N646UA

Part: IDG — LOW (NR 2) · airframe 117,267 hrs · 18,200 cycles

R GEN DRIVE LT AND EICAS INTEROGATED GCU, FOUND "LOW OIL" MSG. RESET GCU. INSPECTED ENG2 TOPPED OFF 1 & 2IDG''S AFTER ENGINE RUN. IDG, DELTA ''P'' NORMAL, NO BURNT SMELL, SERVICED #2 IDG FOUND LOW PULLED RESET RING ON IDG. RESET FIELD SWITCH, SAFTIED DISCONNECT BUTTON COVER. ACP''D #2 ENG RUN, ALL INDICATIONS NORMAL VOLTS & FREQ''S. NO LEAKS NOTED FROM IDG. MM12-13-03-213-007

Part: CONTROL MODULE — FAILED (SPOILERS) · airframe 116,778 hrs · 18,104 cycles

ON DESCENT AFTER SPEED BRAKE RETRACTION LEFT SPOILERS STAYED UP AND REMAINED TILL AFTER LDG DURING CREW DEBRIEF CAPTAIN REPORTS UPON INTIAL DEPLOYMENT OF SPOILERS OPS WERE NORMAL. UPON STOWING SPOILERS LEFT BANK OF SPOILERS STAYED DEPLOYED,RIGHT WING SPOILERS STOWED. CAPTAIN ROLLING. SEE PART 2/2..... SAID HE INPUTED AROUND 45 DEGREES OF YOKE TO PREVENT PLANE FROM DOWN #2 ENGINE AND THE FIRE DEPARTMENT REPORTED LEFT SPOILERS CAME DOWN LEFT WING SPOILERS STAYED UP. AS CREW WAS TAXING IN, CREW SHUT RIGHT WING SPOILERS DID NOT COME UP. STOWED SPOILERS AGAIN AND 2/2. CAPTAIN THEN REDEPLOYED SPOILERS FOR TROUBLESHOOTING AND SDR FLAGGED BITE OF 1L SCM SHOWS FAULT "AMBER DUE TO HYD". RPL L1 SCM REF MM27-09-00-422-008. ACCOMPLISHED INITIAL SYSTEM TEST REF MM27-09-00-742-064 STEP F (1) -(17). CHECKS GOOD. REQUIRE STEP F ROTABLE PARTS CHANGE WAS INDICATED - TT # 1461642 SN OFF 6107 IPC REFERENCE # 27-09-01 (18) TO COMPLETION. PCA XDCR 1 OR 12. M306 IS SPOILER #1 PCA. BITE OF 1R SCM SHOWS FAULT 27-61-13, M306 OR SCM FUSE LIGHT AND REMOVED SPOILER #1 PCA IAW AMM 27-61-02-024-001. PART NUMBER VERIFIED AND CLEARANCE TO INSTALL ACCOMPLISHED ORDIQ U118014 WELL REF AMM 27-09-00-201. THANKS! ORD-TECH SUPPORT UPON ENGINEERING REVIEW OF QAR DATA, PLEASE REPLACE 1R SCM AS REPLACED 1R SCM REF AMM 27-09-00-422. OPS CHECKS (MM 27-09-00-742) REQUIRED AFTER SPOILER PCA REPLACEMENT IS COMPLETED. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1033387 SN OFF 5825 MODULE, CONTROL OFF 99-2761-9-0004 5825

Part: BRACKET — BROKEN (AIR DUCT) · airframe 115,911 hrs · 17,937 cycles

REF AIR RETURN FOR PRESSURIZATION: FOUND GROUND CONDITIONED AIR DUCT SEPARATED AT CLAMP WHERE GROUND AIR ATTACHES TO MAIN DISTRIBUTION DUCT. REF IPC 21-51-01-01 ITEM 335, 345. LABOR UPDATE ALSO FOUND CONDITIONED AIR CONNECTION BRACKET BROKEN, NGS DUCT 47-15-01-01 ITEM 120. SEE ATTACHED PICS. BROKEN REF IPC 47-11-06-01 ITEM 210 AND NGS DUCT DAMAGED REF IPC BROKEN REF IPC 47-11-06-01 ITEM 210 AND NGS DUCT DAMAGED REF IPC 47-15-01-01 ITEM 120. SEE ATTACHED PICS. ALSO FOUND CONDITIONED AIR CONNECTION BRACKET BROKEN, NGS DUCT REMOVED CONDITIONED AIR ADAPTER AND DUCT, REF IPC 21-51-01-01 ITEMS 434 AND 484. ALSO REMOVED NGS DUCT REF IPC 47-11-06-01 ITEM 210. REPLACED DAMAGED DUCT IPC REF 47-15-01-01 ITEM 120. DRILLED OUT DAMAGED BRACKET FOR CONDITIONED AIR ADAPTER. DAMAGED BRACKET REPLACED ON LOGPAGE 6441931 REF ECRA 2150-01569

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 115,911 hrs · 17,937 cycles

CABIN AUTO ONE PRESSURA TION CONTROLLER FAILURE RESULTING IN CAB IN HIGH ALT WARNING AUTO PRESSURE CONTROL 2 STATUS MESSAGE. CONTROLER FAILS BIT TEST. REMOVED AND REPLACED CABIN AUTO PRESS CONTROLER PER TASK 21-31-02-004-001 AND TASK 21-31-02-404-005. STATUS MESSAGE CLEARED. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1059185 SN OFF 0332 CONTROLLER, CAB OFF 19-2131-9-0004 0332 ON 19-2131-9-0004 0119

Part: WARNING MESSAGE — ILLUMINATED (RUDDER RATIO) · airframe 115,872 hrs · 17,928 cycles

RUDDER RATIO EICAS MESSAGE ON DURING CLIMB REPLACED RH RUDDER RATIO MODULE REF AMM 27-09-00, CLEARED EICAS MSG. APPLY PLA 02700 TO ECS MAINTENACE MESSAGE. MAINT MSG FOR RUDDER RATIO, PLA 02700 APPLIED IPC REFERENCE 27-09-01 APPLIED PLA TO ECS RUDDER RATIO MAINTENACE MSG. FURTHER DETAILS AWAITED.FOR CABIN ALT WARNING, AS PER LP 6378758, REPLACED BOTH PRESSURE CONTROLLERS PRECAUTIONARY REF. OPS GOOD. FOUND FLAPPER DOOR ON AC CART SERVICE TUBE HINGE BROKEN. REPLACED DUCT ASSY REF IPC. OPS AND LEAK CHECKED GOOD. CABIN PRESSURIZATION CHECK GOOD

Part: BOTTLE — EMPTY (EVAC SLIDE) · airframe 115,648 hrs · 17,887 cycles

RIGHT AFT DOOR MOUNTED EMERGENCY ESCAPE SLIDE BOTTLE READS EMPTY. REMOVED AND REPLACED RIGHT AFT ENTRY DOOR MOUNTED ESCAPE SLIDE IAW AMM 25-66-01. OPERATIONS CHECK GOOD ADD ROTABLE PARTS CHANGE WAS INDICATED - TT 1156468 SN OFF 2662 SLIDE, RAFT AY, OFF 76-2561-9-0001 2662 ON 76-2561-9-0001 1365 COMPLIED WITH RII REQUIREMENTS FOR RIGHT AFT ENTRY DOOR REPLACEMENT IAW AMM 25-66-01 AND GMM 09-25-05. LOG PAGE REQUIRED CHANGING SDR STATUS TO YES. UNABLE TO UPDATE

Part: ANTI-SKID VALVE — FAULTY (MLG) · airframe 115,537 hrs · 17,870 cycles

REF L/P 4853443 DURING ALTN ANTISKID MEL DDP NOTED "MANUAL BRAKING CAPABILITY ON THE ALTERNATE BRAKE SYSTEM NOT AVAILABLE". ALTERNATE BRAKE SELECTOR VALVE SUSPECT INTERNAL FAULT, CENTER HYD SYSTEM DOES NOT APPLY BRAKES NEITHER KEEP ACCUMULATOR PRESSURIZED. R/R ALTERNATE BRAKE SELETOR VALVE AND PRESSURE SWITCH REF AMM 32-41-04-401, NO HELP, TS NEEDS TO BE CONTINUE ROTABLE PARTS CHANGE WAS INDICATED - TT # 1264168 SN OFF 9478 IPC REFERENCE # 32-41-01 NOTICED PRESS LINES GOING TO LH ALTN ANTISKID VLV MODEULE HEATING AND MAKING NOISE (INTERNAL LEAK). SWAPED LH AND RH ALTN A/S VLV MODULES AND PROBLEM FOLLOWED THE LH MODULE. MODULES NEED TO RETURNED TO THE ORIGINAL POSITION AND THE LH NEEDS REPLACEMENT. ALTN ANTISKID VLV MODULES SWAPED AS PER AMM 32-42-02-401 SWAPPED ALTN A/S VALVES AGAIN FOR THE ORIGINAL/INICIAL POSITION, BAD MODULE SUSPECTED IS ON LH SIDE. R/R LH ALTN A/S MODULE AS PER AMM 32-42-02, LEAK CHECK GOOD. PROBLEM PERSISTS. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1231871 SN OFF 3445 IPC REFERENCE # VALVE, ANTI-SKI OFF 99-3242-9-0004 3445 ON 99-3242-9-0004 3913 R/R A SECOND ALTN BRAKE SELECTOR VALVE AS PER AMM 32-41-04 DUE TO SUSPECT OF BAD FIRST VALVE RECEIVED FROM STORES. LEAK CHECK GOOD. NOW ALL BRAKES OPERATING NORMALLY WITH ONLY THE CTR HYD SYSTEM PRESSURIZED. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1231871 SN OFF 1918 IPC REFERENCE # 32

Part: ACCESS DOOR — MISSING (NR 1 PYLON) · airframe 115,356 hrs · 17,839 cycles

PDA 2 STRUT ACCESS DOOR 436AR DISCOVERED TO BE MISSING FROM NO1 PYLON INBOARD POSITION. REF L/P 4626150 PLACED ON CDL DISPATCH DESK: 62 DATE: 27-FEB-20- RT PYLON PNL 436AR MISSING CDL COMPLIANT ITEM DISCOVERED PART NUMBER 311T3065-16, PAINTED, STENCILED AND INSTALLED.

Part: ACCESS DOOR — MISSING (NR 2 PYLON) · airframe 112,319 hrs · 17,443 cycles

PDA 2 ENG #2 PYLON ACCESS DOOR 446BL MISSING ON ARRIVAL. IPC REF 54-53-01-01, ITEM 525. NIL STOCK. COMPLIED WITH CDL REQUIREMENTS. DISPATCH DESK: 63 DATE: 29-MAY-19- APPROVED CDL 54D CDL APPROVED BY TOMC. PDA PROCEDURES ARE FOLLOWED.

Part: TANK — LEAKING (POTABLE WATER) · airframe 110,378 hrs · 17,182 cycles

FLIGHT CREW REPORTS NO WATER ON ACFT. INDICATORS SHOW ZERO AND NO LAVS OR GALLEYS HAVE WATER. SIGNIFICANT RUNNING LEAK FOUND FROM AFT BELLY DRAIN WITH STANDING ICE IN AFT PIT BELLY. BEGAN VACUUMING STANDING WATER IN BILGE AREA FROM STA 1087-1263 AFT PIT FORWARD WALL TO FORWARD FRAME OF RT SIDE DOOR. OPS NORMAL TANK REPLACED

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 107,328 hrs · 16,788 cycles

NR 2 PYLON PANEL 442AL CUTOUT SKIN, FOUND CRACKED. THE SKIN WAS REPAIRED IAW ECRA 5430-02152.

Part: SPAR WEB — CRACKED (NR 2 PYLON) · airframe 107,328 hrs · 16,788 cycles

NR 2 PYLON STATION 174, FWD UPPER SPAR WEB FOUND TWO CRACKS AT HYD CUTOUT POSITION. REPAIRED IAW ECRA 5450-02486.

Part: SKIN — SCRATCHED (BS 1582-1625) · airframe 107,328 hrs · 16,788 cycles

VERTICAL STAB TO BODY SKIN FOUND SCRATCHED AT BS 1582 - 1625 STRINGER 2L. REPAIRED IAW ECFA 5330 -06344.

Part: SKIN — SCRATCHED (BS 1582-1625) · airframe 107,328 hrs · 16,788 cycles

VERTICAL STAB TO BODY SKIN FOUND SCRATCHED AT BS 1582 - 1625, STRINGER 2R. BODY SKIN SCRATCH AT RH STA 1582-1625 S2R REPAIRED PER ECRA 5330 -06344 RII INSPECTION APPROVED

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 107,328 hrs · 16,788 cycles

CABIN STA 785-790 L11 SEAT TRACK FOUND CRACKED. CABIN STA 782-841 LBL11 SEAT TRACK ATTACH FLOORBEAM REPAIRED AS PER SRM 53-00-51 FIG 201 REPAIR 3 REV 106.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 107,328 hrs · 16,788 cycles

CABIN STA 1518 LBL 0-2 FLOORBEAM UPR CHORD FOUND CORROSION. CABIN FLOOR BEAM AT STA 1518 LBL 35 - RBL 35 REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 REV 106.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 107,328 hrs · 16,788 cycles

CABIN STA 1461 LBL 12 FLOORBEAM FOUND CORRODED AS MARKED. CABIN FLOORBEAM AT STA 1461 LBL 40 -RBL 57 REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 REV 106 AND EC/RA 2500-06804 REV-.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 103,772 hrs · 16,267 cycles

EMERGENCY EXIT EEL SIGNS VERY DIM AT RIGHT OVERWING EMERGENCY EXIT DOORS, LOWER GREEN EXIT SIGNS, AND MID RIGHT LAV FLOOR EEL VERY DIM. SLAVED IN NEW BATTERY PACK. LIGHT TEST GOOD. BATTERY PACK NEED SECURED IN AIRCRAFT REF AMM 33-51-07.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 103,409 hrs · 16,215 cycles

EMERGENCY EXIT SIGN INOPERATIVE IN THE FLIGHT DECK. REPLACED THE SIGN IAW MM 33-51-01. OPS. CHECKED NORMAL.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 102,718 hrs · 16,109 cycles

IN BULK CARGO COMPARTMENT A FRAME 1562 BL0 DRAIN HOLE IS CORRODED. REMOVED UNSERVICEABLE BULK CARGO COMP FRAME 1562 SHEAR-TIE STR 38L-38R AND INSTALLED NEW SHEAR-TIE IAW SRM 51-40-02 PARA 7 AND DRWG 146T1223 REV F. DRAIN HOLE ON SHEAR-TIE BL0 AT FS 1562 FOUND TO BE OUT OF LIMITS- 100% MATERIAL LOSS DOT REMOVED PER 76-5312-1-2607 ON MCN LOG PAGE 9234596.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 102,718 hrs · 16,109 cycles

CORROSION ON MAIN CABIN FLOORBEAM BS 287 RBL 44-54 I-BEAM UPPER REPAIR ANGLE, UPPER AND LWR SIDES. REPAIRED MAIN CABIN FLOORBEAM AT BS 387 IAW ECRA 5310- 00973. ACCOMPLISH INSPECTION REQUIREMENTS OF THE NOTED REPAIR PER PART 2 OF ECRA 5310-06473 ON OR BEFORE THE AIRCRAFT REACHES 27,900 TOTAL A/C FLIGHT CYCLES.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 102,718 hrs · 16,109 cycles

IN BULK CARGO COMPARTMENT A FRAME 1562 BL0 DRAIN HOLE IS CORRODED. REMOVED UNSERVICEABLE BULK CARGO COMP FRAME 1562 SHEAR-TIE STR 38L-38R AND INSTALLED NEW SHEAR-TIE IAW SRM 51-40-02 PARA 7 AND DWG 146T1223 REV F. DRAIN HOLE ON SHEAR-TIE BL0 AT FS 1562 FOUND TO BE OUT OF LIMITS- 100% MATERIAL LOSS DOT REMOVED PER 76-5312-1-2607.

