N384AA

Part: UNKNOWN — VIBRATION · airframe 100,765 hrs · 16,319 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS STRONG VIBRATION DURING GEAR EXTENSION. MAINTENANCE ACCOMPLISHED EXTENSION AND RETRACTION IAW AMM 32-30-00. OPS CHECK OK.

Part: STALL WARNING — FALSE ACTIVATION (COCKPIT) · airframe 100,016 hrs · 16,169 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS IN CRUISE FLT @ FL 340 AND .80 MACH, F/OS O FLAP MIN MANEUVERING INDICATOR (YELLOW HOOK) IN VIEW @ 255KTS OR ABOUT .74 MACH. ERRONEOUS STICK SHAKER WARNING ON FINAL APPROACH @ FLAPS 5 190 KTS. MAINTENANCE ACCOMPLISHED TROUBLESHOOTING, RESET C/B RIGHT ASWC. OPERATIONAL TEST NORMAL IAW AMM 27-32-00.

Part: COMPRESSOR BLADE — DAMAGED (RT ENGINE) · airframe 99,946 hrs · 16,154 cycles

AIRRAFT WAS GROUNDED: PILOT ABORTED TAKEOFF DUE TO RIGHT ENGINE POPING AND FLAMES. SUSPECT RIGHT ENGINE COMPRESSOR STALL. ABORT AT 50 KTS. MAINTENANCE ACCOMPLISHED A BORESCOPE OF THE ENGINE AND FOUND SOME DAMAGED COMPRESSOR BLADES. AN ENGINE CHANGE HAS BEEN DECLARED.***SUPPLEMENTAL INFORMATION: MAINTENANCE REMOVED AND REPLACED RT ENGINE IAW JOB CARD 71-93-01 AND RUNUP TEST CARD 71-95-22. OPS TEST GOOD.*** (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,887 hrs · 16,139 cycles

AIRCRAFT WAS NOT GROUNDED: LEFTHAND CENTER LIGHT INOPERABLE. MAINTENANCE REPLACED EMERGENCY LIGHT ASSEMBLY PER STANDARD PRACTICES.

Part: GEARBOX — BINDING (TE FLAP) · airframe 99,878 hrs · 16,137 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS FLAP RETRACTION AND EXTENSION, BETWEEN UP AND 1 GENERATES A LOUD GRINDING NOISE. SEEMS TO BE ON LEFT (CA) SIDE OF ACFT. INFLIGHT ONLY. MAINTENANCE REPLACED THE LT T/E FLAP OFFSET GEARBOX IAW AMM 27-51-38-401. OPS CHECK OK.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 99,086 hrs · 15,949 cycles

SEAT 22H EMERGENCY LIGHT WAS INOPERATIVE. CONNECTED EMERGENCY LIGHT CONNECTOR AT SEAT 22H IAW AMM 33-51-10. OPS CHECKED NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 98,737 hrs · 15,873 cycles

SEAT EMERGENCY LIGHTS IN THE AFT LEFT CABIN WERE INOPERATIVE. FOUND NO OUTPUT FROM THE CHARGER. REPLACED THE CHARGER.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 98,737 hrs · 15,873 cycles

SEAT AISLE LIGHTS IN AFT LEFT CABIN WERE INOPERATIVE. FOUND NO OUTPUT FROM THE CHARGER. REPLACED BOTH THE BATTERY AND CHARGER,

Part: TRACK — LOOSE (RT WING) · airframe 98,734 hrs · 15,872 cycles

RIGHT WING OUTBOARD FLAP DEFLECTION CONTROL TRACK CAME LOOSE. THE AIRCRAFT WAS GROUNDED. CONNECTED FLAP DEFLECTION CONTROL TRACK IAW AMM 27-51-23-101.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 98,718 hrs · 15,869 cycles

EXTERIOR LEFT EMERGENCY LIGHT AT THE AFT FUSELAGE WAS INOPERATIVE. REPLACED THE BATTERY CHARGER AND BATTERY IAW AMM 33-51-07. OPS CHECKED NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 97,960 hrs · 15,711 cycles

AIR IN FWD OF AIRCRAFT CAUSED DIZZINESS TO FLT ATTENDANTS AND PILOTS, AND SOME FIRST CLASS PAX, SOURCE UNKNOWN. AN EMERGENCY WAS DECLARED AND THE FLIGHT DIVERTED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE PERFORMED ODOR INSPECTION IAW MCM 05-96-70, AND INSPECTIONS PER BOW. OPS CKS NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 97,960 hrs · 15,711 cycles

AIR IN FORWARD OF AIRCRAFT CAUSED DIZZINESS TO FLIGHT ATTENDANTS AND PILOTS, AND SOME FIRST CLASS PAX. SOURCE IS UNKNOWN. THE AIRCRAFT WAS GROUNDED. PERFORMED ODOR INSPECTION IAW MCM 05-96-70. AND INSPECTIONS BOW. OPS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 97,695 hrs · 15,664 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR L1 AND R1 (AALA20180727002) SEE EMERGENCY EXIT LIGHTS NOT WORKING. MAINTENANCE REPLACED BATTERY CHARGER AND BATTERY PER AMM 33-51-07 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 97,695 hrs · 15,664 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR L1 (AALA20180727001) AND R1 SEE EMERGENCY EXIT LIGHTS NOT WORKING. MAINTENANCE REPLACED BATTERY CHARGER AND BATTERY PER AMM 33-51-07 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: WINDOW SHADE — OUT OF ADJUST (CABIN) · airframe 97,564 hrs · 15,645 cycles

AIRCRAFT WAS NOT GROUNDED. WINDOW SHADE AT SEAT 21A DIFFICULT TO MOVE, SEAT IS LOCATED AT AN EMERGENCY EXIT ROW. ADJUSTED WINDOW SHADE TRACKS PER AMM 56-11-00. OPERATIONS CHECK GOOD OK FOR SERVICE.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 97,481 hrs · 15,629 cycles

LEFT WING TRAILING EDGE OUTBOARD FLAP LOWER SKIN HAS WATER INGRESSION. REPAIRED THE FLAP LOWER SKIN IAW EA 282185A.

