N804AL

Part: SKIN — CRACKED (FUSELAGE)

REPAIRED FUSELAGE SKIN CRACK, BELOW THE LAP JOINT, AT BS 727 S-15R. TRIMMED OUT CRACK DAMAGE, VERIFIED WITH HFEC. FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLER IAW ECO 3257. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

REPAIRED 2 INCH SKIN CRACK AT BS 867 S-22R. TRIMMED OUT CRACK AND VERIFIED WITH HFEC, NO DEFECTS NOTED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-1 FIG 1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

REPAIRED 2.25 INCH FUSELAGE SKIN CRACK AT BS 927 S-24R. TRIMMED OUT CRACK DAMAGE AND VERIFIED WITH HFEC, NO DEFECTS NOTED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-1 FIG 1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (RT WING)

RIGHT WING SKIN HAS EXFOLIATION CORROSION AT WBL 326 LOWER SURFACE SKIN AFT OF REAR SPAR. CLEANED UP AND EVALUATED WITHIN LIMITS IAW SRM 57-3000-01. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (RT WING)

RIGHT WING SKIN HAS EXFOLIATION CORROSION AT WBL 330 LOWER SURFACE SKIN AFT OF REAR SPAR. CLEANED UP AND EVALUATED WITHIN LIMITS IAW SRM 57-3000-01. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (RT WING)

RIGHT WING SKIN HAS EXFOLIATION CORROSION AT WBL 166 LOWER SURFACE SKIN FORWARD SPAR CHORD. CLEANED UP WITHIN LIMITS IAW SRM 57-300-01. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED FORWARD OVERHEAD EMERGENCY AISLE LIGHT ASSEMBLY PACK DUE TO NO TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

REPLACED NR 2 AND NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (BS 727)

IDENTIFIED 1.5 INCH FUSELAGE SKIN CRACK AT BS 727, S16R. REMOVED TWO PREVIOUS REPAIRS IN THE IMMEDIATE AREA, TRIM OUT DAMAGED AREA, HFEC INSPECTION COMPLETED AROUND TRIM AREA NO DEFECTS NOTED, .040 INCH INSURANCE CUT COMPLETED, VISUALLY INSPECTED AREA UNDER REPAIR DOUBLERS NO DEFECTS NOTED, FABRICATED AND INSTALLED .032 INCH 2024-T3 DOUBLER AND .050 INCH 2024-T3 TRIPLER, FINISHED ALL BARE ALUMINUM WITH ALODINE AND TWO COATS OF BMS 10-11 TYPE 1 PRIMER, INSTALLED COUNTERSINK REPAIR WASHERS AT EXISTING COUNTERSINK LOCATIONS UNDER REPAIR DOUBLER, INSTALLED REPAIR PARTS WITH BMS 5-95 SEALANT BETWEEN FAYING SURFACES AND AROUND EDGES OF REPAIR. INSTALLED ALL FASTENERS WET WITH BMS-5-95 SEALANT, APPLIED CORROSION INH

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 1, NR 2 AND NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRINGER — DAMAGED (FUSELAGE)

FABRICATED AND INSTALLED STRIGNER S21R BETWEEN BS 947 TO BS 967 DUE TO RUPTURED PORTABLE WATER TANK, IAW SRM 53-10-3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: REGULATOR — INOPERATIVE (AFT FUSELAGE)

FLT 124 - HNL-KOA - DURING CLIMB-OUT FROM HNL, THE CREW HEARD A LOUD BANG FROM THE AFT SECTION OF THE AIRCRAFT. CREW REPORTED ALL INDICATIONS NORMAL. CAPTAIN DECLARED AN EMERGENCY. RETURNED TO HNL FOR AN UNEVENTFUL LANDING. FOUND THE POTABLE WATER TANK RUPTURED. STRUCTURAL DAMAGE NOTED AT S21R, S24R, S25R, S26R AND ELECTRICAL CONDUIT. FOUND THE PRESSURE REGULATOR STUCK OPEN AND PRESSURE RELIEF VALVE STUCK CLOSED. WILL REPLACE THE WATER TANK, PRESSURE REGULATOR, PRESSURE RELIEF VALVE, ANC CHECK VALVE. STRUCTURAL DAMAGE UNDER REPAIR. (M)

