N57111

Part: WARNING MESSAGE — INTERMITTENT (TE FLAPS) · airframe 115,881 hrs · 24,566 cycles

TE FLAP DISAGREE, EMERGENCY LANDING FLAPS 1 191K LBS SOFT LANDING. PERFORMED BITEOF ALL 3 FSUU PER AMM 27-51-TASK 803. FSEU 1 AND 3 BITE NO FAULTS, FSEU 2 HAD LE SLAT ASYM, INTERMITTENT FAULT. RESET AND RAN THE FLAPS COUPLE OF TIME UP AND DOWN. SYSTEM CHECKED OK AND MSG INACTIVE.

Part: SLIDE — LOW PRESSURE (ZONE 800) · airframe 115,111 hrs · 24,394 cycles

SLIDE PACK 4R IN RED R4 DOOR SLIDE PRESSURE NEEDLE IS APPROXIMATELY 2 TO 3 NEEDLES WITH INTO THE RED BAND. REF AMM 25-66-01-206-024. EMERGENCY ESCAPE SLIDE NIS AT IAH. HAS 2 PREVIOUS WRITE-UPS ON R4 DOOR SLIDE, REMOVED AND REPLACED 4R ESCAPE SLIDE REF AMM 25-66-01. AIRCRAFT OKAY FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 114,946 hrs · 24,357 cycles

TE FLAPS DISAGREE CAUTION MSG FSEU 1 LAST LEG HAD FAULT 305 - INTERMITTENT, FSEU 2 HAD FAULT 327. PERFORMED FIM 27-51 TREE 805, BITE TEST GOOD, NO EXISTING FAULTS. MSG CLEARED. CYCLED FLAPS THROUGH FULL TRAVEL MULTIPLE TIMES, FLAPS OPERATED NORMALLY.

Part: TRANSMISSION — FAULTY (ZONE 600 FLAP) · airframe 114,583 hrs · 24,287 cycles

TE FLAP DISAGREE EICAS WHEN SELECTING FLAP 1 FROM UP. QRH ACTION ED ALT FLAP 20 LANDING, DECLARED EMERGENCY, FOUND # 8 TE FLAP OVERLOAD INDICATOR ON FLAP TRANSMISSION TRIPPED. PERFORMED STEP D.(8) IN AMM TASK 27-51-17-024-001 FOR FSEU 1 RESOLVER INPUTS, L FLAP 342.09/R FLAP 340.73. PERFORMED REMOVAL OF RT OTBD T/E FLAP TRANSMISSION IAW AMM 27-51-21-024-001. INSTALLED RT FLAP TRANSMISSION IAW AMM 27-51-17-424-020 UP TO AND INCLUDING G (3) (H) 2). PERFORMED TEST OF POSITION TRANSMITER REF AMM 27-58-01-715-112 UP TO AND INCLUDING I (3) ADD EMP:U427578,U431155 CW IDT REQUIREMENTS FOR FLAP TRANSMISION INSTALL IAW GMM 09-25-05. CONTINUED INSTALLATION OF R8 FLAP TRANSMISSION IN REF WITH AMM 27-51-17-424-020 FROM STEP G (3) (H) (2) TO FINIC/W REQUIRED RII INSPECTION FOR R8 FLAP TRANSMISSION INSTALL.

Part: SLIDE — NO DISCREPANCY (ZONE 800) · airframe 114,347 hrs · 24,247 cycles

DOOR 4R SLIDE OUTSIDE GREEN BAND. INSPECTED DOOR 4 R DOOR SLIDE PER AMM 25-66-01-206-041 FOUND WITH LIMITS THE GREEN TEMP CAN GO 1/2 WIDTH OF GREEN BAND OK TO CONT.

Part: SENSOR — FAULTED (NR 1 ENGINE) · airframe 113,926 hrs · 24,167 cycles

AFTER TAKEOFF DURING INITIAL CLIMBS THE LEFT BLEED OFF LIGHT AND ASSOCIATED PACK OFF LIGHT ILLUMINATED. WE FOLLOWED THE QRH PROCEDURE AND WERE UNABLE TO RESET IT. AFTER CONTACTING TOMC A SECOND ATTEMPT WAS MADE AT 1.22 EPR AND STILL NOT RESET. REFERENCE: 36-10 FAULT TREE 820. PERFORMED CONTINUITY CHECK FROM N3 TACH TRANSMITTER CONNECTOR D1338 PIN 1 AND 2 TO L ENG SPEED CARD CONNECTOR D2996 PIN 1 AND 2. CONTINUITY FOUND. REMOVED AND REPLACED ENGINE SPEED CARD AS PER AMM 77-12-03. OPS CHECK GOOD.

Part: OIL FILTER — DAMAGED (SCAVANGE SYS) · airframe 113,870 hrs · 24,157 cycles

RT ENGINE LOW OIL PSI ON TAKEOFF PRECAUTIONARY SHUTDOWN INFLT ESFR REQUIRED T/S RT ENGINE LOW OIL PSI IAW FIM 79-32 FT 805. REMOVED SCAVANGE AND PRESSURE FILTER IAW AM 79-00-00/601 FOUND DAMAGE ON SCAVANGE FILTER. SEE PICTURES ATTACHED. SEE BLOCK 23 FOR NEXT MAINTENACE PROCEDURE. REQ ENGINE CHANGE. ENGINE CHANGE TO BE PERFORMED.

Part: SLAT SYSTEM — FAULTED · airframe 113,798 hrs · 24,143 cycles

LE SLAT ASYM RAN THE QRH LANED WITH FLAPS 20 AFTER T/O DURING FLAP RETRACTION GOT LE ASSYM LIGHT AND EICAS ACFT ARRIVED AT GATE LE RETRACTED AND FLAPS AT 20 CONFIRMED PHYSICAL L/E ASYM. R SLAT = 25.96 DEG. L SLAT = 10.35 DEG. SLAT PDU = 9.51 DEGFOUND RIGHT SLAT TORQUE TUBE DISCONNECTED ABOVE # 2 ENGINE STRUT AT SUPPORT INSTALLATION (REF IPC 27-81-20-01) RE-CONNECTED TORQUE TUBE COUPLING AND PERFORMED OPERATIONAL TEST AS PER MM-27-81-20-424-015. VERIFIED ALL RII ITEMS HAVE BEEN C/W IAW MM 27-81-20-424-015 AND IPC 27-81-20-01, INCLUDING ALL TORQUES, SAFETIES, AND TESTA. REPLACED MISSING HARDWARE

Part: INDICATOR — FAULTY (FLAP SYSTEM) · airframe 113,761 hrs · 24,138 cycles

TE FLAP DISAGREE AT APPROX 1000FT. FLAPS STUCK AT 25.. INITIATED GO AROUND. CREW REPORTED THAT WHEN FLAP HANDLE WAS MOVED TO 30 THE FLAPS REMAINED AT 25 WITH TE FLAP DISAGREE MESSAGE. AFTER THEY MOVED THE HANDLE BACK TO 25 PER CHECKLIST MESSAGE WENT AWAY. TROUBLESHOOTING PER FIM 27-51 FAULT TREE 808. ACCOMPLISHED BLOCK 1 FSEU BITE PROCEDURE. NO FAULTS ON ALL FSEUS. PERFORMED CONTINUATION OF FIM TASK 27-51 FAULT TREE 808 BLOCK 3, FOUND 5 AND 8 TE FLAP OVERLOAD INDICATORS ON FLAP TRANSMISSION TRIPPED. RESET TRANSMISSION INDICATORS PER FIM TASK 27-51 FAULT TREE 808 BLOCK 53. OPREATED ELECTRICALLY AND HYDRAULICALLY, OPS CHK GOOD. REINSPECTED OVERLOAD INDICATORS, NO DEFECTS FOUND. FLAPS FULLY DEPLOYED AND RETRACTED NUMEROUS TIMES, NO DEFECTS NOTED AT THIS TIME. FLAP POSITION INDICATOR REPLACED AS A PRECATION IAW AMM 27-58-02/401. PERFORMED OPERATIONAL TEST IAW AMM 27-58-02-704-010. OPERATIONAL TEST SATISFACTORY. A/C OK TO CONTINUE

Part: FRAME — DEFORMED (ZONE 100) · airframe 113,224 hrs · 24,028 cycles

FRAME STA 1440 BTW STR 26LH-27LH HAS A DENT ESFR ENTRY DENT OF FRAMESTA 1440 DIMENSIONS; L=1.5, W=.900 D=.070. PERFORME D REPAIR AS PER SRM 53-00-07-2R-5. REQUIRES REPEAT INSPECTIONS ADD EMP:V940985 PER SRM 53-00-07-2R-5 TABLE 2 ZONE 1 37,500 FLIGHT CYCLES AFTER REPAIR OR 50,000 AIRFRAME CYCLES, WHICHEVER COMES FIRST. WITH REPEAT INSPECTIONS EVERY 12,000 CYCLES THEREAFTER.

