTENERS BETWEEN STA 566-588 AT LBL 40. INSTALLED NEW INTERCOSTAL PER SRM 53-30-51.

Part: LIGHT — INOPERATIVE (EXTERIOR)

DOOR R-4 EXTERIOR SLIDE EMERGENCY FLOOD LIGHT INOP. RELAMPED DOOR R-4 EXTERIOR SLIDE EMERGENCY FLOOD LIGHT AND OPS CHECKS NORMAL AS PER THE AMM 33-51-06.

Part: DETECTOR — MALFUNCTIONED (AFT CARGO BAY)

AFT CARGO DETECTOR NR 1 EICAS STATUS MSG DISPLAYED (M) REMAINING DETECTOR IS VERIFIED TO OPERATE NORMAL BEFORE EACH DEPARTURE WITH A LOGBOOK ENTRY. EICAS MESSAGE AFT DET FAN. REMOVED AND REPLACED AFT CARGO DETECTOR PER MM 26-16-00. OPS CHECKS OK.

Part: WIRE — DAMAGED (CABIN)

EMERGENCY LIGHT INOP LEFT HAND SIDE FROM L1 DOOR TO L2 DOOR, CENTER AISLE AND L3 DOOR LOCATIONS AND LEFT HAND SECTION BY L3 DOOR. REPAIRED WIRING AS PER WIRING DIAGRAM 33-51-13 AND 33-51-16, ALL OPS CHECKED NORMAL.

Part: POWER SUPPLY — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS AFT OF DOOR L2 ON THE FLOOR ARE VERY DIM. REMOVED AND REPLACED POWER SUPPLY (M373) PER MM 33-51-07.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY FLOOR LIGHTS INOP BETWEEN 1AB AND 2AB. REPLACED LIGHT ASSY PER MM 33-51-10.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

AFT CARGO DET 1 ON STATUS. REPLACED NR 1 & 2 AFT CARGO SMOKE DETECTORS PER MM 26-16-01.

Part: SHUTOFF VALVE — MALFUNCTIONED (T/E FLAP)

AFTER BOTH ENGINES STARTED FLAP HANDLE MOVED TO 5 STATUS MESSAGE FLAP/SLAT ELEC. REPLACED FLAP/SLAT SHUT OFF VALVE AS PER MM 27-51-48, OPS CHECK OK.

Part: SIGN — BROKEN (EMERGENCY LIGHTS)

L1 DOOR EMERGENCY LIGHT EXIT SIGN BROKEN. REMOVED AND REPLACED L1 DOOR EXIT SIGN ASSY IAW 33-51-01, OPS CHECKS OK.

Part: COMPUTER — INTERMITTENT (AUTOPILOT)

FOUND LEFT A/P ENGAGES INTERMITTENTLY REPLACED LEFT AFCS PER MM 22-11-01.

Part: SERVO VALVE — MALFUNCTIONED (AUTOPILOT)

CENTER AUTOPILOT WILL NOT ENGAGE. REPLACED CENTER AUTOPILOT SERVO VALVE PER MM 22-13-03.

Part: SLIDE — UNWANTED DEPLOY (L2 DOOR)

DOOR SLIDE 2L BLOWN ADVERTENTLY BY FLT ATTENDANT. THE 2L SLIDE PREVIOUSLY REMOVED REF PG 39524 ITEM 1M PAD 76. INSTALLED 2L SLIDE PER JOB CARD 25-029-01 AND AMM 25-66-01. OK FOR SERVICE.

Part: MODULE — MALFUNCTIONED (FIRE DETECTION)

FIRE WARNING BELL INOP DURING WHEEL WELL TEST AND FIRE/OVERHEAT TEST. REMOVED AND REPLACED MASTER WARNING AND BELL/CHIME CARD MODULES PER MM 31-51-04, OPS CHECK NORMAL.

Part: PUMP — MALFUNCTIONED (HYDRAULIC SYS)

C-HYD SYS PRESS EICAS C-SYS PRESS LIGHT ILLUMINATED, AIR PRESS LIGHT ILLUMINATED, AIRCRAFT DUMPED 18.8K LBS OF FUEL. AIRCRAFT HAD AIR TURNBACK TO DFW. REPLACED ADP PUMP ASSY. REPLACED CENTER HYD PRESS SWITCH S35. REPLACED AIR HYD PUMP PRESS SWITCH S28. REPLACED AIR HYD PUMP CONTROL PRESS SWITCH S29AS PER MM 29-11-04.

