N662UA

Part: SKIN — CORRODED (ZONE 100) · airframe 121,456 hrs · 18,522 cycles

IT WAS FOUND CORROSION ON THE SKIN (P/N 146T3241-12) AT THE DRAIN HOLE AREA LOCATED BETWEEN STA 1540 AND 1562 & STR 39LH AND 39RH. MANENT SOLUTION WITH INSPECTION REQUIREMENTS THAT MUST BE ACCOMP ON OR BEFORE THE AIRCRAFT REACHES 37,500 TOTAL FLIGHT CYCLES. AC FLIGHT CYCLES. LISHED AS PER PART 2 OF THE LATEST REVISION OF EC/RA 5360-01874 COMPLISH REPEATED INSPECTIONS AT INTERVALS NOT TO EXCEED 12,000 FUSELAGE SKIN BETWEEN STA 1540 AND STA 1562 & S-39L AND S-39R AT THE DRAIN HOLE LOCATION WAS REPAIRED AT GIG. THIS REPAIR IS PER OK TO INITIATE DIP AS PER EC/RA 5360-01874. FUSELAGE SKIN BETWEEN STA 1540 AND 1562 & STGR39L AND STGR39R AT DRAIN HOLE CORROSION PERFORMED INTERIM REPAIR AS PER ECRA: #5360-01874

Part: STRINGER — DAMAGED (ZONE 100) · airframe 121,456 hrs · 18,522 cycles

BULK CARGO COMPARTMENT WAS FOUND TOOL MARK AT STGR 38LH BETWEEN STA 1562/1582. (NR 2236807)

Part: STRINGER — CORRODED (ZONE 100) · airframe 121,456 hrs · 18,522 cycles

BULK CARGO COMPARTMENT WAS FOUND CORROSION AT STGR 39LH BETWEEN STA 1540/1562. (NR 2231086) UPGRADE OF ATTRIBUTES PERFORMED REPAIR AT STRINGER 39LH AS PER SRM 53-00-03-2R-2 TYPE III AND TABLE III DETAIL IV .

Part: SKIN — DAMAGED (ZONE 100) · airframe 121,456 hrs · 18,522 cycles

THERE ARE OLD SCRIBE MARKS ON EXTERNAL SKIN OF FUSELAGE, LOCATED BETWEEN STA 654 PLUS 110/STA 785.9 AND BETWEEN STR20LH/36LH. FOR REFERENCE SEE SRM 53-30-01-0I-1 FIG 1, SHEET 2(ITEM 3) AND SHEET 4(ITEM 6). IS A PERMANENT SOLUTION WITH INSPECTION REQUIREMENTS THAT MUST B 7363 ON OR BEFORE THE AIRCRAFT REACHES 37,500 TOTAL FLIGHT CYCLE ,000 FLIGHT CYCLES. IS A PERMANENTSOLUTION WITH INSPECTION REQUIREMENTS THAT MUST B 7363 ON OR BEFORE THE AIRCRAFT REACHES 37,500 TOTAL FLIGHT CYCL 12,000 FLIGHT CYCLES. E ACCOMPLISHED PER PART 2 OF THE LATEST REVISION OF EC/RA 5330-0 S. ACCOMPLISH REPEATED INSPECTIONS AT INTERVALS NOT TO EXCEED 12 E ACCOMPLISHED PER PART 2 OF THE LATEST REVISION OF EC/RA 5330-0 E S. ACCOMPLISH REPEATED INSPECTIONS AT INTERVALS NOT TO EXCEED LH FUSELAGE SKIN BETWEEN STA 654 + 110 / STA 720 AND S-20L / S-2 LH FUSELAGE SKIN BETWEEN STA 654 + 110 / STA 720 AND S-20L / S-2 8L - SCRIBE LINES AND SCRATCH WERE REPAIRED AT GIG. THIS REPAIR 8L - SCRIBE LINES AND SCRATCH WERE REPAIRED AT GIG. THIS REPAIR REF ECRA 5330-07363: THIS REPAIR IS A PERMANENT SOLUTION WITH TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTION REQUIREMENTS THAT MUST BE ACCOMPLISHED PER PART 2 OF THE LATEST REVISION OF EC/RA 5330-07363 ON OR BEFORE THE AIRCRAFT REACHES 37,500 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEATED INSPECTIONS AT INTERVALS NOT TO EXCEED 12,000 FLIGHT CYCLES". DIP 53-DIP . PERFORMED INSPECTION IN ALL STEPS OF THIS MAJOR REPAIR AS PER EC/RA 5330-07363 PART 1. PERFORMED LH FUSELAGE SKIN BETW

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 121,456 hrs · 18,522 cycles

INSPECTING BODY BELLOW AFT CARGO FLOOR WAS FOUND CORROSION SIGNS ON FRAME SURFACE, STA 1197, STRINGER 36L.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 121,456 hrs · 18,522 cycles

INSPECTING THE BODY BELLOW THE AFT CARGO FLOOR WAS FOUND SIGNS OF CORROSION ON THE FRAME SURFACE, STA 1197/110 , STRINGER 34L.

Part: PRESSURE BLKHD — DENTED (ZONE 100) · airframe 121,456 hrs · 18,522 cycles

DURING CLEAN PROCESS WAS FOUND STA 1582.0 PRESSURE BULKHEAD WITH DAMAGE LOCATED IN DOME WEB. REPAIR IS A PERMANENT SOLUTION WITH INSPECTION REQUIREMENTS. REVISION OF EC/RA 5380-01408 ON OR BEFORE THE AIRCRAFT REACHES ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 OF THE LATEST 37,500 TOTALFLIGHT CYCLES. DENT AND GOUGE ON THE BULKHEAD DOME WEB BETWEEN STA 1582 AND STA 1605.5 AT LBL 13.5 AND WL 150 WERE INSPECTED/REPAIRED AT GIG.

Part: SKIN — CRACKED (ZONE 200) · airframe 121,456 hrs · 18,522 cycles

DURING HFEC INSPECTION OF THE FASTENER OPEN HOLE, WAS FOUND A CRACK LENGTH 0.040" AT THE FWD SERVICE DOOR CUTOUT AFTER LOWER CORNER.

Part: PANEL — MISSING (NACELLE) · airframe 120,256 hrs · 18,366 cycles

PDA 2 ON ETOPS WALKROUND FOUND PANEL 446BR MISSING. PYLON PANEL 446BR FITTED, AMM REF 54-53-01-404-007 FOR INSTALLATION. PARTS USED: 76-5453-3-0063,QTY :1

Part: CONTROL MODULE — DEFECTIVE (E/E BAY) · airframe 119,790 hrs · 18,301 cycles

STAB TRIM LIGHT CAME ON AFTER T/O WITH FLAPS OUT. WITH FLAPS UP EICAS WENT OUT LEFT AND RIGHT EICAS COMPUTERS. PERFORMED FIM TASK 27-48FT809, FOUND COL TRIM SW FAULT BALL PERFORMED FIM TASK 27-48FT809, COMPLETED TEST 30 MCPD TEST, TEST PRESENT ON RT SAM, NO FAULTS PRESENT ON LT SAM. 64 SP BRK/ FLAP XDCR TEST, TEST 65 STAB TRIM TEST, ALL TESTS PASSED, NO FAULTS. WIRING CHECK BETWEEN LEFT AND RIGHT SAMS AND M525 AT M525 (D667B). NO SHORTS TO GROUND, NO WIRING DEFECTS FOUND. ACCOMPLISHED FIM TASK 27-48 FAULT TREE 809 AT BLOCK 23. ACCOMPLISHED WIRING CHECKS PER WDM 27-41-11 AND 27-41-21, BETWEEN PIN D11 AT M10181 (D881A)AND D11 (D883A) @ M10182. WIERS HAVE GOOD CONTINUITY BETWEEN PLUGS ( D665B) AT M524 PIN C11 AND REFERENCE LOGPAGE 7762720 FOR CORRECTIONREMOVED AND REPLACED SAM 525 REF: AMM 27-09-00-422-008. NEEDS INSTALLATION TEST REF: AMM 27-09-00-742-064 STEP G " STABILIZER TRIM/AILERON LOCKOUT MODULE TEST. PERFORMED STABILIZER TRIM/AILERON LOCKOUT MODULE SAM TEST. PER AMM 27-09-00-742-064 STEP G. TEST PASS AND AIRCRAFT REMAINS FULL CAPABILITY.

Part: RELAY — INOPERATIVE (LAVATORY) · airframe 118,860 hrs · 18,178 cycles

LAV SYS 2 FLUSH CB R-35 POPED ONLY 3 LAVS WORKING R&R LAV FLUSH CONTROL RELAY (K2311) IAW WDM 38-32-11. PERFORM OPS CHECK OF LAV SYSTEM IAW 38-32-00/201, OPS CHECK GOOD. BREAKER NOT POPPING OUT. PARTS USED: 99-2332-3-0034,QTY :1. RNWY TURN OFF CD POPPED N-6 PER GMM 05-30-05 C/B N6 PULLED AND COLLARED. REQUESTING ITEM TO BE PLACED ON MEL DUE TO RUN WAY TURN OFF LIGHT TRANSFORMER INOP, (PARTS IN AOG HOLD EWR) DDP C/W CB N6 COLLARED. ITEM PLACED ON MEL APPROVED MEL 3342S. LEFT RUNWAY TURNOFF LIGHT INOP AFTER FURTHER T/S ITEM IAW WDM 33-42-21-1, FOUND LEFT TURNOFF LIGHT BULB AT FAULT. R & R LEFT TURNOFF LIGHT BULB AND CYCLED SWITCH VARIOUS TIMES. LIGHT WORKS OKAY, REMOVED YELLOW MEL PLACARD. A/C O.K. TO CONTINUE.

Part: WIRE HARNESS — CHAFED (LT ENGINE) · airframe 118,668 hrs · 18,150 cycles

L ENG FIRE LP 2 EICAS. THE LEFT ENGINE FIRE LOOP 2 HAS A FIRE OR THERE IS A FAILURE OUT PUT. INTERMITTENT STATUS MESSAGE NO EICAS MESSAGE ON ARRIVAL. L ENG LP 2 INTERMITANT DURING CRUISE. TALKED TO CREW, WRITE UP IS IN REFERENCE TO LOGPAGE 6821086. MESSAGE WAS INTERMITTANT ALSO IN FLIGHT, PILOTS REPORT MESSAGE WAS ACTIVE ON SECOND HALF OF FLIGHT BUT DISAPPEARED AFTER LANDING. FAULT ALREADY ON DEFERRAL. HISTORY REVIEWED AND NOTED FAULT OCCURED ON PREVIOUS DAY. FIM TASK 26-11 FAULT TREE 805 FOLLOWED TO BLOCK 30. DUE TO MESSAGE BEING INTERMITTEN, ENGINE FIRE DETECTION BITE PROCEDURE FIM TASK 26-11 FAULT TREE 804 FOLLOWED TO BLOCK 100B. DUE TO HISTORY AND TIME, MEL REQUESTED FOR FURTHER T/S. MEL REF 2611D COMPLIED WITH. DISPATCH DESK: 60 NAME: M.C. DATE: 15-JAN-24- MEL 2611D APPROVED INFO ONLY, REF LOGPAGE 6830655, MESSAGE IS INTERMITTENT IN FLIGHT BUT DISAPPEARS AFTER LANDING. **TECH SUPPORT UPDATE** CONTINUE WITH FIM 26-11 TREE 804. RECORD AND REPAIR FAULTS. ALSO REFERENCE SERVICE TIP IN AMM 26-11-00/101 FOR TROUBLESHOOTING AID. THANKS!! ORDLM BEHRENT SPOKE WITH TECH SUPPORT AND CONSULTED WDM, BROKEN PINS ARE NOT IS USE BY CARD, NOT CAUSE OF FAULT. CONTINUING WITH FIM 26-11 COMPLETED FIM 26-11 TASK 804 UP TO STEP 4, FAULT NEVER APPEARED AND DID NOT SWITCH SIDES UPON CARD SWITCH. COULD NOT OPEN MOTOR PLZ REF LP 6850915 FOR FINDINGS ON WIRING CHAFFING PERFORMED FIM 26-11 TASK 804. LED TO BLOCK 2 SHEET 1. UPON REMOVAL OF CARD FROM FILE FOUND 2 PINS SHEARED OFF IN CONNECTOR. PICTURES ATTACHED. TASK 804 PER TECH SUPPORT UPDATE. FOR FIM STEP 100A. WIRE CHAFFING UNDER FIRST CLAMP OF UPPR AFT LH ENG FIRE DETECTOR. PLZ SEE PICS ATTACHED ADDITIONAL PICTURE ORDERED NEW CLAMP P/N TA025041-02 THERE ARE 4 DAMAGED WIRES. W3506-501R-16, W3506-502R-16, W3506-504R-16, W3506-505R-16. TECH SUPPORT IS REQUESTING A PERMANENT REPAIR. NEW WIRE HAS BEEN RECEIVED. IN WORK REMOVING WIRES. PREVIOUS ENRTY WAS MADE IN ERROR. CORRECT WIRE NUMBERS ARE W3520-501R-16, W3520-502R-16, W3520-504R-16 AND W3520-505R-16. CONNECTOR D4154P HAS BEEN REMOVED. WIRES W3520-501R-16 AND W3520-504R-16 HAVE BEEN REMOVED AND NEW WIRES RAN. NEW WIRES TERMINATED AND PINNED WIRES ON CONNECTOR D4154P. INSTALLED CONNECTOR D4145P. LACED AND CLAMPED WIRES FROM D4145P TO TS681 FIRE DETECTORS. TERMINATED AND INSTALLED WIRES W3520-501R, 502R, 504R, AND 505R-16 ON TS681. REF WDM 26-11-11-1, SWPM TERMINATED AND INSTALLED WIRES W3520 - 505R & 502R ON LH SIDE OF TS681. REF WDM26-11-11-1 & SWPM 20-10-11 & SWPM 20-24-26 NEED TO BE TERMINATED, TIED AND CLAMP TIGHTENED. 20-10-11. SWPM 20-24-26. 1 PERFORMED ENG FIRE DETECTION SYSTEM TEST IAW AMM 26-11-00-735-076-003. ALL TEST SATIS.

Part: LIGHT — MISSING (GALLEY 227F/R&22) · airframe 118,179 hrs · 18,087 cycles

EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - 2X FWD GALLEY 227F/R & 228F/R EPL MISSING CLEAR LENSES. PLEASE REPLACE. BOTH EPL LENSES REPLACED IAW CMM 25-07-22.

Part: ELECTRONIC UNIT — FAULTY (SLAT/FLAP SYS) · airframe 117,827 hrs · 18,039 cycles

CONT. LE FLAP ASSYM AGAIN AT FL300 DOING 320 KTS.RTB AFTER SLOWING NORM IND ACFT LANDED @ 318000LBS, OVERWEIGHT LANDING NOT REQD. FLT CREW DEBRIEF: LE ASYM EICAS MSG WITH ASSOCIATED LE EDGE ANNUNCIATOR LT DURING CLIMB FOR 1MIN, THEN AGAIN AT 33000FT @ 320KTS FOR APPRO X 10MINS UNTIL DESCENDED TO 20000FT @ 240KTS. FLAP POS IND READ FSEU BITE C/O REF FIM TASK 27-51-00-815-809. NO CURRENT FAULTS AND SENSOR GROUND TESTS PASSED. PREVIOUS FAULTS SHOW LEG -0: TE FLAPS 27-51104, LE OUTBD ASYM 27-81021, FLAP POS XMTR 8 (M489) 27-51014. LEG -1: SECT 3 27-51-333, SECT 2 27-51222, XMTR 1 RECOMMEND DOWNLOADING FLT DATA TO CONFIRM IF SLATS WERE PHYSICALLY EXTENDED OR NOT, TO DETERMINE IF A SLAT POSITION INDICATION ISSUE EXISTS. IF INDICATION ISSUE ONLY, NO FLAP OVERSPEED INSPS REQUIRED. SEE LP 6014239 FOR PREVIOUS HIT. MAINT NOTE: CREW WERE ASKED IF THEY VISUALLY CONFIRMED THE INDICATED SLAT POSITION, THEY DID NOT. ALSO ASKED IF ACFT HANDLING WAS COMPROMISED OR ANY OTHER ABNORMAL PARAMETERS/INDS, ACFT HANDLED NORMAL AND ALL PARAMETERS NORMAL. FLAGGED FOR SDR EVENT PSEU BITE TEST CARRIED OUT IAW FIM 32-09 FAULT TREE 803. MSG 302 (TARGET LIGHT ON) APPEARS ON PSEU. MSG 302 INDICATES SLAT #10 I/B TARGET/SENSOR FAULT. ACTIONED UP TO BLOCK 4. NEXT STEP TO ACTION IS BLOCK 14A. 0.5 WHEN EICAS MSG PRESENT. FLT CREW NOR FLT ATTNDS VISUALLY CHE CKED IF LE SLATS WERE EXTENDED TO PROVE LE/TE POSITION INDICATIO N. ACFT AIR RETURN COMMENCED BEFORE CONSULTING TOMC 27-51013. LEG -1,-2,-3,-4,-5,-6,-7,-8,-9,

Part: CONNECTOR — UNKNOWN (UNKNOWN) · airframe 117,827 hrs · 18,039 cycles

THRUST MANAGEMENT SYSTEM A/T DISC LIGHT ILLUMINATED WITH AUTOTHR OTTLE ENGAGED IN (STATE MODE) MODE. THRUST REFERENCE MODE DISPLA Y ON EICAS & F/S POINTER DISPLAY ON EADI NORMAL IN VNAV PATH MODE ARRIVAL CREW INFORMATION: A/T DISCONNECTED IN CRUISE, RESET ACCOMPLISHED MCDP TMC TEST 2, TESTED PASSED. MCDP FLIGHT FAULTS ACCOMPLISHED. A/T DISCONNECTED AGAIN NO RESET, ALSO EEC 2 C1 FOR -1 FLIGHT LEG SHOWS A/T DISC EEC R PRIM/TMC MESSAGE. PIMU MESSAGE. SHOWING EEC A CHAN TMC I/F FAULT. REF FIM 71-01-TASK 820, 350-29 EEC A/B-CHAN TMC I/F. FIM 71-01-TASK 820, PARA B (5) FOR PIMU MSG 350-29 EEC A/B-CHAN 01 FAULT TREE 804. IF FAULT MSG PERSISTS, REPLACE EEC. PLS C/O M TMC I/F ON 1 CH (CH A) FOR RIGHT ENG ONLY ACCOMPLISHED. NO WIRIN CDP TEST 30 IN RAISED CAT LP TO RETAIN CAT STATUS. IDT RAISED FO G FAULT FOUND BETWEEN EEC CONNECTOR D11114 AND WING/STRUT DISCON R EEC/FADEC HARNESS CONNECTORS NECT D6382P. NO MSG PRESENT IN PIMU RECALL PROCEDURE REF FIM 71- ADD EMP:U405155 ALL EEC CONNECTORS CHECKED FOR FITMENT AND SECURITY POST WIRING CHECKS REF GMM 09-10-05 I. (21) (A) 4.

