N663UA

Part: BOTTLE — NO DISCREPANCY (ZONE 800) · airframe 125,338 hrs · 19,145 cycles

SLIDE PRESSURE DOOR 2L NOT IN GREEN PERFORMED VISUAL INSPECTION OF DOOR 2L SLIDE PRESSURE GUAGE, FOUND WITHIN TOP OF GREEN BAND, WITHIN LIMITS, REF CYLINDER CHECKTASK 25-66-02-206-001, OK TO CONTINUE.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 124,852 hrs · 19,078 cycles

EMERGENCY LIGHTS, LT FWD ESCAPE SLIDE EMERGENCY LIGHT INOP, ESCAPE LIGHT LAMP RESEATED AND TESTED IAW AMM 33-51-06-902-082, LIGHT NOW OPERATES.

Part: BOTTLE — NO DISCREPANCY (ZONE 800) · airframe 124,406 hrs · 19,020 cycles

PLEASE CHECK DOOR 2L PRESSURE GAUGE INSPECTED DOOR 2L PRESSURE GUAGE. FOUND NEEDLE ONE NEEDLE WIDTH OVER (TOWARDS HIGHER END OF BAND) IAW AMM 25-66-02 A/C OK TO CONT. NOTE: A/C CABIN WAS HOT PRIOR TO APU PACKS BEING TURNED ON.

Part: NONE — NO DISCREPANCY (NONE) · airframe 123,736 hrs · 18,933 cycles

DURING A/C REFUELING, PRIOR TO ENG OR APU START, 1 F/A REPORTED STRONG FUEL SMELL IN ACFT. NO OTHER CREW OR PASSENGERS WERE EFFECTED BY ODOR. CAPTAIN WALKED TO BACK OF ACFT ON 3 DIFFERENT OCCASIONS AND NEVER NOTICED ANY SMELL OR FUMES/ VISIBLE SMOKE. STONG SMELL DISSAPPEARED QUICKLY AFTER REFUELING COMPLETED. AFTER DEBRIEFING CREW SMELL DETERMINED TO BE NON A/C RELATED.

Part: COMPRESSOR — NO DISCREPANCY (ZONE 400) · airframe 123,702 hrs · 18,929 cycles

LOUD BANG AND BRIGHT FLASH ON LEFT SIDE AFTER TAKE OFF POSSIBLE BIRD STRIKE CREW SAID THEY FELT KICKED TO THE LEFT WITH THE LOUD BANG AND THE WHITE FLASH FROM THE LEFT SIDE, ACCMP OVERWEIGHT LANDING INSPECTION AND BIRD STRIKE INSPECTION. REF AMM TASK 05-51-35-212 & AMM 05-51-18-212-001 NO DEFECTS NOTED. ACCOMPLISHED GVI OF 1ST STAGE STATOR REF AMM 72-00-00-206-001-N01 ITEM 2.G.(1)-(2), NO DAMAGE NOTED. BORESCOPE OF #1 ENGINE HPC SECTION, REF. AMM 72-00-00-206-001, NO LIMITING DAMAGE NOTED. REINSTALLED BOROSCOPE PLUGS, CLOSED ENGINE COWLS, ACCOMPLISHED IDLE RUN AND SATISFACTORY LEAK CHECK.

Part: MODULE — FAULTED (ZONE 200) · airframe 123,563 hrs · 18,909 cycles

OXYGEN MASKS DEPLOYED AT SEAT 11F RESTOWED PAX 02 MASKS ABOVE SEAT 11F REF AMM 35-21-15-532-150-001.

Part: UNKNOWN — VIBRATION · airframe 123,288 hrs · 18,872 cycles

AIR RETURN FOR VIBRATIONS IN FLIGHT CONTROLS CREW DEBRIEF STATED AT 10,000 FT FELT VIBRATION IN THE CAPTS AND FOS YOKE IN CLIMB TO CRUISE AT SPEEDS OF 250,280 TO 320 THE INTENSITY RAMPED UP AND STAYED THERE IN ALL PHASES OF FLIGHT. DURING TURNS, ASCENDING AND DESCENDING. HE COULD NOT ISOLATE WHETHER IT WAS AILERONS OR ELEVATOR ASSOCIATION.NOTHING FELT IN THE RUDDER PEDALS. THE INTENSITY STEPPED DOWN TO 50% ON FINAL APPROACH WITH FULL FLAPS. NO FLAP OVERSPEED AT ANY SETTING AND NO ECIAS MESSAGES INSPECTED APU DOOR REF MM 05-51-38-202-001 PART 1(A) "VIBRATION IN FLIGHT CONTROLS" NO DEFECTS NOTED. CHECKED APU DOOR FOR PROPER FAIRING IN CLOSED POSITION AND FOR ANY DEFECTS IN OPENED POSITION. NONE FOUND PERFORMED FIM 05-00 TASK 801 OPERATE ALL FLIGHT CONTROL SURFACES WITH ALL THREE HYDRAULIC SYSTEMS PRESSURIZED, STEP A - N, NO DEFECTS NOTED. NEED TO CONTINUE FROM THIS STEP. REF AMM# 05-51 TASK 801. CONTINUED STEPS O THRU S STAB OPERATION, BLOWOUT PANELS, STAB,APU DOOR AND FLAP LEADING AND TRAILING EDGES. NO DEFECTS FOUND OTHER THAN PANEL/SEAL ON LOG#4939600 AND #4939615. STILL REQUIRES LANING GEAR AND FILLET SEAL INSPECTIONS INSPECTED FLAP SLATS STEPS A THRU J. INSPECTED BLOWOUT PANELS STEPS A THRU C. APU DOOR STEPS A THRU F. STABILIZER STEPS A THRU D. NO DEFTECTS FOUND. REF #05-00 TASK 801 FILLET FAIRING AND ACCESS PANEL VISUALLY CHECKED AND LANDING GEAR DOORS CHECKED. IRW AMM 05-51 TASK 801.

Part: NONE — NONE (NONE) · airframe 122,360 hrs · 18,745 cycles

AFT LEFT DOOR PRESSURE GAUGE BELOW GREEN. VERIFIED GUAGE IS WITHIN SERVICABLE RANGE.

Part: SENSOR — FAULTED (SLAT SYS) · airframe 122,288 hrs · 18,734 cycles

TEST FLIGHT DISCREPANCY . . LE EDGE SLAT ASSYMETRY I N CLIMB. POSSIBLE OVERSPAT 33000 FEET, AIR SPEED REACHED 300 KNOTS FOR A SHORT PERIOD TIME. 50 KNOTS ABOVE MAX SPEED OF 250KNOTS PLUS NOTICED L.E FLAPS INDICATIONS START TO MOVE ALSO. BELOW 250KNOTS EVERYTHING APPEARS NORMAL ...PER TEST PILOT ...TOMC MO THE PANELS FIN 521BB, 521EB, 521JB, 521TB, 521ZB AND 521AFB OF THE LEADING EDGE SLAT SENSOR SWITCH WERE REMOVED AS PER AMM 57-41-01-000-801. PERFORMED OVERSPEED PHASE I INSPECTION AS PER. AMM 05-51-08-212-001. NO DAMAGE WAS FOUND DURING PHASE I INSPECTION. ACCOMPLISHED FLAP/SLAT ELETRONIC UNIT BITE PROCEDURE REF. FIM 27-51 FAULT TREE 809 PERFORMED BITE ON THE FSEU AND FOUND MESSAGE NUMBER 27-81021 WITH FAULT MESSAGE (LE OUTBD ASYM). REF. THE TABLE A FIG 104A PERFORMED BITE TO ISOLATE THE PROXIMITY SWITCH CAUSING THE INDICATION REF FIM 32-09-00/101, FIG 103. AND FOUND SENSOR S286 REF. SLAT #5 DAMAGED. NECESSARY REPLACE LEADING EDGE SLAT SENSOR SWITCH REF. AMM TASK 27-88-01-902-001. REPLACED LEADING EDGE SLAT SENSOR SWITCH OF THE POSITION S286 AND PERFORMED BITE OF THE PSEU SENSOR TARGET TO EXAMINE THE SENSOR SWITCH OPERATION REF. FIM 32-09 FAULT TREE 803 AND NOT FOUND FAULT. ACCOMPLISHED LEADING EDGE SLAT SWITCH INSTHE PANELS FIN 621BB, 621EB, 621JB, 621TB, 621ZB AND 621AFB OF THE LEADING EDGE SLAT SENSOR SWITCH WERE INSTALLED AS PER TASK 57-41-01-400-801 ITEM OK.

Part: SKIN — DAMAGED (RUDDER) · airframe 122,285 hrs · 18,732 cycles

DURING REMOVAL OF STATIC DISCHARGER BASE ON THE RUDDER WAS FOUND UNDER THE BASE FOUR HOLES OUT OF STANDARD ON LH SIDE AND ONE RH SIDE THE RUDDER UPPER PANEL SKIN STATIC DISCHARGER WAS REPAIRED AS PER EC/RA: 5540-01602. ITEM OK TO SERVICE. ALL APPLICABLE INSPECTION STEPS REQUESTED PER EC/RA 5540-01602 WERE ACCOMPLISHED.

Part: ACCESS PANEL — CRACKED (ZONE 100) · airframe 122,285 hrs · 18,732 cycles

DURING THE ACCOMPLISHEMENT OF EA 5300-01600-004, IT WAS FOUND A CRACK ON THE FORWARD OUTER CHORD INSIDE THE HORIZONTAL ACCESS PANEL. CHORD, RH PERMANENT REPAIR. THE PERMANENT REPAIR OF RH CHORD WAS ACCOMPLISHED AT TASK 76-0553-8-0153 AS PER EA5300-01600, OP 05 STA 1809 BHD OUTER

Part: SPAR — CRACKED (ZONE 400) · airframe 122,285 hrs · 18,732 cycles

RII INSPECTION REQUIRED DURING DVI OF STRUT #2 FIRE SEAL AND FIREWALL - TOP SURFACE INSPECTION WAS OBSERVED CRACK ON NACELLE STRUT FWD UPPER SURFACE. ACCOMPLISHED ALL EC/RA# 5451-01467 STEPS.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 122,285 hrs · 18,732 cycles

THERE ARE CORROSION POINTS ON THE BEAM LOCATED AT STA287 BETWEEN LBL 45.0 AND LBL 50.0 OF MAIN DECK FLOOR STRUCTURE. FOR REFERENCE SEE B767 SRM 53-10-51-0I-1 FIGURE 1 DETAIL I ITEM 20. (ORIGINATING DOCUMENT NR 2426011) AS COVERED IN NR 2426011 ALL STEPS OF EC/RA: #5310-08509 WERE ACCOMPLISHED WITHOUT DEVIATIONS.

Part: SKIN — CRACKED (ZONE 200) · airframe 122,285 hrs · 18,732 cycles

IT WAS FOUND A CRACK INDICATION AT FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER AFTER NDT INSPECION PART 6 51-00-16 REV 139. (ORIGINATING DOCUMENT NR2396712)

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 122,285 hrs · 18,732 cycles

DURING REMOVAL OF SHEAR TIE WAS FOUND OLD EXTERNAL DOUBLER SKIN WITH CORROSION AT STA 1540 AND BETWEEN STGR 39 LH AND 39RH (ORIGINATING DOCUMENT NR 2422715). ERMANENT SOLUTION WITH INSPECTION REQUIREMENTS THAT MUST BE ACCO 0 ON OR BEFORE THE AIRCRAFT REACHES 27,732 TOTAL FLIGHT CYCLES. 0 FLIGHT CYCLES. MPLISHED AS PER PART 2 OF THE LATEST REVISION OF EC/RA 5360-0192 ACCOMPLISH REPEATED INSPECTIONS AT INTERVALS NOT TO EXCEED 12,00 FUSELAGE SKIN BETWEEN STA 1540 AND STA 1562 & S-39L AND S-39R AT THE DRAIN HOLE LOCATION WAS REPAIRED ATGIG. THIS REPAIR IS A P

Part: SKIN — CRACKED (ZONE 200) · airframe 122,285 hrs · 18,732 cycles

FWD SERVICE DOOR AFTER CUTOUT - IT WAS FOUND A SKIN AND BEARSTRAP CRACK INDICATION IN THE MARKED HOLE AT 1 AND 7 ON''CLOCK POSITION. ( ORIGINATING DOCUMENT NR 2395993)

Part: UNKNOWN — ODOR (CABIN) · airframe 121,172 hrs · 18,586 cycles

SMELL OF ELECTRICAL SMOKE SMELLED IN ROW 42 PER CREW LIGHT IN THAT AREA FLICKERED FOR A MOMENT DURING EVENT OF SMELL REF L/P 9364747. DURING AND AFTER HIGH POWER ENGINE RUNS NO ELECTRIC SMELL OR FLICKERING LIGHTS NOTICED.CONDITIONAL INSPECTION REQUIRED BY TOMC AS PER AMM 05-51-56. PERFORMED INSPECTION REF 05-51-56-940-801-C1. FLIGHT DECK-C-1 A,B,C. NO EVIDENCE OF BURNING NOR ARCING. PERFORMED INSPECTION REF MM 05-51-56-940-801-C1. STEPS C (2)-(3) NO DEFECTS NOTED PERFORMED INSPECTION REF MM 05-51-56-940-801-C1. STEPS C (4)-(5)-(6). NO DEFECTS NOTED PERFORMED STEP C (7) INSPECTED APU EXTERNAL AIR INLET, WITH FLASHLIGHT AND MIRROR, INSPECTED FOR EVIDENCE OF OIL LEAKS. NO LEAKS NOTED PERFORMED INSPECTION REF MM 05-51-56-940-801-C1. APU EXAUST-D-4. OPERATIONAL CHECK NORMAL REF MM 49-11-00-802-002. NO SMOKE NOTED. OPERATIONAL CHECKS REF MM 05-51-56-940-801-C1. COMPLY WITH STEP D-5-6-7-8. PERFORMED INSPECTION REF MM 05-51-56-940-801-C1 STEPS D(1)A,B,C. PERFORMED INSPECTION REF MM 05-51-56-940-801-C1 STEPS D (2) (A,B,C,D) NO DEFECTS NOTED. PERFORMED INSPECTION REF05-51-56-940-801-C1 STEPS D (3)(A,B,C,D,E,F,G,H) NO DEFECTS NOTED. COMPLIED WITH INSPECTION REF05-51-56-940-801-C1 STEPS D (8 THRU 21A). NO DEFECTS NOTED AND NO SOURCE FOUND AT THIS POINT. ADD EMP:U188290 PER AMM 05-51-56-940-801-C1 PARA 1.6.A. STEPS E AND F DO NOT NEED TO BE ACCOMPLISHED UNLESS REQUESTED BY TOMC. "PER TOMC SHIFT MANAGER NO FURTHER ACTION IS REQUIRED. NO FUTHER ACTION REQUIRED AS PER PREVIOUS UPDATE.

Part: ESCAPE HATCH — OBSTRUCTED (ZONE 200) · airframe 120,382 hrs · 18,480 cycles

DURING REMOVAL OF LH OVERWING ESCAPE HATCH REF LOGPAGE 8707327, ESCAPE HATCH DOOR HITS LH CABIN CLASS DIVIDER FRAME PREVENTING CORRECT OPERATION OF EMERGENCY EXIT DOOR. CABIN CLASS DIVIDER ADJUSTED FORWARD ON SERATED PLATE AND CONFIRMATION OF ECAPE HATCH DOOR CLEARANCE TO DIVIDER CONFIRMED.

Part: NONE — NONE (NONE) · airframe 119,555 hrs · 18,366 cycles

PAX AT SEAT 5A DROPPED 13IN MACBOOK AIR INTO SIDEWALL. UNABLE TO RETREIVE OPENED LWR DECK LH SIDE WALL PANEL AT DRIVE BAY D. RETRIEVED 13 INCH MAC BOOK AS DESCRIBED AND GIVEN TO PILOT. INSPECTED AREA BEHIND DRIVE BAY ''D'' LH SIDE WALL PANEL - NO DAMAGE OR IRREGULARITIES FOUND. PERFORMED CLOSE UP INSPECTION AND RESECURED DRIVE BAY ''D'' SIDE WALL PANEL IAW AMM 25-52-01 REV 141. FWD CARGO BAY GOOD FOR USE.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHTS) · airframe 119,084 hrs · 18,300 cycles

IDT INSPECTION REQUIRED. EMERGENCY PATH LIGHT ASSY REPLACEMENT. EMERGENCY PATH LIGHT REPLACED SEE LOGPAGE: 7475861. IDT INSP REQUIRED. EMERGENCY LIGHT AT 228FR RT SIDE OF FRONT GALLEY INSPECTED REF AMM 33-51-10-962-173 AND SWPM SECTION 20-83. ALL FOUND SATISFACTORY.

Part: LIGHT — NO TEST (FWD GALLEY) · airframe 119,017 hrs · 18,291 cycles

EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - GALLEY 2A COMPARTMANT 228F/R EEL LIGHT INOP. RELAMPED THE EEL NIL HELP. EEL ASSY. SUSPECTED. PARTS ORDERED. EEL ASSEMBLY REPLACED IAW AMM: 33-51-10-962-173 AND SWPM: SECTION 20-83. LIGHT TESTED AND CONFIRMED FUNCTIONS NORMALLY. 75-2530-3-0336,QTY :1

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 118,922 hrs · 18,279 cycles

RIGHT MAIN LANDING GEAR DID NOT RETRACT AFTER TAKEOFF UPON ARRIVAL FIND OUT A MAJOR HYDRAULIC LEACK ON RIGHT MLG SUSPECTED TWO RIGID LINES SEE PICTURES FOUND RETRACT SYS HYDRAULIC HOSE LEAKING ABOVE R MLG, UNDER THE RETRACT ACTUATOR. REF IPC 32-32-54-05 ITEM 152. REMOVED AND REPLACED DAMAGED HYDRAULIC HOSE PER AMM 32-11-01/401. CYCLED GEAR HANDLE MULTIPLE TIMES WITH NO LEAKS NOTED. PERFORMED GEAR SWING PER AMM 32-32-00-735- 020 SEVERAL TIMES. GEAR OPERATION AND INDICATIONS WERE ALL NORMAL NO LEAKS NOTED AT THIS TIME.

Part: SKIN — DAMAGED (STA654 +121) · airframe 118,382 hrs · 18,208 cycles

LIGHTNING STRIKE ON EXTERIOR SKIN LOCASTED APPROX. STA 654+121 STR 34R. 53-00-01-2R-29 REPAIR 29. REPAIRED LIGHTNING STRIKE ON EXTERIOR SKIN AT STA 654+121 STR 34R PER B767-300 SRM RII INSPECTION FOR MJR-RII-SDR EXTERNAL FUSELAGE SKIN DOUBLER REPAIR ACCOMPLISHED PER SRM 53-00-01-2R-29, REPAIR 29 ON NON ROUTINE 167820-0100-0025.

Part: ANGLE — CRACKED (NR 1 NACELLE) · airframe 118,382 hrs · 18,208 cycles

#1 ENGINE PYLON I/B AND O/B SIDE HAS 2 EA. PANEL ATTACH STRAPS CRACKED ON AFT PYLON FRAME STA 410.

Part: SUPPORT ANGLE — CRACKED (BS 530) · airframe 118,382 hrs · 18,208 cycles

FIXED LE BRACE SUPPORT AT WS 530 CRACKED. REPLACED FIXED LE BRACE SUPPORT AT WS 530 IAW B767-300 SRM 51-40 -02.

