N195AN

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHTS) · airframe 55,400 hrs · 17,003 cycles

AIRCRAFT WAS NOT GROUNDED: PATH EMERGENCY LIGHTS AT SEAT 4E DID NOT WORK. MAINTENANCE RESEATED CONNECTION AT SEAT 4E AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.

Part: BATTERY — FAULTY (FWD FLASHLIGHT) · airframe 55,317 hrs · 16,979 cycles

AIRCRAFT WAS NOT GROUNDED: L1 FLIGHT ATTENDANT FLASHLIGHT NEEDED BATTERY REPLACEMENT. MAINTENANCE REPLACED FLASHLIGHT BATTERY PER MM 25-64-00.

Part: BATTERY — FAULTY (FLASHLIGHT) · airframe 55,317 hrs · 16,979 cycles

AIRCRAFT WAS NOT GROUNDED: R3 FLIGHT ATTENDANT FLASHLIGHT NEEDED BATTERY REPLACEMENT. MAINTENANCE REPLACED FLASHLIGHT BATTERY PER MM 25-64-00.

Part: SWITCH — UNRELIABLE (LT ENGINE) · airframe 54,912 hrs · 16,840 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS UPON GATE ARRIVAL, LEFT ENG FUEL CTRL SWITCH DID NOT SHUT DOWN ENGINE. CYCLED TWICE. ENGINE SHUTDOWN WITH T-HANDLE. MAINTENACNE ACCOMPLISHED SYS OPS CHECK IAW AMM 71-00-00, FOUND L/H ENGINE HOUSING ASSEMBLY PRESSURE VALVE SWITCH NEEDS TO BE REPLACED. REMOVED AND REPLACED L/H ENGINE HOUSING ASSEMBLY PRESS VALVE SWITCH IAW AMM 73-21-21-15-40, L/H ENGINE OPS CHECK NORMAL AND SHUT DOWN NORMAL, OK FOR SVC.

Part: CONNECTOR — DIRTY (FUEL CONTROL) · airframe 54,894 hrs · 16,832 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS LEFT ENGINE SLOW TO SHUTDOWN, WHEN FUEL CONTROL SWITCH MOVED TO CUTOFF, APPROX.15 SECONDS. RECYCLED SWITCH ONCE. MAINTENANCE REMOVED AND CLEANED CONNECTOR ON MEC. REINSTALLED CONNECTOR AND OPERATED ENGINE. ENGINE SHUTSDOWN NORMALLY.

Part: MONITOR — UNRELIABLE (VIBRATION) · airframe 54,468 hrs · 16,704 cycles

AIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY ON ACCOUNT OF RT ENGINE VIBRATION INTERMITTENT OVER 5 UNITS, ACCOMPLISHED ENGINE VIBRATION CHECKLIST RETURNED TO HNL. MAINTENANCE REMOVED AND REPLACED #2 ENG AVM ACCELEROMETER IAW AMM 77-31-01-404-020-R00. REMOVED & REPLACED #2 ENG AVM MONITOR IAW AMM 77-31-00-404-005-R00. OPS CHECKS GOOD. (SEE SDR # AALA201908099019)

Part: ACCELEROMETER — UNRELIABLE (RIGHT ENGINE) · airframe 54,468 hrs · 16,704 cycles

AIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY ON ACCOUNT OF RT ENGINE VIBRATION INTERMITTENT OVER 5 UNITS, ACCOMPLISHED ENGINE VIRBRATION CHECKLIST RETURNED TO HNL. MAINTENANCE CURRENTLY WORKING THIS EVENT. MAINTENANCE REMOVED AND REPLACED #2 ENG AVM ACCELEROMETER IAW AMM 77-31-01-404-020-R00. REMOVED & REPLACED #2 ENG AVM MONITOR IAW AMM 77-31-00-404-005-R00. OPS CHECKS GOOD.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 54,173 hrs · 16,628 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS AT 3500 FEET MSL ON DECENT, CABIN DUMPED ALL PRESSURIZATION IN AUTO 1. PRESS DIFF ZERO. NO FAULTS OR EICAS MESSAGES DISPLAYED. MAINTENANCE ACCOMPLISHED FIM TASK 21-30-00-815-802. REMOVED AND REPLACED #1 CONTROLLER IAW AMM 21-31-02. OPS TEST GOOD.

