N818AL

Part: ELEC CONNECTOR — DISCONNECTED (ZONE 200) · airframe 33,325 hrs · 4,706 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT LIGHT OVER 22D OVERHEAD BIN IS NOT ILLUMINATING. MAINTENANCE RESEATED TERMINAL CONNECTOR ON BACK OF LIGHT OVER SEAT 22D. OPS GOOD IAW AMM 33-51-00.

Part: ELEC CONNECTOR — DISCONNECTED (ZONE 800) · airframe 33,325 hrs · 4,706 cycles

AIRCRAFT IN BASE MAINTENANCE: GREEN EMERGENCY EXIT SIGN OVER 2L DOOR IS NOT ILLUMINATING DURING TEST. MAINTENANCE TROUBLESHOT, RESEATED TERMINAL CONNECTOR ON BACK OF LIGHT. OPS CHK GOOD IAW AMM 33-51-00

Part: ESCAPE REEL — DISENGAGED (ZONE 200) · airframe 30,865 hrs · 4,371 cycles

AIRCRAFT WAS NOT GROUNDED: DURING SECURITY SEARCH EMERGENCY DESCENT DEVICE WAS FOUND DISENGAGED AND SECURITY SEAL DAMAGED. MAINTENANCE REPLACED EMERGENCY DESCENT DEVICE AT COCKPIT IAW AMM25-61-02.

Part: FLOORBOARD — DAMAGED (ZONE 100) · airframe 30,336 hrs · 4,293 cycles

AIRCRAFT WAS GROUNDED: RAMP CREW INFORMED MTC ABOUT SOFT FLOOR PANEL AFT CARGO. MAINTENANCE REPLACED CARGO FLOOR PANEL IAW MM 50-11-09.

Part: BATTERY — DISCHARGED (ZONE 200) · airframe 29,423 hrs · 4,168 cycles

AIRCRAFT WAS NOT GROUNDED: AT DOOR R1, FLASHLIGHT IN THE FLIGHT ATTENDANT SEAT WITH BATTERY DEPLETED. REPLACED BATTERY OF FLASHLIGHT AT FLIGHT ATTENDANT SEAT IN R1 DOOR.

Part: BATTERY — INOPERATIVE (WELLS UNIT) · airframe 28,683 hrs · 4,068 cycles

AIRCRAFT WAS NOT GROUNDED: CENTER CABIN SEAT EMERGENCY LIGHTS INOP ROW 14-18 BOTH SIDES. REMOVED AND REPLACED WELS BATTERY #26 PER AMM 33-51-07.

Part: BATTERY — DISCHARGED (L4 FLASHLIGHT) · airframe 27,114 hrs · 3,866 cycles

AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT BY L4 DOOR JUMPSEAT TESTS RED. REPLACED BATTERY IN FLASHLIGHT BY L4 DOOR IAW AMM 25-64-00.

Part: BATTERY — FAULTY (EMERGENCY LIGHTS) · airframe 31,321 hrs · 4,179 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 3 LH FWD SEAT REMOTE WELS CONTROL UNIT BATTERY POWER IS FAILED.MAINT MSG 33-11426. **SUPPLEMENTAL REPORT FOR SDR AALA202405147453.** (CLOSED) MAINTENANCE REPLACED CLASS 26 DOOR 3LH WCU BATTERY IAW AMM 33-51-07.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 31,321 hrs · 4,179 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 3 LH FWD SEAT REMOTE WELS CONTROL UNIT BATTERY POWER IS FAILED.MAINT MSG 33-11426. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: STRUT — BROKEN (ZONE 500 - LH WI) · airframe 19,454 hrs · 2,828 cycles

AIRCRAFT WAS GROUNDED: FLAP DRIVE EICAS MESSAGE ON APPROACH TO LIS. EMERGENCY DECLARED; FLIGHT LANDED SAFELY. #4 GEARED ROTARY ACTUATOR REPLACED PER AMM 27-51-00A-720A-A (AALA202206305038). REPLACED 6 BROKEN STRUT ASSEMBLIES ON LEFT INBOARD WING ABOVE #12 FLAP TORQUE TUBE PER AMM 57-51-10 (AALA202206305270, AALA202206308288, AALA202206308669, AALA202206309409, AALA202206302580, AALA202206309587). REPLACED SHEARED LEFT INBOARD FLAP TORQUE TUBE #12 PER AMM 27-51-34-01A-520A (AALA202206303456). REPLACED LEFT WING INBOARD AND OUTBOARD FLAP POSITION SENSORS PER AMM 27-58-03-00A-522 AND AMM 27-58-03-00A-720A-A (AALA202206303367, AALA202206306230). COMPLETED PRIMARY FLIGHT CONTROL SYSTEM OPERATIONAL CHECK OF ACTUATION CONFIDENCE FCM L AND ELECTRONICS MONITORS FCM L. ALSO COMPLETED HIGH LIFT SYSTEM TEST OF FLAP/SLAT PRIMARY FCM C. ALL SYSTEM CHECKS NORMAL PER AMM 45-11-00.

Part: ACTUATOR — FAULTY (ZONE 500 - LH WI) · airframe 19,454 hrs · 2,828 cycles

AIRCRAFT WAS GROUNDED: FLAP DRIVE EICAS MESSAGE ON APPROACH TO LIS. EMERGENCY DECLARED; FLIGHT LANDED SAFELY. #4 GEARED ROTARY ACTUATOR REPLACED PER AMM 27-51-00A-720A-A (AALA202206305038). REPLACED 6 BROKEN STRUT ASSEMBLIES ON LEFT INBOARD WING ABOVE #12 FLAP TORQUE TUBE PER AMM 57-51-10 (AALA202206305270, AALA202206308288, AALA202206308669, AALA202206309409, AALA202206302580, AALA202206309587). REPLACED SHEARED LEFT INBOARD FLAP TORQUE TUBE #12 PER AMM 27-51-34-01A-520A (AALA202206303456). REPLACED LEFT WING INBOARD AND OUTBOARD FLAP POSITION SENSORS PER AMM 27-58-03-00A-522 AND AMM 27-58-03-00A-720A-A (AALA202206303367, AALA202206306230). COMPLETED PRIMARY FLIGHT CONTROL SYSTEM OPERATIONAL CHECK OF ACTUATION CONFIDENCE FCM L AND ELECTRONICS MONITORS FCM L. ALSO COMPLETED HIGH LIFT SYSTEM TEST OF FLAP/SLAT PRIMARY FCM C. ALL SYSTEM CHECKS NORMAL PER AMM 45-11-00.

Part: STRUT — BROKEN (ZONE 500 - LH WI) · airframe 19,454 hrs · 2,828 cycles

AIRCRAFT WAS GROUNDED: FLAP DRIVE EICAS MESSAGE ON APPROACH TO LIS. EMERGENCY DECLARED; FLIGHT LANDED SAFELY. #4 GEARED ROTARY ACTUATOR REPLACED PER AMM 27-51-00A-720A-A (AALA202206305038). REPLACED 6 BROKEN STRUT ASSEMBLIES ON LEFT INBOARD WING ABOVE #12 FLAP TORQUE TUBE PER AMM 57-51-10 (AALA202206305270, AALA202206308288, AALA202206308669, AALA202206309409, AALA202206302580, AALA202206309587). REPLACED SHEARED LEFT INBOARD FLAP TORQUE TUBE #12 PER AMM 27-51-34-01A-520A (AALA202206303456). REPLACED LEFT WING INBOARD AND OUTBOARD FLAP POSITION SENSORS PER AMM 27-58-03-00A-522 AND AMM 27-58-03-00A-720A-A (AALA202206303367, AALA202206306230). COMPLETED PRIMARY FLIGHT CONTROL SYSTEM OPERATIONAL CHECK OF ACTUATION CONFIDENCE FCM L AND ELECTRONICS MONITORS FCM L. ALSO COMPLETED HIGH LIFT SYSTEM TEST OF FLAP/SLAT PRIMARY FCM C. ALL SYSTEM CHECKS NORMAL PER AMM 45-11-00.

Part: TORQUE TUBE — SHEARED (ZONE 500 - LH WI) · airframe 19,454 hrs · 2,828 cycles

AIRCRAFT WAS GROUNDED: FLAP DRIVE EICAS MESSAGE ON APPROACH TO LIS. EMERGENCY DECLARED; FLIGHT LANDED SAFELY. #4 GEARED ROTARY ACTUATOR REPLACED PER AMM 27-51-00A-720A-A (AALA202206305038). REPLACED 6 BROKEN STRUT ASSEMBLIES ON LEFT INBOARD WING ABOVE #12 FLAP TORQUE TUBE PER AMM 57-51-10 (AALA202206305270, AALA202206308288, AALA202206308669, AALA202206309409, AALA202206302580, AALA202206309587). REPLACED SHEARED LEFT INBOARD FLAP TORQUE TUBE #12 PER AMM 27-51-34-01A-520A (AALA202206303456). REPLACED LEFT WING INBOARD AND OUTBOARD FLAP POSITION SENSORS PER AMM 27-58-03-00A-522 AND AMM 27-58-03-00A-720A-A (AALA202206303367, AALA202206306230). COMPLETED PRIMARY FLIGHT CONTROL SYSTEM OPERATIONAL CHECK OF ACTUATION CONFIDENCE FCM L AND ELECTRONICS MONITORS FCM L. ALSO COMPLETED HIGH LIFT SYSTEM TEST OF FLAP/SLAT PRIMARY FCM C. ALL SYSTEM CHECKS NORMAL PER AMM 45-11-00.