Part: ANGLE — CORRODED (BS 1260-1264) · airframe 102,718 hrs · 16,109 cycles

AFT CARGO BAY LOWER ANGLE HAS CORROSION AT BS 1260-1264 RBL 40. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02 PAR 4,7,9 FIG 3,4,8,12,16.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 102,718 hrs · 16,109 cycles

CORROSION ON AFT CARGO FLOORBEAM T CAP UPPER SURFACE AT STA 1153 LBL 10,13,15,18. REMOVED AND REPLACED WITH NEW AFT CARGO T CAP STA 1153 LBL 10,13 ,15 AND 18 IAW SRM 51-40-02 PAR 4, SRM 51-40-05 FIG 2.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 102,718 hrs · 16,109 cycles

FWD CARGO, CORROSION ON SUPPORT ANGLE LOWER SURFACE AROUND FASTENER HOLES BS 512 RBL-39.

Part: FLOORBEAM — CORRODED (BS 1197) · airframe 102,718 hrs · 16,109 cycles

CORROSION ON AFT CARGO FLOORBEAM TEE CAP AROUND THE NUT PLATE BS 1197+44 RBL 46 REMOVED AND REPLACED THE TEE CAP IAW SRM 51-40-02 PAR 4 FIGS 3+8 AND PAR 7D FIG 12.

Part: SHEAR TIE — CORRODED (BS 1540) · airframe 102,718 hrs · 16,109 cycles

IN AFT BULK CARGO COMPARTMENT AT FRAME BS 1540 AT SHEAR TIE BTWN STRINGER L38 AND L39 IS CORROSION REMOVED UNSERVICABLE SHEAR-TIE AND INSTALLED NEW SHEAR-TIE IAW SRM 51-40-02 PAR 4.

Part: TEE FITTING — CORRODED (BS 566) · airframe 102,718 hrs · 16,109 cycles

FWD CARGO, CORROSION ON TEE ANGLE LOWER SURFACE AROUND FASTENER HOLES BS 566 RBL 40. FOUND TO HAVE 100% MATERIAL LOSS. REMOVED AND REPLACED THE TEE ANGLE IAW SRM 51-40-02 PAR 7 FIG 12.

Part: SHEAR TIE — CORRODED (BS 1246) · airframe 102,718 hrs · 16,109 cycles

IN AFT CARGO COMPARTMENT AT BS 1246 LBL3 SHEAR TIE HAS CORROSION REMOVED CORROSION FROM SHEAR TIE IAW SRM 51-10-02 PARA. 14 FIG 1, CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07 FIG 1 DETAIL 2; REMOVED AND REPLACED SHEAR TIE IAW SRM 51-40-02 PARA 4 FIG 3 + 8,

Part: DOOR SILL — CORRODED (BS 585) · airframe 102,718 hrs · 16,109 cycles

CORROSION FWD PIT DOOR SURROUND LOWER SILL LOWER SURFACE FITTING BS 585 CORROSION AT T-ANGLE IN FWD CARGO B.S. 585 RBL 40 FOUND TO HAVE 100% MATERIAL LOSS + REQUIRED REPLACEMENT OF PART IAW SRM 51-10-02 PAR 9. REMOVED + REPLACED -17 CHORD (T-ANGLE) IAW SRM 51-40-02 PAR 7(D)-FIG 12.

Part: SHEAR TIE — CORRODED (BS 1540) · airframe 102,718 hrs · 16,109 cycles

IN AFT BULK CARGO COMPARTMENT AT FRAME 1540 AT SHEAR TIE BTWN STRINGER R38 AND R39 IS CORROSION REMOVED UNSERVICEABLE SHEAR-TIE AND INSTALLED NEW SHEAR-TIE B.S. 1540 BETWEEN STR 38R-39R IAW SRM 51-40-02 PAR 4.

Part: FLOORBEAM — CORRODED (BS 1197) · airframe 102,718 hrs · 16,109 cycles

CORROSION ON UNDERSIDE OF TEE ON THE FLOORBEAM IN THE AFT CARGO BAY BS 1197 BL 0. THE TEE WAS REMOVED AND REPLACED IAW SRM 51-40-02 FIGS 8,12

Part: OVEN — FIRE (GALLEY) · airframe 101,425 hrs · 15,931 cycles

OVEN R42 A4, PAPER CONTENTS SHEET LEFT ATTACHED TO INSERT & CAUGHT FIRE WHEN OVEN REACHED TEMPERATURE. EXTINGUISHED WITH HALON. NO OTHER DAMAGE NOTED. CONFIRMED ONLY ATTRIBUTED TO A4 PAPER SHEET LEFT ON INSERT. ACCOMPLISHED CHECKS IAW AMM 05-51-56 & FORM 46.6020 COMPLETED. NO OTHER FAULTS NOTED. OVEN R42 DEACTIVATED DUE HALON USED. 26 MAY 16 OVEN DEACTIVATED, DUE TO HALON DISCHARGED INTO CAVITY.

Part: PSEU — UNSERVICEABLE (E&E BAY) · airframe 100,986 hrs · 15,872 cycles

ON APPROACH LG EICAS WARNING 2500. AT 500'' TOO LOW TERRAIN WARNING. ADVISED TOMC TROUBLE SHOT & FOUND CARD 15 FAULTED ON PSEU, INSPECTED ALL RT GEAR SENSORS, NO DEFECTS NOTED. R & R PSEU IAW MM 32-09-04. ALSO REPLACED LG CONFIG WARNING CARD MODULE AS PRECAUTIONARY IAW MM 31-51-04. PERFORMED INSTALLATION TEST IAW MM 32-09-04 & 31-51 -04. ALL TESTS PASSED, NO MSGS & NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 100,364 hrs · 15,786 cycles

EMERGENCY EXIT CEILING LIGHT INOPERATIVE AT ROW 10 RT. RELAMPED & OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 100,364 hrs · 15,786 cycles

EXTERIOR EMER EXIT LIGHT INOPERATIVE AT DOOR 2 LT. RELAMPED EMER LIGHT IAW AMM 33-51-03.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 100,364 hrs · 15,786 cycles

EXTERIOR EMER EXIT LIGHT INOPERATIVE AT DOOR 2 RT. REPLACED EMER EXIT LIGHT IAW AMM 33-51-03.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 100,364 hrs · 15,786 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT AFT GALLEY FLOOR. SECURED CONNECTOR. OPERATIONS CHECKED NORMAL.

Part: CHARGER — DEFECTIVE (CABIN) · airframe 99,670 hrs · 15,686 cycles

EMERGENCY EXIT LIGHTS INSPECTION AT SEAT 19 - 23 AB. R & R EPSU CHARGER FOR SEAT ROWS 19 - 23 AB AMM 33-51-07. POWER SUPPLY OPERATIONS TEST COMPLIED WITH AMM 33-51-07-712-032. TEST CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,670 hrs · 15,686 cycles

SEAT ROWS 8AB, JK 7AB, 2A HAVE ONE EACH BULB INOPERATIVE FOR EMER LIGHTING. RELAMPED SEATS AS REQUIRED. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,670 hrs · 15,686 cycles

SEAT ROWS 28L & 38R ALSO CEILING PANEL 35 LT SIDE EMER LIGHTS INOPERATIVE. RELAMPED SEAT ROWS 28LH, 34LH, 35LH & 33RH. OPERATIONS CHECKED GOOD.

Part: DOOR — OUT OF ADJUST (CABIN O2) · airframe 98,792 hrs · 15,572 cycles

DURING DROP CHECK OF OXYGEN MASKS FOR EA 3520-01330, DOORS FAILED TO OPEN AT 3 LOCATIONS, SEAT 1A, 28 AB, & 35 JK. ADJUSTED DOORS, DROP CHECK WITH INSPECTION. PRESENT DROP CHECKED GOOD IAW AMM 35-21-00 501 STEP 2E.

Part: SIGN — INOPERATIVE (COCKPIT) · airframe 97,386 hrs · 15,392 cycles

EMERGENCY EXIT LIGHT SIGN INOPERATIVE IN FLIGHT DECK. REPLACED FLIGHT DECK EMER EXIT LIGHT IAW MM 33-51-01 PG 201. OPERATIONS CHECKED NORMAL.

Part: ACARS — MALFUNCTIONED (COCKPIT) · airframe 94,204 hrs · 14,943 cycles

NO COMMUNICATION ON ACARS INTERMITTENTLY THROUGHOUT FLIGHT. CYCLED CB & OPERATED ACARS LINK MANAGER TEST WRT AMM, OPERATIONS TEST 23-22-00. ALL INDICATIONS RESPONDED CORRECTLY.

Part: FLAP SYSTEM — MALFUNCTIONED (WING) · airframe 93,837 hrs · 14,895 cycles

FLAP OVER SPEED ON GO AROUND. FLAPS RETRACTED FROM 30 TO 20 & THEN HAD FLAP SHUTDOWN MESSAGE. EG WAS AT 8 KNOTS OVER SPEED. PHASE ONE INSPECTION REQUIRED IAW AMM05-51-08. OPERATED FLAPS IN ALT MODE MESSAGE CLEARED, PERFORMED FLAPS OPERATIONS CHECKED IAW 27-51-00 & FSEU TEST ALL OPERATIONS & INDICATIONS NORMAL MESSAGE CLEARED NO FAULT FOUND.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 93,617 hrs · 14,866 cycles

IAW TASK CARD 6-2006-A, FLOOR MOUNTED EMERGENCY EXIT LIGHT INOPERATIVE AT LT MID LAVATORY. REPLACED EMERGENCY EXIT LIGHT LT AT MID LAVATORY IAW MM 33-50-99, TEST IAW MM33-51-00 TESTED OK.

Part: VALVE — LEAKING (AC BAY) · airframe 93,457 hrs · 14,846 cycles

BOOTS BY THE EQUIPMENT COOLING SOV WORN & LEAKING. INSTALLED NEW VLV IAW V 767-300 AMM 21-58-05 STEP11. REPLACED EQUIPMENT COOLING INDICATION CARD, NO HELP. REINSTALLED OLD CARD, REPLACED RELAYS K1206 & K1008, NO HELP. ACCOMPLISHED FIM TASK 21-58 -939 STEP 49 PG 109, FOUND HEAT EXCHANGER BYPASS SOV V10 NOT OPENING FULLY, NEEDS REPLACED. REPLACED VLV IAW AMM 21-58-13. OPERATIONS CHECKED GOOD. REPLACED BOOTS, NO LEAKS.

Part: SHUTOFF VALVE — FAULTY (FUEL SYSTEM) · airframe 93,351 hrs · 14,830 cycles

FUEL IMBALANCE DUE TO REPEAT GRIPES OF FUEL IMBALANCE WITH RT TANK LESS THAN LT AFTER CTR TANK FUEL IS CONSUMED. OPEN UP ASSOCIATE FUEL TANKS & INSPECT INTERNAL PLUMBING FOR ANY LEAKS. IN ADDITION, REPLACE BOTH THE RT CTR MOTIVE FLOW VLV PCN 615-0008 & RT CTR TANK DISCHARGE CHECK VLV PCN 615-0328. REPLACE CTR TANK MOTIVE VLV IAW MM 28-22-05. RT CTR DISCHARGE CHECK VLV REPLACE SEE SEQ 3512015. REPLACED BOTH FUEL CROSS FEED VLV BODIES DUE TO BYPASSING FUEL, SEE SEQUENCE 3512019 FOR DETAILS.

Part: CONTROL PANEL — INOPERATIVE (1ST OBSERVER'S) · airframe 93,163 hrs · 14,805 cycles

PTT BUTTON INOPERATIVE ON 1ST OBSERVER AUDIO CONTROL PANEL. R & R AUDIO CONTROL PANEL IAW AMM, CHECKED OKAY.

Part: FITTING — FAULTY (COCKPIT) · airframe 92,971 hrs · 14,779 cycles

CREW SHOULDER HARNESS DOES NOT PULLOUT RETRACT POSITION 3. 1 CAPTAINS, 2 FIRST OFFICERS, 3 1ST OBSERVERS, 4 2ND OBSERVERS. NEED ONE BLACK RETENTION CLIP FOR SHOULDER HARNESS, REPLACED HARNESS STRAP STOP CLIP ON LT HARNESS ON OBSERVERS SEAT, OK TO CONTINUE.

Part: CONTROL PANEL — DAMAGED (AUTOPILOT SYS) · airframe 92,786 hrs · 14,757 cycles

KNOB ON AUTOPILOT MODE CONTROL PANEL IS MISSING, BENT, STICKS & LOOSE. HEADING SELECT KNOB IS BROKEN, CANNOT SET HEADING ON MCP, KNOB LOOSE. HEADING HOLD WORKS OK. AFCS MODE CONTROL PANEL REPLACED IAW AMM 22-11-02 PP201 & AMM 22-00-02 P208 TEST 04.

Part: CONNECTOR — DIRTY (FUEL SYSTEM) · airframe 92,770 hrs · 14,755 cycles

RT CTR FUEL PUMP RUNS ON GROUND W ENGINES OFF ALL PUMPS SELECTED ON. PLUGS CHECKED & CLEANED ON FUEL PRESSURE SWITCHES S424 & S806. NORMAL INDICATIONS RECOVERED.

Part: MODULE — INOPERATIVE (COCKPIT) · airframe 92,748 hrs · 14,752 cycles

ENG BOTTLE RT DISCHARGE LIGHT CENTER PEDESTAL INOPERATIVE. IAW ERA 2621-01069 REV A & CF228, REPLACED LED LENS MODULE & SWAPPED CAPS WITH SPARE MODULE ON P5-11 PANEL. OPERATIONS CHECKED GOOD.

Part: PANEL — INOPERATIVE (COCKPIT) · airframe 92,748 hrs · 14,752 cycles

SPARE CAP RT SIDE SECOND ABOVE AIL LOCK LIGHT WITH DASH ON P5-11. ANNUNCIATOR PANEL HAS BEEN USED FOR ENG BLT 2 DISCHARGE POSITION IAW ECRA 2621-01069, INOPERATIVE.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 92,714 hrs · 14,745 cycles

SEAT 29AB & 37AB EMERGENCY LIGHTS INOPERATIVE. RESEATED SEAT 29AB SEAT HARNESS. RESEATED SEAT 37AB EMERGENCY LIGHT CONNECTOR IAW UAL B767 DRAWING 33-51-12. OPERATIONS & FUNCTIONAL CHECKED GOOD IAW B767 MM 33-51-10.

Part: WIRE HARNESS — NOT SEATED (CABIN) · airframe 92,714 hrs · 14,745 cycles

SEAT 21JK EMERGENCY LIGHT INOPERATIVE. RESEATED 21JK EMERGENCY LIGHT SEAT HARNESS CABLE. OPERATIONS CHECKED & FUNCTIONAL, CHECKED GOOD IAW B767 MM 33-51-10.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 92,714 hrs · 14,745 cycles

LT A & B ZONE SEATS EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERY PACK IAW B767 MM 33-51-0 7. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — SHORTED (CABIN) · airframe 92,714 hrs · 14,745 cycles

SEATS 27JK-34JK EMERGENCY LIGHTS INOPERATIVE. CONNECTOR AT SEAT 28JK WAS SHORTING OUT STRING OF EMERGENCY LIGHTS AT SEATS 27JK-34JK. REMOVED CAUSE OF SHORT. OPERATIONS CHECKED & FUNCTIONAL. CHECKED GOOD OF SEATS 27JK-34JK IAW B767 MM 33-51-10.

Part: GENERATOR — FAULTY (APU) · airframe 92,714 hrs · 14,745 cycles

T-3 CABLE LOOSE AT GENERATOR CONNECTION. R & R APU GENERATOR & OPERATIONS CHECKED GOOD IAW UAL B767 AMM 24-21-01 OIL LEVEL GOOD ON APU.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 92,714 hrs · 14,745 cycles

FLOOR BEAM BS 287 RBL 14 TO RBL 79 CORRODED. REMOVED EXISTING T CAP & FABRICATED NEW T-CAP SRM 53-00-01 & DRAWING 1505-100333. INSTALLED T-CAP & SPLICE ANGLE & SPLICE STRAP IAW B767-300 SRM 53-00-51 REPAIR 1 & SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 92,714 hrs · 14,745 cycles

AREA AFT OF FWD CARGO COMPARTMENT BS 745 BL 6R BILGE AREA SHEAR TIE HAS CORROSION. R & R SHEAR TIE IAW B767-300 SRM 57-40-02 & DRAWING 143T1214 REV E.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 92,714 hrs · 14,745 cycles

MAIN CABIN L4 AFT ENTRY DOOR CUTOUT LOWER SILL FLOOR PANEL SUPPORT ANGLE CORRODED FS 1530 WL200. R & R A FABRICATED NEW T CORD IAW DRAWING 146T0051 REV F. INSTALLED T CORD IAW B767-300 SRM 51-40-02 & DRAWING 146T0051.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 92,714 hrs · 14,745 cycles

AREA AFT OF FWD CARGO COMPARTMENT BS 745 BL 0 BILGE AREA SHEAR TIE HAS CORROSION. R & R SHEAR TIE IAW B767-300 SRM 51-40-02 & DRAWING 143T1214 REV E.