Part: COMPUTER — FAULTY (ZONE 100) · airframe 53,822 hrs · 16,535 cycles

AIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY ON ACCOUNT OF MULTIPLE STATUS MESSAGES AFTER TAKE OFF. "AFT CARGO SMOKE DET1" / "EQUIP CLG TEST" / "LT ENGINE EGT" INDICATION RED 696 DEG. MAINTENANCE TROUBLESHOT AND FOUND FAULTY L EICAS COMPUTER. REPLACED IAW AMM 31-41-02 AND HAS CORRECT SOFTWARE CHECKED NORMAL. ALL MESSGES CLEARED.

Part: SEAL — LEAKING (NR 1 BEARING) · airframe 53,094 hrs · 16,322 cycles

THE PILOT REPORTED THAT AFTER TAKEOFF, THE RIGHT ENGINE OIL PRESSURE WAS 33 IN THE YELLOW BAND, ACCOMPANIED BY FUMES IN THE COCKPIT & CABIN. THE AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND OIL COMING DOWN THE OUTLET GUIDE VANES, AND DETERMINDED THAT THE NR 1 BEARING SEAL WAS LEAKING. CHANGED THE ENGINE. ***SUPPLEMANTAL REPORT: MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE IAW 71-94-01, AND DUE TO INITIAL DISCREPANCY ACCOMPLISHED ENGINE SMOKE ODOR FUMES INITIAL TS IAW CARDS 05-96-70 AND 05-96-71. ACCOMPLISHED ENGINE RUN, OPS OK***(CLOSED)

Part: CLAMP — BROKEN (ANTI-ICE DUCT) · airframe 52,611 hrs · 16,170 cycles

WING ANTI-ICE INDICATION DISPLAYED. DUE TO WEATHER, FLIGHT DIVERTED. THE AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND A BROKEN V-BAND CLAMP AT THE ANTI-ICE DUCT. REPLACED THE CLAMP. MAINTENANCE ALSO PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: SKIN — CRACKED (LT WING) · airframe 52,608 hrs · 16,169 cycles

DURING ACCOMPLISHMENT OF ECO F2326AA-001, AND HFEC ROTARY HOLE PROBE INSPECTION, ON THE LEFT WING DIAGONAL BRACE, FASTENER HOLE NR 9, FOUND A CRACK INDICATION IN THE SKIN LAYER ONLY AT THE AFT INBOARD SIDE OF HOLE. REPAIRED IAW EA 287209.

Part: FLOOR SUPPORT — CRACKED (BS 1580-1600) · airframe 52,608 hrs · 16,169 cycles

CRACKED FLOOR SUPPORT REPAIR ANGLE, FROM BS 1580 TO 1600, LBL 0. REPLACED THE FLOOR SUPPORT REPAIR ANGLE IAW RD 51-40-03-03, AND DRAWING 145N5180.

Part: ANGLE — CRACKED (BS 1200-1220) · airframe 52,607 hrs · 16,169 cycles

CRACK IN THE ANGLE AT BS 1200 - 1220. REPLACED THE ANGLE.

Part: ANGLE — CRACKED (BS 1320-1340) · airframe 52,608 hrs · 16,169 cycles

CRACKED ANGLE LOCATED AT BS 1320 - 1340. REPLACED THE ANGLE.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 51,384 hrs · 15,847 cycles

FLOOR EMERGENCY EXIT LIGHT COVER IN FORWARD GALLEY DETACHED. REPLACED THE LIGHT ASSEMBLY, CHECKED GOOD IAW AMM 33-51-02.

Part: SEAL — DAMAGED (SLIDING WINDOW) · airframe 51,240 hrs · 15,806 cycles

FIRST OFFICIERS SLIDING WINDOW WILL NOT CLOSE. REPLACED THE WINDOW SEAL IAW AMM 56-11-53.