Part: ENGINE — FAULTED (#2 ENG) · airframe 117,810 hrs · 18,036 cycles

VIBRATION & STEADY HUM SOUND IN ACFT SINCE REACHING CRUISE ALT. ENTIRE FLT. LOUD HUMMING NOISE NOTABLE INCREASE IN EGT, FUEL FLOW. FLUCTUATING N2 AND VIB INDS. NOISE CHANGED WITH THROTTLE. ON ARRIVAL FOUND RT ENG INTAKE BLOW OUT PANEL UNLATCHED. WITH A SSOCIATED RT ENG EEC MODE EICAS ON LP 6083103, FOUND DEFECTS INCLUDING HPTCC MANIFOLD S FRACTURED & VARIOUS SENSE LINE CLIPS BROKEN. BOROSCOPE INSP OF HPT & LPT REQD WITH DETAILED INSP OF LPT OUTER TRANSITION DUCT. MAN UFACTURER RECOMMENDED INSP. OF HPT STAGE 2 THROUGH AP-11 BORO ACCESS. CTED HIGH VIB/RESONANCE AS THE CAUSE. INSP OF TAIL PIPE SHOW EVIDENCE OF METAL DEBRIS. R & R NR 2 ENG IAW T/C 63-7100-1-9800. LEAK & OPS CHKED GOOD.

Part: SENSOR — INTERMITTENT (SLAT SYS) · airframe 117,804 hrs · 18,035 cycles

LE SLAT ASYM CAME ON RETRACTING FLAPS 1 TO ZERO AND INDCATOR DISPLAY OUT OF UP ACCOMPLISHED FIM 27-81-00/301 LEADING EDGE (LE) SLAT SENSOR INDUCTANCE/RESISTENCE TEST AND IT WAS FOUND SENSOR S279 WITH INDUCTANCE 6.52 (OVER LIMIT). PERFORMED ADJUST REF. AMM SUBTASK 27-88-01-822-159 ITEM FOLLOW OK. ADD EMP:U409449,409438. LE FLAP ASYM RESOVED ITSELF CAME ON AGAIN FL220 330KIAS. OVERSPE ED OVER ALTITUDE. THE PHASE 1 INSPECTION WAS DONE AS PRECATIONARY DUE IT BEING REPORTED ,AS THE OTHER REPORT LOGPAGE 6014239 ,STATED THAT THE FLAPS AND SLATS WERE ALREDY UP IT WAS UNDERTOOD AND AGREED WITH MIKE , FROM TOMC , THAT THE PHASE 2 SHOULD BE DONE IF ANYTHING THIS LOG PAGE REFERS TO LOG PAGE 6014239 ACCOMPLISHED FIM 27-81-00/301 LEADING EDGE (LE) SLAT SENSOR INDUCTANCE/RESISTENCE TEST AND IT WAS FOUND SENSOR S279 WITH INDUCTANCE 6.52 (OVER LIMIT). PERFORMED ADJUST REF. AMM SUBTASK 27-88-01-822-159 ITEM ACCOMPLISHED PHASE I INPECTION REF AMM 05-51-08-212-001 NOT FOUND FAULT, ITEM FOLLOW OK. WAS FOUND , WHICH WAS NOT THE CASE . HOWEVER WE FOLLOWED THE PAHSE 1 JUST IN CASE AND ALSO THERE WAS A MISUNDERTANDING IN THE PILOT''S REPORT . IT WAS SUPPOSE TO BE LE SLAT INSTEAD OF LE FLAP . BASED ON THAT ONLY THE PHASE ONE INSPECTION WAS ACCOMPLISHED . FOLLOW OK. 409438. THE TOMC CONTROLLER AND SENIOR MANAGER CONCUR THAT THE AIRCRAFT CAN BE RELEASED BACK TO SERVICE AFTER EXPERIENCING A DIVERSION O R AIR TURN BACK DUE TO A MECHANICAL REASON LOCKED BY SYSTEM.

Part: CYLINDER — ACTIVATED (STA 1139) · airframe 117,793 hrs · 18,033 cycles

DURING THE ACTIVATION OF THE "OFF WING ESCAPE SYSTEM", ACCIDENTALLY THE SPOILER OVERRIDE ACTUATORS AND AND DOORS LATCH OPENING/SNUBBING ACTUATOR WERE FIRED. REMOVED AND REPLACED CYLINDER,ASSY, OFFWING EVACUATION REPLACED SPOILER OVERRIDE ACTUATOR SQUIB LH PN OUT 6023200-2 SN RAMP/SLIDE. PER AMM 25-65-02/401 OUT 016381 PN IN 6023300 SN IN 016532 AND RH PN OUT 6023200-2 SN ROTABLE PARTS CHANGE WAS INDICATED - TT # 1779100 SN OFF 9066 OUT 015210 PN IN 6023300 SN IN 016534 REF. AMM 25-65-19/401. ITEM OK. CYLINDER, ASSY, OFF 76-2565-9-9002 9066 ON 76-2565-9-9002 1953 REPLACED SPOILER OVERRIDE ACTUATOR SQUIB LH PN OUT 6023200-2 SN OUT 016381 PN IN 6023300 SN IN 016532 AND RH PN OUT 6023200-2 SN OUT 015210 PN IN 6023300 SN IN 016534 REF. AMM 25-65-19/401. ITEM OK.

Part: EXTINGUISHER — UNKNOWN (LAVS) · airframe 117,141 hrs · 17,948 cycles

RAISING SDR FOR INCORRECT FITMENT OF COMPONENT PER TASK CARD 63-2620-1-2827. SDR RAISED FOR DISCOVERY OF INCORRECT FITMENT OF COMPONENT DURING TASK CARD 63-2620-1-2827 ON 15-JUL-23. TSAP RAISED.

Part: CONTROLLER — FAILED (MAIN CABIN) · airframe 113,727 hrs · 17,480 cycles

MID CABIN TEMP EICAS C THE MID CABIN SUPPLY DUCT TEMPERATURE IS MORE THAN 190 DEGREES F (88 DEGREES C); OR THE ZONE TEMPERATURE MID CABIN CHANNEL HAS A FAILURE OR THE SYSTEM IS OFF.REMOVED AND REPLACED THE MAIN CABIN ZONE TEMP CONTROLLER. ALL TEMPS NORMAL.CREW DIVERTED FROM ORD ON THE WAY TO LHR TO EWR WHEN THEY FOUND THEY COULD NOT CONTROL CABIN TEMP AND THE SECTIONS OF THE CABIN WHERE ALL DIFFERENT TEMPERATURES AND TOO UNCOMFORTABLE FOR AFFECTED PASSENGERS. SEE LOGPAGE 8957864

Part: NONE — NONE (NA) · airframe 112,617 hrs · 17,319 cycles

AIRCRAFT REPORTED TO BE TRANSMITTING ON GUARD FREQ (NO VOICE) GROUND MONITORING STATION REPORTS THAT NORMAL ATC COMS FROM AIRCRAFT BEING HEARD ON GUARD FREQ. REPLACED NO.1 TRANSCEIVER PER AMM 23-12-01-424-004 & REPLACED NO.2 (FO SIDE) AUDIO SELECTOR PANEL PER AMM 23-51-01-004-001. ACP RADIO CHECK OK. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1461022 SN OFF 0330 TT # 1652322 SN OFF 0480 SDR FOR THIS ITEM NOW COVERED ON NEWLY CREATED ITEM L/P 8128341. PANEL, AUDIO SE OFF 76-2351-9-9001 0330 ON 76-2351-9-9001 0307 TRANSCEIVER, VH OFF 99-2312-9-0004 0480 ON 99-2312-9-0004 9103

Part: SKIN — CORRODED (STA1205STR36L) · airframe 111,632 hrs · 17,165 cycles

REFER NRC L/P 9131558 FUSELAGE STA 1205 STR 36L STRINGER SECTION CUTOFF FOUND ATTACH SKIN CORROSION. TRANSFER REF NR LP 9131765 AND ORIGINATED BY V896890. AFTER REF NDT PART 6, 53-00-06 REPAIR INSP REQUIREMENTS ARE AS FOLLOWS PER SRM 53-00-01-2R-31 RPR 31 TABLE 203 ZONE A DETAIL II. INITIAL EXTERNAL DETAILED VISUAL INSP AT ACFT TOTAL FC 37500 W/ 3000 FC INTERVAL THERE FUSELAGE SKIN STA 1205 STR 36L SKIN REPAIRED AS PER SRM 53-00-01-2R-31 RPR 31 FIG 201 DETAIL II. 44.0008 ATTACHED COMPLETE TO ITEM 26..HAECO/HKG NRC 9131765, V897532, QC HX185167 ADD EMP:V897532 APPROVED FOR DIP REF SRM 53-00-01-2R-31 RPR31 WITH INITIAL TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTION AT 37500 TOTAL FLIGHT CYCLES WITH CONSECUTIVE REPEAT INPECTION EVERY 3000 FLT CYCLES QC REVIEWED QC REVIEWED INIT: 37500 TAFC (WILL ITO TO RIR -0650) RIR: 3000 FC...UK RECORDS UPDATE...UK

Part: STRINGER — CRACKED (STA1205S36L) · airframe 111,632 hrs · 17,165 cycles

AFT CARGO COMPT STA 1205 S-36L AREA FOUND CORROSION CRACK. TRANSFER REF NR LP 9131558 AND ORIGINATED BY V897013. AFT CARGO COMPT STRINGER 36L BETWEEN STA 1197+120VAND STA 1219 REPAIRED AS PER SRM 53-00-03 REPAIR 2 FIG 201. WORK ACCOMPLISHED BY MECHANIC V897532 INSPECTED BY V897008. ADD EMP:V897008 RII INSPECTED BY HX203084.

Part: NONE — CORRODED (STA 1285) · airframe 111,632 hrs · 17,165 cycles

AFT CGO COMPT STA 1285 LBL 24" FLOOR BEAM UPPER CHORD FOUND CORROSION CRACK. TRANSFER REF. HX NON-ROUTINE LP 9131773 AND ORIGINATED BY EMP NO. V896921 AFT CARGO COMPT STA 1285 LBL 20.5 - LBL 25.5 WL 123 FRAME INNER CHORD J SECTION REPAIRED AS PER EC/RA 5360-01617 REV-. WORK ACCOMPLISHED BY MECHANIC V905418 INSPECTED BY V897008. ADD EMP:V897008 RII INSPECTED BY HX135550.

Part: BEAM — ELONGATED (STA 544) · airframe 111,632 hrs · 17,165 cycles

B767-53-3-7141 CABIN STA 544 LBL 55-68 FLOOR SUPPORT HOLE FOUND ELONGATE. TRANSFER REF. NON-ROUTINE LP 9131173 AND ORIGINATED BY EMP V927004. CABIN BS 544 FLOOR BEAM UPPER CHORD BETWEEN LBL 55 AND LBL 88 REPAIRED AS PER EC/RA 5315-01163 REV-. ADD EMP:V896920 RII INSPECTED BY HX224337.

Part: NONE — NONE (STA 544 LBL) · airframe 111,632 hrs · 17,165 cycles

B767-53-3-7141 CABIN STA 544 LBL 55-68 FLOOR SUPPORT HOLE FOUND ELONGATE. TRANSFER REF. NON-ROUTINE LP 9131173 AND ORIGINATED BY EMP V927004. CABIN BS 544 FLOOR BEAM UPPER CHORD BETWEEN LBL 55 AND LBL 88 REPAIRED AS PER EC/RA 5315-01163 REV-. ADD EMP:V896920 RII INSPECTED BY HX224337.

Part: BEAM — NONE (RBL 10) · airframe 111,632 hrs · 17,165 cycles

B767-53-3-0166 CABIN - BS1500 RBL10 FLOOR SUPPORT HOLE ELONGATED AS MARK. TRANSFER REF. NON-ROUTINE LP 9131246 AND ORIGINATED BY EMP V896926. CABIN BS 1500 FLOOR BEAM UPPER CHORD RBL 10 REPAIRED AS PER SRM 53-00-51 REPAIR 2 FIG 201. ATTACHED FORM 44-0008 ITEM 1 TO ITEM 15 ACCOMPLISHED. ADD EMP:V896920 RII INSPECT IS OKAY. APPROVED BY HX 224337.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 107,252 hrs · 16,569 cycles

REF NR LP B767-06-3-7059 CABIN : STA 955 TO 975 RBL 30 CANTED PRESSURE DECK WEB FOUND CRACK CABIN STA 955 TO STA 975 RBL 30 CANTED PRESSURE DECK WEB INTERIM REPAIRED AS PER EC/RA 5358-01001 REV - PART 1.

Part: STRUCTURE — CRACKED (BS 1809) · airframe 106,996 hrs · 16,532 cycles

02MAR HKG CF -L :LH STA 1809 HORIZ INNER CHORD 1 EA FAST FN D CRK AT 8 O''CLK POS RUNNING TO EDGE.AREA REPAIRED PER EA 5312-0 1059 REV B OP9 STEP 1 AND SRM 53-80-08 REP 10 FIG 201 DET II.REP EAT INSPECTION AS PER SRM 53-80-08 REP 10 TBL 202, INSP THRESHOL D IS 37,000 FLT CYCLES AFTER AIRPLANE DELIVERY AND REPEAT INSP E VERY 6000 FLT CYCLES. BY- 240185 MAINT TEXT:WORK ACCOMPLISHED ON HAECO NRC MFT507121 BY V906028 AND INSPECTOR HX203175, :WORK PERFORMED ON HAECO N RC MFT507121 BY V906028 AND RII INSPECTION BY INSPECTOR HX203175 ** MF6812 CREATED TO MONITOR ** ** MF6812 ADDED TO MONITOR ** RECORDS UPDATE AT CUTOVER....TW INIT: 37,000 TAFC (INIT WILL ITO TO RIR -7334) RIR: EVERY 6K FC.....TW ASSOCIATED CF9130 TO MF6812 QC REVIEWED QC REVIEWED QC REVIEWED REPEAT INSPECTION AS PER SRM 53-80-08 REP 10 TBL 202, INSP THRESHOL D IS 37,000 FLT CYCLES AFTER AIRPLANE DELIVERY AND REPEAT INSP EVERY 6000 FLT CYCLES.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 103,010 hrs · 15,998 cycles

EXTERIOR EMERGENCY LIGHT LEFT SIDE OF AIRCRAFT INOPERATIVE. REPLACED THE FUSES IN M738 CHARGER. OPS CHECKED NORMAL

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 103,010 hrs · 15,998 cycles

EXTERIOR EMERGENCY LIGHT AFT OF L2 DOOR INOP. REPLACED FUSES IN M738 CHARGER OPERATIONAL CHECK NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 103,010 hrs · 15,998 cycles

OVERHEAD EMERGENCY LIGHT AT SEAT ROW 19K INOPERATIVE. REPLACED THE LAMPS. OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 103,010 hrs · 15,998 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 4K INOPERATIVE. REPLACED THE LAMPS, OK FOR SERVICE.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 101,715 hrs · 15,819 cycles

SEAT 17AB TO 32AB CEILING EMERGENCY LIGHT FOUND DIM, THE POWER SUPPLY BATTERY M737 WAS REPLACED AND OPS TESTED NORMAL IAW AMM 33-51-07.

Part: SKIN PANEL — CRACKED (NR 2 PYLON) · airframe 101,715 hrs · 15,819 cycles

NR 2 PYLON SKIN PANEL AT THE 422AL PANEL CUT-OUT CRACKED. INTERIM REPAIR WAS ACCOMPLISHED PER ECRA 5430-02135 PART 1. ITEM 2 OF THE ECRA NEED TO ACCOMPLISH A PERMANENT REPAIR PER ECRA 5430-01235 PART 3 BEFORE 20 OCT 19.

Part: SKIN — DAMAGED (BS 1269-1277) · airframe 101,715 hrs · 15,819 cycles

DAMAGE FOUND TO THE BELLY SKIN JUST UNDER THE AFT CARGO DOOR GOUGED AT BS 1269 & 1277 BETWEEN STRINGERS 37R AND 38R. REPAIRED IAW SRM 53-00-01, REPAIR 14, FIG 201, DETAIL II.

Part: BATTERY — FAULTY (EMERGENCY LIGHTS) · airframe 101,715 hrs · 15,819 cycles

SEATS 22-26 AISLE EMERGECNY LIGHT FOUND DIM. THE POWER SUPPLY BATTERY M1209 WAS REPLACED AND OPS TESTED NORMAL IAW AMM 33-51-07.

Part: TEAR STRAP — DAMAGED (BS 654) · airframe 101,715 hrs · 15,819 cycles

TEAR STRAP DEFORMED. REPAIRED IAW ECRA 5330-06211, REV-, PART 1.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 101,715 hrs · 15,819 cycles

POWER SUPPLY M1210 FOUND INOPERATIVE, THE POWER SUPPLY M1210 WAS REPLACED AND OPS TESTED NORMAL IAW AMM 33-51-07.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 101,715 hrs · 15,819 cycles

NR 2 PYLON PANEL 426BR SKIN FOUND CRACKED. THE SKIN WAS REPAIRED IAW SRM 54-53-01, REPAIR 6, FIG 201, DETAIL III.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 101,715 hrs · 15,819 cycles

NR 1 PYLON SKIN PANEL 736BL FOUND CRACKED. THE SKIN WAS REPAIRED IAW SRM 54-53-01, REPAIR 7, DETAIL I, FIG 201.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 101,047 hrs · 15,726 cycles

3 EA EMERGENCY LIGHT IN CEILING ARE NOT WORKING AT LOCATION 1D 4D AND 24D. RT AISLE ROW 24D AISLE LIGHT OPS CK NORMAL DURING TEST, ROW 1D & 4D AISLE LIGHT. OPS CK NORMAL AFTER RECONNECTING SOCKET CONNECTOR.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 100,737 hrs · 15,684 cycles

EMERGENCY EXIT SIGN COVER IN LEFT AISLE DETACHED. SECURED THE SIGN COVER.

