N587UA

Part: PAN — GOUGED (L4 DOOR HANDLE) · airframe 83,339 hrs · 26,555 cycles

L4 DOOR EXTERNAL HANDLE PAN GOUGED AS MARKED 034-036. L-4 DOOR HANDLE PAN FOUND OUT OF LIMITS IAW B757-200 SRM 52-10-0 1 FIG. 101 L=3.0 W=1.0 D=.025 REMOVED AND INSTALLED NEW L4 DOOR HANDLE PAN P/N 146N6201U7 IAW DWG 146N6100 AND B757-200 SRM 51-4 0-02 PG. 1-10. WORK ACCOMPLISHED AND RECORDED ON ST-SAA N/R 0035 451 BY MECH V919728 AND INSPECTED BY V919675.

Part: CREASE BEAM — CRACKED (BS 1040) · airframe 83,339 hrs · 26,555 cycles

(B757-53-3-6006) MAIN CABIN FLOOR STRUCTURE INBOARD CHORD AT STA 1040 STR 17R HAS A CRACK AROUND FASTNER HOLE. REF ST SAA N/R 0 035277 FOUND 1.0" LONG CRACK ON CABIN CREASE BEAM INNER CHORD AT STA 1 040 S-17R, REMOVED AND INSTALLED NEW CREASE BEAM INNER CHORD BET WEEN STA 900-1040 S17R, RBL60 IAW DWG 144N5152 AND B757-200 SRM 51-40-02 PG 1-10. THIS IS TRANSCRIBED INFORMATION ACCOMPLISHED A ND RECORDED ON ST SAA N/R 0035277. WORK WAS ACCOMPLISHED BY MECH V919728. INSPECTION COMPLETED AND ACCEPTED BY VT-SAA INSP V919676

Part: CREASE BEAM — CRACKED (BS 1040) · airframe 83,339 hrs · 26,555 cycles

(B757-53-3-6006) MAIN CABIN FLOOR STRUCTURE INBOARD CHORD AT STA 1040 STR 17R HAS A CRACK AROUND FASTNER HOLE. REF ST SAA N/R 0 035277 FOUND 1.0" LONG CRACK ON CABIN CREASE BEAM INNER CHORD AT STA 1 040 S-17R, REMOVED AND INSTALLED NEW CREASE BEAM INNER CHORD BET WEEN STA 900-1040 S17R, RBL60 IAW DWG 144N5152 AND B757-200 SRM 51-40-02 PG 1-10. THIS IS TRANSCRIBED INFORMATION ACCOMPLISHED A ND RECORDED ON ST SAA N/R 0035277. WORK WAS ACCOMPLISHED BY MECH V919728. INSPECTION COMPLETED AND ACCEPTED BY VT-SAA INSP V919676

Part: STRAP — CORRODED (BS 1790) · airframe 83,339 hrs · 26,555 cycles

(B757-49-3-8084) APU AIR INLET FWD STRAP AT APPROX. STA 1790, BE TWEEN STGR 3R TO 6R HAS CORROSION. REF STSAA N/R 0035240. FOUND CORROSION REMOVAL ON APU INLET BOX FWD STRAP AT STA 1790 B ETWEEN S-3R AND S-6R OUT OF LIMITS IAW B757-200 SRM 53-80-02-F10 1. L=4.0, W=1.0, D=.063. REMOVED AND INSTALLED NEW STRAP P/N 148 N3138-20 IAW DWG 148N3105 AND B757-200 SRM 51-40-02 PG 2. THIS I S TRANSCRIBED INFORMATION ACCOMPLISHED AND RECORDED ON ST SAA PAPER N/R 0035240. WORK WAS ACCOMPLISHED BY MECH V919728. INSPECTION COMPLETED AND ACCEPTED BY VT-SAA INSP V919676 FOR CORRECTIVE ACTION OF LOGPAGE 8455173 SEE UPDATE ABOVE DATED 09DEC18. INSPECTION COMPLETED AND ACCEPTED BY VT-SAA INSP V919676

Part: ANGLE — CORRODED (BS 1787-1825) · airframe 83,339 hrs · 26,555 cycles

B757-49-3-8084, SECONDARY FINDING AFTER REMOVAL OF APU INLET BOX FOUND CORROSION ON UPPER SUPPORT AT STA 1825 TO 1787 S-3R. REF ST SAA N/R 0035392. FOUND CORROSION REMOVAL ON APU INLET BOX SUPPORT AT STA 1825 TO 1787 S-3R OUT OF LIMITS IAW B757-200 SRM 53-80-02-F101. L=4.0. W =1.0, D=.041. REMOVED AND INSTALLED NEW SUPPORT P/N 654N0244-620 IAW DWG 148N3105 AND B757-200 SRM 51-40-02 PG.2. THIS IS TRANSC RIBED INFORMATION ACCOMPLISHED AND RECORDED ON ST SAA PAPER N/R 0035392. WORK WAS ACCOMPLISHED BY MECH V919728. INSPECTION COMPLETED AND ACCEPTED BY VT-SAA INSP V919676 FOR CORRECTIVE ACTION OF LOGPAGE 8455206 SEE UPDATE ABOVE DATED 09DEC18. INSPECTION COMPLETED AND ACCEPTED BY VT-SAA INSP V919676