Part: WINDOW — DELAMINATED (L3) · airframe 51,108 hrs · 15,770 cycles

COCKPIT WINDOW L3 IS DELAMINATED AT THE AFT CORNER. REPLACED THE L3 WINDOW IAW AMM 56-11-10. OPS CHECKED OK.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 50,453 hrs · 15,598 cycles

EMERGENCY EXIT LIGHT AT L1 DOOR MISSING COVER. MAINTENANCE INSTALLED NEW COVER AT EXIT LIGHT PER AMM 33-51-01 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — DAMAGED (AFT GALLEY) · airframe 50,376 hrs · 15,573 cycles

AFT GALLEY LEFT SIDE EMERGENCY LIGHT FOUND BROKEN AND THE LENS MISSING, LIGHT IS NOT WORKING. REMOVED & REPLACED LIGHT ASSY IAW AMM 33-51-01. OPS CHECKED NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 50,376 hrs · 15,573 cycles

AFT GALLEY LEFT SIDE EMERGENCY LIGHT BROKEN AND LENS MISSING. REPLACED THE LIGHT ASSY IAW AMM 33-51-01.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 50,118 hrs · 15,488 cycles

ROW 35DEF ENERGENCY LIGHT ON SEAT 35D INOPERATIVE. SECURED THE CONNECTOR. THE LIGHT CHECKED NORMAL IAW AMM 35-51-11.

Part: COVER — DAMAGED (L3 DOOR) · airframe 49,818 hrs · 15,405 cycles

AIRCRAFT WAS NOT GROUNDED. L3 EXIT DOOR SLIDE COVER HAS DAMAGED AREA 2X2 AT FORWARD UPPER CORNER OF COVER. REPAIRED DAMAGED AREA PER SRM 51-70-17.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 49,697 hrs · 15,368 cycles

EXIT SIGN DETACHED AT THE L4 DOOR. SECURED THE SIGN.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 49,678 hrs · 15,363 cycles

SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT 26DEF TO 36DEF ARE VERY DIM. REPLACED THE BATTERY IAW AMM 33-51-07.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 48,891 hrs · 15,168 cycles

AIRCRAFT WAS NOT GROUNDED. ROW 35 AISLE SEAT EMERGENCY LIGHT INOPERATIVE. RESEATED AND SECURED LOOSE CONNECTOR UNDERNEATH SEATS 35DEF PER AMM 33-51-00. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: WINDOW — DELAMINATED (ZONE 200) · airframe 48,726 hrs · 15,124 cycles

AIRCRAFT WAS GROUNDED. INSPECTED AND FOUND R2 WINDOW DELAMINATED WITH A LOT OF SCRATCHES ON THE INSIDE AND OUTSIDE OF THE WINDOW. REMOVED AND REPLACED R2 WINDOW AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK IAW AMM 56-11-02.

Part: PUMP — WEAK (RT WING) · airframe 48,724 hrs · 15,123 cycles

AIRCRAFT WAS NOT GROUNDED. A FUEL IMBALANCE OF ABOUT 1700 LBS NOTED AFTER 7 HOURS FLIGHT. BALANCING WORKED SATISFACTORY. IMBALANCE TOOK PLACE WITH FUEL IN CENTER TANK. ACCOMPLISHED AARD 28-00-00-01 RAN BOOST PUMPS AND FOUND RIGHT FORWARD BOOST PUMP RUNNING WEAK. REMOVED AND REPLACED RIGHT FORWARD FUEL BOOST PUMP PER AMM 28-22-03. OPS AND LEAK CHECKED GOOD.

Part: COFFEEMAKER — FAILED (AFT GALLEY) · airframe 48,617 hrs · 15,094 cycles

AFT GALLEY NR 2 COFFEEMAKER IS SPARKING AND EMITTING A BURNED WIRE ODOR. REMOVED AND REPLACED THE COFFEEMAKER IAW AMM 25-32-00. OPERATIONAL CHECKED GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 48,609 hrs · 15,091 cycles

EMERGENCY EXIT LIGHT AT SEAT 4DEF IS INOPERATIVE. SECURED EMERGENCY LIGHT SIDEWALL CONNECTOR. OPERATIONAL CHECKED GOOD IAW AMM 33-51-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,543 hrs · 15,076 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHTS FROM RIGHT SIDE ROW 26 TO AFT GALLEY ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER AMM 33-51-07-902-001. OPERATIONAL CHECK GOOD.

Part: GIRT BAR — DIRTY (L4 DOOR) · airframe 48,173 hrs · 14,981 cycles

AIRCRAFT WAS NOT GROUNDED. L4 EMERGENCY EVACUATION DOOR IS DIFFICULT TO ARM. CLEANED DEBRIS FROM GIRT BAR AND FLOOR. OPERATIONAL CHECK IAW AMM 52-11-00 GOOD.

