N810AL

Part: WHEEL — SEPARATED (MLG) · airframe 48,911 hrs · 58,797 cycles

ON LANDING, CREW HEARD AN UNUSUAL (BUMP) NOISE WITH NORMAL LANDING. TAXI TO GATE WITHOUT FURTHER INCIDENT. CREW FOUND NR 1 MAIN LANDING GEAR WHEEL ASSEMBLY HAD SEPARATED FROM THE AIRCRAFT. MAINTENANCE REMOVED AND REPLACED THE NR 1 MLG BRAKE ASSEMBLY AND THE NR 1 AND NR 2 MLG WHEEL ASSEMBLIES. CONDUCTED HARD LANDING, HIGH DRAG/SIDE LOAD INSPECTIONS. NO EXTERNAL DAMAGE FOUND ON AIRCRAFT. AIRCRAFT RETURNED TO SERVICE.

Part: SPAR — CORRODED (VERTICAL STAB) · airframe 46,586 hrs · 58,071 cycles

VERTICAL STABILIZER RIGHT T/E REAR SPAR CORROSION (3 AREAS).

Part: SPAR — CORRODED (HORIZ STAB) · airframe 46,586 hrs · 58,071 cycles

HORIZONTAL STABILIZER RT REAR SPAR UPPER CHORD CORROSION (3 AREAS).

Part: SKIN PANEL — CRACKED (BS 929 S24L) · airframe 46,213 hrs · 57,252 cycles

A 2 INCH SKIN CRACK AT BS 929 STR 24L. A .04 INSURANCE MADE IAW SRM 53-30-3. RIVET PATTERN LAID OUT AND DRILLED AND MANUFACTURED REPAIR DOUBLER, TRIPLER, AND 2 FILLERS PER SRM 53-30-3 FIG 48 DET XIX. HFEC RIVET HOLES IAW BOEING NDT MANUAL 51-00-00 PT 6. REPAIR COMPLETED.

Part: SPAR — CORRODED (NR 4 SLAT) · airframe 46,195 hrs · 57,212 cycles

CORROSION ON UPPER & LOWER SURFACE OF FRONT SPAR LOWER CORD BETWEEN FSS 297 & FSS-306 AT SLAT NR 4. BLENDED INBOARD - OUTBOARD DIRECTION 10:1 DEPTH TO BLEND RATION. SHOT/FLAP PEEN BLENDED ARE PER SRM. FABRICATED SOLID FILLERS TO REPLACE REMOVED MATERIAL. FORM FAA 8100-9 RECEIVED.

Part: FAN — DEFECTIVE

ON APPROACH THE PILOT SMELLED SMOKE AND AFTER LANDING THE SMELL GREW STRONGER. AIRPLANE TAXIED BACK TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED GASPER FAN. OPS CHECK GOOD, NO HELP. THE CABIN AUGMENTATION FAN WAS FOUND TO BE INOP. REMOVED AND REPLACED THE CABIN AUGMENTATION FAN PER AMM 21-22-11. OPS AND LEAK CHECK GOOD. NO SMELL REPORTED. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CRACKED (BS 937, S21L) · airframe 45,976 hrs · 56,732 cycles

A 4 INCH FUSELAGE SKIN CRACK BS 937 AT STRINGER 21L. MAINTENANCE REPAIRED WITH APPROXIMATELY 24 X 20 INCH SKIN PATCH, FABRICATED DOUBLER, TRIPLER, AND STRUCTURAL FILLER NR 5 AND 6 PER SRM 53-30-3, FIG 48, DET XII.

Part: BLEED VALVE — DEFECTIVE (NR 2 ENGINE)

ON TAKE-OFF NR 2 ENGINE COMPRESSOR STALL ON INITIAL RUN-UP FROM IDLE. R & R NR 2 ENG PRBC IAW MM 75-31-11. BLEED VALVE SCHEDULING COMPLETED PER P&W MM 72-00-00. R.I.I. COMPLETED FOR NR 2 ENG PRBC VALVE CHANGE IAW MM 75-31-11. DID NOT FIX OFF IDLE STALL. LUBRICATED 8TH & 13TH STAGE BLEED VALVES ON NR 2 ENG PER 75-30-00. R&R START BLEED CONTROL VALVE OPERATIONAL CHECK NORMAL. BLEED VALVE SCHEDULING COMPLETED OK PER PWA MM 72-00-00. R & R NR 2 ENG PRBC FOR PRECAUTIONARY IAW MM 75-31-11. BLEED VALVE SCHEDULING COMPLETED, OPS & LEAK CHECK OK. RII COMPLETED FOR PRBC CHECK. NO FAULTS NOTED. AIRCRAFT RETUNED TO SERVICE.

