N816AL

Part: PITOT TUBE — OBSTRUCTED (PITOT/STATIC SYS) · airframe 45,158 hrs · 69,362 cycles

FLIGHT 940 HNL-KOA. AFTER TAKEOFF, CREW NOTED THE LOSS OF FIRST OFFICER'S AIRSPEED INDICATION AND THE ILLUMINATION OF THE DOOR ANNUNCIATOR LIGHT. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED DEBRIS FROM THE FIRST OFFICER'S PITOT TUBE AND RESET THE MAIN ENTRY DOOR THEN COMPLETED THE APPROPRIATE OPERATIONAL CHECKS. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SPEED SWITCH — FAILED (APU)

FLIGHT 922 HNL OGG- APU OVER-SPEED INDICATION ILLUMINATED AND THE APU AUTO SHUT-DOWN. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE 3- SPEED SWITCH; OPS CHECKED NORMAL AND RETURNED THE AIRCRAFT TO SERVICE.

Part: SENSOR — FAILED (AOA SYSTEM) · airframe 43,174 hrs · 64,796 cycles

NON-ETOPS CARGO FLIGHT 913, HNL-LIH: AFTER TAKEOFF, THE STICK-SHAKER ENGAGED AND REMAINED ON UNTIL LANDING. RETURNED TO HNL. REMOVED AND REPLACED AOA SENSOR VANE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LINE — OBSTRUCTED (PT2 SENSE)

FLT 840, NR 2 ENGINE PUTTING OUT LESS POWER THAN THE NR 1 ENGINE AT 1.89 EPR. SUSPECT NR 2 PT2 PROBE. REMOVED DEBRIS FROM THE PT2 SENSE TUBE BETWEEN THE ENGINE AND TRANSDUCER. ENGINE RUN-UP AND EPR CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: PUMP — FAILED (NR 2 ENGINE) · airframe 42,237 hrs · 62,633 cycles

HYDRAULIC SYSTEM FAILED. TURNED TO HNL. REMOVE AND REPLACE NR 2 ENGINE HYDRAULIC PUMP IAW AMM 29-11-32. LEAK AND OPS CHECK GOOD. REMOVE AND REPLACE NR 1 AND NR 2 ENGINE HYDRAULIC PUMP CASE DRAIN FILTERS. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR FRAME — CRACKED (FUSELAGE)

REMOVED DAMAGED INBOARD DORR FRAME AREA, VERIFIED CRACK FREE USING HFEC. FABRICATED AN ANGLE DOUBLER FROM .063 INCH 2024-T3 CLAD MATERIAL. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED ANGLED DOUBLER PER FIGURE B. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IAW ECO 1763, DEVIATION A. (M)

Part: SKIN — CORRODED (FUSELAGE)

REMOVED DAMAGED AREA, VERIFIED CRACK FREE USING HFEC. FABRICATED REPAIR DOUBLER FROM 2024-T3. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED DOUBLER PER FIGURE 1. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IAW ECO 3360. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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

Part: INDICATOR — FAULTY (COCKPIT)

PRIOR TO TAXI, THE CREW NOTICED A STRONG SMELL OF ELECTRIC FUMES FOLLOWED BY SMOKE IN COCKPIT. THE AIRCRAFT WAS SECURED FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE RADAR TRANSCEIVER AND RADAR INDICATOR. OPERATIONAL CHECK OF THE RADAR SYSTEM WAS GOOD AND THE AIRCRAFT RETURNED TO SERVICE. THE AVIONICS SHOP FOUND THE BURNING SMELL ORIGINATING FOR THE RADAR INDICATOR. THE UNIT WAS TAGGED FOR REPAIR BY AN OUTSIDE VENDOR. (M)

Part: LINE — CONTAMINATED (EPR SYSTEM)

ON TAKEOFF, THE NR 2 ENGINE WAS AT W.01 EPR, N1-80 PERCENT, EGT-400 DEGREES C, N2-82 PERCENT WITH FUEL FLOW AT 4000 LBS. THE AIRCRAFT RETURNED AND LANDED, WITH NOT FURTHER INCIDENT. MAINTENANCE REMOVED DEBRIS (BUGS) FROM THE NOSE DOME AND CLEARED THE LINES FOR THE EPR SYSTEM. GROUND OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RELIEF VALVE — DIRTY (CABIN)

AT THE TOP OF CLIMB WHEN THE THRUST LEVERS WERE BROUGHT BACK TO IDLE THE NR 2 ENGINE MADE A LOUD BANG LIKE A COMPRESSOR STALL. THE AIRCRAFT CONTINUED THE APPROACH AND LANDED UNEVENTFULLY. REPLACED THE SAFETY RELIEF VALVE. GROUND OPS CHECKED WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE.