Part: SUPPORT — CORRODED (APU INLET BOX) · airframe 83,339 hrs · 26,555 cycles

B757-49-3-8084, SECONDARY FINDING AFTER REMOVAL OF APU INLET BOX FOUND CORROSION ON UPPER SUPPORT AT STA 1825 TO 1787 S-3R. REF ST SAA N/R 0035392. FOUND CORROSION REMOVAL ON APU INLET BOX SUPPORT AT STA 1825 TO 1787 S-3R OUT OF LIMITS IAW B757-200 SRM 53-80-02-F101. L=4.0. W =1.0, D=.041. REMOVED AND INSTALLED NEW SUPPORT P/N 654N0244-620 IAW DWG 148N3105 AND B757-200 SRM 51-40-02 PG.2. THIS IS TRANSC RIBED INFORMATION ACCOMPLISHED AND RECORDED ON ST SAA PAPER N/R 0035392. WORK WAS ACCOMPLISHED BY MECH V919728. INSPECTION COMPLETED AND ACCEPTED BY VT-SAA INSP V919676

Part: STRAP — CORRODED (APU INLET BOX) · airframe 83,339 hrs · 26,555 cycles

(B757-49-3-8084) APU AIR INLET FWD STRAP AT APPROX. STA 1790, BE TWEEN STGR 3R TO 6R HAS CORROSION. REF STSAA N/R 0035240. FOUND CORROSION REMOVAL ON APU INLET BOX FWD STRAP AT STA 1790 B ETWEEN S-3R AND S-6R OUT OF LIMITS IAW B757-200 SRM 53-80-02-F10 1. L=4.0, W=1.0, D=.063. REMOVED AND INSTALLED NEW STRAP P/N 148 N3138-20 IAW DWG 148N3105 AND B757-200 SRM 51-40-02 PG 2. THIS I S TRANSCRIBED INFORMATION ACCOMPLISHED AND RECORDED ON ST SAA PAPER N/R 0035240. WORK WAS ACCOMPLISHED BY MECH V919728. INSPECTION COMPLETED AND ACCEPTED BY VT-SAA INSP V919676

Part: ANGLE — CORRODED (BS 1825) · airframe 83,339 hrs · 26,555 cycles

B757-49-3-8084 SECONDARY AFTER REMOVAL OF APU INLET BOX FOUND CO RROSION ON LWR SUPPORT AT STA 1825 TO 1787 S-6R. REF ST SAA N/R 0035393. FOUND CORROSION REMOVAL ON APU INLET BOX LWR SUPPORT AT STA 1825 TO 1787 S-6R OUT OF LIMITS IAW B757-200 SRM 53-80-02-F101. L=6. 0 W=1.0 D=.060. REMOVED AND INSTALLED NEW SUPPORT P/N 148N3152-1 IAW DWG 148N3105 AND B757-200 SRM 51-40-02 PG.2. THIS IS TRANSC RIBED INFORMATION ACCOMPLISHED AND RECORDED ON ST SAA PAPER N/R 0035393. WORK WAS ACCOMPLISHED BY MECH V919728 INSPECTION COMPLETED AND ACCEPTED BY VT-SAA INSP V919676

Part: WARNING LIGHT — INOPERATIVE (L2 DOOR) · airframe 79,955 hrs · 25,911 cycles

L2 DOOR SLIDE ARMED LIGHT NOT ILLUMINATED WITH DOOR ARMED. PERFORMED A SYSTEM TEST OF THE R2 GIRT BAR OPS CHECKED GOOD IAW 52-11-25-735-024, SLIDE ARMED LIGHT ILLIMINATES WITH DOOR ARMED.

Part: GIRT BAR — DIRTY (L1 DOOR) · airframe 79,829 hrs · 25,887 cycles

L1 DOOR SLIDE LIGHT INTERMITTENT, CLEANED AND INSPECTED THE GIRT BAR IAW TASK 25-66-802. OPS CHECKED GOOD

Part: LIGHT — INOPERATIVE (SLIDE LIGHT) · airframe 79,641 hrs · 25,852 cycles

1L SLIDE LT OUT RELAMPED, CHECKED GIRT BAR FITTING AREA, OPS NORMAL.

