N677AN

Part: LATCH — LACK OF LUBE (SLIDING WINDOW) · airframe 53,962 hrs · 18,869 cycles

AIRCRAFT WAS NOT GROUNDED. AFTER PARKING, WAS UNABLE TO OPEN CAPTAINS SIDE SLIDING WINDOW. LUBED WINDOW LATCHING MECHANISM. OPERATIONAL CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (R1 DOOR SLIDE) · airframe 53,481 hrs · 18,681 cycles

R1 DOOR EMERGENCY EVACUATION SLIDE PRESSURE GAUGE IS IN THE RED AREA. REMOVED AND REPLACED SLIDE IAW MCM 25-94-34. OPERATIONAL CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,446 hrs · 18,664 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY EXIT LIGHTS FROM ROW 26 BACK ARE DIM. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-00. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 53,424 hrs · 18,652 cycles

EMERGENCY EXIT GROUND ILLUMINATION SLIDE LIGHT BY THE R2 DOOR IS INOPERATIVE AND HAS A BROKEN LENS. REMOVED AND REPLACED LIGHT ASSEMBLY AND LENS IAW AMM 33-51-06. OPS CHECKED GOOD.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 53,424 hrs · 18,652 cycles

EMERGENCY EXIT GROUND ILLUMINATION SLIDE LIGHT BY R2 DOOR IS INOPERATIVE AND HAS A BROKEN LENS. REMOVED AND REPLACED LIGHT ASSEMBLY AND LENS IAW AMM 33-51-06. OPS CHECKED GOOD.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,271 hrs · 18,584 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. HORIZONTAL STIFFENER CORRODED IN LOWER APU FIREWALL, FUSELAGE STATION 1885.2 BL0, 3 INCHES FROM BOTTOM OF FORWARD BULKHEAD ALONG UPPER SURFACE. REMOVED AND REPLACED STIFFENER IAW SRM 51-40-02, AARD 51-00-05-1, EA 269362, AND DRAWING 148N8402.

Part: COVER — DAMAGED (L4 DOOR SLIDE) · airframe 53,107 hrs · 18,517 cycles

L4 DOOR SLIDE COVER HAS A HOLE IN IT AT THE 1 OCLOCK POSITION. REMOVED AND REPLACED THE SLIDE COVER IAW AMM 25-66-01. OPS CHECKED GOOD.

Part: STRAP — LOOSE (L4 DOOR) · airframe 53,068 hrs · 18,499 cycles

AIRCRAFT WAS NOT GROUNDED. L4 DOOR EMERGENCY EVACUATION SLIDE BUSTLE IS LOOSE. SECURED LOWER STRAP ON LOWER LINING IAW AMM 52-11-02. OPERATIONAL CHECK GOOD.

Part: COLLAR — FAULTY (L1 DOOR) · airframe 53,027 hrs · 18,484 cycles

AIRCRAFT WAS GROUNDED. L1 DOOR GUST LOCK RELEASE LEVER IS DIFFICULT TO ARM. REMOVED AND REPLACED HOLD OPEN LOCK LEVER ASSEMBLY IAW AMM 52-11-08 (AALA201703099004) AND THE SPLIT COLLAR ASSEMBLY IAW AMM 52-11-08. OPERATIONAL CHECK GOOD.

Part: LEVER — FAULTY (L1 DOOR) · airframe 53,027 hrs · 18,484 cycles

AIRCRAFT WAS GROUNDED. L1 DOOR GUST LOCK RELEASE LEVER IS DIFFICULT TO ARM. REMOVED AND REPLACED HOLD OPEN LOCK LEVER ASSEMBLY IAW AMM 52-11-08 AND THE SPLIT COLLAR ASSEMBLY IAW AMM 52-11-08 (AALA201703099005). OPERATIONAL CHECK GOOD.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,714 hrs · 18,359 cycles

SEAT MOUNTED EMERGENCY LIGHTS IN ROWS 9DEF THROUGH 15DEF ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND CONTROL MODULE IAW AMM 33-51-07. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,714 hrs · 18,359 cycles

SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 9DEF THROUGH 15DEF ARE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AND CONTROL MODULE IAW AMM 33-51-07. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 52,638 hrs · 18,328 cycles

AIRCRAFT NOT GROUNDED. EMERGENCY EXIT LIGHTS AROUND L1 AND R1 DOOR FAILED TEST. REMOVED AND REPLACED BATTERY ASSEMBLY IAW 33-51-07. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,638 hrs · 18,328 cycles

AIRCRAFT NOT GROUNDED. SEAT MOUNTED EMERGENCY LIGHTS IN FIRST CLASS FAILED TEST. REMOVED AND REPLACED BATTERY PACK M10952 IAW AMM 33-51-07. OPERATIONAL CHECK GOOD.

Part: TRACK — DIRTY (SLIDING WINDOW) · airframe 52,528 hrs · 18,280 cycles

AFTER PARKING, CAPTAIN`S SLIDING WINDOW DIFFICULT TO OPEN. CLEANED AND LUBED L2 WINDOW TRACKS AND SPINDLE ASSEMBLY IAW AMM 56-11-02. OPERATIONAL CHECKED GOOD.

Part: SLIDING WINDOW — FAULTY (COCKPIT) · airframe 52,527 hrs · 18,279 cycles

CAPTAIN`S L2 SLIDING WINDOW DOES NOT OPEN PROPERLY. REMOVED AND REPLACED SLIDING WINDOW ARM LINK IAW AMM 56-11-02. OPERATIONAL CHECKED GOOD.

Part: RESERVOIR — UNSERVICEABLE (L4 DOOR) · airframe 52,483 hrs · 18,260 cycles

AIRCRAFT GROUNDED. L4 EMERGENCY DOOR OVERHEAD EMERGENCY POWER RESERVOIR REQUIRES REPLACEMENT. REMOVED AND REPLACED POWER RESERVOIR ASSEMBLY IAW AMM 52-11-30. OPERATIONAL CHECK GOOD.

Part: SLIDE — DEFECTIVE (L4 DOOR) · airframe 52,483 hrs · 18,260 cycles

L4 DOOR EVACUATION SLIDE GIRT BAR DIFFICULT TO ARM AND DISARM DUE TO SLIDE HAVING A DEFECT IN THE INTERNAL FABRIC. REMOVED AND REPLACED SLIDE. OPERATIONAL CHECKED GOOD.

Part: SWITCH — DEFECTIVE (FUEL SYSTEM) · airframe 52,483 hrs · 18,260 cycles

AIRCRAFT WAS GROUNDED. RIGHT CENTER FUEL PUMP AUTO SHUTDOWN IS INOPERATIVE. REMOVED AND REPLACE SWITCH S346 IAW WDM 28-21-11 AND 28-21-14. SYSTEM CHECKS NORMAL.

Part: COVER — LOOSE (ENTRY DOOR) · airframe 52,265 hrs · 18,172 cycles

AIRCRAFT NOT GROUNDED. FORWARD ENTRY DOOR EMERGENCY EVACUATION SLIDE COVER LOOSE. SECURED COVER IAW AMM 25-66-01. OPERATIONAL CHECK GOOD.

Part: FILTER — DIRTY (RECIRCULATION) · airframe 51,808 hrs · 17,982 cycles

DURING CLIMB THE FLIGHT ATTENDANTS REPORTED A FAINT ELECTRICAL ODOR IN CABIN. THE ODOR DISSIPATED AFTER THE RIGHT RECIRCULATION FAN WAS TURNED OFF. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REMOVED AND REPLACED RIGHT AND LEFT RECIRCULATION FAN FILTERS. ACCOMPLISHED MCM 05-96-70 WITH NO ODORS NOTED.