Part: STRUT — BROKEN (ZONE 500 - LH WI) · airframe 19,454 hrs · 2,828 cycles

AIRCRAFT WAS GROUNDED: FLAP DRIVE EICAS MESSAGE ON APPROACH TO LIS. EMERGENCY DECLARED; FLIGHT LANDED SAFELY. #4 GEARED ROTARY ACTUATOR REPLACED PER AMM 27-51-00A-720A-A (AALA202206305038). REPLACED 6 BROKEN STRUT ASSEMBLIES ON LEFT INBOARD WING ABOVE #12 FLAP TORQUE TUBE PER AMM 57-51-10 (AALA202206305270, AALA202206308288, AALA202206308669, AALA202206309409, AALA202206302580, AALA202206309587). REPLACED SHEARED LEFT INBOARD FLAP TORQUE TUBE #12 PER AMM 27-51-34-01A-520A (AALA202206303456). REPLACED LEFT WING INBOARD AND OUTBOARD FLAP POSITION SENSORS PER AMM 27-58-03-00A-522 AND AMM 27-58-03-00A-720A-A (AALA202206303367, AALA202206306230). COMPLETED PRIMARY FLIGHT CONTROL SYSTEM OPERATIONAL CHECK OF ACTUATION CONFIDENCE FCM L AND ELECTRONICS MONITORS FCM L. ALSO COMPLETED HIGH LIFT SYSTEM TEST OF FLAP/SLAT PRIMARY FCM C. ALL SYSTEM CHECKS NORMAL PER AMM 45-11-00.

Part: STRUT — BROKEN (ZONE 500 - LH WI) · airframe 19,454 hrs · 2,828 cycles

AIRCRAFT WAS GROUNDED: FLAP DRIVE EICAS MESSAGE ON APPROACH TO LIS. EMERGENCY DECLARED; FLIGHT LANDED SAFELY. #4 GEARED ROTARY ACTUATOR REPLACED PER AMM 27-51-00A-720A-A (AALA202206305038). REPLACED 6 BROKEN STRUT ASSEMBLIES ON LEFT INBOARD WING ABOVE #12 FLAP TORQUE TUBE PER AMM 57-51-10 (AALA202206305270, AALA202206308288, AALA202206308669, AALA202206309409, AALA202206302580, AALA202206309587). REPLACED SHEARED LEFT INBOARD FLAP TORQUE TUBE #12 PER AMM 27-51-34-01A-520A (AALA202206303456). REPLACED LEFT WING INBOARD AND OUTBOARD FLAP POSITION SENSORS PER AMM 27-58-03-00A-522 AND AMM 27-58-03-00A-720A-A (AALA202206303367, AALA202206306230). COMPLETED PRIMARY FLIGHT CONTROL SYSTEM OPERATIONAL CHECK OF ACTUATION CONFIDENCE FCM L AND ELECTRONICS MONITORS FCM L. ALSO COMPLETED HIGH LIFT SYSTEM TEST OF FLAP/SLAT PRIMARY FCM C. ALL SYSTEM CHECKS NORMAL PER AMM 45-11-00.

Part: TRANSDUCER — UNSERVICEABLE (ZONE 500 - LH WI) · airframe 19,454 hrs · 2,828 cycles

AIRCRAFT WAS GROUNDED: FLAP DRIVE EICAS MESSAGE ON APPROACH TO LIS. EMERGENCY DECLARED; FLIGHT LANDED SAFELY. #4 GEARED ROTARY ACTUATOR REPLACED PER AMM 27-51-00A-720A-A (AALA202206305038). REPLACED 6 BROKEN STRUT ASSEMBLIES ON LEFT INBOARD WING ABOVE #12 FLAP TORQUE TUBE PER AMM 57-51-10 (AALA202206305270, AALA202206308288, AALA202206308669, AALA202206309409, AALA202206302580, AALA202206309587). REPLACED SHEARED LEFT INBOARD FLAP TORQUE TUBE #12 PER AMM 27-51-34-01A-520A (AALA202206303456). REPLACED LEFT WING INBOARD AND OUTBOARD FLAP POSITION SENSORS PER AMM 27-58-03-00A-522 AND AMM 27-58-03-00A-720A-A (AALA202206303367, AALA202206306230). COMPLETED PRIMARY FLIGHT CONTROL SYSTEM OPERATIONAL CHECK OF ACTUATION CONFIDENCE FCM L AND ELECTRONICS MONITORS FCM L. ALSO COMPLETED HIGH LIFT SYSTEM TEST OF FLAP/SLAT PRIMARY FCM C. ALL SYSTEM CHECKS NORMAL PER AMM 45-11-00.

Part: STRUT — BROKEN (ZONE 500 - LH WI) · airframe 19,454 hrs · 2,828 cycles

AIRCRAFT WAS GROUNDED: FLAP DRIVE EICAS MESSAGE ON APPROACH TO LIS. EMERGENCY DECLARED; FLIGHT LANDED SAFELY. #4 GEARED ROTARY ACTUATOR REPLACED PER AMM 27-51-00A-720A-A (AALA202206305038). REPLACED 6 BROKEN STRUT ASSEMBLIES ON LEFT INBOARD WING ABOVE #12 FLAP TORQUE TUBE PER AMM 57-51-10 (AALA202206305270, AALA202206308288, AALA202206308669, AALA202206309409, AALA202206302580, AALA202206309587). REPLACED SHEARED LEFT INBOARD FLAP TORQUE TUBE #12 PER AMM 27-51-34-01A-520A (AALA202206303456). REPLACED LEFT WING INBOARD AND OUTBOARD FLAP POSITION SENSORS PER AMM 27-58-03-00A-522 AND AMM 27-58-03-00A-720A-A (AALA202206303367, AALA202206306230). COMPLETED PRIMARY FLIGHT CONTROL SYSTEM OPERATIONAL CHECK OF ACTUATION CONFIDENCE FCM L AND ELECTRONICS MONITORS FCM L. ALSO COMPLETED HIGH LIFT SYSTEM TEST OF FLAP/SLAT PRIMARY FCM C. ALL SYSTEM CHECKS NORMAL PER AMM 45-11-00.

Part: TRANSDUCER — UNSERVICEABLE (ZONE 500 - LH WI) · airframe 19,454 hrs · 2,828 cycles

AIRCRAFT WAS GROUNDED: FLAP DRIVE EICAS MESSAGE ON APPROACH TO LIS. EMERGENCY DECLARED; FLIGHT LANDED SAFELY. #4 GEARED ROTARY ACTUATOR REPLACED PER AMM 27-51-00A-720A-A (AALA202206305038). REPLACED 6 BROKEN STRUT ASSEMBLIES ON LEFT INBOARD WING ABOVE #12 FLAP TORQUE TUBE PER AMM 57-51-10 (AALA202206305270, AALA202206308288, AALA202206308669, AALA202206309409, AALA202206302580, AALA202206309587). REPLACED SHEARED LEFT INBOARD FLAP TORQUE TUBE #12 PER AMM 27-51-34-01A-520A (AALA202206303456). REPLACED LEFT WING INBOARD AND OUTBOARD FLAP POSITION SENSORS PER AMM 27-58-03-00A-522 AND AMM 27-58-03-00A-720A-A (AALA202206303367, AALA202206306230). COMPLETED PRIMARY FLIGHT CONTROL SYSTEM OPERATIONAL CHECK OF ACTUATION CONFIDENCE FCM L AND ELECTRONICS MONITORS FCM L. ALSO COMPLETED HIGH LIFT SYSTEM TEST OF FLAP/SLAT PRIMARY FCM C. ALL SYSTEM CHECKS NORMAL PER AMM 45-11-00.

Part: STRUT — BROKEN (ZONE 500 - LH WI) · airframe 19,454 hrs · 2,828 cycles

AIRCRAFT WAS GROUNDED: FLAP DRIVE EICAS MESSAGE ON APPROACH TO LIS. EMERGENCY DECLARED; FLIGHT LANDED SAFELY. #4 GEARED ROTARY ACTUATOR REPLACED PER AMM 27-51-00A-720A-A (AALA202206305038). REPLACED 6 BROKEN STRUT ASSEMBLIES ON LEFT INBOARD WING ABOVE #12 FLAP TORQUE TUBE PER AMM 57-51-10 (AALA202206305270, AALA202206308288, AALA202206308669, AALA202206309409, AALA202206302580, AALA202206309587). REPLACED SHEARED LEFT INBOARD FLAP TORQUE TUBE #12 PER AMM 27-51-34-01A-520A (AALA202206303456). REPLACED LEFT WING INBOARD AND OUTBOARD FLAP POSITION SENSORS PER AMM 27-58-03-00A-522 AND AMM 27-58-03-00A-720A-A (AALA202206303367, AALA202206306230). COMPLETED PRIMARY FLIGHT CONTROL SYSTEM OPERATIONAL CHECK OF ACTUATION CONFIDENCE FCM L AND ELECTRONICS MONITORS FCM L. ALSO COMPLETED HIGH LIFT SYSTEM TEST OF FLAP/SLAT PRIMARY FCM C. ALL SYSTEM CHECKS NORMAL PER AMM 45-11-00.

