N827AL

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

FLIGHT 270 (HNL-KOA) LIGHTNING STRIKE DURING CLIMB-OUT AT 10,000’. NO MALFUNCTIONS. MTX ACTION COMPLIED WITH M-118 LIGHTNING STRIKE INSPECTION. REMOVED AND REPLACED DAMAGED RIVETS ON STATION 188R AND STATIC WICK.

Part: CONNECTOR — DEFECTIVE (FIRE DETECTOR)

FLT 71, HNL-OGG - THE NR 2 ENGINE FIRE WARNING LIGHT CAME ON INTERMITTENTLY DURING FLIGHT. DECIDED TO RETURN TO HNL. THE NR 2 ENGINE FIRE WARNING LIGHT CAME ON STEADY AT TOUCHDOWN. ENGINE SHUTDOWN. BOTTLE DISCHARGED. REPLACED THE NR 2 ENGINE FIRE DETECTOR SENSOR CONNECTORS. SYSTEM TEST WITH ENGINE RUN FOUND NORMAL. OK FOR SERVICE. REPLACED THE FORWARD AND AFT POSITION ENGINE FIRE EXTINGUISHER BOTTLES PER MM 26-21-11. AIRCRAFT RETURNED TO SERVICE.

Part: BYPASS SWITCH — FAILED (NR 1 ENGINE) · airframe 33,585 hrs · 57,562 cycles

NON-ETOPS FLIGHT 67, OGG-HNL: NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. SHUT-DOWN NR 1 ENGINE IAW QRH. REPLACED NR 1 ENGINE OIL FILTER BYPASS SWITCH IAW AMM 79-35-11. OPS/LEAK CHECK OK, AIRCRAFT RETURNED TO SERVICE.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 33,459 hrs · 57,290 cycles

NON-ETOPS FLIGHT 46, HNL-ITO: OUTER PANE OF WINDOW R1 CRACKED. RETURN TO HNL. REMOVE AND REPLACE WINDOW R1 IAW AMM 56-11-11. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (PAX CABIN)

REPLACED FORWARD SERVICE DOOR IDENT EXIT LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

TRIMMED OUT DAMAGED AREA. HFEC VERIFIED CRACK REMOVED. FABRICATED DOUBLER. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAIR PARTS MAKING A FAYING SEAL AROUND REPAIR. REPAIR COMPLETED IAW ECO 2840R2, DEVIATION C. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

REPLACED NR 1 AND NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (PAX CABIN)

REPLACED AFT ENTRY EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ACCESS DOOR — CORRODED (LT WING FUEL)

REMOVED CORROSION DAMAGE BY BLENDOUT REPAIR PER GUIDANCE IN SRM 57-30-3, FIGURE 5, DETAL III. APPLIED ALODINE AND TWO COATS OF BMS 10-20, TYPE II TO BLENDOUT LOCATIONS. FILLED DEPRESSION WITH BMS 5-26, TYPE II SEALANT TO RESTORE SURFACE TO ORGINAL CONTOUR. REPAIR COMPLETED IAW ECO 2268 WITH DEVIATION A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LEG ASSY — CORRODED (WING)

CUTOUT THE DAMAGED FROM THE VERTICAL LEG. BLENDED OUT REMAINING AREA OF THE CHORD MAINTAINING A GREATER THAN .050 INCH THICKNESS. PERFORMED 10X VISUAL AND HFEC INSPECTION TO VERIFY CRACK AND CORROSION FREE. FLAP PEENED REWORKED SURFACES. FABRICATED REPAIR PARTS 1, 2, 3 AND 4 FROM 2024-0 PER FIGURE 1. APPLIED ALODINE AND TWO COATS OF BMS 10-20, TYPE II PRIMER TO ALL BARE SURFACES. INSTALLED REPAIR PARTS WITH FASTENERS IDENTIFIED. REPAIR COMPLETED IAW ECO 2948 R4. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLANGE — CORRODED (WING)

REMOVED CORROSION DAMAGE BY SMOOTHLY BLENDING REWORK AREA. PERFORMED HFEC INSPECTION TO VERIFY CRACK AND CORROSION FREE. FLAT PEENED REWORKED SURFACE. FABRICATED A FILLER FROM 2024-T3 SIZED TO FIT BLENDOUT AREA AND RESTORE TO ORIGINAL CONTOUR. APPLIED ALODINE AND TWO COATS OF BMS 10-20, TYPE II PRIMER TO BARE SURFACES. WET INSTALLED FILLER AND BMS 5-95 SEALANT ON ALL FRAYING SURFACES. REPAIR COMPLETED IAW ECO 3073. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LEG ASSY — CORRODED (WING)

