N69059

Part: FUEL CONTROL — LEAKING (APU) · airframe 94,671 hrs · 13,338 cycles

UPON APU START CABIN FILLED WITH FUEL VAPOR. SHUTDOWN APU UPON INSP OF APU FOUND FUEL LEAK FROM APU FUEL CONTROL FOUND APU FUEL CONTROL LEAKING. SHUT DOWN APU AND VERIFIED FUEL LEAK STOPS WITH SWITCH OFF AND BOOST PUMPS. REQUESTING MEL FOR APU INOP. DDP COMPLIED WITH CLARIFICATION: LEAK STOPS WHEN APU SWITCH IS OFF, EVEN WITH BOOST PUMPS ON NO FURTHER FUMES IN THE CABIN. DISPATCH DESK:TOMC APPROVES MEL 4911F. MEL APPLIED R&R FUEL CONTROL PACKINGS 11 AND 12 ON TUBES 5, 6, 7, AND 8 IAW AMM 49-31-01. OPS AND LEAK CHECK GOOD AT THIS TIME.

Part: WARNING LIGHT — FALSE ACTIVATION (ZONE 800) · airframe 94,365 hrs · 13,293 cycles

LFT AFT MAIN DOOR EICAS MSG CAME ON ON TOCHDOWN EMERGENCY LIGHTS TURNED ON IN THE CABIN CHECKED AFT LH ENTRY DOOR, CLOSED AND REOPEN SEVERAL TIMES. VERIFY WITH CREW MESSAGE DID NOT APPEAR. CLEAN SENSOR.

Part: PROXIMITY SWITCH — DAMAGED (ZONE 800) · airframe 93,775 hrs · 13,215 cycles

E/E ACCESS DOOR EICAS LIGHT ILLUMINATED ON T/O.. INTERMITTENT FLASHING. QRH FOLLOW D VISUALLY INSPECTED E/E DOOR SENSOR FOUND DAMAGE ON SENSOR. REQUESTING MEL FOR E/E DOOR SENSOR. APPROVED DDP COMPLIED, VERIFIED E/E DOOR CLOSED AND SECURED. CONFIRMED DAMAGE TO E/E DOOR PROXIMITY SWITCH. DAMAGE CAUSED BY E/E DOOR LATCH PIN ROTATING AND CONTACTING THE SWITCH WHEN DOOR IS CLOSED. R & R E/E BAY PROXIMITY SWITCH IAW AMM 52-71-01, OPS CK GOOD. ADJUSTED PUSHROD/LATCHPIN ASSEMBLY ON E/E BAY DOOR REF AMM 52-48-04, PIN IS SECURE, ALL OPS NORMAL.

Part: SLIDE — FAULTED (ZONE 800) · airframe 93,592 hrs · 13,191 cycles

EMERGENCY EXIT DOOR MOUNTED ESCAPE SLIDES REPLACE {B767-25-3-0032} - DOOR L3 S/N 0394 REMOVED AND REPLACED EMERGENCY EXIT DOOR MOUNTED SLIDE AT DOOR L3 IN REF WITH AMM 25-66-10. PARTS USED: 64-2566-9-0005, QTY :1 ROTABLE PARTS CHG:TT # 1567912 SN OFF 0394 PN OFF 64-2566-9-0005.SLIDE, B767-400 OFF 64-2566-9-0005 0394 ON 64-2566-9-000ACCOMPLISHED RII INSPECTION OF DOOR 3L EMERGENCY SLIDE INSTALLATION IAW AMM 25-66-10.

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 800) · airframe 93,560 hrs · 13,187 cycles

ACCESS DOOR E/E FWD EICAS ON DEPARTURE BETWEEN 6-10K FT. PRESSUR IZATION NORMAL. FAULT NOT PRESENT ON GROUND. FIM TASK 52-71 FAULT TREE 814 C/OUT AND NO FAULT FOUND. DOOR WARNING SENSOR TEST OF ELECTRONICS DOOR C/OUT SATISFACTORY IAW AMM TASK 52-71-00-735-072 REV. 144

Part: WIRE — EXPOSED (ZONE 200) · airframe 92,873 hrs · 13,104 cycles

AS REPORTED BY FA... WIRES HANGING ABOVE ROWS 40-41 ASSOCIATED W ITH EMER EXIT LIGHTS BACK COVER INSTALLED REF AMM TASK 33-51-10-962-104.PARTS USED: 64-2526-3-0241, QTY :1

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 800) · airframe 92,798 hrs · 13,095 cycles

L AFT ENT DOOR CAUTION MOMENTARILY DISPLAYED SHORTLY AFTER LAND ING INSPECTED L AFT ENTRY DOOR. PERFORMED L AFT ENTRY DOOR FUNCTIONAL TEST REF AMM 52-71-00-735-072. FOUND SATISFACTORY. NO OTHER FAULTS FOUND AT THIS TIME.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 92,759 hrs · 13,090 cycles

EXTERIOR EMERGENCY LIGHTS NEAR DOOR 2RH INOPERATIVE. REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHT NEAR DOOR 2RH AS PER AIPC 33-51-06-02 ITEM 85 AND PERFORMED OPERATIONAL TEST AS PER AMM TASK 33-51-00-715-001 TEST OK. GOOD FOR SERVICE.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 92,682 hrs · 13,081 cycles

EMERGENCY LIGHTS ON THE CEILING NEAR SEAT POSITION 34BA INOPERATIVE. REMOVED AND REPLACED EMERGENCY CEILING LIGHT AS PER AIPC 33-51-04-06A AND PERFORMED OPERATIONAL TEST AS PER AMM ASK 33-51-00-715-001 TEST OK. GOOD FOR SERVICE.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 92,455 hrs · 13,052 cycles

SLIDE PRESSURE GAUGE DOOR 2R OUT OF THE GREEN PERFORMED DOOR 2R INFLATION CYLINDER CHECK IAW AMM 25-66-02. PRESSURE WITHIN LIMITS. OK TO CONTINUE.

