N820AL

Part: WIRE — BROKEN (ZONE 200) · airframe 35,384 hrs · 4,267 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY ESCAPE PATH LIGHT ON SEAT 9H IS INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AND TERMINAL. REPLACED TERMINAL IAW AMM 20-11-02. OPS TEST PASS ON SEAT 9H

Part: LIGHT — BROKEN (ZONE 200) · airframe 33,686 hrs · 4,075 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 31D EMERGENCY EXIT AISLE LIGHTING BROKEN. REPLACED SEAT 31D EPL PER AMM33-51-06.

Part: STRAP — MISSING (ZONE 800)

AIRCRAFT IN BASE MAINTENANCE: MAIN CABIN OFCR E-HATCH HANDEL IS MISSING. MAINTENANCE REPLACED OFCR HATCH STRAP IAW SRM 787-A-51-43-01-01A-010A-A.

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 32,112 hrs · 3,879 cycles

AIRCRAFT IN BASE MAINTENANCE: WELS (WIRELESS EMERGENCY LIGHTING SYSTEM) ONLY REPORTING 28 OUTOF 29 UNITS. MAINTENANCE REPLACED WBU24. IAW B787-AMM-33-50-71-N7A-421A-A.

Part: BATTERY — DISCHARGED (R4 FLASHLIGHT) · airframe 29,942 hrs · 3,616 cycles

AIRCRAFT WAS NOT GROUNDED: FLASHLIGHTS AT 4R DOOR WILL NOT TEST. MAINTENANCE REPLACED BATTERIES IN FLASHLIGHTS AT 4R IAW AMM 25-64-00.

Part: DOOR — OUT OF ADJUST (ZONE 200 - FUSE) · airframe 27,795 hrs · 3,361 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR AT LAV 4L STICKS AND DOES NOT OPEN AND CLOSE PROPERLY. MAINTENANCE ADJUSTED DOOR AT LAV 4L IAW CMM 25-49-85.

Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 27,515 hrs · 3,328 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY DOOR 4L HARD TO OPEN AND CLOSE. ADJUSTED DOOR, FUNCTIONAL CHECK GOOD. PER AMM 25-41-00.

Part: OVEN — DEFECTIVE (ZONE 900 - LAV/G) · airframe 26,230 hrs · 3,167 cycles

AIRCRAFT WAS GROUNDED: ABOUT 30 MINUTES INTO FLIGHT THE FLIGHT ATTENDANTS REPORTED SMOKE AND ELECTRICAL SMELL FROM OVEN 9C IN AFT GALLEY . OVEN DID NOT TURN OFF UNTIL AFT GALLEY MASTER POWER SWITCH WAS TURNED OFF. MAINTENANCE FOUND OVEN FAULT CODES F21 AND F02 ALONG WITH EVIDENCE OF BURNT FOOD. **SUPPLEMENTAL REPORT FOR AALA202307032698: MAINTENANCE REPLACED OVEN PER AMM 25-32-00 . ** (CLOSED)

Part: OVEN — DEFECTIVE (ZONE 900 - LAV/G) · airframe 26,230 hrs · 3,167 cycles

AIRCRAFT WAS GROUNDED: ABOUT 30 MINUTES INTO FLIGHT THE FLIGHT ATTENDANTS REPORTED SMOKE AND ELECTRICAL SMELL FROM OVEN 9C IN AFT GALLEY . OVEN DID NOT TURN OFF UNTIL AFT GALLEY MASTER POWER SWITCH WAS TURNED OFF. MAINTENANCE FOUND OVEN FAULT CODES F21 AND F02 ALONG WITH EVIDENCE OF BURNT FOOD. **SUPPLEMENTAL REPORT WILL BE SUBMITTED. ** (OPEN)

Part: BATTERY — INOPERATIVE (ZONE 200 - FUSE) · airframe 22,921 hrs · 2,716 cycles

AIRCRAFT WAS NOT GROUNDED: OVERHEAD FLIGHT ATTENDANT REST FLASHLIGHT BATTERY INOPERATIVE. REPLACED FLASHLIGHT BATTERY PER AMM 25-64-00.

Part: CONNECTOR — DISCONNECTED (ZONE 200 - FUSE) · airframe 22,155 hrs · 2,613 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 1D, H TO 3D, H EMERGENCY FLOOR PROXIMITY LIGHTS DO NOT EXTINGUISH. FOUND ELECTRICAL CONNECTOR AT WIRELESS EMERGENCY LIGHTING CONTROL UNIT DISCONNECTED. SECURED CONNECTOR. ACCOMPLISHED SATISFACTORY OPERATIONAL TEST PER AMM 33-51-07.