Part: DISPLAY — INTERMITTENT (FO SIDE) · airframe 118,333 hrs · 18,201 cycles

FO CDU BLANK. CDU FUNC NORMAL UNTIL CRUISE THEN FLICKERED AND BL ANKED REF LOGPAGE 6732059 FOR LOGPAGE SIGNOFF.**CHRONIC LVL-0**DUE TO RECENT HISTORY OF FIRST OFFICERS CDU NOT RESPONDING OR FLICKERING ACCOMPISH THE FOLLOWING: 1) FIM 34-61 TREE 843, REPAIR AND REPORT ALL FAULTS. 2) IF NO FAULTS FOUND REPLACE THE FIRST OFFICERS CDU IAW AMM 34-61-02/401. THANKS! ORDLM GABRIEL TECH SUPP:FLT CREW STATED F/O CDU WAS STEADILY ON AFTER ENGINES WERE OFF.REF WD36-61-21-1A,PLEASE REMOVE CDU AND CHECK AT D467P PIN 40/41 FOR VAC,41 TO GND,36 TO GND,34 TO GND.CHECK CONNECTOR CONTACTS FOR INTEGRITY.THANKS CARRIED BY ELB PANEL, MCDU, ET OFF 19-3461-9-0006 3262 ON 0000 PANEL, MCDU, ET OFF 19-3461-9-0006 3262 ON 19-3461-9-0006 1593 PERFORMED FIM 34-61-843 NO DEFECTS WHERE NOTED ALSO SHOT PINS 40/41 FOR VAC AND PINS 41,36,AND 34 TO GND FOR INTEGRITY CHECK CHECK GOOD NO DEFECTS NOTED AT THIS TIME R&R FO CDU REF AMM 34-61-02-400-802 OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME. FOCDU REPLACED AS PRECAUTIONARY REQUESTED BY TECH SUPPORT FUP CLEARED PARTS USED: 19-3461-9-0006,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1544614 SN OFF 3262.

Part: SHUTOFF VALVE — FAILED (RT ENGINE) · airframe 116,190 hrs · 17,908 cycles

R ENG HPSOV EICAS ON T/O ROLL WITH ASSOC BLEED LIGHT. BLEED LIGHT DID NOT EXTINGUISH. V347 FAILED INTERNAL ELECTRICAL CHECK PER WDM 36-11-62, NEEDS NEW VALVE, REF AHM LP 5113215. REF AMM#36-11-18 REMOVED AND REPLACED HPSOV. LEAK AND OPS CHECKS GOOD WITH NO FURTHER MESSAGES NOTED. PARTS USED: 1728403,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1728403 SN OFF 0441 IPC REFERENCE # 36-11-01-50 VALVE, SHUTOFF, OFF 76-3611-9-0001 0441 ON 76-3611-9-0001 2142

Part: CIRCUIT BREAKER — TRIPPED (LT TAT PROBE) · airframe 114,125 hrs · 17,625 cycles

TAT PROBE EICAS MSG AFTER LIFT OFF. RAN QRH AND RETURED TO EWR. FLIGHT CREW STATES L TAT PROBE C/B TRIPPED WITH ASSOCIATED EICAS MSG. RESET C/B AND PERFORMED TAT PROBE HEAT SYSTEM OPERATIONAL TEST REF AMM 30-33-00-715-710. TEST PASSED SEVERAL TIMES WITH NO FAULTS. OK FOR SERVICE. LEFT TAT PROBE HEATER BREAKER ON P6 PANEL WAS RESET.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 113,671 hrs · 17,561 cycles

EMERGENCY ESCAPE SYS R FAILED TEST ON P 61.( EMERGENCY BATT. PACKS M962 (DISCHARGED) (REF AAR NR 9669192) REMOVED, REPLACED AND TESTED NORMAL M962 BATTERY FOR EMERGENCY ESCAPE RIGHT SIDE, PUSH TO TEST TESTED NORMAL REF B767 AMM 25-65-17-004-001-001, 25-65-17-404-008-001 AND STEP 3 G (11) OF 25-65-00-442-010.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 113,671 hrs · 17,561 cycles

SEVERAL EMERGENCY LIGHT INOP THROUGH OUT THE CABIN AREA. (REF AAR NR 9669188) REMOVED AND REPLACED BATTERY PACK POS M732 AS PER B737 AMM 33-51-02. PERFORMED OPS CHECK AND FOUND NORMAL ASSOCIATED EMERGENCY LIGHTS.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 113,671 hrs · 17,561 cycles

EMERGENCY ESCAPE SYS L FAILED TEST ON P 61.( EMERGENCY BATT. PACKS M 961 (DISCHARGED) (REF AAR NR 9669191) REMOVED, REPLACED AND TESTED NORMAL M961 BATTERY FOR LEFT EMERGENCY ESCAPE, PUSH TO TEST TESTED NORMAL REF B767 AMM 25-65-17-004-001-001, 25-65-17-404-008-001 AND STEP 3 G (11) OF 25-65-00-442-010.

Part: BATTERY — INOPERATIVE (STA 873) · airframe 112,764 hrs · 17,437 cycles

ROWS 21-23 AISLE EMERGENCY FLOOR LEVEL LIGHTING AND L+R OVERWING EXIT SIGNS AND RIGHT AISLE OVERHEAD EXIT SIGNS REMAIN ILLUMINATED WHEN AIRCRAFT IS DOWN POWERED WITH P5 EMERGENCY LIGHT SWITCH IN THE "OFF" POSITION. AIRCRAFT COMPLETELY DOWN POWERED WITH EXTERNAL POWER REMOVED AND STILL REMAINS ILLUMINATED. SUSPECT M1209 BATTERY/CHARGER. FOR INFO. SDR RAISED.

Part: DUCT — FAILED (NA) · airframe 111,863 hrs · 17,314 cycles

PER CREW AT 7000'' RIGHT DUCT LEAK LIGHT CAME ON WITH RIGHT BLEED DUCT LEAK EICAS MESSAGE. AT 14,000'' DUMPED 10,000 LBS FUEL. RAN CHECKLIST NO FIX. LANDED ROUGHLY 20,000 LBS OVERWEIGHT. ON P11 OPENED BUT REAPPEARS WHEN CLOSED. RAN FIM 26-18 FAULT TREE 804 BLOCK 1-8 "R BLD DUCT LEAK" EICAS MESSAGE AND RT DUCT LEAK LIGHT REMAIN ON. REPLACED AND REINSTALLED ORIGINAL DUCT LEAK CIRCUIT CARD (M691) FIRELOOP CONNECTOR NEEDS SAFETYING AND COVER PANEL IN RT REFERENCE LP 8765540 FOR OVERWEIGHT LANDING. REF WDM26-18-21-1 FOUND ELEMENT TS214 SHORTED. NEEDS REPLACEMENT SECURED FIRE LOOP CONNECTORS IN RIGHT WHEEL WELL AND SECURED IN P54, REPLACED K693 RELAY IN P37 AND CHECKED RESISTANCE ON RT WHEELWELL CEILING REINSTALLED. M&E 76-2618-3-0002 COVER PANEL REF L/P 8765683. WHEELWELL FIRELOOP READ 1.1 OHMS. NO OBVIOUS DUCT DAMAGE IN WING ROTABLE PARTS CHANGE WAS INDICATED - TT # 1179464 SN OFF 5279 LEADING EDGE OR WING ROOT NOTED. MESSAGE DISAPPEARS WHEN CB B10 ADD EMP:138125 IPC REFERENCE # CARD, ASSY, DUC OFF 64-2618-9-9001 7981 ON 64-2618-9-9001 1053 REPLACED #2 PYLON FIRELOOP TS214 REF AMM 26-11-02-424-033. NO CLOSE UP. EICAS FAULTS, NO #2 DUCT LEAK INDICATOR LAMP. PERFORMED INSTALLATION TEST, TESTS GOOD. DUE TO ITEM WAS A HARD FAULT, NO ENGINE RUN DETERMINATION WAS MADE. SEE L/P 8768314 ASSOCIATED

Part: ENGINE — FAILED (#2 ENGINE) · airframe 110,655 hrs · 17,149 cycles

2 LOUD BANGS FOLLOWED BY RIGHT ENG POWER LOSS - PWR CAME BACK W/IN 10 SECS AT 10000 FEET. R ENG SURGE DET MESSAGE SEE PICTURES FOR INFO. RT ENG PIMU BITE REVEALED NO RELATED OR ASSOCIATED MESSAGES AS T CONTINUING WITH FIM-71-05/803 BLOCK 2 THRU BLOCK 6, VISUALS ACP''D HPC BLADES BORESCOPE FROM STAGE 10 AND UP TO STAGE 11, O POSSIBLE CAUSE OF STALLS OR SURGE AS STATED IN BLOCK 1 OF FIM CHECK GOOD & N1 TURN FREELY BOTH DIRECTIONS. INLET/TAIL NO FOUND MOST BLADES ARE DAMAGED AND TORN. CONDITION IS BEYOND FLY 71-05/803. VISUAL CHECKS PER FIM IN PROGRESS INCL BORO PREP OPEN DAMAGE AND 2.5 / 2.9 BLEED VALVE OPENINGS CLEAN..... BOROSCOPE BACK LIMITS, REF AMM 72-00-00-206-001-N01. VIDEO UPLOADED ON RVI ING PER BLOCK 7. UPDATE TO FOLLOW SITES. ENG SN 727948 REPLACED.ACCOMPLISHED #2 ENGINE RUNUP TEST #3, #6, AND #15 PER AMM 71-00-00/501 OPS CHECK GOOD NO LEAKS NOTED.

Part: PLATE — DENTED (TE FLAP) · airframe 110,397 hrs · 17,107 cycles

RIGHT INBOARD TRAILING EDGE FLAT HAS NUMEROUS DENTS DUE TO HAIL SHOULD READ TRAILING EDGE FLAP. REF SRM 57-53-01-1A-1 LOCKED FOR FERRY FLIGHT - ESC EVALUATED ALLOWABLE DAMAGED. UNLOCKED TO CLEAR LOGPAGE REFER FORM44-0008 ITEM1-32 ACCOMPLISHED. WORK ACCOMPLISHED BY MECHANIC V926591, AND INSPECTED BY V898550 RIGHT INBOARD TRAILING EDGE FLAT PERFORMED REPAIR AS PER RI-57-00-15243 REV A AND ECRA5753-01988. ADD EMP:V898550

Part: BEAM — CORRODED (STA1153) · airframe 110,397 hrs · 17,107 cycles

B767-53-3-7154 AFT CARGO COMPT - FLOOR SUPPORT BEAM BOTTOM SIDE 5EA ANCHOR NUT AREA CORROSION FOUND STA1153 BTN RBL9" TO LBL36" AS MARKED. TRANSFER REF. NON - ROUTINE ZHF510485 AND ORIGINATED BY EMP V896820 AFT CARGO COMPT STA1153 FLOOR BEAM UPPER CHORD REPLACED AS PER SRM51-10-02, ATTACH FORM 44-0008 ITEM1-23 ACCOMPLISHED. WORK ACCOMPLISHED BY MECHANIC V897467 INSPECTED BY V912779 ADD EMP:V912779 RII ACCOMPLISHED BY V898550, SC NG, HX169509

Part: NONE — CORRODED (AFT CARGO COMP) · airframe 110,397 hrs · 17,107 cycles

B767-53-3-7154 AFT CARGO COMPT - FLOOR SUPPORT BEAM BOTTOM SIDE 5EA ANCHOR NUT AREA CORROSION FOUND STA1153 BTN RBL9" TO LBL36" AS MARKED. TRANSFER REF. NON - ROUTINE ZHF510485 AND ORIGINATED BY EMP V896820 AFT CARGO COMPT STA1153 FLOOR BEAM UPPER CHORD REPLACED AS PER SRM51-10-02, ATTACH FORM 44-0008 ITEM1-23 ACCOMPLISHED. WORK ACCOMPLISHED BY MECHANIC V897467 INSPECTED BY V912779 ADD EMP:V912779 RII ACCOMPLISHED BY V898550, SC NG, HX169509

Part: NONE — CORRODED (AFT CARGO COMP) · airframe 110,397 hrs · 17,107 cycles

B767-53-3-7154 AFT CARGO COMPT - FLOOR BEAM BOTTOM SIDE SEVERAL ANCHOR NUT AREA CORROSION FOUND AT STA1329 BTN RBL16"-RBL29" AS MARKED. TRANSFER REF. NON - ROUTINE ZHF513877 AND ORIGINATED BY EMP V896820 AFT CARGO COMPT STA1329 BETWEEN LBL43 AND RBL43 FLOOR BEAM UPPER CHORD REPLACED AS PER SRM51-10-02 AND INSTALLED AS PER SRM51-40-02. ATTACHED FORM 44-0008 ITEM1-28 ACCOMPLISHED. WORK ACCOMPLISHED BY MECHANIC V897467, AND INSPECTED BY V912779 ADD EMP:V912779 RII ACCOMPLISHED BY V896825, CM LUI, HX146276

Part: SKIN — NONE (BULK CARGO DOOR) · airframe 110,397 hrs · 17,107 cycles

SUPPORT TASK - BULK CARGO DOOR OUTER SKIN AFT EDGE PREVIOUS REPAIR DOUBLER HAS DENT. TRANSFER REF. NON - ROUTINE ZHF517134 AND ORIGINATED BY EMP V896888 RII INSPECTED BY HX169509 ADD EMP:V898550 BULK CARGO DOOR OUTER SKIN INTERIM REPAIRED AS PER ECRA 5236-01027. ATTACHED FORM 44-008 ITEM 1 TO ITEM 31 ACCOMPLISHED (ECRA 5236-01027 PART 1A). DOUBLER LOCATED AFT EDGE MIDWAY UP ADD EMP:V906762 REACHING 30,000 TOTAL DR FLIGHT CYCLE. REPEAT THE INSP AT P/N: 146T6301-3 S/N: 000516 IS AN ORIGINAL DR. TOTAL ACFT CYCLE INTERVAL NOT TO EXCEED 3,000 DOOR CYCLES THEREAFTER "NOTE: DR EQUALS TO TOTAL DOOR FLIGHT CYCLE" REF EC 5236-01027 PART 1.B - ACCOMPLISH INSP OF REPAIR INSTALLED ON BULK CARGO DR PER LATEST REV OF EC 5236-01027 PT 2, BEFORE ALL WORK DOCUMENTED ON HAECO NRC ZHF517134 WITH ATTACHED 44-0008, V906762, QC HX169509 REF ECRA 5236-01027, ACCOMPLISH INSP OF RPR INSTALLED ON BULK TOMC-APPROVAL FROM SC1ELBYC COMMENT CARGO DOOR PER PART 2, BEFORE REACHING 30,000 TOTAL DOOR FLIGHT CYCLE. REPEAT THE INSPECTION AT INTERVAL NOT EXCEED 3,000 DOOR CYCLES, THEREAFTER"NOTE: DOOR P/N: 146T6301-3 S/N: 000516 IS AN ORIGINAL DOOR. TOTAL AIRCRAFT CYCLE EQUALS TO TOTAL DOOR FLIGHT CYCLE QC QC REVIEWED. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: NONE — CORRODED (FWD CARGO COMMP) · airframe 110,397 hrs · 17,107 cycles

B767-53-3-7025 FWD CARGO COMPT - FLOOR BEAM UPPER SURFACE CORROSION CRACK AT STA632 BTN LBL30"-LBL32" AS MARKED. TRANSFER REF. NON - ROUTINE ZHF516482 AND ORIGINATED BY EMP V896820 FWD CARGO COMPT STA 632 BETWEEN LBL 43 AND RBL 43 FLOOR BEAM UPPER CHORD REPLACED AS PER SRM 51-10-02. WORK ACCOMPLISHED BY V897532 AND INSPECTED BY V912779 ADD EMP:V912779 RII ACCOMPLISHED BY V898550 SC NG, HX 169509.

Part: FLOORBEAM — CORRODED (BS 632 LBL 30-32) · airframe 110,397 hrs · 17,107 cycles

B767-53-3-7025 FWD CARGO COMPT - FLOOR BEAM UPPER SURFACE CORROSION CRACK AT STA632 BTN LBL30"-LBL32" AS MARKED. FWD CARGO COMPT STA 632 BETWEEN LBL 43 AND RBL 43 FLOOR BEAM UPPER CHORD REPLACED AS PER SRM 51-10-02.

Part: FLOORBEAM — CORRODED (BS 1329 RBL16-29) · airframe 110,397 hrs · 17,107 cycles

B767-53-3-7154 AFT CARGO COMPT - FLOOR BEAM BOTTOM SIDE SEVERAL ANCHOR NUT AREA CORROSION FOUND AT STA1329 BTN RBL16"-RBL29" AS MARKED. TRANSFER REF. NON - ROUTINE ZHF513877 AND AFT CARGO COMPT STA1329 BETWEEN LBL43 AND RBL43 FLOOR BEAM UPPER CHORD REPLACED AS PER SRM51-10-02 AND INSTALLED AS PER SRM51-40-02. ATTACHED FORM 44-0008 ITEM1-28 ACCOMPLISHED.

Part: SHEAR TIE — CORRODED (BS 1540 S37-38R) · airframe 110,397 hrs · 17,107 cycles

B767-53-3-7056 BULK CARGO COMPT - BELOW FLOOR SHEAR TIE CORROSION FOUND AT STA1540 S37R-S38R AS MARKED TRANSFER REF. NON - ROUTINE ZHF512861 AND ORIGINATED BY EMP V896820 BULK CARGO COMPT STA1540 BETWEEN STR37R AND 38R SHEAR TIE REPLACED AS PER SRM51-10-02 ATTACHED FORM 44-0008 ITEM1-11 ACCOMPLISHED. WORK ACCOMPLISHED BY MECHANIC V926514 AND INSPECTED BY V912779 ADD EMP:V912779

Part: BRACKET — CORRODED (STA999) · airframe 110,397 hrs · 17,107 cycles

B767-53-3-7077 CABIN - LH STA999 S-16L TO S-17L SHEAR TIE FOUND CORRODED. TRANSFER REF. NON - ROUTINE LP9130759 AND ORIGINATED BY EMP V926653 CABIN BS999 BETWEEN STR16L AND STR17L SHEAR TIE REPLACED AS PER SRM51-10-02 AND INSTALLED AS PER SRM51-40-02, ATTACH FORM 44-0008 ITEM1 TO ITEM8 ACCOMPLISHED. WORK ACCOMPLISHED BY MECHANIC V897381, AND INSPECTED BY V896920 ADD EMP:V896920

Part: BRACKET — CORRODED (S16L) · airframe 110,397 hrs · 17,107 cycles

B767-53-3-7077 CABIN - S16L - S17L JOINT BRACKET FOUND CORRODED. TRANSFER REF. NON - ROUTINE LP9130782 AND ORIGINATED BY EMP V923418 CABIN BS977 BETWEEN STR16L AND STR17L SHEAR TIE REPLACED AS PER SRM51-10-02 AND INSTALLED AS PER SRM51-40-02, ATTACH FORM 44-0008 ITEM1 TO ITEM8 ACCOMPLISHED. WORK ACCOMPLISHED BY MECHANIC V897381, AND INSPECTED BY V896920 ADD EMP:V896920

Part: BRACKET — CORRODED (S16L-17L) · airframe 110,397 hrs · 17,107 cycles

B767-53-3-7077 CABIN - S16L - S17L JOINT BRACKET FOUND CORRODED. TRANSFER REF. NON - ROUTINE LP9130782 AND ORIGINATED BY EMP V923418 CABIN BS977 BETWEEN STR16L AND STR17L SHEAR TIE REPLACED AS PER SRM51-10-02 AND INSTALLED AS PER SRM51-40-02, ATTACH FORM 44-0008 ITEM1 TO ITEM8 ACCOMPLISHED. WORK ACCOMPLISHED BY MECHANIC V897381, AND INSPECTED BY V896920 ADD EMP:V896920

Part: SHEAR TIE — CORRODED (STA1540) · airframe 110,397 hrs · 17,107 cycles

B767-53-3-7056 BULK CARGO COMPT - BELOW FLOOR SHEAR TIE CORROSION FOUND AT STA1540 S37R-S38R AS MARKED TRANSFER REF. NON - ROUTINE ZHF512861 AND ORIGINATED BY EMP V896820

Part: NONE — CRACKED (NOSE WW) · airframe 110,397 hrs · 17,107 cycles

EA5300-01606 REV A OP 001 NOSE WHEEL WELL BULKHEAD LH VERTICAL CHORD ABOVE WL159 FOUND 1EA CRACK AS MARKED TRANSFER REF. NON - ROUTINE LP9130522 AND ORIGINATED BY EMP V914372 LH NOSE WHEEL WELL VERTICAL STIFFENER ON STA287 BETWEEN WL159 INSPECTED BY V896888 AND WL185 REPAIRED AS PER EA5300-01606 REV A OP 003 REFER SEQ NO.2303 FOR WORK DETAIL. WORK ACCOMPLISHED BY MECHANIC V897381 ADD EMP:V896888

Part: NONE — CRACKED (NOSE WW) · airframe 110,397 hrs · 17,107 cycles

EA5300-01606 REV A OP 001 NOSE WHEEL WELL BULKHEAD LH VERTICAL CHORD ABOVE WL159 FOUND 1EA CRACK AS MARKED TRANSFER REF. NON - ROUTINE LP9130522 AND ORIGINATED BY EMP V914372 LH NOSE WHEEL WELL VERTICAL STIFFENER ON STA287 BETWEEN WL159 INSPECTED BY V896888 AND WL185 REPAIRED AS PER EA5300-01606 REV A OP 003 REFER SEQ NO.2303 FOR WORK DETAIL. WORK ACCOMPLISHED BY MECHANIC V897381 ADD EMP:V896888

Part: DUCT — BROKEN (BLEED AIR SYS)

CAPTAIN REPORTED STRANGE NOISE AND HE WAS UNSURE WHERE IT CAME FROM. TORUBLESHOOTING STARTED AND FOUND NOISE FROM THE MAIN WHEEL BAY. DOORS WERE OPENED AND FOUND BLACK MARKINGS AND HISSING NOISE FROM SUPPLY DUCT FROM THE APU TO THE A/C SYSTEM. FOUND BLEED AIR DUCT CRACKED 40% OF DIAMETER. DUCT REPLACED AND CRS ISSUED. OCCURRENCE REPORT MADE. AFTER DUCT REPLACEMENT NOISE WAS STILL PRESENT, FURTHER T/S CARRIED OUT AND IN CONSULT WITH THE MOC INOPED APU BLEED AIR. NEXT DAY, UNITED FOUND ANOTHER DEFXECT OF THE APU CASING WHICH CAUSED THE VIBRATION/NOISE, DEFECT SOLVED.