Part: RELIEF VALVE — INOPERATIVE (AFT FUSELAGE)

FLT 124 - HNL-KOA - DURING CLIMB-OUT FROM HNL, THE CREW HEARD A LOUD BANG FROM THE AFT SECTION OF THE AIRCRAFT. CREW REPORTED ALL INDICATIONS NORMAL. CAPTAIN DECLARED AN EMERGENCY. RETURNED TO HNL FOR AN UNEVENTFUL LANDING. FOUND THE POTABLE WATER TANK RUPTURED. STRUCTURAL DAMAGE NOTED AT S21R, S24R, S25R, S26R AND ELECTRICAL CONDUIT. FOUND THE PRESSURE REGULATOR STUCK OPEN AND PRESSURE RELIEF VALVE STUCK CLOSED. WILL REPLACE THE WATER TANK, PRESSURE REGULATOR, PRESSURE RELIEF VALVE, ANC CHECK VALVE. STRUCTURAL DAMAGE UNDER REPAIR. (M)

Part: BATTERY PACK — INOPERATIVE (PAX CABIN)

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

Part: TRANSMITTER — MALFUNCTIONED (TE FLAPS)

FLT 91 - OGG-HNL - DURING TAKEOFF FROM OGG, THE STALL WARNING STICK SHAKER BEGAN AT ROTATION AND WAS CONTINUOUS THROUGH 1000 FEET AND INTERMITTENT AFTER THAT. RETURNED TO OGG FOR AN UNEVENTFUL LANDING. REPLACED THE RIGHT TRAILING EDGE FLAP POSITION TRANSMITTER IAW MM 27-58-12. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LAP JOINT — CRACKED (FUSELAGE)

LOWER SKIN LAP JOINT, CRACK REPAIR AND LAP JOINT MODIFICATION COMPLETED AT BS 360-540, STRINGER 14R, STRINGER 10R, STRINGER 10L AND STRINGER 14L, BS 727-908, STRINGER 14R, 10R, STRINGER 10L AND STRINGER 14L, BS 360-908 IAW ECO 3080R1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STIFFENER — CRACKED (FUSELAGE)

INSTALLED A REPAIR CHANNEL AS A PERMANENT REPAIR FOR A CRACK NOTED A BULKHEAD STIFFENER AT BS 540, IAW ECO 3140. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ACTUATOR — LEAKING (TE FLAPS)

FLT 112 - KOA-HNL - UNABLE TO RETRACT L/E DEVICES AND TRAILING EDGE FLAPS AFTER TAKEOFF. RETURNED TO KOA, UNEVENTFUL LANDING. REMOVED AND REPLACED THE FLAP DRIVE UNIT PER MM 27-51-201. ADJUST AND TEST PER MM 27-51-221. GROUND OPS AND LEAK CHECK OK. REPLACED BROKEN TRAILING EDGE FLAP CONTROL CABLES WFFB-2 AND WFFD-2. ADJUST AND TEST PER MM 27-51-201. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

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

Part: TRU — FAILED (E/E BAY)

LIH/HNL - FLT 230 - WHILE PARKED AT GATE, F/A REPORTED SMOKE SMELL IN GALLEY. SMOKE IN CABIN FROM E/E COMPARMENT. PASSENGERS DEPLANED, AIRCRAFT SECURED. CRASH FIRE CREW NOTIFIED. REPLACED NR 3 TRANSFORMER RECTIFIER UNIT AND BATTERY CHARGER DUE TO THE OVERHEATING. TR3 AND BATTERY CHARGER OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR 2000ZZZX501. (X)

Part: BATTERY CHARGER — FAILED (E/E BAY)

LIH/HNL - FLT 230 - WHILE PARKED AT GATE, F/A REPORTED SMOKE SMELL IN GALLEY. SMOKE IN CABIN FROM E/E COMPARMENT. PASSENGERS DEPLANED, AIRCRAFT SECURED. CRASH FIRE CREW NOTIFIED. REPLACED NR 3 TRANSFORMER RECTIFIER UNIT AND BATTERY CHARGER DUE TO THE OVERHEATING. TR3 AND BATTERY CHARGER OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR TSAA200024033.

