N606AA

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,570 hrs · 21,722 cycles

EMERGENCY LIGHTS BETWEEN ROWS 9 AND 15 ARE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW 33-51-07/901-001. OPS CHECKED NORMAL.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT) · airframe 62,570 hrs · 21,722 cycles

EMERGENCY LIGHTING INOPERATIVE BETWEEN ROW 26C AND DOOR R4. REMOVED AND REPLACED TWO CONTROL MODULES AND TWO BATTERY PACKS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,570 hrs · 21,722 cycles

FIRST CLASS SEAT MOUNTED EMERGENCY LIGHTING IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW AMM 33-51-07. OPERATIONAL CHECKED NORMAL.

Part: CONTROL MODULE — FAULTY (EMERGENCY LIGHTS) · airframe 62,570 hrs · 21,722 cycles

EMERGENCY LIGHTING INOPERATIVE BETWEEN ROW 26C AND DOOR R4. REMOVED AND REPLACED TWO CONTROL MODULES AND TWO BATTERY PACKS.

Part: CONTROL MODULE — FAULTY (EMERGENCY LIGHTS) · airframe 62,570 hrs · 21,722 cycles

EMERGENCY LIGHTING INOPERATIVE BETWEEN ROW 26C AND DOOR R4. REMOVED AND REPLACED TWO CONTROL MODULES AND TWO BATTERY PACKS.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT) · airframe 62,570 hrs · 21,722 cycles

EMERGENCY LIGHTING INOPERATIVE BETWEEN ROW 26C AND DOOR R4. REMOVED AND REPLACED TWO CONTROL MODULES AND TWO BATTERY PACKS.

Part: SHAFT — FAULTY (L1 DOOR) · airframe 62,569 hrs · 21,722 cycles

L1 DOOR DIFFICULT TO OPEN AND CLOSE. OUTSIDE HANDLE DOES NOT FULLY EXTEND AND GO OVER CENTER WHEN CLOSING. REMOVED AND REPLACED EXTERNAL HANDLE YOKE, CENTER SHAFT, AND CLUTCH COLLAR IAW AMM 52-11-13. OPERATIONAL CHECK GOOD.

Part: YOKE — FAULTY (L1 DOOR) · airframe 62,569 hrs · 21,722 cycles

L1 DOOR DIFFICULT TO OPEN AND CLOSE. OUTSIDE HANDLE DOES NOT FULLY EXTENDED AND GO OVER CENTER WHEN CLOSING. REMOVED AND REPLACED EXTERNAL HANDLE YOKE, CENTER SHAFT, AND CLUTCH COLLAR IAW AMM 52-11-13. OPERATIONAL CHECK GOOD.

Part: COLLAR — FAULTY (L1 DOOR) · airframe 62,569 hrs · 21,722 cycles

L1 DOOR DIFFICULT TO OPEN AND CLOSE. OUTSIDE HANDLE DOES NOT FULLY EXTEND AND GO OVER CENTER WHEN CLOSING. REMOVED AND REPLACED EXTERNAL HANDLE YOKE, CENTER SHAFT, AND CLUTCH COLLAR IAW AMM 52-11-13. OPERATIONAL CHECK GOOD.

Part: CONTROL MODULE — FAULTY (EMERGENCY LIGHTS) · airframe 62,370 hrs · 21,638 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHTS AT ROWS 26-36 ARE DARK. REMOVED AND REPLACED CONTROL MODULE M10801 AND BATTERY PACK IAW AMM 33-51-11 AND AMM 33-51-00. OPERATIONAL CHECKED GOOD.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 62,370 hrs · 21,638 cycles

EMERGENCY LIGHTS AT ROWS 26-36 ARE DARK. REMOVED AND REPLACED CONTROL MODULE AND BATTERY PACK IAW AMM 33-51-11 AND AMM 33-51-00. OPERATIONAL CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,370 hrs · 21,638 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 26-36 AND THE AFT ENTRY WALL EXIT MARKERS ARE INOPERATIVE. REMOVED AND REPLACED M10801 BATTERY PACK AND CONTROL MODULE IAW AMM 33-51-07. OPERATIONAL CHECK NORMAL. SEE ALSO AALA20161017004.

