N41140

Part: BULB — FAILED (ZONE 200) · airframe 96,276 hrs · 20,238 cycles

AISLE 23 EMERGECY LIGHT INOPERATIVE. REPLACED THE BULB AT AISLE 23 EMERGENCY AISLE LIGHT IAW AMM 33-51-05. OPS CHECKED GOOD.

Part: POTABLE WATER — ODOR (ZONE 900) · airframe 94,694 hrs · 19,928 cycles

PLANE POTABLE WATER FROM ALL GALLEYS TASTE/SMELL STRONG CLORINATION AND DETERGENT. PAX COMPLAINT FLUSHED POTABLE WATER SEVERAL TIMES PER AMM 38-10-00-170-003, OK TO CONTINUE.

Part: DOOR — BENT (SLIDE) · airframe 93,659 hrs · 19,708 cycles

LEFT WING EMERGENY EXIT SLIDE COMPARTMENT DOOR IS BENT OUT OF S HAPE. RESECURED LEFT WING EMERGENCY EXIT SLIDE COMOARTMENT DOOR IAW AMM 52-22-01. OPS CHECK SAT.

Part: BLEED VALVE — FAULTED (NR 1 ENGINE) · airframe 93,587 hrs · 19,692 cycles

L BLEED OFF DURING CLB AT F110. RAN QRH LEVEL AT F130. L DUCT R APID FLUCT FROM 0-45 TOMC LOCKING PAGE - REPEAT L BLD OFF LT - CAPT CONFIRMED L BLD OFF LT DID NOT RESET WITH RESET OF LEFT BLEED PER QRH CK LIST. INBD CREW STATING THAT LH ENGINE BLEED WAS OSCILLATING AFTER TAKE-OFF. THEY SHUT OFF BLEED AND THEN TURNED BLEED BACK ON. LH BLEED STAYED ON ZERO AFTER RESET. INCLUDING STEP 4. H.(1)(E) 1) ROTABLE PARTS CHANGE WAS INDICATED - TT # 1367435 SN OFF 1271 PERFORMED HEALTH CHECK ON #1 ENG PER AMM 36-00-23-705-154-001 INSTALLED LEFT PRSOV CANNON PLUG ON RECEPTACLE AND TWO BONDING CONTINUED INSTALL PER AMM 36-11-09-002-047-001 UP AND INCLUDING RFCC TEST GOOD AT THIS TIME.PERFORMED TEST OF LT PRSOV AND FOUND JUMPERS PER AMM 36-11-09-002-047-001 STEP 4.H.(1) (S) TO BE STICKING. PER AMM 36-00-23-705-152-001.REMOVED AND INSTALLED LEFT PRSOV AS PER AMM 36-11-09-002-047-001 UP TO AND VALVE, PNEU, PR OFF 19-3611-9-0004 1271 ON 19-3611-9-0004 1667 UNLOCKED COMPLETED INSTALL AND LEAK CHECK PER MM 36-11-09. OPS CHECKED GOOD PER 36-11-00-780-923-C1. OK TO CONTINUE

Part: CONTROLLER — FAULTED (NR 1 ENGINE) · airframe 93,140 hrs · 19,588 cycles

LEFT ENGINE EGT OVERHEAT ON CLIMB AND CRUISE REQUIRED REDUCED PO WER SETTING PER CREW DEBREIF EGT 801 FOR APROX 3SECONDS, POWER REDUCED TO AVOID REDLINE. FF 400LBS GREATER THEN #2 ENG AT REDUCED POWER SETTING REF: AMM TASK 75-32-01-742-002-R00, BVCU BITE SHOWED CODE 7E FOLLOWED BY CODE 74 ON LEG F0, NO OTHER FAULTS. REF: AMM TASK 75-32-15-742-001-R00, TPU BITE SHOWED CODE F4 FOLLOWED BY CODE 40, NO OTHER FAULTS. UPDATE FOR PARTS - BVCU BITE CODE 74, REF: FIM 75-32-00/301 CONFIG 4. R/R ENG #1 BVCU IAW AMM 75-32-01 UP TO STEP 9 A. INSTALLED ELECTRICAL CONNECTORS & LOCKWIRED, PERFORMED BVCU INTERROGATION ON NEW BVCU - NO FAULTS. REF: AMM TASK 75-32-01-404-023-R00. NEXT NEED TO DO: STEP H. BLEED VALVE CONTROL UNIT (BVCU) INSTALLATION TEST, REF: AMM TASK 75-32-01-404-023-R00. PERFORMED BLEED VALVE (BVCU) INSTALLATION TEST FOR ENGINE #1 REF. POWER PLANT TEST 3 TASK 71-00-00-715-049-R03. IP/HP COMPRESSOR AIRFLOW CONTROL TESTS GOOD. TOOK ENGINES TO TAKEOFF POWER PER 71-00-00-715-049, NO EXCEEDANCE NOTED.

Part: GIRT BAR — DISENGAGED (ZONE 800) · airframe 93,042 hrs · 19,564 cycles

DOOR 4R WONT ARM GIRT BAR FOUND DISENGAGED. REINSTALLED GIRT BAR. REF AMM TASK 25-66-10-402-022. ADD EMP:U345350

Part: ENGINE — FAULTY (ENG 2) · airframe 92,521 hrs · 19,438 cycles

DURING INCOMING INSPECTION AND DISASSEMBLY OF ENGINE ESN 31805, SASAI HAS DISCOVERED A HOLE IN THE OUTER CASE OF THE 04 MODULE. PICTURES HAVE BEEN UPLOADED TO EXOSTAR UNDER THE INVESTIGATIONS-UNIQUE EVENTS FOLDER. THE HOLE/DAMAGE DENOTED ON THE OUTER CASE IS APPROXIMATELY 2 INCHES LONG WITH A LIFT ON 1/8€? THE DAMAGE TO THE HPT SEAL SEGMENTS, WHICH IS LOCATED DIRECTLY OPPOSITE OF THE HOLE IN THE OUTER CASE IS 1 INCH LENGTH X 3/4 INCH WIDTH.

