N33132

Part: SENSOR — FAULTED (GIRT BAR) · airframe 96,377 hrs · 20,857 cycles

LVL1 CHRONIC HIST OF DOOR R1 ARM LT INOP WHEN DOOR IS ARMED. CHKD FLOOR FITTINGS & GIRT BAR LIFTERS FOR ANY DAMAGED OR LOOSE COMPONENTS. VERIFIED CORRECT HORIZONTAL DIMENSION OF GIRT BAR SLIDE ENGAGEMENT & VERTICAL CLEARANCE BETWEEN GIRT BAR SLIDER & SENSOR IAW AMM 25-66-11/2 01 (FIGURE 201). NO FINDINGS OF DAMAGE OR DEBRIS NOTED. CHKD OK. REMOVED AND REPLACED DOOR L1 GIRT BAR PROXIMITY SENSORS S10216 & S10217 IAW AMM 25-66-11. OPS REQUIRES TO REMOVAL ASSIST BOTTLES SAFTY PINS AND ESCAPE SLIDE SAFTY PINS. OPS TEST NEEDED PERFORMED GRIT BAR ENGAGEMENT INDICATION OPS TEST REF AMM 25-66-00. OPS CHK NORMAL. OPS CHECKED GOOD

Part: LAMP — INOPERATIVE (ZONE 800) · airframe 94,723 hrs · 20,536 cycles

DOOR ARM LIGHT ON 2L NOT ILLUMINATED WHEN DOOR ARMED RELAMPED OPS CKS OK

Part: ELEC CONNECTOR — DISCONNECTED (ZONE 200) · airframe 93,477 hrs · 20,261 cycles

ALL EMERGENCY PATHWAY LIGHTS IN FIRST CLASS INOP FOUND EMERGENCY PATHWAY LIGHT CONNECTOR AT SEAT ROW 4B DISCONNECTED AND NUMEROUS LIGHTS BURNT OUT RECONNECT AND RELAMP BURNT OUT LIGHTS ALL LIGHT OP CHK GOOD REF AMM 33-51-05

Part: LANYARD — OUT OF POSITION (ZONE 800) · airframe 93,246 hrs · 20,212 cycles

2L DOOR SLIDE TETHER PROTRUDING FROM LOWER SIDE OF PACK. PINED BOTTLE, SECURED TETHER REF AMM 25-66-01. REMOVED PIN, DOOR ARMED AND DIARMED NORMAL ADD U034572ACCOMPLISHED IDT INSPECTION OF PIN REMOVED FROM ESCAPE SLIDE. VARIFIED DOOR OPENING AND CLOSING WITH SLIDE ARMING FULLY WITH ARM LIGHT CORRECT.

Part: FRAME — DENTED (ZONE 100) · airframe 92,602 hrs · 20,057 cycles

B757-06-3-0247 AFT CARGO COMPARTMENT FR1320 R/SIDE IS DENTED ON FREE FLANGE (3EA). REPAIRED AFT CARGO COMP FR 1320 BTW 523R TO 526R IAW B757-200 SR M 53-00-07-2R-5.

Part: DOOR — MISSING (ZONE 400) · airframe 92,124 hrs · 19,946 cycles

ENGINE 1 PANEL 413CL MISSING ON ARRIVAL INTO SNN OFF FLIGHT 976-16. REF IPC 71-11-04-02 ITEM 345. M/E 19-7111-3-0005 . PDA EVENT. DUPLICATE LOG, SEE 9272069 FOR ACTIONS TAKEN FOR REPAIR. THIS LOG FOR REPORTING.IDG OIL ACCESS PANEL ENG L SHEARD OFF QC REVIEWED RECORDS UPDATE PANEL WAS GIVEN TO SHEETMETAL FOR INSTALLATION DUE TO LOCK FASTENER NEEDED FOR INSTALL. CARRIED OUT INTERM REPAIR PER PART 1 OF EC/RA # 7111-02688, DIP RAISED FOR PERMANENT REPAIR WITHIN 1 FLT CYCLE TOMC APPROVES 71-DIP PER ECRA 7111-02688. ACCOMPLISH PERMANENT REPAIR PER PART 3 OF ECRA 7111-02688 AFTER 1 FLIGHT CYCLE. NR 1 ENGINE IDG SERVICE PANEL

