N77066

Part: BLOWOUT PANEL — DETACHED (ZONE 500) · airframe 93,117 hrs · 14,774 cycles

LEFT WING LE SLAT PANEL MISSING SDR FLAGGED NR 5 SLAT OTBD SADDLE BRACKET ATTACHED TO THE BLOWOUT PANEL MISSING ALONG WITH WITH BLOWOUT PANEL. ENGINEERINGS ASSISTANCE REQUESTED. REQUIREMENTS OF ECRA: 5743-02021 CARRIED OUT. NO ADDITIONAL FINDINGS FOUND, LEAK CHECKS CARRIED OUT WITH NIL LEAKS, SLATS OPERATE AS NORMAL. CARRIED OUT PER ECRA 5743-02021. AC IS IN CONDITION AND CONFIGURATION FOR MX FERRY BACK TO THE STATES FOR PERM REPAIR.

Part: PRESSURE GAUGE — NO DISCREPANCY (ZONE 800) · airframe 92,609 hrs · 14,707 cycles

DOOR 3L SLIDE PRESSURE GAUGE LOW. INSPECTED SLIDE PRESS GUAGE AT DOOR 3 L, SLIDE IS IN THE GREEN. IAW 25-66-02 OK TO CONTINUE.

Part: FUEL SYS — LEAKING (APU) · airframe 92,173 hrs · 14,650 cycles

CREW REPORTS FUEL SMELL IN CABIN. FUEL FOUND LEAKING FROM APU COPMARTMENT. APU FUEL CONTROLLER LEAKING AT SURGE CONTROL VALVE SUPPLY AND RETURN LINES. REMOVED SUPPLY LINES TO IGV ACTUATOR, FUEL FLOW DIVIDER, AND SCV REF AMM TASK 49-31-01-004-001-001. FOUND PACKINGS TO SUPPLY AND RETURN LINES DAMAGED. REPLACED PACKINGS REF AIPC 49-31-00-02 AND REINSTALLED LINES. NO LEAKS NOTED.PARTS USED: 00-0596-3-1775, QTY :1 00-0586-3-0518, QTY :1 OPERATED APU AND PACKS FOR 30 MINS. NO LEAK NOTED AND ODOR IN CABIN DID NOT RETURM.

Part: COVER — DAMAGED (ZONE 800 SLIDE) · airframe 91,999 hrs · 14,627 cycles

DOOR 2R SLIDE COVER DAMAGED. INSPECTED DOOR 2R SLIDE COVER AND SURROUNDING AREA. COULD NOT FIND ANY DISCREPENSIES. REF AMM 25-66-00.

Part: PCB — FAULTED (ZONE 400) · airframe 91,556 hrs · 14,568 cycles

LOST AIR DRIVEN PUMP ON TAKE OFF-AIR PRESSURE LIGHT ON WITH SWITCH POSITION AT ON OR AUTO. PER CREW UPDATED ON TAKE OFF GEARS SELECTED HYDRAULICS PRESSURE WENT TO LOW , CREW FOLLOWED CHECKLIST FOR EICAS MESSAGES. ADP SWITCH AUTO TO ON PRESSURE LIGHT ON THE WHOLE TIME . ADDING PICTURE OF AUTO EVENT FOR LOW C HYD PRESSURE. PERFORMED FIM 28-11 TASK 896, R&R ADP OVERSPEED ECC M11291 IN THE P50 CARD FILE. PERFORMED OPS CHK FOR EEC INSTALLATION, CENTER ADP FUNCTIONS NORMALLY, ADP PRESSURE LIGHT GOES OUT WHEN ADP IS TURNED TO AUTO AND ON. C HYD PRESSURE BETWEEN 2800-3200. NO FURTHER DEFECTS FOUND AT THIS TIME.

Part: BLEED VALVE — FAULTED (NR 2 ENGINE) · airframe 90,733 hrs · 14,459 cycles

AFTER ADDING TAKEOFF POWER R ENG BLEED AND R PACK MESSAGE APPEA RED. REJECTED AT 85KTS. REQUEST APPROVAL TO DEFER RH HPSOV IAW MEL 3611BR. ENGINE HIGH PRESSURE SHUTOFF VALVE (HPSOV) INOPERATIVE SECURED CLOSED. ASSOCIATED THRUST REVERSER IS CONSIDERED INOPERATIVE. RH HPSOV DEFERRED IAW MEL 3611BR ESN 706217 ENG 2 REMOVED

Part: PRESSURE SWITCH — FAULTED (NR 2 ENG FUEL) · airframe 90,641 hrs · 14,447 cycles

DEBRIEFED CREW, NO OVWT LANDING, 32K FEET, FUEL FILTER BYPASS R MSG, ENG APPEARED AND SHOWED NORMAL, ALL INDICATIONS NORMAL. 2 HRS OUT. ADVISORY TO STATUS. 304-283-6970. PILOT. REMOVED AND REPLACE #2 ENGINE FUEL FILTER REF AMM 73-11-02-404-008-H00, LEAK CHECK GOOD. OPS CHECK SATISFACTORY. REMOVED & REPLACED FUEL FILTER DIFFERENTIAL PRESSURE SWITCH REF AMM 73-34-01. NO LEAKS FOUND AFTER ENGINE RUN. OPS CHECK GOOD. PERFORMED HIGH POWER RUN ON NBR 2 ENGINE NO MESSAGES APPEARED. ALL ENGINE INDICATIONS NORMAL.

