N57869

Part: UNKNOWN — ODOR (CAIBN) · airframe 64,559 hrs · 19,539 cycles

FAS SMELLED INT SMELL OF SMOKE FIRST NEAR ROW 25/26 THEN THE FWD GALLEY PERFORMED VISUAL INSP OF AREA AROUND ROW 25/26 AND FWD GALLEY NO OBVIOUS DEFECTS NOTED , ACCOMPLISHED ENG IDLE RUNS WITH PACKS ON NO SMOKE SMELLS NOTED REF. AMM TASK 21-00-01-002-001. UNABLE TO DUPLICATE.

Part: TRANSMISSION — TRIPPED (TE FLAPS) · airframe 64,274 hrs · 19,455 cycles

TE FLAP DISAGREE ON APPROACH. FLAPS STUCK BETWEEN 15/20. RAN QRH. WHEN FLAPS WERE SET TO 20, FLAPS STOPPED MOVING HYDRAULICALLY BETWEEN 15 & 20 DEGREES & HAD A TE DISAGREE MESSAGE. FLAPS HAD TO BE MOVED TO 20 IN ALT MODE FOR LANDING IAW QRH. REF FIM 27-51 TASK 808. PERFORMED FSEU BITE PROCEDURE, FOUND MSG 305 ON FSEU 1 & MSG 327 ON FSEU 2 INSPECTED TE FLAP OVER TORQUE INDICATORS ON ALL FLAP TRANSMISSIONS IAW FIM 27-51 FAULT TREE 808. FOUND OVER TORQUE INDICATORS TRIPPED ON LT & RT OTBD FLAP, OTBD TRANSMISSIONS. THESE INDICATORS WERE ALSO FOUND TRIPPED ON AUG 02 AT SFO FOR SAME WRITE UP. ACFT HAS HISTORY FOR FLAP ISSUES. REMOVED LT WING TRANSMISSION FOR OTBD TE FLAP IAW AMM 27-51-17-024-001. LT SIDE X DIMENSION IS 11 7/8", ACCOMPD RII REQUIREMENTS FOR PREINSTALL IAW GMM 09-25-05. INSTALLED LT FLAP NR 1 XMISSION. PERFORMED BITE TEST OF FSEU 1 & 2 IAW FIM 27-51 TASK 808 BITE TEST GOOD, NO EXISTING FAULTS NOTED.

Part: SLIDE — NO DISCREPANCY (ZONE 800) · airframe 64,240 hrs · 19,443 cycles

INSTALLED 1EA SAFETY PINS AT DOOR L1 IN EACH DOOR ASSIT BOTTLE AND DOOR SLIDE ASSY. FOR REPLACEMENT OF SLIDE ASSY REMOVED AND STOWED 1EA SAFETY PINS AT DOOR L1 IN EACH DOOR ASSIT BOTTLE AND DOOR SLIDE AFTER COMPLETION OF DOOR SLIDE REPLACEMENT. REF AMM TASK 25-66-01-404-044 VERIFIED DOOR SLIDE INFLATION CYLINDER AND RESERVOIR BOTTLE SAFETY PINS REMOVED.

Part: FSEU — FAULTED (ZONE 100) · airframe 63,723 hrs · 19,291 cycles

EMERGENCY DECLARED DUE TO FLAPS STUCK AT 25. REPLACED FSEU #1 IAW AMM 27-51-01-422-011. OP CHECK GOOD IAW AMM 27-51-01-422-005.

Part: MODULATING VALVE — FAULTED (ZONE 100) · airframe 63,272 hrs · 19,156 cycles

COCKPIT TEMP TOO HOT AND TEMPO UNCOTROLLED AFTER QRH TEMP EVENTU ALY BEGAN TO COME DOWN PER PILOTS-ON THE TAKEOFF ROLL COCKIT VENT OUTLETS POURED OUT AIR THAT WAS EXTREMELY HOT. IN THE CLIMB TEMPS CONTINUED LET OUT HOT AIR. EVENTUALLY AFTER RUNNING QRH TEMPS STARTED TO RETURNTO NORMALL, WITH CONTROLLERS IN THESBY-C POSITION. FOLLOWED FIM 21-60 FAULT TREE 809 AND COCKPIT VALVE NOT FULLY RESPONDING, SUSPECT VALVE NEEDS REPLACED PER FIM. REMOVED AND REPLACED FLT DECK TRIM AIR VALVE IAW 21-61-07-404-031 UP TO BUT NOT INCLUDING STEP F (12) OPERATIO AND LEAK CHECKS , PERFORMED CLEANING OF FLT DECK TEMP CONTROL SENSOR PER SERVICE TIP 21-61-00/201. COMPLETED INSTALLATION OF FLIGHT DECK TRIM AIR MODULATING VALVE REF AMM 21-61-07. OPS CHECK LEAK CHECK GOOD. REF FIM 21-60 FAULT TREE 809. BITE TEST GOOD. NO FAULT NOTED.

Part: BOTTLE — FAULTED (AFT CARGO) · airframe 62,673 hrs · 18,978 cycles

EMER ESCAPE SQUIB TEST 2 L DOES NOT ILLUMINATE REF FIM 25-65 FAULT TREE 803REF FIM 25-65 FAULT TREE 803 BLOCK 13 REMOVED CONNECTOR D5530 FROM PRESSURE SWITCH S10463. REMIVED HEAVY CORROSION FROM SWITCH AND FOUND SWITCH FAULTY PER BLOCK 15. PROVIDED A GROUND AT PIN C OF CONNECTOR AND TEST LIGHT ILLUMINATES VERIFYING THE WIRING STILL OK. REQUIRES BOTTLE REPLACEMENT. P/N 416N2220-32. PART NIS HNL. SQUIB TEST 1 OPERATES NORMALLY. CONFIRMED THE PRESSURE INDICATION ON THE ASSOCIATED PRESSURE GAUGE SHOWS THE BOTTLE IS CHARGED. INSTALLED INOP STICKER AND OPS PLACARD. REQUEST MEL OK TO DEFER EMERGENCY SQUIB TEST 2 LEFT PER MEL C/W MEL BOTTLE SIDE OF CONNECTOR D5530 IS SPINNING IN HOUSING. AFT CARGO FWD PANELS TO VERIFY CONNECTOR ON BOTTLE PRESSURE SWITCH IS DAMAGED. CORRECT POSITION FOR BOTTLE INSTALLATION IS LEFT OVERWING POSITION. CORRECT POSITION FOR BOTTLE INSTALLATION IS LEFT OVERWING POSITION.. VERIFIED CORRECT POS IS LEFT OVERWING. PREVIOUS TO FOUND BENT PINS ON D5530 RECEPTACLE OF S10463 L SLIDE INFLATION BOTTLE PRESS SW. STRAIGHTENED OUT PINS AND PERFORMED OPS CHECK OF ELECTRICAL SYSTEM SQUIB AND PRESSURE SWITCH IAW AMM 25-65-00. OPS CHECK GOOD. MEL CLEARED AND PLACARD REMOVED.