Part: SKIN — GOUGED (ZONE 600) · airframe 113,216 hrs · 24,023 cycles

RIGHT WING O/B GLAP I/B L/E OF THE MAIN FL AP HAS A DEEP GOUGE. ECRA 5753-02305 ACCOMPLISHED ECRA 5753-02305 ON ST ENGINEERING NR 124688 SENT TO AVN FOR REPAIR ENTRY'S

Part: SKIN — DAMAGED (ZONE 200) · airframe 113,205 hrs · 24,018 cycles

(SDR) - R/FUSELAGE BTWN STA 660/640 AND STRG 7/8 FOUND SMALL HOL E AT SKIN AREA. NO DOT. REF: NRC 125035 SMALL HOLE IN SKIN AREA BTWN STA 640-660 STR 7-8.

Part: GATE — CORRODED (ZONE 800) · corrosion level 2 · airframe 113,205 hrs · 24,018 cycles

R4 PAX DOOR UPPER GATE INTERNAL HAS AN AREA WITH CORROSI ON.REF: 124893.

Part: BULKHEAD — DAMAGED (ZONE 100 MLGWW) · airframe 113,205 hrs · 24,018 cycles

MLG WHEEL WELL FWD BULKHEAD LH SIDE AREA APROX 30 INCHES IN LENGTH STARTING AT INBD END. REF: NRC 1 24970.

Part: SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 113,205 hrs · 24,018 cycles

L1 DOOR SURROUND STRUCTURE 1 3 EA FASTENER HOLES WITH DAMAGE AND CORROSION INDICATIONS. REF: NRC 124869

Part: BEAR STRAP — CRACKED (ZONE 200) · airframe 113,205 hrs · 24,018 cycles

L1 DOOR SURROUND STRUCTURE 01 EA FASTENER HOLE WITH CRACK INDICATIONS AT 11 O'CLOCK POSITION ON BEAR STRAP LAYER (HOLE #1). REF: NRC 124873.

Part: SKIN — DENTED (ZONE 800) · airframe 113,205 hrs · 24,018 cycles

AFT CARGO DOOR INNER SKIN BTW RIB 5-6 STA 1400-1420 WITH DENT.

Part: FRAME — DELAMINATED (ZONE 100) · airframe 113,205 hrs · 24,018 cycles

DENT ON FRAME AT STA 760 STR 24 RH, REPAIRED DENT ON FRAME AT STA 760 STR 24RH PER 757-200 SRM 53-00-07-2R-5 REPAIR 5 FIG 201 DETAIL II. INSPECTION THRESHOLD 37500 OR 50000 AIRFRAME FLIGHT CYCLES, WHICHEVER COMES FIRST. REPEAT INSPECTIONS AT 12000 FLIGHT CYCLES.

Part: FRAME — DENTED (ZONE 100) · airframe 113,205 hrs · 24,018 cycles

SUPPORT TASK: FRAME STA 1420 STR 25LH HAS A DENT. REPAIRED IAW B757-200 SRM 53-00-07-2R-5 FIG 201 DETAIL III DIP # 4483385 CREATED IAW B757-200SRM 53-00-07-2R-5 FIG 201 TABLE III RII VERIFIED REPAIR PERFORMED

Part: INTERCOSTAL — CORRODED (ZONE 200) · corrosion level 2 · airframe 113,205 hrs · 24,018 cycles

INTERCOSTAL HAS CORROSION BTW STA 1420 AND 1440 LBL 10.4 5. REF: 124766 SDR REPORTING ONLY REMOVED AND REPLACED INTERCOSTAL IAW B757 SRM 51-40-02

Part: STIFFENER — GOUGED (ZONE 400) · airframe 113,205 hrs · 24,018 cycles

(SDR) - B757-54-3-0055 ENGINE #1 NACELLE STRUT INTERNAL METAL CROSS BEAM LOCATED UNDER PRECOOLER HAS A GOUGE. DOT 75-005 HA-75. REWORKED CROSSBEAM PER EC/RA 5450-03002 AND VT MAE EA 754-5420-1 3-A3877 REV -.

Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 113,205 hrs · 24,018 cycles

LEFT MAIN WHEEL WELL LEADING-EDGE SEAL OUTBOARD BRACKET SHOWS SIGNS OF CORROSION AND DAMAGE. REMOVED AND REPLACED LE SEAL O/B BRACKET IAW B757-200 SRM 57-40- 02

Part: CHANNEL — CRACKED (ZONE 100) · airframe 113,205 hrs · 24,018 cycles

UPON REMOVAL OF O/B LH MLG BRACKET, CRACK FOUND AT MLG DOOR SEAL RETAINER SUPPORT CHANNEL AT FUS STA 1040 FROM LBL 3.0 TO LBL 63 .0 (REPAIR) REF: 124936 SDR REPORTING ONLY REMOVED AND REPLACED SEAL RETAINER SUPPORT CHANNEL IAW B757-200 SRM 51-40-02. VT MAE TRAVELER:T25/1806882.

Part: PANEL — CRACKED (ZONE 600) · airframe 113,205 hrs · 24,018 cycles

RIGHT WING GAP PANEL DAMAGED, BROKEN CORNER PART ON PANEL RACK BRACKET BROKEN IAW B757-200 SRM 51-40-02-0G-0. 03 NEW PARTS; 02 CORNER ANGLE#+25/1806839.

Part: FRAME SPLICE — GOUGED (ZONE 100) · airframe 113,205 hrs · 24,018 cycles

AFT CARGO COMP. FRAME SPLICE STA RH BTW STRG 23R-25R WITH GOUGES(3EA). ENTRY FOR SDR REPORTING FRAME SPLICE FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FRA ME SPLICE FABRICATED ON VT/MAE TRAV T25/1808559 IAW B757-200 SRM 53-00-07-1A-1 FIG 1 51-40-02

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 113,205 hrs · 24,018 cycles

(SUPPORT TASK) CLOSE ZONE 110: NLG W/W THROUGH ACCESS PANEL 117C L NOSE FWD FUSELAGE MAIN DECK FLOORBEAM CHANNEL STA 345 BL0 CRAC KED. SDR REPORTING ONLY REPAIRED MAIN DESK FLOOR STABILIZER IAW B757-2 SRM 53-00-51-2R-1 2 AND REMOVED AND REINSTALL PANEL 117CL TO FOM IAW B757-200 AMM 51-14-01.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 113,205 hrs · 24,018 cycles

UPON PRE-INSTALL INSPECTION, CRACK FOUND AT FWD CARGO FLOOR PANEL 121BF - REF: NRC 125014 6100577518 SDR REPORTING ONLY REPAIRED FWD CARGO DECK PLATE (121BF) IAW B757-200 SRM 51-70-13- 0G-0.

Part: STRINGER — DENTED (ZONE 200) · airframe 113,205 hrs · 24,018 cycles

(SDR) STRINGER HAS A DENT STA 1300 TO 1320 LBL 2.75. STRINGER FROM STA 1280 TO 1340 WAS REPAIRED DUE TO SRM B757-200 53-00-53 DOES NOT PERMIT DENT ON FLOOR STRINGER, AREA WAS REPAIR ED IAW B757-200 SRM 51-70-12 DETAIL VII

Part: FRAME — DENTED (ZONE 100) · airframe 113,205 hrs · 24,018 cycles

FRAME STA 1500 STR 26LH HAS A DENT. REPAIRED STA 1500 STR 26LH FRAME IAW B757-200 SRM 53-00-07-2R-S-DETAIL II. ACCOMPLIHSED ON VT NR 124726. INSPECTION THRESHOLD AT 37500 FLIGHT CYCLES AFTER REPAIR OR 50000 AIRCRAFT FLIGHT CYCLES WHICHEVER COMES FIRST. INSPECTION INTERVAL 12000 FLIGHT CYCLES PER CATEGORY B INSPECTION REQUIREMENTS. REF IS 53-00-07-2R-5. REPAIR 5. ACCOMPLISHED REPAIR PER SRM 53-00-7.

