N665US

Part: CARBON SEAL — LEAKING (NR 2 ENGINE) · airframe 108,522 hrs · 13,444 cycles

NR 2 ENGINE INFLIGHT SHUTDOWN DUE TO LOW OIL PRESSURE. MAINTENANCE PERFORMED NR 2 ENGINE GEARBOX PRESSURE CHECK, FOUND IDG CARBON SEAL LEAKING. MAINTENANCE REPLACED IDG CARBON SEAL, COMPLIED WITH LEAK CHECK AND NO LEAKS NOTED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 106,046 hrs · 13,165 cycles

UPPER DECK ROWS 77-79 EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY PACK.

Part: CARGO TRACK — CORRODED (BS 980) · airframe 105,980 hrs · 13,158 cycles

FWD BAY CARGO TRACK BS 980 RBL 24.75 FOUND CORRODED. REPAIRED IAW SRM.

Part: CARGO TRACK — CORRODED (BS 980) · airframe 105,980 hrs · 13,158 cycles

FWD BAY CARGO TRACK BS 980, RBL 45.5 FOUND CORRODED. REPAIRED IAW SRM.

Part: LIFTER — CRACKED (GIRT BAR) · airframe 105,972 hrs · 13,156 cycles

THE L4 DOOR LOWER GATE, GIRT BAR MECHANISM AFT LIFTER FOUND CRACKED. R & R THE LIFTER, AND ADJUSTED THE GIRT BAR MECHANISM.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE) · airframe 105,972 hrs · 13,156 cycles

THE L3 DOOR ESCAPE SLIDE BOTTLE PRESSURE GAUGE FOUND THE POINTER BELOW THE GREEN BAND. R & R THE ESCAPE SLIDE.

Part: STRUCTURE — CRACKED (R5 DOORWAY) · airframe 105,972 hrs · 13,156 cycles

R5 DOOR AFT UPPER CORNER OF THE CUTOUT FOUND 1 CRACK. REPAIRED.

Part: STRUCTURE — CRACKED (L5 DOOR FRAME) · airframe 105,972 hrs · 13,156 cycles

L5 DOOR AFT UPPER CORNER OF THE CUTOUT FOUND ONE CRACK. REPAIRED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 105,845 hrs · 13,142 cycles

L3 DOOR EMERGENCY EXIT SIGN INOPERATIVE. R & R LIGHT ASSY.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 105,450 hrs · 13,101 cycles

DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS OVER WING LT FWD INOPERATIVE. REPLACED CHARGER ASSY.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 104,243 hrs · 12,958 cycles

EXTERIOR EMERGENCY LIGHT ON LT OVERWING NOT ILLUMINATED. REPLACED FUSE AT POWER SUPPLY.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 102,972 hrs · 12,803 cycles

DURING A NON ROUTINE CHECK. BATTERY CHARGER FOUND INOPERATIVE. R & R BATTERY CHARGER IAW AMM 33-51, OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 102,217 hrs · 12,717 cycles

EMERGENCY EXIT SIGN BETWEEN UPPER DECK DOORS WOULD NOT ILLUMINATE. REPLACED POWER SUPPLY EMERGENCY LIGHT, CHECKED OK IAW AMM 33-51. OK FOR SERVICE.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 102,192 hrs · 12,715 cycles

FOUND EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED FUSE ON BATTERY PACK IAW AMM 33-51, CHECKED OK.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 101,993 hrs · 12,691 cycles

EMERGENCY LIGHTS OUT AT 6A THRU 1A. REPAIRED BROKEN WIRES BEHIND SIDEWALL PANEL AT SEAT 6A. CHECKED GOOD IAW WDM 33-51-23 AND BWSPM 20-30.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 101,901 hrs · 12,679 cycles

DURING CHECK, FOUND UPPER DECK DOOR LIGHT WOULD NOT ILLUMINATE, R & R BATTERY PACK IAW AMM 33-51-04, CHECKED OK.

Part: GROUND STUD — BROKEN (EMERGENCY LIGHT) · airframe 101,842 hrs · 12,669 cycles

UPPER DECK EXIT SIGN FOR BOTH EMERGENCY DOORS HAS BROKEN GROUND STUDS. REMOVED AND REPLACED LIGHT ASSY IAW AMM 33-51-02, OPS CHECKED GOOD, OK FOR SERVICE.

Part: STRUCTURE — DAMAGED (AFT CARGO DOOR) · airframe 101,577 hrs · 12,640 cycles

DURING WALK AROUND, DAMAGE WAS FOUND ON AFT CARGO DOOR AFT CORNER. REPAIRED IAW SRM 52-30-01, REPAIR 2. OK FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 1700) · airframe 99,328 hrs · 12,363 cycles

CORROSION ON FLOOR SUPPORT BS 1700, RBL 48. CORRODED FLOOR SUPPORT REPAIRED IAW ERA 512550-14, REV ORIGINAL.

Part: FLOOR SUPPORT — CORRODED (BS 1700) · airframe 99,328 hrs · 12,363 cycles

CORROSION ON FLOOR SUPPORT BS 1700, RBL 11, WL 199.8. CORRODED FLOOR SUPPORT REPAIRED IAW EAR 512550-14, REV ORIGINAL.

Part: TENSION TIE — DAMAGED (BS 1220) · airframe 99,326 hrs · 12,362 cycles

STA 1220 RT TENSION TIE PLATE FOUND FASTENERS WITH SHORT EDGE MARGINS. REMOVED AND NEW TENSION TIE PLATE INSTALLED IAW DWG:65B09631, SHEET 16, REV G.

