N358AA

Part: MOUNT — BROKEN (EMERGENCY LIGHT) · airframe 109,747 hrs · 17,825 cycles

EMERGENCY EXIT WALL LIGHT IN FRONT OF SEAT 20G, HAS IT`S BASE MOUNT BROKEN. R & R IAW AMM 33-51-00. SYS CHECKED NORMAL.

Part: VALVE — INOPERATIVE (BLEED AIR SYS) · airframe 108,436 hrs · 17,604 cycles

INFLIGHT LT PRESS RELIEF VLV MSG & BLEED LIGHT ILLUMINATED. EMER DECLARED FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. PLACARDED HIGH PRESS BLEED IAW MEL. REPLACED PRU VLV & HP SOV. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 108,367 hrs · 17,592 cycles

SEATS 32AB TO 41AB EMER LIGHTS INOPERATIVE. REPLACED BATTERY PACK M739. OPERATIONS CHECKED NORMAL.

Part: LENS — DIRTY (CABIN) · airframe 108,367 hrs · 17,592 cycles

EMERGENCY LIGHT AT 20H HAS DEBRIS ON IT. REMOVED DEBRIS FROM LENS. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — BROKEN (CABIN) · airframe 108,367 hrs · 17,592 cycles

SEAT 34B EMER LIGHT INOPERATIVE. REPLACED BROKEN LIGHT CONNECTOR AT SEAT 34B. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 106,623 hrs · 17,309 cycles

EMERGENCY LIGHT ON AFT WALL OF MID GALLEY INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY FOR EMERGENCY LIGHT ON AFT WALL OF MID GALLEY. OPERATIONS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 106,623 hrs · 17,309 cycles

LT SIDE FIRST CLASS SEAT & OVERHEAD EMERGENCY LIGHTS FAILED TEST. REPLACED POWER SUPPLY M735 FOR THE LT SIDE FIRST CLASS SEATS & OVERHEAD EMERGENCY LIGHTS. OPERATIONS CHECKED NORMAL.

Part: SMOKE DETECTOR — DIRTY (LAVATORY) · airframe 106,458 hrs · 17,286 cycles

FWD LAVATORY SMOKE ALARM SOUNDED SEVERAL TIMES IN FLIGHT. ATTENDANTS WERE ABLE TO SILENCE. CLEANED & TESTED FWD LAVATORY SMOKE DETECTOR, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 103,245 hrs · 16,771 cycles

OVERHEAD EMERGENCY LIGHT AT SEAT 39H INOPERATIVE. REPLACED LAMP FOR SEAT 39H OVERHEAD EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 103,245 hrs · 16,771 cycles

OVERHEAD EMERGENCY LIGHT AT SEAT 31H INOPERATIVE. REPLACED LAMP FOR SEAT 31H OVERHEAD EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: CHARGER — FAILED (MAIN BATTERY) · airframe 103,146 hrs · 16,755 cycles

SJU - INFLIGHT MIA-GRU CREW REPORTED ELECTRIC ODOR IN THE COCKPIT AND BATTERY CHARGER CIRCUIT BREAKER POPPED. EMERGENCY DECLARED FLIGHT DIVERTED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND BURNING SMELL COMING FROM BATTERY CHARGER. REPLACED BATTERY CHARGER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: WEB — CRACKED (RT PYLON) · airframe 101,225 hrs · 16,457 cycles

RIGHT PYLON UPPER WEB AT GENERATOR FEEDER CABLES, PASS THROUGH. INSTALLED REPAIR DOUBLER AND FILLER SHIM ON RIGHT PYLON UPPER WEB AT GENERATOR FEEDER CABLES PASS THROUGH PER 767 AARD 54-52-01-1.

