N688AA

Part: FSEU — FAULTED (TE FLAP) · airframe 82,426 hrs · 22,785 cycles

AIRCRAFT WAS GNDED. EMER DECLARED & LANDING UNEVENTFUL. DURING APPROACH WHEN FLAPS SELECTED TO 25 RECEIVED, TE FLAP DISAGREE, EICAS MSG & TE FLAP AMBER MASTER CAUTION. ACCOMPLISHED FIM 27-51-00 WITH FSEU 1 SHOWING FAULT CODE 305. FSEU 2 & 3 SHOWED NO FAULTS. R & R FSEU 1 IAW AMM 27-51-01. ACCOMPLISHED OPERATIONAL CHECK. SYS CHECKED NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 82,371 hrs · 22,762 cycles

AIRCRAFT WAS NOT GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFULLY & ACFT WAS NOT OVERWEIGHT. DURING APPROACH, RECEIVED FLAP ASYMMETRY FAULT WHEN FLAPS 25 SELECTED. PERFORMED FIM PROCEDURE IAW 27-81-00 WITH NO CURRENT FSEU FAULTS NOTED. INSPECTED FLAP TRACKS & FLAP TRANSMISSIONS WITH NO DEFECTS NOTED.

Part: ACM — FAULTY (AC BAY) · airframe 82,001 hrs · 22,617 cycles

AIRCRAFT WAS GNDED. SMOKE IN COCKPIT ON TAXI OUT. APPEARED TO BE ELEC IN NATURE. R & R LT ACM IAW AMM 21-51-03. LEAK & OPERATIONAL CHECK PERFORMED. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,001 hrs · 22,617 cycles

EMERGENCY LIGHTS L2 & R2 DIMLY LIT. EMER EXIT LIGHTS ARE DIMLY LIT FROM ROW 10 - 15. R & R BATTERY PACK AT MODULE M10799 IAW AMM 33-51-07. OPERATIONALLY CHECKED NORMAL. THE ACFT WAS NOT GNDED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,001 hrs · 22,617 cycles

EMERGENCY LIGHTS L1 & R1 DOOR, SIDE EXIT LIGHT INOPERATIVE. R & R BATTERY PACK AT MODULE M 10798 IAW AMM 33-51-07. OPERATIONALLY CHECKED NORMAL. THE ACFT WAS NOT GNDED.

Part: ENGINE — FAILED (RIGHT) · airframe 81,508 hrs · 22,435 cycles

RIGHT ENG AUTO SHUTDOWN IN FLIGHT, CRUISE ALTITUDE 360, WITH NO ABNORMAL INDICATIONS PRIOR. RECEIVED RT ENG LP PUMP EICAS MSG AT SHUTDOWN. ATTEMPTED RE-START, NO FUEL FLOW DURING ATTEMPT. EMERGENCY DECLARED, FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO VIBRATIONS OR ANY OTHER INDICATIONS. SINGLE ENG TIME 40 MINUTES FROM FAIL TO TOUCHDOWN. R & R RT ENG IAW MCMS 71-94-01, 71-95-23, 71-95-22, 71-94-42, 71-92-01 & 71-94-03. ALL LEAK & OPERATIONAL CHECKED OK.

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 79,867 hrs · 22,006 cycles

DURING CLIMB A HARD BIRD STRIKE DOWN THE LT SIDE OCCURRED. THE LT ENGINE EXPERIENCED A VIBRATION SPIKE OF 1.4 N-3. RETARDED THROTTLES & VIBRATIONS CEASED. NOTED EVIDENCE OF CORE INGESTION IN THE NR 1 ENGINE. PERFORMED INSPECTION CARD 05-96-14 & FOUND NR 1 ENG MISSING ANNULUS STRIP, MISSING AT 11 O’CLOCK POSITION, SCHEDULED FOR REPLACEMENT. PERFORMED VIBRATION SURVEY TEST NR 6 & TEST NR 5 IAW AMM TASK 71-00-00-715-327-RO3. SYS CHECKED NORMAL.

