N819AL

Part: CLAMP — LOOSE (CABIN AIR)

PRESSURIZATION CHECKED BEFORE TAKEOFF, CABIN CLIMBED TO 1,000 FT BY THE TIME AIRCRAFT LEVELED AT 3,000 FT. RETURNED TO OGG. NOTE THAT THE RIGHT PACK WAS DEACTIVATED PRIOR TO THIS FLIGHT DUE TO REPORTS OF A WHOOSHING SOUND NEAR ROW 7 & 8. THE FIRST OFFICER FOUND THE MIX VALVE INOP AND ALL THE WAY COLD. THE RIGHT PACK WAS DEACTIVATED AND PUT ON MEL. CHECKED LT & RT PACK SYS; INSPECTED FWD ENTRY/SVC DOOR AND AFT SVC/ENTRY DOOR, PRESSURIZED A/C TO 3-4 INCHES, FOUND NO LEAKS. INSPECTED ALL DOORS & PANELS, NO LEAKS. INSPECTED LT PACK & FOUND AIR LEAKING FROM ACM EXHAUST DUCT. RESECURED CLAMP & SEAL. REPRESSURIZED A/C SYS 3-4 INCHES, ALL SYS CHECKS NORMAL. NO LEAKS, A/C OK FOR SERVICE.

Part: ENGINE — FAILED (NR 2)

NON-ETOPS FLT. 241, HNL-LIH: CLIMBING THROUGH 8,000 FEET, HEARD A LOUD BANG AND THE AIRCRAFT YAWED RIGHT. THE NR 2 ENGINE EPR DROPPED FROM 1.82 TO 1.76. REPORTED THAT A PASSENGER OBSERVED FLAMES EXITING THE NR 2 ENGINE EXHAUST. ALL OTHER ENGINE INDICATIONS WERE NORMAL. RETURNED TO HNL, UNEVENTFUL LANDING. REMOVED AND REPLACED THE NR 2 ENGINE IN ACCORDANCE WITH FORM M-212, M213, M215, AND M211. LEAK AND OPS CHECK GOOD. AIRPLANE RETURNED TO SERVICE.

Part: FCU — MALFUNCTIONED (NR 1 ENGINE) · airframe 40,977 hrs · 52,581 cycles

ON TAKEOFF UNABLE TO OBTAIN MAX-POWER ON NR 1 ENGINE, ENGINE POWER ADVANCED NORMALLY UNTIL 1.96-1.97 EPR INDICATION. MAX-POWER OBTAINED WAS 1.97 EPR WITH N1 AT 94 PERCENT; FURTHER THRUST LEVER MOVEMENT HAD NO EFFECT. REMOVED AND REPLACED THE NR 1 ENGINE FCU IAW PRATT MM 79-21-01. PERFORMED LEAK VERIFICATION IAW AQ FORM M-215. OPS AND LEAK CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: INDICATOR — SLOW (AIRSPEED) · airframe 40,967 hrs · 52,558 cycles

NON-ETOPS FLIGHT 62, HNL-OGG: ON TAKEOFF 80KTS CROSS-CHECK WAS OK, AFTER LIFTOFF THE FIRST-OFFICERS AIRSPEED INDICATOR READ 50KTS SLOWER THAN CAPTAIN’S STANDBY INDICATOR. RETURNED TO HNL. CLEARED FIRST-OFFICERS PITOT TUBE OF DEBRIS IAW AMM 34-11-0, LEAK AND OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 40,967 hrs · 52,557 cycles

ON TAKEOFF UNABLE TO OBTAIN MAX-POWER ON NR 1 ENGINE, MAX-EPR INDICATION OF 1.96. RETURNED TO HNL. CLEANED DEBRIS FROM PT2 LINE AND VERIFIED SECURITY OF ALL EPR LINES. PERFORMED ENGINE RUN FOR TAKEOFF POWER VERIFICATION, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE)