Part: CONTROL MODULE — FAULTY (CABIN) · airframe 62,370 hrs · 21,638 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 26-36 AND THE AFT ENTRY WALL EXIT MARKERS ARE INOPERATIVE. REMOVED AND REPLACED M10801 BATTERY PACK AND CONTROL MODULE IAW AMM 33-51-07. OPERATIONAL CHECK NORMAL. SEE ALSO AALA20161017001.

Part: CONTROL MODULE — FAULTY (EMERGENCY LIGHTS) · airframe 61,985 hrs · 21,487 cycles

AFT CABIN, L3 DOOR AND R3 DOOR EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AND CONTROL MODULE IAW AMM 33-51-07. OPERATIONAL CHECKED NORMAL.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 61,985 hrs · 21,487 cycles

AFT CABIN, L3 DOOR AND R3 DOOR EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AND CONTROL MODULE IAW AMM 33-51-07. OPERATIONAL CHECKED NORMAL.

Part: GOVERNOR — FAULTY (NR 1 ENGINE) · airframe 61,874 hrs · 21,441 cycles

DURING TAKE OFF, NR 1 ENGINE LAGGED BEHIND NR 2 AND WAS SLOW TO ATTAIN TAKE OFF POWER. DURING CLIMB THE NR 1 ENGINE REQUIRED MANUAL THROTTLE MOVEMENT TO ATTAIN COMMANDED CLIMB EPR WITH A THROTTLE LEVER SPLIT THAT REACHED 5 INCHES. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. MAINTENANCE REMOVED AND REPLACED HIGH PRESSURE FUEL PUMP IAW AMM 73-11-03 AND FUEL FLOW GOVERNOR IAW AMM 73-94-01. OPS AND LEAK CHECKED NORMAL.

Part: PUMP — FAULTED (FUEL SYSTEM) · airframe 61,874 hrs · 21,441 cycles

DURING TAKE OFF, NR 1 ENGINE LAGGED BEHIND NR 2 AND WAS SLOW TO ATTAIN TAKE OFF POWER. DURING CLIMB NR 1 ENGINE REQUIRED MANUAL THROTTLE MOVEMENT TO ATTAIN COMMANDED CLIMB EPR WITH A THROTTLE LEVER SPLIT THAT REACHED 5 INCHES. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. MAINTENANCE REMOVED AND REPLACED HIGH PRESSURE FUEL PUMP IAW AMM 73-11-03 AND FUEL FLOW GOVERNOR IAW AMM 73-94-01. OPERATIONAL AND LEAK CHECKS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,874 hrs · 21,441 cycles

SEAT MOUNTED EMERGENCY LIGHTS IN FIRST CLASS ARE VERY DIM. REMOVED AND REPLACED BATTERY PACK M10801 IAW AMM 33-51-07. OPS CHECKED NORMAL IAW AMM 33-51-0O.

Part: LENS — BROKEN (CABIN) · airframe 60,609 hrs · 20,945 cycles

AIRCRAFT WAS NOT GNDED. EMER EXIT LIGHT LENS BROKEN ON LT AFT GALLEY. R & R LENS.

Part: SLIDE — FAULTY (L1 DOOR) · airframe 60,414 hrs · 20,871 cycles

AIRCRAFT WAS GNDED. L1 DOOR OPENED WHILE STILL ARMED. ASSIST BOTTLE DISCHARGED BUT SLIDE DID NOT DEPLOY. R & R THE SLIDE PACK IAW AMM 25-66-01.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,276 hrs · 20,821 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 24DEF TO 36DEF. R & R BATTERY PACK AT ROW 24DEF. EMERGENCY LIGHTS OPERATIONALLY CHECKED GOOD IAW AMM 33-51-07. SEE ALSO SDR AALA20151127011.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,281 hrs · 20,823 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 24DEF TO 36DEF. R & R BATTERY PACK AT CEILING ABOVE AFT LAVATORIES. EMER LIGHTS OPERATIONALLY CHECKED GOOD IAW AMM 33-51-07. SEE ALSO SDR AALA20151127001.