Part: TACHOMETER — FAULTED (NR 2 N1) · airframe 62,595 hrs · 18,951 cycles

N1 OVERSPEED INDICATION NUMBER 2 ENGINE N1 OVERSPEED BEGAN DURING CLIMB AT 15,000FT . DURING APPROACH BACK EPR WENT BLANK. PILOTS REDUCED THROTTLE TO MATCH N1. AT DECENT ALL PERIMETERS WERE WITHIN LIMITS.

Part: GOVERNOR — FAULTY (NR 2 ENGINE) · airframe 61,778 hrs · 18,656 cycles

RT ENG REDUCED PWR EPR LIMITED TO 1.44 CREW REPORTS FUEL FLOW INDICATION LOWER ON RH ENGINE REMOVED AND REPLACED #2 ENGINE FUEL FLOW GOVERNOR IAW AMM 73-21-01. ALL ASSOCIATED TESTS PASSED AND LEAK CHECKS GOOD. POWER ASSURANCE AND EPR TESTS GOOD AS WELL. #1 AND #2 ENGINES MATCH AND RISE EVENLY. AC OK FOR SERVICE PARTS USED: 1308662,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1308662 SN OFF 4620 GOVERNOR, FUEL OFF 53-7321-9-0001 4620 ON 53-7321-9-0001 7417 VERIFIED ACCOMPLISHMENT INSTALLATION ENGINE #2 FUEL FLOW GOVERNOR REF AMM.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 61,618 hrs · 18,605 cycles

SEATS (AB) 1-2-3 EMERGENCY LIGHT INOP. REPAIR AS REQUIRE. REMOVE AND REPLACED POS M731 BATTERY PACK IAW B757 AMM 33-51-07- 902-005-002 OPS CHECK GOOD.

Part: CHANNEL — CRACKED (ZONE 600) · airframe 61,618 hrs · 18,605 cycles

B757-06-3-0239 - CRACK ON SEAL RETAINER STRUCTURE FWD FRAME CUT OUT OF RH W/W. REMOVED SEAL AND RETAINER, AND REPLACED RETAINER, BRACET AND SEA L IAW B757 SRM 51-40-02 AND B757 AMM 20-10-23-424-010.

Part: CHANNEL — CRACKED (ZONE 100) · airframe 61,618 hrs · 18,605 cycles

LH WHEEL WELL FWD CUT-OUT SEAL RE TAINER OUTB AREA NEXT TO PROX SENSOR WITH CRACK. REMOVED SEAL SUPPORT CHANNEL AND REPLACED SUPPORT CHANNEL AND SE AL IAW B757 SRM 51-40-02 AND 20-10-23-424-010.

Part: ANGLE — CRACKED (ZONE 100) · airframe 61,618 hrs · 18,605 cycles

B757-06-3-0237 - LH WHEEL WELL AREA PANEL 197BL INTERNAL AFT FRAME INB BRACKET AND OUTB BRACKET (2EA) WITH CRACK.

Part: FLAP TRACK — CORRODED (ZONE 500) · airframe 61,618 hrs · 18,605 cycles

B757-06-3-0302 - LH WING INB MAIN FLAP L/E NOSE SKIN INB AREA TR UNNION FAIRING WITH SEVERAL CORROSION SPOTS. REPAIRED THE L/H I/B MAIN FLAP IAW B757 SRM 57-53-01-2R-2, ACCOM PLISHED REPAIR PARTS 2EA DOUBLER, 2EA STRAPS AND 1EA REPAIR PLAT E IAW B757-300 SRM 57-53-01-2R-2, REPAIR 2.

Part: DECK PLATE — DENTED (ZONE 200) · airframe 61,618 hrs · 18,605 cycles

B757-06-3-0254 - FLT COMPT FLOOR HAS LARGE DENT AFT CENTER AREA.

Part: ANGLE — CORRODED (LH WING) · airframe 61,618 hrs · 18,605 cycles

B757-57-3-0420 - LH WING INB FLAP L/E SKIN NEXT TO AFT TRUNNION FAIRING AREA WITH SEVERAL CORROSION SPOTS AND CHAFING MARKS.

Part: ANGLE — CRACKED (ZONE 600) · airframe 61,618 hrs · 18,605 cycles

B757-06-3-0239 - CRACK ON ANGLE FWD FRAME O/B SIDE OF CUT OUT OF RH W/W. RENOVED AND REINSTALL WTB PANELS 198BR, 198CR, AND 198DR IAW B75 7-300 AMM 53-36-02, REMOVED AND REPLACED SUPPORT CHANNEL BRACKET IAW B757-300 SRM 51-40-02 AND BOEING DWG 149N7550, RESTORED SUR FACE PROTECTION IAW B757-300 AMM 51-21-04-51-21-14 AND 51-21-15.

Part: BULKHEAD — DENTED (ZONE 100) · airframe 61,618 hrs · 18,605 cycles

LOG #8798906 DURING OPENING SIDEWALL ACCESS PANEL LEFT SIDE AFT CARGO PIT, FOUND (01EA) DENT AT FR 1400 STRG 26L.

Part: SKIN — CRACKED (ZONE 400) · airframe 61,618 hrs · 18,605 cycles

PYLON #1 SKIN AT NACELLE L/E GAP PANEL INB LOWER CORNER NEXT TO WS260 WITH CRACK. REPAIRED PANEL IN LOWER CORNER NEXT TO WS 260 IAW B757-300 SRM 5 7-41-01-2R-3. REMOVED AND REINSTALLED THE GAP PANEL IAW B757 SRM 51-40-02-0G. OPERATIONAL TEST - DUCT LEAK DETECTION IS GOOD IAW B757-300 AMM 26-18-00-715-001.