Part: SKIN — CRACKED (FUSELAGE)

IDENTIFIED 3 INCH CRACK AT BS 727, STRINGER 16L. CONFIRMED DEFECT BY VISUAL AND HFEC METHOD. REPAIRED BY REMOVING DAMAGED AREA AND INSTALLING 040 INCH EXTERNAL DOUBLER IAW SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: SKIN — CRACKED (BS 727)

FOUND FUSELAGE SKIN CRACK NOTED APPROXIMATELY .5 INCH LONG AT BS 727A STRINGER 17L, CONFIRMED WITH HFEC. REPAIRED IAW SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (BS 744)

POSSIBLE CRACK NEAR BS 727B-747 AT STRINGER 17R. VERIFIED FUSELAGE SKIN CRACK AT BS 744 STRINGER 17R USING HFEC. CUTOUT CRACK IAW SRM 53-30-03 AND VERIFIED WITH HFEC CRACK WAS COMPLETELY REMOVED. REPAIRED IAW SRM 53-30-03. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: LIGHT — INOPERATIVE (COCKPIT)

REPLACED FLIGHT DECK EMERGENCY EXIT LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONTROL CABLE — OUT OF ADJ (GROUND SPOILER)

FLT 201 - HNL-LIH - AFTER LANDING GEAR HANDLE WOULD NOT MOVE TO UP POSITION, ACCOMPLISHED CHECKLIST AND WARNING HORN STAYED ON. LANDING GEAR STAYED DOWN AND THREE GREEN LIGHTS STAYED ON STEADY. CHECK CB. PUT GEAR HANDLE DOWN WITH THREE GREEN LIGHTS. RETURNED TO HNL. UNEVENTFUL LANDING. ADJUSTED GROUND SPOILER INTERLOCK VALVE CABLE IAW MM 27-62-57. TESTED IAW MM 27-62-51. NO DISCREPANCIES NOTED. OK FOR SERVICE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 4 FLOOR PROXIMITY LIGHT BATTERY PACK DUE TO NO TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: LIGHT — INOPERABLE (CABIN)

REPLACED NR 5 FLOOR PATH LIGHT ASSY PACK DUE TO NO TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: SPAR — CRACKED (HORIZ STAB)

HORIZONTAL STAB CENTER SECTION REAR SPAR UPPER CHORD RIGHT FORWARD ATTACH LUG CRACKED. ACCOMPLISHED BY BOEING AOG TEAM PER 6-1171-TA1224R1. (M)

Part: FITTING — CORROSION (RT WING)

RIGHT WING FRONT SPAR WEB CORROSION AT FSS 435. REPAIRED IAW ECO 2970. (M)

Part: FRAME — CORRODED (CARGO DOORWAY)

FORWARD CARGO COMPARTMENT FORWARD DOOR FRAME HAS EXFOLIATED CORROSION. CLEANED, TREATED, FABRICATED, AND COMPLETED IAW SRM 51-40-3 PAGE 1. (M)

Part: SPAR WEB — CORRODED (RT WING)

RT WING FRONT SPAR WEB CORROSION FROM FSS 425 - 433. REPAIRED PER ECO 2970. (M)

Part: BUSHINGS — CORRODED (RT MLG)

RIGHT MAIN LANDING GEAR SUPPORT BEAM FITTING (TOP) CORROSION NOTED IN FITTING AT BS 706 RT. COMPLETED IAW ECO 2966. (M)

Part: FITTING — CRACKED (RT HORIZ STAB)

RIGHT UPPER HORIZONTAL STABILIZER ATTACHMENT FITTING (FUSELAGE SIDE) FOUND CRACKED AROUND EAR. REPLACED STABILIZER ATTACHMENT FITTING. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

LEFT OVERWING EMERGENCY EXIT IDENTIFIER LIGHT ASSY INOP. REPLACED BATTERY PACK, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

LEFT OVERWING EMERGENCY EXIT IDENTIFIER LIGHT ASSY INOP. REPLACED BATTERY PACK, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

FORWARD ENTRY DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSY INOP. REMOVED AND REPLACED FORWARD ENTRY DOOR EMERGENCY IDENT BATTERY PACK. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOP (CABIN)

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

Part: BATTERY — DISCHARGED (CABIN)