Part: WARNING MESSAGE — FALSE ACTIVATION (RUDDER RATIO) · airframe 109,956 hrs · 17,046 cycles

RUDDER RATIO EICAS ILLUMINATED MSG APPEARED AFTER GO AROUND ON MANCHESTER. IAW FIM 27-21 TASK 8 04 FLAG NO.5 THIS COULD BE A NUISANCE MESSAGE IN GUSTY WIND COND ITIONS. RESET MODULES. PERFORMED BITE IAW FIM 27-09-00-815-814 A ND TEST RUDDER RATION SYST IAW AMM 27-21-00-825-036-001. ALL SAT IS. DISCUSSED COMPLAINT WITH CONTROLLER GORMAN AND SENIOR MANAGER MC NEELY. THEY AGREED WITH THE MAINTENANCE ACTIONS.

Part: SKIN — CRACKED (LT WING) · airframe 107,399 hrs · 16,684 cycles

PERFORMED (BHEC) INSP AT L/W REPAIR/PREVENTATIVE MOD OF I/B SEGMENT STR L-9.5, CRACKS NOTED AT 3 OPEN FASTENER HOLES MARKED IN RED. FABRICATED AND INSTALLED FREEZE PLUG REPAIRS PER DWG 767-9420 & SRM 51-20-07 BY OUTSIDE VENDOR P.O# 1622069 AT L/WING ON EXTREME O/B AND I/B HOLES STR L-9.5

Part: SKIN — CRACKED (RT WING) · airframe 107,399 hrs · 16,684 cycles

12 O''CLOCK & 6 O''CLOCK CRACK FOUND AT R/W LOWER SKIN STR L-9.5 BETWEEN RIB 31 AND 30 MOST OUTBOARD OPEN FASTENER HOLE FABRICATED AND INSTALLED FRAME PLUGE REPAIR PER B767 DWG 767-9420 AND SRM 51-20-01

Part: MODULE — FAULTY (MLG HANDLE) · airframe 101,755 hrs · 15,934 cycles

GEAR DISAGREE LIGHT AND ASSOCIATED EICAS WITH TAILSKID LIGHT, AND EICAS ON FINAL. EMERGENCY DECLARED. FOUND MESSAGE WOULD CLEAR WITH SLIGHT MOVEMENT OF GEAR HANDLE. R & R THE LANDING GEAR CONTROL LEVER MODULE IAW AMM32-31-01. ALL TESTS PASSED.

Part: LIGHT — BROKEN (FWD GALLEY) · airframe 101,207 hrs · 15,855 cycles

FWD GALLEY BS 217 FACING ON RIGHT SIDE LOWER EMERGENCY LIGHT COVER AND BULB BROKEN. REPLACED THE LIGHT ASSY. OPS OK.

Part: GUARD — OUT OF ADJUST (LIGHT PANEL) · airframe 101,148 hrs · 15,845 cycles

EMER LIGHTS WILL NOT ARM. ADJUSTED GUARD ON EMERGENCY LIGHT SWITCH. OPS CK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 101,073 hrs · 15,834 cycles

ONE LT AFT FUSELAGE EMERGENCY LIGHT FWD OF L4 DOOR IS INOP. REMOVED AND REPLACED LT AFT FUSELAGE EMERGENCY LIGHT FWD OF L4 DOOR IAW AMM 33-51-06-902-082. OPS CHECK GOOD.

Part: HOUSING — CHAFED (CRGO DOOR HANDLE) · airframe 101,073 hrs · 15,834 cycles

BULK CARGO DOOR EXTERNAL HANDLE HOUSING IS CHAFED ON THE INSIDE. REMOVED AND REPLACED THE CARGO DOOR HANDLE HOUSING IAW IAW SRM 51-40-02

Part: UNKNOWN — ODOR (LAVATORY) · airframe 100,870 hrs · 15,808 cycles

AFT RIGHT LAVATORY HAS BURNING ODOR, PEFORMED EC/RA 0500-01055. PEFORMED DETAILED IN SPECTION AND OPERATIONAL CHECKS IAW ECRA. NO DEFECTS NOTED ON THE GROUND. OK TO CONTINUE SERVICE.

Part: FLASHLIGHT — DETACHED (CABIN) · airframe 100,775 hrs · 15,795 cycles

FLASHLIGHT INOPERATIVE. SEATED THE FLASHLIGHT IN THE CRADLE, OPS CHECKED NORMAL.

Part: PLUG — DIRTY (LT REVERSER) · airframe 100,186 hrs · 15,720 cycles

LT REVERSER ISOLATION VALVE EICAS THE LEFT THRUST REVERSER ISOLATION VALVE HAS A FAILURE. L REV ISLN VAL EICAS MSG ON LANDING. TR WOULD NOT DEPLOY. TS REF FIM 78-34-00-815-807 NOO. FOUND ISOLATION VALVE PLUG DIRTY. CLEANED PLUG. VERIFIED NO LTS ON TR RELAY MODULE. OPERATED TR THROUGH 10 CYCLES AND ALL INDICATIONS NORMAL. NO MSGS

Part: LENS — CRACKED (EXTERIOR) · airframe 99,181 hrs · 15,580 cycles

EXT EMERG LIGHT SMALL LENS CRACKED LOC. LT JUST AFT OF IB FLAP T/E REPLACED LENS ASSY.

Part: CHILLER — ODOR (AFT GALLEY) · airframe 99,013 hrs · 15,557 cycles

ELECTRICAL ODOR IN AFT GALLEY. REMOVED AND REPLACED THE RT CHILLER. OPS CHECKED GOOD IAW AMM 25-33-02.

Part: FUSE — BLOWN (CABIN) · airframe 98,726 hrs · 15,518 cycles

DURING A CHK EMERGENCY LIGHT OPS CHK, FOUND WING RT SLIDE GND ILLUMINATING LIGHT L644 INOP. REF WIRING MANUAL 33-51-21. T/SHOT WIRING LIGHT FIXTURE, NO VOLTAGE. FOUND LIGHT L644 AND L392 BOTH INOP, FOUND NR 2 FUSE ON BATTERY PACK M733 OPEN. REPLACED FUSE, BOTH LIGHTS NOW OP CHECK GOOD.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 98,680 hrs · 15,511 cycles

1L LOWER EMER EXIT LIGHT IS FLICKERING ON AND OFF . EMER LIGHTS SWITCH IN THE ARMED POSITION. REMOVED AND REPLACED BATTERY POWER SUPPLY M1557 AWM 33-5-14 PG 2A OPS CHECK GOOD.

Part: LIGHT — FAULTY (CABIN) · airframe 98,306 hrs · 15,455 cycles

DOOR 1L EMERGENCY EXIT LIGHTS CAME ON 45 MINS INTO FLT STDY AT FIRST THEN FLICKERED. PRES NORMAL REMOVED UPPER L1 DOOR EMERGENCY EXIT LIGHT, INSPECTED CONNECTION WIRES WITH NO ISSUES NOTED. REPLACED UPPER L1 EXIT LIGHT ASSY REF AMM 33-51-01. OPS CHECK NORMAL.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 97,629 hrs · 15,359 cycles

L1 DOOR EMERGENCY EXIT LIGHT INTERMITTENT. LIGHT OPS CHECKS OK AND NORMAL

Part: FRAME — CRACKED (FUSELAGE) · airframe 86,582 hrs · 9,967 cycles

STATION 1140 RT TENSION TIE FRAME WEB, 2 EACH FASTNER HOLES CRACKED. STATION 1140 RT TENSION TIE FRAME WEB R & R IAW SRM 53-40-07 REPAIR 2 FIG 201 REV 94 & DWG 65B01570 REV C.

Part: FASTENER — LOOSE (BODY FAIRING) · airframe 92,921 hrs · 14,703 cycles

A VIBRATION WAS FELT FROM APPROX MID CABIN GOING AFT. THE RT ELEVATOR INDICATION ON THE LOWER EICAS PAGE WAS INDICATING A FLUTTERING OF ABOUT 1 INDICATOR WIDTH. NO VIBRATION WAS FELT IN THE COLUMN OR YOKE. THE CTR AP WAS ENGAGED & REMAINED ENGAGED. CHANGES IN AIRSPEED & ALTITUDE DID NOT SEEM TO CONSISTENTLY AFFECT THE FLUTTERING IND ON EICAS. WHILE ACCOMPLISHING AIRFRAME VIBRATION CONDITIONAL INSPECTION IAW AMM 05-51-38, FOUND LT MOST AFT WING TO BODY FAIRING FASTENERS LOOSE. SECURED, ACCOMPLISHED ELEVATOR OPERATIONAL CHECK IAW AMM 27-31-00. NO DISCREPANCIES NOTED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 91,822 hrs · 14,560 cycles

2R WING SLIDE EMER LIGHT INOPERATIVE & AFT RT DOOR SLIDE EMER LIGHT INOPERATIVE. FOUND BATTERY & CHARGER FOR EMER LIGHT POWER SUPPLY INOPERATIVE M733 REFERENCE SSM 33-51-0 1. REPLACED BATTERY & CHARGER ASSEMBLY IAW AMM 33-51-07. OPERATIONS CHECKED GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 90,829 hrs · 14,424 cycles

SEAT MOUNTED EMER EXIT LIGHTS INOPERATIVE FROM SEAT ROWS 1 RT - 10 RT. FOUND BROKEN WIRES WDM 33- 51-12 BELOW & OTBD OF SEAT 1R W1222-902R, W1222-902 BLK REPAIRED & SPLICED IAW SWPM 20-30-12. LIGHTS OPERATE NORMAL.

Part: SENSOR — FAULTY (LE SLAT) · airframe 89,505 hrs · 14,246 cycles

GENERATED FOR FLIGHT CREW. AFTER TAKEOFF FLAPS 1 TO UP, EICAS LE SLAT ASYM FLAP INDICATOR STOPPED BETWEEN 1 & 0. ALT FLAP CHECKLIST USED. . S295 SENSOR REPLACEMENT NR 11 SLAT. PERFORMED TESTS IAW AMM 27-88-01. ALL TESTS PASSED AT THIS TIME. OK TO CONTINUE.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 89,504 hrs · 14,244 cycles

DOOR TEST LIGHT IN THE FLIGHT DECK WOULD NOT ILLUMINATE DURING TEST MODE. SECURED LT EMER LIGHT BATTERY PACK CONNECTOR. TESTED SYS OPERATIONS CHECKED NORMAL

Part: WIRE — DISCONNECTED (CABIN) · airframe 89,504 hrs · 14,244 cycles

LEFT, RIGHT & CENTER MID EMER LIGHT BARS INOPERATIVE. RECONNECTED FEEDER WIRES ON CTR, LT & MID EMER LIGHT BARS. R & R RT MID EMER LIGHT BAR IAW MM 33-51-10, OPERATIONS CHECKED GOOD IAW MM 33-51-10.

Part: CABLE — KINKED (EMERGENCY EXIT) · airframe 89,504 hrs · 14,244 cycles

LEFT AFT OVERWING EMER ESCAPE HATCH EXTERIOR AFT DOOR CABLE KINKED. REPLACED LT AFT OVERWING EMER ESCAPE HATCH, EXTERIOR AFT DOOR CABLE IAW MM 52-21-01.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 89,504 hrs · 14,244 cycles

LEFT STATION 955 FAIL SAFE STRAP LOWER FASTENER HOLE HAS CRACK INDICATION. ACCOMPLISHED EA 5340-01478, REV A, OPS 03 AS REQUIRED ON JC COA-691845003.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,504 hrs · 14,244 cycles

AFT CARGO COMPARTMENT BILGE FLOORBEAM T CAP CORROSION UNDER NUTPLATE STATION 1197 PLUS 70 RB 40. REMOVED CORROSION BEYOND ALLOWABLE LIMITS. R & R IAW SRM 51-40-02 & DWG 146T1206. R & R ROLLER TRAY B1A & B6A IAW SRM 51040-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,504 hrs · 14,244 cycles

AFT CARGO COMPARTMENT BILGE FLOOR PAN BEAM AT STATION 1220 CORRODED AT SEVERAL NUTPLATES MARKED APPROXIMATELY 8. R & R FLOORBEAM J CHANNEL UPPER CHORD IAW 51-40-02 & DWG 146 1060.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,504 hrs · 14,244 cycles

AFT CARGO COMPARTMENT BILGE FLOORBEAM T CAP CORROSION UNDER NUTPLATES AT STATION 1197 - 114 RB 43 & LB 43. INSTALLED NEW CHORD IAW 51-40-02 & DWG 146T1060.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,504 hrs · 14,244 cycles

AFT CARGO COMPARTMENT BILGE FLOOR T CAP CORROSION UNDER NUTPLATE AT STATION 1200 RB43. R & R CHORD IAW SRM 51-40-02 & 51-40-05.

Part: WIRE — BROKEN (CABIN) · airframe 89,325 hrs · 14,217 cycles

RIGHT MID LAVATORY MS4 EEL LIGHT STRIP HAS BROKEN WIRES. R & R RT MID LAVATORY EEL LIGHT STRIP IAW AMM 3 3-51-10, OPERATIONS CHECK GOOD.

Part: SMOKE GOGGLES — CONTAMINATED (COCKPIT) · airframe 87,638 hrs · 13,992 cycles

CAP SMOKE GOGGLES & COVER SOILED WITH LIQUID. REPLACED GOGGLES & COVER OK TO CONTINUE.

Part: COOLING FAN — FAULTY (E&E BAY) · airframe 87,619 hrs · 13,990 cycles

FWD EQUIP COOLING EXHAUST FAN EICAS MESSAGE. ODOR SIMILAR TO ELECTRICAL ODOR WAS AFTER TAKE OFF & WHEN POWER RETARDED. ODOR WAS SHORT IN DURATION & DISSIPATED RAPIDLY WITH NO ACTION BY THE CREW OR FLIGHT ATTENDANTS. THE ODOR REMAINED GONE AFTER IT DISSIPATED, NO SMOKE OR FUMES WERE NOTED AT ANY TIME. NO EVIDENCE OF ODOR ON ARRIVAL. PERFORMED ALL REQUIRED CHECKS & PERFORMED HIGH POWER ENG RUN TO CONFIRM ALL ODORS HAVE BEEN CLEARED. AIRCRAFT OK FOR FLIGHT AS STATED IN PREVIOUS LOG ITEMS IAW AMM 05-51-35-201. R & R FWD EXHAUST COOLING FAN MONITOR IAW AMM 21-58-06. OPERATIONS NORMAL STATUS MESSAGE CLEARED.

Part: GROUND WIRE — DAMAGED (NR 1 ENGINE) · airframe 87,618 hrs · 13,989 cycles

AT D41921 FWD PYLON NR 1 ENG HAS MULTIPLE GND WIRES BROKEN. REPAIRED WIRING SHIELD GNDS IAW SWP 20-10-15 & WDM 75-23-11, 78-36-11. SEE PTT 6182027, 6182028, 6182029, 6182040, 6182041, 6182042 & 6182043 FOR SPECIFIC DETAILS. IAW SMC053 FOR CANNON PLUG INSTALLATION & SEALING.

Part: TURBINE BLADES — DAMAGED (NR 1 ENGINE) · airframe 87,618 hrs · 13,989 cycles

ON ENG NR 1 ESN 717550 IAW EC6281, FOUND ONE EACH 2ND STAGE HPT BLADE DAMAGED. DAMAGE IS ON LE APPROXIMATELY 0.400 INCHES LONG BEGINNING 0.300 INCHES FROM THE END OF THE BLADE. THE DAMAGE IS ON BOTH THE CONVEX & CONCAVE SIDES & PARENT METAL IS MISSING WITH A HOLE COMPLETELY THRU TO THE COOLING AREA OF THE BLADE. DAMAGE IN AREA A & B WITHIN 5 CYCLE FLY BACK LIMITS FOR ENG CHANGE, REPLACED ENG IAW AMM SN OFF 717550 & SN ON 727916.

Part: BLANKET — DEBONDED (THRUST REVERSER) · airframe 87,618 hrs · 13,989 cycles

INBD C DUCT NR 1 ENG HAS FIRE BLANKET DISBOND IN 2 AREAS, LOWER IS APPROXIMATELY 30 X 24 INCHES, UPPER IS APPROXIMATELY 10 X 18 INCHES. REPAIRED AREA IAW SRM 78- 31-01.

Part: WIRE — DAMAGED (THRUST REVERSER) · airframe 87,618 hrs · 13,989 cycles

IAW SMC014 WIRE W356-149-20 SHIELD GND NEEDS REPAIR AT CONNECTOR D4192J. IAW WDM 78-36-11 REPAIRED SHIELD GND FOR WIRE W356-149-20 IAW SWP 20-10-15.

Part: WIRE — DAMAGED (THRUST REVERSER) · airframe 87,618 hrs · 13,989 cycles

IAW SMC014. WIRE W356-150-20 NEEDS SHIELD GND REPAIRED AT CONNECTOR D4192J, IAW WDM 78-36-11. REPAIRED SHIELD GND FOR WIRE W356-150-20 IAW SWP 20-10-15.

Part: HEAT SHIELD — DAMAGED (NACELLE) · airframe 87,618 hrs · 13,989 cycles

HEAT SHIELD, BLANKET ABOVE CNA DAMAGED. REPLACED HEAT SHIELD

Part: DUCT — DENTED (ANTI-ICE SYSTEM) · airframe 87,618 hrs · 13,989 cycles

INLET COWL ON NR 1 ENG INLET TIA TUBE HAS MULTIPLE DENTS & GOUGES FROM 3 O'CLOCK TO 6 O'CLOCK AFT FACING FWD. REVIEW OF CMM 36-10-06 PAGE 603 & 604 SHOWS FINDINGS OUT OF LIMITS. REPAIRED DUCT IAW CMM 36-10-06 REP 1-1.

Part: INLET — DAMAGED (NR 1 ENGINE) · airframe 87,618 hrs · 13,989 cycles

NR 1 ENG INBD C DUCT COOLING AIR INLET NOT SEALANT MATING SURFACE. REPAIRED NR 1 ENG INBD C DUCT COOLING AIR INLET MATING SURFACE.

Part: REPAIR — DAMAGED (RT COWLING) · airframe 87,618 hrs · 13,989 cycles

ON ENG NR 1 RT CORE COWL UPPER TE CORNER, PREVIOUS REPAIR IS DAMAGED. REINSTALLED MISSING FILLER MATERIAL 071 2024 & REINSTALLED FASTENERS IAW SRM 51-40-02. IAW NON RII INSP OF REPAIR TO INBD TE CORE COWL NR 1 ENG. REPAIR IS COMPLETE IAW SRM 51-40-02.

