N338AA

Part: SKIN — CRACKED (LE SLAT) · airframe 93,844 hrs · 18,771 cycles

NUMBER 10 LEADING EDGE SLAT SKIN CRACKED. ACCOMPLISHED FLUSH DOUBLER SKIN REPAIR PER SRM 57-43-01-2R 2.

Part: SKIN — DENTED (TE FLAP) · airframe 93,844 hrs · 18,771 cycles

RIGHT WING OUTBOARD FLAP LOWER SURFACE HAS 2 DENTS ON TRAILING EDGE WEDGE 31 AND 43 INCHES FROM OUTBOARD END. ACCOMPLISHED HOT BOND REPAIR PER SRM 51-70-07.

Part: FLAP — DELAMINATED (LT WING) · airframe 93,844 hrs · 18,771 cycles

DELAMINATION FOUND ON OUTBOARD TRAILING EDGE FLAP 31 INCHES FROM INBOARD EDGE. ACCOMPLISHED HOT BOND REPAIR PER SRM 51-70-07.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,844 hrs · 18,771 cycles

FORWARD CARGO STRINGER 35 RIGHT IS CORRODED AT STATION 427. INSTALLED STRINGER SPLICE REPAIR PER SRM 53-00-00-3-2R.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,844 hrs · 18,771 cycles

FOUND CORROSION AROUND STRINGER CLIP HI-LOK COLLAR AT FRAME STATION FRAME 412 AND 39R. ACCOMPLISHED STRINGER SPLICE REPAIR PER SRM 53-00-03-2R.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,844 hrs · 18,771 cycles

BULK CARGO DOOR INNER SILL AREA WEB CORRODED IN MULTIPLE LOCATIONS ON UNDERSIDE, AROUND NUT PLATES. REPLACED WEB PER SRM 51-10-02.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,844 hrs · 18,771 cycles

STATION 1087 STRINGER 39 RIGHT CLIP CORRODED. REPLACED STRINGER CLIP PER SRM 51-10-02.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,939 hrs · 18,387 cycles

CORROSION ON BELLY SKIN FROM STATIONS 1235 TO 1245. CUT OUT DAMAGED SKIN AND INSTALLED REPAIR DOUBLER PER SRM 53-00-01-2R.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,939 hrs · 18,387 cycles

CORROSION ON BELLY SKIN FROM STATIONS 1165 TO 1180. CUT OUT DAMAGED SKIN AND INSTALLED REPAIR DOUBLER PER SRM 53-00-01-2R.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 91,213 hrs · 18,238 cycles

CEILING EMERGENCY LIGHTS IN AFT ZONE INOPERATIVE. REPLACED BATTERY PACK M734.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 91,213 hrs · 18,238 cycles

CEILING EMERGENCY LIGHTS IN LEFT AFT ZONE INOPERATIVE. REPLACED BATTERY PACK FOR POWER SUPPLY EQUIPMENT M734. OPS CHECK NORMAL.

Part: BUSHING — MIGRATED (LT PYLON) · airframe 90,306 hrs · 18,057 cycles

LEFT PYLON OUTBOARD MID SPAR FITTING OUTBOARD HAT BUSHING MIGRATED. REPLACED MIDSPAR FUSE PIN BUSHINGS PER EA B767-54-011847.

Part: BUSHING — MIGRATED (RT PLYON) · airframe 90,306 hrs · 18,057 cycles

RIGHT PYLON INBOARD MID SPAR FITTING INBOARD HAT BUSHING MIGRATED. REPLACED MIDSPAR BUSHINGS PER EA B767-54-011847.

Part: BUSHING — MIGRATED (LT PYLON) · airframe 90,306 hrs · 18,057 cycles

LEFT PYLON INBOARD MID SPAR FITTING OUTBOARD HAT BUSHING MIGRATED. REPLACED MIDSPAR FUSE PIN BUSHINGS PER EA B767-54-011847.

Part: BUSHING — MIGRATED (RT PLYON) · airframe 90,306 hrs · 18,057 cycles

RIGHT PYLON OUTBOARD MID SPAR FITTING INBOARD HAT BUSHING MIGRATED. REPLACED MIDSPAR BUSHINGS PER EA B767-54-011847.

Part: BUSHING — MIGRATED (RT PLYON) · airframe 90,306 hrs · 18,057 cycles

RIGHT PYLON INBOARD MID SPAR FITTING OUTBOARD HAT BUSHING MIGRATED. REPLACED MIDSPAR BUSHINGS PER EA B767-54-011847.