Part: MODULE — INOPERATIVE (CABIN) · airframe 59,656 hrs · 20,608 cycles

SEAT MOUNTED EMER LIGHTS INOPERATIVE FROM ROW 26D TO 36D. R & R BATTERY MODULE IAW AMM 33-51-00.

Part: FILTER — DIRTY (AC BAY) · airframe 59,611 hrs · 20,596 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. JUST AFTER LEVEL OFF, FUMES REPORTED IN COCKPIT & CABIN SUGGESTIVE OF AN ELEC FIRE. FOUND DISPLACED INSULATION CONTACTED HOT DUCT, SECURED INSULATION. EVENT REPEATED ON NEXT FLIGHT WITH AN AIR INTERRUPT RETURN. R & R LT & RT HEPA FILTERS IAW AMM 21-25-02. ACCOMPLISHED SIC 05-96-07 WITH NO FINDINGS NOTED ON ENG RUN UP. SYS CHECKED NORMAL.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 58,849 hrs · 20,320 cycles

LENS COVER MISSING FROM EMERGENCY LIGHT ASSEMBLY AT ROW 16ABC. INSTALLED LENS COVER. OPERATIONS CHECKED GOOD IAW AMM 33-51-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 58,849 hrs · 20,320 cycles

LENS COVER MISSING FROM EMERGENCY LIGHT ASSEMBLY AT ROW 1AB. INSTALLED LENS COVER. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 58,849 hrs · 20,320 cycles

LENS COVER MISSING FROM EMER PATH LIGHT ASSEMBLY AT ROW 10DEF. INSTALLED LENS COVER. OPERATIONS CHECKED GOOD IAW AMM 33-51-00.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,827 hrs · 20,310 cycles

EMERGENCY LIGHTS INOPERATIVE BETWEEN SEAT ROWS 27DEF & 39DEF. R & R BATTERY PACK AT 41 CEILING NEAR VOICE RECORDER IAW AMM 33-51-07 WITH GOOD OPERATIONAL CHECK.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 58,827 hrs · 20,310 cycles

EMERGENCY LIGHTS INOPERATIVE BETWEEN SEAT ROWS 27DEF & 39DEF. R & R BATTERY PACK AT 31 CEILING NEAR VOICE RECORDER IAW AMM 33-51-07 WITH GOOD OPERATIONAL CHECK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 58,827 hrs · 20,310 cycles

EMERGENCY LIGHTS INOPERATIVE BETWEEN SEAT ROWS 27DEF & 39DEF. R & R BATTERY PACK AT CEILING NEAR VOICE RECORDER IAW AMM 33-51-07 WITH GOOD OPERATIONAL CHECK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 58,827 hrs · 20,310 cycles

EMERGENCY LIGHTS INOPERATIVE BETWEEN SEAT ROWS 27DEF & 39DEF. R & R BATTERY PACK AT CEILING NEAR VOICE RECORDER IAW AMM 33-51-07 WITH GOOD OPERATIONAL CHECK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 58,827 hrs · 20,310 cycles

CABIN EMERGENCY LIGHTS FROM RT SEAT ROW 9 - 16 INOPERATIVE. REPLACED BATTERY PACK & CHARGER IAW AMM 33-51-07 WITH GOOD OPERATIONAL CHECK.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,827 hrs · 20,310 cycles

RIGHT OVERWING EMER LIGHT INOPERATIVE. REPLACED BATTERY PACK & CHARGER.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,827 hrs · 20,310 cycles

MID CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED MODULE IAW AMM 33-51-07 WITH NORMAL OPERATIONAL CHECKS.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 58,827 hrs · 20,310 cycles

MID CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK IAW AMM 33-51-07 WITH NORMAL OPERATIONS CHECK.

Part: VALVE — FAULTY (LT ENGINE) · airframe 58,709 hrs · 20,262 cycles

DURING CLIMB LT ENGINE BLEED OFF & HOT BURNING ODOR IN COCKPIT & CABIN. DIVERTED. R & R LT ENG HIGH STAGE PILOT VALVE IAW MM 36-11-08. PERFORMED OPERATIONAL & LEAK CHECKS. ACCOMPLISHED SHED HIGH POWER RUN. NOTED NO BURNING SMELLS THROUGHOUT THE CABIN.

