N807AL

Part: HOSE — LEAKING (HYD SYSTEM)

NON-ETOPS FLIGHT 88 LIH-HNL - AFTER GEAR UP, HYD PRESSURE INDICATOR SHOWED ZERO. LEFT MAIN LANDING GEAR INDICATOR LIGHTS SHOWED BOTH RED AND GREEN (UNSAFE). WHEN EXTENDING FLAPS AND GEAR, HYD SYSTEM A PRESSURE FLUCTUATED AND A SYSTEM LOW PRESSURE CAUTION LIGHT ILLUMINATED. PRESSURE RETURNED TO NORMAL AFTER GEAR AND FLAPS WERE EXTENDED. CREW LANDED IN HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED A LEAKING HYDRAULIC LINE BETWEEN THE LEFT HAND MAIN LANDING GEAR AND TRANSFER TUBE. LEAK CHECKED OK AND PERFORMED ENGINE RUN AND FUNCTION CHECK OF FLIGHT CONTROLS. AIRCRAFT RETURNED TO SERVICE.

Part: FILTER — CONTAMINATED (HYD SYSTEM)

NON-ETOPS FLIGHT 278 HNL - KOA, AFTER TAKEOFF, NR 1 ENGINE HYDRAULIC SYSTEM A LOW PRESSURE LIGHT ILLUMINATED. CREW DISENGAGED ENGINE DRIVEN HYDRAULIC PUMP AND RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND CHANGED HYDRAULIC SYSTEM A CASE DRAIN FILTERS, PRESSURE MODULE FILTERS AND RETURN FILTER. LEAK CHECK OK. NO FLUID CONTAMINATION NOTED. MAINTENANCE CONDUCTED A GEAR SWING CHECK WITH NO DEFECTS FOUND. AIRCRAFT WAS RETURNED TO SERVICE.

Part: CIRCUIT BREAKER — FAILED (MLG)

FLT 71 OGG-HNL, AFTER DEPARTURE, CREW WAS UNABLE TO MOVE LANDING GEAR LEVER TO THE UP POSITION. CREW FOUND CIRCUIT BREAKER POPPED OUT AND THEN RESET IT. GEAR HANDLE WAS THEN MOVED TO THE UP POSITION. THE FLIGHT CONTINUED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CIRCUIT BREAKER AND PERFORMED A GEAR SWING TEST AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LANDING GEAR — MALFUNCTIONED

GEAR WOULD NOT RETRACT ON T/O FROM KONA. ISOLATION VALVE LIGHT CAME ON AND GEAR HANDLE COULD NOT BE RAISED PAST THE OFF POSITION. WITH GEAR HANDLE DOWN, WE HAD NO GEAR LIGHTS. VISUALLY CHECKED GEAR DOWN AND LANDED AT KONA. INSPECTED LANDING GEAR SYSTEM AND FOUND LANDING GEAR LIGHTS CIRCUIT BREAKER OPEN. RESET CIRCUIT BREAKER AND CHECKED OK. NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: ELEMENT — FAILED (NR 2 ENG OVRHT)

DURING PUSHBACK AND PRIOR TO ENGINE START, THE CREW NOTED NR 2 ENGINE OVERHEAT INDICATION ILLUMINATED. THE CREW COMPLETED THE ENGINE OVERHEAT AND ENGINE FIRE CHECK LISTS AND DISCHARGED BOTH ENGINE FIRE EXTINGUISHER BOTTLES. AFTER DISCHARGING THE BOTTLES, THE INDICATION REMAINED ILLUMINATED. RETURNED TO GATE. MAINTENANCE R & R NR 2 ENGINE LOWER FIRE AND OVERHEAT ELEMENT. ENGINE RUN OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — DIRTY (OVERHEAT LOOP)