Part: CONTROL SWITCH — DEFECTIVE (COCKPIT) · airframe 78,679 hrs · 21,721 cycles

EMERGENCY LIGHT WILL NOT SHUT OFF WHEN ACFT IS POWERED DOWN. R & R COCKPIT EMER LIGHT CONTROL SWITCH.

Part: GIRT BAR — BROKEN (R4 DOOR) · airframe 78,506 hrs · 21,680 cycles

R4 DOOR GIRT BAR HANGING DOWN. FOUND R4 DOOR GIRT BAR FWD SLIDER RETAINING SPRING BENT. REPLACED R4 DOOR GIRT BAR IAW AMM 25-66-01.

Part: SLIDE — DETACHED (PAX DOOR) · airframe 78,292 hrs · 21,633 cycles

FLIGHT DECK REPORTED FWD DOOR SLIDE FELL OFF DURING THE PROCESS OF OPENING L1 DOOR. REPLACED DOOR ASSIST BOTTLE & INSTALLED SLIDE IAW AMM 52-11-30 AND AMM 25-66-01. . OPS & LEAK CHECKED NORMAL. ACFT OK FOR CONTINUED TO SERVICE.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 78,077 hrs · 21,567 cycles

CRACKED INTERCOSTAL IN CEILING OF AFT CARGO COMPARTMENT BETWEEN FUSELAGE STATIONS 1661 & 1681 AT RBL 35. R & R INTERCOSTAL IAW AARD 51-00-05-1.

Part: COOLING FAN — INOPERATIVE (E&E BAY) · airframe 77,173 hrs · 21,355 cycles

DURING DESCENT ACRID FUMES IN THE COCKPIT & CABIN. DECLARED EMER FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED FWD E & E EQUIPMENT COOLING FAN. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: OVEN — DIRTY (GALLEY) · airframe 74,040 hrs · 20,581 cycles

ELP INFLIGHT LAX-DFW. SMOKE IN THE FLIGHT DECK. EMERGENCY DECLARED FLIGHT DIVERTED ELP LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FOM SERVICE. FOUND FIRST CLASS OVENS WERE DIRTY CAUSING SMOKE. REMOVED LARGE AMOUNTS OF FOOD DEBRIS & OIL FROM AFT CORNERS OF OVENS. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,377 hrs · 18,925 cycles

CORROSION ON RIGHT CREASE BEAM WEB FROM STATIONS 1380 TO 1400. REPLACED WEB PER AARD 51-10-05-1.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,377 hrs · 18,925 cycles

AFT PRESSURE DECK DOUBLER CORRODED AT STATION 1700. REPLACED AFT PRESSURE DECK DOUBLER PER SRM 53-60-51-2R 2.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,377 hrs · 18,925 cycles

WEB AT STATIONS 1400 TO 1420 LEFT SIDE OF STRINGER 30 CORRODED. REPLACED WEB PER AARD 51-20-00-1.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 67,377 hrs · 18,925 cycles

LOWER DOOR SKIN DAMAGED. REMOVED DAMAGED SKIN AND INSTALLED DOUBLER PER SRM 52-30-01.

Part: SKIN — DAMAGED (LE SLAT) · corrosion level 2 · airframe 67,377 hrs · 18,925 cycles

DEEP BLEND ON NUMBER 2 SLAT AT INBOARD DRIVE TRACK LOWER LEADING EDGE. REMOVED DAMAGED AREA AND INSTALLED SLAT SKIN FLUSH REPAIR PER AARD 57-43-00-1.

Part: BEAM — DAMAGED (CARGO DOOR) · airframe 67,377 hrs · 18,925 cycles

AFT CARGO DOOR- LOWER EDGE BEAM HAS PUNCTURE IN RADIUS AT MID SPAN AREA. DAMAGED EDGE BEAM REMOVED. NEW EDGE BEAM DRILLED AND INSTALLED NEW EDGE BEAM PER ESO 90121.

