N1402A

Part: HINGE FITTING — GOUGED (NR 2 NACELLE) · airframe 84,250 hrs · 30,199 cycles

NR 2 ENGINE, OTBD CORE COWL, CENTER HINGE FITTING WAS GOUGED ON THE FORWARD SIDE. FOUND TO BE OUT OF LIMITS IAW SRM 54-53-90, COMPLIED WITH ER/A 572646-14.

Part: STRUCTURE — CRACKED (BS 1809) · airframe 84,250 hrs · 30,199 cycles

BHEC INSPECTION OF BS 1809 RT OUTER STRUCTURE, SHOWS CRACK INDICATIONS AT 3 HOLE LOCATIONS. COMPLIED WITH E/RA 572634-14.

Part: SKIN — CRACKED (BS 1654.5) · airframe 82,006 hrs · 29,690 cycles

DURING SERVICE CHECK, FUSELAGE SKIN AT BS 1654.5, STRINGER 13L FOUND CRACKED. REMOVED THE DAMAGED AREA, PERFORMED EDDY CURRENT, AND INSTALLED A REPAIR DOUBLER AND FILLER IAW SRM 53-80-01, REPAIR 7.

Part: ANGLE — CRACKED (BULKHEAD) · airframe 81,798 hrs · 29,621 cycles

FUSELAGE BULKHEAD BS 1809.5 LEFT HALF AFT OUTER ANGLE CRACKED. COMPLIED WITH ERA 566145-14AD.

Part: FITTING — CRACKED (BS 1809) · airframe 81,798 hrs · 29,621 cycles

REMOVED AND REPLACED THE LT INNER TENSION FITTING AT BS 1809 DUE TO CRACKING. COMPLIED WITH ERA 566145-14AD.

Part: STRINGER — CRACKED (NOT REPORTED) · airframe 81,798 hrs · 29,621 cycles

LOWER AFT HOLE HAS CRACK INDICATIONS. REPAIRED IAW ERA 566145-14.

Part: SKIN — CRACKED (BS 1654.6) · airframe 81,798 hrs · 29,621 cycles

FUSELAGE SKIN CRACKED AFT OF BS 1654.50, STRINGER 13R. REPAIRED IAW ERA 566160-14.

Part: SLIDE — UNWANTED DEPLOY (RIGHT OVERWING) · airframe 81,777 hrs · 29,614 cycles

RIGHT SIDE OVER WING SLIDE DEPLOYED. REPLACED SLIDE. SYSTEM OPERATION IS NORMAL.

Part: COOLING FAN — FAILED (EQUIPMENT) · airframe 80,091 hrs · 29,170 cycles

SMOKE IN COCKPIT, FOLLOWED BY FORWARD EQUIPMENT EXHAUST FAN STATUS MESSAGE. FOUND EQUIPMENT COOLING FAN INOPERATIVE AND REPLACED.

Part: SEAT TRACK — CORRODED (BS 852) · corrosion level 2 · airframe 79,619 hrs · 29,055 cycles

CORROSION ON RBL 74.75 SEAT TRACK AT BS 852. REPLACED THE SEAT TRACK.

Part: SKIN — CORRODED (BS 1219) · airframe 79,619 hrs · 29,055 cycles

FUSELAGE SKIN BULGING WITH FASTENERS PULLING, BS 1219, STRINGER 32L, APPROXIMATLEY 8 INCH AREA, 12 INCHES AFT OF PREVIOUS REPAIR. REPAIRED IAW ERA 558384-14.

Part: SEAT TRACK — CORRODED (BS 852) · corrosion level 2 · airframe 79,619 hrs · 29,055 cycles

CORROSION ON SEAT TRACK, RBL 88.5, BS 852. REPLACED THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 852) · corrosion level 2 · airframe 79,619 hrs · 29,055 cycles

CORROSION ON RBL 33 SEAT TRACK, BS 852. REPLACED THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 852) · corrosion level 2 · airframe 79,867 hrs · 29,123 cycles

FOUND CORROSION ON SEAT TRACK, RBL 54.75, BS 852, REPLACED.

Part: STRINGER SPLICE — CORRODED (BS 1219-1241) · airframe 79,619 hrs · 29,055 cycles

STRINGER SPLICE 34L, BS 1219 - 1241 CORRODED. REPAIRED IAW ERA 558384-14.

Part: WIRE — OPEN (CABIN) · airframe 78,470 hrs · 28,682 cycles

RED EMERGENCY LIGHT AT DOOR 1R CLOSET WALL INOPERATIVE. FOUND OPEN WIRES AT FLOOR SPLICED IN LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 78,249 hrs · 28,614 cycles

R1 DOOR SLIDE LIGHT INOPERATIVE. MAINTENANCE REPLACED SLIDE LIGHT ASSEMBLY AND ADJUSTED TO SECURE LENS WITHIN LIGHT. SYSTEM OPERATION IS NORMAL.