Part: FAIRING — DAMAGED (ZONE 100) · airframe 113,205 hrs · 24,018 cycles

(SDR) - LH WING-TO-BODY FAIRING 197BL HAS A FEW AFT SUPPORT CLIP FASTENER HOLES ELONGATED (OVER DRILLED) FROM RIVET REMOVALS WIT H 1EA RIVET NOT PUNCHED OUT ENTIRELY RESULTING IN A BENT ANGLE A ND POTENTIAL CRACK. REF: 124978 SDR REPORTING ONLY REMOVED AND REPLACED 1EA BRACKET BATCH #0004365522 P/N:2024-T3 . 040L IAW B757-200 SRM 51-40-02

Part: NUT PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 113,205 hrs · 24,018 cycles

(SDR) - (B757-06-3-0272) AT APU INLET INSIDE AFT TAIL COMPARTMEN T FWD INTERNAL NUTPLATE STRAP HAS CORROSION. DOT 140-009. REF: N RC 124486 SDR REPORTING PURPOSE ONLY REMOVED AND REPLACED NUT PLATE STRAPS IAW B757 SRM 57-40-02.

Part: ANGLE — DAMAGED (ZONE 100) · airframe 113,205 hrs · 24,018 cycles

(SDR) - LEFT WING SIDE OF BODY SPLICE INTERNAL LOWER METALIC ANG LE LOCATED BELOW OVERWING EMERGENCY EXIT HAS 02 PIECES OF SCREW STUCKED INTO NUT PLATE (02 EA). DOT 75-067 HA-75. REF: 124735 SDR REPORTING PURPOSE ONLY ANGLE LOCATED BELOW OVERWING EMRGENCY EXIT WAS REMOVED (2) NUT P LATES ELONGATED FOUND, RECIEVED NEW ANGLE FROM FAB SHOP TRAVELER # T25/1805177, WAS LOCATED AND DRILLED IAW B757-200 SRM 51-40-0 5, NEW ANGLE WAS TREATED AND PAINTED IAW B757-200 SRM 51-20-01, AMM 51-21-15, ANGLE WAS INSTALLED B757-200 SRM 51-40-02.

Part: CHANNEL — CRACKED (ZONE 100) · airframe 113,205 hrs · 24,018 cycles

(SDR) - RIGHT MAIN WHEEL WELL LEADING EDGE SEAL CRACKED, FROM OU T BOARD IN FRONT OF THE SECOND BRACKET. REF: NRC 124935 61005774 39 SDR REPORTING PURPOSE ONLY REMOVED AND REPLACED SUPPORT CHANNEL IAW B757 SRM 51-40-02.

Part: DOOR — CORRODED (ZONE 800) · corrosion level 2 · airframe 113,205 hrs · 24,018 cycles

(SDR) - EA5210-03219 REV B:4L DOOR UPPER GATE HAS CORROSION IN T HE POCKETS REF: NRC 124892 SDR REPORTING PURPOSE ONLY REMOVED AND REPLACED L4 DOOR UPPER GATE IAW B757 AMM 52-11-38-40 4-009.

Part: GATE — CORRODED (ZONE 800) · corrosion level 2 · airframe 113,205 hrs · 24,018 cycles

EA 5210-03219 REV B: R-2 DOOR UPPER GATE HAS CORROSION I N THE POCKETS. REMOVED AND REPLACED UPPER GATE AT R-2 DOOR IAW B757-200 AMM 52- 11-38-004-001 AND 52-11-38-404-009 AND ADJUSTMENT MUST BE PERFOR MED WITH EA 5210-03219 REVISION B.

Part: INTERCOSTAL — CORRODED (STA1480-1500) · corrosion level 2 · airframe 113,205 hrs · 24,018 cycles

CORROSION ON AFT CARGO COMP INTERCOSTAL CHORD BTW STA 1480-1500 STRG 126-127. REF: NRC 124913. INTERCOSTAL ANGLE WAS REMOVED, NEW IN TERCOSTAL ANGLE WAS RECIEVED WITH TRAVELER#T25/1805770 AND NEW I NTERCOSTAL ANGLE WAS INSTALLED I.A.W. B757-200 SRM 51-40-02. RII VERIFIED

Part: LIGHT — DETACHED (ZONE 200) · airframe 112,783 hrs · 23,911 cycles

SEAT 40C EMERGENCY PATH LIGHT HANGING FROM SEAT RESECURED LIGHT ASSY. OK TO CONTINUE.

Part: SLIDE — FAULTY (ZONE 800) · airframe 112,495 hrs · 23,834 cycles

REMOVED R1 DOOR SLIDE REMOVED AND REPLACED R1 DOOR SLIDE IAW AMM 25-66-01. PARTS USED: 19-2566-9-0002, QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1375666 SN OFF 0965.SLIDE, B757-200 OFF 19-2566-9-0002 0965 ON 19-2566-9-0002 5075 RII INSPECTION REQUIREMENTS C/W.

Part: ACTUATOR — MISINSTALLED (ZONE 100) · airframe 112,336 hrs · 23,793 cycles

FOUND AILERON TRIM ACTUATOR INSTALLED INCORRECTLY, BARREL NUT RETAINER MISSING. CORRECTLY REINSTALLED BOLT RETERNER IAW AMM 27-11-14-022-008.

Part: SCREEN — FAULTED (BLEED VALVE) · airframe 111,807 hrs · 23,665 cycles

PDA 2 ON E2 AT 9OCLOCK POSITION. DISCOVERED MISSING ATTENUATOR SCREEN. EWR REPORTED E1 LEFT BLEED VALVE ATTENUATION SCREEN IS MISSING. NO IDEA WHEN IT MAY HAVE DEPARTED THE ENGINE. IT MEASURES APPROX 6 INCH DIAMETER (28.27 INSQ). PER THE GMM 2-30-95 THIS IS A CAT 1 PDA.

Part: GOVERNOR — FAULTY (ENG FUEL FLOW) · airframe 111,785 hrs · 23,662 cycles

RIGHT ENGINE EGT EXCEEDANCE ON CLIMB, CREW REPORTED POWER REQUIRED REDUCTION TO LIMIT EGT. CHECK INLET AND EXHAUST AND CHECK EXCEEDANCE PER FIM 71-05 TASK 824 AND FIM 71-05 TASK 819. EICAS ENGINE EXCEEDANCE REPORT VERIFIED RIGHT ENGINE EGT REACHED A MAX TEMP OF 883 FOR 1.8 SECONDS REF FIM 71-05 FAULT TREE 824 FIGURE 121NO ACTION REQUIRED. SEE LOGPAGE 9323021 FOR RIGHT ENGINE FFG REPLACEMENT AND DEFECT RECTIFICATION.ACCOMPLISH IDT INSPECTION OF RIGHT ENGINE FUEL FLOW GOVERNER REPLACEMENT INCLUDING, LOCKING, CORRECT PARTS, RIGGING AND TRIM. AS PER AMM 73-21-01-404-013-R04 AND GMM 09-10-05. DURING FFG REPLACEMENT PER AMM 73-21-01-404-013-R04, STEP K. EPR P1 SYSTEM TEST WAS SKIPPED REFERENCE EC/RA 7711-01049. ALL P1 SYSTEM B NUTS VERIFIED TO BE SECURE PER AMM SPECIFICATIONS. GOVERNOR, FUEL OFF 53-7321-9-0001 3146 ON 0000 GOVERNOR, FUEL OFF 53-7321-9-0001 3146 ON 53-7321-9-0001 4892 RIGHT ENGINE FUEL FLOW GOVERNER REMOVED AND REPLACED AS PER AMM 73-21-01-404-013-R04. HIGH POWER ENGINE RUNS CARRIED OUT. ALL PERAMETERS NOW NORMAL AND ENGINE FOLLOWS THRUST LEVER INPUTS. PARTS USED: 99-7311-3-0006,QTY :1 99-7311-3-0008,QTY :1 53-7321-9-0001,QTY :1 19-7261-3-0019,QTY :1 19-7311-3-0054,QTY :1 99-7311-3-0004,QTY :1 19-7261-3-0010,QTY :1 1561368,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1561368 SN OFF 3146

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 111,757 hrs · 23,655 cycles

PASSENGER DOOR GIRT BAR SLIDING MECHANISM LUBRICATE {B757-52-3-0071} - DURING INSPECTION OF L-1 DOOR ASSIST BOTTLES, FOUND PLUMBING LINE AND BOTTLE CAPED. REPLACED RESERVOIR BOTTLE PER AMM 52-11-30/401.FUNCTIONS DURING AN ACTUAL EMERGENCY OR DURING TRAINING, TESTING, MAINTENANCE, DEMONSTRATIONS, OR INADVERTENT DEPLOYMENTS.

Part: TIRE — FAILED (NR 5) · airframe 110,972 hrs · 23,500 cycles

#5 MLG TIRE BLOWN ON LANDING. REMOVED AND REPLACED #5 MAIN TIRE IAW BOEING 757 AMM 32-45-01.