Part: COVER — DAMAGED (L4 DOOR SLIDE) · airframe 48,049 hrs · 14,955 cycles

L4 DOOR EMERGENCY EVACUATION SLIDE COVER IS DAMAGED. REMOVED AND REPLACED THE COVER ASSEMBLY IAW AMM 25-66-01. OPS CHECKED GOOD.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 47,378 hrs · 14,757 cycles

AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLES (2 EACH) IN FLOORBEAM UPPER CHORD AT STATION 395 AND LBL 45. REPAIRED FLOORBEAM PER SRM 53-00-51-2R-1 AND EA 267291.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 47,378 hrs · 14,757 cycles

AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLES (2 EACH) IN FLOORBEAM UPPER CHORD AT STATION 418 AND LBL 45. REPAIRED FLOORBEAM PER SRM 53-00-51-2R-1 AND EA 267290.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 47,134 hrs · 14,691 cycles

AIRCRAFT WAS GROUNDED. FIRST OFFICER WINDSHIELD SHATTERED. REMOVED AND REPLACED WINDSHIELD IAW AMM 56-11-01. OPERATIONAL CHECK GOOD.

Part: LIGHT — LOOSE (EXTERIOR) · airframe 47,071 hrs · 14,678 cycles

AIRCRAFT NOT GROUNDED. EXTERIOR EMERGENCY LIGHT AT R1 DOOR IS INOPERATIVE. RESECURED BULB IN LIGHT ASSEMBLY IAW AMM 33-51-00. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,072 hrs · 14,678 cycles

AIRCRAFT NOT GROUNDED. SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 9 THRU 15 ARE VERY DIM. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-07. OPERATIONAL CHECK GOOD.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 46,767 hrs · 14,591 cycles

AIRCRAFT NOT GROUNDED. R1 DOOR EVACUATION SLIDE LIGHT INTERMITTENT. REMOVED DEBRIS FROM GIRT BAR SLIDE IAW AMM 25-66-00. OPERATIONAL CHECK GOOD.

Part: CHARGER — FAILED (EMERGENCY LGHTS) · airframe 46,642 hrs · 14,559 cycles

OVERHEAD EMERGENCY LIGHT AT SEATS 22DEF INOPERATIVE. OPEN WIRE FROM POWER SUPPLY CONNECTOR TO QUICK DISCONNECT CONNECTOR TO INOPERATIVE EMERGENCY LIGHT. REFERENCE WDM 33-51-14. AIRCRAFT GROUNDED. REMOVED AND REPLACED CHARGER ASSEMBLY M735 IAW AMM 33-51-07. OPS CHECKED GOOD.

Part: ENGINE — LEAKING (NR 1) · airframe 45,020 hrs · 14,128 cycles

AIRCRAFT WAS GNDED. FLIGHT CREW REPORTED AN OILY SMELL IN COCKPIT MOST OF FLIGHT THAT SEEMED WORSE ON THE GND. ISOLATED ODOR SOURCE TO BE NR 1 ENG. R & R NR 1 ENG.

Part: LIGHT — BROKEN (CABIN) · airframe 44,703 hrs · 14,045 cycles

AIRCRAFT WAS NOT GNDED. LENS COVER FOR EMER EXIT SIGN AT R1 DOOR WILL NOT STAY ON, BASE IS BROKEN. R & R BASE ASSEMBLY OF R1 EXIT SIGN FWD OF DOOR IAW 33-51-10. SYS CHECKED NORMAL.

Part: ENGINE — POWER LOSS (LEFT) · airframe 44,693 hrs · 14,043 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER NOT DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE, LT ENG THROTTLE 2 FULL KNOBS AHEAD OF RT ENG TO GET BALANCED POWER. THROTTLE SPLIT INCREASES WITH INCREASE IN ALTITUDE. R & R LT ENG.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 43,587 hrs · 13,799 cycles

R4 DOOR EMER ESCAPE SLIDE LIGHT ON THE EXTERIOR OF THE ACFT INOPERATIVE. FOUND POWER SUPPLY M736 BAD. REPLACED POWER SUPPLY M736 IAW AMM 33-51-07. OPERATIONAL CHECKED GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 42,908 hrs · 13,637 cycles