Part: FILTER — DIRTY (RECIRCULATION) · airframe 51,808 hrs · 17,982 cycles

DURING CLIMB, THE FLIGHT ATTENDANTS REPORTED A FAINT ELECTRICAL ODOR IN CABIN. THE ODOR DISSIPATED AFTER THE RIGHT RECIRCULATION FAN WAS TURNED OFF. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REMOVED AND REPLACED RIGHT AND LEFT RECIRCULATION FAN FILTERS. ACCOMPLISHED MCM 05-96-70 WITH NO ODORS NOTED. SEE ALSO AALA20160817010.

Part: WARNING MESSAGE — FALSE ACTIVATION (SLAT SYSTEM) · airframe 51,627 hrs · 17,922 cycles

DURING APPROACH, RECEIVED A LEADING EDGE SLAT DISAGREE EICAS MESSAGE. EMERGENCY DECLARED. LANDING UNEVENTFUL. ACCOMPLISHED FSEU BITE CHECK IAW FIM 27-51-00. FSEU NR 1 SHOWED AUTOSLAT FAIL CODE 309, FSEU NR 2 SHOWED NO DATA CODE 209. ALL THREE FSEU SHOWED NO CURRENT FAULTS. ACCOMPLISHED FIM TASK 27-81-00-815-808. NO FAULTS FOUND. SYSTEM CHECKED NORMAL.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 50,581 hrs · 17,495 cycles

FIRST CLASS LAVATORY SMOKE ALARM WENT OFF DURING DESCENT, NO SIGN OF SMOKE OR HEAT. AN EMER WAS DECLARED & THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. INSPECTED FWD LAVATORY WASTE RECEPTACLE & FIRE EXTINGUISHING SYS. NO EVIDENCE OF SMOKE, FIRE OR OVERHEATING. REPLACED SMOKE DETECTOR WITH DETECTOR FROM AFT LAVATORY IAW MM 26-14-01. PLACARDED THE LT AFT LAVATORY SMOKE DETECTION SYS, MEL 26-15A. REPLACED THE AFT LAVATORY SMOKE DETECTOR IAW AMM 26-14-01. OPERATIONALLY CHECKED GOOD. THE ACFT WAS NOT GNDED.

Part: WINDOW — CRACKED (COCKPIT) · airframe 50,299 hrs · 17,394 cycles

FIRST OFFICER’S WINDSHIELD OUTER PANE SHATTERED AT CRUISE. AN EMER WAS DECLARED & THE FLIGHT DIVERTED WITHOUT FURTHER INCIDENT. REPLACED FIRST OFFICER’S WINDSHIELD IAW AMM 56-11-01. ALSO REPLACED FIRST OFFICER’S SIDE WINDOW HEAT CONTROLLER AS A PRECAUTION IAW 30-41-01. ALL CHECKED NORMAL. THE ACFT WAS GNDED.

Part: CONNECTOR — DEFECTIVE (FLAP SYSTEM) · airframe 50,088 hrs · 17,319 cycles

DURING FLAP RETRACTION, BETWEEN 1 DEGREE & UP, LE SLAT ASYM EICAS MSG APPEARED & LE LIGHT ILLUMINATED. AN EMER WAS DECLARED & ACFT DIVERTED WITH AN UNEVENTFUL LANDING. THE ACFT WAS REMOVED FROM SERVICE. REPLACED CONNECTOR D40302J IAW WDM 27-81-31. FSEU 1 & 2 BITE TESTED GOOD IAW FIM 27-51-01. FLAPS & SLATS OPERATE NORMAL.

Part: STRAP — CORRODED (FUSELAGE) · airframe 50,029 hrs · 17,289 cycles

CORROSION AROUND NUTPLATES ON AFT STRAP FOR APU INLET STATION 1825. REPAIRED STRAP IAW SRM 53-80-15 2R REPAIR 1.