Part: CHANNEL — CRACKED (BS 1160) · airframe 99,326 hrs · 12,362 cycles

ONE CRACK FOUND IN THE TENSION TIE FORWARD CHANNEL AT BS 1160, CRACK LENGTH IS ABOUT 2MM. THE TENSION TIE FORWARD CHANNEL REPAIRED IAW SRM 53-40-30, REPAIR 2, FIG 201.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 98,585 hrs · 12,273 cycles

DURING SERVICE CHECK FOUND FUSELAGE EMERGENCY LIGHT FWD TWO AT LT SIDE INOPERATIVE. REPLACED CHARGER UNIT AT DOOR 3 LT. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 97,836 hrs · 12,183 cycles

EMERGENCY LIGHTS OUT, 2 EACH, UPPER LEFT OVERWING. REPLACED POWER SUPPLY M7919, AMM33-51-04/201, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 96,661 hrs · 12,033 cycles

DURING INSPECTION, FOUND DOOR 1R MOUNTED EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED EMERGENCY DOOR MOUNT LIGHT ASSEMBLY AND CHECKS NORMAL PER AMM 33-51.

Part: STRUCTURE — DAMAGED (L4 DOOR) · airframe 96,625 hrs · 12,029 cycles

DURING INSPECTION FOUND RIVET PULLED THROUGH AND DOOR CRACKED AT DOOR 4L UPPER AFT SIDE BY LATCH TORQUE TUBE BEARING ASSEMBLY. MAINTENANCE FABRICATED DOUBLER PER SRM 52-10-02 REPAIR NR 2. STOP DRILLED CRACK PER SRM 52-10-02 REPAIR NR 2. PERFORMED HFEC ON STOP DRILLS AND DAMAGE IS CONTAINED HFEC INSPECTION IAW NDT MANUAL P6-7170, PART 6,51-00-00. INSTALLED DOUBLER PER SRM 52-10-02.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 96,522 hrs · 12,015 cycles

DURING INSPECTION, FOUND LEFT OVERWING EMERGENCY LIGHTS 1ST AND 2ND POSITION FROM FORWARD INOPERATIVE. MAINTENANCE REPLACED FUSE OF M7919 EMERGENCY LIGHT POWER SUPPLY. LEFT OVERWING EMERGENCY LIGHTS OPERATIONAL CHECK OK

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION MAIN DECK CABIN SEAT TRACK AT BS 980 AND LBL 33 FOUND WITH SURFACE CORROSION. MAINTENANCE REMOVED AND REPLACED MAIN DECK CABIN SEAT TRACK AT BS 980 AND LBL 33 INTERCOSTAL P/N: 140U5280-10 AS PER B747-400 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION, MAIN DECK CABIN SEAT TRACK AT BS 980 AND LBL 40 FOUND SURFACE CORROSION. MAINTENANCE REPAIRED SEAT TRACK AT STA 940 TO STA 1000 AS PER PRI 503092-14 REV0 AND REV1 DATED 24MAY12. PRI 503092-14 REV0 AND REV1 COMPARED TO ER/A 503092-14 REV ORIGINAL FOUND IN COMPLIANCE.

Part: STRINGER — MISINSTALLED (BS 960 S39R) · airframe 96,421 hrs · 12,004 cycles

STRINGER 39R FOUND WITH SHORT EDGE MARGIN AT LAP JOINT INNER AND OUTER SKIN.

Part: TENSION TIE — CRACKED (BS 1140) · airframe 96,421 hrs · 12,004 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION AT R TENSION TIES STATION 1140 ON LOWEST FASTENER FIRST FASTENER HOLE FROM OUTBOARD LOOKING FORWARD.

Part: SPLICE — DAMAGED (BS 1000 S36-40R) · airframe 96,421 hrs · 12,004 cycles

BULKHEAD SPLICE ANGLES AT STRINGER 40R AND 36R FOUND WITH SHORT EDGE MARGINS.

Part: SKIN — CRACKED (BS 980) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION, A CRACK WAS FOUND ON THE BS 980 RIGHT SKIN. MAINTENANCE ACCOMPLISHED SRM 53-20-01 REPAIR AND ER/A 503072-14AD SECTION I.

Part: STRUCTURE — DAMAGED (BS 1000 BULKHEAD) · airframe 96,421 hrs · 12,004 cycles

RIGHT LOWER STRUCTURE OF BULKHEAD FOUND WITH SHORT EDGE MARGIN.

Part: FLOORBEAM — CRACKED (BS 1220) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION FOUND MAIN DECK CABIN FLOORBEAM WEB CRACKED AT BS 1220 AND RBL 109. MAINTENANCE REMOVED AND REPLACED MAIN DECK CABIN FLOORBEAM WEB PER WORKCARD 5313-01014-02H.

Part: FLOORBEAM — CRACKED (BS 1180) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION, FOUND MAIN DECK CABIN FLOORBEAM WEB CRACKED AT BS 1180 AND LBL 109. MAINTENANCE REMOVED AND REPLACED MAIN DECK CABIN FLOORBEAM WEB PER WORKCARD 5313-01014-02B.

Part: FLOORBEAM — CRACKED (BS 1180) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION, FOUND MAIN DECK CABIN FLOORBEAM WEB CRACK AT BS 1180 AND RBL 109. MAINTANENCE REMOVED AND REPLACED MAIN DECK CABIN FLOORBEAM WEB PER WORKCARD 5313-01014-02F.

Part: FLOORBEAM — CRACKED (BS 1200) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION, FOUND MAIN DECK CABIN FLOORBEAM WEB CRACK AT BS 1200 AND RBL 109. MAINTANENCE REMOVED AND REPLACED MAIN DECK CABIN FLOORBEAM WEB PER WORKCARD 5313-01014-02G.

