N373AA

Part: COVER — UNSECURE (EXIT SIGN) · airframe 99,024 hrs · 16,210 cycles

AIRCRAFT WAS NOT GROUNDED. R2 FLOOR LEVEL EXIT SIGN COVER IS OFF. INSTALLED EMERGENCY EXIT LIGHT LENS COVER IAW AMM 33-51-01.

Part: GIRT BAR — OBSTRUCTED (L4 DOOR) · airframe 98,261 hrs · 16,052 cycles

AIRCRAFT WAS NOT GROUNDED. 4L DOOR IS DIFFICULT TO ARM. MAINTENANCE REMOVED DEBRIS AND CLEANED 4L DOOR GIRT BAR SLIDE ON DOOR SADDLE PER MM 25-66-05.

Part: STEP — DEPLOYED (ZONE 800) · airframe 98,035 hrs · 15,997 cycles

AIRCRAFT WAS GROUNDED. LEFT AFT OVERWING EMERGENCY EVACUATION SLIDE STEP DEPLOYED. OPENED LEFT AFT OVERWING HATCH AND STOWED STEP IAW AMM 52-21-01. OPERATIONAL CHECK GOOD.

Part: GIRT BAR — DIRTY (ZONE 800) · airframe 97,823 hrs · 15,945 cycles

AIRCRAFT WAS NOT GROUNDED. R3 DOOR EMERGENCY EVACUATION SLIDE IS DIFFICULT TO ARM. CLEANED DEBRIS FROM GIRT BAR LOCK IAW AMM 52-00-00. OPERATIONAL CHECK GOOD.

Part: NUT PLATE — DETACHED (EMERGENCY LIGHT) · airframe 97,468 hrs · 15,866 cycles

EXTERIOR EMERGENCY LIGHT LEFT SIDE HAS A NUT PLATE FOR LENS COVER DETACHED. SECURED THE NUT PLATE. OPERATIONAL CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 97,383 hrs · 15,842 cycles

FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AFT OF RIGHT SIDE ROW 13 HAS A BROKEN CRADLE. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY IAW AMM 25-64-00. OPERATIONAL CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (MID GALLEY) · airframe 97,344 hrs · 15,834 cycles

FLIGHT ATTENDANT FLASHLIGHT LEFT SIDE MID GALLEY IS INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT. OPS CHECKED GOOD.

Part: RELAY — DEFECTIVE (OVERWING SLIDE) · airframe 96,069 hrs · 15,555 cycles

LEFT OVERWING SLIDE SUCCESSFULLY DEPLOYED WHILE ACCOMPLISHING LT & RT EMERGENCY SQUIB TESTS. FOUND RELAY K838 (SQUIB TEST 1 RELAY) NOT PROVIDING POWER TO LEFT OVERWING ESCAPE SYSTEM POWER SUPPLY. REPLACED THE RELAY IAW SWPM 20-81-22. THE AIRCRAFT WAS GROUNDED.

Part: CHARGER — INOPERATIVE (EVAC SLIDE) · airframe 95,585 hrs · 15,464 cycles

ACFT WAS GNDED. FLIGHT CREW REPORTS BOTH OVERWING SLIDE SQUIBS TEST INOPERATIVE. ACCOMPLISHED FIM 25-65-00 & FOUND EMER BATTERIES AT FAULT. R & R BATTERY ASSEMBLIES & CHARGER ASSEMBLIES AT LOCATIONS M961 & M962. PERFORMED OPERATIONAL CHECKS IAW MM 25-65-00. SYSTEMS CHECKED NORMAL. SEE ALSO AALA 20160516016, AALA 20160516017 & AALA 20160516018.

Part: BATTERY — DISCHARGED (EVAC SLIDE) · airframe 95,585 hrs · 15,464 cycles

AIRCRAFT WAS GNDED. FLIGHT CREW REPORTS BOTH OVERWING SLIDE SQUIBS TEST INOPERATIVE. ACCOMPLISHED FIM 25-65-00 & FOUND EMER BATTERIES AT FAULT. R & R BATTERY ASSEMBLIES & CHARGER ASSEMBLIES AT LOCATIONS M961 & M962. PERFORMED OPERATIONAL CHECKS IAW MM 25-65-00. SYSTEMS CHECKED NORMAL. SEE ALSO AALA 20160514001, AALA 20160516016 & AALA 2016051618.