Part: ANTI-SKID SYS — UNKNOWN (MLG)

ANTI-SKID SYSTEM ONE CHANNEL INOP DUE TO NR 8 TRANSDUCER FAULT. MEGGERED WIRES FROM ANTI-SKID MODULE TO NR 8 TRANSDUCER, CHECKED FOR POWER RESIST AT NR 8 TRANSDUCER. SUSPECT BAD WIRE AT J2 BOX ON RT LANDING DUE TO FAULT NR 7 TRANSDUCER OCCURRED WHEN DISTURBING WIRES AT J2 FOUND WIRE 2688-201B-20 OPEN TO NR 7 TRANSDUCER. RE-PINNED PLUG 02024, ALL CHECKS GOOD BITE ON AS/AB CONTROLLER NO FAULTS, ACCOMPLISHED ANTI-SKID AUTO BRAKE TEST PER MM 32-42-00, NO FAULTS.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY EXIT LAMP INOP AT 18AB. RELAMPED EXIT LAMP AT 18AB, OPS OK.

Part: LAMP — INOPERATIVE (SMOKE DETECTOR)

AFT CARGO DET 1 EICAS STATUS MSG. RELAMPED DET 1, AFT CARGO BIN PER AMM 26-16-01. OPS CHKS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

EXTERIOR EMERGENCY LIGHT AT DOOR 3R INOP. RELAMPED R3 DOOR LIGHT AS PER MM 33-51-06.

Part: CDU — CRACKED (THRUST REVERSER)

LEFT REV ISLN VALVE EICAS CAME ON, ON LANDING WITH LEFT ENG REV MESSAGE IN YELLOW STAYED ON. STATUS MESSAGE L REV ISLN VAL AND L REV INTERLOCK WAS ALSO DISPLAYED. VISUAL INSPECTION SHOW IB REV SHELL FULLY OPEN, FOUND CENTER DRIVE UNIT AND FOUND BACK HOUSING CRACKED. REMOVED AND REPLACED CENTER DRIVE IAW MM 78-31-21, OPS CHECKS GOOD.

Part: DRIVE ASSY — CRACKED (THRUST REVERSER)

LEFT REV ISOLATION VALVE EICAS CAME ON AT LANDING WITH LEFT ENGINE REVERSER YELLOW STAYING ON. STATUS MESSAGE LT REVERSER ISOLATION VALVE & LT REVERSER INTERLOCK WAS ALSO DISPLAYED. VISUAL INSP SHOWS INBOARD REVERSER SHELL FULLY OPEN, FOUND CENTER DRIVE & FWD BACK HOUSING CRACKED. REMOVED AND REPLACED CENTER DRIVE IAW MM 78-31-21.

Part: WIRE — SHORTED (ANTI SKID SYS)

CHRONIC FAULT OF ANTISKID EICAS MESSAGE ALONG WITH NORMAL & ALTN ANTI SKID STATUS MESSAGE AND ANTI-SKID ANNUNCIATOR. TROUBLESHOOT PER WDM 32-42-11 SHEET 2, FAULT FOUND BETWEEN CP D5022P OFF SHORTED. REMOVED WIRING W674-204R-20 W674-204B-20 AND SHIELD WIRE AT J1 CP 5024J PIN 11 PIN 12 AND PIN 15J3 CP D5022J PIN 1, 2, 3 J1 AND J3 HARDWARE ATTACHED TO ORIGINAL POSITION REPLACED WIRE HARNESS D5022J TO D5042P PER WDM 32-42-11. MEGGED WIRING, ALL CHECKS GOOD. OPS CHECKED ANTISKID PER 32-42-00, ALL CHECKED OK.

Part: CONNECTOR — SHORTED (ANTI SKID)

ANTISKID EICAS CAME ON DURING TAXI OUT. PERFORMED FIM TASK 32-42-00 FIG 103 FOUND FAULT BOX 1-5 AND TRANSDUCER 5. REMOVED AND REPLACED TRANSDUCER 5 PER MM 32-42-06. OPS CHECKS NORMAL. NO HELP. TROUBLESHOT PER FIM 32-42-00 ANTI SKID/AUTO BRAKE CONTROL UNIT BITE FAILURE INDICATION BOX 1-5. DISABLE TRANDUCER 1 THRU 5 PER PROCEDURES AND FOUND FAULT NR 5 TRANSDUCER SYS REF WDM 32-42-11 SHEET 2. REMOVED ANTISKID CONTROL UNIT (M102) AND DISCONNECTED NR 5 TRANDUCER AT D2016. CKD WIRING CONTINUITY, OPEN AND SHORT, BETWEEN ANTI-SKID/AB CONTROL UNIT RACK PLUG D2772A AND C/P D2016. FOUND A SHORT BETWEEN PLUG D2772A PIN B5 AND C/P D2016 PIN 1. FURTHER ISOLATION OF FAULTS FOUND SHORT BETWEEN J1 C/P D5024P PIN 11 AN

Part: SENSE LINE — CRACKED (A/C BAY)

LEFT PACK SENCE LINE COMING OUT OF TURBINE IS CRACKED. REMOVED AND REPLACED SENCE LINE COMING OUT OF LEFT PACKS TURBINE.