Part: PRESSURE SWITCH — UNKNOWN · airframe 91,206 hrs · 19,764 cycles

L HYD QTY 0 L SYS PRESS 0 L RSVR MSG ON HYD PG FLAGGING FOR SDR R&R L ENGINE HYD SYSTEM PRESSURE SWITCH REF B757 FIM 27-21 FAULT TREE 809, AMM 29-11-17-004-001. PERFORMED L ENGINE OPPS AND LEAK CHECK OF LEFT HYD SYSTEM, OPS CHECK GOOD. CLEANED LH HYD QTY INDICATOR CANNON PLUG. ALL INDICATIONS NORMAL AT THIS ADD EMP:U412272 TIME. PARTS USED: 19-2911-3-0095,QTY :1 40-0595-3-1976,QTY :1 PARTS USED: 19-2911-3-095,QTY :1 40-0595-3-1976,QTY :1

Part: OVEN — SMOKE (AFT GALLEY) · airframe 90,305 hrs · 19,571 cycles

AFT CENTER OVEN SMOKING IN FLIGHT SOURCE OF OVEN SMOKE IDENTIFIED GO TO STEP E (DISPOSITION OF EVENT). STEPS C AND D DO NOT NEED TO BE ACCOMPLISHED REF AMM SMOKE/ODOR IN THE FLIGHT DECK AND/OR CABIN CONDITIONAL INSPECTION (ADDED BY EC0500-01014) REFERENCE: TASK 05-51-58-910-801-C1. INSPECTED OVEN 2 AFT GALLEY. FOUND EVIDENCE OF CHOCOLATE SAUCE SPILL. NEEDS CLEANING. REF B757-200 AMM TASK 05-51-58-910-801-C1. INFORMED TOMC. OVEN DEFERRED AS PER MEL 2520P. M PROC C/W. APPROVED NEF 2520P NOC DESK: 757 NAME: AHMED Z DATE: 13-APR-24- AFT CENTER OVEN. DIRTY. DEACTIVATED. DEFERRED REF NEF 2520P REMOVEED AND REPLACED AFT CENTER OVEN IAW AMM 25-34-00-000-801,OPS CHECK GOOD.

Part: DOOR — LEAKING (1L) · airframe 87,745 hrs · 18,959 cycles

NO. 1, 2 AND 4 PASSENGER DOORS DOOR (WRITE LOCATION) AIR NOISE PROBLEM WAS ENCOUNTERED WHICH IS NOT COVERED IN THE FAULT CODE DIAGRAMS 01 CREW REPORTS DOOR 1L LEAKING ONLY UPON INITIAL INSPECTION FOUND WAVY SEALANT ON FUSELAGE , NOT CONTACTING THE DOOR VERY WELL . SEALANT REFERENCE DOOR FRAME SEAL REPAIRS AMM REF 52-11-80-280-801-C1 AND ECRASI 5210-02755 ECRA 5210-02548 AT DOOR 1L, SMOOTHED DEFORMED AREAS OF LEVELING COMPOUND AND FOUND THAT FWD LOWER CORNER NEEDS LEVELING COMPOUND BUILD UP IN THIS CORNER. FOUND SEALANT INSTALLED FWD UPPER AND LWR CONORS. REMOVED SEALANT. NEED FILLER EC-3587 TO COMPLETE REPAIR. REF ECRA 5210-02548. APPLIED SEALANT TO DOOR 1L, REF ECRA 5210-02548, PLANE STILL NEEDS TO BE PRESSURIZED TO CHECK FOR LEAKS. PARTS USED: 00-0602-3-0156,QTY :1 APPLIED SEALANT TO DOOR 2R REF ECRA 5210-02548. NEEDS PRESSURIZED AND LEAK CHECKED. SANDED DOWN AND APPLIED SEALANT TO DOOR 4L, REF ECRA 5210-02548.NNEEDS LEAK CHECK. ACP EXCESSIVE CABIN PRESSURE LEAKAGE TEST PER AMM 05-51-24-702-001 DECAY CK WITHIN LIMITS. AT 2 DIFF ACFR SEALED. AT 4 DIFF NO SQUEAL HEARED.