ON CLIMB BETWEEN 11,000 FT AND 13,00 FT, PILOTS REPORTED NR 2 ENGINE OVERHEAT LIGHT FLICKERING AND THEN BECOMING STEADY. THE ENGINE OVERHEAT CHECKLIST WAS COMPLETED AND LIGHT WAS EXTINGUISHED. ENGINE WAS NOT SHUTDOWN, EMERGENCY DECLARED, AND THE AIRCRAFT RETURNED UNEVENTFULLY. CLEANED NR 2 ENGINE LOWER LOOP OVERHEAT DETECTION CONNECTORS. NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: SLIDE — DEPLOYED (FWD SVC DOOR)

DURING GROUND MAINTENANCE, GROUND CREW INADVERTENTLY DEPLOYED THE FORWARD SERVICE DOOR ESCAPE SLIDE. NO INJURIES. REMOVED AND REPLACED THE FORWARD SERVICE DOOR SLIDE IN ACCORDANCE WITH MM 25-61-200.

Part: TRANSMITTER — INOPERATIVE (NR 1 ENG EPR) · airframe 40,378 hrs · 60,053 cycles

ON TAKE-OFF ROLL THE NR 1 ENGINE ONLY INDICATED 1.76 EPR; THE THROTTLES WERE ADVANCED WITH NO RESPONSE FROM ANY INSTRUMENTS. REJECTED TAKE-OFF AND RETURNED TO GATE. REPLACED THE NR 1 ENGINE EPR TRANSMITTER AND CLEARED THE PT2 INLET PROBE OF DEBRIS. RAN NR 1 ENGINE TO REFERENCE PARAMETERS IAW AMM 73-20-00, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BEARING — FAILED (NR 2 ENG GBOX) · airframe 39,983 hrs · 59,179 cycles

NON-ETOPS FLIGHT 206, HNL-OGG: ON DESCENT ONTO OGG THE NR 2 ENGINE OIL PRESSURE LIGHT CAME ON, THE OIL PRESSURE DECREASED TOWARD ZERO AND THE OIL QUANTITY BEGAN DROPPING WITH THE OIL TEMPERATURE IN THE NORMAL RANGE. FOLLOWED QRH AND SHUT DOWN THE NR 2 ENGINE. REMOVED AND REPLACED THE NR 2 ENGINE IAW FORM M-211, 212, 213, 214 AND 215. LEAK AND OPS CHECK GOOD. INSPECTION OF GEARBOX INDICATED REAR LUBE OIL PUMP DRIVE SHAFT BEARING FAILURE. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE)

FOUND AN INCH AND A HALF AND A TWO INCH FUSELAGE CRACK AT BS 767 AND BS 792, ON STRINGER 18L. TRIMMED OUT CRACKS AND VERIFIED CUTOUTS USING HFEC METHOD, NO DEFECTS NOTED. FABRICATED AND INSTALLED STRUCTURAL AND TAPERED FILLERS, DOUBLER, AND TRIPLER FROM CLAD 2024 T3. CLEANED AND TREATED ALL EXPOSED SURFACES. REPAIR COMPLETED IAW SRM 53-30-3 FIGUR 48. AIRCRAFT RETURNED TO SERVICE. (M)

Part: DUCT — FAILED (NR 1 ENGINE)

FLT 240 - HNL-OGG - ENGINE NR 1 OVERHEAT LIGHT CAME ON JUST AFTER TAKEOFF. PULLED THROTTLE BACK AND THE LIGHT WENT OUT. EGT IN GREEN THE ENTIRE TIME. REMOVED AND REPLACED NR 1 COWL ANTI-ICE UPPER DUCTING. LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: HOSE — FAILED ("A" HYD SYSTEM)

AFTER GEAR RETRACTION LOST ENTIRE 'A'SYSTEM HYD QTY. MAINTENANCE REPLACED LEFT MAIN GEAR UPLOCK ACTUATOR PRESSURE RETURN HOSE ASSEMBLY. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

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

Part: SKIN — DENTED (NR 2 SLAT)

GAINED ACCESS TO DENTED AREA. CUTOUT DAMAGE BY SLICING THE LEADING EDGE SKIN PER FIGURE 1. INSTALLED A SPLICE REPAIR AT SS205.46 AND SS 238.71. REPAIR COMPLETED IAW SRM 57-50-3, FIGURE 7 AND ECO 3354. AIRCRAFT RETURNED TO SERVICE. (M)