Part: CHARGER — INOPERATIVE (EVAC SLIDE) · airframe 95,585 hrs · 15,464 cycles

AIRCRAFT WAS GNDED. FLIGHT CREW REPORTS BOTH OVERWING SLIDE SQUIBS TEST INOPERATIVE. ACCOMPLISHED FIM 25-65-00 & FOUND EMER BATTERIES AT FAULT. R & R BATTERY ASSEMBLIES & CHARGER ASSEMBLIES AT LOCATIONS M961 & M962. PERFORMED OPERATIONAL CHECKS IAW MM 25-65-00. SYS CHECKED NORMAL. SEE ALSO AALA 20160514001, AALA 20160516017 & AALA 20160516018.

Part: BATTERY — DISCHARGED (EVAC SLIDE) · airframe 95,585 hrs · 15,464 cycles

AIRCRAFT WAS GNDED. FLIGHT CREW REPORTS BOTH OVERWING SLIDE SQUIBS TEST INOPERATIVE. ACCOMPLISHED FIM 25-65-00 & FOUND EMER BATTERIES AT FAULT. R & R BATTERY ASSEMBLIES & CHARGER ASSEMBLIES AT LOCATIONS M961 & M962. PERFORMED OPERATIONAL CHECKS IAW MM 25-65-00. SYS CHECKED NORMAL. SEE ALSO AALA 20160514001, AALA 20160516016 & AALA 20160516017.

Part: CONTACT — DIRTY (ZONE 200) · airframe 95,072 hrs · 15,352 cycles

AIRCRAFT WAS IN BASE MX. LT AFT ENTRY DOOR SLIDE & GND EXTERIOR LIGHT INOPERATIVE. CLEANED ENTRY DOOR CONTACTS & PERFORMED OPERATIONAL CHECK IAW AMM 33-51-03.

Part: LENS — MISSING (CABIN) · airframe 95,072 hrs · 15,352 cycles

AIRCRAFT WAS IN BASE MX. SEAT B26 EPL PROXIMITY LENS IS MISSING. INSTALLED NEW LENS IAW AMM 33-51-10.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 95,034 hrs · 15,344 cycles

ON APPROACH, WHEN FLAPS 30 SELECTED FOR LANDING, TE AMBER ILLUMINATED, EICAS CAUTION TE FLAP ASYM FAULT WITH NO NEEDLE SPLIT, NO ROLL, & GAUGE INDICATES FLAPS AT 30. EMER DECLARED & FLIGHT LANDED UNEVENTFULLY. ACCOMPLISHED FLAP & SLAT ELEX UNIT RESET, RECENT FAULTS SHOWS TE ASYM XMT 4 - 5 MSG NBN 27-51084. PERFORMED FIM 27-51-03-00/27-51 FAULT TREE 801. MSG DID NOT REAPPEAR. OPERATED SYS TWICE ELECTRICALLY, OPERATIONS CHECKED GOOD. MSG FAULT NOT SHOWN. THE ACFT WAS NOT GNDED.

Part: PROBE — DEFECTIVE (FUEL SYSTEM) · airframe 94,844 hrs · 15,302 cycles

LEFT FUEL QTY INDICATOR & TOTALIZER QTY WENT BLANK DURING CRUISE. THE FLIGHT DECLARED AN EMER & RETURNED WITHOUT FURTHER INCIDENT. THE ACFT WAS GNDED. REPLACED DEFECTIVE FUEL PROBES.

Part: TEST PANEL — FAULTY (ZONE 200) · airframe 93,660 hrs · 15,052 cycles

DURING SQUIB TEST 1 & 2 LT & RT EMER ESCAPE INDICATOR LIGHTS REMAINED EXTINGUISHED. ACCOMPLISHED FIM 25-65-00-815-820-002-2. R & R LT OFF WING ESCAPE SYS EMER BATTERIES IAW AMM 25-65-17. R & R SQUIB TEST PANEL IAW AMM 26-21-04. SQUIB TEST 1 & 2 LT & RT CHECKED NORMAL. SEE ALSO AALA20150911008.

Part: BATTERY — DISCHARGED (ZONE 200) · airframe 93,660 hrs · 15,052 cycles

DURING SQUIB TEST 1 & 2 LT & RT EMER ESCAPE INDICATOR LIGHTS REMAINED EXTINGUISHED. ACCOMPLISHED FIM 25-65-00-815-820-002-2. R & R LT OFF WING ESCAPE SYS EMER BATTERIES IAW AMM 25-65-17. R & R SQUIB TEST PANEL IAW AMM 26-21-04. SQUIB TEST 1 & 2 LT & RT CHECKED NORMAL. SEE ALSO AALA20150911008.