Part: LINE — FAULTY (HYD CASE DRAIN) · airframe 92,293 hrs · 19,386 cycles

R HYD QTY EICAS FOLLOWED BY R HYD SYS PRESS MSQ QTY BEGAN 0.38 A ND WAS 0.7 WITHIN 2 MINS RH ENGINE LEAKING HYDRAULIC FLUID. REMOVED AND REPLACED NR. 2 ENGINE EDP CASE DRAIN HARD LINE SECTION WITH A SERVICEABLE UNIT, REF IPC 29-11-75-02 ITEM NR. 190. TORQUED REF AMM 20-11-00. OPS AND LEAK CHECKS SATIS.PARTS USED: 19-2911-3-0148,QTY :1

Part: SKIN — DAMAGED (ZONE100) · airframe 92,085 hrs · 19,344 cycles

RII INSPECTION REQUIRED REPAIR ON FUSE STA 587L TO STA 594L STR 18L SEE L/P 9287975 INSPECTION WAS NOT NOTIFIED FOR FINAL INSPECTION PRIOR TO EDGE SEALANT AND PAINT. REQUIERS PAINT STRIP AND SEALANT REMOVED FOR FINAL INSPECTION, OF SRM 53-00-01-2R-13 STEPS 7 THRU 9. C/W INSPECTION OF FASTNERS SEVERAL REQUIERS REMOVAL AND REPLACE UNDER AND OVER DRAW ALL MARKED. REMOVED EXT FINISH AND FILLET SEAL IAW TASK 51-21-01-157-011 DUE TO DAMAGE FOUND DURING THE FINAL BUY BACK REPAIR IS NOLONGER VALID. , HAVE REMOVED THE REPAIR DOUBLER TO EVALUATE DAMAGE. IAW SRM 51-40-02 THROUGH P. OK TO INSTALL REPAIR. APPLY DECORATIVE FINISH. VERIFIED ALL STEPS PER AVO13373 REV C IN CONJUNCTION WITH SRM 53-00-01-2R-28 REPAIR 28, HAVE BEEN C/W PER EC/RA 5330-07353 COMPLETED INSTALLATION OF REPAIR DOUBLER/FILLER REF SRM 53-00-01-2R-28 REPAIR 28 AND EC/RA 5330-07353. SEE LOG 9390596.

Part: LAVATORY — FULL (ZONE 200) · airframe 91,623 hrs · 19,238 cycles

AFT LAVS FLUSHED BROWN WATER WITH ODOR. ALL 4 LAVATORIES SERVICED AND PERFORMED OPS CHECK SATIS PER B757 AMM 12-17.

Part: HEAT SHIELD — DAMAGED (NR 2 NACELLE) · airframe 91,092 hrs · 19,133 cycles

AMES NR 171629-0400-0013. REMOVED, REPAIRED, AND REINSTALLED #2 PYLON AFT MOST HEAT SHIELD IAW EX/RA 5452-01005 AND B757 SRM 51- 40-02 PARA 4. SEE PARTIAL WORK ON BACK AND PARTIAL WORK SHEET 16 PAGE 1 OF 1 FOR WORK COMPLETION.

Part: SKIN — DENTED (BS 1400 S25L) · airframe 91,092 hrs · 19,133 cycles

REF AMES NON ROUTINE 171629-0100-0043. GENERATING ITEM:19-0640-1 -2100.DENT ON FUSELAGE SKIN AT STA 1400 S-25L

Part: ENGINE — UNKNOWN (NR 1) · airframe 88,822 hrs · 18,586 cycles

DEBRIEF OF FLIGHT CREW STATES THEY HEARD A LOUD BANG FROM NUMBER 1 ENG WITH AN UNCOMMANDED YAW TO A/C RIGHT AT 38000 FT. ALSO L ENG VIB INDICATION PEAKED AT 3.7. FORCING AN AIR RETURN TO EWR DUE CREW VIB CHECK LIST INSTRUCTION. L ENG BB VIB MSG DISPLAYED ON ECS PAGE. PERFORMED VISUAL INSPECTION OF NUMBER 1 ENG. PHOTOS ATTACHED. REF WORKCARD 19-7200-9-0001 FOR #1 ENGINE REPLACEMENT SCHEDULED PARTS CHANGE

Part: ANTI-ICE VALVE — STUCK (LH ENG) · airframe 88,817 hrs · 18,585 cycles

ENG ANTI ICE L CAUTION MSG. VALVE STUCK IN THE UNCOMANDED POSI. R&R ENG ANTI ICE ENG 1 IRW 30-21-03-404-016 OPS CHECK GOOD. NO DEFECT NOTED AT THIS TIME. PARTS USED: 19-3021-9-0001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1508968 SN OFF 4045 IPC REFERENCE # 30-21-01-01 VALVE, SHUTOFF, OFF 19-3021-9-0001 4045 ON 19-3021-9-0001 2873.

Part: NUT PLATE — DAMAGED (DOOR 4L) · airframe 88,822 hrs · 18,586 cycles

DOOR 4L HOLD OPEN BRACKET 2 LOWER BOLTS LOOSE LOCKED FOR MX FERRY UNLOCKED FOR MX REFERENCE IPC 52-11-01-01A ITEM 822 BRACKET, 2 LOWER BOLTS REMOVED DOOR 4L SLIDE 25-66-00 TO F.O.M. HELICOIL APPEARS STRIPPED. REMOVED AND REPLACED NUTPLATES AS PER SRM 51-40-02.

Part: SKIN — DENTED (RH HORIZ STAB) · airframe 85,850 hrs · 17,967 cycles

SUPPORT TASK- R/H HORIZONTAL STAB UPPER SKIN BETWEEN FORWARD SPAR AND AUX SPAR HAS A DENT AT APPRO STAB STATION 200 TRANSCRIBED FROM HAECO NR 9282966 PERFORMED TAP TEST AND VISUAL, FOUND 3" X 4.25" AREA OF DISBONDE 51-70-10-2R-01. HAECO GSO MECH V899890 INSP QC453 D SKIN ENCIRCLING .500" PUNCTURE. REMOVED DAMAGED SKIN AND CORE IAW B757-200 SRM 55-10-01-1A-1 FIG 101, SRM 51-70-10-2R-3, SRM 5 1-70-10-2R-0 PARA 6. COMPLETED REPAIR IAW B757-200 SRM

Part: TERMINAL — BROKEN (SLIDE LIGHT) · airframe 85,850 hrs · 17,967 cycles

L-1 DOOR SLIDE LIGHT INOP. TRANSCIBED FROM HAECO GSO NR 9282919.REMOVED AND REPLACED L-1 DOOR SLIDE LIGHT ASSY AND OPS CHECKED PER AMM 25-66-11-822-011 AND BSWPM 20-84-00 AND WDM 33-51-12.