Part: CONNECTOR — LOOSE (CABIN) · airframe 100,369 hrs · 16,311 cycles

SEAT MOUNTED EMERGENCY LIGHT AT 39B INOPERATIVE. RE-SECURED LOOSE CONNECTOR AT SEAT 39B. OPS CHECK NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 97,968 hrs · 15,942 cycles

EMERGENCY LIGHT BY RIGHT COAT CLOSET BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT BY RIGHT COAT CLOSET. OPS CHECK NORMAL.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 95,712 hrs · 15,588 cycles

LAVATORY M1 SMOKE DETECTOR HAD TO BE RESET BUT THERE WAS NO SMOKE OR VISIBLE PROBLEMS WITH THE UNIT. LAVATORY LOCKED OUT FROM PUBLIC PER MEL. REPLACED M1 LAVATORY SMOKE DETECTOR AT LAX ON 02/27/2010. OPS CHECK NORMAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,681 hrs · 15,584 cycles

CORROSION WAS FOUND ON STATION 325 FLOORBEAM, BETWEEEN LEFT BUTTLINE 14 AND RIGHT BUTTLINE 47.5. CORROSION WAS BLENDED SMOOTH PER SRM STANDARD PRACTICES, REPAIR STRAPS INSTALLED OVER BLENDED AREAS. REMOVED CORROSION AND FABRICATED REPAIR STRAPS, ALODINED AND APPLY PRIMER. FOR COMPLETE REPAIR INFO, REFERENCE EA B767-015166.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,681 hrs · 15,584 cycles

CORROSION WAS FOUND AT STATION 347 FLOORBEAM BETWEEN RIGHT BUTTLINES 30 TO 77. REMOVED CORROSION BY BLENDING NOT EXCEEDING 0.067 INCH AND 0.069 INCH, ACCOMPLISHED GENERAL VISUAL. ALODINED AND APPLIED PRIMER TO BARE METAL PER EA B767-015169.

Part: FITTING — WORN (RT WING) · airframe 95,681 hrs · 15,584 cycles

WEAR WAS FOUND ON THE RIGHT WING UPPER KICK LOAD FITTING, OUTBOARD OF RIGHT BUTTLINE 97.42. REMOVED DEEP GOUGES, ACCOMPLISHED HFEC INSPECTION TO ENSURE NO CRACKS EXIST. ALODINED AND PRIMED. REFERENCE EA B767-57-015098.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 95,218 hrs · 15,506 cycles

SEAT 21C EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21C. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 95,218 hrs · 15,506 cycles

SEAT 25C EMERGENCY LIGHT INOPERATIVE. ALLOWED BATTERY PACK CHARGE TIME. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 95,218 hrs · 15,506 cycles

SEAT 23C EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23C. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 95,218 hrs · 15,506 cycles

SEAT 22C EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22C. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 95,218 hrs · 15,506 cycles

SEAT 24C EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 24C EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: ANTENNA — FAILED (WEATHER RADAR) · airframe 92,615 hrs · 15,055 cycles

MIA - CREW REPORTED WEATHER RADAR SYSTEM FAILURE. EMERGENCY DECLARED RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED WEATHER RADAR ANTENNA AND TRANSCEIVER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TRANSCEIVER — FAILED (WEATHER RADAR) · airframe 92,463 hrs · 15,027 cycles

MIA - CREW REPORTED BOTH WEATHER RADAR SYSTEMS FAILED. EMERGENCY DECLARED RETURNED MIA LANDED WITHOUT INCIDENT. REPLACED WEATHER TRANSCEIVER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 2B INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR INOPERATIVE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · 86,501 cycles

SFO EMERGENCY FLASHLIGHT AT FIRST CLASS FLIGHT ATTENDANT JUMPSEAT WAS USED. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT FIRST CLASS FLIGHT ATTENDANT JUMPSEAT. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

JFK - EXTERNAL EMERGENCY LIGHT AT LEFT AFT WING INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT LEFT AFT WING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — SCRATCHED (BS 1518-1554) · airframe 84,330 hrs · 13,703 cycles

AFW - FUSELAGE SKIN AT STATION 1518 TO 1554 HAS 48 INCH LONG SCRATCH THAT CROSSES THE LAP SPLICE BETWEEN STATION 1518, SKIN PANEL 146T3230, AND STATION 1554, SKIN PANEL 146T3240, AND EXTENDS FROM STRINGER S34L TO S39R, AREA IS 48 INCHES BY 1 INCH WITH AT DEPTH OF .057 AND .056 INCH. BLENDED AND SMOOTHED GOUGE. REMOVED FASTENERS WITHIN 1.5 DIAMETER OF BLENDED REGION. ALL FASTENER LOCATIONS HAVE A 2 DIAMETER FLAT AREA. MAINTAINED A BLEND RATIO OF 20 TO 1. ACCOMPLISHED A HIGH FREQUENCY EDDY CURRENT TO INSPECT FOR CRACKS. REINSTALLED FASTENERS AND APPLIED ALODINE 1000 TO BLENDED AREAS.