Part: SUPPORT — CORRODED (CARGO DOOR) · airframe 67,377 hrs · 18,925 cycles

AFT CARGO DOOR- 2ND FROM FORWARD LOWER SKIN SUPPORT RIB CORRODED AT LOWER EDGE BEAM AREA. CORRODED RIB REMOVED AND NEW RIB DRILLED AND INSTALLED PER ESO 90121.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 67,377 hrs · 18,925 cycles

AFT CARGO DOOR- SKIN LOWER EDGE OF DOOR HAS MANY FASTENERS DAMAGED. DAMAGED AREA OF SKIN CUT AND REMOVED. REPAIR DOUBLER AND FILLER FABRICATED, DRILLED AND INSTALLED PER 52-30-01-2R 4.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 67,377 hrs · 18,925 cycles

RIGHT WING NUMBER 9 SLAT HAS CORROSION AROUND FASTENER ON TOP SKIN APPROXIMATELY 30 INCHES OUTBOARD OF INBOARD END. INSTALLED FLUSH DOUBLER REPAIR ON NUMBER 9 SLAT PER AARD 57-43-00-01.

Part: SKIN — DAMAGED (LE SLAT) · corrosion level 2 · airframe 67,377 hrs · 18,925 cycles

RIGHT WING NUMBER 10 SLAT HAS DAMAGE AT UPPER SKIN APPROXIMATELY 41.5 INCHES FROM OUTBOARD END AT AUXILIARY TRACK. REMOVED DAMAGED AREA OF SKIN AND INSTALLED FLUSHED DOUBLER PER AARD 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 67,377 hrs · 18,925 cycles

CORROSION AROUND HILOCK HEAD AT INBOARD AUXILARY TRACK RIB UPPR SKIN, NUMBER 10 SLAT. REMOVED DAMAGED AREA OF SKIN AND INSTALLED FLUSHED DOUBLER PER AARD 57-43-00-1

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 67,377 hrs · 18,925 cycles

NUMBER 2 SLAT HAS CORROSION 31 INCHES OUTBOARD FROM INBOARD END ON UPPER NOSE SKIN. REMOVED DAMAGE AREA AND INSTALLED FLUSH REPAIR PER AARD 57-43-00-1.

Part: SKIN — DAMAGED (LE SLAT) · airframe 67,377 hrs · 18,925 cycles

DEEP BLEND ON NUMBER 2 SLAT AT INBOARD DRIVE TRACK LOWER LEADING EDGE. REMOVED DAMAGED AREA AND INSTALLED SLAT SKIN FLUSH REPAIR PER AARD 57-43-00-1.

Part: SKIN — DAMAGED (LE SLAT) · airframe 67,377 hrs · 18,925 cycles

DEEP BLEND AT BLIND FASTNER ON NUMBER 2 SLAT UPPER SKIN AT INBOARD DRIVE TRACK. REMOVED DAMAGED AREA AND INSTALLED FLUSH REPAIR PER AARD 57-43-00-1.

Part: SKIN — DAMAGED (LE SLAT) · airframe 67,377 hrs · 18,925 cycles

DEEP BLEND ON NUMBER 2 SLAT UPPER SKIN AT INBOARD AUXILIERY TRACK RIB. REMOVED DAMAGED AREA AND INSTALLED FLUSH DOUBLER PER AARD 57-43-00-1 AND EA B757-27-021173.

Part: SKIN — DAMAGED (LE SLAT) · airframe 67,377 hrs · 18,925 cycles

DEEP BLEND AND BLIND FASTENER ON NUMBER 1 SLAT AT OUTBOARD DRIVE TRACK UPPER SKIN. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 57-43-00-1 AND EA B757-27-021173.

Part: SKIN PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 64,818 hrs · 18,299 cycles

LEFT WING UPPER SKIN PANEL UPPER SURFACE CORRODED. ACCOMPLISHED REPAIR PER EA B757-57-016736.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 61,483 hrs · 17,519 cycles

CORROSION ON OUTER FORWARD SKIN AT FASTENERS 30 INCHES FROM INBOARD END. INSTALLED DOUBLER.

