N68061

Part: WIRE — BROKEN (RT HYD PUMP) · airframe 92,740 hrs · 13,085 cycles

RIGHT ELEC HYD PUMP INOP.AS PER FIM 29-11- FAULT TREE 891 , FOUND PHASE B MISSING ON CONNECTOR D486 (RT ELEC PUMP). M896. REMOVED & CHECKED FOR 115 VAC ON CONTACTS A1/B1/C1 OK. CONTINUITY FROM M896 B2 TO D486/B SHOWS OPEN CIRCUIT (NO SHORT TO GROUND). FURTHER TROUBLE SHOOTING IN PROGRESS, FURTHER T/S PERFORMED, FOUND WIRE W288-009-06 BROKEN BETWEEN SPLICE SM2 & TERMINAL BLOCK TB5042 (10 INCH FROM SPLICE). FURTHERMORE, OTHER TWO WIRES SHOWING EXTERMAL PLY SHAFING. LOTO APPLIED , P11 C/B L16 TAG OUT , & RT PYLON PANELS 447BR / 447BL OPENED. PRIOR TO WIRING REPAIRS, RT ELEC HYD PUMP PACKAGE REMOVED IAW AMM 29-11-01-024-001. RT ELEC HYD PUMP INSTALLED IAW AMM 29-11-01-424-019. UNABLE TO PERFORM LEAK & OPS CHKS AT THIS TIME DUE TO DAMAGED WIRING. REPAIR OF WIRE W288-001-08 REF WDM 29-11-22-2 IAW SWPM 20-10-13 PERFORMED. REPAIR OF WIRE W442-037-16 IAW WDM 29-11-22-2 IAW SWPM 20-10-13 PERFORMED. ELEC HYD PUMP RT ELCU REPLACED AS PRECAUTION DUE TO R ELEC HYD SYS WIRING DAMAGE. PERFORMED OPS & LEAK CHK OF RT ELEC HYD PUMP IAW AMM 29-11-01-424-019. OPS & LEAK CHKD OK.

Part: SKIN — CRACKED (ZONE 600 SLAT) · airframe 91,862 hrs · 12,970 cycles

DURING INSPECTION AT RIGHT WING OTBD SLAT NR 11 FOUND CRACKED ON SKIN INBD NEAR ACCESS PANEL 625AT. PERFORMED PERMANENT REPAIR IAW EC/RA 5743-02012.

Part: TRACK — FOD (ZONE 800) · airframe 89,646 hrs · 12,684 cycles

4R DOOR SLIDE WILL NOT ARM. INSPECTED SLIDE TRACKS AND FOUND DEBRIS. CLEANED DEBRIS AND OPS CHECK 4R DOOR. REF AMM 52-11-00. ADD 381101, U380359 AND REF AMM 25-66-01 FOR ARMING 4R DOOR SLIDE.

Part: TRANSDUCER — FAULTED (ANTI-SKID SYS) · airframe 89,224 hrs · 12,624 cycles

ANTISKID CAUTION MSG. ANTISKID CONTROLLER, BIT TEST PASS. #7 ANTISKID XDCR SPIN TEST ROTABLE PARTS CHANGE WAS INDICATED - TT # 1527113 SN OFF 0572 STILL NEEDED FOR REPLACEMENT OF TRANSDUCER. AFTER TAKE-OFF, ANTISKID CAUTION MSG BITE CHKD ANTISKID AUTO BRAKE CONTRL UNIT, BITE SHOWS #7 BRAKE ANTISKID/AUTOBRAKE CONTROLLER STILL SHOWS #7 XDCR FAULT. FOUND TRANSDUCER. REPLACED #7 BRAKE TRANSDUCER/INAXLE ASSY IAW AMM HIGH RESISTANCE TO WIRE W1524-204R-20. FUTHER TROUBLESHOOTING 32-42-05. REQS OPS CK OF #7 BRAKE TRANSDUCER IAW AMM TASK AND FOUND WIRE BARELY ATTACHED AT PIN #7 OF D5032P. RETERMINATED 32-42-05-404-007-001. STEP (3) AND BEYOND FOR OPS CK.PARTS IAW SWP CH 20-61-11 AND WDM 32-42-11 PG 6. CLEARED FAULT ON TRANSDUCER, C/W #7 TRANSDUCER INSTALLATION FROM STEP 3. ALL OPS NRML.

Part: ELECTRONIC UNIT — INTERMITTENT (TE FLAPS) · airframe 87,096 hrs · 12,331 cycles

ON SHORT FINAL GOT A TE FLAPS ASYM EICAS TOMC LOCKS FOR REPAIR, TOMC UNLOCKS FOR UPDATING ABOVE UPDATE APPLIES TO FLAPS AT 20 DEGREES PER FIM 27-51 TASK 811, ARMED AND DEARMED ALT TE SWITCH TWICE. MOVED FLAPS FROM 30 DEGREES TO 0 DEGREES WITH C2 HYDRAULICS ONLY, NO EICAS MSG. MOVED FLAPS FROM 0 TO 30 WITH C2 PUMP ONLY, TE FLAP DISAGREE MSG APPEAR BETWEEN 1 DEGREES AND 5 DEGREES THEN PERFORMED BITE TEST OF FSEU IN REFERENCE WITH FIM 27-51 FAULT TREE 809. FOUND NO EXISTING FAULTS. FOUND SECT. 2 AND SECT. 3 NO DATA MESSAGES ON LEG 0. PER FIM, CONTINUED PROBLEMS OF NO DATA FAULTS MAY WARRANT REPLACEMENT OF FSEU. ON SLAVING OF NEW FSEU, FOUND PROGRAM PIN MISMATCH. SEE IMAGES: CURRENT FSEU IMAGES FOR REFERENCE: REPLACED FSEU REF AMM 27-51-01, NO INTIAL FAULTS EXIST. OPS TEST IN WORK. CHECKING THE FLAP POSITION TRANSMITTER TEST, TRANSMITTER 3 & 4 OUT OF LIMITS PER TABLE 202. REQUIRES ADJUSTMENT OR REPLACEMENT OF TRANSMITTERS IF OUT OF LIMITS. DISAPPEARED AFTER PASSING 5 DEGREES. RAN TEST AGAIN WITH C2 AND ADP ASSIST TWICE WITH NO MX MSG. LAST OCCURRENCE OF TE FLAP DISAGREE WAS MAY 4, 2024, APPROXIMATELY 29 DAYS AGO. ADJUSTED FLAP POSITION TRANSMITTERS 3 AND 4 ONE DETENT EACH, VERIFIED RESISTANCE VALUES ARE IN RANGE AT FLAPS 20.

Part: BATTERY PACK — DISCHARGED (EQ#M737) · airframe 83,624 hrs · 11,839 cycles

EMER LT SYSTEM DEEP CYCLE CHECK FOUND BAT PACK EQ NO.M737 (LH STA 980) TEST FAIL TRANSFER REF. NON-ROUTINE HX NRC WO.2019120 AND ORIGINATED BY EMP V897815 EMER LT BAT PACK EQ NO. M737 REPLACED AND TEST RESULT NORMAL AS PER AMM 33-51-07

Part: BATTERY PACK — DISCHARGED (EQ# M739) · airframe 83,624 hrs · 11,839 cycles

EMER LT SYSTEM DEEP CYCLE CHECK FOUND BAT PACK EQ NO.M739 (LH STA 1360) TEST FAIL TRANSFER REF. NON-ROUTINE HX NRC WO.2019164. EMER LT BAT PACK EQ NO. M739 REPLACED AND TEST RESULT NORMAL AS PER AMM 33-51-07.