Part: SHUTOFF VALVE — FAULTED (ZONE 400 - NAC/P) · airframe 97,467 hrs · 15,627 cycles

RIGHT HAND HPSOV EICAS MESSAGE LIGHT CAME ON DURING FLIGHT. COMPLIED WITH QRH AND RETURNED TO DEPARTURE. EMERGENCY DECLARED, AIRCRAFT LANDED. THE AIRCRAFT WAS GROUNDED. REPLACED HIGH PRESSURE SHUT-OFF VALVE AND HIGH PRESSURE SHUT-OFF VALVE CONTROLLER AS A PRECAUTION PER AMM 36-11-07 AND 36-11-08. HIGH POWER ENGINE RUN PERFORMED. ALL PARAMETERS FOUND TO BE NORMAL. NO MESSAGE NOTED AT THIS TIME. OK FOR SERVICE. THIS SDR IS FOR THE HIGH PRESSURE SHUT-OFF VALVE.

Part: CONTROLLER — FAULTED · airframe 97,467 hrs · 15,627 cycles

RIGHT HPSOV EICAS MESSAGE LIGHT ILLUMINATED DURING FLIGHT. COMPLIED WITH QRH AND RETURNED TO DEPARTURE. EMERGENCY DECLARED, AIRCRAFT LANDED. THE AIRCRAFT WAS GROUNDED. REPLACED HIGH PRESSURE SHUT-OFF VALVE AND HIGH PRESSURE SHUT-OFF VALVE CONTROLLER AS A PRECAUTION IAW AMM 36-11-07 AND 36-11-08. HIGH POWER ENGINE RUN PERFORMED. ALL PARAMETERS FOUND TO BE NORMAL. NO MESSAGE NOTED AT THIS TIME. OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 97,304 hrs · 15,592 cycles

ONE LEFT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE CHARGER IAW AMM 33-51-00.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 97,304 hrs · 15,592 cycles

ONE LEFT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE BATTERY PACK IAW AMM 33-51-00.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 97,304 hrs · 15,592 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. TWO LEFT OVERWING SLIDE EMERGENCY LIGHTS WAS INOPERATIVE. REPLACED THE BATTERY AT STA 1340 PER AMM 33-51-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 97,304 hrs · 15,592 cycles

FLIGHT DECK EMERGENCY LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK LIG5192 IAW AMM 33-51-00. OPS CHECKED OK.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 97,304 hrs · 15,592 cycles

TWO LEFT OVERWING SLIDE EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE CHARGER AT BS 1340 IAW AMM 33-51-00.

Part: STRINGER — BULGED (BS 1559-1561) · corrosion level 2 · airframe 97,304 hrs · 15,592 cycles

AFT CARGO STRINGER 39L BULGING AROUND FASTENERS AT BS 1559 - 1561. DAMAGE REMOVED AND REPAIRED THE STRINGER IAW SRM 53-00-30-2R-2.

Part: SLAT SYSTEM — MALFUNCTIONED · airframe 96,886 hrs · 15,513 cycles

AIR INTERRUPTION WITH LEADING EDGE SLAT DISAGREE FAULT. AIRCRAFT TAKEN OUT OF SERVICE FOR TROUBLESHOOTING. THE AIRCRAFT WAS GROUNDED.

Part: LIGHT — BROKEN (CABIN) · airframe 96,791 hrs · 15,489 cycles

AIRCRAFT WAS GROUNDED. SEAT 27H SEAT MOUNTED EMERGENCY LIGHT 0201720-003 FOUND BROKEN. REPLACED LIGHT PER AMM 33-51-10-962-104. OPERATIONS CHECK GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 96,771 hrs · 15,487 cycles

EMERGENCY LIGHT LEFT SIDE, ROW 7 THROUGH 23 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER IAW AMM 33-51-07 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 96,771 hrs · 15,487 cycles

EMERGENCY LIGHT LEFT SIDE, ROW 7 THROUGH 23 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY IAW AMM 33-51-07 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 96,771 hrs · 15,487 cycles

EMERGENCY LIGHT LEFTHAND SIDE, ROW 7 THROUGH 23 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER IAW AMM 33-51-07 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: CHARGER — FAULTED (EMERGENCY LIGHTS) · airframe 96,771 hrs · 15,487 cycles

EMERGENCY LIGHT LEFT SIDE, ROW 7 THROUGH 23 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER IAW AMM 33-51-07 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: CIRCUIT BREAKER — POPPED (ZONE 200) · airframe 96,289 hrs · 15,403 cycles

AIRCRAFT WAS NOT GROUNDED. ON ARRIVAL LOST TOP EICAS, LT AND CTR AP, TERRAIN, GRWS, TCAS, AND FLAPS WOULD NOT EXTEND. FLIGHT DECLARED AN EMERGENCY AND PERFORMED GO AROUND. THE CREW ELECTRICALLY EXTENDED THE FLAPS. THE FLIGHT LANDED ON THE NEXT ATTEMPT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND CB L-AC BUS SECT 2 155V POPPED OUT. RESET SAME, PERF BPCU BITE, NO FAULT IAW AMM 24-41-03, EICAS BITE NO FAULT IAW AMM 31-41-00, GPWS BITE NO FAULT IAW B767-300 AMM 34-46-00. RETRACT/EXTEND FLAP/SLAT HYDRAULICALLY, ALL OK IAW AMM 27-58-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 95,948 hrs · 15,346 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT 24H EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE SEAT 24H EMERGENCY LIGHT WAS REPLACED IAW MM 33-60-98.

Part: GUARD — OUT OF ADJUST (CABIN) · airframe 95,538 hrs · 15,275 cycles

AIRCRAFT WAS NOT GROUNDED. CLOSING GUARD OVER THE EMERGENCY LIGHT SWITCH DISARMS THE LIGHTS. REFITTED LIGHT SWITCH GUARD ACTUATOR LOOP OVER TOGGLE SWITCH PER AMM 33-51-08-404-010. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 94,604 hrs · 15,122 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHT AT SEAT 34H FORWARD IS INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY IAW ESO 11910. OPERATIONAL CHECK GOOD.

Part: SWITCH — INOPERATIVE (CABIN) · airframe 94,472 hrs · 15,095 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT OFF/ARM/ON SWITCH MECHANISM IS INOPERATIVE. CAGING SPRING FELL OFF. REINSTALLED AND SECURED COCKPIT EMERGENCY LIGHT SWITCH GUARD. OPERATIONAL CHECK GOOD.