Part: ALTIMETER — STICKING (STANDBY) · airframe 100,447 hrs · 15,642 cycles

STBY ALTIMETER STICKING DURING CLIMB AND DECENT. REMOVED AND REPLACED STANDBY ALTIMETER IAW MM:34-13-06. OPS CHECKED GOOD.

Part: FUSE — BURNED (CABIN) · airframe 100,273 hrs · 15,619 cycles

FOUND 1ST CLASS EMERGENCY AISLE LIGHTING NOT OPERABLE. (ROWS 1,2 AND 3) FROM FLIGHT ATTENDANT PANEL. OPENED OVERHEAD CEILING PANEL FOR ACCESS TO BATTERY PACK. FOUND 1 BURNT FUSE. REPLACED ALL 4 FUSES BITE CHECK FROM BATTERY PACK PROVES GOOD. DOES NOT OPERATE WHEN TESTING FROM FLIGHT ATTENDANTS PANEL. THESE ROWS TEST AT THE P-40 PANEL REF WDM33-51-15 AND 33-51-21. PERFORMED TEST REF AMM 33-51-00. ALL TEST GOOD AT THIS TIME.

Part: SEAT — INOPERATIVE (6B) · airframe 100,041 hrs · 15,589 cycles

BED MODE INOPERATIVE AT 6B PASSENGER SMELLED BURNED WHILE ATTEMPTING TO MOVE SEAT. SEAT INOPERATIVE RESET SEAT 6B, OPS NORMAL IAW AMM 25-25-00.

Part: SIGN — INOPERATIVE (CABIN) · airframe 99,404 hrs · 15,499 cycles

BOTH RIGHT SIDE OVER THE WING EMERGENCY EXIT DOORS ELECTROLUMINESCENT EXIT IDENTIFIER SIGN LIGHT INOP. T-S PER WDM 33-51-14 PG 1A S 1, FOUND BOTH EXIT DAIL, R+R EXIT LT'S OPN CHK GOOD PER AMM 33-51-00.

Part: WINDSCREEN — CRACKED (COCKPIT) · airframe 97,860 hrs · 15,290 cycles

FO FRONT WINDSCREEN SHATTERED AT CRUISE FL340. PERFORMED R1 WINDOW REMOVAL PER AMM AMM 56-11-01. R&R WHCU.

Part: CONTROLLER — MALFUNCTIONED (APU) · airframe 97,581 hrs · 15,249 cycles

AFTER RT ENGINE GENERATOR DRIVE DISCONNECTED, APU NO START ON FIRST ATTEMPT, 2ND ATTEMPT STARTED AND RAN FOR ONE MINUTE THEN AUTO SHUTDOWN WITH EICAS MESASGE APU OIL QTY, T/865-15. DIVERTED MAINTENANCE CHECKD APU OIL IAW MM 12-13-04(301). FOUND APU OIL LEVEL BELOW THE APU FULL MARK ON SIGHT GAGE AND EVIDENCE OF OIL WETNESS IN APU COMPARTMENT. SERVICED APU TO FULL, R & R APU CONTROLLER IAW AMM 49-62-00, OPS CHECKED GOOD. INSTALLED NEW GEN PHASE LEADS AMM 24-21-07

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,650 hrs · 14,981 cycles

MAIN DECK, STATION 302, RBL 13 - 16, FLOORBEAM FOUND CORROSION. CORROSION FLOORBEAM REPAIR IAW SRM 53-00-51 FIG 201 REPAIR 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,650 hrs · 14,981 cycles

MAIN DECK CABIN STATION 287, LBL 11 FLOORBEAM FOUND CORROSION. CORROSION FLOORBEAM REPAIRED AT BS 287, LBL 32 TO RBL 90 IAW SRM 53-00-51 REPAIR 1 FIG 201.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 95,650 hrs · 14,981 cycles

LEFT STATION 1809 HORIZONTAL INNER CHORD, ONE EACH FAST FOUND CRACKED, AT 8 O CLOCK POSITION, RUNNING TO EDGE. AREA REPAIRED IAW EA 5312-0 1059 REV B OP 9 STEP 1 & SRM 53-80-08 REP 10 FIG 201.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 95,650 hrs · 14,981 cycles

LEFT STATION 1809 HORIZONTAL INNER CHORD, ONE EACH FOUND CRACK AT 8 O CLOCK POSITION RUNNING TO EDGE. AREA REPAIRED IAW EA 5312-0 1059 REV B OP9 STEP 1 & SRM 53-80-08 REP 10 FIG 201 DET II.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 95,650 hrs · 14,981 cycles

MAIN DECK STATION 303, LBL45 FLOORBEAM PANEL FLANGE FOUND CRACK. MAIN DECK CABIN STATION 303, LBL 45. FLOORBEAM UPPER CHORD CRACKED AREA, REPAIRED IAW SRM 53-00-51 REPAIR 2 FIG 201 DETAIL I.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,650 hrs · 14,981 cycles

MAJOR REPAIR, STATION 346, FLOORBEAM UPPER CAP CORRODED, BETWEEN RBL 28 & RBL 53. DAMAGE CUT OUT & REPAIR ACCOMPLISHED IAW 53-00-51 REPAIR 1 DETAIL 5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,650 hrs · 14,981 cycles

MAJOR REPAIR, STATION 324 FLOORBEAM UPPER CAP CORRODED, AT RBL 54. CORROSION REMOVED & REPAIR ACCOMPLISHED IAW SRM 53-00-51 REPAIR 2 DETAIL 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,650 hrs · 14,981 cycles

CABIN STATION 1584, LBL 21 FLOORBEAM HAS CORROSION. CORROSION R & R ACCOMPLISHED IAW SRM 51-10-02 & SRM 53-00-51 REPAIR 2 FIG 201 DETAIL I.

Part: BATTERY — DISCHARGED (CABIN) · airframe 93,874 hrs · 14,750 cycles

AFT LIGHT LAVATORY EMER ESCAPE PATH LIGHT INOPERATIVE. R & R ESCAPE PATH BATTERY AT AFT LT. OPERATIONS CHECK FOUND NORMAL IAW AMM 33-51-07.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 93,355 hrs · 14,679 cycles

EMERGENCY SLIDE LIGHTS AT DR 1 RT & DR 2 RT ARE INOPERATIVE. REPLACED LAMPS FOR LIGHT ASSEMBLY AT DR 1 RT & DR 2 RT IAW AMM 33-51-06.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 92,311 hrs · 14,537 cycles

CABIN CREW REPORTED FUMES DURING CLIMB THRU 6000 FT. REPORTS RANGE FROM ELEC TO OIL. FUMES REPORTED MID CABIN AREA. R & R FILTERS IAW IPC 21-25 -01. PERFORMED IN-DEPTH INSPECTION OF ACFT SYSTEMS IAW FIM 21-00 -801 & AMMS 71-00-00, 79-21-10 & 05-51-56. CORRECTED APU OVER SERVICING & SEVERAL AREAS OF OIL ON ENGS. ENG RUNS & CHECKS COMPLETE. NO DISCREPANCIES NOTED, CLEARED FOR SERVICE.

Part: APU — FAILED (APU BAY) · airframe 91,286 hrs · 14,394 cycles

APU NO START IAW 2862022. APU ALTITUDE NO START COLD SOAKED. APU SHUTDOWN AFTER REACHING 95 PERCENT SPEED AFTER 10 SECONDS. FL 360 FIRST ATTEMPT RAN FOR 4 MINUTES, SECOND FAULT DURING SPOOL UP, THIRD FAULTED RIGHT AFTER 100. REPLACED APU IAW TOD 49-11-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 91,222 hrs · 14,386 cycles

EMERGENCY EXIT FLOOR EEL INOPERATIVE AT AFT GALLEY. REPLACED BATTERY M1556 IAW MM 33-51-07. FLOOR EEL AT AFT GALLEY, OPERATIONS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 91,222 hrs · 14,386 cycles

EMERGENCY EXIT FLOOR EEL INOPERATIVE BETWEEN AFT RT LAVATORIES. REPLACED BATTERY M1556 IAW MM 33-51-07. FLOOR EEL OPERATIONS CHECKED NORMAL.

Part: PROBE — UNKNOWN (PITOT/STATIC SYS) · airframe 89,965 hrs · 14,191 cycles

GROUND RETURN DUE TO CAPTAIN'S PITOT PROBE.

Part: SKIN — DENTED (LE SLAT) · airframe 89,891 hrs · 14,177 cycles

NUMBER 11 SLAT PREVIOUS FIELD REPAIRS FOUND ON LE 68 FRM INBD REQUIRES RE-EVALUATION. SKIN DENT FOUND AT OOS 909 EXTENDING AFT ON NOSE BEAM WAS REPAIRED IAW ECRA 5743-01174.

Part: FUSE — BLOWN (BATTERY CHARGER) · airframe 89,891 hrs · 14,177 cycles

EMERGENCY EXIT LIGHTING INOPERATIVE AT CEILING SEAT ROW LOCATION 26 - 27AB. R & R BATTERY CHARGER FUSE IAW AMM33 51 07. OPERATIONAL CHECK GOOD AT THIS TIME.

Part: SKATE ANGLE — CRACKED (LT WING) · airframe 89,891 hrs · 14,177 cycles

CRACK EXTENDING 2.5 INCHES COMMON TO NR 1 PYLON INBD SKATE ANGLE FOUND AT AFT EDGE BEND RADIUS. CRACK MEASURED 3.620. REMOVED SECTION OF SKATE ANGLE & FABRICATED REPAIR PARTS IAW DWG 112T7001- 45. ACCOMPLISHED IAW ECRA 5724-01015 CAT A RPR IAW SRM51-00-06.

Part: FMU — FAULTY (NR 1 ENGINE) · airframe 88,893 hrs · 14,044 cycles

AFTER NR 1 ENG START EEC C1 STATUS MESSAGE APPEARED. REPLACED NR 1 ENG FMU. ACP TEST 3, LEAK & OPERATIONS CHECKED GOOD, NO MESSAGE.

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS) · airframe 88,529 hrs · 13,996 cycles

REPLACE RT ENGINE PRSOV DUE TO LOW BLEED PRESS DURING ENG RUNS.

Part: SENSOR — FAULTY (BLEED AIR SYS) · airframe 88,529 hrs · 13,996 cycles

REPLACE THE LT ENG FAN AIR TEMP SENSOR DUE TO AIR SUPPLY BITE MODULE FAULTS AFTER ENG RUNS. REMOVED FAN AIR TEMP SENSOR IAW 36-11-17-401 THROUGH STEP 2. COMPLETED INSTALLATION OF FAN AIR TEMP SENSOR.

Part: CONTROLLER — FAULTY (BLEED AIR SYS) · airframe 88,529 hrs · 13,996 cycles

REPLACE THE LT ENG HIGH STAGE CONTROLLER M7191 DUE TO ASM BITE MODULE FAULTS AFTER ENG RUNS. REPLACED NR 1 ENGINE HIGH STAGE CONTROLLER IAW AMM.

Part: TRANSMITTER — FAULTY (BLEED AIR SYS) · airframe 88,529 hrs · 13,996 cycles

DUCT PRESS SPLIT. DURING POWER RUNS USING ASM BLEED MONITORING SOFTWARE, FOUND PRESS OUT OF PRESS RELIEF VLV WAS NORMAL & MATCHED THE LT SIDE AT ALL POWER SETTINGS BUT EICAS INDICATION WAS READING 20-30 PSI LOW COMPARED TO THE ACTUAL PRESS RELIEF VLV OUTPUT PRESS. REPLACE THE RT DUCT PRESS TRANSMITTER M1089.

Part: SENSOR — FAULTY (NR 2 ENGINE) · airframe 88,529 hrs · 13,996 cycles

NEW FAN AIR TEMP SENSOR PLACED IN COCKPIT BEHIND FIRST OFFICER`S SEAT. REPLACED FAN AIR TEMP SENSOR ON NR 2 ENG. DURING OPERATIONS CHECK AIR SUPPLY BITE MODULE LIGHT STAYS ON. THE BOX WILL NOT TEST. REMOVED CANNON PLUG FROM NEW FAN AIR SUPPLY TEMP SENSOR & BOX TESTED GOOD. NEED TO REPLACE FAN AIR TEMP SENSOR AGAIN BECAUSE BAD FROM STOCK MR36112-192 ON-OFF-102.

Part: EXCITER — FAULTY (RT ENGINE) · airframe 88,495 hrs · 13,992 cycles

RT ENG NO START ON IGNITION 2, NORMAL START IN BOTH. REPLACED RT ENG 2 IGNITION EXCITER BOX. ENG WAS RUN IAW JRH, OPERATIONS CHECKED NORMAL.

Part: ISOLATION VALVE — CRACKED (HYDRAULIC SYS) · airframe 88,004 hrs · 13,933 cycles

LT FLIGHT CONTROL SHUTOFF VALVE BODY CRACKED DRAINED LT HYD SYS. R & R LT HYD ISOLATION VALVE, ALL OPERATIONS CHECKED & LEAK CHECKED GOOD AT THIS TIME.

Part: HEATER — INOPERATIVE (COCKPIT) · airframe 87,792 hrs · 13,902 cycles

CAPTAINS SHOULDER HEATER INOPERATIVE IN LOW & HI. REPLACED CAPTAINS SHOULDER HEATER IAW MM 21-45-12.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,728 hrs · 13,894 cycles

RT NR 1 DOOR THE EMERGENCY SEGMENT LIGHTING IS NOT WORKING. RT DOOR ONE EMERGENCY PATH SEGMENT LIGHT ASSEMBLY REPLACED & OPERATION TESTED NORMAL IAW AMM.

Part: CONNECTOR — DIRTY (CABIN) · airframe 87,728 hrs · 13,894 cycles

MID LAVATORY LT SIDE EMERGENCY AISLE LIGHT INOPERATIVE. CONNECTOR OF BATTERY M155 CLEANED & RECONNECTED TEST CARRIED OUT FOUND NORMAL.

Part: COMPUTER — INOPERATIVE (AUTOPILOT SYS) · airframe 87,704 hrs · 13,889 cycles

CAPTAIN FLIGHT DIRECTOR INOPERATIVE. REPLACED LT FCC IAW MM. ACCOMPLISHED CAT III TEST IAW MM. ACFT RETURNED TO FULL CAT III CAPABILITY.

Part: FEEDER CABLE — DAMAGED (AFT GALLEY) · airframe 87,634 hrs · 13,876 cycles

AFT GALLEY, CABLE P53 DAMAGED. R & R AFT GALLEY CABLE P53.

Part: ATTACH ANGLE — CRACKED (NACELLE) · airframe 87,634 hrs · 13,876 cycles

INBOARD ATTACH ANGLE FOR INNER PAN ASSY ON LOWER AFT STRUT FAIRING ATTACH AREA ANGLE IS CRACKED, PN 313T3355-288, REMOVED FROM ACFT.

Part: WEB — CRACKED (LWR AFT STRUT) · airframe 87,634 hrs · 13,876 cycles

INNER WEB ASSY AT LOWER AFT STRUT FAIRING CRACKED.

Part: FAIRING — CRACKED (NACELLE) · airframe 87,634 hrs · 13,876 cycles

REMOVED AFT LOWER STRUT FAIRING FOR INTERNAL STRUCTURAL CRACKS. AFT 2 SECTIONS ON NR 2 ENGINE 5 AND 6 FOR REPAIRS.

Part: ACTUATOR — FAULTY (NR 1) · airframe 87,478 hrs · 13,855 cycles

LEFT ENGINE EEC C1 STATUS DISPLAYED ECM DOWNLINKS SHOW MSG 35 1-25 CHANNEL A & B SVA FD BK FAIL. CHECKED PIMU FOR MESSAGES TO CONFIRM. ACCOMPLISHED FIM WIRING CHECKS BEFORE REPLACING SVA. REPLACED SVA AMM, OPS CHECKED GOOD. NO MESSAGES.

Part: TRANSCEIVER — FAULTY (HF SYSTEM) · airframe 87,418 hrs · 13,847 cycles

HF TRANSMISSION AND RECEPTION ARE INOPERATIVE, WEAK, GARBLED INTERMITTENT. AT ALL CREW STATIONS. R & R HF TRANSCEIVER.

Part: TRANSCEIVER — INOPERATIVE (NR 1 VHF) · airframe 87,291 hrs · 13,831 cycles

NR 1 VHF COMMS TRANSMISSION AND RECEPTION INOPERATIVE AT ALL CREW STATIONS. LT VHF RADIO INOPERATIVE. REPORTED AS UNREADABLE BY MANY GROUND STATIONS. ALL CREW STATIONS AFFECTED. R & R LT TRANSCEIVER IAW AMM, OPS CHECK GOOD.

Part: KEEPER — DAMAGED (NR 1 NACELLE) · airframe 87,220 hrs · 13,822 cycles

NR 1 NACELLE FOUND AFT LATCH KEEPER BROKEN ON CORE COWL OTBD. REPLACED AND ADJUSTED LATCH KEEPER IAW AMM. OK.

Part: SMOKE DETECTOR — NO TEST (E/E BAY) · airframe 86,691 hrs · 13,751 cycles

EQUIPMENT COOLING TEST, SMOKE LIGHT ON P5 AND EICAS ADVSRY MESSAGE FAILS TO APPEAR DURING TEST. REPLACED E&E SMOKE DETECTOR, CHECKED OK, IAW MM.

Part: HYDRAULIC LINE — DAMAGED (HYDRAULIC SYS) · airframe 86,604 hrs · 13,741 cycles

HYD QTY DISPLAY IS BLANK. POS 2 (01=L,02=R,03=C). FRM CODE 29-33-04-XX. CREW COMMENTS: RIGHT QTY IND .49RF ALSO SATUS MSG R HYD SYS MAINT COMPLIED WQRH. FOUND HYDRAULIC TUBE AT RT ENGINE PYLON DAMAGED, REF IPC 29-11-00-002A INDEX 386. REPLACED HYD TUBE AND HYDRAULIC LEAK CHECK PERFORMED REF AMM 29-00-98- 0601, NO LEAKS FOUND. SERVICED RT HYD SYSTEM TO FULL. COMPARED RT HYD INDICATION BETWEEN REFUELING STATION AND FLT DECK BEFORE, DURING AND AFTER SERVICING AND FOUND FLT DECK INDICATION WORKING PROPERLY.

Part: COMPUTER — FAULTED (NR 1) · airframe 86,452 hrs · 13,722 cycles

HAVE "FLAP LIMIT" SHOWING ON BOTH ADI WITH AMBER F-S INDICATION. TURNED OFF A-T, F-S INDICATION NOW INDICATING NORMAL. REPLACED TMC, CARRIED OUT TESTS ON MCDP 02 05 30 AND 40 REF MM. ALL PASSED NO FAULTS RECORDED. A-C RETURNED TO CATIII TMC IS A LUFTHANSA BORROWED PART PART# 105E7026G3 SNBR 92B1352. BOX PLACED IN BULK CARGO. PART REQUIRED TO REPLACE IS MR22300.