Part: RADOME — DELAMINATED (NOSE) · airframe 110,494 hrs · 23,403 cycles

REVIEW ALL DISCREPANCIES RECORDED AND INITIATE SFR/SDR REPORTS AS REQUIRED. {B757-05-3-0003} - SDR TO BE RAISED POST RADOME REPLACEMENT DUE AIRCRAFT BEING OUT OF SERVICE PER GMM 04-20-16 PER GMM 04-20-16 SDR BEING RAISED DUE TO AIRCRAFT BEING OUT OF SERVICE AT AGP. REPORT OF BIRDSTRIKE TO RADOME ON APPROACH TO AGP (LOG PAGE 8125424) CREATING DELAM TO RADOME THAT WAS OUT OF LIMITS. RADOME REPLACEMENT CURRENTLY IN PROGRESS. RETURN TO SERVICE EXPECTED 03-JUN-24

Part: SLAT — TORN (RH WING) · airframe 110,032 hrs · 23,304 cycles

RT WING INBD SLAT T/E TORN. 4 FT X 1 FT SECT SKIN RIPPED OFF HNY COMB EXPOSED AND MISSING SLAT INSTL-WING LE NO. 5 AND NO. 6 INBD REFERENCE: 27-81-01-01 PHOTOS LABOR HOUR AND GROUND TIME INFORMATION UPDATE ONLY. PART ORDERED, REMOVED NO.6 INBOARD LE SLAT IN REFERENCE TO AMM.

Part: GOVERNOR — FAULTY (ENG#2) · airframe 110,023 hrs · 23,302 cycles

NUM 2 ENG GAVE PARTIAL POWER AT CRUISE EPR INDICATED 1.3 APROX 3 0 PERC LOSS TPU BITE SHOWED FAULT CODE 20 PCC/GR TEST FAULT. BVCU BITE SHOWED FAULT CODE 06 PCU1 FAULTY. EEC BITE SHOWED NO FAULTS. REF LOG PAGE 7094082, REPLACED #2 ENG FFG, HP FUEL PUMP, & LP FUEL PUMP. ALL REQUIRED POWERPLANT REFERENCE TEST #1,2,9,10,& 11 PASSED IN REF TO AMM TASK 71-00-00-700-804-R03. DUE TO #2 ENGINE DEGRADED PERFORMANCE REPLACE LP PUMP PER AMM 73-11-01, HP PUMP PER 73-11-03 AND FFG PER AMM 73-21-01. TOMC-MEREDITH VERIFIED REPLACEMENT OF O RINGS, SEAL AND CORRECT PART NUMBERS OF LP FUEL PUMP,HP FUEL PUMP AND FFG PER IPC 73-11-01-01, 73-11-03-01, 73-21-01-01 AND GMM 09-10-05. OK TO INSTALL. ROTABLE PARTS CHANGE UPDATE FOR LP FUEL PUMP, HP FUEL PUMP, & FFG. REQUIRES LEAK CHECKS & OPERATIONAL CHECKS. INSPECTED LP FUEL PUMP, HP FUEL PUMP AND FFG FOR CORRECTS ADJUSTMENT(RIG),SECURITY, TRIM ADJUSTMENTS,PROPER SAFETY AND LEAK CHECKS PER AMM

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 109,631 hrs · 23,206 cycles

DEBRIEFED CREW, DEPRESSURIZATION PROBLEM OCCURED IN CABIN PRESSURIZATION POSITION AUTO 2 MODE WHEN CLIMBING FROM 36,000 TO 38000 FEET WITH ASSOCIATED RED ALARM LIGHT. CREW SWITCHED TO AUTO 1 MODE AND PREPARED TO CONDUCT EMERGENCY DESCENT. AUTO 1 APPEARED TO OPERATE SATISFACTORY PERFORMED BITE CHECK OF CABIN PRESS CONTROLLER 2 IN FWD PIT. NO FAULTS. FWD PIT OPEN FOR CONTROLLER REPLACEMENT. REF AMM21-31-00 REMOVED AND REPLACED #2 AUTO CABIN PRESSURE CONTROLLER REF AMM 21-31-02. BITE CHECK GOOD. FOLLOWED FIM CODE 21 30 20 00 (21-30 FAULT TREE 802). NO FAULTS WERE NOTED, AUTO CABIN PRESSURE CONTROLLER #2 WAS REPLACED AS PRECUATIONARY. IPC REFERENCE # 25-71-91-21N REF LP 6750468, ACPD PRESS CONTRL SYS TEST GOOD IAW AMM 21-31-00-735-023 AND THE CAB PRESS INDICATION AND WARNING TEST GOOD IAW AMM 21-31-00-735-001. CONTROLLER, CAB OFF 19-2131-9-0004 9353 ON 19-2131-9-0004 0178 CONTROLLER, CAB OFF 19-2131-9-0004 9353 ON 0000.

Part: COOLER — UNKNOWN (ENGINE #1) · airframe 109,122 hrs · 23,081 cycles

AFTER TAKEOFF LAV SMOKE EICAS FOLLOWED 30 SECOND BY LEFT ENG HI GH OIL TEM P IN RED. THROTTLE T. CONT... MID POS CLEARED HIGH OIL TEMP AND LAV SMOKE RESET 2 MIN S LATER FLT DECK AND CABIN HAD UPON INSPECTION OF ENGINE 1 FOUND OIL LEAKING OF TUBE COMING FROM THE OIL INLET TUBE OF THE FUEL-OIL HEAT EXCHANGER TO THE BYPASS OIL VALVE. LEAK SMELLS LIKE MIX OF JET A FUEL AND 2197. PERFORMED PACK BURNOUT REF AMM 21-00-01-002-001 NO OIL OR FUEL SMELL AND NO VISIBLE SMOKE IN FLIGHT DECK OR CABIN. REF L/P 6366466 FOR RECIRC FILTER REPLACEMENT. NEED TO REPLACE RE-CIRCULATION FILTERS FOR SMOKE IN THE CABIN PER AMM 05-51-58-910-801-C1 , ITEM 1 E . FILTERS M&E 29-2124-3-0006 REPLACED RECIRC HEPA FILTERS REF MM 21-25-02-404-174 PARTS USED: 29-2124-3-0006,QTY :1. #1 ENG , REF FIM 71-05 FAULT TREE 828 ENG OIL/FUEL SMELL IN CABIN : SIGNS OF OIL LEAKAGE ,AT THE LP COMP BLADES, IPC IGV''S AND STAGE 1 BLADES ( BLOCK 3) . REMOVED THE OIL TANK FILLER CAP FUEL FUMES WHERE PRESENT AND THE OIL TANK LEVEL HIGH ( BLOCK 6). NEED TO REPLACE RE-CIRCULATION FILTERS FOR SMOKE IN THE CABIN PER AMM 05-51-58-910-801-C1 , ITEM 1 E . FILTERS M&E 29-2124-3-0006 REPLACED RECIRC HEPA FILTERS REF MM 21-25-02-404-174 PARTS USED: 29-2124-3-0006,QTY :1. PERFORMED LEAK CHECK OF FCOC. NO LEAKS DETECTED. REMOVED OIL FILTER DRAIN PLUG TO DRAIN SYSTEM. INSTALLED OIL FILTER DRAIN PLUG. REF. AMM 79-21-07. LEAK TEST REQUIRED. PERFORMED LEAK CHECK. NO LEAKS DETECTED. NEED TO FLUSH OIL TANK SYSTEM PER TOMC REQUEST. AND TH

Part: HOSE — DAMAGED (NLG) · airframe 108,360 hrs · 22,915 cycles

AFTER T/O GEAR DID NOT RETRACT CYCLED GEAR LEVER AND NOTICED L HYD QTY ECAM FOUND HOSE ASSY, PLUMBING P/N AS115-08K0322 FOR HYDRAULIC SYSTEM DAMAGED AND LEAKING HYDRAULIC FLUID AT NLG. REPLACED HOSE ASSY REF AMM 20-11-00 LEAK CHECK GOOD. PERFORMED OPERATIONAL TEST - NOSE LANDING GEAR EXTENSION AND RETRACTION, OPS CHECK NORMAL REF AMM 32-34-00-715-017 ADD EMP:U031804,U077346. PART USED: 19-3234-3-0020.