Part: MODULE — FAULTY (COCKPIT) · airframe 94,025 hrs · 15,011 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. DFW-MIA FLIGHT. LANDING GEAR DISAGREE LIGHT ILLUMINATED BEFORE LANDING. COMPLETED GO AROUND AND CYCLED LANDING GEAR. LANDING UNEVENTFUL. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER MODULE ASSEMBLY IAW AMM 32-31-01. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 93,859 hrs · 14,977 cycles

EMERGENCY EXIT SIGNS ARE INOPERATIVE AT THE L1 AND R1 DOORS. RESEATED CONNECTOR ON POWER SUPPLY M1208. OPS CHECKED GOOD.

Part: FILTER — DIRTY (LT ENGINE) · airframe 93,283 hrs · 14,882 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. LHR-RDU FLIGHT RETURNED TO LHR. OVERWEIGHT LANDING UNEVENTFUL. LEFT ENGINE FUEL FILTER EICAS MESSAGE RECEIVED AFTER TAKEOFF. REMOVED AND REPLACED FUEL FILTER IAW AMM 73-11-03 AND SIC 4919. OPERATIONAL CHECK GOOD.

Part: WINDOW — OUT OF ADJUST (COCKPIT) · airframe 93,196 hrs · 14,864 cycles

AIRCRAFT NOT GROUNDED. FIRST OFFICERS SLIDING EMERGENCY EXIT WINDOW IS DIFFICULT TO CLOSE. REMOVED AND REINSTALLED WINDOW TRIM AND ADJUSTED WINDOW IAW AMM 56-11-02. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 93,196 hrs · 14,864 cycles

AIRCRAFT NOT GROUNDED. EXTERIOR EMERGENCY EXIT LIGHT AT L4 POSITION IS INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-51-06. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 93,196 hrs · 14,864 cycles

SEAT MOUNTED LIGHTS BETWEEN SEATS 20HJ AND 21HF ARE INOPERATIVE. REMOVED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY ASSEMBLY IAW AMM 33-51-00. OPERATIONAL CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 93,196 hrs · 14,864 cycles

TWO LEFT OVERWING EMERGENCY EXIT LIGHTS AND THE L4 EXTERIOR DOOR LIGHT ARE INOPERATIVE. REMOVED AND REPLACED THE CHARGER AND BATTERY IAW AMM 33-51-06. OPERATIONAL CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 93,196 hrs · 14,864 cycles

TWO LEFT OVERWING EMERGENCY EXIT LIGHTS AND THE L4 EXTERIOR DOOR LIGHT ARE INOPERATIVE. REMOVED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY PACK IAW AMM 33-51-06. OPERATIONAL CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 93,196 hrs · 14,864 cycles

SEAT MOUNTED EMERGENCY LIGHTS ON SEATS 20HJ AND 21HF ARE INOPERATIVE. REMOVED AND REPLACED THE CHARGER ASSEMBLY & BATTERY ASSEMBL IAW AMM 33-51-00. OPERATIONAL CHECKED GOOD.

Part: STRINGER — CORRODED (BS 1197) · corrosion level 2 · airframe 93,196 hrs · 14,864 cycles

CORROSION AROUND FASTENERS IN STRINGER 35L AT BS 1197+135. REPAIRED IAW SMR 51-10-01 AND SRM 53-00-03.

Part: INTERCOSTAL — CRACKED (BS 347-368) · airframe 93,196 hrs · 14,864 cycles

CRACKED INTERCOSTAL BETWEEN BS 347 AND 368 AT RBL 40. REPLACED THE INTERCOSTAL.

Part: FITTING — CORRODED (BS 610) · airframe 93,196 hrs · 14,864 cycles

CORROSION ON FORWARD CARGO DOOR NR 12 LATCH PIN FITTING AT BS 610. REPLACED THE LATCH PIN FITTING IAW AMM 52-33-09 AND EA 25912.

Part: FLOORBEAM — CORRODED (BS 325) · airframe 93,196 hrs · 14,864 cycles

CORROSION ON FLOORBEAM AT BS 325 BETWEEN BL 0 AND RBL 45. REPAIRED FLOOR BEAM PER SRM 53-00-51.

Part: INTERCOSTAL — CORRODED (BS 325-347) · corrosion level 2 · airframe 93,196 hrs · 14,864 cycles

CORROSION ON INTERCOSTAL BETWEEN BS 325 AND 347 AT RBL 42. REPLACED INTERCOSTAL.

Part: FLOORBEAM — CORRODED (BS 1197) · airframe 93,196 hrs · 14,864 cycles

CORROSION ON AFT CARGO COMPARTMENT FLOORBEAM TEE AT BS 1197 +66. REPLACED THE TEE IAW 51-00-05.

Part: ANGLE — CRACKED (BS 742) · airframe 93,196 hrs · 14,864 cycles

ANGLE BRACKET AT BS 742 CRACKED. REPLACED THE BRACKET.

Part: FLOOR SUPPORT — CRACKED (BS 742-764) · airframe 93,196 hrs · 14,864 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 742 AND 764. REPLACED THE FLOOR SUPPORT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 93,123 hrs · 14,852 cycles

AIRCRAFT NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 27H INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-51-10. OPERATIONAL CHECK GOOD.

Part: SMOKE DETECTOR — FAILED (LAVATORY) · airframe 93,082 hrs · 14,844 cycles

SMOKE ALARM IN LAVATORY M2 SOUNDED AND A BURNING ODOR WAS DETECTED. PASSENGER NOTED LAVATORY LIGHTS FLICKERING. REMOVED AND REPLACED SMOKE DETECTOR IAW AMM 26-13-01-024-010. OPERATIONAL CHECKED GOOD.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 92,888 hrs · 14,814 cycles

AIRCRAFT NOT GROUNDED. LAVATORY M2 SMOKE DETECTOR ALARM WENT OFF DURING DESCENT WITH NO EVIDENCE OF FIRE OR SMOKE. REMOVED AND REPLACED SMOKE DETECTOR IAW AMM 26-13-01. OPERATIONAL CHECK GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (MLG) · airframe 92,803 hrs · 14,802 cycles

DURING APPROACH AND AT GEAR EXTENSION, THE LANDING GEAR DISAGREE AND THE TAIL SKID LIGHTS ILLUMINATED. EMERGENCY DECLARED. LANDING UNEVENTFUL. MAINTENANCE ACCOMPLISHED FIM 32-30-00-815-814, LANDING GEAR DISAGREE AND TAIL SKID LIGHTS EXTINGUISHED. NO EICAS MESSAGES PRESENT. SYSTEM CHECKED NORMAL.