Part: FRAME — CRACKED (LH FRAME STA 760) · airframe 86,747 hrs · 18,762 cycles

FRAME CRACKED THROUGH RIVET HOLE SEEN ON AFT SIDE OF L/H FRAME STA 760 FOR OVERHEAD BIN ATTACH BRACKET BETWEEN STR 8 AND 9L. REPAIRED FRAM CRACK AT STA 760 LH SIDE IAW B757 SRM 53-00-07 REPAIR#8 SHEET 1 DETAIL 1. ACCOMPLISHED ON AMES NR 155339-0200-0215 ENTERED IN ERROR, THIS REPAIR NOT ON AIRCRAFT 0132.

Part: CONTROL MODULE — LEAKING (HORIZ STAB) · airframe 84,549 hrs · 18,269 cycles

CENTER HYD QTY LOSS DOWN TO .05, TURNED OFF PUMP, QTY BACK UP TO .017. FOUND LEFT STAB TRIM CONTROL MODULE LEAKING. REMOVED LEFT STCM AND TRANSFER FITTINGS AND INSTALLED NEW O-RINGS OVER TO NEW PART IAW AMM 27-41-05-022-001. VERIFIED LEFT STCM PN AND FITTING INSTALL ONTO NEW PART AND OK TO INSTALL REF GMM 9-25-05. LOG PAGE 3195571 CREATED FOR STCM PRESSURE SWITCH BENT CONNECTOR. REPLACED LEFT STCM REF AMM 27-41-05-022-001. UNABLE TO STAB TRIM NOSE UP. SUSPECT BAD STCM FROM STOCK. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1198391 SN OFF 1031 MODULE, CONTROL OFF 19-2741-9-0002 1031 ON 19-2741-9-0002 0996. REPLACED LEFT STCM REF AMM 27-41-05-022-001. LEAK CHECK AND OPS CK GOOD. GOOD FOR RETURN TO SERVICE. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1231978 SN OFF 0996 MODULE, CONTROL OFF 19-2741-9-0002 0996 ON 19-2741-9-0002 0983.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 78,822 hrs · 17,105 cycles

DURING A SERVICE CHECK, SEAT 4B FWD EMERGENCY LIGHT INOPERATIVE. FOUND THE CONNECTOR LOOSE IAW DRAWING BR2013-P-7572CO-5. SECURED THE CONNECTOR. CHECKED GOOD.

Part: ALTIMETER — FAILED (COCKPIT) · airframe 78,206 hrs · 16,982 cycles

FO ALTIMETER FAILED TEMPORARIILY. CAME BACK W/700 FT ERROR THEN RESOLVED TO NORMAL. R&R F/O ALTIMETER REF AMM 34-13-01 OPS CHECK NORMAL

Part: FSEU — FAULTY (TE FLAPS) · airframe 77,660 hrs · 16,861 cycles

TRAILING EDGE FLAP SYSTEM EICAS MESSAGE, FLAP/SLAT ELEC DISPLAYED. EMERGENCY DECLARED, DURING DESCENT EXTENDING THE FLAPS FROM 20 TO 25 AT APPROXIMATELY 180 KTS. BITE CHECKED ALL 3 FSEU AND ONLY NOTED FAULT ON FSEU NR 1 WHICH SHOWED FLA FAIL. BITE. ACCOMPLISHED IAW FIM AND FOUND TO OPERATE NORMALLY AT ALL FLAP SETTING INCLUDING FLAP LOAD RELIEF FUNCTIONS. FIM 27-51-00-815-810 FIG .107. REPLACED FSEU NR 1 AS A PRECAUTION IAW MM 27-51-01. BITE TEST FUNCTIONS CHECKED GOOD AND FLAP OPERATIONS CHECKED GOOD.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 75,963 hrs · 16,511 cycles