Part: ACCESS PANEL — MISSING (ZONE 400) · airframe 92,033 hrs · 12,999 cycles

PDA 2 #2 ENGINE OUTBOARD PYLON (ROUND) ACCESS PANEL MISSING. UPDATE, PANEL # 446AR (ENGINE MOUNT ACCES PANEL). REQUEST TO PLACE MISSING PANEL ON CDL. REF CDL MANUAL CHP 54 FIG 106, OK TO PLACE 1 NACELLE STRUT ACCESS DOOR ON MEL. ITEM PLACED ON CDL, C/W DDP. OK TO CONTINUE.

Part: HYDRAULIC LINE — LEAKING (NR 1 ENGINE) · airframe 91,903 hrs · 12,982 cycles

L HYD QUANTITY EICAS CAME ON INFLIGHT UPON ARRIVAL AT GATE, LEFT ENGINE HAD STEADY STREAM OF HYDRAULIC FLUID COMING FROM DRAIN MAST AT PORT LABELED "PYLON". VISUAL INSPECTION OF PYLON "SAILBOAT" COMPARTMENT WAS FOUND TO BE DRY. PRESSURIZING LEFT SYSTEM WITH ELECTRIC PUMP RESULTS IN NO LEAK. LEAK ONLY OCCURS WITH ENGINE MOTORING AND ONLY FROM "PYLON" DRAIN. WHILE MOTORING #1 ENGINE REF AMM71-00-00-712-168-H03 FOUND HYDRAULIC LINE ITEM #270 OF IPC 29-11-51-21 LEAKING FROM SWAGE FITTING. HYDRAULIC LINE ITEM #270 OF IPC 29-11-51-21 HAS BEEN REMOVED. ADD EMP:U408206 REPLACED ITEMS 190 & 270 FROM IPC 29-11-51-21. LEAK CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. SERVICED HYDRAULICS AS REQUIRED.64-2911-3-0039,QTY :1 ADD EMP:U408206,U427832

Part: SKIN — DAMAGED (ZONE 100) · airframe 91,451 hrs · 12,921 cycles

IT WAS FOUND OLD SCRIBE LINE ON FUSELAGE SKIN RH SIDE AT STA 1165 TO 1175 BETWEEN STR19 TO STR20 AS PER SRM 53-00-00-0G-0. PERFORMED REWORK AS PER ECRA 5330-07323. ON IS AN INTERIM SOLUTION WITH INSPECTION REQUIREMENTS. ACCOMPLI EC/RA 5360-01910 ON OR BEFORE THE AC REACHES 30,000 TOTALFC FO 5,000 TOTAL FC FOR THE REMAINING SCRIBES OUTSIDE THE REPAIR. INSPECTIONS REQUIREMENTS PER PART 2 OF THE LATEST REVISION OF R THE REINFORCING REPAIR AND ON OR BEFORE THE AIRCRAFT REACHES 7 SCRIBE LINES IN THE RH FUSELAGE SKIN BTW STA 1065 AND STA 1153 A ND BTW S-19R AND S-20R WERE INSPECTED/REPAIRED AT GIG. DISPOSITI ACCOMPLISHED THE APPROVAL FOR QC. REF EC 5360-01910, ACCOMPLISH INSPECTIONS REQUIREMENTS PER PART TOMC-APPROVAL FROM SC1ELBYC COMMENT 2 OF EC/RA 5360-01910 ON OR BEFORE THE AIRCRAFT REACHES 30,000 TOTALFLIGHT CYCLES FOR THE REINFORCING REPAIR AND ON OR BEFORE THE AIRCRAFT REACHES 75,000 TOTAL FLIGHT CYCLES FOR THE REMAINING SCRIBES OUTSIDE THE REINFORCING REPAIR".

Part: LAMP — INOPERATIVE (SEAT 10A) · airframe 90,991 hrs · 12,859 cycles

CEILING EMERGENCY LIGHT LAMP AT 10A INOP. REPLACED CEILING OVERHEAD EMERGENCY LIGHT LAMP REF. AIPC 33-51-00-11 REV NO. / DATE : 111 / 22 AUG 2024. ITEM OK. GOOD FOR SERVICE.PARTS USED: 00-0596-3-2874,QTY :1

Part: SAFETY VALVE — MALFUNCTIONED (MLG) · airframe 89,421 hrs · 12,635 cycles

DEBRIEFED FLIGHT CREW, REPORTED THAT THEY FELT A DRAG ON AC AFTER STOWING GEARS, EITHER DOOR OR GEAR DOWN ON RIGHT SIDE. ACCOMPANIED BY GEAR DISAGREE AND GEAR DOOR EICAS STATUS MESSAGES. RIGHT GEAR INDICATOR HASHED OUT WHILE OTHER 2 BOXES WERE NORMAL. MLG DOORS WERE STOWED NORMALLY WHEN AC PULLED INTO GATE. PERFORMED BITE PROCEDURE FOR THE PSEU CODE 000 PRESENT, NO FAULT FOUND. ALL TARGET TEST PASSED. SEE PICS ATTACHED. REPLACED RH MLG DOOR SAFETY VALVE AND OPS CHECK NORMAL REF AMM 32-35-10.