Part: STRAP — CORRODED (FUSELAGE) · airframe 50,029 hrs · 17,289 cycles

APU AIR INTAKE DOOR, FWD HOUSING TO FUSELAGE STRAP CORRODED. REPAIRED FWD STRAP IAW EA 255004.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,029 hrs · 17,289 cycles

CORROSION ON LOWER APU INLET ANGLE SUPPORT. REPLACED ANGLE IAW SRM 51-40-02 & 51-20-01.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 50,029 hrs · 17,289 cycles

TEMPORARY EXTERNAL DOUBLER REPAIR ON FUSELAGE NEAR STATION 620, STRINGER 18L REQUIRES ACCOMPLISHMENT OF PERMANENT REPAIR. APPLIED PERMANENT DOUBLER REPAIR ON FUSELAGE FWD & BELOW L2 DOOR, BETWEEN STATION 615 - 640, STRINGERS 17L - 19L IAW EA 254733.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · airframe 50,029 hrs · 17,289 cycles

TRANSITION PANEL LT SIDE, STATION 1360 - 1410 HAS CORROSION. REPLACED TRANSITION PANEL FROM STATION 1310 - 1410 IAW AARD 50-00-05-01.

Part: BULKHEAD — CRACKED (LT PYLON) · airframe 50,029 hrs · 17,289 cycles

AFT BULKHEAD LT PYLON HOLE NR 2 AFT FACE CRACKED. OVERSIZED THE DISCREPANT HOLE TO REMOVE THE CRACK INDICATION. INSTALLED FREEZE PLUG. COMPLETED REPAIR IAW EA 254881.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,029 hrs · 17,289 cycles

R1 DOOR WEB FROM STATION 345 - 365.25 FOUND CORRODED. REPLACED WEB IAW SRM 51-40-02 & AARD 51-00-05.

Part: PAN — GOUGED (L2 DOOR) · airframe 50,029 hrs · 17,289 cycles

L2 DOOR HANDLE PAN IS GOUGED. REPAIRED IAW AARD 51-00-05-1 REPAIR 1 & DWG 143N6100.

Part: SKIN — GOUGED (FUSELAGE) · airframe 50,029 hrs · 17,289 cycles

DURING C CHECK, GOUGE FOUND AT STATION 520 - 540, STRINGER 28L & 27L. REMOVED DAMAGE & INSTALLED EXTERNAL DOUBLER IAW SRM 53-00-01-2R-3.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 50,029 hrs · 17,289 cycles

FLOORBOARD SUPPORT DAMAGED AT STATION 700 - 720, RBL 11. REPAIRED IAW AARD 53-30-53-1 & SRM 53-00-53-2R-1.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 49,396 hrs · 17,072 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH WHEN FLAP HANDLE MOVED FROM 15 TO 20 DEGREES. FLAP MOVEMENT STOPPED BETWEEN 15 & 20 DEGREES. EICAS TE FLAP DISAGREE, WAS RECEIVED. CHECKED FLAPS SEVERAL TIMES & FOUND NORMAL OPERATION WITH NO FAULTS DETECTED. PERFORMED FSEU CHECK IAW FIM 27-51-00-815-814 & FIM 27-51-00-815-808 WITH NO FAULTS FOUND. SYS CHECKED NORMAL. .

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 49,116 hrs · 16,975 cycles

EMERGENCY LIGHTS FAILED IN SEAT ROWS 27D - 36D & EXIT SIGNS AT R4 & L4 DOORS. R & R BATTERY PACK M10801. GOOD OPERATIONAL CHECK IAW AMM 33-51-07.

Part: FSEU — FAULTED (TE FLAP) · airframe 48,245 hrs · 16,657 cycles

EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH TO LANDING WHEN FLAPS EXTENDED TO 20 DEGREES SELECTED, THEY STOPPED AT 16 DEGREES. TE FLAP DISAGREE ILLUMINATED. ACCOMPLISHED BITE OF FSEU IAW BFIM 27-51-00-815-805 WITH FAULT CODE 305 RETURNED ON FSEU 1. R & R FSEU 1. ACCOMPLISHED ALL OPERATIONAL CHECKS & RIG CHECKS IAW AMM 27-51-01. SYS CHECKED NORMAL.

