N655UA

Part: SKIN — DAMAGED (ZONE 100) · airframe 128,508 hrs · 19,829 cycles

DURING WALKAROUND, OBSERVED SMALL DAMAGED ON RT LOWER FUSELAGE BETWEEN BS 1219 & 1241, S36 & 37R. REMOVED PAINT. PERFORMED HFEC AS PER NDT PART 6 51-00-19, IT WAS FOUND A CRACK IN THE AREA. MEASUREMENT: CRACK: 1,5 IN; CRACK TO BS 1219: 15 IN; CRACK TO S-38R 6,5 IN; CRACK TO REPAIR: 16,25; CRACK TO LAP JOINT 5,5 IN. FASTENERS AT DAMAGED AREA WERE REMOVED IAW SRM 53-00-01-2R-1 STEP 2 AND SRM 51-40-02. PERFORMED FASTNER HOLE INSPECTION IN THE OPENED HOLES. IAW NTM PART 6 51-00-16. NO CRACKS WAS FOUND. GOOD TO FOLLOW FOR NEXT STEPS. PERFORMED CUT AT THE DAMGED AREA IAW SRM 53-00-01-2R-1 STEP 3. IT IS NECESSARY TO PERFORM NDT INSPECTION IAW STEP 4 AND NDT PART 6 51-00-01/51-00-19.

Part: GAS CYLINDER — LOW PRESSURE (ZONE 800) · airframe 128,087 hrs · 19,778 cycles

L2 DOOR GAUGE OUT OF THE GREEN. PERFORMED INSPECTION IAW AMM GAS CYLINDER GAUGE CHECK.IAW TASK 25-66-99-702-001, ITEM WITHIN LIMITS. THE PRESSURE IS AT 3100PSI. ITEM GOOD TO GO.

Part: EEC — FAULTED (NR 1 ENG) · airframe 127,649 hrs · 19,727 cycles

LEFT ENGINE HUNG UP AT LOW POWER SETTING AND WOULD NOT INCREASE ON FINAL ON FINAL, DURING THROTTLE LEVER MOVEMENTS. THROTTLES PULLED BACK & LT ENG N1 DID NOT INCREASE WITH THROTTLE LEVER INPUT, PARTIAL RPM LOSS. EPR DID SHOW THE COMMAND BAR TARGET, BUT NO ENGINE RESPONSE. ALL EICAS & STS MSGS APPEARED. ON LANDING LT THRUST REVERSER LEVER DID NOT PULL PAST I NTERLOCK. REVERSER AMBER-GREEN INDICATION WAS NOT OBSERVED. ON TAXI TO GATE, THROTTLES WERE NOT MOVED ABOVE IDLE. MSGS REMAINED, LT PIMU BITE C/O IAW FIM 71-01-TREE 803. FAULTS FOUND: CH A & B CONTROL, CH A & B CAT 1 & 2, CH A & B FMU TR-CHECK FAILED, CH A & B SVA TR-CHECK FAILED, CH A & B TCC TR-CHECK, CH A & B AOC TR-CHECK FAILED. PIMU RECALL IAW FIM 71-01,TREE 804: FLIGHT LEG 00. CH A & B CONTROL, CH A & B CAT 1, CH A & B CAT 2, CH A & B FMU TR-CHECK FAILED. R & R NR 1 ENG EEC IAW AMM 73-21-04-404-016-N00, INSPECTION IDT USING GMM 09-10-05 OF ALL CONNECTIONS. NR 1 ENG EEC INSTALLATION INSPECTED AND CONFIRMED FITTED IAW AMM 73-21-04-404-016-N00. ALL OPS GOOD. OK CONTINUED SERVICE.

Part: SLIDE — NO DISCREPANCY (ZONE 800) · airframe 127,566 hrs · 19,716 cycles

L2 DOOR GAUGE NOT IN THE GREEN. SLIDE PRESSURE IN LIMITS IAW AMM 25-66-99-702-001.

Part: PIN — INSTALLED (ZONE 800) · airframe 127,168 hrs · 19,665 cycles

INSTALLED GROUND LOCK PIN ON L1 DOOR FOR GIRT BAR CARRIER REMOVAL. REMOVED GROUND LOCK PIN ON L1 DOOR AFTER GIRT BAR CARRIER INSTALLATION REF AMM 52-11-13

Part: SLIDE — NONE (ZONE 800) · airframe 127,168 hrs · 19,665 cycles

DEACTIVATED L1 SLIDE IN REF WITH AMM 25-66-03 FOR GIRT BAR CARRIER REMOVAL. REACTIVATED DOOR 1L SLIDE REF AMM 25-66-03-404-098. REMOVED AND STOWED SAFETY PIN FROM INFLATION CYLINDER. FLAGGING FOR INSPECTION INSPECTED REACTIVATION OF DOOR SLIDE AS REQUIRED PER GMM 9-25-05

Part: DOOR — LEAKING (ZONE 800) · airframe 127,150 hrs · 19,660 cycles

PAX REPORTED LOUDER AIR NOISE AT 31D. CONFIRMED BY F/A AND PILOT COMPARE D TO 31A. BOTH EMERGENCY EXIT NO PRESSURIZATION ISSUE REPORTED, GVI OF ALL 4 EMERGENCY EXITS SATIS, FLUSHNESS OF ALL 4 EMERGENCY EXITS ALSO CHECKED SATIS

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 125,993 hrs · 19,520 cycles

EMER EXIT LIGHT COVER BY 1L CAME OFF RESECURED COVER, WHILE OPS CHECK PERFORMED BOTH L1 & R1 DOOR EMERGENCY LIGHT INOP REF AMM TASK 33-51-00-715-019-001. R&R POWER SUPPLY FOR BATTERY PACK M1208 REF AMM 33-51-07, OPS CHECKED GOOD.

Part: IDG — FAULTED (NR 2) · airframe 125,898 hrs · 19,509 cycles

GENERATOR DRIVE SYSTEM EICAS MESSAGE (01=L, 02=R) GEN DRIVE SHOW N. DRIVE LGT ON. GEN DRIVE DISC. NOTE: RECURRENT IDG TEMP AND CO OLING VLV EICAS MSG & ON/OFF OR STEADY ON OF THE DRIVE LGT, MAY BE CAUSED BY IDG TEMP BULB (PIN/SOCKET WEAR). TO VERIFY, FI 02UNABLE TO DEBRIEF INBND. FLT. CREW, SO VERIFIED E2 IDG HAS BEEN DISCONNECTED BY FLT. CREW. VERIFIED IDG OIL LEVEL WAS SIGNIFICANTLY OVERFULL, NO OBVIOUS FUEL SMELL PRESENT AND SCAVENGE FILTER DPI POPPED. REMOVED E2 IDG SCAVENGE OIL FILTER AND FOUND EXCESSIVE AMOUNT OF LARGE BRONZE METAL CHIPS IN FILTER AND IN BOTTOM OF FILTER BOWL, REF. AMM 24-11-01, -02. STILL NEEDS "EXAMINE THE OIL IN THE IDG" PROCEDURE TO BE C/W (AMM 24-11-01-286-075) TO DETERMINE FURTHER MAINT. ACTIONS REQ'D. REMOVED E2 IDG REF AMM 24-11-01, TRANSFERRED FITTINGS TO NEW IDG REF AMM 24-11-01, IDG PRESERVATIVE FLUID STILL NEEDS TO BE DRAINED INSTALLED ENG 2 IDG REF AMM 24-11-01. INSTALLED FEEDER CABLES AND TORQUED INSTALLED ENG 2 IDG REF AMM TASK 24-11-01-404-001-006 OPS CHECKS AND LEAK CHECK STILL REQUIRED. CONTINUE WITH STEP (15).PARTS USED: 76-2411-9-0002, QTY :1 ROTABLE PARTS CHG:TT # 1377564 SN OFF 0473 PN OFF 76-2411-9-0002 GENERATOR, INTE OFF 76-2411-9-0002 0473 ON 76-2411-9-0002 1108 ACCOMPLISHED IDT REQUIREMENTS IAW GMM 09-10-05. VERIFIED FEEDER CABLE TORQACCOMPLISHED LEAK CHECK AND OPS CHECK OF ENG 2 IDG. SERVICED AFTER ENGINE RUNS. REF AMM 24-11-01. NO CURRENT FAULTS OR LEAKS NOTED. A

Part: WINDOW — CRACKED (L1 DOOR) · airframe 125,699 hrs · 19,482 cycles

DOOR 1L INNER PRISM WINDOW CRACKED FOUND HEATED PANE CRACKED. PRISM AND OUTER PANE ARE OK. SEE ATTACHED PIC. REMOVED AND REPLACED INNER MOST HEATED WINDOW. OPS CHECK GOOD. REF AMM 56-31-01 ADD EMP:409288

Part: LIGHT — NO TEST (ZONE 200) · airframe 124,337 hrs · 19,304 cycles

EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - DUNRING WALK AROUND FOUND TREE EMERGENCY LIGHTS INOP, POSITION ONE LH AND TWO RH. REPLACEMENT THE SLIDE AND OVERWING ESCAPE LIGHT LAMP AS PER AMM- TASK 33-51-06-902-082, CHECKED OK.

Part: TRIM SYSTEM — UNKNOWN (RUDDER) · airframe 123,050 hrs · 19,149 cycles

AFTER TAKEOFF NEEDED ALMOST 8 DEGREES RIGHT RUDDER. TRIED TO ALS O USE AILERON TRIM. NO HELP DEBRIEFIED CREW, BOTH ENGINE EPR WAS SAME PASSED. TRIM TEMPERATURE COMPENSATING LINKAGE. NO DEFECTS FOUND. NO SIGNIFICANT FINDINGS AT THIS TIME. FIM: 27-09 TASK 814, AMM: 27-21-23, AMM: 27-21-19. ACP ULTRASOUND OF YAW DAMPER SUMMING LEVER SHEAR RIVETS AS INDICATED IN FIM 27-21, 809 REF NDT PT4 27-20-01. NO FINDINGS, RIVETS ARE NOT SHEARED. UPON ARRIVAL FOUND RUDDER TRIM AT APPROXIMATELY 3 DEGREES RIGHT REF LP 8612926 ACCOMP AMM 27-00-97 PARA E, ALL CHECKS GOOD, 27-21 TASK 809. BLOCK 1 ULTRASONIC TEST WAITING ON TOOLING. ACP AMM RUDDER RATIO CHANGER MECHANISM CHECK 27-21-99-206-001 NO NO SPOILER FLOAT. AILERON, SPOILERS FAIRED REF BLOCK 1 OF FIM 27-21 TASK 809 FOR ULTRASONIC INSPECTION OF PERFORMED BITE TEST OF LEFT AND RIGHT RUDDER RATIO CHANGER AND AILERON TRIM APPROX 2 DEGREES RIGHT. FURTHER TS REQUIRED VISUALLY RIVETS NOT SHEARED. CK''D GOOD TO BLOCK 36. ACP SYSTEM MOVEMENT NOTED.CK''D FUEL LOAD IS BALANCED REF 767 FUEL MANUAL. SHEAR RIVETS OF THE YAW DAMPER SUMMING LEVER. INSPECTION MODULE. BOTH MODULES OPS CHECK GOOD. NO FAULTS NOTED ON EITHER TEST PER AMM 27-21-00-735-188-001 PAR 4N & O, TEST PASSED. ACP NO MOVEMENT NOTED ON AILERON OR SPOILERS. VISUALLY CK''D INBD REQUIRED. MODULE. VISUALLY INSPECTED WIRES ON THE AILERON AND RUDDER TRIM OPERATIONAL TEST PER AMM 27-21-00-715-001-001 PAR 2 H & I TEST AILERON REF AMM 27-11-00-715-417 FIG 510.

Part: OVERHEAD BIN — BROKEN (SEAT ROW 9) · airframe 122,698 hrs · 19,105 cycles

OVERHEAD BIN AT 9 CTR BROKEN. THE BIN WHERE THE AVIOX IS LOCATED . REPOSITIONED LOOSEN ATTACHING SCREW REF AMM 25-00-00. ADDING CORRECT AMM REFERENCE: 25-28-01-902-003 (SUBTASK 25-28-01-422-005).

Part: FLOORBEAM — CORRODED (BS 977 LBL95) · airframe 122,601 hrs · 19,091 cycles

SEC 45- ON THE FLOOR STRUCTURE CABIN PAX, PRESSURE DECK AREA WAS FOUND THE FITTING WITH CORROSION AT STA 977, LBL95, WL 189

Part: FLOOR SUPPORT — CORRODED (BS 977 RBL95) · airframe 122,601 hrs · 19,091 cycles

FLOOR STRUCTURE CABIN PAX, PRESSURE DECK AREA WAS FOUND THE FITTING WITH CORROSION AT BS 977, RBL95, WL 189 ACCOMPLISH THE INSPECTIONS AS PER PART 2 OF THE LATEST REV C, WHICHEVER OCCURS FIRST. PERFORM REPEAT I VER OCCURS FIRST. ISION OF EC/RA 5310-08324 ON OR BEFORE AC REACHES 19,691 TOTAL F NSPECTIONS AT INTERVALS NOT TO EXCEED 600 FC OR 6 MONTHS, PERFORMED INTERIM REPAIR OF THE RT BS 977 FRAME AT WL 190 OBRD CHORD CORROSION IAW ECRA 5310-08324 PART 1, SATISFACTORY. PERFORMED & INSPECTED IAW ECRA 5310-08324 PART 1. AT RH BS 977 FRAME AT WL 190 OBRD CHORD INSPECTION.

Part: SKIN — CRACKED (BS 340 S20R) · airframe 122,601 hrs · 19,091 cycles

DURING NDT PROCEDURE AS PER PART 6, 51-00-16. IT WAS FOUND A CRACK HOLE AT STA 340 AND STGR 20R ON THE FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER. GENERATE UPDATE TO ATTACH IMAGES FROM THE DAMAGED HOLE AND CHANGE THE ATTRIBUTES TO MAJOR REPAIR AND SDR.

Part: SKIN — DAMAGED (STA1582 -1645.5) · airframe 122,601 hrs · 19,091 cycles

DURING INSPECTION AT 321BL; 322AL & 323AL LH UPPER SKIN B.L 0.0 AT SEC 48 BS 1582 TO BS 1654; WAS FOUND SKIN WITH SCRATCHES AND NICK. NECESSARY EVALUATION PROCESS. SEE IMAGES FOR FUTHER DETAILS. 7245 PART 1.A AND PART 1.B. THIS REPAIR IS A CATEGORY ''''B'''' REPA LISH INSPECTION REQUIREMENTS PER PART 2 OF LATEST REVISION OF EC IR AS DEFINED IN 767-300 SRM 51-00-06. IT IS NECESSARY TO ACCOMP /RA 5330-07245 ON OR BEFORE 37,500 TOTAL FLIGHT CYCLES. PERFORMED THE INTERIM REPAIR OF THE WEAR LOCATED AT THE FUSELAGE SKIN BETWEEN STA 1582 - STA 1645.5 AND S-2L AS PER EC/RA#5330-0

Part: NONE — NONE (NONE) · airframe 122,601 hrs · 19,091 cycles

DURING AGING INSPECTION FOUND DOUBLER REPAIR WITH NO RECORDS AT STA. 1788 STR 38R. TEGORY B REPAIR AND REQUIRES RIR, IT IS NECESSARY TO ACCOMPLISH 5375-01010 ON OR BEFORE A/C REACHES 37,500 TOTAL FC. ACCOMPLISH RVALS NOT TO EXCEED 12,000 FC THEREAFTER. INSPECTION REQUIREMENTS AS PER PART 2 OF THE LATEST REV OF ECRA# REPETITIVE INSPECTIONS PER PART 2 OF THE ECRA#5375-01010 AT INTE PERFORMED INTERIM REPAIR OF THE FUSELAGE SKIN STATION 1788 AT ST RINGER S-36R AS PER ECRA#5375-01010 PART 1C. THIS REPAIR IS A CA

Part: SKIN — CORRODED (BS 1562-1582) · airframe 122,601 hrs · 19,091 cycles

DURING ACCOMPLISHMENT OF NR:1896678 WAS FOUND CORROSION IN THE INTERNAL FUSELAGE SKIN PANEL LOCATED BTW STA. 1562/1582 AND STGR 24/25 LH SIDE. FOR REFERENCE SEE: SRM 53-60-01-0I-1.

Part: LANDING — CORRODED (BS 1809 S30-36) · airframe 122,601 hrs · 19,091 cycles

AT 313AL SEC 48 TAIL COMPARTMENT ACESS BETWEEN STA 1809.5 LH AND S-30 TO S-36WAS FOUND CORROSION. SEE IMAGES FOR FUTHER DETAILS. TION ON THE EXISTENT HOLES ON AIRCRAFT SKIN, AT AREA OF STRINGER S 30LH, 32LH AND 36LH, ACCORDING TO B767 NDT MANUAL PART 6, 51-0 0-16 TO ENSURE THAT THEY WERE FREE OF DAMAGE, AND THEY WERE OK. THE STRINGERS 30LH, 32LH AND 36LH, STA 1809,50, WERE REPLACED, A CCORDING TO SRM 53-80-03-0I-1, (MATERIAL INFORMATION 7075 T62 - 0.063", PO#4113226645, BAC1498-144 AND BAC 1498-143). THE STRING ERS WERE MADE ACCORDING TO DWG 148T3280. IT WAS PERFORMED INSPEC

Part: SKIN — DAMAGED (BS 1153-1219) · airframe 122,601 hrs · 19,091 cycles

DURING "OK TO CLOSE" FOR PANEL 196NR FOUND A SCRIBE LINE ALONG UPPER FAIRING EDGE IN AIRCRAFT SKIN BTW STA 1153 - 1219 RH SIDE, SEE PICS FOR DETAILS.

Part: LANDING — CORRODED (BS 1832 S37-39) · airframe 122,601 hrs · 19,091 cycles

DURING INSPECTION AT 313AL TAIL COMPARTMENT SEC 48 STA 1809.5 RH TO STA 1832 RH WAS FOUND RS-39 TO RS-37 STRINGERS WITH CORROSION. SEE IMAGES FOR FUTHER DETAILS. REPLACED THE STRINGER 30RH, 32RH AND 36RH AS PER BOEING 767 SRM 51-40-02 AND DWG 148T3280. ITEM OK TO SERVICE.

Part: STRINGER — CORRODED (BS 1131-1153) · airframe 122,601 hrs · 19,091 cycles

AFT CARGO COMPARTMENT - FOUND SIGNS OF CORROSION AT AREA OF STRINGER S-36L BETWEEN BS 1131-1153.

Part: SKIN — CRACKED (L1 DOOR) · airframe 122,601 hrs · 19,091 cycles

DURING VISUAL INSPECTION AFTER SCUFF PLATE REMOVAL, FOUND SCRIBE LINES IN THE AREA UNDER SCUFF PLATE AT FUSELAGE SKIN 1L DOOR FWD & AFT LOWER CORNER. LOCATED BTW BS 287 & 347 BTW S20L & 21L. THIS IS A CATEGORY B REPAIR. PERFORMED INTERIM REPAIR OF FUSELAGE SKIN 1L DOOR, FWD AND AFT CORNER CRACKS & LOWER PERIMETER SCRIBE LINES AS PER EC/RA 5331- INTERIM REPAIR OF THE FUSELAGE SKIN 1L DOOR WAS SATISFACTORY. PERFORMED & INSPECTED PER ECRA 5331-03104. PER ECRA 5331-03104 AFTER ACCOMPLISHMENT OF INTERIM REPAIR; INITIATE A DTA DIP LOGPAGE TO ACCOMPLISH INSPECTION REQUIREMENTS ON FWD LH ENTRY DOOR CUTOUT LOWER CORNER REPAIR AREA AS PER PART 2 OF LATEST REVISION OF EC5331-03104 ON OR BEFORE THE AIRCRAFT REACHES 37,500 TOTAL FLIGHT CYCLES. LOG 8066917 TOMC APPROVED: QC REVIEWED CREATED TO CONTACT ENGINEERING AFTER AIRCRAFT REACHES 32,000.

Part: NONE — NONE (NONE) · airframe 122,601 hrs · 19,091 cycles

DURING AGING INSPECTION FOUND REPAIR AT APPROX. STA. 1562 STR. 20L-21L WITH NO RECORDS. ART 1. THE REPAIR ACCOMPLISHED IN PART 1 OF ECRA 5330-07244 IS A UIRED REPETITIVE INSPECTION REQUIREMENTS (RIR). IT IS NECESSARY VISION OF ECRA 5330-07244 ON OR BEFORE 37,500 TOTAL FC. CATEGORY B REPAIR AS DEFINED IN 767-300 SRM 51-00-06, WHICH REQ TO ACCOMPLISH INSPECTION REQUIREMENTS AS PER PART 2 OF LATEST RE PERFORMED INTERIM REPAIR OF THE FUSELAGE SKIN ATBETWEEN BS 1560 AND BS 1582 AND BETWEEN S-19L AND S-23 AS PER EC/RA#5330-07244 P

Part: NONE — NONE (NONE) · airframe 122,601 hrs · 19,091 cycles

DURING AGING INSPECTION WAS FOUND A REPAIR AT STA 202-208 STR 29LT SRM 53-00-01 AMIS ITEM 2182092 CATEGORY B REPAIR WITH NO DIP.

Part: FLOORBEAM — CORRODED (BS 325) · airframe 122,601 hrs · 19,091 cycles

DURING INSPECTION WAS FOUND FLOOR BEAM STA 325 UPPER CHORD FLANGE LBL 40- 54.75 CLOSE TO THE PASSENGER DOOR WITH CORROSION SPOTS UPPER SURFACE.