Part: LENS — WRONG PART (EMERGENCY LIGHT) · airframe 78,194 hrs · 28,599 cycles

EMERGENCY ESCAPE LIGHTS AT SEAT 26B LENS INCORRECT COLOR. REPLACED CLEAR LENS WITH RED LENS. SYSTEM OPERATION IS NORMAL.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 78,249 hrs · 28,614 cycles

DURING SERVICE CHECK FOUND A FLOOR PANEL CRACKED IN AFT CARGO AT STA 1200 BETWEEN RBL 20.5 AND 44.0 RT SIDE. C/W ERA 552002-14.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 75,518 hrs · 27,947 cycles

EMERGENCY EXIT LIGHT AT 29AB ARE INOPERATIVE. MAINTENANCE RECONNECTED WIRE AT CONNECTOR. SYSTEM OPERATION IS NORMAL.

Part: ELECTRICAL BOX — CONTAMINATED (SEAT) · airframe 73,856 hrs · 27,535 cycles

F/A REPORTED ELECTRICAL ODOR IN FIRST CLASS NEAR SEAT 4AB. TROUBLESHOT ENTIRE FIRST CLASS SECTION FOR ELECTRICAL ODOR, NONE FOUND. SUSPECT PASSENGER CHARGING UNIT. REPLACED VIDEO SEAT ELECTRIC BOX UNDER ROW 3A/D DUE TO EVIDENCE OF LIQUID SPILLAGE ON UNIT. REPLACED VSEB. SYSTEM OPERATION IS NORMAL.

Part: FLOOR SUPPORT — CORRODED (BS 852-915) · airframe 72,702 hrs · 27,285 cycles

CABIN FLOOR SUPPORT UPPER CHORD CORRODED AT RBL 33.06, BS 852-915. REPAIRED IAW SRM 53-00-51.

Part: FLOOR SUPPORT — CORRODED (BS 852) · corrosion level 2 · airframe 72,702 hrs · 27,285 cycles

CABIN FLOOR SUPPORT UPPER CHORD CORRODED AT RBL 74.18 AND BS 852. REPAIRED IAW SRM 53-00-51.

Part: FLOOR SUPPORT — CORRODED (BS 852-903) · corrosion level 2 · airframe 72,702 hrs · 27,285 cycles

CABIN FLOORBEAM UPPER TEE CORRODED AT RBL 54.81, BS 852-903. REPAIRED IAW SRM 53-00-51.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 72,226 hrs · 27,170 cycles

FOUND EMERGENCY LIGHTS ROWS 1 AB - 12 FG INOPERATIVE. MAINTENANCE REPLACED BLOWN FUSE. SYSTEM OPERATION IS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,905 hrs · 26,618 cycles

LEFT EXTERIOR EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENENACE REPLACED THE POWER SUPPLY M738.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,668 hrs · 26,094 cycles

EMERGENCY ESCAPE PATH LIGHT AT MID LAV AREA UNDER F/A SEAT INOPERATIVE. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT ASSY. CHECKED NORMAL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 66,219 hrs · 25,734 cycles

EMERGENCY EXIT LIGHT AT SEAT 20G INOPERATIVE. MX RECONNECTED MATE-N-LOCK CONNECTOR AT LAMP ASSY. SYS OPS IS NORMAL.

Part: SPAR WEB — CANNING (NR 2 PYLON) · airframe 65,887 hrs · 25,657 cycles

NR 2 PYLON MID SPAR WEB FOUND OIL CANNING AND DEEP CHAFING AT LT SIDE, REPAIR CARRIED OUT IAW ERA 514639-14.

Part: LONGERON FITTING — CRACKED · airframe 65,856 hrs · 25,650 cycles

CRACK INDICATION FOUND APPROX 0.3" IN LENGTH DURING HFEC ON RT SIDE UNDERWING LONGERON FITTING. FITTING REPAIRED IAW ER/A 514635-14AD.

Part: FITTING — DAMAGED (NR 2 PYLON) · airframe 65,887 hrs · 25,657 cycles

DURING HFEC OPEN HOLE INSPECTION ON RT WING NR 2 PYLON AFT DIAGONAL BRACE FITTING, FOUND OTBD FASTENER HOLE (01 EA) WITH HOLE EDGE DAMAGE ON LOWER WING SURFACE SIDE. OTBD FASTENER HOLE DAMAGE REWORKED IAW PRI 514643-14AD, REV 0 AND REV 1.