Part: BLEED VALVE — DEFECTIVE (NR 2 ENGINE)

RUNNING UP ENGINES FOR TAKE-OFF, GOT STEADY BANGING. RPM BARELY PAST IDLE. FLIGHT ATTENDANTS GUESS THE NR 2 ENGINE. TAKE-OFF ABORTED. R&R PRBC IAW MM 75-31-11 OPS CHECK OK ON NR 2 ENGINE. BLEED VALVE SCHEDULING COMPLETED PER PWA MM 72-00-00. LUBED 8TH AND 13TH STAGE BLEED VALVES ON NR 1 AND 2 ENGINES PER PWA MM 75-30-00. NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — LEAKING (NR 1)

FLT 224 - LIH-HNL - LOW OIL PRESSURE ILGHT ON NR 1 ENGINE ILLUMINATED. OIL PRESSURE DROPPED TO 20 PSI. FOLLOWED QRH AND SHUTDOWN THE NR 1 ENGINE. DECLARED EMERGENCY AND HAD UNEVENTFUL LANDING. REMOVED AND REPLACED THE NR 1 ENGINE PER FORMS M-211 THROUGH M-215. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LINE — FAILED (HYD SYSTEM)

FLT 240 - HNL-OGG - ON GEAR RETRACTION 'A' SYSTEM HYDRAULIC ANNUNCIATOR LIGHT CAME ON. SYSTEM QUANTITY AT 1.5 GALLONS. RETURNED TO HNL. FOUND RIGHT MAIN GEAR UPLOCK ACTUATOR FLEX-LINE RUPTURED. REMOVED AND REPLACED FLEX-LINE. LEAK CHECK OK. SERVICED HYDRAULIC FLUID AS REQUIRED. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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

Part: SKIN — CRACKED (FUSELAGE)

NINE RIVETS ON STRINGER 16R SHOW SIGNS OF STRESS CRACKS EMANATING FROM THE FASTENER HOLES. REMOVED RIVETS, OVERSIZED HOLES BY 1/16, HFEC VERIFIED FASTENER HOLES CRACK FREE. FABRICATED FILLER AND DOUBLER. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAIR PARTS PER SRM 53-30-3, FIGURE 17. REPAIR COMPLETED IAW SRM AND ECO 3340. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED LT OVERWING IDENT LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: STRUCTURE — GOUGED (CARGO DOOR)

CUTOUT DAMAGE, PERFORMED A DETAILED VISUAL AND HFEC INSPECTION OF THE CUTOUT AND ALL LAP SPLICE FASTENERS HOLES IN THE REPAIR AREA, NO DEFECTS NOTED. FABRICATED A DOUBLER, TRIPLER STRUCTURAL FILLER. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — CORRODED (APU BAY)

AUXILIARY POWER UNIT COMPARTMENT CORRODED AT BS 1156 REMOVED DAMAGED SECTION OF FRAME FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER FROM SRM, AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE)

FOUND CRACK ON FUSELAGE SKIN, STRINGER 21L AT BS 985.5. TRIMMED OUT DAMAGED AREA AND VERIFIED USING HFEC METHOD NO DEFECTS NOTED. FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER PER SRM. REPAIR COMPLETED IAW SRM. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CORRODED (LT WING)

FOUND CORROSION ON THE LEFT HAND OUTBOARD WING MAIN BOX UPPER SKIN AT WBL 71.24, STR 5, 7 AND WBL92.5 STR 1, 5. BLENDED OUT CORROSION AT A 10:1 RATIO MINIMUM PER SRM. ULTRASOUND INSPECTED TO ENSURE NO REMAINING CORROSION. HFEC AFFECTED FASTENER HOLE BORE FOR CRACK DETECTION. INSPECTED WING SURFACE USING 10X VISUAL. SHOT PEENED WING SURFACE PER OHM. REPLACED REMOVED FASTENERS WITH .0312 INCH OVERSIZE TENSION HEAD HI-LOKS. INSTALLED FASTENERS WITH BMS 5-95 SEALANT IN TRANSITION FIT HOLES AND REFINISHED PER SRM IAW ECO.