NR 4 EMERGENCY FLOOR BATTERY PACK INOP. REPLACED BATTERY PACK, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

REPLACED THE AFT SLIDE EMERGENCY LIGHT BATTERY DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED BATTERY PACK FROM THE AFT DOOR EMERGENCY SLIDE LIGHT. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED BATTERY IN NR 6 POSITION EMERGENCY FLOOR LIGHT DUE TO BEING INOPERABLE. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. TAT: 43,068.7 HOURS. TAC: 59.345. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED BATTERY IN NR 4 POSITION FLOOR PROXIMITY LIGHT DUE TO BEING INOPERATIVE. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: SKIN — CRACKED (BS 727)

FOUND 1 INCH CRACK AT BS 727 PLUS 1.75 AND STRINGER 17R. REPAIRED PER SRM 53-30-3 FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (BS 767)

TWO INCH CRACK FOUND AT BS 767, STRINGER 18R. REPAIRED PER SRM 53-30-3 FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONNECTOR — LOOSE (NR 1 ENGINE)

FLT 95 - NR 1 ENGINE SHUTDOWN IN FLIGHT DUE TO OVHT LIGHT. REPAIRED CONNECTOR ON NR 1 ENGINE LOWER FIRE LOOP. GROUND OPS CHECK OK. GROUND ENGINE RUN OPS CHECK GOOD. REMOVED AND REPLACED NR 1 FIRE BOTTLE. OPS CHECK COMPLETED PER MM 26-21-11 AND SQUIB TEST COMPLETED. REMOVED AND REPLCED NR 2 FIRE BOTTLE. OPS CHECK COMPLETED PER MM 26-21-11. (M)

Part: ACCESSORY UNIT — FAILED (ENGINE)

FLT 302 - HNL-OGG - ON ENGINE RUN UP FOR TAKEOFF, BOTH EPR CIRCUIT BREAKERS POPPED GAUGES FROZE. GROUND RAN BOTH ENGINES. OPS CHECKED OK FOR SERVICE. REPLACED ENGINE ACCESSORY UNIT FOR PRECAUTIONARY REASON. OPS CHECK OK. (M)

Part: BATTERY PACK — LOOSE (CABIN)

LIH/HNL - FLT 220 - PILOT REPORT NR 1. AFT CABIN EMERGENCY LIGHT ILLUMINATED. RESECURED BATTERY PACK, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 41,801:13 HOURS. TAC: 56,497. (X)

Part: SKIN — CORRODED (FUSELAGE)

DURING HEAVY MAINTENANCE VISIT, FOUND CORROSION AROUND AFT LAVATORY SERVICE PANEL CUT OUT. REPAIRED PER ECO2836 W/ DEV A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (BS 947)

DURING HEAVY MAINTENANCE VISIT, FOUND FUSELAGE SKIN BULGING AT BS 947 STRINGER 25L AT FORWARD SIDE OF WATER SERVICE PANEL CUTOUT. REPAIRED PER ECO 2840. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (LT WING)

DURING HEAVY MAINTENANCE VISIT, FOUND LEFT OTB WING LOWER SKIN AT RSS 455 CORROSION AT PREVIOUSLY BLENDED AREA. REPAIRED PER ECO 1684R8 W/DEV F. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BULKHEAD WEB — CORRODED (BS 1088)

DURING HEAVY MAINTENANCE VISIT, NOTED CORROSION AT BS 1088 BULKHEAD WEB APU INLET AREA. REPAIRED PER ECO 1980R9 OPTION VIII. AIRCRAFT RETURNED T SERVICE. (M)

Part: FRAME — CRACKED (BS 460)

DURING HEAVY MAINTENANCE VISIT, SCHEDULED INSPECTION OF LOWER FORWARD CARGO COMPT BODY FRAMES, FOUND BS 460 FRAME INBD CHORD AT S-24L, BS 420 FRAME INBD CHORD AT STRINGER 26, BS 400 FRAME, INBD CHORD AT STRINGER 26L, BS 440 FRAME INBD CHORD AT STRINGER 26L, BS 460 FRAME INBD CHORD AT STRINGER 26L, BS 480 FRAME INBD CHORD AT STRINGER 26L, AND BS 500 FRAME AT STRIGNER 26 CRACKED. REPAIRED PER SRM 53-10-4 AND ECO 1571R7. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SPAR CHORD — CORRODED (RT WING)