Part: BLEED VALVE — MALFUNCTIONED (NR 2 ENGINE)

THE NR 2 ENGINE COMPRESSOR STALLED WHEN THE THRUST LEVERS WERE BROUGHT BACK TO IDLE AT TOP OF DECENT. THE AIRCRAFT CONTINUED THE APPROACH AND LANDED UNEVENTFULLY. MAINTENANCE REPLACED THE PRESSURE RATIO BLEED CONTROL VALVE (PRBC). GROUND OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED LEFT OVERWING IDENT EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: GUIDE — OUT OF ADJUST (PAX DOOR)

FLT 46 - HNL-ITO - FORWARD ENTRY DOOR LIGHT CAME ON DURING THE TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE ADJUSTED THE ROLLER GUIDE SERRATED PLATES AND GUIDE ARM. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRINGER — CRACKED (FUSELAGE)

FOUND CRACKES ON STRINGER 6L AND 7L FORWARD LAV SIDEWALL AREA. TRIMMED OUT DAMAGED PORTIONS OF INTERCOSTAL IAW SRM 51-40-3 FIGURE 1. VERIFIED NO FURTHER CRACKS USING HFEC METHODS AROUND THE TRIMMED OUT AREA. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-30-2. AIRCRAFT RETURNED TO SERVICE. (M)

Part: KEELBEAM — CORRODED (FUSELAGE)

FOUND CORROSION ON THE KEEL BEAM ON RIGHT LOWER FLANGE IN RIGHT AC BAY AT STATION 557 TO STATION 567, STATION 584 AND STATION 608. BLENDOUT THE CORROSION THEN FLAT PEENED IAW SOPM CHAPTER 20-10-03. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S-10R AND S14R ON WINDOW NR 26 RIGHT UPPER AFT HOLES NR 9 AND NR 10. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLER 1 AND DOUBLER FROM .063 INCH THICK 2024-T3. FABRICATED FILLER 2 AND TRIPLER FROM .050 INCH THICK 2024-T3 MATERIAL IAW FIGURES 1, 2, 3 AND 4. INSTALLED REPAIR PARTS SB 737-53A1176R6 FOR S10 AND S14 IAW ECO 3250 DEVIATION J. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S-10R BS 867 PLUS 10 ON WINDOW NR 29 RIGHT UPPER AFT HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLER 1 FROM .032 INCH THICK 2024-T3 AND DOUBLER FROM .063 INCH THICK 2024-T3. FABRICATED FILLER 2 AND TRIPLER FROM .050 INCH THICK 2024-T3 MATERIAL IAW FIGURES 1, 2 AND 3. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION K. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S10L BS 827 PLUS 10 ON WINDOW NR 24 LEFT UPPER AFT HOLES NR 8 AND NR 9. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLERS, DOUBLER AND TRIPLER. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION E. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRINGER — DAMAGED (FUSELAGE)

DAMAGED STRINGER BETWEEN FS 1040 AND FS 1064 STRINGER 27L. REMOVED DAMAGED SECTION IAW SRM 51-40-3 FIGURE 1. FABRICATED REPAIR DOUBLER USING .040 INCH THICK 2024 T3 IAW SRM 51-20-1 PAGES 10A TO 22. PROTECTED MATERIAL USING AN IRIDITE SOLUTION APPLICATION IAW SRM 51-20-2 PAGE 7. PRIMED AND INSTALLED REPAIR PARTS IAW SRM 51-40-3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

IDENTIFIED CORROSION ON FLOOR SUPPORT DIAGONAL LEFT BETWEEN STATION 1006 AND STATION 1016 LBL 5. REMOVED CORROSION IAW SRM 53-10-1 DETAIL I, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SPAR — CORRODED (VERTICAL STAB)