Part: SKIN — WORN (RT WING)

FOUND SKIN WORN THROUGH ON THE RIGHT LEADIN EDGE LOWER WING SKIN SURFACE AT FS 413. CUT OUT DAMAGED LEADING EDGE FILLER AND SKIN. FABRICATED REPAIR PARTS, ALODINED, PRIMED AND INSTALLED THE REPAIR PARTS WITH FASTENERS. APPLIED BMS 5-95 SEALANT TO THE MATING SURFACES. COMPLETED REPAIR. AIRCRAFT RETURNED TO SERVICE.

Part: PRESSURE PANEL — CORRODED (FUSELAGE)

FOUND CORROSION ON NOSE LANDING GEAR BULKHEAD AT BS 227.8. CUT OUT CORROSION AND VERIFIED REMOVED BY VISUAL INSPECTION. FABRICATED CHORD AND REPAIR ANGLES. INSTALLED CHORD AND REPAIR ANGLES. COMPLETED REPAIR.

Part: SLAT — CORRODED (RT WING)

FOUND CORROSION ON THE RIGHT WING AFT OF THE NR 5 SLAT FITTING. BLENDED OUT CORROSION. FABRICATED AND INSTALLED PARTS. REWORK COMPLETED. AIRCRAFT RETURNED TO SERVICE.

Part: BRACKET — CHAFED (T/E FLAP)

FOUND NR 8 FLAP JACKSCREW TRAILING EDGE MOUNT BRACKET CHAFFING AT FLAP TRACK FAIRING. BLENDED OUT DAMAGED AREA. REWORK COMPLETED. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — GOUGED (FUSELAGE)

FOUND GOUGE IN SKIN AT STRINGER 16L AT BS 843. BLENDED OUT DAMAGED AREA TO A SMOOTH SURFACE. VERIFIED NO CRACKS USING HFEC. REPAIR COMPLETED IAW SRM. AIRCRAFT RETURNED TO SERVICE.

Part: SPAR — CORRODED (RT WING)

FOUND CORROSION ON RIGHT WING FRONT SPAR, LOWER CHORD FORWARD HORIZONTAL FLANGE FORWARD LIP AT FSS 413. REMOVED CORROSION BY BLEND OUT. HFEC AREA TO ENSURE FREE OF CRACKS AND CORROSION. FABRICATED A REPAIR FILLER. INSTALLED REPAIR FILLER. REPAIR COMPLETED. AIRCRAFT RETURNED TO SURFACE.

Part: SKIN — WORN (RT WING)

RIGHT WING LEADING EDGE LOWER SKIN AT FSS 413 WORN BEYOND LIMITS. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER, SPLICE PLATE AND DOUBLER. AIRCRAFT RETURNED TO SERVICE.

Part: FLOORBEAM — CRACKED (FUSELAGE)

FOUND CRACKS AT BL 0 FLOOR BEAM AT BS 663 AND BETWEEN BS 700-717 WEB. REMOVED AND DISCARDED A SECTION OF THE WEB AND DOUBLER CONTAINING THE CRACKS. FABRICATED ALL REPAIR PARTS. INSTALLED SPLICE ANGLES AND STRAPS WITH NUT PLATES. COMPLETED INSTALLATION OF REINFORCING ANGLE, FILLER AND SPLICE PLATES. AIRCRAFT RETURNED TO SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE)

FOUND CRACK ON THE BLK 178 AT WL 212, LBL 5.7 DURING INSPECTION PER ECO 3137. CUT OUT CRACK AND REMOVED DAMAGED SECTION OF WEB. VERIFIED CRACK REMOVAL USING HFEC. FABRICATED DOUBLER AND FILLERS. INSTALLED REPAIR PARTS. AIRCRAFT RETURNED TO SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE)

FOUND CRACK ON THE BLK 178 AT WL 212, RBL 5.7 DURING INSPECTION. CUTOUT CRACK AND REMOVED DAMAGED SECTION OF WEB. VERIFIED CRACK REMOVAL USING HFEC. FABRICATED DOUBLER AND FILLERS. INSTALLED REPAIR PART.