FOUND CORROSION ON FORWARD CARGO DOOR FRAME. TRIMMED OUT DAMAGED AREA. HFEC VERIFIED CRACK REMOVED. FABRICATED REPAIR DOUBLERS AND TRIPLER. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAIR PARTS MAKING A FAYING SEAL AROUND REPAIR. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 46, DETAIL II. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CIRCUIT BREAKER — TRIPPED (EPR INDICATOR)

FLT 280 - HNL-KOA - ABORTED TAKEOFF DUE TO BOTH EPR GAUGES INOPERATIVE. C/B'S RESET, NO FLAGS. RAN BOTH NR 1 AND NR 2 ENGINE AFTER EPR C/B RESET. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (PAX CABIN)

REPLACED FORWARD ENTRY EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (PAX CABIN)

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

Part: CREASE BEAM — CORRODED (FUSELAGE)

FOUND CORROSION DISCOVERED ON LEFT CREASE BEAM BETWEEN BS 307 AND 310. REMOVED AND REPLACED SECTION BETWEEN BS 307 AND BS 310. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 51-30-2 AND 51-40-3. (M)

Part: WEB — CORRODED (NR 6 SLAT)

CORROSION DISCOVERED ON RIGHT WING SPAR WEB AT FSS 540-552 BEHIND THE NR 6 SLAT. CUTOUT DAMAGED SECTION OF WEB. FABRICATED REPAIR PARTS AND DRILLED FASTENER HOLES. ALODINE, PRIMED AND INSTALLED REPAIR PART WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 57-10-6, FIGURE 1. (M)

Part: STRINGER — CORRODED (FUSELAGE)

CORROSION DISCOVERED ON STRINGER LOCATED AT BS 967, LBL 7. CUTOUT DAMAGED SECTION OF STRINGER. FABRICATED REPAIR PARTS AND DRILLED FASTENER HOLES. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-1. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

FOUND CORROSION DISCOVERED AT BS 312 FLOORBEAM UPPER TEE. CUTOUT DAMAGED SECTION OF STRINGER. FABRIATED NEW CHORD SECTION AND SPLICE ANGLE. DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-9, FIGURE 5. (M)

Part: STRINGER — CRACKED (FUSELAGE)

CRACK DISCOVERED ON STRINGER 4 LEFT, LOCATED AT BS 907. CUTOUT DAMGED SECTION OF STRINGER. FABRICATED REPAIR PARTS AND DIRLLED FASTENER HOLES. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-30-2. (M)

Part: SKIN — DENTED (FUSELAGE)

DENT DISCOVERED ON FUSELAGE SKIN BETWEEN BS 981 AND 996 ALONG STRINGER 14L. CUTOUT DAMAGED SECTION OF SKIN AND STRINGER. FABRICATED A REPAIR DOUBLER AND TRIPLER. ALODINE, PRIMED AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 48 SHEET 46. (M)

Part: STRINGER — DENTED (FUSELAGE)

DENT DISCOVERED AT BS 376 ALONG STRINGER 17L. CUTOUT DAMAGED SECTION OF SKIN AND STRINGER. FABRICATED REPAIR PARTS AND DRILLED FASTENERS HOLES. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 1. (M)

Part: STRINGER — DAMAGED (FUSELAGE)

DAMAGED STRINGER 2 RIGHT WHILE REMOVING STRINGER CLIP. CUTOUT DAMAGED STRINGER SECTION BETWEEN BS 360 AND BS 389. FABRICATED NEW STRINGER SECTION, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-3, FIGURE 3. (M)

Part: ANGLE — CRACKED (FUSELAGE)

DISCOVERED A CRACKED ATTACHMENT ANGLE LOCATED AT BS 289, WL 239. REMOVED DAMAGED ANGLE. FABRICATED NEW ANGLE, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 51-30-2. (M)

Part: SKIN — DENTED (FUSELAGE)

DENT LOCATED AT BS 396 BETWEEN STRINGER 24 AND 25R. CUTOUT DAMAGED SECTION OF STRINGER. FABRICATED A NEW STRINGER REPAIR SECTION. ALODINE, PRIMED, AND INSTALLED REPAR PART IAW FASTENERS FROM TABLE 1 MAKING A FAYING SEAL. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 1. (M)

Part: SKIN — DENTED (FUSELAGE)