Part: FAILSAFE — CRACKED (BS 1140 S9-10R) · airframe 96,421 hrs · 12,004 cycles

CRACK FOUND IN FAILSAFE CHORD AT BS 1140 STRINGER S9-10R. MAINTENANCE ACCOMPLISHED ER/A 503505-14AD SECTION I REPAIR.

Part: FRAME — CRACKED (BS 1180) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION FOUND CRACK AT RIGHT SIDE TENSION TIES BS 1180 ON TOP FASTENER ROW, 5TH FASTENER HOLE FROM OUTBOARD LOOKING FORWARD. MAINTENANCE REPAIRED PER SRM 53-40-30 REPAIR 1 FIG 201.

Part: FRAME — CRACKED (BS 1000 BULKHEAD) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION FOUND CRACK (EXTERNAL) AT BS 1000 BULKHEAD FRAME AT STRINGER-38R. MAINTENANCE REPLACED FRAME.

Part: FRAME — CRACKED (BS 1160 S9L) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION, FOUND CABIN UPPER LOBE TENSION TIES AREA BS 1160 STINGER-9L FRAME WEB AT STRINGER CUTOUT CRACKED. MAINTENANCE REMOVED AND REPLACED CRACKED FRAME WEB WITH NEW WEB AS PER SRM 53-40-07 REPAIR 3 FIG 201 AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1655) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION, FOUND CORROSION ON LAVATORY FLOOR SUPPORT AT BS 1655 AND LBL 117. MAINTENANCE REMOVED AND REPLACED DAMAGED FLOOR SUPPORT AS PER SRM 51-40-02.

Part: STRINGER — CRACKED (BS 460 S10L) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION FOUND CRACK AT FUSELAGE STRINGER S-10L AT BS 460. MAINTENANCE REPAIRED STRINGER CRACK PER CARD NO: 5314-01048-02G FOR WORK DETAIL.

Part: FITTING — CRACKED (BS 1000 S38R) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION AT BS 1000 S38R FORWARD BATHTUB FITTING, FOUND ONE FASTENER HOLE CRACKED. MAINTENANCE REPLACED BATHTUB FITTING, PER WORKCARD NR 5312-01044-04B FOR WORK DETAILS.

Part: FRAME — CRACKED (BS 1160) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION FOUND CRACK AT RIGHT SIDE TENSION TIE STA1160 ON LOWEST FASTENER ROW, 1ST FASTENER HOLE FROM OUTBOARD LOOKING FORWARD. MAINTENANCE REMOVED AND REPLACED CRACKED STRINGER CLIP AS PER B747-400 SRM 51-40-02. NEW STRINGER CLIP, P/N 65B04174-44, FABRICATED AS PER DRAWING 65B04174.

Part: ANGLE — CRACKED (BS 800 S17R) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION FOUND CRACK ON ANGLE AT RIGHT BS 800 FRAME AT STRINGER 17. MAINTANENCE REPAIR CARRIED OUT AS PER PRI ER/A503096-14AD.

Part: FRAME — CRACKED (BS 1180) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION, FOUND CABIN UPPER LOBE TENSION TIES AREA BS 1180 STRINGER-9L, FOUND FRAME WEB AT STRINGER CUTOUT CRACKED. MAINTENANCE REMOVED CRACKED FRAME DOUBLER AND FABRICATED NEW DOUBLER PER P/N: 65B26275-3 AS PER DWG65B26275. REFER TO SMALL CONTROL NR PO236369. NEW FABRICATED DOUBLER HOLES PICKED UP AS PER B747-400 SRM 51-40-05 AND INSTALLED AS PER SRM 53-40-07, REPAIR 4 FIG 201 AND 51-40-02.

Part: TENSION TIE — CRACKED (BS 1200) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION, FOUND CRACK AT RIGHT SIDE TENSION TIE AT BS 1200 ON TOP FASTENER ROW, 5TH FASTENER HOLE FROM OUTBOARD LOOKING FORWARD. MAINTENANCE REPAIRED CRACK PER SRM 53-40-03 REPAIR 1 FIG 201.

Part: FRAME — CRACKED (BS 1120) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION FOUND CABIN UPPER LOBE TENSION TIES AREA BS 1120 STRINGER-11R FRAME WEB AT STRINGER CUTOUT CRACKED. MAINTENANCE REPAIRED FRAME PER SRM 53-40-07 REPAIR 1 FIG 201.

Part: FRAME — CRACKED (BS 1200) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION, FOUND CABIN UPPER LOBE TENSION TIES AREA BS 1200 STRINGER-9L FRAME WEB AT STRINGER CUTOUT CRACKED. MAINTENANCE REMOVED AND REPLACED CRACKED DOUBLER FRAME AT CABIN UPPER LOBE TENSION TIES AREA BS 1200 STRINGER-9L WITH NEW DOUBLER FRAME AS PER SRM 51-40-02 AND SRM 53-40-07 REPAIR 5 FIG 201.

Part: FRAME — CRACKED (BS 1140) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION FOUND CABIN UPPER LOBE TENSION TIES AREA BS 1140 STRINGER-10L. FOUND FRAME WEB AT STRINGER CUTOUT CRACKED. MAINTENANCE REPAIR CARRIED OUT AS PER SRM 53-40-07 REPAIR 2 FIG 20.

Part: TENSION TIE — CRACKED (BS 1120) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION FOUND CRACK AT LEFT SIDE TENSION TIE AT BS 1120 ON TOP FASTENER ROW, 4TH FASTENER HOLE FROM OUTBOARD LOOKING FORWARD. MAINTENANCE REPAIRED CRACK PER PER SRM 53-40-30 REPAIR 1 FIG 201.