REMOVED CORROSION DAMAGE BY BLENDING TO A 20 TO 1 RATION. PERFORMED 10X VISUAL AND HFEC INSPECTON TO VERIFY CRACK AND CORROSION FREE. FABRICATED A TAPERED SHIM FROM 2024-T3. FLAT PEENED SURFACE. APPLIED ALODINE AND TWO COATS OF BMS 10-11, TYPE I PRIMER TO BLENDOUT LOCATION. WET INSTALLED 1/32 OVERSIZED HI-LOCKS PROTRUDING HEADS WITH BMS 5-95 SEALANT. REPAIR COMPLETED IAW ECO 2948. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SPAR — CORRODED (LT WING)

FOUND CORROSION ON RIGHT FRONT SPAR LOWER CHORD SURFACE AT WSL 557. CONFIRMED COMPLETE REMOVAL OF CORROSION WITH HFEC INSPECTION. FABRICATED A REPAIR FILLER TO FIT IN THE BLENDOUT AREA. FABRICATED A REPAIR STRAP. REPAIR COMPLETED IAW ECO. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SPAR — CORRODED (LT WING)

FOUND CORROSION ON RIGHT FRONT SPAR LOWER CHORD VERTICAL WEB SURFACE AT WSL 554. CONFIRMED COMPLETE REMOVAL OF CORROSION WITH HFEC INSPECTION. FABRICATED TAPERED FILLERS TO FIT IN THE BLENDOUT AREA. FABRICATED A REPAIR DOUBLER AND REPAIR ANGLE. INSTALLED THE REPAIR FILLERS, ANGLE AND DOUBLER. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IAW ECO. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BEARING — BROKEN (NR 2 ENGINE)

CLIMBING THROUGH 15,000 FEET THE NUMBER 2 ENGINE OIL PRESSURE DROPPED TO 20 PSI AND OIL TEMPERATURE CLIMBED TO 130 DEGREES. THE NUMBER 2 ENGINE WAS SHUTDOWN IAW THE QRH. AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL LANDING. REMOVED AND REPLACED THE NR 2 ACCESSORY GEARBOX ASSEMBLY. FOUND THE OIL PUMP GEARSHAFT BEARING BROKEN. LEAK AND OPERATIONAL CHECKS GOOD. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SPAR — CORRODED (HORIZ STAB)

DURING HEAVY CHECK, FOUND CORROSION ON HORIZONTAL STABILIZER REAR SPAR UPPER CHORD. THE CORROSION WAS TRIMMED OUT PER SRM AND VERIFIED REMOVED USING HFEC METHOD. FABRICATED A EXTERNAL DOUBLER AND REPAIR FILLER TO FIT SKIN CUTOUT. FABRICATED REPAIR ANGLE AND REPAIR FILLER IAW FIGURE 4A-4G. INSTALLED ALL REPAIR PARTS. VERIFIED 8110-3 APPROVAL RECEIVED AND COMPLETED REPAIR IAW ECO 2513. AIRCRAFT RETURNED TO SERVICE. (M)

Part: KEELBEAM — CORRODED (FUSELAGE)

DURING HEAVY CHECK, FOUND CORROSION ON LEFT KEEL BEAM LOWER CHORD AT BS 727 STRINGER 27L. THE CORROSION WAS TRIMMED OUT PER SRM. FABRICATED FILLER AND DOUBLER. INSTALLED REPAIR PARTS USING SRM 51-30-2. VERIFIED APPROVAL RECEIVED AND COMPLETED REPAIR IAW ECO 1972. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (WING)

FOUND CORROSION ON LOWER SKIN SURFACE AT WS 435.5, WS 542, WS 567, WS 514.5, AND WS 461. CONFIRMED COMPLETE REMOVAL OF CORROSION WITH A 10X VISUAL INSPECTION. EVALUATED REMAINING WING SKIN THICKNESS AND FILLED DEPRESSIONS WITH BMS 5-95 SEALANT REFERRING TO SRM 51-20-4 IAW ECO 3091. AIRCRAFT RETURNED TO SERVICE. (M)

Part: KEELBEAM — CORRODED (FUSELAGE)

FOUND CORROSION ON LOWER KEEL BEAM SURFACE AT BS 727. CUT OUT SKIN AREA AS REQUIRED TO ACCESS KEEL BEAM LOWER SURFACE. BLENDOUT KEEL BEAM LOWER CHORD SURFACE CORROSION. FABRICATED A FILLER FROM .71 TO .12 INCH 2024-T3. FABRICATED TWO DOUBLERS FROM .063 AND .080 INCH 2024-T3. ASSEMBLED REPAIR PARTS IAW ECO 1972 FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