Part: PRESSURE SWITCH — FAULTED (ZONE 600) · airframe 90,407 hrs · 14,416 cycles

RIGHT FWD WING PRESSURE SWITCH REQUIRE REPLACEMENT PER JC 2820-02563-002 REMOVED AND REPLACED RIGH FWD PRESSURE SWITCH IAW AMM 28-42-01. OPS CK GOOD CK GOOD.PARTS

Part: BLOWOUT PANEL — MISSING (NR 4 SLAT) · airframe 90,407 hrs · 14,416 cycles

PDA 2 REF LOGPAGE 4431885, LEADING EDGE #4 SLAT INBOARD BLOWOUT PANEL FOUND MISSING. REATTCHED NEW BLOWOUT PANEL TO LEADING EDGE SLAT PANEL PER SRM 51-40-02.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 89,609 hrs · 14,316 cycles

SEAT 1F EMERGENCY PATH LIGHT INOP. LIGHT MODULE REPLACED PER AIPC 33-27-00-66. LIGHT WORKING AS EXPECTED. ITEM OK.

Part: SKIN — CRACKED (ZONE 400) · airframe 87,510 hrs · 14,031 cycles

NO.1 PYLON STA 231 UPPER SPAR ELECT CABLE CUTOUT SKIN FOUND CRACKED TRANSFER REF. NON-ROUTINE HX NRC WO.3334709. NO.1 PYLON STA 231 UPPER SPAR WEB CUTOUT AT NAC STA 231 INTERIM REPAIR AS PER EC/RA 5450-02942 REV ORIG PART 1 ITEM A AND CREATED DIP L/P 8704630. RII INSPECT IS OKAY.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 87,510 hrs · 14,031 cycles

CABIN - STA 303 LBL 44 FLR BEAM FOUND CORRODED AS MARK TRANSFER REF. NON-ROUTINE HX NRC WO.3322377. CABIN STA 303 FLOOR BEAM LBL 6 TO LBL 63 REPAIRED AS PER ECRA 5310-08370 REV ORIG. ATTACH MAINTENANCE WORKSHEET FORM 44-0008 ITEM 1 TO ITEM 31 ACCOMPLISHED. (CATEGORY A REPAIR).

Part: STIFFENER — DAMAGED (ZONE 200) · airframe 87,510 hrs · 14,031 cycles

REFER TAR 33 ACCOMPLISHMENT DRAFT RI 53-00-16938 REV A FIG.8, ITEM 15 - CUT STIFFENER AND INSTALL SPLICE BUT PRESSURE DECK O/B SIDE PREVIOUSLY DOUBLER REPAIRED INTERFRENCE NEW SPLICE INSTALL. TRANSFER REF. NON-ROUTINE HX NRC WO.3376315 CABIN STA 955 LBL 85.9 PRESSURE DECK STIFFENER RESTORATION EXISTING REPAIR INTERFERENCE LOCATION SPLICE REPAIRED AS PER ECRA 5340-02201 REV ORIG.

Part: FITTING — CORRODED (CABIN) · airframe 87,510 hrs · 14,031 cycles

BS955 LH T-FITTING FWD LWR FOUND CORRODED. BS955 LH "T"FITTING REPLACED AS PER ECRA 5340-02196 REV- ATTACH MAINTENANCE WORKSHEET 44.0008 ITEM 1-8.

Part: TEE FITTING — CORRODED (RH T-FITTING) · airframe 87,510 hrs · 14,031 cycles

BS 955 RH TEE FITTING FWD LWR FOUND CORRODED. BS 955 RH TEE FITTING REPLACED AS PER EC/RA 5340-02197 REV ORIG. ATTACHED MAINTENANCE WORK SHEET FORM 44-0008 ITEM 1 TO 8 ACCOMPLISHED.

Part: SHEAR TIE — CORRODED (BS 1540 S38-39L) · airframe 87,510 hrs · 14,031 cycles

BULK CARGO COMPT-BELOW FLOOR SHEAR TIE FOUND CORROSION AT STA 1540 BTN S38L TO S39L BULK CARGO COMPT BELOW FLOOR AT STA1540 S38L-S39L SHEAR TIE REPLACED IAW SRM51-10-02 AND FASTENER INSTALLED IAW SRM51-40-02 FORM 44-0008 ITEM1-12 .