FOUND CORROSION ON LEFT REAR SPAR CHORD 46 INCHES UP FROM VERTICAL STABILIZER FIN BETWEEN STATION 99.5 AND 108.7 ATTACH LUG. BLENDED OUT THE CORROSION AND INSTALLED TAPERED FILLERS. REPAIR ACCOMPLISHED IAW ECO 2509. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S14L BS 727 PLUS 10 ON WINDOW NR 20 LEFT LOWER FORWARD HOLE NR 9. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLERS, QUADRUPLER, DOUBLER AND TRIPLER IAW B 737-53A1177. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION F-R1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

FOUND CORROSION ON THE EXISTING UPPER FLANGE FLOORBEAM REPAIR AT STATION 1016, WL 208 BBI 0 TO LBL 15. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-9 FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATION ON WINDOW NR 8 RIGHT UPPER FORWARD CORNER HOLE NR 8 AND NR 9. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLER 1 AND DOUBLER FROM .032 INCH THICK 2024-T3. FABRICATED FILLER 2 AND TRIPLER FROM .050 INCH THICK 2024-T3 MATERIAL IAW FIGURES 1, 2, 3 AND 4. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION D. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

PEFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S-14R BS 420 ONWINDOW NR 4 RIGHT LOWER AFT CORNER HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLER 1 AND DOUBLER FROM .032 INCH THICK 2024-T3. FABRICATED FILLER 2 AND TRIPLER FROM .050 INCH THICK 2024-T3 MATERIAL IAW FIGURES 1, 2, 3, AND 4. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION G. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (WINDOW BELT)

PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS BETWEEN S10L BS 767 PLUS 10 AND BS 827 PLUS 10 ON WINDOW NR 26 LEFT UPPER AFT HOLES NR 10. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLERS TO SUIT THE AREA OF SKIN/DOUBLER TRIMMED. FABRICATED A DOUBLER AND TRIPLER IAW SB 737-53A1177. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION E. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S10R AND S14R ON WINDOW NR 24 RT UPPER AFT HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLERS, DOUBLER AND TRIPLER. INSTALLED REPAIR PARTS SB 737-53A1176R6 AND S10 AND S14 IAW ECO 3250 DEVIATION J. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON WINDOW NR 6 RIGHT UPPER FORWARD CORNER HOLE NR 9. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLER 1 AND DOUBLER FROM .032 INCH THICK 2024-T3. FABRICATED FILLER 2 AND TRIPLER FROM .050 INCH THICK 2024-T3 MATERIAL IAW FIGURES 1, 2, 3 AND 4. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION D. AIRCRAFT RETURNED TO SERVICE. (M)

Part: RIB — CRACKED (HORIZONTAL STAB)

FOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE HAS CRACKS ON VARIOUS SUPPORT RIBS LISTED FROM INBOARD TO OUTBOARD NR 2, 3, 4, 5, 6, 7, AND 8. CUT AND REMOVED PORTIONS OF FORMED SECTIONS. FABRICATED REPAIR PARTS FROM .040 AND .050 INCH THICK 2024 T3. ASSEMBLED THE REPAIR PARTS AND DRILLED HOLES, REMOVED ALL SHARP EDGES TO .015 R TO .030 R. APPLIED ALODINED COATING AND PRIMER. INSTALLED REPAIR PARTS IAW SRM 51-40-3 FIGURE 1 SHEET 1-6 AND SRM 51-30-2 PAGE 2. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S10R ON WINDOW NR 26 RIGHT LOWER FORWARD HOLE NR 10. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREA. FABRICATED FILLER 1 AND DOUBLER FROM .063 INCH THICK 2024-T3. FABRICATED FILLER 2 AND TRIPLER FROM .050 INCH THICK 2024-T3 MATERIAL IAW FIGURES 1, 2, 3, AND 4. INSTALLED REPAIR PARTS SB 737-53A1176R6 FOR S10 AND S14 IAW ECO 3250 DEVIATION J. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SPAR — CORRODED (VERTICAL STAB)