Part: NONE — INOPERATIVE (ZONE 200 - FUSE) · airframe 18,860 hrs · 2,742 cycles

AIRCRAFT WAS NOT GROUNDED: REMOTE DATA CONCENTRATOR 19 INOPERATIVE. L4/R4 DOOR ARE FLIGHT ATTENDANT PANEL EMERGENCY SIGNAL SYSTEM INOPERATIVE. ACCOMPLISHED REPLACEMENT OF REMOTE DATA CONCENTRATOR NUMBER 19 PER AMM 787-A-42-21-07-06A-720A OPERATIONS CHECK OF SYSTEM NORMAL.

Part: SLIDE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 17,699 hrs · 2,546 cycles

AIRCRAFT WAS GROUNDED: SLIDE AT ENTRY DOOR 3LH SHOWING LOW PRESSURE IN THE RED BAND. REPLACED SLIDE PACK ASSEMBLY WITH SERVICEABLE UNIT IAW WORKCARD 78L80025001, OPS CHECK GOOD.

Part: GIRT BAR — WILL NOT ARM (ZONE 800 - DOORS) · airframe 17,435 hrs · 2,469 cycles

AIRCRAFT WAS GROUNDED: THE 4R ENTRY DOOR WILL NOT ARM. RESTORED ESCAPE SLIDE GIRT BAR MATERIAL IN ITS PROPER POSITION PER AMM 25-66-01.

Part: NONE — NONE · airframe 16,798 hrs · 2,345 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY 3L DOOR LATCH INTERIOR KNOB MISSING. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: KNOB — MISSING (ZONE 900 - LAV/G) · airframe 16,798 hrs · 2,345 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY 3L DOOR LATCH INTERIOR KNOB MISSING. **SUPPLEMENTAL REPORT: INSTALLED NEW LATCH KNOB IAW AMM 25-41-00, OPS CHECK GOOD.** (CLOSED)

Part: LATCH — LOOSE (R4 DOOR BUSTLE) · airframe 16,399 hrs · 2,282 cycles

AIRCRAFT WAS NOT GROUNDED: 4R DOOR SLIDE BUSTLERS LOOSE/BROKEN. REMOVED AND REPLACED AFT GRABBER CATCH ASSEMBLY PER CMM 25-21-85.

Part: CONNECTOR — LOOSE (SLAT SKEW SENSOR) · airframe 15,339 hrs · 2,108 cycles

AIRCRAFT WAS GROUNDED: SLAT DRIVE FAILURE MESSAGE CLIMBING THROUGH FL110, FLIGHT DECLARED EMERGENCY AND RETURNED TO FIELD. RECONNECTED SLAT SKEW BREAKAWAY CONNECTOR, OPS CHECK GOOD.

Part: BATTERY — INOPERATIVE (E LITE CONTROL) · airframe 14,469 hrs · 1,945 cycles

AIRCRAFT WAS NOT GROUNDED. 4R DOOR WELS CONTROL UNIT BATTERY POWER IS DEGRADED. REPLACED 4R DOOR WELS BATTERY UNIT, IAW AMM 33-51-07. OPERATIONS CHECK GOOD.

Part: COVER — LOOSE (L2 DOOR SLIDE) · airframe 14,188 hrs · 1,891 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR 2L SLIDE COVER LOOSE. REINSTALLED SLIDE BUSTLE, IAW AMM 52-11-44.

Part: BRACKET — LOOSE (L2 DOOR SLIDE) · airframe 14,188 hrs · 1,891 cycles

AIRCRAFT WAS GROUNDED. DOOR 2L SLIDE BUSTLE AFT HOOK BRACKET ON DOOR SIDE BROKEN. RESET HOOK BRACKET, IAW AMM 52-11-24. OPERATIONS CHECK GOOD.

Part: BRACKET — BROKEN (SLIDE BUSTLE) · airframe 14,103 hrs · 1,871 cycles

AIRCRAFT WAS GROUNDED: SLIDE RAFT BUSTLE AFT LOWER LATCH RETAINER BROKEN AT 2L DOOR **SUPPLEMENTAL REPORT: REMOVED AND REPLACED DOOR EDGE PROTECTOR PER AMM 52-11-24** (CLOSED)

Part: WINDSHEAR SYS — MALFUNCTIONED · airframe 13,246 hrs · 1,738 cycles

AIRCRAFT WAS NOT GROUNDED: DURING TAXI, FLIGHT CREW REPORTED WINDSHEAR ALERT FAULT. TAKE-OFF ATTEMPTED TWICE AND ABORTED, BUT CREW REPORTS SPEED AT ABOUT 5KTS. AIRCRAFT RETURNED TO GATE. ACCOMPLISHED OPERATIONAL TEST ON L+R ISS WEATHER RADAR SYTEM PER AMM 34-42-00-21A-A, NO FAULTS, ALL INDICATIONS NORMAL..

Part: TERMINAL — LOOSE (EXIT SIGN) · airframe 12,563 hrs · 1,648 cycles

AIRCRAFT GROUNDED - L2 DOOR, EMERGENCY EXIT IDENTIFIER INOP DURING EMERGENCY LIGHT TEST. RESEATED LOOSE TERMINAL ON L2 EMERGENCY EXIT LIGHT SIGN PER FIM 33-50-F1, OPERATIONAL CHECK OKAY.

Part: BATTERY — DEFECTIVE (CABIN) · airframe 12,352 hrs · 1,626 cycles

AIRCRAFT GROUNDED - EMERGENCY PATH LIGHTING, ROWS 6-12, COMES ON INTERMITTENTLY. REPLACED WBU (WELS BATTERY UNIT) AT L1 DOOR PER AMM 33-51-07, ACCOMPLISHED WBU SYSTEM RE-KEY, ALL CHECKS NORMAL.

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 11,346 hrs · 1,435 cycles

AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT AT FLIGHT ATTENDANT SEAT FAILED TEST. MAINTENANCE REPLACED BATTERY OF FLASHLIGHT PER AMM 25-64-00.

Part: SUPPORT BRACKET — LOOSE (L3 DOOR SLIDE) · airframe 11,315 hrs · 1,431 cycles

AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS L3 DOOR SLIDE COVER LOOSE. ACCOMPLISHED LATCH ADJUST/REPLACE IAW AMM 25 -11-24 AND ESO41695.

Part: SUPPORT BRACKET — LOOSE (R4 DOOR SLIDE) · airframe 11,315 hrs · 1,431 cycles

AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS R4 DOOR SLIDE COVER LOOSE. MAINTENANCE ACCOMPLISHED LATCH ADJUST/REPLACE IAW AMM 25-11-24 AND ESO 41695.

Part: SUPPORT BRACKET — LOOSE (L3 DOOR SLIDE) · airframe 11,315 hrs · 1,431 cycles

AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS L3 DOOR SLIDE COVER LOOSE. ACCOMPLISHED LATCH ADJUST/REPLACE IAW AMM 25-11-24 AND ESO41695.

Part: SUPPORT BRACKET — MISSING (R2 DOOR) · airframe 11,315 hrs · 1,431 cycles

AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS R2 DOOR AFT SLIDE COVER PRI LATCH STRIKER/RETAINER MISSING. MAINTENANCE ACCOMPLISHED AARD 52-11-00-01 FINAL REPAIR.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 11,133 hrs · 1,392 cycles

AIRCRAFT IN BASE VISIT: SUPPORT ANGLE CRACKED AT WS484.1, RWL185 (L=4.5"). INSTALLED REINFORCEMENT ANGLE REPAIR IAW EA #299902.

Part: RIB — CRACKED (LT WING) · airframe 10,867 hrs · 1,355 cycles

AIRCRAFT WAS GROUNDED: THE LEFT WING FIXED TRAILING EDGE AUXILLARY D RIB CRACKED AT THE AUXILLARY "D" RIB TO SPOILER BEAM JOIN. THE CRACK IS IN THE AFT OUTBOARD UPPER VERTICAL FLANGE. REPAIRED RIB PER EA 299037.

Part: RIB — CRACKED (LT WING) · airframe 10,867 hrs · 1,355 cycles

AIRCRAFT WAS GROUNDED: THE LEFT WING FIXED TRAILING EDGE AUXILLARY D RIB CRACKED AT THE AUXILLARY "D" RIB TO SPOILER BEAM JOIN. THE CRACK IS IN THE AFT OUTBOARD UPPER VERTICAL FLANGE. REPAIRED RIB PER EA 299037.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 5,576 hrs · 589 cycles

LOW BATTERY INDICATION FOR FLASHLIGHT IN OFAR. REMOVED AND INSTALLED A SERVICEABLE BATTERY IAW AMM 25-64-00.