Part: TAT PROBE — INOPERATIVE (UNKNOWN) · airframe 107,689 hrs · 22,788 cycles

TAT PROBE ANNCTR IN FLT UPDATING WITH INDICATED FAULTS. REPLACED THE TAT PROBE REF. MM 34-12-02. PROBE GROUND CHECKS GOOD. ADD EMP:404924

Part: ENGINE — BIRD INGESTION (ENGINE) · airframe 106,104 hrs · 22,440 cycles

BIRDSTRIKE ON TAKEOFF PERFORM BIRDSTRIKE CONDITIONAL INSPECTION PER AMM PILOT REPORTS ON TAKE OFF RIGHT AT V1 THEY SUPECTED A BIRD 05-51-18-212-001 STRIKE ON E1, ALL CONTROLS FELT NORMAL NO SURGE OR VIBRATION, BUT DID SMELL SOMETHING, PILOT CALLED AIRPORT OPS TO INSPECT RUNWAY AND BIRD REMAINS SEEMED APPARENT PERFORMED INSPECTION 05-51-18-219-001 ,EVIDENCE OF BS # 1 ENGINE, NO DAMAGE NOTED ON FUSLAGE,REF LG PG 3299134 FOR FOLLOW UP REF FIM 71-05-FAULT TREE 803

Part: ACTUATOR — INOPERATIVE (SEAT ROW 20L/H &) · airframe 104,311 hrs · 22,024 cycles

SUPPORT TASK> PAX O2 MASKS FAILED TO DEPLOY AT SEAT ROW 37R/H AN D 20L/H. TRANSCRIBED FROM NR 9283870, HAECO NR 43870 REMOVED & REPLACED O2 DOOR ACTUATORS AT SEAT ROWS 20 L/H & 37 R/ H IAW UA B757-200 AMM 35-21-06. OPS CHECK VERIFIED GOOD IAW UAL B757-200 AMM 35-21-00 & AMM 25-23-01-404-021 STEP 3.D(9).

Part: BEAM — CORRODED (BL 0 AND LBL54) · airframe 104,312 hrs · 22,024 cycles

SUPPORT TASK MAIN CABIN FLOOR BEAM 1681 CORRODED UNDER AFT DECK PRESSURE PLATE BETWEEN BL 0 AND LBL 54, TRANSCRIBED FROM HAECO G SO NR 9283143 TRANSCRIBED FROM HAECO LP 9283143. REPAIRED IAW ECRA 5365-01097.

Part: SKIN — CORRODED (LBL10 TO LBL15) · airframe 104,312 hrs · 22,024 cycles

(SUPPORT TASK) EMPENNAGE INTERIOR FUSELAGE SKIN HAS CORROSION BE TWEEN BS1838 AND BS1850 LBL10 TO LBL15 STREAMER ATTACH. TRANSCRI BED FROM HAECO GSO NR 9282270 TRANSCRIBED FROM HAECO LP 9282270. FABRICATED REPAIR FILLER AND DOUBLER AND STRAP; INSTALLED REPAIR IAW REO G23724 AND B757-200 SRM51-40-02 REF ECRA 5381-01016.

Part: SKIN — DENTED (RH I/B FLAP) · airframe 104,312 hrs · 22,024 cycles

REF L/P# 8336284 REMEASURED DENT AT R/H INBOARD MAIN FLAP LOWER SURFACE. DENT MEASURES .375" WIDE BY .030 DEEP UPON FURTHER EVALUATION MEASURED DENT TO BE 2.25 BY .030 A/Y=75, NO FURTHER ACTION REQUIRED SRM 57-53-01 ALLOWABLE DAMAG E 1, DETAIL VII INSPECTED AREA, FOUND DENT TO BE WITHIN LIMITS IAW B757 SRM 57-5 3-01 FIG. 101 DETAO; VII. WORK PERFORMED BY EMP# 62827 P. MOSELE Y REINSPECTED R/H INBD MAIN FLAP LOWER AREA STA. 215. DENT 2.5X 0.065=38.5. WITHIN LIMITS IAW SRM57-53-01 DETAIL V11 REMEASURED DENT AT R/H I/B MAIN FLAP LOWER SURFACE AS PER B757-2 SRM 57-53-01, FIG 101 DETAIL VII, FOUND TO BE WITHIN LIMITS A=2.030" Y=.029" A/Y=70. LOG PAGE WAS CONVERTED TO ELB FORMAT ON JUN 17, 2016 AT 10250792 WORK PERFORMED AT ST-SAA. WORK ACCOMPLISHED BY V920993 AND INSPE CTED BY V919676. VISUALLY INSPECTED DENT AT RH INBD MAIN FLAP LOWER SURFACE AS DE SCRIBED. NO FURTHER DAMAGE AND NO CHANGE IN DENT CONDITION IAW B 757-200 SRM 57-53-01 FIG 101 DETAIL VII. DMG REMAINS. REEVALUATED DENT ON RT I/B MAIN FLAP LOWER SURFACE (W=.375", Y=. 007", A/Y=5.6) AND FOUND TO BE OUT OF LIMITS PER B757-20 SRM 57- 53-01-1A-1. DENT REPAIRED ON UNITED NON ROUTINE # 9282190. HAECO MECH V895396.

Part: SKIN — GOUGED (FLAP LE) · airframe 104,312 hrs · 22,024 cycles

B757-06-3-0318/LW I/B MAIN FLAP LE HAS GOUGED SKIN STREAMER ATTA CH TRANSCRIBED FROM HAECO GSO NR 9282892. DOT:X170

Part: INTERCOSTAL — NONE (L4 DOOR) · airframe 104,312 hrs · 22,024 cycles

(B757-53-3-0531) L4 DOOR FLOORBOARD SUPPORT INTERCOSTAL COMMON T O DOOR SILL CORRODED AT FASTENER HOLE. TRANSCRIBED FROM HAECO G SO NRC 9282975

Part: NONE — NONE (STA1681-1700) · airframe 104,312 hrs · 22,024 cycles

(SUPPORT TASK) MAIN CABIN AFT DECK PRESSURE PLATE GOUGED BETWEEN STA 1681-1700 LBL24, TRANSCRIBED FROM HAECO GSO NRC 9283144

Part: NONE — NONE (BS1715RBL13) · airframe 104,312 hrs · 22,024 cycles

B757-53-3-0575- CABIN FLOOR WEB HAS CORRODED SPOTS BS 1715 BL L3 5-BL RBL13, TRANSCRIBED FROM HAECO GSO NRC 9283419

Part: BEAM — CORRODED (STA345) · airframe 104,312 hrs · 22,024 cycles

(SUPPORT TASK) MAIN CABIN STA 345 FLOORBEAM HAS CORROSION ON UPP ER SURFACE LBL10-LBL15, TRANSCRIBED FROM HAECO GSO NRC 9283462

Part: FLOOR SUPPORT — CORRODED (STA324-345LBL15) · airframe 104,312 hrs · 22,024 cycles

(SUPPORT TASK) MAIN CABIN STA 324-345 LBL15 INTERCOSTAL HAS CORR OSION ON UPPER SURFACE, TRANSCRIBED FROM HAECO GSO NRC 9283461

Part: FLOOR SUPPORT — CORRODED (BS1640) · airframe 104,312 hrs · 22,024 cycles

B757-53-3-0576/CBN FLOOR BEAM T-CAP HAS CORROSION AT FASTENER HO LES BS 1640 BL225-BL-R46. TRANSCRIBED FROM HAECO GSO NR 9283413. REMOVED, FABRICATED AND INSTALLED T-CHORD PN.BAC1505-100880 7075 PO#1020405.1, AT CBN FLOOR BEAM STA 1640 BLR10-BLL39 IAW B757-20 -T6511 PO#1024748.1, 4 EACH ANGLES. -1 PN BAC1490-2832 PO#874714 0 SRM 53-00-51-2R-10 REPAIR SRM 51-40-02/APPLIED CIC IAW B757-20 .3, -2 PN.BAC1490-2793 PO#904570.1, 4 EACH STRAPS, -3 IS .071 70 0 AMM 51-24-03-377-008. HAECO GSO MECH V934680 INSP QC418 75-T6 CLAD PO#1016024.1, -4 IS .063 7075-T6 CLAD

Part: FLOOR SUPPORT — CORRODED (R4 DOOR) · airframe 104,312 hrs · 22,024 cycles

(B757-53-3-0531) R4 DOOR-FLOORBOARD SUPPORT INTERCOSTAL COMMON T O DOOR SILL STRUCTURE-CORROSION AROUND TWO FASTENER HOLES. TRAN SCRIBED FROM HAECO GSO NRC 9282974

Part: SKIN — CRACKED (L4 DOOR) · airframe 104,312 hrs · 22,024 cycles

(SUPPORT TASK} L-4 DOOR INNER SKIN LOWER HINGE ARM LIGHTENING HO LE IS CRACKED. TRANSCRIBED FROM HAECO GSO TASK CARD 9283246

Part: SKIN — DENTED (LH ELEVATOR) · airframe 104,312 hrs · 22,024 cycles

B757-06-3-0270 LH ELEVATOR LOWER SURFACE HAS 2 EACH DENTS BETWEE N ELE STA 200 AND ELE STA 312.673 MARKED, TRANSCRIBED FROM HAECO GSO NON ROUTINE 9282300 REPAIRED DENTS ON LH ELEVATOR LOWER SURFACE IAW B757 SRM 55-20-0 1-2R-1 AND 51-70-17-0G-0. HAECO GSO MECH V894897 INSP QC357