Part: GUIDE — MISALIGNED (SERVICE DOOR)

AFTER TAKEOFF, THE CABIN HAD AN EXCESSIVE RATE OF CLIMB, (2,500 FPM). AUTO FAILED ON THE PRESSURIZATION SYSTEM. LANDED HNL WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE FORWARD SERVICE DOOR WAS IMPROPERLY CLOSED AND LOWER LEFT GUIDE MISALIGNED. MAINTENANCE REALIGNED THE DOOR GUIDE. GROUND OPERATIONAL AND PRESSURIZATION CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: STRAP — CORRODED (FUSELAGE)

KEEL BEAM VERTICAL STRAP CORRODED AT BS 532. BLENDED AND FLAP PEENED REPAIR AREA, FABRICATED TWO FILLER STRAPS, INSTALLED FILLERS AND STRAP.

Part: STRINGER — CORRODED (FUSELAGE)

FOUND CORROSION ON BS 500 AT STRINGER 26R. CUT AND REMOVED DAMAGED PORTION OF FORMED SECTION. FABRICATED REPAIR ANGLES AND DOUBLER IAW SRM. REPAIR COMPLETED IAW SRM. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE)

SKIN CRACK AT BS 380 BETWEEN STRINGER 28L AND 28R. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER, AIRCRAFT RETURNED TO SERVICE.

Part: STRINGER — CRACKED (FUSELAGE)

CRACK LOCATED AT BS 767, S-14L. TRIMMED OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND REPAIR ANGLES.

Part: STRINGER — CRACKED (FUSELAGE)

CRACKS BS 739, S-18R AND BS 745, S-19R. REMOVED DAMAGED AREA, VERIFIED CRACK REMOVAL USING HFEC METHOD, FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: SKIN — CRACKED (FUSELAGE)

REPAIRED 2.5 INCH LONG SKIN CRACK AT FUSELAGE BS 937 STRINGER 26R. CONFIRMED 2.5 INCH REMOVED USING HFEC METHOD. THE REPAIR CONSISTED OF CUTTING OUT THE SKIN CRACK AND FABRICATING A DOUBLER IAW SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: SKIN — CRACKED (FUSELAGE)

FOUND FUSELAGE CRACKED AT BS 767, S19L. TRIM OUT CRACK COMPLETED AND VERIFIED CUT OUT USING HFEC METHOD, NO DEFECTS NOTED. FABRICATED AND INSTALLED REPAIR DOUBLER. CLEANED AND TREATED ALL EXPOSED SURFACES IAW SRM 53-30-3 FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: SPAR — CORRODED (RT WING)

IDENTIFIED CORROSION AT RT WING FRONT SPAR LOWER CHORD FSS 475. REPAIRED CONSISTS OF REMOVING DAMAGED AREA AT HORIZONTAL FLANGE AND INSTALLING A TAPERED FILLER, HFEC COMPLETED ON ALL FASTENER HOLES AND REWORKED AREA. NO DEFECTS NOTED. CLEAN AND TREATED ALL EXPOSED AREAS AND INSTALLED DOUBLER NESTED ANGLES TO COMPLETE REPAIR. (M)

Part: KEEL — CORRODED (FUSELAGE)

IDENTIFIED CORROSION AT THE VERTICAL LEG OF THE KEEL BEAM AT BS 535 APPROXIMATELY LBL 6.30. REPAIRED BY REMOVING CORROSION, BLEND OUT COMPLETED, CLEANED AND TREATED AFFECTED AREA. REPAIR COMPLETED ON 12/26/00, IAW SRM 51-10-6. (M)

Part: SKIN — CRACKED (FUSELAGE)

IDENTIFIED 3.7 INCH CRACK AT BS 747, STRINGER 18L. CONFIRMED USING HFEC METHOD. (M)

Part: BEAM — GOUGED (MLG)