DISCOVERED A DENT LOCATED AT BS 346, BETWEEN STRINGER 24 AND 25 RIGHT. CUTOUT DENTED PORTION OF THE SKIN. FABRICATED A REPAIR PLATE, DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 1. (M)

Part: SHEAR TIE — DAMAGED (FUSELAGE)

DISCOVERED A DAMAGED SHEAR TIE LOCATED AT BS 360, BETWEEN STRINGER 14 AND 15 RIGHT. CUTOUT DENTED PORTION. FABRICATED A NEW SHEAR TIE, DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-4, FIGURE 10. (M)

Part: WEB — CORRODED (FUSELAGE)

CORROSION DISCOVERED BETWEEN FSS 540 AND 552 BEHIND THE NR 6 SLAT. CUTOUT DAMAGED PORTION OF THE WEB. FABRICATED NEW WEB SECTION, DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-6, FIGURE 1. (M)

Part: SHEAR TIE — DAMAGED (FUSELAGE)

DAMAGED SHEAR TIE DISCOVERED AT BD 908 BETWEEN STRINGERS 14 AND 15 LEFT. CUTOUT DAMAGED SECTION. FABRICATED NEW SHEAR TIE, DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-04, FIGURE 10. (M)

Part: SHEAR TIE — DAMAGED (FUSELAGE)

DAMAGE DISCOVERED ON SHEER TIE BETWEEN STRINGER 14 AND 15L AT BS 360. CUTOUT DAMAGED SECTION OF SHEAR TIE. FABRICATED A REPAIR SHEAR TIE AND RADIUS FILLER. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-4, FIGURE 10. (M)

Part: STRINGER CLIP — CRACKED (FUSELAGE)

CLIP DISCOVERED CRACKED OR TORN ON STRINGER 2R LOCATED AT BS 380. REMOVED DAMAGED CLIP. FABRICATED REPAIR PARTS AND DRILLED FASTENER HOLES. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS. REPAIR COMPLETED IAW SRM 51-30-2, FIGURE 1. (M)

Part: STRINGER CLIP — DAMAGED (FUSELAGE)

DISCOVERED A DAMAGED STRINGER CLIP LOCATED AT BS 380, STRINGER 2 RIGHT. REMOVED AND REPLACED DAMAGED CLIP. ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-30-2, FIGURE 1. (M)

Part: SKIN — DENTED (FUSELAGE)

DISCOVERED A 15 INCH GOUGE WITH A DENT LOCATED AT BS 981 THROUGH BS 996, 4 INCHES ABOVE STRINGER 4 LT. CUTOUT GOUGE AND DENTED PORTION OF THE SKIN. FABRICATED DOUBLER AND TRIPLER, DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 48.

Part: STRINGER — CORRODED (FUSELAGE)

CORROSION DISCOVERED AT BS 967, LBL 7, AND WL 171. CUTOUT DAMAGED PORTION OF THE STRINGER. FABRICATED NEW STRINGER SECTION, DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-3. (M)

Part: SKIN — DENTED (FUSELAGE)

DENT DISCOVERED AT BS 376 ALONG STRINGER 17 LT. CUTOUT DENTED PORTION OF THE SKIN. FABRICATED REPAIR PLATE, DRILLED FASTENER HOLES, ALODINED, PRIMED AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-3, FIGURE 1. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

FOUND CORROSION ON C-CHANNEL UPPER STRUCTURE LOCATED BETWEEN BS 312 AND BS 344 AT WL 208, LBL 57. REMOVED AND REPLACED ENTIRE SECTION BETWEEN BS 312 AND BS 344. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 51-40-3. (M)

Part: CREASE BEAM — CORRODED (FUSELAGE)

FOUND CORROSION ON RIGHT CREASE BEAM AROUND NUT PLATE HOLES BETWEEN BS 290 AND 358. REMOVED AND REPLACED ENTIRE SECTION BETWEEN BS 290 AND BS 358. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-2. (M)

Part: STRINGER — GOUGED (FUSELAGE)