Part: SKIN — DENTED (BS 600) · airframe 102,006 hrs · 21,452 cycles

THE LOWER FUSELAGE HAS A DENT AT THE 6 O CLOCK POSITION BELOW THE FORWARD CARGO DOOR S-29L TO 29R (BETWEEN STA 580 - 600) DOT 48-003 REF AAR N/R 9733007 EVALUATED DENT AT LOWER FUSELAGE SKIN BETWEEN STA 580 & STA 600 S-29L TO S-29R DENT MEASURES L=2.300" W=1.600" Y=.058" W/Y=.027 FOUND TO BE IN LIMITS REF. SRM 53-00-01. ACCOMPLISHED REPAIR AT LOWER FUSELAGE SKIN BETWEEN 580 AND STA 600 FROM ADD EMP:V898225 29L TO S-29R REF. B757-200 SRM 53-00-01 FIG. 201 DETAIL I. RII INSPECTION IS ACCOMPLISHED BY AAR INSP 82 DENT MEASURES L=2.300" W=1.600" Y=.058" W/Y=.027 FOUND TO BE OUT OF LIMITS REF. SRM 53-00-01. ACCOMPLISHED REPAIR AT LOWER FUSELAGE SKIN BETWEEN 580 AND STA 600 FROM 29L TO S-29R REF. B757-200 SRM 53-00-01 FIG. 201 DETAIL I. ADD EMP:V898225

Part: GIRT BAR — WORN (L4 DOOR) · airframe 98,214 hrs · 20,648 cycles

(SUPPORT TASK) (AD 2006-22-01) L-4 PASSENGER DOOR GIRT BAR SLIDER FAILED ENGAEMENT DIMENSION AND REQUIRES REPLACEMENT. REF N/R 0040116. REMOVED AND REPLACED L-4 PASSENGER DOOR GIRT BAR SLIDER IAW AMM 25-66-10-402-022. ADJUSTMENT TO BE DONE ON JOB CARD EA 52 12-01364 REV G. SEQ NO. 492, STEP 53.5. AND JOB CARD EA2560-0212 3 REVD SEQ NO 408 STEPS 2.7 AND 2.8. WORK ACCOMPLISHED BY AND INSPECTED. INSPECTION COMPLETED AND ACCEPTED.

Part: GIRT BAR — WORN (R4 DOOR) · airframe 98,214 hrs · 20,648 cycles

(SUPPORT TASK)(AD 2006-22-01) R-4 PASSENGER DOOR AFT LEAF SPRING FAILED TO HOLD GIRT BAR SLIDER DURING INSP.REF N/R 00401 20 REMOVED AND REPLACED R4 PASSENGER DOOR GIRT BAR SLIDER IAW AMM 25-66-10-402-022 ADJUSTMENT TO BE DONE ON JOB CARD EA 5210 -01364 REV G SEQ 494 STEP 53.5 AND JOB CARD EA 2560-02123 REV D SEQ 411 STEP 2.7. WORK WAS ACCOMPLISHED, INSPECTED.

Part: FRAME — DENTED (FUSELAGE) · airframe 98,214 hrs · 20,648 cycles

B757-06-3-0230 2EA DENTS ON AFT CARGO LT FRAME UPPER FLANGE AT S TA 1520 BETWEEN STR 25L-26L. RG21. REF N/R 0040325. -26L FOUND OUT OF LIMITS IAW SRM 53-00-07-A1 L= 1.0, W= .5, D= .032. CUT OUT DAMAGES AND ACCOMPLISHED PERMANENT REPAIR IAW SRM 53-00-07-R5 WITH REPEAT INSPECTION ZONE 1 AT 50 ,000 F/C AND INTERVAL 12,000 F/C PER TABLE 2 FIG 201 PG 211. CUR AFT CARGO FRAME UPPER FLANGE DENT AT STA 1520 BETWEEN 5-25L TO 5 RENT F/C 20648 SEE CONT FORM: 850771. REPAIRED PER SRM 53-00-07 REPAIR 5 REQUIRES REINSPECT PER CAT B TABLE II ZONE 1 M 50000 AIRFRAME FLIGHT CYCLES RII INSPECTION C/W BY ONSITE INSP. TOMC APPROVES PERMANENT REPAIR OF AFT CARGO FRAME UPPER FLANGE DENT AT STA 1520 BETWEEN 5-25L TO 5-26L PER SRM 53-00-07 REPAIR 5 WITH THE FOLLOWING INSPECTION REQUIREMENTS REF TABLE II.

Part: UNKNOWN — UNKNOWN (L4 DOOR) · airframe 94,505 hrs · 19,896 cycles

L4 DOOR WILL NOT DISARM. CHECKED THE DOOR ESCAPE SLIDE ARM - DISARM OPERATION IAW AMM 25-66-01-404-044, STEP I. (6) NO DEFECTS NOTED. OK TO CONTINUE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 93,698 hrs · 19,714 cycles

SEAT ROW 21DEF EMERGENCY EXIT AFT LIGHT INOPERATIVE. REPLACED SEAT ROW 21DEF AFT EMERGENCY EXIT LIGHT BULB IAW AMM 33 -21-30.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 92,900 hrs · 19,553 cycles

EXTERIOR AFT CARGO DOOR EMERGENCY LIGHT INOP. RELAMPED EXTERIOR AFT CARGO DOOR EMERGENCY LIGHT. OPS CHECK GOO D.

Part: GUARD — FAULTY (LIGHT SWITCH) · airframe 92,626 hrs · 19,496 cycles

EMERGENCY LIGHT SWITCH ON OVERHEAD PANEL DOES NOT MOVE TO ARMED POSITION WHEN GUARD IS CLOSED. REPLACED THE SWITCH GUARD

Part: LIGHT — DIRTY (R1 DOOR) · airframe 92,445 hrs · 19,464 cycles

DOOR 1R SLIDE ARMED LIGHT BULB INOP. REMOVED IT AND CLEANED IT, CHECKED GOOD. A/C OK TO CONT.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 92,313 hrs · 19,441 cycles

SLIDE LITE BULB BURNED OUT DOOR 1R. RELAMPED SLIDE ARMED LIGHT IAW AMM CH 33-51-00. OPS CHECK GOOD.

Part: HANDLE — OUT OF ADJUST (R1 DOOR) · airframe 92,313 hrs · 19,441 cycles

DOOR 1R SLIDE ARM LIGHT INOP. RESET DOOR HANDLE. CKS GD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 91,838 hrs · 19,347 cycles

SINGLE BULB INOPERATIVE IN EMERGENCY EXIT LIGHTS. REPLACED THE LAMPS. CHECKED OK.

Part: SEQUENCE VALVE — UNSERVICEABLE (NLG) · airframe 90,325 hrs · 19,041 cycles

GEAR DISAGREE ON EICAS, HAD TO MANUALLY OVERRIDE TO LOWER NOSE GEAR PER QRH. PERFORMED NORMAL OPERATION CHECK OF MLG NUMEROUS TIMES WITH NO FAULTS OR ABNORMAL OPS, REF AMM 32-32-00. PER TOMC REQUEST REMOVED AND REPLACED NLG OPERATED SEQUENCE VALVE, REF AMM 32-34-06, OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 89,093 hrs · 18,784 cycles

R1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. SEATED THE BULB. OPS CHECKED GOOD IAW MM 33-51-06

Part: MONITOR — INOPERATIVE (LT ENGINE) · airframe 86,894 hrs · 18,354 cycles

LEFT VIBRATION INDICATOR INOPERATIVE AFTER TAKEOFF. R & R NR 1 ENG VIB MONITOR IAW AMM 77-31-03. OPERATIONS CHECKED GOOD. VERIFIED EICAS INDICATIONS NORMAL. OK FOR SERVICE. ROTABLE PARTS CHANGE WAS INDICATED TT 1805237, SN OFF 00011 MONITOR, ENG OFF 19-7731-9-0001 0011, ON 19-7731-9-0001 8089.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,679 hrs · 18,307 cycles

OVERHEAD BIN AISLE EMER LIGHTS INOPERATIVE AT POSITIONS 4R, 12L, 12R, 37R & 35L. RELAMPED OVERHEAD BINS AISLE EMER LIGHTS IAW AMM 33-51-05 & TESTED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,679 hrs · 18,307 cycles

EPL LIGHTS AT SEAT ROWS 7L, 20L, 24L, 32L, 33L, 35L, 36L & 37L INOPERATIVE. EPL LIGHTS RELAMPED LIGHTS IAW AMM 33-51-11 & TESTED NORMAL.