Part: CABLE — LOOSE (REHEATER) · airframe 86,343 hrs · 13,707 cycles

CABIN TEMP TOO HOT & UNCONTROLLABLE. FOUND RESTRAINT CABLES LOOSE ON ELBOW AT REHEATER. TIGHTEN AND SECURED HARDWARE ON RESTRAINT CABLE. OPERATED PACKS AND LEAK CHECK ALL INDICATIONS NORMAL, NO LEAK NOTED.

Part: WIRE HARNESS — FAILED (NR 2 ENGINE) · airframe 86,343 hrs · 13,707 cycles

NR 2 ENGINE EGT MESSAGE. REPLACED RIGHT AFT EGT HARNESS AND 'J' BOX. RAN ENGINE AND FOUND NORMAL OPS AND INDICATIONS

Part: PRESSURE SWITCH — FAILED (FUEL SYSTEM) · airframe 86,293 hrs · 13,701 cycles

LEFT AFT FUEL PUMP LIGHT IN SWITCH STAYS ILLUMINATED WITH SWITCH ON. REPLACED PRESSURE SWITCH.

Part: BOLT — FAILED (NR 3 WHEEL) · airframe 86,205 hrs · 13,691 cycles

NR 3 FRONT BRAKE UNIT HAS SUSTAINED DAMAGE FROM BROKEN WHEEL TIE BOLT. REPLACED BRAKE UNIT.

Part: COMPUTER — FAULTY (AUTOPILOT SYS) · airframe 86,120 hrs · 13,680 cycles

F/OS ADI HAS FD FLAG AND NO FD CROSSHAIRS WORKS ON THE LEFT FLIGHT DIR INST SEL. FLT FAULTS NO INFC FCC R MCDP, NO LAND 3 FCCR-FCCL AND FFCR-FFCC. ACCOMPLISHED FIM 22-00-0 2 FIG 110 AND STILL HAS FAULT AND FCC R TEST FAILS. REPLACED FCC R PER MM AND PASSED ALL TESTS AND FD FLAG NO LONGER PRESENT. RAISED SMC ITEM FOR CAT 3 TEST.

Part: VALVE — FAILED (COCKPIT TEMP) · airframe 85,454 hrs · 13,595 cycles

FLIGHT DECK TEMP INOPERATIVE ILLUMINATED IN AUTO. FLT DECK TEMP OPERATES NORMALLY IN MANUAL. FOUND FLIGHT DECK CABIN TEMP SENSOR CLOGGED WITH LINT. CLEANED SENSOR AND ACCOMPLISHED FLIGHT DECK TRIM AIR VALVE OPERATIONAL CHECK. NO FURTHER FAULTS NOTED AT TEMP CONTROLLER. REPLACED FLIGHT DECK TRIM AIR VALVE.

Part: CONTROL PANEL — FAULTY (HF COMM) · airframe 85,344 hrs · 13,580 cycles

TROUBLESHOOTING LOG 002 REF FIM 23-11-00 WE SWAPPED THE HF TUNING PANELS AND GOT THE RIGHT HF TO WORK WITH THE LEFT PANEL. NEED TO REPLACE TUNING PANEL MR23146. REPLACED CAPT CONTROL PANEL.

Part: SEAL — LEAKING (RUDDER PCU) · airframe 85,344 hrs · 13,580 cycles

HYD FLUID LEAKING FROM RUDDER DRAIN HOLE. HEAVY LEAK TO RUNNING LEAK WITH HYD SYSTEM PRESSURIZED. DURING LEAK CHECK FOUND LEFT RUDDER PCU HAD NO SYSTEM PRESSURE. FOUND RIGHT RUDDER PCA LEAKING FROM ROD-END SEAL WITH CENTER SYS PRESSURIZED, DID NOT LEAK WITH SINGLE SYS HYD 090070. REPLACED RIGHT SYS RUDDER PCA.

Part: PANEL — FAULTY (COCKPIT) · airframe 85,310 hrs · 13,575 cycles

FUEL TEMP BLANK ALL QUANTITY INDICATORS NORMAL. REPLACED FUEL TEMP INDICATOR PANEL, OPS CHECK GOOD.

Part: AMPLIFIER — INOPERATIVE (SATCOM) · airframe 85,310 hrs · 13,575 cycles

SATCOM HIGH GAIN ANT INOPERATIVE. NO TIME TO T/S. REPLACED HIGH GAIN AMPLIFIER, OPS CHECK GOOD.

Part: O-RING — LEAKING (TRIM SWITCH) · airframe 85,277 hrs · 13,571 cycles

HYDRAULIC FLUID LEAKING FROM STAB COMPARTMENT DRAIN ON BELLY. FOUND LEFT STAB TRIM CONTROL MODULE BRAKE PRESSURE SWITCH LEAKING 30 DROPS MIN. REPLACED O-RING SEALS. LEAK CHECKED GOOD. CLEANED AND FLUSHED COMPARTMENT OF RESIDUAL FLUID.

Part: EEC — FAULTY (LT ENGINE) · airframe 89,051 hrs · 14,065 cycles

LT ENG EEC C1 STATUS MESSAGE ON CONTINUOUS. PLACED ON MEL DF849, HAS HISTORY. BITE OF PIMU FOR LEG 5 SHOWS EEC CH AB FAULT CAT 1. FMU CROSS CHECK FAIL BOTH CHANNELS. NEED TO CHECK FMU & HARNESS IAW 71-PIMU INDEX PG 62V & 62W. TROUBLE SHOT IAW FIM 71-PIMU MESSAGE INDEX PG 62V, 62W, STEPS A THRU E1. NO FAULTS NOTED R & R ENG 1 EEC IAW AMM 73-21-04 & TS IAW FIM 71-PIMU MESSAGE INDEX PG 62V & 62W. RAN ENG 1, GOT MESSAGE LT ENG CONT & LT EEC C1.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 84,882 hrs · 13,518 cycles

EMERGENCY EXIT SIGN AT DOOR 2L ILLUMINATED. CREW REPORTS PATH LIGHTING ADJACENT TO TOILET AREA IS ALSO ILLUMINATED. REPLACED POWER SUPPLY M1561 AS PER MM AND CHECKED CONNECTOR ON M1560 ALL OPS AND TEST NORMAL.

Part: NUT — LOOSE (LIGHT SWITCH) · airframe 84,767 hrs · 13,504 cycles

EMERGENCY LIGHTS FLICKER ON AND OFF IN COACH ONLY WITH SWITCH IN ARMED. FOUND EMERGENCY LIGHT SWITCH BACK NUT LOOSE, CAUSING WHOLE SWITCH & GUARD TO BE LOOSE. RESECURED SWITCH AND ACP EMERGENCY LIGHT TEST PER MM.

Part: SENSOR — INOPERATIVE (FUEL SYSTEM) · airframe 84,760 hrs · 13,503 cycles

FUEL TEMP INOPERATIVE. REPLACED TEMP SENSOR PER MM, OPS NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 84,712 hrs · 13,494 cycles

DURING LOADING, GROUND STAFF FOUND DAMAGE ON FUSELAGE SKIN AFT OF REAR CARGO DOOR. DAMAGE BURNISHED AND PROTECTED THEN INSPECTED IAW SRM 53-00-01 TAB 1 PG 102. LOC STR 31 STN 1373, GOUGE DEPTH 0.006IN, DENT DEPTH 0.047IN. AREA INSIDE NO DAMAGE. WITHIN SRM LIMITS. REEVALUATED DAMAGED AREA, DENT L=2.15" X W=2.0" X D=.050", AY=42.5, REMAINING THICKNESS OF MATERIAL IS .175", WITHIN LIMITS REF SRM 53-00-01 TAB1, AD1. ACCOMPLISHED DENT DOT PROCEDURES, NO FURTHER ACTION REQUIRED.

Part: SCREW — LOOSE (COCKPIT DOOR) · airframe 84,688 hrs · 13,491 cycles

PILOTS TRAPPED IN COCKPIT AND DOOR WILL NOT OPEN BOTTOM SCREW IS STICKING UP IN DOORWAY. SECURED LOOSE SCREW TO DOOR THRESHOLD. SECURED COCKPIT LOWER DOOR PANEL TO DOOR. OPS NORMAL.

Part: SMOKE GOGGLES — DAMAGED (COCKPIT) · airframe 84,176 hrs · 13,419 cycles

FIRST OFFICER GOGGLES ELASTIC STRAP IS STRETCHED OUT NEEDS REPLACING. REPLACED GOGGLES.

Part: BELLCRANK — DAMAGED (LT ELEVATOR) · airframe 83,283 hrs · 13,299 cycles

ELEVATOR PCA BELLCRANK FUNCTIONALLY CHECK RIG OF ELEVATORS TO IDENTIFY ANY OUT OF RIG CONDITION CAUSED BY SHEARED OR PARTIALLY SHEARED RIVETS IN THE ELEVATOR POWER CONTROL ACTUATOR INPUT LINKAGE ASSEMBLIES. FOUND SHEARED RIVET IN LT OTBD ELEV BELLCRANK. REMOVED AND REINSTALLED REWORKED BELLCRANK IAW AMM. ADJUSTED ELEVATOR CONTROL SYSTEM PER ROUTINE CARD 5232R430

Part: FAILSAFE — CORRODED (BS 1562 S39L-39R) · corrosion level 2 · airframe 83,283 hrs · 13,299 cycles

BS 1562 FAILSAFE BETWEEN STR 39L-39R FOUND CORRODED. ACCOMPLISHED CLEAN-UP, DVI AND NDT OF OPEN HOLES COMMON TO REPAIR. NO CRACKS FOUND. FABRICATED AND INSTALLED REPAIR FILLER, ANGLE, SPLICE WEB AND SHEAR TIE.

Part: BELLCRANK — DAMAGED (ELEVATOR PCA) · airframe 83,283 hrs · 13,299 cycles

ELEVATOR PCA BELLCRANK FUNCTIONALLY CHECK RIG OF ELEVATORS TO IDENTIFY ANY OUT OF RIG CONDITION CAUSED BY SHEARED OR PARTIALLY SHEARED RIVETS IN THE ELEVATOR POWER CONTROL ACTUATOR INPUT LINKAGE ASSEMBLIES. REFERENCE AMM 27-31-98 PAGE SERIES 601. MANDATED BY AD 2001-04-09 AND NOT EXTENDABLE. FOUND SHEARED RIVET IN LT OTBD ELE BELLCRANK. REMOVED AND REINSTALLED, REWORKED BELLCRANK IAW B767 AMM 27-31-06. ADJUSTED ELEVATOR CONTROL SYS PER ROUTINE CARD 5232R430.

Part: BELLCRANK — DAMAGED (LT ELEVATOR) · airframe 83,283 hrs · 13,299 cycles

LEFT ELEVATOR OUTBOARD PCA BELLCRANK SHOWS INDICATION OF SHEARED RIVET. REMOVED RIVETS FROM LT OTBD BELLCRANK AND REPLACED WITH SOLID RIVETS PER SB767-27-0186. BELLCRANK REMOVED AND THE REWORKED BELLCRANK INSTALLED ON NR CARD 5232N00169.

Part: STRUCTURE — DENTED (CARGO DOOR) · airframe 83,283 hrs · 13,299 cycles

BULK CARGO DOOR DENTED AT FWD LWR CORNER. EVALUATED DENT AND FOUND OUT OF SRM LIMITS. CUT OUT DAMAGE AND ACCOMPLISHED HFEC OF CUT OUT AND HOLES COMMON TO REPAIR REF EA PT67-52-001 AND ECRA 5230-01875. NO CRACKS. ACCOMPLISHED INSURANCE CUT. FABRICATED AND INSTALLED EXTERNAL DOUBLER REPAIR REF EA AND ECRA.

Part: SHEAR TIE — CORRODED (BS 1280) · corrosion level 2 · airframe 83,283 hrs · 13,299 cycles

AFT CARGO COMPARTMENT SHEAR TIE ATTACHMENT BETWEEN FRAME AT BS 1280 AND BL 0 FOUND CORRODED. REMOVED CORRODED SHEAR TIE AND FOUND MATERIAL LOSS OUT OF SRM LIMITS. FABRICATED AND INSTALLED NEW SHEAR TIE SRM 51-40-02. MAJOR REPAIR

Part: STRINGER — CORRODED (BS 1540 S39R) · corrosion level 2 · airframe 83,283 hrs · 13,299 cycles

CORROSION FOUND IN AFT CARGO COMPARTMENT AT BS 1540 AT STRINGER 39R. REMOVED DAMAGED STRINGER SECTION. FABRICATED AND INSTALLED NEW STRINGER SECTION AND STRINGER SPLICE REPAIR PARTS REF SRM53-00-03 FIG 201 REPAIR 2 DETAIL IV.

Part: OXYGEN MASK — MISINSTALLED (LEFT) · airframe 83,283 hrs · 13,299 cycles

ALL LEFT O2 MASKS IMPROPERLY PACKED. REPACKED ALL LEFT O2 MASKS PER AMM.

Part: INDICATION SYS — MALFUNCTIONED (POTABLE WATER) · airframe 83,087 hrs · 13,274 cycles

POTABLE WATER SHOWS 140 GALLONS AND NO WATER COMING OUT OF FAUCETS DURING LAST HOUR OF FLIGHT. ON ARRIVAL, POTABLE WATER SHOWING,110 GALLON. SERVICED TO MAXIMUM, INDICATION SHOWING 140 GALLON, MAXIMUM. POTABLE WATER SYSTEM OPS CHECK NORMAL ON GROUND WITH APU RUNNING. INDICATOR ADJUSTED PER MM, CKS OKAY.

Part: WARNING LIGHT — FALSE ACTIVATION (ENGINE BLEED) · airframe 82,749 hrs · 13,225 cycles

DURING TAKEOFF UNDER 80 KNOTS PER QRH PACKS OFF, ENGINES BLEED SWITCH ON, NOTICED BOTH ENGINES BLEED OFF LIGHTS CAME ON.

Part: LAMP — FAILED (SMOKE DETECTION) · airframe 82,250 hrs · 13,158 cycles

E/E COOLING SYSTEM FAILS OPS CHECK. SMOKE LIGHT ON P5 PANEL FAILS TO COME ON WHEN P61 E-C TEST SWITCH IS ACTUATED AND HELD. ALSO, FWD EQUIPMENT SMOKE DETECTION FAILS TO APPEAR ON EICAS DISPLAY. CONFIRMED SMOKE LIGHT DOES COME ON DURING LIGHT TEST. RELAMPED DETECTOR, OPS CK OK

Part: RELAY — FAULTY (ELECTRICAL SYS) · airframe 81,686 hrs · 13,082 cycles

STANDBY POWER OPERATIONAL CHECK FAILS IN AUTO. WITH INV PWR TRU D11 CB OPEN, STBY BUS OFF LIGHT REMAINS ON AND EICAS MESSAGE STANDBY PWR BUS OFF LIGHT SHOWS ON UPPER DISPLAY. REF 'A' CHECK JOB 6-2005-B PAGE 3 ITEM 4. BY- 115803 :CONFIRMED THAT RELAY K113 IN THE P6-1 PANEL IS BAD BY SLAVING IN ANOTHER RELAY. FOUND RELAY K105 AC STBY PWR BAD IN P6 PANEL REF SSM24-33-01-101. REPLACED RELAY, OPS NORMAL.

Part: COMPUTER — FAULTY (AUTOPILOT SYS) · airframe 81,511 hrs · 13,057 cycles

RIGHT FD FAILED AND NO LAND 3 ASA. RIGHT FCC IAW MM & GROUND TEST PASSED. AC FULL CAT III STATUS.

Part: FAN — FAULTY (CABIN) · airframe 81,511 hrs · 13,057 cycles

EICAS MSG: 'L RECIR FAN' DISPLAYED & 'L RECIRC FAN INOP' LIGHT ILLUM, WITH SWITCH 'ON'. SLIGHT ELECT ODOR IN CABIN. SAMC TEXT: CREW WENT TO MAIN CABIN TO INVESTIGATE. UPON RETURN TO FLT DECK THE LEFT RECIRC FAN HAD QUIT WORKING. ODOR CLEARED AFTER FAN WAS SHUT DOWN. VERIFIED FAN INOP. ACP'D MEL REQUIREMENTS. RT RECIRC FAN OPS CHECK NORMAL. REPLACED LEFT RECIRC FAN, SEE SEQ- NBR 5112013.

Part: FAN — FAILED (RECIRCULATION) · airframe 80,711 hrs · 12,954 cycles

ON ARRIVAL, LEFT RECIRCULATON FAN FAILED WITH ASSOCIATED EICAS MESSAGE AND OVERHEAD LIGHT WITH BURNED ODOR IN COCKPIT. LEFT RECIRCULATION FAN CIRCUIT BREAKER ALSO FOUND TRIPPED.

Part: FAN — FAILED (CABIN) · airframe 80,711 hrs · 12,954 cycles

THREE EVENTS OF ONE MINUTE DURATION OF ELECRICAL ODOR THRU COCKPIT AND CABIN NO SMOKE. UNABLE TO LOCATE OR IDENTIFY SOURCE, ON LANDING OF ELECRICAL ODOR. RECIRCULATION FAN INOPERATIVE LIGHT ON. FOUND LEFT RECIRCULATION FAN CIRCUIT BREAKER TRIPPED ON P36 PANEL. REPLACED LEFT RECIRCULATION FAN PER MM. OPS TESTED BOTH LEFT AND RIGHT RECIRCULATION FANS PER MM. RAN BOTH PACKS WITH ENGINES AND APU, NO ODOR EVIDENT.

Part: LATCH — UNSECURE (LT NACELLE) · airframe 80,688 hrs · 12,951 cycles

ON PREFLIGHT F/O FOUND AFT LATCH OF LEFT ENGINE CORE COWL HANGING DOWN FOUND BROKEN KEEPER ASSY FOR LATCH. REPLACED AND ADJUSTED PER AMM.

Part: HEAT EXCHANGER — FAULTY (NR 2 IDG) · airframe 80,447 hrs · 12,915 cycles

RIGHT IDG VALVE STATUS MESSAGE DISPLAYED AT TOP OF DESCENT. PERFORMED BPCU BITE CHECK PER FIM 24-20-00. LAST FLT LEG NR 2 SHOWS COOLER VALVE WIRING FAULT. REPLACED NR 2 ENGINE IDG AIR OIL HEAT EXCHANGER AND VALVE PER MM.