Part: BATTERY PACK — DISCHARGED (EQ#M6760) · airframe 83,624 hrs · 11,839 cycles

EMER LT SYSTEM DEEP CYCLE CHECK FOUND BAT PACK EQ NO.M6760 (RH STA 1190+70) TEST FAIL TRANSFER REF. NON-ROUTINE HX NRC WO.2019135 AND ORIGINATED BY EMP V897815 EMER LT BAT PACK EQ NO. M6760 REPLACED AND TEST RESULT NORMAL AS PER AMM 33-51-07 WORK ACCOMPLISHED BY MECHANIC V898179 INSPECTED BY V924743 IDT INSPECT IS OKAY. APPROVED BY HX206872

Part: BATTERY PACK — DISCHARGED (EQ# M734) · airframe 83,624 hrs · 11,839 cycles

EMER LT SYSTEM DEEP CYCLE CHECK FOUND BAT PACK EQ NO.M734 (RH STA 1380) TEST FAIL TRANSFER REF. NON-ROUTINE HX NRC WO.2019172 EMER LT BAT PACK EQ NO. M734 REPLACED AND TEST RESULT NORMAL AS PER AMM 33-51-07.

Part: BATTERY PACK — DISCHARGED (EQ# M7236) · airframe 83,624 hrs · 11,839 cycles

EMER LT SYSTEM DEEP CYCLE CHECK FOUND BAT PACK EQ NO.M7236 (LH STA 1190+70) TEST FAIL TRANSFER REF. NON-ROUTINE HX NRC WO.2019143. EMER LT BAT PACK EQ NO. M7236 REPLACED AND TEST RESULT NORMAL AS PER AMM 33-51-07

Part: SPAR WEB — CRACKED (NO.2 PYLON) · airframe 83,624 hrs · 11,839 cycles

B767-06-3-7294 NO.2 PYLON MID SPAR WEB AT DISCONNECT BOX CUTOUT FOUND CRACK TRANSFER REF. NON-ROUTINE HX NRC WO.2012233 AND ORIGINATED BY EMP NO. V925649 NO.2 PYLON MID SPAR WEB REPAIRED AS PER SRM 54-55-01-2R-2 REPAIR 2 FIG 203 AND REPAIR 2 IS A CATEGORY A REPAIR AT DISCONNECT BOX CUTOUT AND ATTACH FORM 44-0008 MAINTENANCE WORKSHEET ITEM 1-20.

Part: FAILSAFE — CRACKED (STA955 REAR SPR) · airframe 83,624 hrs · 11,839 cycles

1EA HOLE FOUND CRACK AT LH STA 955 REAR SPAR BULKHEAD FAILSAFE STRAP TRANSFER REF. NON-ROUTINE HX NRC WO.2023425 AND ORIGINATED EMP V906014 LH STA 955 REAR SPAR BULKHEAD FAILSAFE STRAP REPAIRED AS PER EA5340-01385 REV ORIG OP003 WORK ACCOMPLISHED BY MECHANIC V897470 INSPECTED BY V896888 RII INSPECT IS OKAY. APPROVED BY HX243551

Part: FAILSAFE — CRACKED (RH STA 955) · airframe 83,624 hrs · 11,839 cycles

1EA HOLE FOUND CRACK AT RH STA 955 REAR SPAR BULKHEAD FAILSAFE STRAP TRANSFER REF. NON-ROUTINE HX NRC WO.2023412 AND ORIGINATED EMP V906014 RH STA 955 REAR SPAR BULKHEAD FAILSAFE STRAP REPLACED AS PER EA5340-01385 REV ORIG OP 004 WORK ACCOMPLISHED BY MECHANIC V897470 INSPECTED BY V896888 RII INSPECT IS OKAY. APPROVED BY HX243551

Part: TEE FITTING — CORRODED (STA955 REAR SPR) · airframe 83,624 hrs · 11,839 cycles

EA 5340-01385 REV ORIG OP 004 RH SIDE STA 955 REAR SPAR BULKHEAD FAILSAFE STRAP T-FITTING FOUND CORROSION TRANSFER REF. NON-ROUTINE HX NRC WO.2029680 AND ORIGINATED BY EMP V906449 EA5340-01385 REV ORIG OP 004 RHS STA955 REAR SPAR BULKHEAD FAILSAFE STRAP T-FTG REPAIRED AS PER ECRA 5340-02151 REV - ATTACH MAINTENANCE WORKSHEET FORM 44-0008 ITEM 1-8 ACCOMPLISHED WORK ACCOMPLISHED BY MECHANIC V897470 INSPECTED BY V906449 RII INSPECT IS OKAY. APPROVED BY HX341008

Part: TEE FITTING — CORRODED (STA955 REAR SPR) · airframe 83,624 hrs · 11,839 cycles

EA 5340-01385 REV ORIG OP 003 LH SIDE STA 955 REAR SPAR BULKHEAD FAILSAFE STRAP T-FITTING FOUND CORROSION TRANSFER REF. NON-ROUTINE HX NRC WO.2029686 AND ORIGINATED BY EMP V906449 EA5340-01385 REV ORIG OP003 LHS STA 955 REAR SPAR BULKHEAD FAILSAFE STRAP T-FITTING REPAIRED AS PER ECRA 5340-02150 REV- ATTACH MAINTENANCE WORKSHEET FORM 44-0008 ITEM 1-8 ACCOMPLISHED WORK ACCOMPLISHED BY MECHANIC V897470 INSPECTED BY V906449 RII INSPECT IS OKAY. APPROVED BY HX341008

Part: SHEAR TIE — CORRODED (BULK CARGO COMP) · airframe 83,624 hrs · 11,839 cycles

BULK CARGO COMPT - BELOW FLOOR SHEAR TIE FOUND CORROSION AT STA 1417 BTN S37R-S38R (AS MARK) TRANSFER REF. NON-ROUTINE HX NRC WO.2005165 AND ORIGINATED BY EMP NO. V896820 BULK CARGO COMPT BELOW FLOOR AT STA 1417 BTN STR 37R-38R SHEAR TIE REPLACED AS PER SRM 51-10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02. ATTACHED FORM 44-0008 ITEM 1 TO 11 ACCOMPLISHED. WORK ACCOMPLISHED BY MECHANIC V897473 INSPECTED BY V896820 RII INSPECT IS OKAY. APPROVED BY HX 185167.

Part: FILTER — FAILED (LH ENG) · airframe 83,551 hrs · 11,829 cycles

L ENG FUEL FILTER ON BOTH EICAS AND STATUS PAGE.