Part: PANEL — DAMAGED (ZONE 100) · airframe 61,618 hrs · 18,605 cycles

AFT CARGO COMPT, SIDE PANEL, L/H ST STA 1377 D AMAGED. REF: NR #108629. REMOVED AND REINSTALLED SIDEWALL PANEL 153FW AND FLOOR PANEL 153 REF: F. BF IAW B757-300 AMM 25-50-04-004-001;REMOVED,FABRICATED,AND INST ALLED SIDE PANEL P/N 55-60-53-01-1 IAW B757-300 SRM 53-60-53, SR M 51-40-02-0G STEP 4,5 AND 8.AWD PRODUCTION DRAWING #146N5391

Part: TRANSMISSION — FAULTED (TE FLAP) · airframe 61,379 hrs · 18,537 cycles

TE FLAP DISSAGREE INDICATED F25 WITH HANDL E IN F30. EMERGENCY LANDING CREW STATED SOME TIME AFTER TOUCHDOWN AND ARRIVING TO THE GATE FLAPS WENT DOWN TO 30 AND MESSAGE WENT AWAY. FOUND LEFT WING OUTBOARD FLAP OUTBOARD TRANSMISSION OVERLOAD INDICATOR TRIPPED. ALL OTHER TRANSMISSION FLUID AND TRIP INDICATORS ARE GOOD. RESET TRIPPED TRANSMISSION AS REQUIRED. REF FIM 27-51 FAULT TREE 808. VERIFIED INSTALLATION OF TEE GEARBOX IN REF. TO AMM 27-51-18-424-019 UP TP STEP F ( 11 ) ( C ). REMOVED TEE GEARBOX FOR LEFT OUTBOARD FLAP PER AMM PERFORMED INSTALLATION OF TEE GEARBOX FOR LEFT OUTBOARD TE FLAP FILE NUMBER ADDED FOR GEAR BOX INSTALLATION. PARTS DATA INPUTED 27-51-18-024-001. READY FOR INSTALLATION. UP TO STEP F(11)(C) OF OPERATIONAL TEST. STEP F(12) OF OPS TEST. REF AMM 27-51-18-424-019. CONTINUED FROM AMM 27-51-18-424-019, STEP F(12), OPS CHECK GOOD. NO FAULTS OR MESSAGES AT THIS TIME.

Part: GEARBOX — FAILED (TE FLAP SYS) · airframe 61,411 hrs · 18,548 cycles

TE FLAP DISSAGREE INDICATED F25 WITH HANDL E IN F30 POSS SDR FLAGGED FOR EMERGENCY LANDING CREW STATED SOME TIME AFTER TOUCHDOWN AND ARRIVING TO THE GATE FLAPS WENT DOWN TO 30 AND MESSAGE WENT AWAY. FOUND LEFT WING OUTBOARD FLAP OUTBOARD TRANSMISSION OVERLOAD INDICATOR TRIPPED. ALL OTHER TRANSMISSION FLUID AND TRIP INDICATORS ARE GOOD. RESET TRIPPED TRANSMISSION AS REQUIRED. REF FIM 27-51 FAULT TREE 808. REMOVED TEE GEARBOX FOR LEFT OUTBOARD FLAP PER AMM 27-51-18-024-001. READY FOR INSTALLATION. PERFORMED INSTALLATION OF TEE GEARBOX FOR LEFT OUTBOARD TE FLAP UP TO STEP F(11)(C) OF OPERATIONAL TEST. PLEASE CONTINUE FROM STEP F(12) OF OPERATIONAL TEST. REF AMM 27-51-18-424-019 PARTS USED: 1089205,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1089205 SN OFF 0869 GEARBOX, FLAP, OFF 19-2751-9-0023 0869 ON 19-2751-9-0023 0579 VERIFIED INSTALLATION OF TEE GEARBOX IN REF. TO AMM 27-51-18-424-019 UP TP STEP F ( 11 ) ( C ). QC237669. FILE NUMBER ADDED FOR GEAR BOX INSTALLATION. PARTS DATA INPUTED ON PREVIOUS ENTRY. CONTINUED FROM AMM 27-51-18-424-019, STEP F(12), OPS CHECK GOOD. NO FAULTS OR MESSAGES AT THIS TIME.

Part: INDICATOR — FAULTY (TE FLAPS) · airframe 61,339 hrs · 18,524 cycles

TE FLAP DISAGREE MSG FLAPS STUCK AT 25. FAEU #1 AND #2 EXISTING FAULTS BITE SHOWS NO FAULTS. FAULT HISTORY IN FSEU #1 SHOWED FLAPS DISAGREE FOR LAST LEG, FSEU #2 SHOWS NO FAULTS. REFERENCE 8496015, REPLACE PANEL INSTL-CAPT AND FIRST OFFICER AND P3-1 (TRAILING EDGE FLAP POSITION INDICATING SYSTEM ONLY) REFERENCE: 27-58-00-02 INDICATOR P# 215-016-001 INDICATOR, POSI OFF 75-2754-9-0001 1381 ON 0000 INDICATOR, POSI OFF 75-2754-9-0001 1381 ON 75-2754-9-0001 1544 REPACED FLAP POSITION INDICATOR GAUGE, OPS CHECKS GOOD WHEN LOWERING AND RAISING FLAPS. REF AMM TASK 27-58-02-404-015. PARTS USED: 75-2754-9-0001,QTY :1 PARTS USED: 75-2754-9-0001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1731509 SN OFF 1381. OPS OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT GENERATOR) · airframe 60,280 hrs · 18,230 cycles

RT GEN CONT ON OVRHD AND RT GEN OFF EICAS AND ASSOCIATED MSGS. SVC IDG PER AMM 12-13-03 RESET BPCU PER FIM 24-20 RAN #2 ENG NO FAULTS RETURNED