Part: FITTING — CRACKED (NR 2 PYLON) · airframe 65,887 hrs · 25,657 cycles

NR 2 PYLON CRACK INDICATION FOUND ON RT UPPER LINK PITCH LOAD FITTING AT MOST OTBD AFT FASTENER HOLE REPAIRED IAW PRI 514654-14AD, REV 0, REV 1, REV 2 AND REV 3. REPAIR COMPARED AND COMPLIED WITH ER/A 514654-14AD.

Part: FAILSAFE — CRACKED (BS 955) · airframe 65,856 hrs · 25,650 cycles

ULTRASONIC INSPECTION FOUND CRACK INDICATION AT LT BS 955, FAILSAFE STRAP AT LOWER OF THE 3 FASTENER HOLES. 3 FASTENER HOLES REPAIRED IAW PRI 514031-14AD, REV 0. REPAIR COMPARED AND COMPLIED WITH FINAL ER/A 514031-14AD.

Part: FAILSAFE — CRACKED (BS 955) · airframe 65,856 hrs · 25,650 cycles

ULTRASONIC INSPECTION, FOUND CRACK INDICATION AT RT BS 955, FAILSAFE STRAP AT LOWER OF THE THE 3 FASTENER HOLES REPAIR COMPARED AND COMPLIED WITH ER/A 514032-14AD REV ORIGINAL.

Part: SKIN — CORRODED (RT WING) · airframe 65,856 hrs · 25,650 cycles

RT WING UPPER FILLET AREA-CORROSION FOUND ON WING UPPER SURFACE BELOW BRACKET, WITHIN FILLET AREA AT WBL 101 TO WBL 102.5 AND FWD OF RT WING REAR SPAR 22.5" TO 23.5". REPAIR CARRIED OUT IAW PRI 514645-14.

Part: SKIN — CORRODED (RT WING) · airframe 65,856 hrs · 25,650 cycles

FOUND ON RT WING UPPER SURFACE, WITHIN FILLET AREA AT WBL 102 TO WBL 106 AND 11" FWD OF RT WING REAR SPAR. REPAIR COMPARED AND COMPLIED WITH FINAL ER/A 514645-14.

Part: SKIN — CRACKED (RT WING) · airframe 65,887 hrs · 25,657 cycles

NR 2 PYLON, CRACK INDICATION FOUND ON RT UPPER WING SKIN LOAD FITTING AT MOST OTBD AFT FASTENER HOLE. WORK CARRIED OUT IAW PRI 514654-14AD, REV 0, REV 1 AND REV 2 AND REV 3.

Part: FRAME — CRACKED (BS 859.5) · airframe 65,856 hrs · 25,650 cycles

CRACK INDICATION FOUND ON FRAME DURING HFEC INSPECTION ON LT BS 859.5, LBL 89, WL 200 FRAME INNER CHORD TRANSITION RADIUS APPROX 0.5". FRAME REPAIRED.

Part: SKIN — CORRODED (LT WING) · airframe 65,887 hrs · 25,657 cycles

CORROSION FOUND LT WING UPPER SURFACE AT WBL 101.5 TO WBL 104.5 AND 8.5 INCHES TO 12 INCHES FWD OF LT WING REAR SPAR CORRODED AREA. REPAIR CARRIED OUT IAW PRI 514644-14, REV 0.

Part: SKIN — CORRODED (LT WING) · airframe 65,887 hrs · 25,657 cycles

LEFT WING UPPER FILLET AREA-CORROSION FOUND ON LT WING UPPER SURFACE AT WBL 101 TO WBL 104.5 AND FWD OF LT WING REAR SPAR 14" TO 18.5" AS MARKED. REPAIR CARRIED OUT IAW ER/A 514644-14, REV ORIGINAL.

Part: FRAME — CRACKED (BS 903) · airframe 65,856 hrs · 25,650 cycles

CRACK INDICATION FOUND DURING HFEC INSPECTION ON RT BS 903.5, RBL 89, WL 200 FRAME INNER CHORD TRANSITION RADIUS APPROX 1.0" IN LENGTH. RT BS 903.5, RBL 89, WL 200 FRAME REPAIR CARRIED OUT IAW WC 5311-01195-09-03B.

Part: FRAME — CRACKED (BS 883.5) · airframe 65,856 hrs · 25,650 cycles

CRACK INDICATION FOUND DURING HFEC INSPECTION ON RT BS 883.5, RBL 89, WL 200 FRAME INNER CHORD TRANSITION RADIUS APPROX. 0.5" IN LENGTH AS MARKED. FRAME INNER CHORD REPAIR CARRIED OUT.

Part: SKIN — CORRODED (LT WING) · airframe 65,856 hrs · 25,650 cycles

LT WING UPPER FILLET AREA-CORROSION FOUND ON LT WING UPPER SURFACE BELOW BRACKET, AT WBL 101 TO WBL 103.5 AND FWD OF LT WING REAR SPAR 22" TO 24". REPAIR CARRIED OUT IAW PRI 514644-14, REV 0 AND REV 1.