Part: LIGHT — INTERMITTENT (R3 DOOR) · airframe 79,424 hrs · 25,811 cycles

R3 DOOR SLIDE ARMED LIGHT INTERMITTENT. REPLACED AND SECURED THE LIGHT ASSY. OPS CHECKED OK.

Part: OVEN — OVERHEATED (GALLEY) · airframe 79,360 hrs · 25,799 cycles

OVEN IN MID GALLEY OVERHEATED, SMELLS OF SOMETHING BURNING ALSO ADJACENT WALL IS BURNED. REMOVED AND REPLACED THE OVEN IAW AMM 25-32-98. OPS CHECKED OK.

Part: WIRE — CHAFED (EMERGENCY LIGHT) · airframe 79,218 hrs · 25,771 cycles

EMERGENCY LIGHT ABOVE THE R1 DOOR WILL NOT TEST. FOUND THE WIRES W3632-9054-20 AND W3632-9014-20 CHAFED. SPLICED THE WIRES IAW WDM 33-51-12 AND SWP 20-10-13. THE EMERGENCY LIGHT OPS CHECKED GOOD.

Part: LANYARD — OUT OF ADJUST (L2 DOOR) · airframe 78,708 hrs · 25,674 cycles

L2 DOOR ARMED ESCAPE SLIDE WARNING RIBBON WILL NOT SNAP, REPLACED THE RIBBON AND ADJUSTED THE SNAP. OPS CHECKED GOOD.

Part: CHANNEL — DENTED (FWD CARGO DOOR) · airframe 78,693 hrs · 25,671 cycles

FWD CARGO DOOR AFT LOWER EDGE HAS A DENT. REMOVED AND REPLACED THE FWD CARGO LOWER EDGE BEAM IAW SRM 51-40-02, PG 7.

Part: GIRT BAR — NO TEST (R1 DOOR SLIDE) · airframe 78,446 hrs · 25,623 cycles

R1 DOOR GIRT BAR FAILED LEAF SPRING INSPECTION. REMOVED AND REPLACED THE GIRT BAR IAW AMM 25-66-10-002 -001, AND AMM 25-66-10-402-022.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 78,446 hrs · 25,623 cycles

ROW 1 THRU 4, LT SEAT MOUNTED EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED ONE CONNECTOR ON SEAT 1B IAW WDM 33-51-21 AND AMM 33-51-00. OP CHECKED PASSED.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 78,446 hrs · 25,623 cycles

EMERGENCY EXIT SIGN ABOVE THE R2 DOOR FOUND INOPERATIVE. TROUBLESHOT AND FOUND A FUSE TO BE BAD, REMOVED AND REPLACED FUSE IN THE POWER SUPPLY M732, OPS TESTED GOOD IAW WDM 33-51-13, AND AMM 33-51-07-962-071.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 78,446 hrs · 25,623 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT 5B, TROUBLESHOT AND FOUND CONNECTOR P1 UNDER SEAT 5B BROKEN IN HALF. REPLACED THE CONNECTOR IAW SWPM 20-61-28. OP CHECK PASSED IAW AMM 33-51-00

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 78,446 hrs · 25,623 cycles

EMERGENCY LIGHT SIGN INOPERATIVE ABOVE R1 DOOR. TROUBLESHOT AND TERMINATED A WIRE AT CONNECTOR D4528. OP TESTED GOOD IAW SWPM 20-00-12 AND AMM 33- 51-01.

Part: ANGLE — DAMAGED (1R DOOR) · airframe 78,446 hrs · 25,623 cycles

R1 DOOR, INTERIOR ANGLE IS DAMAGED, JUST BELOW UPPER HINGE AND FWD OF DOOR MOUNTED TORQUE TUBE. REMOVED R1 DOOR IAW AMM 52-11-01. REMOVED AND REPLACED THE INTERIOR ANGLE IAW SRM 51-40-0 2. INSTALLED THE R1 DOOR IAW AMM 52-11 -01.

Part: STRAP — CRACKED (BS 345) · airframe 78,446 hrs · 25,623 cycles

FLOOR BEAM STABILIZATION STRAP IS CRACKED AT BS 345, BL0. ACCOMPLISHED A REPAIR IAW SRM 53-00-51, FIG 201, REPAIR 13.