Part: LIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 19,830 hrs · 2,304 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 16H EMERGENCY EXIT LIGHT INOPERATIVE. **SUPPLEMENTAL REPORT FOR AALA202112220842: REPLACED LIGHT PER AMM 33-51-06..** (CLOSED)

Part: NONE — NONE · airframe 19,830 hrs · 2,304 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 16H EMERGENCY EXIT LIGHT INOPERATIVE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: BATTERY PACK — NO TEST (ZONE 200 - FUSE) · airframe 19,018 hrs · 2,157 cycles

AIRCRAFT WAS NOT GROUNDED: 3L FLIGHT ATTENDANT FLASHLIGHT WILL NOT PRESS TO TEST. REPLACED BATTERY PACK AT 3L FLIGHT ATTENDANT STATION PER AMM 25-64-00.

Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 17,625 hrs · 1,966 cycles

AIRCRAFT WAS NOT GROUNDED: SMOKE LAVATORY MESSAGE FALSE WARNING. ACCOMPLISHED 1L SMOKE DETECTOR OPERATIONAL TEST PER AMM 26-13-00.CHECKS NORMAL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 15,867 hrs · 1,726 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY LIGHTS ROW 16-19 WILL NOT EXTINGUISH. FOUND CONNECTOR AT SEAT LEG DISCONNECTED. RECONNECTED CONNECTOR, PER STANDARD PRACTICES.

Part: CONTROL UNIT — NO TEST (EMERGENCY LIGHTS) · airframe 15,364 hrs · 1,662 cycles

AIRCRAFT WAS GROUNDED. WHILE WORKING CARD 2803 FOUND WELS CONTROL UNIT BAD AT DOOR R2 FORWARD. REPLACED WELS CONTROL UNIT AT R2 DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK, PER AMM 33-51-07.

Part: HANDLE — MISSING (ESCAPE HATCH) · airframe 15,170 hrs · 1,636 cycles

AIRCRAFT WAS NOT GROUNDED. THE OFCR ESCAPE HATCH HANDLE IS MISSING AND CANNOT BE OPEN IN FLIGHT. REPLACED THE HANDLE/STRAP, PER AMM 25-51-22.

Part: CIRCUIT CARD — MALFUNCTIONED · airframe 13,364 hrs · 1,408 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS MULTIPLE STS MSGS IN CRZ, FLAP EMCU PWR, CRUISE FLAPS DISAGREE, FLAPS SECONDARY FAIL, ELEC P200 PANEL, CARGO FWD EXHAUST FAN, INTERGRATED CLG RECIRC AIR . MAINTENANCE REPORTS MSG 24-20623 P200 ELCU (P) CARD M2409018 SLOT POSN 5 REPLACED AND TESTED SATISFACTORY IAW AMM 24-09-04-320A. FIM MSG 24-29804, AIRCRAFT POWER RESTART, PROCEDURE COMPLETED. FLAP HIGHLIFT TEST COMPLETED IAW FIM 27-22713 MSG, ALL OPS NORMAL. EDAS SYSTEM TEST COMPLETED SATISFACTORY IAW FIM 27-20-F4-15A-421A.

Part: HINGE PIN — MISSING (ENTRY DOOR) · airframe 13,301 hrs · 1,403 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS OFCR ENTRY DOOR EMERGENCY RELEASE BROKEN, FOUND FLAP COVER FOR MANUAL DOOR RELEASE MISSING HINGE PIN. SUPPLEMENTAL ACTION SECT 4 AND SECT 5: INSTALLED LATCH COVER ON OFCR DOOR. OPS CHK GOOD. (CLOSED)

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 11,058 hrs · 1,148 cycles

AIRCRAFT WAS NOT GROUNDED: 4R FLIGHT ATTENDANT FLASHLIGHT BATTERY DEAD. MAINTENANCE REPLACED 4R FLASHLIGHT BATTERY PER AM 25-64-00.

Part: CONTROLLER — INOPERATIVE · airframe 8,206 hrs · 842 cycles

THE R4 DOOR EXIT LIGHT DIMMER WAS INOPERATIVE. REPLACED THE DIMMING CONTROLLER IAW AMM 56-31-03. OPS CHECKED GOOD.

Part: CONTROL UNIT — FAULTY (CABIN) · airframe 7,405 hrs · 768 cycles

THE AIRCRAFT WAS GROUNDED. EMERGENCY PATHWAY LIGHTING AT SEAT ROW 1,2, AND 3. REPLACED WELS CONTROL AND BATTERY UNIT.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 3,418 hrs · 370 cycles

EMERGENCY FLASHLIGHT IN THE OVERHEAD FLIGHT CREW REST AREA IS INOPERATIVE. REMOVED AND REPLACED THE BATTERY IAW AMM 25-64-00. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 2,664 hrs · 295 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT IN THE OVERHEAD FLIGHT ATTENDANT REST AREA IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW DMC-B787-A-25-64-00. OPERATIONAL CHECK GOOD.

Part: SEAL — OUT OF ADJUST (L2 DOOR) · airframe 2,437 hrs · 273 cycles

AIRCRAFT WAS NOT GROUNDED. L2 DOOR ARMING LEVER COVER IS VERY HARD TO MOVE WHEN ACCESSING THE ARM/DISARM LEVER. REINSTALLED COVER GUIDE SEAL IAW AMM 52-11-24. OPERATIONAL CHECK GOOD.

