N635AA

Part: LENS — BROKEN (CABIN) · airframe 73,360 hrs · 26,310 cycles

LENS ON EXIT IDENTIFIER FWD OF RT NR 2 DOOR BROKEN. REPLACED LENS ON EXIT IDENTIFIER FWD OF RT NR 2 DOOR. OPERATIONS CHECKED NORMAL.

Part: LENS — LOOSE (CABIN) · airframe 73,360 hrs · 26,310 cycles

LENS ON EXIT IDENTIFIER AT ROW 17 SEAT FWD OF OVERWING LATCH LOOSE. REPLACED LENS ON EXIT IDENTIFIER AT ROW 17 SEAT FWD OF OVERWING LATCH.

Part: WIRE HARNESS — UNSECURE (CABIN) · airframe 73,360 hrs · 26,310 cycles

WIRE HARNESS HANGING DOWN UNDER SEAT 21D. SECURED WIRE HARNESS TO ESCAPE PATH LIGHT AT SEAT 21D. OPERATIONS CHECKED NORMAL.

Part: LIGHT — LOOSE (CABIN) · airframe 73,360 hrs · 26,310 cycles

ESCAPE PATH LIGHT ON BULLNOSE AT ROW 22 OVERHEAD BIN LOOSE. SECURED ESCAPE PATH LIGHT ON BULLNOSE AT ROW 22 OVERHEAD BIN. OPERATIONS CHECKED NORMAL.

Part: LENS — LOOSE (CABIN) · airframe 73,360 hrs · 26,310 cycles

ESCAPE PATH LIGHT LENS ON BULLNOSE AT ROW 1 OVERHEAD BIN LOOSE. SECURED LENS ON ESCAPE PATH LIGHT ON BULLNOSE AT ROW 1 OVERHEAD BIN. OPERATIONS CHECKED NORMAL.

Part: LENS — LOOSE (CABIN) · airframe 73,360 hrs · 26,310 cycles

LENS ON EXIT IDENTIFIER ON AFT SIDE OF RT NR 1 DOOR LOOSE. REPLACED LENS FOR EXIT IDENTIFIER ON AFT SIDE OF RT NR 1 DOOR. OPERATIONS CHECKED NORMAL.

Part: RETAINING NUT — MISSING (TE FLAP) · airframe 72,859 hrs · 26,127 cycles

MIA CREW REPORTED TE FLAP ASYMMETRY. EMERGENCY DECLARED FLIGHT RETURNED MIA & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND RETAINING NUT ON BEARING ASSEMBLY MISSING. REPLACED BEARING ASSEMBLY ON RT FLAP, SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: TRANSITION PANEL — CORRODED (CARGO BAY) · corrosion level 3 · airframe 72,620 hrs · 26,037 cycles

FOUND CORROSION ON RT HAND AFT CARGO THRESHOLD TRANSITION PANEL. REPLACED SIDE PANEL IAW SRM 51-10-02-0G.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,455 hrs · 24,922 cycles

SEAT 12D EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT 12D ESCAPE PATH LIGHT. OPS CHECK NORMAL.

Part: PIN — NOT SEATED (EMERGENCY LIGHT) · airframe 69,455 hrs · 24,922 cycles

LEFT NUMBER 2 LAVATORY FLOOR MOUNTED ESCAPE PATH LIGHT INOPERATIVE. RESEATED PINS 27 AND 28 AT D5690. OPS CHECK NORMAL.