FUMES IMMEDIATELY AFTER TAKE OFF, NOTICED IN COCKPIT AND MID CABIN. CHEMICAL ODOR.CLEARED 10 MINUTES LATER. FINISHED INSPECTION AND OPERATIONAL CHECKS. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE

Part: FILTER — ODOR (RECIRCULATION) · airframe 75,963 hrs · 16,511 cycles

DURING TAKEOFF, SMELLED FUMES FOR 5 MINUTES. FLIGHT CREW INDICATED NO FUMES. IAW AMM 05-51- 58-910-801C1 REMOVED AND REPLACED BOTH LEFT AND RIGHT HEPA RECIRCULATION FILTERS IAW AMM 21-25-02. NO OTHER DEFECTS FOUND. OK TO CONTINUE.

Part: FLASHLIGHT — NOT SEATED (CABIN) · airframe 75,682 hrs · 16,456 cycles

1R EMERGENCY FLASHLIGHT INOP. RESEATED EMER FLASHLIGHT AT FWD FLT ATTENDANT STATION, FWD GALLEY, OPS CHK GOOD REF AMM 25-64-00.

Part: SWITCH — FAILED (LAVATORY LATCH) · airframe 72,754 hrs · 15,870 cycles

CONTINUOUS ELECTRICAL ODOR FROM R3 LAVATORY, RETURNED TO DEPARTURE AND FOUND THE RT AFT LAVATORY DOOR LATCH LIGHT SWITCH OVERHEATED AND CAUSING ODOR. REMOVED AND REPLACED THE DOOR SWITCH AND OPS CHECKED GOOD.

Part: LAMP SOCKET — DAMAGED (CABIN) · airframe 70,508 hrs · 15,408 cycles

REFERENCE LOG PAGE 8377435. SPARKS & SMOKE FROM MID-LAVATORY, FOUND WIRING CONNECTING TO A1 TERMINAL ON MID LAVATORY BALLAST DAMAGED FROM HEAT. R & R L1 LAMP SOCKET & WIRING GOING TO MID-LAVATORY BALLAST, RT 1 TERMINALS A1 & 1. REF IFM 25-40-02.

Part: DOOR FRAME — GOUGED (FUSELAGE) · airframe 69,265 hrs · 15,143 cycles

AFT ENTRY R4 DOOR, SURROUND STRUCTURES AT 1640, AT STRINGER 6R FRAME LIP HAS GOUGE. REPAIRED DOOR SURROUND STRUCTURE IAW ECRA 5310-06597.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,265 hrs · 15,143 cycles

CABIN INTERIOR STRUCTURE STATION 800, FRAME IS CRACKED AT FASTENER, BETWEEN STRINGER -8 RT & -9 RT. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED & INSTALLED REP AIR DOUBLERS IAW SRM 53-00-07 REPAIR 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,265 hrs · 15,143 cycles

CABIN INTERIOR STRUCTURE, STATION 760, FRAME IS CRACKED AT FASTENER, BETWEEN STRINGER -8 RT & -9 RT. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED & INSTALLED REPAIR DOUBLERS IAW SRM 53-00-07 REPAIR 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,265 hrs · 15,143 cycles

LIGHT CORROSION ON FLOORBEAM UPPER CHORD STATION 365, BL 0 - RBL 25. ACCOMPLISHED REPAIRED STATION 365 FLOORBEAM LBL 14 - RBL 40 IAW ECRA 5310-06590.