Part: TIRE — BLOWN (ZONE 700) · airframe 728 hrs · 109 cycles

AIRCRAFT WAS GROUNDED. DURING TAXI, NR 3 TIRE BLOWN, CONFIRMED ON WALKAROUND. REMOVED AND REPLACED NR 3 TIRE ASSEMBLY IAW AMM 32-45-01. OPERATIONAL CHECK GOOD.

Part: ISOLATION VALVE — MALFUNCTIONED (THRUST REVERSER)

THRUST REVERSER ISOLATION VALVE ILLUMINATED DURING CLIMBOUT AT 1000 FT. SOCC ADVISED AIRCRAFT TO RETURN TO HNL. LIGHT WENT OUT ON FINAL APPROACH WITH GEAR DOWN. FOUND NOSE GEAR AIR GROUND SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH PER AMM 78-34-61. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE.

Part: ISOLATION VALVE — MALFUNCTIONED (THRUST REVERSER)

THRUST REVERSER ISOLATION VALVE LIGHT ILLUMINATED DURING CLIMBOUT AT 1000 FT. SOCC ADVISED AIRCRAFT TO RETURN TO HNL. LIGHT WENT OUT ON FINAL APPROACH WITH GEAR DOWN. RE-RIGGED THE NOSE GEAR AIR GROUND CABLE AND SWITCH PER AMM 78-34-61 PG 501. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — CRACKED (BS 727 S18L) · airframe 50,015 hrs · 72,837 cycles

BS 737 FRAME CRACKED AT STR 18L. REPLACED 727 FRAME AT STR 18L IAW ALOHA'S ECO 1785.

Part: ISOLATION VALVE — MALFUNCTIONED (THRUST REVERSER) · airframe 50,013 hrs · 72,827 cycles

THRUST REVERSER ISOLATION VALVE LIGHT ILLUMINATED ON CLIMBOUT. SOCC ADVISED AIRCRAFT TO RETURN TO HNL. REPLACED AB CARD IN ENGINE ACCESSORY UNIT. OPS TEST OK PER MM 78-36-01. AIRCRAFT CLEARED FOR SERVICE. ON THE NEXT FLIGHT (208), THE THRUST REVERSER ISOLATION VALVE LIGHT ILLUMINATED AGAIN. AIRCRAFT LANDED IN OGG WITHOUT INCIDENT AND THE THRUST REVERSER SYSTEM WAS PLACED ON MEL 78-1-1. AIRCRAFT RETURNED TO SERVICE. REPLACED NR 1 ENGINE LOW OIL PRESSURE SWITCH IAW AMM 79-33-11. LEAK AND OPS CK OK. PLACARD REMOVED. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN PANEL — CRACKED (BS 767) · airframe 49,456 hrs · 71,621 cycles

FOUND TWO FUSELAGE SKIN CRACKS AFT OF LT AFT WING-TO-BODY FAIRING: .5 INCH CRACK AT BS 767, STRINGER 17L AND 3 INCH CRACK AT BS 787, STRINGER 18L. CUT CRACKS OUT .040 INCH INSURANCE CUT. PERFORMED HFEC AROUND CUTOUTS, NO CRACK PROPAGATION NOTED IAW BOEING NDT MANUAL PART 6, 51-00-00. REPAIRED WITH 21 X 53 INCH SKIN PATCH: FABRICATED DOUBLER (0322024T3) AND TRIPLER (0502024T3). REPAIRED CRACKS PER SRM 53-30-3, FIG 48, DETAIL XI.

Part: PUMP — MALFUNCTIONED (HYDRAULIC SYS)

NON-ETOPS FLT 266 HNL-OGG, AFTER TAKEOFF, HYD SYS QUANTITY INDICATION DROPPED TO 1.5 GAL. AND SYSTEM A LOW PRESSURE LIGHT ILLUMINATED. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED HYDRAULIC RESERVOIR TO FULL, PERFORMED ENGINE RUN, OPERATED HYDRAULIC SYSTEM AND CONDUCTED A VISUAL INSPECTION NR 1 ENGINE CASE DRAIN FILTER. NO HYDRAULIC SYSTEM LEAKS NOTED. FOUND NR 2 ENGINE HYDRAULIC SYSTEM A PUMP LOW PRESSURE LIGHT INTERMITTENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP, IN ACCORDANCE WITH AMM 29-11-31. ENGINE RUN AND LEAK CHECK VERIFIED OK.