Part: SEAT — LOOSE (CABIN) · airframe 68,419 hrs · 24,554 cycles

JFK - INFLIGHT BOS-MIA. CREW REPORTED SEAT ROW 12DEF CAME OUT OF THE TRACK DURING TAKEOFF. EMERGENCY DECLARED FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED COMPLETE INSPECTION OF SEATS ONBOARD AND FOUND NUMEROUS SEATS NOT LOCKED DOWN PROPERLY. SECURED AND TIGHTENED ALL AFFECTED SEATS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FIREWALL — DAMAGED (FUSELAGE) · airframe 68,387 hrs · 24,543 cycles

IMPACT DAMAGE FOUND ON THE FORWARD AUXILIARY POWER UNIT FIRE WALL. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-80-08-2R.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,387 hrs · 24,543 cycles

MAIN CABIN FLOOR SUPPORT INTERCOSTAL 2 EACH AT LEFT NUMBER 4 DRAIN AND SILL AREA HAD EXFOLIATION CORROSION THROUGHOUT AT FASTENER HOLE LOCATION BODY STATIONS 1640 TO 1682, LEFT BUTTLINE 54. INSTALLED 2 EACH INTERCOSTALS, DRAIN PAN, AND SCUFF PLATES PER SRM 51-40-02.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,387 hrs · 24,543 cycles

AFT DECK PLATE FROM STATIONS 1700 TO 1720 LEFT BUTTLINE 40 TO RIGHT BUTTLINE 44 REPAIR CORRODED. INSTALLED DOUBLER AND 2 EACH SHIMS PER SRM 53-60-51-2R.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,387 hrs · 24,543 cycles

FLOOR SUPPORT ANGLE CORRODED AT STATION 1715 RIGHT BUTTLINES 33.5 TO 39.5. REMOVED AND REPLACED ANGLE PER SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,387 hrs · 24,543 cycles

MAIN CABIN FLOOR SUPPORT INTERCOSTAL AT RIGHT NUMBER 4 DRAIN AND SILL AREA HAS EXFOLIATION CORROSION THROUGHOUT FASTENER HOLE LOCATION FROM BODY STATIONS 1640 TO 1682, RIGHT BUTTLINE 54. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,387 hrs · 24,543 cycles

MAIN CABIN FLOOR SUPPORTS CORRODED 2 EACH AT RIGHT NUMBER 1 DOOR SILL. INSTALLED 2 EACH SUPPORTS PER SRM 51-40-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,427 hrs · 24,197 cycles

OVERWING EXIT EMERGENCY LIGHT AT SEAT 18A INOPERATIVE. REPLACED LAMP FOR OVERWING EXIT EMERGENCY LIGHT AT SEAT 18A. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,522 hrs · 23,086 cycles

EMERGENCY LIGHT AT SEAT 17D INOPERATIVE. REPLACED SEAT MOUNTED ASSEMBLY AT SEAT 17D. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 64,054 hrs · 22,912 cycles

AISLE EMERGENCY LIGHT AT SEAT 36DEF INOPERATIVE. REPLACED BATTERY PACK M736. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,578 hrs · 22,742 cycles

SEAT 29D EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 29D EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,578 hrs · 22,742 cycles

SEAT 31D EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR 31D EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 63,427 hrs · 22,695 cycles

AFT OVERWING EXIT LIGHT ON AFT LEFT OVERWING EXIT SIGN INOPERATIVE. REPLACED LAMP FOR AFT OVERWING EXIT LIGHT ON AFT LEFT OVERWING EXIT SIGN. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,484 hrs · 22,020 cycles

RIGHT NUMBER 1 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 1 DOOR EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: SHROUD — MISSING (CABIN) · airframe 60,976 hrs · 21,812 cycles

SEAT MOUNTED EMERGENCY LIGHT AT AFT SEAT 5E IS MISSING SHROUD. REPLACED SHROUD FOR SEAT MOUNTED EMERGENCY LIGHT AT AFT SEAT 5E. OPS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 60,976 hrs · 21,812 cycles

SEAT MOUNTED EMERGENCY LIGHT LENS AT AFT SEAT 5E IS MISSING. REPLACED LENS FOR SEAT MOUNTED EMERGENCY LIGHT AT AFT SEAT 5E, OPS CHECKED NORMAL.