Part: LIGHT — BROKEN (SEAT 40B) · airframe 92,561 hrs · 14,761 cycles

SEAT EMERGENCY LIGHT INOPERATIVE AT ROW 40B. REPLACED THE EMERGENCY LIGHT , OPS CHECKED GOOD IAW AMM 33-51-10.

Part: TRANSDUCER — FAULTED (MLG) · airframe 91,178 hrs · 14,491 cycles

AIRCRAFT WAS GNDED. EMER & DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB ANTI-SKID EICAS & OVERHEAD AMBER LIGHTS ILLUMINATED. ACCOMPLISHED BITE PROCEDURE ON ANTI-SKID CONTROL UNIT IAW FIM 32-42-00. RESULTS SHOWED NR 2 WHEEL TRANSDUCER FAULTED. R & R TRANSDUCER & ACCOMPLISHED OPERATIONAL CHECK IAW AMM 32-42-06.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 90,891 hrs · 14,438 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHTS AT SEATS 32HJ - 41HJ INOPERATIVE. R & R POWER SUPPLY ASSEMBLY M735. SYS CHECKED NORMAL.

Part: SWITCH — INOPERATIVE (CABIN) · airframe 89,670 hrs · 14,209 cycles

P40 EMER LIGHT TEST SWITCH INOPERATIVE. R & R SWITCH IAW SWP 20-30-00.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 88,758 hrs · 14,067 cycles

OBSERVED A CRACK ON THE FORWARD SIDE OF VERTICAL LEG AT FUSELAGE STATION JUST BELOW RADIUS & ABOVE STRINGER 6L. REPAIRED CHORD IAW SRM 53-80-08 REPAIR 9 & EA 253171 & 253080.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 88,758 hrs · 14,067 cycles

CORROSION ON BEAM T CAP AT STATION 1153 & LBL 30. REPLACED BEAM T CAP IAW DWG 146T0250.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 88,758 hrs · 14,067 cycles

FOUND CORROSION ON THE UPPER SURFACE OF PLATE ATTACHED TO T CAP AT STATION 1153. R & R PLATE IAW EA 253119 & DWG 146T5000.

Part: FITTING — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 88,758 hrs · 14,067 cycles

CORROSION ON FWD CARGO DOOR NR 2 LATCH FITTING INNER BORE. REPAIRED LATCH FITTING IAW EA 252912.

Part: FITTING — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 88,758 hrs · 14,067 cycles

CORROSION ON FWD CARGO DOOR NR 12 LATCH FITTING INNER BORE. REPAIRED LATCH FITTING IAW EA 252912.

Part: FITTING — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 88,758 hrs · 14,067 cycles

CORROSION ON FWD CARGO DOOR NR 4 LATCH FITTING INNER BORE. REPAIRED LATCH FITTING IAW EA 252912.

Part: LENS — BROKEN (CABIN) · airframe 88,264 hrs · 13,989 cycles

EMERGENCY EXIT LIGHT COVER BROKEN AT ROW 20HJ. R & R LENS IAW AMM 33-50-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,205 hrs · 13,982 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT 41H. REPLACED EMER LIGHT ASSEMBLY IAW AMM 33-60-98 WITH NORMAL OPERATIONAL CHECKS.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 87,685 hrs · 13,903 cycles

EMERGENCY LIGHTS ON LT SIDE OVERWING INOPERATIVE, ALL 3 EXTERIOR EGRESS EMER EXIT LIGHTS. R & R BATTERY CHARGER & BATTERY M736 IAW AMM 33-51-07. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 87,685 hrs · 13,903 cycles

EMERGENCY PATH LIGHTING FROM ROWS 32ABC - 41ABC & OVERHEAD LIGHTING INOPERATIVE. REPLACED BATTERY PACK OR EMER LIGHTS IAW MM 33-51-07. ALL OPERATIONS OK.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 87,685 hrs · 13,903 cycles

RIGHT FWD CABIN SEAT MOUNTED EMERGENCY LIGHTS FROM 2J - 8J ARE INOPERATIVE. REPLACED BATTERY CHARGER & BATTERY M730 IAW AMM 33-51-07. SYS CHECKED NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 87,685 hrs · 13,903 cycles

EMERGENCY LIGHTS ON LT SIDE OVERWING INOPERATIVE, ALL 3 EXTERIOR EGRESS EMER EXIT LIGHTS. R & R BATTERY CHARGER & BATTERY M736 IAW AMM 33-51-07. SYS CHECKED NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 87,685 hrs · 13,903 cycles

L1 DOOR EXTERIOR EMER LIGHT INOPERATIVE, LT FWD ENTRY DOOR SLIDE ILLUMINATION LIGHT. R & R BATTERY CHARGER & BATTERY M736 IAW AMM 33-51-07. SYS CHECKED NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 87,685 hrs · 13,903 cycles

RIGHT FWD CABIN SEAT MOUNTED EMER LIGHTS FROM 2J - 8J ARE INOPERATIVE. REPLACED BATTERY CHARGER & BATTERY M730 IAW AMM 33-51-07. SYS CHECKED NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 87,685 hrs · 13,903 cycles

LEFT FWD CABIN SEAT MOUNTED EMER LIGHTS ARE INOPERATIVE FROM 2A TO 8A. R & R BATTERY CHARGER & BATTERY M735 IAW AMM 33-51-07. SYS CHECKED NORMAL.

Part: BATTERY — DEFECTIVE (EMERGENCY LIGHTS) · airframe 87,685 hrs · 13,903 cycles

L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE, LT FWD ENTRY DOOR SLIDE ILLUMINATION LIGHT. R & R BATTERY CHARGER & BATTERY M736 IAW AMM 33-51-07. SYS CHECKED NORMAL.