Part: ENGINE — DAMAGED (NR 2) · airframe 60,235 hrs · 18,220 cycles

DUE TO #2 ENGINE IFSD ACCOMPLISH INSPECTION PER AMM 71-00-00-206-015-R00. LOUD BANG AND JOLT COMING FROM NUMBER 2 ENGINE , THEN ALL OILS INDICATING WENT TO 0. AT THAT POINT CREW SHUTDOWN ENGINE. SEE PHOTOS FROM CAPTAIN. PER FLIGHT CREW DURNG CRUISE ALTITUDE 33,000 , OILS PRESSURE UPDATED WITH IMAGES, FOUND METAL DEBRIS AT 0600 POSITION OF CORE WITH FURTHER INSPECTION, FOUND RADIAL DRIVESHAFT PARTS AND INDICATION CAME ON. FLIGHT CREW CHECKED EICAS PAGE OILS COWL AND RUPTURES TO THE 0600 STRUT. RUPTURED 6:00 STRUT FAIRING. PRESSURE SHOWING 0 AND OILS QUANTITY SHOWING 0 , TEMP WAS NORMAL COMPARING TO NUMBER 1 ENGINE. WHILE GOING THRU CHECKLIST HEARD A ENGINE CHANGED USING ETASK CARD #19-7200-1-0902. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1661496 SN OFF 0815 ENGINE CHG IS REFLECTED IN SCEPTRE WITH CORRECT NUMBERS AND REFERENCES ENGINE, BASIC, OFF 19-7200-9-0001 0815 ON 0000 ENGINE, BASIC, OFF 19-7200-9-0001 0815 ON 53-7200-9-0001 1807 IPC REFERENCE # 71-00-02-01A ACP RII INSP OF ENG 2 REPLACEMENT. REF GMM 09-25-05.

Part: TRANSMITTER — INTERMITTENT (HYD SYSTEM) · airframe 60,235 hrs · 18,220 cycles

MAIN LT, RT, AND CNTR C HYD QTY DECREASED. QTY STABLE WITH SYS PUMPS OFF QTY DECREASED TO 0.02. FLUTUATED W/PUMPS ON STABLE AT 1.06 W/PUM PS OFF AFTR 5 MINS OFF PLACE CTR HYD QTY FLUCIATION ON MEL 2933F. VERFIED CTR HYD QTY WAS AT PROPER OPS LEVEL AT PANEL. OPS ALL FLT CONTROLS & VERFIED NO LEAKS. . PLACARD INSTALLED AND VERFIED CENTER HYD QTY AT RESERVOIR. HYD QTY IND SYS ADJ EST FOUND AT AMM 29-33-00/501. MEGGER & RANG WIRES FROM CONNECTOR D2450 TO D2598A. NO FAULTS. WDM 29-31-11-5 PG 5. CONNECTOR D 2450 SECURED TO HYD QTY. DUE TO HISTORY REF WDM 29-33-11 PERFORM WIRING CHECKS BETWEEN D2540 TO HYD QTY MON UNIT D2598A, CHECK FOR TRANSMITTER M339 & HYD QTY MONITOR UNIT M122 REINSTALLED AT E3-4 SHELF AND TEST OK. AMM 29-33-11-5 PG5. RECOMMEND TO RELACE CTR HYD QTY TRANSMITTER M339. AMM 29-33-01-024-001 & 29-33-01-424-010. CONTINUITY AND SHORTS TO GRD & WIRE TO WIRE. ALSO CHK GRDS & SHIELDS. EXCERCISE WIRES BY XTMR WHILE CHECKING. CENTER QUANTITY TRANSMITTER REF AMM 29-33-01 LEAK CHECK AND OPS CHECK PERFORMED NO DEFECTS NOTED

Part: TRANSMITTER — UNKNOWN (ZONE 151) · airframe 59,105 hrs · 17,893 cycles

T/O +15 MIN C HYD QTY AND RSVR LTS. .01 QTYRF INDICATED. AFTER TURNING OFF CTR PUMPS QTY INCR REPLACED CENTER HYDRAULIC FLUID TRANSMITTER. REF 29-33-01/401. PRESSURIZED HYD SYSTEM AND ACCOMPLISHED LEAK CHECKS. REF 29-33-01-024-001. NO LEAKS DETECTED AND PRESSURE INDICATION READS NORMAL. PARTS USED: 1224383,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1224383 SN OFF 5125 IPC REFERENCE # 29-33-01 TRANSMITTER, CE OFF 75-2932-9-9002 5125 ON 0000 TRANSMITTER, CE OFF 75-2932-9-9002 5125 ON 75-2932-9-9002 5440 MONITOR, HYDRAU OFF 75-2932-9-0001 0402 ON 75-2932-9-0001 0557 MONITOR, HYDRAU OFF 75-2932-9-0001 0402 ON 0000 REPLACED HYDRAULIC RESVR QTY MONITOR. REF 29-33-51-714-024. PERFORMED EICAS HYD QTY CHECKS ALL SYSTEMS INDICATION SHOWS NORMAL.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 59,114 hrs · 17,895 cycles

LEFT THR REV ILLUM ON TAKEOFF ROLL 70 KTS AFTER ACHVNG TAKEOFF THRUST ITEM PLACED BACK ON MEL DUE TO HISTORY. REF LOGPAGES 6098424 AND LOG 6104186 FOR MELS. AMBER REV ICON ON LH EPR GAUGE AFTER TAKEOFF THRUST WAS SET. LEFT AMBER ALLUMINATED AFTER THROTTLES WERE ADVANCED FOR TAKEOFF DURING TAKE OFF ROLL AMBER LIGHT CAME ON. PER CREW CONVERSATION. CREW REJECTS TAKEOFF ALL SYSTEM AND INDICATIONS NORMAL. REV OPENED AND CLOSED NORMAL. CONTROL OF AIRCRAFT NORMAL. AFTER REVERSER STOWED AND AIRCRAFT TURNED OFF RUNWAY AMBER LIGHT EXTINGUISHED AND HAS NOT RETURNED. COMPLIED WITH MEL REQUIREMENTS. ADD EMP:U112755, U138028 COMPLIED WITH MEL REQUIREMENTS. ADD EMP:U138028 LEFT ENGINE REVERSER UNLOCK INDICATION INOP. PERFORMED FIM 78-36 TASK 810, WITH NO FAULTS FOUND. PERFORMED LH ENGINE TR ACTUATOR LOCK INTEGRITY TEST AND TEST PSSED REF AMM RETURNED LH TR TO MEL CONDITIONS. 78-31-00-501. NEED TO PERFORM HIGH POWER ENGINE RUN TO SEE IF PROBLEM RE OCCURS. REACTIVATED LH TR REF AMM 78-31-00 OPS CK GOOD. HIGH POWER RUN ACCOMPLISHED, NO FAULTS NOTED ADD EMP:U393837,U002076 REOPEN DEN U130197 26OCT23 FOR: CLOSED PREMATURELY ITEM STILL EXISTS REACTIVATED LH TR REF AMM 78-31-00 OPS CK GOOD. HIGH POWER RUN ACCOMPLISHED, NO FAULTS NOTED ADD EMP:U393837,U002076 PERFORMED PSEU BITE REF. FIM 78-30-00/301, FOUND HISTORY FAULT M ESSAGE "78-36077 T/R NOT LOCKED L" AT LEAST ON THE LAST 20 FAULT S MEMORY RECORDED, PERFORMED LH ENG. RH SLEEVE UNLOCK PROXIMITY SENSOR - TARGET GAP CHECK REF. AMM 78-30-00-835-