Part: CONTACT — DIRTY (EMERGENCY LIGHT)

SFO - LEFT NUMBER TWO DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. CLEANED LEFT NUMBER TWO DOOR EMERGENCY LIGHT ASSEMBLY CONTACT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT IN UPPER LEFT NUMBER FOUR DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT IN UPPER LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

MIA - FOUND EMERGENCY LIGHT AT SEAT 6H INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 6H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 20H BULKHEAD FORWARD OF SEAT INOPERATIVE. FOUND PIN PUSHED BACK. RESECURED PIN TO CONNECTOR FOR E EMERGENCY LIGHT AT SEAT 20H BULKHEAD FORWARD OF SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

MIA - FOUND EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EXTERIOR)

SFO - EXTERIOR EMERGENCY LIGHT AT LEFT AFT DOOR INOPERATIVE. RELAMPED EXTERIOR EMERGENCY LIGHT AT LEFT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE)

MIA INFLIGHT T1970/19JAN , CABIN PRESSURE CLIMBED THROUGH 12000 FEET. AT 13000 FEET, THE CAPTAIN MANUALLY DEPLOYED THE OXYGEN MASKS AND DESCENDED TO 10000 FT. NO AUTO INOPERATIVE LIGHT IN AUTO NR 2. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED ALL CANNISTERS AND REPACKED MASKS. REPLACED CONTROL PANEL NUMBER 2 PRESSURE CONTROLLER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DISPLAY — FAILED (COCKPIT)

CDG INFLIGHT T0120/6 MAR TCAS DISPLAY STARTED SMOKING ABOUT THREE HOURS AFTER TAKEOFF. SMOKE LASTED AROUND 10 SECONDS FOLLOWED BY BURNING ELECTRICAL SMELL. TCAS DISPLAY WENT BLANK. TURNED TRANSPONDER TCAS TO STANDBY AND PULLED TCAS CIRCUIT BREAKERS. NO FURTHER SMOKE OR ELECTRIC BURNING SMELL NOTED. REPLACED TCAS DISPLAY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY EXIT LIGHTS AND EMERGENCY LIGHTS AT SEATS 20 AND 21 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS AND EMERGENCY LIGHTS AT SEATS 20 AND 21. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — CRACKED (FUSELAGE)

FOUND FUSELAGE SKIN HAS SMALL CRACK INDICATION IN FASTENER HOLE, RIGHT SIDE, AREA 1 AT STATIN 1809.5, LOWER FORWARD FASTENER HAD CRACK INDICATION ON THE FUSELAGE SKIN ONLY. OVERSIZE THE HOLE IN THE SKIN ONLY TO 2ND OVERSIZE .341 INCH AND VERIFY CRACK IS REMVOED. REAMED SKIN ONLY FOR FREEZE PLUG. INSTALLED FREEZE PLUG PER SRM 767 51-20-01, INSTALLED FASTENERS AS REQUIRED. WORK ACCOMPLISHED IAW MRB 767-2506. FABRICATE AND INSTALL A RETAINER OVER THE FREEZE PLUG PER SRM 767/REQUIREMENTS. (M)

Part: WIRE — DAMAGED (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT 20AB-23AB WILL NOT TEST. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 21AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TERMINAL — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT AT L389 INOPERATIVE. REPLACED TERMINAL END AT EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: IDG — FAILED (NR 2 ENGINE)

LAX - GENERATOR OFF LIGHT ILLUMINATED ACCOMPANIED BY A RIGHT GENERATOR DRIVE DISCONNECT. REMOVED AND REPLACED NR 2 ENGINE IDG AS REQUIRED, OPS CHECK GOOD. LEAK CHECK GOOD. (M)

Part: IDG — FAILED (LEFT ENGINE)