Part: FRAME — DAMAGED (STA 1300) · airframe 85,850 hrs · 17,967 cycles

THE REPAIR INCORPORATED VIA ECRA 5362-01040 IS APPROVED AS TIME- LIMITED FOR 18 MONTHS PENDING THE RESULTS OF A DAMAGE TOLERANCE ANALYSIS (DTA). REMOVE THE AIRCRAFT FROM SERVICE ON OR BEFORE MA Y 15, 2024, UNLESS ANOTHER 8110-3 FORM IS RECEIVED FINDING APPRO VAL FOR DAMAGE TOLERANCE REQUIREMENTS. REFERENCE ECRA 5362-01040 AND HAECO GSO NR 9282574 WHICH STATES B757-53-3-0524 AFT PIT LH SIDE, STA 1300 FRAME UPPER FLANGE IS D ENTED AT S26L (MARKED). ANALYSIS (DTA). REMOVE THE AIRCRAFT FROM SERVICE ON OR BEFORE MA APPROVAL FOR DAMAGE TOLERANCE REQUIREMENTS. Y 15, 2024, UNLESS ANOTHER 8110-3 FORM IS RECEIVED FINDING THE REPAIR INCORPORATED VIA ECRA 5362-01040 IS APPROVED AS TIME- LIMITED FOR 18 MONTHS PENDING THE RESULTS OF A DAMAGE TOLERANCE REF ECRA 5362-01040, REPAIR IS TIME LIMITED FOR 18MO PENDING TOMC-APPROVAL FROM SC1ELBYC COMMENT RESULTS OF A DAMAGE ANALYSIS. REMOVE ACFT FROM SVC ON OR BEFORE MAY 15, 2024 UNLESS 8110-3 RECEIVED. RECORDS UPDATE RECORDS UPDATE T/A: 15MAY24....DB/U359554 REF L/P 3110365

Part: FRAME — DENTED (BS 740 S24R) · airframe 85,850 hrs · 17,967 cycles

FWD PIT R/H AT STA 740 STR 24 FRAME IS DENTED TOP SIDE, DENT WAS FOUND TO BE IN FREE FLANGE ON FRAME BS 740 S24R, DENTS ARE NOT PERMITED IN FREE FLANGE. OUT OF LIMITS IAW SRM 53-00-07. COMPLETED REPAIR ON FRAME IAW SRM 53-00-07.

Part: FLOOR SUPPORT — CORRODED (BS 400) · airframe 85,850 hrs · 17,967 cycles

(B757-53-3-0480) MAIN CABIN FLOOR STRUCTURE STA 400 RBL 40 FLOOR SUPPORT CORRODED ON UPPER SURFACE. TRANSCRIBED HAECO GSO NR 9282307. REMOVED DAMAGE TO GUTTER SUPPORT STA 400 RBL 40 MAT. 063 REMOVED AND BAC DWG 141N5162 REV. A REMOVED DOT HAECO GSO MECH V935477 .020 REMAINING .043 FOUND TO BE OUT OF LIMITS IAW B757-200 SRM 5 INSP QC258. 3-00-51 FIG 101. DETAIL III AND BAC DWG 141N5162. FABRICATED AND INSTALLED NEW SUPPORT PN: 141N5162-70 IAW B757-200 SRM 51-40-02

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 85,850 hrs · 17,967 cycles

(B757-53-3-0480) MAIN CABIN FLOOR STRUCTURE STA 1640 BL0 FLOOR B EAM PREVIOUS T CAP REPAIR CORRODED ON UPPER SURFACE, TRANSCRIBED FROM HAECO GSO N/R 9282336 ACCOMPLISHED T-CAP REPAIR IAW B757-200 SRM 53-00-51-2R-10 REPAIR 10 AND B757-200 SRM 51-0-02-0G-0. CATEGORY A. ESFR 1030346. H AECO GSO MECH V932675 INSP QC393

Part: FLOOR SUPPORT — CORRODED (STA 400RBL) · airframe 85,850 hrs · 17,967 cycles

(B757-53-3-0480) MAIN CABIN FLOOR STRUCTURE STA 400 RBL 40 FLOOR SUPPORT CORRODED ON UPPER SURFACE. TRANSCRIBED HAECO GSO NR 9282307.

Part: FLOOR SUPPORT — CORRODED (STA1660-1680) · airframe 85,850 hrs · 17,967 cycles

(B757-53-3-0480) MAIN CABIN FLOOR STRUCTURE STA 1660 TO 1680 LBL 60 GUTTER SUPPORT CHANEL CORRODED ON UPPER SURFACE. DOT: R726. TRANSCRIBED FROM HAECO NR 9282335.

Part: FLOORBEAM — CORRODED (STA 363 RBL 58) · airframe 85,850 hrs · 17,967 cycles

(B757-53-3-0480) MAIN CABIN FLOOR STRUCTURE STA 363 RBL 58 FLOORBEAM UPPER SURFACE CORRODED TRANSCRIBED FROM HAECO GSO NR 9282303.

Part: SEAT TRACK — CORRODED (STA 720-STA 760) · airframe 85,850 hrs · 17,967 cycles

(B757-53-3-0480) MAIN CABIN FLOOR STRUCTURE STA 720 TO STA 760 R BL 45 SEAT TRACK CORRODED IN SEVERAL SPOTS REF HAECO GSO NR 9282 325. BLENDED CORROSSION AT 720 RBL45, REMINING THICKNESS .025 FOUND T O BE OUT OF LIMITS PER B757-200 SRM 51-40-02 INSTALLED NEW SEAT TRACK AND SEAT TRACK SUPPORT PER TRAMCO #95-030 REV A. HAECO GS O MECH V932674 INSP QC453

Part: SUPPORT CHANNEL — CORRODED (STA 346 RBL 62) · airframe 85,850 hrs · 17,967 cycles

(B757-53-3-0480) MAIN CABIN FLOOR STRUCTURE STA 346 RBL 62 GUTT ER SUPPORT CHANNEL CORRODED AT R1. TRANSCRIBED FROM HAECO GSO NRC# 9282302 REMOVED AND REPLACED SUPPORT P/N 141N5160-78 IAW BOEING DWG# 141 N5160 REV B AND B757-200 SRM 51-40-02. HAECO GSO MECH V897676 I NSP QC453