FOUND FUSELAGE CRACK AT BS 940 S-21R. TRIMMED OUT DAMAGE AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED, INSTALLED FILLER AND DOUBLER IAW SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: HYDRAULIC LINE — LEAKING (RT MLG)

FLT 62, HNL-OGG, THE HYDRAULIC ANNUNCIATOR CAME ON AFTER TAKEOFF. BOTH 'A' SYSTEM HYDRAULIC LOW PRESSURE LIGHTS ILLUMINATED. THE 'A' SYSTEM QUANTITY READ '0'. DECLARED EMERGENCY AND RETURNED TO HNL FOR AN UNEVENTFUL LANDING. REPLACED THE RIGHT LANDING GEAR ACTUATOR RETURN LINE IAW MM 32-32-11. LEAK CHECK OK. (M)

Part: HARNESS — BURNED (COCKPIT)

FLT - 41 - ITO-HNL - INBOUND FROM HILO, HAD STRONG ELECTRICAL SMOKE SMELL IN COCKPIT AND SOME SMOKE SMELL IN CABIN AROUND ROW 5. DECLARED EMERGENCY. LANDED SAFELY IN HNL. FOUND WINDOW HARNESS AT THE RIGHT SIDE WINDOW BURNED AT THE QUICK DISCONNECT. WINDOW HEAT DEFERRED PER MEL 30-11, CONTROL NR 2428C04. REPAIRED WIRE ON RIGHT SIDE WINDOW HARNESS. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

DURING HEAVY CHECK INSPECTION FOUND A CRACK ON THE AFT LOWER CARGO DOORWAY FRAME. THE CRACK EXTENDS FROM A FASTENER HOLE DOWN INTO A FRAME FLANGE. THE REPAIR INVOLVED TRIMMING OUT THE DAMAGE, PERFORMING A HFEC INSPECTION TO ENSURE THE CRACK AND ANY CORROSION WAS REMOVED. FABRICATED AND INSTALLED A FILLER AND ANGLE. COLD WORK ALUMINUM PARTS COMMON TO THE LAST ROW OF ANGLE PER SRM 51-40-9. INSTALLED COUNTERSUNK REPAIR WASHERS, INSTALLED REPAIR PARTS WITH BMS 5-95 SEALANT BETWEEN FAYING SURFACES, FINISH ALL BARE SURFACES WITH ALODINE AND TWO COATS OF BMS 10-11, TYPE 1 PRIMER IAW 3241. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FWD SERV DOOR)

IDENTIFIED 1.25 INCH SKIN CRACK AT FORWARD SERVICE DOOR LOWER AFT SECTION. (M)

Part: SKIN — CORRODED (RT WING)

DISCOVERED CORROSION AT RIGHT WING LOWER SURFACE WS 581.5, BLENDOUT TO REMOVE ALL CORROSION, OBTAINED A SURFACE OF 125 MICROINCHES RADIUS, CONFIRMED COMPLETE REMOVAL OF CORROSION BY 10 BY GLASS VISUAL INSPECTION, FLAP PEEN REWORKED AREAS PER SOPM 20-10-03, APPLIED ALODINE, PRIMER AND ENAMEL TO ALL EXPOSED SURFACES, IAW ECO 3091R4. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (RT WING)

DISCOVERED CORROSION AT RIGHT WING LOWER SURFACE WS 581.5, BLENDOUT TO REMOVE ALL CORROSION, OBTAINED A SURFACE OF 125 MICROINCHES RADIUS, CONFIRMED COMPLETE REMOVAL OF CORROSION BY 10 BY GLASS VISUAL INSPECTION, FLAP PEEN REWORKED AREAS PER SOPM 20-10-03, APPLIED ALODINE, PRIMER AND ENAMEL TO ALL EXPOSED SURFACES, IAW ECO 3091R4. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (WING)

CORROSION FOUND ON LOWER SKIN SURFACE AT WS 435.5, WS 567, WS 542, WS 514.5, AND WS 461. CONFIRMED COMPLETE REMOVAL OF CORROSION WITH A 10X VISUAL INSPECTION. EVALUATED REMAINING WING SKIN THICKNESS AND FILLED DEPRESSIONS WITH BMS 5-95 SEALANT REFERRING TO SRM 51-20-4 IAW ECO 3091. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (PAX CABIN)