Part: ENGINE — FIRE (LEFT) · airframe 122,301 hrs · 19,038 cycles

L ENG TAIL PIPE FIRE ON FUEL INTRO NO FIRE INDICATIONS BUT LARGE FIRE REPORTED

Part: VALVE — FAULTY (RH ENGINE) · airframe 122,239 hrs · 19,030 cycles

R SPAR VALVE EICAS AND LIGHT ON ENGINE START. REMOVED AND REPLACED RH SPAR VAVE PER AMM 28-22-01.DEVICE WORKS FINE. PARTS USED: 1165583,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1165583 SN OFF 6128 IPC REFERENCE # 28-22-01-02 ACTUATOR, VALVE OFF 29-2822-9-9014 2858 ON 29-2822-9-9014 6245

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 122,017 hrs · 18,997 cycles

L PACK OVER TEMP. CREW REJECTED TAKE OFF AROUND 80KNOTS. CREW REPORT NOT SURE LEFT OR RIGHT PACK TEMP MSG REQ TOMC APRVL DEFERRED LT AND RIGHT PACK AUTO FUNCTION PER MEL TO DEF AUTO MODE LT AND RT PACK NO FAULTS NOTICED. ON CONTROLLERS ... PRECAUTIONARY PUT BOTH PACKS ON MANUAL TEMP... APPROVED... TOMC MO PREFORMED PACK TEMP CONTROLLER BITE TEST REF AMM TASK 21-51-14-705-035. NO FAULTS NOTED. REVERSED MEL, RETURNED AIRCRAFT TO NORMAL CONFIGURATION. PERFORMED HIGH ENERGY INSP PER AMM TASK 05-51-14-212-089 NO PROBLEMS OR DMG FOUND OK FOR SVC

Part: MODULATING VALVE — FAULTY (STA 840) · airframe 121,910 hrs · 18,984 cycles

FLT DK PACK INOP ANNUNCIATOR LIGHT INOP.FLT DECK TEMP EICAS MESSAGE. REQUEST MEL FOR FLIGHT DECK ANNUN LIGHT. DDP COMPLIED WITH. OK TO DEF TRIM AIR FLIGHT DECK ANNUNCIATOR LIGHT. AFFECTED ITEM IS TRIM AIR FLIGHT DECK ANNUNCIATOR LIGHT. SEE PICTURE OF LIGHT REPLACED THE FLT DECK PACK ANNUNCIATOR LIGHT ASSY. OPS GOOD. PLACARD REMOVED. FLIGHT DECK TEMP CONTROL INOP COMPLIED WITH AMM PACK TEMP CONTROL BITE 21-51-14-705-035. NO FAULTS,NO MSG SHOWING. OPS BOTH PACKS WITH NO DISCREPENIES. SYS OPS NORMAL REOPEN IAH U064797 02NOV23 FOR: CLOSED IN ERROR PROBLEM STILL THERE... VALVE, TRIM AIR OFF 75-2161-9-0005 3233 ON 75-2161-9-0005 2497 VALVE, TRIM AIR OFF 75-2161-9-0005 3233 ON 0000 F/D TEMP MSG RETURNED. NOW SHOWING TRIM AIR VALVE FAULT ON ZONE COMPLIED WITH AMM PACK TEMP CONTROL BITE 21-51-14-705-035. NO FAULTS,NO MSG SHOWING. OPS BOTH PACKS WITH NO DISCREPENIES. SYS TEMP CONTROL BITE. REPLACED F/D TRIM AIR MODULATING VALVE, ALL OPS & LEAK CKS GOOD. REF AMM 21-61-07. PARTS USED: OPS NORMAL 75-2161-9-0005,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1715704 SN OFF 3233.

Part: LIGHT — INOPERATIVE (STA252, 238) · airframe 121,795 hrs · 18,971 cycles

EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - THE FLIGHT DECK EXIT SIGN LIGHT IS INOPERATIVE AFTER PUT SWITCH EMERGENCY LIGHT, P5, TO ON. ADD PHOTO INFO. REMOVED AND REPLACED LIGHT EMERG EXIT, OPS CHECK GOOD PER AMM 33-51-01. PARTS USED: 1550953,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1550953 SN OFF 3833 IPC REFERENCE # 33-51-01-01-01-30

Part: NONE — DAMAGED (FWD ZONE R/H NO2) · airframe 119,006 hrs · 18,594 cycles

CEILING PANEL EMERGENCY LIGHT CONNECTOR DAMAGE AT FWD ZONE R/H NO.2,AFT ZONE R/H NO.4,AFT ZONE R/H NO.9,AFT ZONE L/H NO.9 CEILI NG PANEL,1A-10A,1L-10L CEILING PANEL REF HAECO NON-ROUTINE NO.: 9404868,ORIGINATED BY EMP V905488,EA 2500-12986 OP001. PERFORMED BY EMP V905488,REPLACED CEILING PANEL EMERGENCY LIGHT 51-05-402-024 REV138.IDT BY TA587. CONNECTORS AT FWD ZONE R/H NO.2,AFT ZONE R/H NO.4,AFT ZONE R/H NO.9,AFT ZONE L/H NO.9,1A TO 10A,1L TO 10L CEILING PANEL AND INSTALLATION TEST FOUND PASS AS PER SWPM 20-61-28 REV81,AMM 33-

Part: TERMINAL — DAMAGED (L297) · airframe 119,006 hrs · 18,594 cycles

OVERWING HATCH EXIT SIGN DIM AT L322 AND L297 REF HAECO NON-ROUT INE NO.:9407719,ORIGINATED BY EMP V905488,SPEC NO.:B767-33-3-700 0. PERFORMED BY EMP V905488,PERFORMED WIRING CHECK FOUND L297 LIGHT TERMINAL POOR CONDITION,REPLACED L297 TERMINAL AND INSTALLATION FOUND PASS AS PER WDM 33-51-14 REV76,SWPM 20-30-11 REV81,AMM 33 -51-01-402-030 REV138,IDT BY TA587. SDR SHOULD BE Y.

Part: SKIN — NONE (STA 456-478) · airframe 119,006 hrs · 18,594 cycles

FUS STA 456-478 S-32L TO S-35L FOUND A DENT ON EXISTING SKIN REPAIR DOUBLER. SEE MRO ENGINEERING DOCUMENT EN.: EG 53-1105 (INCLUDED IN ECRA 5330-07058). PART 2 INSPECTION REQUIREMENTS FOR THE REINFORCING SKIN DOUBLER INSPECTION REQUIREMENTS EVERY 9,000 FLIGHT CYCLES AS PER ECRA INSTALLED BETWEEN STA456-478 S-32L-S35L. REPEAT PART 2 5330-07058 REQD. INTERIM REPAIR ACCOMPLISHED PER ECRA 5330-07058 PART 1. ON OR BEFORE 37,500 FLIGHT CYCLES ACCOMPLISH AN INITIAL INSPECTION PER REF EC 5330-07058, ON OR BEFORE 37,500 FLT CYCLES ACCOMPLISH AM TOMC-APPROVAL FROM SC1ELBYC COMMENT INITIAL INSPECTION PER PART 2 INSPECTION REQUIREMENTS FOR THE REINFORCING SKIN DOUBLER INSTALLED BETWEEN STA 456- STA 478 AND S-32L - S-35L. REPEAT PART 2 INSPECTION REQUIREMENTS EVERY 9,000 FLT CYCLES QC QC REVIEWED INIT : 37,500 TAFC (INIT WILL ITO TO RIR) RIR : 9000 FC.HC/U389717 SELECTED TO YES. ARMENTA TOMC CONFIRM PER ECRA 5330-07058 INSPECTION REQUIREMENTS ARE BASED ON RECORDS UPDATE.....HC TOTAL AIRCRAFT FLIGHT CYCLES AS INDICATED IN MATCH TO A/C TIME

Part: SKIN — DENTED (STA412/S33L-34L) · airframe 119,006 hrs · 18,594 cycles

FUS STA 412 S 33L-34L FOUND A DENT ON EXISTING REPAIR DOUBLER. REVISION OF ECRA 5310-08118 BEFORE AIRCRAFT REACHES 37,500 TOTAL NOT TO EXCEED 9,000 FLIGHT CYCLES. FLIGHT CYCLES. REPEAT THE INSPECTIONS THEREAFTER AT INTERVALS ACCOMPLISH INSPECTION OF REINFORCING REPAIR INSTALLED ON FUSELAGE SKIN AT STA 412 S33L-34L PER PART 2 OF THE LATEST REF EC 5310-08118, ?ACCOMPLISH INSP OF REPAIR INSTALLED ON FUSE TOMC-APPROVAL FROM SC1ELBYC COMMENT SKIN AT STA 412 BETWEEN S33L & S34L PER PART 2 OF EC/RA 5310-08118 BEFORE 37,500 TOTAL FLIGHT CYCLES. REPEAT THE INSPECTIONS THEREAFTER AT INTERVALS NOT TO EXCEED 9,000 FLIGHT CYCLES?. REFER TO HAECO XMN NRC NQL8388. INTERIM REPAIR ACCOMPLISHED PER HAECO-XMN ENGINEERING GENERATED EN, EG-53-1106 INCLUDED IN ECRA 5310-08118. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE. QC REVIEWED QC REVIEWED

Part: LAMP — MALFUNCTIONED (2645) · airframe 119,006 hrs · 18,594 cycles

L/H WING AFT SLIDE LIGHT L645 INOP,REF TO HAECO NON ROUTINE NO.9 403690,ORIGINATED BY EMP V905488,SPEC NO.B767-33-3-7004. PERFORMED BY EMP V905488,REPLACED L/H WING AFT SLIDE LIGHT L645 LAMP AND NEW LAMP TEST FOUND PASS AS PER AMM 33-51-06-902-082 RE V 138,IDT BY TA408.

Part: LAMP — MALFUNCTIONED (L392) · airframe 119,006 hrs · 18,594 cycles

R/H AFT DOOR SLIDE LIGHT L392 INOP,REF TO HAECO NON ROUTINE NO.9 403694,ORIGINATED BY EMP V905488,SPEC NO.B767-33-3-7004. PERFORMED BY EMP V905488,REPLACED R/H AFT DOOR SLIDE LIGHT L392 LAMP AND NEW LAMP TEST FOUND PASS,AS PER AMM 33-51-06-902-082 RE V 138,IDT BY TA 408.

Part: CONNECTOR — CRACKED (CEILING PANEL) · airframe 119,006 hrs · 18,594 cycles

CEILING PANEL EMERGENCY LIGHT CONNECTOR LOOSEN AT 33AB,23AB,44AB ,9L,21LK,30LK,33LK,36LK,39LK,42LK,45LK,50LK,REF TO HAECO NON ROU TINE NO.9404153,ORIHINATED BY EMP V905488,EA 4420-03294 REV B OP 001. PERFORMED BY EMP V905488,REPLACED CEILING PANEL EMERGENCY LIGHT CONNECTORS AT 33AB,23AB,9L,21LK,30LK,33LK,36LK,39LK,42LK,45LK,50 LK,AND INSTALLATION TEST FOUND NORMAL,AS PER AMM 33-51-05-402-02 4 REV 138,SWPM 20-61-28 REV 81.IDT BY TA 408.

Part: LAMP — MALFUNCTIONED (L394) · airframe 119,006 hrs · 18,594 cycles

R/H FIRST OVER WING EGRESS LIGHT L394 INOP,REF TO HAECO NON ROUT INE NO.9403697,ORIGINATED BY EMP V905488,SPEC NO.B767-33-3-7004. PERFORMED BY EMP V905488,REPLACED R/H FIRST OVER WING EGRSS LIGH T L394 LAMPS AND NEW LAMP TEST FOUND PASS AS PER AMM 33-51-06-90 2-082 REV 138,IDT BY TA 408.

Part: STAND OFF — BROKEN (THRUST REVERSER) · airframe 118,831 hrs · 18,564 cycles

DURING THRUST REVERSE MEL T/S(3421891), FOUND PANEL ASSY FOR RELAY K10359 LOOSE SUPPORTS BROKEN. FIM 78-34. REMOVED AND REPLACED 04EA STANDOFFS IAW SRM 51-40-02-0G-0 PARAGRAPH 7. SUPPLYED ELECTRICAL POWER ON A/C AS PER AMM 24-22-00-201. NO DISCREPANCIES FOUND. P33 PANEL NOW OK.

Part: SKIN — CORRODED (ZONE 100) · airframe 112,787 hrs · 17,502 cycles

BULK CARGO - STA 1542 STR 39 BL0 WATER DRAIN VALVE SURROUNDING SKIN FOUND CORR REFER NR LP 9131165 BULK CARGO STA 1542 STR 39 BLD WATER DRAIN VALVE SKIN AREA. REPLACED AS PER ECRA 5360-01578 REV - PART 1 INTERIM REPAIR ADD.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 112,787 hrs · 17,502 cycles

B767-53-3-7154 AFT CGO - STA 1219 BILGE AREA S36R - S38R SHEAR TIE FOUND CORRODED AS MARKED REF NR LP 9131157 AFT CARGO STA 1219 S36R-S38R 2EA SHEAR TIE REPLACED AS PER SRM 5 1-10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02

Part: SKIN — DENTED (CARGO DOOR) · airframe 112,787 hrs · 17,502 cycles

B767-53-3-7006 BULK CGO - CGO DOOR EXTERIOR AREA STA 1461 EXISTING PATCH FOUND DENT AS MARKED REF NR LP 9130916 ACCOMPLISH INITIAL INSPECTIONS AS DEFINED IN LATEST REVISION EC5236-01021 PART 2 ON OR BEFORE THE BULK CARGO DOOR REACHES 30,000 FLT CYCLES. PERFORM REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 3,000 FLT CYCLES THEREAFTER. THIS CARGO DOOR IS ORIGIONAL TO THIS AIRCRAFT. DOOR FLT CYCLES ARE EQUIV TO A-C FLT CYCLES. INITIATE A DIP ITEM TO "ACCOMPLISH INITIAL INSPECTIONS DEFINED IN LATEST REVISION OF EC5236-01021 PART 2 ON OR BEFORE THE BULK CARGO DOOR [P/N: 146T6301-3; S/N: 000470] REACHES 30,000 TOTAL FLIGHT CYCLES. PERFORM REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 3,000 FLIGHT CYCLES THEREAFTER.

Part: SHEAR TIE — CORRODED (BULK CARGO) · airframe 112,787 hrs · 17,502 cycles

B767-53-3-7058 BULK CARGO - STA 1540 STR 38R-39R INTERNAL SHEAR TIE FOUND CORR REF NR LP 9131254 BULK CARGO STA 1540 STR 38R-39R SHEAR TIE REPLACED AS PER SRM 51 -10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BULK CARGO) · airframe 112,787 hrs · 17,502 cycles

B767-53-3-7058 BULK CARGO - STA 1540 STR 36R-37R INTERNAL SHEAR TIE FOUND CORR REF NR LP 9131257 BULK CARGO STA 1540 STR 36R-37R SHEAR TIE REPLACED AS PER SRM 51 -10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02 ADD EMP:V897532 RII OK BY HX 179805

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 112,787 hrs · 17,502 cycles

B767-53-3-7154 AFT CGO - STA 1197+110 BETWEEN S38R-S39R SHEAR TIE FOUND CORRODED AS MARKED REF NR LP 9131151 AFT CARGO STA 1197+110 S38R-S39R SHEAR TIE REPLACED AS PER SRM 5 1-10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02.

Part: STRINGER — CORRODED (BULK CARGO) · airframe 112,787 hrs · 17,502 cycles

BULK CGO STA 1542 S39R FOUND CORRODED CRACK AS MARKED REFER NR LP 9131050 BULK CGO STA 1542 S39R STRINGER REPAIRED AS PER ECRA 5360- 01581 REV A ADD EMP:V897526 RII BY HX 203141

Part: STRINGER — DENTED (BULK CARGO) · airframe 112,787 hrs · 17,502 cycles

BULK CARGO STA 1540 STR 38R FOUND DENT AS MARKED REFER NR LP 9131236 BULK CARGO STA 1540 - STR 38R STRINGER REPAIRED AS PER ECRA 5360-01581 REV A ADD EMP:V897526 RII BY HX 203141

Part: STRINGER — DENTED (ZONE 100) · airframe 112,787 hrs · 17,502 cycles

B767-53-3-7021 FWD CGO - STA 522-544 LBL 30 S-36L STRINGER FOUND DENT REF NR L/P 9131368 FWD CGO STA 522-544 S36L STRINGER PERMANENT REPAIRED AS PER SRM 53-00-03 REPAIR 2 FIG 201 DETAIL 111. FORM 44.0008 ITEM 1-14 ACC OMPLISHED.

Part: STRINGER — CORRODED (ZONE 100) · airframe 112,787 hrs · 17,502 cycles

AFT CARGO - STA 1197+132 - 1219 S33R STRINGER FOUND CORR REF NRC LP 9131499 AFT CARGO STA 1197+132 - 1219 S33R STRINGER REPAIRED AS PER ECRA 5360-01582 REV.- ATTACH FORM 44-0008 WORKSHEET ITEM 1 TO 21 ACCOMPLISHED.

Part: SKIN — CORRODED (ZONE 100) · airframe 112,787 hrs · 17,502 cycles

B767-53-3-7154 AFT CGO - STA 1197+132 TO 1219 S-33R SKIN FOUND C ORRODED AS MARKED REF NR LP 9131154 AFT CGO STA 1197+132 TO 1219 S-33R SKIN REPAIRED AS PER EC/RA NO . 5360-01582 REV-. ATTACHED FORM 44.0008 ITEM 1-14 ACCOMPLISHED.

Part: STRINGER — CORRODED (ZONE 100) · airframe 112,787 hrs · 17,502 cycles

AFT CGO - BILGE AREA STA 1219 - 1229 S-36L STRINGER FOUND CORRODED AS MARKED REFER NR LP 9131161 AFT CGO BILGE AREA STA 1219-1229 S-36L STRINGER REPAIRED AS PER ECRA 5360-01580 REV - ADD EMP:V897532 RII BY HX 122680

Part: STRINGER — CORRODED (ZONE 100) · airframe 112,787 hrs · 17,502 cycles

AFT CARGO STA 1213 TO 1217 S-35L STRINGER FOUND CORRODED AS MARKED REFER NR LP 9131162 AFT CARGO STA 1213 TO 1217 S-35L STRINGER REPAIRED AS PER ECRA 5360-01579 REV.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 112,787 hrs · 17,502 cycles

CABIN STA 303 LBL 36 TO 53 FLOOR BEAM FOUND CORROSION REFER NR LP 9130939 CABIN STA 303 LBL 36 TO 53 FLOOR BEAM UPPER CHORD PERMANENT REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 AND ECRA 5315-01153 REV.

Part: RUDDER — FROZEN · airframe 106,784 hrs · 16,581 cycles

ON DESCENT AIRCRAFT EXPERIENCED DUTCH ROLLS LIMITED AUTHORITY ON RIGHT RUDDER CHECKING RUDDER . PER INBD CREW, THE RT RUDDER WAS FROZE(WOULD NOT MOVE0 AND THE L EFT RUDDER WOULD BARELY MOVE. A/P WAS SELECTED OFF, NO CHANGE. CHECKING RUDDER HARDAWARE. ALL REQUESTED CHECKS FROM EG & BOEING COMPLETE` COMPLETED WORK REFERENCE AVO7270 REV A IN ADDITION TO CORROLATED TASKS COMPLETED ON LP 8482210,8482187,8478714,8469708,8471728,8 471733,8471741,8471755,8471761,8471779 AND 8471772.TOMC K.HUTCHI NSON AND TOMC MANAGER MIKE MC NEELEY CONCUR WITH TASKS ACCOMPLIS HED. ADD EMP:U332741 U331675

Part: FRAME — CRACKED (BS 1809 BULKHEAD) · airframe 103,334 hrs · 16,137 cycles

BS 1809, BULKHEAD LT FOUND CRACKED. REPAIRED IAW EA 5300-01600, REV A, OP 002.

Part: STRINGER — CRACKED (BS 1809) · airframe 103,334 hrs · 16,137 cycles

BS 1809, STRINGER 12A, FOUND CRACKED REPAIRED IAW EA 5300-01600, REV A, OP 002

Part: FAILSAFE — CRACKED (BS 955) · airframe 103,334 hrs · 16,137 cycles

BS 955 RT FAILSAFE STRAP FOUND CRACKED. THE FAILSAFE WAS REPAIRED IAW EA 5340-01478, REV C, OP 04.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 103,334 hrs · 16,137 cycles

NR 2 PYLON, LT ACCESS DOOR 446BL FWD UPPER CORNER CUTOUT FOUND CRACKED. THE SKIN WAS REPAIRED IAW ECRA 5430-02146, REV- .

Part: TEE FITTING — CRACKED (BS 955) · airframe 103,334 hrs · 16,137 cycles

BS 955 COMMON TO THE FAILSAFE STRAP AND THE TEE FITTING WAS CRACKED, THE TEE FITTING WAS REPLACED IAW EA 5340-01478 REV.C OP.04

Part: SKIN — CRACKED (BS 1809) · airframe 103,334 hrs · 16,137 cycles

BS 1809, STRINGER 12A, SKIN CRACKED. REPAIRED IAW EA 5300-01600, REV A, OP 002, FIG 4.

Part: FLOOR SUPPORT — CRACKED (BS 245-266) · airframe 103,334 hrs · 16,137 cycles

BS 245 - 266, RBL 60 THE FLOOR SUPPORT WAS FOUND CRACKED. THE FLOOR SUPPORT WAS REPAIRED IAW ECRA 5310-07350 REV -.

Part: FLOORBEAM — CORRODED (BS 324) · airframe 103,334 hrs · 16,137 cycles

BS 324, RBL 16 - 64 FLOORBEAM FOUND CORRODED. THE FLOORBEAM WAS REPAIRED IAW SRM 53-0051, REPAIR 1, FIG 201.