Part: PIN — BACKED OUT (ZONE 400) · airframe 93,331 hrs · 14,985 cycles

EMERGENCY DECLARED & LANDING UNEVENTFUL. DURING CRUISE RECEIVED ANTI-SKID INOPERATIVE INDICATION & RIGHT ENGINE BLEED FAULT. FOUND A PUSHED BACK SOCKET PIN ON CONNECTOR D10984. REINSTALLED PIN IAW WPM 20-61-00. BITE CHECK & OPERATIONAL CHECK PERFORMED IAW AMM 36-23-00 & MCM CARD 71-95-02. NO EICAS MESSAGES OR DISCREPANCIES NOTED. SYSTEM CHECKED NORMAL. SEE ALSO AALA20150729005.

Part: WIRE — SHORTED (LANDING GEAR) · airframe 93,331 hrs · 14,985 cycles

EMERGENCY DECLARED & LANDING UNEVENTFUL. DURING CRUISE RECEIVED ANTI-SKID INOPERATIVE INDICATION & RIGHT ENGINE BLEED FAULT. REPAIRED SHORTED WIRING IN LANDING GEAR HARNESS. ALL EICAS MESSAGES ARE CLEAR & ANTI-SKID SYSTEM BITE CHECKED GOOD IAW AMM 32-42-01. SEE ALSO AALA20150731003.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 93,329 hrs · 14,984 cycles

STRINGER 36R IS CRACKED AT FS 1194. ACCOMPLISHED STRINGER REPAIR IAW SRM 53-00-03-2R-3 & EA 252880 & 252893.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,329 hrs · 14,984 cycles

STRINGER 34R IS CORRODED AT FS 440. INSTALLED NEW STRINGER SECTION WITH SPLICES IAW AMM 25-53-01 & SRM 53-00-03.

Part: SKIN — CORRODED (FUSELAGE) · airframe 93,329 hrs · 14,984 cycles

SKIN LAP CORRODED AT FS 1194 & STRINGER 36R. ACCOMPLISHED DOUBLER REPAIR IAW SRM 53-00-01-2R-12.

Part: SKIN — CORRODED (LT WING) · airframe 93,329 hrs · 14,984 cycles

LEFT WING UPPER SKIN IS CORRODED UNDER OVERWING FILL PORT. REPAIRED OVERWING FILL PORT IAW AMM 28-11-04 & EA 252212.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,329 hrs · 14,984 cycles

NUMBER 6 SEAT TRACK OTBD FLANGE AT RBL11.6 IS CORRODED BETWEEN FS 840 & 848. ACCOMPLISHED SPLICE REPAIR SRM 53-00-51-2R2-3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,329 hrs · 14,984 cycles

CABIN FLOORBEAM CAP AT STATION 325 IS CORRODED BETWEEN LBL 30 & RBL 58. R & R BEAM CAP IAW SRM 53-00-51-2R-1 & EA 252357.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,329 hrs · 14,984 cycles

AFT CARGO COMPARTMENT FLOORBEAM AT FS 1153 IS CORRODED AT NUTPLATES & ROLLER TRAY ATTACH POINTS BETWEEN LBL 32 & RBL 32. R & R FLOORBEAM T CHORD IAW AARD 51-00-05.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,329 hrs · 14,984 cycles

AFT CARGO COMPARTMENT FLOORBEAM AT FS 1197 IS CORRODED AT NUTPLATES & ROLLER TRAY ATTACH POINTS BETWEEN LBL 32 & RBL 32. R & R FLOORBEAM T CHORD IAW AARD 51-00-05.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,329 hrs · 14,984 cycles

AFT CARGO COMPARTMENT CTR TOP WEB CORRODED BETWEEN FS 1153 & 1175. R & R WEB IAW SRM 51-10-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,329 hrs · 14,984 cycles

AFT CARGO COMPARTMENT FLOORBEAM AT FS 1173 IS CORRODED AT NUTPLATES & ROLLER TRAY ATTACH POINTS BETWEEN LBL 32 & RBL 32. R & R FLOORBEAM T CHORD IAW AARD 51-00-05.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,329 hrs · 14,984 cycles

FORWARD GALLEY MOUNT FITTING AT RBL 68 & FS 284 IS CORRODED. R & R GALLEY MOUNT IAW AARD 51-00-05.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,329 hrs · 14,984 cycles

AFT CARGO COMPARTMENT FLOORBEAM AT FS 1197 + 132 IS CORRODED. REPLACED FLOORBEAM T CAP IAW AARD 51-00-05-1.