Part: BATTERY — DEFECTIVE (EMERGENCY LIGHT) · airframe 87,865 hrs · 13,903 cycles

LEFT FWD CABIN SEAT MOUNTED EMER LIGHTS ARE INOPERATIVE FROM 2A - 8A. R & R BATTERY CHARGER & BATTERY M735 IAW AMM 33-51-07. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 87,193 hrs · 13,832 cycles

L4 DOOR EXTERNAL EMER LIGHT IS INOPERATIVE. R & R L4 EXTERNAL EMER LIGHT BULBS IAW AMM 33-51-06. SYS CHECKED NORMAL.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 86,983 hrs · 13,801 cycles

EMERGENCY LIGHT AT SEAT ROW 13 RT IS INOPERATIVE. RESEATED EMER ESCAPE PATH LIGHTING CONNECTOR AT SEAT ROW 13 RT.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 86,983 hrs · 13,801 cycles

FORWARD FLIGHT ATTENDANT SEAT BATTERY CHARGER INOPERATIVE. R & R POWER SUPPLY. PERFORMED GOOD OPERATIONAL CHECK IAW AMM 33-51-07-002-006 & 33-51-07-402-010. SYS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 86,983 hrs · 13,801 cycles

SEAT ROW 32 LT EMER EXIT LIGHT LENS MISSING. R & R EMER LIGHT ASSEMBLY. PERFORMED OPERATIONAL CHECK IAW AMM 33-51-10-962-104. SYS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 86,983 hrs · 13,801 cycles

AFT RT FLIGHT ATTENDANT SEAT EMER EXIT LIGHT BATTERY INOPERATIVE. R & R BATTERY PACK. PERFORMED OPERATIONAL CHECK IAW AMM 33-51-07-22-001 & 33-51-07-422-012. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 86,983 hrs · 13,801 cycles

LEFT AFT ENTRY DOOR OUTSIDE EMER LIGHT INOPERATIVE. RELAMPED & PERFORMED GOOD OPERATIONS CHECK IAW MM 33-51-06-902-082.

Part: IDG — LOW (RT ENGINE) · airframe 86,251 hrs · 13,674 cycles

ON TAKEOFF RT IDG LIGHT ILLUMINATED & ELEC ODOR REPORTED IN CABIN. PERFORMED QRH PROCEDURES & RETURNED. NO EMER DECLARED, LANDING UNEVENTFUL & WAS NOT OVERWEIGHT. SERVICED RT IDG. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: PROBE — FAULTY (RT ENGINE) · airframe 84,378 hrs · 13,377 cycles

JFK CREW REPORTED LT ENG EGT INCREASED UNTIL JUST BELOW MINIMUM LIMIT. EMER DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND LT ENG EGT FOUND TO BE IN LIMITS BUT RT ENG EGT WAS LOWER THAN REQUIRED. REPLACED RT ENG 1 THRU 4 EGT PROBES & ENG JUNCTION BOX. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 84,231 hrs · 13,356 cycles

LEFT AFT FUSELAGE GND SCAN EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LT AFT FUSELAGE GND SCAN EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 83,816 hrs · 13,286 cycles

FOUND WIRE BROKEN AT SEAT DISCONNECT FOR EMERGENCY AISLE LIGHTING. REPAIRED BROKEN WIRE, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 83,554 hrs · 13,255 cycles

LT FUSELAGE MOUNTED NR 3 OVERWING SLIDE ILLUMINATION LIGHT INOPERATIVE. REPLACED LAMP FOR LT SIDE FUSELAGE MOUNTED NR 3 OVERWING ILLUMINATION LIGHT. OPERATIONS CHECKED NORMAL.

Part: SENSOR — FAULTY (LE SLAT) · airframe 82,857 hrs · 13,128 cycles

MIA LE SLAT ASYMMETRY INDICATION. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LE NR 8 SLAT INBD SENSOR 304. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: IDG — FAILED (RIGHT) · airframe 82,230 hrs · 13,022 cycles

LAX INFLIGHT DFW-HNL CREW REPORTED RT GENERATOR FAILED DURING CIIMB OUT. EMERGENCY DECLARED FLIGHT DIVERTED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RT INTEGRATED DRIVE GENERATOR. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: PSEU — INOPERATIVE (LE SLAT) · airframe 81,190 hrs · 12,865 cycles

CREW REPORTED L/E SLAT ASYMMETRY MESSAGE. EMERGENCY DECLARED, FLIGHT RETURNED, LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED PROXIMITY SWITCH ELECTRONIC UNIT. SYS GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,390 hrs · 12,737 cycles

LEFT AFT DOOR EMERGENCY EXIT WINDOW LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT AFT DOOR EMERGENCY EXIT WINDOW LIGHT. OPS CHECK NORMAL.

Part: CONNECTOR — DISCONNECTED (ZONE 500) · airframe 79,245 hrs · 12,547 cycles

WHILE PERFORMING THE PREFLIGHT TEST SEQUENCE THE LEFT WING SQUIB FAILED TO TEST. FOUND LEFT LATCH OPENING ACTUATOR C PLUG DISCONNECTED. RECONNECTED PLUG.

Part: FRAME — CRACKED (LT PYLON) · airframe 78,529 hrs · 12,442 cycles

LEFT PYLON OUTBOARD FRAME CHORD CRACKED AT STATION 285.45. INSTALLED REPAIR DOUBLER PER AARD 54-52-02-2.

Part: FRAME — CRACKED (LT PYLON) · airframe 78,529 hrs · 12,442 cycles

LEFT PYLON INBOARD FRAME CHORD AT STATION 285.45 CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER PER AARD 54-52-02-2.

Part: SHIM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,529 hrs · 12,442 cycles

SHIM AT STATION 1373 FROM STRINGERS 35 TO 36 LEFT CORRODED. REPLACED SHIM PER SRM 51-40-02.