DAMAGED OR GOUGE STRINGER DISCOVERED AT BS 382. CUTOUT GOUGED AREA. FABRICATED FILLER, ALODINED, PRIMED AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-3, FIGURE 3. (M)

Part: FRAME — CRACKED (FUSELAGE)

FOUND BS 244 FRAME CRACKED AT RIGHT CREASE BEAM. CUT OUT DAMAGED SECTION. FABRICATED REPAIR PARTS AND DRILLED FASTENERS HOLES. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 51-40-3, FIGURE 1. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

FOUND CORROSION ON UPPER FLOORBEAM AT BS 344 BLENDED OUT 1 INCH BY 1 INCH AREA IN TWO PLACES. CUTOUT DAMAGED AREA. FABRICATED NEW FLOORBEAM SECTION PER TABLE II, DETAIL I. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 51-10-9, FIGURE 5. (M)

Part: BATTERY PACK — INCORRECT (PAX CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 1,2,4, AND 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK, OK. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — GOUGED (FUSELAGE)

REMOVED DAMAGE ON FWD CARGO DOOR CUT OUT. PERFORMED A DETAILED VISUAL AND HFEC INSPECTION OF THE CUTOUT AND ALL LAP SPLICE FASTENERS HOLES IN THE REPAIR AREA, NO DEFECTS NOTED. INSTALLED REPAIR IAW SRM. AIRCRAFT RETURNED TO SERVICE.(TSAA8003321)

Part: SLIDE — DEFECTIVE (CABIN)

DURING A ROUTINE TRAINING EXERCISE AND AFTER SUCCESSFUL SLIDE DEPLOYMENT, THE SLIDE ASSEMBLY EXPLODED AT THE SEAM. NO HARM TO PERSONNEL. REMOVED AND REPLACED SLIDE; CONTINUED WITH EXERCISE. SLIDE SENT TO VENDOR FOR EVALUATION.

Part: SWITCH — STUCK (COCKPIT)

ANTI-SKID INOPERATIVE LIGHT ILLUMINATED ON BOTH SYSTEMS DURING FLIGHT. DUE TO WEATHER CONDITIONS, RUNWAY LENGTH AND AIRCRAFT WEIGHT FOR THE AIRPORT, THE AIRCRAFT RETURNED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED A DEFECTIVE LANDING GEAR LEVER UP SWITCH. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE)

BLENDED OUT CORROSION ON THE FUSELAGE SKIN AT BS 990 STRINGER 27L BY CUTTING STRINGER 27L IAW SRM 51-10-2. VERIFIED CORROSION REMOVED, CLEANED AND TREATED IAW SRM 51-10-6. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-20-2 FIGURE 3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRUCTURE — CRACKED (NR 4 SLAT)

REPAIRED CRACK AT NR 4 SLAT STATION 35.84. REPAIR CONSISTS OF BLENDING OUT THE DAMAGED AREA, MAINTAINING A BLEND OUT LENGTH OF .075 INCH MAXIMUM AND USING A MINIMUM RADIUS OF .50 INCH. REMOVED ALL BURRS AND SHARP EDGES IAW SRM 57-20-1 PAGE 2 DETAIL II. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRUCTURE — CRACKED (NR 5 SLAT)

REPAIRED CRACK AT NR 5 SLAT STATION 195.53. REPAIR CONSISTS OF BLENDING OUT THE DAMAGED AREA, MAINTAINING A BLEND OUT LENGTH OF .075 INCH MAXIMUM AND USING A MINIMUM RADIUS OF .050 INCH. REMOVED ALL BURRS AND SHARP EDGES IAW SRM 57-20-1 PAGE 1 FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SLAT — CRACKED (WING)

REPAIRED CRACK AT NR 6 SLAT STATION 370.56. BLENDED OUT THE DAMAGED AREA IAW SRM 57-20-1, FIG 1, PAGE 1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FOUND CABIN INTERIOR LONGITUTIONAL FLOOR SUPPORT UPPER CHORD AND WEB CRACKED AT BS 663.75 BL 0. VERIFIED CRACK REMOVED USING HFEC. REPAIRED LONGITIONAL FLOORBEAM IAW ECO 2223R2 PART II, DEVIATION 'C'. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