Part: SEAT TRACK — CORRODED (STA 720-STA 760) · airframe 85,850 hrs · 17,967 cycles

(B757-53-3-0480) MAIN CABIN FLOOR STRUCTURE STA 720 TO STA 760 R BL24 SEAT TRACK CORRODED IN SEVERAL SPOTS. TRANSCRIBED FROM HAE CO GSO NRC# 9282323 BLENDED SEAT TRACK, REMOVED .030, FOUND TO BE OUT OF LIMITS PER 95-030 REV A. HAECO GSO MECH V932674 INSP QC456 B757-200 SRM 53-00-52. REMOVED SEAT TRACK PER B757-200 SRM 51-40 -02. LOCATED AND DRILLED PER B757-200 SRM 51-40-05. INSTALLED SE AT TRACK SUPPORT PER B757-200 SRM 51-40-02 AND TRAMCO DWG#

Part: FLOOR SUPPORT — CORRODED (STA722) · airframe 85,850 hrs · 17,967 cycles

(B757-53-3-0480) MAIN CABIN FLOOR STRUCTURE STA 722 RBL 60 GUTTE R SUPPORT CHANNEL CORRODED ON UPPER SURFACE. TRANSCRIBED FROM H AECO GSO NRC# 9282319

Part: STRUCTURE — CORRODED (SA1625) · airframe 85,850 hrs · 17,967 cycles

(B757-53-3-0480) MAIN CABIN FLOOR STRUCTURE STA 1625 LBL60 CHOR D CORRODED ON UPPER SURFACE. TRANSCRIBED FROM HAECO GSO NRC# 92 82332 REMOVED DAMAGE TO CHORD STA 1625, LBL60. ORIG MAT. 070. REMAININ HFEC OF BLEND USING T8257H. IAW NDTM PT. 6, 51-00-19. NO CRACKS MAT ID FOR-1 I/B CHORD BAC 1515-533, PO #1042201.1, 7075-T6511 E 7075-0 TO T6. MAT ID FOR -3 STRAP IS 7075-T6 CLAD, .100, PO #102 ALODINED & PRIMED IAW B757-200 53-00-13-2R-1. PAINTED IAW B757 A G MAT. 048. REMOVED MAT. 022. FOUND OUT OF LIMITS IAW B757-200 S NOTED. REMOVED DAMAGED PART OF CREASE BEAM IAW B757-200 SRM 53-0 XTRUSION IAW B757-200 SRM 53-00-13-2R-1. FULL ANNEALED 2EA EXT. 033.2 IAW B757-200 SRM 53-06-13-2R-1. MAT ID FOR -2 CHANNEL IS 7 MM 51-21-00. INSTALLED CREASE BEAM IAW BAC PWG 146N8722 + B757-2 RM 53-60-13, FIG 101 DET III. ACCOMPLISHED DVI OF CHORD IAW B757 0-13-2R-1, STEPS 4B, 4C. ACCOMPLISHED HFEC OF CUT EDGES & OPEN 7075-T6511 TO "0" IAW BAL 5602. FORMED I/B REPAIR CHORD SECTION 075-T62, BAC 1493-895 EXT, PO #1042244.1 IAW B757-200 SRM 53-00- 00 SRM 51-40-02 & B757-200 SRM 53-00-13-2R-1. REF HAECO GSO MECH -200 SRM 51-10-08. NO OTHER DAMAGE NOTED. PERFORMED SURFACE HOLES IAW B757 NDTM 51-00-19. PT 6. NO CRACKS FOUND. IAW B757-200 SRM 53-00-13-2R-1. HEAT TREATED 1EA. REPAIR SEAL 13-2R-1. FABBED REPAIR PARTS IAW B757-200 SRM 53-00-13-2R-1. V900838 / INSP QC401

Part: NONE — GOUGED (STA 1640) · airframe 85,850 hrs · 17,967 cycles

(SUPPORT TASK) MAIN CABIN FRAME AT STA 1640 HAS 1EA SUBSTRUCTURA L TEE CLIP IS GOUGED AND KNIFE EDGED ON THE UPPER LOWER LEGS AT S14L. TRANSCRIBED FROM HAECO GSO NRC# 9282170 REMOVED AND REPLACED TEE-CLIP AT STA 1640 PN: 146N8749UP IAW B757-200 SRM 51-40-02-0G-0 AND BOEING DWG 146N8735 REV A PO: 1041690.1. REF HAECO GSO MECH V932675 QC453

Part: ANGLE — GOUGED (STA 1640) · airframe 85,850 hrs · 17,967 cycles

(SUPPORT TASK) MAIN CABIN FRAME AT STA 1640 SUBSTRUCTURAL TEE CL IP UPPER AND LOWER LEG IS GOUGED AND KNIFE EDGED AT S14R. TRANS CRIBED FROM HAECO GSO NRC# 9282166

Part: FLOOR SUPPORT — CORRODED (STA 371 LBL 58) · airframe 85,850 hrs · 17,967 cycles

(B757-53-3-0480) MAIN CABIN FLOOR STRUCTURE STA 371 LBL 58 GUTTE R SUPPORT CHANNEL CORRODED ON UPPER SURFACE. DOT: R889. TRANSCRI BED FROM HAECO NR 9282314.

Part: FLOOR SUPPORT — CORRODED (STA 400 RBL17) · airframe 85,850 hrs · 17,967 cycles

(B757-53-3-0480) MAIN CABIN FLOOR STRUCTURE STA 400 RBL17 FLOOR PANEL SUPPORT CORRODED ON UPPER SURFACE. TRANSCRIBED FROM HAECO GSO NRC# 9282308 REMOVED DAMAGE TO FLOOR SUPPORT, ORIGINAL MAT. .050 REMOVED AND BAC DWG 141N5162 REV.B REMOVED DOT. REF HAECO GSO .010 REMAINING .040 FOUND TO BE OUT OF LIMITS IAW BAC DWG MECH V935477 QC453 141N5162 AND SRM 53-00-51 FIG 101 DET. III.RECEIVED NEW PART. 141N5182U57 PO: 1041786.1 AND INSTALLED IAW SRM 51-40-02 INFO TOOL NO T8224L CAL DUE 15OCT22 EFSR # 1030131

Part: FLOOR SUPPORT — CORRODED (RBL 20 TO RBL50) · airframe 85,850 hrs · 17,967 cycles