FOUND CORROSION ON LEFT REAR SPAR CHORD 6 INCHES UP FROM VERTICAL STABILIZER ATTACH LUG. BLENDED OUT THE CORROSION AND INSTALLED TAPERED FILLERS. REPAIR ACCOMPLISHED IAW ECO 2509. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS BETWEEN S10L BS 767 PLUS 10 AND BS 827 PLUS 10 ON WINDOW NR 25 LEFT UPPER AFT HOLES NR 10. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLERS, DOUBLER AND TRIPLER. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION E. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S14R BS 360 PLUS 10 ON WINDOW NR 1 RIGHT UPPER FORWARD CORNER HOLE NR 8 AND NR 9. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLERS AND DOUBLERS. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION D. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON WINDOW NR 5 RIGHT UPPER FORWARD CORNER HOLE NR 9. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLER 1 AND DOUBLER FROM .032 INCH THICK 2024-T3. FABRICATED FILLER 2 AND TRIPLER FROM .050 INCH THICK 2024-T3 MATERIAL IAW FIGURES 1, 2, 3 AND 4. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION D. AIRCRAFT RETURNED TO SERVICE. (M)

Part: KEELBEAM — CORRODED (FUSELAGE)

FOUND CORROSION ON THE KEEL BEAM LOWER CHORD. CONFIRMED CORROSION REMOVED AND NO EVIDENCE OF CRACKS USING HFEC METHOD. REPAIR COMPLETED IAW ECO 3269. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON WINDOW NR 10 RT AT BS 500B PLUS 10 UPPER FORWARD CORNER HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLERS AND DOUBLERS. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION G. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S14R BS 360 PLUS 10, BS 4200 PLUS 10 AND BS 500 PLUS 10 ON WINDOW NR 1 RIGHT LOWER AFT CORNER. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLERS AND DOUBLERS. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION G. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S14R BS 360 PLUS 10 ON WINDOW NR 2 RIGHT UPPER FORWARD CORNER HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLERS AND DOUBLERS. INSTALLED REPAIR PARTS IAW ECO 3250 DEVIATION D. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BULKHEAD — CORRODED (FUSELAGE)

REMOVED CORROSION AT 1016 SKIN BULKHEAD AND ATTACHING FRAME AFT SIDE OF BULKHEAD BETWEEN LBL 5 TO RBL 5 IAW SRM 53-10-1 FIGURE 1 DETAIL 16. CUT OUT ACCESS HOLE AFT OF BULKHEAD PER DRAWING 65C28106. DOUBLER AND FILLER COMPLETED IAW DRAWING 65C28106. CUT OUT DAMAGED PORTION OF WEB AT BULKHEAD 1016 BETWEEN STRINGER 26L AND 26R COMPLETED IAW SB 737-53A1075. ACCESS HOLE FILLER AND DOUBLER INSTALLATION COMPLETED IAW SRM 51-30-2 PAGE 2 PARAGRAPH 4 ITEM A-E. COMPLETED INSTALLATION OF RADIAL STIFFENERS, SPLICE AND WEB REPAIR IAW B737 SB 737-53A1075. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: CIRCUIT BREAKER (P6 PANEL)

FLT 242 - LIH-OGG - THE CREW NOTICED A STRONG ELECTRICAL SMELL COMING FROM THE CENTER OF THE CABIN DURING DESCENT. SMELL DISSIPATED AFTER LANDING. MAUI MAINTENANCE PERSONNEL INSPECTED AND RELEASED THE AIRCRAFT WHEN NO EVIDENCE OF ELECTRICAL FUMES OR ORIGIN COULD BE LOCATED. AGAIN EXPERIENCED AN ELECTRICAL ODOR THAT WAS CONCENTRATED IN THE FORWARD CABIN. HNL MAINTENANCE REPLACED THE NR 3 TR RECTIFIER AND RELEASED THE AIRCRAFT FOR FLIGHT. AFTER PUSHBACK AND STARTING BOTH ENGINES, THE CREW HAD VISIBLE SMOKE IN THE CABIN. THE CREW EXECUTED THE CHECKLIST ON PAGE 4-2 IN THE QRH, SHUTDOWN BOTH ENGINES AND HAD THE AIRCRAFT TOWED BACK TO THE GATE. REMOVED AND REPLACED THE NR 3 TRANSFORMER RECTIFIER (2X), EQUIPMEN

Part: BATTERY PACK — INOPERATIVE (PAX CABIN)

REPLACED AFT SERVICE DOOR IDENT POWER PACK DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (PAX CABIN)

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

Part: TURBINE — SEIZED (RT AC PACK)