REPAIRED LT MLG BEAM AT THE OUTBOARD STABILIZER ATTACH POINT. REPAIR CONSISTS OF BLENDING OUT GOUGE AND REAMING OUT FASTENER HOLES AND INSTALLATIONS OF BUSHINGS IAW ECO 3146. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

REPAIRED FUSELAGE SKIN 3 INCH CRACK AT BS 886 STRINGER 24 IAW SRM 53-30-3 FIG 1. VERIFIED BY HFEC METHOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: SKIN — CRACKED (FUSELAGE)

REPAIRED 1.5 INCH CRACK ON FUSELAGE SKIN AT BS 744, STRINGER 19L IAW SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

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

Part: BATTERY PACK — INOPERATIVE (CABIN)

REPLACED THE FORWARD ENTRY EXIT IDENTIFIER POWER PACK DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

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

Part: BATTERY PACK — INOPERATIVE (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: BLEED VALVE — FAILED (NR 2 ENGINE)

FLT 263 - HNL-LIH - COMPRESSOR STALL NR 2 ENGINE THROTTLE UP OFF OF IDLE. ABORTED TAKEOFF. RETURNED TO GATE. REMOVED AND REPLACED NR 2 ENGINE PRESSURE BLEED CONTROL VALVE. SYSTEM LEAK CHECK AND OPS CHECK GOOD PER MM 75-31-11. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: SKIN — CRACKED (BS 947)

FOUND 4.125 INCH CRACK 2 INCH FORWARD OF BS 947 AT STRINGER 24L. SKIN REPAIR IAW SRM 53-30-3 FIGURE 6 SHEET 4 PAGE 12B. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED NR 6 POSITION FLOOR EMERGENCY LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLAP — CRACKED (LT TE MID FLAP)

LEFT OUTBOARD MID FLAP CRACKED AT AFT FLAP INBOARD TRACK ATTACH POSITION. CRACKED AT BOTH INBOARD AND OUTBOARD TRACK ARM POSITION. REMOVED AND REPLACED MID FLAP IAW 27-51-72, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BUSHING — CORRODED (VERTICAL FIN)

VERTICAL FIN AFT SIDE OF RIGHT OUTBOARD AFT SPAR ATTACH FITTING CORRODED UNDER BUSHING FLANGE. REPAIR IAW ECO 2973. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FRAME — CRACKED (CARGO DOOR)

AFT CARGO DOOR FORWARD FRAME SUSPECT 3 CRACKS RADIATING FROM BOLT HOLE IN CENTER OF FORWARD FRAME. REPAIRED IAW ECO 2971. AIRCRAFT RETURNED TO SERVICE. TAT: 30,874.2 HOURS. TAC: 38,783. (X)

Part: FRAME — CRACKED (CARGO DOORWAY)

FORWARD CARGO PIT DOOR LOWER AFT CORNER FRAME CRACKED. REPAIRED IAW ECO 1988R1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WASHER — DEFECTIVE (HORIZ STABILIZER)

HORIZONTAL STABILIZER AFT ATTACH FITTINGS UPPER AND LOWER BOLTS HAVE MIGRATING WASHERS UNDER THE NUTS. REPAIR IAW ECO 2975. AIRCRAFT RETURNED TO SERVICE. TAT: 30,874.2 HOURS. TAC: 38,783. (X)

Part: BUSHINGS — CORRODED (VERTICAL FIN)

FUSELAGE LUGS FOR VERTICAL FIN AFT SPAR ATTACH HAVE HEAVY FRETTING ON FACES ON BUSHINGS. REPAIRED PER ECO 2978. AIRCRAFT RETURNED TO SERVICE. (M)

Part: PANEL — CORRODED (RT WING)

RIGHT WING LOWER ACCESS PANEL CUT-OUT AT PANEL NR 7406 CORRODED. BLENDED OUT CORROSION PER SRM 57-30-3, AND AREA RE-ASSESSED BEYOND LIMITS PER SRM 57-30-3. FILLER FABRICATED IAW ECO 2869 PT1. AREAS REFINISHED WITH BMS 10-20 TYPE II PER MM 53-42-11. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED FORWARD SLIDE LIGHT BATTERY PACK DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 5 FLOOR LIGHT BATTERY PACK FOR RETIREMENT. REPLACED BATTERY, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SWITCH — MALFUNCTIONED (NR 1 ENGINE)