Part: FLOOR SUPPORT — CORRODED · airframe 103,334 hrs · 16,137 cycles

B767-20-3-6043 FWD CGO STA 520 LWR OF 5R PDU RH AFT MOUNT BOLT BELOW AREA CORROSION CRACKED FORWARD CARGO STA 520 LOWER OF 5R PDU RH AFT MOUNT BOLT BELOW IN TERCOSTAL REPLACED PER SRM 51-10-02 AND INSTALLED PER SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 287) · airframe 103,334 hrs · 16,137 cycles

BS 287, RBL 23 FLOORBEAM FOUND CORRODED. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 103,279 hrs · 16,129 cycles

LENS IS MISSING FOR CEILING EMERGENCY LIGHT AT 24J. REPLACED LENS BEZEL ASSY.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 102,585 hrs · 16,023 cycles

FLASHLIGHT INOPERATIVE. REPLACED THE BATTERY. OPS CHECKED GOOD

Part: HOSE — LEAKING (RT MLG) · airframe 101,290 hrs · 15,820 cycles

LOST CENTER HYD SYS IN FLIGHT. EMREGENCY DECLARED. REPLACED RIGHT MAIN GEAR RETRACT PRESSURE FLEX HOSE IAW GPM 1-13-021. OPS CHECKED NORMAL AND SERVICED CENTER HYD SYSTEM.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 99,635 hrs · 15,573 cycles

SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. SECURED THE CONNECTOR. OPS CHECKED NORMAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 96,426 hrs · 15,128 cycles

AFT PIT, BS 1197+132, FRAME WEB CRACKED, AT LBL 32 & 35. REMOVED DAMAGE, HFEC, FABRICATED & INSTALLED REPAIR PARTS IAW ERA 5360-01433.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,426 hrs · 15,128 cycles

BS 1197+132, AFT PIT FRAME, T CAP CORRODED. REMOVED & INSTALLED NEW T CAP IAW SRM 51-40-05.

Part: CAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,426 hrs · 15,128 cycles

AFT CARGO COMPARTMENT BS 1197, RBL 44, T CAP HAS CORROSION ON LOWER SURFACE. FABRICATED, DRILLED & INSTALLED T CAP IAW SRM 51-40-02 PARA 4 FIG 3 & 8 PARA 7D FIG 12 & SRM 51-30-01 PARA 7 FIG 7, 51-40-05 PARA 4 FIG 1 & DWG 146T1206.

Part: CAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,426 hrs · 15,128 cycles

AFT CARGO COMPARTMENT, BS 1197+44, RBL 46, T CAP HAS CORROSION ON LOWER SURFACE. R & R NEW T CAP, PN 146T1060-1, IAW DWG 146T1225 & SRM 51-40-02 PARA 4 FIGS 3, 8, 12 & SRM 51-40-05 FIG 2.

Part: SKIN — DENTED (FUSELAGE) · airframe 96,426 hrs · 15,128 cycles

BODY STATION 347, STRINGER 28L - S29L, EXT FUSELAGE SKIN DENT. REMOVED DAMAGE. HFEC FABRICATED & INSTALLED REPAIR PARTS IAW SRM 53-00-01 REPAIR 29 FIGURE 201.

Part: WARNING SYSTEM — INTERMITTENT (CARGO DOOR) · airframe 95,547 hrs · 15,001 cycles

FORWARD CARGO DOOR INDICATION COMES ON INTERMITTENTLY, ALONG WITH THE EICAS ADVISORY MSG IN FLIGHT. CHECKED PSEU & HAD NO FLIGHT FAULTS LAST 20 LEGS. CHECKED GAP OF SENSORS S214 & S215 RIG & FOUND GOOD. DUE TO HISTORY & DIVERSION, RECOMMEND REPLACING S214 & S215, PN 75-3261-3-0042. BOTH ARE HARDWIRED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 95,540 hrs · 15,000 cycles

FORWARD CARGO DOOR INDICATION COMES ON INTERMITTENTLY ALONG WITH THE EICAS ADVISORY MSG IN FLIGHT. ACCOMPLISHED CARGO DOOR INSPECTION IAW MEL 5271B IAW FOM 5 70 2.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 95,489 hrs · 14,993 cycles

LEFT WING SLIDE EICAS MSG. UPON ARRIVAL NO EICAS MSG PRESENT. TROUBLE SHOT IAW FAULT CODE 52 90 21 41, LT WING SLIDE EICAS. CHECKED FOR DEBRIS, CLEANED & INSPECTED SWITCHES S218 & S198. CLEARANCES WITH LIMITS IAW AMM 52-71-00. DISARMED & REARMED LT OVERWING SLIDE IAW MM 25-65-08, NO DEFECTS FOUND. PERFORMED PSEU BITE IAW FIM 32-09 FAULT TREE 805. NO CURRENT FAULTS FOUND.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 94,089 hrs · 14,812 cycles

EMERGENCY EXIT FLOOR EEL INOPERATIVE AT FWD GALLEY & FWD LT COAT CLOSET. SECURED CONNECTOR. OPERATIONS CHECKED NORMAL.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 93,381 hrs · 14,720 cycles

CREW REPORT ELEC ODOR & SMOKE IN AREA OF FWD LAVATORY E & GALLEY. ISOLATED FWD BALLAST BETWEEN FWD GALLEY & LAVATORY. INSPECTED ALL GALLEYS, LAVATORY’S, EE COMPARTMENT & FLIGHT DECK. R & R FWD DIRECT LIGHTING BALLAST M656 WITH SERVICEABLE UNIT. OPERATIONS NORMAL.

Part: DOOR — STUCK (EVAC SLIDE) · airframe 92,571 hrs · 14,615 cycles

RIGHT OFF WING SLIDE COMPARTMENT, DOOR PAINTED SHUT. IAW AMM 25-65-98, 25-65-08 & 25-65-00. FOUND DOOR OPEN. CLEANED ROUGH EDGES OF PAINT ON PERIMETER OF DOOR. DOOR OPERATED NORMAL DURING CLOSE UP.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 90,662 hrs · 14,354 cycles

EMERGENCY EXIT FLOOR LIGHT BETWEEN DOOR 1L & PAX SEAT 1A INOPERATIVE. REPLACED EMER LIGHT BATTERY PACK & TESTED IAW MM 33-51-10, CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 90,662 hrs · 14,354 cycles

EMERGENCY EXIT FLOOR LIGHT BETWEEN DOOR 1L & 1R INOPERATIVE. REPLACED EMER EXIT BATTERY PACK & TESTED IAW MM 33-51-10, CHECKED NORMAL.

Part: WEB — PUNCTURED (FUSELAGE) · airframe 90,133 hrs · 14,277 cycles

FORWARD PIT STATION 742 WEB PUNCTURED AT LBL 20. REMOVED DAMAGE, FABRICATED & INSTALLED DOUBLER IAW SRM 53-00-07. THIS IS A CAT A REPAIR IAW SRM 53-00-07, REPAIR 3, FIG 201. NO FURTHER ACTIONS REQUIRED.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,133 hrs · 14,277 cycles

MAIN CABIN AT STATION 955 APPROXIMATELY RBL 80 - 90 OVER WING BOX AREA HAS CORROSION ON UPPER SURFACE. BLENDED OUT CORROSION & FOUND OUT OF SRM ALLOWABLE LIMITS. REPAIR ACCOMPLISHED IAW REO-G17363, REV D & ECRA 5710-02373. THIS IS A CAT A REPAIRED, NO FURTHER ACTION REQUIRED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,133 hrs · 14,277 cycles

FORWARD CARGO FLOOR STATION 742 FRAME CHORD HAS CORROSION UNDER NUTPLATES AT APPROXIMATELY LBL 10. R & R UPPER CHORD AT STATION 742 IAW DWG 143T1214 & SRM 51-40-02.

Part: WIRE — SHORTED (CABIN) · airframe 90,133 hrs · 14,277 cycles

P11 PANEL EMERGENCY LIGHT WING ECS CB AT P36 LOCATION POPS. FOUND WIRE W1064-52-20 ON CONNECTOR D5154J PIN 28 SHORTED. R & R PIN 28. OPERATIONS CHECKED GOOD IAW WDM 33-51-11 & 33-51-00.

Part: CABLE — DETACHED (EMERGENCY EXIT) · airframe 90,133 hrs · 14,277 cycles

RIGHT OVERWING EMER EXIT STEP SUPPORT CABLE FOUND DETACHED FROM STEP & GROMMETS MISSING. REPLACED PN 45T6088-1 IAW DWG 145T6080. FUNCTIONAL CHECKED GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,133 hrs · 14,277 cycles

MAIN CABIN FLOORBEAM FOUND CORRODED ON UPPER SURFACE AT STATION 287, RBL 79. R & R CORRODED PN 141T5111-79 IAW SRM53-00-51 REPAIR 1. CAT A REPAIR, NO FURTHER ACTION NEEDED.

Part: SKIN — GOUGED (FUSELAGE) · airframe 90,133 hrs · 14,277 cycles

FORWARD LOWER EXTERNAL FUSELAGE SKIN GOUGED 3 PLACES, BS 368, STRINGER 37R & STRINGER 38R. REPAIR IS A ZONE A CAT B REPAIR.

Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 90,133 hrs · 14,277 cycles

BULK CARGO DOOR INTERNAL AFT MID-SECTION BARE METAL & SEVERAL TOOLING MARKS FOUND ON T CORD. REMOVED BULK DOOR T CORD PN 146T6318-8 WITH SAME PO 806695 IAW SRM51-40-02 & DWG 146T6301.

Part: SKIN — CHAFED (FUSELAGE) · airframe 90,133 hrs · 14,277 cycles

RIGHT AFT FUSELAGE H STAB FWD CUT OUT SKIN FOUND CHAFED IN 2 PLACES BELOW BANANA FAIRING APPROX BS 1737, STRINGER 19R. DAMAGE FOUND BEYOND REPAIRABLE LIMITS. R & R IAW SRM51-40-02 & DWG 14 8T7320. RECEIVED FABRICATED PANEL AND INSTALLED IAW DWG.

Part: SKIN — CHAFED (FUSELAGE) · airframe 90,133 hrs · 14,277 cycles

LEFT AFT FUSELAGE STAB FWD CUT OUT SKIN FOUND CHAFED IN 2 PLACES UNDER BANANA PANEL APPROX STATION 1737 STRINGER 19 - 20L. REMOVED DAMAGED SECTION & REPAIRED IAW SRM 53-80-01 REPAIR 3 DT VI & DWG 148T7321.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 90,133 hrs · 14,277 cycles

AFT PIT FLOOR FRAME UPPER CORD CORRODED UNDER NP'S STATION 1285, RBL 20 - RBL 30. REMOVED FLOOR BEAM CORROSION, PN 146T1210-20 IAW SRM51-40-02 & SRM51-40-01, NR 33012.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 90,133 hrs · 14,277 cycles

MAIN CABIN SEAT TRACK CORRODED STATION 999 - 1050, RBL 11. REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED & INSTALLED NEW SECTION IAW SRM51-40-02 & SRM53-00-52, NR 33324.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 90,133 hrs · 14,277 cycles

MAIN PASSENGER CABIN SEAT TRACK FOUND CORRODED AT STATION 990 - 1340 RBL 89. REMOVED & FABRICATED NEW SEAT TRACK SECTION IAW DWG 145T5256 & 145T5213. INSTALLED IAW DWG 145T5256.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,133 hrs · 14,277 cycles

AFT CARGO COMPARTMENT FLOOR, CORROSION UNDER SEVERAL NUTPLATES & TOP SIDE OF FLOOR STRUCTURE AT STATION 1219 LT TO RT. REMOVED CORRODED CHORD IAW SRM 51-40-02, RECEIVED NEW CHORD PN 146T1060-2 PO 805780. 12 LOCATED, DRILLED & INSTALLED NEW CHORD IAW DWG 146T0250. THIS IS A PART REPLACEMENT NO FURTHER ACTION REQUIRED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,133 hrs · 14,277 cycles

AFT CARGO COMPARTMENT FLOOR STATION 1175 BL 0.0 APPROXIMATELY 8 INCHES TO RIGHT, THREE NUTPLATES CORRODED. REMOVED CORROSION ON FLOORBEAM ORIGINAL THICKNESS .100, MATERIAL REMOVED .030. MATERIAL REMAINING .070 FOUND TO BE OUT OF LIMITS IAW SRM 53-00- 07. FLOOR BEAM REPLACED IAW SRM 53-00-07.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,133 hrs · 14,277 cycles

AFT CARGO COMPARTMENT FLOOR, STATION 1153 FLOORBEAM 6 AREAS MARKED CORROSION ON BEAM & UNDERSIDE OF NUTPLATES. REMOVED CORROSION AT 1153 FLOORBEAM, ORIGINAL THICKNESS .100, MATERIAL REMOVED .030, MATERIAL REMAINING .070, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07. RECEIVED NEW J CHORD PN 146T1060-2 PO 805592.1. LOCATED, DRILL & INSTALLED NEW J CHORD IAW DWG 146T1204 & SRM 52-4 0-02.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 90,133 hrs · 14,277 cycles

CABIN FLOORBEAM GOUGED AT FASTENER HOLE STATION 434, RBL 29 & WL 199. CUT OUT DAMAGE & INSTALLED REPAIR IAW SRM 53-00-51, FIG 201. REPAIR ANGLES & STRAP REPAIR.

Part: WEDGE — DENTED (LE SLAT) · airframe 90,133 hrs · 14,277 cycles

RIGHT WING NR 12 SLAT TE WEDGE UPPER SURFACE DENTED 3 INCHES FROM TE & 57 INCHES FROM INBD EDGE OF WEDGE. EVALUATED 1 EA DENT IAW SRM 57-43-02 ALLOWABLE DAMAGE 1 NOTE J DETAIL ELEVAN FIG 101. DENT FOUND TO BE WITHIN LIMITS WITH NO CREASES, GOUGES CRACKS OR DELAMINATION. A=0.7, Y=.025 A OVE Y =56. RESTORED FINISH IAW AMM51-21-10.

Part: CIRCUIT BREAKER — POPPED (COCKPIT) · airframe 89,621 hrs · 14,207 cycles

CREW REPORTS ON PUSH BACK FOUND LT CTR FUEL PUMP CB IS POPPED.

Part: INDICATION SYS — FLUCTUATES (COCKPIT) · airframe 89,621 hrs · 14,207 cycles

NR 2 ENG EICAS VIB INDICATION FLUCTUATES. VARIABLE 1.5 TO 3.6 AT DIFFERENT POWER SETTINGS.

Part: MOTOR — FAULTY (WINDSHIELD WIPER) · airframe 89,590 hrs · 14,203 cycles

LT WIPER CONTINUES TO WIPE WHEN SWITCHED TO OFF. REPLACED WIPER MOTOR, CHECKED OKAY.

Part: OXYGEN MASK — DEFECTIVE (COCKPIT) · airframe 89,590 hrs · 14,203 cycles

CAPTAIN`S O2 MASK EMERGENCY TEST BUTTON STICKS. REPLACED MASK, GND CHECKED NORMAL.

Part: FAN — MALFUNCTIONED (LEFT) · airframe 89,371 hrs · 14,169 cycles

LT RECIRCULATING FAN LIGHT ON OVERHEAD & ON EICAS. PLACED LT RECIRCULATING FAN ON MEL IAW 2125A.

Part: WIRE — BURNED (CARGO BAY) · airframe 89,353 hrs · 14,167 cycles

WIRE W710-572-20 IS BURNT IN TWO UNDER LT SIDE CARGO BIN FLOOR PANEL NEXT TO LT WALL AT STATION 1220. SPLICED WIRE W0710-0572 STATION 1220 LT SIDEWALL IAW WDM 25-53-24 & SWP 20-30-12.

Part: WIRE — BURNED (CARGO BAY) · airframe 89,353 hrs · 14,167 cycles

WIRE W710-551-20 IS BURNT IN TWO UNDER LT SIDE CARGO BIN FLOOR PANEL NEXT TO LT WALL AT STATION 1220. SPLICED WIRE 0710-0551 STATION 1220 LT SIDEWALL.

Part: WIRE — BURNED (CARGO BAY) · airframe 89,353 hrs · 14,167 cycles

WIRE W710-562-20 IS BURNT IN TWO UNDER LT SIDE CARGO BIN FLOOR PANEL NEXT TO LT WALL AT STATION 1220. SPLICED WIRE W0710-0562 STATION 1220 LT SIDEWALL.

Part: WIRE — BURNED (CARGO BAY) · airframe 89,353 hrs · 14,167 cycles

WIRE W710-582-20 IS BURNT IN TWO UNDER LT SIDE CARGO BIN FLOOR PANEL NEXT TO LT WALL AT STATION 1220. SPLICED WIRE 0710-0582 STATION 1220 LT SIDEWALL.

Part: WIRE — BURNED (CARGO BAY) · airframe 89,353 hrs · 14,167 cycles

WIRE W710-581-20 IS BURNT IN TWO UNDER LT SIDE CARGO BIN FLOOR PANEL NEXT TO LT WALL AT STATION 1220. SPLICED WIRE 0710-0581 STATION 1220 LT SIDEWALL.

Part: WIRE — BURNED (CARGO BAY) · airframe 89,353 hrs · 14,167 cycles

WIRE W710-591-20 IS BURNT IN TWO UNDER LT SIDE CARGO BIN FLOOR PANEL NEXT TO LT WALL AT STATION 1220. SPLICED WIRE 0710-0591 STATION 1220 LT SIDEWALL WDM 25-53-24.

Part: WIRE — BURNED (CARGO BAY) · airframe 89,353 hrs · 14,167 cycles

WIRE W710-592-20 IS BURNT IN TWO UNDER LT SIDE CARGO BIN FLOOR PANEL, NEXT TO LT WALL AT STATION 1220. SPLICED WIRE W0710-0592 STATION 1220 LT SIDEWALL IAW WDM 25-53-24 SWP 20-30-12.

Part: WIRE — BURNED (CARGO BAY) · airframe 89,353 hrs · 14,167 cycles

AFT CARGO DRIVE UNITS INOPERATIVE. FOUND NINE EACH CIRCUIT BREAKERS OUT. UPON FURTHER INSPECTION FOUND WIRE BUNDLE WITH SEVERAL WIRES BURNED IN AFT CARGO LOWER SIDEWALL APPROXIMATELY STATION 1230. REPAIRED SEVERAL WIRES, STATION 1220 LT SIDEWALL FLOOR LEVEL IAW WDM 25-53-22 & 25-53 -25 & SWP 20-30-12. ALL OPERATIONS CHECKED NORMAL.

Part: WIRE — BURNED (CARGO BAY) · airframe 89,353 hrs · 14,167 cycles

WIRE W710-566-20 IS BURNT IN TWO UNDER LT SIDE CARGO BIN FLOOR PANEL NEXT TO LT WALL AT STATION 1220. SPLICED WIRE 0710-0566 STATION 1220 LT SIDEWALL.

Part: WIRE — BURNED (FUSELAGE) · airframe 89,353 hrs · 14,167 cycles

WIRE W0710-327-20 THREE WIRES TWISTED PAIR IS BURNT IN TWO UNDER FLOOR PANEL NEXT TO LT SIDEWALL AT STATION 1220. SPLICED WIRE 0710-0327 RBY STATION 1220 SIDEWALL LT.

Part: WIRE — BURNED (CARGO BAY) · airframe 89,353 hrs · 14,167 cycles

WIRE W710-338-20 THREE WIRES TWISTED PAIR IS BURNT IN TWO UNDER LT SIDE CARGO BIN FLOOR PANEL NEXT TO LT WALL AT STATION 1220. SPLICED WIRE 0710-0338 STATION 1220 LT SIDEWALL IAW WDM 25-53-22 & SWP 20-30-12.

Part: WIRE — BURNED (CARGO BAY) · airframe 89,353 hrs · 14,167 cycles

WIRE W0710-302-20 BURNT IN TWO, THREE WIRES TWISTED PAIR AT STATION 1220 BELOW LT FLOOR EDGE. REPAIRED WIRE IAW SWP 20-10-13 WITH TWO SPICES & A ONE FOOT SECTION OF WIRE AT STATION 1220 UNDER LT CARGO FLOOR PANEL NEXT TO LT SIDEWALL.

Part: WIRE — BURNED (CARGO BAY) · airframe 89,353 hrs · 14,167 cycles

WIRE W710-335-20 THREE WIRES TWISTED, PAIR IS BURNT IN TWO UNDER LT SIDE OF CARGO BIN FLOOR PANEL NEXT TO LT CARGO BIN WALL. SPLICED WIRE 0710-0335 STATION 1220 LT SIDEWALL.

Part: WIRE — BURNED (CARGO BAY) · airframe 89,353 hrs · 14,167 cycles

WIRE W710-323-20 THREE WIRES TWISTED PAIR IS BURNT IN TWO UNDER CARGO BIN FLOOR PANEL NEXT TO LT WALL AT STATION 1220. SPLICED WIRE W0710-0323 RBY STATION 1220 LT SIDEWALL.

Part: WIRE — BURNED (CARGO BAY) · airframe 89,353 hrs · 14,167 cycles

WIRE W0710-167-20 BURNT IN TWO UNDER CARGO BIN FLOOR AT STATION 1219 UNDER LT EDGE OF FLOOR. REPAIRED WIRE IAW SWP 20-10-13 WITH TWO SPLICES & A ONE FOOT SECTION OF WIRE AT STATION 1220 UNDER LT CARGO BIN FLOOR PANEL NEXT TO LT SIDEWALL.

Part: WIRE — BURNED (CARGO BAY) · airframe 89,353 hrs · 14,167 cycles

WIRE W0710-304 BURNT IN TWO AT STATION 1220 UNDER LT SIDE OF FLOOR IN CARGO BIN. SPLICED WIRE W0710-0304 RBY IAW WDM 25-53-22 & SWP 20-30-12 STATION 1220 LT SIDEWALL.

Part: WIRE — BURNED (CARGO BAY) · airframe 89,353 hrs · 14,167 cycles

WIRE W0710-62-20 DAMAGED WIRE BURNT IN TWO. REPAIRED WIRE WITH TWO SPLICES & A ONE FOOT SECTION OF WIRE IAW SWP 20-10-13. REPAIR LOCATED AT STATION 1220 UNDER LT SIDE OF CARGO BIN FLOOR NEXT TO LT WALL.