HNL - WHILE ON THE GROUND AT GATE 51 WITH APU AND ONE PACK OPERATING (RIGHT), THE CAPTAIN REPORTED SMOKE IN THE COCKPIT AND CABIN. THE AIRCRAFT WAS EVACUATED AND CRASH CREW CALLED. NOTE THAT THE LEFT PACK WAS ON DEACTIVATED FOR MEL 26-12 AND THE RIGHT PACK WAS OPERATING. REMOVED AND REPLACED THE ACM, RIGHT PACK TEMP SWITCH AND WATER SEPARATOR. OPS LEAK AND OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SWITCH — FAILED (RT AC PACK)

HNL - WHILE ON THE GROUND AT GATE 51 WITH APU AND ONE PACK OPERATING (RIGHT), THE CAPTAIN REPORTED SMOKE IN THE COCKPIT AND CABIN. THE AIRCRAFT WAS EVACUATED AND CRASH CREW CALLED. NOTE THAT THE LEFT PACK WAS ON DEACTIVATED FOR MEL 26-12 AND THE RIGHT PACK WAS OPERATING. REMOVED AND REPLACED THE ACM, RIGHT PACK TEMP SWITCH AND WATER SEPARATOR. OPS LEAK AND OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. REF TSAA01080. (M)

Part: GYRO — MALFUNCTIONED (E/E BAY)

FLT 96 - HNL-KOA - WHILE CLIMBING THROUGH 6000 FEET, FLIGHT CREW REPORTED A PROBLEM WITH THE FIRST OFFICER'S ADI TO MAINTENANCE CONTROL. MAINTENANCE CONTROL ADVISED THE CREW TO RETURN TO HNL FOR REPAIRS. LANDING WAS ACCOMPLISHED WITH NO FURTHER PROBLEMS. MAINTENANCE REPLACED THE F/O'S ADI AND THE NR 2 VERTICAL GYRO. GROUND OPS CHECK OF THE ATTITUDE SYSTEM TESTED GOOD. AIRCRAFT RETURNED TO SERVICE. REF TSAA0134064. (M)

Part: ADI — MALFUNCTIONED (COCKPIT)

FLT 96 - HNL-KOA - WHILE CLIMBING THROUGH 6000 FEET, FLIGHT CREW REPORTED A PROBLEM WITH THE FIRST OFFICER'S ADI TO MAINTENANCE CONTROL. MAINTENANCE CONTROL ADVISED THE CREW TO RETURN TO HNL FOR REPAIRS. LANDING WAS ACCOMPLISHED WITH NO FURTHER PROBLEMS. MAINTENANCE REPLACED THE F/O'S ADI AND THE NR 2 VERTICAL GYRO. GROUND OPS CHECK OF THE ATTITUDE SYSTEM TESTED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 5 AND NR 6 EMERGENCY EXIT BATTERY PACKS DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LANDING GEAR — MALFUNCTIONED (NLG)

FLT 275 - OGG-HNL - AFTER TAKEOFF AND RAISING THE LANDING GEAR, NOSE WHEEL RED WARNING LIGHT REMAINED ON. CYCLED THE LANDING GEAR, LIGHT WENT OUT. ETOPS AIRCRAFT ON A NON-ETOPS FLIGHT. INSPECTED NOSE LANDING GEAR DOWN AND UPLOCK SENSORS. ADJUSTED LEFT AND RIGHT DOOR ROD ENDS AND DOOR STOPS. THE NOSE LANDING GEAR OPERATIONAL CHECKED OK PER BOEING MM 32-61-41. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

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

Part: BATTERY PACK — INOPERATIVE (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED 4 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOP. OP CK OK.A/C RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED 6 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOP. OP CK OK.A/C RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY POWER PACK DUE TO INOPERATIVE. OP CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (PAX CABIN)

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

Part: BATTERY PACK — INOPERATIVE (CABIN)

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

Part: BATTERY PACK — INOPERATIVE (CABIN)

REPLACED EMERGENCY FLOOR LIGHT BATTERY PACKS IN POSITION 5, DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED EMERGENCY FLOOR LIGHT BATTERY PACKS IN POSITIONS 1-6 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 TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — DAMAGE (RT TE FOREFLAP)