Part: SPAR — CORRODED (WING)

DISCOVERED CORROSION AT WBL 245, 254, 336, AND 341 ON THE UPPER WING SURFACE REAR SPAR. REPAIR CONSISTED OF BLENDING OUT THE DAMAGED AREA PER SRM 57-30-1, FIGURES 1A AND 1B INSTRUCTIONS. REMOVED FASTENERS IN THE BLEND OUT AREA. INSTALLED HI-LOCKS WET WITH BMS 5-26 SEALANT IN TRANSITION FIT HOLES. CLEAN AND TREEATED ALL EXPOSED SURFACES, FILLED REMAINING VOIDS AND GAPS WITH BMS 5-95 SEALANT. REPAIR COMPLETED IAW ECO 3403. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SPAR — CORRODED (WING)

DISCOVERED CORROSION AT WBL 349 AND 503 ON THE UPPER WING SURFACE REAR SPAR. REPAIR CONSISTED OF BLENDING OUT THE DAMAGED ARE PER SRM 57-30-1, FIGURE 1A AND 1B INSTRUCTIONS. FABRICATED AN .020 INCH THICK EXTERNAL REPAIR DOUBLER FROM 7075-T6 SHEET. CLEAN AND TREATED ALL EXPOSED SURFACES. BONDED THE EXTERNAL DOUBLER OVER THE BLEND AREA, WITH BMS 5-95 SEALANT. INSTALLED AND SECURED THE EXTERNAL DOUBLER IN PLACE USING THE EXISTING FASTENERS WITH THE BLEND OUT AREA. INSPECTED REWORKED AREA ENSURING CORROSION AND CRACK FREE. APPLIED TOP COAT FINISHES TO REPAIR AREA. FILLET/TAPERED SEAL AROUND EDGES. REPAIR COMPLETED IAW ECO 3403. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FRAME — CRACKED (BULKHEAD)

DISCOVERED CRACK AT BS 727 OUTBOARD CHORD. REMOVED FASTENERS AS REQUIRED COMMON TO BS 727 OUTER CHORD FROM S-27 UP TO S-18. TRIM END OF VERTICAL STIFFENER TO PROVIDE CLEARANCE FOR CHORD SPLICE COMPONENTS. LAID OUT LOCATION FOR CUTTING CHORD. USED REMOVED SECTION OF CHORD FOR TEMPLATE. REPLACED RIGHT UPPER CHORD SECTION. APPLIED CHEMICAL FILM TREATMENT AND ONE COAT BMS 10-11, TYPE 1 PRIMER TO ALL BARE SURFACES. REPAIR COMPLETED IAW ECO 1785 R5 WITH DEVIATION O. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (LEADING EDGE)

REMOVED CORROSION FROM RIGHT FIXED LEADING EDGE AT WBL 375. TRIMMED OUT DAMAGED AREA. FABRICATED A FILLER AND DOUBLER PER TABLE 1. ALODIZED ALL TRIMMED EDGES AND BARE SURFACES. INSTALLED REPAIR PARTS WET WITH BMS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 57-40-1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRINGER — CORRODED (APU BAY)

APU INLET LONGERON STIFFENER, TORQUE BOX, EXFOLIATED. CUT AND REMOVED DAMAGED PORTION OF FORMED STRUCTURE. FABRICATED REPAIR PARTS FROM MATERIALS SPECIFIED IN TABLE 1. APPLIED ONE COAT OF BMS 10-11, TYPE 1 PRIMER, AND INSTALLED REPAIR PARTS WET WITH FASTENERS, MAKING A FAYING SURFACE SEAL WITH BMS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 51-40-1, FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

TRIMMED AREA AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED 3 FILLERS AND REPAIR DOUBLER FROM 2024-T3 AS SHOWN IN PHOTO 1, MAINTAINING 2D EDGE MARGIN, MIN .5 INCH OUTSIDE CORNER RADIUS WITH 2.0 INCH INSIDE CORNER RADIUS AND 5D-6D SPACING AT NEW FASTENER LOCATIONS. FINISH ALL BARE ALUMINUM WITH ALODINE AND TWO COATS OF BMS 10-11 TYPE 1, PRIMER. INSTALLED FILLERS AND REPAIR DOUBLER WITH FASTENERS INDICATED IN FIGURES 1, 2, AND TABLE 1. APPLIED FILLET SEAL OF BMS'S 5-95 SEALANT AROUND EDGES OF REPAIR, BS 420, 440, 460, 480 AND 767. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IAW ECO3250, DEVIATION AF. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WEB — CRACKED (FUSELAGE)

TRIMMED OUT DAMAGED WEB. HFEC INSPECTED THE EDGE OF CUTOUT. ENLARGED TRIM BY .04 AS A INSURANCE CUT. FABRICATED A .50 INCH THICK REPAIR WEB, TOW .063 INCH THICK DOUBLERS AND A .063 INCH THICK TAPER FILLER FROM 2024-T3 CLAD SHEET. FABRICATED THREE EACH REPAIR STIFFENERS FROM7075-T6511 EXTRUSION. FABRICATED A 50:1 TAPER FILLER FROM 2024-T3 CLAD. FLAT PEENED REPAIR T-STIFFENERS. ALODINED AND PRIMED REPAIR PARTS AND BARE ALUMINUM. INSTALLED REPAIR PARTS IAW FIGURE 3, USING FASTENERS IDENTIFIED, WET WITH BMS 5-95 SEALANT MAINTAINING 5D TO 6D SPACING AT NEW LOCATIONS. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IAW ECO 2917. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRUCTURE — CORRODED (FUSELAGE)