Part: LIGHT — BROKEN (CABIN) · airframe 92,351 hrs · 14,818 cycles

SEAT MOUNTED EMER LIGHT AT 32HJ IS BROKEN. R & R LIGHT ASSEMBLY. PERFORMED OPERATIONAL CHECK IAW AMM 33-51-10. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (ZONE 100) · airframe 92,351 hrs · 14,818 cycles

FOUND EMER EXIT OVERWING LIGHT ASSEMBLY L396 INOPERATIVE. R & R LAMPS ON LIGHT ASSEMBLY IAW AMM 33-51-04. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 91,935 hrs · 14,749 cycles

RIGHT AFT EMER DOOR EXTERIOR LIGHT L392 INOPERATIVE. R & R EXTERIOR LIGHT LAMP AT L392 IAW AMM 33-51-06. SYS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 91,935 hrs · 14,749 cycles

LEFT AFT DOOR EMER EXTERIOR LIGHT 397 INOPERATIVE. R & R POWER SUPPLY M738 IAW AMM 33-51-07. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 90,703 hrs · 14,533 cycles

LEFT NR 4 DOOR EXTERIOR GND ILLUMINATION EMER LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 4 DOOR EXTERIOR EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,290 hrs · 14,463 cycles

RIGHT NR 1 DOOR THRESHOLD EMER LIGHT INOPERATIVE. REPLACED LAMP FOR RT NR 1 DOOR THRESHOLD EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 90,290 hrs · 14,463 cycles

SEAT 5H AFT EMER LIGHT INOPERATIVE. SECURED LOOSE CONNECTOR FOR SEAT 5H AFT EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 90,290 hrs · 14,463 cycles

RIGHT FIRST CLASS EMER LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR RT FIRST CLASS EMER LIGHTS. OPERATIONS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 89,921 hrs · 14,402 cycles

EMERGENCY LIGHT AT SEAT 36H MISSING LENS. REPLACED LENS FOR EMER LIGHT AT SEAT 36H. OPERATIONS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 89,921 hrs · 14,402 cycles

EMERGENCY LIGHT AT SEAT 32H MISSING LENS. REPLACED LENS FOR EMER LIGHT AT SEAT 32H. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,921 hrs · 14,402 cycles

EMERGENCY AISLE LIGHT AT SEAT 6B INOPERATIVE. REPLACED LAMP FOR EMER AISLE LIGHT AT SEAT 6B. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 89,387 hrs · 14,318 cycles

RIGHT NR 4 DOOR EXTERIOR EMER LIGHT INOPERATIVE. REPLACED LAMP FOR RT NR 4 DOOR EXTERIOR EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 89,387 hrs · 14,318 cycles

LEFT EXTERIOR EMER LIGHT ABOVE ADP EXHAUST PORT IS INOPERATIVE. REPLACED LAMP FOR LT EXTERIOR EMER LIGHT ABOVE ADP EXHAUST PORT. OPERATIONS CHECKED NORMAL.

Part: PUMP — INOPERATIVE (FUEL SYSTEM) · airframe 88,426 hrs · 14,173 cycles

LHR CREW REPORTED RT FUEL QTY DECREASING IN CTR TANK. EMERGENCY DECLARED FLIGHT RETURNED LHR LANDED WITHOUT INCIDENT. ACCOMPLISHED FIM 28-22-00-815-829 WITH NO EXTERNAL LEAKS NOTED. FLIGHT CONTINUED TO DESTINATION. REPLACED RT OVERRIDE PUMP & SHUT OFF SLEEVE AT MIA ON 03/15/2014. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: LENS — DEFECTIVE (CABIN) · airframe 88,044 hrs · 14,107 cycles

SEAT 20H AFT ESCAPE PATH LIGHT LENS INOPERATIVE. REPLACED LENS FOR SEAT 20H AFT ESCAPE PATH LIGHT, OPERATIONS CHECKED NORMAL.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 87,973 hrs · 14,094 cycles

CRACK ON OUT STOP WEB SUPPORT AT STATION 1295. R & R WEB SUPPORT IAW AARD 53-60-53-1.

Part: WEB — CRACKED (FUSELAGE) · airframe 87,973 hrs · 14,094 cycles

CRACKED WEB AT STATION 1320. INSTALLED EXTERNAL DOUBLER IAW SRM 51-70-13-0G.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 87,799 hrs · 14,065 cycles

RT NR 5,6 & 7 EXTERIOR FUSELAGE MOUNTED SLIDE & EXIT ILLUMINATION LIGHTS INOPERATIVE. REPLACED BATTERY PACK M731 FOR RT SIDE EXTERIOR FUSELAGE MOUNTED SLIDE & EXIT ILLUMINATION LIGHTS. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,799 hrs · 14,065 cycles

SEAT MOUNTED EMERGENCY WHITE LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY WHITE LIGHT. OPERATIONS CHECKED NORMAL.