Part: PUMP — INOPERATIVE (MAIN FUEL TANK) · airframe 87,022 hrs · 13,969 cycles

CREW REPORTED RT FWD BOOST PUMP INOP WITH LOW PRESS LIGHT ILLUMINATED AND EICAS MSG DISPLAYED INDICATION ISSUE. SUSPECT GFI TRIPPED DUE PUMP IS DEFECTIVE. REC STILL OPEN FOR THE GFI TEST. THE GFI TEST IS AN ALI NEED AN IDT OMMEND TO RPL BOTH. INSPECTION. PARTS USED: 9324G10675,QTY :1 ACCOMPLISHED CDCCL/ALI INSPECTION OF FUEL BOOST PUMP INSTALLATION, ELECT HARNESS/CONNECTOR AND BONDING RESISTANCE CHECK REF 767 AMM 28-22-03-404-074. BONDING RESISTANCE IS 0.29 MILLI OHMS. PUMP INSTALLATION ACCEPTABLE. DEBRIEFED CREW AND NOTED APPROX 3HRS INTO CRUISE, RT FWD BOOST P PICS ADDED OF BOOST PUMP AND P6-3 CB PANEL. ACCOMPLISHED SCEPTRE -9 ROTABLE PARTS CHANGE ONLY. REPLACED THE RFWD FUEL BOOST PUMP GFI RELAY K10704 IN P141 REF INSTALLED RH FWD BOOST PUMP REF AMM 28-22-03--404-074. ADDED INSPECTION FOR THE GFI OPERATIONAL TEST REF AMM ACP THE FAULT INTERPUTER GFI OPERATIONAL TEST FOR THE RFWD BOOST INSPECTION REQUEST FOR THE OPERATIONAL TEST. ADDED INSPECTION ACCOMPLISHED ALI INSPECTION AND THE GROUND FAULT INTERPUTER UMP INOP FAILED. AT ARRIVAL, CONFIRMED SUBJECT BOOST PUMP DOES N ROTABLE PARTS CHANGE WAS INDICATED - TT # 1540208 SN OFF 3498 AMM 28-22-18. NEED TO ACCOMPLISH THE GROUND FAULT INTERPUTER 28-22-00-715-696 PUMP RF AMM 28-22-00-715-696 (GFI) OPERATIONAL TEST REF TASK 28-22-00-715-696. TEST IS OT OPERATE BY FEEL AT PUMP ACCESS AND LOW PRESS LT STAYS ILLUMIN (GFI) OPERATIONAL TEST REF TASK 28-22-00-715-696 AFTER THE RFWD ACCEPTABLE. ATED. DUE DIVERSION INTO SFO, NEED TS. THI

Part: TRANSMITTER — DEFECTIVE (LT WING TE FLAP) · airframe 85,423 hrs · 13,739 cycles

FLAP ASYM L FL25 R FL30. DE-BRIEFED WITH CREW, AT FLAPS 25 ALL NORMAL,THEN WENT TO FLAP 30, RT SIDE WENT TO 30 LEFT SIDE WENT TO 25. FLT CHARACTERISTICS WERE GOOD WITH ONLY 2 UNITS OF RUDDER TRIM. SEE PIC RAN FLAP FULL DOWN AND FULL UP MULTIPLE TIMES. FAULT EICAS MSG WAS INTERMITTENT AT DIFFERENT INTERVALS. FLAPS APPEAR TO BE MOVING SMOOTHLY AND TOGETHER WITH NO BINDING SOUNDS. PERFORMED FSEU BITE PER AMM TASK 27-51-00-735-080. NO CURRENT FAULTS RECORDED. FLIGHT LEG 0 HAD MULTIPLE FAULTS. FURTHER TROUBLESHOOTING REQUIRED. TRANSMITTER, FL OFF 64-2751-9-0016 0175 ON 64-2751-9-0016 0030 TRANSMITTER, FL OFF 64-2751-9-0016 0175 ON 0000 FOUND ON LAST LEG 0 MSG ON THE FSEU FOR TE SKEW XMT 2 THAT HIT WHILE PLANE WAS FLYING AT 135 KNOTS. REPLACED AND INTSALLED #2 FLAP POSITION XMIT IN REFERENCE WITH AMM 27-51-45. COMPLETED AND CHECKED ADJUSTMENT. NOT FAULTS FOUND AT THIS TIME. PARTS ADD EMP:U389299 USED: 64-2751-9-0016,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1262315 SN OFF 0175.

Part: FAN — FAULTY (STA 434, ZONE 12) · airframe 84,883 hrs · 13,661 cycles

EQUIP COOLING OVHT LIGHT ON/W STATUS MSG FWD EQ SUP FAN 1 CHECK OVERHEAD P6 PANEL BREAKER C331 CONTINUITY, PERFORM VISUAL AND CONTINUITY CHECKS OF K629 RELAY, K343 RELAY AND P11-3 CB C65 WAITING TOMC APPROVAL MAINTENANCE PROCEDURE C/OUT TOMC APPROVAL GRANTED 4 AS WELL. PERFORM CONTINUITY CHECK OF THE FAN THERMAL CIRCUIT, IF NO DEFECTS FOUND ON THESE RELAYS AND CBS CONTINUE TO STEP THR OUGH FIM 21-58 TASK 855 FROM BEGINNING. NOTE DOWN FAN VMU STATUS LIGHT COLOR ON SEPARATE LP AND ANY MM PRESENT. PERFORM THE VIBRATION MONITOR RESET AT THE END WHEN ROOT CAUSE IDENTIFIED. (STATUS) FWD EQ SUP FAN 1 DEFERRED REF MEL 2158X REQUIRES FAN VIBRATION MONITOR 99-2125-9-9005 NIS IN EWR ADD EMP:U397952 PART NUMBER CORRECTION UPDATE AIRCRAFT REQUIRES P/N 99-2158-3-0024 FWD EQUIPMENT COOLING SUPPLY FAN VMU BLINKS GREEN-RED, SHOWS PRIOR FAN FAULT. TRIED BYPASSING VMU AND RUNNING FAN DIRECTLY REMOVED AND REPLACED FWD EQUIPMENT COOLING SUPPLY FAN VMU AS PER AMM TASK 21-58-06-000-947-C1 & TASK 21-58-06-400-947-C1. NO BUT STATUS MSG:"FWD EQ SUP FAN 1" APPEARS AND HORN SOUNS. REMOVED AND REPLACED RELAY K343, FAN WORKS WHEN VMU BYPASSED BUT WITH THE VMU CONNECTED, BLINKS RED AND GREEN. HELP, FAN RAN FOR 6 MINUTES BEFORE SHUTTING OFF. TRIED VMU RESET PROCEDURE AND ALSO NO HELP. REQUIRES FURTHER T/S. COMPLIED WITH DDP PROCEDURES, ITEM REMAINS ON MEL. REF L/P:5886560 FOR WORK PERFORMED. T/S PER FIM 21-58 FAULT TREE 855. REQUIRES REPLACEMENT OF FWD SUPPLY FAN B10 PER FIM.