Part: GUARD — BROKEN (CABIN) · airframe 59,316 hrs · 17,031 cycles

EMERGENCY LIGHT AT FORWARD SEAT 17D DAMAGED AND MISSING RED LENS. REPLACED GUARD AND LENS.

Part: PLACARD — PEELING (CABIN)

DFW - FORWARD LEFT OVERWING EMERGENCY EXIT IDENTIFIER PLACARD PEELING. REPLACED EXIT STICKER FOR FORWARD LEFT OVERWING EMERGENCY EXIT IDENTIFIER.

Part: LIGHT — INOPERATIVE (CABIN)

DFW FORWARD RIGHT NUMBER ONE DOOR EXIT MARKER INOPERATIVE. REPLACED LAMP AT FORWARD RIGHT NUMBER ONE DOOR EXIT MARKER.

Part: PLACARD — DAMAGED (CABIN)

DFW RIGHT FORWARD EXIT DECAL DAMAGED. REPLACED DECAL.

Part: LIGHT — INOPERATIVE (CABIN)

DFW FORWARD LEFT NUMBER ONE DOOR EXIT MARKER INOPERATIVE. REPLACED LAMP AT FORWARD LEFT NUMBER ONE DOOR EXIT MARKER.

Part: PLACARD — DAMAGED (CABIN)

DFW AFT LEFT NUMBER 2 DOOR EXIT MARKER DECAL DAMAGED. REPLACED DECAL.

Part: PLACARD — DAMAGED (CABIN)

DFW LEFT AFT EXIT DECAL DAMAGED. REPLACED DECAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 56,833 hrs

DFW - LEFT FORWARD EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT FORWARD EXTERIOR OVERWING.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 55,898 hrs · 16,179 cycles

INTERCOSTAL TOP ANGLE CRACKED, REPAIRED INTERCOSTAL IAW SRM 51-70-11-0G.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 55,898 hrs · 16,179 cycles

DRAIN SUPPORT CORRODED. REPLACED DRAIN SUPPORT IAW SRM 53-00-51.

Part: MOUNT — CORRODED (ZONE 100) · corrosion level 2 · airframe 55,989 hrs · 16,179 cycles

CENTER FORWARD GALLEY MOUNT FITTING CORRODED, REPLACED FITTING IAW SRM 53-60-51-2R.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 55,898 hrs · 16,179 cycles

HAT CHANNEL CORRODED. REPLACED HAT CHANNEL IAW SRM 53-00-51.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 55,898 hrs · 16,179 cycles

AFT MAIN DECK PLATE CORRODED. REPAIRED IAW SRM 53-60-51-2R2

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 55,898 hrs · 16,179 cycles

HAT CHANNEL CORRODED UNDER THRESHOLD OF R-4 PASSENGER/SERVICE DOOR, REPLACED CHANNEL IAW SRM 53-60-51-2R2.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 55,898 hrs · 16,179 cycles

CORROSION ON HAT CHANNEL FLOOR THRESHOLD SUPPORT AT R NR 4 PASSENGER/SERVICE DOOR. REPLACED HAT CHANNEL IAW SRM 53-00-51.

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 55,898 hrs · 16,179 cycles

TRANSITION PANEL CORRODED, REPLACED TRANSITION PANEL IAW SRM 53-60-53-2R.

Part: MOUNT — CORRODED (ZONE 100) · corrosion level 2 · airframe 55,898 hrs · 16,179 cycles

FORWARD RT GALLEY MOUNT FITTING CORRODED, REPLACED FITTING IAW SRM 53-60-51-2R.

Part: MOUNT — CORRODED (ZONE 100) · corrosion level 2 · airframe 55,898 hrs · 16,179 cycles

AFT LT GALLEY MOUNT FITTING CORRODED, REPLACED FITTING IAW SRM 53-60-51-2R.