Part: BATTERY — FAULTY (CABIN) · airframe 2,980 hrs · 312 cycles

THE AIRCRAFT WAS NOT GROUNDED. *AHM ALERT* CLASS 30 - REMOTE WELS CONTROL UNIT CONFIGURATION DOES NOT AGREE WITH OTHER WIRELESS EMERG LIGHTING SYS CONTROL UNITS. REMOVED AND REPLACED CLASS 30 WELS CONTROL UNIT (AALA201711109016) AND BATTERY PER AMM 33-51-07. OPERATIONAL CHECK GOOD.

Part: BATTERY — FAULTY (CABIN) · airframe 2,980 hrs · 312 cycles

THE AIRCRAFT WAS NOT GROUNDED. **AHM ALERT** CLASS 02 - DOOR 1 RT REMOTE WELS CONTROL UNIT CONFIGURATION DOES NOT AGREE WITH OTHER WIRELESS EMERG LIGHTING SYS CONTROL UNITS. REMOVED AND REPLACED CLASS 2 WELS CONTROL UNIT (AALA201711109014) AND BATTERY PER AMM 33-51-07. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — FAULTY (CABIN) · airframe 2,980 hrs · 312 cycles

THE AIRCRAFT WAS NOT GROUNDED. **AHM ALERT** CLASS 30 - REMOTE WELS CONTROL UNIT CONFIGURATION DOES NOT AGREE WITH OTHER WIRELESS EMERG LIGHTING SYS CONTROL UNITS. REMOVED AND REPLACED CLASS 30 WELS CONTROL UNIT AND BATTERY (AALA201711149019) PER AMM 33-51-07. OPERATIONAL CHECK GOOD. (CLOSED)

Part: CONTROL UNIT — FAULTY (CABIN) · airframe 2,980 hrs · 312 cycles

THE AIRCRAFT WAS NOT GROUNDED. **AHM ALERT** CLASS 02 - DOOR 1 RT REMOTE WELS CONTROL UNIT CONFIGURATION DOES NOT AGREE WITH OTHER WIRELESS EMERG LIGHTING SYS CONTROL UNITS. REMOVED AND REPLACED CLASS 2 WELS CONTROL UNIT AND BATTERY (AALA201711149018) PER AMM 33-51-07. OPERATIONAL CHECK GOOD. (CLOSED)

Part: LATCH — UNSECURE (ZONE 800) · airframe 1,682 hrs · 182 cycles

AIRCRAFT WAS NOT GROUNDED. R3 DOOR SLIDE BUSTLE LOOSE. REPLACED R3 DOOR SLIDE BUSTLE LATCH AND MISSING SCREW PER AMM 52-11-24.

Part: LATCH — UNSECURE (ZONE 800) · airframe 1,682 hrs · 182 cycles

AIRCRAFT WAS NOT GROUNDED. L3 DOOR SLIDE BUSTLE LOOSE. REPLACED L3 DOOR SLIDE BUSTLE LATCH PER AMM 52-11-24.

Part: TRACK — DIRTY (LEVER COVER) · airframe 963 hrs · 101 cycles

L3 DOOR ARM-DISARM CLEAR PLASTIC COVER IS DIFFICULT TO SLIDE TO EXPOSE LEVER. REMOVED DEBRIS FROM COVER TRACK. OPERATIONAL CHECKED GOOD.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 53,706 hrs · 74,491 cycles

CRACK FOUND LT SIDE OF FUSELAGE SKIN DIRECTLY BELOW LAST PASSENGER WINDOW ON LOWER FUSELAGE BS 932 JUST BELOW STRINGER 21L. MAINTENANCE REPAIRED WITH APPROXIMATELY 19 BY 16 EXTERNAL SKIN PATCH, FABRICATED DOUBLER AND TRIPLER PER SRM 53-30-3, FIGURE 48, DETAIL XII.

Part: FIRE LOOP — FALSE INDICATION (APU BAY) · airframe 53,515 hrs · 74,038 cycles

APU FIRE WARNING LIGHT ILLUMINATED IN FLIGHT. APU WAS NOT OPERATING AT THE TIME OF INDICATION; THE FIRE BOTTLE WAS DISCHARGED. AIRCRAFT RETURNED TO HNL AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED FIRE LOOP ELEMENT IAW AMM 26-15-1 FOR TROUBLESHOOTING, OPERATIONAL CHECK OK, NO FIRE WARNING WHILE THE APU IS OPERATING. REMOVED AND REPLACED THE APU FIRE BOTTLE IAW AMM 26-22-11, ELECTRICAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN PANEL — CRACKED (BS 787 S19L) · airframe 53,023 hrs · 72,957 cycles

A 1.75 INCH CRACK AT BS 787 STR 19L. CRACK CUT OUT AND REPAIRED IAW SRM 53-30-3 FIGURE 48 DETAIL XI. NDT ACCOMPLISHED IAW BOEING NDT MANUAL 51-00-00 PT 6. REPAIR APPROXIMATE SIZE 9 X 12 INCHES.

Part: SKIN — GOUGED (WS 340 LE) · airframe 53,023 hrs · 72,957 cycles

WING LEADING EDGE SKIN GOUGED AT WBL 340.

Part: SPAR — CORRODED (WS 560) · airframe 53,023 hrs · 72,957 cycles

CORROSION ON LOWER SURFACE CHORD FORWARD FLANGE FRONT SPAR AT FSS-560.

Part: SPAR — CORRODED (WING) · airframe 53,023 hrs · 72,957 cycles

CORROSION ON LOWER SURFACE CHORD FORWARD FLANGE FRONT SPAR AT FSS-560.

Part: SPAR — CORRODED · airframe 53,023 hrs · 72,957 cycles

CORROSION ON LOWER SURFACE CHORD FORWARD FLANGE FRONT SPAR AT FSS-301. REMOVED CORROSION AND INSTALLED REPAIR FILLER IAM ALOHA'S ECO 3560. FAA 8100.9 RECEIVED.

Part: SPAR — CORRODED (WING) · airframe 53,023 hrs · 72,957 cycles

WBL 157 CORROSION BY WING REAR SPAR. REMOVED CORROSION AND REPLACED RIVETS. REPAIR COMPLETED IAW ALOHA'S ECO 3091. FAA 8100.9 RECEIVED.

Part: SKIN PANEL — CRACKED (BS 747 S17R) · airframe 53,023 hrs · 72,957 cycles

A 1.5 INCH CRACK AT BS 747 + 8 STR 17R. REPAIR DOUBLER COMPLETED IAW 53-30-3 FIG 48 DET VIII. NDT PERFORMED IAW BOEING NDT MANUAL 51-00-00 PT 6. REPAIR SIZE APPROX 9 X 12 INCHES.

Part: SKIN — CRACKED (BS 727A S15-18R) · airframe 53,023 hrs · 72,957 cycles

A 2.75 INCH CRACK AT BS 727A + 15 STR 18R. A 15 MONTH INTERIM REPAIR COMPLETED IN ACCORDANCE WITH ALOHA'S ECO 3521. DOUBLER 0.032 INCH, TRIPLER 0.050 INCH. APPROXIMATE REPAIR SIZE 23" X 31". FAA 8100.9 RECEIVED.

Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 52,767 hrs · 72,405 cycles

LEFT HAND HORIZONTAL STABILIZER REAR SPAR UPPER CHORD CORROSION SS 111.1 - SS 101.9. MAINTENANCE REPAIRED WITH FILLERS TO SEAT IN BLEND OUTS AND SKIN TRIM OUT. FABRICATED EXTERNAL SKIN DOUBLER PER ECO 3392.

Part: CIRCUIT CARD — FAILED (PROXIMITY SYS)

LANDING GEAR LEVER WOULD NOT GO TO UP POSITION AFTER TAKEOFF. NO GREEN OR RED GEAR LIGHTS ILLUMINATED. RETURNED TO HNL. MAINTENANCE INSPECTED AND LUBED THE TELEFLEX CABLE. MEASURED PROXIMITY SENSOR AND GAP WITHIN TOLERANCE. REPLACED PROXIMITY CARD AND SWUNG GEARS PER AMM 32-09-200. OK. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE)

TRIMMED OUT DAMAGED AREA. HFEC VERIFIED CRACK REMOVED. FABRICATED DOUBLER. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAIR PARTS MAKING A FAYING SEAL AROUND REPAIR. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 48, DETAIL X. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONTROL CABLE — OUT OF ADJUST (RT MLG)

AFTER TAEKOFF, DURING CLIM THE LANDING GEAR CONTROL LEVER WOULD NOT MOVE UP AND SIMULTANEOUSLY THE TAKEOFF WARNING HORN SOUNDED WHEN THE FLAPS WERE RETRACTED. PERFORMED GROUND SPOILER INTERLOCK VALVE CONTROL CABLE ADJUSTMENT AND TEST IAW MM 27-62-51. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRINGER — DAMAGED (FUSELAGE)

CUT OUT AND REMOVED DAMAGED SECTION OF STRINGER. FABRICATED REPAIR PARTS AND DRILLED FASTENER HOLES IAW TABLE 1. ALODINE AND APPLIED ONE LAYER OF BMS 10-11, TYPE 1 PRIMER. INSTALLED REPAIR PARTS AND MADE A FAYING SURFACE SEAL PER SRM 53-10-03, FIGURE 1. REPAIR COMPLETED IAW ECO 3394. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LEG ASSY — CORRODED (FUSELAGE)