Part: SPLICE PLATE — CORRODED (LT HORIZ STAB) · airframe 57,275 hrs · 19,721 cycles

LEFT UPPER OUTER PIVOT SPLICE PLATE HORIZONTAL STABILIZER CORRODED. BLENDED OUT CORROSION. PERFORMED FPI & HFEC SURFACE AREA, FLAPPER PEEN AREA, TREAT & PRIME.

Part: SKIN PANEL — DAMAGED (RT HORIZ STAB) · airframe 57,367 hrs · 19,754 cycles

HAIL DAMAGE TO RT HORIZONTAL STABILIZER INBD PANEL. ACCOMPLISHED REPAIR IAW EA B757-55-036288.

Part: SKIN PANEL — DAMAGED (LT HORIZ STAB) · airframe 57,369 hrs · 19,755 cycles

HAIL DAMAGE TO LT HORIZONTAL STABILIZER INBD TORQUE PANEL. ACCOMPLISHED REPAIR IAW EA B757-55-036288.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 57,275 hrs · 19,721 cycles

AREAS OF CORROSION ON RT KEEL BEAM WEB AROUND HYD BULKHEAD FITTINGS AT STATIONS 1110 & 1117, APPROX 11 INCHES BELOW THE PRESS DECK. ADDITIONAL RELATED AREA ON LT KEEL BEAM WEB AT STATION 1115 APPROXIMATELY 15 INCHES BELOW THE PRESS DECK. REPAIRED CORRODED WEB AREAS IAW EA B757-53-036389.

Part: PLACARD — PEELING (OVERWING EXIT) · airframe 57,241 hrs · 19,706 cycles

17F OVERWING DOOR ARROW PEELED. REPLACED 17F OVERWING DOOR ARROW. OPERATIONS CHECKED NORMAL.

Part: PLACARD — PEELING (R4 DOOR) · airframe 57,241 hrs · 19,706 cycles

RIGHT NR 4 DOOR ARROW PEELED. REPLACED RT NR 4 DOOR ARROW. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,241 hrs · 19,706 cycles

SEAT 18B EMER LIGHT AT OVERWING DOOR INOPERATIVE. REPLACED LAMP FOR SEAT 18B EMER LIGHT AT OVERWING DOOR. OPERATIONS CHECKED NORMAL.

Part: PROBE — OBSTRUCTED (PITOT/STATIC SYS) · airframe 57,070 hrs · 19,644 cycles

AIRSPEED SPLIT FROM PILOT TO CO-PILOT. THE SPLIT WAS FOLLOWED BY AN ELEVATOR ASYMMETRY EICAS MSG. FOUND DEBRIS IN CAPTAINS, FIRST OFFICERS, AUXILIARY ONE & TWO PITOT PROBES. REPLACED PROBES. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: FUEL — CONTAMINATED (FUEL TANK) · airframe 56,523 hrs · 19,445 cycles

RDU INFLIGHT BWI TO MIA. CREW REPORTED FUEL QTY INDICATION, LT & RT FUEL TOTALIZERS FAILED IN FLIGHT. FLIGHT DIVERTED RDU LANDED WITHOUT INCIDENT. PERFORMED OPERATIONAL TEST OF FUEL QTY INDICATION SYS IAW AMM 28-41-00 WITH NO FAULTS NOTED. FOUND WATER IN TANKS, DRAINED WATER. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: BYPASS VALVE — LEAKING (HYDRAULIC SYS) · airframe 55,710 hrs · 19,163 cycles

DFW INFLIGHT LAX-MCO CREW REPORTED TOTAL LOSS OF LT HAND SYS HYD PRESS. EMERGENCY DECLARED FLIGHT DIVERTED DFW LANDED WITHOUT INCIDENT. MAINTENANCE NOTICED HYD FLUID LEAKING FROM LT HAND ENG COWL. REPLACED ELEVATOR BYPASS VLV. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: PLATE — CORRODED (HORIZ STAB) · corrosion level 3 · airframe 52,835 hrs · 18,132 cycles

HORIZONTAL STABILIZER CENTER BOX LOWER LEFT PIVOT PLATE HAS AN AREA OF CORROSION. REMOVED CORROSION PER EA B757-55-028819.