Part: ACTUATOR — MALFUNCTIONED (TE FLAP) · airframe 60,463 hrs · 21,617 cycles

LAX - CAPTAIN REPORTED ON APPROACH TRAILING EDGE FLAP DISAGREE LIGHT ILLUMINATED. EMERGENCY DECLARED LANDED LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED INBOARD AND OUTBOARD ACTUATORS THAT HAD TRIPPED. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: INDICATOR — TRIPPED (TE FLAP) · airframe 60,459 hrs · 21,615 cycles

LAX - DURING APPROACH FLAPS POSITIONED TO 1 DEGREE TRAILING EDGE DISAGREE LIGHT ILLUMINATED. FOUND LEFT OUTBOARD FLAP INBOARD ANGLE GEARBOX TRIP INDICATOR POPPED AND RIGHT INBOARD FLAP INBOARD ANGLE GEARBOX TRIP INDICATOR POPPED. RESET INDICATORS AND RAN FLAPS NUMEROUS TIME AND NO FAULTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — SHORTED (CABIN) · airframe 60,400 hrs · 21,594 cycles

SEAT MOUNTED EMERGENCY LIGHTS OUT AT SEAT 26D TO AFT CABIN. REMOVED AND REPLACED MODULE AND BATTERY. OP CHECK OK.

Part: SKIN — BULGED (LE SLAT) · airframe 60,025 hrs · 21,456 cycles

RIGHT WING NUMBER 8 SLAT SKIN BULGED TOP UPPER SURFACE SKIN AT STATION 460 FORWARD OF MAIN DRIVE TRACK. REMOVED DAMAGED SKIN, INSTALLED DOUBLER PER AARD 57-43-00-1.

Part: SKIN — DAMAGED (LE SLAT) · corrosion level 2 · airframe 60,025 hrs · 21,456 cycles

RIGHT WING NUMBER 8 SLAT HAS DEEPLY BLENDED AREA. REMOVED DAMAGED SKIN INSTALLED DOUBLER PER AARD 57-43-00-1.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 60,025 hrs · 21,456 cycles

NUMBER 4 SLAT INBOARD UPPER TRAINING EDGE WEDGE DELAMINATED. REMOVED DAMAGED TRAILING EDGE INSTALLED NEW WEDGE PER ESO 90248.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,025 hrs · 21,456 cycles

CORROSION ON NUMBER 3 SLAT UPPER SKIN AROUND FASTENER APPROXIMATELY 69 INCHES FROM INBOARD END. CUT OUT CORROSION AREA AND INSTALLED FLUSH DOUBLER PER AARD 57-43-00-1 PAGE 1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,025 hrs · 21,456 cycles

RIGHT WING NUMBER 7 SLAT SKIN BULGED AT TOP UPPER SURFACE SKIN STATION 350 FORWARD OF MAIN DRIVE TRACK. REMOVED DAMAGE PER SRM 57-43-00-2R PG 1 AND INSTALLED FLUSH DOUBLER REPAIR PER SRM 57-43-00-2R PG 2.

Part: PAN — CRACKED (R1 DOOR) · airframe 60,025 hrs · 21,456 cycles

RIGHT NUMBER ONE ENTRY DOOR HANDLE BOX CRACKED. REMOVED AND REPLACED RIGHT NUMBER ONE ENTRY DOOR HANDLE MECHANISM BOX PER ESO 90284.

Part: TORQUE BOX — CRACKED (R4 DOOR) · airframe 60,025 hrs · 21,456 cycles

RIGHT NUMBER FOUR DOOR HANDLE TORQUE BOX CRACKED. REMOVED AND REPLACED TORQUE BOX PER ESO 90108.

Part: TORQUE BOX — CRACKED (R4 DOOR) · airframe 60,025 hrs · 21,456 cycles

RIGHT NUMBER FOUR DOOR HANDLE TORQUE BOX CRACKED. REMOVED AND REPLACED TORQUE BOX PER ESO 90108.