Part: RVDT — NONE (L/E O/B PDU) · airframe 82,115 hrs · 11,630 cycles

ON APPROACH GOT TE FLAP DISAGREE WHEN ATTEPTING TO MOVE FLAPS F ROM 1 TO 5 PERFORMED BITE OF FSEU GOT MESSAGE NUMBER27-81041 L/E OUTBD PDU RVDT REQUIRES MORE T/S PARTS USED: 64-2781-3-0320,QTY :1 76-2781-3-0173,QTY :1 T/S IRW FIM 27-51 TASK 809. FOUND FAULT 27-81041. FOUND RVDT 27-81-11-424-029. OP''S CHECKED GOOD. READING NOW -8.62 RETRACTED M544 READING -3.77 IN RETRACTED POSITION WHEN THE NOMINAL SHOULD (-8.69 NOMINAL) 5.63 TKF (5.58 NOMINAL) & 10.34 LDG (10.27 BE -8.69. ATTEMTED TO ADJUST BUT THE READING FROM RVDT BECAME NOMINAL) ERRATIC AND UNRELIABLE. R&R RVDT M544 ON L/E O/B PDU IAW MM

Part: FLAP SYSTEM — NONE (TE FLAPS 1) · airframe 82,115 hrs · 11,630 cycles

TE DISAGREE EICAS FLAPS 1 HAD TO EXTEND ELECTRICALLY UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V123456 83, FAULT TREE 82 AND 809...TOMC MO PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC RELATED WORK ORDER 000000003067778 AND PRTR ACCOMPLISHED BITE TEST ON FSEU , NOTICED. MSG 27-81041(LE OUTBOARD PDU RVDT )...ERASED. MSG. ACCOMPLISHED VISUAL INSPECTION OF FLAPS AND SLATS AND OPERATED FLAP AND SLATS ON NORMAL MODE SEVERAL TIMES, AND DID BITE TEST ON FSEU AGAIN, NO MSGS NOTICEDACCOMPLISHED BITE TEST ON FSEU , ON FSEU AGAIN, NO MSGS NOTICED..REF : FIM 27-81 FAULT TREE NOTICED. MSG 27-81041(LE OUTBOARD PDU RVDT )...ERASED. MSG. 83, FAULT TREE 82 AND 809.TOMC MO ACCOMPLISHED VISUAL INSPECTION OF FLAPS AND SLATS AND OPERATED FLAP AND SLATS ON NORMAL MODE SEVERAL TIMES, AND DID BITE TEST ADD EMP:V901260

Part: FSEU — FAULTED (WING) · airframe 81,609 hrs · 11,545 cycles

L/E SLAT DISAGEE EICAS AND 6, LEFT INBOARD AND RIGHT INBOARD WERE NOT FULLY EXTENDED. FURTHER INSPECTION REQUIRED. REFER TO FAULT TASK 27-51 FAULT TREE 809 AND 27-51 FAULT TREE 815. FSEU BITE REQUIRED. UPON ARRIVAL DEBRIEF CREW. NO OVERSPEED OCCURRED. ISSUED OCCURED WHEN TRYING TO MOVE FLAP/SLATS FROM 15 TO 5. THEY HAVE A LOCK OUT AND LE SLAT SHUT DOWN MESSAGE.THEY BROUGHT DOWN FLAPS USING ALTERNATE TO FLAPS 20. NOTICE THAT LE EDGE SLATS 5 T/S FIM 27-81 FAULT TREE 816, PERFORMED FSEU BITE AND FOUND 2 OPS CK GOOD. PARTS USED: 76-2751-9-0010,QTY :1 1869460,QTY EXISTING FAULTS 27-51325, AND 27-51326. REMOVED AND REPLACED :1 FSEU REF AMM 27-51-01, BOTH FAULTS CLEARED. CYCLED FLAPS FULL ROTABLE PARTS CHANGE WAS INDICATED - TT # 1869460 SN OFF 1050 DOWN AND UP SEVERAL TIMES, NO FAULTS NOTED. LEADING EDGE SLAS

Part: LINE — BLOCKED (LAVATORY DUMP) · airframe 81,468 hrs · 11,524 cycles

LEFT SIDE LAVATORIES INOPERATIVE DURING FLIGHT ABOVE 16K, LAVATORY TANK FULL LIGHT ILLUMINATED. FWD WASTE SYS INOPERATIVE LIGHT ILLUMINATED, AND FWD WASTE TANK SHOWS MORE THAN 3/4 FULL. UNABLE TO DUMP FWD WASTE TANK SYS, MAY HAVE A BLOCKAGE IN DUMP LINE. REMOVED BLOCKAGE FROM FWD WASTE TANK DRAIN TUBE. SERVICED LAVATORIES, SYS OK.

Part: NONE — NONE (STA 325 LBL 22 -) · airframe 81,274 hrs · 11,489 cycles

EA 2500-12538 OP 2 DURING ACCESS G2 GALLEY FLOOR SUPPORT REWORK, STA 325 LBL 22 - 44 FLOOR BEAM UPR SURFACE FOUND CORROSION. REF HX NR WO. 968113, ORIG BY V898556 CABIN FLOOR BEAM STA 325 UPPER CHORD REPAIRED AS PER ECRA 5315-0 1179 REV- BTN LBL 22" AND LBL 44" INSPECTED AND APPROVED BY HX310582

Part: NONE — CORRODED (STA 325) · airframe 81,274 hrs · 11,489 cycles

EA 2500-12538 OP 2 DURING ACCESS G2 GALLEY FLOOR SUPPORT REWORK, STA 325 LBL 22 - 44 FLOOR BEAM UPR SURFACE FOUND CORROSION. REF HX NR WO. 968113, ORIG BY V898556 CABIN FLOOR BEAM STA 325 UPPER CHORD REPAIRED AS PER ECRA 5315-0 1179 REV- BTN LBL 22" AND LBL 44" INSPECTED AND APPROVED BY HX310582

Part: MANIFOLD — UNSERVICEABLE (LEFT) · airframe 80,881 hrs · 11,429 cycles

L ENG OVHT CAUTION AT CRUISE FL310 CONTACT TOMC EMC DESK WITH FINDINGS PRIOR TO CLEARING ITEM.. TOM EMC R. TOTH DOWN WIRING AND DETECTORS. UNABLE TO GENERATE ANY FAULTS. VISUALLY CHECKED ALL DETECTOR CONNECTIONS , NO SIGNS OF DEFECTS REF WDM26-11-12-2. L/P UNLOCKED BY TOMC FOR EDITING CONTACT TOMC EMC DESK WITH FINDINGS PRIOR TO CLEARING ITEM. UNLOCK FOR EWR TECH UPDATE. REVEIW TS WITH TOMC. TOMC KEIPER ACCOMPLISHED TROUBLESHOOTING REF FIM26-11 FT804. NO CURRENT OR REMOVED AND REPLACED LEFT ENG FIRE OVERHEAT DETECTION FILE CARD RAN #1 BETWEEN 80% AND TAKEOFF POWER FOR 9 MINUTES, NO FAULTS ACTIVE FAULTS SHOW IN HISTORY, CHECKED RESISTANCE OF LOOP 1 & 2 ASSY M687 & M688 PRECAUTIONARY. REF AMM TASK 26-11-02 BITE CHECK FOUND, ALL ENG PARAMETERS NORMAL OVERHEAT DETECTION SYSTEM LEFT ENGINE BETWEEN PINS 20 AND 21 AND NORMAL. TO GROUND OF M687 (D2834) & M688 (D2840) NORMAL, ALSO SHOOK ADD EMP:U159815 ADD EMP:U159815 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1058775 SN OFF 1326 TT # 1267578 SN OFF 1326 CARD, ASSY, FIR OFF 64-2611-9-9002 1326 ON 64-2611-9-9002 1537 TECHS FOUND LEAKING HI STAGE DUCT. UNLOCKED TO CLEAR LOG PAGE INSPECTED LEFT ENGINE PNEUMATIC SYSTEM DUCTS, CLAMPS, SENSE THE HPSOV. REMOVED AND REPLACED HP/IP MANIFOLD DUCT, MFG P/N AND ISO VALVES CLOSED. NO DEFECTS NOTED. OK TO CONTINUE. LINES, AND VALVES, NO DEFECTS NOTED. PRESSURIZED LEFT ENGINE 323U2324-10, PER AMM 36-11-01. LEAK CHECKS GOOD. PER TOMC ENGINE PNEUMATIC SYSTEM UPSTREAM OF THE PRSOV AND WR