Part: FRAME — PUNCTURED (FUSELAGE) · airframe 92,714 hrs · 14,745 cycles

AFT CARGO BS 1197+88, FRAME WEB PUNCTURED AT LBL33 & LBL24.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 92,714 hrs · 14,745 cycles

AFT PIT BS 1219 FRAME UPPER T-FLANGE CORRODED RBL 6. R&R T CAP STATION 1219 IAW B767-300 SRM 51-40-02 & DRAWING 146T0250 REV H TIMCO GSO NR 25540.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 92,714 hrs · 14,745 cycles

AFT CARGO COMPARTMENT FLOOR, FRAME UPPER CHORD CORRODED AT BS1197+66, LBL 15 TO LBL 24, WL 124. R&R T CAP WITH NEW LBL 37 TO RBL 37 STATION 1197 IAW B767-300 SRM 51-40-2 & DRAWING 146T1226 REV B GSO NR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 92,714 hrs · 14,745 cycles

MAIN CABIN FLOOR PANEL SUPPORT ANGLE CORRODED, BS 810-845, LBL 87. REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED A NEW -65 SEAT TRACK & INSTALLED PER BAC DWG 145T5213 & SRM 51-40-2 ON NON ROUTINE.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 92,714 hrs · 14,745 cycles

NR1 PYLON MID SPAR OUTBOARD LOWER TANG CLOSE OUT ANGLE, HFEC INDICATES CRACKED OUTBOARD MOST AFT FASTENER . CORRECTION SHOULD BE MID SPAR INBOARD LOWER, ACCOMPLISHED IAW ECRA 5400-01140. CRACK WAS STOP DRILLED AND VERIFIED BY HFEC. ACCOMPLISHED CLOSE OUT ANGLE REPAIR IAW FIG 1,2 & 3 OF THE ECRA. ACCOMPLISH PERMANENT REPAIR NO LATER THAN 10 SEPT 2014. NR1 PYLON MID SPAR OUTBOARD LOWER TANG CLOSE OUT ANGLE WAS REPLACED IAW ECRA 5400-01140 AT C16 VISIT ON JIC COA-6960103A0, & SB 767-54-0080, PYLON SIP MOD AS DOCUMENTED ON N-R 24406.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 92,714 hrs · 14,745 cycles

MAIN CABIN SEAT TRACK SCALLOPS CORRODED, BA 1197+132-1219, RBL 84. REMOVED SEAT TRACK & FABRICATED NEW IAW B767-300 SRM 53-00-52 ALODINED & PRIMED IAW B767-3 00 SRM 51-20-01 & INSTALLED SEAT TRACK SECTION IAW B767-300 SRM 53-00-52.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 92,714 hrs · 14,745 cycles

MAIN CABIN FLOOR SUPPORT IS CORRODED AT BS 835 LBL 34. REPLACED FLOOR SUPPORT IAW B767-300 SRM 53-00-51 FIG 201 DETAIL II REPAIR III.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 92,714 hrs · 14,745 cycles

MAIN CABIN FLOOR SUPPORT IS CORRODED AT BS 835 LBL 34. REPLACED FLOOR SUPPORT FROM BS 830 TO 860 LBL 34 IAW B767-300 SRM 53-00-51 FIG 201 DETAIL II REPAIR NR 3.

Part: FLOORBEAM — CORRODED (BS 852) · corrosion level 2 · airframe 92,714 hrs · 14,745 cycles

MAIN CABIN TRANSVERSE FLOORBEAM IS CORRODED AT BS 852, LBL 55. REMOVED CORROSION FROM UPPER CHORD & FOUND MATERIAL LOSS EXCEEDED ALLOWABLE LIMITS PER SRM 53-00-51, FIG. 101. REMOVED PREVIOUS UPPER CHORD REPAIR & FABRICATED REPAIR CHORD, SPLICE ANGLES & FILLERS & INSTALLED PER SRM 53-00-51. MAJOR REPAIR.

Part: MODULE — FAULTY (METERING VALVE) · airframe 92,646 hrs · 14,734 cycles

BOTH THE NLG AND TILLER DO NOT CENTER WITH HYDRAULIC PRESSURE ON. REPLACED NOSE GEAR STEERING METERING VALVE MODULE IAW MM.

Part: BUSHING — WORN (NLG) · airframe 92,646 hrs · 14,734 cycles

DURING INSPECTION FOR EXCESSIVE TOW ANGLE ON NLG, FOUND TOW FITTING TO FWD LUG OF SHOCK STRUT BUSHINGS TO BOLT HAS WORN OUT OF LIMITS. REMOVED NOSE GEAR TOW FITTING ASSY IAW AMM.

Part: MODULE — FAULTY (AILERON) · airframe 92,612 hrs · 14,729 cycles

EICAS MESSAGE AILERON LOCKOUT DISPLAYED. OTBD AILERONS INDICATED MOVEMENT. UNLOCKED, BOTH. REPLACED RIGHT STAB TRIM AILERON LOCKOUT MODULE. TESTED OK.

Part: SCREW — MISSING (PANEL) · airframe 92,521 hrs · 14,717 cycles

THREE SCREWS MISSING FROM PANEL 194LR ON ACFT UNDERSIDE. SCREWS INSTALLED.

Part: NUT PLATE — LOOSE (NACELLE) · airframe 92,514 hrs · 14,716 cycles

UNDER THE HEAT SHIELD PLATE WITH THE LOOSE BLIND FASTENERS ARE NUMEROUS BROKEN NUTPLATES THAT ALSO SECURE PYLON SIDE PANEL, REF EC RA 5430-1959A, REPLACED. NUTPLATES.

Part: CONNECTOR — UNSECURE (ISOLATION VALVE) · airframe 92,514 hrs · 14,716 cycles

AFTER NR 2 ENGINE THRUST REVERSER REACTIVATION, HAVE RT ENG ISOLATION VALVE MESSAGE AND FAULT ON CTR PEDESTAL. THRUST REVERSER OPS NORMAL WITH ENGINE RUNNING. SECURED THRUST REVERSER ISOLATION VALVE CONNECTOR, NR 2 ENG, RESET PRRM M1987 IAW FIM 78-34-00, CLEARED MESSAGE. RAN ENG AND CYCLED REVERSER, OPS CHECKED NORMAL, NO MESSAGES.

Part: WEB — CRACKED (NACELLE) · airframe 92,514 hrs · 14,716 cycles

NR 1 ENGINE LOWER AFT PAN ATTACHMENT APPEARS LOOSE. REMOVED NR 1 ENGINE PYLON SAIL TAIL FOR INSPECTION AND REPAIRS. FOUND AFT FORMED WEB CRACKED. ALSO FOUND AFT VERTICAL WEB CRACKED IN SAME LOCATION.

Part: SKATE ANGLE — CRACKED (NR 2 NACELLE) · airframe 92,514 hrs · 14,716 cycles

NR 2 ENGINE AFT LOWER PAN ATTACHMENT LOOSE, REMOVED NR 2 PYLON SAIL TAIL FOR INSPECTION AND REPAIRS. FOUND INBD SKATE ANGLE, STRAP, AFT FORMED WEB AND AFT VERTICAL WEB CRACKED.

Part: STRUCTURE — DAMAGED (NR 2 PYLON) · airframe 92,514 hrs · 14,716 cycles

NR 2 ENGINE AFT LOWER PAN ATTACHMENT LOOSE, SUSPECT LONGITUDINAL CRACK IN INBD CHORD STRAP. REMOVED NR 2 ENGINE PYLON SAILTAIL FOR INSPECTIONS & REPAIRS. FOUND INBD SKATE ANGLE STRAP, AFT FORMED WEB & AFT VERTICAL WEB CRACKED.

Part: TUBE — DENTED (COOLING MANIFOLD) · airframe 92,514 hrs · 14,716 cycles

TURBINE COOLING MANIFOLD, COOLING TUBE HAS A DENT EXCEEDING 20 PERCENT LIMIT ON NR 1 ENGINE RT SIDE, LOW PRESSURE SIDE. NEAR 3 O'CLOCK POSITION. REMOVED NR 1 ENGINE LPT COOLING MANIFOLD AC13 IAW MM. REPLACED ON NR 1 ENG COOLING MANIFOLD AC13.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 92,486 hrs · 14,710 cycles

CENTER HYD STATUS MESSAGE. C2 HYD PUMP ONLY SHOWING 2700 PSI. MIN IS 2850. REPLACED C2 HYD PUMP, LEAK AND OPS CHECKED GOOD.

Part: FAN — FAULTY (NR 1) · airframe 92,133 hrs · 14,662 cycles

FWD EQ EXHAUST FAN STATUS MSG ON EICAS. CYCLED BREAKERS AS REQUIRED IN MEL, FAN RECOVERS AND QUITS. SUSPECT FAN. BREAKERS NOW OPEN AND SAFTIED. R & R EQ EXHAUST FAN. RESET VIBRATION MONITOR. OPS CHECK GOOD.

Part: COUPLING — LEAKING (RT IDG) · airframe 92,133 hrs · 14,662 cycles

CHRONIC RT IDG LOW OIL. DUE TO CONTINUED RT IDG TRIPPING INCLUDING A REJECTED TAKEOFF ACCOMPLISH THE FOLLOWING. FOUND PUDDLE OF OIL IN CORE COWLS JUST UNDER IDG. CLEANED COWLS AND IDG OIL LINES, INSPECTED LINES FROM IDG TO AIR-OIL COOLER AND TO FUEL-OIL COOLER WITH ENG AT IDLE NO LEAKS NOTED. FOUND LEAK COMING FROM IDG 118169 OIL OVERFLOW COUPLING. REPLACED OVERFLOW COUPLING, REF SUBTASK 24-11-01-434-033. REPLENISHED IDG OIL TO FULL REF AMM 12-13-03-301. RAN NR 2 ENG AT IDLE FOR 10 MIN AND ACCOMPLISHED LOAD TEST REF STEP F, AMM 24-11-00-715-105. LOAD TEST GOOD. NO OIL LEAK FROM OVERFLOW COUPLING.

Part: COUPLING — DEFECTIVE (NR 2 IDG) · airframe 92,133 hrs · 14,662 cycles

EICAS MSG RT GEN OFF DISPLAYED. RT GENOFF&FIELD OFF LGT'S ILLUM. OPERATED NORM AFTER RESET. RT ENG GENERATOR TRIPPED OFF LINE ON TAKEOFF ABOUT 200 FT RESET NORMALLY. REPLACED NR 2 ENG IDG OIL OVERFLOW COUPLING REF AMM SUB TASK 24-11-01-434-033. RAN ENG AT IDLE FOR 10 MIN, NO LEAKS.

Part: IDG — UNDERSERVICED (RT GENERATOR) · airframe 92,104 hrs · 14,658 cycles

RT GENERATOR TRIPPED OFF ON TAKEOFF ROLL AT 70 KTS. FOUND ON EICAS ELCT PAGE, RT IDG DRIVE MESSAGE AND ON AUTO EVENT RT IDG RISE TEMP TWICE HIGHER THAN LT IDG BPCU. CONFIRMED HIGH RISE ON RT IDG, SERVICED RT IDG IAW 12-13-03-613-26.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,005 hrs · 14,645 cycles

EMERGENCY LIGHTS INOPERATIVE. SEAT ROWS 19 - 23 LT. REPLACED BATTERY POWER SUPPLY, OPS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,005 hrs · 14,645 cycles

CEILING EMERGENCY EXIT SIGN INOPERATIVE. JUST AFT OF SEAT ROW 14AB. REPLACED BATTERY POWER SUPPLY, OPS CHECKED NORMAL.

Part: LATCH — BROKEN (CARGO DOOR) · airframe 91,926 hrs · 14,636 cycles

AFT CARGO DOOR, CONTROL PANEL DOOR LATCH BROKEN. REMOVED AFT CARGO DOOR CONTROL EXTERIOR PANEL DUE TO BROKEN UPPER LATCH. LATCH WAS REPLACED.

Part: PUMP — FAULTED (FUEL SYS) · airframe 91,709 hrs · 14,610 cycles

FUEL CONFIGURATION LIGHT AT 2.6 OUT OF BALANCE. FOLLOWED QRH PROCEDURE AND REBALANCED. TROUBLESHOT IAW SERVICE TIP 28-11-94. NO DISCREPANCIES NOTED. REMOVED AND REPLACED RIGHT CTR OVERRIDE FUEL PUMP IAW AMM, OPS AND LEAK CHECKED GOOD.

Part: ACTUATOR — LEAKING (SPOILERS) · airframe 91,660 hrs · 14,605 cycles

CENTER HYD LEAK ON RIGHT WING SPOILER. FOUND NR 10 SPOILER PCA LEAKING FROM FILTER CASE. REPLACED PCA AS PER MM 27-61-02 ALL OPS AND INDICATIONS NORMAL NO LEAKS AFTER FUNCTIONAL TEST.

Part: ACTUATOR — LEAKING (SPOILERS) · airframe 91,622 hrs · 14,601 cycles

NR 10 SPOILER ACTUATOR LEAKING HYDRAULIC FLUID FROM ACTUATOR FILTER CAP. NR 10 SPOILER FILTER CAP FITTED WITH NEW SEALS FILTER CAP TIGHTENED AND WIRE LOCKED PER AMM. ACP FUNCTIONAL CHECKED, NO LEAKS DETECTED.

Part: O-RING — CUT (HYD SYSTEM) · airframe 91,549 hrs · 14,592 cycles

CENTER SYSTEM HYDRAULIC RESERVOIR READS .09 ON EICAS. TROUBLESHOT FOUND HYD LEAK AT NR 10 SPOILER ACTUATOR FILTER HOUSING CAP. FOUND O-RING CUT. REPLACED O-RING IAW MM 20-10-19. RESERVICED CTR HYD SYSTEM. LEAK AND OPS CHECKED GOOD.

Part: FASTENER — LOOSE (NR 1 PYLON) · airframe 91,492 hrs · 14,584 cycles

NR 1 PYLON HEAT SHIELD HAS FASTENER LOOSE UPPER EDGE 7TH ONE BACK FROM FWD EDGE. REPLACED FASTENERS.

Part: WIRE — DAMAGED (GALLEY) · airframe 91,492 hrs · 14,584 cycles

PIGTAIL AT AFT GALLEY P62 IS DAMAGED AT CONNECTOR. REPLACED AFT PIGTAIL AT POSITION P62.

Part: CLAMP — MISSING (NR 2 FIRE LOOP) · airframe 91,492 hrs · 14,584 cycles

NR 2 ENGINE FIRE LOOP AT 7 O'CLOCK JUST BEHIND BREATHER, INSULATOR TOP CLAMP AND SCREW IS MISSING. INSTALLED NEW CLAMP AND SCREW.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 91,492 hrs · 14,584 cycles

EMERGENCY LIGHT INOPERATIVE SEAT ROW 19AD-23AB. REPLACED EMERGENCY LIGHT BATTERY CHARGER AND BATTERY PACK.

Part: BLANKET — DAMAGED (NR 2 ENGINE) · airframe 91,476 hrs · 14,582 cycles

NR 2 ENGINE HYD AND FUEL LINE BLANKET ON RIGHT SIDE OF ENGINE IS DAMAGED. REPLACED BLANKET.

Part: O-RING — CUT (NR 10 SPOILER) · airframe 91,237 hrs · 14,547 cycles

FLUID LEAK RIGHT INBOARD SPOILER. FOUND HYDRAULIC LEAK COMING FROM THE NR 10 SPOILER ACTUATOR FILTER HOUSING. FOUND CAP O-RING CUT. REPLACED NR 10 SPOILER FILTER, PACKINGS AND FILTER COVER O-RINGS PER MM. LEAKED CHECK AND OPERATED SPOILERS AND NO LEAKS NOTED.