Part: CREASE BEAM — CORRODED (BS 430) · airframe 86,679 hrs · 18,307 cycles

OUTER CREASE BEAM CORRODED STATION 430 RT. R & R CREASE BEAM RT SIDE, BETWEEN BS 430 - BS 450 IAW SRM 51-40-02, PN BAC1515-53 2024 T35.

Part: FLOORBEAM — CORRODED (BS 1681) · airframe 86,679 hrs · 18,307 cycles

AFT CABIN PAX AT WET AREA ON BS 1681, LBL 40, FLOORBEAM UPPER FWD FLANGE HAS EXFOLIATION CORROSION. REMOVED CORROSION ON FLOORBEAM, FOUND BEYOND LIMITS. FABRICATED REPAIR STRAP, ANGLES & FILLER. TREATED, PRIMED & TOP COATED PARTS. REWORKED AREAS & INSTALLED REPAIR PARTS ON FLOORBEAM IAW SRM 53-60-51 REPAIR 3 DETAIL I ES 2009602-23 & ECRA 5310-06691.

Part: DECK PLATE — CORRODED (FUSELAGE) · airframe 86,679 hrs · 18,307 cycles

AFT CABIN FLOOR STRUCTURE & AREA BELOW THE FLOOR LT STATION 1681, BETWEEN LBL 0 & LBL 60, SUBFLOOR SHOWS EVIDENCE OF SURFACE CORROSION. REMOVED CORROSION ON DECK PLATE, STATION 1681, LBL 12, LBL 24, LBL 40 X LBL 48, MAT LOST LBL 12 .031, LBL24, .016,LBL 40 .018 & AREAS BEYOND LIMITS LBL 48, .005 WITHIN LIMITS IAW SRM 53-60-51 FIG 101. FABRICATED REPAIR DOUBLER IAW SRM 53-60-51 REP 2. TREATED, PRIMED & TOP COATED AREAS IAW AMM 51-21-04.

Part: OVEN — FIRE (GALLEY) · airframe 83,556 hrs · 17,749 cycles

OVEN FIRE IN FWD GALLEY OVEN 204, FLIGHT ATTENDANT PULLED CB & FIRE WENT OUT, VERY LITTLE SMOKE. CREW MEAL BURNED. REPLACED OVEN, NEW OVEN OPERATIONS NORMAL. ROTABLE PARTS CHANGE WAS INDICATED, TT 1711707, SN OFF 00794 OVEN, SMALL SG OFF 99-2532-9-0003 0794 ON 99-2532-9-0003 0560.

Part: CONTROL UNIT — MALFUNCTIONED (ELEC BAY) · airframe 75,339 hrs · 16,253 cycles

INFLIGHT AT FL350, BOTH LT & RT UTILITY BUSS AMBER LIGHTS CYCLED ON AND OFF 4 TIMES IN A 30 MINUTE PERIOD. DIVERTED BACK TO DEPARTURE. TROUBLESHOT IAW FIM 24-20-00, FOUND BPCU INTERMITTENT. R & R BPCU IAW AMM 24-41-03-404-008. UTILITY BUSS SYS OPS CHECKED NORMAL IAW AMM 24-22-00. ACFT OK TO CONTINUE.

Part: FRAME — DAMAGED (BS 205.59) · airframe 52,709 hrs · 11,956 cycles

FUSELAGE FRAME BS 205.59 DAMAGED. REWORKED FRAME, INSPECTED AND FOUND NO CRACKS, AND INSTALLED A REPAIR ANGLE DOUBLER REF. ECRA 5310-04640 REV A, PART 1.

Part: TRANSMITTER — FAILED (TE FLAPS) · airframe 74,432 hrs · 16,103 cycles

SPLIT FLAPS. FLAPS EXTEND NORMALLY TO 20 DEG. FROM 20 TO 25 L F LAPS STAY AT 20 R FLAPS EXTEND NORMALLY TO 25 DEG. NO EICAS MES SAGE. FLAPS DO NOT LOCK OUT. MULTIPLE PREVIOUS WRITEUPS. REPLACED T/E FLAP POSITION TRANSMITTER IAW AMM 27-58-03-424-015 AND AMM 27-58-01-715-112. OPS CHECK NORMAL AT THIS TIME.. ROTABLE PARTS CHANGE WAS INDICATED - TT 1538552, SN OFF 00794 TRANSMITTER, T/ OFF 19-2751-9-0015 0794 ON 19-2751-9-0015 0686.

Part: PCU — MALFUNCTIONED (E&E BAY) · airframe 71,073 hrs · 15,522 cycles

WHEN IN TURBULENCE, UTILITY BUS DROPS OFF LINE AND THEN BACK ON MOMENTARILY. FLIGHT ATTENDANTS COMPLAIN OF OVENS, LIGHTS AND VIDEO SYSTEM GO OFF/ON AS WELL, MASTER CAUTION (L UTIL BUS) (R UTIL BUS) OVERHEAD UTILITY BUS LIGHT ON & R REC LIGHT (CONTINUOUS DURING TURBULENCE). T/S PER WDM 24-51-15 AND FIM TASK 24-51-00-815-802 REMOVED AND REPLACED K10109 AND REMOVED AND REPLACED BUS POWER CONTROL UNIT. LEFT AND RIGHT UTILITY BUSSES CHECK NORMAL NO FAULTS NOTED. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1458101 SN OFF 02250 CONTROL, BUS PO OFF 99-2441-9-0001 2250 ON 99-2441-9-0001 2315.

Part: HOSE — LEAKING (LAVATORY) · airframe 70,768 hrs · 15,468 cycles

BLUE LAV FLUID LEAKING ON TO FLOOR IN FWD LAV. ONLY LEAKING IF FLUSH MOTOR IS RUNNING. LEAKING INTO FLT DECK ON LANDING REMOVED SHROUD AND CLEANED UP FLUID. FOUND ONLY LEAK TO BE DURING FILL, NO OTHER LEAKS FOUND. PLACARD FIRST CLASS LAV FILL SYSTEM INOP. REQUIRES MANUAL FILL. HOSE FROM FILL VALVE TO FLUSH MOTOR LEAKING. NEEDS 19-3832-3-01 00. NIS EWR EXT#115992 REF L/P 8936817 FOR CORRECTIVE ACTION.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 69,749 hrs · 15,287 cycles

T/E FLAP DISAGREE ON SHORT FINAL. RAN CHECKLIST, LANDED FLAP S 20. NORMAL LANDING. CYCLED FLAPS SEVERAL TIMES. NO DEFECTS NOTED. OK TO CONTINUE.

Part: CONTROL PANEL — FAILED (COCKPIT) · airframe 68,475 hrs · 15,055 cycles

STARTING TAXI LOUD POP & ELECTRICAL ARC & EL SMELL IN COCKPIT L GEN CONTROL BREAKER POPPED W/ NR 2 ELECTRIC HYDRAULIC INOP LIGHT ON (NO C/B POPPED) TAXI BACK TO GATE REMOVED & REPLACED ELECTRIC CONTROL PANEL PER MM 24-22-01 OPS CHECK NORMAL PERFORMED ENG RUN UP ON BOTH GENERATORS OPS CHECK CHECK NORMAL NO ABNORMAL SMELL OR DEFECT NOTED IN COCKPIT REFER TO L/P 8797562 FOR NR 1 GEN WILL NOT COME ON LINE. AUTOMATIC MUST BE MANUALLY RESET. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1449878 S/N OFF 01374 PANEL, ELECTRIC OFF 19-3112-9-0018 1374, ON 19-3112-9-0018 1625.

Part: SMOKE DETECTOR — MALFUNCTIONED (E&E BAY) · airframe 68,163 hrs · 15,000 cycles

DURING DEPARTURE, HEARD A THUMP OR BANG IN WHAT WE THOUGHT CAME FROM BELOW THE FO`S FLOOR SHORTLY AFTER WE STARTED SMELLING A VERY STRONG ELECTRICAL BURNING TYPE SMELL. RETURN TO EWR. SMELL REDUCED DURING DESCENT AND WENT AWAY F/O AWHILE BUT RETURNED DURING APPROACH REF LG PG 8695594 R&R OF FWD EQUIPTMENT EXHAUST DETECTOR ALSO FOUND FO`S EHSI SCREEN DEGRADED BRIGHTNESS. REMOVED AND REPLACED PER MM 34-22-04 PAGEBREAK 401 OPS CHECK GOOD A/C SET UP FOR EVAL FLIGHT REF LG PG 8695595.