Part: SLIDE — DEPLOYED (OVERWING EXIT) · airframe 87,367 hrs · 13,995 cycles

BOG RT OVERWING EMERGENCY SLIDE DEPLOYED & SEPARATED FROM AIRCRAFT DURING CLIMB OUT. EMERGENCY DECLARED FLIGHT RETURNED BOG LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FLIGHT FERRIES TO TUL FOR FURTHER MAINTENANCE. SYSTEM GROUND CHECKED NORMAL OPERATION OPEN.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 87,339 hrs · 13,989 cycles

INTERIOR LT FWD OVERWING, LOWER EXIT MARKER, 1 SEGMENT INOPERATIVE. REPLACED LAMP FOR EXIT SIGN. OPERATION CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 87,339 hrs · 13,989 cycles

RT EXTERIOR FS MOUNTED NR 4 ESCAPE PATH ILLUMINATION LIGHT. REPLACED LAMP FOR RT SIDE EXTERIOR FS MOUNTED NR 4 ESCAPE PATH ILLUMINATION LIGHT. OPERATIONS CHECKED NORMAL.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 86,372 hrs · 13,819 cycles

CORROSION & CRACKS FOUND BASE AREA OF NR 3 VHF ANTENNA. REMOVED DAMAGE & INSTALLED DOUBLERS IAW SRM 53-60-01 & EA B767-53-030564.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,737 hrs · 13,246 cycles

RIGHT KEEL BEAM FLANGE HAS AREA OF CORROSION TOP SIDE AT STATION 1052. INSTALLED FREEZE PLUG REPAIR PER SRM 51-20-07.

Part: WEB — CRACKED (LT PYLON) · airframe 82,737 hrs · 13,246 cycles

LEFT PYLON FORWARD TORQUE BOX FEEDER CABLE THRU HOLE CRACKED. REPAIRED PER AARD 54-52-01.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 82,737 hrs · 13,246 cycles

INTERCOSTAL FROM STATIONS 478 TO 497 RIGHT BUTTLINE 40 CRACKED. REPLACED INTERCOSTAL PER AARD 51-40-02.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,737 hrs · 13,246 cycles

FORWARD CARGO, CORROSION UNDER OUTBOARD AFT MOUNT OF POWER DRIVE UNIT 5R. REPLACED PDU MOUNT PET SRM 51-40-02.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,737 hrs · 13,246 cycles

AUXILIARY CHORD FROM STATIONS 478 TO 632 CORRODED. REPLACED AUXILAIRY CHORD PER SRM 51-40-02.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,737 hrs · 13,246 cycles

SKIN CORRODED AT STATION 1087 AND STRINGERS 39 LEFT AND RIGHT. BLENDED CORROSION.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,737 hrs · 13,246 cycles

SKIN AT STATION 1197 + 142 AND STRINGER 39 RIGHT CORRODED. INSTALLED EXTERNAL DOUBLER REPAIR PER SRM 53-00-01.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,737 hrs · 13,246 cycles

SKIN STRAP AT STATION 1582 STRINGER 39 LEFT AND RIGHT CORRODED. REPLACED STRAP PER SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 82,737 hrs · 13,246 cycles

LEFT BUTTLINE 40 UPPER CHORD BETWEEN STATIONS 742 TO 764 CRACKED. REPLACED INTERCOSTAL PER AARD 53-30-00.

Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 82,737 hrs · 13,246 cycles

CORROSION ON RIGHT TOP SIDE OF STABILIZER IN TWO PLACES. INSTALLED DOUBLER PER B767-55-024567.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 81,259 hrs · 12,995 cycles

LEFT DOOR AFT EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED LAMP FOR LEFT DOOR AFT EXTERIOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 81,259 hrs · 12,995 cycles

LEFT NUMBER 4 DOOR WALLSIDE EMERGENCY SIGN LOWER PORTION INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 4 DOOR WALLSIDE EMERGENCY SIGN. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 81,259 hrs · 12,995 cycles

RIGHT AFT EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED LAMP FOR RIGHT AFT EXTERIOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY) · airframe 80,366 hrs · 12,857 cycles

RIGHT MID LAVATORY SMOKE DETECTOR SOUNDED DURING APPROACH. NO SMOKE WAS PRESENT. RESET BY CREW BUT WENT OF AGAIN AFTER ARRIVING AT GATE. REPLACED SMOKE DETECTOR AT M2 LAVATORY.