Part: SKIN — CRACKED (LE SLAT) · airframe 60,025 hrs · 21,456 cycles

UPPER SKIN CRACKED AT HI-LOC HOLE AT OUTBOARD MAIN TRACK DRIVE RIB. INSTALLED DOUBLER PER SRM 57-43-01-2R 2 AND AARD 57-43-00-1.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,926 hrs · 21,411 cycles

EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK.

Part: TRANSMITTER — OUT OF POSITION (TE FLAP) · airframe 67,656 hrs · 20,620 cycles

DEN - INFLIGHT DFW-EGE. CREW REPORTED, HAD A TRAILING EDGE FLAP DISAGREEMENT AND PROCEEDED TO DEN, DECLARED AN EMERGENCY. LANDED IN DEN WITHOUT INCIDENT. ADJUSTED POSITION TRANSMITTER FOR TRAILING EDGE FLAP POWER DRIVE UNIT. SYSTEM GROUND CHECK NORMAL.

Part: SHROUD — BROKEN (EMERGENCY LIGHT) · airframe 57,022 hrs

DFW - EMERGENCY LIGHT SHROUD AT AFT SEAT 13D IS BROKEN. REPLACED SHROUD AT AFT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN) · airframe 57,022 hrs

DFW - EMERGENCY LIGHT AT LEFT AISLE BULL NOSE AT SEAT ROW 27 BROKEN. REPLACED LIGHT ASSEMBLY AT LEFT AISLE BULL NOSE SEAT ROW 27. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHT) · airframe 57,022 hrs

DFW - EMERGENCY LIGHT SHROUD AT AFT SEAT 3E IS BROKEN. REPLACED SHROUD AT AFT SEAT 3E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHT) · airframe 57,022 hrs

DFW - EMERGENCY LIGHT SHROUD AT AFT SEAT 22D IS BROKEN. REPLACED SHROUD AT AFT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN) · airframe 57,022 hrs

DFW - EMERGENCY LIGHT EXIT MARKER AT LEFT OF AFT RIGHT PASSENGER DOOR BROKEN. REPLACED LIGHT ASSEMBLY AT RIGHT PASSENGER DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHT) · airframe 57,022 hrs

DFW - EMERGENCY LIGHT SHROUD AT AFT SEAT 28D IS BROKEN. REPLACED SHROUD AT AFT SEAT 28D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHT) · airframe 57,022 hrs

DFW - EMERGENCY LIGHT SHROUD AT AFT SEAT 24D IS BROKEN. REPLACED SHROUD AT AFT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHT) · airframe 57,022 hrs

DFW - EMERGENCY LIGHT SHROUD AT AFT SEAT 35D IS BROKEN. REPLACED SHROUD AT AFT SEAT 35D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

DFW - EMERGENCY INTERIOR LIGHT EXIT MARKER L00750 AT AFT RIGHT NUMBER ONE DOOR HAS BROKEN BASE. REPLACED THE EMERGENCY INTERIOR LIGHT EXIT MARKER ASSEMBLY L00750 AT AFT RIGHT NR ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — BROKEN (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 18D HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — BROKEN (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 36D HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 36D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — BROKEN (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 17D HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — BROKEN (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 27D HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

DFW - BULLNOSE EMERGENCY FLOOD LIGHT AT LEFT HAND AISLE AT SEAT ROW 12 INOPERATIVE. RELAMPED THE BULLNOSE EMERGENCY FLOOD LIGHT AT LEFT HAND AISLE AT SEAT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — BROKEN (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 20D HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MANIFOLD — STUCK (FUEL SYSTEM)

DFW - UNABLE TO FEED FUEL FROM LEFT WING TANK. FUEL ONLY USED FROM RIGHT HAND TANK. LANDED DFW WITHOUT INCIDENT. CROSSFEED MANIFOLD APPEARED STUCK OPEN WITH RIGHT HAND PUMPS STRONGER THAN LEFT HAND PUMPS BURNING RIGHT HAND FUEL FIRST. PERFORMED FUEL QUANTITY BITE CHECKS, FUEL QUANTITY SYSTEM CHECK AND FUEL PUMP CHECK. NO FAULTS FOUND. COULD NOT DUPLICATE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

