N752AT

Part: DOOR FRAME — CONTAMINATED (R3 DOOR) · airframe 95,753 hrs · 39,678 cycles

R3 DOOR HAS TROUBLE ARMING, TWO CONSECUTIVE FLIGHTS CAUSING DELAYS. CLEANED AND LUBED DOOR, FOUND DEBRI IN DOOR FRAME, DOOR OPS NORMAL IAW AMM 52-11.

Part: SKIN — DENTED (BS 215) · airframe 95,470 hrs · 39,601 cycles

ON WALK AROUND FOUND DENT ON RK FWD FUSELAGE. BS 215. 7 O'CLOCK POSITION. 15" AFT OF RADOME BULKHEAD. REF ERA 539404-14, REV ORIG FOR REPAIR.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 93,891 hrs · 39,230 cycles

IN-SEAT ESCAPE PATH LIGHT AT ROW 27R INOPERATIVE. FOUND CONNECTOR DISCONNECTED AT 27F. RECONNECTED, OPS OK.

Part: WIRE HARNESS — DISCONNECTED (EMERGENCY LIGHTS) · airframe 93,189 hrs · 39,050 cycles

23D IN SEAT EMERGENCY LIGHT INOPERATIVE. FOUND HARNESS DISCONNECTED UNDER SEAT. RECONNECTED HARNESS, OPS OK.

Part: SKIN — CORRODED (BS 1680-1700) · corrosion level 2 · airframe 91,068 hrs · 38,497 cycles

DURING A SERVICE CHECK, CORROSION WAS FOUND ON SKIN BS 1680-1700 STRINGERS 26-29R UNDER THE LAV SERVICE PAN, REPAIRED IAW ER/A 519950-14AD, REV A.

Part: SKIN — DAMAGED (BS 1621) · corrosion level 2 · airframe 91,068 hrs · 38,497 cycles

FUSELAGE SKIN DAMAGED BS 1621, S26R. REPAIRED IAW ER/A 519947-14AD, REV A.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 90,434 hrs · 38,347 cycles

ON SERVICE CHECK FOUND ROW 20DEF EMERGENCY LIGHT INOPERATIVE. FOUND ELECTRIC CONNECTOR DISCONNECTED, RECONNECTED AND OPS CHECKED GOOD.

Part: SHUTTLE VALVE — FAILED (RT MLG) · airframe 90,427 hrs · 38,345 cycles

AFTER TAKEOFF AT ROTATION, SEVERAL UPPER EICAS AMBER ANNUCIATORS ILLUMINATED BRIELY AND THEN WENT OUT WHEN THE GEAR HANDLE WAS RAISED IT WOULD NOT GO PAST OFF POSITION INTIALLY, BUT THEN WENT UP AND GEAR RETRACTED NORMALLY. FOUND RT GEAR TRUCK POSITIONER SHUTTLE VALVE SEIZED NOT ALLOWING THE TRUCK TILT ACTUATOR. R & R RT GEAR TRUCK SHUTTLE VLAVE AND TRUCK ACTUATOR IAW AMM 32-32 PERFORMED GEAR SWINGS COUPLE TIMES NO FAULTS NOTED. OPS AND LEAK CHECK GOOD SHUTTLE VALVE.

Part: STRUT — LOW PRESSURE (NLG) · airframe 90,427 hrs · 38,345 cycles

CAPTAIN COULD NOT GET THE GEAR HANDLE TO COME TO FULL UP POSITION, WITH GEAR AMBE LIGHTS ON, ACFT DIVERTED. PERFORMED QRH PROCEDURES, OVERRIDE BUTTON WAS UNSUCCESSFUL, LOWERED GEAR HANDLE AND GOT 3 GREEN LIGHTS. ON ARRIVAL PERFORMED PSEU BITE WITH "NOSE GEAR NOT COMPRESSED TARGET" MSG. FOUND NLG TARGETS COVERED IN GREASE, CLEANED TARGETS. FOUND NLG STRUT NEEDING SERVICE, SERVICED STRUT IAW AMM 12-15. SUBSQUENTLY THE RT MLG TRUCK TILT ACTUATOR WAS REPLACED AFTER A SIMILAR LOG WRITE UP ON THE FOLLOWING FLIGHT LEG.

Part: LIGHT — INOPERATIVE (SEAT 20F) · airframe 90,266 hrs · 38,302 cycles

SEAT 20F, INSEAT EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-51. OPS CHECKED GOOD.

Part: SKIN — DENTED (BS 1382) · airframe 89,124 hrs · 38,002 cycles

FUSELAGE SKIN DENTED AT BS 1382 BELOW STRINGER 19L. COMPLIED WITH ERA 526120-14, REV ORIGINAL.

Part: SKIN — DAMAGED (BS 1380) · airframe 89,129 hrs · 38,004 cycles

FUSELAGE SKIN STR 18L DAMAGED AT BS 1380, C/W ERA 526120-14, REV ORIG.

Part: SKIN — DENTED (FUSELAGE) · airframe 89,129 hrs · 38,004 cycles

DENT AND TOOL DAMAGE FOUND ON SKIN.