Part: NONE — MISSING (4 SLAT) · airframe 79,075 hrs · 11,111 cycles

#4 INBD LEADING EDGE SLAT IS MISSING A BLOWOUT PANEL AND SUSPECT INTERSTITIAL DUCT SEPARATED FROM LEADING EDGE TAI DUCT, REF IPC30-11-02-01, ITEM 365 ID,ITEM 355 DUCT NOTED IN #3 SLAT INTERSTITIAL DUCT. REMOVED SLAT PANELS 522DT, 523AT,523FT, 524AT. REMOVED INBOARD AND OUTBOARD SLAT INTERCONNECT TUBES AND ASSOCIATED HARDWARE. DISCONNECTED 4 SLAT DRIVE RODS AND OUTBOARD LOWER RIB SEGMENTS / SEALS AS REQUIRED FOR INTERSTITIAL DUCT REMOVAL. DEBRIS FROM FAILED TUBE REMAINS IN FORWARD SLAT CAVITY AND ADDIIONAL DEBRIS REMOVED ALL DABRIS FROM L.E. CAVITIES OF SLATS 4,3,2 &1. REMOVED ALL DABRIS FROM TAI DUCTS 3 & 1. INSTALLED NEW #4 SLAT TAI DUCT REF.I.P.C. 30-11-02-01 ITEM 355. CONECTED 4 SLAT INPUT RODS I.A.W. M.M. 27-81-02-424-099 SUBTASK POERFORMED 4 SLAT INBOARD & OUTBOARD INTERSTITIAL DUCT SHEET METAL REQUIRED FOR SUBTASK 30-11-06-434-013!. 27-81-02-400-002. INSTALLATION I.A.W. M.M. 30-11-06-404-009 UP TO & INCLUDING STEP 3D4. REMOVED INTERSTITIAL DUCT SEPERATED FROM LEADING EDGE TAI DUCT PER 30-11-06-004-001. TO FOM BETWEEN SLAT 4 AND 5 ADD EMP:U233543 ACCOMPLISHED INSPECTION REQUIREMENTS FOR STEP 13 OF AMM 27-81-02-429-099, ATTACHED 4 SLAT INBD AND OUTBD SLAT CONTROL RODS TO ROTORY ACTUATORS. REMOVED THE 2 CONTROL RODS ON THE 4 SLAT TO ALLOW SHEET METAL ACCOMPLISHED STEP 13 OF AMM 27-81-02-429-099, ATTACHED 4 SLAT INSTALLED 4 SLAT INBD & OUTBD INTERSITIAL DUCT UP TO AND TO HAVE ACCESS FOR THEIR REPAIR. IN REF TO AMM 27-81-02. INBD AND OUTBD SLAT CONTROL RO

Part: PANEL — DENTED (LT WING TE FLAP) · airframe 78,647 hrs · 11,049 cycles

LEFT OUTBOARD AFT FLAP HAS NUMEROUS DENTS, WORST BEING 35.5 INCHES OUTBOARD OF INBOARD EDGE 45 1/2 INCHES FROM TRAILING EDGE, 1.5 " DIAMETER, .040" DEEP. NO HOLES, TAP TESTED AND FOUND NO DELAMINATION. CORRECTION TO ORIGINAL WRITE UP: SHOULD READ LEFT OUTBOARD AFT FLAP HAS NUMEROUS DENTS, WORST BEING 35.5 INCHES OUTBOARD OF INBOARD EDGE, 4.5 INCHES FROM TRAILING EDGE, 1.5 " DIAMETER, .040" DEEP. NO HOLES, TAP TESTED AND FOUND NO DELAMINATION. REVIEWED AND LOCKED FOR MAINT FERRY UNLOCK LHW O/B AFT FLAP UPPER FLAP PNL IN DENT LOCATION LISHED IN RI PA R4 PERFORMED REPAIR AS PER SRM 51-70-10 REPAIR 4 AND ALL OTHER D ENTS EXPECT DENT LOCATIONS LISHED IN RI PAR4. ACCEPT THE DENT AS IS AS PER ECRA 5746-01010.REFER FORM 44-0008 ITEM 1 TO 21

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 78,647 hrs · 11,049 cycles

RIGHT INBOARD AFT FLAP HAS NUMEROUS DENTS FROM HAIL, THE LARGEST IS 1.25 INCH DIAMETER, .093 INCH DEEP, TAP TESTED AND NO DELAMINATION NOTED. REVIEWED AND LOCKED FOR MAINT FERRY UNLOCK RHW I/B AFT FLAP IN DENT LOCATIONS LISHED IN RI PAR4 PERFORMED REPAIR AS PER SRM 51-70-10 REPAIR 2,IN DENT LOCATION LISHED IN RI PAR 5 PERFORMED REPAIR AS PER RI NO:RI-57-00-14810, REV A AND ECRA 5753-01940.ALL OTHER DENTS EXCEPT DENT LOCATIONS LISHED IN RI PAR 4 AND 5,ACCEPT THE DENT AS IS AS PER ECRA 5753-01940.FORM 44-0008 ITEM 1 TO 39.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 78,647 hrs · 11,049 cycles

