N808AL

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 42,623 hrs · 53,692 cycles

AFT CARGO DOOR CUT-OUT DAMAGED (LOWER AFT CORNER). ALOHA ECO 3622 ISSUED.

Part: SWITCH — FAILED (STAB TRIM) · airframe 42,433 hrs · 53,263 cycles

NON-ETOPS FLIGHT 206 HNL OGG. ON TAKEOFF THE CONFIGURATION WARNING ALARM SOUNDED WHEN THROTTLES WERE ADVANCED. CREW ABORTED TAKEOFF AT 15 KTS. AIRCRAFT WAS CONFIGURED PROPERLY FOR TAKEOFF WITH THE SPEED BRAKE DOWN, FLAPS SET TO 5 AND TRIM AT 5.5 UNITS. CREW RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE STABILIZER TRIM SWITCH S132 FAILED. MAINTENANCE REMOVED AND REPLACED SWITCH S132 IAW AMM 31-26-24 AND TESTED NORMAL IAW AMM 31-26-00/501. AIRCRAFT WAS THEN RETURNED TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 42,013 hrs · 52,364 cycles

NON-ETOPS FLT 224 LIH-HNL. ON TAKE OF ROLL, CREW NOTED THE NR 2 ENGINE THRUST REVERSER UNLOCKED LIGHT ON WITH ALL OTHER ENGINE INDICATIONS NORMAL. CREW ABORTED TAKEOFF AT 60 KTS AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE OPENED AND INSPECTED THE NR 2 THRUST REVERSER AND HAD NO FAULT FOUND. GROUND OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE.

Part: LATCH — LACK OF LUBE (THRUST REVERSER) · airframe 41,959 hrs · 52,229 cycles

ON TAKEOFF ABOVE 80 KNOTS AND CLIMB, CREW NOTED NR 2 THRUST REVERSER UNLOCKED LIGHT ILLUMINATED INTERMITTENTLY. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE DEFERRED PER MEL 78-2 AND RELEASED THE AIRCRAFT FOR SERVICE. ON 7/16/06 MAINTENANCE CLEARED THE MEL 78-2 AS FOLLOWS: INSPECTED THE THRUST REVERSER LOCK LATCH FITTING IN ACCORDANCE WITH AMM 78-32-102. INSPECTED DEFLECTOR DOOR IN ACCORDANCE WITH AMM 78-32-112. LUBED LATCH ASSEMBLY. OPERATIONAL CHECK GOOD ON THE GROUND. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 41,783 hrs · 51,813 cycles

2.25 INCH SKIN CRACK FOUND LEFT SIDE OF FUSELAGE BS 786 JUST ABOVE STRINGER 24L. MAINTENANCE REPAIRED WITH APPROXIMATELY 11 IN X 15 IN EXTERNAL SKIN PATCH, FABRICATED DOUBLER AND TRIPLER PER SRM 53-30-3, PROCEDURE VII, DETAIL VII.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 41,783 hrs · 51,813 cycles

2.5 INCH SKIN CRACK FOUND RIGHT SIDE OF FUSELAGE AT BS 941 JUST ABOVE STRINGER 24R. MAINTENANCE REMOVED TWO EXISTING REPAIRS AND REPAIRED WITH 36 IN X 46 IN EXTERNAL SKIN PATCH, FABRICATED FILLERS, DOUBLER, AND TRIPLER PER SRM 53-30-3, PROCEDURE VII, DETAIL XII.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 41,783 hrs · 51,813 cycles

3 INCH CRACK FOUND RT SIDE OF FUSELAGE SKIN AFT OF AFT CARGO DOOR CUTOUT AS BS 867 STRINGER 23R. MAINTENANCE REMOVED ONE EXISTING REPAIR AND REPAIRED WITH APPROXIMATELY 19-1/2 IN X 19-1/2 IN EXTERNAL SKIN PATCH, FABRICATED DOUBLER AND TRIPLER PER SRM 53-30-3, PAGE 256, DETAIL VII.

Part: SLAT — BIRD STRIKE (NR 1)

ON CLIMB AT 1000 FT AIRCRAFT STRUCK A LARGE BIRD AT NR 1 LEADING EDGE SLAT. THE CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE COMPLIED WITH FORM M-106 BIRD STRIKE INSPECTION AND FOUND A LARGE DENT APPROXIMATELY 1.5 INCH WIDE ON THE OUTBOARD LEADING EDGE TOP OF THE NR 1 SLAT. REMOVED AND REPLACED NR 1 SLAT IN ACCORDANCE WITH MM 27-81-21, AND RETURNED AIRCRAFT TO SERVICE.

Part: SKIN — CRACKED (NR 2 SLAT) · airframe 41,135 hrs · 50,347 cycles

FOUND 3 CRACKS AROUND CENTER UPSTOP OF NR 2 SLAT; WING LEADING EDGE. BETWEEN LEFT WS 453 AND WS 479. L/E SKIN FABRICATED, TRIMMED, CLEANED, ALODINED, PRIMED, AND SEALED IAW SRM 57-30-04. REPAIR SIZE APPROX 14" BY 25".