REPAIRED A 2.5 INCH CRACK ON THE FUSELAGE SKIN AT BS 727 JUST BELOW STRINGER 19 RT. VERIFIED CUTOUT USING HFEC. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-30-3 PAGE 11 FIGURE 6. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — DELAMINATED (RT ELEVATOR)

FOUND DELAMINATION ON LOWER SURFACE OF RIGHT ELEVATOR. TRIMMED OUT DAMAGED LAMINATION TO A SMOOTH SHAPE WITH ROUNDED CORNERS. FABRICATED, CLEANED AND INSTALLED HONEYCOMB REPLACEMENT CORE PLUG. PREPARED AND APPLIED REPAIR PLIES. INSTALLED HEATED BLANKET AND EVACUATED THE REPAIR REPAIR AREA MAINTAINING A VACCUM OF 22 INCHES OF MERCURY MINIMUM. REPAIR COMPLETED IAW SRM 51-40-12, REPAIR 14, FIGURE 22. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRUCTURE — CRACKED (NR 4 SLAT)

REPAIRED CRACK AT NR 4 SLAT STATION 35.84. REPAIR CONSISTS OF BLENDING OUT THE DAMAGED AREA, MAINTAINING A BLEND OUT LENGTH OF .075 INCH MAXIMUM AND USING A MINIMUM RADIUS OF .50 INCH. REMOVED ALL BURRS AND SHARP EDGES IAW SRM 57-20-1 PAGE 1 FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

REPAIRED A 4 INCH CRACK ON THE FUSELAGE SKIN AT BS 727 JUST BELOW STRINGER 18 RT. VERIFEID CUTOUT USING HFEC. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-30-3 PAGE 11 FIGURE 6. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CRACKED (FUSELAGE)

FOUND CABIN INTERIOR LONGITUDINAL FLOORBEAM UPPER CHORD AND WEB CRACKED AT BS 663.75 BL 0. VERIFIED CRACK REMOVED USING HFEC. REPAIRED LONGITUDINAL FLOORBEAM IAW ECO 223R2 PART II, DEVIATION "C". AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — INOPERATIVE (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED NR 1 FLOOR PROXIMITY LIGHT ASSY FOR RETIREMENT. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: VALVE — DEFECTIVE (NR 2 ENGINE)

FLT 210 - HNL-OGG - DURING TAKEOFF, NR 2 ENGINE BLEED LIGHT CAME ON. ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AND REPLACED THE NR 2 ENGINE PNEUMATIC SHUTOFF VALVE IAW MM 21-11-011-6. OPS AND LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (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: HYDRAULIC LINE — BROKEN (NR 2 ENGINE)

FLT 86 - HNL-KOA - DURING TAKEOFF, EXPERIENCED A COMPLETE LOSS OF A SYSTEM HYDRAULICS. PERFORMED CHECKSLIST AND RETURNED TO HNL FOR AN UNEVENTFUL LANDING. AFTER LANDIG THE STANDBY LOW QUANTITY LIGHT CAME ON. AFTER THE LANDING GEAR WAS LOWERED, WAS UNABLE TO LOWER FLAPS BEYOND 10 DEGREE WITH ALTERNATE FLAPS. REMOVED AND REPLACED THE NR 2 THRUST REVERSER ACTUATOR PRESSURE LINE AND RESERVICED THE A SYSTEM, B SYSTEM, AND STANDBY HYDRAULIC FLUIDS. OPS CHECKED ALL SYSTEMS AND RUNUP CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

REPLACED NR 2 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — INOPERATIVE (CABIN)

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

Part: APU — LEAKING (APU BAY)

FLT 29 - HNL-KOA - APU SHUTDOWN IN FLIGHT. INSPECTED APU AND FOUND LOW OIL QTY. APU LEAKING OIL. REMOVED AND REPLACED APU PER FORM M-133. LEAK AND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: CONTROLLER — INOPERATIVE (CABIN)