Part: KEELBEAM — CORRODED (RT MLG WW) · corrosion level 2 · airframe 89,124 hrs · 38,002 cycles

CORROSION ON KEEL BEAM RT WHEEL WELL JUST AFT OF A/C LEVELING PLACARD. REPAIRED IAW ERA 525717-14 REV O

Part: SKIN — CORRODED (BS 440) · corrosion level 2 · airframe 89,124 hrs · 38,002 cycles

SKIN FOUND CORRODED BS 440 STRINGER 24L. REPAIRED IAW ERA 525750-14 REV O

Part: SKIN — CORRODED (BS 440) · corrosion level 2 · airframe 89,124 hrs · 38,002 cycles

FOUND CORROSION ON THE BUTT SPLICE PLATE AT APPROX BS 440, STRINGER 24L. REPAIRED IAW ER/A 525750-14 SECTION II.

Part: SEALANT — LOOSE (SKIN) · corrosion level 2 · airframe 89,124 hrs · 38,002 cycles

SEALANT BLOWN OUT AND POWDER FALLING OUT FROM BETWEEN SKINS 13L AND 14L. REMOVED LOOSE SEALANT AND CLEANED AREA IAW ERA 525753-14

Part: SKIN — DAMAGED (BS 1705) · airframe 89,036 hrs · 37,974 cycles

FASTENER AT BS 1705 AND S8L BURNED. R & R BLIND FASTENER IAW SRM 53-00-01, SECTION 2, PARA 4.

Part: SKIN — DAMAGED (BS 1337) · airframe 89,036 hrs · 37,974 cycles

ACFT SKIN AT BS 1337, TWO INCHES DOWN FROM STRINGER 6L, LIGHTNING STRIKE DAMAGE DRILLED OUT DAMAGE INSPECTED WITH 10X. TREATED, PAINTED INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.

Part: SKIN — DAMAGED (BS 1051) · airframe 95,729 hrs · 39,671 cycles

FASTENER AT BS 1051 AND S6L HAD A LIGHTNING STRIKE.

Part: SKIN — DAMAGED (BS 952) · airframe 89,036 hrs · 37,974 cycles

FASTENER AT BS 952 S6L, LIGHTNING DAMAGE. REMOVED FASTENER, CLEANED AREA, INSPECTED WITH 10X. DAMAGE REMOVED, TREATED & PAINTED. INSTALLED BLIND FASTENER IAW SRM 53-00-01, FIG 201.

Part: SKIN — DAMAGED (BS 886) · airframe 89,036 hrs · 37,974 cycles

FASTENER AT BS 886 AND S56L IS BURNED. REMOVED FASTENER, CLEANED AREA, INSPECTED, WITH 10X DAMAGE REMOVED, TREATED & PAINTED, INSTALLED BLIND FASTENER IAW SRM 53-00-01, FIG 201.

Part: SKIN — DAMAGED (BS 500) · airframe 89,036 hrs · 37,974 cycles

FASTENER AT BS 500 S11L BURNED. R & R WITH BLIND FASTENER IAW SRM 53-00-01, SECTION 2, PARA 4.

Part: SKIN — DAMAGED (BS 977) · airframe 89,108 hrs · 37,997 cycles

FASTENER AT BS 977, S6L LIGHTNING BURNED. REMOVED FASTENER CLEANED AREA INSPECTED WITH 10X MAGNIFICATION. REMOVED, TREATED, PAINTED AND INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.

Part: SKIN — DAMAGED (BS 1086) · airframe 89,036 hrs · 37,974 cycles

ACFT SKIN AT BS 1086, SIX INCHES DOWN FROM STRINGER 6L HAS LIGHTNING STRIKE DAMAGE. DRILLED OUT DAMAGE INSPECTED WITH 10X. TREATED PAINTED INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.

Part: SKIN — DAMAGED (BS 525) · airframe 89,036 hrs · 37,974 cycles

FASTENER AT BS 525, S11L, LIGHTNING STRIKE, R & R FASTENER WITH A BLIND FASTENER IAW 757-200, SRM 53-00-01, SECTION 2, PARA 4.

Part: SKIN — DAMAGED (BS 1130) · airframe 89,036 hrs · 37,974 cycles

FASTENER AT BS 1130, STRINGER 7L HAS A LIGHTNING STRIKE, REMOVED FASTENER, CLEANED AREA INSPECTED WITH 10X. DAMAGE REMOVED, TREATED & PAINTED, INSTALLED BLIND RIVET IAW SRM 53-00-01 FIG 201.

Part: SKIN — DAMAGED (BS 1030) · airframe 95,729 hrs · 39,671 cycles

ACFT SKIN HAD LIGHTNING STRIKE DAMAGE AT BS 1030 TWO INCHES UP FROM S6L.

Part: SKIN — DAMAGED (BS 1160) · airframe 89,036 hrs · 37,974 cycles

ACFT SKIN AT BS 1160, FOUR INCHES DOWN STRINGER 7L LIGHTNING STRIKE DAMAGE, REMOVED FASTENER, CLEANED AREA INSPECTED WITH 10X. DAMAGE REMOVED, TREATED & PAINTED, INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.

Part: SKIN — DAMAGED (BS 1004) · airframe 89,036 hrs · 37,974 cycles

FASTENER AT BS 1004, STRINGER 6L HAS A LIGHTNING BURN. REMOVED FASTENER CLEANED AREA INSPECTED WITH 10X. DAMAGE REMOVED TREATED & PAINTED, INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.