Part: WEDGE — DAMAGED (TE FLAP) · airframe 78,529 hrs · 12,442 cycles

RIGHT OUTBOARD FLAP DISBONDED ON LOWER TRAILING EDGE WEDGE DUE TO BIRD STRIKE. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-07.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 77,669 hrs · 12,316 cycles

AFT RIGHT NUMBER 4 DOOR WALL FRAME MOUNT EMERGENCY EXIT SIGN LOWER PORTION HAS ONE LIGHT OUT. REPLACED LAMP FOR AFT RIGHT NUMBER 4 DOOR WALL FRAME MOUNT EMERGENCY EXIT SIGN. OPS CHECK NORMAL.

Part: WIRE HARNESS — FAULTY (EGT) · airframe 75,002 hrs · 11,891 cycles

JFK - INFLIGHT DFW-FRA. CREW REPORTED RIGHT ENGINE EXHAUST GAS TEMPERATURE INDICATION ERRATIC. EMERGENCY DECLARED FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE UPPER AND LOWER EGT HARNESSES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,506 hrs · 11,505 cycles

FOUND SURFACE CORROSION ON THE FUSELAGE FORWARD CARGO DOOR SURROUND STRUCTURE LOWER SILL OUTER CHORD. BLENDED, INSPECTED AND REFINISHED DAMAGED AREA IN ACCORDANCE WITH B767 SRM 53-00-15-1A FIGURE 101. REFERENCE B767-53-014380 FOR COMPLETE DETAILED REPAIR INFORMATION.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,506 hrs · 11,505 cycles

CORROSION WAS FOUND IN FUSELAGE SKIN INNER SURFACE AT AFT CARGO FORWARD WALL AT STATION 1087 AND BUTTLINE 0. REMOVED CORROSION BY BLENDING TO ENSURE CORROSION DOES NOT CONTINUE UNDER THE FORWARD SHEAR TIE. REFERENCE EAB 767-53-014349 FOR COMPLETE DETAILED REPAIR INFORMATION.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,506 hrs · 11,505 cycles

CRACKS WERE RECORDED ON ALL FOUR INSPECTED HOLES AT LEFT HAND SIDE STATION 1809.5 TENSION FITTING. HOLES WERE OVERSIZED TO 0.2807 IN ORDER TO REMOVE CRACK INDICATIONS. BOEING APPROVED OVERSIZED HOLE WITH AMOC TO AD 2005-11-02. ACCOMPLISHED OPEN HOLE HFEC TO ENSURE ALL CRACK INDICATIONS ARE REMOVED. INSTALLED NEW APPLICABLE FASTENER PER WC 2011. REFERENCE EAB767-53-014351 FOR COMPLETE DETAILED REPAIR INFORMATION.

Part: WIRE HARNESS — DEFECTIVE (BLEED AIR SYS) · airframe 71,153 hrs · 11,261 cycles

LAX INFLIGHT DFW-HNL, CREW REPORTED RIGHT ENGINE HIGH PRESSURE SHUTOFF VALVE LIGHT ILLUMINATED IN FLIGHT. SHUT OFF BLEED PER CHECK LIST. EMERGENCY DECLARED FLIGHT DIVERTED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED HARNESS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,898 hrs · 11,224 cycles

SEAT EMERGENCY LIGHTS AT SEATS 22HJ TO 25HJ INOPERATIVE. REMOVED AND REPLACED BATTERY PACK FOR SEAT EMERGENCY LIGHTS AT SEAT 22HJ TO 25HJ. OPS CHECKED NORMAL.

Part: SLIDE — UNWANTED DEPLOY · airframe 69,497 hrs · 10,968 cycles

ACCIDENTAL SLIDE DEPLOYMENT. REPLACED SLIDE AND ACTUATORS. (OPEN)

Part: SWITCH — FAULTED (AC PACK) · airframe 67,955 hrs · 10,680 cycles

DURING CLIMB LEFT AIR CONDITIONING PACK OVERHEATED AND TRIPPED OFF. RIGHT PACK ON PLACARD. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED LEFT PACK ALTITUDE SWITCH, COMPRESSOR OUTLET SENSOR AND COMPRESSOR OVER TEMPERATURE SWITCH PART NUMBER 6411371. ALSO REPLACED LEFT PACK LOW LIMIT VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

MIA - RIGHT MID FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY FOR RIGHT MID FLIGHT ATTENDANT EMERGENCY FLASHLIGHT.

Part: CDU — INOPERATIVE (ZONE 200) · airframe 67,081 hrs · 10,544 cycles

LAX - INFLIGHT DFW-HNL. LEFT FLIGHT MANAGEMENT COMPUTER FAILED. LANDED LAX WITHOUT INCIDENT. REPLACED THE CONTROL DISPLAY UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LENS — BROKEN (EMERGENCY LIGHTS)

JFK - LENS AT SEAT 24H BROKEN. REPLACED LEN AT SEAT 24H.

Part: LAMP — BROKEN (EMERGENCY LIGHTS)

JFK - EMERGENCY LIGHTS AT SEAT 24H INOPERATIVE. REPLACED LAMP AT SEAT 24H

Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · 63,989 cycles

JFK EMERGENCY EXIT SIGN AT RT HAND LOWER FORWARD OVERWING EXIT DAMAGED. REPLACED EXIT SIGN ASSEMBLY FOR EMERGENCY LIGHT AT RT HAND LOWER FORWARD OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPS.

Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · 63,989 cycles

JFK EMERGENCY EXIT SIGN AT LT HAND LOWER FORWARD OVERWING EXIT DAMAGED. REPLACED SIGN ASSEMBLY FOR EMERGENCY LIGHT AT LT HAND LOWER FORWARD OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPS.

Part: FRAME — CORRODED (BS 610) · airframe 61,723 hrs · 9,748 cycles

AFW - CARGO FLOOR FRAME J INNER CHORD AT STATION 610 RIGHT BUTT LINE 7 TO 10 IN FORWARD CARGO HAS CORROSION ON BOTTOM SIDE AT NUTPLATE. REMOVED CORROSION FORM AFFECTED AREA PER SRM 59 00 07 1A AND APPLIED ALODINE AND PRIMER. REINSTALLED HARDWARE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHEAR TIE — CORRODED (BS 742 S37-38L) · airframe 61,732 hrs · 9,748 cycles

AFW - SHEAR TIE AT FORWARD CARGO STATION 742 BETWEEN STRINGER 38L AND 37L CORRODED BEYOND LIMITS. REPLACED SHEAR TIE AT FORWARD CARGO STATION 742 BETWEEN STRINGER 38L AND 37L.