Part: FRAME — CRACKED (BS 1180) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION FOUND CRACK AT LEFT SIDE TENSION TIE AT BS 1180 ON TOP FASTENER ROW, 5TH FASTENER HOLE FROM OUTBOARD LOOKING FORWARD. MAINTENANCE REPAIRED AS PER SRM 53-40-30 REPAIR 1 FIG 201.

Part: SHEAR TIE — CRACKED (BS 1200) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION FOUND CABIN UPPER LOBE TENSION TIES AREA BS 1200. FOUND SHEAR TIE NEAR STRINGER CUTOUT CRACKED. MAINTENANCE FABRICATED NEW SHEAR TIE AS PER DWG 65B01735. CRACKED SHEAR TIE REMOVED AND NEW FABRICATED SHEAR TIE INSTALLED AS PER SRM 51-40-02. HEAT TREAT CARRIED OUT AS PER 5602 REV AF. HARDNESS TESTED AVERAGED HRB 88.7 AS PER 5946 REV AA. CONDUCTIVITY TEST CARRIED OUT FOUND VALUE 32 .5 PERCENT IACS WITHIN LIMIT AS PER 5651 REV B.

Part: FRAME — CRACKED (BS 1140 S10R) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION FOUND CABIN UPPER LOBE TENSION TIES AREA BS 1140 STRINGER-10R. FOUND FRAME WEB AT STRINGER CUTOUT CRACKED. MAINTENANCE REPAIR CARRIED OUT AS PER SRM 53-40-07 REPAIR 2 FIG 201.

Part: FRAME — CRACKED (BS 1120) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION CRACK WAS FOUND AT RIGHT TENSION TIE BS 1120 ON TOP FASTENER ROW, 8TH FASTENER HOLE FROM OUTBOARD LOOKING FORWARD. MAINTENANCE REPAIRED PER SRM 53-40-30, REPAIR 1 FIG 201.

Part: SKIN — CRACKED (FUSELAGE) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION FOUND CRACK ON 01 HOLE ON SKIN AT STA 984 STRINGER 38R UNDER LOWER DRAG SPLICE FITTING. MAINTENANCE REPAIRED AS PER PRI 503072-14AD REV 0 TO REV 3 DATED 26 MAY 2012. PRI 503072-14AD REV 0 TO REV 3 FOUND IN COMPLIANCE WITH ER/A 503072-14AD

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION, FOUND HORIZONTAL STABILIZER COMPT BS 2598 BULKHEAD LEFT LOWER AFT INNER CHORD CRACKED. MAINTENANCE REPAIRED HORIZONTAL STABILIZER COMPT BS 2598 BULKHEAD LT LOWER AFT INNER CHORD AS PER PRI 503068-14AD REV 0 DATED 23 MAY 2012 16 00 HRS. PRI 503068-14AD REV 0 FOUND IN COMPLIANCE WITH ER/A 503068-14AD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION FOUND AFT CARGO DOOR SILL AREA, ONE FLOORBEAM UPPER TEE WITH CORROSION. NEW TEE FABRICATED PER DWG 65B04331 REV F. INSTALLED TEE PER SRM 51-40-02.

Part: STRUCTURE — CRACKED (NR 2 SPOILER) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION FOUND NR 2 SPOILER CRACKED. NR 2 SPOILER REPLACED PER AMM 27-61-02.

Part: STRUCTURE — CRACKED (NR 6 SPOILER) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION FOUND NR 6 SPOILER CRACKED. NR 6 SPOILER REPLACED PER AMM 27-62-01.

Part: FLOORBEAM — CORRODED (BS 1840 RBL 56) · airframe 96,421 hrs · 12,004 cycles

AFT CARGO DOOR SILL FLOORBEAM UPPER CHORD CORRODED OUT OF LIMITS STATION 1840 RBL 56.

Part: FRAME — CRACKED (BS 1000) · airframe 69,421 hrs · 12,004 cycles

DURING INSPECTION, FOUND CRACK AT BS 1000 BULKHEAD FRAME AT S38R. REPAIRE IAW WORK CARD.

Part: SKIN — CRACKED (BS 984) · airframe 96,421 hrs · 12,004 cycles

DURING INSPECTION FOUND CRACK INDICATION ON ONE HOLE IN SKIN AT STA 984 STR-38R UNDER LOWER DRAG SPLICE FTG AS MARKED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 96,001 hrs · 11,953 cycles

DURING A MAINTENANCE VISIT, THE UPPER DECK FLOOR AND CEILING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND PACK M7919 AT DOOR 3L CAUSING THE FAULT. MAINTENANCE REPLACED THE BATTERY PACK AT 3L DOOR. SYSTEM OPERATION WAS NORMAL AFTER THE POWER PACK WAS REPLACED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 96,001 hrs · 11,953 cycles

DURING A MAINTENANCE VISIT, THE 3R DOOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AT 3R DOOR. SYSTEM OPERATION WAS NORMAL AFTER THE POWER SUPPLY WAS REPLACED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 96,001 hrs · 11,953 cycles

DURING A MAINTENANCE VISIT, THE CEILING EMERGENCY LIGHTS ON THE LEFT AND RIGHT SIDE FROM ROWS 22 TO 31 WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND PACK M7919 AT DOOR 3L CAUSING THE FAULT. MAINTENANCE REPLACED THE POWER PACK AT 3L DOOR. SYSTEM OPERATION WAS NORMAL AFTER THE POWER PACK WAS REPLACED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 95,888 hrs · 11,939 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY LIGHT AT FIRST/SECOND OF THE OVERWING ESCAPE SLIDE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. SYSTEM OPERATION WAS NORMAL AFTER THE BATTERY WAS REPLACED. (2012-00101)