Part: WIRE — BURNED (CARGO BAY) · airframe 89,353 hrs · 14,167 cycles

WIRE W0710-307-2 THREE WIRES TWISTED. TWO WIRES BURNT IN TWO AT STATION 1220 JUST UNDER LT SIDE OF CARGO BIN FLOOR. SPLICED WIRE W0710-0307 RBY STATION 1220 LT SIDEWALL IAW WDM 25-53-22 & SWP 20-30-12.

Part: WIRE — BURNED (CARGO BAY) · airframe 89,353 hrs · 14,167 cycles

WIRE W710-328-20 3 WIRE TWISTED PAIR IS BURNT IN TWO UNDER LT CARGO BIN FLOOR PANEL NEXT TO LT SIDEWALL PANEL AT STATION 1220. SPLICED WIRE 0710-0327 RBY STATION 1220 LT SIDEWALL, IAW WDM 25-53-22 & SWP 20-30-12.

Part: WIRE — BURNED (CARGO BAY) · airframe 89,353 hrs · 14,167 cycles

WIRE W710-501-20 IS BURNT IN TWO UNDER LT SIDE CARGO BIN FLOOR PANEL NEXT TO LT WALL AT STATION 1220. SPLICED WIRE 0710-0501 STATION 1220 LT SIDEWALL.

Part: WIRE — BURNED (CARGO BAY) · airframe 89,353 hrs · 14,167 cycles

WIRE W710-331-20 THREE WIRES TWISTED, PAIR IS BURNT IN TWO UNDER CARGO BIN FLOOR PANEL LT SIDE NEXT TO SIDEWALL AT STATION 1220. SPLICED WIRE W0710-0331 STATION 1220 LT SIDEWALL.

Part: WIRE — BURNED (FUSELAGE) · airframe 89,353 hrs · 14,167 cycles

WIRE W0710-315 THREE WIRES TWISTED, PAIR IS BURNT IN TWO UNDER LT EDGE OF FLOOR PANEL NEXT TO LT SIDEWALL AT STATION 1220. SPLICED WIRE W0710-0315 RBY STATION 1220 SIDEWALL LT.

Part: WIRE — BURNED (CARGO BAY) · airframe 89,353 hrs · 14,167 cycles

WIRE W710-502-20 IS BURNT IN TWO UNDER LT SIDE CARGO BIN FLOOR PANEL NEXT TO LT WALL AT STATION 1220. SPLICED WIRE 0710-0502 LT SIDEWALL STATION 1220.

Part: WIRE — BURNED (CARGO BAY) · airframe 89,353 hrs · 14,167 cycles

WIRE W0710-308-20 BURNT IN TWO. THREE WIRES TWISTED PANEL STATION 1220 JUST UNDER CARGO BIN FLOOR PANEL NEXT TO SIDEWALL. SPLICED WIRE W0710-0308 RBY STATION 1220 LT WDM 25-53-22 & SWP 20-30-12.

Part: PRESSURE SWITCH — SHORTED (FUEL SYSTEM) · airframe 89,298 hrs · 14,159 cycles

LT ENG FUEL FILTER EICAS, RTFL. IAW AMM 73-34-00 FIG 103 FOR TROUBLESHOOTING. ALSO REPLACE & INSPECT THE LT ENG FUEL FILTER IAW AMM. TROUBLESHOT IAW FIM 73-34-00, ENG CHECK 3 & 12 REPLACED THE NR 1 ENG FUEL FILTER & A SHORTED FUEL PRESS SWITCH. NO DEBRIS IN THE FUEL FILTER & ALL LEAK & OPERATIONS CHECKED OK IAW AMM 73-34-01 & 73-11-02 EICAS CLEARED OK FOR SERVICE.

Part: ANTI-ICE VALVE — MALFUNCTIONED (LT ENGINE) · airframe 89,099 hrs · 14,130 cycles

LT ENG TAI VLV STATUS MESSAGE. LT ENG TAI VLV DEFERRED IN LOCKED OPEN POSITION IAW MEL 3021G.

Part: ANTI-ICE VALVE — FAULTY (LT ENGINE) · airframe 89,071 hrs · 14,126 cycles

EICAS MSG ENG ANTI- ICE DISPLAYED & ENG ANTI-ICE VLV LIGHT REMAINED ILLUMINATED WITH SWITCH ON, POSITION 1. TROUBLESHOOT IAW MM 30-21-00-0100 SERIES PAGES FIGURE 105. ON & OFF INTERMITTENTLY WITH ANTI-ICE SELECTED ON. REPLACED ANTI ICE VLV, RAN ENG, CONFIRMED VLV OPENS & CLOSES NORMALLY. EICAS INDICATION OPERATIONS NORMALLY. MEL RAISED FOR SWITCH INDICATION FAULT

Part: PITOT HEAD — FAULTY (PITOT/STATIC SYS) · airframe 88,960 hrs · 14,111 cycles

IAW LOG1 REPLACED FIRST OFFICERS PITOT STATIC CURRENT SENSING RELAY K310 IAW WAM 30-31-21, NO HELP. SLAVED NEW PITOT PROBE ALL TESTED GOOD, NEED NEW FIRST OFFICERS PROBE AMM. OLD PROBE CONNECTOR SAFETY WIRE BROKEN, REPLACED PITOT, FIRST OFFICERS SIDE IAW AMM. PN 08561LU6 SN OFF 218422 SN ON 1666701.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,871 hrs · 14,099 cycles

FWD GALLEY STATION 322 FLOOR PROXIMITY LIGHT INOPERATIVE. FWD GALLEY STATION 322 FLOOR PROXIMITY LIGHT REPLACED & LIGHT TESTED NORMAL.

Part: LOOP — FAULTY (APU BAY) · airframe 88,562 hrs · 14,057 cycles

LT BLEED DUCT LEAK ON EICAS AT GATE. AUXILIARY POWER UNIT BLEED ON ONLY. REPLACED TS208 LEAK DETECTOR LOOP IAW MM, OPERATIONS CHECKED NORMAL.

Part: PUMP — INOPERATIVE (FUEL SYSTEM) · airframe 87,894 hrs · 13,971 cycles

RIGHT CENTER FUEL PUMP LOW PRESSURE LIGHT DOES NOT ILLUMINATE WITH BOTH ENGINES SHUTDOWN AND SWITCH ON. FUEL PUMP INOPERATIVE.

Part: BALLAST — INOPERATIVE (CABIN LIGHTS) · airframe 87,910 hrs · 13,973 cycles

BALLAST BETWEEN SEAT 1A AND 1B IS INOPERATIVE. 1A SIDEWALL LIGHT IS INOPERATIVE. SIDEWALL LIGHT AT SEAT 1A IS INOPERATIVE. CONNECTOR HAS BEEN REMOVED AND SECURED. THE DISCONNECTION WAS PROMPTED BY A HIGH PITCH NOISE AT SEAT 1A.

Part: VIDEO MONITOR — FAILED (SEAT 6B) · airframe 87,719 hrs · 13,949 cycles

CABIN VIDEO SCREEN PRODUCED SMOKE AND IS INOPERATIVE AT SEAT 6B. TURNED OFF ENTIRE IFE SYS AND SMOKE FROM MONITOR AT 6B STOPPED. INSPECTED ALL CABLE HARNESSES GOING TO MONITOR WITH NO DEFECTS NOTED. FOUND SMOKE ODOR AT BACK OF MONITOR AND GROUND STUD BROKEN ON SEAT POWER MODULE. R &R MONITOR IAW MM 23-32-14 & SPM IAW MM 23-34-18, OPS CHECKED GOOD.

Part: SHUTOFF VALVE — FAILED (LT BLEED SYS) · airframe 87,656 hrs · 13,941 cycles

LEFT ENGINE BLEED OFF EICAS, NO AIR AVAILABLE WHEN ENGINE UP AND CYCLED S11 BREAKER. ACCOMPLISHED HEALTH CHECK IAW 36-00-99. FOUND PRSOV FILTER MORE THAN 90% CLOGGED. FOUND PRV SHAFT WORN OUT AND PRV CONTROLLER OUTSIDE OF HEALTH CHECK PARAMETERS. REPLACED SHUTOFF VALVE.

Part: ADC — FAILED (RIGHT) · airframe 87,608 hrs · 13,935 cycles

RIGHT ADC APPEARED TO HAVE FAILED DURING AIR DATA TEST. REPLACED RT ADC IAW MM. ALL TESTS AND INDICATIONS NORMAL.

Part: STARTER — FAILED (APU) · airframe 87,510 hrs · 13,921 cycles

APU FAULT DURING START. HUNG AT 33 PERCENT AND DIED. REPLACED STARTER IAW MM, OPS CHECKED GOOD.

Part: PUMP — LEAKING (FUEL SYSTEM) · airframe 87,400 hrs · 13,901 cycles

LEFT ENGINE DRIPPING FUEL AT A RATE OF 24 DROPS PER MINUTE. PERFORMED LEAK CHECK AND FOUND DRAIN NR 3 LEAKING FUEL AT A RATE OF 24 DROPS A MINUTE. ITEM CARRIED FORWARD IAW AMM 71-71-00, PAGE 604, REF: NOTE 4, FOR 50 HRS. FOUND FUEL LEAKING FROM FUEL PUMP DRIVE, REQUIRES FUEL PUMP REPLACEMENT.

Part: ACCESS PANEL — MISSING (NR 2 NACELLE) · airframe 87,409 hrs · 13,902 cycles

NR 2 ENG PYLON INBD SIDE ENGINE MOUNT ACCESS PANEL 446BL IS MISSING. REPLACED PER AMM 54-53-01, REF CF634 FOR PAINTING PANEL.

Part: SHUTOFF VALVE — FAULTY (LT ENGINE) · airframe 87,324 hrs · 13,892 cycles

LEFT ENGINE HPSOV STATUS MESSAGE DURING DESCENT. REPLACED HPSOV IAW MM RAN ENGINE DUCT PRESSURE, NORMAL. NO FAULTS.

Part: WIRE — DAMAGED (FIRE LOOP) · airframe 86,830 hrs · 13,837 cycles

LEFT ENGINE FIRE LOOP 2 STATUS MESSAGE INTERMITTENTLY IN FLT. FOUND FIRE LOOP WIRES INSULATION AND BROKEN STRANDS DEFECTIVE. WIRE REPAIRED IAW MM 71-51-00. GROUND FUNCTIONAL TESTED GOOD.

Part: CLAMP — DEFECTIVE (FEEDER CABLE) · airframe 86,839 hrs · 13,838 cycles

NR 1 ENGINE FEEDER CABLE CLAMP INSULATION BAD AT 10:00 POSITION. REPLACED DEFECTIVE CLAMP.

Part: FAIRING — OUT OF TOLERANCE (NR 2) · airframe 86,700 hrs · 13,820 cycles

REF CF0606 NEED TO REMOVE STRUT BIFURICATION PANEL AT THE 12 O'CLOCK POSITION ON THE NR 2 ENGINE. REPLACED OUTBOARD BIFURICATION FAIRING AT THE 12 O'CLOCK POSITION.

Part: PRECOOLER — CRACKED (NR 2 ENGINE) · airframe 86,700 hrs · 13,820 cycles

FOUND NR 2 ENGINE PRECOOLER HOUSING CRACKED AT LEFT SIDE FORWARD LOWER CORNER. REMOVED NR 2 PRECOOLER IAW MM. INSTALLED PRECOOLER IAW AMM.

Part: SWITCH — FAULTY (APU) · airframe 86,684 hrs · 13,818 cycles

APU FAULT NO START 2 ATTEMPTS. APU INOP. DF. REF MEL 49 11D. INF- :BIT APUC FAULTING THE FAN VALVE. INF- :IPC 49-51-00-00K PAGE 1 ITEM 100. (PCN 645-3645). RPL- :DISREGARDED NUISANCE OIL COOLER FAN AIR VALVE. VALVE HAS BEEN ELIMINATED REF POST SB 49-73-91. REPLACED LOP SWITCH REF AMM 49-27-00.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 86,665 hrs · 13,814 cycles

EMERGENCY LIGHT LENS COVER AT SEAT 14AB IS DAMAGED. REPLACED LENS.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,665 hrs · 13,814 cycles

EMERGENCY LIGHT IS INOPERATIVE ON RIGHT AFT CABIN NEAR R2 DOOR. SECURED LOOSE CONNECTOR, OPS NORMAL.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 86,665 hrs · 13,814 cycles

EMERGENCY LIGHT LENS COVER IS MISSING AT SEAT 8AB. REPLACED LENS.

Part: LINE — DAMAGED (ENGINE OIL) · airframe 86,665 hrs · 13,814 cycles

TWO .375 INCH DIAMETER STAINLESS STEEL TUBING DAMAGED FROM CHAFING; HAS FLAT SPOT APPROX .750 INCH LONG BY.125 IN WIDE LOCATED APPROXIMATELY 6 INCH FWD OF MAIN OIL FILTER ON NR 1 ENG. REMOVED LINES. REPLACED DAMAGED LINES.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,665 hrs · 13,814 cycles

EMERGENCY LIGHTS ARE INOPERATIVE ON LEFT SIDE FROM SEAT 24AB TO SEAT 33AB. REPLACED POWER SUPPLY AND BATTERY NEAR SEAT 29AB, OP CHECKED OKAY.

Part: BLADE — DAMAGED (NR 1 ENGINE) · airframe 86,554 hrs · 13,798 cycles

NR 1 ENGINE BLADE NR 15 REQUIRES REWORK. ACCOMPLISHED BLEND IAW MM72-31-02-801 AND ACP HFEC INSPECTION PER NTM UAL PART6 72-31-401.

Part: BLEED VALVE — INOPERATIVE (APU BLEED SYS) · airframe 86,446 hrs · 13,784 cycles

APU BLEED VALVE INOPERATIVE CLOSED. FLT CREW CONFIRMED VALVE CLOSED. REPLACED APU BLEED VALVE PER AMM, OPS CHECK GOOD WITH NO DEFECTS NOTED.

Part: FAUCET — LEAKING (LAVATORY) · airframe 86,446 hrs · 13,784 cycles

MID LAV LEAKING WATER ON FLOOR. MID LEFT LAV WATER SINK LEAKING SHUTOFF WATER OFF TO SINK NO OTHER LEAKS NOTED. FOUND WATER LEAKING FROM FAUCET. REPLACED FAUCET, OPS GOOD. NO FURTHER LEAKS NOTED. OK TO CONTINUE.

Part: TIRE — CRACKED (NLG) · airframe 86,444 hrs · 13,783 cycles

RIGHT NOSE TIRE GROOVE CRACKING. REMOVED AND REPLACED RIGHT NOSE TIRE AND WHEEL ASSEMBLIES PER AMM.

Part: BLEED VALVE — FAILED (NR 2 ENGINE) · airframe 86,087 hrs · 13,737 cycles

NR 2 PRSOV FAILED HEALTH CHECK. SOLENOID FAILED TO ACTUATE WHEN ENERGIZED. REPLACED NR 2 ENGINE PRSOV IAW MM. NO LEAK PRESENT. SYSTEM OPERATED NORMAL PER MM.

Part: AUDIO PANEL — INOPERATIVE (CAPTAIN'S) · airframe 86,053 hrs · 13,733 cycles

CAPTAIN`S FLIGHT INTERPHONE IS NOT WORKING. ALL OTHER COMMS FUNCTION ON CAPTAIN`S PANEL, WORK NORMAL. REPLACED CAPTAINS AUDIO CONTROL PANEL,OPS CHECKED GOOD.

Part: WINDSHIELD — FAULTY (COCKPIT) · airframe 86,038 hrs · 13,731 cycles

CAPTAINS WINDOW HEAT INOPERATIVE. REPLACED WINDOW PER AMM 5 6-11-01. COMPLETED UP TO ITEM 12 AND FIRST TORQUE.

Part: TERMINAL BLOCK — DAMAGED (SENSOR) · airframe 86,038 hrs · 13,731 cycles

TERMINAL BLOCK TB322 SENSOR 1 ON CONNECTOR IS SEPARATED FROM MOUNTING IN AVIONICS BAY. RESECURED TB322 BLOCK 6 AND PINNED TO NORMAL POSITION IAW WDM 30-41-11 PAGE 1. 1 SHEET 2.

Part: ACTUATOR — FAULTY (SPOILERS) · airframe 85,658 hrs · 13,676 cycles

DURING CLIMB, 7.5 UNITS OF LT TRIM NEEDED AND DURING CRUISE 4.5 UNITS LT TRIM NEEDED. FOUND NR 6 SPOILER DROPS AFTER HYDRAULIC. REMOVED DURING DROP TEST. REPLACED NR 6 SPOILER ACTUATOR PER MM 27-61-02 .

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,555 hrs · 13,661 cycles

FLOOR EEL INOP: IN FRT OF RT MID LAV AND CLOSET. REPLACED EEL LIGHT STRIP ACCORDING TO AMM, OPS CHECK GOOD.

Part: WIRE — DAMAGED (GALLEY) · airframe 84,959 hrs · 13,580 cycles

ACRID ODOR IN AFT GALLEY. DIMINISHED AFTER TURNING OFF CHILLERS AND LIGHTS IN GALLEY. FOUND A BURNED SPEAKER WIRE. FOUND 3 GALLEY CART PIGTAILS DAMAGED. REPLACING SPEAKER & WIRE AND REPAIRED AND REPLACED GALLEY CART PIGTAILS.

Part: STARTER — FAULTY (APU) · airframe 84,752 hrs · 13,551 cycles

APU WILL NOT START EGT 715 & RPM 25 THEN SHUT DOWN PERFORMED BITE CHECK AND SHOWS NO ACCELL LAST 2 START ATTEMPTS WITH PT SENSOR. SEE 49-11-00 FOR T/S INFO. TESTED HYD GEN PER MM. REPLACED STARTER AND APU STARTED NORMAL.

Part: CONTROLLER — FAILED (BLEED AIR SYS) · airframe 84,072 hrs · 13,458 cycles

RIGHT ENGINE PRC FAILED PNEUMATIC HEALTH AND PRV SHAFT HAS EXCESS PLAY. REPLACED PRC PER AMM AND PRV PER AMM. ACP'D BLEED SHIFT, ALL PRESSURES AND INDICATIONS NORMAL.

Part: CONTROLLER — MALFUNCTIONED (BLEED VALVE) · airframe 84,020 hrs · 13,452 cycles

BLEED LT RT SIDE AND RT ENG HPSOV EICAS AND STATUS MESSAGE. REPLACED HPC PER AMM. ALL PRESSURES & INDICATIONS NORMAL HIGH POWER RUN.

Part: WARNING LIGHT — FALSE ACTIVATION (BLEED SYS) · airframe 83,999 hrs · 13,450 cycles

RT ENG BLEED LGT AND R ENG HPSOV EICAS MSG DURING DESCENT WITH ENG BLEED SW ON, AND ENG RUNNING. DUCT PRESSURE IS 15PSI. ACCOMPLISHED AIR SUPPLY CONTROL SYSTEM TEST PER AMM TASK 36-23-00-715-001. NO FAULTS NOTED ON AIR SUPPLY BITE MODULE.

Part: PANEL — DAMAGED (CARGO SIDEWALL) · airframe 83,619 hrs · 13,397 cycles

FWD PIT SIDE WALL PANEL DAMAGED BEYOND REPAIR REF FCD2553-01115. REPLACED PANEL.

Part: LIGHT — INOPERATIVE (FIRE BOTTLE) · airframe 83,538 hrs · 13,387 cycles

NUMBER 2 FIRE BOTTLE DISCHARGE LIGHT INOPERATIVE.

Part: CONTROLLER — FAULTY (NR 2 ENGINE) · airframe 83,501 hrs · 13,382 cycles

RIGHT ENG HPSOV EICAS ILLUMINATED. OCCURED WHEN POWER STABILIZED AT LEVEL OFF. TROUBLESHOT HPSOV-HPC SYSTEM. REPLACED HPC FOR FAILURE. PERFORMED AIR SUPPLY BITE SYSTEM TEST, OPS CHECK GOOD.

Part: FAILSAFE — CORRODED (BS 1562 S39L/R) · corrosion level 2 · airframe 83,499 hrs · 13,381 cycles

AFT CARGO BAY BS 1562 FAILSAFE CORRODED BETWEEN STR 39L -39R AT FUSELAGE DRAIN HOLE. REMOVED CORROSION FROM FAILSAFE & FOUND MATL LOSS WITHIN LIMITS OF SRM 51-10-02.

Part: WIRE — OPEN (EMERGENCY LIGHTS) · airframe 83,499 hrs · 13,381 cycles

WHEN MOVING SWITCH FOR EMERGENCY LIGHTS CONTROL TO OFF POSITION ON THE P5 PANEL LIGHTS ARE ILLUMINATED. FOUND OPEN WIRE W1240-005 3-20 IN ROW 31 CEILING OVERHEAD AREA. REPAIRED AND INSTALLED SPLICE IAW B767-300 SWPM 20-30-12. OPS CHECK GOOD IAW 767 AMM 31-51-00.

Part: OXYGEN MASK — MISINSTALLED (CABIN) · airframe 83,499 hrs · 13,381 cycles

LEFT CABIN O2 MASKS PACKED INCORRECTLY. REPACKED LEFT CABIN O2 MASKS AND CLOSED PSU'S REF B767-300 AMM 35-21-14.

Part: OXYGEN MASK — MISINSTALLED (RT PSU) · airframe 83,499 hrs · 13,381 cycles

RIGHT PSU O2 MASK INCORRECTLY PACKED. REPACKED RT O2 MASK PER AMM.