Part: MEC — INOPERATIVE (RT ENGINE)

LAX INFLIGHT T284/25JUN - INFLIGHT EMERGENCY DECLARED DUE TO INABILITY TO REDUCE POWER ON RIGHT ENGINE BELOW 68 PERCENT N1 AND 4500 FUEL FLOW DURING DESCENT. LANDED LAX WITHOUT INCIDENT. REPLACED RIGHT ENGINE MAIN ENGINE CONTROL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - BATTERY PACK AT M739 FOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT M739 FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

DFW - FOUND EMERGENCY LIGHT AT SEAT 33B INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 33B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COVER — LOOSE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT OVER AT LEFT NUMBER ONE DOOR LOOSE. SECURED EMERGENCY LIGHT COVER AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT SEAT 31B INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT SEAT 31B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 15B INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 15B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 26H HAS MISSING LENS. REPLACED EMERGENCY LIGHT LENS AT SEAT 26H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 3B INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 3B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - GREEN LIGHTS FOR EMERGENCY ESCAPE SLIDES FAILED TEST. REPLACED M961 AND M962 BATTERY PACK FOR GREEN LIGHTS FOR EMERGENCY ESCAPE SLIDES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — BROKEN (EMERGENCY LIGHTS)

AFW - EMERGENCY LIGHT WIRE BROKEN AT CONNECTOR LOCATED AT KICK PANEL OF SEAT 29H. REPINNED WIRE WITH CONTACT SOCKET FOR EMERGENCY LIGHT WIRE BROKEN AT CONNECTOR AT KICK PANEL OF SEAT 29H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS)

SFO - EMERGENCY EXIT LIGHT AT SEAT 25B INOPERATIVE. CONNECTED SEAT HARNESS FOR EMERGENCY LIGHT AT SEAT 25B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FLOORBEAM — CORRODED (FUSELAGE)

FLOORBEAM AT RIGHT BUTTLINE 49 AT STATION 325 HAS CORROSION 1.0 INCH BY 1.0 INCH WITH DEPTH OF .069. MATERIAL REMAINING IS BEYOND SRM LIMITS. FABRICATE REPAIR STRAP OUT OF 301 AND ONE HALF HARD STAINLESS STEEL 0.050 THICK. ALODINE ALL BARE ALUMINUM SURFACES. FINISH BLENDS WITH 2 COATS BMS10 11 PRIMER. FILL BLENDS WITH BMS 5 95 SEALANT. INSTALL REPAIR STRAP WET WITH BMS 5 95 SEALANT. FASTNERS TO BE INSTALLED WITH 4 6D SPACING.

Part: FLOORBEAM — CORRODED (FUSELAGE)

AFW - FLOORBEAM SECTION 41 AT STATION 347 HAS CORROSION. MATERIAL REMAINING IS BEYOND SRM LIMITS. FABRICATE REPAIR STRAP OUT OF 301 AND ONE HALF HARD STAINLESS STEEL 0.050 THICK. ALODINE ALL BARE ALUMINUM SURFACES. FINISH BLENDS WITH 2 COATS BMS10 11 PRIMER. FILL BLENDS WITH BMS 5 95 SEALANT. INSTALL REPAIR STRAP WET WITH BMS 5 95 SEALANT. FASTNERS TO BE INSTALLED WITH 4 6D SPACING.

Part: WIRE — LOOSE (EMERGENCY LIGHTS)

MIA EMERGENCY LIGHT AT A6 LAVATORY HAS WIRE HANDING DOWN FROM BUMPER RUB STRIP. REINSTALLED WIRING IN CHANNEL FOR EMERGENCY LIGHT AT A6 LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: REFLECTOR — INOPERATIVE (EMERGENCY LIGHT)

ORD RT EMERGENCY LIGHTS IMMEDIATELY AFT OF FLAPS INOPERATIVE. REPLACED SOCKET REFLECTOR ASSEMBLY FOR RT EMERGENCY LIGHTS AFT OF FLAPS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (SEAT 35HJ)

SFO EMERGENCY LIGHT AT SEAT 35HJ INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT 35H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS)

ORD T088/28 EN ROUTE ORD TRAILING EDGE FLAP DISAGREE LIGHT ILLUMINATED DURING FLAP RETRACTION. ORD MAINTENANCE EXERCISED FLAPS SEVERAL TIMES ON GROUND. NO LIGHT ILLUMINATED DURING RETRACTION. UNABLE TO DUPLICATE. SYSTEM GROUND CHECKED NORMAL OPERATION. --CLOSED--

Part: WIRE — BROKEN (EMERGENCY LIGHT)

MAINTENANCE OBSERVED EMERGENCY LIGHT AT DOOR R1 INOPERATIVE. REPAIRED BROKEN WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CRACKED (FUSELAGE)

FOUND FUSELAGE SKIN HAS SMALL CRACK INDICATION IN FASTENER HOLE. FIRST OVERSIZE ON FASTENER HOLE. FASTENER HOLE OUTER SKIN ONLY HAS BEEN OVERSIZED TO .3075 INCHES TO REMOVED CRACK INDICATION. REAM OUTER SKIN ONLY FOR FREEZE PLUG .063 PLUS/MINUS .006 INCH PAST .3075 INCHES. INSTALL FREEZ PLUG PER 767 SRM 51-20-07 AND RETAIN PLUG PER SRM REQUIREMENTS. INSTALL FASTENER AS REQUIRED. (M)

Part: PIN — BENT (IDG)

FOUR HOURS INTO FLIGHT R GEN DRIVE ILLUMINATED STEADY WITH GEN DRIVE EICAS MESSAGE. COMPLIED WITH QRH AND DISCONNECTED IDG. REPEAT WRITE-UP 37, 50. BPCU AND IDG PREVIOUSLY REPLACED. T/S PER FIM 24-20-00 AND WD 24-11-21 AND FOUND PINS 2 AND 8 ON IDG D10966J CANNON JACK BENT, REALIGNED THEM, RECCON AND SERVICED IDG AND RAN RIGHT ENGINE DURING 15 MINUTES WITH ALL ELECTRICAL POWER SUPPLIED BY THE RIGHT GENERATOR. BPCU BITE TEST ACC AND NO FAULTS SHOWN. RT ENGIEN GEN SYSTEM OK FOR SERVICE. (M)