Part: RUB STRIP — MISSING (ENG #2 EXHST NOZ) · airframe 82,588 hrs · 13,312 cycles

PDA 3 #2 ENG EXHAUST NOZZLE 1 WEAR PAD MISSING AND 1 WEAR PAD LOOSE AT 7 O-CLOCK POS AFT LOOKING FWD. REPLACE THE LOOSE, DAMAGED, AND/OR MISSING RUB STRIPS WITHIN 10 DAYS OR 10 CYCLES, WHICH EVER COMES FIRST. INSTALLED NEW WEAR PADS.

Part: TRANSCEIVER — FAILED (LT & RT WXR) · airframe 80,963 hrs · 13,055 cycles

BOTH SIDES WX RADAR FAILED IN FLIGHT TESTED BOTH RADAR SYSTEMS, SYSTEM TEST. LEFT SYSTEM TESTED NORMALLY, BUT SELECTING MODE WX+T CAUSED RADAR TO SPOKE. REPLACED LEFT RADAR TRANSCIEVER AND RETESTED VIA SYSTEM TEST, LEFT RADAR TESTS GOOD.

Part: PANEL — MISSING (RH PYLON 621CB) · airframe 79,480 hrs · 12,823 cycles

PDA 2 DURING WALKAROUND FOUND MISSING PANEL ON RT WING OUTBD OF PYLON. PANEL 621CB. UPDATED WITH PICTURES INSTALLED PANEL REF AMM 57-41-01

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 77,868 hrs · 12,565 cycles

LEFT INBOARD AFT FLAP HAS MULTIPLE DENTS IN UPPER SURFACE, THE BIGGEST BEING 1.25 INCH DIAMETER .095 INCH DEEP. TAP TESTED NO DELAMINATION NOTED. ITEM REVIEWED AND LOCKED FOR MAINT FERRY UNLOCKED FOR MAINTENANCE FOR L/P 6678263 LHW INBOARD AFT FLAP T/E WEDGE DAMAGE AREA PERFORM REPAIR AS PER UNITED EC/RA 5753-01941 REF FORM 44.0008 ITEM 1-21.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 77,868 hrs · 12,565 cycles

RIGHT INBOARD AFT FLAP UPPER SURFACE HAS MULTIPLE DENTS, THE LARGEST BEING 1.5 INCH DIAMETER, .090 INCH DEEP. TAP TESTED NO DELAMINATION NOTED. ITEM REVIEWED AND LOCKED FOR MAINT FERRY UNLOCKED FOR MAINTENANCE FOR L/P 6678313 RHW INBOARD AFT FLAP T/E WEDGE DAMAGE FOR UPPER AREA PER UNITED EC/RA 5753-01942 REF FORM 44.0008 ITEM 1-21 ACCOMPLISHED.

Part: SKIN — CRACKED (BS1630-1654) · airframe 77,868 hrs · 12,565 cycles

FUSELAGE SKIN 4 EACH CRACKS FOUND AT STA1630-1654 STR 14AR WHILE PERFORMING INSPECTION BY EA 5380-01178 OPS 004. INSTALLED DOUBLER REPAIR STA 1630-1654 STR 14AR IAW SRM 53-80-01-2R-7 REPAIR 7 FIG 201. REPAIR IS PERMANENT CAT B. INSPECTION THRESHOLD IS 30,000 FLT CYCLES AFTER ACFT DELIVERY OR WITHIN 7500 FLT CYCLES FROM THE REPAIR INSTALLATION, WHICHEVER COMES LAST. REF SRM 53-80-01-2R-7 REPAIR 7 INSPECTION REQRMNTS PARAGRAPH 5 TABLE 202.