Part: ALTIMETER — UNRELIABLE (COCKPIT) · airframe 79,854 hrs · 12,778 cycles

HNL - CREW REPORTED STANDBY ATTITUDE INDICATOR INOPERATIVE. EMERGENCY DECLARED FLIGHT RETURNED HNL LANDED WITHOUT INCIDENT. REPLACED INTEGRATED STANDBY AIRSPEED ALTIMETER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BRAKE — FAILED (NR 7) · airframe 79,502 hrs · 12,724 cycles

ORD - CREW REPORTED AFTER LANDING AND CLEAR OF RUNWAY ANOTHER AIRCRAFT AND TOWER ADVISED THAT RIGHT MAIN LANDING GEAR ON FIRE. EMERGENCY EVACUATION WAS DECLARED. LEFT SLIDES WERE DEPLOYED FOR EVACUATION. AIRCRAFT REMOVED FROM SERVICE. MAINTENANCE FOUND NUMBER 7 BRAKE HAD FAILED. REPLACED NUMBER 7 BRAKE AND NUMBERS 7 AND 8 TIRES. INSPECTION OF THE RIGHT LANDING GEAR AXLES SHOWED NO EVIDENCE OF DAMAGE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: IDG — FAULTY (LT ENGINE) · airframe 79,028 hrs · 12,658 cycles

ORD - CREW REPORTED AFTER TAKEOFF LEFT ENGINE INTEGRATED DRIVE GENERATOR DROPPED OFF LINE AND WOULD NOT RESET. EMERGENCY DECLARED FLIGHT RETURNED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT IDG. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SLAT — DAMAGED (RT WING) · airframe 77,880 hrs · 12,478 cycles

DAMAGE WAS FOUND TO THE NUMBER 7 SLAT OUTBOARD EDGE AT APPROXIMATE WING STATION 345 NEAR THE TRAILING EDGE. ACCOMPLISHED REPAIR PER MAJOR EA COMP-57-015661.

Part: FLOORBEAM — PUNCTURED (FUSELAGE) · airframe 77,880 hrs · 12,478 cycles

PUNCTURE TO THE FUSELAGE PASSENGER FLOORBEAM UPPER WEB ASSEMBLY AT STATION 246 RIGHT BUTTLINE 64 AND WATERLINE 201. ACCOMPLISHED DOUBLER REPAIR PER MAJOR EA B767-53-015560.

Part: LIGHT — MISSING (CABIN) · airframe 74,705 hrs · 11,900 cycles

SEAT 26H EMERGENCY LIGHT MISSING LAMP. REPLACED LAMP IN SEAT 26H EMERGENCY EXIT LIGHT. OPS CHECKED NORMAL.

Part: FLASHLIGHT — NOT SEATED (CABIN) · airframe 74,705 hrs · 11,900 cycles

FIRST CLASS GALLEY LEFT FLIGHT ATTENDANT SEAT FLASHLIGHT INOPERATIVE. RESEATED FLIGHT ATTENDANT EMERGENCY FLASH LIGHT CHARGING PORT. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,138 hrs · 11,611 cycles

EMERGENCY EXIT LIGHT WILL NOT COME ON WHEN LIGHT SWITCH ON. REPLACED EXIT LIGHT.

Part: STRIKER — FAILED (COCKPIT DOOR) · airframe 72,426 hrs · 11,489 cycles

IN CRUISE AT FLIGHT LEVEL 350 A STRONG SMELL WAS PREVALENT IN COCKPIT FOLLOWED BY THE "LOCK FAIL" LIGHT ILLUMINATING. THE COCKPIT DOOR LATCH WAS WARM TO TOUCH AND APPEARED THE SOURCE OF THE ACRID SMELL. PULLED CIRCUIT BREAKERS FOR FLIGHT DECK LOCK AND FORWARD ENTRY. LANDED LGW WITHOUT INCIDENT. REPLACED FLIGHT DECK DOOR STRIKE.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 72,410 hrs · 11,485 cycles

IMPACT DAMAGE TO FLOORBEAM UPPER WEB AT STATION 246 LEFT BUTTLINE 9 TO LEFT BUTTLINE 13. REINFORCED FLOORBEAM UNDER ENGINEERING AUTHORITY 007533.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 72,410 hrs · 11,485 cycles

FOREIGN OBJECT DAMAGE TO INNER CHORD AT STATION 522 STRINGER 30 LEFT TO 31 LEFT. REPLACED CHORD UNDER EA 007417.

Part: LIGHT — BROKEN (ZONE 200) · airframe 71,439 hrs

JFK - SEAT 6B EMERGENCY PATH LIGHTING INOPERATIVE AND AISLE SIDE PANEL IS NOT INSTALLED. REPLACED EMERGENCY PATH LIGHT ASSEMBLY AND REINSTALLED PANEL.