Part: SAFETY VALVE — FAULTY (RT MLG) · airframe 89,396 hrs · 12,631 cycles

GEAR DOORS STATUS MSG WOTH GEAR DISAGREE PER CPT MSG APPEARED ON RETRACT. ON TAXI IN NOTICED RH MAIN GEAR DOOR DOWN. FLAGGED FOR IAD TO COMPLETE SDR. SUSPECT RESTRICTOR CHECK VALVE REF FIM 32-30 FAULT TREE 837 SHEET 3 BLOCK 7 INSTALLED HYDRAULIC TUBE MFG PN 272T4508-131. LEAK CHECK GOOD. CLAMPS STILL NEED TO BE INSTALLED. REF IPC 32-32-55-05 ITEM 340. VALVE, SAFETY, OFF 64-3235-9-9002 0006 ON 0000 VALVE, SAFETY, OFF 64-3235-9-9002 0006 ON 64-3235-9-9002 0070 REMOVED AND REPLACED THE RT MLG DOOR SAFETY VALVE & PERFORMED THE INSTALLATION TEST PER AMM 32-35-10. TEST IS GOOD.

Part: BOLT — MISSING (RT NACELLE) · airframe 88,796 hrs · 12,547 cycles

RH ENG PYLON HYDRAULIC BAY INBD ACCESS PANEL ONE BOLT MISSING FROM LATCH THIRD LATCH BACK HAS UPPER SCREW MISSING FROM LATCH QC 1 CYCLE BUT BEFORE 2 FLIGHT CYCLES PART 1 INTERIM REPAIR ACCOMPLISHED IAW EC/RA 5453-01262.PERMANENT REPAIR TO BE ACCOMPLISHED PER PART 3 AFTER APPROVED FOR ONE CYCLE DIP REF ECRA 5453-01262 TOMC-APPROVAL FROM SC1ELBYC COMMENT TOMCQC REV PERFORMED INSTALLED BOLT AND RETAINER AS PER ECRA 5453-01262. OK TO CONTINUE.

Part: SKID SHOE — PILOT ERROR (TAIL) · airframe 88,264 hrs · 12,480 cycles

POTENTIAL TAILSTRIKE TAIL SKID PAD PER AMM TASK 05-51-32-202-025, 05-51-32-202-052, 05-51-32-202-038. SHOE DAMAGE WITHIN LIMITS. YELLOW CRUSH INDICATORS NOT SHOWING. SHOE BOLT HEAD TO TIP GAP IS 1.2 INCH THICKNESS. INTERIOR STRUCTURE HAS NO DAMAGE FOUND. OPERARION OF HORIZONTAL STABILIZER GOOD NO BINDING. TAKE OFF WARNING CHECK FOR STABILIZER GOOD. REPAINTED TAIL SKID TIP BLUE. AIRCRAFT BACK IN SERVICE.

Part: PRESSURE SWITCH — FAULTED (LEFT ENG FUEL) · airframe 87,509 hrs · 12,379 cycles

LEFT ENG FUEL FILT EICAS S THE PRESSURE DIFFERENCE ACROSS LEFT ENGINE FUEL FILTER IS NEAR T HE BYPASS. REMOVED AND REPLACED ENG#1 FUEL FILTER IAW AMM 73-11-02. REMOVED AND REPLACED FUEL FILTER DIFFERENTIAL PRESSURE SWITCH IAW AMM 73-34-01. NO FAULTS ,OPS AND LEAK CHECK GOOD THIS TIME.

Part: SHUTOFF VALVE — DAMAGED (STA 243.18) · airframe 86,360 hrs · 12,217 cycles

AT 500FT ON TAKEOFF GOT R ENG BLEED AND R PACK OFF. RAN CKLST. DID NOT RESET. SEE LOGPAGES 5639053 AND 5644759 FOR RIGHT ENGINE HPSOV REPLACMENT AND SUBSIQUENT BLEED SYSTEM OPERATIONAL TEST. HPSOV REMOVED IAW AMM TASK 36-11-07-024-001-003 FOUND BROKEN HARDWARE. REMOVED PART DATA PLATE REMOVED PART DATA PLATE 2 HPSOV INSTALLED IAW AMM 36-11-07-424-014-003.STATIC LEAK PERFORMED WITH APP AND DRY MOTORING. SATIS. ENG REQUIRED CORRECTION FORM PREVIOUS UPDATE PLEASE READ ENG RUN REQUIRED. ADD PART CHANGING INFORMATION ROTABLE PARTS CHANGE WAS INDICATED - TT # 1928120 SN OFF 4091 VALVE, ASSY, HI OFF 64-3611-9-0014 4091 ON 0000 VALVE, ASSY, HI OFF 64-3611-9-0014 4091 ON 64-3611-9-0014 0150 HIGH POWER ENGINE RUN ACCOMPLISHED FOLLOWING RIGHT ENGINE HPSOV REPLACEMENT. AIR SYSTEM DISTRIBUTION SYSTEM, OPERATIONAL TEST ACCOMPLISHED AS PER AMM 36-11-00-715-029-001. TEST PASSED AND ALL RESULTS NORMAL.