Part: SKIN — CRACKED (BS1630-1654 S14R) · airframe 77,868 hrs · 12,565 cycles

SUPPORT TASK EA 5380-01178 REV A OP 4 4EA CRACKS FOUND BETWEEN B S1630 AND BS 1654 STR -14AR FUSELAGE SKIN TRANSFER REF NR LP 913 0582 AND ORIGINATED BY EMP V924736 FX- SKIN BETWEEN BS1629-BS1654 S-14AR PERMANENT REPAIRED (CAT B) AS PER SRM 53-80-01-2R-7 REPAIR 7 FIG 201 WORK DETAIL REFER TO ATTACH FORM 44.0008 ITEM 1 TO 23 ACCOMPLISHED AND WORK ACCOMPLIS HED BY EMP V906028 AND INSPECTED HX243551 INSPECTED BY HX139007, APPROVED

Part: STIFFENER — CRACKED (NLG WW) · airframe 77,868 hrs · 12,565 cycles

AD2017-17-16 SUPPORT TASK EA 5310-07143 REV D 1EA CRACK FOUND ON L/H NOSE WHEEL WELL STIFENER ON STA 287 BETWEEN WL 159 TO 185 A T RADIUS AREA APPROX 3/4" IN LENGTH PLS PRINT AND ACCOMPLISH OP 003 TRANSFER REF NR LP 9130932 AND ORGINATED BY EMP V898555 REPAIR REFER TO EA 5310-07143 REV D OP 003 SEQ 1351 HX JOB YXX01 3519 WORK ACCOMPLISHED BY EMP V898555 AND INSPECTED BY HX243551 ADD EMP:V898555 INSPECTED BY HX139007, APPROVED

Part: STIFFENER — CRACKED (NLG WW) · airframe 77,868 hrs · 12,565 cycles

AD2017-17-16 SUPPORT TASK EA 5310-07143 REV D 1EA CRACK FOUND AT R/H NOSE WHEEL WELL STIFFENER ON STA 287 BETWEEN WL 159 AND 185 AT RADIUS AREA APOPROC 7/8" IN LENGTH PLS PRINT AND ACCOMPLISH OP 004 TRANSFER REF NR LP 9130933 & ORIGINATED BY EMP V898555 REPAIR REFER TO EA 5310-07143 REV D OP 004 SEQ 1354 HX JOB YXX01 3543 WORK ACCOMPLISHED BY EMP V898555 AND INSPECTED BY HX243551 INSPECTED BY HX139007, APPROVED

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,850 hrs · 12,561 cycles

EMERGENCY BATTERY PACK NEEDS TO BE REPLACED. ROW 30 LK. REPLACED BATTERY PACK ROW 30 LK. REF 767/400 AMM 33-51-07

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,850 hrs · 12,561 cycles

EMERGENCY BATTERY PACK NEED TO BE REPLACED POSITION ROW 41 BA REPLACED EMERGENCY BATTERY PACK POSITION 41BA REF. B767-400 AMM 33-51-07

Part: ACCESS PANEL — MISSING (NR 2 PYLON) · airframe 75,825 hrs · 12,253 cycles

REF LOG 3221237, NUMBER 2 ENG PYLON INBD NACELLE STRUT ACCESS PANEL MISSING. REF GMM 02-30-95 PDA CAT 2.

Part: ACTUATOR — FAULTY (SPOILER) · airframe 75,780 hrs · 12,247 cycles

SPOILER EICAS SHORTLY AFTR T/O. SUSPCT SPLR EXTNSN. A/C ROLLED RT ROTATN AND THROUT FLT. FOUND #10 SPOILER UP ABOUT 4" ABOVE THE WING, WITH HYDRAULICS APPLIED #10 SPOILER WENT TO FULL UP POSITION WITH SPOILER HANDLE IN STOWED POSITION. T/S REF. FIM 27-09-00-815-808 FOUND SPOILER CONTROL MODULE 2 LEFT " PCA 10 FAULT". REMOVED #10 SPOILER PCA REF. AMM 27-61-00. STARTED NEW PCA INSTALLATION REF. AMM ACTUATOR, OUTBO OFF 76-2763-9-0002 3868 ON 76-2763-9-0002 3098 27-61-02-424-023 STEPS G(1)-(9). NEED TO CONTINUE INSTALLATION FROM STEP G(10). ROTABLE PARTS CHANGE WAS INDICATED - TT # 1120349 SN OFF 3368 IPC REFERENCE # 27-61-02-01B INSTALATION OF SPOILER ACTUATOR VERIFIED PART NUMBER AND ACOMPLISHED RII INSPECTION OF THE COMPLETED INSTALLATION REF TO LOG PAGE 3179249.

Part: CLOSEOUT PANEL — DAMAGED (LE SLAT) · airframe 73,741 hrs · 11,971 cycles

PDA 1 REF LP 9125027, LEFT WING LEADING EDGE SLAT PANEL MISSING PIECE OF CLOSURE PANEL. REFERENCE IPC 27-81-02-10A SHEET 7 ITEM 345J PART NUMBER 114T4151-401. LOG PAGE ENTERED TO REPORT SDR REPORTABLE. ENTRY MADE TO CORRECT ATA.