Part: ENGINE — DEFECTIVE (NR 2) · airframe 41,115 hrs · 50,307 cycles

OGG-HNL: ON TAKEOFF NR 2 ENGINE EGT ROSE TO 650 DEGREES CELSIUS. ENGINE THROTTLED BACK UNTIL EGT WAS WITHIN LIMITS AND AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 ENGINE IAW FORM M-211, M-212, M-213, AND M-215. NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN PANEL — CRACKED (BS 927) · airframe 40,557 hrs · 48,991 cycles

A 3.5 INCH CRACK FOUND RIGHT SIDE OF FUSELAGE SKIN AFT OF AFT CARGO DOOR AT BS 927 STRINGER 23R. CUT OUT CRACK .040 INCH INSURANCE CUT. PERFORMED HFEC AROUND CUTOUT, NO CRACK PROPAGATION NOTED IAW BOEING NDT MANUAL 51-00-00, PART 6. REPAIRED WITH 10 X 13 INCH SKIN PATCH, FABRICATED DOUBLER (0322024T3) AND TRIPLER (0502024T3). REPAIR COMPLETED IAW SRM 53-30-3, FIG 48, DETAIL XI.

Part: ACTUATOR — LEAKING (NR 1 SPOILER)

CREW HAD INDICATION OF HYDRAULIC SYSTEM A, DROP IN PRESSURE. CREW DECLARED AN EMERGENCY AND WERE ABLE TO DEPLOY THE LANDING GEAR. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 SPOILER ACTUATOR AND INSPECTED AND REPLACED BOTH ENGINE CASE DRAINS, SYSTEM A MODULE AND RETURN FILTERS AND RETURNED THE AIRCRAFT TO SERVICE.

Part: ACTUATOR — FAILED (NR 5 SLAT)

COOPESA TO BROWNSVILLE TX FERRY FLIGHT 808. NR 5 SLAT DID NOT RETRACT. LEFT WING TO BODY OVERHEAT INDICATION. THE CREW RETURNED TO COOPESA WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 5 SLAT ACTUATOR AND PNEUMATIC DUCT AND CLAMP. OPS AND LEAK CHECKS OK. AIRCRAFT RETURNED TO SERVICE.

Part: SLAT — INFLT SEPARATION (NR 3)

AFTER ARRIVAL IN LIH A PASSENGER ADVISED THE FLIGHT ATTENDANT THAT PART OF THE WING SEPARATED IN FLIGHT. CAPTAIN THEN OBSERVED A SECTION OF THE NUMBER THREE LEADING EDGE SLAT MISSING. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE LEADING EDGE SLAT ASSEMBLY AND VERIFIED GROUND OPERATION OK.

Part: SEAL — LEAKING (HYDRAULIC PUMP)

NON-ETOPS FLT 104, HNL-KOA: LOST A SYSTEM HYDRAULICS DURING CLIMB-OUT. RETURNED TO HNL. FLAPS WOULD NOT EXTEND TO 15 USING ALTERNATE FLAP SYSTEM. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE HYDRAULIC PUMP DUE TO INPUT SHAFT SEAL LEAKING PER AMM 29-11-31. OPS AND LEAK CHECK GOOD. MAINTENANCE REMOVED AND REPLACED THE FLAP ALTERNATE DRIVE UNIT. OPERATIONAL AND LEAK CHECK GOOD PER MM 27-51-241. AIRCRAFT RETURNED TO SERVICE.

Part: SEAL — LEAKING (HYDRAULIC PUMP)

NON-ETOPS FLT 104, HNL-KOA: LOST A SYSTEM HYDRAULICS DURING CLIMB-OUT. RETURNED TO HNL. FLAPS WOULD NOT EXTEND TO 15 USING ALTERNATE FLAP SYSTEM. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE HYDRAULIC PUMP DUE TO INPUT SHAFT SEAL LEAKING PER AMM 29-11-31. OPS AND LEAK CHECK GOOD. MAINTENANCE REMOVED AND REPLACED THE FLAP ALTERNATE DRIVE UNIT. OPERATIONAL AND LEAK CHECK GOOD PER MM 27-51-241. AIRCRAFT RETURNED TO SERVICE.

Part: LINE — LEAKING (HYD SYSTEM)

LOST A SYSTEM HYDRAULICS ON SHORT FINAL. MAINTENANCE MET THE AIRCRAFT ON THE RUNWAY. MAINTENANCE REPLACED THE NOSE GEAR DOWN ACTUATOR LINE PER AMM 32-3-11. SERVICED HYDRAULIC SYSTEM TO FULL. LEAK CHECK OKAY. REPLACED THE NR 1 AND NR 2 CASE DRAIN FILTERS, LEAK CHECK OK PER AMM 29-11-91. AIRCRAFT RETURNED TO SERVICE.