BLENDED REWORK AREA TO A 10 TO 1 RATION SPANWISE. PERFORMED 10X VISUAL TO ENSURE CORROSION COMPLETELY REMOVED. FLAT PEENED, ALODINED AND PRIMED REWORKED AREA WITH BMS 10-11, TYPE 1. FABRICATED EXTERNAL DOUBLER AND REPAIR STRAP FROM .150 INCH 7075-T7351 PLATE. FABRICATED REPAIR FILLERS FROM 7075-T6. SHOT PEENED, ALODINED AND PRIMED ALL REPAIR PARTS. INSTALLED REPAIR PARTS WET WITH BMS 5-95 SEALANT. APPLIED FINISH COAT. REPAIR COMPLETED IAW ECO 2513. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — GOUGED (FUSELAGE)

TRIMMED OUT DAMAGED AREA. HFEC INSPECTED THE EDGE OF CUTOUT. ENLARGED TRIM BY .04 AS AN INSURANCE CUT. ALODINED AND PRIEMD REWORKED AREA WITH BMS 10-11, TYPE 1. FABRICATED EXTERNAL DOUBLER FROM .063 INCH 2024-T3 CLAD. FABRICATED REPAIR FILLERS FROM 2024-T3 CLAD. ALODINED AND PRIMED ALL REPAIR PARTS. INSTALLED REPAIR PARTS WET WITH BMS 5-95 SEALANT. APPLIED FINISH COAT AND VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IAW ECO 3317. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LINE — LEAKING (NR 2 ENGINE)

DURING TAKEOFF ROLL, UNABLE TO ACHIEVE TAKEOFF POWER ON ENGINE NR 2, FIREWALL ONLY GAVE 1.86 EPR. ABORTED TAKEOFF AND RETURNED TO GATE. FOUND A LEAK IN THE TURBINE EXHAUST LINE, REPLACED THE PT7 TUBE ASSY IAW MM 77-00. LEAK CHECK OF LINE OK. JETCAL ACCOMPLISHED IAW FORM M-215. AIRCRAFT RETURNED TO SERVICE. (M)

Part: PRESSURE SWITCH — MALFUNCTIONED (NR 1 ENGINE)

DURING TAKEOFF, WITH TAKEOFF POWER SET THE NR 1 ENGINE EPR WAS 0.25 TOO HIGH. THE AIRCRAFT RETURNED TO HNL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND FOD IN THE NR 1 ENGINE PT2 LINE. THE PT2 LINE WAS CLEANED, AND ENGINE PERFORMANCE RUN WAS COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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

Part: FRAME — CORRODED (FUSELAGE)

BLENDED SURFACE IS SMOOTHLY RADIUSED AND RIDGES BLENDED TO A 10 TO 1 RATIO SPANWISE. VERIFIED CORROSION REMOVED USING NDT METHOD. FLAT PEENED REWORKED AREA. APPLIED ALODINE AND TWO COATS BMS 10-11, TYPE 1 PRIMER TO REPAIR WASHERS AND REWORKED SURFACE. APPLIED BMS 5-95 SEALANT TO ALL FAYING SURFACES. FILLED BLENDOUT WITH BMS 5-95 SEALANT. VERIFIED 8110-3 RECEIVED. REPAI COMPLETED IAW ECO 2154R3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

TRIMMED AREA AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED 3 EACH FILLERS AND A REPAIR DOUBLER FROM 2024-T3 AS SHOWN IN PHOTO 1, MAINTAINING 2D EDGE MARGIN AND 5D-6D SPACING AT NEW FASTENER LOCATIONS. FINISH ALL BARE ALUMINUM WITH ALODINE AND TWO COATS OF BMS 10-11 TYPE 1, PRIMER. INSTALLED FILLERS AND DOUBLERS WITH FASTENERS INDICATED IN FIGURES 1, 2 AND TABLE 2. APPLIED FILLET SEAL OF BMS 5-95 SEALANT AROUND EDGES OF REPAIR. REPAIR COMPLETED IAW ECO 3250, DEVIATION AG. WINDOW FRAME P/N 65-465271, 291, 311, 321 AND 65-465491, BS 420, 440, 460, 480 AND 767. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WEB — CRACKED (FUSELAGE)

REMOVED EXISTING FASTENERS, STIFENERS, FILLERS, AND DAMAGED SECTION OF WEB AS SHOWN ON FIGURE 5. FABRICATED A .050 INCH THICK REINFORCING DOUBLER FROM 7075-T6. ALODINE AND APPLIED BMS 10-11 TYPE 1 PRIMER TO ALL BARE SURFACES. INSTALLED RE-ENFORCING DOUBLER, WEB, STIFFENERS, AND FILLERS WITH NEW FASTENERS IAW ECO 2223 FIGURE 5 AND FIGURE 7. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE)