Part: SKIN — DAMAGED (BS 1405) · airframe 89,036 hrs · 37,974 cycles

ACFT SKIN AT BS 1405 AND FOUR INCHES DOWN FROM STRINGER 6L HAS LIGHTNING DAMAGE. DRILLED OUT DAMAGE. INSPECTED WITH 10X MAGIFICATION. TREATED AND PAINTED INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.

Part: SKIN — DAMAGED (BS 1516) · airframe 89,036 hrs · 37,974 cycles

ACFT SKIN AT BS 1516, JUST BELOW STRINGER 7L HAS A LIGHTNING STRIKE. DRILLED OUT DAMAGE AND INSPECTED WITH 10X MAGNIFICATION, TREATED, PAINTED AND INSTALLED BLIND RIVET IAW 53-00-01, FIG 201.

Part: SKIN — DAMAGED (BS 1585) · airframe 89,036 hrs · 37,974 cycles

ACFT SKIN AT BS 1585, THREE INCHES DOWN FROM STRINGER 7L HAS A LIGHTENING STRIKE. DRILLED OUT DAMAGE AREA .159 IAW SRM 53-00-01, FIG 201, SECTION I, PERFORMED BHEC IAW NDT 51-00-16. NO DEFECTS FOUND. TREATED, PAINTED AND INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.

Part: SKIN — DAMAGED (BS 1482) · airframe 89,036 hrs · 37,974 cycles

ACFT SKIN AT BS 1482 STRINGER 7L HAS LIGHTNING STRIKE DAMAGE. BLENDED OUT DAMAGE. FOUND BEYOND LIMITS IAW SRM 53-00-01, CUT OUT DAMAGE, ONE INCH HOLE IAW SRM 53-00-01, REPAIR 13. HFEC INSPECTED CUTOUT IAW NDT PART 6 51-00-01, NO CRACKS FOUND. FABRICATED DOUBLER IAW SRM 53-00-01, REPAIR 13, FIG 201. ALODINED AND PRIMED, INSTALLED WET.

Part: SKIN — DAMAGED (BS 1195) · airframe 89,036 hrs · 37,974 cycles

STATIC DISCHARGE ON SKIN AT BS 1195 AND 2.5 INCHES ABOVE STRINGER 9L. DRILLED OUT DAMAGE AND INSPECTED WITH 10X MAGNIFICATION. TREATED, PAINTED AND INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.

Part: SKIN — DAMAGED (BS 1259) · airframe 89,036 hrs · 37,974 cycles

STATIC DISCHARGE ON FASTENER AT BS 1259 AND FIVE INCHES BELOW STRINGER 9L DRILLED OUT DAMAGE, INSPECTED WITH 10X MAGNIFICATION. TREATED, PAINTED AND INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.

Part: SKIN — DAMAGED (BS 1225) · airframe 89,036 hrs · 37,974 cycles

STATIC DISCHARGE ON SKIN AT BS 1225, THREE INCHES BELOW STRINGER 9L. DRILLED OUT DAMAGE INSPECTED WITH 10X MAGINIFCATION. TREATED, PAINTED AND INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.

Part: SKIN — DAMAGED (BS 1550) · airframe 89,036 hrs · 37,974 cycles

ACFT SKIN AT BS 1550 ABOUT FIVE INCHES DOWN FROM STRINGER 7L HAS A LIGHTNING STRIKE. DRILL OUT DAMAGE AREA .159 IAW SRM 53-00-01, FIG 201, SECTION I. PERFORMED HFEC IAW NDT 51-00-16, NO DEFECTS FOUND. TREATED, PAINTED AND INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.

Part: SKIN — DAMAGED (BS 1233) · airframe 89,036 hrs · 37,974 cycles

STATIC DISCHARGE ON SKIN AT BS 1233, FIVE INCHES BELOW STRINGER 9L. DRILLED OUT DAMAGE, INSPECTED WITH 10X MAGNIFICATION. TREATED, PAINTED AND INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.

Part: SKIN — DAMAGED (BS 1374) · airframe 89,036 hrs · 37,974 cycles

ACFT SKIN AT BS 1374, FOUR INCHES DOWN FROM STRINGER 6L HAS LIGHTNING DAMAGE. DRILLED OUT DAMAGE AND INSPECTED WITH 10X MAGNIFICATION. TREATED, PAINTED, INSTALLED BLIND RIVET IAW SRM 53-00-01, FIG 201.

Part: SKIN — CRACKED (BS 1700) · airframe 87,069 hrs · 37,491 cycles

FOUND FUSELAGE SKIN CRACKED DURING HFEC INSPECTION IAW PRI 519950-14 REV O STEP 4 AT BS 1700 BETWEEN STRINGERS 29 & 30R APPROXIMATELY LENGTH 1 INCH. REMOVED SKIN AND REPAIRED IAW PRI 519950-14AD REV 4 C/W ERA 519950-14 AD.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,069 hrs · 37,491 cycles

SKIN AT AFT LAVATORY SERVICING PANEL IS CORRODED. REMOVED CORROSION IAW PRI 519950-14 AND IAW SRM 53-00-01. CORROSION FOUND TO BE BEYOND SRM LIMITS. REPAIRED IAW PRI 519950-14 AD C/W ON ERA 519950-14AD, REV O, 28OCT13 D.