FOREFLAP ON RIGHT WING ABOVE BEARING TRACK DAMAGED. REPAIRED PYLON SKIN PER ECO 3025. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 2 AND NR 6 FLOOR EMERGENCY LIGHT BATTERY PACK 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 TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 4 AND NR 6 FLOOR PROXIMITY LIGHT BATTERY PACK ASSY DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 3 AND NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 2 FLOOR EMERGENCY LIGHT BATTERY PACK FOR LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED AFT CONTROL MODUEL BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY — DISCHARGED (CABIN)

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

Part: BATTERY — DISCHARGED (CABIN)

REPLACED BATTERY PACK IN POSITION 3 FLOOR PROXIMITY LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

REPLACED FORWARD PASSENGER DOOR EXIT IDENTIFIER BATTERY PACK FOR BEING TOO LOW. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

REPLACED EMERGENCY FLOOR LIGHT BATTERY PACK FOR POSITIONS 1 AND 2 DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY FLOOR LIGHT NR 3 AND NR 6 INOPERATIVE. REPLACED BATTERY PACKS. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

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

Part: BATTERY — DISCHARGED (CABIN)

NR 5 SEAT EMERGENCY LIGHT ASSEMBLY BATTERY INOPERATIVE. REPLACED BATTERY PACK, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (EMERGENCY EXIT)

REPLACED THE EMERGENCY EXIT WALKWAY LIGHT BATTERY POWER SUPPLY. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED NR 1 POSITION FLOOR PROX LIGHT ASSY DUE TO INOP. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

REPLACED FLOOR EMERGENCY LIGHT BATTERIES. SYSTEM OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (NR 2 POS)

REPLACED NR 2 POSITION PROXIMITY FLOOR LIGHT BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 2 POSITION EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 1 POSITION EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED FORWARD ENTRY DOOR EMERGENCY EXIT IDENTIFIER BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED FORWARD ENTRY DOOR EMERGENCY EXIT IDENTIFIER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 3 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK ASSY DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 4 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK ASSY DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: SIGN — INOPERATIVE (CABIN)

REPLACED FORWARD SERVICE DOOR EMERGENCY EXIT IDENTIFIER DUE TO BEING INOP. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED NR 1 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY PACK DUE TO BEING INOP. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED NR 4 POSITION EMERGENCY FLOOR LIGHT ASSY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED THE NR 1 POSITION EMERGENCY LIGHT BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 4 POSITION EMERGENCY LIGHT BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FORWARD ENTRY EXIT IDENTIFIER INOP ON TEST. REPLACED EXIT IDENTIFIER. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

REPALCED NR 2 SEAT EMERGENCY LIGHT BATTERY PACKS DUE TO UNIT WILL NOT TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 31,618.2 HOURS. TAC: 38,510. (X)

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED NR 1 SEAT EMERGENCY LIGHT BATTERY PACKS DUE TO UNIT WILL NOT TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 31,618.2 HOURS. TAC: 38,510. (X)

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED NR 3 SEAT EMERGENCY LIGHT BATTERY PACKS DUE TO UNIT WILL NOT TEST. AIRCRAFT RETURNED TO SERVICE. TAT: 31,618.2 HOURS. TAC: 38,510. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 3 AND NR 5 SEAT EMERGENCY LIGHT BATTERY PACKS DUE TO UNIT WILL NOT TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED NR 4 SEAT EMERGENCY LIGHT BATTERY PACKS DUE TO UNIT WILL NOT TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 5 POSITION EMERGENCY LIGHT BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 3 POSITION EMERGENCY LIGHT BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED NR 4 SEAT EMERGENCY LIGHT ASSEMBLY DUE TO NOT RECEIVING TRANSMITTING SIGNAL. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 6 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO CONDITION LED'S INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 1 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO CONDITION LED'S INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 2 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO CONDITION LED'S INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 3 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO CONDITION LED'S INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 4 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO CONDITION LED'S INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (BS 947)

LAP JOINT CORRODING AT STR 24L AND BS 947, ALSO SHOWS SIGNS OF BULGING. FORWARD OF POTABLE WATER ACCESS PANEL CUT-OUT. REPAIRED PER ECO 2907. AIRCRAFT RETURNED TO SERVICE. TAT: 31,369.6 HRS. TAC: 37,949. (X)