Part: THRUST REVERSER — WARNING MESSAGE (LH ENG) · airframe 59,083 hrs · 17,887 cycles

RTO AT 85 KTS AIRCRAFT WEIGHT 249.000. AT TIME OF REJECTED TAKEOFF ACP. HIGH ENERGY STOP/HEAT DAMAGE CONDITION INSPECTION PER AMM 05-51-14/201. NO DEFECT FOUND. AMBER REV ICON ON LH EPR GAUGE AFTER TAKEOFF THRUST WAS SET. LEFT AMBER ALLUMINATED AFTER THROTTLES WERE ADVANCED FOR TAKEOFF DURING TAKE OFF ROLL AMBER LIGHT CAME ON. PER CREWCONVERSATION. CREW REJECTS TAKEOFF ALL SYSTEM AND INDICATIONS NORMAL. REV OPENED AND CLOSED NORMAL. CONTROL OF AIRCRAFT NORMAL. AFTER REVERSER STOWED AND AIRCRAFT TURNED OFF RUNWAY AMBER LIGHT EXTINGUISHED AND HAS NOT RETURNED. COMPLIED WITH MEL REQUIREMENTS. ADD EMP:U112755, U138028 COMPLIED WITH MEL REQUIREMENTS. ADD EMP:U138028 LEFT ENGINE REVERSER UNLOCK INDICATION INOP. PERFORMED FIM 78-36 TASK 810, WITH NO FAULTS FOUND. PERFORMED LH ENGINE TR ACTUATOR LOCK INTEGRITY TEST AND TEST PSSED REF AMM RETURNED LH TR TO MEL CONDITIONS. 78-31-00-501. NEED TO PERFORM HIGH POWER ENGINE RUN TO SEE IF PROBLEM RE OCCURS. REF. LOG PAGE 6098424 AMBER INDICATION INOP ENGINE 1 REVERSER, APPLY MEL 7831E TO LOCK OUT #1 REVERSER IN STOWED POSITION. APPLIED MEL 7831E AND COMPLIED WITH MEL REQUIREMENTS. ADD EMP:U112755,U138028 APPLIED MEL 7831E AND COMPLIED WITH MEL REQUIREMENTS. ADD EMP:U138028 DISPATCH DESK: 07 NAME: JED DATE: 23-OCT-23-NOC DESK: 757 NAME: DONNY DATE: 23-OCT-23-. LEFT ENGINE REVERSER UNLOCK INDICATION INOP. PERFORMED FIM 78-36 TASK 810, WITH NO FAULTS FOUND. PERFORMED LH ENGINE TR ACTUATOR LOCK INTEGRITY TEST AND TEST PSSED REF AMM RETURNED LH

Part: ACTUATOR — FAULTY (ENG#1) · airframe 59,069 hrs · 17,882 cycles

L REV CAUTION ON TAKEOFF .REV CAUTION OUT AFTER THROTTLE RETARDED MEL TO BE APPLIED WITH TOMC APPROVEL REV ISOL VALVE PIN INSTALLED , MECH DEACT PINS INSTALLED , LEFT ENG SYNC LOCK P11 PULLED AND SAFETIED. PLACARD INSTALLED FWD OF THROTTLE THRUST REV INOP PERFORMED PROXIMITY SENSOR ELECTRONICS UNIT BITE PROCEDURE REF FIM 32-09 FAULT TREE 812, FOUND FIVE FAULTS IN FAULT HISTORY ON THE SAME LEG. L T/R IN TRANSIT, T/R NOT LOCKED L, T/R AUTO RESTOW L, L T/R DEPLOYED, T/R NOT STOWED L. FURTHER TROUBLE SHOOTING REQUIRED REF FIM 78-30-00/301 MATERIAL UPDATE MATERIAL UPDATE PERFORMED PSEU SYSTEM TEST REF AMM 32-09-812. FAULTED T/R NOT LOCKED L MSG #78-360063. REF FIM 78-30-00/301 LEFT ENGINE, RIGHT SIDE ACTUATOR LOCK PROXIMITY SENSOR S10436 INDICATES FAR FOR T/R LOCKED. THIS SENSOR NEEDS TO BE CHECKED FOR PROPER RIGGING REF AMM 78-30-00-835-024-R04. PERFORMED ADJUSTMENT OF THE LOCK PROXIMITY SENSOR PER AMM 78-30-00-835-024-R04, ADDED .010 SHIM WASHER TO BRING SENSOR WHILE ACCOMPLISHING #1 ENG LOWER REVERSER ACTUATOR LOCKING INDICATOR FOUND WOULD NOT FAIR WHILE CLEANING MECHANISM FOUND AMM 78-30-00-835-016-R04 REF. SUSPECT LOWER INBOARD SYNCHRONIZED ACTUATOR MFG. P/N 1616000-1, M&E P/N 19-7831-9-0004 WITHIN LIMITS. REACTIVATED T/R SYSTEM PER 78-31-00-912-023-R04. CYCLED T/R NO HELP. FOUND RH LOCKING INDICATOR NOT FULLY ENGAGED. WHEN INDICATOR IS PUSHED IN MANUALLY YELLOW REV LIGHT C

Part: TRANSMITTER — FAULTY (HYD SYS) · airframe 58,450 hrs · 17,679 cycles

CENTER HYD QTY EICAS DURING CLIMB. QTY FLUX BETWEEN ZERO & FULL. HYD PRESS REMAINED NORM PLACE CENTER HYD QTY INDICATION EICAS. ON MEL PLACED CENTER HYD. QTY. INDICATION EICAS. ON MEL, QTY DDP C/W. OK TO DEFER CENTER QTY INDICATION PER MEL. CHECKED WIRES FROM D2598A A13 TO PIN 3, B13 TO PIN 4, C13 TO PIN 5 ON D2540 THAN PINS 3,4,AND 5 TO GROUND, NO FAULTS NOTED, MEGGED ALL WIRE, CHECKED GOOD WITH NO FAULTS, CHECKED D2598A B13 TO PIN 7 ON D2540 & MEGGED, NO FAULTS. CHECKED B13 TO C10 NO CONTINUITY FOUND, MEGGED SAME NO FAULTS FOUND, SUSPECT BAD QTY TRANSMITTER. REMOVED UNSERVICEABLE CENTER HYD RESERVIOR TRANSMITTER & INSTALLED SERVICEABLE ONE IAW AMM. COMPLETED TRANSMITTER INSTALL IAW 29-33-01. OPS CHECK GOOD.