Part: SUPPORT STRAP — CRACKED (BS 369) · airframe 78,446 hrs · 25,623 cycles

MEC BS 369, LBL 25 FLOORBEAM LWR SUPPORT STRAP HAS A CRACK AT A PREVIOUS REPAIR. ACCOMPLISHED A REPAIR BS 365 - 377, LBL 25 IAW SRM 53-00-51, FIG 201, REPAIR 12 AND 13.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 78,446 hrs · 25,623 cycles

FOUND EMERGENCY LIGHT INOPERATIVE AT ROW 4AB BULLNOSE. TROUBLESHOT AND FOUND A BAD FUSE IN THE POWER SUPPLY M10567. REPLACED THE FUSE IAW AMM 53-51-07. OP CHECK PASSED.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 78,446 hrs · 25,623 cycles

FOUND THE EMERGENCY LIGHT INOPERATIVE AT ROW 5AB. TROUBLESHOT AND FOUND THE CONNECTOR P1 UNDER SEAT 5B BROKEN IN HALF. REPLACED THE CONNECTOR IAW SWPM 20-61-28. OP CHECK PASSED IAW AMM 33-51-00.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 78,446 hrs · 25,623 cycles

FOUND THE EMERGENCY LIGHT INOPERATIVE AT THE L2 DOOR. TROUBLESHOT AND FOUND A BAD FUSE IN POWER SUPPLY M10567. REPLACED THE FUSE IAW AMM 33-51-07. OPS CHECK PASSED.

Part: GIRT BAR — BINDING (L2 DOOR) · airframe 77,754 hrs · 25,489 cycles

DOOR MOUNTED ESCAPE SYSTEM DOOR 2L. EVACUATION SLIDE ARMING LEVER, FAILED TO MOVE, BINDING, AT ENTRY/SERVICE DOOR DOOR 2L. ARM LEVER BINDING CLEAN GIRT BAR AND LUBE IT AS REQUIRE. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,666 hrs · 25,472 cycles

OVERHEAD BIN EMERGENCY LT AT ROW 3AB INOP. RELAMPED EMERGENCY LT. OPS CHECK GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 77,666 hrs · 25,472 cycles

EMERGENCY EXIT SIGN INOP AT ROW 21D. REPLACED EXIT SIGN. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (L4 DOOR) · airframe 77,581 hrs · 25,456 cycles

DOOR 4L SLIDE LIGHT APPEARS BURNT OUT. RELAMPED OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 77,141 hrs · 25,370 cycles

ROW 4AB EMERGENCY LITE IN BULLNOSE INOP. RPLD POWER SUPPLY M733. OPS CK OK PERFORMED RII INSP OF POWER SUPPLY AND OPS CK . NO DEFECTS FOUND.

Part: LIGHT — LOOSE (CABIN) · airframe 77,130 hrs · 25,368 cycles

MID LAV EEL LITE INOP. SECURED LOOSE LAMP, CKS OK ACCOMPLISHED IDT MID LAV EEL LITE. OP CK GOOD.

Part: RELAY — FAULTY · airframe 76,985 hrs · 25,339 cycles

STARTED LEFT ENGINE ALL NORMAL. STARTED RT ENGINE, ALL NORMAL LEFT ENG ROLLED BACK, SHUTDOWN, VISUALLY INSPECTED THE NR 1 ENG INLET AND EXHAUST, INTERROGATED EPCS AND EICAS, NO FAULTS OR DEFECTS NOTED. PERFORMED FIM TASK 73-21-00-815-802-P00, PERFORMED FUEL PUMP PRESSURE CHECK 4 ON NR 1 ENGINE IAW FIM TASK. REMOVED AND REPLACED NR 1 ENGINE FUEL PUMP FILTER. IAW MM 73-11-02 PERFORMED WIRING CHECK ON LEFT EEC TO PMA USING FIM 73-21- NO FAULT MESSAGES SHOWN. INSPECTED FILTER AND FOUND NO DEBRIS. 00-815-802-POO STEP 8. NO FAULT FOUND. PERFORMED STEP 9 OPEN CIR THE FIM FUEL PUMP FILTER REQUIRES LEAK CHECK PER POWER PLANT TABLE. CUIT CHECK PER SAME FIM ABOVE WITHOUT ANY FAULT. IAW MM 71-00-00/501. R & R RELAYS K10523 & K10124 PER WDM 73-21-32 & 76-11-11. OPS CK GOOD.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 76,554 hrs · 25,253 cycles

AT FLAP EXTENSION TE FLAP DISAGREE LT ON. FLAP HANDLE 1 WITH IND ICATOR SHOWING FL UP. EMERGENCY DECLARED. BITE TEST ALL THREE FSEU NO EXISTING FAULT, FAULT HISTRY 00 LEG FAULT 305 ON NR 1 FSEU, FAULT CODE 327 ON NR 2 FSEU FOR FAULT HIST RY LEG 00. PERFORMED SYSTEM TEST NO ACTIVE OR EXISTING FAULTS AT THIS TIME. OPS CHECKED GOOD IAW FIM 27-51-00

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 72,101 hrs · 24,386 cycles

FOUND DAMAGE TO STRINGER 16L, BETWEEN STATION 600 & 620. IAW AVO 151106-5687-1 PART 2, CAREFULLY REMOVED THE EXISTING STRINGER SPLICES & REPAIRED SECTION.