Part: FRAME — CORRODED (BS 1197) · airframe 65,856 hrs · 25,650 cycles

CORROSION ON CABIN FRAME BS 1197+132 INBD FACE BETWEEN STRINGER 12-13L, CARRIED OUT REPAIR IAW ER/A514973-14.

Part: LONGERON — CORRODED (BS 1540) · corrosion level 2 · airframe 65,856 hrs · 25,650 cycles

LONGERON 38R FOUND CORRODED AT BS 1540. BULK CARGO IAW SRM 53-00-03, FIG 201, REPAIR 2, REV 92. NEW STRINGER ANGLE AND CHANNEL FABRICATED USING MATERIAL 7075-0-0.050" AND 7075-0-0.040" AND INSTALLED REPAIR PARTS AT STA 1510 AND STA 1542 S38R IAW SRM 53-00-03, REPAIR 2.

Part: FRAME — CRACKED (BS 1809 S7-8R) · airframe 65,856 hrs · 25,650 cycles

BS 1809, BULKHEAD RT FWD OUTER CHORD CRACKED AT STR 7-8R, REPAIRED IAW SRM 53-80-08, REPAIR 9.

Part: FRAME — CRACKED (BS 1809 BULKHEAD) · airframe 65,856 hrs · 25,650 cycles

DURING HFEC INSPECTION ON BS 1809 BULKHEAD LT FWD OUTER CHORD AT STR 6L TO 7L FOUND CRACKED. REPAIRED SRM 53-80-08, REPAIR 9, REV 92.00.

Part: FLOORBEAM — CORRODED (BS 1153) · corrosion level 2 · airframe 65,856 hrs · 25,650 cycles

AFT CARGO FLOORBEAM SEVEN AREAS FOUND CORRODED BS 1153, RBL 20-42. REMOVED AND INSTALLED WITH NEW SPLICE IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 347) · corrosion level 2 · airframe 65,856 hrs · 25,650 cycles

CABIN AT STA 347, RBL 55+20 FLOORBEAM UPPER SURFACE FOUND CORRODED. REPAIRED FROM LBL 15 TO RBL 60.

Part: FLOORBEAM — CORRODED (BS 347) · corrosion level 2 · airframe 65,856 hrs · 25,650 cycles

CABIN AT BS 347 RBL 55+20 FLOORBEAM UPPER SURFACE CORRODED. REPAIRED FROM LBL 15 TO RBL 60 IAW SRM 53-00-51, FIG 201, REPAIR 1, REV.

Part: FLOORBEAM — CORRODED (BS 325) · corrosion level 2 · airframe 65,856 hrs · 25,650 cycles

CABIN FLOORBEAM AT STA 325 BETWEEN RBL 20 -54.75 FOUND CORRODED. MX REPAIRED FROM LBL 45 TO RBL 60.

Part: FLOORBEAM — CORRODED (BS 325) · corrosion level 2 · airframe 65,856 hrs · 25,650 cycles

CABIN FLOORBEAM AT BS 325 BETWEEN RBL 20 - 54.75 FOUND CORRODED. REPAIRED FROM LBL 45 TO RBL 60.

Part: FLOORBEAM — CORRODED (BS 347) · corrosion level 2 · airframe 65,856 hrs · 25,650 cycles

CABIN AT BS 347 RBL 55 +20 FLOORBEAM UPPER SURFACE FOUND CORRODED. REPAIRED FROM LBL 15 TO RBL 60.

Part: FLOORBEAM — CORRODED (BS 347) · airframe 65,856 hrs · 25,650 cycles

CABIN AT STA 347 RBL 55 +20 FLOORBEAM UPPER SURFACE FOUND CORRODED. REPAIRED FROM LBL 15 TO RBL 60.

Part: SKIN — CRACKED (BS 1210 S37R) · airframe 63,578 hrs · 25,086 cycles

DURING WALK AROUND CRACK ON FUSELAGE SKIN NOTED AT BS 1210 STR 37R ABOUT 18 IN BELOW AFT CARGO DOOR OPEN/CLOSE SWITCH PANEL. CUT OUT DAMAGE PER B767 SRM 53-00-01 FIG 201. HFEC INSPECTED CUTOUT PER B767 SRM 53-00-01 FIG 201 WITH NO ITEMS. DRILLED REPAIR PARTS PER SRM 53-00-01 FIG 201. INSTALLED REPAIR PER -SRM 53-00-01 FIG 201.