ON CLIMB OUT, AIRCRAFT WAS UNABLE TO MAINTAIN PRESSURIZATION. AIRCRAFT RETURNED AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER. BITE AND OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROLLER — FAILED (CABIN PRESSURE)

FLT 66 - HNL-OGG - PRESSURIZATION AUTO FAIL LIGHT ILLUMINATED AT 14,000 FT AND STANDBY LIGHT CAME ON. SWITCHED TO STANDBY MODE. CABIN RATE STARTED CLIMBING AND DESCENDING AT 4,000 FPM. SWITCHED TO MANUAL DC THEN AC MODE AND STILL UNABLE TO CONTROL PRESSURIZATION. DECLARED AN EMERGENCY AND DESCENDED TO 5400 FEET AND UNABLE TO CONTROL PRESSURE. UNEVENTFUL LANDING IN OGG. AIRCRAFT FERRIED TO HNL. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER. GROUND CHECKED OK PER MM 21-31-00. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

DISCOVERED CRACK AT BS 727A, S-15R. FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: SKIN — DAMAGED (FUSELAGE)

AIRCRAFT SKIN AND FRAME DAMAGED AT BS 847 THROUGH BS 887, STRINGER 25L THROUGH STRINGER 25R. REMOVED DAMAGED AREA ,PERFORMED HFEC INSPECTION AROUND CUT OUT NO DEFECTS NOTED. REPAIRED STRINGER S27L AT BS 847 IAW SRM 53-10-3 FIG INSTALLATION OF REPAIR DOUBLER COMPLETED IAW SRM 53-30-3 FIG 28. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SPAR — CORRODED (RT HORIZ STAB)

IDENTIFIED SURFACE CORROSION ON THE RIGHT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD SS 101.90. REPAIRED BY REMOVING CORROSION, BLEND OUT COMPLETED, CLEANED AND TREATED CORRODED AREA. REPAIR COMPLETED ON 12/26/00 IAW SRM 57-10-1 PAGE 6. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

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

Part: POWER SUPPLY — FAILED (E/E BAY)

FLT 302 - HNL-OGG - AFTER ENGINE START BOTH NR 1 AND NR 2 FF INDICATORS HAD INDICATION HOWEVER BOTH WERE PULSING. ABORTED TAKEOFF RY8L, NO INDICATION OF FUEL FLOW. TAXIED BACK TO GATE. UPON POWER APPLICATION NEITHER FF INDICATOR ROSE ABOVE MINIMUM SETTINGS. REPLACED FUEL FLOW POWER SUPPLY. GROUND IDLE RUN CHECKS GOOD, AIRCRAFT RETURN TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

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

Part: SENSOR — INOPERATIVE (NR 4 SLAT)

FLT 278 - HNL-OGG - RIGHT KRUEGER FLAP (NR 4 LED) WOULD NOT RETRACT AFTER TAKEOFF. CALLED IN WITH SLAT INDICATION PROBLEM. RETURNED TO HONOLULU. NO EMERGENCY DECLARED, AIRCRAFT LANDED WITH NO FURTHER PROBLEMS. REMOVED AND REPLACED EXTEND SENSOR ON THE NR 4 KRUEGER FLAP. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

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

Part: BATTERY PACK — INOPERATIVE (PAX CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 1 FLOOR EMERGENCY POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ENGINE — BIRD STRIKE (NR 1)

FLT 63 - HNL-LIH - BIRD STRIKE NR 1 ENGINE. ENGINE ROLLED BACK INITIALLY AND RETURNED TO NORMAL PARAMETERS. RETURNED TO HNL. UNEVENTFUL LANDING. PERFORMED BIRD STRIKE CONDITION INSPECTION IAW FORM M-106. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED AFT SERVICE EMERGENCY EXIT LIGHT POWER PACK DUE TO FLICKERING. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: SKIN — CORRODED (WS 382)

FOUND CORROSION ON LEFT WING AT WS 382. CLEANED AND TREATED. MATERIAL REMOVAL EXCEEDED SRM 57-30-1 LIMITS. ACCOMPLISHED FINAL REPAIR PER ECO 1684R10. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO NO TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 1, NR 2, AND NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — GOUGED (BS 867-887)

AIRCRAFT SUSTAINED SKIN DAMAGE BETWEEN BS 867 AND BS 887 AT STRINGER 27 RIGHT. THREE GOUGES NOTED. REPAIRED IAW SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FORWARD ENTRY EMERGENCY IDENTIFIER LIGHT ASSEMBLY NO TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

REPLACED AFT EMERGENCY SLIDE BATTERY POWR SUPPLY. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: LIGHT — INOP (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: CONTROL MODULE — INOPERATIVE (CABIN)

CENTER EMERGENCY EXIT CONTROL MODULE ASSY INOP. REPLACED CENTER EMERGENCY EXIT CONTROL MODULE, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