18DEF WALL MOUNTED EMER LIGHT ASSEMBLY DAMAGED. REPLACED LIGHT ASSEMBLY IAW MM 33-51-00. OPERATIONAL CHECKED OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 42,648 hrs · 13,583 cycles

EMERGENCY LIGHT BATTERY AT SEATS 25 DEF - 26 DEF INOPERATIVE. R & R CHARGER & BATTERY AT 25 DEF IAW AMM 33-51-07. SYS CHECKED NORMAL. SEE ALSO AALA20150813006.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 42,648 hrs · 13,583 cycles

EMERGENCY LIGHT BATTERY AT SEATS 25DEF - 26DEF INOPERATIVE. R & R CHARGER & BATTERY AT 25 DEF IAW AMM 33-51-07. SYS CHECKED NORMAL. SEE ALSO AALA20150813008.

Part: BALLAST — FAULTY (CABIN) · airframe 42,256 hrs · 13,494 cycles

LIGHT ABOVE LT FWD EMER LIGHT INOPERATIVE. R & R BALLAST IAW WDM 33-51-13. PERFORMED OPERATIONAL CHECK AMM 33-50-00. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 39,538 hrs · 12,842 cycles

RIGHT OVERWING AFT EMER LIGHT INOPERATIVE. REPLACED LAMP FOR EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 39,538 hrs · 12,842 cycles

RIGHT NR 4 DOOR EXTERIOR EMER LIGHT INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: SIGN — INOPERATIVE (CABIN) · airframe 39,168 hrs · 12,759 cycles

OVERWING EMER EXIT SIGN AT SEAT 17A INOPERATIVE. REPLACED OVERWING EMER LIGHT FIXTURE AT SEAT 17A. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,715 hrs · 12,648 cycles

FLOOR LEVEL EMERGENCY EXIT LIGHT AT FIRST CLASS GALLEY INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR FLOOR LEVEL EMERGENCY EXIT LIGHT AT FIRST CLASS GALLEY. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 38,368 hrs · 12,576 cycles

RIGHT FWD OVER THE WING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RT FWD OVER THE WING SLIDE LIGHT, OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,368 hrs · 12,576 cycles

RIGHT OVERWING EMERGENCY INTERIOR DOOR LIGHT INOPERATIVE. REPLACED M10568 BATTERY PACK & M10614 LIGHT ASSEMBLY, OPERATIONS CHECKED NORMAL.

Part: TAT PROBE — INOPERATIVE (ZONE 200) · airframe 37,126 hrs · 12,260 cycles

JFK CREW REPORTED "TAT PROBE" EICAS MESSAGE FOLLOWED BY "EEC L FAIL" & "EEC R FAIL" EICAS MESSAGE. EMERGENCY DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED TOTAL AIR TEMPERATURE PROBE. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,454 hrs · 11,615 cycles

RIGHT NUMBER 1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 1 DOOR EMERGENCY EXIT LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,454 hrs · 11,615 cycles

RIGHT NUMBER 4 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 4 DOOR EMERGENCY EXIT LIGHT. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 34,454 hrs · 11,615 cycles

ESCAPE PATH LIGHTS IN FIRST CLASS RIGHT SIDE INOPERATIVE. REPLACED BATTERY PACK M10952. OPS CHECK NORMAL.

Part: SKIN PANEL — DAMAGED (TE FLAP) · airframe 34,186 hrs · 11,536 cycles

LEFT WING INBOARD MAIN FLAP, UPPER SKIN PANEL 113N2401 IS MISDRILLED IN 2 LOCATIONS, MF STATIONS 145.5 AND 209. INSTALLED FREEZE PLUGS PER REO-G15813 REVISION A. INSTALLED FASTENERS THROUGH FREEZE PLUGS AND COMPLETED REPAIR PER EA B757-57-027773.

Part: GATE — CORRODED (L4 DOOR) · corrosion level 2 · airframe 34,186 hrs · 11,536 cycles

LEFT NUMBER 4 DOOR LOWER GATE EXTERIOR CORRODED BOTH SIDES OF RUB STRIP. REPAIRED CORRODED LOWER GATE PER EA B757-52-027758.