Part: MONITOR — SPARKS (CABIN) · airframe 58,836 hrs · 24,004 cycles

CREW REPORTED SEAT 5D MONITOR IS INOPERATIVE DUE TO SHOOTING SPARKS. MAINTENANCE REMOVED AND REPLACED SEAT 5D SDU MONITOR PER AMM.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 56,994 hrs · 23,595 cycles

EMERGENCY EGRESS AISLE LIGHTING INOPERATIVE FROM ROWS 35 THROUGH 46. SPLICED BROKEN WIRE AT ROW 42, CHECKS OK.

Part: GASPER FAN — MALFUNCTIONED (CABIN) · airframe 55,457 hrs · 23,242 cycles

ACID FUMES REPORTED IN CABIN FOLLOWED BY ILLUMINATION OF GASPER FAN SWITCH OFF LIGHT. SWITCH TURNED OFF AND C/B PULLED. FUMES CLEARED. REMOVED AND REPLACED GASPER FAN AS PER M/M 21-24-01. FAN OPS NML (DL76P101990).

Part: DETECTOR — MALFUNCTIONED (E&E BAY) · airframe 51,776 hrs · 22,424 cycles

EQUIPMENT COOLING OVERHEAT. *** ATB *** T/S PER FIM 21-58-00. FOUND LOW FLOW DETECTOR DAMAGED MFG P/N 11197-5. REPLACED DETECTOR, CHECKED OK. CHECKED CONICAL SCREEN AT SUPPLY FAN AND EXHAUST FAN. NO OBSTRUCTIONS NOT STRUCTIONS AT CAPTS VOR PANEL. NONE NOTED. REP AN PER AMM. SYSTEM OPS CHECKED NORMAL.

Part: FUSE — BLOWN (CABIN) · airframe 51,766 hrs · 22,422 cycles

EXTERIOR EMERGENCY EXIT LIGHT OUT SECOND LIGHT AFT OF LEFT WING. FOUND FUSE BAD ON POWER SUPPLY. REPLACED FUSE SYSTEM, OPS NORMAL.

Part: IDG — MALFUNCTIONED (RT ENGINE) · airframe 51,755 hrs · 22,420 cycles

RIGHT GEN DROPPED OFF LINE AND WOULD RESET. APU UP AND ONLINE. ATB TO SLC FOR MTC. REMOVED AND REPLACED GCU AND R IDG, ALL CHECKS GOOD.

Part: FAN — ODOR (GASPER) · airframe 50,799 hrs · 22,228 cycles

GASPER FAN FAILED OFF FOLLOWING REPORT OF NOISE IN CABIN OVERHEAD. FOLLOWED BY FUNNY ODOR. FOLLOWED BY GASPER SWITCH LIGHT OFF LIGHT ILLUMINATING. THIS RESULTED IN NO MORE NOISE OR SMELLS. TOTAL TIME FROM FIRST REPORT TO LIGHTOFF APPROX 10-15 MIN. TROUBLESHOOT PER FIM. REPLACED GASPER FAN. OPS OK NORMAL.

Part: STARTER — INOPERATIVE (LT ENGINE) · airframe 49,476 hrs · 21,922 cycles

LEFT ENGINE FAILED TO START, EGT STABILIZED AT 290 N2 GOT UP TO 27 PERCENT THEN STARTED TO DECREASE. REPLACED NR 1 ENGINE STARTER PER AMM. CKS GOOD.

Part: LINE — LEAKING (OIL COOLER) · airframe 48,302 hrs · 21,604 cycles

AIRCRAFT ATB FOR NR 2 ENG LOSS OF OIL QTY AND OIL PRESSURE. CREW SHUT DOWN ENGINE PRIOR TO LANDING. T/S IN PROGRESS AIR/OIL COOLER OIL RETURN LINE FOUND CRACKED. REPLACED NR 2 ENGINE.

Part: ENGINE — FAILED (NR 2) · airframe 48,302 hrs · 21,604 cycles

OIL LOSS IN FLIGHT AND IFSD. REPLACED RT ENG PER TRANSMITTAL 1T149AD9.

Part: OIL SYSTEM — LOW (IDG) · airframe 48,176 hrs · 21,570 cycles

ON TAXI OUT, LT GENERATOR OFF FOLLOWED QRD AND GEN RESET.

Part: GENERATOR — MALFUNCTIONED (LEFT) · airframe 47,993 hrs · 21,520 cycles

LEFT ENGINE GEN OFF. STATUS MSGS L ENG EEC C1/TE FLAP SHUTDOWN/HI FLOW INHIBIT, WOULD NOT RESET. RESET EICAS MSGS. NO FAULTS ON BPCU. RAN FLAPS, ALL CKS GOOD.