Part: INDICATOR — FAULTY (AIRSPEED) · airframe 58,414 hrs · 17,665 cycles

ON TAKEOFF ROLL CAPT AIR SPEED INDICATOR FLAG APPEARED. T/O REJ ECTED AT 8 0KTS. CAPT''S MACH AIRSPEED INDICATOR FLUCTUATING WITH AIRCRAFT PARKED. REPLACED CAPT''S MACH AIRSPEED INDICATOR REF AMM 34-13-02-404-004, CKS GOOD. PARTS USED: 75-3111-9-0001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1775347 SN OFF 2800 INDICATOR, MACH OFF 75-3111-9-0001 2800 ON 75-3111-9-0001 4393

Part: FLAP SYSTEM — STUCK (TE FLAPS) · airframe 57,827 hrs · 17,490 cycles

TE FLAP DISAGREE ON SHORT FINAL. FLAPS STUCK AT 25 RETRACTED FLAPS IN OVERRIDE AND PERFORMED FSEU 1+2 BITE TESTS REF AMM 27-51-01, NO FAULTS NOTED. CYCLED FLAPS HYDRAULICALLY FULL DOWN AND UP, LEADING EDGE SLATS AND FLAPS AND TRAILING EDGE FLAPS OPS CK GOOD. ACFT OK TO CONTINUE AT THIS TIME.

Part: LIGHT — INOPERATIVE (DOOR 2R) · airframe 57,770 hrs · 17,472 cycles

DOOR 2R EXTERIOR EMERGENCY LIGHT INOP. RELAMPED DOOR 2R EXTERIOR EMERGENCY SLIDE LIGHT REF AMM 33-51-06-962-001-002. OPS TEST GOOD.

Part: LAMP — BURNED OUT (L895 + L50) · airframe 57,400 hrs · 17,348 cycles

L/H EXTERNAL L3 DOOR EMERGENCY LIGHT AND R/H EXTERNAL R3 EMERGENCY DOOR SLIDE LIGHT ARE INOP REMOVED AND REPLACED LIGHT BULBS AT L895 AND L50 IAW B757 AMM 33-51-06, OPERATIONAL CHECK GOOD.

Part: FRAME — CRACKED (STA 780) · airframe 57,400 hrs · 17,348 cycles

FRAME CRACKED THROUGH RIVET HOLE FOR OVERHEAD BIN ATTACH BRACKET AT STA 780 + 20 AND JUST BELOW STR 8 REPAIRED RH FUSELAGE FRAME AT FS 780 + 20 STR 8 IAW B757-300 SRM 53-00-07 REPAIR 8. FOR DETAILS SEE PWA AND PWS #31 PG 1 OF 1.

Part: FRAME — CRACKED (STA 1540) · airframe 57,400 hrs · 17,348 cycles

UPPER CABIN INTERIOR FUSELAGE FRAME IS CRACKED AT STATION 1540 STRINGER 8LL AT THE OVERHEAD BIN ATTACH RACKET. REPAIRED RH FUSELAGE FRAME AT FS 1540 STR 8L IAW B757-300 SRM 53-00-07 REPAIR 8. FOR DETAILS SEE PWA AND PWS #30 PG 1 OF 1.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 57,383 hrs · 17,343 cycles

L ENG BLD OFF NO NO RESPONSE RE CHKLST PREFORMED FIM 36-10-00-815-816, PREFORMED HEALTH CHECK REMOVED A ND REPLACED PRSOV IAW AMM 36-11-07-401 NEEDS HIGH POWER ENG. RUN. VALVE, PNEU, PR OFF 19-3611-9-0004 1061 ON 19-3611-9-0004 1652 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1923846 SN OFF 1061 UPDATE FOR PARTS INFORMATION PERFORMED LEFT ENGINE RUN 80% N1 .LEFT ENG BLEED DROPS TO 0 PSI DUCT PRESS...LEFT ENG BLEED OFF LIGHT ON AMM 36-11-004-048-001 REMOVE AND 36-11-17-404-062-001 INSTALL. REMOVED AND REPLACED FAN AIR TEMPERATURE SENSOR #1 ENGINE. REF ALSO REMOVED AND REPLACED AIR SUPPLY OVERTEMPERATURE LIMITING (450 DEG) SENSOR. REF AMM 36-11-13-004-000-001 REMOVAL AND 36-11-13-404-021-001 INSTALLALATION. OFF LINE AFTER 1.13 EPR. PERFORMED ENGINE #1 BLEED SYSTEM ENGINE RUN TEST AFTER SENSORS CHANGED. NO HELP. CONDITION REMAINS. LEFT ENGINE PNEUMATICS DROP IN LEFT AC BAY. REF AMM 36-22-01-000-801 REMOVAL AND REMOVED AND REPLACED AIR SUPPLY THERMAL OVERTEMPERATURE SWITCH 36-22-01-400-801 INSTALL. ON 129626-6, S/N ON 3098. IPC REFERENCE # 36-11-13 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1273746 SN OFF 2697 INFORMATION ONLY. THE F.A.M.V. SENSOR WAS REPLACED, THE INFORMATION IS AS FOLLOWS. P/N OFF 129626-6, S/N OFF 2697. P/N ENGINE R.F.C.C. GAVE SWING SHIFT TURNOVER AND PAPERWORK. PERFORMED STEPS 1-7 OF A.M.M. 36-00-23-705-154-001 1 ON THE LEFT PERFORMED RFCC TEST REF AMM 36-023-705-154-001 . OPS TEST GOOD PERFORMED SENSE LINE INSPECTION AT THE RFCC AREA AND THE 3 SENSE LINES