Part: STRINGER — DENTED (FUSELAGE)

FOUND DENT ACROSS STRINGER 15L AT BS 900. CUTOUT STRINGER SEGMENT AT BS 900. REMOVED THE SEGMENT OF THE STRINGER AFT TO THE PRODUCTION SPLICE. FABRICATED NEW STRINGER SEGMENT. INSTALLED STRINGER PER SRM 53-10-3. COMPLETED REPAIR. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE)

REMOVED CORROSION DAMAGE ON STRINGER 5R UPPER CHORD AT BS 1093. REMOVED FORWARD PORTION OF DAMAGED CHORD. FABRICATED REPLACEMENT CHORD AND SPLICE ANGLES AND INSTALLED REPAIR PARTS PER FIGURE 1 IAW ECO 3259. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: DOWNLOCK SENSOR — FAILED (RT MLG)

INBOUND TO HNL FROM LIH - REPORTED TO MAINTENANCE CONTROL OF THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ON IN-FLIGHT. CAPTAIN PERFORMED FLYBY FOR TOWER TO CHECK GEARS DOWN WHILE F/O ALSO CHECKED BY GOING TO BACK OF AIRCRAFT. GEARS RECYCLED ONCE AND LIGHT STILL ON. TOWER ADVISED CAPTAIN GEARS SEEM TO BE DOWN AND EVERYTHING LOOKS OK. CAPTAIN LANDED AIRCRAFT WITH NO FURTHER INCIDENT. T/S TO THE RIGHT DOWNLOCK SENSOR THAT WAS REPLACED AND OPERATIONALLY CHECKED OK PER MM 32-61-31, PAGE 401-404. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY — INOPERATIVE (CABIN) · airframe 36,594 hrs · 35,841 cycles

REPLACED NR 4 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY — INOPERATIVE (CABIN)

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

Part: SKIN — DENTED (FUSELAGE)

REPAIRED A DENT AT LEFT FUSELAGE BS 360-380 STRINGER 17L, AFT OF FORWARD ENTRY DOOR. CUT OUT DAMAGED AREA PERFORMED HFEC INSPECTION. FABRICATED AND INSTALLED DOUBLER PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FCU — FAILED (NR 1 ENGINE)

FLT 71 - OGG-HNL - THE NR 1 ENGINE RPM GAGE IMMEDIATELY DECREASED TO ZERO THE MOMENT THE AIRCRAFT LIFTED OFF THE RUNWAY. DID NOT ATTEMPT A RESTART, ACCOMPLISHED NORMAL SINGLE ENGINE LANDING WITH NO FURTHER PROBLEMS NOTED. REMOVED AND REPLACED NR 1 ENGINE FUEL PUMP P/N 7436025, PER PWA MM 72-60, PAG 611. OPS AND LEAK CHECK OK. REMOVED AND REPLACED NR 1 ENGINE FUEL CONTROL UNIT PER PWA MM 73-21-1. OPS AND LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

REPLACED NR 3, 4, 5, AND 6 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SENSOR — INTERMITTENT (LT MLG UPLOCK)

FLT 101 - OGG-HNL - LEFT MAIN GEAR RED UNSAFE GEAR LIGHT COMES ON INTERMITTENTLY DURING FLIGHT. REMOVED AND REPLACED UPLOCK SENSOR LEFT GEAR PER MM 32-61-21 AND ALSO CHECKED UPLOCK MECHANISM PER MM 32-32-31. ALL OK, OPS OK ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: CONTROLLER — FAILED (CABIN)