BLENDED OUT THE CORROSION TO A 10:1 RATIO. VERIFIED CORROSION FREE USING 10X VISUAL INSPECTION. FLAT PEEN BLENDOUT AREA. REMOVED ANGLES. FABRICATED A FILLER AND STRAP FROM 7075-T6 PER FIGURE 1. ALODINED AND TWO COATS BMS 10-11 TYPE II PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS AND ANGLES. REPAIR COMPLETED IAW ECO 3295 AND DEVIATION A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRINGER SPLICE — CRACKED (FUSELAGE)

TRIMMED OUT THE DAMAGED AREA, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED AND INSTALLED STRINGER SPLICE. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACE. REPAIR COMPLETED IAW SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SPLICE — CORRODED (FUSELAGE)

TRIMMED OUT THE DAMAGED AREA, VERIFIED CORROSION FREE USING 10X INSPECTION. FABRICATED AND INSTALLED STRINGER SPLICE. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACE. REPAIR COMPLETED IAW SRM 53-10-3. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRINGER — CORRODED (FUSELAGE)

TRIMMED OUT THE DAMAGED AREA, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED AND INSTALLED STRINGER SPLICE PER TABLE 1. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACE. INSTALLED REPAIR PARTS AND MADE A FAYING SEAL WITH BMS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 51-10-1 AND SRM 53-10-3, FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (WING)

BLENDED OUT THE CORROSION, VERIFIED FREE USING 10X VISUAL INSPECTION. FLAT PEEN BLENDOUT AREA. DRILLED AND SPOTFACE FASTENER HOLE. COLD WORKED FASTENER HOLE. ALODINED AND TWO COATS BMS 10-79 TYPE III PRIMER TO BLEND AND SPOT FACE AREA. INSTALLED 1/32 INCHE OVERSIZE PROTRUDING TENSION HEAD HI-LOCKS. REPAIR COMPLETED IAW ECO 3390. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

TRIMMED OUT THE SKIN, BONDED DOUBLER, AND BEARSTRAP, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED THE REPAIR PARTS AS SHOWN IN 737 SRM 53-30-3, FIGURE 46. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS, AFT CARGO DOOR CUTOUT FORWARD LOWER CORNER P/N 6547950, BS 807. REPAIR COMPLETED IAW ECO 3398. AIRCRAFT RETURNED TO SERVICE. (M)

Part: DOOR — CRACKED (MAIN PAX)

TRIMMED OUT THE CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. ACCOMPLISHED FASTENER HOLE INSPECTION ON HOLES COVERED BY REPAIR. UTILIZED REPAIR PARTS FROM KIT PER FIGURE 1. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED APPROPRIATE REPAIR PER BOEING REPAIR DRAWING. REPAIR COMPLETED IAW BOEING DRAWING AND ECO 1896R1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRINGER SPLICE — DAMAGED (FUSELAGE)

TRIMMED OUT THE DAMAGED AREA, VERIFIED CRACK FREE USNG HFEC INSPECTION. FABRICATED AND INSTALLED STRINGER SPLICE. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACE. REPAIR COMPLETED IAW SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

TRIMMED OUT THE CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED TAPERED FILLERS AND PLATES FROM 2024-T3 CLAD. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS PER FIGUR 24. REPAIR COMPLETED IAW SRM 53-30-03, PAGE 83. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

TRIMMED OUT THE CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED TAPERED FILLERS AND PLATES FROM 2024-T3 CLAD, PER TABLE 1. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS PER FIGURE 24. REPAIR COMPLETED IAW SRM 53-30-03, PATE 86A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: PANEL — CORRODED (WING)

BLENDED OUT THE CORROSION TO A 20:1 RATIO. VERIFIED CORROSION FREE USING 10X VISUAL INSPECTION. REMOVED FASTENERS IN REPAIR AREA. FLAT PEEN BLENDOUT AREA. ALODINED AND TWO COATS BMS 10-20 TYPE II PRIMER TO BLEND AND SPOT FACE AREAS. INSTALLED 1/32 INCH OVERSIZE PROTRUDING TENSION HEAD HI-LOCKS WET WITH BMS 5026 TYPE II IN COLD WORKED TRANSITION FIT HOLES. REPAIR COMPLETED IAW ECO 3397. AIRCRAFT RETURNED TO SERVICE. CENTER FUEL TANK LOWER PANEL P/N 6545403, BS 638.60 AT STRINGER 4C WAS REPAIRED.(M)

Part: SKIN — CRACKED (FUSELAGE)

TRIMMED OUT THE CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED REPAIR DOUBLER. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS WET WITH BMS 5-95 PER FIGURE 1. REPAIR COMPLETED IAW SRM 53-30-03, PAGE 2B. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

TRIMMED OUT CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. ENLARGED TRIM BY .040 INCH INSURANCE CUT. HFEC INSPECTED ALL FASTENER HOLES. FABRICATED A .071 INCH STRUCTURAL FILLER, .063 INCH INNER PLATE, .063 INCH PLATE, .125 OUTER PLATE AND .0180 INCH THICK FILLER FROM 2024-T3 CLAD SHEET AS SHOWN IN FIGURE 1. ALODINED AND TWO COATS BMS 10-79, TYPE III PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS. APPLIED A FILLET SEAL OF BMS 5-95 AROUND THE EDGES OF THE REPAIR. REPAIR COMPLETED IAW ECO 3396. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

TRIMMED OUT THE CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED DOUBLER AND FILLER FROM .063 INCH, 2024-T3. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS EPR FIGURE 1. REPAIR COMPLETED IAW ECO 3391. AIRCRAFT RETURNED TO SERVICE. (M)

Part: VENT — CORRODED (WING)

BLENDED OUT THE CORROSION TO A 10:1 RATIO. VERIFIED CORROSION FREE USING 10X VISUAL INSPECTION. FLAT PEEN BLENDOUT AREA. FABRICATED A .020 INCH EXTERNAL DOUBLER FROM 7075-T6. ALODINED AND ONE COAT BMS 10-11, TYPE I PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. BOND THE EXTERNAL DOUBLER OVER THE BLEND AREA, WITH BMS 5-95 SEALANT. REPAIR COMPLETED IAW ECO 3387. (M)

Part: SKIN — CRACKED (FUSELAGE)

TRIMMED OUT THE CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED DOUBLER AND FILLER FROM .063 INCH, 2024-T3. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS PER FIGURE 33. REPAIR COMPLETED IAW SRM 53-30-03, PAGE 119. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

TRIMMED OUT THE CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED FILLER, DOUBLER, AND TRIPLER FROM 2024-T3 PER TABLE I. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS PER FIGURE 34. REPAIR COMPLETED IAW SRM 53-30-03, PAGE 123. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (FUSELAGE)

BLENDED OUT THE CORROSION TO A 10:1 RATIO. VERIFIED CORROSION FREE USING 10X VISUAL INSPECTION. FLAT PEEN BLENDOUT AREA. AT EXISTING RIVET LOCATION, INSTALL 1/32 INCH OVERSIZE. RESTORE AERODYNAMIC SURFACE BY FILLING THE AREA WITH BMS 5-95 SEALANT. REPAIR COMPLETED IAW ECO 3389. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (PAX CABIN)

REPLACED AFT ENTRY IDENTICAL POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

REPLACED AFT SERVICE DOOR POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

REPLACED AFT ENTRY DOOR POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

REPLACED FORWARD ENTRY DOOR POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: PUMP — INOPERATIVE (B HYD SYS)

DURING TAKEOFF AT 100 KNOTS, THE NR 2 HYDRAULIC SYSTEM 'B' PUMP LIGHT CAME ON STEADY WITH NO OTHER ABNORMAL INDICATIONS. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. THE HYDRAULIC PUMP WAS PUT ON MEL AS INOPERABLE AND THE AIRCRAFT COMPLETED THE SCHEDULED FLIGHT DAY. REPLACED THE NR 2 HYDRAULIC SYSTEM 'B' PUMP. OPS CHECK WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED CENTER EMERGENCY CONTROL MODULE BATTERY PACK DUE TO LOW VOLTAGE. OP CHECK, OK. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CORRODED (LT WING)

LEFT LOWER OUTBOARD WING TRAILING EDGE CORRODED AT WSL 453. BLENDOUT TO REMOVE ALL CORROSION CONFIRMED USING 10X VISUAL INSPECTION NO DEFECTS NOTED, OBTAINED A SURFACE FINISH OF 125 MICROINCHES RADIUS OR SMOOTHER, FLAT PEENED REWORKED AREA, ALODINED AND PRIMED. FILLED DEPRESSIONS WITH BMS 5-95 SEALANT REFERRING TO SRM. APPLIED ONE COAT BMS 10-79, TYPE III PRIMER OVER THE SEALANT IAW ECO. AIRCRAFT RETURNED TO SERVICE.