Part: SHUTOFF VALVE — FAULTY (APU) · airframe 87,598 hrs · 13,987 cycles

HAVE APU FUEL VLV EICAS & APU FAULT LIGHT. R & R APU FUEL SOV.

Part: IDG — FAULTY (NR 2 ENGINE) · airframe 87,577 hrs · 13,982 cycles

RT GEN OFF LIGHT ILLUMINATED ON DESCENT. RAN CHECKLIST RESET, DID NOT RESET. BPCU READOUT FOUND SHORTED PMG TRIP & GEN FIELD WIRING GCU. AFTER RESET PB BPCU TESTED OK. AFTER RT ENG RUN GEN OFF AGAIN. AIRCRAFT RELEASED IAW MEL.

Part: VALVE — MALFUNCTIONED · airframe 87,234 hrs · 13,939 cycles

LT & RT DUCT PRESSURE SPLIT DURING CRUISE, WITH ENGINES RUNNING. LT & RT ISOLATION VALVES CLOSED & BLEED SWITCH ON. LT PRESSURE 35 PSI & RT PRESSURE 20 PSI, CRUISE FL 370 LEPR 1.17 REPAIR 1.22. PERFORMED AIR SUPPLY DISTRIBUTION SYSTEM TEST PER AMM 36-11-00-501. BLEED PRESSURES AND BLEED SHIFT POINTS NORMAL. SYSTEM TEST ACCOMPLISHED.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 86,974 hrs · 13,901 cycles

CTR FCC PROBLEM, RTFL UNABLE TO ENGAGE CENTER OR RT AUTO PILOT NO EICAS MESSAGE. TROUBLE SHOT IAW FIM 22-00-02, PREV FLIGHT FAULT, NO INFC FCC C MCDP SHOWN. REPLACED FCC CENTER IAW MM. MCDP GROUND TEST 1 & TEST 56 PASSED.

Part: WINDOW — OUT OF ADJUST (COCKPIT) · airframe 86,972 hrs · 13,900 cycles

NR 2 WINDOW ASSEMBLY6 AIR LEAKS POSITION 2 2=2L, 5=2R. AIR LEAK AT BOTTOM OF WINDOW, NOT SQEAL, LEAK. MOVING CRANK STOPS LEAK, RELEASING RESUMES. PERFORMED NR 2 POSITION 2 WINDOW ADJUSTMENT TEST IAW AMM 56-11-02-501. PRESSURIZATION LEAK CHECKED GOOD, & WINDOW HEAT OPERATIONAL CHECKED GOOD IAW AMM 05-51-24-201.

Part: CONTROL PANEL — DAMAGED (COCKPIT) · airframe 86,932 hrs · 13,895 cycles

HEADING SELECT KNOB FALLING APART. HEADING SELECT INOPERATIVE. MODE CONTROL PANEL REPLACED IAW AMM 22-11-02, MCDP TEST 04 CARRIED OUT, ALL SATISFACTORY.

Part: CONTROL PANEL — INOPERATIVE (COCKPIT) · airframe 86,677 hrs · 13,858 cycles

HDG SELECT BINDS WITH BANK LIMIT. MODE CONTROL PANEL SECTOR BANK LIMIT SELECTOR INOPERATIVE. REPLACED MODE CONTROL PANEL IAW MM. TEST CHECKED GOOD.

Part: DUCT — SPLIT (RT A/C PACK) · airframe 86,139 hrs · 13,789 cycles

RIGHT PACK COMPRESSOR OUTLET DUCT SPLIT AT COMP OUTLET TEMP SENSOR BOSS. REPLACED DUCT ASSY, LEAK CHECKED AND TESTED IAW MM 21-51-00 PG 501 ALL GOOD. REPLACED ELBOW FITTING & ACCOMPLISHED PACK TEST WRT MM. ALL INDICATIONS CHECKED OK. ALSO LEAK CHECK ACCOMPLISHED, NO LEAKS FOUND.

Part: PUMP — MALFUNCTIONED (LT CENTER) · airframe 86,077 hrs · 13,781 cycles

LEFT CENTER FUEL PUMP ON WITH ENGINES SHUTDOWN AT GATE.

Part: PRESSURE SWITCH — MALFUNCTIONED (FUEL SYSTEM) · airframe 86,020 hrs · 13,772 cycles

LEFT FUEL PUMP LOW PRESSURE LIGHT DOES NOT COME ON. CLEANED AND INSPECTED LT CENTER FUEL PUMP PRESSURE SWITCH. ACCOMPLISHED FUEL PRESSURE INDICATING OPS CHECK.

Part: O-RING — FAILED (HYD SYSTEM) · airframe 85,970 hrs · 13,766 cycles

HYDRAULIC FLUID DRIPPING FROM RT WING INBD OF RT ENGINE PYLON. REMOVED UNDER WING PANELS ON RT SIDE NEAR INBD CANOE. ACCOMPLISHED CHECK IAW MM 29-11-00. OPERATED ALL CONTROLS SPOILERS AND FLAPS NO LEAKS FOUND, QTY 0.95 & STEADY. ACCOMPLISHED STATIC LEAK CHECK, NO LEAK FOUND. FOUND FLUID COMING FROM #8 SPOILER PRESSURE LINE. REPLACED ORING UNDER UNION. LEAK CHECK GOOD. CLEANED AREA. OK TO CONTINUE.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 85,834 hrs · 13,748 cycles

HYD LEAK, RT WING JUST INBD OF INBD AILERON. FOUND DC MOTOR OPERATED SHUTOFF LATERAL CONTROL EMPENNAGE VALVE LEAKING. CYCLED LATERAL CONTROL VALVE, AND TIGHTENED PRESSURE LINE, NO LEAKS NOTED.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 85,740 hrs · 13,736 cycles

FOUND LEAK ON FLEX LINE BETWEEN STAB TRIM CONTROL MODULE AND STAB TRIM ACTUATOR. REPLACED LINE, LEAK CHECKED NORMAL.

Part: ACTUATOR — LEAKING (AUTO PILOT SYS) · airframe 85,740 hrs · 13,736 cycles

LEFT HYDRAULIC SYS DOWN TO .85 ON ARRIVAL. NOTED HYD FLUID ON TAIL AREA OF ACCESS PANEL TO HORIZONTAL STABILIZER. SERVICED HYD SYS TO FULL. CLEANED TAIL AREA ENTERED ACCESS PANEL TO HORIZONTAL STABILIZER BAY FOUND LEFT AP ELEVATOR SERVO ACTUATOR ROD LEAKING TWO DROPS PER MINUTE, REF TABLE ONE 29-00-99 PG601. REPLACED LT AP SERVO IAW AMM 22-12-01. ADJUSTED, LEAK CHECKED AND TESTED GOOD.

Part: SDU — FAILED (SATCOM) · airframe 85,383 hrs · 13,692 cycles

SATCOM INTERMITTENT. CALLS TO DISPATCH DO NOT STAY CONNECTED. REPLACED SDU IAW AMM, GROUND CHECKS NORMAL.

Part: FAIRING — DELAMINATED (RT PYLON) · airframe 84,987 hrs · 13,646 cycles

RIGHT ENGINE PYLON INBD AFT FAIRING HAS DELAMINATION. PERFORMED METAL BOND REPAIR PER AMM.

Part: INLET — DENTED (NR 1 ENGINE) · airframe 84,987 hrs · 13,646 cycles

NR 1 ENGINE INLET COWL DENTED. REPAIRED.

Part: FASTENER — MISSING (NR 2 PYLON) · airframe 84,987 hrs · 13,646 cycles

WHILE PERFORMING MF8840, FOUND ONE MISSING FASTENER ON NR 2 ENGINE OUTBD PYLON HEATSHIELD. REPAIRED.

Part: SATCOM — FAULTY (NR 1) · airframe 84,826 hrs · 13,626 cycles

NO COMM DISPLAYED ON ACARS DISPLAY UNIT OVER OCEAN, ACARS SENDS OK IN VHF RANGE. ACCOMPLISH CHRONIC REVIEW. PLACARD SATCOM DUE TO HISTORY PER 2325A, C-B'S COLLARED. REMOVED AND REPLACED SAT DATA UNIT IAW AMM. OPS CHECK GOOD REF 23-25-00. SEE 8262003 FOR PARTS INFO

Part: DISPLAY — FAILED (COCKPIT) · airframe 84,804 hrs · 13,623 cycles

UPPER EICAS FAILED. REMOVED AND REPLACED UPPER EICAS DU, OPS CHECK NORMAL.

Part: RELAY — FAULTY (PITOT HEAT) · airframe 84,792 hrs · 13,621 cycles

CAPT PITOT LIGHT AND EICAS MESSAGE ON ENGINE START. REPEAT WRITE-UP. RELAY K241 PART N.770540- 2 AND K516 PART N. BACR13CG2A. REPLACED SPEED CARD TEST PERFORMED IAW AMM. PITOT HEAT TEST PERFORMED IAW AMM.

Part: DISPLAY — INTERMITTENT (ACARS) · airframe 84,768 hrs · 13,618 cycles

NO COMMS DISPLAYED ON ACARS DISPLAY UNIT, OVER OCEAN. ACARS SENDS OK IN VHF RANGE. REPLACED SDU PER AMM, GROUND CHECKED NORMAL.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 67,290 hrs · 24,723 cycles

DENT ON EXISTING DOUBLER REPAIR 2 INCHES BELOW STR 16L BS 768. MAJOR REPAIR ACCOMPLISHED. REMOVED EXTERNAL REPAIR DOUBLER 2 INCHES BELOW STR 16L AT BS 768 IAW B757-200 SRM 51-40-02 FIG 8. FABBED, LOCATED, AND DRILLED DOUBLER AND FILLER IAW B757- 200 SRM 53-00-01 FG 201 REPAIR 2. INSTALLED DOUBLER AND FILLER IAW B757-200 SRM 53-00-01 FIG 201 REPAIR 2.

Part: LATCH — BROKEN (CARGO DOOR) · airframe 84,544 hrs · 13,588 cycles

FWD CARGO DOOR, CARGO HANDLING PANEL, BOTTOM LATCH BROKEN. DEF PER CDL. REMOVED DOOR AND STOWED IN FORWARD CLOSET IN CABIN. REPLACED LATCH AND SECURED ACCESS PANEL TO FWD CARGO CONTROL AREA.

Part: LOCK RING — MISSING (COCKPIT DOOR) · airframe 84,476 hrs · 13,577 cycles

LOCKING RING MISSING FROM BOTTOM PANEL OF COCKPIT DOOR. REPLACED LANYARD RINGS.

Part: CONTROL PANEL — NO TEST (WX RADAR SYS) · airframe 84,370 hrs · 13,553 cycles

WEATHER RADAR TEST MODE DOES NOT TEST PROPERLY. TEST MODE CONTINUES TO DISPLAY AND, UNABLE TO DE-SELECT. REPLACED WEATHER RADAR CONTROL PANEL AS PER MM AND ACCOMPLISHED SYSTEM TEST AS PER MM.

Part: CONNECTOR — UNSECURE (TEMP SELECTOR) · airframe 84,238 hrs · 13,536 cycles

COCKPIT TEMP EICAS. BITE CHECK AUX ZONE CONTROLLER, SHOWS CTR YEP CONTROL FAULT. FOUND CONNECTOR ON CTR AUX TEMP SELECTOR LOOSE. SECURED CONNECTOR, BITE CHECK ZONE CONTROLLERS, NO FAULTS. CLEARED EICAS MSG. SIGN OFF TEXT SHOULD STATE: SECURED CONNECTORS IN PROPER LOCATION.

Part: INSULATION — DELAMINATED (THRUST REVERSER) · airframe 83,887 hrs · 13,484 cycles

NR 2 ENGINE THRUST REVERSER LEFT HALF HAS DELAMINATED FIRE SEAL INSULATION ON LOWER QUADRANT. RE-ADHERED FIRE SEAL INSULATION TO INNER THRUST REVERSER HALF ON LOWER QUADRANT. FIRE SEAL IS STILL IN PARTIAL CURE. ALL SEAMS MUST BE SEALED. THERE IS A PART OF THE SEAL THAT IS NOT ADHERING AND NEEDS TO BE RE-ADHERED AGAIN. IT IS IN THE UPPER FORWARD QUADRANT AREA AND NEEDS TO BE RESEALED. COMPLETED REPAIR.

Part: STATOR — FAULTY (EEC) · airframe 83,793 hrs · 13,472 cycles

RIGHT ENGINE EEC C1 STATUS MSG, RTFL. REPLACED NR 2 ENGINE EEC ALTERNATOR STATOR. RAN ENGINE, NO MESSAGES, INDICATIONS NORMAL.

Part: GCU — FAULTY (APU) · airframe 83,783 hrs · 13,470 cycles

RIGHT GENERATOR TRIPPED OFF-LINE JUST AFTER TAKEOFF. A/C POWER AVAILABLE FROM APU. FLIGHT CONTINUING TO MUC. TOMC PLANNING TO DEFER RIGHT ENGINE GENERATOR IN MUC. REPLACED APU GCU.

Part: SDU — FAULTY (NR 1) · airframe 83,746 hrs · 13,465 cycles

VOICE ON SATCOM NOT WORKING. ACARS CAN USE OK. MSG "LOW GAIN" ON LINE 6 OF CDU. REPLACED SATELLITE DATA UNIT PER MM. CALLED SAMC, OPS CHECKED NORMAL.

Part: IDG — FAULTY (NR 2 ENGINE) · airframe 83,746 hrs · 13,465 cycles

RIGHT GENERATOR OFF, RESET DID NOT WORK. REPLACED IDG PER MM. RAN ENGINE LOADED GENERATOR TO 71%. OPS CHECKED GOOD. RE-SERVICED IDG AND ACCOMPLISHED LEAK CHECK. NO LEAKS FOUND.

Part: POWER UNIT — FAULTY (CARGO DOOR) · airframe 83,698 hrs · 13,459 cycles

UNABLE TO OPEN AFT CARGO PIT DOOR EITHER MANUALLY OR ELECTRICALLY. REPLACED AFT DOOR LIFT LATCH POWER UNIT, OPS CHECK GOOD.

Part: EEC — FAULTY (NR 2 ENGINE) · airframe 83,633 hrs · 13,451 cycles

CREW REPORTS THEY HAVE A "R ENG EEC C1" STATUS MSG. TRIED TO CYCLE THE SYSTEM, ENGINE SHUTDOWN AND RESTART. MSG CLEARED WITH RESTART OK. TO DEFER PER MEL 7321H. BITE FAULT CH A N2 RANGE FAIL. REPLACED RIGHT ENG EEC REF MM 73-21-04 RAN ENG NO STATUS MESSAGE.

Part: LAP JOINT — DAMAGED (FUSELAGE) · airframe 83,416 hrs · 13,417 cycles

BS 1582 LAP SEAM APPEARS TO BE UNEVEN, ENTIRE CIRCUMFERENCE OF FUSELAGE, AFT PRESSURE BULKHEAD ATTACHMENT POINT. MAINT TEXT: ACCOMPLISHED ALL REQUIRED INSPECTIONS AND ACCOMPLISHED STRINGER SHIMMING REPAIRS AT THE FOLLOWING LOCATIONS: SECTION 46, STR'S 3R, 12R, 14R, 14L, 34L: AND SECTION 48, STR'S 3R, 6R, 12R, 14R, 24R, 29R, 31R, 33R, 39R, 12L, 14L, 19L, 24L, 32L, 34L, AND 39L PER REO G-15401, REV L AND EC-RA 5361-01028.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,416 hrs · 13,417 cycles

BS 303 RBL 54 TRANSVERSE FLOORBEAM UPPER CHORD CORRODED (TOP SIDE). MATERIAL REMAINING OUT OF LIMITS PER SRM 53-00-01 IN 5 AREAS BETWEEN RBL 37 TO RBL 63. REMOVED DAMAGED SECTION OF T-CHORD AND FABRICATED AND INSTALLED REPAIR ANGLES, STRAPS, SHIMS AND CLIPS PER SRM 53-00-51, RPR 4, ON NON ROUTINE 46845.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 83,416 hrs · 13,417 cycles

BS 1582, STRINGER END FITTING AT STRINGER 34 LEFT, SECTION 46 IS DAMAGED. MAJOR REPAIR ACCOMPLISHED: REPLACED THE STRINGER 34 LEFT END FITTING, P/N 146T0307Y1 AND LOCATED AND DRILLED PER SRM AND INSTALLED PER SRM.

Part: SKIN — DAMAGED (E&E DOOR) · airframe 83,416 hrs · 13,417 cycles

E+E DOOR, EXTERIOR SKIN FOUND TO HAVE MINOR PITTING. ORIGINAL MATERIAL THICKNESS IS .050", MATERIAL REMAINING AFTER BLENDOUT IS .039" RIGHT SIDE & .044" LEFT SIDE. FABRICATED AND INSTALLED 2 EACH REPAIR DOUBLERS PER SRM 52-40-01, REPAIR 5, ON NON ROUTINE 46891.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 83,416 hrs · 13,417 cycles

MJR RPR. LOWER EXTERNAL FUSELAGE SKIN TOOLING DAMAGE BETWEEN BS 1329-1351 AT STR 35L-36L. BLENDED OUT DAMAGE & FOUND MATL LOSS OUT OF SRM LIMITS. CUT OUT DAMAGE & ACP HFEC REF NDT MAN 51-00-19. NO DEFECTS. FABRICATED & INSTALLED AN EXTERNAL DOUBLER & FILLER REPAIR REF SRM53-00-01 REPAIR 14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 83,416 hrs · 13,417 cycles

UNDER PAINT TOOLING BLENDOUT AT STR 2 RIGHT NEXT TO THE TCAS ANTENNA. EVALUATED DAMAGE & FOUND MATERIAL LOSS OUT OF SRM LIMITS. CUT OUT DAMAGE & ACP HFEC REF NDT MAN 51-00-19. NO CRACKS. FABRICATED & INSTALLED EXTERNAL DOUBLER & FILLERS REPAIR REF SRM 53-00-01 RPR 12.

Part: SKIN — CRACKED (FUSELAGE) · airframe 83,416 hrs · 13,417 cycles

EXTERIOR FUSELAGE LOWER SKIN LEFT SIDE DENTED, BS 610 - BS 632, STR 32L - STR 33L. EVALUATED DENT & FOUND CRACKED OUTER SKIN. CUT OUT DAMAGE & ACP NDT OF CUT-OUT REF NDT MAN 51-00-19. FABRICATED & INSTALLED EXTERNAL DOUBLER & FILLER REPAIR REF SRM 53-00-01.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 83,416 hrs · 13,417 cycles

UNDER PAINT TOOLING BLENDOUT AT STR 2 RIGHT NEXT TO THE TCAS ANTENNA. EVALUATED DAMAGE & FOUND MATERIAL LOSS OUT OF SRM LIMITS. CUT OUT DAMAGE & ACP HFEC REF NDT MAN 51-00-19. NO CRACKS. FABRICATED & INSTALLED EXTERNAL DOUBLER & FILLERS REPAIR REF SRM 53-00-01 RPR 12.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,416 hrs · 13,417 cycles

AFT FUSELAGE LOWER INTERNAL BILGE AREA WEB TIES CORRODED AT SEVERAL AREAS BS 1540, STR 36R - STR 39R. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION ON SHEAR TIE STA 1540 BETWEEN STR 39R-38R, ARE OUT OF LIMITS. INST 3EA NEW SHEAR TIES STA 1540, STR 36R-39R IAW BAC DWG 140T2102, 146T1222 SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,416 hrs · 13,417 cycles

AFT CARGO COMPARTMENT BILGE, SHEAR TIE CORRODED BS 1395 - 1396, STR 39L - 39R. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED & INSTALLED NEW SHEAR TIE IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,416 hrs · 13,417 cycles

MAIN CABIN FLOORBEAM AT STA 852 AT RBL 74.81 UPPER SURFACE HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: CORROSION IS OUT LIMITS IAW SRM 53-00-51, PG 102. FABRICATED & INSTALLED T-CHORD, FILLER & SPLICE ANGLE IAW SRM 53-00-51, REPAIR 3.