Part: SEAL — SEPARATED (SLIDING WINDOW) · airframe 71,355 hrs · 11,641 cycles

LOUD HIGH PITCH SOUND COMING FROM CAPTAIN WINDOW CAPTAINS NUMBER 2 SLIDING WINDOW INSPECTED AND FOUND TO HAVE GLASS TO FRAME SEAL IN POOR CONDITION. CAPTAINS NUMBER 2 WINDOW ASSY REPLACED AS PER AMM 56-11-02-004-001. CABIN PRESSURISED TO 4PSI DIFF PRESSURE AS PER AMM 05-51-24-782-001-001 AND NO LEAKS EVIDENT. ROTABLE PARTS CHANGE WAS INDICATED - TT 1636382 SN OFF 0851 WINDOW, AY, PIL OFF 76-5613-9-9001 0851 ON 76-5613-9-9001 0376.

Part: O-RING — LEAKING (SPOILER PCA) · airframe 70,341 hrs · 11,507 cycles

RIGHT HYD QTY EICAS MESSAGE QTY DROPPED FROM 0.51 TO 0.46. ON ARRIVAL NOTICED HYD LEAK COMING FROM RIGHT OUTBOARD AFT FLAP INBOARD TRACK FAIRING AREA. THE PUMP WAS TURNED OFF IAW DVI. NR 11 SPOILER PCA LEAKING FROM HYD FILTER HOUSING CAP O-RING. REMOVED, INSPECTED & REPLACED THE NR 11 SPOILER PCA FILTER & CAP O-RING ASSY IAW AMM 27-61-02 I 1-9. LEAK & OPS CHECKED GOOD. TOPPED OFF HYD QTY. & CYCLED ALL FLT CONTROLS MULTIPLE TIMES TO BLEED OUT SYSTEM & CONFIRM INTEGRITY.

Part: SPAR — CRACKED (NR 1 NACELLE) · airframe 70,255 hrs · 11,495 cycles

NR 1 PYLON MID SPAR WEB FOUND CRACKED AT THE IDG FEED THROUGH CUTOUT, THE SPAR WEB WAS REPAIRED IAW SRM 54-55-01, REPAIR 2, FIG 202.

Part: WEB — CORRODED (BS 955-977) · airframe 70,255 hrs · 11,495 cycles

CABIN BS 955 TO 977, LBL 86 TO 97, WHEEL WELL UPPER FACE SLOPE WEB FOUND CORRODED. REPAIRED IAW ECRA 5310-07418, REV-, PART 1. INTERIM REPAIR.

Part: FLOORBEAM — CORRODED (BS 325) · airframe 70,255 hrs · 11,495 cycles

FLOORBEAM, BS 325, LBL 27 - 57 WAS FOUND CORRODED. REPAIRED THE FLOORBEAM IAW ECRA 5315-01104.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 70,255 hrs · 11,495 cycles

COCKPIT DOOR OVERHEAD EXIT LIGHT FOUND DIM. THE EXIT LIGHT ASSY WAS REPLACED AND THE LAMP TESTED NORMAL IAW AMM 33-51-01.

Part: UNKNOWN — ODOR (CABIN) · airframe 68,600 hrs · 11,272 cycles

CABIN ROWS 22-26 HAS A FUEL ODOR. PERFORMED ENGINES HIGH POWER SETTING WITH PACKS ON AND OFF IAW MM 71-00-00. FOUND NO EVIDENCE OF FUEL ODOR OR LEAKS AT THIS TIME.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 68,085 hrs · 11,189 cycles

EMERGENCY LIGHT LENS MISSING, AFT OF THE L1 DOOR AT STORAGE CLOSET CORNER. REPLACED THE LENS .

Part: TUBE — LEAKING (NR 2 ENGINE OIL) · airframe 67,529 hrs · 11,118 cycles

RIGHT ENGINE OIL QTY 5, WITH ENGINE AT IDLE AT 10000 FT. REMOVED THE TUBE B SCAVENGE INTO THE REAR CASE. THE TUBE THAT GOES INTO THE CASE HAS A SEAL WHICH LOOKS WORN AND OIL BYPASS AROUND SEAL. SEEMS TO BE CIRCUMFERENTIAL PLAY AROUND THE TUBE. REMOVED AND REPLACED NR 2 ENGINE LEAK AND OPS CHECKED GOOD IAW WORK CARD 64-7100-1-9800.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 66,015 hrs · 10,908 cycles

EMERGENCY LIGHT OUT AT ROWS 42,43,44 DEF. R&R POWER SUPPLY AND BATTERY PACK FOR SEATS 42,43,44 DEF IAW AMM 33-51-07-022-005-001 AND AMM 33-51-07-402-018-001. OPS CHK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 64,377 hrs · 10,656 cycles

LT EXTERIOR AFT SERVICE DOOR EMERGENCY LIGHT INOP. REMOVED CORROSION FROM LAMP HOLDER AND RELAMPED. NO HELP. SUSPECT BAD SOCKET. RELAMPED LIGHT, OPS CHECK NORMAL.

Part: WIRE — LOOSE (LIGHT SWITCH) · airframe 63,364 hrs · 10,515 cycles

EMERGENCY LIGHT SWITCH ON OVERHEAD PANEL, ACTIVATION WIRE IS LOOSE. REMOVED AND REPLACED SWITCH GUARD AND OPS CHECKED GOOD.