Part: ACTUATOR — LEAKING (RUDDER) · airframe 80,447 hrs · 12,915 cycles

RUDDER RATIO CHANGER ACTUATOR LEAKING. REPLACED RUDDER RATIO CHANGER ACTUATOR. INSTALLED RRCA FAILED TEST. REINSTALLED ORIGINAL RUDDER RATIO CHANGER ACTUATOR PER MM. OPS CHECKED GOOD, NO FAULTS.

Part: RATIO CHANGER — LEAKING (RUDDER) · airframe 80,418 hrs · 12,911 cycles

LEFT SYSTEM HYDRAULIC QUANTITY DROPPED TO 0.47 OVERNIGHT. HYDRAULIC FLUID EVIDENT BELOW REAR OF AIRCRAFT. FOUND LEAK FROM RUDDER RATIO CHANGER. REPLACED RUDDER CHANGER AS PER MM AND PERFORMED LEAK CHECK ALL OK. RUDDER RATIO CHANGER IS A BRITISH AIRWAY 7 DAY LOAN PART, P-N 3790011-107 SN 0592 BA DOC NUMBER 83697561. CONTAINER IN LOB BOX. PART REQUIRED MR27210.

Part: AUDIO PANEL — FAILED (COCKPIT) · airframe 80,383 hrs · 12,907 cycles

NO AUDIO FOR ILS ON CAPTAIN'S SIDE. FAULT FOUND TO BE AUDIO SELECTOR PANEL CAPT. PANEL REPLACED AND TESTED PER MM, SYSTEM TESTS OKAY.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 80,383 hrs · 12,907 cycles

ROW 37 AND BACK THE FLOOR BOUNCED UP AND DOWN. ACCOMPLISHED CHECK PER FIM MM 52-35-00 FIG 113 AND RAISED ITEM FOR LUB JOB SMC6. INSPECTED FLOOR AND SEAT LOCKS AND ALL NORMAL. MOVEMENT WAS AC MOVEMENT DUE TO DOOR NEEDING LUBE.

Part: HINGE — LACK OF LUBE (AFT CARGO DOOR) · airframe 80,391 hrs · 12,908 cycles

DURING CLOSING AFT CARGO DOOR, OPERATION WAS ERRATIC (NOT SMOOTH) AT START OF DOOR LOWERING DUE TO ROD EYE END BOLTS REQUIRING LUBE JOB. LUBED AFT DOOR HINGE ASSY PER MM. DOOR STILL ERRATIC CLOSING. LUBED LOWER HINGE POINTS AFT CARGO DOOR.

Part: PUMP — FAULTY (HYDRAULIC SYS) · airframe 79,054 hrs · 12,721 cycles

C ADP LOW PRESS LIGHT ILLUMINATED IN AUTO. EICAS MSG DISPLAYED C HYD DEM PUMP. ADP PRESS IS NORMAL. FRM CODE 29-11-54-00. CREW COMMENTS: C HYD DEM PUMP EICAS & PRESS LT ON AFTER TAKEOFF. STAYED ON AFTER SW SELECTED TO ON. MAINT TEXT: REPLACED S28 PSI SWITCH AT CENTER HYD MODULE & TRIED ADP RESET, NO HELP. REPLACED ADP, OPS CHECK GOOD.

Part: WIRE HARNESS — FAULTY (LT ENGINE) · airframe 79,036 hrs · 12,718 cycles

LEFT ENGINE EEC MODE EICAS MESSAGE DISPLAYED. ECS MESSAGE DISPLAYED ARE LT ENGINE EEC MODE AND LT ENGINE PROBE HEAT. REMOVED AND REPLACED BLUE HARNESS REF WDM. EEC BIT CHECK NORMAL AND GROUND RUN NORMAL.

Part: PUMP — FAULTY (HYDRAULIC SYS) · airframe 79,004 hrs · 12,713 cycles

GEAR VERY SLOW TO RETRACT. BOTH CENTR ELEC PUMPS LOW PRESS ILLUM AND GEAR DISAGREE EICAS. FOUND DURING TROUBLESHOOT ADP PER FIM 29-11-00 FIG 109 ADP AUTO FUNCTION INOP. DEFERRED PER MEL. ADP MANUAL FUNCTION CHECKED GOOD. 06AUG IAD INF- :REPLACED OVERSPEED CARD AND ADP PRESSURE SWITCH S29. SEE SEQ 0042010 AND 0042009. TROUBLE SHOT DOWN TO ADP REF FIM 29-11-00 FIG 109 SHEET 2 BLOCK 24. REPLACED ADP AS PER MM.

Part: ACCESS PANEL — LEAKING (FUEL TANK) · airframe 78,709 hrs · 12,664 cycles

CONTINUOUS FUEL SEEP FROM LT DRAIN INBD OF NR 1 ENGINE. FUEL IS POOLING IN THE LT DRY BAY. CONTINUOUS FUEL SEEP FROM LT DRAIN INBOARD OF NR 1 ENGINE. FOUND FUEL LEAKING FROM UPPER FWD INBD ANGLE OF DRY BAY. REPAIRED SEALANT. LEAK CHECKED LEFT WING DRY BAY AND 2EA INBD FUEL TANK ACCESS PANELS AFTER SEALANT CURED 0730-13. FUELED LEFT MAIN TANK HAS NO LEAKS NOTED FROM DRY BAY OR FUEL ACCESS PANELS.

Part: ACM — FAULTY (AC BAY) · airframe 78,388 hrs · 12,619 cycles

ACM AND STDBY CONTRL NEED REPLACED. REPLACED LT PACK ACM PER AMM AND THE STBY PACK CONTROLLER PER AMM. PACK OPERATION NORMAL.

Part: A/C PACK — SHUTDOWN (LEFT) · airframe 78,321 hrs · 12,610 cycles

LEFT PACK DROPPED OFF SEVERAL TIMES ON ARRIVAL WITH POWER ABOVE FLT IDLE. REPLACED HIGH PRESSURE SHUTOFF VALVE PER MM. REPLACED HPC, RAN ENG OPS GOOD.

Part: CIRCUIT CARD — FAULTY (NR 1 EEC) · airframe 78,283 hrs · 12,604 cycles

NR 1 EEC MESSAGE. MESSAGE ERASED AT P61. REF FIM 73-21-00 PG 151 LEFT PIMU SHOWS T2-P2 PROBE HEAT CHAN A, AND CHAN B SHOWS EEC-PI MU MODE DISAGREE. OVERHEAD NR 1 EEC ALTERNATE SWITCH LIGHTS FLICKER ON AND OVERHEAD LIGHT IND FOR PROBES ALSO FLICKERED, INDICATION OCCURED WHEN PULLING AWAY FROM GATE. ACCPL 71-PIMU MESSAGE INDE X FOR PIMU MESSAGE EEC CH A-B T2 P2 PROBE HEAT MESSAGE. REPLACED LEFT ENGINE SPEED CARD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 78,280 hrs · 12,603 cycles

RT AFT OVERWING SLIDE EMERGENCY LIGHT NEAR AFT CARGO DOOR INOPERATIVE. RELAMPED, OP CHECKED GOOD.

Part: PUMP — LEAKING (NR 2 ENGINE) · airframe 78,257 hrs · 12,599 cycles

NR 2 ENGINE HYD PUMP LEAKING AT MATING SURFACES. REPLACED NR 2 EDP PER MM. GROUND RUN OKAY.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 78,249 hrs · 12,598 cycles

HI FLOW INHIBIT EICAS STATUS MESSAGE. REPLACED FLOW CONTROL VALVE.

Part: CIRCUIT CARD — FAULTY (LT ENGINE) · airframe 78,249 hrs · 12,598 cycles

LEFT ENG SPEED CARD IS FAULTY. REPLACED LEFT SPEED CARD.

Part: WIRE — CHAFED (CONTROL PANEL) · airframe 78,241 hrs · 12,597 cycles

FOUND CHAFED AND EXPOSED ELEC WIRES AT COCKPIT HYDR CONTROL PANEL. SPLICED WIRES IAW SWMP, MOIST RESISTANT. ALL SATIS NOW.

Part: SPLICE — DAMAGED (CABIN) · airframe 77,928 hrs · 12,549 cycles

RT AFT DOOR EMERGENCY LIGHT INOP. REPAIRED SPLICE AT EMERGENCY LIGHT L309 PER WD, OPS CHECK GOOD.

Part: STRUCTURE — DAMAGED (R1 DOOR) · airframe 77,924 hrs · 12,548 cycles

DOOR 1L DOOR HAS DAMAGE TO OUTER SLIDE BUSSLE ASSY. DOOR 1R HAS DAMAGE. REMOVED BUSSLE ASSY CHECKED SECURITY AND INTEGRITY OF DOOR SLIDE ASSY, NO DAMAGE NOTED. ACCOMPLISHED INTERIM REPAIR WITH TAPE TO BUSSLE ASSY. WILL NEED COMPOSITE REPAIR. WILL NEED 2 SHIFT SLOT TO CURE, PAINT AND REPAIR. DOOR 1L OKAY. DAMAGE IS TO DOOR 1R. 1R BUSTLE LINING HAS BEEN REPAIRED BY SHOP. REINSTALLED TO 1R DR REF PTT 9242922.

Part: PUMP — DAMAGED (FUEL SYSTEM) · airframe 77,924 hrs · 12,548 cycles

UNWANTED FUEL TRANSFER. RT MAIN TNK AFT BOOST PMP NEEDS TO BE REMOVED FOR INSPECTION. REMOVED RT MAIN TANK AFT BOOST PUMP AND SLEEVE. FOUND IMPELLER AND SLEEVE DAMAGED. ORDERED NEW PMP AND SLEEVE. NEW PMP ON SITE WITH NEW O'RINGS. WAITING FOR SLEEVE. REPLACED RT AFT BOOST PUMP AND SLEEVE WITH NEW O-RINGS. OPS AND LEAK CHECK GOOD.

Part: GENERATOR — CRACKED (APU) · airframe 77,563 hrs · 12,497 cycles

APU OIL CONSUMPTION ABOVE LIMIT. APU SAMC TEXT: TROUBLESHOOT USING MM. APU GENERATOR HAS 8 INCH CRACK. REPLACED APU GEN, CHECKED OK.

Part: AUDIO PANEL — INOPERATIVE (COCKPIT) · airframe 77,513 hrs · 12,490 cycles

CAPTAIN'S AUDIO SELECT PANEL R HF AND FLT INPH LIGHT OUT. REPLACED CAPTAIN'S AUDIO SEL PANEL, OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 77,191 hrs · 12,442 cycles

EEL CEILING LIGHT AT 6AB INOP. RELAMPED (1317) BUT NO HELP. FOUND BROKEN WIRE AT THE LAMP SOCKET TERMINAL. RESPLICED WIRE TERMINAL AND OP CKD GOOD.

Part: ANTENNA — DAMAGED (VHF COMM) · airframe 77,187 hrs · 12,441 cycles

LOWER VHF ANTENNA HAS EVIDENCE OF LIGHTNING STRIKE. DAMAGED MARKED WITH TAPE. HARDWARE, GEL GASKET AND SEALANTS PLANESIDE. COMPLETED REPLACEMENT OF RT VHF ANTENNA. OP TEST PASS.

Part: CONNECTOR — SEPARATED (VHF ANTENNA) · airframe 77,187 hrs · 12,441 cycles

RIGHT VHF ANTENNA COAX CONNECTOR SEPARATED FROM ANTENNA END OF CABLE WHEN INSULATING TAPE REMOVED DURING ANTENNA CHANGE. REPLACED RT VHF ANT COAX CONNECTOR, CHECKS OKAY.

Part: ANTENNA — DAMAGED (DME SYSTEM) · airframe 77,187 hrs · 12,441 cycles

LOWER, CENTER YELLOW ANTENNA HAS EVIDENCE OF LIGHTNING STRIKE. DAMAGED MARKED WITH TAPE. REMOVED LT DME ANTENNA IAW MM. INSTALLED LWR DME ANTENNA FROM MM. TEST ACCOMPLISHED NORMAL.

Part: CONTROL VALVE — INOPERATIVE (FLOW CONTROL) · airframe 76,964 hrs · 12,408 cycles

ON TAKEOFF-INITIAL CLIMB, RT PACK OFF EICAS AND ON OVERHEAD PANEL. REPEAT PACK PROBLEM. RT PACK FLOW CONTROL VALVE. REPLACED VALVE. NO HELP. SUSPECT BAD VALVE FROM STOCK. CLEARED EICAS MESSAGE. WHEN PACK WAS TURNED ON RT PACK BITE MESSAGE RETURNED. CHECKED CONTROLLER, FAULTS FLOW CONTROL VALVE. SWAPPED CONTROLLERS NO HELP. SWAPPED FLOW CONTROL CARD, NO HELP. REPLACED FLOW CONTROL VALVE IAW MM. RT PACK OPS CHECKED GOOD. PREVIOUS FLOW CONTROL VALVES BAD FROM STOCK.

Part: FSEU — ILLUMINATED (SLAT SYSTEM) · airframe 76,669 hrs · 12,367 cycles

L/E SLAT ASSY EICAS, RTFL. TROUBLE SHOT, DIRECTED BY FIM TO L/E SLAT PROX SENSOR HEALTH CHECK, HEALTH CHECK FOUND SENSOR S298 WITH HIGH RESISTANCE. INSPECTED FOUND SENSOR SPLICES DAMAGED. REMOVED SENSOR AND RESPLICED. REPEATED HEALTH CHECK ALL CHECKS OK. DUE HISTORY AND ACFT AIR TURN BACK REPLACED FSEU, ALSO TESTED PSEU, NO FURTHER DEFECTS.

Part: LINE — INOPERATIVE (LAVATORY) · airframe 76,609 hrs · 12,359 cycles

ALL LAVS INOP, RTFL. NO LAV-FLUSH FLUID AVAILABLE IN ECONOMY OR BUSINESS LAVS. ONLY 1ST LAV WORKS CORRECTLY. ALL LAVS IN BUS CLASS AND ECONOMY ARE DRY FLUSH ONLY. NO RINSE WATER WITH FLUSH. TRIED PRIMING BY POURING WATER INTO TOILET BOWL-NO HELP. NORMAL WATER FLOW IN GALLEYS AND LAV SINKS. WATER QTY INDICATED FULL AND LAV WASTE TANKS INDICATED LESS THAN 25 PERCENT FULL. FOUND AIR IN RINSE LINES. OPENED B-NUT ON TOILET RINSE LINES AND RESECURED. FLUSH CHECKS NORMAL.

Part: PROXIMITY SWITCH — FAULTY (LE SLAT) · airframe 76,605 hrs · 12,358 cycles

L/E SLAT ASYM MSG. ACCOMPLISHED SERVICE TIP MM. FOUND NR 8 LE SLAT PROX SW S298 RESISTANCE ON THE HIGH SIDE 23 OHMS, S304 PROX SW RESISTANCE WAS 15.6 OHMS. STARTED REMOVAL AND INSTALLATION OF S298 PROX SW. COMPLETED INSTALLATION OF S298. ACCOMPLISHED TEST PER AMM. GROUND CHECKS NORMAL.

Part: LINE — LEAKING (HYS SYSTEM) · airframe 76,532 hrs · 12,347 cycles

HYD LEAK FOUND OVER RT MLG COMING FROM WING LEADING EDGE. LEAK AT ANTI-SKID SHUTTLE VALVE MODULE. SECURED LINE AT 'B' NUT, PRESSURIZED SYSTEM. NO LEAKS. ANOTHER HYD LEAK COMING FROM LEFT MAIN GEAR BREAK LINE. F1 BRAKE PRESSURE TUBE ASSY FOUND BUSTED DUE CHAFING. REPLACED TUBE ASSY PER AMM. TIGHTENED TUBE BRACKET. OPS CHK GOOD, NO LEAK. ANOTHER HYD LEAK COMING FROM LEFT MAIN GEAR BREAK LINE. F1 BRAKE PRESSURE TUBE ASSY FOUND BUSTED DUE CHAFFING. REPLACED TUBE ASSY PER AMM. TIGHTENED TUBE BRACKET. OPS CHK GOOD, NO LEAK.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 76,532 hrs · 12,347 cycles

ANOTHER HYD LEAK COMING FROM LEFT MAIN GEAR BREAK LINE. F1 BRAKE PRESSURE TUBE ASSY FOUND BUSTED DUE CHAFING. REPLACED TUBE ASSY PER AMM. TIGHTENED TUBE BRACKET. OPS CHECK GOOD. NO LEAK.

Part: SIGN — MISSING (CABIN) · airframe 76,206 hrs · 12,304 cycles

EXIT SIGN MISSING NEAR RT OVERWING. REFITTED COVER AND TESTED LIGHTS AND OPS NORMAL

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,116 hrs · 12,290 cycles

EMERGENCY LIGHTS FLICKER. REPLACED BATTERY PACK.

Part: SERVO — FAILED (YAW DAMPER) · airframe 75,951 hrs · 12,266 cycles

2 YAW DAMPER DISPLAYED ON EICAS AND YAW DAMP INOP LIGHT ILLUMINATED RIGHT AFTER TAKEOFF. TESTED RIGHT YAW DAMPER. TEST FAILED FAULTING THE RIGHT YAW DAMP ACTUATOR. LEFT YAW DAMPER OPS NORMAL PER MM, FAILED RT YAW DAMPER ACTUATOR. REPLACED RT YAW DAMPER SERVO PER MM. OPS CHECKED NORMAL.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 75,935 hrs · 12,264 cycles

PASSENGER REPORTED EMERGENCY LIGHTS BY DOOR 2L FLASHED ON AND OFF MOMENTARILY DURING FLIGHT. MAINT TEXT: EMERGENCY LIGHTS ON, WITHIN 20 TO 30 SECONDS SEATS 19AB THRU 23AB GO OFF, ALONG WITH OVERHEAD EXIT AISLE LIGHT AT SEAT 19AB. REPLACED PWR SUPPLY, OPS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,893 hrs · 12,254 cycles

EMERGENCY CEILING LIGHTS ON THE LEFT SIDE ROWS 19JK THRU 22JK AND EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1209 DO NOT OPERATE. REPLACED EMERGENCY LIGHT BATTERY PACK AT M1209 POWER SUPPLY PER MM. OPS CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 75,893 hrs · 12,254 cycles

EXTERIOR EMERGENCY LITES AFT OF RT WING WHICH OPERATE VIA M733 EMERGENCY LIGHTS BATTERY PACK DO NOT ILLUMINATE WHEN TESTED. REPLACED AND OPS CHECKED THE M733 EMERGENCY LIGHT BATTERY ASSEMBLY PER MM. INSPECTED BY QC STAMP NR 822. OPS CHECKED GOOD. PEMCO NR 2354N00494.