Part: FASTENER — BURNED (FUSELAGE) · airframe 83,473 hrs · 13,377 cycles

FOUND 26 BURNED FASTENERS ON RIGHT FORWARD FUSELAGE BETWEEN STA 246 AND 434, STRINGERS 24 TO 28. REMOVED AND REPLACED 26 BLIND FASTENERS ON NR 4999N00397 IAW B767-300 SRM 53-00-01 REPAIR 8.

Part: WIRE HARNESS — BROKEN (NR 1 ENGINE) · airframe 82,528 hrs · 13,251 cycles

FOUND EGT HARNESS AT PROBE NR 2 BROKEN. HARNESS IN NR 1 ENG REPLACED PER MM.

Part: O-RING — LEAKING (OIL TANK CAP) · airframe 82,214 hrs · 13,209 cycles

AFTER 5 MIN IDLE FOUND LEAKAGE AROUND THE OIL TANK CAP AREA. REPLACED OIL TANK CAP O-RING PER A-CK J-C.

Part: FIRESEAL — MISSING (PYLON) · airframe 82,214 hrs · 13,209 cycles

PANEL 437AR AFT FIRE SEAL MISSING. REPAIRED FIRE SEAL SECTION.

Part: FMU — FAULTY (NR 2 ENGINE) · airframe 82,020 hrs · 13,185 cycles

RT ENG FUEL FILTER IND, RTFL. PUMP METERING VALVE READY TO BE RMV'D. NR 2 ENG FUEL PUMP & FUEL METERING UNIT RMV'D FOR LOG2. ACCMP'D REMOVAL REF MM 73-11-01 PAGE 412 PARAGRAPH 3A AND MM 73-21-03 PARAGRAPH 3 E 2. INSTALLED NEW FUEL PUMP AND FUEL METERING UNIT AS ONE ON NR 2 ENG. REF: MM 73-11-01 AND COMPLETED INSTALLATION OF FMU FROM 3E4 THRU 3E8 ON TOD. SEE SMC 15 FOR INSTALLATION OF COMPRESSOR STATOR MANIFOLD LINE. COMPLETED INSTALLATION OF FMU PER TOD. RAN ENG PER JRH, OPS CK NORMAL. NO LEAKS NOTED.

Part: REGULATOR — LEAKING (CREW O2) · airframe 81,908 hrs · 13,170 cycles

PRIOR TO COA 615671 FOUND O2 SYSTEM LEAKING WHEN SUPPLY WAS SHUTOFF. OXYGEN LEAK EXCEEDS LIMITS. OXY PRESS REG RPLC'D, OPS CK LEAK CKD SYS GOOD.

Part: BLADE — NICKED (ENGINE) · airframe 81,798 hrs · 13,156 cycles

UNFILED NICK ON OUTER BLADE (7 O'CLOCK) POSITION ENG NR 1. FOUND NR 4 FAN BLADE WITH NICK AT LEADING EDGE 0185 INCH DEEP ABOUT FIVE EIGHT INCH FROM EDGE AND ONE TREE QUARTER OF INCH AT END. ACCOMPLISHED BLADE BLEND PER AMM. BLADE WILL REQUIRE EDDY CURRENT INSPECTION WITHIN 6 FLT CYCS. IDT INSPECTION ACCOMPLISHED. ACCOMPLISHED HFEC INSPECTION OF BLENDED AREA OF BLADE NR 4 PER NDTM72-31-401 PT6. NO DEFECTS FOUND.

Part: BRAKE — DAMAGED (NR 1) · airframe 81,744 hrs · 13,148 cycles

NR 1R BRAKE LEAKING AND PUCKS DAMAGED ON ARRIVAL. REPLACED BRAKE PER MM.

Part: COMPUTER — INOPERATIVE (AUTOTHROTTLE SYS) · airframe 81,723 hrs · 13,144 cycles

TMC INOPERATIVE. REPLACED TMC PER MM. OPERATED NORMAL, AIRCRAFT REMOVED FROM CATIII, ACCOUNT OF TMC CHANGE SEE DEFERRED ITEM FOR CATIII CHECK.

Part: GCU — FAULTED (LT GENERATOR) · airframe 81,574 hrs · 13,125 cycles

LT GENERATOR FAULT, FLIGHT DIVERTED. CARRIED OUT BPCU BITE CHECK. FOUND LEFT GENERATION SYSTEM FAULTS. REPLACED LT GCU AND IDG REF MM. FURTHER T- S REQUIRED DUE FAULTS STILL EXISTING. ITEM TRANSFERRED TO SMC6 AS FAULT NOW WITH DAMAGED C901 CONTACTOR IN P31 PWR PANEL. CONTACTOR C901 RMV'D FOR REPLACEMENT DUE TO DAMAGE. MR24229 REQUIRED. C901 HAS BEEN TEMPORARILY INSTALLED TO ALLOW FOR 18 GAUGE WIRING REPAIR. ALL WIRES EXCEPT FOR T3 HAVE BEEN FITTED TEMPORARILY IN POSITION, WASHERS AND NUTS FITTED LOOSELY. TAG AND LUG COVERS ARE IN AIRCRAFT FWD MIRRORED COUNTER. WILL REQUIRE CORRECT INSTALLATION PER MM BEFORE PWR IS RESTORED TO AIRCRAFT. CONFIRMED CORRECT INSTALLATION OF WIRING RO CONTACTOR C901, APPLIED ACFT POWER ALL SATISFACTORY.

Part: DISPLAY — FAILED (COCKPIT) · airframe 81,481 hrs · 13,112 cycles

ACARS CDU BLANKING. REPLACED ACARS CDU.

Part: CONTROLLER — FAILED (BLEED SYSTEM) · airframe 81,316 hrs · 13,089 cycles

RT ENG BLEED OFF AND NO AIR AVAILABLE FOR RT ENGINE ANTI ICE, ACCOMPLISHED PNEUMATIC HEALTH CHECK ON RT ENG PRIORITY VALVE PER MM. FOUND WIRE W3508-009-18 CHAFED TO GROUND APPROX 14" AWAY FROM D11116P. REPAIRED INSULATION PER SWPM. ALSO PRC FAILED HEALTH CHECK. REPLACED PRC PER AMM. ACCOMPLISHED BLEED SHIFT, ALL PRESSURES NORMAL.

Part: CONTROL VALVE — MALFUNCTIONED (AC BAY) · airframe 81,316 hrs · 13,089 cycles

RIGHT PACK OFF-RIGHT BLEED OFF PROBLEMS. ACCOMPLISH RIGHT PACK LOW LIMIT VALVE TEST PER MM. ACCOMPLISH PACK TEMP CONTROLLER BITE PROCEDURE PER MM. IF NO FAULTS FOUND WITH THE LOW LIMIT VLV OR PACK TEMP CONT BITE, REPLACE THE RIGHT PACK FLOW CONTROL VLV PCN (643-9118) MR21290. ALSO REPLACE THE RIGHT PACK FLOW CONTROL CARD PCN (481-9037) MR21511. CHECK ON ONLINE IPC FOR THE MOST CURRENT EFFECTIVITIES.

Part: LINKAGE — UNSECURE (NLG STEERING) · airframe 81,306 hrs · 13,088 cycles

ON WALKAROUND FOUND STEERING LINK AT NLG WITH ONE BOLT LOOSE AND THE OTHER ONE NOT INSTALLED. REPLACED MISSING BOLT AND CHKD IAW MM, CKD OKAY. BOLT REPLACED IS IAW ECRA3251-01031 INSTALLED SUBSTITUTE BOLT NAS67004U15 AND TWO EXTRA WASHERS CKD OK AS PERMANENT REPAIR.

Part: SHUTOFF VALVE — LEAKING (RT BLEED SYSTEM) · airframe 81,296 hrs · 13,087 cycles

RIGHT BLEED ISSUE, RTFL. PRSOV LEAKING. REPLACED PRSOV. LEAK CHECKED LINE TO PRSOV, OK. COMPLETED RUN UP BLEED SHIFT, OK. ALL PRESSURES NORMAL.

Part: CIRCUIT CARD — INOPERATIVE (SMOKE DETECTION) · airframe 81,136 hrs · 13,066 cycles

FWD CARGO ARM LIGHT INOPERATIVE. REPLACED CIRCUIT CARD PER MM, ALL TESTS PASSED.

Part: PRESSURE SWITCH — FAULTY (FUEL SYSTEM) · airframe 81,067 hrs · 13,056 cycles

LOW PRESS LT ON RT FWD FUEL PUMP NOT ON WITH SWITCH IN OFF POSITION. LT TESTS GOOD ON IND LT. REPLACED AFT RT FUEL PRESSURE SWITCH PER MM.

Part: COMPUTER — INOPERATIVE (THRUST MANAGE) · airframe 80,720 hrs · 12,993 cycles

TMC CONTROL PANEL INOPERATIVE. REPLACED TMC, OP CHECKED NORMAL.

Part: TRANSMITTER — MALFUNCTIONED (TE FLAPS) · airframe 80,720 hrs · 12,993 cycles

FLAP LOCK OUT REPORTED. FSEU FAULT DIFFERENCE BETWEEN NR 1 AND NR 8 POSITION TRANSMITTERS. REPLACED NR 8 TRANSMITTER M489, ADJUSTMENT CHECKED PER 27-51-45. REPLACED NR 1 FLAP POSITION TRANSMITTER PER AMM AND CHECKED RESOLVER READ OUTS WITHIN LIMITS OF AMM. RAN FLAPS SEVERAL TIMES NO MTC. OR STATUS MESSAGES.

Part: COMPUTER — FAULTY (NR 1) · airframe 80,025 hrs · 12,886 cycles

UNABLE TO ENTER ASSUMED TEMP FOR REDUCED TAKE OFF, REPLACED THRUST MANAGEMENT COMPUTER, ALL TEST PASSED.

Part: FSEU — MALFUNCTIONED (FLAP SLAT SYS) · airframe 79,723 hrs · 12,845 cycles

EICAS MESSAGE FLAP SLAT ELEC. FIM PERFORMED WITHOUT SUCCESS. SEVERAL RESET PERFORMED. NOT OK. FSEU RERACK NOT OK. BITE TEST SHOWS M545 AMBER LIGHT. FLAP SLAT ELEC FULLY DEPLOYED AND RETRACTED OKAY. EICAS MSG NOT RESETABLE. FSEU REPLACED AS PER AMM.

Part: DETECTOR — FAULTED (CARGO BAY) · airframe 79,675 hrs · 12,838 cycles

"FWD CARGO DET 2" STATUS MESSAGE. WILL NOT CLEAR. COMPLIED WITH MEL. REPLACED DETECTOR PER MM.

Part: PRESSURE SWITCH — FAULTY (OIL SYSTEM) · airframe 79,608 hrs · 12,828 cycles

L ENG OIL FILTER EICAS, RTFL. ALL OTHER (OIL QTY, OIL PRESS, OIL TEMP AND LOW OIL PRESS) INDICATIONS NORMAL, OIL FILTER LIGHT WENT OUT INITIALLY BUT CAME BACK ON NOW STEADY. SAMC TEXT: L ENG S/N 727897. REF AMM 79-35-00 PG 106 FOR OIL FILTER MESSAGE T-SHOOTING, CHECK ALL 6 CHIP DETECTORS AND MAIN OIL FILTER FOR CONTAMINATION, IF NO DEFECTS FOUND, REPLACE MAIN OIL FILTER PCN 280-7113, PACKING 754-8168, O-RING 754-4119, DELTA PRESS SWITCH MR79371, PCN 481-1960. CHECKED ALL CHIP DETECTORS AND MAIN OIL FILTER FOUND NO METAL. REPLACED DELTA PRESS SWITCH PER MM. NO LEAKS OR MSG'S.

Part: ACTUATOR — FAULTY (NR 2 ENGINE) · airframe 79,449 hrs · 12,807 cycles

NR 2 TCC MSG. TCC ACTUATOR MANUALLY ACTUATED, OPS NORMAL. NO DISCREPANCY WITH ELEC CONNECTOR. REPLACED TCC AIR VLV ACTUATOR PER MM.

Part: GENERATOR — INOPERATIVE (APU) · airframe 79,221 hrs · 12,773 cycles

APU GENERATOR QUIT, TRIPS AND FIELD OFF. BPCU BITE SHOWS DP TRIP, GEN POR FDR GEN, OVERLAP ZONE AND UNDER VOLT. PER MM 24-20-00 PD 1 82P ITEM AF ACCOMPLISHED WIRING CHECKS AT GCU AND FOUND T3 WINDING OPEN CIRCIUT, CONFIMED AT GEN THAT GEN AT FAULT. REPLACED GEN ERATOR AND TESTED PER MM. TESTED NORMAL.

Part: CHECK VALVE — FAULTY (RT BLEED) · airframe 79,196 hrs · 12,769 cycles

RT BLEED OFF RT ISLN CLOSED & STILL GETTING 10 PSI OF PRESS IN SYSTEM WITH RT PACK RUNNING. REPLACED ISOLATION CHECK VALVE PER MM, RAN ENG PER JRH. OPS NORMAL.

Part: VALVE — FAULTY (EQUIP COOLING) · airframe 79,009 hrs · 12,743 cycles

FWD EQUIPMENT VALVE LT AND EICAS. REPLACED SUPPLY VALVE, MESSAGE CLEARED.

Part: ACM — OVERHEATED (LEFT) · airframe 78,975 hrs · 12,739 cycles

LT PACK TEMP EICAS DISPLAYED. NO RESET PER CHECK LIST. REPLACED LEFT PACK ACM PER MM.

Part: WIRE — DAMAGED (LT ENGINE) · airframe 78,526 hrs · 12,679 cycles

CREW REPORTS: GOT A FUEL FILTER "STATUS" MESSAGE PASSING 5000FT. THIS IS A "STATUS" MSG ONLY NO EICAS MSG. SAMC TEXT: LEFT ENG FUEL FILTER, REPEAT WRITEUP REF PTT SEQ 1742007, REF AMM 73-34-00 FIG 103 PG 103 FOR FAULT ISOLATION, FUEL FILTER PCN 615-1695, PACKINGS 754-3833 & 750-4553, FUEL FILTER DP SWITCH PCN 621-4506 & 2EA O-RINGS 750-3785. PERFORMED FIM 73-34-00 FIG 103, FOUND ONE WIRE BROKEN AND ONE WIRE CHAFED TO PRESS SWITCH. RESPLICED WIRE. CHECKED FILTER PER 73-22-03 & REPLACEDD FILTER. PERFORMED ENG RUN TEST 3 & CHECKED FOR LEAKS, NONE FOUND.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 78,517 hrs · 12,678 cycles

FUSELAGE INCURRED LIGHTNING STRIKES. REPLACED RADOME.

Part: MODULE — FAULTY (SPOILER) · airframe 78,305 hrs · 12,651 cycles

SPOILER CONTROL MESSAGE ON EICAS. REPLACED SPOILER CONTROL MODULE NR 3 PER MM, OPS CHECK NORMAL.

Part: FAN — FAULTY (FWD POSITION) · airframe 78,305 hrs · 12,651 cycles

FWD EQUIPMENT LOW FLOW WITH HORN. REPLACED FWD RACK SUPPLY FAN PER AMM. OPS CHECK NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 77,670 hrs · 12,565 cycles

AFT LT LAV AISLE EMERGENCY INOPERATIVE. FEEDER CABLE OK. REPLACED BATTERY, OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (SEAT 31AB) · airframe 77,670 hrs · 12,565 cycles

SEAT 31AB EMERGENCY INOP. REPLACED LIGHT, OP CHECK NORMAL.

Part: LIGHT — INOPERATIVE (SEAT 37AB) · airframe 77,670 hrs · 12,565 cycles

SEAT 37AB EMERGENCY INOPERATIVE. REPLACED LIGHT, OPS NORMAL.

Part: RELAY — FAULTY (ENGINE FUEL) · airframe 77,516 hrs · 12,542 cycles

LEFT CTR FUEL PUMP LOW PRESS LIGHT NOT ILLUMINATED WHEN SHOULD BE DURING PREFLIGHT. NO TIME. RELAY K329 REPLACED WITH NO HELP. REPLACED LT ENGINE SPEED CARDS IAW MM. LT CTR BOOST PUMP OPERATIONAL.

Part: ISOLATION MOUNT — FAILED (APU BAY) · airframe 77,372 hrs · 12,519 cycles

APU AFT LEFT ISOLATION MOUNT HAS BAD BEARING AT DIAGONAL BRACE ATTACH POINT. REPLACED APU AFT LT ISOLATION MOUNT ASSY.

Part: BRACKET — DAMAGED (APU BAY) · airframe 77,372 hrs · 12,519 cycles

AFT LEFT APU DIAGONAL TOP MOUNT BRACKET BEARING BAD. REPLACED APU AFT LT DIAGONAL TOP MOUNT BRACKET ASSY.

Part: COOLING FAN — FAULTY (APU) · airframe 77,372 hrs · 12,519 cycles

APU AUTO SHUTDOWN AT GATE. FOUND APU COOLING FAN-OIL COOLING AIR DISCHARGE, TO BE REVERSE FLOW. THIS SHOULD BE AN EXHAUST, INSTEAD IS ACTING AS AN INTAKE. SUSPECT FAN IS RUNNING IN REVERSE. REMOVED FAN. FOUND APU GEARBOX DRIVE GEAR WITHOUT TEETH. REMOVED APU. COMPLETED INSTALLATION FROM SUB TASK 864-043 TO END.

Part: PUMP — INOPERATIVE (FUEL SYSTEM) · airframe 77,310 hrs · 12,507 cycles

LEFT CENTER FUEL PUMP LOW PRESSURE LIGHT NOT ILLUMININATED WHEN SWITCH SELECTED TO "ON" POSITION. LEFT CENTER PUMP LOW PRESS LIGHT WONT ILLUMINATED. LEFT CENTER PUMP INOP. PUMP GROUND CHECKS NORMAL. NO AMIS HISTORY.

Part: VALVE — FAULTY (CABIN TEMP) · airframe 77,172 hrs · 12,486 cycles

HAVE FWD CABIN AUTO TEMP CONTROL INOP. FWD TRIM AIR VALVE FAULT. REPLACED FWD CAB TRIM AIR VALVE IAW MM, VALVE OPS CHECKED OK AND NO LEAKS NOTED.

Part: GENERATOR — FAULTY (APU) · airframe 76,995 hrs · 12,459 cycles

APU GENERATOR WON'T ACCEPT LOAD. GENERATOR FOUND OUT OF TOLERANCE. REPLACED APU GENERATOR IAW MM. OPS ARE GOOD.

Part: STARTER — FAULTY (LT ENGINE) · airframe 76,888 hrs · 12,447 cycles

CREW REPORTS NR1 ENG REACHED 21P PERCENT N2 THEN ROLLED BACK TO 5 PERCENT. ABORTED START ATTEMPT, ENG SPOOLED DOWN TO 0 AND START VALVE LIGHT REMAINED ON. REPLACED LT ENG STARTER IAW MM. REPLACED LT ENG STARTER CONTROL VALVE. OPS CHECK NORMAL.

Part: RELAY — FAULTY (HYD INDICATOR) · airframe 76,555 hrs · 12,403 cycles

ON POWER UP - EICAS MESSAGES EQUIPMENT COOLING AFT FAN - CARGO FIRE DET FAN - BATTERY CHARGER AND HYD QTY DISPLAYED - NO HYD QTY INDICATIONS. ACCOMPLISHED WIRING CHECKS PER WD 24-51-52 PG1A SHT 1 FOUND NO POWER ON K102 PIN A2 WHEN APU OR EXTERNAL CONNECTED AND 115V ON PIN A2 WHEN AC ON GROUND SERVICE POWER. VERIFIED 115V ON A2 OF K103 AND A1 OF K102. REPLACED RELAY K102 PER MM. HYD QTY RETURNED TO NORMAL, ALL STATUS MSGS NOW CLEARED AND BAT CHARGER CHARGING AND EQUIP COOL AND FIRE TEST NORMAL.

Part: CONTROLLER — MALFUNCTIONED (RT ENGINE) · airframe 76,321 hrs · 12,371 cycles

RT ENG BLEED PROBLEM. REPLACED NR2 ENG PRV. REPLACED NR2 ENG PRVC. REPLACED NR2 ENG BLEED AIR CONTROL CARD. REPLACED RT ENG OVERPRESSURE SWITCH, NO HELP. CHECKED AND FOUND FAULT WIRE, PRC ON AIR SUPPLY BITE CHECK. REPLACED CONTROLLER HP VALVE MR36157, CONTROLLER MR36140, VALVE AIR SUPPLY SHUTOFF VALVE MR36159. RAN ENG, CAN ONLY GET 7 PSI 75 PERCENT, COMPARED TO THE LT ENGINE 34 PSI 65 PERCENT. NEEDS MORE TROUBLESHOOTING. SECURED SENSE LINE ELBOW ON RT ENG HP VALVE AND RERACKED RT BLEED AIR CONTROL CARD. RAN ENG AND CYCLED RT BLEED NUMEROUS TIMES AND BLEED INDICATION AND BLEED PRESSURE NORMAL.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 76,319 hrs · 12,370 cycles

EMERGENCY EVACUATION LIGHTS COME ON WHEN POWER IS REMOVED FROM AIRCRAFT AFT FIRST CLASS OVERHEAD AISLES AND EXTERIOR AT FWD AND OVERWING DOORS. REPLACED THE BATTERY PACKS PER TASK CARD 2300R284. OPS CHECKED GOOD.

Part: CONTROLLER — FAILED (POS 1) · airframe 76,319 hrs · 12,370 cycles

NR 1 ENGINE HPC FAILED PNEUMATIC HEALTH CHECK. NR 1 ENGINE REMOVED PRC AND HPC. INSTALLED SERVICEABLE HIGH PRESSURE CONTROLLER IAW MM. INSTALLED PRC IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,218 hrs · 12,357 cycles

EMERGENCY LIGHTS AT 31 AND 37 ARE INOPERATIVE. EMERGENCY LIGHTS AT 31 AND 37 OPS CHECK NORMAL, OK FOR SERVICE.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 76,034 hrs · 12,335 cycles

FWD GALLEY X AISLE EMERGENCY LIGHT INOP. SECURED CONNECTOR, OPS CHECKS GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 76,034 hrs · 12,335 cycles

EMERGENCY LIGHT ADJACENT TO DOOR 1L INOPERATIVE. SECURED CONNECTOR, OPS CHECKS GOOD.