Part: SKIN — CRACKED (BS 377)

MAIN CARGO DOOR LOWER FRAME AT NR 2 LATCH CUT-OUT HAS A CRACK AT FORWARD OUTBOARD CORNER CUT-OUT BS 377. HFEC CONFIRMED. REPAIRED PER ECO 2912. AIRCRAFT RETURNED TO SERVICE. TAT: 31,369.6 HRS. TAC: 37,949. (X)

Part: LIGHT — INOPERATIVE (CABIN)

LEFT FORWARD PASSENGER DOOR EXIT IDENTIFIER 'ALL'S WELL' LIGHT INOP. REPLACED IDENTIFIER. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

FORWARD SERVICE DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOP. REPLACED BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FRAME — CRACKED (BS 325)

BODY FRAME CRACKED AT BS 325 ABOVE STR 27L (ACCESS FOR E/E COMPARTMENT UNDER PITCH CONTROL CHANNEL BOX). REPAIRED PER SRM 51-40-3. AIRCRAFT RETURNED TO SERVICE. TAT: 31,369.6 HRS. TAC: 37,949. (X)

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED AFT PASSENGER DOOR EMERGENCY EXIT LIGHT DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 2 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 5 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — DAMAGED (BS 318/322/328)

THREE HOLES IN LEFT SIDE OF AIRCRAFT BELOW FORWARD ENTRY DOOR CAUSED BY RUNAWAY BAGGAGE CART. LOCATIONS ARE BS 328 BETWEEN STRINGER 19L/20L, BS 322 BETWEEN STRINGER 21L/22L, AND BS 318 AT STRINGER 23L. REPAIRED DAMAGE PER ECO 2897. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHT INOP. REPLACED BATTERY PACK OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND POSITION NR 6 EMERGENCY FLOOR LIGHT INOP. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED LIGHT ASSY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 30,719:11 HOURS. TAC: 36,568. (X)

Part: HYDRAULIC LINE — FAILED (MLG)

FLT - 283 - PILOT REPORT ON TAXI OUT, AIRCRAFT LOST 'A' HYDRAULICS. UPON RETURN, REPLACED THE HYDRAULIC PRESSURE LINE ON THE MAIN LANDING GEAR ACTUATOR. SERVICED HYDRAULICS TO FULL AND CYCLED GEAR SEVERAL TIMES WITH GEAR PINS INSTALLED, NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. TAT: 30,711:25 HOURS. TAC: 36,561. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND POSITION NR 5 EMERGENCY FLOOR LIGHT ALL WELL LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 30,453:50 HOURS. TAC: 35,976. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND POSITION NR 6 EMERGENCY FLOOR LIGHT ALL WELL LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 30,453:50 HOURS. TAC: 35,976. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND POSITION NR 3 EMERGENCY FLOOR LGIHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 30,406:02 HOURS. TAC: 35,874. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 30,406:02 HOURS. TAC: 35,874. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK FOUND POSITION NR 5 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 30,406:01 HOURS. TAC: 35,874. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND POSITION NR 6 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 30,406:01 HOURS. TAC: 35,874. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 30,406:02 HOURS. TAC: 35,874. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND NR 1 POSITION EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 30,288:16 HOURS. TAC: 35,598. (X)

Part: CONTROLLER — MALFUNCTIONED (E/E COMPARTMENT)

HNL/OGG - FLT 114 - PILOT REPORT. AFTER TAKEOFF, THE CABIN PRESSURIZATION STARTED FLUCTUATING. THE CABIN CLIMB INDICATOR INDICATED +2,000 FEET BACK AND FORTH, THEN SWITCHED TO STANDBY, AND CABIN CLIMB CONTINUED TO FLUCTUATE BETWEEN +1,000 FEET AND -1,000 FEET. IN MANUAL, UNABLE TO MOVE OUTFLOW VALVE FROM CLOSED INDICATION IN EITHER AC OR DC. REPLACED PRESSURE CONTROLLER. SECURED CANNON PLUG ON EQUIPMENT RACK. GROUND CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND NR 1 POSITION EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 30,236:07 HOURS. TAC: 35,478. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND POSITION NR 6 EMERGENCY FLOOR LIGHTS UNABLE TO TEST. REPLACED BATTERY PACK. OPS CEHCK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