Part: FRAME — DENTED (FUSELAGE) · airframe 34,186 hrs · 11,536 cycles

AFT CARGO COMPARTMENT, STATION 1400 AT STRINGER 25 LEFT, FUSELAGE FRAME IS DENTED. INSTALLED REPAIR ANGLE AND STRINGER CLIP PER SRM 53-00-072R5, FIGURE 201 DETAIL III.

Part: STOP FITTING — GOUGED (L1 DOOR) · airframe 34,186 hrs · 11,536 cycles

LEFT NUMBER 1 DOOR UPPER FORWARD STOP FITTING GOUGED. INSTALLED NEW FITTING PER BAC DRAWING 141N8341 AND AARD 51-00-05-1.

Part: FRAME — DENTED (FUSELAGE) · airframe 34,186 hrs · 11,536 cycles

AFT CARGO COMPARTMENT, STATION 1500, STRINGERS 25 TO 26 LEFT, FUSELAGE FRAME IS DENTED IN TWO LOCATIONS (DOTS F112 AND F113). INSTALLED REPAIR ANGLE PER SRM 53-00-07-2R5.

Part: STOP FITTING — WORN (FUSELAGE) · airframe 34,186 hrs · 11,536 cycles

LEFT NUMBER 1 UPPER FORWARD DOOR STOP FITTING WORN. REMOVED AND REPLACED FITTING PER AARD 51-00-05 FIGURE 1.

Part: SHEAR TIE — GOUGED (FUSELAGE) · airframe 34,186 hrs · 11,536 cycles

SHEAR TIE GOUGED IN THE AFT CARGO STATION 1540, STRINGER 25 RIGHT. REPAIRED SHEAR TIE PER SRM 53-00-03-2R FIGURE 201.

Part: FRAME — DENTED (FUSELAGE) · airframe 34,186 hrs · 11,536 cycles

AFT CARGO, STATION 1540 STRINGER 25 RIGHT FRAME DENTED. INSTALLED NESTED ANGLE REPAIR PER SRM 53-00-07-2R.

Part: FRAME — DENTED (FUSELAGE) · airframe 34,186 hrs · 11,536 cycles

FRAME DENTED AT SATTION 1440, STRINGER 26 LEFT. INSTALLED NESTED ANGLE REPAIR PER SRM 53-00-07-2R 5 FIG 201 DETAIL I.

Part: FRAME — DENTED (FUSELAGE) · airframe 34,186 hrs · 11,536 cycles

AFT CARGO, FRAME STATION 1480 DENTED FROM STRINGERS 25 TO 27 LEFT. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-07-2R.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,982 hrs · 11,483 cycles

EMERGENCY EXIT LIGHT ABOVE 16B ON OVERHEAD BIN INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT LIGHT ABOVE 16B. OPS CHECK NORMAL.

Part: GENERATOR — INOPERATIVE (LT ENGINE) · airframe 31,997 hrs · 11,073 cycles

MIA - CREW REPORTED LEFT ENGINE N1 / N2 / EGT EXCEEDENCE ALERTS ON EICAS. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED DEDICATED GENERATOR AND BOTH DEDICATED GENERATOR CONTROL UNITS FOR LEFT ENGINE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,596 hrs · 10,928 cycles

DECK PLATE STATION 1680 TO 1720 CORRODED. REPLACED AFT DECK PER AARD 51-10-05-1.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 30,756 hrs · 10,620 cycles

LEFT NUMBER 1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 1 DOOR EMERGENCY LIGHT. OP CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,558 hrs · 9,819 cycles

SEAT 18DEF SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 18DEF SEAT MOUNTED EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,558 hrs · 9,819 cycles

SEAT MOUNTED EMERGENCY LIGHTS AT 36DEF INOPERATIVE. REPLACED LAMP AND REPINNED CONNECTOR FOR SEAT MOUNTED EMERGENCY LIGHTS AT 36DEF. OPS CHECK NORMAL.