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 76,010 hrs · 12,330 cycles

HYDRAULIC FLUID LEAKING FROM LT STABILIZER AREA RUNNING DOWN BELLY OF AIRCRAFT. LEAK APPEARS TO BE FROM A RUDDER AUTOPILOT SERVO. FOUND LEFT RUDDER RATIO CHANGER LEAKING AT SUPPLY AND RETURN B-NUTS. CHANGED OUT BOTH O RINGS NO LEAKS NOTED DURING OPS CHECK.

Part: CONTROL UNIT — TRIPPED (APU GENERATOR) · airframe 75,827 hrs · 12,302 cycles

BOTH UTILITY BUSSES TRIPPING OFF IN FLT AND ON GND WITH APU PWR. INOPED APU GEN PER MEL. HMG VERIFIED OPERATIONAL. ACCOMPLISH BPCU BITE PROCEDURE. REPLACED BPCU PER AMM. OPS CHECKS GOOD ON GROUND.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 75,636 hrs · 12,271 cycles

THE 1L ENTRY SLIDE RAFT LACING CABLES FOUND PULLED FROM SLIDE PACK, LEFT SIDE. REPLACED SLIDE ON DOCK WU L0302H.

Part: SWITCH — FAILED (OIL SYSTEM) · airframe 75,407 hrs · 12,241 cycles

LEFT OIL FILTER MESSAGE IN FLIGHT. MESSAGE WAS ON AND OFF FOR FIRST (2) HRS OF FLIGHT. MAIN OIL FILTER REPLACED IAW AMM. MASTER MAGNETIC CHIP DETECTOR INSP PFMD OK. CHECKED PLUG ON DIFFERENTIAL PRESSURE SWITCH OK. PFMD ENG RUN-UP WITH CREW CHECKED FOR LEAKAGE AND EICAS STATUS MSG OK. REPLACED OIL FILTER DELTA "P" SWITCH PER MM, NO MESSAGE ON ENGINE RUN, NO LEAKS NOTED.

Part: SHUTOFF VALVE — FAULTY (HYD SYSTEM) · airframe 75,064 hrs · 12,195 cycles

ON TAXI COULD ONLY GET 2040 PSI FROM LT ELEC HYD PUMP ALONG WITH EICAS MESSAGE AND AUDIO. LT ELEC HYD PMP PSI AT 2200. LT ELEC PUMP, ELCU REPLACED, NO HELP. SUSPECT INTERNAL COMPONENT BYPASSING. WILL NEED TO ACP CHECKS. WITH REF TO LOW PRESSURE ON LT ACMP, FIM SUGGESTS THAT THE HYD SYS NEEDS AN INTERNAL LEAKAGE CHECK. (WHENEVER WING & TAIL FLT CONTROL SHUTOFF VLVS ARE POSITIONED TO 'OFF' PRESSURE THEN STABILIZES AT 2800-3200 PSI). IAW SERVICE TIP REPLACE M895 ELCU FOR LT ELEC HYD PUMP. REPLACED M895, NO HELP. REPLACED LT HYD RUDDER AND ELEVATOR SHUTOFF VALVE. HYD PRESSURE NORMAL.

Part: SEAL — DISLODGED (BLEED VALVE) · airframe 74,886 hrs · 12,166 cycles

NR 2 ENGINE HAS APPROX. 5-INCH SEGMENT OF 2.5 BLEED VALVE SEAL PROTRUDING FROM BLEED PORT. REPLACED NR 2 ENGINE.

Part: LIGHT — MISSING (CABIN) · airframe 74,851 hrs · 12,161 cycles

AFT GALLEY CEILING EMERGENCY LIGHT ASSY MISSING. REPLACED EMERGENCY LIGHT L1199, OPS CHECK OK.

Part: VALVE — INOPERATIVE (RT PACK TEMP) · airframe 74,732 hrs · 12,143 cycles

NO COOLING WITH PACKS ON APU FOUND RT PACK TEMP VALVE INOP AT 51 PERCENT OPEN. REPLACED RT PACK TEMP VALVE. GROUND CHECKS NORMAL.

Part: STRUCTURE — DAMAGED (RT WING TE FLAP) · airframe 74,671 hrs · 12,136 cycles

AFTER BIRD STRIKE INSP FOUND DAMAGE ON RT OTBD FLAP T/E. DAMAGE AREA IS 2.5 6" X 2.36" DEPTH OF 0.044" AND IS 6" FROM FAIRING CANAPE AND 5.5" FROM T/E. SECOND AREA IS 1.77"X4.33" DEPTH OF 0.039" AND 0.59" FROM THE FIRST AREA AND 2.76" FROM THE T/E. CARRIED FWD IAW UA EVA 73801 WITHIN 2 FLIGHT CYCLES REMOVE SPEED TAPE AND REINSPECT IAW EVA 73801 (MF5916 CREATED TO MONITOR) WITHIN 2 FLT CYC REMOVE SPEED TAPE AND ACP RE-INSP OF AREA IAW EVA 73801 INSTRUCTION STEPS 1 AND 2 AND ACP. INJECTION REPAIR TO DELAM AREAS IAW GNMM AND APPLY 2 LAYERS OF SPEED TAPE. ACCOMPLISHED INJECTION REPAIR AND REINSPECTED DAMAGE & RETAPED IAW EVA 73801.

Part: CONTROL PANEL — FAULTY (WX RADAR) · airframe 74,659 hrs · 12,134 cycles

CAP WX RADAR FAIL WHEN FO DESELECTS WXR. REPLACED WX RADAR CONTROL PANEL AND TESTED CAPT'S AND FO'S WX SYS, NO FAULTS FOUND.

Part: CONTROL PANEL — FAULTY (WX RADAR) · airframe 74,653 hrs · 12,132 cycles

CAPT SIDE RADAR SELECTIONS APPEAR NOT TO CONTROL ANY FUNCTION OF RADAR SYS. NO TERRAIN FEATURES APPEAR ON HSI AND ALSO IF "WX" AND "TERR" ON CAPT SIDE ARE DESELECTED RADAR STILL PAINTS BUT NO TERRAIN AT ANY TIME. WHEN FO'S "WX" S W IS SELECTED OFF THE CAPT SIDE SHOWS "WEATHER FAIL" ON HSI. REPLACED CTR EFIES SYMBOL GENERATOR REF MM AND WX RADAR SYS. CKD NORMAL.

Part: TRANSCEIVER — FAILED (WX RADAR) · airframe 74,651 hrs · 12,131 cycles

WX RADAR TEST FAILED. RADAR FAILED TEST. REPLACED FAULTY WEATHER RADAR TRANSCEIVER IAW AMM. OPS ARE GOOD.

Part: GYRO — TUMBLES (STANDBY) · airframe 74,039 hrs · 12,043 cycles

STANDBY GYRO HAS TUMBLED, RTFL. REPLACED STANDBY ATTITUDE IND, GROUND CHECK NORMAL.

Part: VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 74,032 hrs · 12,040 cycles

RIGHT ENG BLEED OFF AND RT PACK OFF LIGHTS CAME ON DURING T/O ROLL AND STAYED ON THRU CLIMB AND L-O, THEN BLEED SHUTS OFF. DID BITE CHECK ON AIR SUPPLY BITE MODULE. HITS PRV AND WIRING. SWAPPED LT AND RT AIR SUPPLY CONTROL CARDS-NO HELP, RETURNED CARDS TO ORIGINAL POS. REPLACED RT ENG PRV-NO HELP. REMOVED NEWLY INSTALLED PRSOV FROM NR 2 ENG REMOVED PRSOV FROM NR 1 ENG AND INSTALLED IN NR 2 ENG. NEEDS RUN ACCMP 1 AND 2 ENG FOR PRSOV CHANGES. RAN AT HIGH POWER BOTH ENGS, BLEED PRESSURES NORMAL.

Part: CONTROL UNIT — MALFUNCTIONED (LAVATORY) · airframe 73,950 hrs · 12,025 cycles

LEFT AFT LAV CB P11 U7 FOUND POPPED. PER FLIGHT CREW, "THAT BREAKER THAT'S OUT" IS ACTUALLY P11-U34, RIGHT AFT GALLEY. WITH D392 DISCONNECTED FROM M226 ELCU, CB DOES NOT TRIP. REPLACED ELCU M226, GALLEY POWER CHECKS NORMAL.

Part: CONTROLLER — FAULTY (BLEED AIR SYS) · airframe 73,774 hrs · 12,002 cycles

RT DUCT PRESS 30-50 IN UNISON WITH RIGHT ENG N1 FLUCTUATION .5 PERCENT AND CABIN RATE FLUCT SNPSHT VLV LOCKED CLOSED. REPLACED NR 2 HIGH PRESSURE VALVE CONTROLLER. REOPENED BY OPBLM FOR FAILED ENG RUN. DURING ENGINE START HPSOV EICAS MESSAGE APPEARED. AT IDLE BLEED LIGHT WAS ON. WENT OUT UPON TAXI FOR RUN-UP. AT TAKE OFF POWER RT ENG BLEED LIGHT ON AND OFF WITH EICAS MESSAGE ON AND OFF. ENG SURGED, NO INCREASE OF EGT. REPLACED NR 2 ENGINE PRSOV (PN 773288-7-8-10 / SN 20, POSITION 2) AND HPSOV. RESET BLEED MONITOR AND ACCOMPLISHED ENG RUN. NO FURTHER FAULTS NOTED.

Part: TIRE — DAMAGED (RT MLG) · airframe 73,746 hrs · 11,997 cycles

IAW DISPATCH, CREW FELT NOSE GEAR POSSIBLY STRUCK SOMETHING OR BLEW A NOSE TIRE ON TAKEOFF ROLL. GEAR RETRACTED NORMALLY. INSPECTED ACFT IAW MOP. FOUND NO DAMAGE TO AIRFRAME ON FLAP SURFACES, MLG WHEEL WELL AREAS AND ENGINE INTAKE AND ENGINE COWL AREAS, WING TO FUSELAGE AREAS AND T/E FLAP HINGE AREAS FLAPS WERE LOWERED FOR VISUAL INSPECTIONS. REPLACED NR3 & NR4 FWD MAIN AND NR3 & NR4 AFT MAIN. FOUND NR3 AFT MAIN TIRE BLOWN ON LANDING. NO NOSE DAMAGE NOTED.

Part: SHUTOFF VALVE — FAULTY (RT A/C PACK) · airframe 73,635 hrs · 11,980 cycles

RIGHT PACK OFF LIGHT AND RT DUCT PRESSURE, FLIGHT DIVERTED. ACCOMPLISHED T-S PER MM. PERFORMED BITE OF M15 AIR SUPPLY MODULE, FOUND PRV, PRSOV AND PRC FAULTED. RT ENGINE PRSOV LOCKED IN CLOSED POSITION AND FAMV IN FULL OPEN POSITION. REPLACED PRV AND PRVC. BLEED LIGHT STILL CLOSES WHEN PULLING UP POWER. REPLACED NR 2 ENG PRSOV, LEAK CK'D AND RAN ENG, OPERATES NORMAL.

Part: HEAT EXCHANGER — CRACKED (RT A/C PACK) · airframe 73,442 hrs · 11,951 cycles

HEAVY AIR LEAK NOISE COMING FROM RT PACK. FOUND DURING TOWING, UPON VISUAL INSP FOUND SECONDARY HEAT EXCHANGER WITH A CRACK 7 INCHES LONG. R & R SECONDARY HEAT EXCHANGER. OP CKS NORMAL.

Part: SHUTOFF VALVE — MALFUNCTIONED (NR 1) · airframe 73,402 hrs · 11,945 cycles

1 SPAR VALVE LIGHT REMAINED ILLUMINTATED WITH FUEL CONTROL SWITCH SELECTED (CUTOFF, RICH, RUN). EICAS MSG (L,R) SPAR VALVE DISPLAYED. POS(01=L,02=R) AFTER LT ENGINE START SPAR VALVE AND FUEL VALVE LIGHT ILLUMINATED ENGINE SHUTDOWN. REPLACED NR1 ENG FUEL SHUTOFF VALVE.

Part: BLEED VALVE — FAULTY (APU) · airframe 73,158 hrs · 11,910 cycles

APU BLEED BLEED AIR ON WITH SWITCH OFF. APU VALVE LOCK CLOSED. SUSPECT THE APU BLEED SWITCH AT FAULT. REPLACED VALVE, OPS TEST NORMAL.

Part: LINE — LEAKING (SHUTOFF VALVE) · airframe 73,022 hrs · 11,892 cycles

LEFT ENG BLEED OFF TRIP OFF ON DECENT. ACP BITE CK PRSOV HIT. REPLACED PRSOV. DURING ENG RUN, FOUND NR 2 ENG SOMETIMES FOLLOWS THROTTLES UP PAST 60 PSI OTHER TIMES AFTER BLEED SHIFT, NR 2 KEEPS ON DECREASING TO 8 PSI THEN BLEED GOES OFF. ALSO FOUND AT IDLE HAD L 33-R 5 PSI WITH RT BLEED LIGHT ON, COULD RESTORE RT BLEED BY TURNING ON RT BLEED ISO FOR 1-2 SEC, AND RT BLEED WOULD BE NORMAL. ACCOMP BITE AIR SUPPLY MODULE FAULT PRSOV. REMOVED OLD PRSOV NEW PRSOV PARTIALLY INSTALLED. NEEDS AI VLV CLAMPS INST AND SENSE LINE BONDING WIRES AND ACCESS DOOR LEAK CK AND RUN FOR PROPER PRESSURES. COMPLETED PRSOV INSTALLATION. VALVE OPS NORMALLY. BITE CKS GOOD. FLEXIBLE METAL BRAIDED PRESSURE SENSE LINE THAT CONNECTS TO AFT SIDE OF PRSOV FOUND TO BE LEAKING APPROX 6IN AFT OF FWD 'B' NUT WHERE LINE CONNECTS TO PRSOV. INSTALLED NEW SENSE LINE. LEAK CHECK GOOD. ACP'D ENG RUN. ALL PRESSURES NORMAL AT IDLE,BLEED SHIFT AND HI POWER.

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 72,577 hrs · 11,823 cycles

ONE SPAR VALVE LIGHT REMAINED ILLUMINATED WITH FUEL CONTROL SWITCH SELECTED (CUTOFF, RICH, RUN). EICAS MSG (L, R) SPAR VALVE DISPLAYED. REPLACED ENG FUEL SHUTOFF VALVE & OPS CHECKS NORMAL.

Part: CIRCUIT CARD — FAULTY (EVAC SLIDE) · airframe 72,458 hrs · 11,804 cycles

LT WING SLIDE ECAM INTERMITTENTLY CAME ON. CHECKED OVER WING SLIDE SENSORS S198 PINS C-5, D-5 RESISTANCE READ 13.5, S218 PINS A-5, B-5 RESISTANCE READ 18.6. REPLACED CARD DRIVER, OPS CHECKS NORMAL. NO EICAS MSGS WERE NOTED. NO LIGHTS AT LT OVERWING SLIDE.

Part: SENSOR — OUT OF ADJUST (SLIDE) · airframe 72,410 hrs · 11,794 cycles

LT WING SLIDE EICAS MSG, RTFL. FOUND SENSOR S218 ON LT OVERWING PACK DOOR LOOSE BUT APPEARED TO BE WITHIN TOLERANCE (0.10) BUT WITH MOVEMENT CAUSED EICAS MSG. REMOVED SHIM FROM SENSOR S218 FOR TROUBLESHOOTING, NO HELP. WILL NEED TO RE-GAP S-218. AFTER REMOVING SHIM COCKPIT OVER HEAD LIGHT STILL FLICKERS, WHEN MOVING DOOR INTEGRATOR. FOUND 2 (EA) AFT LATCHES ON LT OFF WING SLIDE COMPARTMENT DR WORN. REPLACED BOTH LATCHES. CHECKED GAP OF SENSOR S218 AND ADJUSTED. NEED SYS CKS AFTER CLOSE UP. CHECKED AND CLOSED LT SIDE DOOR. NO MESSAGES AND NO LIGHT ON P5 PANEL.

Part: DUCT — MALFUNCTIONED (EXHAUST VALVE) · airframe 72,182 hrs · 11,760 cycles

CABIN PRESSURE LOSS, RTFL. REPLACED EQ COOLING OVERBOARD EXHAUST VALVE. NEW VALVE BAD FROM STOCK, ROBBED VALVE FROM KNOWN GOOD AC STILL FAILED, NEEDS MORE T-S. FOUND DUCT CONNECTED TO EXHAUST VALVE CRUSHED. REPLACED DUCT. A/C OKAY FOR SERVICE.

Part: PUMP — FAULTY (HYDRAULIC SYS) · airframe 71,973 hrs · 11,732 cycles

THE C HYD DEM PUMP EICAS MSG DURING GEAR FLAP RETRACTION. REPLACED ADP PRESSURE SWITCH S28, NO HELP. FOUND CTR DEM PUMP ADP OVERSPEED. REPLACED ADP. NO LEAKS AND OPERATIONAL TEST PASSED.

Part: PUMP — MALFUNCTIONED (HYDRAULIC SYS) · airframe 71,799 hrs · 11,697 cycles

CTR HYD PRESS LIGHT ON, EICAS "C HYD DEM PUMP" MSSG W/ SWITCH IN "ON" POS. AS PER VERBAL WITH ARRIVING CREW. EICAS C-HYD DEM PUMP DURING GEAR AND FLAP RETRACTION. LIGHT EXTINGUISHED AFTER RETRACTION. CHECKED ADP. OPS NORMAL ON GROUND. REMOVED ADP, AND HUNG NEW ADP IN POSITION. TROUBLESHOT TO BAD ADP FROM STOCK, REPLACED ADP AGAIN. ADP OPERATION NORMAL WITH THE EXCEPTION OF A LEAK, 60 DROP PER MIN, AT THE PUMP FLANGE. REPLACED HYD SYS ADP. SYS OPS NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 71,776 hrs · 11,691 cycles

THE 'LT ENG FUEL FILTER' EICAS, FLT DIVERTED. AFTER LANDING CAPT REPORTED ENG RAN NORMAL WITH NO PARAMETER SHIFTS. NORMAL SHUTDOWN AT GATE. NO CONTAMINATION FOUND AT FUEL SYS, RPL FUEL FILTER & FUEL FILTER BYPASS SWITCH. LEAK CHECKED, NO LEAKS FOUND. ALSO RAN ENG 5 MIN IDLE RUN. NO LEAKS ON FUEL FILTER PRESS SWITCH. THE SAMC CONTROLLER AND MANAGER CONCURR THAT THE AIRPLANE CAN BE RELEASED BACK TO SERVICE.

Part: GENERATOR — FAILED (APU) · airframe 71,378 hrs · 11,630 cycles

APU GEN ISSUE. APU INOP ELECTRICAL. UNABLE TO LOAD GENERATOR. CREW COMMENTS: APU GEN TRIPPED OFF. WILL NOT RESET. REPLACED GENERATOR. ALL OPS AND CHECKS OKAY.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 71,167 hrs · 11,589 cycles

THE C ADP INOP IN AUTO OR MAN MODE. CREW COMMENTS: AFTER PUSHBACK & AFTER FLAP ACTIVATION GOT EICAS C HYD DEM PUMP. SWITCH TO ON-NO CHANGE. AREA AROUND ADP REQUIRES CLEAN-UP. APPEARS THAT PAINT HAS DEGRADED DUE TO HYD LEAK. REQUIRES CLEAN-UP. REPLACED CENTER ADP. CLEANED AREA AFTER ADP REPLACEMENT.

Part: SKATE ANGLE — LEAKING (FUEL TANK) · airframe 70,990 hrs · 11,564 cycles

NR 2 ENGINE I/B SKATE ANGLE LEAKING FUEL AT AFT TANK SEAM. FOUND LEAK UNDERNEATH OF SKATE ANGLE AFT SEAM PYLON AREA. REMOVED TAIL SAIL PANELS. SCRAPPED SMALL AREA AT SEAM. CONFIRMED FUEL LEAK FROM SEAM UNDER SKATE ANGLE. SCRAPED SEAM AS REQUIRED CLEANED AND SEALED WITH A1-2 B1-2 AT 1800. NEEDS TO BE LEAK CHECKED AFTER 12HRS. LEAK CHECK PASSED WITH TANK TOPPED OFF FOR 2 HRS.

Part: BATTERY — FAULTY (MAIN) · airframe 70,582 hrs · 11,501 cycles

RECEIVED "MAIN BATTERY CHARGER" STATUS MSG. REPLACED MAIN BATTERY & CHARGER. CHECKS OKAY.

Part: OIL FILTER — DEFECTIVE (NR 1 ENGINE) · airframe 70,360 hrs · 11,467 cycles

NR 1 ENGINE OIL FILTER MESSAGE DISPLAYED. MESSAGE REMAINED WHEN THRUST REDUCED AND AFTER ENGINE SHUTDOWN. REPLACED OIL FILTER. CHK C-D'S OK, RAN ENG, NO LEAKS NOTED. PROBABLE PART IS OIL FILTER DIFF PRESSURE SWITCH, REPLACED SWITCH.

Part: SENSOR — OUT OF ADJUST (OVERWING EXIT) · airframe 70,102 hrs · 11,430 cycles

LEFT OVERWING SLIDE EICAS MESSAGE. RTFL. ACCOMPLISHED BITE OF PSEU AND GOT CARDS (005,007 AND 004) FAULT. ALSO GOT S218 SENSOR & TARGET FAULT. FOUND DOOR WARNING SENSOR OUT OF LIMITS. DEACTIVATED OVERWING SLIDES. ADJUSTED TO CORRECT GAP & REACTIVATED SYSTEM, OPS CHECKED OKAY, NO MESSAGE ON EICAS.