Part: FLOORBEAM — CRACKED (BS 770) · airframe 75,893 hrs · 12,254 cycles

BS 770, MID GALLEY FLOOR CENTER RIGHT TRANSITION FLOORBEAM CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED TRANSITION BEAM IAW SRM, LOCATED, DRILLED AND DEBURRED NEW BEAM P/N STA 770 MID GALLEY FLOOR. INSTALLED NEW FLOORBEAM IAW SRM.

Part: BUSHING — MISSING (OVERWING DOOR) · airframe 75,893 hrs · 12,254 cycles

LEFT OVERWING BSLIDE DOOR DEPLOY CABLE IS MISSING SPACER, BUSHING ON THE FWD LOWER PULLEY. SUPPLEMENTAL DATA UPDATE, INSTALLED BUSHING INTO OVERWING SLIDE DOOR DEPLOY CABLE LOWER FWD PULLEY. OPS CHECKS GOOD.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,610 hrs · 12,219 cycles

EMERGENCY LIGHTS ON SEATS 19AB THRU 24B ARE INOP. SECURED BATTERY CONNECTOR. CHECKS GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 75,610 hrs · 12,219 cycles

LEFT SIDE EEL AILSE LIGHTS ARE INOP BY SEATS 21AB THRU 29AB. SECURED BATTERY CONNECTOR. CHECKS GOOD.

Part: ENGINE — FAULTY (APU) · airframe 75,354 hrs · 12,186 cycles

APU INOP. AUTO SHUTDOWN 10 SECONDS AFTER REACHING 95 PERCENT RPM. APU FAULT LIGHT ON. APU WOULD NOT STAY RUNNING. APU FAULT EICAS MESSAGE. NO TIME TO T/S ON ACCT OF TOW ACTIVITY WITH THIS ACFT. FOUND HEAVY METAL PARTICLES OVER .050 ON MAIN GEAR BOX CHIP DETECTOR. REPLACED APU IAW AMM.

Part: GENERATOR — MAKING METAL (APU) · airframe 75,177 hrs · 12,155 cycles

APU QUIT WITH FAULT. NO START WITH FAULT LIGHT ON 2 RESTART ATTEMPTS. COMPLIED WITH MEL. REPLACED APU GENERATOR DUE TO MAG CHIP DETECTOR CONTAMINATION, GENERATOR SEIZED. ALSO RPL OIL FILTER ASSY. APU OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 75,044 hrs · 12,143 cycles

EMERGENCY CEILING LIGHT INOP AT SEAT 13AB. RELAMPED AND OP CK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 75,044 hrs · 12,143 cycles

EMERGENCY CEILING LIGHT INOP AT SEAT 21HJ. RELAMPED AND OP CHECKED GOOD.

Part: ACTUATOR — DAMAGED (RT WING SPOILER) · airframe 74,944 hrs · 12,128 cycles

FILTER HOUSING BROKEN OFF OF RIGHT INBOARD SPOILER POWER CONTROL ACTUATOR CAUSING LOSS OF CENTER SYS HYDRAULIC FLUID. REPLACED INBOARD SPOILER ON RIGHT WING PER AMM. OPERATION AND LEAK CHECKS ARE OKAY.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 74,944 hrs · 12,128 cycles

CTR HYD SYS, ADP LEAKING HYD FLUID FROM ADP GEAR CASE. CENTER ADP REMOVAL STARTED. REMOVED ADP REF MM. REPLACED ADP. NO LEAKS DETECTED.

Part: CONTROLLER — MALFUNCTIONED (RT BLEED SYS) · airframe 74,865 hrs · 12,116 cycles

RT ENG BLEED DOES NOT OPEN TIL ABOUT 45 PERCENT N1 AFTER ENG START. OK REST OF FLIGHT. RT HPSOV VALVE SECURED CLOSED. REPLACED HP CONTROLLER AND PRV CONTROLLER. OPS CHECK GOOD SEVERAL TIMES. BLEED SHIFT NORMAL.

Part: SQUIB — NO TEST (RT OVRWG SLIDE) · airframe 73,318 hrs · 11,883 cycles

RT OVERWING SLIDE SPOILER SQUIB WILL NOT TEST. REPLACED RT SPOILER OVERRIDE ACTUATOR AND REACTIVATED SLIDE AND TESTED NORMAL.

Part: STARTER — FAULTY (NR 2 ENGINE) · airframe 73,247 hrs · 11,872 cycles

NR 2 ENG MAX MOTOR FOR START 8 PERCENT N2 USING APU OR CROSSBLEED ENG START. STARTER & STARTER VALVE FOUND DEFECTIVE. REPLACED STARTER AND START VALVE. OPS GOOD.

Part: TRANSDUCER — MISRIGGED (LE SLAT) · airframe 72,973 hrs · 11,830 cycles

FLAP SPLIT FSPM SHOWING A FAULT OF THE O/B SLAT PDU RVDT, RTBL.

Part: OVEN — DIRTY (GALLEY) · airframe 72,923 hrs · 11,822 cycles

F/A'S SMELLED ELECTRICAL BURNING SMELL BUT NO SMOKE IN THE OVERWING JUMPSEAT AREA. PER SAM TURNED OFF THE F/A OVERWING READING LIGHTS. NO REOCCURRENCE OF SMELL. ALL MID GALLEY FLIGHT ATTENDANT READING LIGHTS AT MID GALLEY AREA TURNED ON FOR DURATION OF GROUND TIME ZURICH WITHOUT NOTE CEILING PANELS OPENED AND P19 PANEL ASSY LIGHTING DISTRIBUTION CHECKED FOR BURNING SMELLS OR SIGNS OF OVERHEATING NONE FOUND CEILING PANELS REPLACED. MID GALLEY ELECTRICAL EQUIPMENT OVENS COFFEEMAKERS CHECKED FOR BURNING SMELL FOUND PARTIALLY BURNED PLASTIC IN OVEN 408, REMOVED AND OPS CHECKED GOOD. ALL LIGHTING IN MID GALLEY CHECKED FUNCTIONAL, NO SMELLS. READING LIGHT CHECKED IN BOTH ECONOMY AND BUSINESS CABINS ALL WORKING LIGHTS REMAINED ON FOR 3 HRS GND ZURICH WITHOUT NOTE.

Part: CDU — INOPERATIVE (COCPIT) · airframe 72,853 hrs · 11,811 cycles

CAPT'S CDU BLANK, RTFL. REPLACED LEFT CDU, OPS CHECK OKAY. CDU INOPERATIVE. REPLACED LEFT CDU, OPS CHECK OKAY.

Part: PANEL — LEAKING (RT WING) · airframe 72,796 hrs · 11,803 cycles

FUEL LEAK UNDER RT INBD WING. 12 FOOT SEEP AT SEAM WITH WIDE AREA OF DRIPS. LOCATED LEAK EXTERNALLY AND INTERNALLY. REMOVED SEALANT EXTERNALLY, CLEANED AND RESEALED WITH A1-2 AND B1-2 AT 1400 HRS. NEEDS TO RESEAL INTERNALLY. RESEALED INTERNALLY WITH A1-2 AND B1-2 AT 1800HRS. STATIC CHECKED REPAIR NO LEAKS.

Part: CONTROL PANEL — FAULTY (AUDIO) · airframe 72,557 hrs · 11,768 cycles

FO'S AUDIO CONTROL PANEL NR 2 VHF INOPERATIVE. ACCOMPLISHED CAT III CHECK, NO FAULTS. REPLACED FO'S AUDIO CONTROL PANEL. CHECKED OKAY.

Part: PUMP — OVERHEATED (HYD SYSTEM) · airframe 72,354 hrs · 11,735 cycles

RT EDP HYD PUMP 'OVHT' LIGHT ILLUMINATED WITH ASSOCIATED STATUS MSG. DISPLAY ELEC- HYD PG AND NOTICED A STEADY RISE IN RT HYD TEMP. REPLACED EDP AND REPLACED PRESSURE FILTER. PERFORMED LEAK CHECK ALL OK. RAN ENG AND ALL INDICATIONS GOOD.

Part: FAN — FAILED (E/E BAY) · airframe 71,810 hrs · 11,658 cycles

FWD EQ EXH FAN STATUS MESSAGE DISPLAYED, BURNING ODOR DETECTED, HAS DISSIPATED, IAW CREW. REPLACED EQ FWD EXHAUST FAN, ALL OPS AND INDICATIONS NORMAL.

Part: VALVE — MALFUNCTIONED (CTR HYD ADP MOD) · airframe 71,766 hrs · 11,651 cycles

CTR HYD ADP PRESSURE BEING BELOW OPS LIMITS. REPLACED CTR HYD ADP MODULATOR VALVE. VALVE OPS CKS NORMALLY WITH NORMAL CTR HYD PRESSURE.

Part: PRESSURE SWITCH — FAULTY (FUEL SYSTEM) · airframe 71,471 hrs · 11,603 cycles

RIGHT CENTER FUEL PUMP LIGHT OUT PRIOR TO ENG START. SUSPECT PRESS SWITCH. REPLACED RT CENTER OVERRIDE PUMP PRESS SWITCH, CHECK OKAY.

Part: SENSOR — INOPERATIVE (FUEL TEMP) · airframe 70,839 hrs · 11,506 cycles

FUEL TEMP INDICATOR BLANK. FOUND FUEL TEMP INDICATOR BLANK INTERMITTENT, ALSO CHECKED FUEL TEMP RESISTANCE BULB SENSOR, OK. NEEDS NEW FUEL QTY INDICATOR PANEL. INSTALLED NEW INDICATOR PANEL, NO HELP. REINSTALLED OLD PANEL, BOTH PANELS WILL NOT TEST ON TEMP INDICATION ONLY. SUSPECT NO POWER TO TEMP INDICATOR LCD DISPLAY. UNABLE TO FIND POWER WIRE IN DIA. REPLACED FUEL TEMP SENSOR TS0168, OPS CHECK GOOD.

Part: ADC — FAULTED (NR 2) · airframe 70,806 hrs · 11,501 cycles

ALT SPLIT. RTFL. REPLACED RIGHT ADC, NO HELP. REPLACED CAPT FMC. ACP FMS NAV DATA BASE UPDATE. OPS TESTED GOOD.

Part: INDICATOR — MALFUNCTIONED (ALTIMETER) · airframe 70,805 hrs · 11,500 cycles

ALT DISAGREE CONDITION. FLIGHT WAS TAKEN OUT OF RVSM EN ROUTE AND FLEW AT FL270. REPLACED FIRST OFFICER'S ALTIMETER, GROUND CHECK NORMAL.

Part: STATIC INVERTER — FAILED (NR 1 GYRO) · airframe 70,775 hrs · 11,492 cycles

SAI GYRO FLAG, FLIGHT DIVERTED. SAI GYRO FLAG IN VIEW INTERMITTENTLY. SAI PREVIOUSLY REPLACED. REPLACED ILS STATIC INVERTER AND TESTED GOOD. REPLACED STANDBY ATTITUDE INDICATOR. TESTED GOOD. ACFT RELEASED BACK TO SERVICE.

Part: PUMP — INADEQUATE (CENTER TANK) · airframe 70,627 hrs · 11,467 cycles

CENTER TANK RT OVERRIDE PUMP INADEQUATE. REPLACED CENTER TANK RT OVERIDE PUMP, LEAK CHECK ACPD, NO LEAKS FOUND.

Part: BATTERY — FAULTY (MAIN) · airframe 70,380 hrs · 11,429 cycles

STATUS MESSAGE MAIN BATTERY CHARGER. REPLACE MAIN BATTERY AND MAIN CHARGER. MSG CLEARED ON EICAS DISPLAY.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 69,946 hrs · 11,362 cycles

EXTERIOR EMERGENCY LIGHT AT DOOR 1R INOP. SOCKET WAS CLEANED AND LIGHT RELAMPED, NO HELP. OTHER LIGHTS ON THIS BATTERY PACK CHECK GOOD. LIKELY A FUSE OR POWER SUPPLY UNIT PROBLEM. WILL NEED TO REMOVE THE 1ST ROW RIGHT SIDE 1ST CLASS SEAT ASSY FOR ACCESS TO THE DADO PANEL AND POWER SUPPLY UNIT. REPLACED PWR SUPPLY. SLIDE LIGHT OPS CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,946 hrs · 11,362 cycles

EXTERIOR EMERGENCY LIGHT AT DOOR 1L INOP. RELAMPED, CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,946 hrs · 11,362 cycles

EXTERIOR EMERGENCY LIGHT JUST FORWARD OF AFT CARGO DOOR INOP. RELAMPED, CHECKS GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 69,404 hrs · 11,279 cycles

EXTERIOR EMERGENCY LIGHT AT DOOR 2R IS INOP. SECURED AND CLEANED LAMP IN SOCKET.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 69,404 hrs · 11,279 cycles

EXTERIOR EMERGENCY LIGHT ON RT SIDE FUSELAGE JUST FWD OF AFT CARGO DOOR INOP. CLEANED AND SECURED LAMP IN SOCKET.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,968 hrs · 11,216 cycles

A19 POPPED IN FLIGHT, RESET NO OTHER INDICATIONS (ALT EMER ESCAPE LTS). DISPLACED AND RECONNECTED 1A SEAT BACK. REMOVED AND REPLACED BATTERY PACK AND BATTERY CHARGER UNIT. OPS CHECKED GOOD.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS) · airframe 68,966 hrs · 11,215 cycles

DOOR 2L 3 MOST AFT EXT EMERGENCY LIGHTS INOP. INSTALLED NEW POWER SUPPLY AND BATTERY, SYSTEM OPS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,966 hrs · 11,215 cycles

DOOR R1 LOWER EXIT IDENTIFIER SIGN AND FWD RT EEL LIGHT BAR INOP. REPLACED BATTERY PACK, OPS CHECKS GOOD.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · airframe 68,966 hrs · 11,215 cycles

AFT GALLEY FLOOR MOUNT CORRODED STA 1593, LBL 6. INSTALLED NEW GALLEY MOUNT FITTING.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 68,966 hrs · 11,215 cycles

AFT PIT BS 1562 FAIL SAFE CHORD CORRODED AT BL 0. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER AND FILLER REPAIR.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 68,966 hrs · 11,215 cycles

MAIN CABIN RT SEAT TRACK GOUGED STA 488, RBL 100. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF SEAT TRACK STA 423.45 TO 511.45, RBL 88.5 AND INSTALLED NEW SECTION OF SEAT TRACK AND SPLICED PARTS.

Part: WIRE — CHAFED (THRUST REVERSER) · airframe 68,966 hrs · 11,215 cycles

NR 1 PYLON HYDRO BAY WIRES W390-102-18 AND W 390-103-18 FOR L ENG T-R ISOLATION VALVE ARE CHAFED THROUGH SHIELDING. REPLACED WIRES W390-102-18 AND W390-103-13 FROM PLUG D20118 REF BSWPM 20-61-11 TO JACK 4474J. ASSY GROUNDS FOR SHIELD REF BSWPM 20-10-15, AND REASSEMBLE JACK REF BSWPM 20-61-11.

Part: FEEDER CABLE — DAMAGED (RT GENERATOR) · airframe 68,966 hrs · 11,215 cycles

RIGHT GENERATOR FEEDER CABLE PRIMARY INSULATION DAMAGE TO CABLE. INSTALLED GENERATOR FEEDER CABLE. OPS CHECKS NORMAL.

Part: FRAME — CORRODED (FUSELAGE) · airframe 68,966 hrs · 11,215 cycles

AFT CARGO COMPARTMENT FRAME T-CAP, LOWER SURFACE CORRODED AT NUT PLATE, BS 1197+132, RBL 45, S-33R. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED T-CAP. INSTALLED NEW T-CAP.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 68,966 hrs · 11,215 cycles

AFT PIT FLOOR SUPPORT HAS CORROSION AROUND NUT PLATES STA 1219, LBL 20 TO LBL 24. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW UPPER CHORD (P/N 146T1060-2).

Part: SHEAR TIE — CORRODED (BS 1562, BL 0) · airframe 68,966 hrs · 11,215 cycles

AFT BULK COMPARTMENT SHEAR TIE CORRODED FWD AND AFT SIDE BS 1562, BL 0. MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW SHEAR TIE AND INSTALLED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,966 hrs · 11,215 cycles

AFT CARGO COMPARTMENT, BILGE ANGLE SHEAR TIE, CORRODED BS 1241, RBL 0. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW SHEAR TIE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,966 hrs · 11,215 cycles

AFT PIT STA 1219, ATTACH ANGLE, SHEAR TIE, HAS CORROSION BETWEEN S-39L AND S-39R BY- 85625. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW SHEAR TIE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,966 hrs · 11,215 cycles

CORROSION CABIN FLOORBEAM CAP AT STA 287, AT RBL 15. MAJOR REPAIR ACCOMPLISHED: REPLACED PREVIOUS DOUBLER REPAIR. INSTALLED NEW T-CAP SECTION AND SPLICES.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,966 hrs · 11,215 cycles

AFT BULK CARGO COMPARTMENT SHEAR TIE CORRODED BS 1540, BL 0. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SHEAR TIE.

Part: SLIDE — UNSERVICEABLE (OVERWING EXIT) · airframe 68,966 hrs · 11,215 cycles

LT OVERWING SLIDE FWD LACING CLIP BROKEN OFF AT THE UNLACE BAR. SLIDE NOT LACED AT POINT. REPLACED SLIDE ON SNR 6195 04016.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,966 hrs · 11,215 cycles

EVIDENCE OF CORROSION AT LOWER AFT ATTACH POINT OF BULK COMPARTMENT FLOOR SUPPORT FRAME BS 1540, RBL 39 TO RBL 38. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SHEAR TIE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,966 hrs · 11,215 cycles

AFT BULK CARGO COMPARTMENT SHEAR TIE CORRODED BS 1540, STR 38L. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SHEAR TIE.

Part: CABLE — FAULTY (ESCAPE SLIDE) · airframe 68,966 hrs · 11,215 cycles

LT AFT ESCAPE SLIDE STEP AFT CABLE IS WORN AND HAS A KNOT IN CABLE. *S/D* REPLACED AFT STEP CABLE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,282 hrs · 11,077 cycles

FLOOR EEL LIGHT ADJACENT TO DR 1R INOP. INSTALLED NEW EEL STRIP, P S-CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,282 hrs · 11,077 cycles

AFT GALLEY'S X AISLE EEL LIGHT INOP. REPLACED EEL LIGHT, OPS CHECKS GOOD.