Part: SKIN — DENTED (FUSELAGE) · airframe 72,101 hrs · 24,386 cycles

DENT FOUND ON WALK AROUND, FWD OF L2 DOOR APPROX BS 600, 24 INCHES BELOW PAX WINDOW, 1 INCH WIDE, 1 - 4 INCH DEEP APPROX. IAW AVO ESC151106-5687-1 PERFORMED STEP 1, CAREFULLY REMOVED ALL FASTENERS ATTACHING THE EXISTING REPAIR SKIN & SPLICES, DISCARDED CONT OF AMIS ITEM 1012003, VERIFIED STEP 01 COMPLETED IAW AVO ESC151106-5687-1 CONT OF AMIS ITEM 1012005.

Part: SKIN — DENTED (FUSELAGE) · airframe 65,493 hrs · 23,126 cycles

DENT IN THE FUSELAGE SKIN & DOUBLER AT LOWER AFT CORNER OF FWD CARGO DOOR CUT OUT AT BS 613 ABOVE STRINGER 26R. REPAIR ACCOMPLISHED ON ECRA 5331-0 1783.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 71,661 hrs · 24,301 cycles

A REPAIR WAS INSTALLED ON STATION 1460 FRAME WEB, BETWEEN STRINGER 29R & 30 IAW ECRA 5310-06603. ON OR BEFORE THE ACCUMULATION OF 74,300 TOTAL AIRFRAME FLIGHT CYCLES, PERFORM INSPECTION IAW PART 2 OF ECRA 5310-06603. PLANNING TO CONTACT ENGINEER AFTER 70,300 BUT BEFORE 71,300 AIRFRAME FLIGHT CYCLES FOR THE INSPECTION REQUIREMENTS.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,661 hrs · 24,301 cycles

AFT PIT BILGE, SHEAR TIE ANGLE AT STATION 1600, BETWEEN STRINGER 29 - 28L HAS CORROSION. REMOVED & INSTALLED NEW SHEAR TIE IAW DWG 146N1021-224 & SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,661 hrs · 24,301 cycles

AFT LOWER PIT BILGE, SHEAR TIE ANGLE AT STATION 1460, BETWEEN STRINGER 29L - 28L HAS CORROSION. INSTALLED NEW SHEAR TIE IAW DWG 146N104-345 & AMM 51-40-02.

Part: SKIN — DENTED (FUSELAGE) · airframe 65,493 hrs · 23,126 cycles

DENT IN THE FUSELAGE SKIN & DOUBLER AT LOWER AFT CORNER OF FWD CARGO DOOR CUT OUT AT BS 613 ABOVE STRINGER 26R. REPAIR ACCOMPLISHED ON ECRA 5331-01783.

Part: SKIN — DENTED (FUSELAGE) · airframe 65,493 hrs · 23,126 cycles

DENT IN THE FUSELAGE SKIN & DOUBLER AT LOWER AFT CORNER OF FWD CARGO DOOR CUT OUT, AT BS 613 ABOVE STINGER 26R. REPAIR ACCOMPLISHED ON ECRA 5331-01783, BUT HAS FIRST STAGE APPROVAL. THE INSPECTION THRESHOLD FOR REPAIR IS 24 MONTHS. A NEW FAA APPROVAL FINDING COMPLIANCE WITH 14CFR 26.43D & 25.57 IS REQUIRED BEFORE 10 N0V 15 FOR THE ACFT TO REMAIN AIRWORTHY AFTER THAT TIME. CALL ENGINEERING AFTER 10 SEP 15 BUT BEFORE 10 OCT 15 FOR DISPOSITION.

Part: FUSE — DEFECTIVE (CABIN) · airframe 66,941 hrs · 23,404 cycles

R1 PAX DOOR EMER LIGHT INOPERATIVE. RELAMPED R1 PAX DOOR EMER LIGHT. PERFORMED TROUBLESHOOTING & FOUND DEFECTIVE FUSE AT POWER SUPPLY M370. R & R FUSE & PERFORMED OPERATIONS TEST, TESTED OK IAW WDM 33-51-12 & AMM 33-15-07.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,657 hrs · 23,350 cycles

DOOR 1R & DOOR 1 AISLE EXIT LIGHTS INTERMITTENT ON & OFF. REPLACED BATTERY PACK IAW MM 33-51-07 PAGE 204 & EMERGENCY LIGHTS OPERATED SATISFACTORY .