(B757-53-3-0480) MAIN CABIN FLOOR STRUCTURE STA 720 RBL 20 TO RB L 50 UPPER STRAP CORRODED ON UPPER SURFACE. TRANSCRIBED FROM HA ECO GSO NRC# 9282322

Part: FAIRING — DAMAGED (#2 ENG) · airframe 85,546 hrs · 17,898 cycles

#2 ENG I/B CENTER GAS GENERATOR COMPRESSOR FAIRING HAS DAMAGE. REF IPC 72-03-01-02 ITEM 220. INSTALLED NEW INBOARD CENTER GAS COMPRESSOR FAIRING ON ENGINE 2 REF AMM 72-03-01

Part: SLIDE — BLOWN (R1 DOOR) · airframe 85,134 hrs · 17,807 cycles

SLIDE BLOWN DOOR 1R REMOVED AND REPLACED DOOR SLIDE AT 1R IAW MM 25-66-01-404-044 IPC REFERENCE # 52-11-30-004-007 ALSO REMOVED AND REPLACED DOOR ASSIST BOTTLE FOR 1R IAW MM 52-11-30-004-007 ALL CHECKS GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1650327 SN OFF 1032 TT # 1192415 SN OFF 0260 RII REQUIREMENTS C/W SLIDE, B757-200 OFF 19-2566-9-0002 1032 ON 19-2566-9-0002 8042

Part: PANEL — MISSING (ENG 2) · airframe 84,384 hrs · 17,652 cycles

PDA 2 L ENG OIL SERVICE ACCESS DOOR MISSING PANEL REFITTED WITH TEMP REPAIR IAW ECRA ON WALK AROUND FOUND L ENGINE OIL SERVICE DOOR MISSING. DOOR WAS TOMC-APPROVAL FROM SC1ELBYC COMMENT RECOVERED AND RETURNED TO AIRCRAFT. PER ECRA 7110-01125 COMPLY WITH TEMP REPAIR DISPOSITION. PRIOR TO EACH DEPARTURE INSPECT REPAIR FOR SEVICEABILITY. WITHIN 5 CYCLES COMPLETE PERMANENT REPAIR. ADDING PHOTOS TOMC APPROVED : QC REVIEWED. RECORDS UPDATE TOMC APPROVED : QC REVIEWED. RIR: M-METER PRIOR TO EACH DEPARTURE (NO M&E RQRD) T/A: WITHIN 5 FC.....LN TOMCQC REV PERFORMED REMOVED AND REPLACED DAMAGED HINGE AND DOOR REF SR 51-40-02

Part: WARNING LIGHT — MALFUNCTIONED (PITOT) · airframe 80,238 hrs · 16,680 cycles

RT AUX PITOT LIGHT NOT ON AFTER SHUTDOWN ON GND. T/S PER AMM 30-31-00-705-001 UP TO STEP D7. WHEN YOU PULL THE R AUX PITOT C/B YOU SHOULD GET R AUX PITOT EICAS MSG AND THAT DOESNT HAPPEN. ORDER RELAY K312 ON P37. HAD TO RUN NUMBER 2 ENG BECAUSE ENGINE ANTI ICE VALVE LIGHT WAS ON.WHEN NUMBER 2 ENG WAS AT IDLE ALL PITOT LIGHTS WENT OUT ON ENG SHUTDOWN ALL PITOT LIGHTS CAME ON AT SHUTDOWN AND DUE TO NO HISTORY RT AUX PITOT LIGHT OP`S CHECKS GOOD.M.M. REF 30-31-00-705-001.

Part: ACCESS PANEL — MISSING (TE FLAP) · airframe 79,228 hrs · 16,478 cycles

PDA 2 RIGHT INBOARD FLAP FAIRING INBOARD SIDE. MISSING ACCESS PANEL. ECRA 5750-05134 ISSUED TO ACCOMPLISH INTERIM REPAIR. TEMP PANEL MANUFACTURED, INSTALLED AND SECURED PER PART 1 OF ECRA. CHECK EACH FLIGHT FOR SPEED TAPE AND REPAIR CONDITION PER PART 2. ECRA 5750-05134 ISSUED TO ACCOMPLISH INTERIM REPAIR. TEMP PANEL MANUFACTURED, INSTALLED AND SECURED PER PART 1 OF ECRA. CHECK EACH FLIGHT FOR SPEED TAPE AND REPAIR CONDITION PER PART 2. MUST BE REPAIRED WITHIN 3 CYCLES TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEW NEED TO VERYFY MATERIAL PANEL FABRICATION 2024T3 .100" PER ECRA 5750-05134 PART 3. VERIFIED MATERIAL 2024T3 .100" REF ECRA 5750-05134 UNDER PO# 0288208. FAB NEW PANEL PER ECRA 5750-05134 PART 3 AND INSTALLED PANEL. TOMCQC REV PERFORMED FAB NEW PANEL PER ECRA 5750-05134 PART 3 AND INSTALLED PANEL. QC REVIEW INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: SLIDER — MISSING (GIRT BAR) · airframe 77,704 hrs · 16,161 cycles

R-1 DOOR SLIDE GIRT BAR HANGING DOWN.FOUND FWD GIRT BAR SLIDER AND PROX SWITCH TARGET MISSING, INSTALLED NEW GIRT BAR SLIDER AND PROX SWITCH TARGET AT FWD SIDE OF R1 DOOR REF AMM 25-66-10-402-022 OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 73,129 hrs · 15,222 cycles

EMER LIGHTS OVERHEAD CAUTION LIGHT BULB OUT. RELAMPED BOTH BULBS. OPS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,043 hrs · 15,201 cycles

EMERGENCY EXIT LIGHT ON OUTSIDE OF AIRCRAFT R3 DOOR INOPERATIVE. REPLACED THE LAMPS. OPS CHECKED NORMAL.

Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 72,693 hrs · 15,121 cycles

MID CABIN EMERGENCY EXIT SIGN BETWEEN ROWS 20 21 DISLODGED REPOSITIONED EMER EXIT SIGN ABOVE ROWS 20 21. LIGHTS TESTED GOOD .

Part: OVEN — SMOKE (GALLEY) · airframe 72,358 hrs · 15,047 cycles

CREW REPORTS OVEN 204 EMITTING SMOKE. TURNED OFF AND DEACTIVATED.. SUSPECT GREASE ON FAN CAUSING SMOKE. R&R OVEN 204 IAW AMM 25-32-00. OPS CHK GOOD.