Part: LENS — BROKEN (EMERGENCY LIGHT)

DFW EMERGENCY LIGHT AT LT NR 1DOOR HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LT NR 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: LENS — MISSING (EMERGENCY LIGHT)

DFW EMERGENCY LIGHT AT SEAT 16D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW SEAT MOUNTED EMERGENCY LIGHT AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHT AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: LENS — MISSING (EMERGENCY LIGHT)

DFW EMERGENCY LIGHT AT SEAT 15D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,795 hrs

JFK - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 16D INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: APU — LEAKING · airframe 53,684 hrs

LAX INFLIGHT T285/17APR - CREW REPORTED STRONG ELECTRICAL SMELL IN AFT CABIN FOLLOWED BY SMOKE ALARM SOUNDING IN AFT LAVATORY. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. FOUND OIL IN APU AIR DISCHARGE DUCT. REPLACED APU DUE TO OIL LEAK. ACCOMPLISHED CONTAMINATION REMOVAL. REPLACED AIR CYCLE MACHINES AND PRIMARY AND SECONDARY HEAT EXCHANGERS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — MISSING (EMERGENCY LIGHTS)

LAX - EMERGENCY LIGHT AT SEAT 9D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

LAX - EMERGENCY LIGHT AT SEAT 9D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

LAX - EMERGENCY LIGHT LENS ILLEGIBLE AND MOUNTING BRACKET BROKEN AT RIGHT MID CABIN OVER WING AT SEAT 18F. REPLACED LIGHT ASSEMBLEY FOR EMERGENCY LIGHT AT MID CABIN OVERWING AT SEAT 18F. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TRANSFER VALVE — INOPERATIVE (RT HYD QTY)

ORD - EICAS MESSAGE RIGHT HYDRAULIC QUANTITY WITH RESERVOIR LIGHT ILLUMINATED. FLIGHT CONTROLS WERE NORMAL UNTIL APPROACH WHEN CONTROL PROBLEM STARTED. REINSTATED BOTH RIGHT HAND HYDRAULIC PUMPS. FLIGHT CONTROLS WERE THEN NORMAL FOR LANDING. TIGHTENED LOOSE B-NUT AT BRAKE TRANSFER VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — LOOSE (EMERGENCY LIGHT)

DFW EMERGENCY LIGHT AT SEAT 22 INOPERATIVE. FOUND LOOSE WIRE. REINSTALLED WIRE CONNECTION FOR EMERGENCY LIGHT AT SEAT 22. SYSTEM GROUND CHECKED NORMAL OPERTION.

Part: LIGHT — BROKEN (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN AT SEAT 16D BROKEN. REPLACED EMERGENCY EXIT SEAT LIGHT AT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — LOOSE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATHWAY LIGHTING AT SEAT 22DEF INOPERATIVE. SECURED EMERGENCY EXIT PATHWAY LIGHT SOCKET AT 22DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: IDG — FAILED (GENERATOR)

OGG - FLT 161 - DURING DESCENT, LEFT GEN CONT OFF LIGHT ILLUMINATED, RAN CHECKLIST UNABLE TO RESTORE GENERATOR. REMOVED AND REPLACED LEFT IDG PER MM, OPS AND LEAK CHECK OK. (M)

Part: B-NUT — LOOSE (HYD SYSTEM)

SJU - FLT 633 - LEFT HYDRAULIC SYSTEM FLUID LOSS TO .33. FOUND B-NUT LOOSE ON HYDRAULIC RETURN LINE IN DOG HOUSE AREA FOR NR 1 ENGINE ACCOMPLISHED TORQUE ON B-NUT PER MM. REPLENISHED LEFT HYDRAULIC SYSTEM ACCOMPLISHED LEAK CHECK ON NR 1 ENGINE. NO LEAKS NOTED. OK FOR SERVICE. (M)

Part: B-NUT — LOOSE (HYD SYSTEM)