Part: CONNECTOR — DAMAGED (HYD SYSTEM) · airframe 56,227 hrs · 16,952 cycles

DURING CLIMB C HYD QTY DROPPED TO 0 WITH SYS PRESSURE CAUTION LO W INDICATION LOW RSV LIGHT PILOT REPORTED ISSUE OCCURRED AFTER 20 MINUTES OUT BEFORE RETURN TO FIELD. CONTACT TOMC TO UNLOCK AFTER REPAIRS ARE COMPLETE. UNLOCKED FOR UPDATING. CHECKED HI-Z WIRING AND FOUND RESISTANCE READINGS CHANGING WHEN MOVING WIRES ON D41406J.READINGS TAKEN FROM D2598A B11/C10 WITH D2540 PINS 1/7 JUMPERED.READINGS JUMPING FROM 5 OHMS TO 300 OHMS ALSO INSPECTED RES XMTR SHROUD WITH NO DISCREPANCIES NOTED.NEED D41406J/P AND D40350J/P RPL''D PER FUP.REF WDM 29-33-11. REMOVED AND REPLACED CONNECTORS D41406J/P AND CONNECTORS D40350J /P REF WDM 29-33-11. SEE LP 3600512 FOR OPS CK

Part: WIRE — SHORTED (FUEL SYSTEM) · airframe 53,517 hrs · 16,144 cycles

AIR RETURN DUE TO R/H CNTR FUEL PUMP EICAS LOW PRESSURE LIGHT ON REF FIM 28-22-00-815-804 FOUND FAULTS 22 AND 33 REPLACED RAM NEEDS PUMP REPLACED AS WELL AS K10012 PUMP CONTROL RELAY. FOUND WIRE NUMBER 3 (BLUE) AT CONNON PLUG D1838, SHORTING TO GROUND AT SOLDER FOR SHIELDING, WITH PUMP OPERATIONAL AND SHAKING WIRES. CUT TO NEW WIRE LENGTH WHILE REMOVING DEFECTIVE AREA AND INSTALLED SERVICEABLE CONNECTOR, REF SWPM 20-00-00 AND WDM 28-22-11. OPS CK GOOD. VERIFIED CDCCL REQUIREMENTS PER SWPM 20-20-00 AND PER WDM 28-22-11 PER QC

Part: UNKNOWN — FAULTY (R1 DOOR) · airframe 52,805 hrs · 15,908 cycles

DOOR-MOUNTED ESCAPE SYSTEM DOOR 1R - A EVACUATION SLIDE PROBLEM WAS ENCOUNTERED WHICH IS NOT COVERED IN THE FAULT CODE DIAGRAMS FLICKERING INDICATOR LIGHT. LIGHT IN QUESTION IS THE SMALL LIGHT ABOVE DOOR 1R. LIGHT IS NOT WORKING AT ALL. TESTED BULBS AND THEY TESTED OKAY. GOING TO CONTINUE TROUBLESHOOTING WITH AMM 25-66-00-815-802. TROUBLESHOT GIRT BAR ENGAGEMENT LIGHT IN ACCORDANCE WITH FIM 25-66-00-815-802. VERTICAL AND HORIZONTAL CLEARANCES ON SENSORS ARE WITHIN LIMITS, SUGGEST REPLACING ONE OR BOTH GIRT BAR PROXIMITY SWITCHS. REF AMM 25-66-11/201. DEFERED PER MEL 2566R DOOR 1R SLIDE LIGHT INOP DEFERRED PER MEL 2566R. DOOR VERIFIED ARMED BEFORE FLIGHT. FOUND S10217 BAD, REPLACED AND OP-CHECK SATS . AMM5211, SSM25-66-01

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,765 hrs · 15,266 cycles

R4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS, OPS CHECKED GOOD IAW AMM 33-51-06.

Part: LIGHT — LOOSE (1R DOOR) · airframe 50,254 hrs · 15,107 cycles

R1 DOOR SLIDE LIGHT INTERMITTENTLY BLINKING IN FLIGHT. SECURED THE LIGHT ASSY .

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,828 hrs · 14,979 cycles

EMERGENCY LIGHTS AT ROWS 20 AND 22 ON THE RT SIDE OF THE CABIN INOP DURING LIGHT CHECK. RELAMPED, OPS CHECKED GOOD. REF AMM 33-51-00.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 49,611 hrs · 14,916 cycles

RIGHT AFT EXTERIOR EMERGENCY LIGHT LAMP BURNED OUT. (BY R3 DOOR) R&R R3 AFT EXT EMER LAMP. CKD OK.

Part: SEAT TRACK — DAMAGED (BS 1030) · airframe 49,212 hrs · 14,804 cycles

SEAT TRACK BS 1030, RBL 24.75 HAS DAMAGE. REPAIRED THE SEAT TRACK IAW SRM 53-00-52, REPAIR 4, FIG 201.

Part: INDICATOR — BINDS (L4 DOOR) · airframe 48,963 hrs · 14,728 cycles

DOOR 4L SLIDE ARM PLACARD INDICATOR BINDS AND DOES NOT FULLY EXTEND WHEN DOOR ARMED. CLEANED INDICATOR. NO BINDING NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,160 hrs · 14,201 cycles

EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP. OPS CHECKED GOOD .OK FOR SERVICE IAW 33-51-15

Part: SIGN — MISSING (CABIN) · airframe 45,871 hrs · 13,834 cycles

EXIT SIGN MISSING MID CABIN PERMANENT REPAIR IAW PART 3 WITHIN 2 FLIGHT CYCLED. ACCOMPLISH ECRA 3351-01129 PART 1. R & R HOUSING ASSEMBLY SIGN EXIT, MID CABIN IAW AMM 33 -51-01. INSPECTIONS CREATED BY AUTO DIP PENDING ACFT RECORDS AUDIT & UPDATE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 45,658 hrs · 13,774 cycles

WE GOT TE FLAP DISAGREE LIGHT ON APPROACH SIGN. IAW FIM 27-51-00 BITE FSEU, NO FAULT NOTED. BITE FSAM, NO EXISTING FAULTS. RAN FLAPS HYDRAULICALLY & ELECTRICALLY, NO BINDING & NO NOISE NOTED.