Part: SWITCH — LEAKING (HYD SYSTEM) · airframe 71,642 hrs · 14,894 cycles

LT HYD QTY LOSS. EMERGENCY DECLARED. FOUND EVIDENCE OF HYD LEAK IN LEFT ENG. PYLON. FOUND LEFT ENGINE EDP PRESSUE SWITCH S10540 LEAKING. REMOVED AND INSTALLED EDP PRESSURE SWITCH REF MM29-11-17. CLEANED PLYON AND DRY MOTORED ENGINE NO LEAKS NOTED.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 70,979 hrs · 14,766 cycles

AFT LEFT DOOR SLIDE PRESSURE IN THE RED. SLIDE REPLACED IAW AMM 25-66-01, SATIS.

Part: OVEN — FAILED (AFT GALLEY) · airframe 70,415 hrs · 14,660 cycles

FAN BROKEN, MAKES NOISE SET OFF SMOKE ALARM. FOUND OVEN TO BE MAKING THE NOISE. REMOVED AND REPLACED THE OVEN IAW AMM 25-34-00. OPS CHECKED NORMAL

Part: ENGINE — SURGES (RIGHT) · airframe 70,327 hrs · 14,638 cycles

RIGHT ENGINE ON CLIMB SURGED PLUS/MINUS 10 PERCENT N1. ACTIONED FIM 85-32-00-815-826-R06 NO FAULT FOUND ,TEST 3 ACTIONED OK. REF ITEM 4565525 EEC, BVCU BITE SHOWS NO FAULT ,REF FIM 71-05-00-815-824 EGT 804 FOR 7 SECS NO FURTHER ACTION NECESSARY A/C OK FOR SVC.

Part: SWITCH — DIRTY (L4 DOOR) · airframe 70,230 hrs · 14,621 cycles

SLIDE AT DOOR 4L SHOWS DISARMED IN FLIGHT. CLEANED GIRT BAR SWITCHES OPERATES OK.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 70,098 hrs · 14,597 cycles

EXIT EMERGENCY LIGHT LENS IN THE COCKPIT BROKEN. REPLACED THE LENS ASSY, GROUND CHECKED OK.

Part: SKIN — DENTED (FUSELAGE) · airframe 69,245 hrs · 14,420 cycles

FUSELAGE DENTED IN AREA FORWARD OF EXISTING REPAIR AT STATION 620 STR 16L REF NR 9006912 MEASURED DENT FOUND TO BE OUT OF LIMITS AS PER SRM 53-00-01 FIG 101 DETAIL III. CUT OUT DAMAGE AREA FAB DOUBLER TO INCORPORATE EXISTING REPAIR IAW SRM 53-00-01 FIG 101 SHEET 4 DETAIL III. TREATED AND PRIMED DOUBLER REPAIR PARTS AND AREA AS PER SRM 51-20-01. INSTALLED REPAIR AS PER SRM 51-40-02. CATEGORY B REPAIR NEXT INSPECTION F/C CURRENT F/C IS 14420 AS PER SRM 53-00-01 FIG 201 TABLE V.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,245 hrs · 14,420 cycles

CABIN SEAT TRACK LBL 24.75 FS 395, HAS LIGHT CORROSION AT CROWN BOTTOM AREA AND GOUGE MARKS AT CROWN LIP AND STUD HOLES EDGES. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52. REMOVED DAMAGED TRACK LBL 24.75 STA 377 TO STA 440. LOCATED AND DRILLED NEW TRACK IAW SRM 51-40-05 AND INSTALLED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,245 hrs · 14,420 cycles

CABIN SEAT TRACK AT LBL 45.5 BETWEEN FS 395 AND 381 HAS CORROSION. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52. REMOVED DAMAGED SEAT TRACK LBL 45.5 STA 377 TO STA 440. LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-05 AND INSTALLED IAW SRM 51-40-02.

Part: THRESHOLD — CORRODED (BS 703) · airframe 69,245 hrs · 14,420 cycles

R2 DOOR THRESHOLD HAS CORROSION AT STA 703, RBL 70. REF. AAR NR 9006708. REMOVED CORROSION AT R2 DOOR THRESHOLD SILL INNER CHORD, FOUND O UT OF LIMITS. REMOVED AND REPLACED CHORD PN 143N8328-53 P.O. NO. 1442041 IAW B757-200 SRM 51-10-02, 53-30-15, 51-40-02 REMOVE D CORROSION AT R2 DRAIN GUTTER SUPPORT BETWEEN STA 700-720, FOUN D WITHIN LIMITS . TREATED , PRIMED AND TOP COATED GUTTER SUPPOR T AS PER B757-200 SRM 51-10-02, 53-30-15 AND 51-20-01.

Part: WIRE HARNESS — DAMAGED (NLG) · airframe 68,822 hrs · 14,319 cycles

EXTENSION AND RETRACTION EICAS MESSAGE GEAR DOORS LAMP; GEAR DISAGREE DISPLAYED WITH GEAR HANDLE UP. DOORS LAMP; GEAR AMBER LIGHTS ON. ALL GREEN DOWN LIGHTS OFF GEAR DISAGREE THEN QRH PROCEDURE. NORMAL LANDING BUT NOSE GEAR GREEN LIGHT FAILED TO ILLUM. FOUND NOSE LANDING GEAR SENSOR HARNESS W2152 AND W2052 CONDUIT CRUSHED AND DAMAGED. REMOVED AND REPLACED SYSTEM 1 AND 2 NOSE GEAR HARNESS PER WDM 32-61-13 AND AMM 32-61-03-402-019. ACCOMPLI SHED OPS TEST OF PROXIMITY SENSORS FOR NOSE LANDING GEAR PER AMM TASK 32-61-03-472-043, ALL TEST AND INDICATIONS NORMAL. REF L/P 3520296 FOR GEAR SWING. AIRCRAFT OK TO CONTINUE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 68,822 hrs · 14,319 cycles

RT AFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED RT AFT EXTERIOR EMERGENCY LIGHT. OPS CHECK GOOD.