LEFT INBOARD AFT FLAP UPPER SURFACE HAS 3 HOLES AND NUMEROUS DENTS. HOLES: 1. 64 INCHES INBOARD FROM OUTBOARD EDGE, 14.75 INCHES FROM TRAILING EDGE, THREE-QUARTER INCH DIAMETER. 2. 65.25 INCHES INBOARD FROM OUTBOARD EDGE, 5.5 INCHES FROM TRAILING EDGE, 5/8" DIAMETER. 3. 85.25 INCHES INBOARD FROM OUTBOARD EDGE, 3.75 INCHES FROM TRAILING EDGE, 5/8" DIAMETER. DENTS: DEEPEST DENT IS 30.25" OUTBOARD FROM INBOARD EDGE, .125" DEEP, 2" DIAMETER. TAP TESTED DENTS AND FOUND NO DELAMINATION. REVIEWED AND LOCKED FOR MAINT FERRY UNLOCK LHW I/B AFT FLAP UPPER SURFACE DENTS LOCATION LISTED IN RI PAR 4 PERFORMED REPAIR AS PER SRM 51-70-10 REPAIR 2,DENTS LOCATION LIS TED IN RI PAR 6 PERFORMED REPAIR AS PER SRM 51-70-10 REPAIR 2. ADD EMP:V910922 AS PER SRM 51-70-10 REPAIR 2 AND ECRA 5753-01939,FOR ALL DENTS EXCEPT DENTS LISTED IN RI STEP 4-7,ACCEPT THE DENT AS IS AS PER AND REPAIR 4.DENTS LOCATION LISTED IN RI PAR 7 PERFORMED REPAIR RI NO:57-00-14822 REV A AND ECRA 5753-01939.REFER FORM 44-0008 WORK ACCOMPLISHED BY MECHANIC V910922 INSPECTED BY V896921 ITEM 1 TO 39 ACCOMPLISHED RII BY HX185167,APPROVED

Part: SKIN — DAMAGED (LEFT ELEVATOR) · airframe 78,647 hrs · 11,049 cycles

LOG# 6677208 LEFT OUTBOARD ELEVATOR HAS EIGHT PUNCTURES FROM HAIL DAMAGE. 1. 23.5 INCHES IN BOARD FROM OUTBOARD EDGE, 3.5 INCHES FROM TRAILING EDGE, 1 INCH DIAMETER. 2. 35.5 INCHES INBOARD FROM OUTBOARD EDGE, 20" FROM TRAILING EDGE, 1 INCH DIAMETER. 3. 55.5 INCHES INBOARD FROM OUTBOARD EDGE, 21.75 FROM TRAILING EDGE, 1.250 INCHES IN DIAMETER. 4. 56.25 INCHES INBOARD FR. WORK DETAIL REF ELB 6677208 FOR MORE WORK DETAIL LH O/N ELEVATOR UPPER SURFACE DAMAGE AREA PERFORMED PERMANENT REPAIR AS PER SRM 51-70-04 PAR 5A(1) AND ECRA 5520-01612 REV A REFER FORM 44-0008 ITEM 1 TO 13 ACCOMPLISHED

Part: STIFFENER — CRACKED (LH NOSE WW) · airframe 78,647 hrs · 11,049 cycles

AD 2017-17-16 SUPPORT TASK - EA 5310-07143 OP1 - LH NOSE WHEEL WELL VERTICAL STIFFENER ON STA287 BETWEEN WL159 TO 185 FOUND 1EA CRACK RUNNING VERTICALLY APPROX 7/8 " IN LENGTH.PLS PRINT AND AC COMPLISHED REPAIR PER OP3. TRANSFER REF. EA 5310-07143 REV D OP1 L/H NOSE WHEEL WELL VERTICAL STIFFENER O N STA287 BETWEEN WL159 TO 185 CRACKED AREA REPAIRED AS PER EA 5310-07143 REV D OP3 REFER SEQ 1385 FOR WORK DETAIL

Part: STIFFENER — CRACKED (NOSE WW) · airframe 78,647 hrs · 11,049 cycles

AD2017-17-16 SUPPORT TASK EA 5310-07143 OP2 - RH NOSE WHEEL WELL VERTICAL STIFFENER ON STA287 BETWEEN WL 159-185 FOUND 1EA CRACK RUNNING VERTICALLY APPROX 7/8" IN LENGTH.PLS PRINT AND ACCOMPLISH REPAIR PER OP4 EA 5310-07143 REV D OP2. R/H NOSE WHEEL WELL VERTICAL STIFFENER O N STA287 BETWEEN WL 159 AND WL 185 CRACKED AREA REPAIRED AS PER EA 5310-07143 REV D OP4.

Part: STIFFENER — CRACKED (NLG WW) · airframe 78,647 hrs · 11,049 cycles

AD 2017-17-16 SUPPORT TASK - EA 5310-07143 OP1 - LH NOSE WHEEL WELL VERTICAL STIFFENER ON STA287 BETWEEN WL159 TO 185 FOUND 1EA CRACK RUNNING VERTICALLY APPROX 7/8 " IN LENGTH.PLS PRINT AND AC COMPLISHED REPAIR PER OP3. TRANSFER REF. NON-ROUTINE LP 9130629 AND ORIGINATED BY EMP V 897008 EA 5310-07143 REV D OP1 L/H NOSE WHEEL WELL VERTICAL STIFFENER O N STA287 BETWEEN WL159 TO 185 CRACKED AREA REPAIRED AS PER EA 5310-07143 REV D OP3 REFER SEQ 1385 FOR WORK DETAIL WORK ACCOMPLISHED BY MECHANIC V897381 INSPECTED BY V912779 ADD EMP:V912779 RII BY HX169509,APPROVED

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 78,647 hrs · 11,049 cycles

MULT-33-3-0004 EMER LT PWR SUPPLY M6758 FAILED FUNCTIONAL TEST. EMER LT PWR SUPPLY M6758 CHARGER REPLACED & TESTED NORMAL AS PER AMM 33-51-07.

Part: STIFFENER — CRACKED (NLG WW) · airframe 78,647 hrs · 11,049 cycles

AD2017-17-16 SUPPORT TASK EA 5310-07143 OP2 - RH NOSE WHEEL WELL VERTICAL STIFFENER ON STA287 BETWEEN WL 159-185 FOUND 1EA CRACK RUNNING VERTICALLY APPROX 7/8" IN LENGTH.PLS PRINT AND ACCOMPLISH REPAIR PER OP4 TRANSFER REF. EA 5310-07143 REV D OP2 R/H NOSE WHEEL WELL VERTICAL STIFFENER O N STA287 BETWEEN WL 159 AND WL 185 CRACKED AREA REPAIRED AS PER EA 5310-07143 REV D OP4.REFER SEQ 1388 FOR WORK DETAIL.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 78,647 hrs · 11,049 cycles

MULT-33-3-0004 EMER LT PWR SUPPLY M7236 FAILED FUNCTIONAL TEST TRANSFER REF. EMER LT PWR SUPPLY M7236 CHARGER REPLACED & TESTED NORMAL AS PER AMM 33-51-07.

Part: SKIN — CRACKED (BS 1654 - 1678) · airframe 78,099 hrs · 10,969 cycles

DOUBLER REPAIR INSTALL BTWN STA 1654.5 AND STA 1678 ALONG STR 13 R, REF SRM 53-80-01 REPAIR 7 DETAIL 7. THIS REPAIR NEEDS REPEAT INSPECTIONS EVERY 7500 FLIGHT CYCLES EITHER 30,000 CYCLES AFTER AC DELIVERY OR 7500 CYCLES FROM REPAIR INSTALLION, WHICHEVER COM ES LAST REF SRM 53-80-0, REPAIR 7, TABLE 202. DOUBLER REPAIR INSTALLED BTWN STA 1654.5 AND STA 1678 ALONG STR R, REF SRM 53-80-01 REPAIR 7 DETAIL 7. THIS REPAIR NEEDS REPEAT INSPECTIONS EVERY 7500 FLIGHT CYCLES, EITHER 30,000 CYCLES AFTER AC DELIVERY OR 7500 CYCLES FROM REPAIR INSTALLION, WHICHEVER COM ES LAST. REF SRM 53-80-0, REPAIR 7, TABLE 202. APPROVED FOR DIP:DOUBLER REPAIR INSTALL BTWN STA 1654.5 AND STA 1678 ALONG STR 13 R, REF SRM 53-80-01 REPAIR 7 DETAIL 7. THIS REPAIR NEEDS REPEAT INSPECTIONS EVERY 7500 FLIGHT CYCLES EITHER 30,000 CYCLES AFTER AC DELIVERY OR 7500 CYCLES FROM REPAIR INSTALLATION, WHICHEVER COM ES LAST REF SRM 53-80-0, REPAIR 7, TABLE 202.