Part: WIRE HARNESS — FAULTY (CABIN) · airframe 68,282 hrs · 11,077 cycles

FLOOR EEL LIGHT AT SEAT 1EF INOP. REPAIRED FLEX HARNESS TO EEL LIGHT, OPS CHECKS GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 68,282 hrs · 11,077 cycles

FLOOR EEL LIGHT AT SEAT 5EF INOP. SECURED EEL'S CONNECTOR, OPS CHECKS OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,282 hrs · 11,077 cycles

FLOOR EEL LIGHT RT OF MID-GALLEY INOP. REPLACED EEL LIGHT. OPS CHECKS OKAY.

Part: SIGN — UNSECURE (CABIN) · airframe 68,257 hrs · 11,073 cycles

RT OVER WING EXIT SIGN OVER AISLE LENS ON AFT SIDE WILL NOT STAY ON LIGHT ASSY. SECURED IN PLACED WITH TAPE.

Part: CONTROL VALVE — INOPERATIVE (RT AC PACK) · airframe 67,960 hrs · 11,028 cycles

RIGHT PACK OFF LIGHT NOT ILLUMINATED WITH PACK OFF. REPLACED FLOW CONTROL CARD, NO HELP. FOUND FLOW CONTROL VALVE INOP. REPLACED RT PACK FLOW CONTROL VALVE. OP CHECK GOOD.

Part: GENERATOR — MALFUNCTIONED (NR 2 ENGINE) · airframe 67,461 hrs · 10,938 cycles

LOST RT GENERATOR AND APU. FLIGHT DIVERTED. NR 2 ENGINE GENERATOR REPLACED. (OFF: P/N 745329C, S/N G0796)

Part: GENERATOR — FAILED (NR 2 ENGINE) · airframe 67,461 hrs · 10,938 cycles

LOST RT GENERATOR AND APU. FLIGHT DIVERTED. NR 2 ENGINE GENERATOR REPLACED. APU REPLACED (P/N 3800298-1-7). AFTER APU REPLACEMENT FAULT LIGHT AND MSG FUEL SEL VLV. REPLACED FUEL CONTROL UNIT (P/N 3882500-17), NO HELP. REPLACED APU CONTROLLER (P/N 2117342-19). APU OP CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (SEAT 1EF) · airframe 67,287 hrs · 10,912 cycles

EMERGENCY LIGHT FLEX STRIP LIGHT INOP AT SEAT 1EF. REPLACED EMERGENCY LIGHT STRIP. OPS CHECKED OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,287 hrs · 10,912 cycles

EMERGENCY EEL FLEX STRIP LIGHT INOP AT SEAT 5EF. REPLACED EMERGENCY LIGHT STRIP. OPS CHECKED OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,287 hrs · 10,912 cycles

EMERGENCY EEL LIGHT STRIP INOP FROM SEAT 5AB TO 6AB. REPLACED FLEX EMERGENCY LIGHT STRIPS. OPS CHECKED OKAY.

Part: LIGHT — TORN (CABIN) · airframe 67,194 hrs · 10,898 cycles

EEL STRIP TORN LEFT SIDE FIRST ROW OF BUSINESS CLASS. REPLACED 18 FT SECTION FROM ROW 1 TO ROW 8.

Part: SHUTOFF VALVE — ILLUMINATED (BLEED SYSTEM) · airframe 66,631 hrs · 10,805 cycles

IN POWER REDUCTIONS ON DESCENT, RECEIVED L ENG HPSOV AND ASSOC BLEED LIGHT. WENT OUT AFTER 1 MINUTE. FOUND FAULTY HIGH PRESSURE SHUTOFF VALVE. HPSOV AND CONTROLLER REPLACED. OPS CK GOOD ON ENG.

Part: IDG — FAULTY (LEFT) · airframe 66,600 hrs · 10,798 cycles

LH GENERATOR WILL NOT COME ON LINE, WITH "FIELD OFF" LIGHT ILLUMINATED. SUPPLEMENTAL DATA UPDATE FOUND FAULTY IDG. REPLACED #1 IDG. TESTS OKAY. OK FOR SVC.

Part: ASPIRATOR — LEAKING (RT OWING SLIDE)

ASPIRATOR LEAKS FROM BARREL. *S/D* FOUND LEAKING ASPIRATOR SUSPECT PACKING. REPLACED SLIDE ASSEMBLY. AC OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 66,313 hrs · 10,753 cycles

AFT LT EXTERIOR EMERG LIGHT INOP 2L MED. *S/D* SUSPECT BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (AFT GALLEY) · airframe 66,313 hrs · 10,753 cycles

AFT GALLEY X AISLE INOP. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHT) · airframe 66,313 hrs · 10,753 cycles

EEL INOP AT SEAT 5EF TO 6EF. *S/D* FOUND FAULTY LEAD CABLE. REPLACED FEEDER, OP CHECK GOOD. AC OK FOR SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 66,313 hrs · 10,753 cycles

FWD X AISLE EEL INOP. *S/D* FOUND LIGHT ASSEMBLY BROKEN. REPAIRED LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: ENGINE — VIBRATION (LEFT) · airframe 66,166 hrs · 10,728 cycles

LEFT ENGINE VIBRATIONS. *S/D* VIBRATION WAS NOT CONFIRMED BY ENGINE CONDITION MONITORING. GROUND RUN VIBRATION SURVEY WAS WELL WITHIN LIMITS. BORESCOPE INSPECTION REVEALED NOTHING ABNORMAL. LUBRICATED THE FAN BLADE ROOTS AND RERAN THE VIBRATION SURVEY. ALL STILL WELL WITHIN LIMITS. REPLACED VIBRATION ACCELEROMETER, PRECAUTIONARY.

Part: INDICATION SYS — MULTIPLE FAIL (COCKPIT) · airframe 66,063 hrs · 10,712 cycles

CAPT AIR SPEED ALTIMITER & VSI FAILED. RTFL.

Part: ADC — FAULTY (COCKPIT) · airframe 66,063 hrs · 10,712 cycles

CAPT AIR SPEED ALTIMETER & VSI FAILED. RTFL. FOUND FAULTY ADC. REPLACED CAPTAIN'S AIR DATA COMPUTER & REPLACED CABIN PRESSURE CONTROLLER 1.

Part: BRAKE — LEAKING (LT MLG) · airframe 65,754 hrs · 10,661 cycles

LEFT MLG HAD HYDRAULIC LEAK ON FWD LEFT BRAKE. ARRIVED WITH THE MAIN GEAR SMOKING. LT MLG HAD HYD LEAK ON FWD LEFT BRAKE. SUSPECT BRAKING ACTIVITY MIXED WITH HYD FLUID CAUSED THE FIRE. IADMM PUT THE FIRE OUT. REPLACED NR 1 FWD BRAKE. ACP'D BRAKE TEMP-HIGH ENERGY STOP CONDITION. NO DEFECTS FOUND AND ALSO ACP'D BRAKE SEIZURE CONDITIONAL INSPECTION. NO DEFECTS FOUND.

Part: VALVE — MALFUNCTIONED (APU) · airframe 65,136 hrs · 10,566 cycles

APU WILL NOT PRODUCE COOL AIR 89 DEGREES IN CABIN AT GATE. ACCOMPLISHED EXSTENSIVE TROUBLE SHOOTING FOUND LOW LIMIT VALVE TO BE FAULTY. REPLACED LOW LIMIT VALVE PER MM21-51-11. PERFORMED LEAK CHK NO LEAKS NOTED. OP CHECKED GOOD.AC OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,978 hrs · 10,393 cycles

EMERGENCY EEL LIGHT INOP AT RT MID CLOSET. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,978 hrs · 10,393 cycles

EMERGENCY EEL LIGHT ASSY INOP AT RT MID LAV. REPLACED BATTERY PACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,978 hrs · 10,393 cycles

MASTER CALL LIGHT ON EMERGENCY EXIT SIGN (ROW 15 RT SIDE) INOP. RELAMPED LIGHT ON EMERGENCY EXIT SIGN.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,978 hrs · 10,393 cycles

EMERGENCY EEL LIGHT INOP FROM SEAT 6EF TO 10EF. REPLACED BATTERY PACK.

Part: HOSE — LOOSE (CREW O2) · airframe 63,907 hrs · 10,383 cycles

CREW O2 REPORTED LOW ON ARRIVAL. CHECKED ALL FLT DECK MASK CONNECTIONS. FOUND LOOSE CONNECTION AT 1ST OFFICER POS. SECURED HOSE ASSY 192-2103, SERVICED OXYGEN AND PERFORMED LEAK CHECK, NO DEFECTS NOTED.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 63,907 hrs · 10,383 cycles

SECOND OBSERVERS O2 MASK FOUND DAMAGED DURING LEAK CHECKS. SUSPECT DAMAGED FROM PRE FLIGHT CHECKS. REPLACED 2ND OBSERVERS O2 MASK OPS CHECKS NORMAL. ACFT OK FOR SERVICE.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 63,462 hrs · 10,316 cycles

RTFL DUE TO NR 1 ENGINE SURGE (COMPRESSOR STALL) AS A RESULT OF A BIRDSTRIKE.

Part: FITTING — CRACKED (NR 2 PYLON) · airframe 63,306 hrs · 10,284 cycles

NR 2 PYLON OUTBD MID SPAR FITTING AS SEEN FROM LWR INSIDE TORQUE BOX CRACKED AT 3 - 8INCHES BOLT I/B POSITION. MAJOR REPAIR ACCOMPLISHED: REMOVED FASTENER FROM CLOSEOUT ANGLE. VERIFIED CRACK BY HFEC. STOP DRILLED END OF CRACK. FABRICATED & INSTALLED A REPAIR SPLICE STRAP & FILLER. ANGLE TO BE REPLACED AT C-12.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,306 hrs · 10,284 cycles

DOOR 2L EXTERIOR EMERGENCY EXIT LIGHT IS INOP.

Part: LIGHT — MISLOCATED (CABIN) · airframe 63,306 hrs · 10,284 cycles

EEL AT LEFT C-ZONE AISLE MIS-LOCATED.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 63,306 hrs · 10,284 cycles

EMERGENCY LIGHTS ABOVE OVERWING DOORS ARE INOP. REMOVED & REPLACED BATTERY CHARGER & BATTERY ASSY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,306 hrs · 10,284 cycles

RIGHT EXTERNAL EMERGENCY LIGHTS ARE INOPERATIVE.

Part: SLIDE — DAMAGED (SERVICE DOOR) · airframe 63,306 hrs · 10,284 cycles

RIGHT AFT SERVICE DOOR SLIDE FABRIC TORN ON TOP AND IS MISSING YEAR OVERHAULED STICKER BY.

Part: STIFFENER — CRACKED (BS 246 FLOORBEAM) · airframe 63,306 hrs · 10,284 cycles

FLOORBEAM AT FS 246 FORWARD SIDE VERTICAL STIFFENER CRACKED AT LBL 26.39. REMOVED & REPLACED STIFFENER.

Part: FLOORBEAM — CRACKED (BS 246) · airframe 63,306 hrs · 10,284 cycles

ON THE FORWARD FACE OF FLOORBEAM LOCATED AT BS 246 LBL 22L AT STIFFENER IS CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED STIFFENER.

Part: TRANSFORMER — OUT OF RIG (TE FLAPS) · airframe 61,739 hrs · 10,017 cycles

CAPTAIN REPORTED, T/E FLAP DISAGREE ON FINAL. [08-17-07] FSEU BITE CARRIED OUT WITH FLAP HANDLE SET FOR 30 AND READOUT SHOWING 20. THIS CONFIG RESULTED FROM THE FLAP LEVER ROTARY VARIABLE DIFFERENTIAL TRANSFORMER BEING IN MISRIGGED CONFIGURATION & OUTBD SLAT PEDISTAL FLAP CONTROL ROTARY TRANSFORMER ALSO BEING MISRIGGED. SYSTEM RESET BY CYCLING ARMING SW'S, LIGHTS SHOWN AFTER THE BITE CHECK. L, C, R BITE - ALL OK,THEN FLAP OPERATION NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,656 hrs · 10,001 cycles

AFT LEFT & AFT RIGHT DOOR EXTERNAL EEL LIGHTS ARE INOP. [07-27-07] RELAMPED. CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,656 hrs · 10,001 cycles

LEFT SIDE EXTERNAL EEL LIGHT JUST AFT OF WING IS INOP. [07-27-07] RELAMPED. CHECKS GOOD.

Part: FEEDER CABLE — UNSECURE (EMERGENCY LIGHTS) · airframe 61,656 hrs · 10,001 cycles

AFT GALLEY LONG EEL STRIP IS INOP. [07-27-07] SECURED FEEDER CABLE. CHECKS GOOD.

Part: FAN — FAULTY (GALLEY) · airframe 61,547 hrs · 9,980 cycles

AFT EQ EXH FAN 2 STATUS MSG AFTER AIRCRAFT PWR UP. SOME HOT SMELLING ODOR. REPLACED EXHAUST FAN PER MM 21-26-01. ODOR GONE AND OP CHECKS OK.

Part: COMPUTER — NO TEST (THRUST MANAGE) · airframe 61,462 hrs · 9,965 cycles

NO LAND THREE DISPLAYED NO MALFUNCTION NOTED. [07-20-07] MCDP CODE "SLAT SW-FCC L", ACP MM 22-00-03 & CAT III CHK PER MM 22-10-00, THRUST MANAGEMENT COMPUTER FAILED TEST. RPL TMC PER MM 22-31-01, OP CK GOOD. AC REMAINS IN CAT III STATUS .

Part: UNKNOWN — ODOR (GALLEY) · airframe 61,434 hrs · 9,961 cycles

CREW REPORTS ELECTRICAL BURNING ODOR EMANATING FROM AFT GALLEY AREA. [07-20-07] SUSPECT GALLEY HI-TECH FOODCART TO BE ODOR SOURCE PULLED AFT GALLEY LEFT CIRCUIT BREAKER U7 AND AFT GALLEY RIGHT CB U34 ON PANEL P11 TO ISOLATE POWER. RESET CBS U7 AND U34 0N P1 1 RAN ALL AFT GALLEY CHILLERS COFFEEMAKERS AND HI-TEC CARTS UNAB LE TO DUPLICATE PROBLEM. FAULT REMOVED. SENT SUSPECT PROBLEM HI-TEC CART FOR SERVICING AT CATERING UNIT.

Part: LAMP — INOPERATIVE (NAV LIGHTS) · airframe 61,182 hrs · 9,923 cycles

LT AND RT AFT NAV INBD LIGHTS ARE INOPERATIVE. RELAMPED. OPS CKS GOOD.

Part: CONNECTOR — FAULTY (EMERGENCY LIGHT) · airframe 61,182 hrs · 9,923 cycles

EEL LIGHT IN FRONT OF RT MID LAV IS INOPERATIVE. SPLICED CONNECTOR TO PWR STRIP.

Part: TRANSFORMER — SHORTED (CABIN) · airframe 60,726 hrs · 9,843 cycles

ELECTRICAL POWER PROBS CAUSED RTFL. REPLACED CURRENT TRANSFORMER T9000. REF WDM25-31-12, WDM25-31-13, WDM33-31-13 & WDM33-27-12. RELUGGED WIRE (32-16) AT C9010 W12 DUE TO HEAT DAMAGE. PERFORMED LOAD TEST AND LOAD SHED TEST OPS CHECKS NORMAL REF GNMM02-0-21-001. APPLIED POWER TO GALLEY AND TESTED ALL FUNCTIONS. ALL FUNCTIONS TESTED NORMAL.

Part: INDICATION SYS — MALFUNCTIONED (HYD QTY) · airframe 60,653 hrs · 9,824 cycles

RTFL DUE TO RIGHT AND CENTER HYDRAULIC SYSTEMS QUANTITY INDICATION PROBLEMS. [SUP 05-16-07] REPLACED HYD. QTY. MONITOR UNIT PER MM 29-33-01. OP CHECKS NORMALLY. A/C RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (LT ENGINE) · airframe 60,520 hrs · 9,800 cycles

THE -L ENG PRV- EICAS MSG DISPLAYED ON TAKEOFF. [SUP 5-1-07] REPLACED PRV AND PRVC PER MM 36-11-18 AND 36-11-19. PERFORMED SUCCESSFUL TEST OF PRV-PRC SYSTEM. NO DEFECTS OBSERVED. A/C RETURNED TO SERVICE.

Part: SHEAR TIE — DAMAGED (BS 143 S24-30R) · airframe 60,415 hrs · 9,783 cycles

WEB AND SHEAR TIE DAMAGE TO CIRCUMFERENTIAL AT STA 143.5 BETWEEN STR 24R & 30R. MAJOR REPAIR ACCOMPLISHED: REPLACED DAMAGED FRAME & CHORD ANGLE.

Part: SKIN — DENTED (BS 143 S25R) · airframe 60,415 hrs · 9,783 cycles

FUSELAGE DAMAGE SECTION 41 APPROX STA 143 S25R, DENT APPROX 1 FT X 2 FT. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SKIN. FABRICATED & INSTALLED SKIN SECTION & DOUBLERS.

Part: ENGINE — DAMAGED (NR 1) · airframe 60,414 hrs · 9,782 cycles

RTFL UNDER AMBER ALERT WITH NR 1 ENGINE SHUT DOWN DUE TO BIRD STRIKE (TOWED TO GATE). A/C ENCOUNTERED A FLOCK OF DUCKS. BOTH ENGINES HAD COMPRESSOR SURGES DUE TO INGESTION. NR 1 WAS MUCH MORE SEVERELY DAMAGED & ENGINE WAS REPLACED. NR 2 ENGINE BORESCOPED & PLACED ON 25 HOUR LIMIT TO BE REPLCD AT GSO. NUMEROUS SHEET METAL DAMAGE SITES INCLUDING 1 X 2 FT DENT ON LEFT SIDE OF FUSELAGE, DMG TO STA 132.5 AT STR 212R, STA 204.5 AT STR 32L, STA 266.5 AT STR 11R. ALSO DMGED WERE BOTH NOSE GEAR DOORS, NR 1 ENG NOSE COWL & PITOT STATIC PROBES. DAMAGE FROM FOD.