Part: INDICATOR — TRIPPED (TE FLAP) · airframe 45,333 hrs · 13,679 cycles

TRAILING EDGE FLAP DISAGREE EICAS MSG ON APPROACH. RAN QRH PROCEDURE & LANDED WITH FLAPS AT 20. NO OTHER ISSUES NOTED. ACCOMPLISHED FIM 27-51-00-815-808, FOUND FLAP OVERLOAD INDICATOR 1 & 7 TRIPPED, RESET & RAN FLAPS, DID NOT TRIP AGAIN, MX CONTROL TO MONITOR.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 41,563 hrs · 12,757 cycles

GO AROUND, HAD TE FLAP DISAGREE EICAS MSG WHILE SELECTING FLAPS TO 20 POSITION. RETURNED FLAP HANDLE TO ZERO, NO FAULTS ON FSEUS. RAN FLAPS NO MSGS.

Part: ENGINE — SMOKE (LEFT) · airframe 33,744 hrs · 10,803 cycles

AFTER TAKE OFF, TOWER REPORTED LT ENGINE TRAILING VISIBLE BLACK SMOKE, ALL COCKPIT INDICATIONS NORMAL. F/A REPORTED STRONG BURNING ELECTRICAL ODOR TOWARDS REAR OF CABIN. AIR RETURN, PERFORMED AMM TASK 05-51-58-910-801C1, CHECKED SATISFACTORY. MX TEST FLIGHT PERFORMED. INITIAL OIL/FUEL ODOR NOTED DURING TAXIOUT. ODOR DISSIPATED AFTER TAKE OFF IAW FIM 71-R-05-828 SATISFACTORY. TROUBLESHOT FURTHER IN FLIGHT WITH BLEED SOURCE OF ENG AND APU. NO FURTHER ODOR FOR TEST FLIGHT DURATION OF 1 HR, 16 MI.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,293 hrs · 10,438 cycles

DOOR 3L OUTSIDE EMERGENCY LIGHT INOPERATIVE. RLEAMPED EMERGENCY LIGHT BULB AT 3L. OPS CHECKED GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 29,561 hrs · 9,532 cycles

DAMAGE TO SKIN NEAR L-4 DOOR AT STA 1695& 12 IN BELOW WATER LINE REF I/B WRITE UP LOG PAGE 8743016 SEQ 570-573 REMOVED DAMAGE AND INSTALLED DOUBLER REF EC/RA 5330-04135 INITATED DIP TO ACCOMPLISH PERMINANT REPAIR WITHIN 12 MONTHS 53-DIP CONTROL NUMBER 11353 ACCOMPLISH PERM REPAIR WITHIN 12 MONTHS FROM 6/17/2011. PLANNING TO CONTACT ENGR AFTER 10 MONTHS BUT BEFORE 11 MONTHS FOR PERM REPAIR. 1) INIT: AFTER 10 MONTHS BUT BEFORE 11 MONTHS (PLG/ENG) & 2) T/A: W/I 12 MONTHS FROM 17 JUN 2011-ODEE

Part: LENS — MISSING (CABIN) · airframe 28,926 hrs · 9,329 cycles

OVERHEAD EXIT SIGN MISSING IN MAIN CABIN. REPLACED MISSING LENSE CENTER OVERWING EXIT AFT SIDE, LIGHT CHECKS NORMAL.

Part: SPAR — DAMAGED (RT WING) · airframe 25,399 hrs · 8,221 cycles

SUPPORT TASK OP 17. RIGHT WING, FWD SPAR AT WS 80-6, MIS-DRILLED DURING DRILL-UP OF RIB 26 P/N 757-3263-1 RIB POST. REF EA 5700-02220, REV E, OP 17, STEP 93 REWORK OPENED DISCREPANT HOLE TRUE AND ROUND TO .6265, INSTALLED A FREEZE PLUG AND MADE FILLERS A & B, PICKED UP HOLE IN FILLERS AND NDT, ROTO PEENED AND INSTALLED FILLER AND LOCATED NEW FASTENER HOLE THROUGH FREEZE PLUG. ALODINED AND TOUCHED UP WITH PAINT IAW ECRA 5700-02803 AND EA 100375 IR.

Part: PLATE — DAMAGED (L2 DOOR) · airframe 25,347 hrs · 8,200 cycles

L2 DOOR REQUIRES EXCESSIVE FORCE TO OPEN- AT TIMES IT BINDS REPORTED BY FLT ATTENDANTS ALSO HARD TO OPEN AND CLOSE. T/S REF FIM 52-11-00 PG 119 WITH DOOR IN COCKED POSITION LOUD NOISE AND ROUGH MOVEMENT FROM INNER HANDLE. FOUND COCKING CRANK BEARING AND CONTROL CAM PLATE DAMAGED. R&R WORN COMPONENTS OPS CHECKS NORMAL.

Part: PLATE — OUT OF ADJUST (CABIN) · airframe 24,167 hrs · 7,809 cycles

DOOR R1 SLIDE LIGHT INOPERATIVE. FOUND SLIDE LIGHT INTERMITTENT DURING OPERATIONS. ADJUSTED AFT GIRT BAR FLOOR FITTING PLATE IAW AMM 52-11-25 R-1, SLIDE LIGHT OPERATES NORMAL.

Part: FAN — OVERHEATED (FWD CARGO BAY) · airframe 22,050 hrs · 7,133 cycles

AFTER ENCOUNTERING TURBULENCE CABIN FILLED WITH SMOKE. LEFT RECIRC FAN ANNUNCIATED, WITH OVERBOARD EXHAUST VALVE OPEN STATUS, SMOKE DISSIPATED. FOUND LEFT RECIRC FAN INOPERATIVE. REMOVED AND REPLACED LEFT RECIRC FAN PER AMM 21-25-01 404-094, OPERATIONAL CHECKS OK.

Part: SKIN — CRACKED (L4 DOOR) · airframe 20,446 hrs · 6,567 cycles

L4 DOOR INNER SKIN IS CRACKED AT THE UPPER HINGE CUTOUT AREA. REPAIRED PER ECRA 5210-02031. DIP WRITTEN TO ACCOMPLISH PERMANENT REPAIR WITHIN 12 MONTHS FROM SEP 15 2008 PLANNING TO CONTACT ENGINEERING AFTER 10 MONTHS BUT BEFORE 11 MONTHS FOR A PERMANENT REPAIR. DIP CTL 090286.