Part: TRANSMITTER — FAULTY (LT ENGINE) · airframe 70,102 hrs · 11,430 cycles

LEFT ENGINE OIL QTY INDICATION READS INACCURATE HIGH. REPLACED OIL QUANTITY TRANSMITTER, 1.5 MIN IDLE RUN, NO LEAKS NOTED.

Part: EXCITER — UNKNOWN (NR 2) · airframe 69,380 hrs · 11,330 cycles

REPLACED NR 2 EXCITER BOX. OPS CHECKS OK. REPLACED NR 2 EXCITER BOX P/N 50T847 - SHIELD; P/N AA134S1 - IGNITER PLUG; P/N 48174 - CABLE; P/N 44958 - CABLE & P/N 10-621630-1 - EXCITER.

Part: UNKNOWN — ODOR (CABIN) · airframe 69,380 hrs · 11,330 cycles

FLT ATTENDANTS REPORT SMOKE SMELL IN MID CABIN. ACCOMPLISHED VISUAL AND SMELL TEST FOR 30 MINUTES. NO ODOR DETECTED. RAN PACKS AND UTILITY BUSSES FOR 30 MINUTES, CHECKS GOOD. SUSPECT GLYCOL RESIDUE.

Part: UNKNOWN — ODOR (CABIN) · airframe 69,380 hrs · 11,330 cycles

FLIGHT ATTENDANTS REPORT, SMOKE SMELL IN MID CABIN. ACCOMPLISHED VISUAL AND SMELL TEST FOR 30 MINUTES. NO ODOR DETECTED. RAN PACKS AND UTILITY BUSSES FOR 30 MINUTES, CHECKS GOOD. SUSPECT GLYCOL RESIDUE.

Part: LIGHT — FAULTY (CABIN) · airframe 69,310 hrs · 11,320 cycles

EEL LIGHT BAR L901 NOT FULLY ILLUMINATED. REPLACED LIGHT BAR L901 AT FWD RT GALLEY AND REPLACED BATTERY AT CHARGER M730, OPS CHECK GOOD.

Part: LIGHT — FAULTY (CABIN) · airframe 69,310 hrs · 11,320 cycles

EEL LIGHT BAR L910 PARTIALLY ILLUMINATES. REMOVED BAD EEL LIGHT BAR AND INSTALLED SERVICEABLE LIGHT BAR L910 AT AFT LT LAV, AND OPS CHECK GOOD.

Part: LIGHT — FAULTY (CABIN) · airframe 69,310 hrs · 11,320 cycles

EEL LIGHT BAR L985 AND L904 PARTIALLY ILLUMINATES. REMOVED BAD LIGHT BARS AND REPLACES WITH SERVICEABLE LIGHT BARS L985 AND L904 AT RT AFT LAV AND CENTER AFT GALLEY AREA AND OPS CHECK GOOD.

Part: LIGHT — FAULTY (CABIN) · airframe 69,310 hrs · 11,320 cycles

EEL LIGHT BARS L905 AND L897 DO NOT FULLY ILLUMINATE. REMOVED BAD LIGHT AND INSTALLED SERVICEABLE LIGHT BARS L905 AND L897 AT MID LT LAV AND CENTER PARTITION AND OPS CHECK GOOD.

Part: LIGHT — FAULTY (CABIN) · airframe 69,310 hrs · 11,320 cycles

EEL LIGHT BAR L896 PARTIALLY ILLUMINATES. REPLACED LIGHT BAR L896 AT RT MID LAV-CLOSET AND OPS CHECK GOOD.

Part: LIGHT — FAULTY (CABIN) · airframe 69,310 hrs · 11,320 cycles

FWD EEL LIGHT BARS L900 AND L908 DO NOT FULLY ILLUMINATE. REMOVED BAD LIGHT BARS AND REPLACED WITH SERVICEABLE BARS L900 AND L908 AT FWD LT CLOSET AND CENTER GALLEY AREA, AND OPS CHECK GOOD.

Part: DISC — DAMAGED (EVAC SLIDE) · airframe 68,942 hrs · 11,263 cycles

LOW BOTTLE. DAMAGE TO BURST DISC CAUSING A SLOW LEAK. R&R BURST DISC.

Part: SWITCH — FAILED (RT FUEL PUMP) · airframe 68,971 hrs · 11,269 cycles

FUEL CONFIG EICAS AND LIGHT. RT TANK 2.6 LOW. DURING BALANCE PROCEDURE THE RT AFT FUEL PUMP EICAS NOT DISPLAYED. NEEDS SWITCH ASSY. REMOVED AND REPLACED AFT PRESSURE SWITCH. OPS CKS NORMAL.

Part: ACTUATOR — FAULTY (RT AILERON) · airframe 68,794 hrs · 11,242 cycles

AILERON LOCKOUT EICAS AND OVERHEAD LIGHT CAME ON AROUND 300 KTS. CREW ADVISED BOTH O/B AILERONS APPEAR TO BE LOCKED OUT IN CRUISE. RT AIL LOCKOUT MODULE FAULT BALL DISPLAYED, RT AIL LOCKOUT ACTUATOR REPLACED.

Part: IDG — INOPERATIVE (NR 1 ENGINE) · airframe 68,764 hrs · 11,237 cycles

L GEN OFF EICAS & L GEN CONT OFF LIGHT ILLUMINATED. COMPLIED WITH MEL - NR 1 ENG GENERATOR DISCONNECTED. GENERATOR HAS UNDER VOLTAGE PER BPCU MSG. SWAPPED GCU'S, NO HELP. REPLACED LEFT IDG. GROUND RAN, OPS CHECK NORMAL.

Part: BLEED VALVE — EXCESS PLAY (NR 1 ENGINE) · airframe 68,696 hrs · 11,227 cycles

NR 1 ENGINE 2.5 BLEED VALVE HAS EXCESSIVE PLY ON THE RIGHT SIDE OF THE RING. ALSO FOUND METAL SHAVINGS IN RING AREA AROUND 3 O`CLOCK POS. REPLACED ESN 724666 WITH ESN 727987 IN POS 01.

Part: STARTER — INOPERATIVE (NR 2 ENGINE) · airframe 68,621 hrs · 11,218 cycles

NR 2 ENGINE NO START. REPLACED STARTER.

Part: ENGINE — HOT START (NR 1) · airframe 68,571 hrs · 11,212 cycles

NR 1 ENG HOT START, MAX EGT 768. (EXCEEDS 535). SEE EICAS ENG EXCD FOR MAX EGT AND DURATION. CREW COMMENTS: NO FUEL INITIATED DURING START. INSPECTED ENGINE INLET AND EXHAUST. RAN ENGINE IN GATE START WAS NORMAL. CREW STATED IT HAD EGT INDICATION ON PUSHBACK BEFORE ATTEMPTING TO START.

Part: IDG — FAULTY (NR 1 ENGINE) · airframe 68,063 hrs · 11,140 cycles

LEFT IDG RISE SHOWS 0 TEMP, RIGHT IDG SHOWS 17. CLEANED AND SECURED L IDG CONNECTORS. INSTALLED NEW GCU WITH NO HELP. REINSTALLED OLD GCU. REPLACED NR 1 ENGINE IDG. IDG OP CHECKS NORMAL.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 67,695 hrs · 11,084 cycles

EMERGENCY EXIT LIGHTING STRIP DISCONNECTED NEAR SEATS 10E. LIGHT STRIP FOUND DISCONNECTED. SECURED LOOSE LIGHT STRIP. OP CHECKS OKAY.

Part: ACTUATOR — LEAKING (NR 2 ENGINE) · airframe 67,673 hrs · 11,081 cycles

NR 2 ENG, TURBINE CASE COOLING ACTUATOR IS LEAKING FUEL AT A RATE OF 30 DROPS PER MINUTE.

Part: FMU — FAULTY (NR 2 ENGINE) · airframe 67,673 hrs · 11,081 cycles

NR 2 ENG, TURBINE CASE COOLING ACTUATOR IS LEAKING FUEL AT A RATE OF 30 DROPS PER MINUTE. FOUND CHUNKS OF RUBBER COVERING 10 PERCENT OF STRAINER. PERHAPS O-RING MATERIAL. NO METAL FOUND. CLEANED AND REINSTALLED STRAINER. COMPLETED INSP OF STRAINER INSTALLATION FOUND SECURE. REPLACED NR 2 ENG FUEL PUMP AND FMU. REPLACED CUT O-RING AT OIL COOLER OUTLET FUEL FLANGE. OP CHECKED AND LEAK CHECKS OKAY. REPLACED FUEL PUMP FILTER P/N 75912-102. ACCMP'D LEAK CHECK. CHECKS GOOD. REPLACED TCC ACTUATOR. REPLACED NR 2 ENG VSV ACTUATOR. LEAK CHECK AND OP CHECKS GOOD. RT ENGINE TURBINE CASE COOLING MANIFOLD AFT SUPPORT STANDOFFS SLIGHTLY WORN. REPLACED MANIFOLD P/N 50T120 AND CLAMPS P/N 53T422-01.

Part: GENERATOR — MALFUNCTIONED (LEFT) · airframe 67,382 hrs · 11,034 cycles

LEFT GEN DID NOT STAY ONLINE AFTER ENG START.

Part: CIRCUIT BREAKER — FAULTY (LT GENERATOR) · airframe 67,382 hrs · 11,034 cycles

LEFT GEN DID NOT STAY ONLINE AFTER ENG START. REPLACED GCU, NO HELP. REPLACED IDG, NO HELP. REPLACED GENERATOR CONTROL BREAKER C901 UP TO IDG PHASE CABLES. SYSTEM TEST GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 67,235 hrs · 11,004 cycles

EEL STRIP LOOSE ON FLOOR BY MID LAV. *S/D* FOUND LOOSE LIGHT ASSEMBLY. SECURED LIGHT ASSEMBLY, OP CHECK GOOD. AC OK FOR SERVICE.

Part: ACTUATOR — FAULTY (LT A/C PACK) · airframe 66,883 hrs · 10,945 cycles

LT PACK TEMP MSG IN CRUISE. *S/D* SUSPECT RAM AIR DOOR ACTUATOR. REPLACED ACTUATOR, OP CHECK GOOD. AC OK FOR SERVICE.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 66,824 hrs · 10,935 cycles

CABIN EEL INOP AFT GALLEY. *S/D* FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (SLIDE) · airframe 66,824 hrs · 10,935 cycles

EXTERIOR EEL LT INOP AFT RT SIDE SLIDE LT. *S/D* FOUND FAULTY LAMP. REPLACED LAMP, OP CHECK GOOD. AC OK FOR SERVICE.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 66,824 hrs · 10,935 cycles

EMERGENCY EXIT LIGHT INOP RT MID LAV. *S/D* FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECK GOOD. AC OK FOR SERVICE.

Part: HEAT EXCHANGER — FAULTY (ENVIRON CONTROLS) · airframe 66,718 hrs · 10,919 cycles

CREW COMMENTS: GOT HOT IN CABIN 74-79-81, HAVE TO OPERATE RT PACK IN STBY C TO HAVE A COMFORTABLE TEMP. *S/D* SUSPECT FAULTY HEAT EXCHANGER. REPLACED LEFT HEAT EXCHANGER IAW MM 21-51-02, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: STRUCTURE — DAMAGED (A/C BAY) · airframe 66,718 hrs · 10,919 cycles

DAMAGE TO LWR CHORD IN LT AC BAY ABOVE PLENUM.

Part: STRUCTURE — DAMAGED (LT A/C BAY) · airframe 66,718 hrs · 10,919 cycles

DAMAGE TO LWR CHORD IN LT AC BAY ABOVE PLENUM. MAJOR REPAIR ACCOMPLISHED. AFTER HEAT TREAT AND CAD PLATING INSTALLED ANGLES, STRAP AND CHORD SECTION. LOWER CHORD REPAIRED PER UA-EVA-71685.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,407 hrs · 10,868 cycles

EMERGENCY ESCAPE LIGHT STRIP IN FRONT OF RT MID LAV IS INOP. FOUND LIGHT ASSEMBLY BROKEN. REPAIRED LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: COVER — UNSECURE (CABIN) · airframe 66,392 hrs · 10,866 cycles

BUSINESS EMERGENCY LIGHTING COMING OUT AGAIN. FOUND LIGHT ASSEMBLY LOOSE RE-ATTACHED EMERGENCY LIGHT STRIP COVER. AC OK FOR SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 66,362 hrs · 10,862 cycles

EMERGENCY LIGHT STRIP IN BUSINESS GALLEY LOOSE. FOUND LIGHT ASSEMBLY LOOSE. SECURED LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 66,327 hrs · 10,857 cycles

EMERGENCY LIGHTS IN FLOOR LOOSE RIGHT SIDE ACROSS FROM BUSINESS GALLEY. FOUND DAMAGED LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY. AC OK FOR SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 66,314 hrs · 10,855 cycles

EMERGENCY FLOOR LIGHTING INOP WHEN ACTUATED FROM CABIN. CARRIED OUT TROUBLESHOOTING PER MM AND ACTIONED OPS TEST OF EMERGENCY ESCAPE PATH LIGHTING EEL SYSTEM PER MM 33-51-00 PAGE 503-504, SATIS. AC RELEASED FOR SERVICE.

Part: ASPIRATOR — DAMAGED (SLIDE)

SLIDE HAS A DAMAGED ASPIRATOR. BARREL IS BENT FROM EXTERNAL PRESSURE OR CONTACT. NO VISIBLE DAMAGE TO SLIDE MATERIAL. REPLACED ASPIRATOR.

Part: BATTERY — FAULTY (MASTER) · airframe 65,901 hrs · 10,792 cycles

MAIN BATTERY CHARGER STATUS MSG. SUSPECT FAULTY BATTERY. REPLACED MAIN BATTERY OP CHECKED GOOD. AC OK FOR SERVICE.

Part: MODULE — BROKEN (LAVATORY) · airframe 65,730 hrs · 10,768 cycles

LAV 124 OXYGEN MASK COMPARTMENT DOOR BROKEN OFF AND MASK FELL DOWN. REPLACED PASSENGER OXYGEN MODULE. AC OK FOR SERVICE

Part: IDG — FAILED (NR 1) · airframe 65,724 hrs · 10,765 cycles

L GENERATOR DRIVE LIGHT ILLUMINATED. LOST LEFT GENERATOR. NR 1 ENGINE IDG DISCONNECTED DUE TO FAULTS. REPLACED IDG AND GEN CONTROL UNIT (PRECAUTIONARY). GENERATING SYSTEM OP CHKD OK FOR SERVICE.

Part: LIGHT — UNSECURE (CABIN) · airframe 65,686 hrs · 10,758 cycles

EMERGENCY LIGHT STRIP COMING UP AT RT SIDE OF BUS GALLEY AT ROWS 10E-F.

Part: IDG — DISCONNECTED (LEFT) · airframe 65,675 hrs · 10,756 cycles

EICAS MSG L GEN DRIVE DISPLAYED. GEN DRIVE LIGHT ILLUM. GEN DRIVE DISCONNECTED.

Part: LIGHT — BROKEN (MID GALLEY) · airframe 65,571 hrs · 10,739 cycles

EEL STRIP BROKEN BY MID GALLEY. REPLACED SPLICES, CRIMPER AND PLASTIC COVER. CHECKED EMERGENCY LIGHT OK.

Part: WIRE — EXPOSED (CABIN) · airframe 65,510 hrs · 10,729 cycles

EMERGENCY LIGHT STRIP ON FLOOR ROW 14B IS PULLED UP W-WIRES SHOWING. REPAIRED LIGHT BAR OPS CHECKED GOOD. AC OK FOR SERVICE.

Part: VALVE — LEAKING (ASPIRATOR)

ASPIRATOR LEAKING. FAULTY VALVE. REPLACED SLIDE AND ASPIRATOR. ACFT OK FOR SERVICE.

Part: WIRE — ARCED (CABIN) · airframe 64,950 hrs · 10,650 cycles

THE 9B READING LIGHT WIRES EXPOSED AND ARCING. REPLACED READING LIGHT OPS CHECK NORMAL. AC OK FOR SERVICE.

Part: ACTUATOR — INTERMITTENT (RUDDER TRIM) · airframe 64,926 hrs · 10,647 cycles

RUDDER TRIM INTERMITTENTLY INOP. SUSPECT FAULTY TRIM ACTUATOR. REPLACED RUDDER TRIM ACTUATOR. OP CHECKS NORMAL. ACFT OK FOR SERVICE.

Part: INDICATOR — MALFUNCTIONED (RUDDER TRIM) · airframe 64,313 hrs · 10,551 cycles

CREW REPORT RUDDER TRIM INDICATOR IS HESITANT WHEN TRIM SELECTED PRIOR TO DEPARTURE.

Part: POWER SUPPLY — INTERMITTENT (EMERGENCY LIGHT) · airframe 64,021 hrs · 10,502 cycles

EEL LIGHTS FLICKER ON AND OFF AT LEFT SIDE OF FIRST CLASS. SUSPECT BAD PWR PACK. PREVIOUS HISTORY. REPLACED BATTERY POWER SUPPLY PACK. TEST FLOOR EEL LIGHTS. OP CHKS GOOD.

Part: STARTER — MAKING METAL (NR 2) · airframe 63,771 hrs · 10,470 cycles

NR 2 ENG STARTER MAG CHIP DETECTOR SHOWS LARGE FLAKES OF METAL. ALSO THE NR 1 ENG STARTER DRAINED AN INSUFFICIENT AMOUNT OF OIL. ALSO BLACK AND BURNED AND HAS AN ODOR. NR 1 STARTER FOUND WITH LOW OIL AND OIL LOOKS BLACK AND BURNED REPLACED STARTER. AFTER SERVICING NR 2 STARTER FOUND WITH LARGE METAL CHIPS. REPLACED NR 2 STARTER. AC OK FOR SERVICE

Part: CONNECTOR — OUT OF ADJUST (EMERGENCY LIGHTS) · airframe 63,665 hrs · 10,456 cycles

EMERGENCY EEL LIGHT TURN ON AND OFF AT SEATS 1AB. ADJUSTED PLUG AT POWER SUPPLY NEXT TO THE SEAT 1AB. CHECKED OK.

Part: BULKHEAD — GOUGED (NR 1 NACELLE) · airframe 63,017 hrs · 10,346 cycles

NR 1 PYLON, GOUGED BULKHEAD FITTING AT NAC STA 237.39. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA. CUT OUT PREVIOUSLY TRIMMED FLANGE FROM BULKHEAD (P/N 311T3281). FABRICATED A REPAIR ANGLE & A REPLACEMENT BRACKET (272T0082-28) & A REPLACEMENT CLIP (313T3310-469).

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 63,017 hrs · 10,346 cycles

LEADING EDGE OF LEFT OUTBOARD ELEVATOR UPPER SURFACE IS CHIPPED ABOVE HINGE AT 240.

Part: SKIN — CORRODED (BS 1554 S24-25L) · airframe 63,017 hrs · 10,346 cycles

EXTERNAL FUSELAGE, STA 1554 BETWEEN STR 24L AND STR 25L, FWD LAV VENT, SKIN AROUND EXHAUST BULGED AND CORRODED. REPAIRED PER REO G12120 REV A AND EVA-70582. STARTING AT 37,500FC MUST ACP A DETAILED VISUAL INSP EXT AND INTERNAL AND A LFEC EXT SKIN AND MUST CONTINUE EVERY 3000FC THERE AFTER PER EVA70582. REPAIR INSTALLED. AIRCRAFT READY FOR SERVICE.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,017 hrs · 10,346 cycles

FLOORBEAM STA 246 VERTICAL STIFFENER CRACKED AT RBL 26 FWD SIDE. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKED STIFFENER. INSTALLED NEW STIFFENER.

Part: FASTENER — IMPROPER PART (FUSELAGE) · airframe 63,017 hrs · 10,346 cycles

REPAIR AT BS 294-303 AT STR 27L FOUND WITH BLIND FASTENERS. REMOVED BLIND FASTENERS AND REPLACED WITH SOLID FASTENERS.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 63,017 hrs · 10,346 cycles

FLOORBEAM INTERCOSTAL ATTACH BRACKET CRACKED AT STA 303, BL 0. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKED ANGLE. FABRICATED & INSTALLED NEW ANGLE.

Part: SKIN — DENTED (FUSELAGE) · airframe 63,017 hrs · 10,346 cycles

EXTERNAL FUSELAGE STA 1197+110 BETWEEN STR 39R AND 38L SKIN DENTED INSIDE OUT. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE. HFEC INSPECTION TO VERIFY DAMAGE REMOVAL. NO CRACKS FOUND. FABRICATED & INSTALLED FILLER AND DOUBLER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,017 hrs · 10,346 cycles

FLOORBEAM STA 246 T-CAP ANGLE CRACKED AT LBL 12, AFT SIDE. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKED SECTION OF CAP ANGLE. FABRICATED & INSTALLED ANGLE REPAIR.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,017 hrs · 10,346 cycles

FLOORBEAM STA 246 VERTICAL STIFFENER CRACKED AT RBL 12 FWD SIDE. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKED STIFFENER. LOCATED, DRILLED & INSTALLED NEW STIFFENER.

Part: CYLINDER — INADEQUATE (EVAC SLIDE) · airframe 63,017 hrs · 10,346 cycles

RIGHT OVERWING SLIDE INFLATION CYLINDER IS INADEQUATE. REPLACED SLIDE INFLATION CYLINDER TO ACCOMPLISH COA 616942. ALSO FOUND COLLAPSED INFLATION HOSE DUE TO HYD FLUID CONTAMINATION. CHECKED OK FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 62,178 hrs · 10,196 cycles

EMERGENCY FLASHLIGHT INOPERATIVE. LOCATION FLIGHT ATTENDANT SEAT 260 MID CABIN. [07-10-07] REPLACED EMERGENCY FLASHLIGHT ASSY. AIRCRAFT OK FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 59,504 hrs · 9,733 cycles

RETURNED TO JFK UNDER DUE TO LEADING EDGE FLAP INDICATION. ALL CHECKS FOUND NORMAL.