Part: BULB — INOPERATIVE (SEAT 1A CEILING) · airframe 84,647 hrs · 11,968 cycles

SEAT 1A CEILING EMERGENCY LIGHT INOP, REFER TO N0109 REPLACED SEAT 1A CEILING EMERGENCY LIGHT BULB, THE TEST RESULT I S NORMAL AS PER AMM 33-51-05 R138, WORK ACCOMPLISHED BY V913662

Part: BULB — INOPERATIVE (G5 FWD L/H CEILI) · airframe 84,647 hrs · 11,968 cycles

THE G5 FWD L/H CEILING PANEL EMERGENCY LT INOP, REFER TO N0110 REPLACED THE G5 FWD L/H CEILING PANEL EMERGENCY LT BULB, THE TES T RESULT IS NORMAL AS PER AMM 33-51-05 R138.

Part: SKIN — CRACKED (STA. 1654) · airframe 84,647 hrs · 11,968 cycles

FUSELAGE EXTERNAL SKIN FOUND CRACK AT STA. 1654 5+5" S-13L T AS GIVEN IN TABLE 202/REPAIR 7, REQUIRE A RE-INSPECTION DVI AN RY OR WITHIN 7500 CYCLES FROM THE REPAIR INSTALLATION, WHICHEVER D LFEC INSPECTION ACCOMPLISHED AT 30000 FC AFTER AIRCRAFT DELIVE COMES FIRST WITH REPEAT INSPECTIONS SET AT 7500FC THEREAFTER. DURING 8C CHECK IN PVG, AREA REPAIRED REF. SRM 53-80-01-2R-7, TH IS IS A CATEGORY B REPAIR AND SUPPLEMENTAL INSPECTION REQUIREMEN PER SRM 53-80-01-2R-7: THIS IS A CATEGORY B REPAIR AND TOMC-APPROVAL FROM SC1ELBYC COMMENT SUPPLEMENTAL INSPECTION REQUIREMENT AS GIVEN IN TABLE 202/REPAIR 7, REQUIRE A RE-INSPECTION DVI AND LFEC INSPECTION ACCOMPLISHED AT 30000 FC AFTER AIRCRAFT DELIVERY OR WITHIN 7500 CYCLES FROM THE REPAIR INSTALLATION, WHICHEVER COMES FIRST WITH REPEAT INSPECTIONS SET AT 7500 CYCLES THEREAFER. QC RECORDS UPDATE....HC QC REVIEWED. RIR : 7500 FC (DVI & LFEC) (ONLY ONE M&E NEEDED AS LIMIT FOR INIT AND RIR ARE SAME)...HC/U3 89717....HC/U389717

Part: LIGHT — UNKNOWN (37D SEAT) · airframe 84,647 hrs · 11,968 cycles

SEAT 37D EMERGENCY LIGHT INOP, REFER TO BSH N0107 REPLACED THE 37D EMER LT ASSY AS PER AAMM 33-51-10 R138 INSTALLA TION TEST TRANSFER TO N0545, WORK ACCOMPLISHED V913662

Part: DOOR — WARNING LIGHT (L FWD DOOR) · airframe 83,702 hrs · 11,828 cycles

L FWD DOOR LIGHT ILLUMINATED ON T/O ROLL DEFERRED PER MEL 5271C . MAINT PROCEDURES COMPLIED WITH . DEFERRED PER MEL 5271C . MAINT PROCEDURES COMPLIED WITH. DOOR VERIFIED CLOSED . L FWD ENTRY DOOR INDICATION INOP F/A NOTED EMERGENCY LIGHTS FLICKERED. REF MEL 5271C AND TARGET TEST REQUIREMENT VIA PSEU. VERIFIED LEFT FWD MAIN CABIN DOOR IS LOCK AND ARMED PER MEL 5271C. OK TO CONTINUE. ISSUE. UPON EXTERIOR INSPECTION FOUND DOOR TO HAVE GAPPING ALONG INSPECTION REQ. INCLUDING IMAGE OF POSSIBLE SEATING ISSUE. REF TOP SIDE. DOOR IS POSSIBLY NOT RIGGED CORRECTLY. FURTHER AMM 52-11-00/501 DOOR 1L EICAS AND OVERHEAD DOOR INDICATION OPERATES NORMALLY. PERFORMED DOOR OPERATION FROM INSIDE AND DID NOT FIND INDICATION DOOR 1L WITHIN LIMITS AT THIS TIME REF AMM 52-11-00-825-008. PERFORMED FIM REF 52-71 FAULT TREE 806 , CLEANED SENSOR CLOSED AND OPENED DOOR SEVERAL TIMES ,INDICATIONS NORMAL AND BITE TEST NO ISSUE WITH TARGET NEAR OR FAR . MEL CLEARED AND PLACARD REMOVED .