Part: TRANSMISSION — FAILED (TE FLAPS) · airframe 48,180 hrs · 16,632 cycles

DURING APPROACH SELECTED 20 DEGREE FLAPS AT 170 KIAS. FLAP STUCK AT 17 DEGREES, GOT TE DISAGREE LIGHT & TE FLAP DISAGREE MESSAGE. ACCOMPLISHED CHECKLIST. TRAILING FLAPS DIDN`T MOVE DURING CHECKLIST, TRANSMISSION NR 8 INDICATOR TRIPPED. RESET INDICATOR, RAN FLAPS, INDICATION DID NOT TRIP. TO ACCOMPLISHED AT FOR FLAP TRANSMISSION NR 8 & FULL OPERATIONS CHECKED OF SYSTEM, EMERGENCY DECLARED DIVERTED & LANDED UNEVENTFULLY. REMOVED AND REPLACED NUMBER 8 FLAP TRASMISSION IAW AMM 27-51-17-024-001 AND AMM 27-51-17-434-020. OPS CHECKED GOOD. OK FOR SERVICE.

Part: TRANSMISSION — LOW (TE FLAP) · airframe 48,111 hrs · 16,605 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH FLAPS FAILED TO EXTEND HYD OR ELEC. PERFORMED NO FLAP LANDING. PERFORMED FIM 27-51-00-815-808. SERVICED OIL ON FLAP TRANSMISSIONS 1, 2, 3, 5, 6, 7 & 8. ACFT FLOWN ON FCF IAW SM 12-050 FOR VERIFICATION OF FIX. FLAPS EXTENDED & RETRACTED SEVERAL TIME WITH NO DISCREPANCIES.

Part: TRANSMITTER — FAILED (TE FLAP SYSTEM) · airframe 48,111 hrs · 16,605 cycles

DURING APPROACH TE FLAP DISAGREE OCCURRED. PERFORMED QRH PROCEDURE, FLAPS EXTENDED TO 20 DEGREES, EMERGENCY DECLARED, LANDING UNEVENTFUL. FOUND LT OTBD TE FLAP TRANSMITTER INTERMITTENT. R & R TRANSMITTER IAW AMM 27-58-03. SYS CHECKED NORMAL.

Part: INDICATOR — TRIPPED (TE FLAP) · airframe 47,634 hrs · 16,422 cycles

TRAILING EDGE FLAP DISAGREE EICAS INDICATION. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND LT WING INBD TE FLAP INBD FLAP TRANSMISSION OVERLOAD INDICATOR TRIPPED. RESET INDICATOR. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 47,629 hrs · 16,421 cycles

CONNECTION TO EMER FLOOD LIGHT AFT LAVATORY WALL INOPERATIVE. SECURED CONNECTION. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — UNSECURE (EXIT SIGN) · airframe 47,594 hrs · 16,408 cycles

EMERGENCY EXIT LOCATOR SIGN ARROW AT FWD WALL OF RT NR 4 AFT LAVATORY INOPERATIVE. SECURED CONNECTOR. OPERATIONS CHECKED NORMAL.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,816 hrs · 16,125 cycles

CORROSION ON DOOR DRAIN SUPPORT FROM STATIONS 1660 TO 1681 & RBL 59. R & R DRAIN SUPPORT.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,816 hrs · 16,125 cycles

HAT CHANNEL FROM STATIONS 1640 TO 1660 & BL 0. R & R HAT CHANNEL IAW AARD 51-00-05-1.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,816 hrs · 16,125 cycles

LEFT NR 4 DOOR FWD GUTTER BOX FROM STATIONS 1640 TO 1660 CORRODED. REPLACED GUTTER BOX IAW AARD 51-00-05-1.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,816 hrs · 16,125 cycles

GUTTER BOX AT LT NR 4 DOOR CORRODED. REPLACED GUTTER BOX IAW AARD 51-00-05-1.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,816 hrs · 16,125 cycles

CORROSION ON HAT CHANNEL FROM STATIONS 1660 TO 1681. R & R HAT CHANNEL IAW AARD 51-00-05-1.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 45,380 hrs · 15,600 cycles

DFW INFLIGHT MIA-LAS CREW REPORTED EICAS MESSAGE FOR WINDOW HEAT & CAPTAINS LT WINDSHIELD CRACKED. EMERGENCY DECLARED FLIGHT DIVERTED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CAPTAINS LT WINDSHIELD. SYSTEM GND CHECKED NORMAL OPERATION CLOSED.