Part: TORQUE TUBE — CORRODED (FLIGHT CONTROL)

CORROSION PITS ON INBOARD TORQUE TUBE SPLINES NR 17, 24, 25 AND 26. REMOVED AND REPLACED TORQUE TUBE.

Part: BRACKET — CRACKED (T/E FLAP)

BRACKET CRACKED ON RIGHT WING O/B FLAP I/B END CAP NEAR DATA PLATE. REMOVED AND REPLACED CRACKED BRACKET ON RIGHT WING I/B END OF O/B FLAP.

Part: SPRING — CORRODED (LT AILERON)

LEFT WING INBOARD AILERON OUTBOARD DROOP QUADRANT SPRINGS ARE CORRORED INTERNALLY. REMOVED AND REPLACED SPRINGS, RIGGED SPRINGS PER AMM 27-11-38-404-046. INSTALLED QUADRANT PER AMM, RIGGED CHECKED GOOD, OPS CHECKED GOOD.

Part: ROD END BEARING — CORRODED (RT AILERON)

RIGHT WING AILERON OUTPUT QUADRANT UPPER CONTROL ROD (TO OUTPUT QUADRANT) ROD ENDS RUSTY. REMOVED CONTROL ROD, REPLACED ROD END BEARINGS, INSTALLED RIGHT AILERON OUTPUT QUADRANT UPPER CONTROL ROD PER MM RIG CHECKED GOOD, OPS CHECKED GOOD.

Part: SPRING — CORRODED (RT AILERON)

RIGHT WING AILERON BREAKOVER MECHANISM SPRINGS RUSTED. BLOCKED CABLE, REMOVED RIGHT WING AILERON OVERRIDE QUADRANT, REMOVED & REPLACED SPRINGS & OVERRIDE BEARINGS PER MM. INSTALLED OVERRIDE QUADRANT. RIG CHECKED GOOD, OPS CHECKED GOOD. P\N OF BEARING 5673491 2 EACH, 2 SPRINGS REMOVED AND REPLACED.

Part: BATTERY — BROKEN (CABIN)

FLT ATTENDANT SEAT NEXT TO L1 DOOR, EPL EMERGENCY BATTERY IS BROKEN, NEEDS REPLACEMENT. REPLACED EPL BATTERY AT L1 DOOR FLT ATTENDANT SEAT. OPS CHECKED GOOD.

Part: KEELBEAM — CORRODED (FUSELAGE)

CORROSION ON UPPER SURFACE OF KEEL BEAM IN RIGHT WHEEL WELL AT STA 977-979. REMOVED CORROSION ON UPPER SURFACE OF KEEL BEAM AT STA 977-979 RT, FOUND TO BE WITHIN LIMITS. ALODINED, PRIMED PAINTED AREA.

Part: SPRING — CORRODED (RT AILERON)

RIGHT WING AILERON OUTPUT QUADRANT SPRINGS RUSTED. INSTALLED NEW SPRINGS PER MM ON OUTPUT QUADRANT. RIG CHECK GOOD, OPS CHECKED GOOD.

Part: WARNING MESSAGE — ILLUMINATED (THRUST REVERSER)

DURING TAKEOFF BELOW 80 KNOTS LEFT ENGINE REVERSE CAUTION ILLUMINATED, AND LEFT REVERSE ISOLATION VALVE MSG. THEN DURING TAXI-IN, THERE WAS A IDLE DISAGREE MESSAGE DISPLAY. ASSIGNED CI 78-19 MEL 78-31-1 LEFT T/R LOCKED IN THE FWD THRUST POSITION. PER DDG REMAINED OPENED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

FOUND EXTERIOR EMERGENCY LIGHTS AT R2, R4, AND L1 INOP. RELAMPED LIGHTS AT R2, R4, AND L1 PER AMM 33-51-06. OPS CHECKED NORMAL.

Part: CONTROL PANEL — MALFUNCTIONED (EMERGENCY LIGHTS)

EMERGENCY LIGHTS CAME ON IN FLIGHT UN-COMMANDED. REPEAT WRITE UP, SEE 10/14/06. REMOVED AND REPLACED EMERGENCY CONTROL PANEL PER AMM 33-51-08. OPS CHECKS NORMAL, OK FOR SERVICE.