Part: NONE — NONE (R PACK) · airframe 83,518 hrs · 11,799 cycles

R PACK MODE + R PACK OFF EICAS FL225 - MULTIPLE RECUR. AT CRUI SE R PACK TEMP ALSO. CKLIST DO TOUBLESHOOTING PER PILOTS R PACK TEMP CONTROL AND R SECONDARY HEAT EXCHANGE CREW REPORTED PACK OPERATED BELOW 16K ON ARRIVAL REF FIM 21-51 TASK 832, MULTIPLE FAULTS STORED ON RIGHT CABIN SENSOR STATUS MESSAGES DISPLAYED ABOVE 20K. R PACK TEMP MESSAGE TEMP CONTROL BOTH CHANNELS FOR FLIGHT LEG 0. 21-51237, DISPLAYED ON MAINT PAGES AFTER SHUTDOWN 21-51231 AND 21-51013. GROUND SYSTEM TEST PASSES ON BOTH CHANNELS AT THIS TIME. LEG 0 FAULTS REQUIRE FURTHER 375 AND 380. BOTH SENSORS P/N 810218-2, M&E 25-2152-3-0053 AND THROUGH END OF TASK REQUIRED FOR COMPLETION. REQUIRED FOR COMPLETION. WILL ALSO REQUIRE 2 EA PACKING P/N 69494J908 M&E 40-0596-3-5426 CTC FAULT TIME STAMPS SHOW THE FOLLOWING PROGRESSION FROM FIRST AS RECOMMENDED BY TROUBLE SHOOTING. REMOVED CHANNEL 1 SECONDARY AS RECOMMEND BY TROUBLE SHOOTING. REMOVED RIGHT PACK CHANNEL 2 REPLACED BYPASS VALVE M/E 64-2151-9-0005. M/E S/N 5082 NEEDS TO REPLACED R/H BYPASS VALVE PART ON M/E 64-2151-9-0005 S/N 5082 TO LAST -> 21-51237, 21-51231, 21-51013. RECOMMEND REPLACEMENT HEAT EXCHANGER OUTLET TEMPERATURE SENSOR REF AMM 21-51-44. CONDENSER INLET TEMPERATURE SENSOR REF AMM 21-51-45. INSTALLED BE OP CHECKED. REMOVED S/N 2016 TRACKING NUMBER 1089397. WAITING FOR DUCT OF TS551 FOR 21-51237 FAULT REF FIM 21-51 TASK 836 AND TS537 FOR INSTALLED CHANNEL 1 SECONDARY HEAT EXCHANGER OUTLET TEMPERATURE CHANNEL 2 CONDENSER INLET T

Part: COVER — MISSING (OTHER) · airframe 83,166 hrs · 11,739 cycles

EMERGENCY PATH LIGHTING COVERS MIISSING THROUGHOUT CABIN FOUND THE FOLLOWING SEATS LENS ASSEMBLIES DAMAGED:-3D, 7D, 16D, 18F, 19F, 21F, 24D, 29F, 31F, 42D, 44D EMERGENCY PATH LIGHTING COVERS REPLACED AT 3D, 7D, 16D, 18F, 19F, 21F, 24D, 29F, 31F, 42D AND 44D AND TESTED OK PER B767-400 AMM 33-51-00.

Part: NONE — NONE (ELEVATOR) · airframe 81,548 hrs · 11,494 cycles

ELEV FEEL EICAS AND STATUS MSG CAME ON AFTER TAKEOFF DEBRIS NOTED . DISCONNECTED PITOT AND STATIC LINES FROM ELEV FEEL COMPUTER AND FOUND HYD FLUID PRESENT ON STATIC SIDE OF FEEL COMPUTER. SUSPECT FEEL COMPUTER TO BE BAD. PERFORMED FIM TASK 27-31/806 AND AUX PITOT STATIC SYSTEM LEAK REMOVED ELEVATOR FEEL COMPUTER REF AMM TASK 27-31-19-024-001. PART REMOVED SEE PIC TEST PER AMM 34-11-00/501. NO LEAKS NOTED. PER FIM TASK OF AUX ADD EMP:U233291 STATIC DRAINS IN AFT ACCESS COMAPRTMENT AND THEY HAVE NO SIGNS OF FLUID. ALSO PERFORMED PITOT/ STATIC SYSTEM FLUSH WITH NO IDT REQUIREMENTS C/W FOR ELEVATOR FEEL COMPUTER INSTALLATION UP C/W IDT REQUIREMENTS FOR ELEVATOR FEEL COMPUTER INSTALL FOR STEP TO AND INCLUDING 3. H10 3(H)11 REF AMM 27-31-19-424-015 INSTALLED ELEVATOR FEEL COMPUTER REF AMM TAKS 27-31-19-424-015 VERIFIED ELEVATOR FEEL COMPUTER INSTALLATION REF AMM TAKS PERFORMED PITOT/STATIC LEAK CHECK OF ELEVATOR FEEL COMPUTER AS REMOVE ELEVATOR FEEL COMPUTER AS MM TASK 27-31-19-024-001 CONTINUED WITH THE REMOVAL OF THE ELEV FEEL COMPUTER REF MM PERFORMED LOW LEVEL LEAK CK OF AUX PITOT AND AUX STATIC LINES TO UP TO AND INCLUDING 3 -H STEP (10) 27-31-19-424-015 UP TO AND INCLUDING 3 -H STEP (10).IDT C/W. PER AMM 34-11-00, FOUND LEAK IN #2 AUX STATIC SYSTEM. ISOLATED PARAGRAPH 2 UPTO AND INCLUDING STEP E(5) NEED TO COMPLETE FROM 27-31-19-024-001 TO THE END. INSTALLED NEW ELEV FEEL COMPUTER ELEVATOR FEEL COMPUTER AS PER AMM 27-31-19-424-015 STEP 3(H) 11. ROTABLE PARTS CHANGE WAS