Part: LINE — LEAKING (MLG ACTUATOR)

FLT 89, KOA-HNL: A SYSTEM HYDRAULICS FAILED ON SHORT FINAL. LEFT MAIN GEAR LEAKING. FOUND THE LEFT HAND MAIN LANDING GEAR ACTUATOR UP PRESSURE HOSE ASSEMBLY LEAKING. REMOVED AND REPLACED THE HYDRAULIC PRESSURE HOSE ASSEMBLY AND SERVICED THE HYDRAULIC RESERVOIR. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DOWNLOCK SENSOR — DEFECTIVE (LT MLG)

NON-ETOPS FLT. 82, HNL-KOA - DURING DESCENT, LEFT GEAR RED LIGHT WAS ON WITH THE LANDING GEAR HANDLE IN THE DOWN POSITION. FLEW BY TOWER TO VERIFY GEAR DOWN. UNEVENTFUL LANDING AT KOA. VERIFIED LEFT DOWNLOCK SENSOR BAD. REPLACED PROXIMITY SENSOR PER AMM 32-61-31. OPS CHECK OK. OK FOR SERVICE. AIRCRAFT RETURNED TO SERVICE.

Part: INDICATOR — FAILED (TE FLAPS) · airframe 38,942 hrs · 45,391 cycles

NON-ETOPS FLIGHT 110, HNL-OGG: FLAPS DID NOT DEPLOY DURING NORMAL FLAP EXTENSION, USED ALTERNATE MODE TO DEPLOY LEADING EDGE FLAPS. THE TRAILING EDGE FLAPS WERE ASYMMETRICALLY SPLIT AT LESS THAN ONE UNIT. RETURNED TO HNL. REMOVED AND REPLACED THE FLAP POSITION INDICATOR. OPS CHECK OK, AIRCRAFT RETURNED TO SERVICE.

Part: WINDSHIELD — FAILED (COCKPIT)

CAPTAIN'S NR 1 WINDOW OUTER PANE CRACKED. RETURNED TO HNL. REMOVED AND REPLACED CAPTAIN'S NR 1 WINDOW IAW AMM 56-11-11, PAGES 401-411 AND 580. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DUCT — FAILED (NR 1 ENG FUEL HE)

FLT 286 - LIH-HNL - PASSING 10,000 FEET ON CLIMB-OUT, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. ALL OTHER ENGINE INSTRUMENTS IN GREEN. RETARDED NR 1 ENGINE AND THE LIGHT WENT OUT. REPLACED NR 1 ENGINE FUEL HEAT DUCT DUE TO CRACKED WELD. LEAK CHECK OK, AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

REPLACED FORWARD SERVICE DOOR IDENT EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

TRIMMED OUT THE SKIN CRACK. VERIFIED HFEC CUTOUT AND ROTARY PROBE INSPECTION OF LAP SPLICE FASTENER HOLES. FABRICATED AND INSTALLED STRUCTURAL FILLERS, A DOUBLER, AND TEARSTRAP PER FIGURE 48. ALODINED AND PRIMED ALL REPAIR PARTS AND BARE SURFACES. APPLIED CORROSION INHIBITING COMPOUND. ASSEMBLED REPAIR PARTS WITH BMS 5-59 SEALANT ON ALL MATING SURFACES PRIOR TO FASTENER INSTALLATION. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 48, DETAIL XII. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FIRE DETECTOR — FAILED (MLG WW)

APPROXIMATELY 25 MILES FROM HNL, A WHEEL WELL FIRE LIGHT CAME ON. DEFER IAW MEL 26-4, SYSTEM DEACTIVATED IAW MEL. PLACARDS INSTALLED. REMOVED AND REPLACED WHEEL WELL FIRE AND OVERHEAT ELEMENT. OPS CHECK OK. PLACARD REMOVED FROM AIRCRAFT AND LOGBOOK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

REPLACED LT OVERWING IDENT EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

REPLACED RIGHT OVERWING IDENT EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

REPLACED FORWARD SERVICE DOOR IDENT EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (PAX CABIN)

REPLACED NR 6 FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (PAX CABIN)

REPLACED AFT PASSENGER CABIN EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (PAX DOOR)

REPLACED FORWARD PASSENGER CABIN EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — DAMAGED (FUSELAGE)

REMOVED ALL EXISTING REPAIRS COMMON TO THE LAP JOINT AREAS. ACCOMPLISHED A HFEC OF FASTENERS HOLES TO ASSURE CRACK FREE CONDITION. FABRICATED TWO TAPERED FILLERS, A .032 INCH THICK FILLER AND FOUR .071 INCHE THICK FILLERS, A .032 INCH THICK SPLICE STRAP, A .032 INCH THICK DOUBLER AND .050 INCH THICK TRIPLER. INSTALLED REPAIR PARTS ALONG STRINGER 4L AND 4R FROM BS 360 TO BS 908, ALONG STRINGER 10L AND 10R FROM BS 360-540 AND BS 727 TO BS 908, AND ALONG STRINGER 14L AND 14R FROM BS 360-540 AND BS 727 TO BS 908 P/N'S 6545818, 6546535, 6546547, 6546558, LAP JOINT REPAIR MODICICATION COMPLETED IAW ECO 3080, WITH DEVIATIONS BJ, BK, BL, BM BN, BO, BP, BQ, BR AND BS.