Part: TRANSMITTER — INOPERATIVE (WATER QTY) · airframe 91,078 hrs · 14,527 cycles

NO WATER PRESSURE THROUGHOUT ACFT QTY SHOWS 150 GAL AND HOLDING STEADY. NO AIR COMING FROM FAUCETS WHEN OPENED. ALL LAVATORIES DRY FLUSHING. REPLACED WATER QTY TRANSMITTER AND PRESSURE SWITCH, OPS CHECKED GOOD. NO LEAKS NOTED.

Part: HOSE — DISCONNECTED (EVAC SLIDE) · airframe 91,012 hrs · 14,518 cycles

SLIDE INFLATION HOSE DISCONNECTED FROM BOTTLE, LEFT SLIDE BOTTLE. INSTALLED AND SECURED SLIDE INFLATION HOSE.

Part: BOTTLE — MISINSTALLED (LT OVERWING SLID) · airframe 91,012 hrs · 14,518 cycles

LEFT OVERWING INFLATION BOTTLE BALL IN THE MIDDLE OF INFLATION CABLE IS NOT INSTALLED BEHIND THE RETAINER SPRING. REMOVED LEFT OVERWING INFLATION BOTTLE AND REPLACED IAW AMM 25-65-02.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 90,913 hrs · 14,506 cycles

EMERGENCY LIGHT INBD AFT GALLEY INOPERATIVE. SECURED LOOSE CONNECTOR AT LAMP, CHECKED OKAY.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 90,913 hrs · 14,506 cycles

EMERGENCY LIGHT INOPERATIVE. SECURED LOOSE CONNECTOR, OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 90,913 hrs · 14,506 cycles

EMERGENCY LIGHT ABOVE COCKPIT DOOR INOPERATIVE. REPLACED LAMPS, CHECKED OKAY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 90,913 hrs · 14,506 cycles

EMERGENCY LIGHT AT SEAT 33J INOPERATIVE. REPLACED LAMP, OPS NORMAL.

Part: MODULE — MALFUNCTIONED (TIME DELAY) · airframe 90,882 hrs · 14,501 cycles

LOW PRESSURE LIGHT ILLUMINATED POS 1 (01=1,02=2). EICAS MESSAGE DISPLAYED C HYD PRIM (1,2). FRM CODE 29-11-07 --. TROUBLE SHOT PER MM AND FOUND TIME DELAY MODULE M303 AT FAULT. REPLACED M303 IAW WD 29-11-31. TESTED PER MM 201 AND 501 AND TESTED NORMALLY.

Part: SHUTOFF VALVE — FAILED (BLEED AIR SYS) · airframe 90,364 hrs · 14,429 cycles

NR 2 ENGINE PRV FAILED HEALTH CHECK. REPLACED NR 2 ENGINE PRV AMM 36-11-18. COMPLETED UP TO AND INCLUDING STEP D-13 PAGE 413.

Part: CONTROLLER — FAILED (BLEED AIR SYS) · airframe 90,364 hrs · 14,429 cycles

NR 2 ENGINE HP CONTROLLER FAILED HEALTH CHECK, NEEDS REPLACEMENT. REPLACED NR 2 ENGINE HP CONTROLLER AMM.

Part: SHUTOFF VALVE — FAILED (BLEED AIR SYS) · airframe 90,364 hrs · 14,429 cycles

NR 2 ENGINE PRSOV FAILED HEALTH CHECK, NEEDS REPLACEMENT. (SEE AMSITM 3642073 FOR FAILED MM STEP). REMOVED AND REPLACED NR 2 ENGINE PRSOV.

Part: PANEL — SHEARED (FUSELAGE) · airframe 90,364 hrs · 14,429 cycles

DURING FLAP RETRACTION PANEL SEPARATED FROM AIRCRAFT AT LEFT FUSELAGE WING TO BODY FAIRING BY LEFT INBD T/E FLAP. REMOVED TORQUE TUBE FOR SHEARED DOOR PER MM 27-51-07. CONT OF AMIS ITEM 3642044. INSTALLED REPLACEMENT FAIRING DOOR AND TORQUE TUBE ASSY AS REQUIRED REF MM.

Part: THERMOSTAT — FAULTY (BLEED AIR SYS) · airframe 90,364 hrs · 14,429 cycles

ON ENGINE RUN RT ENGINE ON HIGH STAGE AIR FLUX + - 5 PSI. AFTER RUNNING ENGINE ON HI STAGE FOR APPROX 10 MIN (PACK ON) AND SHIFTING TO LOW STAGE, LOW STAGE AIR BLED TO ALMOST ZERO. (SUSPECT TEMP THEROMOSTAT). REPLACED RT ENGINE FAN AIR TEMP SENSOR PER MM 36-11-17. NEED TO COMPLETE FROM STEP 3E(11) PG 406.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,364 hrs · 14,429 cycles

EEL LIGHT AT SEAT 20AB INOPERATIVE. RELAMPED, OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,364 hrs · 14,429 cycles

EEL LIGHT AT SEAT 38AB INOPERATIVE. RELAMPED, OPS NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 90,364 hrs · 14,429 cycles

EXT MID SLIDE GRD ILLUM LIGHT RIGHT SIDE INOPERATIVE. RELAMPED, OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,364 hrs · 14,429 cycles

EEL LIGHT AT SEAT 35JK INOPERATIVE. RELAMPED, OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,364 hrs · 14,429 cycles

EEL LIGHT AT SEAT 37JK INOPERATIVE. RELAMPED, OPS NORMAL.

Part: LENS — MISSING (CABIN) · airframe 90,364 hrs · 14,429 cycles

EMERGENCY CEILING LIGHT AT 6JK MISSING LENS. REPLACED LENS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,364 hrs · 14,429 cycles

EEL LIGHT AT SEAT 36JK INOPERATIVE. RELAMPED, OPS NORMAL.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 90,364 hrs · 14,429 cycles

FWD EEL LIGHT AT SEAT 9AB INOPERATIVE. FOUNDED CONNECTOR DISCONNECTED. RECONNECTED, CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,364 hrs · 14,429 cycles

EMERGENCY CEILING LIGHT INOP AT 8JK. RELAMPED, OPS NORMAL.

Part: VALVE — FAULTY (AC BAY) · airframe 90,043 hrs · 14,383 cycles

PACK 'INOP' & 'PACK OFF' LIGHTS ON. EICAS MSG 'R PACK OFF' DISPLAYED. COULD NOT RESET FIG 105A BLOCK 1. REPLACED FCSO VAVLE.

Part: AUDIO PANEL — FAULTY (COCKPIT) · airframe 89,992 hrs · 14,377 cycles

F/O'S MIC SELECT PANEL BACKGROUND LIGHTS INOP. FOUND AS STATED SWAPPED W ITH FIRST OBSERVERS AUDIO SELECT PANEL TO COMPLY WITH MEL F/O'S AUDIO SELECT PANEL, ALL OPS CHECKS GOOD. REMOVED AND REPLACED AUDIO SELECTOR PANEL IAW AMM, OPS CHECK NORMAL. REMOVED PANEL RETURNED TO 1ST OBSERVERS. POSITION.

Part: O-RING — LEAKING (NR 10 SPOILER) · airframe 89,794 hrs · 14,350 cycles

SPOILER ON THE RIGHT SIDE 5 OUTBOARD FROM THE FUSELAGE IS LEAKING. FOUND NR 10 SPOILER LEAKING HYD FLUID FROM FILTER CAP. REPLACED O-RING. OP'S CHECK NORMAL. NO LEAKS NOTED.

Part: COFFEEMAKER — SPARKS (GALLEY) · airframe 89,794 hrs · 14,350 cycles

CREW REPORTED WHEN FLT ATTENDANT MOVED LEVER ON COFFEEMAKER M51 IN RT AFT GALLEY TO REMOVE BREW TRAY, COFFEEMAKER SPARKED AND LIGHT SMOKE NOTICED. FLIGHT ATTENDANT PULLED C/B FOR M51 AT RIGHT AFT GALLEY POWER CONTROL PANEL. NO FURTHER SMOKE OR SPARKS NOTICED REF WDM 25-31-34. REPLACED COFFEEMAKER AS PER AMM.

Part: ACTUATOR — FAILED (LT AILERON) · airframe 89,564 hrs · 14,318 cycles

"AIL LOCK" LT ON AT HIGH SPEED. EICAS MSG "AILERON LOCKOUT" DISPLAYED. OUTBOARD AILERONS INDICATED MOVEMENT - UNLOCKED, BOTH. CREW COMMENTS: 290 KNOTS AT 13,000FT,TEMP -8, THE RT SAM HAD AN ADC AND A LT AILERON LOCKOUT ACTUATOR FAULTBALL. BOTH DID RESET. PER LM THE LLEFT AILERON LOCKOUT ACTUATOR NEEDS TO BE REPLACED. REPLACED LEFT AILERON LOCKOUT ACTUATOR, OPS CHECK GOOD.

Part: STARTER — FAULTY (APU) · airframe 89,443 hrs · 14,301 cycles

APU FAULT ON START WILL NOT START. TORUBLESHOT AS PER MM AND REMOVED AND REPLACED APU STARTER AS PER MM. OPS CHECKS GOOD. PCN 651-1150.

Part: SENSE LINE — LOOSE (BLEED AIR SYS) · airframe 89,410 hrs · 14,296 cycles

SPLIT DUCT PRESSURES AT CRUISE. L-18 R-42 AT FL39 RT ENG HPSOV SECURED CLOSED. FOUND SENSE LINE ON NR 2 HP VALVE LOOSE. SECURED LINE. PERFORMED ENGINE RUN UP ALL BLEED PARAMETERS NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,352 hrs · 14,287 cycles

'L PACK INOP' LIGHT ON. EICAS MSG 'L PACK TEMP' DISPLAYED. OPERATED NORM AFTER 'STANDBY' SELECTED. L ZONE TEMP CONTROLLER SHOWED RAM AIR OUTLET ACT. RESET AND VERIFY OK PACK OPS OK IN AUTO.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 89,339 hrs · 14,284 cycles

NR 1 PYLON MID SPAR O/B LOWER TANG CLOSE OUT ANGLE, HFEC INDICATES CRACKED O/B MOST AFT FASTENER (CRACK INDICATED ON AFT SIDE) :CORRECTION-SHOULD BE MID SPAR I/B LOWER TANG. :VERIFIED CRACK WITH FPI INSPECTION AND NOTIFIED FOREMAN. PERM REPAIR WAS ACP'D REF ECRA 5400-01140. CRACK WAS STOP DRILLED AND VERIFIED BY HFEC. ACP'D CLOSE OUT ANGLE REPAIR PER FIG 1, 2, AND 3 OF THE ECRA. ACCOMPLISH PERMANENT REPAIR NO LATER THAN 10/SEP/14 BY REPLACING MIDSPAR FITTING. BOEING RECOMMENDS THAT THE SIP SB 767-54-0080 BE PERFORMED UPON THE UPCOMING PERMANENT REPAIR.

Part: FITTING — CRACKED (NR 1 PYLON) · airframe 89,339 hrs · 14,284 cycles

NR 1 PYLON MIDSPAR FITTING LOWER I/B TANG-PERFORM OPEN HOLE HFEC INSPECTION REF TASK 54-51-92-206-802 THE 2 MOST AFT FASTENERS AT THE CLOSEOUT ANGLE (AD 2010-14-18). ACP OPEN HOLE HFEC PER ND TM PART6 51-00-16 OF NR 1 PYL MIDSPAR LOWER INBD FITTING. FOUND CRACK INDICATION FOR BOTH HOLES. MFG STRAP REPAIR.

Part: TRANSMITTER — DEFECTIVE (HYDRAULIC SYS) · airframe 89,300 hrs · 14,279 cycles

RT QTY EICAS MSG, RTFL. DISPLAYED AND RIGHT QTY LIGHT ILLUMINATED ON OVERHEAD PANEL. QTY INDICATION INDICATED RF ON STATUS PAGE. FLT CREW TURNED OFF RIGHT HYD PUMPS PER QRH PROCEDURE. DURING RETURN TO FIELD CREW STATED QTY STABILIZED. PUMPS TURNED ON PER TOMC. INSPECTED ACFT FOR HYD LEAKS NONE FOUND. CHECKED RIGHT HYD QTY AT RESERVOIR PER MEL PROCEDURES. FOUND QTY FULL. PLACARD RIGHT QTY PER MEL. REPLACED RIGHT SYSTEM QTY TRANSMITTER PER MM. LEAK AND OPS CHECK GOOD.

Part: MODULE — FAULTY (SPOILER) · airframe 89,203 hrs · 14,266 cycles

EICAS MSG SPOILERS DISPLAYED. SPOILERS LIGHT ILLUM WITH SPOILERS SELECTED TO ARMED POSITION. TROUBLESHOT AND FOUND M53 0 SPOILER CONTROL MODULE AT FAULT. REMOVED AND REPLACED IAW AMM. PERFORMED SYSTEM TEST, ALL TEST NORMAL, OK TO CONTINUE.

Part: WIRE — SEVERED (CABIN) · airframe 89,198 hrs · 14,265 cycles

REF DF983, SEAT 8J EEL LIGHT WIRES SEVERED ON ACCOUNT OF SHEARED OTTOMAN FOOTREST. REPLACED EEL LIGHT ASSEMBLY, OPS CHECK GOOD.

Part: CONNECTOR — DIRTY (HYD QTY) · airframe 88,974 hrs · 14,235 cycles

80 KTS A RT HYD QTY EICAS ILLUMINATED AND HYD QTY SHOWED .57 AND RAPIDLY DECREASING. CLEANED CONNECTOR. PRESSURIZED RH HYDRAULIC SYSTEM. CHECKED HYDRAULIC QUANTITY. SAME QUANTITY IN COCKPIT AND AT RESERVOIR.

Part: INDICATOR — INOPERATIVE (COCKPIT) · airframe 88,847 hrs · 14,221 cycles

LOST RT UPPER CRT, RTFL. RIGHT UPPER CRT DEAD. REPLACED FIRST OFFICERS EADI IAW AMM.

Part: COMPUTER — INOPERATIVE (LEFT) · airframe 88,748 hrs · 14,207 cycles

CAPTAIN'S FLIGHT DIRECTOR INOPERATIVE. REPLACED LT FCC PER AMM.

Part: SHUTOFF VALVE — FAILED (BLEED SYS) · airframe 88,687 hrs · 14,198 cycles

LT ENGINE HPSOV EICAS MSG. ACCOMPLISHED PNEUMATIC HEALTH CHECK OF THE HPSOV-HPC SYSTEM. AILED ITEM C (22) & (27). RESISTANCE READINGS NOT WITHIN LIMITS. HPSOV. REPLACED HIGH PRESSURE CONTROLLER PER MM. PERFORMED ENGINE RUN, OPS CHECKED NORMAL. ACCOMPLISHED ENGINE AIR BLEED OPERATIONAL CHECK.

Part: BLEED VALVE — FAILED (LT ENGINE) · airframe 88,546 hrs · 14,180 cycles

OVERHEAD BLEED LIGHT ON EICAS LT ENGINE HPSOV AND LT ENGINE HPSOV STATUS MESSAGE. HPSOV IS LOCK CLOSED. REPLACED VALVE NEEDS ENGINE RUN TO OPS CHECK VALVE. AFTER RUN STILL NO GOOD. AFTER VALVE CHANGE AND ENGINE RUN. THE STATUS OF THE PROBLEM HAS BEEN CHANGED. LEFT BLEED OFF LIGHT AND EICAS ADVISORY REPORTED WITH BLEED OPS NORMAL. REPAIR ACCOMPLISHED ENG RUN PER JRH, ALL BLEED IND NORMAL WITH LOAD ON AND OFF, BLEED SHIFT NORMAL. NO FAULTS NOTED.