Part: CONNECTOR — DAMAGED (RUDDER)

RUDDER RATION LIGHT ILLUMINATED AT 1000 FEET AFTER TAKEOFF. PERFORMED FIM 27-21-00. NO FAULTS NOTED, CHECKED WIRING IAW WDM 29-11-12. FOUND PIN NR 2 AT PLUG D56 PUSHED BACK, SECURED PIN IAW 20-11-00, OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

FOUND EMERGENCY EXIT EXTERIOR LIGHT AT R2,R4 DOOR OUT. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BULB.

Part: MODULE — UNKNOWN (STALL WARNING)

RIGHT PITCH LIMIT INDICATOR INDICATION. REPLACED RIGHT STALL WARNING MODULE, OPS NORMAL.

Part: ACTUATOR — MALFUNCTIONED (O2 MASKS)

DURING ACCOMPLISHEMENT OF MAINTENANCE WHICH REQUIRED A PSU OXYGEN MASK DROP THE FOLLOWING DID NOT DEPLOY: 20GH, 31CDEF L1 FWD, L1 AFT AND MID RT LAV. REPLACED 02 MASK ACTUATORS AT 31CDEF L1 FWD, L1 AFT AND MID RT LAV, RECONNECTED PSU AT 20GH, OPS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

EMEREGENCY LIGHTS INOP AT SEATS 10GH THRU 25GH. REMOVED AND REPLACED POWER SUPPLY.

Part: COMPUTER — FAULTED (LEFT)

CA/FD FAILED AND NO LAND 3, TEST FOUND LEFT FCC AT FAULT. REMOVED AND REPLACED LEFT FCC.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 56,466 hrs · 9,295 cycles

RED EMERGENCY EXIT FLOOR LIGHT INOP AT DOOR 2R.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 54,466 hrs · 9,295 cycles

DOOR R2 FLOOR PROXIMITY 2 RED EMERGENCY LIGHTS INOP.

Part: LIGHT — INOPERATIVE (CABIN)

E-PATH LIGHTS AFT L2 DOOR, SEATS 36AB & 3AB INOP. REPLACED LENS AND RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN)

E-PATH AT 2G INOP. REPLACED BULB, OPERATION NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

FLOOR MOUNTED E-PATH LIGHTS BETWEEN L3 AND 29B INOP. INSTALLED ASSY, OPERATION NORMAL.

Part: CONNECTOR — LOOSE (CABIN)

FLOOR MOUNTED E-PATH LIGHTS AFT LAV INOP. FOUND LOOSE CONNECTOR, OPERATION NORMAL.

Part: LIGHT — DAMAGED (CABIN)

E-PATH BETWEEN L1 DOOR AND SEAT 2B. REPLACED 2 DAMAGED LIGHT ASSY OPERATION NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

EXIT SIGN ON BULKHEAD NEXT TO R2 JUMPSEAT INOP. REPLACED BATTERY PACK, OPERATION NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

CEILING MOUNTED E-PATH LIGHT 13G INOP. REPLACED LIGHT BULB, OPERATION NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

CEILING MOUNTED EMERGENCY LIGHT (OUTSIDE RT MID LAV) INOP. REPLACED LIGHT BULB, OPERATION NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

CEILING MOUNTED E-PATH LIGHT 10G INOP. REPLACED LIGHT BULB, OPERATION NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR)

EXTERIOR MOUNTED E-PATH LIGHT R2 INOP. RESECURED BULB, OPERATION NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR)

EXTERIOR MOUNTED E-PATH LIGHT R3 INOP. RESECURED BULB, OPERATION NORMAL.

Part: CONNECTOR — LOOSE (CABIN)

FLOOR MOUNTED E-PATH LIGHTS BETWEEN R2 AND 18G INOP. FOUND LOOSE CONNECTOR AT BATTERY PACK, OPERATION NORMAL.

Part: CONNECTOR — LOOSE (CABIN)

RED FLOOR MOUNTED E-PATH LIGHT AT L3 INOP. FOUND LOOSE CONNECTION, OPERATION NORMAL.

Part: TRANSDUCER — INOPERATIVE (ANTI SKID SYS)

ON LANDING AUTOBRAKE DISARMED ANTI-SKID AUTOBRAKE EICAS AMBER MESSAGE APPEARED. REVERSER DEPLOYMENT WAS DELAYED UNTIL FIRM NOSE WHEEL CONTACT. T/S PER FIM 32-42-00 FOUND NR 6 TRANSDUCER PER AMM 32-42-06, OPS CHECK OK.