Part: FLOORBEAM — CRACKED (FUSELAGE)

FOUND A 2.5 INCH CRACK AT BS 710 FLOORBEAM BBL .07 ON THE WEB. CUT OUT DAMAGED AREA ON THE WEB. FABRICATED A REPAIR DOUBLER IAW FIGURE 6. INSTALLED DOUBLER, STIFFENERS AND FILLERS. REPAIR COMPLETED IAW ECO 2223 R1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: KEELBEAM — CORRODED (FUSELAGE)

FOUND CORROSION ON THE KEEL BEAM LOCATED IN THE MAIN WHEEL WELL AT BS 685 LEFT CHORD AT THE MOUNT SCREW HOLES. REPAIRED BY REMOVING CORROSION IAW DETAIL VII, VIII AND IX. REPAIR COMPLETED IAW SRM 53-10-1, FIGURE 7, BS 685. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRINGER — CORRODED (FUSELAGE)

FOUND EXFOLIATION CORROSION ON STRINGER 27L AT BS 967. REMOVED THE DAMAGED SECTION OF THE STRINGER. FABRICATED AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-3 PAGE 10. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FITTING — CORRODED (FUSELAGE)

FOUND CORROSION ON THE FORWARD LOWER EXTRUSION ON THE FRAME IN THE LEFT WHEEL WELL AT BS 680. REMOVED THE FORWARD LOWER EXTRUSION. INSTALLED NEW EXTRUSION SECTION IAW SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CRACKED (FUSELAGE)

FOUND A CRACK AT FUSELAGE STATION 665 FLOORBEAM BL 0 ON THE UPPER CHORD. FABRICATED AND INSTALLED REINFORCING DOUBLER, STIFFENERS, FILLERS, SPLICE PLATE AND ANGLE. REPAIR COMPLETED IAW ECO 2223 R1 PART II DEVIATION D. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FITTING — CORRODED (FUSELAGE)

FOUND CORROSION ON THE FORWARD LOWER EXTRUSION, LOWER FRAME SECTION IN THE RIGHT WHEEL WELL BETWEEN BS 680 AND BS 690. CUT OUT DAMAGED SECTION OF WEB. FABRICATED AND INSTALLED NEW WEB SECTION IAW SRM 51-40-2. AIRCRAFT RETURNED TO SERVICE. (M)

Part: KEELBEAM — CRACKED (FUSELAGE)

FOUND CRACK ON THE LOWER CHORD IN THE LEFT MAIN WHEEL WELL AT BS 652 KEEL BEAM FUSELAGE SKIN AREA. TRIMMED OUT CRACK AND VERIFIED REMOVED USING HFEC METHOD. FABRICATED A REPAIR ANGLE AND FILLER. REPAIR COMPLETED IAW ECO 2726R3 PART II. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRUCTURE — CRACKED (FUSELAGE)

PERFORMED WINDOW CORNER FASTENERS HOLE INSPECTION PER S/B 737-53A1177R 6 AND DISCOVERED DEFECTS IN WINDOW CORNERS WITH CRACK INDCIATION AT BS 440 RT WINDOW UPPER FORWARD CORNER USING HFEC METHODS. REPAIRED IAW SRM, AIRCRAFT RETURNED TO SERVICE. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

PERFORMED WINDOW CORNER FASTENERS HOLE INSPECTION PER S/B 737-53A1177R6 AND DISCOVERED DEFECTS IN WINDOW CORNERS WITH CRACK INDICATION AT BS 787 RIGHT WINDOW UPPER AFT CORNER USING HFEC METHODS. TRIMMED OUT THE THREE HOLES IN THE DAMAGED AREA. HFEC THE EDGE OF THE TRIM. FABRICATED A DOUBLER AND A TRIPPER THICK AND FILLER AS SHOWN IN FIGURE 1 DEVIATION P/U. INSTALLED REPAIR PARTS. RECEIPT OF 8110-3 FROM BOEING. REPAIR COMPLETED IAW ECO 3250 AND DEVIATION P/U. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW S/B 737-53A1177R 6 AND DISCOVERED DEFECTS IN WINDOW CORNERS WITH CRACK INDICATION AT BS 867 RIGHT WINDOW BOTTOM FORWARD CORNER USING HFEC METHODS. TRIMMED OUT THE THREE HOLES IN THE DAMAGED AREA. HFEC THE EDGE OF THE TRIM. ENLARGED TRIM BY .04 INCHS, AN INSURANCE CUT MAINTAINING A .05 INCH MINIMUM CORNER RADIUS AND 2D EDGE MARGIN FROM FASTENERS. REPAIRED IAW SRM AIRCRAFT RETURNED TO SERVICE. (M)

Part: BULKHEAD — CRACKED (NLG WW)

FOUND CRACK ON UPPER BULKHEAD IN THE NOSE WHEEL WELL. TRIMMED OUT CRACK ENSURING A .50 INCH MINIMUM RADIUS. VERIFIED CRACK REMOVED USING HFEC METHOD AND MADE A .040 INCH INSURANCE CUT. FABRICATED A FILLER FROM .050 INCH, A DOUBLER FROM .063 INCH AND TWO TAPPERED FILLERS AS SHOWN IN FIGURE 1 WITH A 50:1 TAPER RATION FROM 2024-T3 CLAD SHEET. INSTALLED ALL REPAIR PARTS IAW FIGURE 1. VERIFIED 8110-3 RECEIVED FROM BOEING. REPAIR COMPLETED IAW ECO 3194. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SENSOR — MALFUNCTIONED (A/C BAY)

FLT 201 - HNL-LIH - AFTER TAKEOFF, NR 2 PACK TRIPPED. RESET AND TRIPPED AGAIN. RETURNED TO HNL FOR UNEVENTFUL LANDING. REPLACED THE 365 TEMPERATURE SENSOR AND MODULATING VALVE. OPS CHECK, LEAK CHECK AND ENGINE RUN OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: VALVE — MALFUNCTIONED (A/C BAY)

FLT 201 - HNL-LIH - AFTER TAKEOFF, NR 2 PACK TRIPPED. RESET AND TRIPPED AGAIN. RETURNED TO HNL FOR UNEVENTFUL LANDING. REPLACED THE 365 TEMPERATURE SENSOR AND MODULATING VALVE. OPS CHECK, LEAK CHECK AND ENGINE RUN OK. AIRCRAFT RETURNED TO SERVICE. REF TSAA0221021. (M)

Part: VALVE — MALFUNCTIONED (A/C BAY)

FLT 201 - HNL-LIH - AFTER TAKEOFF, NR 2 PACK TRIPPED. RESET AND TRIPPED AGAIN. RETURNED TO HNLG FOR UNEVENTFUL LANDING. REPLACED THE 365 TEMPERATURE SENSOR AND MODULATING VALVE. OPS CHECK, LEAK CHECK AND ENGINE RUN OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SENSOR — MALFUNCTIONED (A/C BAY)

FLT 201 - HNL-LIH - AFTER TAKEOFF, NR 2 PACK TRIPPED. RESET AND TRIPPED AGAIN. RETURNED TO HNLG FOR UNEVENTFUL LANDING. REPLACED THE 365 TEMPERATURE SENSOR AND MODULATING VALVE. OPS CHECK, LEAK CHECK AND ENGINE RUN OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

REPAIRED 1.25 INCH FUSELAGE SKIN CRACK AT BS 787 S-11L. TRIMMED OUT CRACK DAMAGE AND VERIFIED WITH HFEC, NO DEFECTS NOTED. FABRICATED, INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 53-30-3 FIGURE 25. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED LEFT OVERWING IDENT POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: SKIN — CRACKED (FUSELAGE)

IDENTIFIED 3 INCH CRACK AT BS 500 STRINGER 15R. TEMPORARY REPAIR INSTALLED BY TRIM OYT OF CRACK, INSPECTED CUTOUT USING HFEC METHOD AND INSTALLED EXTERNAL DOUBLER. RECEIVED 8110-3 APPROVAL. PERMANENT REPAIR REQUIRED WITHIN 1 MONTH OR 500 CYCLES WHICHEVER IS LESS, IAW ECO 3197. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

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

Part: BATTERY PACK — INOPERATIVE (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

REPAIRED BROKEN WIRE TO LEFT OVERWING EXIT IDENTIFIER LIGHT. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

REPAIRED BROKEN WIRE TO LEFT OVERWING EXIT IDENTIFIER LIGHT. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

REPLACED AFT SERVICE DOOR EMERGENCY EXIT IDENTIFIER BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONNECTOR — CONTAMINATED (YAW DAMPER/AFCS)

FLT 87-KOA-HNL-AT FL190, A/C STARTED ROLLING AND YAWING INCREASING IN RATE. DISENGAGED AUTOPILOT, ROLL AND YAW INCREASED. YAW DAMPER DISENGAGED, PILOT CONTROLLED ROLL AND A/C STABILIZED. DECLARED EMERG, FOUND YAW DAMPER C/B TRIPPED DUE TO COFFEE SPILLAGE ON YAW DAMPER COUPLER CONNECTOR. INSPECT REVEALED DRIP SHIELD BEHIND E1-1 NOT ATTACHED. REMOVED YAW DAMPER COUPLER AND PDC COMPUTER, CLEANED AREA OF COFFEE SPILLAGE. INSPECTED, FOUND NO DAMAGE TO CONNECTOR. REMOVED ADJACENT COMPONENTS ON E1 RACK, CLEANED/INSPECTED RACK AND COMPONENTS FOR MOISTURE CONTAM. REPLACED YAW DAMPER COUPLER. PERFORMED ADJ/TEST PER AMM 22-12-0. INSTALLED PDC. R/R''D DFDR. OPS CHECK OK. FOUND FWD GALLEY TRASH BIN MISSING SEALANT, SEALED T