Part: KEELBEAM — CORRODED (FUSLEAGE)

TRIMMED OUT FUSELAGE SKIN BETWEEN KEEL BEAMS AND AFT OF BS 727. REMOVED AND REPLACED LEFT AND RIGHT KEEL BEAM FROM BS 500 TO BS 727 PLUS 16. VISUALLY AND HFEC INSPECTED TRIMLINE AND AREA UNDER REPAIR FOR SIGNS OF CORROSION AND DISBONDING. FABRICATED AND INSTALLED THREE FILLERS, A DOUBLER AND TRIPLER. FINISHED ALL BARE ALUMINUM WITH ALODINE AND TWO COATS BMS 10-79, TYPE III PRIMER. REPAIR COMPLETED IAW ECO 3327, FIGURE 1. AIRCRAFT RETURNED TO SERVICE (M)

Part: WEB — CORRODED (FUSELAGE)

TRIMMED RIGHT WEB SECTION FROM BS 675 TO BS 695 FROM BL 0 TO RBL 70. FABRICATED NEW PRESSURE WEB SECTION, STIFFENERS AND FILLERS. SHOT PEENED, ALODINED AND PRIMED ALL BARE SURFACES AND REPAIR PARTS. INSTALLED REPAIR PARTS PER FIGURE 3. REPAIR COMPLETED IAW ECO 3328, PART II AND V. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SPLICE — CORRODED (FUSELAGE)

TRIMMED LEFT WEB SECTION FROM BS 675 TO BS 695 FROM BL 0 TO LBL 24.5. FABRICATED NEW PRESSURE WEB SECTION AND STEP FILLERS FOR TRANSVERSE I BEAM. FABRICATED FOUR DOUBLER I BEAM TIE STRAPS AND TEE STIFFENERS. ALODINED AND PRIMED ALL BARE SURFACES AND REPAIR PARTS. INSTALLED REPAIR PARTS PER SRM 53-60-51, FIGURE 203. REPAIR COMPLETED IAW ECO 3328, PART II AND V. AIRCRAFT RETURNED TO SERVICE. (M)

Part: PRESSURE PANEL — CORRODED (FUSELAGE)

FABRICATED NEW PRESSURE WEB REPAIR DOUBLER. ALODINED AND PRIMED ALL BARE ALUMINUM. FAY SURFACE SEAL INSTALLED REPAIR DOUBLER WITH BMS 5-95 AND FASTENERS IDENTIFIED. APPLIED CORROSION INHIBITING COMPOUND TO THE INTERNAL SURFACES. REPAIR COMPLETED IAW ECO 3328, PART 1 AND V. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FITTING — CRACKED (HORIZONTAL STAB)

THE LEFT HORIZONTAL STABILIZER CENTER SECTION REAR SPAR ATTACHMENT FITTING CLEVIS LUGS BUSHINGS REMOVED. EDDY CURRENT INSPECTED LUGS FOR CRACKS BEFORE AND AFTER OVERSIZING AND SHOT PEENING. MACHINED, SHOT PEENED, AND FINISHED THE LUG/CLEVIS. INSTALLED BUSHING/SLEEVE WET WITH MBS 5-95 SEALANT. APPLIED A FILLET SEAL USING BMS 5-95 AND CORROSION INHIBITING COMPOUND BMS 3-23 TO THE BUSHINGS AND LUG FACES. MODIFICATION COMPLETE IAW ECO 2887. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FITTING — CORRODED (HORIZONTAL STAB)

THE LEFT HORIZONTAL STABILIZER CENTER SECTION REAR SPAR LOWER FITTING ASSEMBLY FAIL/SAFE AND LOWER CLEVIS LUG REQUIRED REWORK BEYOND THE LIMITS PROVIDED IN SB 737-55-1055. REFINISHED THE LUG BORE AND FABRICATED A NEW SLEEVE BUSHING AND FLANGE BUSHING PER DRAWING. SHOT PEENED, REFINISHED THE LUG FACES, AND INSTALLED BUSHINGS. REPAIR COMPLETED AIW ECO 3331. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SPLICE — CORRODED (FUSELAGE)

TRIMMED WEB SECTION FROM BS 675 TO BS 695 FROM BL 0 TO LBL 24.5. FABRICATED NEW PERSSURE WEB SECTION AND STEP FILLERS FOR TRANSVERSE I BEAM. FABRICATED FOUR DOUBLER I BEAM TIE STRAPS AND TEE STIFFENERS. ALODINED AND PRIMED ALL BARE SURFACES AND REPAIR PARTS. INSTALLED REPAIR PARTS PER SRM 53-60-51, FIGURE 203. REPAIR COMPLETED IAW ECO 3328. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FITTING — CORRODED (HORIZONTAL STAB)

THE LEFT HORIZONTAL STABILIZER CENTER CENTER SECTION REAR SPAR UPPER FITTING ASSEMBLY UPPER CLEVIS LUG REQUIRED REWORK BEYOND THE LIMITS PROVIDED IN SB 737-55-1055. REFINISHED THE LUG BORE AND FABRICATED A NEW OVERSIZED BUSHING PER DRAWING. SHOT PEENED, REFINISHED THE LUG FACES, AND INSTALLED BUSHING. REPAIR COMPLETED IAW ECO 3330. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CANNING (FUSELAGE)