Part: CHECK VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 60,204 hrs · 9,750 cycles

LANDED UNDER AMBER ALERT DUE TO NR 1 ENGINE AT FLIGHT IDLE DUE TO COMPRESSOR STALL AND HIGH EXHAUST GAS TEMPERATURE. EMERGENCY EQUIPMENT CALLED AS PRECAUTION. TROUBLESHOOTING IDENTIFIED FAILED 8TH STAGE PNEUMATIC CHECK VALVE. AFTER EXTENSIVE TROUBLESHOOTING, IDENTIFIED CAUSE AS 8TH STAGE PNEUMATIC CHECK VALVE. REPLACED VALVE & CORRECTED RESULTANT DAMAGE. VALVE FAILED RELEASING THE POPPET SHAFT.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 59,958 hrs · 9,706 cycles

MAIN CABIN SEAT TRACK AT RBL 88.50, APPROX STA 753 TO 819 IS CRACKED OUT, 2 PLACES AT UPPER SCALLOPS WHERE GALLEY MOUNTS. REPLACED SEAT TRACK SECTION RBL 88.5, STA 753 TO 819, A/C READY FOR SERVICE. SUSPECT DAMAGE IS DUE TO SERVICE CARTS & IMPACT BY PAX CARRY-ON ITEMS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,958 hrs · 9,706 cycles

WING LEFT SLIDE GROUND L646 AND AFT DOOR LEFT SIDE DOOR GROUND (L397) EXTERIOR EMERGENCY LIGHTS INOP. RELAMPED L397 AFT LT DOOR SLIDE LIGHT PER MM 33-51-06. OPS CHECKS NORMALLY.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 59,958 hrs · 9,706 cycles

EXTERNAL FUSELAGE AFT RIGHT EMERGENCY LIGHT L392 INOP. REPLACED LIGHT. OP CHECKS OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,958 hrs · 9,706 cycles

LEFT C-ZONE EEL INOPERATIVE. REPLACED BATTERY PACK AT SEAT 18 A-B. OPS CHECKS NORMALLY.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 58,786 hrs · 9,502 cycles

FAILED HYDRAULIC PUMP. RETURNED TO THE BLOCKS. REPLACED NR 1 ENG ENGINE DRIVEN HYDRAULIC PUMP. LEAK CHECK OK, RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,912 hrs · 9,372 cycles

AFT GALLEY RIGHT HAND EEL STRIP INOPERATIVE. REPLACED EEL STRIP, OPS CHECKS GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 57,912 hrs · 9,372 cycles

EEL LIGHTS INOP AT SEATS 18AB-27AB. REPLACED EEL POWER FEEDER CABLE, OPS CK OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,912 hrs · 9,372 cycles

EEL LIGHTS INOPERATIVE AT SEATS 6AB-5AB. REPAIRED EEL LIGHT POWER RIBBON. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,912 hrs · 9,372 cycles

EEL STRIP BETWEEN MID GALLEY AND FWD OF SEATS 15FG IS INOPERATIVE. REPLACED EEL STRIP, OPS CK OK.

Part: PRESSURE SWITCH — LEAKING (FUEL SYSTEM) · airframe 57,421 hrs · 9,288 cycles

LEFT JETT NOZZLE LEAK. MANUALLY CYCLED LEFT JETT VALVE, OPEN SEVERAL TIMES AND LET IT DRIVE TO THE CLOSED POSITION. STARTED FUELING AGAIN AND NOZZLE STARTED LEAKING AGAIN. SUSPECT LEAKING NOZZLE TUBE. REF IPC 28-31-01-001 ITM 65 CONT OF AMIS ITEM 4202009 :REPLACED LT FUEL JETTISON NOZZLE VALVE, NO HELP. TROUBLESHOT FUEL JETTISON SYSTEM. PROBLEM TRACED TO PRESS SWTCH. CLEANED TERMINALS OF JETTISON PUMP PRESSURE SWITCH. SYSTEM TESTED OK WITH NO LEAKAGE. OK FOR SVC.

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 57,419 hrs · 9,286 cycles

NR 2 PYLON INBOARD MIDSPAR FITTING CLOSE OUT ANGLE OUTBD FASTENER HOLE HAS APPROX .375 INCH CRACK. CRACK FOUND IN CLOSEOUT ANGLE THAT COVERS TWO AFT-MOST FASTENERS IN LOWER HORIZONTAL TANG OF NR 2 PYLON INBOARD MIDSPAR FITTING. HFEC TO ENSURE THERE ARE NO CRACKS IN OTHER SURROUNDING STRUCURE. NO CRACKS FOUND. REPAIR INSTALLED PER EVA 60418 IN ORDER TO COMPLY WITH AD 2005-19-23, REPETITIVE INSPECTION OF REPAIR MUST BE ACCOMPLISHED BY EDDY CURRENT INSPECTION AT 1500 FLT CYCLES OR OPEN HOLE HFEC AT 8000 FLT CYCLE INTERVAL. SUSPECT THERMAL AND VIBRATIONAL CAUSED EARLY FATIQUE.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 57,419 hrs · 9,286 cycles

NR 1 PYLON INBOARD END OF MIDSPAR CLOSE OUT ANGLE OUTBD FASTENER HOLE HAS APPROX 1 INCH CRACK. REPAIRED CLOSE OUT ANGLE WITH DOUBLER, TRIPLER, FILLER. THE CLOSE OUT ANGLE NEEDS TO BE 85625 REPLACED AT C12 TO FACILITATE MIDSPAR FITTING INSPECTIONS.

Part: WIRE HARNESS — CORRODED (SATCOM ANTENNA) · airframe 57,419 hrs · 9,286 cycles

RIGHT SATCOM ANTENNA HARNESS IS CORRODED. REPLACED RT HIGH GAIN ANTENNA 'AFT' HARNESS PER MM 23-25-17 AND 23-25-19. CONTINUITY CHECK OK. READY FOR SERVICE.

Part: BUSHING — MIGRATED (NLG) · airframe 57,419 hrs · 9,286 cycles

NLG ACTUATOR SUPPORT BEAM-FWD SUPPORT LINK-LOWER FUSE PIN HAS MIGRATING BUSHINGS LT AND RT SIDES AT BULKHEAD FITTING. REPLACED 2 EA. 141T2914-1 BUSHINGS PER MM 32-21-04 AND GN-MM 1-0-1-013. NOSE GEAR EXTENSION AND RETRACTION TEST PERFORMED PER 32-34-00 AND LEAK CHECK GOOD. RETURNED TO SERVICE. BUSHING MIGRATION LIKELY RESULTS FROM CLEARANCE OPEN-UP, VIBRATION AND JARRING DURING LANDING CYCLE.

Part: CLAMP — STRIPPED (SLIDE) · airframe 57,419 hrs · 9,286 cycles

RT OVERWING SLIDE CYLINDER CLAMPS ARE STRIPPED. REMOVED AND REPLACED SLIDE CYLINDER CLAMPS. OK FOR RETURN TO SERVICE. ROOT CAUSE WAS SUSPECTED TO BE OVER TORQUING OF SLIDE CYLINDER CLAMPS DUE TO IMPROPER MAINTENANCE TRAINING.

Part: BRACKET — BROKEN (TORQUE BAR)

TORQUE BAR SUPPORT BRACKETS BROKEN. INSTALLED NEW SUPPORT BRACKETS.

Part: CONNECTOR — MISPINNED (FUEL PUMP) · airframe 51,224 hrs · 8,307 cycles

FUEL JETTISON SYSTEM FAILED. THE JETTISON SYSTEM FAULT LIGHT ILLUMINATED AND THE LH JET PUMP EICAS MESSAGE APPEARED WHEN THE LH JETTISON PUMP FAILED TO GENERATE SUFFICIENT PRESSURE TO SET THE PRESSURE SWITCH. THIS WAS A RESULT OF THE PUMPS SHIP SIDE ELECTRICAL CONNECTOR BEING PINNED INCORRECTLY. TWO OF THE THE AC PHASE LEADS AT CONNECTOR D12188 WERE SWAPPED. REPINNED ELECTRICAL CONNECTOR D12188 PER 767 WDM 28-31-21.

Part: BLADE — FRACTURED (NR 1 ENGINE) · airframe 51,224 hrs · 8,307 cycles

NR 1 ENGINE SURGED, FLAMED OUT AND SEIZED. ENGINE WAS REMOVED FROM SERVICE AND DISASSEMBLED. ROOT CAUSE OF THE FAILURE WAS DETERMINED TO BE A FRACTURE OF THE 5TH STAGE HPC BLADE IN THE ROOT.

Part: LATCH — FAILED (CABIN)

LT O/W SLIDE DOOR INTEGRATOR FAILS TORQUE CHECK. REPLACED LATCHES IAW 767 MM 25-65-98.

Part: O-RING — MISSING (NR 1 ENGINE) · airframe 45,692 hrs · 7,393 cycles

DIVERTED DUE TO OIL LOSS IN NR 1 ENGINE. NR 3 CHIP DETECTOR FALLING OUT OF THE DETECTOR HOUSING AND A MISSING O-RING ON THE CHECK VALVE IN THE HOUSING CAUSED THE LOSS OF OIL. THERE WAS NO WEAR ON THE HOUSING TO CAUSE THE DETECTOR TO BECOME FREE. A COA WILL REPLACE THE OLD DESIGN OF THE CHIP DETECTOR WITH AN IMPROVED DESIGN.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,521 hrs · 7,187 cycles

SEAT TRACK CORRODED LBL 12 FROM BS 859-999. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE SECTION, ANGLES AND FILLERS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,521 hrs · 7,187 cycles

CABIN AT BS 852, RBL 56, TRANSBEAM UPPER CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE, ANGLE AND FILLER REPAIR.

Part: FITTING — CRACKED (T/E FLAP) · airframe 44,521 hrs · 7,187 cycles

LEFT INBOARD FLAP, INBOARD FITTING FOR AFT FLAP ATTACH POINT CRACKED ON INBOARD SIDE OF FITTING. MAJOR REPAIR ACCOMPLISHED. REPAIRED FITTING.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 44,521 hrs · 7,187 cycles

MAIN CABIN FLOORBEAM TOP CAP GOUGED AT BS 340, RBL 28 TO RBL 30. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM T-CAP WITH SPLICE SECTION, ANGLES AND FILLERS.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 44,521 hrs · 7,187 cycles

CABIN STA 776-796, LBL 56, SHORT SEAT TRACK IS GOUGED AT CROWN. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW SEAT TRACK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,521 hrs · 7,187 cycles

CABIN FLOORBEAM BS 286, RBL 88 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE SECTION, ANGLES AND FILLERS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,521 hrs · 7,187 cycles

CABIN FLOOR AT BS 852, RBL 56, TRANSBEAM UPPER CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE SECTION, ANGLES AND FILLERS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,521 hrs · 7,187 cycles

FASTENER HOLES CORRODED AT SEAT TRACK FLANGE BS 830-862, RBL 34 COMMON TO FLOORBEAM. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE SECTION, ANGLES AND FILLERS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,521 hrs · 7,187 cycles

FLOOR BEAM TOP CAP CORRODED AT BS 266 RBL 76. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE SECTION, ANGLES AND FILLERS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,521 hrs · 7,187 cycles

FLOORBEAM CORRODED AT STATION 830-873, LBL 12. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE SECTION WITH ANGLES AND FILLERS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,521 hrs · 7,187 cycles

MAIN CABIN BS 1043, RBL 90, SEAT TRACK CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE SECTION, ANGLES AND FILLERS

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,521 hrs · 7,187 cycles

MAIN CABIN STATION 246 FLOORBEAM IS CORRODED AT RBL 78- T-CAP. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE SECTION, ANGLES AND FILLERS .

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,521 hrs · 7,187 cycles

LT MAIN DECK FLOOR, SEAT TRACK CORRODED BEYOND LIMITS BETWEEN BS 764-776, LBL 56-LBL 59. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SECTION SPLICE.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 44,521 hrs · 7,187 cycles

MAIN CABIN AT STATION 1065, LBL 11, SEAT TRACK WORN.

Part: BATTERY PACK — DETERIORATED · airframe 43,400 hrs · 6,986 cycles

EEL PATH LIGHTS FROM FORWARD GALLEY TO BUSINESS CLASS ON RH SIDE VERY DIM. REPLACED BATTERY PACK

Part: WIRE — SHORTED (FIRE LOOP) · airframe 42,991 hrs · 6,926 cycles

FLIGHT ENCOUNTERED STRONG ODOR, POSSIBLY ELECTRICAL SMOKE, IN COCKPIT. RT GENERATOR TRIPPED APPROX 20 MIN AFTER ODOR; FLIGHT DIVERTED TO DTW. FOUND RT ENGINE FIRE DETECT CARD M684 HEAT DAMAGED. CARD REPLACED; MAINTENANCE FOUND IDG WIRE W3538-301Y-18 (115VAC) SHORTED TO FIRE LOOP WIRE W3520-505R-16 (28VDC), LT SIDE OF ENG BEHIND OIL TANK. INTERIM REPAIR MADE; AFTER MAINT FERRY TO ORD, PERMANENT REPAIR ACCOMPLISHED.

Part: WIRE — SHORTED (IDG) · airframe 42,832 hrs · 6,901 cycles

SMOKE IN COCKPIT. WHEN SWITCHING OFF UTILITY BUSSES RT GENERATOR TRIPPED. UPON ARRIVAL AT BAQ, REPLACED RT GENERATOR CONTROL UNIT. ALSO FOUND RT ENGINE FIRE DETECTION CIRCUIT BREAKER OPEN ON P11 PANEL, AND HEAT DAMAGED RT ENGINE FIRE DETECT CARD M684. CARD REPLACED, AND CHECKED E AND E BAY FOR POSSIBLE WATER INGRESS. FOUND IDG WIRE W3538-301Y-18 SHORTED TO FIRE LOOP WIRE W3520-505R-16. REPAIRED SHORTED WIRE.

Part: PIN — BURNED (COCKPIT) · airframe 41,163 hrs · 6,611 cycles

POWER LOST TO FIRST OFFICERS PRIMARY INSTRUMENT BUSS. FLAGS IN VIEW ON FO AIRSPEED INDICATOR, RDMI, VERTICAL SPEED INDICATOR, EHSI AND EADI BLANK. FOUND PIN 4 OF D6430P BURNT, REPLACED PIN. THIS IS 'A' PHASE FROM FIRST OFFICER'S INSTRUMENT BUS VOLTAGE SENSE UNIT COMMON TO FIRST OFFICER'S INDICATORS. REPLACED D6430J DUE TO INSULATION DAMAGE. ALL SYSTEMS AND INDICATORS CHECK GOOD.

Part: CONTROLLER — SMOKE (GALLEY) · airframe 35,606 hrs · 5,648 cycles

P62 CART CONTROLLER IS SMOKING WHEN THE PIGTAIL IS UNPLUGGED.

Part: AIR DIST — ODOR (CABIN)

WITH RT RECIRC FAN OFF HAD CHEMICAL SMELL SIMILAR TO CHLORINE, THEN HAD HOT ELECTRICAL BURNING SMELL WITH RECIRC FAN BACK ON. THIS CONDITION OCCURRED ON THREE SEPARATE OCCASIONS. COULD NOT ISOLATE SOURCE. DIVERT YJT, EMERGENCY DECLARED, OVERWEIGHT LANDING. *S/D* CHEMICAL AND/OR ELECTRICAL SMELLS COULD NOT BE DUPLICATED ON THE POSITION FERRY FLIGHT TO IAD. IAD MAINTENANCE COULD NOT DUPLICATE THE CONDITION LISTED ABOVE. AIRCRAFT HAS NOT EXPERIENCED A REPORT OF CHEMICAL OR ELECTRICAL SMELL SINCE THIS OCCURANCE. SMELL MAY BE NON-AIRCRAFT RELATED.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY FLOOR LIGHTS FLICKER ON AND OFF. REPLACED BATTERIES, OPS CHECK OK.

Part: FIRE LOOP — MALFUNCTIONED (RT ENGINE)

RIGHT ENGINE FIRE LOOP 2 FAILS TEST. *S/D* ACFT EXPERIENCED A CHRONIC RIGHT ENGINE FIRE LOOP STATUS MESSAGE INFLIGHT, OK ON GROUND. SYSTEM WIRING WAS EXTENSIVELY CHECKED AND SEVERAL SYSTEM COMPONENTS WERE REPLACED. PROBLEM WAS ATTRIBUTED TO THE LWR AND/OR LWR AFT ENGINE FIRE LOOP. IT IS SUSPECTED THAT THESE LOOPS WERE FAILING DUE TO ENGINE VIBRATION. AFTER REPLACEMENT OF THESE LOOPS, THE ACFT HAS OPERATED NORMALLY.

Part: PIN — SHEARED (BLEED VLV)

2.5 BLEED DISCONNECTED FROM BLEED VALVE. ENGINE CHANGE REQUIRED. *S/D* BELL CRANK PIVOT PIN SHEARED. REPAIRED 2.5 BLEED LINKAGE. REPLACED PIVOT PIN WITH IMPROVED PIN, (P/N 510264). REPLACED BLEED VALVE SLIDER BLOCKS WITH ROLLERS.

Part: BATTERY — FAILED (APU)

APU WILL NOT START. BATTERY VOLTAGE DROPS TO 15 VOLTS DURING OPERATIONAL CHECK. *S/D* APU BATTERY FAILED. REPLACED BATTERY.

Part: MODULE — FAILED (FWD LAVATORY)

FORWARD LAVATORY WASTE TANK LOGIC CONTROL MODULE/CONTINUOUS LEVEL SENSOR REFLECTED FALSE FULL TANK INDICATION. CALIBRATION OF LOGIC CONTROL MODULE/CONTINUOUS LEVEL SENSOR LOST. REMOVED FOREIGN OBSTRUCTION AND RECALIBRATED LOGIC CONTROL MODULE.

Part: CONTROLS — STIFF (ELEVATOR)

UNABLE TO HOLD ALTITUDE AT 10,000 FEET ON AUTO-PILOT. DISCONNECTED AUTO-PILOT AND ELEVATOR WAS STIFF. FLEW FOR 5 TO 10 MINUTES USING STABILIZER FOR PITCH CONTROL. WHILE PUSHING UP AND DOWN SOMETHING LET GO AT 4,000 FEET. AIRCRAFT FLEW NORMAL FOR THE REST OF THE FLIGHT. *S/D* PERFORMED VISUAL INSPECTION OF CONTROL CABLE SYSTEM PER MM 27-31-00. NO FAULTS WERE FOUND IN MAINTENANCE CONTROL DISPLAY UNIT. CHECKED ELEVATOR WITH EACH HYDRAULIC SYSTEM INDIVIDUALLY AND FOUND NO FAULTS. NO SPECIFIC PARTS FOUND DAMAGED OR FAULTED.

Part: STRIP — INOPERATIVE (CABIN)

MID CROSS AISLE EEL STRIP INOPERABLE. REPLACED EEL STRIP, OPERATIONS CHECK NORMAL.