Part: STRUCTURE — DENTED (CARGO DOOR) · airframe 83,416 hrs · 13,417 cycles

BULK CARGO DOOR FWD LOWER CORNER HAS 6 EA DENTS 1" TO 5.5" FROM FWD EDGE, 1.5" TO 6.25" FROM BOTTOM EDGE. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 52-30-01, DET VI NOTE J. REPAIRED IAW SRM 52-30 -01, FIG 201. THIS REPAIR IS CATEGORY A.

Part: INDICATOR — OUT OF TOLERANCE (DOOR) · airframe 83,416 hrs · 13,417 cycles

AFT RIGHT DOOR LOAD LIMITER INDICATOR NUT OUT OF LIMITS, MORE THAN 1-8 INCH FROM HOUSING. REMOVED AND REPLACED AFT RIGHT DOOR LOAD LIMIT INDICATOR IAW B767 AMM.

Part: GCU — POPPED (NR 2 ENGINE) · airframe 83,415 hrs · 13,416 cycles

RIGHTT ENGINE IDG VALVE C/B POPPING. THIS IS M31 CB(28VDC). IT IS CHRONIC AND MEL 7521D CANNOT BE USED TO DF THE RIGHT IDG VALVE, DUE TO STATING AFTER DEACTIVATION OF THE VALVE PUSH THE C/B IN. THIS ITEM NEEDS TO BE FIXED OR PROVISION OF MEL GET CHARGED. REPLACED GCU NR 2; RIGHT ENGINE, OPS CHECK GOOD.

Part: WARNING MESSAGE — ILLUMINATED (RT WING SLIDE) · airframe 83,398 hrs · 13,414 cycles

RIGHT WING SLIDE DOOR EICAS MESSAGE.

Part: WIRE — DAMAGED (ELECTRICAL) · airframe 83,396 hrs · 13,413 cycles

OFF GATE, AFTER ENG START, CIRCUIT BREAKER M31 FOR RT ENGINE IDG VALVE TRIPPED. REPLACED CIRCUIT BREAKER AS PRECAUTION. WIRE W3538-017-20 REPLACED. PERFORMED ENGINE IDLE RUN FOR 5 MINUTES ALL INDICATIONS NORMAL. WIRE REPLACED IAW SWP AND WDM 24-11-21.

Part: CHARGER — FAULTY (MAIN BATTERY) · airframe 83,396 hrs · 13,413 cycles

DURING PREFLT EICAS MESSAGE MAIN BATTERY CHARGER ON STATUS PAGE CANNOT ERASE. REMOVED & REPLACED BATTERY CHARGER, OPS CHECKS GOOD.

Part: OIL COOLER — FAULTY (IDG) · airframe 83,330 hrs · 13,404 cycles

CB M31 POPPED OUT WITH NO FURTHER INDICATIONS DF420. IDG AIR OIL COOLER DEACTIVATED IN OPEN POS SECURED TO CLOSE BY ELECTRICAL HARNESS. CB PULLED AND SECURED. REPLACED IDG AIR OIL HEAT EXCHANGER AND VLV NO LEAKS, NO FAULTS, NO MESSAGES.

Part: TRANSMITTER — LEAKING (NR 1 ENGINE) · airframe 83,025 hrs · 13,367 cycles

NR 1 ENG OIL PRESSURE INDICATION FAULT, TEMPERATURE AND QUANTITY NORMAL; OIL PRESSURE FLUCTUATING OR INTERMITTENT. WENT TO 400 PSI AFTER CLIMB POWER SELECTED INTERMITTENT NORMAL TO 400 PSI. NO LEAKS FOUND AFTER OIL PSI TRANSMITTER REPLACED. STATIC RUN CHECKED OKAY.

Part: SLIDE — DAMAGED (R1 DOOR) · airframe 82,749 hrs · 13,330 cycles

DOOR 1R EVACUATION SLIDE BUSTLE HAS DAMAGE FROM GALLEY CONTAINER. BUSTLE HAS PUNCTURE APPROX 2 BY 2 INCHES LOCATED 6 INCHES FROM BOTTOM OF BUSTLE ON TRAILING EDGE, TWO GOUGES APPROX 18 INCHES AND 24 INCHES FROM BOTTOM OF BUSTLE. REMOVED BUSTLE AND INSPECTED SLIDE ASSY, NO DAMAGE TO SLIDE ASSY. ACCOMP INTERIM REPAIR TO BUSTLE WITH TAPE. BUSTLE TO BE REPAIRED WITHIN 20 DAYS. REPAIRED PUNCTURED BUSTLE PER GNMM, FILLED SMALL GOUGES, SMOOTHED AND PAINTED. REMOVED DOOR 1R EVACUATION SLIDE BUSTLE FOR REPAIR FOR CF0385. INSTALLED 1R BUSTLED.

Part: ACTUATOR — FAULTY (AC BAY) · airframe 82,513 hrs · 13,294 cycles

RIGHT PACK INOP, LIGHT ON. EICAS MSG 'RIGHT PACK TEMP 'DISPLAYED. PERFORMED BITE CHECK THAT REVEALED BAD PACK EXHAUST ACTUATOR. REMOVED AND REPLACED RIGHT PACK EXHAUST ACTUATOR. WORKS OK. NO FAULTS.

Part: CONNECTOR — CONTAMINATED (STABILIZER) · airframe 82,003 hrs · 13,225 cycles

AIR RETURN DUE TO STAB TRIM INDICATION. TROUBLESHOOTING FOUND STAB WOULD RUN AT FULL SPEED IN NOSE UP DIRECTION AND HALF SPEED IN NOSE DOWN DIRECTION. IN BLOCK 6 OF FIM FOUND STAB WOULD NOT GO IN NOSE DOWN DIRECTION 104400 ALSO HAD 0.2 OHMS, AND IN NOSE UP DIRECTION IT RAN AT HALF SPEED, NORMAL. IN STEP 7 OF FIM FOUND CONNECTOR D2211 OF L-H STAB MODULE M1607 FULL OF HYD FLUID AND PIN 2 PUSHED BACK. CLEANED CONNECTOR AND REINSTALLED PIN. RERAN FIM AND ALL CK'S NORMAL. MESSAGES CLEARED AND NO FAULT BALLS ON LT OR RT SAM'S.

Part: SEAL — LEAKING (ACCESS PANEL) · airframe 81,736 hrs · 13,190 cycles

MAINT REPORTS FUEL LEAK FROM RT WING ACCESS PANEL INBOARD NR 5 DRIP STICK. PANEL 641KB MOLDED RUBBER SEAL DAMAGED. MOLDED RUBBER SEAL REPLACED PER AMM. FUEL LEAK CHECK PERFORMED. FOUND NO LEAK.

Part: SLIDING WINDOW — DEFECTIVE (COCKPIT) · airframe 81,584 hrs · 13,168 cycles

CAPTAIN'S SLIDING WINDOW DEFECTIVE. REMOVED CAPTAIN'S SLIDING WINDOW IAW MM.

Part: WINDOW — DAMAGED (COCKPIT) · airframe 81,584 hrs · 13,168 cycles

FIRST OFFICER'S FIXED WINDOW DAMAGED. INSTALLED NEW WINDOW IAW MM.

Part: WINDOW — DEFECTIVE (COCKPIT) · airframe 81,584 hrs · 13,168 cycles

CAPTAIN'S NR 3 FIXED WINDOW DEFECTIVE. REMOVED AND INSTALLED NEW WINDOW IAW MM 56-11-10.

Part: SDU — INOPERATIVE (COCKPIT) · airframe 81,470 hrs · 13,154 cycles

SATCOM INOP FROM ORD TO LHR. REPLACED SDU PER MM.

Part: INTERCOSTAL — GOUGED (FUSELAGE) · airframe 81,430 hrs · 13,149 cycles

INTERCOSTAL IN AREA OF DAMAGE IS DENTED. REMOVED DAMAGE INTERCOSTAL. REPLACEMENT PART ON ORDER. PER ENGINEERING REMOVED 5 FASTENERS AND MAPPED OUT DAMAGE AREA FOR SKIN THICKNESS CHECK. ACCMP'D THICKNESS INSP OF BLENDED AREA, FOUND THICKNESS BLEND TO BE .046 INCH OR 23% OTHERS WERE .016, .002 AND .002. COMPLETED BLENDING OF 4 AREAS. CURRENT PTT 81,389.24 GOUGE AT RT FUSELAGE BS 1373. GOUGE WORKED AS PER EC-RA#5330-04217. OK TO CONTINUE IN SERVICE FOR 50 FLYING HOURS MAX. ACCMP'D PERMANENT REPAIR PER ECRA 5330-04217.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 81,389 hrs · 13,144 cycles

DAMAGE AT RT FUSELAGE STATION 1373 BELOW STRINGER 28R REQUIRES BLENDING TO REMOVE DAMAGE AND HFEC. BLENDED 4 AREAS REF SRM 53 -00-01, AND ACP'D HFEC INSPECTION OF DAMAGED AREAS REF NDT MAN PART 6 FOUND NO CRACKS. TWO UPPER DAMAGED AREAS OUT OF SRM ALLOWABLE DAMAGE LIMITS.

Part: COMPUTER — FAULTY (EICAS) · airframe 81,342 hrs · 13,138 cycles

RIGHT ELEVATOR POSITION INDICATION INOP DURING FLT CONTROL CHECK. ALL 3 HYD SYSTEMS PRESSURIZED. CYCLE FCC AC CB'S, NO HELP. SWITCHED EICAS COMPUTER FROM LEFT, RIGHT AND BACK TO AUTO, NO HELP. VERIFIED OPERATION 908-12. RPL'D LEFT EICAS COMPUTER PER MM, CHECKED WIRES TO XMITTR. NO INDICATION PROBLEMS, SYSTEM OPS NORMAL.

Part: IRU — FAULTY (NR 1) · airframe 81,303 hrs · 13,132 cycles

LEFT IRS FAULT ON ALIGNMENT. REPLACED LEFT IRU PER MM, ACCOMPLISHED TEST 30 PER MM. OPS CHECK GOOD.

Part: ACTUATOR — FAULTY (RUDDER) · airframe 80,892 hrs · 13,077 cycles

RUDDER RATIO LIGHT & EICAS MSG, RTFL. FAULT BALL FOUND IN PCA POSTION ON BOTH RRCM'S. REPLACED RRCA WITH BORROWED PART S-N 1008. OPS CHECKS GOOD, NO FAULTS.

Part: ANTI-ICE VALVE — FAULTY (LT ENGINE) · airframe 80,769 hrs · 13,061 cycles

LEFT ENG ANTI-ICE VALVE LIGHT ON. VERIFIED SOLENOID AND VALVE OPERATION PER MEL ITEM 3021C. MEL REF: 3021C. PARTS: 643-9002 MR30133 VALVE ASSY. REPLACED WITH NEW TAI VLV, OPS CHECKED NORMAL PER MM

Part: UNKNOWN — MALFUNCTIONED (ANTI-ICE SYS) · airframe 80,737 hrs · 13,057 cycles

LEFT ENG ANTI ICE VALVE LT ON WITH ENG SHUT DOWN AND SWITCH IN OFF POS. CLEANED ELEC CONNECTOR ON ENG INLET THERMAL ANTI-ICE VLV. LIGHT EXTINGUISHED. PROBLEM RECURRED.

Part: DOOR — OPEN (FUEL SYSTEM) · airframe 80,305 hrs · 12,996 cycles

AT DEPARTURE CENTER FUEL PUMPS REMAINED ON WHEN THEY SHOULD HAVE SHUTOFF. FOUND FUELING DOOR AJAR SECURED FUELING DOOR, OPS CKS OKAY.

Part: THRUST REVERSER — DAMAGED (RT ENGINE) · airframe 80,240 hrs · 12,987 cycles

FOUND RT ENG INB TR DAMAGED AND STRUT FAIRING COVER MISSING AT THE 9 O'CLOCK POSITION. DAMAGE IS APPROX 7"X .5" WIDE WITH A DEPTH OF .5". PER AVO #1103 COMPLETED REPAIR STEPS 1-5. SEALANT NEEDS TO BE CONFIRMED CURED AND STEP 6 & 7 NEED TO BE COMPLETED. REF EC-RA #7831-01716 PERFORMED TEMP REPAIR OF CRACK AND GOUGE WITH RE-CHECK DUE AT EVERY #3SV & PERM REPAIR WITHIN 412 NOT TO EXCEED PTT 80652 HOURS. RE-CHECKED TO BE ACCMP'D EVERY 2SV NOT 3SV. -INF- :EC-RA #7831-01716 REVISED TO EC-RA 7831-01716 REV A TO ACCOMPLISH INSPECTION AT EACH 2 SVC. -INF- :MF8446 CREATED TO ACCOMPLISH RECHECK AT EACH #2SV.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 80,053 hrs · 12,960 cycles

EXTERNAL EEL LIGHT INOP BY NR 1 RIGHT DOOR. REPLACED LIGHT ASSY, CHECKS GOOD.

Part: BATTERY — ACTIVATED (CABIN) · airframe 80,053 hrs · 12,960 cycles

EEL LIGHTS ON SEATS 19J THRU 22J ARE INOP. REPLACED CHARGER AND BATTERY, CHECKS GOOD.

Part: UNKNOWN — MALFUNCTIONED (ELEVATOR) · airframe 79,784 hrs · 12,924 cycles

RT ELEVATOR MOVEMENT INDICATOR DOESN'T MOVE. DEFERRED PER SAMC. IF NEEDED REPLACE XMTR PER MM. RPL : TROUBLESHOOT PER FIM 27-3 1-00, NO FAULTS FOUND. REPLACED RIGHT ELEVATOR POSITION CB (4102 ) PRECAUTIONARY. ELEVATOR POSTION INDICATONS ARE NORMAL.

Part: ACTUATOR — OUT OF ADJUST (RUDDER TRIM) · airframe 79,784 hrs · 12,924 cycles

5 UNITS LEFT RUDDER TRIM NEEDED BOTH AT CRUISE AND DESCENT. ADJUSTED TOP RUDDER PCA FOR CTR SYS INPUT ROD PER MM. AIRCRAFT TRIM DISCREPANCY CHECK ACCOMPLISHED PER MM.

Part: TRANSMITTER — FAULTY (NR 1 ENGINE) · airframe 79,766 hrs · 12,922 cycles

AT CRUISE, LEFT OIL PRESS FLUCTUATED FROM 190-400,THEN STAYING FROM 350-400. ALL ELSE NORMAL. REPLACED NR 1 ENG OIL PRESSURE TRANSMITTER PER MM. ACP'D ENG RUNS AND OIL PRESSURE INDICATIONS NORMAL. NO LEAKS NOTED.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 79,509 hrs · 12,889 cycles

COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT ASSY, OPS CHECKED OKAY.

Part: ACTUATOR — LEAKING (RUDDER) · airframe 79,323 hrs · 12,860 cycles

ON ARRIVAL FOUND EVIDENCE OF HYDRAULIC LEAKING LEFT SIDE FUSELAGE BY APU. FURTHER INVESTIGATION SHOWED FLUID COMING FROM LOWER RUDDER AFT TRAILING EDGE DRAIN HOLE. FOUND UPPER RUDDER PCU PISTON SEAL LEAK POINT SEAPING UNDER 5 DROPS PER MINUTE AND CYCLE.

Part: ADAPTER — LEAKING (LT WING) · airframe 79,098 hrs · 12,830 cycles

FUEL LEAK FROM THE TOP OF LEFT ENGINE FROM THE FUELING LINES. MAINT TEXT: DURING FUELING OPERATION, FUEL LEAKING FROM PYLON DRAIN AND IMMEDIATELY OUTBOARD OF FWD PYLON AREA ADJACENT TO L/E SLAT. FOUND FUEL LEAKING AT INBD FUELING ADAPTER, TIGHTENED ALL BOLTS AND PRESSURIZED FUEL MANIFOLD, ADDED ADDITIONAL 2000 LBS TO VERIFY NO FURTHER LEAKAGE AT MANIFOLD ADAPTER NOR PYLON DRAIN OF L/E AREA. SECURED PANELS.

Part: COOLING FAN — INOPERATIVE (E&E BAY) · airframe 79,098 hrs · 12,830 cycles

EQUIPMENT COOLING OVERHEAT. REPLACED EQUIP COOLING SUPPLY FAN 1 DUE TO PRIOR HISTORY, VIBE SENSOR TRIPS NEW SUPPLY FAN, TRIED NEW VIBE SENSOR, STILL TRIPS NEW FAN. ORDERED ANOTHER NEW FAN OSTF U4874, NEED TO REPLACE FAN AGAIN.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 79,097 hrs · 12,829 cycles

FUSELAGE DAMAGED RT SIDE JUST AFT OF WING TO BODY FAIRING. GOUGED STA 1197 & 48 BETWEEN STRINGERS 32R AND 33R GOUGE IS 17 INCHES LONG BY 1-4 INCH WIDE AND 3-8 INCH AT THE DEEPEST POINT. PHOTOS ON THE RVI SITE. DAMAGE WAS CUTOUT AND RPR'D REF SRM RPR 14 BY INSTALLING FILLERS AND TWO DOUBLERS. INSPECTION THRESHOLD FOR THIS CAT-B RPR IS PTC:37500 WITH REPEAT INSPECTION INTERVAL OF 3,000 FLIGHT CYCLES REF SRM 53-00-01 RPR 14 TABLE V. THICKNESS OF EACH DOUBLER IS .071. ACCOMPLISH EXTERNAL LFEC REF NDT PART 6 AND EXTERNAL DETAILED INSPECTION.

Part: SHUTOFF VALVE — FAILED (BLEED AIR SYS) · airframe 78,964 hrs · 12,806 cycles

LT ENG BLEED VALVE STUCK CLOSED ON GROUND. BITE TEST OF AIR SUPPLY MODULE FAULTS "PRSOV". REPLACED PRSOV FAILED HEALTH CHECK. REPLACED PRSOV. RAN NR 1 ENG PRSOV, OPERATES NORMAL.

Part: WINDSHIELD WIPER — DEFECTIVE (WINDSHIELD) · airframe 78,827 hrs · 12,788 cycles

F/O WINDSHIELD WIPER WON'T STOP. ALSO THE CAPT'S OUTER PORTION OF WINDSHIELD WIPER DOES NOT CLEAN RAIN FROM WINDOW. REPLACED F/O WIPER ARM ASSY IAW MM. REPLACED CAPT'S WIPER BLADE. OPS CHECK NORMAL.

Part: IDG — FAILED (NR 2) · airframe 64,767 hrs · 12,601 cycles

ELEC GEN DRIVE R RIGHT IDG FAULT (LOW INTERNAL OIL PRESSURE). REPLACED IDG PER MM AND ALSO REPLACED IDG DRIVE SEAL.

Part: IDG — FAILED (NR 1) · airframe 78,803 hrs · 12,783 cycles

PER INBOUND CREW, LEFT BUSS TRIPPED ON THROTTLE ADVANCE DURING T/O. RESET AS REQUIRED. ITEM HAS HISTORY. DUE HISTORY OF THIS FAULT, THIS ITEM IS GENERALLY CAUSED BY A DEFECTIVE IDG. SUSPECT IDG INSTALLED BY PREVIOUS STATION FOR ANOTHER TYPE FAULT, NEEDS RPL. NO TIME TO T-S. IDG DISCONNECTED PER MEL AND APU SERVICED TO FULL PRIOR TO DEPARTURE. IDG REPLACED. AFTER TROUBLESHOOTING AND LOOKING AT HISTORY. REPLACED GCU AND OPS CHECK LEFT IDG. OPS OKAY.

Part: IDG — FAILED (NR 1 ENGINE) · airframe 78,808 hrs · 12,785 cycles

CREW REPORT: JUST PRIOR TO TAKING RUNWAY L AC BUS FAILED. ACP TROUBLESHOOTING PER TABLE 102 REF MM P163 FOR DP TRIP AND MAIN BUS-OVERLAP. ALL WIRE CHECKS SAT. CREW ALSO REPORTED THE LEFT GENERATOR CONTROL TRIPPED AND THE LEFT TIE BUS ALSO FAILED. BOTH THE LEFT GEN CONTROL AND TIE BUS WERE ABLE TO BE RESET. WHEN THE LEFT AC BUS WAS NOT POWERED THE RIGHT GEN POWER DIDN'T AUTO TRANSFER TO THE LEFT AC BUS. REMOVED AND REPLACED NR 1 ENG IDG PER MM. OPS CHECKED GOOD. NO LEAKS.