TRIMMED OUT THE SKIN SNAP DAMAGE AND OIL-CANNING. VISUALLY INSPECTED FOR DISBONDING. FABRICATED AND INSTALLED THREE STRUCTURAL FILLERS, AND DOUBLER AND TEARSTRAP PER FIGURE 1. ALODINED AND PRIMED. APPLIED CORROSION INHIBITING COMPOUND. REPAIR COMPLETED IAW ECO 3315. AIRCRAFT RETURNED TO SERVICE. (M)

Part: GPS — FAILED (NR 1 AND 2)

ENROUTE, THE NR 1 AND NR 2 GPS WERE UNABLE TO LOCK ON TO THE SATELLITE SIGNAL. THE AIRCRAFT RETURNED FOR MAINTENANCE WITH NO FURTHER INCIDENT. REMOVED AND REPLACED THE NR 1 AND NR 2 GPS NPU. GROUND OPS CHECKS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. FLIGHT VERIFICATION CHECKED GOOD ON BOTH UNITS ENROUTE.

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECKED, OK. AIRCRAFT RETURNED TO SERVICE. (TSAA80003325)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED NR 2 FLOOR PROXIMITY LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

REPLACED RIGHT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: COUPLER — DEFECTIVE (HF COMM)

FLT 351 - HNL-JON - DURING THE VERIFICATION PHASE OF FLIGHT AND CHECKING THE HF RADIO SYSTEM, THE NR 1 HF HAD NO TUNE AND THE TRANSMIT WAS INOPERATIVE. RETURNED TO HNL FOR AN OVERWEIGHT LANDING, VERY LOW SINK RATE. REPLACED NR 1 HF TRANSCEIVER (P/N 6223371001). OPS CHECK ON GROUND WITH SFO AND SELCAL CHECK OK. VERIFICATION FLIGHT REQUIRED. PERFORMED OVERWEIGHT LANDING INSPECTION IAW FORM M-121. NO DEFECTS NOTED IN PHASE 1 STEP 2A. OK FOR SERVICE. SUBSEQUENTLY, THE HF COUPLER WAS REPLACED (P/N 792-6140-001) AND VERIFIED AS THE CAUSE. AIRCRAFT RETURNED TO SERVICE. REF TSAA0123113. (M)

Part: TRANSCEIVER — MALFUNCTIONED (HF COMM)

FLT 351 - HNL-JON - DURING THE VERIFICATION PHASE OF FLIGHT AND CHECKING THE HF RADIO SYSTEM, THE NR 1 HF HAD NO TUNE AND THE TRANSMIT WAS INOPERATIVE. RETURNED TO HNL FOR AN OVERWEIGHT LANDING, VERY LOW SINK RATE. REPLACED NR 1 HF TRANSCEIVER (P/N 6223371001). OPS CHECK ON GROUND WITH SFO AND SELCAL CHECK OK. VERIFICATION FLIGHT REQUIRED. PERFORMED OVERWEIGHT LANDING INSPECTION IAW FORM M-121. NO DEFECTS NOTED IN PHASE 1 STEP 2A. OK FOR SERVICE. SUBSEQUENTLY, THE HF COUPLER WAS REPLACED (P/N 792-6140-001) AND VERIFIED AS THE CAUSE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: SPAR — CORRODED (RT WING)

EXFOLIATED CORROSION DISCOVERED ON RIGHT UNDER WING T/E AFT SPAR LOWER APPROXIMATELY 21 INCHES OUTBOARD OF WBL 355 SKIN PANEL. CLEANED AND TREATED AS EP SRM 51-10-6 PAGE 12. EVALUATED AND REPAIRED IAW ECO 3213. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

EXFOLIATION CORROSION DISCOVERED ON FLOORBEAM AT BS 277. REMOVED CORROSION BY CLEANING AND TREATING AFFECTED AREA PER SRM 51-10-6. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

EXFOLIATED CORROSION DISCOVERED ON FLOORBEAM AT BS 294.5 PLUS 8 AND PLUS 13 RBL 12. REMOVED CORROSION BY REPLACING THE FLOORBEAM SECTION AT BS 294.5 PLUS 8 AND PLUS 13 IAW BOEING DRAWING 65-45808. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SURFACE CORROSION DISCOVERED ON FLOORBEAM AT BS 312, LBL 12 TO RBL 12. REMOVED CORROSION BY REPLACING THE INTERCOSTAL IAW SRM 51-10-01. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ENGINE — MALFUNCTIONED (NR 1 ENGINE)

FLT 531 - LNY-HNL - TAXIED TO RUNWAY. WHEN POWER ADVANCED FOR TAKEOFF, A LOUD BANG CAME FROM THE NR 1 ENGINE. ABORTED TAKEOFF AT APPROXIMATELY 20 KNOTS AND SHUT DOWN THE NR 1 ENGINE. NR 2 ENGINE NORMAL. RETURNED TO GATE. REMOVED AND REPLACED THE NR 1 ENGINE IAW M-213, M-21-, AND M-215. OPS AND LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

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

Part: BULKHEAD — CRACKED (FUSELAGE)

REPAIRED CRACKED WEB AT BS 178 AROUND RIVET HEADS AT WL 234 BETWEEN RBL 5-7, RBL 17.1. INSTALLED DOUBLER AND VERIFIED NO DEFECTS AROUND CUTOUT USING HFEC METHOD, IAW ECO 3138. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (PAX CABIN)