Part: MICROPHONE — INOPERATIVE (VHF SYSTEM) · airframe 88,409 hrs · 14,162 cycles

NR 1 VHF NO TRANSMIT OR RECEIVE ON BOTH HEADS OF RADIO. NR 1 AND NR 3 VHF SETS INTERCHANGED NO GOOD. VHF CONTROL HEADS INTERCHANGED NO GOOD, AUDIO SELECTORS INTERCHANGED AND CAPTAINS AND F/O'S MIC`S INTERCHANGED ALL OPS RETURNED TO NORMAL. SUSPECT NR 1 MIC KEY LINE STUCK ON & RELEASED BY INTERCHANGE. CREW REPORT BOTH VHFS NOW OK.

Part: SLIDE — DETACHED (L2 DOOR) · airframe 88,113 hrs · 14,124 cycles

CUSTOMER SERVICE INADVERTENTLY OPENED DOOR 2L AND PARTIALLY DEPLOYED ESCAPE SLIDE. SLIDE UNIT DETACHED FROM DOOR 2L. DOOR SECURED CLOSED PER MEL 52-11H.

Part: FITTING — LEAKING (NR 2 ENGINE) · airframe 87,123 hrs · 13,999 cycles

NR 2 ENGINE HAS HYDRAULIC LEAK. REPLACED QUICK DISCONNECT FITTING ON SUPPLY LINE TO NR 2 ENG EDP RAN ENGINE, OPS CHECKS NORMAL.

Part: COUPLER — LEAKING (HYDRAULIC SYS) · airframe 87,003 hrs · 13,983 cycles

NR 2 ENG HYD PUMP RETURN LINE COUPLER LEAKING AT PYLON. RMV'D LINE & QUICK DISCONNECT FITTING NEED TO INSTALL NEW LINE & NEW QUICK DISCONNECT FITTING. RMV'D AND PARTIALLY INSTALLED NEW PUMP PER MM. MR29157 DASH 3 REMOVED AND DASH 444 INSTALLED.

Part: BATTERY — FAULTY (MAIN) · airframe 86,832 hrs · 13,961 cycles

MAIN BATTERY CHARGER STATUS MSG. REPLACED MAIN BATTERY AND BATTERY CHARGER PER MM, OPS CKS GOOD. CLEARED MESSAGE. BATTERY READING 29 VOLTS.

Part: HYDRAULIC SYSTEM — UNKNOWN (NR 2 NACELLE) · airframe 86,652 hrs · 13,939 cycles

HYDRAULIC FLUID DRIPPING FROM NR 2 ENGINE. OPENED RT NACELLE, HYD FLUID WETNESS IN AREA OF EDP AND HYD LINES. CLEANED & DRIED. RAN ENGINE 5 MINS, REINSPECTED, NO LEAKS NOTED. HYD QTY CHECKED GOOD.

Part: VALVE — FAULTY (COCKPIT TEMP) · airframe 86,528 hrs · 13,921 cycles

DIFFICULT TO CONTROL TEMP IN COCKPIT. MIX VALVE SHOWS FULL WARM WITH COLD AIR STILL BLOWING. FLT DECK TRIM VLV SHOWS WARM, BUT COLD AIR IS COMING IN, CREW CYCLED MASTER TRIM VLV AND OPERATED FLT DECK TRIM VLV IN MANUAL, NO HELP. REPLACED TRIM AIR VALVE.

Part: ENGINE — SURGES (NR 2) · airframe 86,456 hrs · 13,910 cycles

NR 2 ENG SURGE DURING T/O. ABORTED T/O AT 40KTS. RPLC NR 2 ENG SN 717690 DUE ENGINE SURGE, RESULTING IN ABORTED TAKEOFF & RECENT PARAMETER SHIFT. RMV'D NR 2 ENG SN 717690. INSTALLED ENG 727968.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,365 hrs · 13,899 cycles

EEL LIGHT STRIP BETWEEN DOORS 1 RT AND 1 LEFT JUST AFT OF G1 GALLEY INOP. REPLACED EEL STRIP IAW B767 GNMM 2-0-15-005. OPS CHECKS GOOD.

Part: BATTERY — FAULTED (MASTER) · airframe 86,339 hrs · 13,894 cycles

APU RUNNING WITH FAULT LIGHT. REPLACED AIRCRAFT BATTERY AND OPS OK ALL SYSTEMS NORMAL.

Part: CONTROLLER — FAILED (ECM) · airframe 86,282 hrs · 13,886 cycles

ECM HAS PARAMETER SHIFTS DETECTED AT CRUISE & TAKEOFF. NO MESSAGES DOWNLINKED. REPLACED CONTROLLER PER MM 36-11-08. BITE CHECKED GOOD PER MM.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 85,915 hrs · 13,830 cycles

HEADING SELECT 1ST DIGITS SOMETIMES STICK (WILL NOT MOVE). REPLACED MODE CONTROL PANEL PER MM.

Part: LINE — CRACKED (APU) · airframe 85,910 hrs · 13,828 cycles

APU OIL CONSUMPTION ABOVE LIMIT. WHILE PREPPING FOR APU CHANGE FOUND FLOW SENSING MODULE LOOSE AND MISSING. MOUNT HARDWARE FOUND IN CONTACT WITH SCAVANGE LINE BELOW SHOP. TESTED LINE. FOUND CRACKED AND LEAKING. REPLACED LINE AND INSTALLED MOUNT HARDWARE.

Part: PANEL — DENTED (FUSELAGE) · airframe 85,887 hrs · 13,823 cycles

PANEL 193GL HAS DENT WHICH IS DELAMINATED 1" BY 2" APPROX. ROBBED AND INSTALLED PANEL FROM 6676.

Part: GUIDE VANE — DAMAGED (RT ENGINE) · airframe 85,879 hrs · 13,821 cycles

RIGHT ENGINE MULTIPLE EXIT GUIDE VANES DAMAGED AT THE 4 O'CLOCK TO 7 O'CLOCK POSITIONS. MAINT TEXT: TWO ADJACENT FAN EXIT VANE BETWEEN 4:00 AND 5:00 REMOVED, AN ADDITIONAL VANE REMOVED AT 6:00 POSITIONS. VANES TO BE REPLACED NO LATER THAN NEXT ENGINE SHOP VISIT REF MM. IN ADDITION, 20 PREVIOUSLY TAPED VANES WITH LEADING EDGE EROSION BETWEEN 3:00 AND 7:00 THAT HAD DETERIORATED TAPE, TAPE REPLACED. -CQT- :TAPED VANES ARE ROUTINELY CHECKED AT "A" CHECKS AND RECONDITIONED DURING THE "A" CHECK. THREE VANE REMOVALS ACP PER MM. ** MF8305 CREATED TO MONITOR **.

Part: DETECTOR — FAULTED (FUEL CELL) · airframe 85,663 hrs · 13,786 cycles

FUEL CONFIGURATION LIGHT ILLUMINATED. TANK QUANTITIES ARE 40.6 LEFT, 23.0 CTR, AND 38.8 RIGHT. RIGHT FUEL QTY DENSITOMETER INOPERATIVE. REPLACED RT FUEL TANK DENSITOMETER ELECTRONIC UNIT PER MM. BITE CHECKED GOOD. NO FAULTS FOUND.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 85,637 hrs · 13,782 cycles

AFTER FD OFF, SMELL DISSIPATED. ALL R CRTS REMOVED AND COOLING SCREENS CHECKED FOR OPENESS ALL GOOD. NO ELECTRICAL SMELL EVIDENT. FCC R MCDP TEST PASSED.

Part: ACTUATOR — LEAKING (RUDDER) · airframe 85,630 hrs · 13,781 cycles

HYDRAULIC FLUID LEAK COMING FROM RIGHT SIDE OF VERTICAL STAB AT APPROX THE CENTER ACTUATOR VICINITY DURING ARRIVAL 1SV CHECK. HYD LEAK COMING FROM RUDDER AREA. ACTUATED RUDDER FLUID DRIPPING FROM DRAIN HOLE ON TRAILING EDGE OF RUDDER ALSO EVIDENCE FROM HINGES. UPPER RUDDER PCU LEAKING OUT OF LIMITS. REMOVED AND REPLACED RUDDER UPPER PCA. OPS CHECKED AND LEAKED CHECKED GOOD. ACCOMPLISHED INSPECTION OF UPPER PCA PER MM, CKS OKAY.

Part: FMC — MALFUNCTIONED (LEFT) · airframe 85,580 hrs · 13,774 cycles

LEFT FMC WILL NOT ACCEPT NAVIGATION DATA. REPLACED LEFT FMC, LOADED NAVIGATION DATA, CHECKED GOOD.

Part: DUCT — LEAKING (PYLON) · airframe 84,967 hrs · 13,691 cycles

RT DUCT LEAK. PLACED 2 ELEMENTS ON AOG REF T2959 & C4755. REPLACED ELEMENTS. ACCESS VERY TIGHT IN TOP OF PYLON AND LEADING EDGE INPUT ACCEPTED RECONNECT D10222 BEHIND P61 PANEL ACCT DISCONNECTED FOR TROUBLESHOOTING DUCT LEAK PROBLEM. RECONNECTED D10222. TEST PANEL OP CHECKS OKAY.

Part: ACTUATOR — MALFUNCTIONED (APU) · airframe 84,947 hrs · 13,689 cycles

APU INOP KEEPS POPPING APU DOOR C/B WITH APU DOOR STATUS MSG. REPLACED APU INTAKE DOOR ACTUATOR REF MM, OPS CHECK OKAY.

Part: GUIDE VANE — DAMAGED (NR 2 ENGINE) · airframe 84,915 hrs · 13,685 cycles

NR 2 ENGINE EXIT GUIDE VANES HAVE METAL TAPE COMING LOOSE. RETAPED NR 2 ENGINE EXIT GUIDE VANES FROM 9 O'CLOCK TO 3 O'CLOCK POSITIONS.

Part: SERVO VALVE — FAILED (RUDDER) · airframe 84,856 hrs · 13,676 cycles

CENTER RUDDER SERVO CMD FAULT NEED TO REPLACE CENTER RUDDER DAS VALVE DUE TO FAILED. REPLACED DAS CENTER SERVO VALVE.

Part: CABLE — INOPERATIVE (CABIN) · airframe 84,748 hrs · 13,661 cycles

SEAT MOUNTED EEL INOP AT 30JK. REPLACED SEAT CABLE, OPS CHECK OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,748 hrs · 13,661 cycles

RT MID LAV AREA FLOOR EEL STRIP INOPERATIVE. REPLACED EEL STRIP, OPS CHECK OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,748 hrs · 13,661 cycles

EEL INOP BETWEEN SEAT 8 AND 9JK. REPLACED LIGHT ASSEMBLY. OPS CHECK OK.

Part: CABLE — DEFECTIVE (CABIN) · airframe 84,748 hrs · 13,661 cycles

SEAT 38JK MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED SEAT CABLE, OPS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 84,748 hrs · 13,661 cycles

SEVERAL CEILING EEL LIGHTS AND SIGNS INOP AFT LT SECTION. REPLACED BATTERY AT M739, OP CHECK NORMAL.

Part: ACTUATOR — LOOSE (AILERON) · airframe 84,374 hrs · 13,609 cycles

NO LAND 3 & LEFT AUTO PILOT INOPERATIVE. ACCOMPLISHED MCDP BITE, LAST FLT FAULTS SHOWS "AIL SRVO-FCC L. FLIGHT CONTROL COMPUTER NIS EZEJL, PCN 481-9097. INSTALLED FCC PER MM, NO HELP. STILL FAILING "AIL SERVO FCC L. RMV'D LEFT UPPER LCCA. NEW LCCA IN PLACE. HYDRAULIC LINES ON LOWER MOUNT BOLTS ON TIGHT. RIGHT UPPER MOUNT BOLT ON HAND TIGHT. UPPER LEFT NUT NEEDS TO BE INSTALLED. INSTALLED LOWER LEFT LCCA AND SECURED UPPER LEFT LCCA PER MM. OPS NORMAL.

Part: MODULE — FAULTY (STAB TRIM) · airframe 84,407 hrs · 13,614 cycles

INTERMITTENT STAB TRIM EICAS AND STAB TRIM LIGHT ON OVERHEAD. REPLACED R SAM PER MM, GROUND CHECK NORMAL.

Part: COMPUTER — FAULTY (FLT DIRECTOR) · airframe 84,251 hrs · 13,590 cycles

NO FLIGHT DIRECTOR INDICATION ON CAPTAINS ADI. LEFT AUTO PILOT INOP DEFERRED PER MEL 2210A. MAINTENANCE PROCEDURE ACCOMPLISHED ACFT DOWN GRADED TO CAT 2 PER MEL. REPLACED LEFT FCC PER MM, TESTED GOOD.

Part: TIRE — DAMAGED (MLG) · airframe 84,154 hrs · 13,575 cycles

NR 3 AFT TIRE HAS FOUR WHEEL-HALF TIE BOLTS SHEARED AND HAS GONE FLAT. REPLACED NR 3 AFT AND NR 4 AFT TIRES IN ACCORDANCE WITH MM.

Part: STARTER — FAULTY (LT ENGINE) · airframe 83,654 hrs · 13,504 cycles

CREW REPORT: L ENGINE START VALVE LIGHT ILLUMINATES BUT NO DUCT PRESSURE DROP DURING START ATTEMPT. REPLACED STARTER AND START VALVE PER MM. OPS ARE GOOD.

Part: GCU — FAULTY · airframe 83,642 hrs · 13,502 cycles

APU FIELD OFF LT IS ON. WHEN GND PWR WAS DISCONNECTED PLANE WENT DARK. HMG VERIFIED TO OP NORMAL AS PER MEL. NEED TO REPLACE APU GENERATOR PER MM. NEED LEAK CHECK AND SYS TEST PER MM. REPLACED GENERATOR PER MM. OPS CHECK OF APU GEN NORMAL. REPLACED GCU PER MM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 83,642 hrs · 13,502 cycles

EMERGENCY EXIT SIGNS L335 AND L1199 INOP. REPLACED M739 POWER SUPPLY, OPS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,642 hrs · 13,502 cycles

EMERGENCY EXIT LIGHT ON SEAT 30AB INOP. REPLACED LIGHT ASSY, OPS GOOD.

Part: SWITCH — INOPERATIVE (AC PACK) · airframe 83,615 hrs · 13,498 cycles

RIGHT PACK INOP LIGHT FOUND TO BE INOPERATIVE. DEF RT PACK INOP LIGHT PER MEL. RT PACK STILL INOP. RESET RT PACK FLOW CONTROL PC ASSY. REPLACED COMPLETE LIGHT SWITCH ASSY. RT PACK OPS NORMAL NOW.

Part: O-RING — LEAKING (APU) · airframe 83,575 hrs · 13,493 cycles

OIL LEAKING FROM APU GENERATOR RT OIL PASSAGE TEST PORT JUST FORWARD OF ELECTRICAL HARNESS STUDS. REPLACED PLUG. APU GENERATOR LEAKING OIL FROM THE DRAIN PLUG. REPLACED O-RING, LEAK CHECKS GOOD.

Part: PACKING — DAMAGED (HYDRAULIC SYS) · airframe 83,409 hrs · 13,469 cycles

LEFT AIR DRIVEN HYDRAULIC PUMP PRESSURE LINE LEAKING. REPLACED PACKING AT UNION TO PUMP BODY. OP CHECKS NORMAL.

Part: PANEL — FAULTY (VHF COMM) · airframe 83,334 hrs · 13,457 cycles

NR 1 VHF COMM CNTRL PNL HAS MECHANICAL DEFECT: BROKEN, MISSING OR LOOSE PARTS. (01=L VHF, 02=R VHF). REPLACED NR 1 COMM PANEL, ALL OPS CHECK SATISFACTORY.

Part: AUDIO PANEL — FAULTY (COCKPIT) · airframe 83,342 hrs · 13,458 cycles

CAPT AUDIO PANEL INTERMITTENTLY INOP. LOUD STATIC WITH ALL VOL CONTROLS OFF. UNABLE XMIT-REC. REPLACED AUDIO SELECT PANEL. OPS CHECK GOOD.

Part: SLIDE — DEPLOYED (R2 DOOR) · airframe 83,334 hrs · 13,457 cycles

PASSENGER DOOR 2R ESCAPE SLIDE RAFT REMOVED FOR DEPLOYMENT. NEEDS TO BE RE-INSTALLED AND SOLD TO INSPECTION PER MM. REPLACED SLIDE PER MM.