HNL - FLT 123 - LEFT GENERATOR OFF LIGHT ILLUMINATED, WITH ASSOCIATED LIGHTS. PER QRH ATTEMPTED RESET, BUT NOT SUCCESSFUL. STARTED APU AND CONTINUED FLIGHT. REPLACED LEFT ENGINE IDG AND LT GCU PER MM. ENGINE RUN AND OPS CHECK OK. LEAK CHECK OF IDG OK. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT PATH LIGHTING AT SEAT 2H INOPERATIVE. REPLACED BATTERY PACK AND BATTERY CHARGER AT SEAT 2H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRUCTURE — CORRODED (TE FLAP)

AFW - FOUND CORROSION IN 2 MOUNT HOLES FOR LEFT NR 4 INBOARD FLAP ATTACH BEAM HOLES OVERSIZED TO .6450. VISUALLY INSPECT BORES TO ENSURE CORROSION REMOVAL. FABRICATED FREEZE PLUG FROM 7075-T6 TO ACHIEVE .001, INTERFERENCE FIT. ALODINE PLUGS INSTALL WET WITH BM5 5-95, REAM BORE HOLES TO ORIGINAL DIAMETERS MAINTAIN .060 WALL THICKNESS. INSTALL PRODUCTION TYPE WASHERS AT REWORK LOCATIONS INSTALL FLAP PER 767 AMM. (M)

Part: STRUCTURE — CORRODED (TE FLAPS)

AFW - FOUND CORROSION FOUND IN TWO MOUNT HOLES FOR RIGHT RN 5 INBOARD FLAP ATTACH BEAM. HOLES OVERSIZED TO REMOVE CORROSION, FINK HOLE SIZE .6440. VISUALLY INSPECT BORES TO ENSURE COMPLETE CORROSION REMOVAL. FABRICATED FREEZE PLUGS FROM 7075-T6 TO ACHIEVE MIN .001 INCH INTERFERENCE FIT. ALODINE AND INSTALL WET WITH BMS 5-95. REAM BORE TO ORIGINAL HOLE DIAMETER MAINTAIN .060 WALL THICKNESS. INSTALLED PRODUCTION TYPE WASHERS AT THE REWORKED LOCATIONS INSTALL FLAP PER 767 AMM. (M)

Part: STRUCTURE — CORRODED (TE FLAPS)

AFW - FOUND CORROSION IN HOLES AT AFT ATTACH OF RIGHT FLAP 9-10 BEAM. HOLES CLEANED UP BEYOND DIAMETER LISTED IN AARD 27-50-00-01. VISUALLY INSPECT BORES TO ENSURE CORROSION REMOVAL. FABRICATED BUSHINGS OF A1-N1-BR TO ACHIEVE MIN .001 INCH INTERFERENCE PIT, ALODINE AND INSTALLED WET W/BMS 5-95, REAM BORE BUSHING TO ORIGINAL HOLE DIAMETER. FABRICATED REPAIR WASHERS FROM .125 INCH THICK CRES WITH O/D OF .75, REFINISH REPAIR WASHER PER AARD 51-20-01-1. INSTALL WASHER IN PLACE OF ORIGINAL WASHERS. INSTALL FLAP PER 767 AMM. (M)

Part: FITTING — CORRODED (TE FLAPS)

AFW - FOUND CORROSION IN HOLES OF FITTING. CLEANED OUT CORROSION FROM HOLES DIAMETER NOW .5440 AND .5340. VISUALLY INSPECT BORES TO ENSURE CORROSION REMOVAL. FABRICATED FREEZE PLUG FROM 7075-TL TO ACHIEVE .001 INCH INTERFERENCE. ALODINE AND INSTALL WET WITH BMS 5-95. BEAM BORE TO ORIGINAL HOLE DIAMETER MAINTAIN .050 INCH WALL THICKNESS. FABRICATED REPAIR WASHERS FROM .25 INCH THICK AND .90 INCH OLD TO BE USED IN LIEU OF EXISTING PROD WASHERS. INSTALL FLAP PER 767 AMM. (M)

Part: ENGINE — VIBRATION (RIGHT)