FLT 297 - OGG-HNL - ON CLIMB-OUT, NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. REDUCED NR 1 ENGINE THROTTLE TO IDLE AND LIGHT STAYED ON. NR 1 ENGINE WAS SHUT DOWN IAW THE QRH. EMERGENCY DECLARED AND UNEVENTFUL LANDING MADE AT HNL. INSPECTED OIL FILTER ON NR 1 ENGINE. NO CLOGGING FOUND. PERFORMED OPERATIONAL CHECK OF BYPASS SWITCH. SYSTEM CHECK OK. AS A PRECAUTION, REPLACED ENGINE OIL BYPASS SWITCH IAW MM 79-35-0. GROUND OPS CHECK AND LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (NR 2 POS)

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

Part: LIGHT — INOPERATIVE (FD ENTRY)

REPLACED EMERGENCY EXIT LIGHT AT FORWARD ENTRY DOOR DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 4 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (BS 787)

FUSELAGE SKIN CRACK APPROXIMATELY 2.5 INCHES LONG AT BS 787 AND STR 18L. VERIFIED CRACK USING HIGH FREQUENCY EDDY CURRENT. REPAIRED PER SRM 53-30-3 FIG 1. AIRCRAFT RETURNED TO SERIVCE. TAT: 29,087.1 HRS. TAC: 34,722. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 1 POSITION EMERGENCY FLOOR LIGHT ASSY, INOPERABLE. REPLACED BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 6 POSITION EMERGENCY FLOOR LIGHT ASSY, INOPERABLE. REPLACED BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

OUTSIDE LEFT SIDE OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY POWER SUPPLY. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED NR 5 POSITION EMERGENCY FLOOR LIGHT ASSY DUE TO YELLOW LED STAYING ON ALL THE TIME IN POSITION. OPS CHECKED OK AIRCRAFT RETURNED TO SERVICE. (M)

Part: BUSHING — CORRODED (RT HORIZ STAB)

HORIZONTAL STABILIZER RT SIDE UPPER AFT BUSHING CORRODED. REPAIRED BUSHING PER ECO 2895. BLEND OUT DIMENSION 1.2560 INCH BY 1.2640 INCH. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FRAME — CORRODED (CARGO DOORWAY)

APPLIED PREVENTATIVE MODIFICATION TO AFT LOWER CARGO DOORWAY FORWARD AND AFT BODY FRAMES PER ECO 1474R9. DEVIATION 'F' APPLIED TO ECO 1474R9 INSTRUCTIONS DUE TO CORROSION ON FORWARD FRAME WEB. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FITTING — CORRODED (BS 1016)

FOUND CORRODED END FITTING AT BS 1016 AFT PRESSURE BULKHEAD AND STRINGER 20L. REPLACED FITTING PER ECO 2894. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORROSION (WS 495)

CORROSION FOUND ON LEFT SIDE OUTBOARD WING LOWER SKIN AT WING STATION 495. REWORKED AREA PER ECO 1684R8 AND DEVIATION 'F' FOR ECO 1684R8. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (BS 850)

ON SERVICE CHECK, FUOND A FUSELAGE SKIN CRACK AT BS 850 STRINGER 21R. REPAIRED PER SRM 53-30-3 FIG 6. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND LT OVERWING EMERGENCY LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 28,188:25 HOURS. TAC: 32,705. (X)

Part: BULB — FAILED (CABIN)

ON SERVICE CHECK, FOUND LEFT WING EMERGENCY SLIDE LIGHT INOP. REPLACED BULB. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SIGN — BROKEN (CABIN)