FLT 270 - HNL-KOA - EN ROUTE TO KONA, AIRCRAFT PRESSURIZATION FAILED. RETURNED TO HNL. UNEVENTFUL LANDING. FOUND AC AND DC MANUAL C/B'S OPEN FOR PRESSURIZATION CONTROL. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER. GROUND CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: LIGHT — DISCHARGED (CABIN)

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

Part: PT7 TUBE ASSY — FAILED (NR 1 ENGINE)

FLT 263 - HNL-LIH - NR 1 ENGINE UNABLE TO GET TAKEOFF POWER (1.73 EPR MAX). ABORTED TAKEOFF AT 60 KNOTS. RETURNED TO GATE. REMOVED AND REPLACED TUBE ASSY. PERFORMED GROUND RUN PER 71-09-200. ALL PARAMETERS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED NR 4 FLOOR PROXIMITY LIGH TASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: TRACK — LOOSE (TE FLAP)

DURING WALKAROUND INSPECTION, THE NR 1 ENGINE AFT MOUNT INDICATOR MARKINGS WERE NOTED AS BEING MISALIGNED BY THE MECHANIC. UPON FURTHER INVESTIGATION IT WAS DISCOVERED THAT ON THE NR 3 TRACK ASSY (1) ONE MOUTN BOLT WAS LOOSE AND ALSO THE AFT MOUNT BORE WAS FOUND ELONGATED OUT OF LIMITS DUE TO THE TRACK ASSY BEING LOOSE AND FREE TO MOVE. WORK IN PROGRESS TO REPLACE WORN TRACK ASSY AND ASSOCIATED HARDWARE. (M)

Part: SWITCH — CONTAMINATED (NR 2 ENGINE)

FLT 404 - HNL-ITO - NR 2 ENGINE OIL FILTER BYPASS ILLUMINATED IN FLIGHT. SHUTDOWN ENGINE PER QRH. DECLARED EMERGENCY AND MADE UNEVENTFUL LANDING IN KAHALUI (OGG). REMOVED AND REPLACED OIL FILTER SCREEN AND OIL PRESSURE BYPASS SWITCH. LEAK CHECK AND POWER RUN CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED BATTERY FOR POSITION NR 4 FLOOR PROX LIGHT ASSY DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED FORWARD SERVICE EXIT IDENTIFIER BATTERY PACK DUE TO RETIRE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED LEFT OVERWING EXIT IDENTIFIER BATTERY PACK DUE TO TIRE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED FORWARD ENTRANCE EXIT IDENTIFIER BATTERY PACK DUE TO RETIRE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED POWER PACK FOR FORWARD CONTROLLER DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED BOTH BATTERY PACKS FOR EMEGNECY PACKS 1 AND 2 DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED RIGHT OVERWING EXIT IDENTIFIER LIGHT ASSY DUE TO INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 1 EMERGENCY FLOOR LIGHTING BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ENGINE — FAILED (NR 2 NACELLE)

ON TAKEOFF FROM HNL, A LOUD BANG FROM NR 2 ENGINE WAS HEARD FOLLOWED BY LOSS OF THRUST AND ENGINE VIBRATIONS. REDUCED POWER AND MADE SINGLE ENGINE LANDING AT HNL. ENGINE WAS NOT SHUT DOWN. REMOVED AND REPLACED NR 2 ENGINE. FOUND CONTAINED TURBINE FAILURE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED AFT ENTRY DOOR EMERGENCY ID LIGHT ASSY BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED AFT ENTRY DOOR EMERGENCY ID LIGHT ASSY S/N 2436, ON 2540. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 4 AND NR 6 EXIT FLOOR LIGHT BATTERY PACK. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED BATTERY PACK FOR AFT ENTRY DOOR EXIT LIGHT DUE TO BEING INOP. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED BATTERY PACK ON NR 3 POSITION FLOOR EMERGENCY LIGHT DUE TO BEING INOPERATIVE. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: SWITCH — FAILED (NR 1 LE FLAP)

T/O WARNING CONFIG COMES ON WITH POWER ADVANCE. RE-GAP PROX SENSOR NR 1 LE FLAP UNIT AND REPLACE FLAP/SLAT POSITION SWITCH UNIT. PERFORM OPS AND FUNCTIONS CHECK OF T/O CONFIG AND WARNING SYSTME OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY ASSY — DISCHARGED (CABIN)