RT OVERWING INTERIOR EMERGENCY EXIT LIGHT AND EMERGENCY EXIT LOCATOR LIGHT ABOVE 14ABC INOPERATIVE. REPLACED BOTH BATTERY PACKS AND CHARGERS FOR RT OVERWING INTERIOR EMERGENCY EXIT LIGHT AND EMERGENCY EXIT LOCATOR LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN)

JFK - EMERGENCY EXIT LIGHT OVER 3L INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DISCONNECTED (EXIT SIGN)

DFW - RIGHT HAND EMERGENCY EXIT SIGN AT ROW 17 INOPERATIVE. RECONNECTED RIGHT HAND EMERGENCY EXIT SIGN WIRES AT ROW 17. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRUT — LOW (NLG)

ATL - FLT 1461 - EN ROUTE ATL-DFW, AFTER TAKEOFF, GEAR HANDLE BUT BOTH GEAR AND GEAR DOORS LIGHT REMAINED ILLUMINATED AND WARNING HORN ON. GEAR WAS PLACED DOWN AND RECEIVED THREE GREEN LIGHTS. RETURNED ATL AND LANDED WITHOUT INCIDENT. ACCOMPLISHED BITE CHECK OF PSEU. SERVICED NOSE STRUT WITH AIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: O-RING — CUT (RT ENGINE)

JFK - FLT 837 - EN ROUTE LGA-MCO, AFTER TAKEOFF, CLIMBING THROUGH 8,000 FEET, RIGHT ENGINE OIL PRESSURE DROPPED INTO YELLOW BAND. OIL PRESSURE FLUCTUATED AND THEN STEADILY DECREASED. DECLARED EMERGENCY AND LANDED AT JFK WITHOUT INCIDENT. INSPECTED AND FOUND RIGHT ENGINE PRESSURE OIL FILTER LEAKING. REMOVED PRESSURE OIL FILTER HOUSING AND FOUND OIL RING CUT. REPLACED O-RING AND INSPECTED PRESSURE OIL FILTER ELEMENT. SERVICED ENGINE. SYSTEMS GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - THE RIGHT EXTERIOR DOOR EMERGENCY LIGHT, THE BULLNOSE EMERGENCY FLOOD LIGHT AT 5E AND FORWARD ENTRY AISLE EMERGENCY EXIT SIGN LIGHT INOPERATIVE. ALL INOPERATIVE LIGHTS POWERED BY BATTERY PACK M730. REPLACED BATTERY PACK M730. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HYDRAULIC LINE — LEAKING (HYD SYSTEM)

(HYDRAULIC LINE) ENROUTE, LEFT HAND HYDRAULIC SYSTEM LOSS OF ALL FLUID IN FLIGHT. RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. REPLACED HYDRAULIC LINE TO DOWNLOCK ACTUATOR, ENGINE DRIVEN PUMP AND ENGINE DRIVEN PUMP FILTERS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — DEFECTIVE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AISLE PATH LIGHTING WAS INOPERATIVE. REPLACED EMERGENCY EXIT AISLE PATH LIGHTING CONTROL MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, CENTER CABIN EMERGENCY EXIT FLOOR LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT STRIP AT CENTER CABIN FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PASSENGER SEATS 9D THROUGH 17D FOUND INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 9D. SYSTEM GROUND CHECK, NORMAL OPERATION. (X)

Part: FLOOR BEAM — CORRODED (BS 1661)

AFW - FLOOR BEAM AT STATION 1661 HAS CORROSION REMOVED BEYOND SRM LIMITS. PER MRB 757-635. (M)

Part: DECK PLATE — CORRODED (BS 1681/1720)

AFW - DECK PLATE, AT STATION 1681 AND 1720, HAS CORROSION REMOVED AT VARIOUS BL LOCATIONS BEYOND SRM LIMITS. PER MRB 757-637. (M)