Part: IDG — DISCONNECTED (NR 1) · airframe 78,781 hrs · 12,778 cycles

LEFT GENERATOR DRIVE EICAS & DRIVE LIGHT ON DRIVE DISCONNECTED. REPLACED NR 1 ENGINE IDG, OPS CHECKED NORMAL.

Part: IGNITION SYS — FAILED (APU) · airframe 78,779 hrs · 12,777 cycles

APU WILL NOT START. REPLACED IGNITION UNIT.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT) · airframe 78,779 hrs · 12,777 cycles

EXIT SIGN DOOR 1R AS WELL AS FLOOR LIGHTING STRIP BY SAME DOOR ARE FLASHING ON AND OFF. REPLACED POWER SUPPLY BATTERY PACK M1552, OPS CHECKED OKAY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 78,395 hrs · 12,715 cycles

EXTERNAL EEL LIGHT ON AFT RT DOOR IS INOPERATIVE. RELAMPED & REPLACED POWER SUPPLY ASSY, WORKS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 78,395 hrs · 12,715 cycles

EMEGENCY LIGHT BY FWD GALLEY IS INOPERTIVE. REPLACED BATTERY, WORKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,395 hrs · 12,715 cycles

EMERGENCY LIGHT ABOVE FLIGHT DECK DOOR IS INOPERATIVE. RESEATED LIGHT ASSY. WORKS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 78,395 hrs · 12,715 cycles

SMALL EMERGENCY EXIT SIGN BY DOOR 1 RIGHT IS INOPERATIVE. REPLACED BATTERY, WORKS NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 78,395 hrs · 12,715 cycles

EMERGENCY LIGHT ON SEAT 19K IS INOPERATIVE. SECURED SEAT CONNECTOR, CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 77,887 hrs · 12,645 cycles

FLAP LT ON FMA W-FLAPS IND UP & VERIFIED UP VISUALLY AT 250 KTS. FMA CLR'D LATER. *SUPPLEMENTAL DATA UPDATE* PERFORMED MCDP GRD TEST PER MM, FOUND LAST FLT FAULTS, AP CTR MODE ERR, DIAGNOSTIC CODES, 110780, 120780, 130780, NO CURRENT FAULT ON TEST 30, FLAP SLAT ELECTRONIC UNIT BITE TEST OK. CREW REPORTED THAT AFTER MOVING THE FLAPS DOWN TO 1 DEG AND UP AGAIN ALL RETURNED TO NORMAL THROUGH THE FLIGHT.

Part: SWITCH — FAULTY (CTR TANK) · airframe 77,871 hrs · 12,643 cycles

CREW REPORTED CENTER TANK RIGHT FUEL PUMP PRESSURE LIGHT IS NOT ON WITH PUMP SELECTED ON PRIOR TO START. REPLACED THE LOW PRESSURE SWITCH S424 PER AMM. NO LEAKS NOTED. PRESSURE SWITCH SWAPPED FROM S806 R FUEL JETTISON PUMP. LOW PRESSURE SWITCH S806 INOP. REPLACED PRESSURE SWITCH S806. OPS CHECK OKAY.

Part: PUMP — FAULTY (FUEL SYSTEM) · airframe 77,230 hrs · 12,551 cycles

PRIOR TO START RIGHT CENTER FUEL PUMP SHOWED ON. DEFERRED RT CENTER FUEL PUMP AS PER MEL 2822H. ACP TEST OF RT CT OVERRIDE JETTISON PUMP PER MM, TEST OKAY. OPERATED PUMP TO TRANSFER FUEL FROM THE AUX TANK TO LEFT AND RIGHT MAIN TANKS, PUMP OPERATED OKAY. NEEDS TO FUEL AUX TANK AND PERFORM ENG START TO SEE IF FAULT RETURNS. COMPLETED TEST PER MM. ALL CHKS WERE GOOD.

Part: SKIN — MISSING (RT ENG STATOR) · airframe 76,624 hrs · 12,457 cycles

RT ENGINE REAR STATOR MISSING WHOLE LOWER SKIN, UPPER SKIN BEGINNING TO COME OFF. INSPECT INTERMEDIATE CASE STRUT FAIRING IAW MM. INSPECTED COMPRESSOR INTERMEDIATE CASE STRUT AT 3 O'CLOCK POS. LOWER FAIRING MISSING. DAMAGE. CF IAW AMM.

Part: CHARGER — FAULTY (MASTER BATTERY) · airframe 76,522 hrs · 12,443 cycles

MAIN BATTERY CHARGER STATUS MSG WILL NOT CLEAR. CHANGED APU CHARGER WITH MAIN BATTERY CHARGER. STATUS MESSAGE CLEARED, CHARGER OPERATES SATISFACTORY.

Part: OXYGEN MASK — MISINSTALLED (CABIN) · airframe 76,434 hrs · 12,429 cycles

OXYGEN MASK INSP FOUND NUMEROUS O2 MASKS NOT PROPERLY PACKED. REPACKED AND STOWED 416 PASSENGER O2 MASKS IAW MM.

Part: LIGHT — MISSING (CABIN) · airframe 76,434 hrs · 12,429 cycles

RT REAR ENTRY DOOR IS MISSING EMERGENCY LIGHT ILLUMINATION FOR DOOR RELEASE HANDLE. REPLACED RT REAR (4RT) EMERGENCY LIGHT ASSY. OPS CHECKS GOOD.

Part: SHUTOFF VALVE — INTERMITTENT (BLEED AIR SYS) · airframe 76,122 hrs · 12,385 cycles

BLEED AIR DUCT PRESSURE INTERMITTENTLY SURGING BTWN 20-40 PSI AT ALTITUDES BELOW 8000 FT. OCCURRED TWICE ON CLIMB POWER SETTINGS (1.46 EPR). ON ARRIVAL IDLE POWER (1.02-.99EPR) WITH BOTH ISOLATION VALVES CLOSED AND RT PRESSURE WAS SLIGHTLY HIGHER SURGING. SEEMS OK (1.05-1.20 EPR RANGE). REPLACED PRSOV IAW MM, CHECKS OK.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 75,986 hrs · 12,361 cycles

WINDOW EICAS MESSAGE DISPLAYED. INOP LIGHT ILLUMINATED & DID NOT EXTINGUISH WHEN SWITCH WAS RECYCLED TO OFF/ON. SWAPPED WINDOW HEAT CONTROLLER, NO HELP. SUSPECT BAD WINDOW. WINDSHIELD CONTROL BITE FAILED, UNIT REPLACED; NOW FAULTS WINDOW 3R. INTERNAL RESISTANCE OUT OF LIMITS BETWEEN J12 AND J9. OPS CHECK FAILS 3R. REPLACED WINDOW ASSY.

Part: CIRCUIT CARD — FAULTY (E/E COOLIN ANNUN) · airframe 76,029 hrs · 12,370 cycles

RAMP REPORTED WHILE TOWING ACFT TO GATE EQUIPMENT COOLING HORN CAME ON AND AT GATE FOUND FWD EQ SUP FAN 1 STATUS MESSAGE. T-S IAW FIM 21-23-08 PAGE 107 BLOCK 6, WILL NEED RELAYS K1325, K1326 TO CONT. T-S. REPLACED RELAY K1319 AND NO HELP. REPLACED M876 EQUIP COOLING ANNUNCIATOR CARD, OPS CKS NORMAL.

Part: CONTROL UNIT — FAULTY (SPOILERS) · airframe 76,029 hrs · 12,370 cycles

RECENT HISTORY OF 'SPOILER' EICAS MSG WITH 'PCA' FAULT BALL SET ON SCM 2L. DUE TO RECENT HISTORY OF 'SPOILER' EICAS MSG WITH 'PCA' FAULT BALL SET ON SCM 2L. DUE TO SUCCESSFUL RESET AFTER REMOVAL & CLEANING OF PCA CONNECTORS; REMOVE INSPECT AND REPLACE IF NECESSARY NR3 & NR10 CA CONNECTORS, CHECK THE RESISTANCE OF NR3 AND NR10 PCA CONNECTORS IAW FIM AND DOCUMENT MEASURED RESISTANCE. IF RESISTANCE OK REPLACE SCM 2L WITH A -200 SERIES SPOILER CONTROL MODULE (481-9211). CONSULT ON-LINE IPC FOR PARTS LIST CURRENCY. RESISTANCE READINGS NR3 1-3 940 2-4 950. NR10 1-3 945 2-4 940. REPLACED SCM 2. OPS CHECKS OK.

Part: DRAIN VALVE — LEAKING (FUEL TANK) · airframe 75,480 hrs · 12,285 cycles

RIGHT TANK FUEL SUMP HAS FUEL SEEP AT OUTER CIRCUMFERENCE. REPLACED RT TANK SUMP DRAIN VALVE. OPS NORMAL.

Part: CABLE — EXPOSED (EMERGENCY LIGHTS) · airframe 75,262 hrs · 12,253 cycles

FLOOR CABLE EXPOSED 30B. SECURED CABLE.

Part: ISOLATION VALVE — FAILED (RT ENGINE) · airframe 75,218 hrs · 12,247 cycles

RIGHT ENGINE BLEED OFF LIGHT ON & RT ENG BLEED OFF EICAS MESSAGE, WITH ENG RUNNING, ENG BLEED SWITCH ON, LT & RT ISOLATION VALVES CLOSED, AC PACK SELECTED ON, & DUCT PSI IS ZERO. OFF LIGHT STAYS ON WHEN N1 IS ABOVE 41%. REPLACED PRSOV PER MM. ACP ENG RUN PER JRH ALL OPERATION AND INDICATIONS NORMAL.

Part: INDICATOR — FAULTY (ALTITUDE) · airframe 75,191 hrs · 12,244 cycles

FO'S ALT FAILURE, RTFL. REPLACED F-O'S ALTITUDE INDICATOR PER MM, OPS CKS GOOD.

Part: CONTROL ROD — DAMAGED (RT WING SLAT) · airframe 75,025 hrs · 12,220 cycles

DAMAGE TO RT WING L/E. RT WING INBD SLAT OTBD TIE ROD DAMAGED. PANEL R & R TO SHOP 273 (AOG D0385). WORKING WITH EG FOR REPAIR OF L/E WHERE PANEL SCREWS UP TO. ALSO ROBBING PANEL FROM TPA. REPLACED CONTROL ROD. ACCMP'D INSTALLATION INSP.

Part: CONTROL VALVE — FAULTY (LT A/C PACK) · airframe 75,017 hrs · 12,219 cycles

EICAS RT PACK OFF. RAN C-L.PACK RETURNED TO NORMAL OPS. PROBLEM REOCURRED. ACCOMPLISHED TROUBLESHOOTING. NO FAULTS ON PACK TEMP CONTROLLER. PACK INOP ON GROUND. SUSPECT FLOW CONTROL VALVE PCN 643-9118. FLOW CONTROL VALVE LOCKED. REPLACED RT FLOW CONTROL VALVE, TESTED OK.

Part: CONTROLLER — FAULTY (RT ENGINE BLEED) · airframe 75,025 hrs · 12,220 cycles

RIGHT ENGINE BLEED LIGHT CYCLED ON AND OFF 3 OR 4 TIMES DURING DESCENT AT 80 PERCENT N2. AIR SUPPLY BITE MODULE FAULTS HPC. DEFFERED PER MEL AND LOCKED HPSOV. REPLACED RIGHT ENG HPC PER MM, OPS NORMAL DURING ENG RUN.

Part: CONTROL VALVE — FAULTY (RT PACK) · airframe 75,017 hrs · 12,219 cycles

EICAS R PACK OFF. RAN C-L. PACK RETURNED TO NORM OPS. THEN PROB REOCCURRED. ACCOMPLISHED TROUBLESHOOTING. NO FAULTS ON PACK TEMP CONTROLLER. PACK INOP ON GROUND. SUSPECT FLOW CONTROL VALVE FLOW CONTROL VALVE LOCKED. REPLACED RT FLOW CONTROL VALVE, TESTED OKAY.

Part: BLEED VALVE — FAULTY (RT ENGINE) · airframe 75,025 hrs · 12,220 cycles

RIGHT ENGINE BLEED LIGHT CYCLED ON AND OFF 3 OR 4 TIMES DURING DESCENT AT 80 PERCENT N2. AIR SUPPLY BITE MODULE FAULTS HPC. DEFFERED IAW MEL AND LOCKED HPSOV. REPLACED RT ENG HPC, OPS NORMAL DURING ENG RUN.

Part: FMU — FAILED (NR 1 ENGINE) · airframe 75,011 hrs · 12,218 cycles

NR 1 ENGINE VALVE LIGHT INDICATION, RTFL. FMU FOUND FAULTY. REPLACED FMU. GROUND TEST NR 3 IDLE RUN TEST NORMAL.

Part: PUMP — FAULTED (FUEL BOOST) · airframe 74,556 hrs · 12,154 cycles

BSTR PUMP LOW PRESS LIGHT-ON, RTFL. REPLACED RT AFT BOOST PUMP. FOUND R AFT FUEL BOOST PUMP CB (G21) TRIPPED. REPLACED CIRCUIT BREAKERS C371, C370 AND WIRES CONNECTED TO CB'S. ALL BOOST PUMPS TEST GOOD.

Part: GUARD — LOOSE (COCKPIT) · airframe 74,551 hrs · 12,152 cycles

EEL LIGHT SWITCH GUARD ON FLIGHT DECK OVERHEAD PANEL IS LOOSE. SECURED GUARD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 74,551 hrs · 12,152 cycles

EEL LOWER EXIT SIGN BY FWD RIGHT OVERWING EXIT DOOR IS INOPERATIVE. REPLACED BATTERY, CHECKS GOOD.

Part: CONTACT — DIRTY (EXTERIOR) · airframe 74,551 hrs · 12,152 cycles

EXTERIOR EEL LIGHT BY DOOR 1 RIGHT IS INOPERATIVE. RELAMPED, NO HELP. CLEANED AND ADJUSTED LAMP CONTACTS, CHECK OKAY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 74,551 hrs · 12,152 cycles

EMERGENCY FLOOR STRIP BY RIGHT MID LAV IS INOP. REPLACED BATTERY, CHECKS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 74,551 hrs · 12,152 cycles

LOWER EEL EXIT SIGN BY RIGHT AFT OVERWING EXIT DOOR IS INOP. BY- 116760 REPLACED BATTERY, CHECKS GOOD.

Part: CONNECTOR — DIRTY (TRU) · airframe 74,503 hrs · 12,146 cycles

GROUND HANDLING TRU CB ON P34 POPPED. REPLACED TRU AND TRU CB PER MM, NO HELP. CB APPEARED TO POP WHEN UNDER LOAD AND WOULD ONLY STAY IN WHEN FWD AND AFT CARGO HANDLING CBS WERE PULLED. REMOVED AND CLEANED CONNECTOR D4926P. INSPECTED WIRING IN P34 PANEL AND ACCOMPLISHED SHAKE CHECK OF WIRING AROUND P34 PANEL. CB NOW STAYS SET EVEN WHEN UNDER HIGH LOAD.

Part: PUMP — DEFECTIVE (FUEL BOOST) · airframe 74,486 hrs · 12,144 cycles

R AFT BOOST PUMP C/B POPPED, FLT DIVERTED. REPLACED RIGHT BOOST PUMP PER MM, ALL OPS AND CHECKS NORMAL.

Part: ACTUATOR — FAULTY (FUEL CROSSFEED) · airframe 73,738 hrs · 12,044 cycles

FUEL CROSSFEED VALVE LIGHT-ON-& "FUEL CROSSFEED" EICAS MSG. DISPLAYED WHEN CROSSFEED SWITCH -OPEN OR CLOSED- SELECTED. AFT CROSSFEED VALVE WILL NOT OPEN- VALVE LIGHT ON WITH SWTCH IN OPEN POSIT. VALVE LIGHT OUT WITH SWITCH CLEARS DEFERRED AFT CROSSFEED VALVE INOP IAW MEL 2822R PROCEDURES. REPLACED ACTUATOR FOR AFT CROSS FLOW VALVE. OPS NORMAL.

Part: WARNING LIGHT — ILLUMINATED (RUDDER RATIO) · airframe 73,715 hrs · 12,041 cycles

RUDDER RATIO LIGHT ILLUMINATED, FLT DIVERTED. ACCOMPLISHED OVERWEIGHT LANDING CHECK. CREW REPORTED SOFT LANDING NO DAMAGE FOUND. ACCOMPLISHED TROUBLESHOOTING IAW FIM, NO FAULTS INDICATED. ACCOMPLISHED CSEU CKS IAW MM. NO FAULTS INDICATED. UNABLE TO DUPLICATE FAULT ON GRD LHR.

Part: PUMP — FAULTY (FUEL SYSTEM) · airframe 73,683 hrs · 12,035 cycles

L FUEL PUMPS OVERRIDING CENTER. DID FUEL CONFIG IRREG PROC TO CORRECT PROBLEM. OK NOW WITH 3000 LBS SPLIT UNTIL CENTER USED. LEFT CENTER PUMP INOP. REPLACED SLEEVE IAW WITH COA. ALSO REPLACED PUMP. SYSTEM OPS CK'D AND REACTIVATED.

Part: LATCH — CRACKED (R2 DOOR) · airframe 73,609 hrs · 12,026 cycles

DOOR 2R BUSTLE UPPER AFT LATCH IS CRACKED. BOTH ITEMS ON AOG. (160-1143 = AOG K1897, 160-1158 = AOG N1993) LATCH CLOSES, LATCHES AND LOCKS NORMAL, BUT ONE SIDE OF LATCH IS BROKEN AND NEEDS TO BE REPLACED. LATCH ASSY PCN 160-1158 ON EXP E1777.

Part: UNKNOWN — LEAKING (CABIN) · airframe 71,986 hrs · 11,791 cycles

38E, OVRHEAD BIN, STILL DRIPPING WATER, SEEMS TO BE ONLY IN FLIGHT. REPLACED SEVERAL CROWN ARE A INSULATION BLANKETS THAT WERE FOUND WET WITH CONDENSATION. REPLACED CEILING PANELS.

Part: MONITOR — FAULTY (ENG VIBRATION) · airframe 71,986 hrs · 11,791 cycles

NR 2 ENG N1 VIB INDICATION FLUCTUATES WITH EPR CHANGE. NO VIBES FELT IN STABLE CRUISE. NO ACTUAL VIB FELT, CREW FELT ISSUE TO BE FAULTY IND. REPLACED AVM UNIT.

Part: SKIN — GOUGED (AILERON) · airframe 71,880 hrs · 11,777 cycles

RT INBD AILERON IS GOUGED ON LOWER SURFACE. DAMAGE MEASURES .5" BY 10" IN LENGTH. PREPPING TO REMOVE AILERON. DURING THE RT INBD AIL OPS TEST, ACFT FAILS TEST. ALL OTHER TEST REQUIREMENTS CK NORMAL. ACCOMPLISHED REMOVAL AND INSTALLATION OF ROBBED AILERON IAW MM. COMPLETED INSTALL OF AILERON IAW MM. DURING TEST FOUND SPOILERS 6 & 7 DO NOT FUNCTION PROPERLY DURING SINGLE HYDR SYS OPS. AFTER RESET THEY WILL WORK TWICE AND LOCK OUT. TRIED SEVERAL SCM'S 3R. SEVERAL FROM STOCK AND SWAPPED POSITION WITH OTHER SCM'S, NO HELP. WILL REQUIRE FURTHER TROUBLESHOOTING. RT WING INBD AILERON POSITION TRANSMITTER CONTROL CRANK EARS ARE CRACKED. REPLACED AS REQUIRED. REPLACED CONTROL CRANK AND ADJUSTED, OPS NORMAL.

Part: CONNECTOR — BURNED (CARGO DOOR) · airframe 71,420 hrs · 11,714 cycles

CARGO DOOR EICAS MSG, RTFL FOUND BURNED PIN ON FWD CARGO DOOR HARNESS CONNECTOR D6266.PIN 20 POWER FOR DOOR LTS, ARCING TO PIN 8 WHICH IS PROX SENSOR S215. REPLACED CONNECTOR D6266 AND BACK CONNECTOR. DOOR OPS CHECKS GOOD.