Part: ENGINE — VIBRATION (RIGHT)

LAX INFLIGHT T297/28SEP - CREW REPORTED NUMBER TWO ENGINE N2 VIBRATION INDICATING 3.7 ON CLIMB. NUMBER TWO ENGINE FIRE LOOP ONE ILLUMINATED FIVE TO TEN MINUTES THEN EXTINGUISHED. LANDED LAX WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE ON 30 SEP 2007 AT LAX DUE TO HIGH N2 VIBRATION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: GROUND WIRE — LOOSE (EMERGENCY LIGHTS)

ORD - EMERGENCY LIGHTS AT RIGHT SIDE OF FIRST CLASS INOPERATIVE. SECURED TWO LOOSE GROUND WIRES GD90000DC AND GD900015 FOR EMERGENCY LIGHTS AT RIGHT SIDE OF FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

MIA - EMERGENCY EXIT LIGHT AT LEFT NUMBER THREE ENTRY DOOR INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT LEFT NUMBER THREE ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

SFO - EXTERIOR EMERGENCY LIGHT AFT OF RIGHT FLAP INOPERATIVE. RELAMPED EXTERIOR EMERGENCY LIGHT AFT OF RIGHT FLAP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 23H INOPERATIVE. RELAMPED SEAT MOUNTED EMERGENCY LIGHT AT SEAT 23H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (SEAT 28H)

DFW - EMERGENCY LIGHT AT SEAT 28H INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 28H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA - EMERGENCY LIGHT EXIT SIGN BY SEAT 20G BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY FOR EMERGENCY LIGHT EXIT SIGN AT SEAT 20G. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

ORD - EMERGENCY LIGHTS AT SEAT 2H INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHTS AT SEAT 2H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DEFECTIVE (CABIN)

ORD - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 26B INOPERATIVE. REPLACED CONNECTOR AND CONTACT SOCKET (1703663 MID STATE AEROSPACE) FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 26B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE HARNESS — FAULTY (CABIN)

EMERGENCY LIGHTS AT SEATS 26AB INOPERATIVE. REPLACED HARNESS AT 26AB FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT SEAT 24B INOPERATIVE. REPLACED EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 24B. SYSTEM GROND CHECKED NORMAL OPERATION. (M)

Part: LINE — DAMAGED (HYD SYSTEM)

DURING CLIMB, RECEVIED EICAS MESSAGE, LOW CENTER HYDRAULIC QUANTITY. PERFORMED PROCEDURE, TURNED OFF CENTER PUMPS WITH CENTER SYSTEM SHOWING APPROX .25 QUANTITY. RETURNED TO ORD, ACCOMPLISHED ALTERNATE GEAR AND FLAP EXTENSION. LANDED ORD WITHOUT INCIDENT. REPLACED RIGHT MLG TRUCK POSITION ACTUATOR LINE AND NR 1 CENTER HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING AT AT 30H INOPERATIVE. REPINNED BROKEN EMERGENCY ESCAPE PATH LIGHTING WIRES TO CONNECTOR AT SEAT 30H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 28H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 29H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 29H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 23H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRING AT SEAT 23H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMEREGNCY LIGHTS AT SEAT 25B INOPERATIVE. RE-SECURED CONNECTOR. SYTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 38H INOPERATIVE. REPAIRED EMERGENCY EIT SEAT LIGHT CONNECTOR AT 38H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: UNKNOWN — ODOR (CABIN)

LAX - FLT 222 - AFTER TAKEOFF, CREW REPORTED BURNING SMELL AND HAZE THROUGHOUT CABIN. FLIGHT ATTENDANT REPORTED GRINDING NOISE OVER LEFT WING. GEAR AND DOORS WERE CLOSED. RETURNED AND LANDED LAX WITHOUT INCIDENT. ACCOMPLISHED INSPECTION AND PACK BURNOUT PER MM. NO SMOKE OR BURNING SMELL FOUND. UNABLE TO DUPLICATE. OPERATED FLAPS AND SPOILERS NO GRINDING NOISE HEARD. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — OPEN (FUSELAGE)

LAX - DURING OVERNIGHT MAINTENANCE, LEFT SPOILER SQUIB TEST INOPERATIVE. REPAIRED WIRE FOR LEFT SPOILER SQUIB. OPEN BETWEEN D5124P AND D5088. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — BROKEN (COCKPIT)

JFK - FLT 34 - ON LANDING, FLIGHT DECK EMERGENCY EXIT LIGHT ASSY DISLODGED FROM SOCKET. REPLACED FLIGHT DECK EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — CHAFED (ROW 2D)

ORD - FLT 99 - DURING LANDING ORD, A FLASH AND SPARKS WERE OBSERVED IN THE AREA OF THE L-1 DOOR AND THE AREA ABOVE THE CREDENZA AT SEAT 2D. AIRCRAFT LANDED WITHOUT INCIDENT. REPAIRED CHAFFED FORWARD GALLEY POWER WIRE, REPAIRED CHAFFED FORWARD FLIGHT ATTENDANT 02 MODULE WIRE. REPAIRED CHAFFED FORWARD GALLEY BALLAST WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (BS 1480)