Part: FRAME — CORRODED (BS 1700) · airframe 87,069 hrs · 37,491 cycles

TWO FRAME ANGLES CORRODED AT BS 1700 BETWEEN STRINGERS 29 & 30R. REMOVED FRAME ANGLES AND REPLACED.

Part: SKIN — BULGED (BS 1620 S26R) · airframe 87,069 hrs · 37,491 cycles

SKIN BS 1620 S26R BULGED AND HAS POPPED RIVET HEADS. REPAIRED IAW PRI 519947-14, REV 3. COMPLETED THROUGH STEP (11).

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,529 hrs · 37,341 cycles

DURING DRC, FOUND EMERGENCY PATH LIGHT SEAT 36D, INOPERATIVE. R & R LAMP ASSY. OPS CHECKED NORMAL.

Part: FRAME — CRACKED (BS 1440) · airframe 84,907 hrs · 36,917 cycles

WHILE PERFORMED EDDY CURRENT INSPECTION OF CARGO DOOR, FRAMES IAW OPN 50321AD. FOUND BS 1440 FRAME WEB CRACKED AT STOP FITTING NR 6 AND ADJACENT FASTENER. CUT AND REMOVED DAMAGED SECTION OF WEB AND INSPECTED, NO DISCREPANCIES. INSURANCE CUT MADE FABRICATED REPAIR SRM 53-00-07. TREATED AND PAINTED REPAIR PARTS.

Part: THRESHOLD — CRACKED (R1 DOORWAY) · airframe 89,124 hrs · 38,002 cycles

R1 CORNER CAP FWD CRACKED. REMOVED DAMAGED PART IAW ERA 06-489867-14MA, REV F, SECTION 3. THRESHOLD REPAIRED IAW ERA 06-489867-14, REV F. INSTALLED IAW ERA 06-489867-14 MA, REV F, SECTION 3.

Part: WIRE — BROKEN (CABIN) · airframe 78,768 hrs · 35,427 cycles

LINE MAINTENANCE FOUND WIRE BROKEN FROM EMERGENCY LIGHT CONNECTOR AT SEAT 37F. REPLACED CONNECTOR. LIGHT OPERATION NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,280 hrs · 35,308 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHT AT SEAT 40DEF INOP. MAINTENANCE REPLACED LIGHT ASSEMBLY PER AMM. OPERATION OF LIGHT CHECK OK.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

CRACK ON STR 16R AT STA 478. REPAIRED AT SAA DURING HMV ON N/R CARD 182774.

Part: SKIN — CORRODED (LT WING) · airframe 75,877 hrs · 34,709 cycles

AFTER REMOVAL OF OVERWING FILLER CAP FOUND SKIN CORRODED AROUND EDGE CUTOUT, LEFT WING. COMPLIED WITH ERA 490329-14 REV ORIG AT SAA DURING HMV ON NR CARD 172786.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

MAIN CABIN SEAT TRACK GOUGED STA 418-640 RBL45. REPAIRED AT SAA DURING HMV ON N/R CARD 172539.

Part: DOOR FRAME — GOUGED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

FWD EQUIP COMPT DOOR CUTOUT STA 231 BL 0 FRAME AND LATCH FITTING IS GOUGED 77-30. ACCOMPLISHED ERA 489479-14 REV ORIG AT SAA DURING HMV ON NR CARD 172513.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

MAIN CABIN AFT BULKHEAD OIL CANS STA 1720 WL 251 LBL 37. COMPLIED WITH ERA 489480-14 REV ORIG AND REV A AT SAA DURING HMV ON NR CARD 175461.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

MAIN CABIN FLOORBEAM UPPER SURFACE CORRODED STA 345 LBL18. REPAIRED AT SAA DURING HMV ON N/R CARD 175471.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

MAIN CABIN FLOOR CHORD BL 0 CORRODED AT STA 377-440. REPAIRED AT SAA DURING HMV ON N/R CARDS 175476 AND 175471.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

MAIN CABIN FLOORBEAM UPPER FWD FLANGE CORRODED STA 1640 LBL 17-RBL 17. ADDITIONAL CORROSION LBL 55-59 / ACCOMPLISHED ERA 488913-14MA REV ORIGINAL.

Part: SKIN — CORRODED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

FUSELAGE SKIN CORRODED AT AIR PHONE ANTENNAS AREA STA 1510 S28L AND S28R. ACCOMPLISHED ERA 490199-14 AT SAA DURING HMV ON N/R CARD 162359.

Part: FRAME — DENTED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

AFT CARGO FRAME DENTED ON UPPER FLANGE STA 1620 ABOVE STR 25L. REPAIRED AT SAA DURING HMV ON N/R CARD 173241.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

AFT CARGO STRINGER CORRODED STA 1680-1700 I/B OF LAV SERVICE PAN INSIDE STR 29R. COMLIED WITH ERA 490332-14 REV A AT SAA DURING HMV ON NR CARD 173250.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

AFT CARGO INTERCOSTAL CORRODED STA 1600-1620 BETWEEN STR 29 AND 30L. REPAIRED AT SAA DURING HMV ON N/R CARD 173239.