Part: BATTERY PACK — INOPERATIVE (CABIN)

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

Part: BATTERY PACK — INOPERATIVE (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: SKIN — CRACKED (BS 957/970)

FOUND TWO CRACKS ON LEFT OF AIRCRAFT BELOW AFT ENTRY DOOR, BELOW STRINGER 21L AT BS 957 AND 970. REPAIRED PER SRM 53-30-3 PAGE 2B. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED BATTERY PACK FOR NR 1 FLOOR PROXIMITY LIGHT ASSY DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (EMER EXIT)

REPLACED RIGHT OVERWING SLIDE LIGHT BATTERY POWER SUPPLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (EMER EXIT)

REPLACED RIGHT OVERWING SLIDE LIGHT BATTERY POWER SUPPLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (EMER EXIT)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED LEFT OVERWING SLIDE LIGHT BATTERY POWER SUPPLY DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED RIGHT OVERWING SLIDE LIGHT BATTERY POWER SUPPLY DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED POWER PACK FOR POSITION NR 6 FLOOR PROXIMITY LIGHT ASSEMBLY DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: LIGHT — INOPERATIVE (PAX DOOR)

REPLACED AFT ENTRY DOOR OVERHEAD EMERGENCY LIGHT ASSY DUE TO INOPERATIVE. OPS CHECKS OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONTROL MODULE — INOPERATIVE (CABIN)

AFT INTERVALVE EMERGENCY CONTROL MODULE TRIGGERING LIGHT ASSEMBLY. REPLACED AFT CONTROL MODULE, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

AFT INTERVALVE EMERGENCY CONTROL MODULE TRIGGERING LIGHT ASSEMBLY. REPLACED AFT CONTROL MODULE BATTERY PACK, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (SERVICE DOOR)

REPLACED FORWARD SERVICE DOOR EMERGENCY EXIT IDENTIFIER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (SERVICE DOOR)

REPLACED FORWARD SERVICE DOOR EMERGENCY EXIT IDENTIFIER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED THE INTERIOR OVERWING EMERGENCY LIGHT BATTERY DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (BS 947)

DURING HEAVY CHECK, FOUND LAP JOINT BULGING AND SHOWING SIGNS OF CORROSION, BS 947, STRINGER 25L, FORWARD OF POTABLE WATER SERVICE PANEL. CLEANED CORROSION ON LAP JOINT IAW SRM 51-10-6. REPAIRED IAW ECO 2907 R1, PER OPTION 11. (M)

Part: SKIN — CRACKED (BS 1155)

DURING HEAVY CHECK, FOUND UPPER FUSELAGE SKIN CRACK AT BS 1155, 10 INCHES LEFT OF BL 0. CRACK APPROXIMATELY 2 INCHES LONG. VERIFIED PER HFEC. REPAIRED PER SRM 53-30-3. (M)

Part: MOUNT — LOOSE (NR 2 ENGINE)

DURING HEAVY CHECK, FOUND NR 2 ENGINE FORWARD MOUNT LOOSE. REMOVED AND REPLACED BEARING AND BUSHINGS PER OHM 71-23-01. REPLACED BOLTS AND BUSHINGS USING ECO 2908, AD 98-14-09 AND REFERENCE PER MM 54-41-11. (M)

Part: SPAR — CORRODED (HORIZ STAB)

DURING HEAVY CHECK, FOUND LEFT STABILIZER TOP SIDE STABILIZER STATION 83.50 AFT SPAR HAS CORROSION, TWO PLACES. REPAIRED PER ECO 1889. (M)

Part: SKIN — CORRODED (BS 967)

DURING HEAVY CHECK, FOUND LAP JOINT BULGING DUE TO POSSIBLE CORROSION BS 967, STRINGER 25L, AFT OF POTABLE WATER SERVICE PANEL. CLEANED CORROSION ON LAP JOINT IAW SRM 51-10-6. REPAIRED IAW ECO 2497 R1, PER OPTION 11. (M)

Part: STRINGER — CORRODED (BS 967)

DURING HEAVY CHECK, FOUND CORROSION ON STRINGER 25L AT BS 967, JUST AFT OF WATER SERVICE PANEL. REPAIRED STRINGER 25L PER SRM 53-10-3. (M)

Part: SKIN — CORRODED (WS 418)

DURING HEAVY CHECK, FOUND LOWER LEFT WING SURFACE AT RSS 418 CORRODED, INBOARD OF NR 1 TRACK. REPAIRED PER ECO 1684 R9. (M)

Part: PRESS BULKHEAD — CRACKED (BS 727)

DURING HEAVY CHECK, FOUND LEFT WHEEL WELL AREA BS 727 PRESSURE BULKHEAD CRACK APPROX 2.5 INCH LONG, LOWER CHORD. REPLACED LOWER CHORD IAW ECO 1785. (M)

Part: BATTERY PACK — DISCHARGED (NR 6 POS)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: LIGHT ASSY — INOPERATIVE (NR 5 POS)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

REPLACED NR 3 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

REPLACED NR 5 POSITION EMERGENCY FLOOR LIGHT ASSY. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: INDICATOR — FAILED (HYD SYSTEM)

SYSTEM 'B' HYDRAULIC BRAKE PRESSURE IS LOW AT 2300 PSI AFTER TAKEOFF. HYDRAULIC SYSTEM PRESSURE IS NORMAL AND 'A' BRAKE PRESSURE NORMAL. REPLACE INDICATOR AND TRANSMITTER. OPS AND LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (SERVICE DOOR)

FORWARD SERVICE DOOR EXIT IDENTIFICATION LIGHT ASSY DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

FORWARD SERVICE DOOR EMERGENCY LIGHT DOES NOT TEST. REPLACED BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

FORWARD ENTRY DOOR EMERGENCY LIGHT DOES NOT TEST. REPLACED BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: FITTING — CRACKED (BS 695)

RIGHT SIDE MAIN LANDING GEAR SUPPORT FITTING CRACKED AT BS 695 AND INBOARD OF STR 18R. CRACKED CONFIRMED TO BE 2.25 INCHES LONG. REMOVED AND REPLACED SUPPORT FITTING PER SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: LIGHT — INOPERATIVE (CABIN)

FORWARD SERVICE DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSY, INOPERABLE AND CRACKED. REPLACED LIGHT ASSY. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X)

Part: LIGHT — INOPERATIVE (CABIN)

ON SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHT INOP. REPLACED FLOOR LIGHT PROXIMITY ASSY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND POSITION NR 6 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 38,634:27 HOURS. TAC: 40,591. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SERVICE CHECK, FOUND POSITION NR 1 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 38,634:27 HOURS. TAC: 40,591. (X)

Part: SIGN — INOPERATIVE (CABIN)

ON SERVICE CHECK, FOUND FORWARD SERVICE DOOR IDENTIFIER INOP. REPLACED IDENTIFIER SYSTEMS. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SIGN — INOPERATIVE (CABIN)

ON SERVICE CHECK, FOUND FORWARD SERVICE DOOR EXIT IDENTIFIER INOP. REPLACED EXIT IDENTIFIER. 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: SWITCH — INOPERATIVE (COCKPIT)

DURING OVERNIGHT CHECK, REPLACED EMERGENCY LIGHT SWITCH DUE TO SWITCH BEING INTERMITTENTLY INOPERABLE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 37,453:56 HOURS. TAC: 37,958. (X)

Part: BATTERY — DISCHARGED (CABIN)

DURING OVENRIGHT CHECK, REPLACED BATTERY FOR ROW 4 EMERGENCY FLOOR PROXIMITY LIGHT ASSY DUE TO INOPERABLE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 37,420:04 HOURS. TAC: 37,880. (X)

Part: ENGINE — FAILED (NR 1)

PILOT REPORT - FLT 133 - NR 1 ENGINE EGT AT 555 DEGREES, CLIMB POWER SETTING. ABLE TO REDUCE TEMPERATURE BY PULLING BACK EPR BY .04 TO 545 DEGREES. TEMPS OK IN DESCENT AT FLIGHT IDLE, ALL OTHER ENGINE INDICATIONS OK. TEMP AT TAKEOFF, RIGHT AT RED LINE 590 DEGREES. REPLACED NR 1 ENGINE ASSY 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. (X)

Part: BATTERY — DISCHARGED (CABIN)

DURING OVERNIGHT CHECK, REPLACED ROW 17 EMERGENCY FLOOR LIGHT ASSY BATTERY DUE TO LIGHT ASSY LED'S INOP. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 37,355:14 HOURS. TAC: 37,731. (X)

Part: CONNECTOR — LOOSE (CABIN)

DURING OVERNIGHT CHECK, CORRECTED CENTER AND AFT FLOOR EMERGENCY LIGHT TRANSMITTER WIRING HOOK-UP PER 33-51-43. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 37,310:57 HOURS. TAC: 37,634. (X)