Part: BATTERY — DISCHARGED (CABIN) · airframe 95,457 hrs · 11,890 cycles

DURING A MAINTENANCE VISIT, THE OVERHEAD EXIT EMERGENCY SIGNAL THE LEFT EXIT DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE BATTERY DEAD ON THE POWER SUPPLY AND REPLACED IT. SYSTEM OPERATION WAS NORMAL AFTER THE BATTERY WAS REPLACED.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 93,970 hrs · 11,702 cycles

DURING A MAINTENANCE VISIT, THE EMERGENCY EXIT PATH LIGHTS AT SEATS 26C AND 60C WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY PATH LIGHT AT 60C AND RECONNECTED THE LIGHT AT 26C. SYSTEM OPERATION WAS NORMAL AFTER THE EMERGENCY PATH LIGHT WAS REPLACED AND RECONNECTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 93,970 hrs · 11,702 cycles

DURING A MAINTENANCE VISIT THE EMERGENCY EXIT PATH LIGHT FROM ROWS 1 THROUGH 4 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY PATH LIGHT AT 4R. SYSTEM OPERATION WAS NORMAL AFTER THE LIGHT WAS REPLACED.

Part: CONTROLLER — MALFUNCTIONED (GALLEY) · airframe 93,527 hrs · 11,647 cycles

DURING FLIGHT, OVEN NR 2 IN GALLEY NR 1 EMITTED SMOKE UNTIL THE CIRCUIT BREAKER WAS PULLED. ELECTRIC SMELL WAS NOTED AS WELL. MAINTENANCE CHECKED THE OVEN CONTROLLERS AND OVENS AND REPLACED THE NR 2 OVEN CONTROLLER. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 91,900 hrs · 11,454 cycles

CREW FOUND THE EMERGENCY PATH LIGHT, GALLEY UNIT NR 1, AFT CENTER TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE LIGHT ASSEMBLY. SYSTEM OPERATION WAS NORMAL.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 91,797 hrs · 11,442 cycles

DURING A MAINTENANCE VISIT THE EMERGENCY FLOOR AT ZONE A WAS FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED WIRES AT SEAT 4J. SYSTEM OPERATION CHECKED NORMAL AND AIRCRAFT GOOD FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,489 hrs · 11,284 cycles

DURING A LINE CHECK, MAINTENANCE FOUND THE DOOR 2R EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD. (2010-00841)

Part: SHEAR BEAM — DAMAGED (FUSELAGE) · airframe 88,045 hrs · 10,973 cycles

DURING L-CHECK, DOOR NR 5, CREW REST SHEAR BEAM MODIFICATION FOUND SHORT EDGE MARGIN ON BEAM. REPAIRED IAW ERA 480405-14AD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,702 hrs · 10,925 cycles

DURING LAYOVER CHECK, MX FOUND DR4R2 LAV EMERGENCY FLOOR PROXIMITY LIGHTS INOPERATIVE. MX REPLACED THE FLOOR PROXIMITY LIGHT. OPS CHECK WAS GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 87,073 hrs · 10,855 cycles

DURING OVERNIGHT CHECK, MAINTENANCE FOUND DOOR 4 RIGHT EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED M7922 POWER SUPPLY WITH BATTERY AND SECURED CONNECTIONS D11418P & D13637. OPERATIONAL CHECKS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 85,022 hrs · 10,628 cycles

DURING OVERNIGHT CHECK FOUND OVERWING LEFT SIDE 2 EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DENTED (BS 260 S34L)

DURING TURN AROUND, CHECK A SHARP DENT WAS FOUND IN THE LAP SPLICE UPPER SKIN AT BS 260, S34L. REPAIRED IAW EA63-215127, SECTION II REQUIRES REPEAT INSP NOT TO EXCEED 15,000 FLIGHT CYCLES THEN REPEAT AT 1500 FLIGHT CYCLE INTERVALS. (K)

Part: POWER SUPPLY — DISCHARGED (CABIN)

DURING OVERNIGHT CHECK FOUND 2 EXTERIOR EMERGENCY LIGHTS ON THE LT SIDE INOP. MX REMOVED AND REPLACED PWR SUPPLY. OPS CHECKED GOOD, AND ACFT WAS RETURNED TO SERVICE. (K)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

DURING OVERNIGHT CHECK FOUND UPPER DECK MIDDLE EXIT SIGNS ILLUMINATED WHEN EMERGENCY LIGHT SWITCHED TO OFF POSITION. MX REMOVED AND REPLACED POWER SUPPLY. OPS CHECKED GOOD AND ACFT WAS RETURNED TO SERVICE. (K)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,861 hrs · 10,360 cycles

DURING OVERNIGHT CHECK FOUND UPPER DECK EMERGENCY EXIT SIGN OVER RT EMERGENCY EXIT DOOR IS INOP. MX R&R POWER SUPPLY AND BATTERY PACK. OPS CHECKED GOOD AND ACFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,861 hrs · 10,360 cycles

UPPER DECK OVERHEAD EMERGENCY EXIT SIGN INOP. MX R&R POWER SUPPLY AND BATTERY PACK. OPS CHECKED GOOD AND ACFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,016 hrs · 9,451 cycles

DURING OVERNIGHT LINE CHECK, EMERGENCY LIGHTS AT ROWS 1 TO 4 RIGHT SIDE WERE INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,058 hrs · 9,319 cycles

DURING "M" CHECK, FOUND CRACK IN LT FRAME WEB AT BS 1265 STRINGER 26L. REPAIRED PER EA 63-208883 SECTION I. REPETITIVE INSPECTIONS PER SECTION II TO BE ACCOMPLISHED EVERY 2000 CYCLES. SECTION III WILL BE BASED ON SECTION II FINDINGS.