Part: PROBE — DEFECTIVE (PITOT/STATIC SYS) · airframe 63,749 hrs · 13,350 cycles

ON TAKEOFF ROLL AN AIRSPEED DISCREPANCY WAS NOTED AT 100 KTS, INDICATED ON CAPTAINS & STANDBY AIRSPEED INDICATORS. THE FIRST OFFICER AIRSPEED WAS LAGGING SIGNIFICANTLY. AIR RETURNED, AFTER ACCOMPLISHING ALL RELEVANT CHECKLIST. R & R FIRST OFFICERS PITOT PROBE IAW AMM 34-11-01-024- 041. FIRST OFFICERS PITOT PROBE LEAK CHECKED IAW AMM 34-11-00-501, NO LEAKS FOUND.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,731 hrs · 13,347 cycles

STOW BIN BULLNOSE EMER LIGHT INOPERATIVE 39 ABC. RELAMPED STOW BIN BULLNOSE EMER LIGHT AT ROW 39 ABC. PERFORMED OPERATIONS CHECK, FOUND NORMAL IAW AMM 33-51-05.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,928 hrs · 12,239 cycles

FOUR SCRATCHES ON SKIN FUSELAGE STATION 1708 - 1714 AT STRINGER 15RT. A DENT IN THE FUSELAGE SKIN AT STATION 1711 & STRINGER 15R WHICH WAS OUT OF LIMITS DUE TO CLOSE PROXIMITY OF THE STRINGER FASTENERS. ACCOMPLISHED THE REPAIR OF THE FUSELAGE SKIN AT STATION 1711 & STRINGER 15R IAW ECRA 5331-01808.

Part: FRAME — DENTED (FUSELAGE) · airframe 57,928 hrs · 12,239 cycles

B757-53-3-0478, AFT CARGO COMPARTMENT LOWER LOBE FUSELAGE ON FRAME 126 0, STRINGER 25R HAS A DENT. INTERIM REPAIR CARRIED OUT IAW ECRA 5311-01666 PART 1.

Part: ACTUATOR — FAILED (EVAC SLIDE) · airframe 57,928 hrs · 12,239 cycles

B757-25-3-0019 LT OFF WING ESCAPE SYS ACTUATOR FAILED OPERATIONS & FUNCTION CHECK LEAKING. R & R LT OFF WING ESCAPE SYS ACTUATOR IAW B75 7 AMM 25-65-05. ROTABLE PARTS CHANGE WAS INDICATED TT 1607870, SN OFF 01361 ACTUATOR, WING OFF 19-2565-9-0003 1361 & ON 19-2565-9-0003 1367.

Part: ENGINE — POWER LOSS (NR 2) · airframe 57,427 hrs · 12,137 cycles

DURING TAKEOFF LOUD POP FROM RT ENGINE, N1 ROLLED BACK TO 100%, THEN RECOVERED. ALL ENG INDICATIONS APPEARED NORMAL, BUT AIR RETURNED EWR AS PRECAUTION. PERFORMED TEST 3 IP HP COMPRESSOR AIRFLOW CONTROL TEST IAW M/M 71-00-00-715-049-R03. OPERATIONS CHECKED GOOD.

Part: SKIN — GOUGED (BS 580) · airframe 33,176 hrs · 7,639 cycles

FUSELAGE SKIN GOUGED BS 580 AT S29L. REMOVED DAMAGE MATERIAL; INSTALLED DOUBLER REF SRM 53-00-01.

Part: GOVERNOR — INOPERATIVE (NR 2 ENGINE) · airframe 53,325 hrs · 11,383 cycles

NR 2 ENGINE, NO PROBLEM WITH INDICATION OR THROTTLE CONTROL, HAD NO CONTROL OF NR 1 ENGINE THROTTLE (STUCK IN FULL POWER) THROTTLE LEVEL MOVED BUT NO CONTROL OF ENGINE. PERFORMED A PRECAUTIONARY NR 1 ENGINE SHUTDOWN. R & R FFG IAW MM 73-21-01 AND ACCOMPLISHED POWER PLANT TEST IAW 71-00-00. OPS CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (EICAS) · airframe 51,992 hrs · 11,144 cycles

EICAS MESSAGES C IRS FAULT AND RT IRS FAULT ILLUMINATED PERFORMED INERTIAL REF SYS BITE CHECK IAW AMM 34-21-00-715-04. 4 NR FAULTS OR DEFETCS NOTED. PERFORMED MCDP BITE TEST 30 IAW AMM 22-00-02, NO CURRENT FAULTS, TEST PASSED. ACFT FULL CAPABILITY CAT III, LAND III.

Part: FUSE — BLOWN (CABIN) · airframe 50,755 hrs · 10,930 cycles

EMER LIGHTS ROW 20 THRU 30 INOP. T/S PER WDM 33-51-11. REMOVED AND REPLACED FUSE F4 IN EMERGENCY PWR PACK M10699. EMERGENCY LIGHTS OPS CK GOOD.

Part: HYDRAULIC LINE — CRACKED (LT MLG WW) · airframe 49,442 hrs · 10,691 cycles

REF L/P 8950321. LEFT HYD QTY LOSS. FOUND CRACKED LINE P/N 271N6443-1114 REF IPC 29-11-84 FIG 06A ITEM 275. REPLACED SAME. NO FURTHER LEAKAGE NOTED AT THIS TIME CREW DECLARED AN EMERGENCY LANDING.

Part: UNKNOWN — SMOKE (CABIN) · airframe 46,740 hrs · 10,217 cycles

APPROX 2 HR 20 MIN INTO FLT CABIN STARTED FILLING WITH SMOKE IN VICINITY OF ROW 11. FAINT BURNING SMELL IN C/P / FOLLOWED BY F.O. AIRSPEED INDICATING RED WARNING LTS IAS DISAGREED, ONCE BEG AN DESCENT SMOKE BEGAN TO DISSIPATE IN CABIN AND A/C IND RETURNED TO NORMAL HAD FLT CREW FILLOUT FORM 46.6020 SMOKE IN PLANE AND FAXED TO MC. INSPECTED A/C PER MM 05-51-58-910-80-1C1 AND GMM 07-62-58 COULD NOT DUPLICATE SMOKE. REPLACED RT FCC PER MM 34-12-01 AND RT AIR DATE PER MM 34-12-01 401. PERFORMED TEST 30, TEST PASS A/C REMAINS CAT 111A AND ANN IN C/P READS SAME. REF LP 4270957 MORE ROTABLE PARTS CHANGE WAS INDICATED - TT # 1434761 SN OFF 03024 TT # 1444315 SN OFF 05058 COMPUTER, FLIGHT OFF 99-2211-9-0001 3024 ON 99-2211-9-0001 8571 COMPUTER, AIR D OFF 19-3412-9-0003 5058 ON 19-3412-9-0003 5776.