Part: WIRE — OUT OF POSITION (COCKPIT) · airframe 45,921 hrs · 20,972 cycles

WHEN BASE OF GRIMES LT TOUCHES FOOT SHOULDER HEATER SWITCH SPARKS ARE EMITTED. BOTH CAPT AND F/O SIDE. PULLED CB P-32 TO DEACTIVATE ALL GRIMES LTS FWD TO MCO AND PLACARD PER MEL 33-11-01. DISCONNECTED F/O LIGHT ASSY FRM TERMINAL STRIP FOR CIRCUIT ISOLATION. RECONNECTED F/O LIGHT ASSY TO TERMINAL STRIP. FO WIRES AT TB5100 5102 5104 SWAPPED. REWIRED PER W/D CKS GOOD PER MM. MCO/PLACARD REMOVED.

Part: ENGINE — FAILED (NR 2) · airframe 45,792 hrs · 20,937 cycles

CREW REPORTS LOSING N2 INDICATIONS ALONG WITH A C1 MESSAGE EN ROUTE TO HNL ON FLT 1465. WHEN PMA STATOR REMOVED MTC NOTED THE PMA ROTOR DRIVE HAS FAILED. REPLACED RT ENGINE PMA.

Part: DOOR — MISSING (NR 2 NACELLE) · airframe 43,564 hrs · 20,377 cycles

FOUND BY MTC ON DAILY RELIABILITY/WEEKLY CHECK NUMBER 2 ENGINE PYLON INBOARD STRUT DOOR MISSING. AOG PART 311T3065-127 INSTALLED NEW ACCESS PANEL PER MM.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,146 hrs · 20,276 cycles

RT CEILING EMERGENCY LIGHTS FROM 37EF AFT INOP. SEAT TRACK LIGHTS INOP AFT CABIN RIGHT SIDE ROW 25 EF TO 45EF. REPLACED CHARGER AND BATTERY MODULE NR M737. OPS NORMAL. BATTERY VOLTAGE LOW. REPLACED BATTERY PACK AT M732. OPS CHECKED NORMAL. PART BORROWED FROM NW.

Part: BATTERY — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 43,097 hrs · 20,266 cycles

AFT RIGHT CEILING EMERGENCY LIGHTS AND EXIT SIGNS INOP. REPLACED ONE FUSE AND BATTERY ON M734 POWER SUPPLY TESTS GOOD.

Part: RELAY — INOPERATIVE (RT ENGINE) · airframe 42,864 hrs · 20,210 cycles

RT ENG EEC MODE MESSAGE, RETURN TO BLOCK. T/S PER FIM REPLACED RELAYS K403 AND K670 RAN ENG MESSAGE ERASED.

Part: SKIN — DENTED (BS 1351-1395) · airframe 42,369 hrs · 20,096 cycles

DURING HMV, SEVERAL DENTS AND GOUGES WERE FOUND AND REPAIRED BETWEEN STA 1351 AND 1395, S-26R TO S-33R.

Part: SKIN — DENTED (BS 620-654) · airframe 42,369 hrs · 20,096 cycles

DURING HMV, SEVERAL DENTS, SCRATCHES AND GOUGES WERE FOUND AND REPAIRED FROM STA 620 TO 654, S-26R TO S-33R.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 42,369 hrs · 20,096 cycles

DURING HMV, THE RT HORIZ STAB PIVOT FITTING BEARING WAS FOUND ROTATED. UPON REMOVAL, THE FITTING BORE WAS FOUND CORRODED. FITTING WAS REPAIRED PER BOEING S/B 767-55-0008.

Part: SKIN — DENTED (BS 474 S33-34R) · airframe 42,369 hrs · 20,096 cycles

FUSELAGE SKIN, STA 474, STR 33R-34R DENTED. REPAIRED IAW ERA 461757-14.

Part: SKIN — DENTED (BS 1197) · airframe 42,369 hrs · 20,096 cycles

DURING HMV2 AT BFM, FOUND LT LOWER EXTERNAL FUSELAGE AT STA 1197+ 22 STR 37L DENTED. OUT OF LIMITS PER SRM 53-00-01. REPAIRED PER SRM 53-00-01 REPAIR 12.

Part: FLOORBEAM — CORRODED (BS 287 RBL18) · airframe 42,369 hrs · 20,096 cycles

FWD GALLEY FLOOR SUPPORT TOP SURFACE CORRODED STA 287 RBL18. REPAIRED PER SRM 53-00-51D REF NR 67268820001 STA 287 FLOORBEAM.

Part: FLOORBEAM — CORRODED (STA 740 LBL29-46) · airframe 42,369 hrs · 20,096 cycles

DURING HMV2 AT MAE, FOUND FWD CARGO COMPARTMENT BILGE AREA STA 740 LBL 29-46 FLOOR PANEL SUPPORT ANGLE CORRODED. REPAIRED PER SRM 53-00-07 REPAIR 4.