Part: BOTTLE — EMPTY (CREW OXYGEN) · airframe 75,637 hrs · 10,633 cycles

DURING FLIGHT, CREW EMERGENCY O2 LEVEL FOUND DEPLETED TO 11 LBS. CREW O2 BOTTLE REPLACED ACC AMM12-15-08-603-001. P/N42365-1 S/N ON:R08-000164 S/N OFF:R14-000449. PERFORMED FURTHER T/S, FOUND F/O O2 MASK REPLACED IN MARCH BEFORE SEVERAL O2 SERVICES OCCURED. FO MASK REPLACED ACC AMM 35-11-51-404-060 REV 127. LEAK CHECK PERFORMED WITHOUT FINDINGS. AC RETURNED TO SERVICE.

Part: SOCKET — BURNED (CABIN) · airframe 74,720 hrs · 10,511 cycles

READING LIGHT ASSY AT 16L SMOKED UPON PAX TURNING LIGHT ON. F/A SHUT LIGHT OFF AND SMOKE DISSAPATED. PANEL WAS WARM/HOT TO THE TOUCH. LOCKING LOG TO ENSURE PSU IS DROPPED AND AN INSPECTION OF WIRING AND COMPONENTS ON BACK SIDE OF PANEL IS ACCOMPLISHED. SMOKE ISSUE RESOLVED FOUND SEAT 16L OVERHEAD READING LIGHT SOCKET TO BE THE SOURCE OF THE SMOKE IN THE CABIN. REMOVED AND REPLACED LIGHT ASSY PER AMM 33-00-00. OPS CHECK GOOD AT THIS TIME. NO SMOKE PRESENT DURING OPS CHEC. CONDITIONAL INSPECTION PERFORMED PER AMM 05-51-58-200-801C1. SPOKE TO TOMC WHO CONCURS A/C IS OK FOR FLT.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 72,826 hrs · 10,248 cycles

LE SLAT DISAGREE SHORT FINAL ON ARRIVAL, ANY MSG DID NOT LATCH. PERFORMED FSEU BITE TEST OK AS PER AMM 27-51-00-815-809.THEN FLAP OPS CHECKED NORMAL ON GROUND. RETURN TO SERVICE.

Part: BUTTON — STUCK (ESCAPE ROPE) · airframe 72,006 hrs · 10,097 cycles

EMERGENCY ESCAPE ROPE PANEL ON CA SIDE WON’T STAY IN LATCHED POSITION. ESCAPE ROPE COMPARTMENT BUTTON FOUND STUCK BUTTON FREED AMM TASK 25-61-02-202-023 ESCAPE ROPE INSPECTION ACCOMPLISHED ALL CHKS OK. PANEL NOW SECURED.

Part: OVEN — ODOR (GALLEY) · airframe 69,894 hrs · 9,820 cycles

OVEN EMITS A VERY STRONG ELECTRICAL BURNING ODOR WHEN ON. REPLACED THE OVEN. OPS CHECKED NORMAL.

Part: SPAR — CRACKED (NR 1 PYLON) · airframe 69,575 hrs · 9,777 cycles

ENGINE NR 1 PYLON INTERNAL STA 223 MID SPAR WEB FOUND CRACKED AT IDG FEED THROUGH CUTOUT POSN AS MARK. ENG NR 1 PYLON INTERNAL STA 223 MID SPAR WEB REPAIRED AS PER SRM 54-55-01 REPAIR 2 FIG 202.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,575 hrs · 9,777 cycles

CABIN STA 325 LBL 36-40 FLOORBEAM FOUND CORRODED. CABIN STA 325 FLOORBEAM UPPER CHORD AT LBL 8- LBL 66.5 REPAIRED AS PER SRM 53-00-51 REPAIR 1 AND ECRA 5310-07326 REV-.

Part: LIGHT — DIM (COCKPIT) · airframe 69,575 hrs · 9,777 cycles

(200-1302) SUPPORT TASK - COCKPIT EMERGENCY EXIT SIGN FOUND DIM. COCKPIT EMERGENCY EXIT SIGN REPLACED AND TEST NORMAL IAW AMM 33-51-01.

Part: DUCT — BROKEN (A/C PACK) · airframe 68,862 hrs · 9,676 cycles

UNABLE TO MAINTAIN CABIN PRESSURE. EMERGENCY DECLARED. FOUND BROKEN AIR CONDITIONING DUCT. R/R I.A.W. AMM 21-23-08. OPS OK. PRESSURIZATION CHECK ACCOMPLISHED. ALL VALUE OK. PRESS 1-3 NEGATIVE. FOUND COUPLE OF DRAIN VALVE NOT CLOSING. CLEANED AND OPS CHECKED. LAST PRESSURIZATION CHECK ALL VALUE ABOVE THE MINIMUM LINE.

Part: ROD END — FAILED (LT MLG ACTUATOR) · airframe 68,772 hrs · 9,663 cycles

GEAR DISAGREE MESSAGE, LEFT MAIN DID NOT RETRACT AFTER TAKE OFF. EMERGENCY DECLARED. COMPLIED WITH FIM 32-30-00-815-840-001 AND FOUND SIDE BRACE LOCK ACTUATOR ROD END PULLED FROM ACTUATOR PISTON. REMOVED & REPLACED THE SIDE BRACE LOCK ACTUATOR ON LT MLG IAW MM 32-32-02. OPS CHECKED GOOD, NO LEAKS NOTED. SWUNG GEAR IAW 32-32-00. OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,872 hrs · 9,247 cycles

SEAT 21E MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP. OPS CHECKED GOOD.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 62,222 hrs · 8,717 cycles

R1 DOOR SLIDE DEPLOYED ON GROUND ACCIDENTALLY. INSTALLED SERVICEABLE DOOR SLIDE IAW AMM 25-66-01.

Part: RIB — CRACKED (RT WING) · airframe 58,471 hrs · 8,230 cycles

CRACK FOUND AT RT WING LE CAVITY SUPPORT RIB UPPER FLANGE LES 900. REPLACED IAW SRM 57-10-02 & INSTALLED IAW SRM 51-40-02. NEW RIB FABRICATED.