Part: BUSHING — MIGRATED (LT PYLON) · airframe 90,306 hrs · 18,057 cycles

LEFT PYLON INBOARD MID SPAR FITTING INBOARD HAT BUSHING MIGRATED. REPLACED MIDSPAR FUSE PIN BUSHINGS PER EA B767-54-011847.

Part: BUSHING — MIGRATED (LT PYLON) · airframe 90,306 hrs · 18,057 cycles

LEFT PYLON OUTBOARD MID SPAR FITTING INBOARD HAT BUSHING MIGRATED. REPLACED MIDSPAR FUSE PIN BUSHINGS PER EA B767-54-011847.

Part: BUSHING — MIGRATED (RT PLYON) · airframe 90,306 hrs · 18,057 cycles

RIGHT PYLON OUTBOARD MID SPAR FITTING OUTBOARD HAT BUSHING MIGRATED. REPLACED MIDSPAR BUSHINGS PER EA B767-54-011847.

Part: BATTERY PACK — DISCHARGED (FUSELAGE) · airframe 88,093 hrs · 17,604 cycles

LEFT AFT CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT CABIN EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,880 hrs · 17,361 cycles

THE 7B EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR 7B EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,880 hrs · 17,361 cycles

THE 30H EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR 30H. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 85,583 hrs · 17,100 cycles

EMERGENCY LIGHTS ARE DIM IN FORWARD GALLEY AND LEFT FORWARD AISLE SEATS. REMOVED AND REPLACED BATTERY PACK AT STA 445 LEFT. OPS CHECKED NORMAL.

Part: WIRE HARNESS — BROKEN (FIRE WARNING) · airframe 84,503 hrs · 16,884 cycles

SLC - INFLIGHT JFK-SFO. CREW REPORTED LEFT ENGINE FIRE WARNING LOOP TWO EICAS MESSAGE. FLIGHT DIVERTED SLC LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE FIRE DETECTION SYSTEM LOOP 2 HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 83,941 hrs · 16,770 cycles

LEFT AND RIGHT NR 1 DOOR SIDE WALL EMERGENCY LIGHT INOPERATIVE. SECURED LOOSE POWER PACK CONNECTOR.

Part: BEAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 83,596 hrs · 16,694 cycles

SPOT CORROSION WAS FOUND ON THE NUMBER 4 BEAM INNER CHORD OF THE AFT CARGO DOOR. DURING THE DISMANTLING THE INNER CHORD BUCKLED IN THE MIDDLE OF THE BEAM AT STATION 200. REPAIRED CHORD USING 1 FORMED ANGLE AND A REPAIR STRAP. THE CORROSION WAS LIMITED TO 3 NUT PLATE FASTENERS. BLEND LOCATIONS ARE AT STATIONS 169, 175, AND 224 AND WERE REPAIRED USING STRAPS AND NESTED FORMED ANGLES.

Part: CIRCUIT BREAKER — POPPED (COCKPIT) · airframe 82,597 hrs · 16,484 cycles

ORD - INFLIGHT JFK-LAX. CREW REPORTED RIGHT DC CIRCUIT BREAKER POPPED AND THEN ELECTRICAL SMELL IN CABIN. EMERGENCY DECLARED, LANDED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CIRCUIT BREAKER C891 AND LEFT AND RIGHT RECIRCULATION FAN FILTERS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ACTUATOR — FAILED (THRUST REVERSER) · airframe 81,622 hrs

ELP INFLIGHT LAX TO MIA - NUMBER TWO THRUST REVERSER UNLOCK LIGHT ILLUMINATED. SHUT DOWN NUMBER TWO ENGINE AS PRECAUTION. LANDED ELP WITHOUT INCIDENT. SINGLE ENGINE TIME APPROXIMATELY 12 MINUTES. VISUAL INSPECTION SHOWED REVERSER SLEEVE PARTIALLY OPEN ONE HALF TO ONE INCH. OTHER REVERSER WAS FLUSH. REPLACED NUMBER TWO ENGINE INBOARD THRUST REVERSER CENTER HYDRAULIC LOCKING ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN) · airframe 79,057 hrs

LAX - EMERGENCY LIGHT AT AFT CENTER FLIGHT ATTENDANT SEAT BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT AFT CENTER FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 78,695 hrs · 15,684 cycles

AFT CARGO FLOOR BEAM J CHANNEL INNER CHORD AT STATION 1285 HAS CORROSION REMOVAL ON UPPER HORIZONTAL FLANGE. MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIRED IN ACCORDANCE WITH MRD 767 3196. CHORD SHOULD BE REPLACED BY THE NEXT C CHECK FOLLOWING 05 09 2008. (A)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,950 hrs