Part: BATTERY — DISCHARGED (CABIN)

DURING OVERNIGHT CHECK, REPLACED ROW 22 EMERGENCY FLOOR PROXIMITY LIGHT ASSEMBLY BATTERY DUE TO INOP. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONTROL MODULE — FAILED (CABIN)

DURING OVERNIGHT CHECK, REPLACED EMERGENCY FLOOR LIGHT CENTER CONTROL MODULE ASSEMBLY DUE TO TRANSMITTER BAD. OPERATIONAL CHECK OF AIRCRAFT RETURNED TO SERVICE. (M)

Part: GCU — FAILED (E/E COMPT)

FLT 40 - HNL-ITO - SWITCHING FROM EXTERNAL TO APU ELECTRICAL POWER, SMOKE BEGAN BELLOWING OUT OF CIRCUIT BREAKER PANEL NEAR THE G-5 GENERATOR CONTROL BOX, POWER SECURED. REPLACED GCU. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRINGER — CORRODED (BS 520)

DURING HEAVY MAINTENANCE VISIT AT TIMCO, FOUND STA 520 STR 10R CORRODED AT FRAME CLIP. FABRICATED SPLICE AND TRIMMED NEW STRINGER SECTION IAW B737 SRM 53-10-3, FIG 3. REPAIRED IAW B737 SRM 51-30-2 AND FINISHED IAW SRM 51-10-2. AIRCRAFT RETURNED TO SERVICE. MATERIAL I.D. .040 INCH 7075T6 STRINGER SPLICES. TIMCO NON-ROUTINE CARD NR 28302. (X)

Part: FRAME — CORRODED (BS 727)

DURING HEAVY MAINTENANCE VISIT AT TIMCO, FOUND SHEAR TIE AND FRAME CORRODED BETWEEN S20L AND S21L, FS 727A. REMOVED DAMAGED SHEAR TIE AND DAMAGED SECTION OF FRAME IAW B737 SRM 51-30-3. FABRICATED REPAIR FILLER AND DOUBLER IAW B737 SRM 53-10-2 AND SRM 53-10-4. FINISHED IAW B737 SRM 51-10-2. INSTALLED SHEAR TIE, FILLER, AND REPAIR DOUBLER IAW B737 SRM 51030-2. AIRCRAFT RETURNED TO SERVICE. MATERIAL I.D. .063 INCH 204T3 FILLER, AND .071 INCH 2024 T3 DOUBLER. TIMCO NON-ROUTINE CARD NR 28429. (X)

Part: STRINGER — CORRODED (BS 767)

DURING HEAVY MAINTENANCE VISIT AT TIMCO, FOUND AFT CARGO COMPARTMENT STR 19L CORRODED AT FS 767. FABRICATED REPAIR CHANNEL AND ANGLE IAW B737 SRM 53-10-3. INSTALLED REPAIR IAW SRM 53-30-0, AND FINISHED IAW SRM 51-10-2. AIRCRAFT RETURNED TO SERVICE. MATERIAL I.D. .063 INCH 7075-0 REPAIR CHANNEL AND ANGLE. TIMCO NON-ROUTINE CARD NR 28435. (X)

Part: SKIN — GOUGED (BS 188-196)

DURING HEAVY MAINTENANCE VISIT AT TIMCO, FOUND FUSELAGE EXT SKIN GOUGED FROM BS 188 TO BS 196, S17R. FABRICATED DOUBLER IAW B737 SRM 53-30-3. REPAIRED IAW B737 SRM 53-30-3 AND SRM 51-30-2. FINISHED IAW SRM 51-10-2. AIRCRAFT RETURNED TO SERVICE. MATERIAL I.D. .080 INCH 2024-T3 ALUMINUM SHEET, DOUBLER. TIMCO NON-ROUTINE CARD NR 28202. (X)

Part: FLOORBEAM — CRACKED (BS 807)

DURING HEAVY MAINTENANCE VISIT AT TIMCO, FOUND AFT CARGO COMPARTMENT FLOORBEAM ABOVE S26R AT FS 807 BENT AND CRACKED. FABRICATED REPAIR ANGLE AND FILLER IAW B737 SRM'S 51-30-5, 51-30-6, AND 51-40-3. REPAIRED IAW B737 SRM'S 51-40-3 AND 51-30-2. FINISHED IAW SRM 51-10-2. AIRCRAFT RETURNED TO SERVICE. MATERIAL I.D. .071 INCH 7075T6 REPAIR ANGLE. MATERIAL I.D. .063 7075T6 FILLER. TIMCO NON-ROUTINE CARD NR 28433. (X)

Part: SKIN — DAMAGED (VERTICAL STAB)

DURING HEAVY MAINTENANCE VISIT AT TIMCO, FOUND VERTICAL STABILIZER L/E STA 245 DENTED. FABRICATED DOUBLER IAW B737 SRM 55-30-6. RPAIRED IAW B737 SRM 51-30-0 AND FINISHED IAW SRM 51-10-2. AIRCRAFT RETURNED TO SERVICE. MATERIAL I.D. .063 INCH 2024-T3 ALUMINUM SHEET. TIMCO NON-ROUTINE CARD NR 28635. (X)

Part: INTERCOSTAL — CRACKED (BS 332)

DURING HEAVY MAINTENANCE VISIT AT TIMCO WHILE PERFORMING FUSELAGE-FORWARD SERVICE DURING AFT FRAME INSPECTION, FOUND CRACK ON INTERCOSTAL AT STA 332 WL 268 UPPER AFT STOP FITTING. FABRICATED -3 STIFFENER, -10 WEB -7, -8, AND -9 FILLERS IAW DWG NR 65C33288. REPAIRED IAW SRM 51-20-1 AND 51-30-2. ACFT RETURNED TO SERVICE. MATERIAL I.D. -3 STIFFENER AND -10 WEB 7075T6 .063 INCH. MATERIAL I.D. -7, -8, AND -9 FILLERS 2024T3 .050 INCH. TIMCO NON-ROUTINE CARD NR 28375. (X)

Part: FRAME — CORRODED (BS 500B)

DURING HEAVY MAINTENANCE VISIT AT TIMCO, FOUND FORWARD BAGGAGE PIT RT STA BS 500B FRAME CORRODED WHERE SLANT PANEL ANGLE COVERS IT. FABRICATED REPAIR ANGLE IAW B737 SRM 51-40-3 FIG 1. REPAIRED IAW B737 SRM 51-40-3 AND FINISHED IAW SRM 51-10-2. AIRCRAFT RETURNED TO SERVICE. MATERIAL I.D. .050 INCH 7075-0 ALUMINUM SHEET. TIMCO NON-ROUTINE CARD NR 28910. (X)

Part: FRAME — CORRODED (BS 500A)

DURING HEAVY MAINTENANCE VISIT AT TIMCO, FOUND FWD BAGGAGE PIT BS 500A FRAME CORRODED WHERE SLANT PANEL ANGLE ATTACHES RT SIDE. FABRICATED REPAIR ANGLE IAW B737 SRM 51-40-3, FIG 1. REPAIRED IAW B737 SRM 51-40-3 AND FINISHED IAW SRM 51-10-2. AIRCRAFT RETURNED TO SERVICE. MATERIAL I.D. .050 INCH 7075-0 ALUMINUM SHEET. TIMCO NON-ROUTINE CARD NR 28907. (X)

Part: STRINGER — CORRODED (BS 436)

DURING HEAVY MAINTENANCE VISIT AT TIMCO, FOUND STA 436 STR 9R CORRODED FORWARD OF FRAME CLIP. REPAIRED IAW SRM'S 51-10-6, 53-10-3, FIG 3, 51-10-2 AND 51-30-2. AIRCRAFT RETURNED TO SERVICE. MATERIAL I.D. STRINGER SPLICE .040 INCH 7075 T6. TIMCO NON-ROUTINE CARD NR 28998. (X)

Part: STRINGER — DAMAGED (BS 277)

DURING HEAVY MAINTENANCE VISIT AT TIMCO, FOUND STA 227 STR 3L PUNCTURED. REPAIRED DAMAGED STRINGER SECTION IAW B737 SRM 53-10-3, FIG 3, SRM 51-10-3, SRM 51-20-4, AND SRM 51-30-2. AIRCRAFT RETURNED TO SERVICE. MATERIAL I.D. .040 INCH .040 7075 T6 STRINGER SPLICE. TIMCO NON-ROUTINE CARD NR 28994. (X)

Part: SKIN — GOUGED (BS 907)

DURING HEAVY MAINTENANCE VISIT AT TIMCO, FOUND FUSELAGE EXTERIOR SKIN GOUGED AT BS 907, S14L. FABRICATED DOUBLER AND FILLER IAW B737 SRM 53-30-3. REPAIRED IAW B737 SRM 53-30-3 AND 51-30-2. FINISHED IAW SRM 51-10-2. AIRCRAFT RETURNED TO SERVICE. MATERIAL I.D. .080 INCH 2024T3 FILLER. MATERIAL I.D. .090 INCH 2024T3 DOUBLER. TIMCO NON-ROUTINE CARD NR 28176. (X)