Part: AUDIO PANEL — FAULTY (COCKPIT) · airframe 83,305 hrs · 13,453 cycles

NR 3 AUDIO SEL PNL PUSH-TO-TALK SW IS DEFECTIVE. (03=CAPT, 04=1ST OFF, 5=1ST OBS). CREW COMMENTS: INTERMITTENT. REPLACED THE CAPT'S ASSEMBLY.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 82,543 hrs · 13,345 cycles

EMERGENCY FLOOR PATH LIGHT, RT AISLE FWD GALLEY (L901) AND EMERGENCY EXIT IDENTIFIER (L972) AT DOOR 1 RT ARE INOP. DISCONNECTED FLOOR PATH LT FROM POWER FEEDER, EXIT LIGHT STILL FAILS TO COME ON. SUSPECT POWER SUPPLY(M1552). REPLACED POWER SUPPLY BATTERY PACK, OPS CK NORMAL.

Part: WINDOW — DEFECTIVE (NR 1) · airframe 82,470 hrs · 13,329 cycles

NR 1 WINDOW FOUND TO BE DEFECTIVE WHEN WE ATTEMPTED TO CONNECT HARNESS AT J2 AND J3 TERMINAL BLOCK, REMOVED CAPTAIN'S NR 1 WINDOW AND INSTALLED NEW NR 1 WINDOW. ACCOMPLISHED FIRST TORQUE OF WINDOW BOLTS 05:00. SECOND TORQUE TO BE ACCOMPLISHED 08:00 IAW MM. COMPLETED INSTALLATION OF NR 1 WINDSHIELD. OPS CHECKS GOOD.

Part: WARNING MESSAGE — ILLUMINATED (AC BUSS) · airframe 82,369 hrs · 13,315 cycles

F/O INSTRUMENT TRANSFER STATUS MESSAGE. CB 21C "115V AC BUSS RT SECT1" ON THE P6-4 FOUND POPPED OUT. AFTER CB CLOSED, SYS OPS OK. TESTED IAW AMM 24-51-04-0401 PFMD, OK. PROBABLY DUE TO CREW DOCUMENTS BAG.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 82,078 hrs · 13,278 cycles

FOUND HYDRAULIC LINE LEAKING IN THE RIGHT WHEEL WELL. REPLACED BRAKE PRESSURE LINE 272T4500-899. NO LEAKS NOTED.

Part: FITTING — CRACKED (FLAP/SLATS) · airframe 82,078 hrs · 13,278 cycles

CREW REPORTED EICAS STATUS MESSAGE FLAP-SLAT ELEC GROUND SEE`S VISIBLE HYD LEAK. REPLACED CRACKED FITTING ON THE FLAP-SLAT SHUTOFF VALVE MODULE. OPS NORMAL AND NO LEAKS NOTED.

Part: PRESSURE SWITCH — INOPERATIVE (LT FUEL SYS) · airframe 81,849 hrs · 13,246 cycles

LT CTR FUEL PUMP LOW PRESSURE LIGHT DOES NOT COME ON. LT CTR FUEL PUMP INOPERATIVE. REPLACED PRESSURE SWITCH S423. OPS NORMAL.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 81,234 hrs · 13,160 cycles

EMERGENCY LIGHT LENS MISSING AT SEAT 8A. REPLACED LENS. OPS NORMAL.

Part: COUPLING — FAILED (NR 2 STARTER) · airframe 81,084 hrs · 13,139 cycles

RIGHT ENGINE WILL NOT ROTATE FOR START, START VALVE LIGHT ON AND PRESSURE DROP NOTED. REPLACED STARTER & VALVE, NO HELP. SUSPECT STARTER DRIVE PAD COUPLING SHEARED, CHECKED N2 ROTOR FOR TURNING USING MANUAL CRANK PAD ON THE IDLER PAD OF THE OIL PUMP. COUPLER AND REMOVAL TOOL ON FLT 972 ETA 0920. REPLACED ENGINE 2 STARTER COUPLING. OPS NORMAL.

Part: WIRE — SHORTED (GALLEY CART) · airframe 80,824 hrs · 13,100 cycles

CREW REPORTS LT AFT GALLEY CART PIGTAIL NR62 WAS ARCING. CREW PULLED CBS FOR CART CONTROLLERS M61, M62 , M63 PRECAUTIONARY. WIRES DAMAGED, CB PULLED AND COLLARD FOR CART 62 CONTROLLER M62. REPLACED PIGTAIL, OPS CK OK.

Part: LINE — LEAKING (ENGINE OIL) · airframe 80,208 hrs · 13,022 cycles

RT ENGINE HAS OIL LEAK AT APPROX 6 O'CLOCK UNDER CORE COWL. FOUND LINE LEAKING FROM OIL SCAVENGE PUMP TO OIL TANK UNDERNEATH RUBBER. REPLACED MAIN OIL FILTER LINE, LEAK CHECKED GOOD.

Part: SMOKE DETECTOR — FAULTY (AFT CARGO BAY) · airframe 79,925 hrs · 12,980 cycles

EICAS MSG POS4 "CARGO DET 1" DISPLAYED. REPLACED AFT CARGO 1 DET PERFORMED DET TEST IAW MM. SYS OPS CHECKED OK.

Part: WINDOW — SCRATCHED (COCKPIT) · airframe 79,917 hrs · 12,977 cycles

CAPTAIN'S FIXED SIDE-AFT WINDOW'S VISIBILITY IS AFFECTED BY DEFECTS. REPLACE FIRST AVAILABLE. WINDOW SCRATCHES WITHIN LIMITS PER MM.

Part: CIRCUIT CARD — FAULTY (COOLING PANEL) · airframe 79,695 hrs · 12,944 cycles

DURING CLIMB THRU 8000' FWD EQUIP OVHT EICAS AND EQ COOLING VALVE LIGHT ON EQ COOLING PANEL. FOUND FAULTY EQ COOLING CARD. REPLACED EQ COOLING INDICATION CARD. OPERATES NORMAL ON GROUND.

Part: COMPUTER — FAULTY (AUTOPILOT) · airframe 79,540 hrs · 12,920 cycles

AUTOPILOT DISC LIGHT ON & EICAS MSG 'AUTOPILOT DISC' DISPLAYED WITH 2 AUTOPILOT SYS ENGAGED IN COMMAND (1=L, 2=C, 3=R). CREW COMMENTS: CTR AP INOP IN CRUISE WOULD NOT RESET LT AND RT AP OK: MCDP STORED FAULTS SHOWS NO INFC FCC CTR, CONFIRMED BY TEST. FCC C RESET PERF, THEN ALL 3 FCC TEST PERF ACC, TESTS PASSED. AC DOWNGRADED TO CAT2 ONLY. REPLACED CTR FLIGHT CONTROL COMPUTER AND CAT CK PERFORMED.

Part: SHUTOFF VALVE — FAULTED (RT ENGINE) · airframe 79,523 hrs · 12,917 cycles

RT ENG HPSOV EICAS MSSG ON TAKEOFF. DEF DUE TIME. HPSOV SECURED IN CLOSED POSITION. REPLACED HPSOV.

Part: LIGHT — LOOSE (ENG OVERHEAT) · airframe 79,488 hrs · 12,912 cycles

RT ENG OVHT LT LOOSE TESTS OK. REPLACED BASE ASSY RT ENG OVHT LIGHT, OPS NORMAL.

Part: ACTUATOR — LEAKING (RT POSITION) · airframe 79,392 hrs · 12,893 cycles

FUEL LEAK AT RT JETTISON NOZZLE. REPLACED RT FUEL JETTISON NOZZLE VALVE. PRESSURIZED JET PUMP, STILL LEAKING FUEL AT RT JETTISON NOZZLE. FERRIED TO ORD FOR REPAIR. RIGHT JETTISON FUEL NOZZLE VALVE LEAKING OUT OF LIMITS. *NO CENTER TANK FUEL*. REMOVED FUEL JETTISON NOZZLE VALVE. NEW VALVE ON AOG W0989. FUEL JETTISON TUBE CLAMP (INBD OF VALVE) REMOVED FOR REMOVAL OF GAMMA COUPLING. COMPLETED REPLACEMENT OF RT NOZZLE VALVE.

Part: INDICATION SYS — INOPERATIVE (FUEL QTY) · airframe 79,301 hrs · 12,877 cycles

ALL FUEL QTY INDICATORS BLANK.

Part: INDICATOR — FAULTY (FUEL QTY) · airframe 79,299 hrs · 12,876 cycles

FUEL QTY BITE SHOWED FAULT CODES FOR CHANNEL 1&2 A4 B4 B8 A3 B3. PROCESSOR PREVIOUSLY REPLACED. REMOVED PROCESSOR AND CHECKED FOR PUSHED PINS, NONE NOTED. NO QTY PROCESSOR AT ORD. TROUBLESHOOT IAW MM CONFIG 1 PAGE 182A. REPLACED FQIS PROCESSOR AND QTY IND, TEST PASSED. DUE TO CHRONIC ALL MFQ INDICATORS BLANKING IN FLT REQUEST WAS MADE TO REPLACE FQIS PROCESSOR WITH A KNOWN GOOD UNIT. INSTALLED NEW FQIS PROCESSOR IAW MM. BITE CHECK IAW MM TABLE 101, CHECKS GOOD. P-36 DEFUELING VALVE C-B POPPING OUT. REPLACED DEFUELING VALVE (PN S343T003-39/ SN 464). OP CK IAW AMM. OPS CK GOOD. FOUND DEFUELING VALVE WIRE SHORTED TO SHIELD IN LT W-W. PLUG D1254 BLUE WIRE 458- 301B-20. REPAIRED IAW SWPM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,293 hrs · 12,873 cycles

LEFT OVERWING EMERGENCY EGRESS LIGHT L389 IS INOP. RELAMPED AND OPS CHECKS GOOD REF AMM.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 79,293 hrs · 12,873 cycles

PERFORM OPERATION CHECK ON NR 2 ACMP. PERFORM CONTINUITY CHECK IAW W-D, CHECK GOOD IAW W-D, FURTHER CK ON C2 ACMP IAW AMM. FOUND OPS CHECK FAIL PUMP BURN OUT, R & R ACMP IAW MM, OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,293 hrs · 12,873 cycles

RIGHT AFT EXTERIOR EMERGENCY LIGHTS L644, L391 AND L392 ARE INOP. RELAMPED AND OPS CHECKS GOOD.

Part: PUMP — LEAKING (NR 1) · airframe 79,293 hrs · 12,873 cycles

NR 1 ACMP IS LEAKING AT BREATHER PLUG PUMP R29140 S-N MX-514350F. REMOVED & REPLACED NR 1 ACMP. ACP LEAK CHECK. OPS CHECK GOOD.

Part: PUMP — FAULTY (HYD SYSTEM) · airframe 79,293 hrs · 12,873 cycles

NR 1 ALTERNATING CURRENT MOTOR PUMP (ACMP) CURRENT DRAW EXCESSIVE AT 40 AMPS AT 45 DEGREES CELCIUS DURING ROUTINE TASK 640014210 TEST. INSTALLED NEW ACMP IAW SNR 640014210 TEST. INSTALLED NEW ACMP SNR 640014210. INSPECTED BY QC.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 79,125 hrs · 12,846 cycles

EEL LIGHT AT SEAT 7A INOPERATIVE. SECURED CONNECTOR, CHECK OKAY.

Part: CONNECTOR — LOOSE (CABIN) · airframe 79,125 hrs · 12,846 cycles

EEL LIGHT AT SEAT 33HJ INOPERATIVE. SECURED CONNECTOR, OPS CHECK OK.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 78,900 hrs · 12,815 cycles

FLAP IND SHOWS 1-2 WIDTH NEEDLE SPLIT AFTER SELECTING FLAPS 5. NO ASSOC ROLL NOTED. REPLACED FLAP INDICATOR. OPS CHECKS OKAY.

Part: ANTI-ICE VALVE — FAULTY (RT WING) · airframe 78,089 hrs · 12,688 cycles

RT WING ANTI-ICE IS INOP. DURING TROUBLESHOOTING VALVE FOUND DEFECTIVE. REPLACED RT WING A/I VALVE. OPS CKS ARE NORMAL.

Part: CONTROL VALVE — FAULTY (LT A/C PACK) · airframe 77,818 hrs · 12,646 cycles

LT PACK OFF WITH GOOD FLOW FROM APU. FLOW CONTROL VALVE FOUND FAULTY. REPLACED LT PACK FLOW CONTROL VALVE. OP CHKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,441 hrs · 12,581 cycles

EMERGENCY LIGHTS INOP FROM ROW 27-34HJ. TRIED TO REPLACE BATTERY PACKS LOCATED BETWEEN SEATS 37 & 38HJ AND AT SEAT 22HJ, NO HELP. INSTALLED ORIGINAL BATTERY. DISCONNECTED EA SEAT FROM 27-34HJ FOR SHORTS, NO HELP. RE-INSTALLED AND SECURED BACK CONNECTORS. NEEDS MORE T-S. REPLACED BATTERY PACK AT SEAT 32K, CHECKS GOOD.

Part: COMPUTER — MALFUNCTIONED (EICAS) · airframe 77,429 hrs · 12,577 cycles

LEFT ENGINE OIL FILTER MESSAGE ON INTERMITTENTLY. REPLACED LEFT EICAS COMPUTER, ACP SOFTWARE LOAD OF DISK OPS 3171-COL-DEO-02 AND OPC 3100-BCG-006 -E7, ACP BITE TEST OF LEFT EICAS COMPUTER, TESTED GOOD, NO MESSAGES.

Part: WIRE — CHAFED (PYLONE) · airframe 77,435 hrs · 12,579 cycles

NR 1 ENG OIL FILTER MSSG, FLIGHT DIVERTED. FOUND CHAFED WIRE IN WIRE HARNESS ON TOP OF NR 1 ENG CLOSE TO ELEC CONNECTOR JUNCTION BOX ON PYLON. WIRE WAS CHAFING ON METAL INSULATION BLANKET ON ENG, 3" AFT OF WIRE HARNESS SUPPORT BRACKET. NO STRANDS WHERE BROKEN ON WIRE. REPAIRED WIRE AND RETIRED WRAPPED SECTION WITH HIGH TEMP TAPE. REPAIRED IAW MM 2-0-15-001. REPAIR WAS DONE IAW MM 71-51-00.

Part: IDG — MALFUNCTIONED (NR 2) · airframe 77,201 hrs · 12,544 cycles

EICAS MSG R GEN DRIVE DISPLAYED. GEN DRIVE LIGHT ILLUM. GEN DRIVE DISCONNECTED. REPLACED RT ENG IDG. NO LEAKS DETECTED. IDG OPERATIONAL TEST IS GOOD.

Part: VALVE — MALFUNCTIONED (AC PACK) · airframe 77,053 hrs · 12,522 cycles

LEFT A-C PACK DROPS OFF. REPLACED LEFT PACK LOW LIMIT VALVE, ALL OPS & INDICATIONS NOW NORMAL.

Part: PRESSURE SWITCH — MALFUNCTIONED (HYDRAULIC SYS) · airframe 76,582 hrs · 12,455 cycles

CENTER HYDRAULIC SYSTEM PRESSURE LOW LIGHT DOES NOT COME ON WITH PUMPS OFF. REPLACED CENTER HYDRAULIC SYSTEM PRESSURE SWITCH, ALL CHECKS OKAY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 75,792 hrs · 12,332 cycles

EXT EMERGENCY LIGHT AFT OF TRAILING EDGE IS INOP AT RT. OPS CHECKED LIGHT OKAY AFTER BATTERY CHARGED.

Part: CONNECTOR — LOOSE (CABIN) · airframe 75,792 hrs · 12,332 cycles

SEAT MOUNTED EMERGENCY LIGHT ASSY AT 31J INOP. SECURED LIGHT ASSY CONN, CHECKED OKAY.