LAX - EMERGENCY EXIT LIGHT IN COCPIT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT LIGHT IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

JFK - EMERGENCY LIGHTS AT LEFT NUMBER THREE AND LEFT NUMBER FOUR DOOR EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER M1210 FOR EMERGENCY LIGHTS AT LEFT NUMBER THREE AND LEFT NUMBER FOUR DOOR EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - EMERGENCY LIGHTS AT RIGHT NUMBER ONE DOOR AND OVERWING INOPERATIVE. REPLACED BATTERY PACK AT M731 FOR EMERGENCY LIGHTS AT RIGHT NUMBER ONE DOOR AND OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LAX - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 5AB TO 22AB INOPERATIVE. REPLACED BATTERY PACKS AT SEATS 5AB AND 12AB FOR INOPERATIVE SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 5AB TO 22AB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

JFK- EMERGENCY LIGHTS AT SEAT ROWS 2AB TO 9AB INOPERATIVE. REPLACED MODULE AND BATTERY PACK AT FIRST CLASS POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LINE — LEAKING (METERING VALVE)

APPROX 5 MINUTES INTO CRUISE ALTITUDE, 37,000 FT, AN EICAS MESSAGE APPEARED INDICATING LOW QUANTITY IN THE CENTER HYDRAULIC SYSTEM. AT THAT TIME THE QUANTITY INDICATED .57 AND CONTINUED TO DECREASE TO .28. THE GEAR AND FLAPS WERE DEPLOYED USING ALTERNATE PROCEDURES. RETURNED AND LANDED LAX WITHOUT INCIDENT. REPLACED LEFT BRAKE METERING VALVE LINE. SYSTEM GROUND CHECKED NROMAL OPERATION. (M)

Part: WIRE — DAMAGED (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, MID GALLEY RIGHT EMERGENCY EXIT FLOOR FLOOD LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DISCONNECTED (CABIN)

BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 27H INOPERATIVE. RECONNECTED EMERGENCY EXIT FLOOR PATH LIGHT ASSEMBLY AT SEAT 27H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: OVEN — DIRTY (CABIN)

LHR - FLT 142 - NR 2 GALLEY OVEN SMOKES WHEN HEATED. OVEN DEACTIVATED AND FLIGHT LANDED LHR WITHOUT INCIDENT. CLEANED RESIDUAL FOOD FROM OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (COCKPIT DOOR)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN ABOVE COCKPIT DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY SIGN ABOVE COCKPIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — FAILED (EMERGENCY EXIT)

SFO - DURING OVERNIGHT MAINTENANCE, MID-GALLEY EMERGENCY EXIT SIGN INOPERATIVE. REPAIRED OPEN WIRE INTO CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT AFT GALLEY CROSS AISLE INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT AFT GALLEY CROSS AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (BS 325)

AFW - FLOORBEAM AT STATINO 325 HAS CORROSION REMOVAL ON UPPER SURFACE. ALODINED AREA, FABRICATED STRAP FROM .050 301.5 HARD STAINLESS STEEL. ATTACHED STRAP USING BACB30NW6 HI-LOCKS. APPLIED TWO COATS PRIMER TO STRAP AND FLOORBEAM. (M)

Part: FLOORBEAM — CORRODED (BS 852-933)

AFW - FLOORBEAMS AT LT AND RT BL 11 HAVE CORROSION REMOVAL ON UPPER SURFACE STATION 933. ROTO PEEN BLENDED AREA, ALODINE BEFORE PRIMER, APPLIED TWO COATS PRIMER. FILL BLENDS WITH BMS5-95. (M)

Part: IDG — INOPERATIVE (LT ENGINE)

ORD - FLT 95 - STEADY EICAS MSG L GEN DRIVE 'DRIVE' LIGHT ON STEADY OH GEN DRIVE DISC. PLACARDED LT IDG INOP PER MEL ENTERED IN MIC SHEET CHECKED LT AND RT IDG OILS AND APU OIL. REMOVED AND REPLACED LT IDG, LEAK CHECK GOOD. OPS CHECK GOOD. REMOVED PLACARD. (M)

Part: GENERATOR — FAILED (RT ENGINE)

RDU - FLT 0173 - RIGHT DRIVE CAME ON DURING CLIMB-OUT FL 280. DISCONNECT PROCEDURE WAS DONE IAW MANUAL. PLACARDED RIGHT ENGINE GENERATOR INOPERABLE PER MEL RF NR 24-1 AUTH 2-280DC-B. TRANSFERRED TO MIC SHEET. SERVICED BOTH IDGS AND APU OIL. GENERATOR DISCONNECTED. REMOVED AND REPLACED RIGHT ENGINE GENERATOR PER MM. OPS CHECKED AND LEAK CHECK GOOD. REMOVED MEL PLACARD 24-1 AUTH NR 2-28-0DC-B. CLEARED MIC SHEET. 33824FA00/1627.17FEB.RDU. (X)