MIA - FLT 633 - EN ROUTE SJU-DFW, LEFT HYDRAULIC SYSTEM FLUID LOSS. CAPTAIN DECLARED EMERGENCY AND LANDED AT MIA WITHOUT FURTHER INCIDENT. INSPECTED AND FOUND B-NUT LOOSE ON HYDRAULIC RETURN LINE IN DOGHOUSE AREA FOR NR 1 ENGINE. ACCOMPLISHED RETORQUE OF B-NUT AND SERVICED HYDRAULIC SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DUCT — BLOWN (CABIN)

HNL - AFTER TAKEOFF AT KOA PASSENGERS AND F/A HEARD LOUD BANG MID MAIN CABIN CEILING PANEL IS BUCKLED NO PRESSURIZATION PROBLEM NOTED. FOUND BLOWN DUCT AT ROWS 17 A/C TO BE FERRIED TO LAX FOR CONT REPAIR LOOSE PANELS REMOVED AND PLACARD IN CGO COMPARTMENT. AIRCRAFT INSPECTED AND FOUND IN SAFE CONDITION FOR FERRY FLIGHT FROM HNL TO LAX PER SPOTTING MSG. FERRIED TO LAX FOR DUCT REPLACEMENT. (M)

Part: TIRE — FAILED (NR 3 MLG)

NR 3 MLG TIRE RECAP DEPARTED ON TAKEOFF LAX, FOUND ON RUNWAY. CREW ELECTED TO LAND IN HNL VERSUS LIH. FOUND TIRE STILL INFLATED YET RECAP DAMAGED NR 7 BRAKE LINE. REPLACED NR 3 AND NR 4 MLG TIRES AND DEACTIVATED NR 7 BRAKE PER MEL. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

AFW - FOUND CORROSION ON 1640 LBL 25 FLOORBEAM 2 INCHES WL RT. CORROSION ON 1640 AT WL FLOORBEAM 8 INCHES RIGHT. INSTALLED REPAIR STRAP FROM 301.5 H STAINLESS STEEL .50 THICKNESS. PER ATTACH ALODINE ALL BARE METAL SURFACE. FINISH BLEND AND REPAIRS PARTS WITH TWO COATS BMS 10-11 PRIMER UNTIL BLENDS WITH BMS 5-92. INSTALLED STRAPS WET WITH BMS 5-95 SEALANT PROSEAL 870. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, L2 DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPLACED EMERGENCY EXIT SIGN LIGHT MODULE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE FIRST CLASS LIGHT SEGMENT AT SEAT 1 AND BROKEN. REPLACED EMERGENCY EXIT LIGHT SEGMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: AIR DIST — SMOKE (COCKPIT)

BOG - FLT 910 - EN ROUTE BOG-MIA - CREW REPORTED SMOKE IN CABIN. AFT LAVATORY GOING OFF. RETURNED BOG AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT BUT NO EVIDENCE OF SMOKE FOUND. MAINTENANCE FERRY TO MIA WITH NO SMOKE NOTED ON FERRY FLIGHT. NO DEFECTS NOTED. ATBS ISSUED TO REINSPECT OVENS, COFFEE MAKERS, LAVATORIES FOR EVIDENCE OF SMOKE OR BEING HOT. AIRCRAFT FLEW FOUR TRIPS WITHOUT ANY SMOKE IN CABIN PROBLEMS. ATBT WAS ACCOMPLISHED WITH NO DISCREPANCIES NOTED. AIRCRAFT OK FOR SERVICE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SQUIB CARTRIDGE — DEFECTIVE (CABIN)

GYE - DURING OVERNIGHT CHECK, LEFT AND RIGHT SYSTEM SQUIB TEST FOR OVERWING EMERGENCY EVACUATION SLIDES FAILED TO ILLUMINATE. AIRCRAFT MAINTENANCE FERRY GYE. REPLACED LEFT AND RIGHT OVERWING EMERGENCY EVACUATION SLIDE SQUIB CARTRIDGES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL WIRE — EXPOSED (CABIN)

JFK - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT WIRING EXPOSED. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 5E AND 17D INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT PASSENGER SEAT ROW 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)