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

Part: BATTERY PACK — INOPERATIVE (CABIN)

REPLACED LEFT OVERWING EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

REPLACED LEFT OVERWING EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: MOUNT — WORN (RT ENGINE)

DISCOVERED NR 2 ENGINE FORWARD OUTBOARD MOUNT BUSHING AND LUG ASSY WORN DURING NR 2 ENGINE TIME CHANGE. FABRICATED OVERSIZE BUSHING AND REAMED LUG ASSY IAW ECO 2129. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

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

Part: BATTERY PACK — INOPERATIVE (CABIN)

REPLACED NR 2 PROXIMITY FLOOR BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

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

Part: ENGINE — MALFUNCTIONED (NR 1)

FLT 504 - CXI-HNL - DURING THRUST REDUCTION AT TOP OF CLIMB, LOUD COMPRESSOR STALL NR 1 ENGINE, 2 MORE AT CRUISE POWER. RETURNED TO XMAS ISLAND. REMOVED FOD ON NR 1 INTAKE (ENGINE). PERFORMED/INSPECTED NR 1 ENGINE, FRONT AND BACK. GROUND RUN ENGINE AT MAX POWER SETTING AND PART POWER. NO COMPRESSOR STALL NOTED AT THE TIME. ENGINE IS WITHIN LIMIT AT DIFFERENT POWER SETTINGS, FINAL INSPECTION ON NR 1 ENGINE. OK FOR RELEASE BACK TO SERVICE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — DELAMINATION (TE FLAP)

REPAIRED RIGHT INBOARD MID-FLAP TRAILING ASSEMBLY IAW ECO 3068. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (WS 383-418)

REPAIRED RIGHT UPPER/LOWER TRAILING EDGE LOWER WING SKIN AT WS 383-418 IAW ECO 3051. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (LT WING)

REPAIRED LEFT LOWER WING SKIN AT TANK PANEL NR 7212 IAW ECO 3061. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORROSION (TE FLAP)

REPLACEMENT OF LEADING EDGE SKIN RIGHT INBOARD AFT FLAP IAW ECO 3069. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (WS 531-583)

REPAIRED RIGHT WING LOWER SKIN ALONG TRAILING EDGE IN NUMEROUS LOCATIONS BETWEEN WS 531 TO WS 583 IAW ECO 3059. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BEAR STRAP — CORRODED (BS 491)

REPAIRED FORWARD CARGO DOOR BEARSTRAP BS 491 IAW ECO 3062. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (NR 4 SLAT)

REPAIRED NR 4 SLAT TRAILING EDGE EXTRUSION IAW ECO 3057. AIRCRAFT RETURNED TO SERVICE. (M)

Part: HEAT PROBE — FAILED (LT PITOT)

FLT 505 - HNL-CXI - LEFT ELEVATOR PITOT HEAT LIGHT CAME ON IMMEDIATELY AFTER TAKEOFF. RETURNED TO HNL. UNEVENTFUL LANDING. REMOVED AND REPLACED LEFT ELEVATOR PITOT PROBE. OPS CHECK OK IAW MM 27-31-141. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 6 FLOOR LIGHT BATTERY PACK DUE TO INOPERABLE. OPS CHECK OKAY. AIRCRAFT RETURNED TO SERVICE. TAT: 31,375.7 HOURS. TAC: 37,575. (X)

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 1, 2, 3, 4, 5, AND 6 FLOOR LIGHT BATTERY PACKS DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED FORWARD CENTER AISLE LIGHT EMERGENCY BATTERY DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 1 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: LIGHT — INOPERABLE (CABIN)

REPLACED FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT ASSY DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 1 AND NR 2 FLOOR LIGHT BATTERY PACKS DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: SKIN — INOPERATIVE (NR 1 LE SLAT)

NR 1 LEADING EDGE SLAT L/E SKIN HAS 3 CLOSE DENTS 14.5 INCHES INBOARD OF SLAT OUTBOARD EDGE. HFEC REVEALED NO CRACKS AT DENTS. THREE DENTS LOCALIZED WITHIN 2 INCH AREA WITH DEEPEST POINT .067 INCH DEEP. PER SRM 57-50-1 FIG 2, DENT IS OUT OF LIMITS. REMOVED AND REPLACED NR 1 SLAT IAW MM 27-81-21. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED AFT DOOR EMERGENCY SLIDE LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 3, NR 4, NR 5 FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED LEFT OVERWING EMERGENCY SLIDE LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED AFT EMERGENCY SLIDE LIGHT BATTERY PACK DUE TO WEAK. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (SERVICE DOORWAY)

REPLACED AFT SERVICE DOOR EXIT IDENTIFIER DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (RT EMER EXIT)

REPLACED RIGHT OVERWING IDENTIFIER BATTERY PACK DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (RT EMER EXIT)

REPLACED RIGHT OVERWING IDENTIFIER DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (LT EMER EXIT)