Part: ENGINE — LEAKING (NR 2) · airframe 59,501 hrs · 9,731 cycles

DIVERTED TO BOS DUE TO LOST OF OIL IN THE NR 2 ENGINE. FOUND STARTER TO GEARBOX MOUNTING FLANGE CRACKED AND LEAKING. STARTER HAD BEEN REPLACED PRIOR TO FLIGHT. REPLACED NR 2 ENGINE GEARBOX HOUSING ASSEMBLY.

Part: WIRE — DAMAGED (ANTI SKID XDUCER) · airframe 59,199 hrs · 9,686 cycles

EICAS MESSAGE NORM ANTISKID & ALTN ANTI-SKID DISPLAYED. TAKEOFF FOLLOWED BY STATUS MESSAGE :ANTISKID CNTRL SHOWS XDUCR 7 FAULT, REPLACED TRANSDUCER 7. PROBLEM CONTINUED. FOUND WIRE TO PIN 1 IN TRANSDUCER CONNECTOR, D2024, BROKEN IN BACKSHELL CLAMP. REPLACED CONNECTOR D2024. THOROUGHLY CHECKED CIRCUIT FROM ANTISKID AUTOBRAKE CONTROL UNIT TO TRANSDUCER. CHECKED GOOD. EICAS MESSAGES AND TRANSDUCER 7 FAULT CLEARED.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 58,195 hrs · 9,530 cycles

RETURNED TO IAD DUE TO MULTIPLE NAVIGATIONAL DISPLAY PROBLEMS. CAPT & F/O ADI'S WERE LOSING COLOR & BLANKING. DURING IN-FLIGHT TROUBLESHOOT CREW ALSO NOTED CONFIG LIGHT AND GEAR NOT DOWN MESSAGE. AS A RESULT, 4 LRU'S WERE REMOVED:CAPT. ADI, CENTER SG, LANDING CONFIG WARNING CARD AND RAD ALT XCVR. ADI HAD EVIDENCE OF DIRT BUILD-UP, WHICH MAY HAVE CAUSED OVERHEAT CONDITION. SG AND WARNING CARD WERE NFF. RAD ALT XCVR NEEDED 2 CCOA'S & FAILED TX FREQ & SELF TEST. A/C HAS NOT EXPERIENCED SIMILAR PROBLEMS SINCE INCIDENT.

Part: UNKNOWN — UNKNOWN (ELECTRICAL) · airframe 57,544 hrs · 9,420 cycles

DIVERTED TO YYZ WITH ELECTRICAL PROBLEMS. RT GEN TRIPPED OFF ON TAKEOFF DRIVE LIGHT & EICAS ILLUM, DISCONNECTED IDG. OIL WAS FOULD LOW, SERVICED WITH 4 QUARTS OF OIL, NO EXTERNAL LEAKS EVIDENT. RAN ENGINE WITH IDG ON LINE FOR 20 MINS ALL OPS NORMAL. RE-INSPECTED IDG FOR LEAKS AND OIL LEVEL ALL OK.

Part: SLIDE — DEPARTED (LT WING) · airframe 57,448 hrs · 9,404 cycles

LEFT WING SLIDE APPEARS TO HAVE DEPARTED THE AIRCRAFT ON CLIMBOUT.

Part: SKIN — CRACKED (BS 1197 S19L) · airframe 57,448 hrs · 9,404 cycles

AFT LT FUSELAGE SKIN DENTED & CRACKED AT STA 1197 + 84 AND STRINGER S-19L.

Part: GENERATOR — UNKNOWN (NR 2) · airframe 57,302 hrs · 9,377 cycles

RETURNED TO IAD DUE TO NR 2 GENERATOR PROBLEM. AFTER EVENT, INITIAL IDG SERVICE AND ENGINE RUN PRODUCED NO FAULTS OR LEAKAGE, AND MONITORING AC REVEALED NO DUPLICATE EVENTS. INDICATION OF LOW OIL PRESSURE FROM INTERNAL CHARGE PRESSURE SWITCH CLOSURE MOST LIKELY DUE TO UNIT'S LOW OIL QUANTITY.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 55,306 hrs · 9,082 cycles

CAPTAINS WINDSHIELD CRACKED. FLIGHT DIVERTED TO LHR.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,339 hrs · 8,606 cycles

FLOORBEAM STA 246 STIFFENER AT APPROX RBL 20 IS CRACKED. CRACK CAUSED BY CYCLIC DEFLECTION FATIGUE. FABRICATED & INSTALLED NEW STIFFENER.

Part: HINGE FITTING — CRACKED (LT WING) · airframe 52,339 hrs · 8,606 cycles

LT WING IB FLAP OB HINGE FITTING CRACKED AFT VANE. SUPPLEMENTAL DATA UPDATE REPAIRED FITTING WITH ANGLE AND FILLER REPAIR.

Part: FLOORBEAM — CRACKED (FUSLEAGE) · airframe 52,339 hrs · 8,606 cycles

FLOORBEAM STA 246 STIFFENER AT RBL 15 IS CRACKED. CRACKS CAUSED BY CYCLIC DEFLECTION FATIGUE. FABRICATED AND INSTALLED NEW BRACKET.

Part: SKIN — PUNCTURED (CARGO DOOR) · airframe 45,934 hrs · 7,503 cycles

FOUND 3/8 INCH HOLE IN BULK CARGO PIT DOOR 25 INCHES FROM TOP OF DOOR AND 1-3/4 INCHES FROM AFT SIDE OF DOOR. DOUBLER INSTALLED.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 45,934 hrs · 7,517 cycles

TEMPORARY DOUBLER OVER THE 3 INCH X 4 INCH HOLE IN ACFT FUSELAGE, 1 FOOT AFT OF AFT MAIN CARGO AREA LOADING LIGHT, ON RIGHT SIDE OF ACFT. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPLACED.

Part: HEATER — FAILED (PITOT TUBE) · airframe 44,460 hrs · 7,270 cycles

CAPTAIN'S PITOT TUBE, RUDDER RATIO AND AILERON LIGHT CAME ON. CAPTAIN'S AIRSPEED INDICATOR NON OP, ALTIMETER VARIED PLUS 100, MINUS 200 FT AT FL330 WITH AUTOPILOT ENGAGED. ON DESCENT SYSTEMS RETURNED TO NORMAL. FLIGHT DIVERTED TO LAS. SUPPLEMENTAL DATA UPDATE AFTER A "CAPT PITOT TUBE" LIGHT CAME ON WITH THE CAPTAIN'S AIRSPEED IND INOP, ALTITUDE VARIED PLUS 100 MINUS 200 FT AT FL 330 AND C A-P ENGAGED, FOUND AN ICING ON CAPTAIN'S PITOT PROBE. CAUSED BY A DEFECTIVE HEATER ELEMENT. LOSS OF CAPTAIN'S PITOT INPUT TO THE LT AIR DATA COMPUTER CAUSED THE CAPTAIN'S PITOT, RUDDER RATIO, AND AILERON LIGHT TO DISPLAY ON EICAS. REPLACED CAPTAIN'S PITOT TUBE TO CORRECT HEATING ELEMENT AND LIGHTS.

Part: PUMP — FAULTY (FUEL SYSTEM) · airframe 43,074 hrs · 7,024 cycles

INDICATION OF A LEFT CENTER BOOST PUMP FAILURE WITH POSSIBLE FUEL IMBALANCE. THE LEFT CENTER FUEL TANK OVERRIDE PUMP WAS REPLACED AND OPS CHECKED OK. SYSTEM OPERATION NORMAL THROUGH 8/25/2002. SHOP TEST OF THE REMOVED PUMP WAS PERFORMED WITH NO DEFECTS NOTED. 8/26/02 THE LT OVERRIDE PUMP AGAIN EXHIBITED THE SAME SYMPTOM. THE PUMP WAS REMOVED AND A PUMP WITH MACHINED DIFFUSER WAS INSTALLED AND SYSTEM OPERATION HAS BEEN NORMAL TO DATE.

Part: PANEL — MISSING (VERTICAL STAB) · airframe 41,544 hrs · 6,723 cycles

ON ARRIVAL FOUND DORSAL FIN PANEL MISSING. THE DORSAL FIN PANEL WAS REPLACED. THE FUSELAGE SKIN IN THE AREA OF THE DORSAL FIN WAS VISUALLY AND HFEC INSPECTED TO ENSURE THAT NO DAMAGE TO THE FUSELAGE SKIN OCCURRED.

Part: FRAME — GOUGED (FUSELAGE) · airframe 41,085 hrs · 6,641 cycles

FORWARD PIT STATION 654+66 FRAME GOUGED OUT OF LIMITS AT STRINGER 32L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME.

Part: FRAME — GOUGED (FUSELAGE) · airframe 41,085 hrs · 6,641 cycles

FORWARD PIT STATION 654+121 FRAME GOUGED OUT OF LIMITS AT STRINGER 31L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME.

Part: FRAME — GOUGED (FUSELAGE) · airframe 41,085 hrs · 6,641 cycles

FORWARD PIT STATION 654+110, FRAME GOUGED OUT OF LIMITS AT STRINGER 31L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME.

Part: FRAME — GOUGED (FUSELAGE) · airframe 41,085 hrs · 6,641 cycles

FORWARD PIT STATION 654+88, FRAME GOUGED OUT OF LIMITS AT STRINGER 31L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,085 hrs · 6,641 cycles

FUSELAGE LOWER SKIN CRACKED AT RIGHT HAND LOWER FORWARD STAB CUTOUT STATION 1740, STRINGER 19R. MAJOR REPAIR ACCOMPLISHED. REPAIRED SKIN.

Part: SKIN — GOUGED (FUSELAGE) · airframe 41,085 hrs · 6,641 cycles

FUSELAGE SKIN GOUGED OUT OF LIMITS AT LEFT HAND LOWER FORWARD STAB CUTOUT AT STATION 1735, STRINGER 19R. MAJOR REPAIR ACCOMPLISHED. REPAIRED SKIN.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,085 hrs · 6,641 cycles

FUSELAGE SKIN CRACKED AT RIGHT HAND LOWER STAB CUTOUT STATION 1735 AT STRINGER 19R. MAJOR REPAIR ACCOMPLISHED. SKIN CRACKED.

Part: STRINGER — MISDRILLED · airframe 41,085 hrs · 6,641 cycles

FORWARD CARGO PIT STATION 654+88, INBD UPPER LEG OF STRINGER 31L HAS DOUBLE DRILLED HOLE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPAIRED DAMAGE STRINGER SECTION.

Part: SKIN — GOUGED (FUSELAGE) · airframe 41,085 hrs · 6,641 cycles

FUSELAGE LOWER SKIN GOUGED OUT OF LIMITS AT LEFT HAND STAB CUTOUT AT STATION 1740, STRINGER 19R. MAJOR REPAIR ACCOMPLISHED. REPAIRED SKIN.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,085 hrs · 6,641 cycles

CABIN FLOORBEAM CORRODED AT BODY STATION 852, LBL 53. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,085 hrs · 6,641 cycles

BODY STATION 266.5 BL 72 FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SECTION AND SPLICES.

Part: FLANGE — CORRODED · airframe 41,085 hrs · 6,641 cycles

BODY STATION 287 STRINGER 20R RBL 88.5 FLOORBEAM FLANGE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM FLANGE AND SPLICES.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 41,085 hrs · 6,641 cycles

BODY STATION 266.5-286.5 RBL 86 DOOR CHORD CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED CHORD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,085 hrs · 6,641 cycles

MAJOR BS 344-348 STRINGER 20R RBL 82-83 FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 41,085 hrs · 6,641 cycles

MAJOR BS 790 STRINGER 39 RBL 9 KEEL BEAM FASTENER HOLE IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED RETAINER.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 41,085 hrs · 6,641 cycles

MAJOR BS 246 RBL 70-72 WL 199.5 ANGLE ATTACHING TO BULKHEAD IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED CHORD AND SPLICE ANGLES.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,085 hrs · 6,641 cycles

MAJOR BS 1197+88 LBL 40-45 T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW T-CAP.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 41,085 hrs · 6,641 cycles

MAJOR BS 794.5 STRINGER 39 RBL 9 LOWER KEELBEAM FASTENER HOLE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED RETAINER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,085 hrs · 6,641 cycles

BODY STATION 1197+110 LBL 40-45 T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,085 hrs · 6,641 cycles

BODY STATION 1197+88 LBL 40-45 T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP.

Part: SKIN — CORRODED (FUSELAGE) · airframe 41,085 hrs · 6,641 cycles

CORROSION ON SKIN BASE DISTANCE MEASURING EQUIPMENT ANTENNA M763. MAJOR REPAIR ACCOMPLISHED INSTALLED REPAIR DOUBLER AT BODY STATION 548, BL 0.

Part: WASHER (DPLOY BAR) · airframe 39,279 hrs · 6,332 cycles

DURING EMERGENCY EVACUATION DOOR 2L FAILED TO FULLY OPEN. SUPPLEMENTAL DATA UPDATE FOUND SNAP RING AND WASHER (CMM 25-66-30-1003 ITEM 65 & 70 RESPECTIVELY) MISSING ON AFT SEPARATOR LINK ASSY (CMM 25-66-30-1003 ITEM 80)REPLACED PARTS AS NECESSARY; REINSTALLED ASSEMBLY AND PERFORMED ESCAPE SLIDE DEPLOYMENT SIMULATION WITH NO DEFECTS NOTED.RING MFG P/N MS16624-4031

Part: COMPRESSOR — FAILED (NR 1 ENGINE) · airframe 39,279 hrs · 6,332 cycles

TAKEOFF ROLL LOUD NOISE ABOUT 30-50 KNOTS & LOSS OF THRUST NR 1 ENGINE. RTO. AFTER CLEARING RUNWAY TOWER ADVISED SMOKE AROUND LEFT SIDE OF PLANE AND FA'S REPORTED SMOKE IN REAR OF CABIN. BLEW EXTINGUISHERS ON BOTH ENGINES AND APU AFTER SHUTDOWN. EMERGENCY EVACUATION OF AIRCRAFT THROUGH DRS 1L,1R & 2L. ONE EACH 5TH STAGE HPC VANE ARM DISCONNECTED FROM UPPER RING. ONE 6TH STAGE BLADE FAILED IN THE DOVETAIL AREA AND NUMEROUS OTHERS WERE CRACKED AS A RESULT OF THE VANE ARM FAILURE. ALL COMPRESSOR STAGES AFT OF THE 6TH STAGE WERE SEVERELY DAMAGED. INDICATIONS OF RESIDUAL FUEL FIRE IN THE TAILPIPE AREA.

Part: VIDEO UNIT — ODOR (ROWS 6 - 8) · airframe 35,023 hrs · 5,581 cycles

ON FINAL DESCENT, FLT ATT REPORTED ELECTRICAL SMELLORIGINATING FROM ROWS 6, 7 & 8 SEATS E & F. *S/D* REPLACED VIDEO DISPLAY UNITS (VDU) AT SEATS 7 E & F, REPLACED VIDEO DISPLAY BOX (VDB) AND SEAT CABLE AT SEAT 7E. SHOP FOUND VDB POWER SUPPLY BAD, C6 AND C7 CAPACITORS LEAKING. 10/30/00

Part: SWITCH — FAILED (COCKPIT) · airframe 35,397 hrs · 5,648 cycles

FAINT ELECTRICAL BURNING SMELL IN FLT DECK ONLY. TURNED OFFRECIRC FANS AND SMELL DIMINISHED. NO CB''S POPPED. UPDATE: FAINT ELEC SMELL NOW DETECTED BY F/A IN MID AND 1ST CLASS, RECIRC OFF AND EQUIP COOLING TO OVERRIDE AND CABIN ALT TO 9500 FT. O2 MASKS WERE USED IN THE FLIGHT DECK BECAUSE OF THE BURNING SMELL. *S/D* REPLACED KORRY LED SWITCH ASSY FOR ''SYS PRESSURE'' IN HYDRAULICS PANEL, ON P5 OVHD PANEL. INSPECTED ALL FLT DECK CB AND INSTRUMENT PANELS AND E&E COMPT PANELS FOR EVIDENCE OF ELECTRICAL OVERHEATING. SMELL SEEMS TO BE FROM P5 OVHD HYD PANEL CENTER SYSTEM ''SYS PRESSURE'' LED. REPLACED KORRY LED SWITCH ASSY FOR ''SYS PRESSURE'' IN HYDRAULICS PANEL. SWITCH ASSY SENT TO KORRY FOR EVALUATI

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 34,997 hrs · 5,576 cycles

EMERGENCY EXIT FLOOR LIGHTING STRIP ROWS 15-20 ON STEADY. EXIT LIGHTS UNDER WINDOW 15 FLICKERING RT SIDE ROW 19FG. RPL BATTERY-PWR SPL P/N 563-1188. RPL BATTERYPACK P/N 585-4495. RPL CHARGER P/N 563-1046. EEL LIGHTS CHECKED OK ONGROUND.

Part: VALVE — LEAKING (FUEL SYSTEM) · airframe 34,147 hrs · 5,416 cycles

FOUND UNWANTED FUEL XFER FROM LT TO CENTER TANK AT A RATE OF 100 LBS IN 3 MINUTES WITH LT FUEL LEVEL INDICATING 30,000 LBS. FOUND FUEL ENTERING CENTER TANK THRU FILL MANIFOLD DRAIN VALVE. SUSPECT O/B FILL VALVE ACCOUNT OF XFER CEASES WHEN LEVEL IS DROPPED TO 10,000 LBS. CONDITION WAS BOOST PUMPS OFF, DEFUEL VALVES CLOSED, FILL VALVES CLOSED, AND XFEED CLOSED. *S/D* TRANSFER WAS FOUND TO BE RESULT OF LEAKS FROM MAIN TANKS TO CENTER TANK AT LEFT AND RIGHT RIB 3 AND THE LEFT OUTBOARD FILL VALVE WAS FAILING TO FULLY CLOSE. THE LEAKS WERE SEALED AND THE FILL VALVE (PN40884-4) REPLACED. THERE HAS BEEN NO FURTHER FUEL TRANSFER.

Part: BATTERY PACK — DISCHARGED (ROW 20) · airframe 33,084 hrs · 5,230 cycles

EEL LIGHTS IN COACH TO ROW 20 FLASHES ON-OFF. REPLACE BATTERY PACK PER MM 33-51-07. OP CHECKS NORMAL.

Part: ACTUATOR — FAILED (RUDDER TRIM)

RUDDER TRIM INOP. DIVERTED TO ORD. C/B RESET, NO HELP. *S/D* THE INOP CONDITION OF THE RUDDER TRIM SYSTEM WAS DUE TO AN INTERMITTENT INTERNAL FAULT OF THE OF THE RUDDER TRIM ACTUATOR. THE SUBJECT ACTUATOR WAS REPLACED PER MM 27-21-11 AND ALL OPS CHECKS ARE NORMAL.

Part: COMPRESSOR — DETERIORATED (NR 2 ENGINE)

NR 2 ENGINE, MULTIPLE STALLS AT TAKEOFF. DIVERTED TO LHR. *S/D* ENGINE EXPERIENCED A GROUPE 3 SURGE EVENT. GROUPE 3 SURGES ARE THE RESULT OF EXCESSIVE BLADE TIP CLEARANCES IN THE REAR STAGES OF THE HIGH PRESSURE COMPRESSOR. ENGINE WAS REMOVED FOR HIGH PRESSURE COMPRESSOR REFURBISHMENT.

Part: RETRACT MECH — MALFUNCTIONED (LT MLG)

LEFT MAIN LANDING GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO SFO.

Part: ACTUATOR — LEAKING (RT MLG TRUCK)

CENTER HYD QUANTITY DROPPED TO .44. WITH PUMPS OFF, QUANTITY DROPPING SLOWLY. DIVERTETED TO GRU. FOUND RT MLG TRUCK POSITION ACTUATOR LEAKING. REPLACED ACTUATOR AND FILLED CTR SYSTEM.

Part: BPCU — MALFUNCTIONED (FLIGHT DECK)

FLIGHT DECK EXPERIENCED A MOMENTARY ELECTRICAL POWER FAILURE. AUTO-PILOT DROPPED-OFF, POWER SELF RESTORED WITH NO EICAS MESSAGES. PASSENGER CABIN EXPERIENCED NO ELECTRICAL POWER LOSS. *S/D* BUS POWER CONTROL UNIT WAS REPLACED. NO FURTHER DISCREPANCY HAS OCCURRED.

Part: START SYST — MALFUNCTIONED (APU)

UNABLE TO START APU AT ARRIVAL. *S/D* RAN APU, OPERATIONS CHECK NORMAL. AN OIL QUANTITY INDICATION SYSTEM FALSE MESSAGE IS SOMETIMES REPORTED AND IS SUSPECT IN THIS DISCREPANCY. THIS CAN RESULT FROM SERVICING THE APU OIL WHEN IT IS RUNNING. NO OTHER INCIDENCES HAVE OCCURRED.

Part: PRSOV — DIRTY FILTER (RT ENGINE)

AIRCRAFT RETURNED TO BLOCKS DUE TO RIGHT ENGINE PRSOV FAILURE. REPLACED PRSOV, THE FILTER ASSEMBLY WAS CLOGGED.

Part: EEL BATTERY — DISCHARGED (CABIN)

EMERGENCY ESCAPE PATH LIGHTING INOP ON THE LEFT SIDE IN FIRST CLASS. REPLACED BATTERY PACK, CHECKS OK.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS RT SIDE NR 5, 6 AND 7 ARE OUT. REPLACED BATTERY PACK, OPS CHECK NORMAL.