REPLACED NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: TIRE — FAILED (NR 4 MLG)

FLT 66 - HNL-OGG - ON TAKEOFF, REPORTED TIRE BLOWN ON MLG. DECLARED EMERGENCY. RETURNED TO HNL WITHOUT FURTHER INCIDENT. FOUND NR 4 MLG TIRE RECAP SEPARATED. REMOVED AND REPLACED THE NR 4 MAIN WHEEL ASSY IAW FORM M-139. INSTALLATION, SPIN AND SECURITY CHECK VERIFIED. REMOVED AND REPLACED NR 3 MAIN WHEEL ASSY IAW FORM M-139 AS A PRECAUTION. INSTALLATION, SPIN AND SECURITY CHECK VERIFIED. INSPECTED GEAR AREA AND FOUND DAMAGE TO THE CENTER AND OUTER DOOR. REMOVED CENTER, INNER AND OUTER DOOR FOR REPAIR PER CDL. TIRES RETURNED TO VENDOR FOR ANALYSIS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: PRESSURE SWITCH — FAILED (NR 1 ENGINE OIL)

FLT 224 - HNL-OGG - NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED AT APPROXIMATELY 70 KNOTS. TAKEOFF ABORTED. ALL OTHER ENGINE PARAMETERS WERE NORMAL. ALL QRH PROCEDURES REVIEWED. RETURNED TO HNL RAMP. REMOVED AND REPLACED NR 1 ENGINE OIL BYPASS SWITCH. OPS CHECK GOOD PER MM 79-35-0. REMOVED AND REPLACED NR 1 ENGINE OIL BYPASS SWITCH, OPS CHECK GOOD PER MM 79-35-0. REMOVED AND REPLACED THE NR 1 ENGINE MAIN OIL FILTER. OPS LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STOP — OUT OF ADJUST (PASSENGER DOOR)

HNL/OGG - FLT 264 - FORWARD DOOR ENTRY WARNING LIGHT ILLUMINATED MOMENTARILY AFTER TAKEOFF. PRESSURIZATION REMAINED NORMAL. ABORTED TAKEOFF. CHECKED DOOR LEVER AND WARNING EXTINGUISHED. ALL OTHER INDICATIONS WERE NORMAL. AIRCRAFT TAXIED BACK FOR DEPARTURE. NO FURTHER PROBLEMS NOTED. ADJUSTED FORWARD ENTRY DOOR STOPS PER MM 52-11-0. PRESSURIZATION TEST AND GROUND OPS GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — INOPERATIVE (CABIN)

REPLACED POWER PACKS IN FORWARD AND AFT INTERVALVE CONTROL MODULES DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

REPLACED NR 1 AND NR 5 POSITION BATTERY PACK IN FLOOR PROXIMITY LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 1 FLOOR EMERGENCY LIGHT BATTERY ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 3 FLOOR EMERGENCY LIGHT BATTERY ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED NR 5 FLOOR EMERGENCY LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 4 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED NR 2 EMERGENCY FLOOR LIGH TASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 2 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED FORWARD ENTRY DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 2 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 4 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED BATTERY FOR POSITION NR 4 FLOOR PROX LIGHT ASSY DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED BATTERY FOR RIGHT OVERWING EMERGENCY EXIT IDENTIFIER LIGHT ASSY DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED BATTERY FOR FORWARD SERVICE DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSY DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (AFT ENTRY)

REPLACED AFT ENTRY EMERGENCY EXIT IDENTIFIER LIGHT. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED EMERGENCY PATH LIGHTING BATTERY PACK AT NR 1 POSITION. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED EMERGENCY PATH LIGHTING BATTERY PACK AT NR 5 POSITION. OPS CHECKED OK. AIRCRAFT RETURNED SERVICE. (X)

Part: BATTERY PACK — DISCHARAGED (CABIN)

REPLACED EMERGENCY PATH LIGHTING BATTERY PACK AT NR 3 POSITION. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED EMERGENCY PATH LIGHTING BATTERY PACK AT NR 2 POSITION. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED RT OVERWING EMERGENCY EXIT IDENTIFIER LIGHT. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED EMERGENCY PATH LIGHTING BATTERY PACK AT NR 4 POSITION. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED EMERGENCY PATH LIGHTING BATTERY PACK AT NR 6 POSITION. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED RT OVERWING EMERGENCY EXIT IDENTIFIER BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED AFT ENTRY EMERGENCY EXIT IDENTIFIER LIGHT. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED AFT ENTRY EMERGENCY EXIT IDENTIFIER BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X)