Part: SKIN — DENTED (FUSELAGE) · airframe 65,493 hrs · 23,126 cycles

DENT IN THE FUSELAGE SKIN & DOUBLER AT LOWER AFT CORNER OF FWD CARGO DOOR CUT OUT AT BS 613 ABOVE STRINGER 26R. REPAIR ACCOMPLISHED ON ECRA 5331-01783.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 65,978 hrs · 23,221 cycles

EMERGENCY EXIT LIGHTS INTERMITTENT ABOVE 1R. ACCOMPLISHED CALL OUT, ALL CONNECTORS CHECKED GOOD TO POWER SUPPLY IAW WDM33-51-12 PG10B. REPLACED POWER SUPPLY BATTERY PACK M730 IAW AMM33-51-07 PG201, OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,972 hrs · 23,220 cycles

EMERGENCY EXIT LIGHTS ON FIRST CLASS COCKPIT DOOR 1R ON WHILE EMERGENCY LIGHTS ARMED. REPLACED M730 BATTERY PACK, OPERATIONS CHECKED OK.

Part: ACTUATOR — FAULTY (NR 1 SPOILER) · airframe 65,495 hrs · 23,127 cycles

CREW REPORTS THAT DURING TEST FLT THE NR 1 SPOILER FLOATED APPROXIMATELY 6 INCHES WITH THE CTR HYD SYS DEPRESSURIZED. NR 1 SPOILER ACT CHANGED IAW PTT 4952017, OPERATIONS CHECKED NORMAL IAW MM.

Part: SKIN — DENTED (BS 613) · airframe 65,493 hrs · 23,126 cycles

DENT IN THE FUSELAGE SKIN & DOUBLER AT LOWER AFT CORNER OF FWD CARGO DOOR CUT OUT AT BS 613 ABOVE STRINGER S26R. REPAIRED IAW ECRA 5331-01783.

Part: SKIN — DENTED (FUSELAGE) · airframe 65,493 hrs · 23,126 cycles

DENT IN FUSELAGE SKIN 12 TO 15 IN AFT OF L1 DOOR CUTOUT BETWEEN STRINGER 16 - 15L. INSTALLED DOUBLER AT BS 377 - 395 BETWEEN STRINGER 15L - 17L. CUTOUT DAMAGE IAW 757 NDT 51-00-19, NO CRACKS. REPAIR DONE IAW ECRA 5300-01790 PART 1.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 65,493 hrs · 23,126 cycles

FUSELAGE EXTERIOR BS 748 HAS 7 LIGHTNING STRIKES. REMOVED DAMAGED SKIN BETWEEN BS 746-750 & ACP HFEC OF CUT OUT & REPAIR HOLES IAW NTM 51-00-16 & 51-00-019, NO CRACKS. FABRICATED & INSTALLED EXTERNAL DOUBLER REPAIR IAW SRM53-00-01 REPAIR NR 2 FIG 201.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 65,493 hrs · 23,126 cycles

LIGHTNING STRIKE REPAIR HOLE AT FUSELAGE SKIN STATION 476 AT STRINGER 26R FELL TOO CLOSE TO LAP SEAM IAW SRM REQUIREMENTS. CUT OUT DAMAGE & ACP NDT & INSURANCE CUT IAW NTM51-00-19 & 51-00-16 & ECRA 5300-01786, NO CRACKS. FABRICATED & INSTALLED EXTERNAL DOUBLER & FILLER REPAIR IAW ECRA 5300-01786.

Part: SKIN — DENTED (BS 422-432) · airframe 65,493 hrs · 23,126 cycles

DENT IN FUSELAGE SKIN BS 422-432 STRINGERS 21-22L. CUT OUT DAMAGE & INSTALLED DOUBLER REPAIR IAW SRM 53-00-01 FI G 201 REPAIR 3.

Part: SKIN — GOUGED (FUSELAGE) · airframe 65,493 hrs · 23,126 cycles

FUSELAGE EXTERIOR STATION 525 JUST ABOVE STRINGER 28L SKIN GOUGED. DAMAGE REPAIRED IAW B757-200 SRM 53-00-01 FIG 201 REPAIR 3 AT STATION 525 STRINGER 28L.

Part: DRAIN VALVE — JAMMED (LAVATORY) · airframe 65,261 hrs · 23,035 cycles

AFT LAVATORY HAS OVER FLOWING BLUE WATER. BLUE WATER CONTAINED IN LAVATORY. DID LIQUID CLEAN UP & PLACED AFT LAVATORY ON MEL. WASTE TANK DRAINED VALVE ASSEMBLY JAMMED. REPLACED IAW MM38-32-16. OPERATIONS CHECKED OKAY, NO LEAKS NOTED.