Part: CIRCUIT CARD — FAULTED (RT WING SLIDE) · airframe 71,316 hrs · 11,698 cycles

RT WING SLIDE EICAS, RTFL. FOUND S219 PROX SENSOR WIRING CHAFED AT AFT SIDE OF SLIDE COMPARTMENT, REPLACED SENSOR AND ASSOCIATED WIRING. FOUND HARD FAULT ON PSEU FOR PROX, LOGIC AND DRIVER CARDS FOR S219 SENSOR. REPLACED PROX, LOGIC AND DRIVER CARDS FOR S219 IN POSITIONS 3 - 5 AND 7 RESPECTIVELY. OP CHECKS NORMAL.

Part: ANTI-ICE VALVE — INOPERATIVE (NR 1) · airframe 71,235 hrs · 11,688 cycles

EICAS MSG ENG ANTI-ICE DISPLAYED AND ENG ANTI-ICE VALVE LIGHT REMAINED ILLUM WITH SWITCH OFF, POSITION 1. PERFORMED T-S FOUND ENG ANTI-ICE VALVE INOP. REPLACED VALVE. RAN ENGINE. ENG ANTI-ICE VALVE WORKS OKAY.

Part: PUMP — INOPERATIVE (HYD SYSTEM) · airframe 71,210 hrs · 11,685 cycles

RIGHT EDP EICAS MSG. OVERHEAT LIGHT CAME ON WITH LOW PRESS, CREW TURNED THE PUMP OFF AND OVERHEAT LIGHT WENT OUT, PUMP LOW PRESS LIGHT ON. REPLACED NR 2 ENG EDP. OP CHECKS NORMAL.

Part: STARTER — FAILED (LT ENGINE) · airframe 70,980 hrs · 11,652 cycles

NO LIGHT OFF ON START OF LEFT ENG. RAN QRC. PUSH CREW ADVISED SPARKS SEEN FROM FRONT OF ENG. FOUND STARTER FAILED. REPLACED STARTER AND START VALVE. ACP'D IDLE RUN AND ALL OPS GOOD.

Part: LAMP — INOPERATIVE (EXTERIOR) · airframe 70,539 hrs · 11,587 cycles

LEFT EXTERIOR EMERGENCY LIGHT INOP 2EA AT FUSELAGE JUST AFT OF T/E FLAPS. REPLACED BOTH LAMPS, OPS CHECKED OKAY.

Part: COMPUTER — MALFUNCTIONED (EICAS) · airframe 70,369 hrs · 11,561 cycles

R EICAS COMPUTER MSG ON STATUS: WHEN RIGHT EICAS COMP SELECTED, BOTH UPPER AND LOWER EICAS DISPLAYS ARE BLANK. REPLACED RIGHT EICAS COMPUTER, DOWN LOADED SOFTWARE BOTH RIGHT AND LEFT ARE THE SAME, RAN TEST AND BOTH UPPER AND LOWER SCREENS ARE OK.

Part: OVEN — DIRTY (MID GALLEY) · airframe 70,294 hrs · 11,548 cycles

VERY STRONG SMELL IN MID GALLEY (SMELLS LIKE BURNING PLASTIC). NEEDS DEEP CLEAN OVEN W41. CLEANED MELTED PLASTIC TRAY FROM BOTTOM OF WARMING OVEN.

Part: RADOME — DENTED (FUSELAGE) · airframe 69,685 hrs · 11,449 cycles

FOUND DENT AT 10 O'CLOCK POSITION AT 18 INCHES FROM RADOME AFT EDGE. AREA COVERED WITH TAPE. INSPECTED RADOME. DENT IS WITHIN LIMITS. REPLACED RADOME.

Part: TRANSCEIVER — FAILED (LT VHF) · airframe 69,607 hrs · 11,434 cycles

NR 1 VHF COMM XMISSION & RECEPTION INOP. REPLACED LT VHF RECEIVER TRANSMITTER, OP CHECKED OKAY.

Part: CIRCUIT BOARD — FAULTY (EQUIP COOLING) · airframe 69,582 hrs · 11,424 cycles

EQUIP COOLING EICAS AND OVERHEAD. REPLACED EQUIP COOLING INDICATION CIRCUIT BOARD. REMOVED AND CLEANED LOW FLOW SENSORS, HAVE HAD NO FAULTS FOR 1.5 HOURS AT ORD. EQUIP COOLING TEST OKAY.

Part: COUPLER — FAULTY (HF SYSTEM) · airframe 69,541 hrs · 11,416 cycles

RIGHT HF ISSUE. FLIGHT DIVERTED. REPLACED RIGHT HF COUPLER. SAFTIED ALL CONNECTORS AS REQUIRED. FOUND D4839P AND D4841P LOOSE, MADE WRITE UP. NEED TO ACCOMPLISH OP CK OF LEFT AND RIGHT HF. PERFORMED MM23-11-00 AND MADE CALLS FROM AIRPLANE TO AIRPLANE AND AIRPLANE TO ANDREWS AIR FORCE BASE BOTH LEFT AND RIGHT OPS OK.

Part: PANEL — DAMAGED (LE SLAT) · airframe 69,499 hrs · 11,408 cycles

RIGHT L/E NR 7 SLAT CLOSURE PANEL HAS DAMAGE. NR 7 LEADING EDGE SLAT REPAIRED BY SFO SHOP ON R&R R42774, REINSTALLED ORIGINAL SLAT WITH NO ADJUSTMENTS DISTURBED DURING REMOVAL OR INSTALL. CHECKED FIT & FAIR AFTER INSTALLATION AND SOLD TO INSPECTION. INSPECTED SAFETY AND SECURITY OF NR 7 SLAT, VERIFIED FIT AND FAIR AND PROPER OPERATION.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 69,433 hrs · 11,390 cycles

MAIN CABIN STA 1307, STR 17R DRILL DAMAGE IN RADIUS OF STRINGER. MAJOR REPAIR ACCOMPLISHED: BLENDED BEAR STRAP DAMAGE AND INSTALLED STRINGER SPLICE REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,433 hrs · 11,390 cycles

EXT FUSELAGE SKIN STA 1542, BL 0 IS CORRODED AROUND DRAIN HOLE STR 39L - 39R. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER TRIPLER REPAIR.

Part: WIRE — DISCONNECTED (G4 CHILLER) · airframe 69,433 hrs · 11,390 cycles

DURING G4 GALLEY CHILLER CIRCUIT BREAKER INSP, FOUND BUS WIRE DISCONNECTED AT C-B C9032 A1 POSITION. INSTALLED BUSS WIRE. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,433 hrs · 11,390 cycles

LEFT AFT DOOR EMERGENCY LIGHT (EXTERNAL) IS INOP. RELAMPED AND OPS CHECKS GOOD.

Part: WIRE — CHAFED (NR 1 PYLON) · airframe 69,433 hrs · 11,390 cycles

NR 1 PYLON HYD BATTERY HARNESS WIRE W390-082-18 FOR L ENG T-R HYD ISLN VALVE PRESSURE SWITCH IS CHAFED TO PRIMARY CONDUCTOR. REMOVED WIRE FROM PLUG D20 122, INSTALLED NEW SOCKET AND RE-ASSEMBLED. INSTALLED NEW WIRE. OPS CHECKS GOOD.

Part: WIRE — CHAFED (NR 2 PYLON) · airframe 69,433 hrs · 11,390 cycles

NR 2 PYLON HYD BATTERY HARNESS WIRE W394-8-18 FOR T-R PRESSURE SWITCH IS CHAFED PAST PRIMARY CONDUCTOR. REMOVED DAMAGED WIRE FROM PLUG D2138 AND JACK D41705. INSTALLED NEW WIRE. T-R OPS CHECKS GOOD.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 69,433 hrs · 11,390 cycles

STA 1307 STR 17R STR CLIP CORRODED. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED NEW STRINGER CLIP.

Part: SPLICE — DEFECTIVE (APU POWER) · airframe 69,433 hrs · 11,390 cycles

DURING INSPECTION OF APU GEN POWER CABLES, FOUND EVIDENCE OF OVERHEATING AT SPLICE AREAS. DAMAGE AT STA 1809 BULKHEAD BELOW RT HORIZ STAB PIVOT PIN. REMOVED OLD APU GENERATOR SPLICES. INSTALLED NEW SPLICES REF BSWPM 20-30-13 AND INSTALLED STAR SPACERS. OPS CHECKS GOOD.

Part: FEEDER CABLE — DETERIORATED (NR 1 IDG) · airframe 69,433 hrs · 11,390 cycles

NR 1 ENG IDG FEEDERS ARE DETERIORATED. INSTALLED NEW FEEDER IDG CABLES. OPS CHECKS GOOD.

Part: SLIDE — UNLACED (R2 DOOR) · airframe 69,433 hrs · 11,390 cycles

DOOR R2 SLIDE UNLACED. REPLACED SLIDE DEPLOY PEN.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 69,433 hrs · 11,390 cycles

AFT CARGO PIT STATION 1562 FAIL SAFE CHORD CORRODED AT BL 0. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SECTION OF FAIL SAFE CORD. FABRICATED & INSTALLED REPAIR ANGLE DOUBLER AND FILLER.

Part: WIRE — DAMAGED (NR 1 PYLON) · airframe 69,433 hrs · 11,390 cycles

NR 1 PYLON HYD BAY HARNESS WIRE W398-201R-18 FOR L ENG HYD PUMP HAS AN IMPROPER SPLICE INSTALLED. REPAIRED WIRING REF BSWPM 20-00-13, 20-61-11 AND B767 WDM 29-11-12. RE-ASSEMBLED PLUG 0916 AND JACK D4280J TO INSTALL NEW SECTION OF WIRING.

Part: SHEAR TIE — CORRODED (BS 1307, S35-36L) · airframe 69,433 hrs · 11,390 cycles

AFT CARGO COMPT BILGE SHEAR TIE EVIDENCE OF CORROSION AT LWR SKIN ATTACH POINT AFT SIDE OF FLOOR WEB STA 1307, STR 35L TO 36L. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: SHEAR TIE — CORRODED (BS 1351, LBL 12) · airframe 69,433 hrs · 11,390 cycles

AFT CARGO COMPT SHEAR TIE CLIP EVIDENCE OF CORROSION AT LWR AFT SIDE OF WEB STA 1351, LBL 12- LBL 17, STR 35L -37L. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: SHEAR TIE — CORRODED (BS 1285, S39R) · airframe 69,433 hrs · 11,390 cycles

EVIDENCE OF CORROSION AT LWR SKIN TO FLOOR WEB AFT SHEAR TIE STA 1285, STR 39R - 39L. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: SHEAR TIE — CORRODED (BS 1219, S38-39R) · airframe 69,433 hrs · 11,390 cycles

AFT CARGO COMPARTMENT BILGE SHEAR TIE CORRODED STA 1219, STR 39R TO 38R. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: SHEAR TIE — CORRODED (BS 1285, BL 0) · airframe 69,433 hrs · 11,390 cycles

EVIDENCE OF CORROSION AT LWR SKIN TO FLOOR WEB AFT SHEAR TIE STA 1285, BL 0, STR 39R TO 38R. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: SKIN — CORRODED (BS 1563, S39L/R) · airframe 69,433 hrs · 11,390 cycles

BULK COMPARTMENT STA 1563 DRAIN HOLE AT CENTER LINE CORRODED AT AFT SIDE OF SHEAR TIE STA 1563, STR 39L - STR 39R. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: SKIN — DAMAGED (BS 1317-1320) · airframe 69,433 hrs · 11,390 cycles

EXTERNAL FUSELAGE SKIN GOUGED-DENTED, STA 1317 TO 1320, STR 31L TO 31L. MAJOR REPAIR ACCOMPLISHED, CUTOUT DAMAGED SKIN. FABRICATED AND INSTALLED DOUBLER REPAIR.

Part: CABLE — LOOSE (R2 DOOR SLIDE) · airframe 69,433 hrs · 11,390 cycles

DOOR 2R SLIDE RELEASE CABLE UNLACED. REINSTALLED RELEASE CABLE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,433 hrs · 11,390 cycles

AFT FUSELAGE STA 1540 SHEAR TIE BETWEEN STR 37R AND 36R IS CORRODED. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: SHEAR TIE — CORRODED (BS 1540 S37-38R) · airframe 69,433 hrs · 11,390 cycles

AFT FUSELAGE STA 1540 SHEAR TIE BETWEEN STR 38R AND 37R IS CORRODED. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: SHEAR TIE — CORRODED (BS 1219, S39L/R) · airframe 69,433 hrs · 11,390 cycles

AFT CARGO COMPT BILGE SHEAR TIE CORRODED STA 1219, STR 39R TO 39L. MAJOR REPAIR ACCOMPLISHED: FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: SHEAR TIE — CORRODED (BS 1540 S39L/R) · airframe 69,433 hrs · 11,390 cycles

AFT FUSELAGE LWR INTERIOR SHEAR TIE STA 1540 BETWEEN STR 39L AND 39R CORRODED. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,433 hrs · 11,390 cycles

AFT CARGO COMPARTMENT BILGE SHEAR TIE CORRODED STA 1197+132, STR 39R. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,433 hrs · 11,390 cycles

AFT FUSELAGE LWR INTERIOR SHEARTIE STA 1540 BETWEEN 38L AND 37L IS CORRODED. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,433 hrs · 11,390 cycles

MAIN CABIN SEAT TRACK HAS SEVERAL AREAS OF CORROSION STA 754 - 786, RBL 88. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED NEW SEAT TRACK SECTION.

Part: FITTING — MISSING (OVERWING EXIT) · airframe 69,433 hrs · 11,390 cycles

CABIN, LT FWD OVERWING HATCH, LINER HANDLE PULL SHROUD FWD AND AFT CLIPS MISSING. REPLACED CLIPS.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,433 hrs · 11,390 cycles

AFT CARGO COMPARTMENT BILGE SHEAR TIE CORRODED STA 1197+132, STR 39L. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED SHEAR TIE.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 69,433 hrs · 11,390 cycles

MAIN CABIN FLOOR LEVEL SEAT TRACK HAS A BROKEN SECTION STA 786.0, LBL 89.5. MAJOR REPAIR ACCOMPLISHED, CUTOUT DAMAGED SEAT TRACK, FABBED AND INSTALLED NEW TRACK SECTION.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,433 hrs · 11,390 cycles

AFT FUSELAGE LWR INTERIOR SHEAR TIE STA 1549 BETWEEN STR 39L AND 38L IS CORRODED. MAJOR REPAIR ACCOMPLISHED, INSTALLED NEW SHEAR TIE P-N 140T2102U585.

Part: SHEAR TIE — CORRODED (BS 1540 S38-39R) · airframe 69,433 hrs · 11,390 cycles

AFT FUSELAGE LWR INTERIOR SHEAR TIE STA 1540 BETWEEN STR 39R AND 38R CORRODED. MAJOR REPAIR ACCOMPLISHED, INSTALLED NEW SHEAR TIE P-N 140T2102U585.

Part: FLOORBEAM — WORN (FUSELAGE) · airframe 69,433 hrs · 11,390 cycles

MAIN CABIN FLOORBEAMS FLANGE WORN AT CLIPNUT HOLES BS 1197 - BS 1197, RBL 12 - 50. MAJOR REPAIR ACCOMPLISHED, CUTOUT DAMAGE AND INSTALLED REPAIR STRAP AND ANGLE DOUBLER.

Part: SKIN — DAMAGED (NR 2 PYLON) · airframe 69,433 hrs · 11,390 cycles

NR 2 PYLON INBOARD SAILTAIL AT AFT LOWER STRUT FAIRING, 3 -8TH HUCK BOLT INSTALLED. MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGED SKIN SECTION. FABRICATED NEW SKIN FROM .05 INCH INCONEL AND INSTALLED.

Part: HOUSING — CRACKED (RH OVRWNG SLIDE) · airframe 69,433 hrs · 11,390 cycles

R-H OVERWING SLIDE DISCONNECT HOUSING CRACKED. SUPPLEMENTAL DATA UPDATE INSTALLED NEW DISCONNECT HOUSING. OPS CHECKED CABLE, OPS CHECKS GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,433 hrs · 11,390 cycles

MAIN CABIN, STA 1330 FAR RT OTBD SEAT TRACK, RBL 88, CORROSION IN SEAT TRACK. MAJOR REPAIR ACCOMPLISHED, INSTALLED NEW SECTION OF SEAT TRACK STA 1197 +44 TO 1430, RBL 88.5. PN 654T0513-1146.

Part: PIN — SHEARED (SLIDE DOOR) · airframe 69,433 hrs · 11,390 cycles

RT OVERWING SLIDE DOOR ALIGNMENT PIN SHEARED. REPLACED SHEARED PIN.

Part: LATCH — UNSERVICEABLE (OVERWING SLIDE) · airframe 69,433 hrs · 11,390 cycles

R-H OVERWING SLIDE DOOR LATCHES REQUIRE REPLACEMENT DUE TO PLANNED SLIDE DEPLOYMENT. INSTALLED NEW SLIDE DOOR LATCHES. ADJUSTED LATCHES AS REQUIRED.

Part: SLIDE — UNSERVICEABLE

ASPIRATOR LEAKS. BARREL LEAKS, NO EXTERNAL DAMAGE, CAUSE UNKNOWN. REPLACED ASPIRATOR.

Part: MOTOR — FAILED (TE FLAP) · airframe 69,394 hrs · 11,380 cycles

ALT FLAP SYSTEM WILL NOT EXTEND AND THE TRAILING EDGE INDICATION COMES ON EVEN WITH HYDRAULICS. NO MOVEMENT OF THE ALT SYSTEM (T/E SELECTED ONLY). REPLACED ALTERNATE FLAP MOTOR.

Part: WIRE — EXPOSED (CABIN) · airframe 68,737 hrs · 11,251 cycles

EMERGENCY EXIT LIGHT STRIP HAS EXPOSED WIRES LEFT SIDE FIRST CLASS. REPAIRED EMERGENCY LIGHTS STRIP.

Part: PANEL — DAMAGED (LE SLAT) · airframe 68,014 hrs · 11,135 cycles

LEFT WING NR 4 OUTBOUND SLAT LINKAGE PANEL HANGING DOWN. REPLACED LEFT WING NR 4 OUTBOARD SLAT LINKAGE PANEL, OPERATED SLATS, OPS CHECK NORMAL.

Part: PUMP — FAULTY (HYDRAULIC SYS) · airframe 67,868 hrs · 11,112 cycles

EICAS "C HYD PRIM 1" DISPLAYED. REPLACED NR 1 ACMP AND CONNECTOR D482. CASE AND DRAIN FILTERS REPLACED. ALL CHECKS OKAY. NO FAULTS NOTED.

Part: DISPLAY — FAULTY (EICAS) · airframe 67,744 hrs · 11,094 cycles

LOSING UPPER EICAS DISPLAY INTERMITTENT NO COLOR AND DISPLAY MSG. REPLACED UPPER EICAS DISPLAY.

Part: PROBE — FAILED (LEFT) · airframe 67,691 hrs · 11,085 cycles

LT ASI DURING TAKEOFF ROLL WENT TO ZERO KNOTS. REPLACED LT PITOT STATIC PROBE.

Part: ADC — FAILED (E&E BAY) · airframe 67,691 hrs · 11,085 cycles

ADC FAILURE. RTFL.

Part: ACTUATOR — LEAKING (NR 2 SPOILER) · airframe 67,690 hrs · 11,084 cycles

FOUND NR 2 SPOILER ACTUATOR POURING HYD FLUID FROM PCU. NR 2 SPOILER ACTUATOR LEAKING. REPLACED ACTUATOR. VERIFIED RIG AND OPS CHECKS.

Part: HF COMM — FAULTY (COCKPIT) · airframe 67,690 hrs · 11,084 cycles

HF SYSTEM FAULTY.

Part: COUPLER — FAULTY (HF COMM) · airframe 67,690 hrs · 11,084 cycles

HF INTERFERENCE FAULTS. REPLACED LT & RT COUPLER. OPS CHECKED. NO FAULTS. REPLACED LT TRANSCEIVER.