Part: SWITCH — TRIPPED (LE SLAT) · airframe 45,348 hrs · 15,587 cycles

MIA CREW REPORTED LE SLAT ASYMMETRY MESSAGE. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RT SLAT LOST SWITCH TRIPPED & CABLE CLAMP LOOSE. RESET SWITCH & SECURED CLAMP. SYSTEM GND CHECKED NORMAL OPERATION CLOSED.

Part: SKIN — DENTED (LT HORIZ STAB) · airframe 45,344 hrs · 15,583 cycles

LT HAND STABILIZER INBD UPPER TORQUE BOX HAS NUMEROUS HAIL DENTS. ACCOMPLISHED REPAIR IAW EA B757-55-032561.

Part: SKIN — DENTED (RT HORIZ STAB) · airframe 45,344 hrs · 15,583 cycles

RT HAND STABILIZER INBD UPPER TORQUE BOX SKIN HAS NUMEROUS HAIL DENTS. ACCOMPLISHED REPAIR IAW EA B757-55-032553.

Part: CONNECTOR — LOOSE (CABIN) · airframe 44,782 hrs · 15,381 cycles

EMERGENCY LIGHT AT SEAT 29D INOPERATIVE. RE-SECURED LOOSE CONNECTOR FOR SEAT 29D EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,782 hrs · 15,381 cycles

EMERGENCY EXIT LIGHTING AT SEAT ROW 29 INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT LIGHT AT SEAT ROW 29. OPS CHECK NORMAL.

Part: JACKSCREW — LACK OF LUBE (TE FLAP) · airframe 44,455 hrs · 15,263 cycles

SFO - CREW REPORTED EICAS MESSAGE TRAILING EDGE FLAP DISAGREE. EMERGENCY DECLARED FLIGHT LANDED SFO WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND NUMBER 6 TORQUE LIMITER TRIPPED. RESET AND LUBED JACKSCREW. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: INDICATOR — TRIPPED (TE FLAP) · airframe 44,088 hrs · 15,118 cycles

BOS - CREW REPORTED FLAP ASYMMETRY EICAS WARNING ON APPROACH. EMERGENCY DECLARED FLIGHT LANDED BOS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND INBOARD FLAP DRIVE UNIT OVER TORQUE INDICATOR TRIPPED. RESET INDICATOR AND SERVICE FLAP TRANSMISSION. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,148 hrs · 14,768 cycles

EMERGENCY LIGHT AT 1AB INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT 1AB. OPS CHECK NORMAL.

Part: FLAP — DAMAGED (LT WING) · airframe 42,433 hrs · 14,513 cycles

LEFT INBOARD AFT FLAP HAIL DAMAGED. REPAIRED FLAP ASSEMBLY PER ESO 90252 AND EA COMP-57-022935.

Part: WIRE HARNESS — LOOSE (CABIN) · airframe 40,581 hrs · 13,834 cycles

SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 18 D,E,F ARE INOPERATIVE. SECURED LOOSE HARNESS CONNECTION AT SEATS 18 D,E,F. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,061 hrs · 12,592 cycles

SEAT EMERGENCY LIGHTS OUT FROM ROWS 90 TO 150. REPLACED BATTERY PACK FOR SEAT EMERGENCY LIGHTS FROM ROWS 90 TO 150. OPS CHECKED NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 37,061 hrs · 12,592 cycles

SEAT EMERGENCY LIGHTS OUT FROM ROWS 90 TO 150. REPLACED CHARGER ASSEMBLY FOR BATTERY PACK FOR SEAT EMERGENCY LIGHTS FROM ROWS 90 TO 150. OPS CHECKED NORMAL.