REPLACED LEFT OVERWING IDENTIFER ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED BOTH LAMPS AT AFT ENTRY DOOR AND AFT SERVICE DOOR SLIDE LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED LEFT OVERWING SLIDE LIGHT DUE TO INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED LEFT OVERWING EMERGENCY LIGHT BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED THE FORWARD LEFT SERVICE DOOR EMERGENCY LIGHT BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED FORWARD ENTRY DOOR EXIT IDENTIFIER BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED LEFT OVERWING EMERGENCY LIGHT BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED NR 1 POSITION EMERGENCY FLOOR LIGHT DUE TO BEING 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 BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 6 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO BEING NOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED BATTERY IN NR 3 POSITION FLOOR PROXIMITY LIGHT ASSY DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRINGER — CORRODED (BS 500)

FOUND CORROSION ON STRINGER 21L BETWEEN BS 500 AND 500A IN FORWARD PIT. INSTALLED REPAIR PER SRM 53-10-3, FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRINGER — CORRODED (BS 500)

FOUND CORROSION UNDER NUT PLATE ON STRINGER 22L BETWEEN BS 500 AND 500A IN FORWARD PIT. INSTALLED REPAIR PER SRM 53-10-3, FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SPAR — CORRODED (HORIZONTAL STAB)

FOUND CORROSION ON RT SIDE HORIZONTAL STABILIZER REAR SPAR UPPER CHORD AT STAB STATION 68.14 AND STRIGNER S-1. REPAIRED PER ECO 1889R3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CRACKED (BS 663)

FOUND CRACK AT BBL .07 FLOORBEAM REPAIR AT BS 663. REPAIRED PER ECO 2223R2 FIGURE 4. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SPAR — CORRODED (RT WING)

FOUND CORROSION AT WBL 318 ON RT WING FRONT SPAR LOWER CHORD HORIZONTAL FLANGE LOWER SURFACE. REPAIRED CORROSION PER ECO 1803 R4. AIRCRAFT RETURNED TO SERVICE. (M)

Part: POWER PACK — INOPERATIVE (CABIN)

REPLACED AFT SERVICE DOOR EMERGENCY IDENTIFICATION LIGHT POWER PACK DUE TO LIGHT BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BRAKE — LEAKING (NR 3)

FLT 90 - HNL-KOA - AFTER TAKEOFF WITH GEARS AND FLAPS COMING UP, SYSTEM 'A' HYDRAULIC QUANTITY WAS DECREASING'. LANDED 26R WITHOUT INCIDENT. TOWED TO GATE. MAINTENANCE FOUND NR 3 BRAKE LEAKING. REPLACED NR 3 BRAKE ASSY AND REPLENISHED HYDRAULIC FLUID, OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 27,863:43 HOURS. TAC: 31,837. (X)

Part: MECHANISM — OUT OF ADJUST (CABIN DOOR)

HNL - FLT 302 - PILOT REPORT. DOOR ANNUNCIATOR LIGHT ILLUMINATED ON TAKEOFF. ABORTED TAKEOFF. ADJUSTED DOOR STOPS AND CAM PLATES AND OVER CENTER CONTROL ROD PER MM 52-11-0, PAGES 510-514. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X)

Part: GPS NPU — FAILED (LEFT)

HNL/CXI - FLT 505 - PILOT REPORT. NR 1 GPS ANTENNA FAILED. RETURNED TO HNL. REPLACED NR 1 GPS NPU. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

PILOT REPORT NR 1. REAR EMERGENCY FLASHLIGHT INOPERABLE. REPLACED FLASHLIGHT BATTERY SYSTEM. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 27,643:24 HOURS. TAC: 31,440. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK FOUND AFT EMERGENCY EXIT LIGHT INOPERABLE. REPLACED BATTERY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 27,598:44 HOURS. TAC: 31,365. (X)

Part: HANDLE — OPENED (PAX DOOR)

FLT 217 - HNL-OGG - MAIN CABIN DOOR HANDLE OPENED DURING LANDING ROLL. ADJUSTED UPPER CAMS ON FWD ENTRY DOOR. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING OVERNIGHT CHECK, REPLACED FORWARD SERVICE DOOR EMERGENCY S.L. EXIT LIGHT ASSY DUE TO GREEN LIGHT STAYS ON. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 26,767:13. TAC: 29,791. (X)

Part: EXIT SIGN — INOPERATIVE (CABIN)

DURING OVERNIGHT CHECK, REPLACED FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT IDENTIFIER DUE TO INOP. OPS CEHCK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — DAMAGED (BS 887)

DURING HEAVY MAINTENANCE VISIT, FUSELAGE SKIN DAMAGE CAUSED BY OVERHEAD SAFETY CABLE LATCH CONTACT DURING TAILSTAND REMOVAL BS 887 BETWEEN STR 7R AND STR 8R. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. NRTC NR 019329. (X)

Part: KEEL BEAM — CRACKED (BS 663.75-727)

DURING CORROSION PHASE 1 INSPECTION, KEEL BEAM WAS FOUND BUCKLING IN 4 PLACES BETWEEN BS 663.75 TO BS 727. ONE CRACK WAS FOUND AND REPAIRED WITH A DOUBLER PER ECO 2352 R4, PART III.B. TAT: 29,591:17 HOURS. TAC: 29,409. (X)