AFT EMERGENCY SLIDE LIGHT INOP. REPLACED BATTERY POWER PACK, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 2 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY CONDITION INOP. REPLACED BATTERY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 6 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY CONDITION INOP. REPLACED BATTERY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: PROXIMITY SWITCH — MALFUNCTIONED (RT MLG)

FLT 80 - HNL-KOA - RIGHT MAIN GEAR UNSAFE. RED LIGHT REMAINED ILLUMINATED AFTER GEAR UP. RETURNED TO HNL. PERFORMED LANDING GEAR EXTENSION/RETRACTION TEST. NO DISCREPANCIES. MEASURED AND FOUND UPLOCK SENSOR GAP TO BE WITHIN TOLERANCES IN MM CHAPTER 32-61-21. REPLACED RT MLG UPLOCK PROXIMITY SWITCH AND MLG RED LIGHT PC CARD FOR T/S PURPOSES AND PRECAUTIONARY REASONS. (M)

Part: LOGIC CARD — MALFUNCTIONED (RT MLG)

FLT 80 - HNL-KOA - RIGHT MAIN GEAR UNSAFE. RED LIGHT REMAINED ILLUMINATED AFTER GEAR UP. RETURNED TO HNL. PERFORMED LANDING GEAR EXTENSION/RETRACTION TEST. NO DISCREPANCIES. MEASURED AND FOUND UPLOCK SENSOR GAP TO BE WITHIN TOLERANCES IN MM CHAPTER 32-61-21. REPLACED RT MLG UPLOCK PROXIMITY SWITCH AND MLG RED LIGHT PC CARD FOR T/S PURPOSES AND PRECAUTIONARY REASONS. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 6 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY CONDITION INOP. REPLACED BATTERY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 5 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY CONDITION INOP. REPLACED BATTERY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED CABIN

REPLACED AFT SLIDE BATTERY POWER SUPPLY DUE TO LIGHT BEING INOP. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 1 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY CONDITION LED'S INOP. REPLACED BATTERY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 6 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY CONDITION LED'S INOP. REPLACED BATTERY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CHANNEL — CRACKED (BS 328)

CHANNEL ATTACHED TO FLOORBEAM WAS FOUND TO BE CRACKED IN 2 PLACES. CHANNEL LOCATED AT BS 328 AND BL 32R. REPAIRED IAW SRM 53-10-2 FIGURE 7. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — DAMAGED (BS 716)

SEAT TRACK AT BS 716 AND BL 24L DAMAGED BEYOND LIMITS. REPLACED SEAT TRACK PER SRM 53-10-5. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STIFFENER — CRACKED (BS 328)

STIFFENER CRACKED ON THE FLOORBEAM AT BS 328 AND RBL 32. REPLACED MANUFACTURED AND REPLACED STIFFENER IAW BOEING SRM 53-10-2. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — DAMAGED (BS 597)

SEAT TRACK AT BS 597 AND BL 48R DAMAGED BEYOND LIMITS. REPLACED SEAT TRACK PER SRM 53-10-5. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND POSITION NR 6 EMERGENCY FLOOR LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: TURBINE — FAILURE (NR 1 ENGINE)

FLT 81 - KOA-HNL - SERVICE VIBRATION ON NR 1 ENGINE AFTER TAKEOFF AND SUDDEN LOSS OF THRUST, EPR DECREASED FROM 1.98-1.5 EGT AT 550 ONE MINUTE THEN CLIMBED TO RED LINE. NR 1 THRUST REVERSER FOD DAMAGE. NR 1 TAILPIPE EXTENSION FOD DAMAGE. RETURNED AIRCRAFT TO KOA. REPLACED NR 1 ENGINE ASSY IAW FORMS 17211, 17212, 17213, 17214, M-215. RUN-UP CHECK OK. REPLACED NR 1 THRUST REVERSER ASSY IAW FORM M-211. OPS AND LEAK CHECK OK. REPLACED NR 1 TAILPIPE EXTENSION IAW FORM M-211. RII COMPLETED FOR INSTALLATION OF NR 1 ENGINE PER FORM M-211, M-212, M-213, M-214, AND M-215. (M)

Part: RAM AIR INLET — CRACKED (LEFT)

DURING CPCP VISIT, FOUND CRACK AT LT RAM AIR DUCT INLET; RT CORNER AT RADIUS. REPAIRED CRACK PER SRM 51-40-00 AND INSTALLED REPLACEMENT WEB. TAT: 35,050.9 HOURS. TAC: 39,058. (X)

Part: RAM AIR INLET — CRACKED (RIGHT)

DURING CPCP VISIT, FOUND CRACK AT RT RAM AIR DUCT INLET; LT CORNER AT RADIUS. REPAIRED CRACK PER SRM 51-40-00 AND INSTALLED REPLACEMENT WEB. TAT: 35,050.9 HOURS. TAC: 39,058. (X)

Part: LIGHT — INOPERATIVE (CABIN)