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

Part: GUIDES — WORN (NR 3 LE SLAT)

FLT 272 - HNL-OGG - DURING APPROACH PHASE WITH FLAPS 5 SET, THE NR 3 SLAT TRANSIT LIGHT REMAINED ILLUMINATED AND PILOTS VISUALLY CONFIRMED THE SLAT PARTIALLY EXTENDED. DECLARED EMERGENCY AND LANDED WITHOUT NO INCIDENT. REPLACED NR 3 SLAT OUTBOARD TRACK GUIDES PER MM 27-81-0 AND ADJUSTED NR 3 SLAT OUTBOARD AND INBOARD AUXILIARY TRACK DETENTS PER MM 29-81-21. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ENGINE — MALFUNCTIONED (NR 2)

FLT 297 - NR 2 ENGINE OIL PRESSURE LIGHT ILLUMINATED ON CLIMB-OUT FOLLOWED BY 'O' OIL QTY INDICATION AND OIL PRESSURE SLOWLY DECREASED TO FLUCTUATE BETWEEN 10-15 LBL PSI. SHUTDOWN PERFORMED. REPLACED NR 2 ENGINE IAW M-211, M-212, M-213, M-214 AND M-215. OK FOR SERVICE REQUIRED INSPECTION C/W FOR NR 2 ENGINE. REMOVE AND INSTALL IAW M-211, M212, M-213, M-214, AND M-215. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ON SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED LIGHT ASSY AND BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 28,317:22 HOURS. TAC: 24,021. (X)

Part: BULB — FAILED (CABIN)

ON SERVICE CHECK, FOUND RIGHT AFT EMERGENCY SLIDE LIGHT OUT. RELAMPED OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BULB — FAILED (CABIN)

ON SERVICE CHECK, FOUND RIGHT OVERWING EMERGENCY LOWER SLIDE LIGHT OUT. RELAMPED OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK WITH LOW VOLTAGE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

DURING OVERNIGHT CHECK, REPLACED BATTERY FOR ROW 1 EMERGENCY FLOOR PROX LIGHT ASSY DUE TO INOP. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

DURING OVERNIGHT CHECK, REPLACED BATTERY FOR ROW 1 EMERGENCY FLOOR PROXIMITY LIGHT ASSY DUE TO INOPERABLE. OPERATIONAL CHECK OF AIRCRAFT RETURNED TO SERVICE. TAT: 27,168:07. TAC: 21,442. (X)

Part: BATTERY — DISCHARGED (CABIN)

DURING OVERNIGHT CHECK, REPLACED ROW 4 AND ROW 12 EMERGENCY FLOOR LIGHT BATTERIES DUE TO LIGHT ASSY LED'S INOPERABLE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 26,992:17 HOURS. TAC: 21,041. (X)

Part: LIGHT — INOPERATIVE (CABIN)

ROW 4D EMERGENCY EXIT FLOOR LIGHT DOES NOT TURN ON. REPLACED 4D FLOOR LIGHT. AIRCRAFT RETURNED TO SERVICE. (X)

Part: LIGHT — INOPERATIVE (CABIN)

ROW 1 FLOOR EMERGENCY LIGHT INOPERATIVE. REPLACED FLOOR LIGHT EMERGENCY LIGHT UNIT. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY — DISCHARGED (CABIN)

DURING OVERNIGHT CHECK, REPLACED ROW 8 AND ROW 12 EMERGENCY FLOOR LIGHT BATTERIES DUE TO LIGHT ASSY LED'S INOP. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 26,966:24 HOURS. TAC: 20,986. (X)

Part: BATTERY — DISCHARGED (CABIN)

DURING OVERNIGHT CHECK, REPLACED ROW 6 EMERGENCY FLOOR LIGHT BATTERY DUE TO INOP. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 26,962:28 HOURS. TAC: 20,976. (X)

Part: LAMP — INOPERATIVE (CABIN)