HNL/ITO - FLT 248 - PRESSURIZATION FAILURE AT FL 230. LOST AUTO, STANDBY, AND A/C MANUAL SHOWED VALVE CLOSED BUT DID NOT CONTROL CABIN. LATER, MANUAL AND STANDBY WORKED. DIVERTED TO OGG AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER. GROUND CHECK OK. REMOVED AND REPLACED LOWER PRESSURE RELIEF VALVE IAW 21-32-20 FOR PRECAUTIONARY. AIRCRAFT RETURNED TO SERVICE. (X)

Part: RELIEF VALVE — FAILED (CABIN)

HNL/ITO - FLT 248 - PRESSURIZATION FAILURE AT FL 230. LOST AUTO, STANDBY, AND A/C MANUAL SHOWED VALVE CLOSED, BUT DIDN'T CONTROL CABIN. LATER, MANUAL AND STANDBY WORKED. DIVERTED TO OGG AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER. GROUND CHECK OK. REMOVED AND REPLACED LOWER PRESSURE RELIEF VALVE IAW 21-32-20 FOR PRECAUTIONARY. AIRCRAFT RETURNED TO SERVICE. PRESSURE RELIEF VALVE INSTALLATION SUSPECT. CPC TESTED GOOD. MONITORED A/C, NO PROBLEMS.

Part: BATTERY — DISCHARGED (CABIN)

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

Part: BATTERY — DISCHARGED (CABIN)

REPLACED NR 6 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK FOR LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

REPLACED FORWARD SERVICE DOOR EXIT IDENTIFIER LIGHT POWER SUPPLY DUE TO BEING INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

REPLACED NR 4 FLOOR EMERGENCY BATTERY PACK FOR HAVING LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

REPLACED NR 2 AND NR 4 EMERGENCY PATH LIGHTING BATTERY PACK DUE TO BEING INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 6 EMERGENCY GROUND PROXIMITY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 5 EMERGENCY GROUND PROXIMITY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

REPLACED BATTERY IN POSITION 6 FLOOR PROXIMITY LIGHT ASSY DUE TO INOP. OPS CHECK OK. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED BATTERY PACK ON RIGHT SIDE FORWARD EXIT IDENTIFIER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED BATTERY PACK ON LEFT SIDE FORWARD EXIT IDENTIFIER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

RIGHT FORWARD SERVICE DOOR SLIDE EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: PIN — BROKEN (PAX DOOR)

LOUD HIGH PITCHED SQUEAL COMING FROM FORWARD ENTRY DOOR. STARTED ABOVE 2 PSI. FOUND BROKEN HINGE PIN ASSY. REPLACED ASSY AND PRESSURIZED AIRCRAFT TO 7.6 PSI. NO NOISE NOTED UPON CHECK. ALSO CLEANED DOOR SEALS AND HINGE SEAT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: DADC — FAILED (NR 2)

FIRST OFFICER AIRSPEED, ALTIMETER, AND VERTICAL SPEED INDICATOR ERRATIC. REPLACED NR 2 DADC IAW MM 34-12-11. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHT INOP. REPLACED BATTERY PACK OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: GEARBOX — LEAKING (NR 1 ENGINE)

FLT 247 - ITO-HNL - SHUT DOWN NR 1 ENGINE DUE TO LOW OIL PRESSURE. ENGINE WAS SHUT DOWN FOR APPROXIMATELY 12 MINUTES. DIVERTED TO OGG. SERVICED OIL (4 QTS). PULLED ENGINE OIL FILTER. CHECK OK. INSTALLED NEW OIL FILTER PER ENGINE MANUAL 72-61-00, PAGE 1005-1006. REINSTALLED COMBUSTION CHAMBER FUEL DRAG LINE. NO OIL IN LINE. REMOVED OIL PRESSURE DIFFERENTIAL LINE. MOTORED ENGINE. POSITIVE FLOW FROM OIL PUMP. OIL PRESSURE RISE AND OIL TEMP RISE. QIL QTY READS ZERO. REPLACED NR 1 ENGINE GEARBOX ASSY PER PWA MM 72-60. REPLACED OIL COOLER. PRECAUTIONARY LOW OIL QTY. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONTROL CABLE — BROKEN (NR 7 SPOILER)