Part: SLAT — PUNCTURED (LT WING) · airframe 49,437 hrs · 16,898 cycles

NUMBER 4 SLAT HAS A .5 INCH PUNCTURE MID SPAN UNDERSIDE OF TRAILING EDGE. INSTALLED HOT BOND DOUBLER REPAIR PER SRM 51-70-10-2.

Part: STRAP — CRACKED (FUSELAGE) · airframe 49,437 hrs · 16,898 cycles

AFT CARGO STRAP CRACKED ABOVE CARGO DOOR AT STATION 1380. INSTALLED DOUBLER TO STRAP PER SRM 53-60-51-4.

Part: DOOR — DENTED (CARGO BAY) · airframe 49,437 hrs · 16,898 cycles

LOWER AFT CORNER OF CARGO DOOR DENT BEYOND LIMITS. ACCOMPLISHED REPAIR PER SRM 52-30-01-2R4 FIGURE 201.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,437 hrs · 16,898 cycles

CORROSION ON FRAME STATION 1480, STRINGER 26 RIGHT. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-00-07-2R.

Part: SKIN — DENTED (FUSELAGE) · airframe 49,437 hrs · 16,898 cycles

DENT AT STATION 1305 STATION 8 LEFT. INSTALLED DOUBLER PER SRM 53-00-01-2R.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,437 hrs · 16,898 cycles

CORROSION ON UPPER FLANGE OF FLOORBEAM STATION 1640 RIGHT BUTTLINES 3 TO 14. REMOVED CORROSION AND INSTALLED PERMANENT REPAIR PER SRM 53-00-51-2.

Part: WEDGE — DAMAGED (LE SLAT) · airframe 49,437 hrs · 16,898 cycles

NUMBER 3 SLAT TRAILING EDGE WEDGE UPPER SURFACE HAS TWO AREAS OF DISBOND APPROXIMATELY MID-SPAN. HOT-BONDED BOTH AREAS OF DISBOND PER SRM 51-70-10.

Part: WEDGE — DAMAGED (LE SLAT) · airframe 49,437 hrs · 16,898 cycles

AREA WORN TO CORE ON BOTTOM OF TRAILING EDGE WEDGE 33.25 INCHES FROM INBOARD SIDE ON AFT EDGE. INSTALLED DOUBLERS AND HOT BONDED AREA PER SRM 51-70-10.

Part: SKIN — CORRODED (LE SLAT) · airframe 49,437 hrs · 16,898 cycles

LEFT WING NUMBER 3 SLAT UPPER SKIN AREA CORRODED AT NOSE RIB INBOARD MAIN TRACK AREA. INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.

Part: STRUCTURE — CRACKED (R2 DOOR) · airframe 49,437 hrs · 16,898 cycles

CRACK IN INNER CHORD ON THE RIGHT NUMBER 2 PASSENGER/SERVICE ENTRY DOOR, AT THE UPPER FRAME. ROUTED AREA TO REMOVE CRACK. FABRICATED AND INSTALLED DOUBLER PER EA COMP-52-019858.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 49,437 hrs · 16,898 cycles

OUTBOARD AFT LEFT FLAP HAS DELAMINATION ON BOTTOM SIDE APPROXIMATELY 12 INCHES FROM OUTBOARD END. BONDED AND SANDED ALL CORES AND SKINS. COMPLETED HOT BOND REPAIR PILES PER SRM 51-70-04-0G.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 49,437 hrs · 16,898 cycles

OUTER SKIN LOWER AFT CORNER IS BENT AND DAMAGED. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED DOUBLER AND FILLER PER AARD.