Part: SOCKET — DEFECTIVE (CABIN) · airframe 66,830 hrs · 14,725 cycles

EMERGENCY SLIDE LIGHT (EXT) AT L4 DOOR WILL NOT TEST. CHANGED ATA 3300 TO 3350. RELAMPED, NO HELP. CHECKED FUSES, ALL OK. FOUND 6.5VDC AT LIGHT ASSY. REQ'S LIGHT ASSY, NSU LAX. PLACARD INOP PER MEL. REMOVED AND REPLACED SOCKET IAW AMM 35-51-09 OPS CHECKED GOOD. OK FOR SERVICE. REMOVED MEL 33-51-2 CNTL NUMBER 529486.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,203 hrs · 14,004 cycles

FLOOR LEVEL EMERGENCY EXIT SIGN AT LEFT FWD EMERGENCY OVERWING EXIT HAS BULB INOPERATIVE. REMOVED AND REPLACED BULBS IN EXIT SIGN, OPS CHECK GOOD IAW AMM 33-51-10.

Part: GCU — MALFUNCTIONED (E&E BAY) · airframe 62,888 hrs · 13,939 cycles

LT AND RT UTILITY BUSES TRIPPED FOR ABOUT 3-4 SECONDS IN FLIGHT. ALSO LT AND RT UTILITY BUS MESSAGE APPEARED ON EICAS. UTILITY BUSES RESET THEMSELVES. GALLEY POWER AND VIDEO TURNED OFF. T/S PER MM 24-22-00, REMOVED AND REPLACED LT AND RT GCU AND BPCU AS PER MM 24-22-02 AND 24-41-03. PERFORMED INSTALLATION TEST AND AC POWER SYSTEM OPERATIONAL TEST AS PER 24-22-00. ALL TESTS SATISFACTORY, OK TO CONTINUE.

Part: SKIN — CRACKED (R-4 DOOR) · airframe 62,813 hrs · 13,916 cycles

R-4 DOOR LIGHTENING HOLE NEAR VERTICAL ADJUSTMENT TORQUE TUBE HAS CRACK. ACCOMPLISHED REPAIR PER ECRA 5210-02105.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,813 hrs · 13,916 cycles

STATION 1640 T-CAP ON FLOORBEAM HAS CORROSION NEAR BUTTLINE 0 FOUND CORROSION OUT OF LIMITS. REPAIRED T-CAP PER SRM 53-00-51 REPAIR 3.

Part: FLOORBEAM — MISREPAIRED (FUSELAGE) · airframe 62,813 hrs · 13,916 cycles

STATION 720 FLOORBEAM APPROXIMATELY LBL 45 PREVIOUS REPAIR IMPROPERLY ACCOMPLISHED. REMOVED AND REPLACED REPAIR PER B757 SRM 53-00-51.

Part: FUSE — BLOWN (CABIN) · airframe 61,523 hrs · 13,670 cycles

L4 EXTERIOR EMERGENCY LIGHT NO POWER. T/S IAW WDM 33-51-22 & AMP; SSM 33-51-01. FOUND BAD FUSE ON M737. REPLACED FUSE & AMP; RELAMPED. ALL OPS NORMAL.

Part: CONTROL PANEL — DEFECTIVE (COCKPIT) · airframe 56,555 hrs · 12,721 cycles

AT 23,000 FT, RT ENG FIRE AND OVERHEAT WARNING CAME ON. ACCOMPLISHED ENGINE FIRE / SHUTDOWN CHECKLIST. FIRE LIGHTS STAYED ON. BLEW BOTH BOTTLES. POSITIVE OIL PRESSURE ON SHUTDOWN, 15 MINUTE WINDMILL ON ENGINE. TROUBLESHOT PER FIM 26-11-00. FOUND NR 2 ENG TEST CIRCUIT STUCK IN TEST MODE. REPLACED FIRE/OVERHEAT TEST PANEL PER MM 26-11-02. OPS CHECK GOOD. REF LOG PAGES 7992436 AND 7992437 FOR FIRE BOTTLE REPLACEMENT. WINDMILL TIME WITH OIL PRESSURE WITHIN LIMITS OF MM 71-00-00 P605. A/C OK TO CONTINUE. ROTABLE PARTS CHANGE WAS INDICATED - TT 1200263 SN OFF 00392 PANEL, TEST, FI OFF 19-3111-9-9002 0392 ON 19-3111-9-9002 0504.

Part: SKIN — DELAMINATED (RUDDER) · airframe 52,709 hrs · 11,956 cycles

THE RUDDER TRAILING EDGE SKIN WAS FOUND DELAMINATED OVER AN AREA OF APPROXIMATELY 0.50 INCH BY 1.9 INCH AT RUDDER STA 175. THE DELAMINATION WENT THROUGH THE ENTIRE THICKNESS OF THE LT RUDDER PANEL AND APPROXIMATELY 20% OF THE THICKNESS OF THE RT RUDDER PANEL. THE RUDDER SKIN WAS REPAIRED IAW ECRA 5540-01236.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,709 hrs · 11,956 cycles

INSPECTION FOUND FUSELAGE SKIN CORRODED UNDER RT AIRFONE ANTENNA AT STA 1510, RBL 10, S28R-29R. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-00-01, REPAIR NR 5.

Part: STRINGER CLIP — CORRODED (BS 1140 S3R) · airframe 47,535 hrs · 10,852 cycles

INSPECTION FOUND STRINGER CLIP CORRODED AT STA 1140, S3R. THE STRINGER CLIP WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SKIN — DELAMINATED (LT WING) · airframe 42,604 hrs · 9,808 cycles

INSPECTION FOUND THE LT WING O/B FIXED LEADING EDGE SKIN TOP SURFACE DELAMINATED AT WS 380. REPAIRED IAW SRM 51-40-02, 51-70-07, 51-70-17 AND EA 5731-01010.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,604 hrs · 9,808 cycles

INSPECTION FOUND FLOORBEAM UPPER STRAP CORRODED AT BS 720 FROM LBL 60 TO RBL 60. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND REPLACED IAE SRM 51-40-05.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,604 hrs · 9,808 cycles

INSPECTION FOUND CORROSION ON FLOORBEAM IN L-2 DOOR AREA AT BS 720, LBL 65. REPAIRED IAW SRM 53-00-51, FIGURE 201.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,604 hrs · 9,808 cycles

INSPECTION FOUND MAIN CABIN INTERCOSTAL CORRODED BETWEEN BS 680 AND 700, RBL 56, WL 208. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, PARA 4 AND 7.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,604 hrs · 9,808 cycles

INSPECTION FOUND GALLEY SUPPORT INTERCOSTAL CORRODED AT BS 680-700, RBL 15. THE GALLEY SUPPORT INTERCOSTAL WAS REPLACED IAW SRM 51-40-02, PARA 4 AND 7.

Part: SKIN — DENTED (FUSLEAGE) · airframe 40,556 hrs · 9,326 cycles

INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 215.25-223.5, S15R TO S16R, WL 188 JUST BELOW RT AOA VANE. THE SKIN WAS REPAIRED IAW ECRA 5310-04429. A DIP WAS ISSUED TO ACCOMPLISH AN INITIAL INSPECTION WITHIN 25,000 FLIGHT CYCLES AND TO PERFORM REPEAT INSPECTIONS EVERY 3,000 FLIGHT CYCLES.

Part: STRINGER — CRACKED (BS 1610-1640)

INSPECTION FOUND A CRACK IN STRINGER 22L AT STA 1610-1640. A STRINGER SPLICE REPAIR WAS PERFORMED IAW SRM 53-00-03 AND ECRA 5331-01055.

Part: FLOORBEAM — CORRODED (BS 324)

INSPECTION FOUND TOP CHORD OF FLOORBEAM CORRODED AT STA 324, RBL 42. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, PAGES 216-219 AND ECRA 5321-01049.

Part: PANEL — CRACKED (RT WING LE)

INSPECTION FOUND THE RT WING LEADING EDGE CRACKED IN TWO PLACES BETWEEN SLATS NR 7 AND NR 8. THE CRACKS WERE 5.5 AND 9.5 INCHES LONG. THE SURFACE WAS PREPARED IAW SRM 51-70-06. THE AREA WAS REPAIRED IAW ECRA 5720-01662. A DIP WAS ISSUED FOR FOLLOW-UP INSPECTION AND PERMANENT REPAIR PER ECRA 5720-01662, REV A.

Part: PANEL — CRACKED (LT WING LE)

INSPECTION FOUND A 10.5 INCH CRACK IN LT WING LEADING EDGE AT THE OUTBOARD END OF NR 1 LEADING EDGE SLAT. THE SURFACE WAS PREPARED IAW SRM 51-70-06. THE AREA WAS REPAIRED IAW ECRA 5720-01662. A DIP WAS ISSUED FOR FOLLOW-UP INSPECTION AND PERMANENT REPAIR PER ECRA 5720-01662.