Part: FRAME — DENTED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

AFT CARGO FRAME DENTED ON UPPER FLANGE STA 1400 BETWEEN STR 25 AND 26L. REPAIRED AT SAA DURING HMV ON N/R CARD 173141.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

AFT CARGO INTERCOSTAL CORRODED I/B AND O/B SIDE STA 1420-1440 BETWEEN STR 28 AND 29R. REPAIRED AT SAA DURING HMV ON N/R CARD 173149.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

AFT CARGO STRINGER CORRODED ON FLANGES I/B AND O/B STA 1467-1472 STR 28L. REPAIRED AT SAA DURING HMV ON N/R. CARD 173155

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

AFT CARGO INTERCOSTAL CORRODED STA 1320-1340 BETWEEN 28/29L. REPAIRED AT SAA DURING HMV ON N/R CARD 173135.

Part: CONNECTOR — BROKEN (CABIN) · airframe 75,877 hrs · 34,709 cycles

CONNECTOR FOR EMERGENCY LIGHT CABLE SEAT 25DEF BROKEN. REPLACED CONNECTOR AT SAA DURING HMV ON N/R CARD 162441.

Part: SKIN — DENTED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

DENTS (2EA) ON FUSELAGE SKIN STA 778 AND BELOW S17L. COMPLIED WITH ERA 489474-14 REV ORIG AT SAA DURING HMV ON NR CARD 162057.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

CREASE ON FUSELAGE SKIN STA 600 AND BELOW S 27R. COMPLIED WITH ERA 489469-14 REV ORIG AT SAA DURING HMV ON NR CARD 162372.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

RT SIDE OF FUSELAGE AT STA 475 BELOW S 14R HAS A PROTRUDING DENT. ACCOMPLISHED ERA 489476-14AD REV ORIG AT SAA DURING HMV ON NR CARD 174190.

Part: SKIN — GOUGED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

2 GOUGES ON FUSELAGE AT STA 524 BELOW S27L. REPAIRED AT SAA DURING HMV ON N/R CARD 162023.

Part: SKIN — DENTED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

DENTS 2 EA ON FUSELAGE SKIN STA 613 ABOVE S17L AND BELOW S17L. ACCOMPLISHED ERA 489477-14 AT SAA DURING HMV ON N/R CARD 162055.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

PULLING THRU FASTENER AT FUSELAGE SKIN STA 199 AND 12 IN BELOW LAP S20R. COMPLIED WITH ERA 490198-14 REV ORIG AT SAA DURING HMV ON NR CARD 162062.

Part: SKIN — DENTED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

2 EA DENTS ON FUSELAGE SKIN STA 778 BELOW S17L. ACCOMPLISHED ERA 489474-14 AT REV ORIG AT SAA DURING HMV ON N/R CARD 162057.

Part: FASTENER — PULLED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

PULLING THRU FASTENER AT FUSELAGE STA 199 AND 12 IN BELOW LAP S20L. COMPLIED WITH ERA 490197-14 ORIG AT SAA DURING HMV ON NR CARD 162059.

Part: SKIN — GOUGED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

GOUGES (2EA) ON FUSELAGE SKIN STA 670 AND BELOW S26R. COMPLIED WITH ERA 489482-14 REV ORIG AT SAA DURING HMV ON NR CARD 162351.

Part: SKIN — GOUGED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

LT AFT OF L4 DOOR 2 PLACES HAS GAUGE STA 1681.8 UPPER SKIN & STRINGER L4 LEFT AND LWR SKIN FROM STRINGER, L4 LEFT UP TO 2.5 INCH BELOW STRINGER 15 LEFT. COMPLIED WITH FINAL ERA 490336-14 REV ORIG AT SAA DURING HMV ON NR CARD 174177.

Part: SKIN — WRINKLED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

LT AFT OF L4 DOOR CENTER SECTION AT APPX STA 1680.8 SKIN HAS WRINKLE. COMPLIED WITH ERA 490326-14 REV ORIG AT SAA DURING HMV ON NR CARD 174178.

Part: SKIN — DENTED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

DENT ON FUSELAGE SKIN, STA 1630 AND BELOW S26L. COMPLIED WITH ERA 489472-14 REV ORIG AT SAA DURING HMV ON NR CARD 162030.

Part: SKIN — DENTED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

DENT ON FUSELAGE SKIN STA 416 AND ABOVE S17R. COMPLIED WITH ERA 489468-14 REV ORIG AT SAA DURING HMV ON NR CARD 162027.

Part: SKIN — DENTED (FUSELAGE) · airframe 75,877 hrs · 34,709 cycles

DENT ON FUSELAGE SKIN STA 416 ABOVE S17R. REPAIRED PER ERA 489468-14 REV ORIG.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 74,116 hrs · 34,229 cycles

ACTION DURING LAYOVER CHECK, MAINTENANCE FOUND EMERGENCY PATH LIGHT (RED) AT SEAT 25D INOPERATIVE. MAINTENANCE REPAIRED THE WIRING HARNESS. OPERATIONAL CHECK WAS GOOD ODI 2010-D0931 (DL75E101998).