Part: PLACARD — DAMAGED (CABIN) · airframe 37,061 hrs · 12,592 cycles

EXIT MARKER DECAL AT RIGHT FORWARD OVERWING EXIT DAMAGED. REPLACED EXIT MARKER DECAL AT RIGHT FORWARD OVERWING EXIT. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,374 hrs · 12,351 cycles

EMERGENCY LIGHTS FROM ROW 27 AND AFT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM ROW 27 AND AFT. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,374 hrs · 12,351 cycles

EMERGENCY LIGHTS INOPERATIVE FROM ROW 27 AND AFT. REPLACED LIGHT ASSEMBLY AT SEAT 33. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,374 hrs · 12,351 cycles

EMERGENCY LIGHTS INOPERATIVE FROM ROW 27 AND AFT. REPLACED BATTERY PACK AT ROW 19. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,374 hrs · 12,351 cycles

EMERGENCY LIGHTS INOPERATIVE FROM ROW 27 AND AFT. REPLACED BATTERY PACK OVER AFT LAVATORIES. OPS TESTED NORMAL.

Part: RIB — CORRODED (TE FLAP) · corrosion level 2 · airframe 35,998 hrs · 12,207 cycles

LEFT INBOARD AFT TRAILING EDGE FLAP ASSEMBLY HAS CORROSION INTERNALLY IN TORQUE TUBE AREA OF INBOARD RIB. REPLACED CORRODED RIB WITH NEW RIB PER ESO 90252.

Part: ANGLE — WORN (DOOR FRAME) · airframe 35,993 hrs · 12,202 cycles

FORWARD EMERGENCY EQUIPMENT ACCESS (113AL) FORWARD FRAME TOP ANGLE HAS HOLE WORN IN FROM DOOR LATCH ROD JUST ABOVE LATCH PLATE. INSTALLED DOUBLER REPAIR PER SRM 51-70-11 AND EA B757-53-009111.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,993 hrs · 12,202 cycles

AFT CARGO FLOOR SUPPORT CRACKED CORRODED AT STATION 1470. REMOVED AND REPLACED FLOOR SUPPORT PER IAW SRM 51-10-02-G9.

Part: SKIN — CORRODED (TE FLAP) · corrosion level 2 · airframe 35,993 hrs · 12,202 cycles

SEVERAL AREAS OF CORROSION FOUND ON UPPER SURFACE OF UPPER FLAP SKIN ALONG AFT ROW OF FASTNERS. INSTALLED DOUBLER COUNTER BORED HONEYCOMB FROM INSIDE OF FLAP TO SHOOT RIVETS OF DOUBLER. REPAIRED HONEYCOMB POTTING AND HOT BONDED DOUBLER PER SRM 51-70-10-2R PARAGRAPH 7A SUB5.

Part: PAN — GOUGED (R1 DOOR) · airframe 35,993 hrs · 12,202 cycles

RIGHT NUMBER 1 DOOR OUTER HANDLE PAN IS GOUGED. REMOVED OLD AND INSTALLED NEW HANDLE PAN ON RIGHT NUMBER 1 DOOR PER ESO 90284.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,993 hrs · 12,202 cycles

AFT RIGHT LAVATORY MOUNT HAS LIGHT CORROSION RIGHT BUTTLINE 48 STATION 1640. REMOVED AND REPLACED LAVATORY FLOOR FITTING PER SRM 51-10-02-0G.

Part: WIRE — DAMAGED (CABIN) · airframe 35,804 hrs · 12,140 cycles

MOUNTED EMERGENCY LIGHT AT MID GALLEY INOPERATIVE. FOUND WIRES AT LIGHT ASSEMBLY DAMAGED. REPLACED LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,938 hrs · 11,824 cycles

RIGHT NUMBER FOUR DOOR EMERGENCY LIGHT INOPERATIVE. RELAMPED RIGHT NUMBER FOUR DOOR EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 34,788 hrs · 11,772 cycles

EMERGENCY ESCAPE PATH LIGHTING IN FIRST CLASS INOP. REPLACED BATTERY PACK.