Part: MODULE — FAILED (E&E) · airframe 81,477 hrs · 11,485 cycles

LE SLAT AND TE FLAP DISAGREE BWN F20 AND 25 DID GO AROUND AND DI D QRH LOCKED TO CONFIRM FIX UNLOCKED TO UPDATE LOG PAGE LOCKED FOR FIX CREW DEBRIEF - CREW STATED FLAP HANDLE SELECTED TO 25 AND FLAPS UPON ARRIVAL FOUND FLAPS STUCK AT 22 AND FLAP HANDLE BINDING STOPPED AT 22 WITH LE SLAT DISAGREE AND TE FLAP DISAGREE JUST AFT OF THE FLAPS 20 DETENT. NEEDS FURTHER T/S. MESSAGES, THEN POSITIONED FLAP HANDLE TO 20 PER QRH, FLAPS REMAINED AT 22. UNLOCKED, ITEM TO BE UPDATED FOUND MX MSG NUMBERS 27-81043, 27-81044, 27-81045 IN LAST LEG ALTERNATELY NO FAULTS FOUND & RVDT VOLTAGE WITHIN RANGE REF AMM FAULT HISTORY, REF FIM 27-81-00/101, FIG.106. ACCOMPLISHED PSEU 27-51-26-424-020. AS PER NOTE(1) IN FIM R/R FLOW REGULATOR FOR BITE TARGET PROCEDURE FOR ALL FLAP SLAT SENSORS, TARGETS FLAP/SLAT SHUTOFF VALVE MODULE REF AMM 27-51-48/201 OPS CHECK INDICATE NORMAL. RAN THE FLAPS/SLATS THROUGH FULL TRAVEL HYD & GOOD. ADD EMP:U345750 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1088171 SN OFF 0848 MODULE, FLAP & OFF 64-2751-9-0029 0848 ON 64-2751-9-0029 1879

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,909 hrs · 11,084 cycles

SUPPORT TASK - EA 5380-01178 REV A OP004, CRACKS FOUND AT STR 13AR BETWEEN STA 1660 AND 1665 APPROX 4.5" IN LENGTH. DETAIL REFER ATTACHED FIGURE REFER NR LP 9130664 (VENDOR) FX STA 1654 - 1668 STR 13AR SKIN REPAIRED AS PER SRM 53-80-01 REPAIR T DETAIL IV FIG 201. ATTACH MAINTENANCE WORK SHEET FORM 44-0008 ITEM 1 TO ITEM 26 ACCOMPLISHED. REPECT INSPECTION PER SRM 53-80-01 REPAIR T TABLE 202 AND FIG 204 DETAIL XI. ADD EMP:V897529 THE SIZE OF DOUBLE: 8" X 13" AND THICKNESS 0.063" WEIGHT 0.48 LBS. CAT B REPAIR DONE; REQUIRES REPEAT INSPECTION PER SRM 53-80-01 TABLE 202 AT INITIAL 30,000 C AND INTERVAL 7,500 C THEREAFTER. CURENT PTT 78909 & PTC 11084 CAT B REPAIR DONE; REQUIRES REPEAT INSPECTION PER SRM 53-80-01 TABLE 202 AT INITIAL 30,000 C AND INTERVAL 7,500 C THEREAFTER. CURENT PTT 78909 & PTC 11084. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 75,023 hrs · 10,526 cycles

C HYD QTY C HYD SYS PRESS CONTACT TOMC WITH FINDINGS PRIOR TO CLEARING LOG ITEM. UNLOCKED DUE TO POSITIVE FIX. REF L/P 9260836 & L/P 9263730, FOUND ADP PUMP LEAKS. RPL''D & FLU SHED SYS. CONCURRED WITH TOMC.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 74,992 hrs · 10,522 cycles

REF L/P 9258197. FOUND ADP LEAKING FLUID FROM THE MIDDLE MATING FLANGE. REMOVED AND REPLACED ADP UP TO AND INCLUDING STEP F(2)(J) IAW 767-4 AMM 29-11-03-424-021-004. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1219065 SN OFF 5323 PUMP, HYD ENG D OFF 25-2910-9-0001 5323 ON 25-2910-9-0001 8319 TASK 29-11-03-424-021-004 INSTALL THE ADP FOR THE CENTER HYDRAULIC SYSTEM WAS COMPLETED TO FINISH. OPS AND LEAK CHECK GOOD.

Part: SHAFT — SHEARED (HYDRAULIC PUMP) · airframe 74,573 hrs · 10,465 cycles

EICAS MSG R ENG PRIM PUMP ILLUMINATED PER CREW DE-BRIEF PUMP WAS TURNED OFF IMMEDIATELY AFTER EICAS MESSAGE 29-11-05. MUST PERFORM OPS AND LEAK CHECKS. ENGINE 2 HYDRAULIC PUMP SHAFT SHEERED. R&R PUMP PER AMM IPC REFERENCE 29-11-05 ROTABLE PARTS CHANGE WAS INDICATED - TT 1206943 SN OFF 2983 REPLACEMENT AGAIN. R&R RIGHT HAND CASE DRAIN AND PRESSURE FILTERS IAW AMM REQUIRES SYSTEM FLUSH REF AMM 29-11-00-172-113 AND FILTER 29-11-17-004-001 STEP G 1 - 5. FOUND DEBRIS IN CASE DRAIN FILTER. PERFORMED HYD FLUID FLUSHING, CHANGED ALL THE 3 FILTERS, CASE DRAIN FILTER, PRESSURE FILTER, FILTER ELEMENT RETURN, OPS CHECK EDP AND FILTERS FOR LEAK NO ABNORMAL NOTED, ALL WORK DONE PER AMM 29-11-00-172-113. OK TO CONT.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 70,064 hrs · 9,848 cycles