ON SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY LIGHT BROKEN. REPLACED LIGHT ASSEMBLY. OPS CHECK GOOD. AIRCRAFT REUTRNED TO SERVICE. TAT: 28,070:37 HOURS. TAC: 32,446. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND FORWARD SLIDE LIGHT INOPERABLE, REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 28,063:56 HOURS. TAC: 32,432. (X)

Part: FLOOR BEAM — CORRODED (BS 294)

UPON INSPECTION OF ECO 2317 BS 294.5 FLOOR BEAM FOR CRACKS, CORROSION WAS FOUND AT BS 294.5 STR 17R. REPAIRED PER ECO 2867. AIRCRAFT RETURNED TO SERVICE. TAT: 28,046:22 HOURS. TAC: 32,394. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND THE NR 6 POSITION EMERGENCY FLOOR LIGHTING INOPERABLE. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 28,046:22 HOURS. TAC: 32,394. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND THE NR 1 POSITION EMERGENCY FLOOR LIGHTING INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 28,046:22 HOURS. TAC: 32,394. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND THE NR 5 POSITION EMERGENCY FLOOR LIGHTING INOPERABLE. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 28,046:22 HOURS. TAC: 32,394. (X)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

ON SERVICE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INTERMITTENT. REPLACED POWER SUPPLY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: SOLENOID — MALFUNCTIONED (LANDING GEAR)

FLT 201 - HNL-LIH - LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION AFTER TAKEOFF. COMPLIED WITH QRH, NO HORN AFTER FLAPS RETRACTED PROBLEM WITH LEVER LACKING SOLENOID. JACKED AIRCRAFT, NOTED SAFETY SOLENOID ENGAGED ON LANDING LEVER. PERFORMED AIR SAFETY SENSOR ADJ/TEST IAW MM 32-09-200. AIRCRAFT RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

ON SERVICE CHECK, FOUND LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY POWER SUPPLY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

ON SERVICE CHECK, FOUND FORWARD EMERGENCY SLIDE LIGHT INOP. REPLACED BATTERY POWER SUPPLY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING OVERNIGHT CHECK, REPLACED BATTERY POWER SUPPLY FOR LT EXTERIOR OVERWING EMERGENCY LIGHT DUE TO LIGHT REMAINS ON. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 27,780:23 HOURS. TAC: 31,804. (X)

Part: LIGHT — INOPERATIVE (CABIN)

DURING OVERNIGHT CHECK, REPLACED RT OVERWING EXIT IDENT LIGHT ASSY DUE TO INOPERABLE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 27,690:21 HOURS. TAC: 31,613. (X)

Part: BATTERY — DISCHARGED (CABIN)

DURING OVERNIGHT CHECK, REPLACED BATTERY FOR ROW 8 EMERGENCY FLOOR PROX LIGHT ASSY DUE TO INOP. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FRAME — CRACKED (CARGO DOORWAY)

DURING SCHEDULED INSPECTION OF AFT LOWER CARGO DOORWAY, FORWARD AND AFT BODY FRAME (FAA AD 93-14-10 AMDT 39-8-8634), FOUND CRACK PROPAGATING FROM UNDER NR 5 STOP ON AFT BODY FRAME. JFEC CONFIRMED. REPLACED AFT BODY FRAME PER ECO 1474R7. AIRCRAFT RETURNED TO SERVICE. TAT: 27,199:07 HOURS. TAC: 30,493. (X)

Part: BATTERY — DISCHARGED (CABIN)

DURING OVERNIGHT CHECK, REPLACED ROW 22 EMERGENCY FLOOR LIGHT BATTERY DUE TO INOPERABLE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 27,199:07 HOURS. TAC: 30,493. (X)

Part: LIGHT — INOPERATIVE (CABIN)

DURING OVERNIGHT CHECK, ADJUSTED FORWARD ENTRY DOOR EMERGENCY EXIT IDENTIFIER DUE TO INOPERABLE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 27,199:07 HOURS. TAC: 30,493. (X)

Part: COMPRESSOR — STALLED (ENGINE)