Part: SENSOR — FAILED (LE SLAT) · airframe 57,905 hrs · 8,150 cycles

LEADING EDGE ASYMMETRIC EICAS MSG HAPPENED INTERMITTENTLY ABOVE 14K WITH SPEED ABOVE 280 KNTS. MSG ACCOMPANIED BY FLAP CONTROL SYNOPTIC WITH AMBER LE INDICATION 27-81021. TROUBLE SHOT IAW FIM 32-09-03-101. PERFORMED PSEU BITE CHECK FOUND STRINGER 276 NR 1 SLAT OTBD SENSOR AT FAULT. R & R S276 IAW AMM 27-88-01-9 02-001. OPERATIONS CHECKED IAW AMM 27-88-00-715-098, OPERATIONS CHECKED GOOD NO FURTHER FAULTS NOTED AT THIS TIME. OK TO CONTINUE.

Part: SENSOR — FAILED (AC PACK) · airframe 55,629 hrs · 7,846 cycles

TIME AFTER FOLLOWING THE QRH PROCEDURES THE RT PACK BEGAN TO CYCLE ON & OFF CONTINUOUSLY, 5 MIN OFF, 1 MIN ON. PERFORMED ASCTU BITE & CTC BITE, FOUND MSG 21-51245 RT PACK OUTLET TEMP SENSOR AT FAULT IAW FIM TASK 21-51-00-810-859. R & R RT PACK OUTLET TEMP SENSOR 2 IAW AMM21-51-46. OPERATED PACKS & NO FAULTS NOTED.

Part: HMU — INOPERATIVE (RT ENGINE) · airframe 51,595 hrs · 7,289 cycles

NR 2 ENG COMPRESSOR STALL. R & R NR 2 HMU IAW AMM 73-21-14-404-030- HOO. OPS AND LEAK CHECKED GOOD.

Part: FRAME — CRACKED (NR 1 NACELLE) · airframe 47,047 hrs · 6,677 cycles

SUPPORT TASK NR 1 PYLON INBD FRAME FOUND CRACKED AT NAC STA 285 NR 1 PYLON INBD FRAME CHORD REPLACED IAW SRM 51-10-02 AND FASTENER INSTALLED IAW SRM 51-40-02.

Part: STIFFENER — CRACKED (LT WING) · airframe 47,047 hrs · 6,677 cycles

LT WING LES 679.8 FRONT SPAR UPPER STIFFER FOUND CRACKED. LT WING LES 679.8 FRONT SPAR UPPER STIFFER REPLACED IAW SRM 51-10-02 AND FASTENER INSTALLED IAW SRM 51-40-02. (NEW STIFFER FABRICATED DETAIL (REF NRC 5327522 (500-0070).

Part: SKIN — CRACKED (LE SLAT) · airframe 47,047 hrs · 6,677 cycles

RIGHT WING NR 10 SLAT I/B MAIN TRACK FITTING SKIN 1EA FASTENER HOLE FOUND CRACKED AT OSS 724. RIGHT WIING NR 10 SLAT I/B MAIN TRACK FITTING SKIN REPAIRED AS PER SRM 57-43-01 REPAIR 2 FIG 201 HFEC NIL CRACK FOUND.

Part: SKIN — CRACKED (LT WING NR4 SLAT) · airframe 47,047 hrs · 6,677 cycles

LT WING NR 4 SLAT INBD MAIN TRACK FITTING EXTERNAL SKIN 1EA FASTENER HOLE FOUND CRACKED AT OSS572.55. LT WING NR 4 SLAT INBD MAIN TRACK FTG EXTERNAL SKIN REPAIRED IAW SRM 57-43-01, REPAIR 2, FIG 201, HFEC NIL CRACK FOUND.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,047 hrs · 6,677 cycles

CABIN LT STA 303 LBL 30-45 FLOORBEAM UPPER SURFACE FOUND CORROSION. CABIN LT STA 303 LBL 5 TO LBL 58 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 AND HFEC NIL CRACK FOUND.

Part: SKIN — CORRODED (LE SLAT) · airframe 47,047 hrs · 6,677 cycles

RIGHT WING NR 10 SLAT O/B MAIN TRACK FITTING SKIN 1EA FASTENER HOLE FOUND CRACKED AT OSS 792.52. RIGHT WING NR 10 SLAT O/B MAIN TRACK SKIN REPAIRED AS PER SRM57-43-01 REPAIR 2 FIG 201 AND HFEC NIL CRACK FOUND.

Part: SKIN — CRACKED (LT WING NR4 SLAT) · airframe 47,047 hrs · 6,677 cycles

LEFT WING NR 4 SLAT OTBD MAIN TRACK FITTING EXTERNAL SKIN 1 EA FASTENER HOLE FOUND CRACKED AT OSS646.35 LT WING NR 4 SLAT OTBD MAIN TRACK FITTING EXTERNAL SKIN REPAIRED IAW SRM 57-43-01, REPAIR 2, FIG 201 AND HFEC NIL CRACK FOUND.

Part: SKIN — CRACKED (RT WING NR9 SLAT) · airframe 47,047 hrs · 6,677 cycles

RT WING NR 9 SLAT OTBD MAIN TRACK FITTING SKIN 1EA FASTENER HOLE FOUND CRACKED AT OSS646.35. RT WING NR 9 SLAT OTBD MAIN TRACK FITTING SKIN REPAIRED IAW SRM 57-43-01, REPAIR 2, FIG 201 AND HFEC NIL CRACK.

Part: SKIN — CRACKED (LE SLAT) · airframe 47,047 hrs · 6,677 cycles

RIGHT WING NR 9 SLAT I/B MAIN TRACK FITTING SKIN 1EA FASTENER HOLE FOUND CRACKED AT OSS 572.55 LOCATION. RIGHT WING NR 9 SLAT I/B MAIN TRACK FITTING SKIN REPAIRED AS PER SRM 57-43-01 REPAIR 2 FIG 201 HFEC NIL CRACK FOUND.

Part: SKIN — CRACKED (LT WING 3 SLAT) · airframe 47,047 hrs · 6,677 cycles

LT WING NR 3 SLAT INBD MAIN TRACK FITTING EXTERNAL SKIN 1EA FASTENER HOLE FOUND CRACKED AT OSS724. LT WING NR 3 SLAT INBD MAIN TRACK FITTING EXTERNAL SKIN REPAIRED IAW SRM 57-43-01 AND HFEC NIL CRACK FOUND.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,047 hrs · 6,677 cycles

CABIN RT STA 325 RBL 20-25 FLOORBEAM VPR SURFACE FOUND CORROSION. CABIN RT STA 325 RBL 16 TO RBL 36 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 AND HFEC NIL CRACK FOUND.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,047 hrs · 6,677 cycles

CABIN - LT STA 325 LBL 30-45 FLOORBEAM UPPER SURFACE FOUND CORROSION. CABIN LT STA 325 LBL 12" TO LBL 62" FLOOR SUPPORT BEAM UPPER CHORD REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 AND HFEC NIL CRACK FOUND.

Part: FLOOR SUPPORT — CORRODED (BS 303-325) · airframe 47,047 hrs · 6,677 cycles

CABIN BS 303 - 325 LBL 30 FLOOR SUPPORT UPPER SURFACE FOUND CORRODED. FLOOR SUPPORT REPLACED AS PER SRM 51-10-02.