Part: WIRE — DETACHED (EMERGENCY LIGHT) · airframe 74,033 hrs · 34,207 cycles

SEAT 39D EMERGENCY ESCAPE PATH LIGHT WAS INOPERATIVE. MX FOUND ONE WIRE PULLED FROM SOCKET. THE WIRE WAS RE-SEATED, A LENS WAS REPLACED, AND THE LIGHT OPERATIONALLY CHECKED GOOD.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 74,023 hrs · 34,205 cycles

DURING LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY PATH LIGHTS AFT OF ROW 36 INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY FUSE. OPERATIONAL CHECK WAS GOOD (2010-D0881)(DL75E101940).

Part: OVEN — ODOR (GALLEY) · airframe 73,743 hrs · 34,139 cycles

DURING FLIGHT ACRID/BURNING ODOR IN AFT GALLEY WHEN OVENS TURNED OFF, FELT HOT AIR FROM OVENS. TURNED GALLEY POWER OFF PULLED OVEN CB IN LAST 15 MINUTES ODOR AND HEAT HAS GONE AWAY. (DL75E101666)

Part: OVEN — ODOR (GALLEY) · airframe 73,743 hrs · 34,139 cycles

DURING FLIGHT, ELECTRICAL ODOR EMITTED FROM THE LEFT AFT OVEN. CIRCUIT BREAKER WAS PULLED. MAINTENANCE RESET THE OVEN CIRCUIT BREAKER AND AN OPERATIONAL CHECK OF THE OVEN WAS GOOD.

Part: SOCKET — BURNED (GALLEY LIGHT) · airframe 72,763 hrs · 33,895 cycles

SMOKE IN CABIN COMING FROM MID GALLEY AFT PARTITION FOUND WORK LIGHT LAMP ASSY SOCKET BURNED MELTING PLASTIC. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK.

Part: THROTTLE — MALFUNCTIONED (NR 2 ENGINE) · airframe 71,136 hrs · 33,488 cycles

AFTER NORMAL ENG START ON LT ENG, NO RESPONSE TO ENG WHEN THROTTLE ADVANCED FOR TAXI. NO EICAS MSG. UPON RESTART AT THE GATE ALL INDICATIONS NORMAL, ENG RUN AT GATE. ALL INDICATIONS NORMAL. THROTTLE ADVANCE NORMAL, ETOPS CATEGORY 'E': PROBLEMS WITH SYS, CRITICAL TO ETOPS.

Part: VALVE — MALFUNCTIONED (APU) · airframe 71,045 hrs · 33,469 cycles

APU SHUTDOWN ON SECOND ENGINE START ATTEMPT. APU FAULT LIGHT DISPLAYED. FOUND APU SURGE VALVE DUCT BOOT WITH HOLE. PERFORMED BITE ON APU ECU FAULTED REVERSE FLOW. REPLACED SURGE VALVE AND RUBBER BOOT. APU CHECKS NORMAL. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: APU — SHUTDOWN (APU BAY) · airframe 70,235 hrs · 33,261 cycles

APU AUTO SHUTDOWN ON ITS OWN WHEN PACKS WERE TURNED OFF. PERFORMED ECU BITE, NO FAULTS FOUND. CHECKED OIL LEVEL. CHECKS GOOD.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 66,008 hrs · 32,084 cycles

UPON LEFT ENG START, NO THROTTLE RESPONSE AFTER BLEED VALVE RESET, OPS NORMAL. NO MSGS, RESTARTED LEFT ENG, ALL PARAMETERS WERE NORMAL. ON THE GROUND,THE ENG IS RESPONSIVE IMMEDIATELY, ALL CHKS SUCCESSFULLY.

Part: PROBE — MALFUNCTIONED (ADC) · airframe 65,058 hrs · 31,700 cycles

TAT TEMP DISPLAY ERRONEOUS AT FL310 TAT READ -75 SAT -96. FOUND TAT AND SAT TEMPS SHOWING -56. REMOVED AND REPLACED TAT PROBE, PAMM TAT AND SAT NOW READ 14. PERFORMED OPS TEST OF AIR DATA COMPUTING SYS PER MM. OPS TEST GOOD.

Part: SKIN — CORRODED (1720 S27-29R) · airframe 64,031 hrs · 31,271 cycles

FUSELAGE SKIN CORROSION AT STA 1720 BETWEEN S-27R AND S-29R. CUTOUT DAMAGED SKIN AND INSTALLED REPAIR DOUBLER.

Part: SKIN — CORRODED (BS 430 S28L) · airframe 64,031 hrs · 31,271 cycles

FUSELAGE SKIN CORROSION AT THE AFT RT CORNER OF THE FWD LAVATORY SERVICE PANEL LOCATED AT STA 430, S-28L. CUTOUT THE DAMAGED SKIN AT INSTALLED A REPAIR DOUBLER.

Part: FIRE BOTTLE — MALFUNCTIONED (APU BAY) · airframe 62,550 hrs · 30,721 cycles

APU QUIT ON PUSHBACK AS POWER CORD WAS REMOVED SIMULTANEOUSLY APU FIRE DISCHARGE LIGHT ILLUMINATED. FOUND BOTTLE DISCHARGED. CHECKING CIRCUITRY FOR UNCOMMANDED BOTTLE DISCHARGE. TESTED OK PER AMM.

Part: COFFEEMAKER — FAILED (GALLEY) · airframe 61,266 hrs · 30,195 cycles

POP WITH SMOKE OUT OF COFFEE MAKER, RETURNING TO GATE TO HAVE IT CHECKED OUT. NO HISTORY. MAINTENANCE REMOVED AND INSPECTED COFFEE MAKER. CIRCUIT BREAKER TO REMAIN PULLED AND FWD COFFEE MAKER TO MCO/PLAC. REPLACED DC CONVERTER, CKS GOOD.