Part: STRAP — CRACKED (FUSELAGE) · airframe 69,265 hrs · 15,143 cycles

CABIN FWD ENTRY STRUCTURE, BETWEEN STATION 345 TO 363.5, AT BL 0 STABILIZATION STRAP IS CRACKED. COMPLETED STRAP REPAIR AT STATION 345-363.5, BL 0 IAW SRM 53-00-51 REPAIR 13.

Part: PAN — GOUGED (L4 DOOR) · airframe 69,265 hrs · 15,143 cycles

L4 DOOR EXTERIOR HANDLE PAN HAS 2 GOUGES IN PAN. R & R, INSTALLED NEW HANDLE PAN COMPLETE IAW SRM 51-40-02.

Part: STRAP — CRACKED (FUSELAGE) · airframe 69,265 hrs · 15,143 cycles

AFT CARGO COMPARTMENT CEILING, STABILIZATION STRAP IS CRACKED AT STATION 1380, RBL 45. COMPLIED WITH REPAIR 12 OF SRM 53-00-51.

Part: HYDRAULIC LINE — RUPTURED (RT MLG) · airframe 68,793 hrs · 15,053 cycles

FLIGHT RETURNED DUE TO ZERO HYD QTY ON LT HYD SYS. SYS SHUTDOWN & EMER DECLARED. NOSE WHEEL STEERING AFFECTED. FOUND FWD FLEXIBLE LINE ON RT MLG DOWN LOCK ACTUATOR RUPTURED. INSTALLED NEW MLG FLEX LINE, SERVICED HYDS, BLED SYS & PERFORMED OPERATION CHECKS OF ENG & ELEC PUMPS. INSPECTED PRESS & CASE DRAIN MODULE DIFF PRESS IND IAW MM 29-11-00-201. EXTENDED LEAK CHECKED GOOD.

Part: HYDRAULIC LINE — RUPTURED (RT MLG) · airframe 68,786 hrs · 15,052 cycles

REFERENCE LOG PAGE 8047966. LT HYD SYS LEAKED TO ZERO. FOUND FWD FLEXIBLE LINE ON RT MLG DOWN LOCK ACTUATOR RUPTURED. INSTALLED NEW FLEXIBLE LINE, PN 19-3232-3-0067. REFERENCED IPC 32-32-51-15 ITEM 270. SERVICED LT HYD SYS TO 48%.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,477 hrs · 14,995 cycles

SEAT EMER LIGHTS INOPERATIVE ROW 20 TO 30. REPLACED LIGHT ASSEMBLY AT ROW 20 & PACK FUSES OPERATIONS GOOD. REF LOG PAGE 8173409, REPLACED SPLICE UNDER SEAT 30 EMER EXIT.

Part: CONNECTOR — BROKEN (CABIN) · airframe 67,328 hrs · 14,765 cycles

ALL OF FIRST CLASS SEATS EMER LIGHTS INOPERATIVE. REPLACED CONNECTORS D9011J, D90112J & D90112P AT SEAT 4B IAW SWPM 20-61-28 SDR.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,945 hrs · 14,680 cycles

CABIN PAX L1, R1, L4 RT SIDE OVERHEAD BEAM, 5 ROW SEATS, SOME EMER LIGHTS INOPERATIVE & L1 EXTERIOR EMER LIGHTS INOPERATIVE & L1 EXTERIOR EMER LIGHT INOPERATIVE. SDR FORM ATTACHED. BATTERY PACK AT POS 737 WAS R & R AND AT POS 4730, 4731, L763 WERE RECONNECTED. ALL HAD OPERATIONS TEST OK IAW AMM 33-51-07 & 33-51-11.

Part: PITOT HEAD — FAULTY (PITOT/STATIC SYS) · airframe 64,430 hrs · 14,228 cycles

RT AUX PITOT EICAS MESSAGE. REMOVED RT AUX PITOT PROBE. INSTALLED RT AUX PITOT PROBE IAW AMM 34-11-01-024-044. OPERATIONS CHECKED GOOD, LEAK TEST PASSED IAW AMM 34-11-00-735-175.