Part: POWER SUPPLY — DEFECTIVE (COCKPIT) · airframe 59,607 hrs · 10,020 cycles

SUPPORT TASK, COCKPIT ONE EACH EMER LIGHT FOUND DIM. COCKPIT EMER LIGHT POWER SUPPLY ASSEMBLY REPLACED & TEST CARRIED OUT NORMAL IAW AMM 33-51-07.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 59,607 hrs · 10,020 cycles

SUPPORT TASK, L2 DOOR EXTERIOR EMER LIGHT FOUND DIM. M6759 POWER PACK & BATTERY CHARGER REPLACED & TESTED NORMAL IAW AMM 33-51-07 & AMM 33-51-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,607 hrs · 10,020 cycles

SUPPORT TASK, L4 DOOR EXTERIOR EMER LIGHT FOUND DIM. M739 POWER PACK REPLACED & L4 DOOR EXTERIOR EMER LIGHT LAMP TESTED NORMAL IAW AMM 33-51-07 & AMM 33-51-00.

Part: ACTUATOR — LOOSE (LT MLG) · airframe 57,658 hrs · 9,774 cycles

LEFT MLG AFT SIDE BRACE DOWN LOCK ACTUATOR LOWER ROD END LOCK IS LOOSE. REMOVED LT MAIN GEAR LOCK ACTUATOR IAW AMM 32-32-02 MV 41991. INSTALLED LT GEAR LOCK ACTUATOR IAW AMM 32-32-02. LEAK CHECKED & OPERATIONS CHECKED OK. ROTABLE PARTS CHANGE WAS INDICATED. TT 0783450, SN OFF 00053 ACTUATOR, MLG, OFF 64-3232-9-0010 0053 ON 64-3232-9-0010 0037.

Part: SKIN — DAMAGED (BS 654 S31R) · airframe 21,945 hrs · 4,072 cycles

SKIN BS 654+22, STG 31RT DAMAGED. REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR A .

Part: SKIN — CRACKED (RT WING SLAT) · airframe 46,643 hrs · 8,326 cycles

RT WING 10 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED RT WING 10 SLAT OTBD SKIN REPARED IAW SRM 57-43-01, REPAIR 2, FIG 201 AND HFEC NIL CRACK FOUND ATTACH MX WORK SHEET.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 46,643 hrs · 8,326 cycles

RT WING 9 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED RT WING 9 SLAT INBD NOSE SKIN REPAIRED IAW SRM 57-43-01, REPAIR 2, FIG 201 AND HFEC NIL CRACK FOUND ATTACH MX WORK SHEET.

Part: SHEAR TIE — CORRODED (BS 1417) · airframe 46,643 hrs · 8,326 cycles

FOUND CORROSION ON THE SHEAR TIE AT BULK CARGO BS1417 BL0 BULK CARGO, BS1417 BL0. SHEAR TIE REPLACED IAW SRM 31-10-02 AND FASTENER INSTALLED IAW SRM 51-40-01 ATTACH MX WORK SHEET FORM 44.0008 ITEM 1 TO 2 ACCOMPLISHED.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 46,643 hrs · 8,326 cycles

LT WING 3 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED LT WING 3 SLAT OTBD NOSE SKIN RIVET AREA. REPAIRED IAW SRM 57-43-01. REPAIR 2, FIG 201 AND HFEC NIL CRACK FOUND ATTACH ACCOMPLISHED WORK SHEET FORM 44.0008 ITEM 1 TO 17.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 46,643 hrs · 8,326 cycles

LT WING 3 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED LT WING 3 SLAT INBD NOSE SKIN REPAIRED IAW SRM 57-43-01. REPAIR 2, FIG 201 AND HFEC CRACK FOUND ATTACH MX WORK SHEET.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 46,643 hrs · 8,326 cycles

LT WING 4 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED LT WING 4 SLAT INBD NOSE SKIN REPAIRED IAW SRM 57-43-01, REPAIR 2, FIG 201 AND HFEC NIL CRACK FOUND ATTACH MX WORK SHEET.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 46,643 hrs · 8,326 cycles

RT WING 10 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED, RT WING 10 SLAT INBD NOSE SKIN REPAIRED IAW SRM 57-43-01, REPAIR 2, FIG 201 AND HFEC NIL CRACK FOUND ATTACH MX WORK SHEET.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 46,643 hrs · 8,326 cycles

RT WING 9 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING 9 SLAT, OTBD NOSE SKIN REPAIRED IAW SRM 57-43-01. REPAIR 2, FIG 201 AND HFEC CRACK FOUND ATTACH MX WORK SHEET.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 46,643 hrs · 8,326 cycles

LT WING 4, SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED LT WING 4 SLAT OTBD NOSE SKIN REPAIRED IAW SRM 57-43-01, REPAIR 2, FIG 201 AND HFEC NIL CRACK FOUND ATTACH MX WORK SHEET.

Part: FLOORBEAM — CORRODED (BS 325) · airframe 46,643 hrs · 8,326 cycles

CABIN BS 325, LBL 21-55 FLOORBEAM CORRODED CABIN BS325, LBL 11-65 FLOORBEAM UPR CHORD FLANGE REPAIRED IAW SRM 53-00-51. REPAIR 1, FIG 201 AND HFEC NIL CRACK FOUND ATTACH MX WORK SHEET FORM 44.0008, ITEM 1-34 ACCOMPLISHED.