Part: VALVE — INOPERATIVE (TEMP CONTROL) · airframe 59,102 hrs · 29,442 cycles

SMOKE IN COCKPIT AT T/O. FOUND TEMP CONTROL VALVE ON LT PACK INOP. REPLACED AND PERFORMED HIGH POWER RUN ON BOTH ENGINES, NO SMOKE NOTED.

Part: RING — OUT OF POSITION (ESCAPE SLIDE) · airframe 57,133 hrs · 28,778 cycles

RIGHT AFT ENTRY DOOR DIFFICULT TO CLOSE AND ARM DURING PREFLIGHT. RT AFT ENTRY LIGHT ILLUMINATED AFTER AIRBORNE. REPOSITIONED RT AFT ENTRY DOOR ESCAPE SLIDE SKIRT AND SURVIVAL PACK D-RING. DOOR OPN NORMAL.

Part: SKIN — TOOL DAMAGE (FUSELAGE) · airframe 55,809 hrs · 28,274 cycles

TOOLING DAMAGE TO THE FUSELAGE SKIN AT STATION 631 AND STR 4L.

Part: SKIN — TOOL DAMAGE (FUSELAGE) · airframe 55,809 hrs · 28,274 cycles

TOOLING DAMAGE TO THE FUSELAGE SKIN AT STATION 899 AND STR 3L. REPAIRED IAW ERA 096211-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 55,809 hrs · 28,274 cycles

TOOLING DAMAGE TO THE FUSELAGE SKIN AT STATION 453 AND STR 4L. REPAIR IAW ERA 096138-14.

Part: SKIN — DENTED (FUSELAGE) · airframe 53,708 hrs · 27,580 cycles

THE FUSELAGE SKIN WAS FOUND DENTED AT FS 1645, JUST BELOW STRINGER 19R. THE DENT WAS REMOVED WITH A 3.5 X 3.2 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 089688-14, REV A.

Part: BALLAST — FAILED (FORWARD CABIN) · airframe 49,711 hrs · 25,978 cycles

APPROXIMATELY 3 PLUS HOURS FROM ATL DURING FLT ELECTRICAL ODOR IN FIRST CLASS CABIN - REPLACED 2CD BALLAST AND LAMPS

Part: SKIN — CORRODED (FS 426, S-1) · airframe 48,001 hrs · 25,200 cycles

FUSELAGE / SKIN / FS 426 / STRG. 1-2R / TCAS ANTENNA CUTOUT CORROSION REPAIR CORROSION WAS FOUND AROUND THE TCAS ANTENNA CUTOUT AT FS 426 BETWEEN STRINGERS 1 AND 2R. THE EXISTING TCAS DOUBLER WAS REMOVED AND DISCARDED. THE CUTOUT WAS ENLARGER TO REMOVE THE CORROSION. THE NEW CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM DOUBLERS PER ER/A 382746-14, REV. A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 48,001 hrs · 25,200 cycles

THE FUSELAGE SKIN AND UNDERLYING BEAR STRAP WERE FOUND WITH AREAS OF CORROSION NEAR THE C2 DOOR CUTOUT AT FS 1440 AND STRINGERS 25R-26R. THE CORROSION WAS REMOVED FROM THE BEAR STRAP AND ANOTHER IN THE SKIN. THE CUTOUTS WERE REPAIRED WITH EXTERNAL DOUBLERS PER ER/A 382594-14, REV A.

Part: SKIN — GOUGED (FS 676, S-23R) · airframe 48,001 hrs · 25,200 cycles

FUSELAGE / SKIN / FS 676 / STRG. 23R : GOUGE CUTOUT REPAIR THE FUSELAGE SKIN WAS BADLY GOUGED BY A WORK STAND AT FS 676 NEAR STRINGER 23R. THE GOUGE WAS REMOVED WITH A 7.9" X 3" CUTOUT. THE CUTOUT WAS REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER AND INTERNAL ALUMINUM EDGE ROW DOUBLERS. THE REPAIR WAS ACCOMPLISHED PER ER/A 382725-14, REV A.

Part: SKIN — CORRODED (FS 900, S-28) · airframe 48,001 hrs · 25,200 cycles

FUSELAGE / SKIN / FS 900 / STRG. 28L-28R : CORROSION REPAIR THE FUSELAGE SKIN WAS FOUND BADLY CORRODED AT FS 900 AND BETWEEN STRINGERS 28L & 28R. THE SKIN WAS CUT AT FS 885 AND THE AFT SECTION REMOVED TO FS 900. A NEW SECTION OF SKIN WAS FABRICATED AND INSTALLED USING EXTERNAL AND INTERNAL ALUMINUM DOUBLERS TO SPLICE THE NEW SECTION. THE REPAIR WAS ACCOMPLISHED PER ER/A 382586-14, REV. A.