Part: TRANSDUCER — FAULTY (STAB TRIM) · airframe 75,753 hrs · 12,325 cycles

EICAS MSG STAB TRIM DISPLAYED & STAB TRIM LIGHT ILLUMINATED. STABILIZER TRIM OPERATES AT ONE-HALF SPEED, RTFL. REPLACED RELAY K1070 (LEFT TRIM LIMIT SELECT RELAY) NO HELP. STAB TRIM OPERATES NORMAL WITH FLAPS EXTENDED. FLAPS RETRACTED WILL TRIM NOSE DOWN BUT WILL NOT TRIM NOSE UP. INSTALLED LEFT STAB TRIM AILERON LOCKOUT FOR T-S. NEW STAB TRIM AILERON LOCK OUT DID NOT HELP. REMOVED AND INSTALLED ORIGINAL. REPLACED STAB TRIM MODULE. STAB TRIM MODULE ON WAS MR 27025-11, NO HELP WITH PROBLEM. REPLACED STAB TRIM MODULE, NO HELP. REPLACED LT STAB POS XDUCR. TESTS OKAY.

Part: PUMP — FAULTY (FUEL SYSTEM) · airframe 75,509 hrs · 12,291 cycles

'FUEL CONFIG' LIGHT ON WITH 'C' PUMPS ON AND TANK QUANTITIES 40.4-4.1-38.7. ACCOMPLISHED SERVICE TIP. SYSTEM CHECKED GOOD. REPLACED THE RIGHT CENTER OVERRIDE JETTISON PUMP. SYSTEM CHECK FOUND GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,258 hrs · 12,255 cycles

EXTERNAL SKIN STA 1220 RT SIDE BETWEEN LAP AND STR 36 HAS CRACK INDICATION. DRILLED OUT CRACK AND INSTALLED SOLID RIVET.

Part: PUMP — FAULTY (HYD SYSTEM) · airframe 74,939 hrs · 12,210 cycles

RIGHT CENTER HYDRAULIC PUMP WILL NOT PRESSURIZE. REPLACED NR 2 CTR ACMP. NR 2 CTR ACMP PRESSURE LINE AND OR UNION LEAKING, LINE DISCONNECTED AND UNION REMOVED. REPLACED UNION, CONNECTED LINE. OPS CK'D PUMP, LEAK CK'D GOOD.

Part: ACOUSTIC LINER — DAMAGED (NR 2 ENGINE) · airframe 74,915 hrs · 12,206 cycles

NR 2 ENGINE ACOUSTIC LINER HAS A DENT WHICH IS PUNCTURED BETWEEN 2 PERFORATIONS, LOCATED AT THE 9 O'CLOCK POSITION AND IS 8 INCHES FWD OF THE BLADES. IT IS 3-8TH INCH WIDE. ACCOMPLISHED REPAIR. APPLIED HEAT TO EXPEDITE CURE TIME.

Part: PIN — BACKED OUT (CABIN) · airframe 73,490 hrs · 12,011 cycles

SEAT 20 HJ EMERGENCY LIGHT INOP RELAMP NO HELP RED OVERWING EXIT. FOUND PUSHED BACK PIN, SECURED PIN AT CONNECTOR. OPS NORMAL.

Part: LIGHT — INOPERATIVE (FAIRING) · airframe 72,934 hrs · 11,935 cycles

RT EMERGENCY SLIDE LIGHT INOP AT FAIRING. RELAMPED. OPS OKAY.

Part: ACTUATOR — LEAKING (RUDDER) · airframe 72,675 hrs · 11,900 cycles

FOUND MIDDLE RUDDER PCA LEAKING HYDRAULIC FLUID. REPLACED MIDDLE RUDDER PCA. OPS CHECK NORMAL.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 72,510 hrs · 11,879 cycles

DURING TAXI IN, F/A REPORTED ESCAPE PATH LIGHTING CYCLING OFF AND ON. REPLACED M1557 BATTERY PWR SUPPLY. GOOD OP CHECK.

Part: HEATER — ODOR (COCKPIT WINDOW) · airframe 72,482 hrs · 11,873 cycles

ELECTRICAL ODOR IN FLIGHT DECK. FLIGHT DIVERTED. IDENTIFIED CAUSE TO THE FO'S NR 1 WINDOW HEAT LOWER AFT CONNECTION AND ASSOCIATED WIRES AND CONTACTS. TURNING OFF WINDOW HEAT INDUCED CESSATION OF ODOR. AREA COOLED TO NORMAL TEMPERATURE. REPLACED FIRST OFFICER'S NR 1 WINDOW.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,442 hrs · 11,867 cycles

DOOR FWD RT EMERGENCY EXIT SIGN INOP. REPLACED LIGHT ASSY & BATTERY PACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,442 hrs · 11,867 cycles

CEILING MOUNTED EMERGENCY LIGHT AT 6K IS INOP. LIGHT FOUND INOPERATIVE. REPLACED LIGHT ASSY & REPAIR WIRING. SYSTEM CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,442 hrs · 11,867 cycles

EEL FLOOR MOUNTED LIGHT STRIP ON RIGHT FWD AISLE INOP BETWEEN DOOR 1 RT AND SEAT 1K. REPLACED LIGHT ASSY & BATTERY PACK. OP CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,355 hrs · 11,853 cycles

RT AFT LIGHT BAR INOP.

Part: SKIN — DENTED (FUSELAGE) · airframe 72,355 hrs · 11,853 cycles

LT UPPER FUSELAGE EXT SKIN HAS DENT AT STA 1197 + 88 BETWEEN STR 1L AND STR 1R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE & INSTALLED DOUBLER REPAIR.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 72,355 hrs · 11,853 cycles

THREE EACH CROSS AISLE LIGHTS INOP. FOUND BROKEN AND CUT WIRES ON LIGHT BARS AT FWD VCC CABINET AREA. REPLACED LIGHT BARS , OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,355 hrs · 11,853 cycles

EEL LIGHT BAR INOP AT LEFT FWD CLOSET.

Part: CABLE — BROKEN (CABIN) · airframe 72,355 hrs · 11,853 cycles

RIGHT AFT LIGHT BAR INOP. FOUND BROKEN RIBBON CABLE FROM POWER SUPPLY. REPLACED WITH NEW LIGHT BAR. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,355 hrs · 11,853 cycles

EEL LIGHT BAR AT RT FWD G2 GALLEY IS INOP.

Part: SPRING — WEAK (R2 DOOR) · airframe 72,355 hrs · 11,853 cycles

DOOR R2 DOOR DEPLOYMENT BAR GAS SPRING WEAK. SPRING FOUND INADEQUATE. REPLACED GAS SPRING. OPS OKAY.

Part: ATTACH ANGLE — CRACKED (NR 2 STRUT) · airframe 72,355 hrs · 11,853 cycles

NR 2 STRUT AFT STRUT BULKHEAD INBOARD ATTACH ANGLE CRACKED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED ANGLE. FABRICATED & INSTALLED NEW ANGLE.

Part: WIRE — DAMAGED (CABIN) · airframe 72,355 hrs · 11,853 cycles

EEL LIGHT BARS INOP AT AFT LT LAV. FOUND EEL LIGHT BAR WITH CUT WIRES AND POOR SPLICES. REPLACED PER MM33-51-10, AND OPS CHECKS GOOD.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 72,355 hrs · 11,853 cycles

UPPER FUSELAGE AT STA 1197 + 88 SHEAR TIE BETWEEN STR 1L AND STR 1R HAS DOUBLED DRILLED HOLE. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SHEAR TIE. FABRICATED & INSTALLED A NEW SHEAR TIE.

Part: SPRING — WEAK (R1 DOOR) · airframe 72,355 hrs · 11,853 cycles

DOOR R1 DEPLOYMENT BAR GAS SPRING WEAK. GAS SPRING DEFECTIVE. REPLACED DEPLOYMENT BAR GAS SPRING. OP CHECKS OKAY.

Part: CONNECTOR — ARCED (HYDRAULIC SYS) · airframe 72,355 hrs · 11,853 cycles

CENTER SYS NR 1 ACMP CONNECTOR D482 SHOWS SIGNS OF ARCHING AND HAS A RECESSED PIN. REPLACED CONNECTOR D482P. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,355 hrs · 11,853 cycles

EEL LIGHT BARS INOP AT MID LEFT AND RIGHT LAVS.

Part: SKIN — CRACKED (NR 2 STRUT) · airframe 72,355 hrs · 11,853 cycles

NR 2 STRUT, ONBOARD AFT SKIN CRACKED AT PANEL CUTOUT RADIUS, FORWARD OF AFT BULKHEAD. MAJOR REPAIR ACCOMPLISHED. STOP-DRILLED CRACK. VERIFIED HFEC. INSTALLED -1 & -3 DOUBLERS.

Part: LATCH — CORRODED (EMERGENCY EXIT) · airframe 72,355 hrs · 11,853 cycles

LT OVERWING COMPARTMENT DOOR LATCHES (4 EA) HAS CORROSION AND EXCESSIVE WEAR MARKS. REPLACED 4 LATCHES AT LT OVERWING SLIDE COMPARTMENT DOOR. INSPECTED AND OPS CHECKED GOOD.

Part: O-RING — LEAKING (FUEL PUMP) · airframe 71,886 hrs · 11,777 cycles

EVIDENCE OF FUEL LEAK FROM RIGHT WING MAIN FUEL PUMP PANEL. *S/D* SUSPECT O-RING PACKING. REPLACED O-RING LEAK CHECKED GOOD. AC OK FOR SERVICE.

Part: FAN — SMOKE (EQUIP COOLING) · airframe 71,751 hrs · 11,756 cycles

SMOKE ODOR IN CABIN. FLT DIVERTED. FOUND APU OPERATION NORMAL. REPLACED EQUIP COOLING EXHAUST FAN AS A PRECAUTION.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 71,405 hrs · 11,700 cycles

EICAS MESSAGES T/E FLAP DISAGREE & T/E FLAP SHUTDOWN DISPLAYED.

Part: INDICATION SYS — MALFUNCTIONED (TE FLAP) · airframe 71,405 hrs · 11,700 cycles

EICAS MESSAGES T/E FLAP DISAGREE & T/E FLAP SHUTDOWN DISPLAYED. CREW COMMENTS: FLAPS DISAGREE FROM 20 TO 25. RAN L/E AND T/E DEVICES THRU SEVERAL CYCLES AND OPERATED IN RAPID FLAP POSITION CHANGES. OPERATION APPEARS NORMAL. FSEU BITE=NO FAULTS. MESSAGE CLEARED AND DID NOT RE-APPEAR.

Part: VALVE — FAULTY (E/E BAY COOLING) · airframe 71,109 hrs · 11,652 cycles

FWD EQUIPMENT OVERHEAT EICAS MESSAGE CAME ON PASSING 10000 FEET AND EXTINGUISHED PASSING 18000 FT. SUSPECT FAULTY COOLING OVERRIDE VALVE. REPLACED FWD E&E COOLING OVERRIDE VALVE PER MM 21-58-20. OPS CHECK OK. AC OK FOR SERVICE.

Part: HEAT EXCHANGER — CRACKED (NR 1 A/C PACK) · airframe 71,021 hrs · 11,639 cycles

NR 1 PACK IS PUTTING OUT 50 DEGREE AIR, FOUND A 8" CRACK IN NR 1 HEAT EXCHANGER. FOUND CRACK IN HEAT EXCHANGER. REPLACED HEAT EXCHANGER ASSEMBLY. IAW MM21-51-02 RAN BOTH PACKS NO DEFECTS NOTED. AC OK FOR SERVICE.

Part: FAN — FAILED (E/E BAY) · airframe 70,538 hrs · 11,552 cycles

EQUIPMENT COOLING FAN FAILURE. REPLACED FWD EQUIPMENT COOLING FAN OPS CHECKED GOOD. AC OK FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (AILERON LOCKOUT) · airframe 70,200 hrs · 11,498 cycles

AILERON LOCKOUT EICAS SLOWING THRU 270 AT 11000.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,630 hrs · 11,412 cycles

EEL LIGHT ADJACENT TO DOOR 1R INOP. OPS CHECKS GOOD.

Part: LAMP — INOPERATIVE (SMOKE DETECTOR) · airframe 69,630 hrs · 11,412 cycles

EQUIPMENT COOLING SYSTEM TEST FAILED. SMOKE ANNUNCIATOR LIGHT INOP. EQUIPMENT COOLING SYS TEST FAILED. SMOKE ANNUNCIATOR LIGHT INOP. RELAMPED DETECTOR. OPS CHECK OK. ACFT OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (SATCOM) · airframe 69,582 hrs · 11,405 cycles

RTFL DUE TO SATCOM FAILURE.

Part: INDICATOR — FAULTY (STBY ATTITUDE) · airframe 68,661 hrs · 11,267 cycles

RTFL DUE TO STANDBY ATTITUDE INDICATOR PROBLEMS. REPLACED STANDBY ATTITUDE INDICATOR WITH BORROWED UNIT. OPERATIONAL TEST CARRIED OUT SUCCESSFULLY. ACFT CATII-III STATUS NOT ALTERED.

Part: BULB — INOPERATIVE (FLASHLIGHT) · airframe 68,597 hrs · 11,257 cycles

EMERGENCY FLASHLIGHT AT MID GALLEY CLOSET INOP. SUSPECT FAULTY BULB OR BATTERIES. REPLACED FLASHLIGHT, NOW OPS OK. ACFT OK FOR SERVICE.

Part: HOSE — COLLAPSED (EVAC SLIDE) · airframe 68,597 hrs · 11,257 cycles

HOSE ASSY FOR RAMP SLIDE INFLATION HAS COLLAPSED. SUSPECT HOSE DAMAGED DURING MAINTENANCE. REPLACED HOSE ASSEMBLY. ACFT OK FOR SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 68,555 hrs · 11,252 cycles

EMERGENCY LIGHTING STRIP BROKEN AT 2B. REPAIRED BROKEN SECTION. OPS CHECK, OK.

Part: TOILET — INOPERATIVE (LAVATORY) · airframe 41,699 hrs · 5,083 cycles

FOUR OUT OF EIGHT LAVS INOP THE 4 GOOD LAVS FLUSH CLEAR FLUID. *S/D* AFTER 10 DAYS & CONSIDERABLE TROUBLESHOOTING & TANK SERVICING, DETERMINED LEFT AFT TOILET HAD VALVE PROBLEM WITH CONTINUOUS FLUSHING PROBLEM. REPLACED TOILET ASSEMBLY. LAV SYSTEM CHECKED OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (RT OF MID GALLEY) · airframe 68,228 hrs · 11,197 cycles

EEL LIGHTS AT RIGHT OF MID GALLEY & AT ROW 5AB ARE INOP. 10-26-07 REPAIRED EEL POWER STRIP. OP CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,740 hrs · 11,115 cycles

FOUND EEL LIGHTS INOP COACH RIGHT SIDE. REPLACED BATTERY PACK. TESTS OK .

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 67,740 hrs · 11,115 cycles

FOUND EEL LIGHTS INOP MID LAV. REPAIRED EEL FEEDER CABLE. TESTS OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,740 hrs · 11,115 cycles

FOUND AFT GALLEY RT EEL STRIP INOPERATIVE. REPLACED LAMP STRIP. TEST OK.

Part: OXYGEN SYSTEM — READS LOW (CREW) · airframe 67,466 hrs · 11,070 cycles

CREW 02 LOW READS 1300 PSI.

Part: MASK — FAULTY (COPILOT'S O2) · airframe 67,466 hrs · 11,070 cycles

CREW OXYGEN MASK PROBLEM, POSITION 2. (1=CAPT,2=FO, 3=1ST OBS, 4=2ND OBS). CREW COMMENTS: COPILOTS O2 MASK HAS LEAK IN HEAD BAND AND DOES NOT FULLY EXPAND.

Part: SKIN — DAMAGED (NR 3 SLAT) · airframe 67,177 hrs · 11,021 cycles

LEFT WING NR 6 LEADING EDGE SLAT HAS A FOUR INCH LONG BY THREE QUARTER INCH DEEP PIECE OF FIBERGLASS MISSING FROM THE LOWER EDGE CLOSE OUT PANEL. [08-08-07] REPAIRED BY BACKSHOP 273 MECHANIC. REPAIRED PER SHOP MM AND INSPECTED. RETURNED TO SERVICE.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 66,973 hrs · 10,987 cycles

EEL LIGHT RT AISLE TORN LOOSE AT BUSINESS CLASS GALLEY. FOUND CONNECTORS DISCONNECTED AND TRANSPARENT COVER APPR 8 INCHES TOO SHORT. RECONNECTED PLUGS, APPLIED INTERIM REPAIR TO PROTECT. REPAIR DOES NOT OBSTRUCT LIGHTED PORTION OF STRIP. NEEDS TRANSPARENT COVER CUT TO PROPER LENGTH TO REPAIR.