EMERGENCY LIGHT LENS DETACHED BY THE L3 DOOR. ATTACHED THE LENS. OK TO CONTINUE

Part: PCA — LEAKING (RT ELEVATOR) · airframe 69,320 hrs · 9,724 cycles

C HYD QTY EICAS ENROUTE. EMERGENCY DECLARED. INSPECTED AND FOUND HYD. LEAK AT RT ELEVATOR INBD PCA. LEAK COMING FROM PISTON ACTUATOR HOUSING. REMOVED AND REPLACED RIGHT ELEVATOR INBD PCA IAW AMM 27-31-05. ALL OPS CHECK AND LEAK CHECKED GOOD.

Part: LAMP — INOPERATIVE (OVERHEAD PANEL) · airframe 68,742 hrs · 9,645 cycles

LIGHT BULB BURNED OUT AT EMERGENCY EXITS, UNARMED LIGHT ON OVERHEAD PANEL REPLACED THE LAMPS, CHECKED OK

Part: TUBE — BROKEN (NR 1 ENGINE) · airframe 68,615 hrs · 9,621 cycles

DURING TAKEOFF POWER UP, THE LEFT ENGINE N1 FAILED TO REACH TAKEOFF THRUST, ONLY REACHED 89 PERCENT. FOUND BROKEN PS3 LINE. R & R THE LINE IAW AMM 73-21-24-206-001-H00. HIGH POWER RUN SATISFACTORY. AIRCRAFT OK FOR SERVICE.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 67,155 hrs · 9,416 cycles

CORROSION FOUND ON PRESSURE DECK CLOSURE PANEL BETWEEN STA 955-9 66 AND LBL 85.9-97.42. CORROSION WAS FOUND BEYOND SRM LIMITS. REPAIR WAS ACCOMPLISHED IAW ECRA 5310-07124. REPEAT INSPECTION REQUIRED IAW ECRA 5310-07 124 PART 1 STEP 2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,155 hrs · 9,416 cycles

STA 303, LBL 24-53 FLOORBEAM FOUND CORROSION. CABIN STA 303, LBL 24-53 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201.

Part: SIGN — DIM (EMERGENCY LIGHT) · airframe 67,155 hrs · 9,416 cycles

FLIGHT DECK DOOR OVERHEAD PORTABLE EMERGENCY EXIT SIGN FOUND DIM. FLIGHT DECK DOOR OVERHEAD PORTABLE EMERGENCY EXIT SIGN ASSY REPLACED AND TEST CARRIED OUT NORMAL IAW AMM 33-51-01.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 66,814 hrs · 9,368 cycles

DOOR 3R EMER FLASHLIGHT INOP. REPLACED BATT AND SEAL. OPS CKS GOOD

Part: BLADE — DAMAGED (RT ENGINE) · airframe 61,104 hrs · 8,564 cycles

RIGHT ENG VIB FAN EXCEEDED 4.2, SUSPECTED BIRD STRIKE. ENG OPERATED WITHIN NORMAL PARAMETERS AT REDUCED POWER DURING DIVERSION. REMOVED 3 DAMAGED FAN BLADES 23, 24 & 25. REPLACED IN PAIRS WITH BLADES 4, 5 & 6. PERFORMED VIBE SURREY ON NR 2 ENG, MAX VIBE IS 0.5 UNITS, PERFORMED IAW AMM 72-31-02.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 47,608 hrs · 6,788 cycles

SEAT 19KL, CEILING EMERGENCY LIGHT WAS FOUND NOT ILLUMINATED. SEAT 19KL CEILING EMERGENCY LIGHT LAMP REPLACED AND TESTED NORMAL IAW AMM33-51-05.

Part: FLOORBEAM — CORRODED (BS 303) · airframe 47,608 hrs · 6,788 cycles

CABIN BS 303, LBL 20 TO 25 FLOORBEAM SPLICE CORRODED. CABIN BS 303, LBL 20 TO LBL 62 FLOORBEAM UPPER FLANGE REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 101 AND HFEC NIL CRACK FOUND.

Part: FLOORBEAM — CORRODED (BS 325) · airframe 47,608 hrs · 6,788 cycles

CABIN BS 325, RBL 21 TO 31 FLOORBEAM CORRODED. CABIN BS 325 LBL 62 TO RBL 56 FLOORBEAM UPPER FLANGE REPAIRED IAW SRM53-00-51, REPAIR 1, FIG 201, HFEC NO CRACK FOUND.

Part: FLOOR SUPPORT — CORRODED (BS 325) · airframe 47,608 hrs · 6,788 cycles

CABIN BS325, LBL 36 LONGITUDINAL FLOOR SUPPORT FWD END CORRODED. CABIN BS 325, 347, LBL 36 LONGITUDINAL FLOOR SUPPORT REPLACED IAW SRM 51-10-02 AND FASTENER INSTALLED IAW SRM 51-40-02.