Part: CONNECTOR — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 29H FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 29H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: IDG — FAILED (LEFT)

LEFT GEN OFF LIGHT ILLUMINATED. DEF ENGINE DRIVEN GENERATOR. PLACARD RAISED AND ENT IN MICS, AS PER MPM 24-1 SERVICED BOTH IDGS AND APU OIL AND INLET PLENUM CHECKED. ALL GCU'S CHECK OK. REMOVED AND REPLACED LEFT ENGINE IDG PER MM 24. OPS AND LEAK CHECK GOOD. REMOVED PLACARD 24-1 AUTH NR 10-466DC-B. REMOVED MIC SHEET. (M)

Part: LIGHT — DEFECTIVE (MID-GALLEY)

SFO - DURING OVERNIGHT CHECK, MID-GALLEY RIGHT FORWARD FLOOR EMERGENCY LIGHT INOPERATIVE. REPLACED MID-GALLEY RIGHT FORWARD FLOOR EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: IDG — INOPERATIVE (LT ENGINE)

JFK - LEFT IDG INOP PER MEL 29-1, ENT IN MIC SHEET. ACCOMP BITE CHECK OF NR 1 ENGINE GCU. NO FAULTS NOTED. RESET GENERATOR FIELD MANUAL RESET. ACCOMP RESET OF IDG PER MM AND FIM FOUND FILL SERVICE PORT ON IDG LEAKING. REPLACED FILL PORT FITTING. SERVICED IDG AND ACCOMP RUN UP OF ENG. ISOLATED NR 1 GENERATOR ALL CHECKED NORMAL. NO LEAKS FOUND. ACCOMP BITE OF NR 1 GENERATOR GCU NO FAULTS NOTED. CLEARED MEL 29-1 AUTH 8-117DC-B. CLEARED MIC SHEET. OK FOR SVC. TECH SVCS ADVISED. (M)

Part: LIGHT — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT AT LEFT FORWARD CROSS AISLE INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT ASSEMBLY AT LEFT FORWARD CROSS AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 31HJ INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 31HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 31H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 31H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 23H FOUND INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AND TWO PINS AT PASSENGER SEAT 23H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: HOUSING — DEFECTIVE (CABIN)

ORD - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 33H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT HOUSING AT PAX SEAT 33H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOOR BEAM — CORRODED (BS 325)

FOUND FLOOR BEAM CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND FILLED BLENDED AREAS. FABRICATED AND INSTALLED REPAIR STRAP USING .050 INCH 301.5 HARD STAINLESS STEEL. PRIMED REPAIR STRAP AND FLOOR BEAM APPROVED BY ENGINEERING PER MRB 767-1081. (M)

Part: FLOOR BEAM — CORRODED (BS 347)

AFW - FOUND CORROSION IN THE VERTICAL FLANGE OF THE FLOOR BEAM. ALODINED ALUMINUM SURFACES. FABRICATED, INSTALLED AND PRIMED REPAIR PARTS. ACCOMPLISHED AND APPROVED BY ENGINEERING PER MRB 767-1084

Part: FLOOR BEAM — CORRODED (BS 347)

AFW - FOUND FLOOR BEAM CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND FILLED BLENDED AREAS. FABRICATED, PRIMED AND INSTALLED REPAIR STRAP USING .063 INCH 7095T6 ALUMINUM. APPROVED BY ENGINEERING AND INSTALLED PER MRB 767-1082. (M)

Part: SKIN — CORRODED (CTR WING)

AFW - FOUND UPPER SKIN CORRODED. AFTER BLENDING, FOUND BEYOND LIMITS OF SRM 57-10-01 FIG 101, SQUARE NOTE A. PEENED BLENDED AREAS AND REFINISHED. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1085. (M)

Part: EEL CONNECTOR — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE BETWEEN ROWS 31 AND 37 ON THE RT SIDE. REPAIRED CONNECTOR ON EMERGENCY EXIT FLOOR PATH LIGHTS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: EEL MODULE — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT RIGHT AISLE FROM PASSENGER SEAT ROW 31 AFT INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT CONTROL MODULE FOR RIGHT AISLE AFT CABIN AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTOR — NEEDED SECURED (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT AT PAX SEAT ROW 35B INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT PAX SEAT ROW 35B. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z)