DURING HEAVY MAINTENANCE VISIT, CORROSION NOTED ON RT WING FRONT SPAR LOWER CHORD FORWARD HORIZONTAL FLANGE LOWER SURFACE AT FSS 317, 36S, 461, 550, 417, BY NR 4 SLAT ACTUATOR, AND BY NR 5 SLAT ACTUATOR. REPAIRED PER ECO 1803R4. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (BS 294)

DURING HEAVY MAINTENANCE VISIT, FOUND CORROSION ON FLOORBEAM UPPER CHORD AT BS 294 BL '0', BS 294 BL 6L, BS 294 BL 18L AND BS 294 BL 36L. REPAIRED PER ECO2096R3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

DURING HEAVY MAINTENANCE VISIT, CRACK NOTED ON AFT RIGHT CORNER OF FWD NOSE COMPARTMENT DOOR CUT OUT AND ON T-CHORD INBOARD FLANGE. REPAIRED PER ECO 2834R3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: POWER PACK — INOPERATIVE (CABIN)

DURING OVERNIGHT CHECK, REPLACED LEFT OVERWING EXIT IDENTIFIER POWER PACK DUE TO INOP. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: PROX SENSOR — INOPERATIVE (NR 4 LE SLAT)

FLT 644 - OGG-HNL - AFTER TAKEOFF, NR 4 SLAT INDICATED EXTEND WITH FLAPS RETRACTED. NO ROLL NOTED. RETURNED TO OGG. REPLACED NR 4 FULL POSITION PROX SENSOR (SLAT). SYSTEM OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (BS 785)

DURING OVERNIGHT CHECK, DISCOVERED FUSELAGE SKIN CRACK APPROXIMATELY .75 INCH ON LENGTH AT BS 785, STR 17L. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. TAT: 40,769:35 HOURS. TAC: 54,204. (X)

Part: LIGHT — INOPERATIVE (CABIN)

AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: EPR TRANSDUCER — STICKING (NR 1 ENGINE)

FLT 229 - OGG - ON TAKEOFF, NR 1 ENGINE FF ADVANCED NORMAL WHILE EPR, N1, N2, EGT HUNG. WHEN NR 2 ENGINE REACHED 1.97 EPR, NR 1 RAN AWAY N1, N2, AND EGT-EPR FOLLOWED AFTER 1 TO 2 SEC. ABORTED TAKEOFF WITH NO LIMITS BEING EXCEEDED. REMOVED AND REPLACED EPR TRANSDUCER PER MM 71-12-21 AND CHECK PT2 AND PT7 LINES PER MM 77-11-0. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FITTING — CORRODED (TE FLAP TRACK)

DURING C-CHECK VISIT, CORROSION FOUND IN THE FLAP TRACK ATTACH FITTING NRTC NR 105139. REPAIRED PER ECO 2767 DEVIATION A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: INTERCOSTAL — CRACKED (BS 332)

DURING SCHEDULED INSPECTION OF FUSELAGE, FORWARD SERVICE DOORWAY AFT FRAME, DISCOVERED CRACK AT DOOR STOP SUPPORT INTERCOSTAL AT BS 332, STRINGER 8A (REF AD88-03-03 AMDT39-5832, AND AD 90-06-02 AMDT 39-6489). REPAIRED PER ECO 1475R4, PER DRAWING 65C33288, FIG 3, PT 2 AND 3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STEERING COMP — FAILED (E/E BAY)

FLT 257 - HNL-LIH - FLIGHT OFFICERS VERTICAL GYRO COMPUTER FLAG CAME ON IN FLIGHT. FLIGHT DIRECTOR 2 AC CIRCUIT BREAKER OPEN. NOT RESET. FLIGHT ATTENDANT REPORTED STRONG ELECTRICAL SMOKE/SMELL IN CABIN. REPLACED STEERING COMPUTER. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (BS 967)

DURING HEAVY MAINTENANCE VISIT, FOUND SKIN BULGE AROUND RELIEF VALVE CUT OUT AT BS 967 STRINGER 26R-27R. REPAIRED PER ECO 2203R1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: REAR SPAR — CORRODED (VERT STAB)