Part: FRAME — CRACKED (PYLON) · airframe 75,054 hrs · 9,313 cycles

DURING "M" CHECK, FOUND CRACK IN AFT LOWER SIDE OF PYLON FRAME OUTBOARD CUTOUT FOR PANEL 484ER. REPAIRED PER EA 63-208900.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,058 hrs · 9,319 cycles

DURING "M" CHECK, FOUND CRACK ON THE BS 1256 FRAME WEB AT STRINGER 26R. INTERIM REPAIR WAS ACCOMPLISHED PER SECTION I OF EA 63-208895. REPETITIVE INSPECTIONS PER SECTION II TO BE ACCOMPLISHED EVERY 2000 CYCLES. SECTION III WILL BE BASED ON SECTION II FINDINGS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,058 hrs · 9,319 cycles

DURING "M" CHECK, FOUND CRACK ON BS 340 BL 0 FRAME. REPAIRED PER EA 63-208887.

Part: DOOR FRAME — CORRODED (BS 1990) · corrosion level 2 · airframe 75,058 hrs · 9,319 cycles

DURING "M" CHECK, FOUND CORROSION ON BULK CARGO DOOR REVEAL WEB AT BS 1990. REPAIRED PER EA 63-208888.

Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 75,058 hrs · 9,319 cycles

DURING "M" CHECK, FOUND CRACK IN BS 1220 RT TENSION TIE DOUBLER AT STRINGER 8R AND STRINGER 9R AND A EXISTING TRIM OUT ON THE FRAME DOUBLER AT STRINGER 9R. REPAIRED PER EA 63-208886 SECTION I AND II.

Part: SKIN — CRACKED (LT NACELLE) · airframe 75,054 hrs · 9,313 cycles

DURING "M" CHECK, FOUND CRACK IN NR 4 PYLON LT INBOARD SKIN NAC STA 276, NWL 170, PANEL 482EL CUTOUT. REPAIRED PER EA 63-208898.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 74,706 hrs · 9,270 cycles

DURING OVERNIGHT CHECK, SEVERAL EMERGENCY LIGHTS INOP. UPPER DECK FLOOR. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL SYSTEM — MALFUNCTIONED (SPOILERS) · airframe 70,978 hrs · 8,785 cycles

DURING CLIMB, THERE WAS A TOTAL LOSS OF HYDRAULIC SYSTEM NR 2. FOLLOWED COM PROCEDURE. CONTINUED ON TO DESTINATION PER DISPATCH, AND LANDED WITHOUT INCIDENT. NGO MAINTENANCE REMOVED AND REPLACED NR 10 SPOILER CONTROL PACKAGE, AND ENG HYDRAULIC PUMP. OPERATIONAL CHECK GOOD, A/C RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,725 hrs · 8,753 cycles

DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS FROM NOSE TO DR 2 RT INOP. REPLACED POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK GOOD. A/C RETURNED TO SERVICE.

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,302 hrs · 7,827 cycles

DURING LINE CHECK, FOUND D-ZONE RIGHT AND E-ZONE LEFT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED WIRING AT 43J AND DOOR 4L. OPERATIONAL CHECK GOOD.

Part: WIRE — DAMAGED (CABIN) · airframe 59,848 hrs · 7,409 cycles

DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE AFT OF DOOR 1R. REPAIRED WIRE. OPERATIONAL CHECK GOOD.

Part: MOTOR — BURNED (Zone 900) · airframe 57,189 hrs · 7,063 cycles

During flight a flight attendant reported an electrical fume odor coming from galley elevator when in overide position. Aircraft continued to destination and landed without incident. Replaced elevator motor actuator. Operational check good.

Part: WIRE — DISCONNECTED (CABIN) · airframe 56,226 hrs · 6,941 cycles

DURING LINE CHECK (PEK), FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 22C - 31C AND FROM 21A - 31A. RECONNECTED WIRE AND SECURED ADAPTER. OPERATIONAL CHECK GOOD.

Part: SKIN — CRACKED (PYLON) · airframe 49,509 hrs · 6,108 cycles

DURING H-CHECK FOUND CRACK ON NUMBER ONE PYLON SKIN AT NACELLE STATION 293. REPAIRED PER EA 63-183398.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,509 hrs · 6,108 cycles

During H-check found corrosion on crown of seat track at BS 1080 LBL 12. Repaired per EA 63-182922.

Part: WIRE — DISCONNECTED (CABIN) · airframe 49,318 hrs · 6,083 cycles

DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE BETWEEN ROWS 25ABC-31ABC. MAINTENANCE RECONNECTED LOOSE WIRING. OPERATIONAL CHECK NORMAL.

Part: SEQUENCE VALVE — MALFUNCTIONED (MLG) · airframe 46,886 hrs · 5,777 cycles

DURING CLIMB AFTER RETRACTING THE LANDING GEAR, RECEIVED A LANDING GEAR DOOR EICAS MESSAGE. PERFORMED COCKPIT OPERATION MANUAL PROCEDURE, RECYCLED THE LANDING GEAR, AND PERFORMED COCKPIT OPERATION MANUAL PROCEDURE AGAIN AND EACH TIME A DIFFERENT LANDING GEAR DOOR WOULD NOT CLOSE. AIRCRAFT DUMPED FUEL AND RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE MAIN LANDING GEAR UPLOCK SEQUENCE VALVE AND RIGHT WING LANDING GEAR ALTERNATE EXTEND ACTUATOR. OPERATIONAL CHECK GOOD.