Part: STRAP — CRACKED (FUSELAGE) · airframe 49,437 hrs · 16,898 cycles

STABILIZER STRAP BETWEEN FRAMES STATION 1380 RIGHT BUTTLINE 45 CRACKED. ACCOMPISHED DOUBLER REPAIR PER AARD 53-60-51-4.

Part: PAN — GOUGED (L1 DOOR) · airframe 49,437 hrs · 16,898 cycles

LEFT NUMBER 1 DOOR OUTER HANDLE PAN IS DEEPLY GOUGED. REPLACED HANDLE PAN PER ESO 90283.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,767 hrs · 15,958 cycles

BULLNOSE EMERGENCY LIGHT ABOVE 12C INOPERATIVE. REPLACED LAMP FOR BULLNOSE LIGHT ABOVE 12C. OPS CHECK NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 46,767 hrs · 15,958 cycles

AFT EMERGENCY LIGHT ON 9D BROKEN. REPLACED LAMP FOR EMERGENCY LIGHT AT 9D. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,767 hrs · 15,958 cycles

RIGHT NUMBER 2 EXTERNAL EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 EXTERNAL SLIDE LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,767 hrs · 15,958 cycles

BULLNOSE EMERGENCY LIGHT ABOVE 20C INOPERATIVE. REPLACED LAMP FOR BULLNOSE LIGHT ABOVE 20C. OPS CHECK NORMAL.

Part: INTERCOSTAL — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 44,894 hrs · 15,280 cycles

FORWARD CARGO DOOR LOWER INTERCOSTAL STATION 570 HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-40-02.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 44,894 hrs · 15,280 cycles

STRINGER 15 LEFT STATIONS 1700 TO 1720 DAMAGED. DOUBLER INSTALLED WITH CHERRY MAX FASTENERS AFT OF LEFT NUMBER 4 DOOR. REPAIRS WERE MADE PER EA B757-53-010082, EA B757-53-010081 AND SRM 53-00-01-2R 3 TO AREA STATIONS 1700 TO 1720 STRINGERS 13 TO 15 LEFT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,894 hrs · 15,280 cycles

CORROSION ON FLOORBOARD SUPPORT AT CL STATION 1651. BLENDED OUT CORROSION AND INSTALLED FLOORBOARD SUPPORT AT STATIONS 1640 TO 1660 BUTTLINE 0 PER SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,894 hrs · 15,280 cycles

FORWARD CARGO DOOR LOWER INTERCOSTAL STATION 580 HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-40-02.

Part: SKIN — CRACKED (LE SLAT) · airframe 44,894 hrs · 15,280 cycles

NUMBER 2 SLAT COVE SKIN CRACK BETWEEN 2 EACH BLIND FASTENERS FORWARD OF THE INBOARD SLAT TRACK. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER PER AARD 57-43-00-4.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,050 hrs · 14,953 cycles

EMERGENCY EXIT SEAT LIGHTS AT SEAT ROWS 9ABC TO 16ABC INOPERATIVE. REPLACED MODULE ASSEMBLY AND BATTERY PACK.

Part: LENS — MISSING (CABIN) · airframe 44,050 hrs · 14,953 cycles

EMERGENCY EXIT LIGHT LENS MISSING AT SEAT 10ABC. REPLACED LENS.

Part: WIRE HARNESS — UNSECURE (EMERGENCY LIGHTS)

DFW - EMERGENCY PATH LIGHTING HARNESS UNDER SEAT 9DE NOT SECURE. SECURED HARNESS FOR EMERGENCY PATH LIGHTING HARNESS UNDER SEAT 9DE.

Part: WIRE HARNESS — UNSECURE (EMERGENCY LIGHTS)

DFW - EMERGENCY PATH LIGHTING HARNESS UNDER SEAT 13D NOT SECURE. SECURED EMERGENCY PATH LIGHTING HARNESS UNDER SEAT 13D.

Part: LIFE VEST — UNSECURE (ZONE 200)

DFW - LIFE VEST BOX UNDER SEAT 11F NOT SECURED. SECURED LIFE VEST BOX UNDER SEAT 11F.