Part: OUTFLOW VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 34,465 hrs · 11,659 cycles

BOS - CREW REPORTED CABIN UNABLE TO PRESSURIZE. EMERGENCY DECLARED, RETURNED TO BOS WITHOUT INCIDENT. REPLACED OUTFLOW VALVE AND ACTUATOR ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATIONS.

Part: CONNECTOR — BROKEN (CABIN)

DFW - EXIT LOCATOR SIGN ABOVE HATCH AREA INOPERATIVE. REPLACED CONNECTOR ON EXIT LOCATOR SIGN.

Part: TRANSMITTER — FAILED (TE FLAPS) · airframe 32,560 hrs

STL INFLIGHT. TRAILING EDGE FLAP DISAGREE INDICATION ON APPROACH. LANDED STL WITHOUT INCIDENT WITH FLAPS AT 20 DEGREES. REPLACED RIGHT HAND FLAP TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: HOSE — LEAKING (HYD SYSTEM)

PTY INFLIGHT T2189/15JUL - CREW REPORTED LT HYDRAULIC SYSTEM QUANTITY DECREASED RAPIDLY. LANDED PTY WITHOUT INCIDENT. FOUND NOSE GEAR ACTUATOR LINE BROKEN FROM NOSE WHEEL WELL. REPLACED NOSE GEAR ACTUATOR LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHT AT SEAT 30C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 30C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PIN — DAMAGED (TE FLAP)

JFK INFLIGHT T1298/20MAY MIA TO LGA - TRAILING EDGE FLAP DISAGREE INDICATION ILLUMINATED ON APPROACH. LANDING MADE WITH FLAPS AT 20. DECLARED EMERGENCY AND LANDED JFK WITHOUT INCIDENT DUE TO HIGHER LANDING SPEED. FOUND LEFT INBOARD FLAP INBOARD TRANSMISSION OVER TORQUE PIN POPPED. RESET PIN AND SERVICED TRANSMISSION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS)

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

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. REPAIRED WIRE AT SIDEWALL CONNECTION FOR SEAT 26D EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT SEAT 31D MISSING LENS AND BULB. REPLACED CLEAR LENS AND RELAMPED EMERGENCY LIGHTS AT SEAT 31D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SNA - SEAT MOUNTED EMERGENCY LIGHT AT ROWS 16 THROUGH 27DEF INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHT AT ROWS 16 THROUGH 27DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT)

ORD - SEAT SIDE EMERGENCY LIGHT AT SEAT 27D INOPERATIVE. FOUND WIRES DISCONNECTED. RECONNECTED WIRES FOR SEAT SIDE EMERGENCY LIGHT AT SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SPRING — OUT OF ADJUST (GIRT BAR)

DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, ONE GIRT BAR SPRING OUT OF ADJUSTMENT. ADJUSTED ONE GIRT BAR SPRING. SYTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

ORD - FIRST CLASS EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. SECURED LOOSE CONNECTOR UNDER FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PUMP — FAILED (HYD SYSTEM)

BDL - FLT 623 - EN ROUTE BDL-SJU, AFTER TAKEOFF, LEFT ENGINE DRIVEN HYDRAULIC PUMP FAILED. AIRCRAFT LOST ALL LEFT SYSTEM HYDRAULIC FLUID. PERFORMED AN ALTERNATE GEAR EXTENSION. AIRCRAFT RETURNED TO BDL AND LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE HYDRAULIC PUMP AND ALL LEFT SYSTEM FILTERS. SERVICED HYDRAULIC SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 12 AND 13 LOOSE. SECURED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — FAILED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH FLOOR LIGHT JUMPER WIRE BETEEN COFFEE BAR AND MAIN CABIN INOPERATIVE. REPLACED EMERGENCY EXIT PATH FLOOR LIGHT JUMPER WIRE. SYSTEM GROUND CHECK, NORMAL OPERATION. (X)