FLT 65 - HNL-LIH - OUTER RGT SPOILER PANEL STAYS FAIRED DURING TURNING OF YOKE (ALERON INPUT). FOUND NR 7 FLT SPOILER 'WSA1-4' CABLE BROKEN APPROX 2 FT INBOARD OF NR 7 SPOILER QUADRANTS. INSTALLED NEW CABLE AND RIGGED IAW MM 261-0. OPS CHECK OK. NO OTHER DEFECTS NOTED. RIGHT COMPLETED FOR RIGGING OF NR 7 FLT SPOILER CABLE WSA1-4. OPS CHECK OK. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 1 POSITION EMERGENCY LIGHT BATTERY PACK DUE TO INOPERABILITY OF NR 1 POSITION EMERGENCY LIGHT. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

DURING OVERNIGHT CHECK, REPLACED BATTERY FOR ROW 4 EMERGENCY FLOOR PROX LIGHT ASSY DUE TO INOP. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

DURING OVERNIGHT CHECK, REPLACED BATTERIES FOR POS 1 THROUGH 5 FLOOR PROX LIGHT ASSEMBLIES DUE TO LOW VOLTAGE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

DURING OVERNIGHT CHECK, REPLACED BATTERY FOR ROW 22 EMERGENCY FLOOR PROXIMITY LIGHT ASSY DUE TO INOPERABLE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 30,443:00 HOURS. TAC: 22,060. (X)

Part: BATTERY — DISCHARGED (CABIN)

DURING OVERNIGHT CHECK, REPLACED BATTERIES FOR ROW 12 AND 17 EMERGENCY FLOOR PROX LIGHT ASSY DUE TO INOP. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — MISSING LENS (CABIN)

DURING OVERNIGHT CHECK, REPLACED FWD SERVICE DOOR EMERGENCY LIGHT ASSY DUE TO LENS MISSING. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: PIN — DISPLACED (PAX DOOR)

FLT 82 - HNL - KOA - LOUD NOISE FROM FORWARD ENTRY DOOR AFTER TAKEOFF. REINSTALLED UPPER HINGE SEAL RETAINING PIN, PRESSURIZED AIRCRAFT. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

DURING OVERNIGHT CHECK, REPLACED BATTERY FOR ROW 22 EMERGENCY FLOOR PROX LIGHT ASSEMBLY DUE TO INOP. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BYPASS SWITCH — FAILED (NR 2 ENGINE)

HNL/LIH - FLT 232 - PILOT REPORT, NR 2 ENGINE OIL FILTER BYPASS LIGHT ON. SHUT DOWN ENGINE IN-FLIGHT. REMOVED, INSPECTED, AND REPLACED NR 2 ENGINE OIL FILTER. NO METAL NOTED. REPLACED NR 2 ENGINE OIL FILTER BYPASS SWITCH. LEAK AND OPS CHECK OK PER MM 79-35-0. PAGES 501-503. AIRCRAFT RETURNED TO SERVICE. (X)

Part: LAMP — INOPERATIVE (CABIN)

DURING OVERNIGHT CHECK, RE-LAMPED LEFT OVERHEAD RACK EMERGENCY LIGHT DUE TO INOPERABLE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 29,878:51 HOURS. TAC: 20,765

Part: SKIN — CORRODED (VERT STAB)

DURING C-CHECK VISIT, CORROSION NOTED ON VERTICAL STABILIZER LEFT SIDE BETWEEN FS 111 - FS 113. REPAIRED PER ECO 2509 R2. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (WS 505-557)

DURING C-CHECK VISIT, NOTED EXFOLIATION CORROSION LOWER WING SKIN RIGHT, CORROSION AT INBOARD AILERON ATTACH POINT WING TO FITTING WS 505 - 557 REPAIRED PER ECO 1684 R7. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAL — BLOWN (AFT CARGO DOOR)

KOA/HNL - FLT 481 - PILOT REPORT: 4 LOUD THUMPS FOLLOWED BY LOSS OF PRESSURIZATION AT FL 220. BEGAN DESCENT AND DECLARED EMERGENCY. LANDING UNEVENTFUL. POST-FLIGHT INSPECTION SHOWS AFT CARGO DOOR SEAL BLOWN OUT. MAINTENANCE REPLACED AFT CARGO DOOR SEAL. LEAK AND PRESSURIZATION CHECK OK. (X)