Part: FIRE DETECTOR — MALFUNCTIONED (MLG WW)

DURING TAKEOFF, THE WHEEL WELL FIRE WARNING ACTIVATED. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. REPLACED FIRE LOOPS M694, M693, M692, AND M691. OPERATIONAL CHECK GOOD..

Part: RELAY — FAILED (WHEEL WELL)

DURING TAKEOFF, THE WHEEL WELL FIRE WARNING ACTIVATED. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. REPLACED R8048 RELAY. OPERATIONAL CHECK OK.

Part: RELAY — FAILED (MLG WW)

DURING TAKEOFF, THE WHEEL WELL FIRE WARNING ACTIVATED. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. REPLACED R8048 RELAY. OPERATIONAL CHECK GOOD.

Part: WIRE — FAILED (CABIN)

DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE AT 43C, 9J, AND L1 LAV. REPAIRED WIRING. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING LINE CHECK, FOUND UPPER DECK AFT FLOOR EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK GOOD.

Part: WIRE — LOOSE (CABIN)

DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 25R TO 30R, 51L TO 55L, AND AT DOOR 3L. RECONNECTED WIRES, OPERATIONAL CHECK GOOD.

Part: WIRE — FAILED (CABIN)

DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE AT DOOR 4R. REPAIRED WIRING, OPERATIONAL CHECK GOOD.

Part: CONTROL MECH — OUT OF ADJUST (SPOILER SYST)

DURING TAKEOFF, RECEIVED A SPOILER CONFIGURATION TAKEOFF WARNING. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE. ADJUSTED THE SPEED BRAKE CONTROL SYSTEM AND REPLACED THE AUTO SPEED BRAKE ACTUATOR, OPERATIONAL CHECK GOOD.

Part: SWITCH — MALFUNCTIONED (LT MLG)

DURING TAKEOFF, RECEIVED A GEAR CONFIGURATION TAKEOFF WARNING MESSAGE. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE. RESEATED THE RIGHT ACTUATOR SWITCH ON THE LEFT BODY LANDING GEAR. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — LOOSE (CABIN)

DURING LINE CHECK, FOUND RIGHT 'E' ZONE FLOOR PATH EMERGENCY LIGHTS AND DOOR 3R EMERGENCY LIGHT INOPERATIVE. RECONNECTED ELECTRICAL CONNECTORS, OPERATIONAL CHECK OK.

Part: ANTENNA — DEFECTIVE (FWD FUSELAGE)

DURING CRUISE, BOTH WEATHER RADARS BECAME INOPERATIVE. AIRCRAFT DIVERTED TO KIX AND LANDED WITHOUT INCIDENT. REPLACED THE WEATHER RADAR DRIVE UNIT AND ANTENNA. OPERATIONAL CHECK GOOD.

Part: WIRE — FAILED (CABIN)

DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 35 TO 45C. REPAIRED WIRE, OPERATIONAL CHECK GOOD.

Part: CONNECTOR — LOOSE (CABIN)

DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 35ABC - 42ABC AND FROM ROWS 24HJK - 31HJK. RECONNECTED CONNECTOR. OPERATIONAL CHECK GOOD.

Part: WIRE — LOOSE (CABIN)

DURING LINE CHECK, FOUND EMERGENCY FLOOR PATH LIGHTS INOPERATIVE FROM ROWS 35C TO 42C, SEAT 3R, SEAT 4R, BY LAV 1L, AND BY GALLEY 3 AFT CENTER DIVIDER. RECONNECTED WIRES AND REPLACED LIGHT ASSEMBLIES, OPERATIONAL CHECK GOOD.

Part: WIRE — LOOSE (CABIN)

DURING LINE CHECK, FOUND EMERGENCY FLOOR PATH LIGHTS INOPERATIVE FROM ROWS 35L-42L. RECONNECTED WIRE. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING LINE CHECK, FOUND UPPER DECK EMERGENCY FLOOR PATH LIGHTS INOPERATIVE FROM ROWS 72 TO 75. REPLACED BATTERY PACK, OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (CABIN)

DURING LINE CHECK, FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE AT DOORS 3L AND 2L. REPAIRED BROKEN WIRE. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

DURING LINE CHECK, FOUND EMERGENCY LIGHTS AT DOOR 4R AND 2L INOPERATIVE. REPAIRED PIN AND WIRING, OPERATIONAL CHECK GOOD.

Part: CONNECTOR — LOOSE (CABIN)

DURING LINE CHECK, FOUND THE RIGHT EMERGENCY FLOOR TRACK LIGHTING FROM ROWS 51 TO 55 INOPERATIVE. RECONNECTED TERMINALS AND OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (CABIN)

DURING LINE CHECK, FOUND EMERGENCY LIGHTS FROM ROWS 35ABC TO 42ABC INOPERATIVE. REPAIRED BROKEN WIRE AND OPERATIONAL CHECK GOOD.

Part: CONNECTOR — LOOSE (CABIN)

DURING LINE CHECK (TPE), THE FLOOR MOUNTED EMERGENCY LIGHT AT SEAT ROWS 24 TO 31 WERE FOUND INOPERATIVE. RECONNECTED LIGHT ASSEMBLY AT SEAT 24. OPERATIONAL CHECK OK.