AFW - FOUND FLOORBEAM CORRODED FOUND DAMAGE TO EXCEED SRM LIMITS AFTER BLENDING. ALODINED BLENDED AREA. FABRICATED AND INSTALLED REPAIR STRAP USING 0.050 INCH 301 1/2 HARD STAINLESS STEEL. APPROVED BY ENGINEERING PER MRB 767-1646. TST: 27,257.02 HOURS. CYCLES: 4,345. (X)

Part: FRAME — CORRODED (BS 1285)

AFW - BLENDED OUT CORROSION AT NUTPLATES. BLEND OUTS EXCEED SRM LIMITS. REFINISHED BLENDED AREAS. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION OF ENGINEERING PER MRB767-1643. TST: 27,257.02 HOURS. CYCLES: 4,345. (X)

Part: FRAME — CORRODED (BS 1263)

AFW - FLAP CORRODED. BLEND-OUT EXCEEDS SRM LIMITS. REFINISHED BLENDED AREAS. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1645. TST: 27,257.02 HOURS. CYCLES: 4,345. (X)

Part: FLOORBEAM — CORRODED (BS 347)

AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF THE UPPER CAP OF FLOORBEAM. THE BLENDOUT EXCEEDED SRM MAX ALLOWABLE LIMITS. ALODINED BLENDOUT. FABRICATED AND INSTALLED REPAIR STRAP USING .050 301.5 HARD STAINLESS STEEL. FILLED AND PRIMED AS REQUIRED. APPROVED BY ENGINEERING PER MRB 767-1647. (M)

Part: FIRE LOOP — MALFUNCTIONED (LT ENGINE)

MIA - FLT 2101 - LT ENGINE FIRE LP2, VERIFIED FIRE DETECTION WITH MANUAL MEL AND TUL TECH. NO ABNORMAL ENGINE INDICATIONS. CHECK NR 1 ENGINE FIRE PROTECTION, ERASED STATUS MESSAGE. AIRCRAFT OK FOR SERVICE PER RMM 26-2. (M)

Part: WIRE — BROKEN (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 28B INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT PASSENGER SEAT 28B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: OVERHEAT SWITCH — FAILED (RT MLG WW)

DFW - FLT 0945 - SHORTLY AFTER TAKEOFF, R-DUCT LEAK LIGHT CAME ON. BOTH EICAS AND OVERHEAD PANEL R-BLEED AND R-PACK SHUT DOWN WITH LIGHT. REPLACED DUCT LEAK WHEELWELL OVERHEAT CARD. TEST GOOD. REMOVED AND REPLACED STRUT OVERHEAT SWITCH. SYSTEM OPS CHECK GOOD. (X)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY LIGHTS AT PASSENGER SEAT 24H FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 24H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: PINS — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS BETWEEN PAX SEAT ROWS 8B TO 23B AND 35H TO 41H INOPERATIVE. RESEATED LOOSE EMERGENCY EXIT LIGHT PINS AT PAX SEAT ROWS 8B TO 23B AND 35H TO 41H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (SEAT 4B-12B)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PAX SEATS 4B THROUGH 12B INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT SIDEWALL CONNECTORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT RIGHT AISLE JUST FORWARD AND AFT OF MID GALLEY INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT SIDEWALL CONNECTOR BY PAX SEAT ROW 18H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

SJC - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PAX SEAT 2H AND AT PAX SEATS 7H THROUGH 29H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT PAX SEAT 2H AND RESECURED LOOSE EMERGENCY EXIT LIGHT SIDEWALL CONNECTOR AT PAX SEAT ROW 20H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL ASSY — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, THE EMERGENCY FLOOR EXIT PATH LIGHTS AT ROW 24H AND AFT GALLEY CROSS AISLE LIGHTS WERE FOUND INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT ASSEMBLY AT ROW 24H AND AFT GALLEY CROSS AISLE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROW 7AB TO 12AB INOPERATIVE. RESEATED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 7AB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: EEL STRIP — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS AT RIGHT SIDE MID GALLEY INOPERATIVE. REPLACED MID GALLEY RIGHT SIDE EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)

Part: EEL WIRE — BROKEN (CABIN)

JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 26AB AND 33AB FOUND INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRE BY PASSENGER SEAT 26AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)

Part: EEL INVERTER — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN MID-GALLEY INOPERATIVE. REPLACED INVERTER FOR EMERGENCY FLOOR LIGHTS IN MID-GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)