Part: BATTERY PACK — FAILED (CABIN) · airframe 36,887 hrs · 5,447 cycles

DURING TEST OF EMERGENCY LIGHT BATTERY PACK REPLACEMENT, W/C 64-3350-1-3800 STEP 1B FOUND BATTERY AT RT STA 401 WL 204 RBL 95 FAILED TEST. REMOVED AND REPLACED BATTERY POWER SUPPLY ASSY PER AMM 33-51-0 7 STEP 5. P/N OFF D717-02-030 S/N OFF 6448 AND P/N ON D717-02- 030 S/N ON 5254. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — FAILED (CABIN) · airframe 36,887 hrs · 5,447 cycles

DURING TEST OF EMERG. LIGHT BATTERY PACK REPLACEMENT W/C 64-335 0-1-3800 STEP 1B FOUND BATTERY AT LT STA 841 WL 204 RBL 95 FAILED TEST. REMOVED AND REPLACED BATTERY POWER SUPPLY ASSY. PER AMM 33-51-0 7 STEP 5. P/N OFF D717-02-030 S/N OFF 16301 AND P/N ON D717-02- 030 S/N ON NONE. OPERATIONAL CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,554 hrs · 5,408 cycles

LEFT EMERGENCY EXTERNAL LIGHT BY AT L4 DOOR IS INOPERATIVE. REMOVED AND REPLACED LAMP AND LAMP HOLDER OPS CHECK GOOD, IAW AMM 33-51-06.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 32,195 hrs · 4,827 cycles

AFT EMERGENCY LIGHTS FROM ROW 39 BACK ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND CHARGER, RESEATED CONNECTOR TO AFFECTED AREA, OPS CHECK NORMAL.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 23,036 hrs · 3,572 cycles

LIGHT ASSY CONNECTOR DISCONNECTED. EMERGENCY LIGHT INOP AT 18D. RECONNECTED AND PER MM 33-51-10.

Part: ATTACH FITTING — CRACKED (NR 1 NACELLE) · airframe 22,279 hrs · 3,464 cycles

INSPECTION FOUND A 1 INCH CRACK IN NR 1 PYLON INTERNAL STRUCTURE O/B CLIP AT STA 285.4. THE CLIP WAS REPLACED IAW SRM 51-10-02, PAGE 8 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 303-325) · airframe 22,279 hrs · 3,464 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 303-325, LBL 31. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02.

Part: ATTACH FITTING — CRACKED (NR 1 NACELLE) · airframe 22,279 hrs · 3,464 cycles

INSPECTION FOUND NR 1 PYLON STA 285.4 O/B MID SPAR FITTING ATTACHMENT AREA MOST FORWARD I/B HOLE UPPER CLIP CRACKED (1 INCH LONG). THE CLIP WAS REPLACED IAW SRM 51-10-02.

Part: FLOORBEAM — CORRODED (BS 325) · airframe 22,279 hrs · 3,464 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT BS 325, LBL 31 TO LBL 55. THE CORRODED SECTION OF FLOORBEAM WAS REPLACED IAW SRM 53-00-51, FIGURE 201, REPAIR 1.

Part: FLOORBEAM — CORRODED (BS 303) · airframe 22,279 hrs · 3,464 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT BS 303, LBL 28 TO LBL 40. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 1.

Part: CHARGER — INOPERATIVE (BS 654) · airframe 17,867 hrs · 2,842 cycles

THE EMERGENCY LIGHTS AT STA 654+33, WL 204, LBL 85 FAILED TEST. THE CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-07.

Part: CHARGER — INOPERATIVE (BS 1197) · airframe 17,867 hrs · 2,842 cycles

THE EMERGENCY LIGHTS FAILED TEST AT STA 1197+77, WL 204, RBL 95. THE BATTERY CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-07.

Part: ELECTRICAL BOX — FAILED (SEAT 5AB) · airframe 11,172 hrs · 1,808 cycles

FLT CREW REPORTED PROBLEMS WITH READING LIGHTS AT ROWS 1-6AB. PROBLEMS WITH INFLT ENTERTAINMENT SYS AND READING LIGHTS AT SEAT 5AB WHILE ENROUTE. SMOKE ODOR NOTICED WHILE FLT CREW ATTEMPTED TO RESET IFE SYS. SYS TURNED OFF AND SMOKE ODOR DISSIPATED. SYS LEFT OFF FOR REMAINDER OF FLT. AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE FOUND SEAT 5AB DIGITAL SEAT ELECTRONICS BOX(DSEB) FAN NOT WORKING. DSEB WAS PULLED OFF. UNIT AND WIRING WAS INSPECTED AND A LOT OF LINT OR DUST WAS FOUND CLOGGING FAN. IT IS SUSPECTED THAT LINT/DUST CAUSED THE FAN TO FAIL AND IN TURN CAUSED THE BOX TO OVERHEAT. THE DSEB AT SEAT 5AB WAS REMOVED AND REPLACED. OPERATIONAL CHECKS WERE NORMAL.

Part: SLIDE — DEPLOYED (R-4 DOOR) · airframe 10,528 hrs · 1,707 cycles

THE R-4 DOOR ESCAPE SLIDE WAS INADVERTENTLY DEPLOYED BY CATERING WHILE AT AMS. THE SLIDE DEPLOYED TO THE GROUND, BUT DID NOT INFLATE. THE SLIDE WAS REMOVED AND REPLACED IAW MM 25-66-01-404-036. INVESTIGATION BY ENGINEERING CONCLUDED THAT WHEN THE SLIDE DEPLOYED IT STRUCK A CATERING VEHICLE RESULTING IN A 38 INCH TEAR IN THE SLIDE WHICH PREVENTED IT FROM INFLATING.