Part: CONTROL VALVE — MALFUNCTIONED (APU) · airframe 66,957 hrs · 10,980 cycles

APU SHUT DOWN ON START, ATTEMPTED 2 STARTS, BOTH FAILED WITH FAULT INDICATION. [07-20-07] REPLACED APU SURGE CONTROL VALVE PER MM 49-53-01-401. ACCOMPLISHED MAIN ENG START PER JRH. OP CHECKS SATISFACTORY.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 66,572 hrs · 10,915 cycles

FLT CREWS REPORTED INTERIOR EMERGENCY LIGHTS ON RIGHT SIDE TURNS ON INTERMITTENTLY IN FLIGHT, THE LIGHTS ARE FROM ROWS 19-27 ON THE RIGHT SIDE. [SUP 06-06-07] REPLACED BATTERY PACK.

Part: COVER — WRONG PART (EMERGENCY LIGHT) · airframe 65,947 hrs · 10,805 cycles

EEL LIGHTING AT ROWS 1&2 RT FOUND TORN UP AND DAMAGED. FOUND EEL CABLES DAMAGED DUE TO IMPROPER CABLE COVER. ORDERED & INSTALLED COVER STRIP OF PROPER LENGTH AND END PIECES AS WELL. OP CHECKS OK.

Part: CHILLER — MALFUNCTIONED (GALLEY) · airframe 65,838 hrs

F/A'S REPORTED C/B'S IN AFT GALLEY POPPED. F/A'S IN MID CABIN REPORTED SMELL PRIOR TO C/B POPPING. [SUP 4-20-07] ALL CART CONTROLLER CB'S REPORTED POPPED AT SAME TIME. RESET CB'S. RAN CART CONTROLLERS FOR 5 MINUTES EACH. COULD NOT REPEAT PROBLEM. SUSPECT POWER SURGE. MID GALLEY ODOR DUE TO C31 CHILLER. CHILLER OPERATES LOUDLY AND CAUSING ELECTRICAL ODOR. NEEDS NEW CHILLER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 65,827 hrs · 10,773 cycles

AFT CARGO PIT AT BS 1197+132 TO BS 1219 AT STR 36L SKIN AT LAP SPLICE & CIRCUMFERENTIAL JOINT IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRICATED & INSTALLED REPAIR FILLER AND 3 EACH DOUBLERS.

Part: FLOORBEAM — DAMAGED (BS 654) · airframe 65,827 hrs · 10,773 cycles

DOUBLE DRILLED FIGURE 8 HOLES ON FLOORBEAM UNDER CABIN FLOOR AT BS 654+22, RBL 66 TO RBL 77, 2 PLACES. MAJOR REPAIR ACCOMPLISHED: FABRICATED AND INSTALLED 2 EACH FREEZE PLUGS AND REPAIR STRAPS.

Part: WEB — CRACKED (RT WING) · airframe 65,827 hrs · 10,773 cycles

RIGHT WING LEADING EDGE CAVITY, WEB CRACKED AT LES 588. DAMAGE TO WING FIXED LEADING EDGE NOSE BEAM WEB. AFFECTED SRM REPAIR PROCEDURE. VERIFIED CRACK CONTAINED BY STOP DRILLS PER HFEC NDT 51-00-19, PRT 6. FABRICATED REPAIR PARTS AND INSTALLED PER SRM 57-41-13. A/C READY FOR SERVICE.

Part: FLOORBEAM — DAMAGED (BS 654 RBL 77) · airframe 65,827 hrs · 10,773 cycles

ELONGATED HOLE ON FLOORBEAM AT BS 654+88, RBL 77.0. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF UPPER CHORD FLANGE. FABRICATED & INSTALLED CHORD ANGLE AND SPLICE STRAPS.

Part: SEAT TRACK — GOUGED (BS 488 LBL 11) · airframe 65,827 hrs · 10,773 cycles

MAIN CABIN SEAT TRACK GOUGED AT BS 488 AND LBL 11. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF SEAT TRACK AND EXISTING FWD REPAIR SPLICE AT BS 422. FABRICATED NEW SEAT TRACK AND REPAIR SPLICES.

Part: FLOORBEAM — CORRODED (BS 1562) · airframe 65,827 hrs · 10,773 cycles

AFT GALLEY AREA, MAIN FLOORBEAM STA 1562, RBL 48 AREA, TOP BEAM FLANGE CORRODED AND BLEND OUT EXCEEDS LIMITS. MAJOR REPAIR ACCOMPLISHED: CUT-OUT DAMAGED AREA. FABRICATED & INSTALLED UPPER CHORD ANGLE SPLICE SECTION.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 65,827 hrs · 10,773 cycles

RIGHT SIDE STA 280 FLOORBEAM HAS CORROSION AND BLEND-OUT EXCEEDS LIMITS. MAJOR REPAIR ACCOMPLISHED: REMOVED SECTION OF T-CAP. FABRICATED & INSTALLED NEW SECTION OF T-CAP CHORD.

Part: STRINGER — CRACKED (BS 1210-1219) · airframe 65,827 hrs · 10,773 cycles

AFT PIT STR 36L AT STA 1210 TO 1219 IS CORRODED. MAJOR REPAIR ACCOMPLISHED: FORMED NEW STRINGER SECTION. INSTALLED NEW SECTION WITH SPLICES, ANGLES AND CHORD.

Part: SEAT TRACK — CRACKED (BS 785) · airframe 65,827 hrs · 10,773 cycles

MAIN CABIN SEAT TRACK CRACKED AT BS 785 AND RBL 56. REMOVED DAMAGED SEAT TRACK SECTION AND FABRICATED SPLICE SECTION AND SPLICE CHANNELS AND INSTALLED PER SRM 53-00-52, DETAIL IV AND V, PG 206 AND SRM 51-40-2. SUSPECT COMBINATION OF SERVICE CART LOADING AND PAX/ FLIGHT ATTENDANT TRAFFIC.

Part: SEAT TRACK — FRACTURED (BS 745-758) · airframe 65,827 hrs · 10,773 cycles

FRACTURED SEAT TRACK SCALLOPES AT RBL 88.0, STA 745 TO 758. *S/D* REPLACED SEAT TRACK SECTION REF SRM 51-40-02. FABRICATED TRACK PER BOEING AC DWG. A/C READY FOR SERVICE. SUSPECT SERVICE CART DAMAGE COMBINED WITH FLIGHT ATTENDANT/ PAX TRAFFIC.

Part: SLIDE — BROKEN (RT OVERWING) · airframe 65,827 hrs · 10,773 cycles

RIGHT OVERWING SLIDE PACK UNLACE TRIGGER IS BROKEN OFF. REPLACED SLIDE. A/C RETURNED TO SERVICE. SLIDE PROBLEM ROOT CAUSE: UNLACE TRIGGER FITTING BROKEN BY SIGNIFICANT IMPACT.

Part: INSULATION — BURNED (BS 1365 S28L) · airframe 65,827 hrs · 10,773 cycles

AFT CARGO COMP HEAT DUCT BURNED INSULATION BLANKETS. BLANKETS CONTACT AFT CARGO COMPARTMENT HEAT DUCT IN AFT CARGO PIT, BS 1365 AND BETWEEN STR 28L TO STR 32R, (2 PIECES OF INSULATION). REPLACED & CHKD POSITION OF 2 PIECES OF INSULATION IN A/C BELLY NEAR AFT CARGO COMP HOT AIR DUCT. POSITIONED BLANKETS SO THEY DO NOT CONTACT HEATER DUCT. OK FOR SERVICE. SUSPECT DUCT RUN HOT WHEN CREW SELECTS MAX TEMP TO AFT CARGO COMPARTMENT.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 63,833 hrs · 10,444 cycles

NR 2 ENG COMPRESSOR STALL IN FLIGHT. ENG RECOVERED AND CONTINUED OPERATING. RECOVERED AND CONTINUED OPERATING. PRIOR TO STALL, ENG POWER WAS DECELERATING. ACCOMPLISHED BOROSCOPE OF NR 2 ENGINE, REPLACED ELECTRONIC ENGINE CONTROL, REPLACED IPCV VALVE, HPSOV, HIGH PRESSURE CONTROLLER. POST REPAIR RUNS AND OPS CHECKS WERE GOOD.

Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 62,759 hrs · 10,290 cycles

EMERG EXIT SIGN ABOVE COCKPIT DOOR STAYS ON CONTINUOUSLY. LIGHT ASSY CIRCUIT BOARD DAMAGED. REPLACED LIGHT ASSY, CHECKS OK.

Part: CONE — DELAMINATED (LT ENGINE) · airframe 62,734 hrs · 10,287 cycles

RETURN TO FIELD DUE TO LT ENGINE COMPRESSOR STALL. COMPRESSOR SURGE WAS CAUSED BY A DELAMINATION OF THE FAN SPINNER CONE. KEVLAR AND FIBERGLASS FROM THE SPINNER ENTERED THE CORE, AND DAMAGED NUMEROUS FAN BLADES. PWA SERVICE BULLETIN PW4ENG 72-594 INTRODUCES A NEW STRENGTHENED CONE CONE THAT REDUCES THE PROBABILITY OF DELAMINATION. THIS CONE WAS PRE-SB 72-594.

Part: LATCH — WORN (CABIN)

NR 3 LATCH EDGE MARGIN BEYOND LIMITS. REPLACED LATCH, IAW B767 MM 25-65-98.

Part: PUMP — OVERHEATED (HYDRAULIC SYS) · airframe 60,188 hrs · 9,855 cycles

CANCELLED DUE TO INBOUND HYDRAULIC PUMP OVERHEAT AND LOSS OF HYDRAULIC SYSTEM PRESSURE. MAINTENANCE REPLACED RIGHT ENGINE HYDRAULIC DRIVEN PUMP AND CASE DRAIN AND PRESSURE FILTERS. PERFORMED ENGINE RUN AND REQUIRED OP CK. ALL OK.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 59,972 hrs · 9,820 cycles

FOUND SMALL AREA OF ELECTRICAL ARCH DAMAGE TO VERTICAL FRAME RT FLANGE APPROX 1.5 INCHES ABOVE BASE.

Part: LATCH — ODOR (PAX DOOR) · airframe 48,605 hrs · 7,947 cycles

ACRID AND BURNING RUBBER ODOR ON THE FLIGHT DECK. THE SOURCE OF THE ODOR WAS THE FLIGHT DECK DOOR LATCH ASSEMBLY. REPLACED THE LATCH ASSEMBLY AND THE SYSTEM OPS CHECKS GOOD.

Part: SKIN — DENTED · airframe 48,014 hrs · 7,853 cycles

EXTERNAL LOWER FUSELAGE SKIN HAS DENT AT BS 654 + 66, STRINGER 31R. MAJOR REPAIR ACCOMPLISHED. REPAIRED WITH DOUBLER AND FILLER.

Part: SPAR — CRACKED (RT PYLON) · airframe 48,014 hrs · 7,853 cycles

RT PYLON, STA 180 JUST FORWARD OF WING FRONT SPAR, UPPER SPAR WEB IS CRACKED IN WEB RADIUS. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEB WITH DOUBLER ANGLE.

Part: SPAR — CRACKED (NR 1 PYLON) · airframe 48,014 hrs · 7,853 cycles

NR 1 PYLON, AFT UPPER SPAR WEB, IS CRACKED AT CORNER OF FEED THROUGH CUT-OUT. MAJOR REPAIR ACCOMPLISHED W/DOUBLER AND STIFFENERS.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 45,616 hrs · 7,438 cycles

LEFT ENGINE CONTROL MESSAGE DISPLAYED ON EICAS IN FLIGHT AND ENGINE, REVERTED TO IDLE SPEED.

Part: WIRE — DAMAGED (CABIN) · airframe 44,386 hrs · 7,210 cycles

EEL STRIP IN FRONT OF SEAT 1E NOT OPERATING. REPAIRED DAMAGED POWER FEED PER GNMM 2-0-15-5. OPERATIONALLY CHECKED NORMAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,935 hrs · 6,971 cycles

FLOORBEAM AT BODY STATION 347, BL 48 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER ON FLOORBEAM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 42,935 hrs · 6,971 cycles

CABIN FLOORBEAM CRACKED AT STATION 303, LBL 57. MAJOR REPAIR ACCOMPLISHED. INSTALLED T-CAP AND DOUBLER ON FLOORBEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,935 hrs · 6,971 cycles

CORROSION ON FLOORBEAM AT STATION 1188 TO 1197, RBL 38, AFT CARGO COMPARTMENT. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW T-CAP SECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,935 hrs · 6,971 cycles

FORWARD PIT, FS 588, RBL 42, CARGO FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR ON FLOORBEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,935 hrs · 6,971 cycles

FLOORBEAM CORRODED AT STATION 1197, RBL 15, AFT CARGO COMPARTMENT. MAJOR REPAIR ACCOMPLISHED. INSTALLED T-CAP AND DOUBLER REPAIR ON FLOORBEAM.

Part: HANDLE — STUCK (MLG) · airframe 40,410 hrs · 6,548 cycles

UNABLE TO RAISE GEAR HANDLE WITHOUT USING OVERRIDE.

Part: O-RING — CUT (OIL COOLER VALVE) · airframe 37,029 hrs · 5,914 cycles

NR 1 ENGINE IFSD (IN FLIGHT SHUT DOWN) DUE TO OIL LEAK AT LP20 FUEL OIL COOLER VALVE ADAPTER AND PACKING. DIVERTED TO LIM. *S/D* FOUND FUEL OIL COOLER BYPASS VALVE ADAPTER FITTING (P/N 227435) LOOSE AND O-RING (AS3208-06) CUT, (REF IPC 79-21-00A-005C PG1 ITEMS 220 AND 230). LOOSE FITTING WAS FOUND CORRECTLY SAFETY WIRED. NO INDICATION OF MAINTENANCE IN THIS AREA SINCE ENGINE INSTALLATION. NO PREVIOUS INDICATION OF HIGH OIL CONSUMPTION ON THIS ENGINE. REPLACED O-RING AND ADAPTER FITTING.

Part: WIRE — FAILED (VIDEO UNIT) · airframe 35,950 hrs · 5,725 cycles

RTF, AMBER ALERT. BURNING SMELL IN CABIN, MOSTLY AROUND SEAT 1C. *S/D* VDB SMELLS BURNT. REPLACED SEAT 1C VDB, OPS CHECK GOOD.

Part: TUBE — CRACKED (GEARBOX OIL) · airframe 35,888 hrs · 5,713 cycles

EN ROUTE TO SCL SHUT DOWN LEFT HAND ENGINE DUE TO OIL PRESSURE FLUCTUATIONS. DIVERTED TO GYE. *S/D* ANGLE GEARBOX OIL PRESSURE TUBE (LP09) FAILED BEHIND THE FORWARD B-NUT. REPLACED THE OIL LINE AND SUPPORTIING CLAMPS. ENGINE WAS REPLACED AFTER FERRY FLIGHT ,TO TEST FOR POTENTIAL HIGH VIBRATION IN THE ANGLE GEARBOX. PRATT WHITNEY WILL RELEASE SERVICE BULLETIN THIS YEAR TO ADD SUPPORT BRACKETS AND CLAMPS. TEST CELL RESULTS PENDING. NO INDICATION OF EXCESSIVE OR UNUSUAL GEARBOX VIBRATION.

Part: BATTERY CHARGER — FAILED (BATTERY COMPT)

MAIN BATTERY CHARGER EICAS MSG DISPLAYED. RETURNED TO MIA. *S/D* REPLACED BATTERY CHARGER, SYSTEM OP CHECK GOOD.

Part: EEL STRIP — INOP (CABIN)

EMERGENCY ESCAPE PATH LIGHTING INOP AT AFT GALLEY BETWEEN DOORS NR 2 LEFT AND NR 2 RIGHT. REPLACE LIGHT STRIP. CHECKS O.K.

Part: BLEED VALVE — MALFUNCTIONED (NR 2 ENGINE)

ABORTED TAKEOFF DUE TO NR 2 ENGINE BLEED VALVE PROBLEM. REPLACED HI-STAGE VALVE.