Part: CONNECTOR — LOOSE (CABIN)

DURING LINE CHECK, THE FLOOR EMERGENCY PATH LIGHTS BETWEEN SEAT ROWS 35R TO 42R WERE FOUND INOPERATIVE. RECONNECTED EMERGENCY LIGHT CONNECTOR PIN. OPERATIONAL CHECK OK.

Part: CONNECTOR — LOOSE (CABIN)

DURING LINE CHECK, THE EMERGENCY PATH LIGHTS AT SEAT ROWS 52R TO 56R WERE FOUND INOPERATIVE. RECONNECTED LIGHT ASSEMBLY PIN IN FLOOR TRACK AND OPERATIONAL CHECK OK.

Part: EEL CONNECTOR — LOOSE (CABIN)

DURING LINE CHECK, THE FLOOR PATH EMERGENCY LIGHTS BETWEEN SEAT ROWS 36L TO 42L WERE FOUND INOPERATIVE. RECONNECTED LOOSE CONNECTOR PINS AT ROW 36L AND OPERATIONAL CHECK OK.

Part: CONTL HANDLE — MALFUNCTIONED (LANDING GEAR)

DURING CLIMB, THE LANDING GEAR WOULD NOT RETRACT. CYCLED GEAR HANDLE, SELECTED OVERRIDE AND GEAR RETRACTED NORMALLY. AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE LANDING GEAR CONTROL HANDLE MODULE, RELAY R127, SWITCH S1340, AND THE LANDING GEAR CONTROL MODULE. OPERATIONAL CHECK OK.

Part: SUPPORT — CORRODED (FS 980-1000)

DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE FLOOR BEAM AT FS 980 - 1000, RBL 20 - 30. REPLACED INTERCOSTAL AND REPAIRED PER EA 63-97992.

Part: WEB — DAMAGED (FS 540)

DURING PERIODIC INSPECTION, FOUND FORWARD CARGO COMPARTMENT WEB DAMAGED AT FS 540, RBL 50. REMOVED DAMAGE AND INSTALLED DOUBLER.

Part: FLOOR BEAM — DENTED (FS 720)

DURING PERIODIC INSPECTION, FOUND THE FORWARD CARGO FLOOR BEAM DENTED AT FS 720, LBL 54. REPAIRED FLOOR BEAM PER DRAWING 6A-53-38129.

Part: FLOOR BEAM — CRACKED (FS 660)

DURING PERIODIC INSPECTION, A CRACK WAS FOUND ON THE FLOOR BEAM SPLICE PLATE AT FS 660, LBL 5. REPLACED SPLICE PLATE.

Part: FLOOR BEAM — CORRODED (FS 980)

DURING PERIODIC INSPECTION, FOUND CORROSION ON THE UPPER DECK FLOOR BEAM FAIL SAFE STRAP AT FS 980, RBL 16 - RBL 34. REMOVED DAMAGE AREA AND INSTALLED REPAIR DOUBLERS AND STRAP PER EA 63-97992.

Part: SEAT TRACK — CORRODED (FS 2265-2270)

DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE SEAT TRACK AT FS 2265 TO 2270, RBL 34. REMOVED CORROSION AND INSTALLED REPAIR STRAP PER EA 63-97884.

Part: DOORS — CORRODED (LT WING)

DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE SEALING FLANGES OF THE LEFT LOWER WING FUEL ACCESS DOORS 545BB, 553JB, 553HB, 553DB, 553CB, AND 556DB. REPLACED ACCESS DOORS.

Part: SUPPORT — CRACKED (WS 547)

DURING PERIODIC INSPECTION, A CRACK WAS FOUND ON THE LEFT WING INBOARD TRAILING EDGE LATERAL SUPPORT AT PANEL 572BB TO WS 547. STOP DRILLED AND INSTALLED DOUBLER.

Part: SUPPORT — CORRODED (FS 820-920)

DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE FLOOR SUPPORT AT FS 820 TO 920, LBL 38. REMOVED CORROSION AND INSTALLED REPAIR PER EA 63-97882.

Part: SEAT TRACK — CORRODED (FS 480-885)

DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE SEAT TRACK AT FS 480 TO 885, RBL 75. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FS 1640-1670)

DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE SEAT TRACK AT FS 1640 TO 1670, LBL 75. REPLACED SEAT TRACK.

Part: SUPPORT — CORRODED (FS 2276)

DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE FLOOR SUPPORT AT FS 2276, LBL 20 TO 30. REPLACED FLOOR SUPPORT.

Part: SEAT TRACK — CORRODED (FS 800-815)

DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE SEAT TRACK AT FS 800 TO 815, LBL 98. REPLACED SEAT TRACK.

Part: CHANNEL — CORRODED (FS 995)

DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE HAT CHANNEL AT FS 995, LBL 15 IN THE UPPER DECK GALLEY AREA. REPLACED HAT CHANNEL.

Part: FLOORBEAM — CORRODED (FS 980)

DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE FLOORBEAM AT FS 980, RBL 33 TO 75. REMOVED CORROSION AND INSTALLED REPAIR STRAP.

Part: SUPPORT — DAMAGED (LEFT WING LE)

DURING LINE CHECK (KIX), DAMAGE WAS FOUND ON THE LEFT WING LEADING EDGE LOWER PANEL SUPPORT AT WS 838 AND THE OUTBOARD FUELING DOOR. REPLACED DOOR AND SUPPORT.

Part: SKIN — CRACKED (NR 1 ENG PYLON)

DURING OVERNIGHT LINE CHECK, A CRACK WAS FOUND ON THE NR 1 ENGINE PYLON INBOARD SKIN AT THE FORWARD UPPER CORNER OF THE NR 452 PANEL CUTOUT. STOP DRILLED CRACK AND REPAIRED PER EA 63-96730.