Part: HANDLE — INOPERATIVE (L4 DOOR) · airframe 41,916 hrs · 14,214 cycles

JFK - CREW REPORTED LEFT NUMBER 4 DOOR HANDLE RAISING APPROXIMATELY SIX INCHES IN FLIGHT WITH ASSOCIATED DOOR WARNING MESSAGE IN COCKPIT. RETURNED JFK WITHOUT INCIDENT. REPLACED LEFT NUMBER 1 AND 4 DOOR EXTERIOR HANDLE MECHANISM. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SHROUD — MISSING (CABIN) · airframe 38,572 hrs

DFW - EMERGENCY LIGHT AT SEAT 29D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 29D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — DAMAGED (CABIN) · airframe 38,572 hrs

DFW - EMERGENCY LIGHT AT SEAT 17D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SJU - EMERGENCY LIGHTS FROM SEAT ROWS 16D TO 25D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT ROWS 16D TO 25D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CHECK VALVE — OBSTRUCTED (AIR CONDITIONING)

MIA INFLIGHT T2039/18JUN - DURING CLIMB CABIN ALTITUDE ALERT MESSAGE SOUNDED AND DISPLAYED. CREW MANUALLY DEPLOYED MASKS IN CABIN AND MADE AN EMERGENCY DESCENT. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. FOUND REMOVED BROKEN SECTION OF AIR STRAIGHTENED FROM CHECK VALVE AND REPLACED ALL OXYGEN GENERATORS AND MASKS. REPLACED CABIN ALTITUDE WARNING SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HYDRAULIC LINE — LEAKING (RT MLG)

LAS - DURING CLIMB, LOST LEFT HYDRAULIC SYSTEM. RETURNED TO LAS AND LANDED WITHOUT INCIDENT. MANUALLY LOWERED LANDING GEAR. FOUND RIGHT MAIN LANDING GEAR DOWN LOCK ACTUATOR HYDRAULIC LINE LEAKING. REPLACED HYDRAULIC LINE ASSEMBLY FOR RIGHT MAIN LANDING GEAR DOWN LOCK ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: GCU — INOPERATIVE (NR 1 GENERATOR)

ON APPROACH INDICATION SHOWED OIL PRESSURE FOR NUMBER ONE ENGINE DROPPING. CREW SHUT LEFT ENGINE DOWN AT ABOUT 16 POUNDS PER SQUARE INCH. LANDED TUL WITHOUT INCIDENT. SINGLE ENGINE TIME APPROXIMATELY THREE MINUTES. REPLACED BLEED VALVE CONTROL UNIT AND BOTH DEDICATED GENERATOR CONTROL UNITS FOR LEFT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PSEU — INOPERATIVE (E/E BAY)

BOS INFLIGHT T586/13JAN AT FLIGHT LEVEL 320, AIRCRAFT YAWED HARD TO THE LEFT. EMERGENCY DOOR MESSAGE ON FORWARD EICAS. MULTIPLE DOOR LIGHTS ON OVERHEAD PANEL. LEFT YAW DAMPER EICAS MESSAGE ILLUMINATED AND REMAINED ON. TURNED OFF LEFT YAW DAMPER. DURING DESCENT MORE DOOR AND ELECTRONIC COMPARTMENT LIGHTS CAME ON. AUTOBRAKES DISCONNECTED ON APPROACH. AFTER INITIAL YAW AIRCRAFT FLEW NORMALLY. LANDED BOS WITHOUT INCIDENT. REPLACED PROXIMITY SENSOR ELECTRONIC UNIT. REPLACED RIGHT YAW DAMPER ACTUATOR AND D347 CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SEAL — DAMAGED (LT ENGINE)

MIA - LEFT ENGINE OVERHEAT LIGHT ILLUMINATED DURING CLIMB-OUT. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE HIGH PRESSURE NUMBER TWO AND SIX DUCT SEALS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT)

LAS - EMERGENCY LIGHTS FROM ROW 16 TO 25 AND FOUR EXIT SIGNS AT OVERWING HATCH INOPERATIVE IN TEST MODE. AIRCRAFT FERRIED TO DFW FOR EVALUATION. FOUND LIGHT SOCKET AT FORWARD SEAT 16 SHORTED. REPLACED LIGHT SOCKET AND BATTERY PACK FOR EMERGENCY LIGHTS FROM ROW 16 TO 25 AND FOUR EXIT SIGNS AT OVERWING HATCH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FAN — FAILED (CABIN)