DURING OVERNIGHT CHECK, ADJUSTED RECEIVER SENSITIVITY ON ROWS 2 AND 6 FLOOR PROXIMITY LIGHT ASSEMBLIES AND REPLACED BATTERY FOR ROW 4 FLOOR PROXIMITY LIGHT ASSEMBLY DUE TO INOPERABLE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 29,875:20 HOURS. TAC: 34,685. (X)

Part: BATTERY — DISCHARGED (CABIN)

FLIGHT ATTENDANT REPORTS LIGHT WAS ON THEN WENT DIM, NR 2 FLOOR PROX AISLE LIGHT. REPLACED BATTERY, 'ON' TEST OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONTROL MODULE — INOPERABLE (CABIN)

DURING OVERNIGHT CHECK, REPLACED AFT INTERVALVE CONTROL MODULE DUE TO INOPERABLE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 29,551:03 HOURS. TAC: 33,970. (X)

Part: LIGHT — INOPERATIVE (CABIN)

DURING OVERNIGHT CHECK, REPLACED ROW 17 EMERGENCY FLOOR PROXIMITY LIGHT ASSY DUE TO INOPERABLE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 29,551:03 HOURS. TAC: 33,970. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING OVERNIGHT CHECK, REPLACED CENTER CONTROL MODULE BATTERY PACK DUE TO NO RESPONSE WHEN TURNED ON. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 29,448:11 HOURS. TAC: 33,737. (X)

Part: FLOOR BEAM — CORROSION (BS 312)

DURING CPC PHASE 1 INSPECTION OF FUSELAGE UPPER LOBE, FOUND MAIN DECK FLOOR BEAM UPPER CHORD CORROSION ON NUTPLATE AT STA 312. REPAIRED PER ECO 2096R3. AIRCRAFT RETURNED TO SERVICE. MATERIAL USED - CHORD - 7075-T6511 EXTRUSION. SPLICE ANGLES - 7075-T6 STOCK. NON-ROUTINE TASK CARD NR 019989. TAT: 29,363:34 HOURS. TAC: 33,549. (X)

Part: FIRE ELEMENT — FAILED (NR 2 ENGINE)

OGG/HNL - FLT 207 - PILOT REPORT, NR 2 FIRE WARNING LIGHT AND BELL ON. ENGINE FIRE/SEVERE DAMAGE CHECK LIST FOLLOWED. FIRED BOTH FIRE EXTINGUISHER BOTTLES. UNEVENTFUL LANDING AND TAXI. REPLACED FIRE DETECTION SENSING ELEMENT IAW MM 26-11-11. OPS CHECK OK PER MM 26-11-0. REPLACED BOTH BOTTLES. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

AFT EXIT EXTERIOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: KEEL BEAM — CORRODED (BS 727)

DURING C-CHECK VISIT, CORROSION FOUND ON LOWER LIP KEEL BEAM RT SIDE FROM TURBO FAN EXHAUST TO BS 727 (NRTC 015492). REPAIRED PER ECO 1943 R5 DEV D. AIRCRAFT RETURNED TO SERVICE. TAT: 28,374.43 HOURS. TAC: 31,279.

Part: STIFFENER — CRACKED (BS 178)

DURING C-CHECK VISIT, CRACK FOUND ON LT STIFFENER BS 178. REPAIRED PER ECO 2518 R1 DEV B. AIRCRAFT RETURNED TO SERVICE. TAT: 28,374:43 HOURS. TAC: 31,279. (X)

Part: RELEASE MECH — LACK OF LUBE (NLG)

DURING C-CHECK VISIT, EXTENSION AND RETRACTION TEST WAS PERFORMED ON NOSE AND MAIN LANDING GEAR SYSTEM. NOSE GEAR DID NOT EXTEND WHEN MANUALLY ACTIVATED. MANUAL EXTENSION RELEASE MECHANISM WAS LUBED AND THE NOSE LANDING GEAR DOOR MECHANISM BELLCRANK BUSHING WAS REPLACED. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: TRUNNION — CORROSION (NLG)

DURING C-CHECK VISIT, FOUND CORROSION ON NLG TRUNNION BOSS HOLE BORE. REPAIRED PER ECO 2383 R2. AIRCRAFT RETURNED TO SERVICE. (M)