Part: SKIN — DENTED (BS 1375, S29R) · airframe 38,356 hrs · 18,484 cycles

FUSELAGE SKIN AT STA 1375, STR 29R WAS FOUND DENTED AND GOUGED BEYOND SRM LIMITS, TOO CLOSE TO DOOR OPENING. INSTALLED REPAIR DOUBLER PER ER/A 452043-14

Part: BATTERY — DISCHARGED (1L DOOR) · airframe 34,788 hrs · 16,975 cycles

NR 1 LEFT DOOR EMERGENCY FLASHLIGHT BATTERY LOW. REPLACED BATTERY AND BULB.

Part: FITTING — CORRODED (TE FLAPS) · airframe 32,882 hrs · 15,974 cycles

INSPECTION OF THE COLLAR BOLTS ON THE INBOARD MAIN FLAP COLLAR FITTING (LT & RT) AT THE INBOARD END OF THE FLAP REVEALED CORROSION IN THE HOLE BORES OF THE FITTINGS. THE DAMAGED COLLAR FITTINGS WERE REMOVED AND REPLACED PER BAC S/B 57A0066 AND ER/A 088153-14AD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,029 hrs · 15,045 cycles

DURING L/O CHECK FOUND ALL E-PATH LIGHTS FROM ROW 35 AFT INOP. REPLACED BATTERY SLED M9010 ALL E-PATH LTS OPS CKS NML.

Part: VALVE — LEAKING (FLAP/SLAT) · airframe 30,448 hrs · 14,758 cycles

C-HYD QTY MESSAGE HYD QUANTITY DOWN TO .43. A/C RETURNED TO CVG. FOUND FLAP/SLAT S/O VLV MODUAL LEAKING IN RT W/W. REPLACED SAME PER M/M. REFILLED HYD SYS, NO RII PER TOPP 40-30-05.

Part: ENGINE — STALLED (NR 2) · airframe 29,161 hrs · 14,113 cycles

BETWEEN 100 AND 200 AGL THE RT ENGINE BEGAN TO COMPRESSOR STALL. MAX EGT710. THROTTLE RETARDED AND ENGINE INDICATIONS RETURNED TO NORMAL. REPLACED NR 2 ENGINE

Part: LIGHT — LOOSE (CABIN) · airframe 28,285 hrs · 13,692 cycles

EMERGENCY PATH LIGHTS INOP AT SEAT 4E-38B-42B.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,861 hrs · 13,490 cycles

LT SIDE EXT EMERGENCY LIGHTS INOP. REPLACED M738 BATTERY RACK.

Part: IDG — MALFUNCTIONED (NR 2 ENGINE) · airframe 27,292 hrs · 13,199 cycles

AIR TURNBACK AT 17,000 LVL FLT RIGHT GENERATOR FAILED ALONG WITH AIRFRAME VIBRATION. APU GEN OPER OK. SERVICED RIGHT IDG, RAN ENGINE AND NO VIBRATIONS. NO HISTORY. CREW DID NOT DISCONNECT IDG. DISCONNECTED IDG AND FWD TO MCO/PLC PER MEL 24-00-01.

Part: WIRE — BROKEN (CABIN) · airframe 26,258 hrs · 12,692 cycles

ON L/O FOUND SEAT ROWS 12 AND 17 FG EMERGENCY LIGHTS INOP. FOUND WIRES BROKEN. REPLACED LIGHT ASSEMBLIES, OPN CKS GOOD.

Part: SKIN — DENTED (STA 1373, 1395) · airframe 25,791 hrs · 12,471 cycles

FUSELAGE SKIN DENTED 4" FWD OF STA 1395, AT S-34R AND STA 1373 BETWEEN S-34R AND S-35R. BOTH DAMAGE LOCATIONS ARE TRIMMED OUT AND DOUBLER/TRIPLER INSTALLED. CORRECTIVE ACTION: ER/A 397815-14

Part: TORQUE TUBE — BROKEN (FUSELAGE) · airframe 22,952 hrs · 11,076 cycles

RIGHT WING I/B TORQUE TUBE DOOR BROKEN. REPAIRED DOOR.

Part: WIRE — CHAFED (NR 1 PYLON)

SETUP TO INSPECT EEC WIRING HARNESSES RUNNING THROUGH ENGINE PYLONS FOR ANY CHAFFING OR DAMAGED WIRING. FOUND 3 WIRES CHAFFED IN NR 1 ENGINE PYLON WIRE HARNESS AND COMPLETED TEMPORARY REPAIR OF WIRES PER STANDARD WIRING PRACTICES 20-10-13 PAR 2.