DURING OVERNIGHT CHECK, RELAMPED ROW 4 OVERHEAD RACK EMERGENCY LIGHT DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 26,962:28 HOURS. TAC: 20,976. (X)

Part: ENGINE — FAILED (NR 2)

FLT 208 - HNL-OGG - UNABLE TO GET TAKEOFF POWER. ONLY ABLE TO GET 1.73 EPR MAX, EGT OIL PRESSURE NORMAL. REJECTED TAKEOFF PRIOR TO 80 KTS. REPLACED NR 2 ENGINE ASSEMBLY PER FORM M-212, M-213, AND M-214 AND JETCAL PER FORM M-215. GROUND OPS AND LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (LT WING)

DURING HEAVY MAINTENANCE VISIT, FOUND CORROSIO NON LEFT WING LOWER SKIN AT RSS 517. REPAIRED PER ECO 1684RT. OUTBOARD WING MAIN WING BOX LOWER SKIN REWORK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING OVERNIGHT CHECK, FOUND FIRST TWO EMERGENCY FLOOR LIGHTS - ONLY ONE LED WORKING. REPLACED FIRST EMERGENCY FLOOR LIGHT ASSY, AND RE-RACK BATTERY PACK FOR NR 2. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 26,886:04 HOURS. TAC: 20,803. (X)

Part: MECHANISM — OUT OF ADJUST (PAX DOOR)

FLT 230 - LIH-HNL - FORWARD ENTRY DOOR HANDLE WENT TO FULL UNLOCK ON TAXI IN. FLIGHT ATTENDANT SAYS DOOR STARTED TO OPEN. FORWARD ENTRY DOOR ADJUSTED ROD ENDS ON UPPER AND LOWER DOOR GATES. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR BEAM — CORRODED (BS 312)

DURING HEAVY MAINTENANCE VISIT, FLOOR BEAM AT BS 312, FILIFORM CORROSION NOTED AROUND SEVERAL NUTPLATE HOLES. REPLACED FLOOR BEAM FROM LBL 62 TO RBL 20 PER SRM 53-10-9. AIRCRAFT RETURNED TO SERVICE. NRTC: 11,911. (X)

Part: ATTACH LUGS — CORRODED (HORIZ STABILIZER)

DURING HEAVY MAINTENANCE VISIT, FOUND CORROSION ON LEFT AND RIGHT HORIZONTAL STABILIZER ATTACH LUGS, FACE AND BORES. REPAIRED PER ECO 2689, PARTS I AND II. AIRCRAFT RETURNED TO SERVICE. TAT: 24,124.20 HOURS. TAC: 14,610.

Part: TRANSVERSE BEAM — CRACKED (BS 674)

DURING HEAVY MAINTENANCE VISIT, BS 674 TRANSVERSE BEAM CRACKED, THIRD SEAT TRACK FROM LEFT. REPAIRED PER ECO 1933R3. AIRCRAFT RETURNED TO SERVICE. NRTC: 11,582. (X)

Part: DOORWAY FRAME — CRACKED (BS 787)

DURING HEAVY MAINTENANCE VISIT, FUSELAGE AFT LOWER CARGO DOORWAY FRAME CRACKED AT BS 787 PLUS 6 INCHES BETWEEN S24R - S26R. REPAIRED PER ECO 2679. AIRCRAFT RETURNED TO SERVICE. NRTC: 11,369. (X)

Part: SKIN — CRACKED (FUSELAGE)

DURING HEAVY MAINTENANCE VISIT, SEVERAL CRACKS NOTED AT FORWARD AND AFT SIDES OF THE LT WING ILLUMINATION LIGHT ASSY. REPAIRED PER ECO 2429. AIRCRAFT RETURNED TO SERVICE. NRTC: 11,646. (X)

Part: TRANSVERSE BEAM — CRACKED (BS 677)

DURING HEAVY MAINTENANCE VISIT, BS 677 TRANSVERSE BEAM CRACKED, 2ND SEAT TRACK FROM LEFT. REPAIRED PER ECO 1933R3. AIRCRAFT RETURNED TO SERVICE. NRTC: 11,579. (X)