Part: SKIN — DENTED (LE SLAT) · airframe 25,561 hrs · 8,711 cycles

LEFT WING NUMBER 1 SLAT INBOARD UPPER SURFACE DENTED AND DELAMINATED. REWORKED DENT USING EDR PER SRM 57-70-01-2R1. DENT IS WITHIN LIMITS PER SRM 57-43-02-1A1. TAP TESTED AND NO DELAMINATION FOUND. DYE CHECKED AREA, NO CRACKS FOUND.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,843 hrs · 8,432 cycles

EMERGENCY LIGHTS AT SEAT ROWS 9D TO 15D INOPERATIVE. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 23,822 hrs · 8,093 cycles

CABIN CLEANERS USED EMERGENCY LIGHTS AS LIGHT SOURCE TO CLEAN AIRCRAFT. EMERGENCY LIGHT BATTERIESS DRAINED. REPLACED ALL EMERGENCY LIGHT BATTERY PACKS. OPS CKD OK.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT FOR SLIDE AT LEFT NUMBER 3 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT FOR SLIDE AT LEFT NUMBER 3 DOOR.

Part: LENS — MISSING (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 23D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23D.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - BULL NOSE LIGHT AT SEAT 5D INOPERATIVE. REPLACED LAMP FOR BULL NOSE LIGHT AT SEAT 5D.

Part: GUARD — BROKEN (CABIN)

DFW - SEATS 16 AND 17 EMERGENCY LIGHT GUARDS BROKEN. REPLACED GUARDS FOR SEATS 16 AND 17 EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

LEFT NR 1 AND NR 3 DOOR EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED LAMPS FOR LT NR 1 AND NR 3 DOOR EMERGENCY SLIDE LIGHT.

Part: IGNITION UNIT — INOPERATIVE (APU) · airframe 22,845 hrs

IND - LEFT ENGINE DRIVE LIGHT ILLUMINATED AND APU AUTO SHUTDOWN. LANDED IND WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. SERVICED LEFT ENGINE GENERATOR. REPLACED IGNITION UNIT.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 21,769 hrs

DFW - EMERGENCY LIGHT AT SEAT ROW 18DEF MISSING LENS. REPLACED LENS AT SEAT ROW 18DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 21,693 hrs

LAX - EMERGENCY LIGHTS AT CENTER CABIN INOPERATIVE. REPLACED BATTERY PACK AT CENTER CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHT) · airframe 19,260 hrs

DFW - EMERGENCY LIGHT AT SEAT 19D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 19D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (STAB ASYMMETRY) · airframe 18,934 hrs

BOS INFLIGHT T1501/05JAN - RETURNED TO BOS DUE TO STABILIZER TRIM MOVEMENT. LANDED WITHOUT INCIDENT. REPLACED THE STABILIZER ASYMMETRY MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HEATER — OVERHEATED (WING DE ICING)

AIRCRAFT AIR INTERRUPTED INTO BNA DUE TO HOT SPOT AND DISCOLORIZATION OF SIDEWALL PANEL AT SEAT 17A. FOUND OVERWING DE-ICING HEATER OVERHEATING. PULLED AND COLLARED CIRCUIT BREAKER AND PLACARDED SYSTEM. AIRCRAFT DEPARTED TO BWI. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ODOR — DETECTED (COCKPIT)

STRONG BURNING SMELL PLUS LIGHT SMOKE ON FINAL AT 4000 FEET. NOTICED STRONG SMELL ON TAKEOFF FROM LGA. NO OTHER INDICATIONS. DISSIPATED ON LANDING. NOTHING IN CABIN REPORTED BY FLIGHT ATTENDANT. ACCOMPLISHED FAULT ISOLATION PROCEDURES 21 00 01. NO SMOKE OR BURNING SMELL NOTICED. PERFORMED EXTENSIVE INSPECTION IN COCKPIT AND AIRCRAFT BAY AREA. UNABLE TO LOCATE ANY EVIDENCE OF SMOKE. INSPECTED ELECTRONIC EQUIPMENT AREA WITH NO DISCREPANCIES NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FSEU — LOOSE (E/E BAY)

MIA T921/17 EN ROUTE MCO-MIA TRAILING EDGE FLAPS DISAGREE LIGHT ON ENGINE INDICATING AND CREW ALERT SYSTEM. LANDED MIA WITHOUT INCIDENT WITH FLAPS AT 20 ABNORMAL CONFIGURATION. RESEATED NUMBER ONE FLAP/SLAT ELECTRICAL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 10D. REPLACED SEAT MOUNT EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 3EF INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 3EF INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

DFW - EMERGENCY PATH LIGHT ON SEAT 24D INOPERATIVE. REPLACED BROKEN WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)