ON SERVICE CHECK, FOUND POSITION NR 6 EMERGENCY FLOOR LIGHT INOP. REPLACED LIGHT ASSY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: RELIEF VALVE — OUT OF ADJUST (NR 2 ENGINE)

FLT 110 - HNL-OGG - DURING TAKEOFF ROLL WITH MAX POWER SET, THE NR 2 OIL PRESSURE EXCEEDED UPPER REDLINE LIMITS. ALL OTHER ENGINE PARAMETERS WERE NORMAL. ADJUSTED OIL PRESSURE RELIEF VALVE FOR PWA MM 72-00, PAGE 598L-H. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND NR 6 POSITION EMERGENCY FLOOR LIGHT LED'S INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON DAILY CHECK, FOUND POSITION NR 5, FLOOR EMERGENCY LIGHT INOP. REPLACED LIGHT BATTERY PACK. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON DAILY CHECK, FOUND POSITION NR 3 FLOOR EMERGENCY LIGHT INOP. REPLACED LIGHT BATTERY PACK. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON DAILY CHECK, FOUND POSITION NR 2, FLOOR EMERGENCY LIGHT INOP. REPLACED LIGHT BATTERY PACK. OPS 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 OK. AIRCRAFT RETURNED TO SERVICE. TAT: 34,500:07 HOURS. TAC: 37,853. (X)

Part: BATTERY — DISCHARGED (CABIN)

DURING OVERNIGHT CHECK, REPLACED FLOOR PROXIMITY LIGHT ASSY AND BATTERY FOR ROW 8 DUE TO INOPERABLE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 34,500:07 HOURS. TAC: 37,853. REF: OPERATOR CONTROL NR TSAA9733260.

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: BATTERY — DISCHARGED (CABIN)

DURING OVERNIGHT CHECK, REPLACED BATTTERY FOR ROW 17 EMERGENCY FLOOR PROX LIGHT ASSEMBLY DUE TO INOP. OPERATIONAL CHECK OF AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING OVERNIGHT CHECK, REPLACED ROW 12 EMERGENCY FLOOR PROXIMITY LIGHT ASSY DUE TO RED LIGHT REMAINS ON. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 34,314:15 HOURS. TAC: 37,428. (X)

Part: BATTERY — DISCHARGED (CABIN)

DURING OVERNIGHT CHECK, REPLACED BATTERY FOR ROW 12 FLOOR PROXIMITY LIGHT ASSY DUE TO GREEN LIGHT INOPERABLE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 34,314:15 HOURS. TAC: 37,428. (X)

Part: ENGINE — FAILED (NR 1)

HNL/OGG - FLT 78 - PILOT REPORT - SPARKS COMING OUT OF NR 1 ENGINE DURING CLIMB-OUT. AIRCRAFT RETURNED TO HNL. REMOVED AND REPLACED NR 1 ENGINE ASSY PER M-212, M-213, M-211, M-214, AND M-215. OPS AND LEAK CHECK OK. (X)

Part: UNSAFE LIGHT — ILLUMINATED (LT/RT MLG)

FLT 70 - HNL-OGG - UNSAFE GEAR INDICATION AFTER TAKEOFF, LEFT AND RIGHT MAIN GEAR. RETURNED TO HNL GEAR RETRACTION AND EXTENSION (6 CYCLES) IAW MM 32-32-0, PAGE 501. SYSTEM AND INDICATION FUNCTIONED NORMAL. OIL FOR SERVICE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

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: 33,942:17 HOURS. TAC: 36,586. (X)

Part: FRAME — CORRODED (BS 460)

DURING SCHEDULED INSPECTION OF FWD CARGO COMPARTMENT BODY FRAME (ECO 1571R7, AD 89-11-06), DISCOVERED BS 460 EXFOLIATED AT STR 24L. REPAIRED PER ECO 2804 W/DEV. A - BSL 460 LT LOWER FRAME CORROSION REPAIR. AIRCRAFT RETURNED TO SERVICE. MATERIAL I.D. - FABRICATED SPLICE DOUBLER .063 INCH 7075-0 HEAT TREAT TO T-6, REPAIR STRAP .040 INCH 7075-T6. TAT: 33,459.:49 HOURS. TAC: 35,509. (X)

Part: FRAME — CORRODED (BS 480/500)

DURING SCHEDULED INSPECTION OF FWD CARGO COMPARTMENT BODY FRAME (ECO 1571R7, AD 89-11-06) , DISCOVERED BS 480 AND BS 500 FRAMES EXFOLIATED AT STR 24L. REPAIRED PER ECO 2803, BS 480 AND 500 LT LOWER LOBE FRAME CORROSION REPAIRS. AIRCRAFT RETURNED TO SERVICE. MATERIAL I.D. FABRICATED REINFORCING EXTERIOR AND SECTION EXTENDED. SPLICE .063 INCH 7075-0 HEAT TREAT TO T6. TAT: 33,459.:49 HOURS. TAC: 35,509. (X)