Part: FSEU — MALFUNCTIONED (TE FLAPS)

DURING APPROACH INTO RSW WITH FLAPS 30 SELECTED, FLAP GOT TO 27 DEG THEN STARTED RETRACTING AUTOMATICALLY TO 20 DEG. AIRSPEED WAS AT 155 KTS. RECEIVED FLAP DISAGREE MESSAGE WHEN THIS HAPPENED. DID NOT GET -FLAP LOAD RELIEF- EICAS MESSAGE. ABORTED APPROACH. PERFORMED GO-AROUND AND ALTERNATELY EXTENDED THE FLAPS. MTC FOUND NO RELATED FSEU FAULTS. REPLACED FSEU AND RT ADC AS PRECAUTION.

Part: SWITCH — CORRODED (COCKPIT)

IN LANDING CONFIG, NOSE GEAR GREEN LIGHT WOULD NOT ILLUMINATE. LIGHT WOULD NOT ILLUMINATE WHEN LIGHTS TEST BUTTON PUSHED, BUT WOULD ILLUMINATE WITH PUSHING THE LIGHT. ACCOMP ABNORMS, LIGHT DID NOT ILLUMINATE WITH MTC DIRECT. RECYCLED GEAR, LIGHT STILL NOT ILLUMINATED. CONTINUED TO WIGGLE LIGHT AND IT FINALLY ILLUMINATED. LANDED WITH NORMAL INDS. REPLACED SWITCH.

Part: SKIN — DENTED (BS 435-465)

THE FUSELAGE SKIN WAS DEEPLY DENTED ADJACENT TO AN EXISTING SKIN CUTOUT REPAIR AT FS 457, BETWEEN STRINGER 33R AND 34R. THE EXISTING REPAIR WAS REMOVED, THE NEW DAMAGE CUTOUT, AND A NEW EXTERNAL ALUMINUM REPAIR DOUBLER INSTALLED TO REPAIR BOTH DAMAGE CUTOUTS. THE REPAIR WAS ACCOMPLISHED PER ER/A 367009-14, REV A.

Part: SKIN — GOUGED (BS 450)

FUSELAGE SKIN WAS FOUND DENTED/GOUGED AT BS 457 BETWEEN S33R AND S34R JUST AFT OF AN EXISTING EXTERNAL REPAIR (FOR A SKIN CUTOUT ALSO BETWEEN S33R AND S34R). THE NEW CUTOUT IS APPROX 1 INCH DIA, THE EXISTING CUTOUT IS APPROX 9 BY 3. REPAIRED PER ERA 367009-14.

Part: SKIN — DENTED (BS 1197)

FUSELAGE SKIN FS 1197+77, STRG 36R : REPAIR FOR SKIN CUTOUT AT LAP SPLICE. THE FUSELAGE SKIN WAS BADLY DENTED BY GROUND EQUIPMENT AT THE STRINGER 36R LAP SPLICE AT FS 1197+77. THE DAMAGED SKIN WAS CUTOUT AND EXTERNAL ALUMINUM REPAIR DOUBLERS WERE INSTALLED TO REPAIR THE DAMAGE. THE REPAIR WAS ACCOMPLISHED PER ER/A 365068-14, REV A.

Part: RETRACT MECH — MALFUNCTIONED (TE FLAPS)

ON FINAL WITH FLAPS POSTIONED TO 30 DEG, THEY RETRACTED TO 20 DEG. FLAP HANDLE MOVED TO MATCH FLAP POS. STATUS MSG T/E FLAP SHUT DOWN. DIVERTED TO JFK. INSP AND OPS CHECKED FLAPS ALL NORMAL. NO FAULTS ON FLAP/SLAT ECU. ADP ON MCO.

Part: ACTUATOR — FAILED (NR 8 SPOILER)

NUMBER 8 SPOILER CASTING FAILED AT FILTER. REPLACED NUMBER 8 SPOILER ACTUATOR.

Part: RETRACT MECH — LACK OF LUBE (NR 12 LE SLAT)

LE SLAT ASSY EICAS MESSAGE AND LEADING EDGE LIGHT DID BITE CK ON PROX BOX CHECKED FSEC CHECKED AIR GAP ON NR 12 SLAT ALL OK. FOUND NR 12 SLAT CHETTERING LUBED SLAT GRD OPS NML NO FAULTS LOGGED NOTE: CHECKED SENSORS GAP FULL UP ALL OK AT 20 DEGREES FLAP SENSORS ALL CHECKED NML AND FULL DN NML.

Part: PROJECTOR — FAILED (CABIN)

DURING CRUISE, AFTER MOVIE WAS SHOWN AND DURING HBO VIDEO BEGAN TO SMELL LIKE OVERHEATED ELECTRICS. TRACED TO C-ZONE PROJECTOR. DEACT PROJECTOR, REPLACED MID PROJECTOR AND OPS NML. MCO AND PLACARD REMOVED.