Part: POWER SUPPLY — NO TEST (CABIN) · airframe 46,432 hrs · 6,602 cycles

EMERGENCY LIGHTS POWER SUPPLY M1208 DOOR 1LT WILL NOT TEST. REF W/ C 64-3350-1-3800. R&R PWR SUPPLY M1208. REF AMM 33-51-07. OPS CK NORMAL.

Part: POWER SUPPLY — NO TEST (CABIN) · airframe 46,432 hrs · 6,602 cycles

EMERGENCY LIGHT POWER SUPPLY M730 AT SEAT 1KL WILL NOT TEST. REF W/C 64-3350-1-3800 R&R PWR SUPPLY M730, REF AMM 33-51-07. OPS CK NORMAL.

Part: POWER SUPPLY — NO TEST (CABIN) · airframe 46,432 hrs · 6,602 cycles

EMERGENCY LIGHTS POWER SUPPLY M7236 AT SEAT 32AB WILL NOT TEST. REF W/C 64-3350-1-3800. R&R PWR SUPPLY M7236. REF AMM 33-51-07. OPS CK NORMAL.

Part: SENSOR — OUT OF ADJUST (LE SLAT) · airframe 45,423 hrs · 6,466 cycles

AFTER FLAP RETRACTION GOT L/E SLAT ASYM MESSAGE, WITH TRAILING EDGE FLAPS FULLY RETRACTED. PSEU FAULT CODE 303 ( NR 9 L/E SLAT SENSOR) REPOSITIONED NR 9 SLAT INBOARD AND OUTBOARD SLAT SENSOR TARGETS REF AMM 27-88-01 -201 OPS CHECK OF FLAP SYSTEM SATISFACTORY. PSEU 303 FAULT COMMENTS : NR 9 L/E SLAT SENSOR.

Part: TRANSDUCER — OUT OF ADJUST (RT ENGINE) · airframe 43,355 hrs · 6,205 cycles

RIGHT ENGINE DID NOT RESPOND ON ENGINE RUN FOR TAKEOFF N1 READ 50 PERCENT EGT 400 WITH THROTTLE FULL POWER. PERFORMED RE-ADJUSTMENT OF POSITION FEEDBACK TRANSDUCER IAW AMM 78-36-03/401. PERFORMED MAXIMUM POWER ASSURANCE GROUND TEST 5 IAW AMM 71-00-00 P538. ALL TEST PASSED, A/C OK TO CONTINUE.

Part: ENGINE — MAKING METAL (NR 1) · airframe 39,635 hrs · 5,725 cycles

"L OIL FILTER" EICAS ANNUNCIATED PRIOR TO DESCENT. LIGHT DID NOT EXTINGUISHED WITH THROTTLE TO IDLE. PARAMETERS NORMAL. PER CHECKLIST INITIATED PRECAUTIONARY ENGINE SHUTDOWN. FOUND METAL CONTAMINATION IN ENG OIL. REPLACED NR 1 ENG IAW M/M 71-00-02 PG 401 AND TASK CARD 64-7100-1-9800. ROTABLE PARTS CHANGE WAS INDICATED - TT 1012543, S/N OFF 06454 ENGINE, BASIC, OFF 64-7200-9-0001 6454 ON 64-7200-9-0001 6273.

Part: GEARBOX — FAILED (ENGINE) · airframe 39,643 hrs · 5,726 cycles

FOR DELAY REPORTING PURPOSE ONLY FOR DELAY REPORTING PURPOSE ONLY. ENGINE SHUT DOWN IN FLIGHT, ENGINE CHANGE OCCURRED IN HNL, DID NOT CLOSE THIS LOGPAGE AS ENGINE CHANGE WAS IN PROCESS.

Part: FRAME — DAMAGED (NR 1 PYLON) · airframe 33,612 hrs · 4,964 cycles

NR 1 PYLON NAC STA 285 O/B FRAME CHORD FOUND DAMAGED. NR 1 PYLON NAC STA 285 O/B FRAME CHORD REPLACED PER SRM 51-40-02.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 27,985 hrs · 4,194 cycles

WHILE REPLACING EMERGENCY LIGHT BATTERY AT STA 654 FOUND CHARGER WOULD NOT TEST. REPLACED BATTERY CHARGER PER AMM 33-51-07.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 27,985 hrs · 4,194 cycles

WHILE REPLACING EMERGENCY LIGHT BATTERY CHARGER WOULD NOT TEST. REPLACED BATTERY CHARGER PER AMM 33-51-01.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 27,985 hrs · 4,194 cycles

WHILE REPLACING EMERGENCY LIGHT BATTERY AT STA 1340 FOUND BATTERY CHARGER WOULD NOT TEST. REPLACED BATTERY CHARGER PER AMM 33-51-07.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 27,985 hrs · 4,194 cycles

WHILE REPLACING EMERGENCY BATTERY AT STA 1010 CHARGER WOULD NOT TEST. REPLACED CHARGER PER AMM 33-51-07.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 27,985 hrs · 4,194 cycles

WHILE REPLACING EMERGENCY LIGHT BATTERY PACK AT STA 841 FOUND BATTERY CHARGER WOULD NOT TEST. REPLACED CHARGER PER AMM 33-51-07.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 27,985 hrs · 4,194 cycles

WHILE REPLACING EMERGENCY LIGHT BATTERY AT STA 1362 FOUND BATTERY CHARGER WOULD NOT TEST. REPLACED BATTERY CHARGER PER AMM 33-51-07.

Part: FLOORBEAM — CORRODED (BS 303) · airframe 22,553 hrs · 3,432 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT BS 303, LBL 28 TO 50. THE CORROSION WAS REMOVED AND THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, REPAIR 1, FIGURE 201.

Part: FLOORBEAM — CORRODED (BS 325) · airframe 22,553 hrs · 3,432 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT BS 325, LBL 30 TO LBL 55. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, REPAIR 1, FIGURE 201.

Part: FLOOR SUPPORT — CORRODED (BS 303-325) · airframe 22,553 hrs · 3,432 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 303-325, LBL 30. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02.

Part: ELECTRICAL BOX — OVERHEATED (SEAT 19DEF) · airframe 16,863 hrs · 2,628 cycles

FLIGHT CREW REPORTED SMOKE COMING FROM BELOW SEAT 19E WHILE ENROUTE FROM AMS TO EWR. THE SMOKE LASTED FOR ONLY ABOUT 15 SECONDS. AN EMERGENCY DECLARED AND AIRCRAFT LANDED AT EWR W/O INCIDENT. MECHANIC FOUND THE DSEB (DIGITAL SEAT ELECTRONIC BOX) AT SEAT GROUP 19DEF HAD A BURNED SMELL BUT NO VISUAL EVIDENCE OF FIRE. THE DSEB WAS REMOVED AND REPLACED IAW MM 23-38-55. THE CONNECTORS WERE VISUALLY INSPECTED AND LOOKED GOOD. OPS CHECKS WERE NORMAL. INITIAL EXAMINATION OF THE UNIT REVEALED THAT THE COOLING FANS APPEARED TO BE BLOCKED. THERE WAS DEBRIS (PARTICLES OF FOOD) ON TOP OF AND AROUND THE DSEB. MODIFICATIONS PLAN TO BE INCORPORATED INTO THE UNITS TO HELP PREVENT THIS TYPE OF FAILURE IN THE FUTURE.