Part: REAR SPAR — CORRODED (HORIZ STAB)

DURING HEAVY MAINTENANCE VISIT, EXFOLIATION NOTED ON LEFT HORIZONTAL STABILIZER LOCATED AT ELEVATOR STATION 42 ON REAR SPAR, UPPER CHORD REPAIRED AS PER ECO 1889 R3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (WS 440)

DURING HEAVY MAINTENANCE VISIT, FOUND RIGHT OUTBOARD WING MAIN WING BOX LOWER SKIN CORROSION AT WS 440. REPAIRED PER ECO NR 1684 R7. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (RT WING)

DURING HEAVY MAINTENANCE VISIT, REFERENCE EA 737-57-007, PERMANENT REPAIR TO RT WING LOWER SKIN TRAILING EDGE BETWEEN RSS 484 AND 583. REPAIRED PER ECO NR 2782. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BUSHING — WORN (HORIZ STAB)

DURING HEAVY MAINTENANCE VISIT, FOUND HORIZONTAL STABILIZER JACKSCREW ACTUATOR SUPPORT FITTING RT BORE BUSHING WORN. REPAIRED PER ECO2784. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — GOUGED (BS 807)

DURING HEAVY MAINTENANCE VISIT, PERMANENT REPAIR TO FUSELAGE SECTION 46 GOUGE BLENDOUT ADJACENT EXISTING REPAIR BS 807, S25R-S27R. REPAIRED PER ECO2783. AIRCRAFT RETURNED TO SERVICE. (M)

Part: NUT — LOOSE (TE FLAPS)

DURING PREFLIGHT CHECK DISCOVERED, RIGHT AILERON AND TAB DAMAGED. SUBSEQUENT INSPECTION REVEALED NR 8 FLAP TRANSMISSION SPLINED COUPLING RETAINING NUT BACKING OFF CAUSING DAMAGES TO THE ABOVE. REPLACED NR 8 AND NR 7 FLAP TRANSMISSIONS FOR PRECAUTIONARY, TORQUE CHECK ACCOMPLISHED ON FLAP DRIVE COUPLING NUTS. REPLACED DAMAGED RIGHT T/E FLAP MID FLAP, AILERON, AND TAB ASSY. PERFORMED TEST FLIGHT AND AIRCRAFT RETURNED TO SERVICE. (M)

Part: BEAM — CORRODED (LT HORIZ STAB TE)

DURING HEAVY MAINTENANCE VISIT, LEFT HORIZONTAL STABILIZER TRAILING EDGE BEAM UPPER SURFACE EXFOLIATION CORROSION NOTED AT ES 145. REPAIRED PER ECD 1584R3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (RT WING)

DURING HEAVY MAINTENANCE VISIT, RT WING LOWER EXTERIOR SURFACE EXFOLIATION CORROSION NOTED JUST AFT OF NR 6 SLAT TELESCOPING DUCT. REPAIRED EPR ECO 1684R6. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BEAM — CORRODED (LT HORIZ STAB TE)

DURING HEAVY MAINTENANCE VISIT, LEFT HORIZONTAL STABILIZER TRAILING EDGE BEAM UPPER SURFACE EXFOLIATION CORROSION NOTED AT ES 176.64. REPAIRED PER ECO 1584R3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BEAM — CORRODED (LT HOR STAB TE)

DURING HEAVY MAINTENANCE VISIT, LEFT HORIZONTAL STABILIZER TRAILING EDGE BEAM UPPER SURFACE FILIFORM CORROSION NOTED AT ES 94.07. REPAIRED PER ECO 1584R3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ATTACH FINGER — CORRODED (BS 1016)

DURING HEAVY MAINTENANCE VISIT, DISCOVERED EXFOLIATION CORROSION ON BS 1016 ATTACH FINGER AT STRINGER 17R. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BEAM — CORRODED (LT HORIZ STAB TE)

DURING HEAVY MAINTENANCE VISIT, LEFT HORIZONTAL STABILIZER TRAILING EDGE BEAM UPPER SURFACE EXFOLIATION CORROSION NOTED AT ES 149.12. REPAIRED PER ECO 1584R3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LINK ASSY — BROKEN (NLG DOOR)

KOA/HNL - FLT 207 - PILOT REPORT, NOISE AND VIBRATION ABOVE 230 KNOTS IN-FLIGHT FROM FORWARD NOSE WHEEL AREA. REPLACED NOSE GEAR DOOR RT UPPER LINK. NOSE GEAR RETRACTION COMPLETED. INSPECTED DOOR, OPS CHECKED OKAY. NO OTHER DAMAGE NOTED IN NOSE AREA. OKAY FOR SERVICE. AIRCRAFT RETURNED TO SERVICE. (X)

Part: HYD LINE — FAILED (NLG)

PILOT REPORT FLT 97 - HNL-LIH - NOSE GEAR WOULD NOT COME UP AFTER TAKEOFF. RETURNED TO HNL. FOUND RUPTURED LINE ON DOWNLOCK ACTUATOR. REPLACED LINE. OPS AND LEAK CHECK OK. AIRCRAFT RETURNED TO SREVICE. (Z)