HNL - FLT 298 - RIGHT ENGINE VIBRATION IND 2.8 WITH MASTER CAUTION ON ROTATION. ACCOMPLISHED VIBRATION SURVEY PER MM 71-00-00-5-H NR 7 VIBRATION WITHIN LIMITS 1.8 ON RUN-UP. NO PRV LIGHT OR MASTER CAUTION LIGHT BITE CHECK ON AIRSUPPLY MODULE ENGINE VIBRATION MONITOR OK. CONCURRED WITH TECH SERVICE. CHECKED ALL ENGINE PNEU DUCTS, CLAMPS, LINES. ALL OK. INLET AND EXHAUST OK 1.8 AT 104-1.4 AT 98.7 AT 95. (M)

Part: CONNECTOR — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE LIGHTS AT SEAT 28H AND 35B INOPERATIVE. REPAIRED CONNECTOR AT SEAT 28H AND 35B. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: COALESCER BAG — ODOR (CABIN AIR)

LAX - FLT 0002 - RIGHT AFTER TAKEOFF, CABIN AND COCKPIT CREW NOTICED A BURNING RUBBER/PLASTIC ODOR. MAINTENANCE ACCOMPLISHED OPERATIONS CHECK OF ELECTRICAL EQUIPMENT. UNABLE TO DUPLICATE ELECTRICAL SMOKE ODOR. AS A PRECAUTION, CHANGED COALESCER BAGS. OPERATED PACKS WITH ENGINES AND APU WITH NO SMOKE OR ELECTRICAL ODOR NOTED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: FLASHLIGHT — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT 3L DOOR INOPERATIVE. REPLACED FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT 3L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (BS 764)

AFW - FLOORBEAM AT STA 764 HAS CORROSION REMOVAL ON UPPER SURFACE. REMAINING IS BEYOND SRM LIMITS. BLENDED OUT CORROSION AND REFINISHED THE SURFACE PER SRM. THE BLEND REPAIR IS SATISFACTORY FOR CONTINUED SER SERVICE AS NOTED CONDITION. TST: 49,449 HOURS. CYCLES: 5,146. (X)

Part: SEAT TRACK — CORRODED (BS 770)

AFW - SEAT TRACK AT STA 770 AND LBL 11 HAS CORROSION REMOVAL ON UPPER SURFACE. BLENDED OUT CORROSION AND REFINISHED SURFACE PER SRM. THE BLENDED REPAIR IS SATISFACTORY FOR CONTINUED SERVICE AS NOTED CONDITION. TST: 49,949 HOURS. CYCLES: 8,146. (X)

Part: FLOORBEAM — CORRODED (BS 347)

AFW - FLOORBEAM AT STA 347 HAS CORROSION REMOVAL ON UPPER SURFACE. BLENDED OUT CORROSION AND REFINISHED SURFACE PER SRM. FILLED BLENDED AREA WITH BM55-95. THE BLEND REPAIR IS SATISFACTORY FOR CONTINUED SERVICE WITH NOTED. TST: 49,449 HOURS. CYCLES: 5,146. (X)

Part: LIGHT — DEFECTIVE (GALLEY)

MIA - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY RIGHT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FORWARD GALLEY RIGHT EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FMC — FAILED (E/E COMPT)

LEFT FMC FAILED EN ROUTE ORD-FRA RESET, FAILED. LANDED JFK. REPLACED LEFT FMC CROSSLAND SYSTEM ACCOMPLISHED. OPS TEST OK, ALL CHECKS GOOD. (M)

Part: TRANSFORMER — FAILED (E/E COMPT)

JFK - DURING CRUISE, THE COCKPIT EXPERIENCED SMOKE FOR A SHORT DURATION. SMOKE APPEARED TO BE COMING FROM THE CENTER CONSOLE ON THE FIRST OFFICER SIDE. LANDED JFK WITHOUT FURTHER INCIDENT. REPLACED BLEED AIR BITE MODULE TRANSFORMER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 11B INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT SIDEWALL CONNECTOR AT PAX SEAT 11B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTOR — NEED RESECURING (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT PASSENGER SEATS 7AB, 12AB, 34AB, TO AFT LAVATORY, AND 40HJ FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHTS CONNECTORS AT PASSENGER SEATS 7AB AND 34AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)