Part: FLOORBEAM — CORRODED (BS 303) · airframe 46,643 hrs · 8,326 cycles

CABIN BS 303, LBL 21-53, FLOORBEAM CORRODED CABIN BS 303 LBL9" TO LBL 65" FLOORBEAM UPPER CHORD FLANGE REPAIR ED IAW SRM 53-00-51, REPAIR 1, FIG 201 AND HFEC CRACK FOUND ATTACH MX WORK SHEET FORM 44.0008 ITEM 1 TO 30, ACCOMPLISHED.

Part: MONITOR — MALFUNCTIONED (HYDRAULIC SYS) · airframe 42,179 hrs · 7,690 cycles

RT HYD QTY IND INOP FAULT CONFIRMED. PERFORMED VIS INSP EXT & OPS CKED ALL SURFACES NTF & NO LEAKAGE FOUND. HYD PRESS IND SYS NORMAL. ALSO RT RES TANK VIS INSP FULL & NO LEAKAGE. ITEM DEF PER MEL 29-33-02R C/N 565391. FLWD DDPG COMPLETED PER MEL 29-33-02 CHK'D CONTINUITY FROM D2704B & D60 PER WDM29-33-11, CHK'S GOOD. (CONT) EXTENSION C/N: 066083012. VERIFIED GROUND(S) AT D2704B & D60, ALSO CHK'S GOOD. NO TIME TO MEG WIRES, PLA REMAINS FOR FURTHER TROUBLESHOOTING. VERIFIED HYD QTY AT RESERVOIR PER MEL 29-33-02R, OK TO CONTINUE. NEED TO CHECK POWER AT HYD QTY MONITOR UNIT AT CONNECTOR D2 704B PIN A11 (115AC). ALSO MEGGER WIRING BETWEEN D60 AND D2704B REF WDM 29-33-11 SHEET 2 INSTALLED KNOWN GOOD HYD QTY MONITOR UNIT PER AMM 29-33-01 & REMOVED ANAD REPLACED HYD FLUID QTY TRANSMITTER IAW AMM 29-33-02, OPS & LEAK CHECK GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1198322 S/N OFF 00478 TT # 1438002 S/N OFF 05242 MONITOR, HYD QT OFF 64-2933-9-0001 0478 ON 64-2933-9-0001 0488 TRANSMITTER, HYD OFF 99-2936-9-9002 5242 ON 99-2936-9-9002 653.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,417 hrs · 7,218 cycles

EMERGENCY LIGHTS AT ROWS 22 TO 38 INOP. REPLACED BATTERY PACK & BATTERY AT ROW 22 RIGHT PER AMM 33-52-02, OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,272 hrs · 6,096 cycles

R4 AFT SERVICE DOOR EXTERIOR SLIDE LIGHT INOPERATIVE. RELAMPED PER AMM 33-51-06, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,272 hrs · 6,096 cycles

R2 SERVICE DOOR EXTERIOR SLIDE LIGHT INOPERATIVE. RELAMPED PER AMM 33-51-06, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,512 hrs · 5,963 cycles

L1 DOOR EXTERIOR EMERGENCY LIGHT NOT ILLUMINATE. L1 DOOR EXTERIOR EMERGENCY LIGHT LAMP REPLACED AND CHECKED NORMAL IAW AMM 33-51-06.

Part: SKIN — DENTED (TAILCONE) · airframe 32,512 hrs · 5,963 cycles

DENT ON APU TAIL CONE AREA AT STA 1920, 11 O`CLOCK POSITION. DIMENSIONS ARE .130 INCH DEEP 3 X 2.25 INCH FX STA 1913 TO STA 1920 BETWEEN STR 0-STR 12AL. SKIN REPAIRED PER SRM 53-00-01 FIG 201, REPAIR 14 AND HFEC NO CRACK FOUND.

Part: BATTERY — INOPERATIVE (R1 FLASHLIGHT) · airframe 29,717 hrs · 5,440 cycles

R-1 EMER FLASHLIGHT IS NOT WORKING. REPLACED FLASHLIGHT BATTERY, OPERATIONAL TEST GOOD IAW MM 25-64 -00.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,261 hrs · 4,812 cycles

BUSINESS FIRST EMERGENCY AISLE LIGHTS INOP. REMOVED & REPLACED POWER SUPPLY UNIT & BATTERY PER AMM 33-51-07-022-005.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 7,851 hrs · 1,595 cycles

THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE AT STA 841, WL 204, RBL 95 DURING TEST. THE EMERGENCY LIGHT POWER SUPPLY BATTERY CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-07.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 7,851 hrs · 1,595 cycles

THE EMERGENCY LIGHTS DID NOT ILLUMINATE AT STA 533, WL 204, RBL 95 DURING TEST. THE EMERGENCY LIGHT POWER SUPPLY BATTERY CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-07, PAGE 206.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 7,851 hrs · 1,595 cycles

THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE AT STA 401, WL 204, RBL 95 DURING TEST. THE EMERGENCY LIGHT POWER SUPPLY BATTERY CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-07, PAGE 206.