DURING HEAVY MAINTENANCE VISIT, FOUND EXFOLIATION ON RIGHT VERTICAL STABILIZER REAR SPAR AT FS 67 TO 83. REPAIRED PER ECO 2509R2. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRINGER — CORRODED (BS 827)

DURING HEAVY MAINTENANCE VISIT, FOUND EXFOLIATION CORROSION ON STRINGER 27R BS 827. REPAIRED STRINGER PER SRM 53-10-3 AND REPAIRED SKIN PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (BS 727)

DURING HEAVY MAINTENANCE VISIT, LOWER FUSELAGE SKIN BULGE BS 727 PLUS 12 INCHES THROUGH BS 727A AT STRINGER 28R. REPAIRED PER ECO 2726 WITH DEVIATION A, B, C, D, AND E. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (BS 400)

DURING HEAVY MAINTENANCE VISIT, FOUND LOWER FUSELAGE SKIN CRACK AT BS 400 BL-0. REPAIRED PER ECO 2724R1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (BS 344)

DURING HEAVY MAINTENANCE VISIT, FOUND .625 INCH CRACK AT BS 344 LOWER AFT CORNER OF FORWARD AIRSTAIR DOOR CUT OUT. REPAIRED PER ECO 1143. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (BS 727)

DISCOVERED FUSELAGE SKIN CRACKS, 1.25 INCH AT BS 727A PLUS 15, 1 INCH ABOVE STRINGER 16L, AND 4.5 INCHES AT BS 727A PLUS 15, 1 INCH ABOVE STRINGER 17L. HFEC VERIFIED. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (BS 328)

DURING DAILY CHECK, DISCOVERED FUSELAGE SKIN CRACK 4 INCHES IN LENGTH AT BS 328 PLUS 6 INCHES AND 2 INCHES BELOW STRINGER 22R. HFEC CONFIRMED. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (BS 727)

DISCOVERED FUSELAGE SKIN CRACK 2.25 INCH AT BS 727A, 1 INCH BETWEEN STRINGER 17L AND STRINGER 18L. HFEC CONFIRMED. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (BS 727)

DURING OVERNIGHT INSPECTIONS, DISCOVERED FUSELAGE SKIN CRACK 1 INCH IN LENGTH, 2 INCHES FORWARD OF BS 727A AND ABOVE S17R. VERIFIED BY HFEC. CARRIED OUT REPAIR WORK WITH REFERENCE PER SRM 53-30-5. AIRCRAFT RETURNED TO SERVICE. TAT: 38,401:42 HRS. TAC: 49,191. (X)

Part: SKIN — CRACKED (BS 764)

DURING OVERNIGHT CHECK DISCOVERED FUSELAGE SKIN CRACK 1 INCH LONG AT BS 764, STRINGER 16L. VERIFIED ENDS OF CRACK WITH HFEC. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FAN — FAILED (CABIN)

ELECTRICAL BURNING SMELL IN CABIN COMING FROM GASPERS. DEFERRED GASPER FAN IAW MEL 21-24. AIRCRAFT PLACARDED. REPLACED GASPER FAN. PLACARD REMOVED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (BS 727)

DURING OVERNIGHT CHECK, DISCOVERED FUSELAGE SKIN CRACK 1.6250 INCHES LONG AT BS 727B PLUS 16.5, 1 INCH ABOVE S17L. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. TAT - 36,534.34. TAC - 60,358. (X)

Part: SPAR WEB — CORRODED (FSS 433)

DURING HEAVY MAINTENANCE VISIT, CORROSION FOUND UNDER NR 5 SLAT ACTUATOR ATTACH FITTING FRONT SPAR WEB AT FSS 433. REPAIRED PER ECO 2132R2. AIRCRAFT RETURNED TO SERVICE. (Z)

Part: BULKHEAD CHORD — CRACKED (BS 727)

DURING HEAVY MAINTENANCE VISIT, FOUND BS 727 BULKHEAD OUTER CHORD CRACKED BETWEEN S22L AND 23L, 5.25 INCHES LONG. STOP DRILLED PER SRM 51-10-01 IAW BOEING MESSAGE ALO-HNL 94-0388RR DATED 29 DECEMBER 94 AND REPAIRED PER ECO 1325. AIRCRAFT RETURNED TO SERVICE. (X)