Part: SKIN — CRACKED (L4 DOOR) · airframe 46,282 hrs · 10,118 cycles

SUPPORT TASK - L-4 DOOR LOWER HINGE INNER SKIN CRACKED AT LIGHTENING HOLE. REPAIRED INNER DOOR SKIN CRACK PER ECRA 5210-02237.

Part: SKIN — CRACKED (R1 DOOR) · airframe 46,282 hrs · 10,118 cycles

SUPPORT TASK - R-1 DOOR INNER SKIN CRACK AT LIGHTENING HOLE UPPER AFT CORNER. INNER SKIN CRACK REPAIRED AS PER ECRA 5210-02235.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,282 hrs · 10,118 cycles

CABIN INTERIOR FRAME CRACKED AT PSU RAIL ATTACH POINT STA 1580 BETWEEN S-8R AND S-9R (MARKED). REPAIRED FRAME AT STA 1580 BETWEEN S-8 AND S-9R PER ECRA 5310-05353.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,282 hrs · 10,118 cycles

LEFT CABIN FLOOR STRUCTURE CREASE BEAM STA 1320-1340 HAS CORROSION (MARKED). REPAIR LT CREASE BEAM INBD CHORD SECTION STA 1370 PER EC/RA 5310-05352 SEE SUB-TASKS WORK ACCOMPLISHED. INITIATED DIP53-DIP CTL#09133 TO ACCOMPLISH PERMANENT REPAIR WITHIN 12 MONTHS OF FEB-02-2011. PLANNING TO CONTACT ENGINEERING AFTER 10 MONTHS BUT BEFORE 11 MONTHS FOR A PERMANENT REPAIR. ACCOMPLISH A PERMANENT REPAIR WITHIN 12 CALENDAR MONTHS FROM FEB. 02, 2011. PLANNING TO CONTACT ENGINEERING AFTER 10 MONTHS BUT BEFORE 11 MONTHS FOR A PERMANENT REPAIR. THIS ECRA IS BEING EVALUATED FOR DAMAGE TOLERANCE UNDER 14 CFR 25.571 AND WILL LIKELY BE MADE PERMANENT WITH REPEAT INSPECTIONS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,282 hrs · 10,118 cycles

AFT CABIN FLOORBEAM AT STA 1661 HAS CORROSION AROUND NUMEROUS FASTENER HOLES AT RBL 54 TO LBL 54 (MARKED). SEE WIPS FOR REMOVAL OF CORROSION AND REPAIR OF AFT CABIN FLOORBEAM AT STA 1661 LBL 54 TO RBL 54 WORK ACCOMPLISHED PER ECRA 5321-01744.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,282 hrs · 10,118 cycles

SUPPORT TASK CARD: A/B/B AT STA 1470 LBL 5 FLOOR SUPPORT (STRINGER) HAS CORROSION UPPER SURFACE THE CORRECT ECRA ACCOMPLISHED WAS 5321-01746. SEE WIPS FOR REMOVAL OF CORROSION AND REPAIR OF ABB FLOOR SUPPORT AT STA 1470 AND LBL 7.55 (INSTEAD OF LBL-5 ) ALL WORK ACCOMPLISHED PER ECRA 5320-01746.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,282 hrs · 10,118 cycles

AFT CABIN FLOORBEAM AT STA 1640 HAS CORROSION AT FASTENER HOLE AT LBL 3 TO RBL 3. REMOVED DAMAGED AREA AND INSTALLED FLOORBEAM REPAIR REF SRM 53-00-51 REPAIR 3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,282 hrs · 10,118 cycles

SUPPORT TASK: CABIN SEAT TRACK CORRODED BETWEEN STA 720-740 APPROX LBL 24.75 (MARKED). REMOVED, FAB'D NEW SEAT TRACK, TREATED, PRIMED AND INSTALLED IN REF TO SRM 51-10-02 AND BOEING DRWG 140N2069.

Part: STRAP — CORRODED (FUSELAGE) · airframe 46,282 hrs · 10,118 cycles

CABIN FLOORBEAM STRAP CORRODED AT STA 720 REMOVED AND REPLACED CABIN FLOORBEAM STRAP AT STA 720 REF 757-200 SRM 51-40-02 MODIFICATION OF FLOORBEAM PREVIOUSLY COMPLIED WITH SEE E/A 5320-01454 REV G.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,282 hrs · 10,118 cycles

B757-53-3-0443 AFT CABIN FLOORBEAM AT STA 1620 HAS CORROSION AROUND TWO FASTNER HOLES AT LBL 3 TO RBL 3 ( MARKED) . CUT OUT DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53 -00-51 REPAIR 3.

Part: OVEN — DEFECTIVE (GALLEY) · airframe 43,456 hrs · 9,578 cycles

BURNING SMELL, SMOKE FROM NR 205 FWD GALLEY. PULLED CIRCUIT BREAKER. PLACARD OVEN NR 205 INOP. BREAKER PULLED AND COLLARED. NEEDS OVEN 99-2532-9-0003. NO TIME DUE TO QUICK TURN INBOARD DISCREPANCIES. EXT 084979.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 40,923 hrs · 9,065 cycles

EMERGENCY EXIT DOOR INDICATOR LIGHT SIGN (LWR) DOES NOT COME ON WHEN TESTED AT MAIN DOOR R2. REPLACED BATTERY PACK CHARGER P/N 2012-1 M732 PER W/D 33-51-21, PG 902, OPERATIONAL CHECKS GOOD. S/N ON 34671, OFF 48982.

Part: TRIGGER — WORN (L1 DOOR) · airframe 38,367 hrs · 8,595 cycles

L-1 DOOR LOCKING LATCH RELEASE HOOK BROKEN, DOOR WILL NOT LOCK OPEN. REMOVED AND REPLACED TRIGGER CATCH AND COLLAR ASSY PER AMM 52-11-08, STEP D, ITEMS 1-7.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 2,398 hrs · 571 cycles

EMERGENCY LIGHTS ON WITH SWITCH IN ARMED POSITION. REMOVED AND REPLACED CHARGER PER MM 33-51-11.