Part: FMC — FAILED (LEFT)

LEFT FMC FAILED IN FLIGHT, AIRCRAFT AIR TURNBACK.

Part: SOCKET — NOT SEATED (EMERGENCY LIGHT)

THREE E-PATH LIGHTS MOST FORWARD RIGHT SIDE BY R1 INOP. THE SOCKET FOR THE LIGHT WAS RESEATED, LIGHT THEN FUNCTION PROPERLY.

Part: TIRE — FAILED (MLG)

ON WALKAROUND FOUND NR 8 TIRE FLAT. BOTH TIRES NR 7 AND NR 8 TIRES REPLACED. WHEN NR 8 TIRE WENT FLAT THE THREAD SEPARATED CAUSING DAMAGE TO NR 7 SPOILER, UNDER WING PANELS, INBOARD AFT AND MAIN FLAP.

Part: WARNING LIGHT — ILLUMINATED (EQUIP COOLING)

ON CLIMBOUT EICAS MESSAGE FWD EQUIPMENT COOLING OVHD LIGHT. FOLLOWED QRH PROCEDURES WENT TO STBY MODE 4 MIN STATUS OVHD FOLLOWED QRH TO OVRD MODE. FOUR MINS LATER EICAS MESSAGE EQUIPMENT COOLING ILLUMINATED QRH PROCEDURES FOLLOWED, LANDED WITHIN 40 MIN.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

A-CHECK L1 DOOR EMERGENCY LIGHT INOP. RELAMPED L1 EMERGENCY LIGHT OPS CHECKED NORMAL. FWD GALLEY EMERGENCY LIGHT STRIP FADING.

Part: CHARGER — BURNED OUT (EMERGENCY LIGHTS)

L2 DIVIDER AND ROW 10 AB THROUGH 14AB EMERGENCY LIGHT INOPERATIVE.

Part: SLIDE — MISINSTALLED (FUSELAGE)

LT SLIDE ASSEMBLY BOTTOM ATTACH POINTS NOT SECURED DUE TO IMPROPER INSTALLATION, SLIDE REPLACED.

Part: SLIDE — MISINSTALLED (FUSELAGE)

L4 DOOR SLIDE DEPLOYED. ON INSPECTION FOUND SLIDE FELL OUT OF BUSTLE AND INFLATED. SLIDE WAS REPLACED FAILURE DUE TO IMPROPER INSTALLATION.

Part: LIGHT — INOPERATIVE (1L DOOR)

ROUTINE MAINTENANCE FOUND 1L EMERGENCY PATH ARROW LIGHT INOP.

Part: DOOR — STIFF (L2 DOOR)

DOOR L AT HARD TO ARM. ESCAPE SYSTEM EXAMINED AND EXERCISED FOR DOOR L AT IN ACCORDANCE WITH 25-66-01 206-001. OPERATION CHECKED NORMAL.

Part: BULB — INOPERATIVE (4R DOOR)

ROUTINE MAINTENANCE FOUND 4R EMERGENCY EXIT EXTERIOR LIGHT INOPERATIVE. RELAMPED 4R EMERGENCY EXIT EXTERIOR LIGHT, OPS CHECK OK.

Part: DOOR — MALFUNCTIONED (L2)

BEFORE DEPARTURE DOOR L2 UNABLE TO CLOSE PROPERLY. CLOSED BY FLIGHT MECHANIC. NO FURTHER PROBLEMS.

Part: TRANSMITTER — INOPERATIVE (HYD SYSTEM)

C- HYDRAULIC PRESSURE EICAS MESSAGE AND BOTH CENTER HYDRAULIC LOW PRESSURE LIGHTS ILLUMINATED, AFTER ACCOMPLISHMENT OF QRH NO HELP, CREW DECIDED TO RETURN BACK TO SNN. UNEVENTFUL LANDING WAS ACCOMPLISHED. TROUBLESHOOT SYSTEM AND FOUND CENTER HYDRAULIC AIR PUMP AUTO FUNCTION INOPERATIVE. ITEM DEFERRED PER MEL 29-11-4-1. CENTER HYDRAULIC SYSTEM TRANSMITTER REPLACED OPERATES NORMALLY.

Part: BATTERY PACK — INOPERATIVE (L2 DOOR)

DURING DAILY CHECK, FOUND EMERGENCY PATH LIGHTING FROM L1 TO L2 DOORS INOP. REPLACED EMERGENCY PATH LIGHTING BATTERY PACK, SYSTEM OPERATES NORMALLY.