Part: HEAT EXCHANGER — LEAKING (LEFT) · airframe 65,072 hrs · 22,972 cycles

DUCT LEAK LP EICAS MESSAGE DISPLAYED. REPLACED PRIMARY AND SECONDARY HEAT EXCHANGER. LEAK AND OPS CHECKED GOOD.

Part: SEAL — LEAKING (L4 DOOR) · airframe 64,985 hrs · 22,949 cycles

L4 DOOR HAS AN AIR LEAK, & IS VERY NOISY. REMOVED, RESEALED AND INSTALLED DOOR 4L LOWER SILL SCUFF PLATE, LEAK CK GOOD.

Part: COVER — UNSECURE (GALLEY FLOOR) · airframe 64,648 hrs · 22,836 cycles

PAX & CREW TRIPPING ON SEAM OF RUBBER FLOORING-CARPET BY MID GALLEY. SURFACE NOT SMOOTH. REMOVED STRIPPING AT FWD AND AFT ENDS OF MID GALLEY FLOOR MAT AND INSTALLED DOUBLE BACK TAPE AND CLEAR MYLAR OVER IAW ECRA 2533-01004 AND TRM 25-33-01-004.

Part: CONVERTER — FAILED (WINDSHIELD WIPER) · airframe 64,228 hrs · 22,717 cycles

FIRST OFFICER`S WINDSHIELD WIPER DOESN'T COMPLETE A FULL SWEEP AND CONTINUES TO RUN WITH SWITCH OFF. REPLACED WINDSHIELD WIPER MOTOR CONVERTER.

Part: TUBE — LEAKING (LAV WASTE) · airframe 64,015 hrs · 22,654 cycles

AFT LAVATORY "Y" TUBE ABOVE SERVICE PANEL IN AFT CARGO BAY AREA IS LEAKING. BLUE LAVATORY WATER DRAINING FROM AFT LAV ACCESS PANEL REMOVED DAMAGED "Y" TUBE. REPLACED RUPTURED LAVATORY WASTE Y DUCT AT AFT DUMP VALVE CHECKED OKAY.

Part: OXYGEN MASK — MALFUNCTIONED (CAPTAIN'S) · airframe 66,478 hrs · 23,392 cycles

CAPT'S OXYGEN MASK HARNESS INFLATES, BUT NOT ENOUGH TO PLACE OVERHEAD COMFORTABLY. REPLACED MASK ASSY.

Part: B-NUT — LEAKING (LT ENGINE) · airframe 63,357 hrs · 22,427 cycles

CREW REPORTED LEFT ENGINE LEAKING FUEL OUT OF FAN COWL. FOUND FUEL LEAKING AT B-NUT ON BLEED CONVERTER VALVE. CUT SAFETY WIRE AND RETORQUED B-NUT AND RESAFTIED. LEAK CHECKED GOOD.

Part: ACTUATOR — FAULTY (NLG) · airframe 63,357 hrs · 22,427 cycles

NOSE GEAR WOULD NOT EXTEND IN FLIGHT. REPLACED NOSE GEAR LOCK ACTUATOR PER MM. FAILED OP CHECK. STILL HAVE SAME FAULT. GEAR WILL NOT EXTEND.

Part: MODULE — FAULTY (ELEVATOR) · airframe 63,013 hrs · 22,312 cycles

ELEV ASYM EICAS MSG ON TAXI IN. REPLACED LEFT SAM M524 REF MM27-09-00 AND FIM 27-09-00, ACCOMPLISHED CAT III TEST, NO FAULTS.

Part: ACTUATOR — FAULTY (ELEVATOR) · airframe 63,003 hrs · 22,310 cycles

ELEV ASYM STATUS MESSAGE ON CLIMBOUT. CONTROLS FEEL NORMAL AND ELEV INDICATORS APPEAR NORMAL. REMOVED AND REPLACED ASYMMETRY LIMITER ACTUATOR IAW AMM, OPS CHECKS GOOD.

Part: LIGHT — FAULTY (CABIN) · airframe 62,734 hrs · 22,220 cycles

EEL INOP FROM FWD COAT CLOSET THROUGH MID LAV. FOUND MID LAV EEL WITH BARE WIRE CAUSING A SHORT. REPLACED MID LAV EEL STRIP. EEL FROM CLOSET THROUGH MID LAV OPS NORMAL.