Part: HF COMM — INTERFERENCE · airframe 67,690 hrs · 11,084 cycles

HF INTERFERENCE FAULTS.

Part: CONNECTOR — LOOSE (CABIN) · airframe 67,690 hrs · 11,084 cycles

EEL EMERGENCY LIGHT STRIPS INOP ON LEFT AISLE IN THE VICINITY 1AB THRU 5AB. SECURED CONNECTOR, TEST OK.

Part: COVER — LOOSE (CABIN) · airframe 67,677 hrs · 11,082 cycles

EMERGENCY LIGHT STRIP LOOSE AT 14B. SECURED EMERGENCY LIGHT PLASTIC COVER AT SEAT 14B. OPS GOOD.

Part: CONTROL UNIT — FAULTY (AILERON) · airframe 67,467 hrs · 11,047 cycles

RUDDER AND AILERON TRIM EXCESSIVE WITH AILERON DEFLECTED. SUSPECT LEFT INBD AILERON STUCK IN UP POSITION, AS IND ON EICAS FLT CONT, IS DEFLECTED APPX HALF UP AND NOT RESPONDING TO INPUT. RUDDER AND AIL TRIM IS EXCESSIVE. AILERON FOR 6 HRS WAS ABOUT HALF DEFLECTED AND THEN WORKED ITS WAY TO ABOUT 1-4 DEFLECTION AS SEEN IN YOKE AND TRIM USED. FOUND LT INBOARD AIL, BOTH LT & CNTR SYS PCA'S HAVE QUICK DROOP & ARE BYPASSING (BOTH PCA'S MANUAL MANIPULATION WITH SYS PRESS APPLIED). REPLACED CTR SYS PCA. REPLACED LT INBOARD & OUTBOARD AILERON LEFT SYSTEM PCA. REPLACED RT NR 7 OVERRIDE SPOILER ACTUATOR & LT SPOILER OVERRIDE ACTUATOR.

Part: PUMP — DAMAGED (LT ENGINE) · airframe 67,052 hrs · 10,984 cycles

L HYD SYS MAINT STATUS MESSAGE. FOUND L EDP SHAFT SHEARED, REPLACED PUMP, OKAY.

Part: TRANSMITTER — READS HIGH (OIL PRESSURE) · airframe 66,212 hrs · 10,842 cycles

DURING CLIMB LEFT ENG OIL PRESS PEGGED OUT AT 400 PSI AT LEVEL OFF PRESS JUMPED TO 200. REPLACED OIL PRESSURE TRANSMITTER.

Part: BRACKET — CRACKED (L2 WINDOW) · airframe 66,096 hrs · 10,822 cycles

WINDOW L2 LOWER TRACK BRACKET CASTING CRACKED AT FWD OUTBOARD EDGE. REPLACED 2L WINDOW BRACKET.

Part: ASPIRATOR — LEAKING (EVAC SLIDE)

ASPIRATOR LEAKING. SUSPECT FAULTY O-RING. REPLACED ASPIRATOR. AC OK FOR SERVICE.

Part: BRACKET — BROKEN (LT MLG) · airframe 65,421 hrs · 10,718 cycles

ON WALK AROUND, FOUND FRONT END OF LT GEAR BOGIE LOWER TRAY DAMAGED 4 RIVETS BROKEN AND 1 INCH CRACK ON MOUNTING BRACKET, BRACKET BEND. INSTALLED NEW FWD MOUNT BRACKET AND STRAIGHTENED LOWER TRAY. AC OK FOR SERVICE.

Part: SWITCH — INOPERATIVE · airframe 65,382 hrs · 10,712 cycles

RTFL DUE TO DOUBLE TRANSPONDER FAILURE. RPLACED ATC ANTENNA SWITCH.

Part: LIGHT — BROKEN (CABIN) · airframe 65,369 hrs · 10,709 cycles

FLOOR LIGHT STRIP AFT OF 9AB BROKEN.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 65,087 hrs · 10,657 cycles

STATUS LIGHT ON FLASHLIGHT AT BUSINESS GALLEY NOT ON. REPLACED BATTERY OPS CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 64,587 hrs · 10,583 cycles

EEL LIGHT COVER ON FLOOR AT 13AB AND 14AB IS PULLED UP. SUSPECT NORMAL CREW AND PASSENGER BOARDING AND DEBOARDING. SPLICED IN NEW EEL STRIP OPS CHECK GOOD. AC OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 64,524 hrs · 10,574 cycles

EMERGENCY LIGHTS ON LEFT + MID SIDE OF 1ST CLASS GALLEY + LEFT SIDE OF CABIN FROM 1L TO MID LAVS. REPLACED EEL BATTERY.

Part: CAP — MISSING (SEATS 1B & 1F) · airframe 64,482 hrs · 10,565 cycles

END CAPS MISSING FROM EEL LIGHTING AT SEATS 1B AND 1F. INSTALLED END CAPS

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,165 hrs · 10,517 cycles

LEFT SIDE CABIN FLOOR LIGHTING INOP IN BUSS AND 1ST CLASS. REPLACED LIGHTS, OPS CHECKS GOOD.

Part: UNKNOWN — SMOKE (CABIN) · airframe 64,136 hrs · 10,513 cycles

CREW REPORTED SMOKE IN CABIN AND RETURN TO FIELD.

Part: ENGINE — LEAKING (NR 2) · airframe 64,122 hrs · 10,512 cycles

RTFL UNDER AMBER ALERT DUE TO ELECTRICAL ODOR. REMOVED NR 2 ENGINE AFTER CONFIRMATION OF DIAGNOSTIC TEST FLT. LABEL ENGINE REMOVAL REASON AS CABIN OIL ODOR & CHRONIC HUNG START. OIL SMOKE ENTERING THROUGH THE BLEED INLETS.

Part: UNKNOWN — UNKNOWN · airframe 63,765 hrs · 10,457 cycles

EICAS MSG R GEN OFF DISPLAYED. GEN OFF LIGHT ILLUM. CREW COMMENTS: A-C DID NOT PICK UP AC BUS AFTER RT ENGINE STARTED.

Part: UNKNOWN — UNKNOWN (COWL) · airframe 63,727 hrs · 10,451 cycles

FLIGHT DIVERTED DUE TO RIGHT ENGINE CORE COWL PROBLEM.

Part: PUMP — MALFUNCTIONED (HYDRAULIC SYS) · airframe 63,673 hrs · 10,443 cycles

NR 1 ACMP DOES NOT COME ON LINE WHEN IN AUTO MODE AND EDP IS SWITCHED OFF.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,673 hrs · 10,443 cycles

EEL EXTERIOR DOOR 1R AND 2L INOP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,673 hrs · 10,443 cycles

EXTERIOR EMERGENCY LIGHT AT L-1 DOOR IS INOP.

Part: CYLINDER — FAULTY (EVAC SLIDE) · airframe 63,673 hrs · 10,443 cycles

RIGHT OVERWING SLIDE CYLINDER BOTTLE BALL IS BELOW THE SPRING FORCE MECHANISM.

Part: LIGHT — LOOSE (CABIN) · airframe 63,673 hrs · 10,443 cycles

RIGHT FUSELAGE EVACUATION (EMERGENCY) LIGHT LOOSE STA 1230, STR 23R.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,673 hrs · 10,443 cycles

B-ZONE LEFT SIDE FWD 2 EA EEL LIGHT STRIPS ARE INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,673 hrs · 10,443 cycles

EMERGENCY EXIT LIGHT AT LEFT AND RIGHT AFT DOORS, LWR PORTION OF LIGHT (DOOR HANDLE ILLUMINATION) IS INOP.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,673 hrs · 10,443 cycles

BS 246 FLOORBEAM STIFFENER CRACKED RBL 26. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED STIFFENER.

Part: BLADES — DAMAGED (NR 1 ENGINE) · airframe 60,909 hrs · 9,970 cycles

BIRD STRIKE TO NR 1 ENGINE. ACCOMPLISHED BOROSCOPE INSP OF NR 1 ENG HPC 5TH, 6TH, 10TH AND 11TH STG BLADES PER MM 72-00-00. FOUND 1 EA 6TH STG BLADE WITH LARGE TEAR IN AREA C OF L/E BEYOND FLYBACK LIMITS, 18 EA 10TH STG BLADES WITH DAMAGE BEYOND LIMITS IN AREA B AND C, AND 2 EA 11TH STG BLADES WITH LARGE TEARS BEYOND LIMITS IN AREA C. BY- 41440: REMOVED ENG 717676 & REPLACED. COMPLETED VERIFICATION FLIGHT & ENGINE TESTED GOOD.

Part: WIRE — BURNED (WINDOW HEAT) · airframe 60,551 hrs · 9,909 cycles

F/O`S NR 1 WINDOW & CAPT'S SIDE WINDOW HEAT INOP. FOUND WINDOW HEAT WIRES BURNT BEHIND E2-1 RACK AT CONN D4294P, REF WDM 30-41-12. CONTROL SENSOR FOR LEFT WINDOW 2 MELTED AND OTHER WIRES HAVE HEAT DAMAGE. PWR WIRE W1120-203B-12 EXTENSIVELY DAMAGED. WIRES WERE REPAIRED AND HARNESS REINSTALLED IN A/C. HARNESS OPERATED OK. SUSPECT LOOSE PINS CAUSED HIGH CURRENT DRAW & C-B FAILED TO OPEN SOON ENOUGH TO PROTECT WIRES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,903 hrs · 9,469 cycles

FWD GALLEY CROSS AISLE EEL STRIP INOP.

Part: POWER SUPPLY — INOPERATIVE (SEAT 20FG) · airframe 57,440 hrs · 9,399 cycles

EMERGENCY POWER SUPPLY AT SEAT 20FG IS INOP. REPLACED POWER SUPPLY PER MM 33-51-07 AND OPS CHECK GOOD.

Part: INSERT — MISSING (OVERWING SLIDE) · airframe 57,440 hrs · 9,399 cycles

LT OVERWING SLIDE DOOR ACTUATOR SQUIB SHUNT CAP MISSING INSERT. REPLACED 3SF5951-501 SHORTING CAP. OK FOR RETURN TO SERVICE.

Part: SPRING — SHEARED (NLG) · airframe 57,205 hrs · 9,364 cycles

RIGHT DOWN LOCK SPRING ON NOSE LANDING GEAR SHEARED. REPLACED DEFECTIVE SPRING DUE TO WEAR WAS BEYOND LIMIT.

Part: ADC — FAILED (RIGHT)

FAILURE OF F/O AIR DRIVEN COMPUTER AND ALTIMETER. RT AIR DATA COMPUTER RPL, MR41190, NO DASH, BUT S/N=88041280. A/C HAD PREVIOUS HISTORY ON 18 MAY. NO UNIT HISTORY AVAILABLE IN CIDER FOR THIS S/N, SUSPECT THIS IS 1ST REMOVAL.

Part: LATCH — FAILED (CABIN)

LT O/W HATCH FAILS INTEGRATOR TORQUE CHECK. REPLACED LATCHES.

Part: HYDRAULIC SYSTEM — LEAKING (RIGHT) · airframe 50,166 hrs · 8,220 cycles

FLIGHT DIVERTED DUE TO RIGHT HYDRAULIC SYSTEM QUANTITY LOSS. REPLACED RIGHT SYSTEM EDP. NO FURTHER REPORTS NEXT 20 AC CYCLES.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,594 hrs · 7,290 cycles

MAIN CABIN BETWEEN BS 785.9 AND BS 814, LBL 55, SEAT TRACK CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SPLICE SECTION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,594 hrs · 7,290 cycles

MAIN CABIN BETWEEN STA 774 AND 785 AND LBL 55, SEAT TRACK HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SECTION WITH SPLICE DOUBLERS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 44,594 hrs · 7,290 cycles

CORROSION OUT OF LIMITS ON FLOOR SUPPORT ANGLE AT STA 368. OTBD BY LWR AFT R-2 DOOR ON STRUCTURE. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,594 hrs · 7,290 cycles

MAIN CABIN SEATTRACK AT STA 654+14 RBL 89 IS CORRODED OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION WITH SPLICE DOUBLERS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,594 hrs · 7,290 cycles

MAIN CABIN AT STA 1197+80 LBL 89 SEAT TRACK HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPLACEMENT TRACK AND SPLICES.

Part: FRAME — PUNCTURED (FUSELAGE) · airframe 44,594 hrs · 7,290 cycles

AFT PIT FRAME HAS 3 INCH PUNCTURE STA 1351, STR 24R TO 25R. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER REPAIR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,445 hrs · 7,266 cycles

LEFT MOST FWD EMERGENCY EEL STRIP INOPERATIVE. SECURED EEL STRIP, OPS CHECK OK.

Part: WARNING LIGHT — ILLUMINATED (HYD SYSTEM) · airframe 50,166 hrs · 8,220 cycles

RT PRIM HYD OVERHEAT EICAS AND LIGHT. RIGHT HYDRAULIC QUANTITY DROPPED TO ZERO. RIGHT ENGINE DRIVEN PUMP REPLACED. FAILURE DUE TO FROZEN BEARINGS, PUMP OVERHEATED DUE TO LACK OF LUBRICATION.

Part: PBE — DAMAGED (CABIN) · airframe 410,410 hrs · 6,761 cycles

PASSENGER BREATHING EQUIPMENT DAMAGED AT CLOSET 309. REPLACED PBE.

Part: GENERATOR — DEFECTIVE (DIODE,ROTOR, EXCEITO) · airframe 40,695 hrs · 6,613 cycles

ON CLIMB FROM SFO RIGHT HAND GENERATOR DROPPED OFFLINE AND WAS UNABLE TO BE RESET. SUPPLEMENTAL DATA UPDATE REPLACED RIGHT GENERATOR.DEFECTIVE PARTS - FOUND DIODE, ROTOR AND EXCITER FAILED.

Part: OXYGEN MASK — DEFECTIVE (COCKPIT) · airframe 38,104 hrs · 6,163 cycles

CAPTAINS OXYGEN MASK ASSEMBLY HEADBAND LEAKS AND WILL NOT COLLAPSE AROUND HEAD. MASK FAILED DUE TO NORMAL WEAR AND TEAR.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 36,761 hrs · 5,925 cycles

"MAIN BATT CHGR" MESSAGE DISPLAYED ON EICAS.

Part: CARD — FAULTY (OVERHEAT SYS) · airframe 35,795 hrs · 5,765 cycles

RT ENG OVHT EICAS MESSAGE. FOLLOWED FLIGHT MANUAL PROCEDURE, REDUCED THROTTLE, MESSAGE REMAINED. SHUTDOWN ENGINE. *S/D* THE EICAS RT ENG OVHT MSG WITHOUT DISCRETE LIGHT ON WAS CAUSED BY AFOLTS CARD M10274. THE CARD WAS REPLACED AND SYSTEM CHECKED OK. SHOP CHECK OF THE CARD CONFIRMED THE FAULT WAS A SHORTED COMPONENT ON THE CARD.

Part: OVEN — FIRE (MID GALLEY) · airframe 33,910 hrs · 5,431 cycles

FIRE IN MID GALLEY OVEN, LOCATION R31 RECON-OVEN. HAND HELD EXTINGUISHER USED. DIVERTED PHL. OVERWEIGHT LANDING. *S/D* FOUND PAPER BURNED BETWEEN TOP OF OVEN RACK AND EXHAUST FAN OPENING. THE OVEN WAS REMOVED AND THE ELECTRICAL CONNECTORS WERE INSPECTED. NO DAMAGE WAS NOTED. THE C-B PANEL ABOVE THE OVEN WAS ALSO REMOVED AND INSPECTED. NO DAMAGE WAS NOTED. THE OVEN AND ALL GALLEY EQUIPMENT WERE OPERATED FOR 1 HOUR WITH NO FAULTS FOUND. THE OVEN WAS TESTED PER MM 25-31-00.

Part: WINDOW — UNSECURE (NR 1 COCKPIT)

REJECTED TAKEOFF AT 100 KT DUE TO FLIGHT DECK WINDOW PROBLEM. *S/D* AIRCRAFT INSPECTED FOR HIGH SPEED RTO. NO DISCREPENCIES FOUND. NUMBER 1 SLIDING WINDOW WAS APPARENTLY NOT FULLY SECURED PRIOR TO DEPARTURE.

Part: VIDEO UNIT — ODOR (CABIN) · airframe 30,647 hrs · 4,815 cycles

STRONG ELECTRICAL SMELL IN MID CABIN. NO SMOKE OBSERVED, UNABLE TO CLEAR SMELL FROM CABIN. DIVERTED OMA. *S/D* TRACED SMELL TO SEAT 10C VDU. ISOLATE WIRING TO MONITOR ASSY AND SEAT ELEC BOX. CAPS AND SECURE CABLES. (DEFERRED) REPLACED VDB (VIDEO DISTRIBUTION BOX) AND CONNECTED CABLES. OPS CHECKED NORMAL.

Part: SNUBBER — DEFECTIVE (SERVICE DOOR) · airframe 30,154 hrs · 4,732 cycles

FORWARD SERVICE DOOR 1 RIGHT REQUIRES INTERIOR HANDLE TO BE PUSHED FULLY UP TO CLOSE. *S/D* MAINTENANCE FOUND THE INTERIOR HANDLE NOT HOLDING THE CORRECT POSITION WITH THE DOOR OPEN. THE SPRING HYDRAULIC SNUBBER WAS DEFECTIVE. REPLACED SNUBBER PER MM 52-11-31. OPS CHECKS WERE NORMAL.

Part: OVEN — FIRE (GALLEY)

SMOKE REPORTED FROM OVEN NR 305, FLT ATTENDANT DISCHARGED HALON FIRE EXTINGUISHER INTO OVEN. CB PULLED. CAUSE DUE TO PLASTIC AND PAPER MELTING AND OVERHEATING IN THE FAN AREA ON THE BAFFLE. OVEN REPLACED.

Part: LIGHT — MALFUNCTIONED (LT EXTERIOR)

AIRCRAFT RETURNED TO BLOCKS WITH REPORT OF LEFT AFT EXTERIOR EMERGENCY LIGHTS ILLUMINATED. *S/D* PERFORMED EXTERIOR EMERGENCY LIGHTS TEST PER MM. NO PARTS REPLACED, NO FURTHER REOCCURRENCE OF DISCREPANCY.

Part: INDICATION — MALFUNCTIONED (LANDING GEAR)

AFTER LANDING GEAR EXTENSION, EICAS GEAR DISAGREE AND TAIL SKID WARNINGS. GEAR AND TAIL SKID WARNING LIGHTS ILLUMINATED ON LANDING GEAR INDICATION PANEL BUT HAD ALL GEAR DOWN LIGHTS GREEN. RECYCLED LANDING GEAR AND GOT ALL NORMAL INDICATIONS WITH NO ABNORMAL EICAS OR GEAR WARNINGS.

Part: CIRCUIT BREAKER — FAILED (LT/RT GCU)

AIRCRAFT RETURNED TO SFO AFTER BOTH UTILITY BUS OFF LIGHTS CAME ON DURING TAKEOFF. *S/D* LEFT GENERATOR CONTROL BREAKER AUXILIARY CONTACT FAILED. REPLACED LEFT AND RIGHT GENERATOR CONTROL BREAKERS.

Part: TARGET SENSOR — OUT OF ADJUST (DOOR)

THE LEFT OVERWING EXIT DOOR REQUIRED 12 POUNDS OF FORCE TO OPEN DURING A MAINTENANCE CHECK. THE TARGET SENSOR WAS MISALIGNED IN THE INBOARD CORE OF THE DOOR. ADJUSTED TARGET SENSO, THE DOOR THEN OPENED FREELY AND THE ACTUATORS OPERATED PER DESIGN.

Part: SURGE VALVE — DEFECTIVE (APU)

THE APU SHUTDOWN PRIOR TO ENGINE START. THE APU WOULD NOT RESTART. *S/D* THE SURGE CONTROL VALVE WAS DEFECTIVE AND REPLACED, OPERATIONS CHECK NORMAL. NO OTHER APU DISCREPANCIES HAVE OCCURRED SINCE THIS INCIDENT.

Part: LAMP — INOPERATIVE (NR 6 SLIDE)

THE RIGHT NR 6 SLIDE LIGHT IS INOP. REPLACED LAMP, OPS CHECK NORMAL.