Part: CONNECTOR — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 33H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 33H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 35H INOPERATIVE. RESEATED CONNECTOR AT SEAT 35H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHT AT SEAT 34B INOPERATIVE. INSTALLED NEW CONNECTOR ON EMERGENCY ESCAPE PATH LIGHTING HARNESS. SYSETM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, L1 EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED L1 EMERGENCY EXIT LIGHT CONTACTS AND RELAMPED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SUPPORT — CORRODED (T/E FLAP)

AFW - FOUND CORROSION IN MOUNT HOLE FORWARD OUTBOARD LEFT INBOARD FLAP SUPPORT BEAM. VISUALLY INSPECT BORE TO ENSURE COMPLETE CORROSION REMOVAL. FABRICATE FREEZE FIT PLUG TO ACHIEVE A MIN .001 INCH INTERFERENCE FIT. (M)

Part: SUPPORT — DAMAGED (TE FLAPS)

AFW - FOUND CORROSION IN MOUNT HOLE AFT OUTBOARD HOLE, ON RIGHT INBOARD FLAP SUPPORT BEAM. PERFORM A DETAILED VISUAL INSPECTION OF THE RE-WORKED HOLE TO VERIFY COMPLETE CORROSION REMOVAL. APPLY ALODINE AND TWO COATS OF PRIMER TO RE-WORKED AREAS. (M)

Part: LIGHT — BROKEN (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 2B BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 2B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TERMINAL — INOPERATIVE (LT WING)

LAX - DURING OVERNIGHT MAINTENANCE, LEFT SIDE WING EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED AND SECURED EMERGENCY EXIT LIGHT WIRE TERMINAL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 36B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHTS WIRES AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT ROW 36 AB INOPERATIVE. REPLACED EMERGENCY EXIT CONNECTOR AT SEAT ROW 36 AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SEAL — LOOSE (PAX DOOR)

JFK - FLT 96 - EN ROUTE ORD-MXP, DURNIG CRUISE DETECTED NOISE AND VIBRATION AT FORWARD FLOOR CABIN. DIVERTED JFK AND LANDED WITHOUT FURTHER INCIDENT. REINSTALLED UPPER CARGO DOOR SEAL RETAINER AT FORWARD CARGO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (SEAT 33)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 33H INOPERATIVE. REPLACED EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 33H. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 31H INOPERATIVE. RESECURED CONNECTOR TO EMERGENCY EXIT LIGHT AT SEAT 31H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PAX SEAT 23H INOPERATIVE. RESEATED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 23H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PAX SEAT 21B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 21B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — FAILED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT 23AB INOPERATIVE. REINSTALLED PUSHBACK PIN IN SEAT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — FAILED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT 26AB INOPERATIVE. REPAIRED WIRE FOR EMERGENCY EXIT SEAT LIGHTS AT 26AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LATCH — FAILED (LT OW DOOR)

SFO - DURING OVERNIGHT MAINTENANCE, LEFT OVERWING SLIDE COMPARTMENT DOOR DIFFICULT TO OPEN. REPLACED TWO LEFT OVERWING SLIDE COMPARTMENT DOOR LATCHES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY EXIT LIGHT AT PASSENGER SEAT 31HJ INOPERATIVE. RE-SEATED EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 31HJ. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT AT 34H FOUND INOPERATIVE. RE-SECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 34H. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)

Part: RELAY — FAILED (LT GEN SYSTEM)

MIA - FLT 0063 - LEFT GENERATOR 'OFF' AND 'FIELD' LIGHTS CAME ON 15 MINUTES PRIOR TO LANDING. IDG REPLACED PER E58, NO HELP. REPLACED K109 RELAYS, PERFORMED SYSTEM CHECK, ISOLATED AND LOAD SHARED WITH APU ENGINES. ALL OPS CHECKS GOOD. (X)

Part: IDG — FAILED (NR 1 ENGINE)

SEA - FLT 27 - APPROX 1 HOUR INTO FLT LEFT GEN DRIVE ILLUMINATED. DISCONNECTED LEFT GEN PER AFM REF PIREP 15-11. REPLACED NR 1 ENGINE IDG RELIEF VALVE. RAN ENGINE. OPS CHECK GOOD. LEAK CHECK GOOD. REMOVED PLACARD MEL NR 24-1 AUTH NR 6-359DC-B. CLEARED MIC SHEET. (M)

Part: WIRE HARNESS — FAILED (LT ENG IDG)

DFW - FLT 1994 - LEFT IDG AUTO DISCONNECT 1.5 HOURS INTO FLT FOLLOW AND PROCEED SHUT DOWN LT GEN NO INDICATIONS PRIOR TO DISCONNECT ALL A/P FLT CONTROLS INSTRUMENTION NORMAL. INSTALLED NEW IDG ELECTRICAL HARNESS NR 5341 RAN ENGINE LEFT IDG OPS CHECKED NORMAL REMOVED PLACARD CLEARED MIC. (M)

Part: SWITCH — SHORTED (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS IN CABIN FOUND INOPERATIVE. REPLACED SHORTED SWITCH S28 AFT, FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: IDG — FAILED (LT ENGINE)

GRU - FLT 0006 - LEFT GENERATOR DRIVE LIGHT STAYED ON AFTER ENGINE START. GENERATOR CONT LIGHT OFF. LT IDG DEF INOPERATIVE PER MEL 24-01 AUTH 4-233DC-B. CHECKED IDGS/APU OIL LEVELS AND HISTORY. NO HISTORY. FLIGHT CREW ADVISED TO DISCONNECT. MIC SHEET ENTERED. REMOVED AND REPLACED NR 1 ENGINE IDG. PERFORMED ALL CHECKS PER MM. ALL CHECKS OK. REMOVED PLACARD 24-01 AUTH 4-233DC-B AND CLEARED MIC SHEET. (X)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 24B INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL WIRE — NEED RESECURING (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT RT AISLE MID-GALLEY BY PASSENGER SEAT 19EF FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT WIRE AT RT AISLE BY PASSENGER SEAT 19EF. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)