MIA - INFLIGHT T922/04 AT ROW 12 SEAT-F SMOKE APPEARED TO COME FROM FLOOR VENT. ACRID BURNED WIRE ODOR ACCOMPANIED SMOKE. POWER PORT WAS NOT SOURCE OF SMOKE. TURNED OFF UTILITY BUSS AND RECIRCULATION FANS. SMOKE AND ODOR DISSIPATED. LANDED MIA WITHOUT INCIDENT. FOUND RIGHT RECIRCULATION FAN FAILURE. REPLACED RIGHT RECIRCULATION FAN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING ROW 9 THROUGH 15 INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK AND CHARGER AT M10952 UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AT MID GALLEY HAS ONE BULB INOPERATIVE. REPLACED LIGHT STRIP. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING BY RIGHT AFT LAVATORY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP BY RIGHT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FIRE DETECTOR — DEFECTIVE (CARGO COMPT)

DW - FLT 1203 - EN ROUTE SJU/DFW DURING CRUISE, AFT CARGO DETECTION STATUS CAME ON IN-FLIGHT. DISCHARGED BOTH AFT CARGO FIRE BOTTLES. AIRCRAFT LANDED DFW WITHOUT INCIDENT. CHECKED AFT CARGO COMPARTMENT AND CARGO FOR EVIDENCE OF FIRE OR OTHER DAMAGE WITH NO DEFECTS NOTED. REPLACED BOTH FIRE WARNING DETECTORS AND THE TWO FIRE BOTTLES/SQUIBS THAT WERE EXTINGUISHED IN-FLIGHT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — SHORTED (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS FROM ROW 24 AFT FOUND INOPERATIVE. REPAIRED WIRE AT SEAT ROW 24. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: IDG — FAILED (LT ENGINE)

MIA - FLT 931 - ON TAKEOFF LEFT BUS FAILED AND ISOLATED, UNABLE TO RESTORE ANY POWER ON LAC BUS. REPLACED LEFT ENGINE IDG PERFORMED BITE LOAD AND DISCONNECT CHECKS PER MM OPERATION NORMAL LEAKS CHECKS OK. AS PRECAUTIONARY, REF MM 24-51-08-4 P. 403 AND ACCOMPLISH A TEST OF THE INSTRUMENT BUS VOLTAGE SENSING UNIT. REPORT YOUR FINDINGS IN FMR. ACCOMPLISHED TFI, LEFT AND RIGHT INSTRUMENT BUSSES TRANSFER NORMALLY. PERFORMED BITE ON BPCU. NO FAULTS FOUND. (M)

Part: SENSOR — OUT OF ADJUST (LT MLG)

DFW - FLT 2303 - UPON GEAR RETRACTION, THE AMBER GEAR LIGHT REMAINED ON AND RECEIVED AN EICAS GEAR DISAGREE MESSAGE. REMAINED ON FOR ABOUT AN HOUR AND 40 MINUTES THEN EXTINGUISHED. LANDED DFW WITHOUT INCIDENT. ADJUSTED LEFT MLG UPLOCK SENSORS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: ACTUATOR — DEFECTIVE (LT MLG DOOR)

DFW - UPON GEAR RETRACTION, THE AMBER GEAR LIGHT REMAINED ON AND RECIEVED AND EICAS GEAR DISAGREE MESSAGE. RETURNED TO NORMAL AT 235 KNOTS DURING DESCENT. RETURNED AND LANDED DFW WITHOUT INCIDENT BUT OVERWEIGHT. REPLACED LEFT MAIN GEAR DOOR ACTUATOR. ACCOMPLISHED LANDING GEAR RETRACTION. ACCOMPLISHED OVERWEIGHT INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

JFK - DURING OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTS AT MID-SECTION OF MAIN CABIN INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR AT MID-SECTION OF MAIN CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)