HNL/KOA - FLT 86 - PILOT REPORT, LOUD BANG AND YAW PASSING 9,000 FEET AFTER TAKEOFF. ENGINE INSTRUMENTS LOOK NORMAL. RETURNED TO HNL. VISUALLY INSPECTED BOTH ENGINES, FUSELAGE, AND CONTROL SURFACES. NO VISUAL DEFECTS NOTED. EXERCISED FLIGHT CONTROLS AND VERIFIED CONTROL SURFACE MOVEMENT. ACCOMPLISHED RUN-UP OF BOTH ENGINES. ALL PARAMETERS NORMAL. OK FOR SERVICE. (X)

Part: SKIN — CRACKED (BS 787)

DURING OVERNIGHT CHECK, FOUND FUSELAGE SKIN CRACK .50 INCH LONG AT BS 787 + 3 INCHES APPROXIMATELY 1 INCH BELOW S17L. CONFIRMED BY HFEC. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. TAT: 27,160:45 HOURS. TAC: 30,404. (X)

Part: FUEL SHUTOFF VLV — INOP (NR 1 ENGINE)

FLT 302 - HNL-OGG - AFTER TAKEOFF, THE NR 1 FUEL VALVE CLOSED LIGHT ILLUMINATED BRIGHT. ALL ENGINE INDICATIONS REMAINED NORMAL. RETURNED TO HNL. REMOVED AND REPLACED NR 1 ENGINE FUEL SHUTOFF VALVE IAW MM 28-22-11. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FAIRING SEAL — MISSING (RT WING/FUS)

FLT 257 - HNL-LIH - RECURRING VIBRATION, LOUD HIGH FREQUENCY VIBRATIONS FROM RIGHT SIDE WING ROOT AREA. STARTED AT 11,000 FEET DURING CLIMB AND STOPPED AT 9,000 FEET. DURING DESCENT, VIBRATION FELT IN NR 2 THRUST LEVER AND CABIN FLOOR. VIBRATION NOTICED WITH HIGHER SPEED ONLY, STARTED AT 310 KNOTS AND STOPPED AT 270 KNOTS. FOUND AERODYNAMIC MOISTURE SEAL PORTION MISSING FROM RT FORWARD WING-TO-BODY FAIRING. COVERED AREA WITH SPEED TAPE. (M)

Part: STALL WARN MOD — MALFUNCTIONED (STALL WARN SYST)

ITO/HNL - FLT 437 - PILOT REPORT. DURING TAKEOFF, ROLL 'WINDSHEAR INOP' LIGHT CAME ON. TAKEOFF CONTINUED, AND AFTER BECOMING AIRBORNE, STICK SHAKER BEGAN. AIRSPEED APPROXIMATELY 140 KNOTS TO 150 KNOTS. MOVING STALL WARNING SWITCH TO 'TEST' POSITION STOPPED SHAKER. EMERGENCY DECLARED. RETURNED TO ITO. LANDING NORMAL. REPLACED STALL WARN MOD AND AOA SENSOR, FUNCTIONAL CHECK IAW MM 27-32-0 OK. WINDSHEAR BITE CHECK OK. AIRCRAFT RETURNED TO SERVICE. REFERENCE CONTROL NR TSAA9534126.

Part: AOA SENSOR — MALFUNCTIONED (STALL WARN SYST)

ITO/HNL - FLT 437 - PILOT REPORT. DURING TAKEOFF, ROLL 'WINDSHEAR INOP' LIGHT CAME ON. TAKEOFF CONTINUED, AND AFTER BECOMING AIRBORNE, STICK SHAKER BEGAN. AIRSPEED APPROXIMATELY 140 KNOTS TO 150 KNOTS. MOVING STALL WARNING SWITCH TO 'TEST' POSITION STOPPED SHAKER. EMERGENCY DECLARED. RETURNED TO ITO. LANDING NORMAL. REPLACED STALL WARN MOD AND AOA SENSOR, FUNCTIONAL CHECK IAW MM 27-32-0 OK. WINDSHEAR BITE CHECK OK. AIRCRAFT RETURNED TO SERVICE. REFERENCE CONTROL NR 95ZZZX3970. (X)