Part: MOTOR — FAILED (OUTFLOW VALVE) · airframe 58,067 hrs · 13,108 cycles

PRESSURIZATION AT FL 350 CABIN HORN SOUNDED. CABIN RATE OF CLIMB WAS 2000 PLUS PRIOR TO THIS EVENT CABIN TEMP WAS 80+ PACK SWITCH SET TO MANUAL "C" TO COOL THEN BACK TO AUTO PERFORMED FIM TASK 21-30-00-815-803. CONTROLLER DISPLAYED A/C MOTOR FAULT. R & R FWD & AFT A/C MOTORS FOR THE CABIN PRESSURE OUTFLOW VALVE ACTUATOR IAW MM 21-31-05. OPS CHECKED GOOD, PRESSURIZED CABIN, ALL SYS NORMAL RT PACK FLOW NORMAL AND COLD NO DEFECTS NOTED WITH RT & LT PACKS.

Part: SENSOR — FAILED (LT ENGINE) · airframe 56,593 hrs · 12,860 cycles

12 MIN AFTER T/D LEVEL AT FL230 THE LEFT ENG BLEED OFF LIGHT CAME ON, AS WELL AS THE L CENTER FUEL PUMP PRESSURE LIGHT AS WELL AS 0 ON THE N3 INDICATOR AND ZERO ON STDBY N3 INDICATOR. REMOVED AND REPLACED N3 (HP) TACHOMETER TRANSMITTER AT NR 1 ENG PER AMM 77-12-02-404. LEAK TEST GOOD. OPS CHECK PER AMM 77-12-0 0-715 OK. ALL PARAMETERS MATCHES. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1492008 SN OFF 01442 SENSOR, SPEED, OFF 19-7712-9-9001 1442 ON 19-7712-9-9001 6556.

Part: SOLENOID — FAILED (COCKPIT DOOR) · airframe 54,645 hrs · 12,531 cycles

FLIGHT DECK DOOR OPEN LIGHT ILLUMINATES INTERMITTENTLY INFLIGHT WITH DOOR CLOSED AND LOCKED ITEM PLACED ON PLACARD IAW MEL 52-51-1 CONTROL 569483 NO TIME DUE TO WORKLOAD R&R FLIGHT DECK DOOR SOLENOID ACTUATED DOOR STRIKE AND MECHANICAL L CATCH ASSY IAW AMM 52-52-01. OPS CHECK GOOD. MEL CLEARED, A/C OK TO CONTINUE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 45,983 hrs · 10,804 cycles

SUPPORT TASK STATION 1640 BL-0 FLOORBEAM CORRODED. REPAIRED SECTION CABIN FLOORBEAM AT STA 1640 BL-0 PER SRM 53-00-51 FIG 201 REPAIR 3.

Part: MONITOR — BURNED (ROW 20) · airframe 39,421 hrs · 9,465 cycles

REPORT OF ELECTRICAL SMOKE IN THE AREA OF ROW 20 OVERHEAD. REMOVED POWER TO THE RIGHT UTILITY BUS AND TURNED OFF THE L+R RECIRC FANS, SMELL DISSIPATED. CONTINUED TO EWR WITH NO FURTHER ACTION. FOUND OVERHEAD MONITOR ATE ROW 20 BURNED.

Part: SKIN — CRACKED (RT WING) · airframe 22,772 hrs · 5,209 cycles

INSPECTION FOUND A 4.5 INCH CRACK IN RIGHT WING FIXED LEADING EDGE SKIN BETWEEN OSS 397 AND OSS 421. THE SKIN WAS REPAIRED IAW EA 5731-01010, REV D, OP 4 AND SRM 57-41-01.

Part: SKIN — CRACKED (RT WING) · airframe 22,772 hrs · 5,209 cycles

INSPECTION FOUND A 6.25 INCH CRACK IN RT WING FIXED L/E SKIN AT STA OSS 421- OSS 471. THE SKIN WAS REPLACED IAW EA 5731-01010, REV D, OP 3.