Part: BULKHEAD — CORRODED (FS 900, S-28) · airframe 48,001 hrs · 25,200 cycles

FUSELAGE / BULKHEAD / FS 900 / STRG. 28L-28R / LOWER CHORD AND WEB : CORROSION REPAIR THE LOWER CHORD AND WEB OF THE FS 900 BULKHEAD WAS FOUND CORRODED BETWEEN STRINGERS 28L & 28R. THE DAMAGED SECTION OF WEB WAS CUTOUT AND THE LOWER CHORD WAS CUT AT STRINGER 28L & 28R. THE WEB CUTOUT WAS REPAIRED WITH 2 ALUMINUM REPAIR DOUBLERS. A NEW SECTION OF CHORD WAS SPLICED AT THE CUT LOCATION WITH STEEL REPAIR ANGLES. THE REPAIR WAS ACCOMPLISHED PER ER/A 382587-14, REV. A.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 48,001 hrs · 25,200 cycles

C1 DOOR OPENING LOWER CHORD CORRODED, THE FS 620 OPENING FRAME OUTER CHORD AND WEB WERE CUT AND THE LOWER SECTIONS REMOVED TO ALLOW ACCESS TO THE CHORD. AFTER REPLACEMENT OF THE CHORD, THE LOWER SECTION OF FRAME CHORD AND WEB WERE REINSTALLED AND SPLICE WITH REPAIR ANGLES AND A DOUBLER PER ER/A 382597-14, REV A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,001 hrs · 25,200 cycles

THE UPPER CAP OF THE FS 1681 FLOORBEAM WAS FOUND WITH SEVERAL AREAS OF CORROSION. THE UPPER CAP WAS TRIMMED OFF TO REMOVE ALL AREAS OF CORROSION. A NEW CAP WAS FABRICATED AND INSTALLED PER ER/A 382554-14, REV A.

Part: TRUNNION — CORRODED (RT MLG) · airframe 48,001 hrs · 25,200 cycles

INSPECTION OF THE RT MLG FWD TRUNNION SUPPORT FITTING FUSE PINS PER AD 2000-07-13 REVEALED CORROSION IN THE FUSE PIN LUG BORES OF THE FITTING. THE CORROSION WAS REMOVED BY OVERSIZING THE LUG BORES AND INSTALLING OVERSIZED BUSHINGS. THE REPAIR WAS ACCOMPLISHED PER ER/A 382613-14.

Part: FLAP — CORRODED (LT WING) · airframe 48,001 hrs · 25,200 cycles

LEFT MAIN FLAP, LWR CHORD WAS FOUND CORRODED. REPAIR PER ER/A 410943-14.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 45,713 hrs · 24,336 cycles

3L ENTRY DOOR OPENED WHILE ARMED, SLIDE DID NOT DEPLOY, IT FELL ON SERVICE TRUCK - REPLACED SAME

Part: ENGINE — FLAMED OUT (NR 2) · airframe 42,781 hrs · 23,117 cycles

RT ENGINE ROLLED BACK AND QUIT DURING DESCENT INTO ATL PASSING THRU 21,000 FT. REPLACED RT ENGINE.

Part: INDICATOR — INTERMITTENT (WEATHER RADAR)

STRONG ACID ODOR IN COCKPIT JUST PRIOR TO TAKEOFF WHEN TRANSPONDER WAS TURNED ON. RETURNED TO GATE. FOUND WEATHER RADAR INDICATOR INTERMITTENT PER CREW. REMOVED AND REPLACED WEATHER RADAR INDICATOR AND TRANSCEIVER CK OK. INSPECTED FWD AND MAIN E AND E COMPARTMENTS AND NO ODORS FOUND. INSPECTED WIRING TO WEATHER RADAR INDICATOR, NO PROBLEMS FOUND.

Part: MEGAPHONE — MISSING (CABIN)

AFT CABIN MEGAPHONE MISSING. INSTALLED NEW MEGAPHONE.

Part: BULB — FAILED (CABIN)

EXTERIOR EMERGENCY LIGHT FOR L2 DOOR INOP. RELAMPED SAME, OPS CHECK GOOD.

Part: CONNECTOR — OVERHEATED (LT COCKPIT)

ELECTRICAL BURNING SMELL IN CO AND CN FL310. LATER ELEC SMOKE EMERGING FROM UNDER CA GLARESHIELD NEAR LT CORNER OR CA WINDSHIELD. SECURED WINDOW HEAT, SMOKED STOPPED. MTC FOUND LWR LT DISCONNECT PLUG OVERHEATED. REPLACED PLUG.

Part: ESCAPE SLIDE — FAIL TEST (RT OVERWING)

IND - DURING ROUTINE ESCAPE SLIDE OPERATIONAL CHECK, THE RT OVERWING SLIDE REMAINED ON TOP OF WING, ALL SECTIONS INFLATED, DOOR OPENED PROPERLY. SECTION OF VELCRO STRAPPING DID NOT LET LOOSE PREVENTING 3 BOTTOM SAETY WIRES (FUSE) FROM BREAKING. LARGE VELCRO STRAP, 6 FEET, DID NOT RELEASE. EVALUATION FOUND WHAT APPEARS TO BE A TEMPORARY TIE AROUND SLIDE RESTRICTING SLIDE TO BRAKE THE FRANGIBLE LINKS. ADDITIONALLY, LACING COVERS (2 EACH) WERE TORN ALONG LOWER SEAM. A FLEET CAMPAIGN WAS SCHEDULED BY VENDOR. REPLACED ESCAPE SLIDE.