Part: CABLE — FAILED (APU IGNITER) · airframe 61,878 hrs · 21,911 cycles

APU WILL NOT START. REPLACED APU IGNITER CABLE AND PLUG REF MM 49-41-04 AND MM49-41-02. APU OP CHECKED RUN OK

Part: ENGINE — FAULTY (NR 2) · airframe 61,753 hrs · 21,872 cycles

NR 2 ENGINE EGT ISSUE, FLIGHT DIVERTED. NR 2 ENGINE REPLACED PER AMM 71-00-02

Part: CIRCUIT BREAKER — MALFUNCTIONED · airframe 61,731 hrs · 21,865 cycles

CENTER TANK WON'T TAKE FUEL. CYCLED BREAKER AND NOW BOTH VALVES OPENED AND CENTER TANK TAKES FUEL.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 61,161 hrs · 21,677 cycles

ACRID ODOR IN COCKPIT, FLIGHT DIVERTED. TURNED OFF WEATHER RADAR, ODOR DISSIPATED. AFTER A SHORT TIME A HAZE APPEARED IN THE COCKPIT WITH THE REPORTED SMOKE ORIGINATING FROM THE AREA JUST BELOW THE FIRST OFFICER'S INSTRUMENT SOURCE SELECTOR SWITCHES.

Part: TRANSCEIVER — ODOR (WX RADAR) · airframe 61,153 hrs · 21,674 cycles

DIVERTED FOR AN ODOR IN THE CABIN AND SMOKE IN THE COCKPIT. FOUND ELECRICAL ODOR COMING FROM WEATHER RADAR RT UNIT. REPLACED AND TESTED OK REF MM.

Part: SKIN — DENTED (FUSELAGE) · airframe 61,124 hrs · 21,665 cycles

FOUND DENT ON LT FUSELAGE APPROX 7 FT FWD OF DOOR 2L AND 2 FT BELOW WINDOW. DENT MEASURES APPROX 4 IN LENGTH BY 4 WIDTH. .062 DEPTH BY- 113877 :DENT OK PER SRM 53-00-01 PG 104. NO PULLED FASTENERS OR STRINGER DAMGE NOTED. ACCOMPLISHED SKIN AND STRINGER REPAIR PER ECRA 5330.04228 REPAIRED PER ECRA 5330-04 228 REV A.

Part: SKIN — DAMAGED (BS 223.5 S23R) · airframe 61,124 hrs · 21,665 cycles

ONE BURNISHED AREA ON RT FWD FUSELAGE SKIN AT BS 223.5 AND APPROX 7 INCH BELOW STR 23R. REMOVED DAMAGED SECTION OF SKIN, INSTALLED REPAIR DOUBLER.

Part: GATE — CORRODED (L1 DOOR) · corrosion level 2 · airframe 61,124 hrs · 21,665 cycles

L1 DOOR LOWER GATE CORRODED. REMOVED AND REPLACED LOWER GATE IAW 52-11-38.

Part: SLIDE — DAMAGED (LT OVERWING) · corrosion level 2 · airframe 61,124 hrs · 21,665 cycles

LEFT OVERWING ESCAPE SLIDE POUCH RELEASE CABLE HAS BEEN PULLED OUT OF LACING. INSTALLED NEW LT OVERWING SLIDE PACK. ARMING OF OVERWING SLIDE IS CW ON TC 5R52I9044.

Part: RELEASE CABLE — LOOSE (OVERWING SLIDE) · airframe 61,124 hrs · 21,665 cycles

RIGHT OVERWING ESCAPE SLIDE POUCH RELEASE CABLE HAS BEEN PULLED OUT OF LACING. INSTALLED NEW RT OVERWING SLIDE PACK. ARMING OF OVERWING SLIDE IS CW ON TC 5R52I9044.

Part: CREASE BEAM — CORRODED (BS 377 - 395) · corrosion level 2 · airframe 61,124 hrs · 21,665 cycles

CREASE BEAM DOUBLER FASTENER HOLES ARE CORRODED BS 377 THRU 395. REMOVED AND REPLACED CORRODED CREASE BEAM REF SRM 51-40-02.

Part: FRAME — DENTED (BS 520 S24L) · airframe 61,124 hrs · 21,665 cycles

FWD CARGO FRAME BS 520 AT S24L HAS DENT DAMAGE. REMOVED DAMAGED UPPER FLANGE & INSTALLED REPAIR ANGLE PER ECRA 5310-05486.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,427 hrs · 14,082 cycles

FWD PIT FRAME STA 600, LT EACH DENT STR 24L. MAJOR REPAIR: TRIMMED OUT DAMAGE, ACP HFEC INSP, NO CRACK FOUND. FABRICATE AND INSTALL REPAIR PER TIMCO REO-G10763, REV B, AND EVA-50518.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,427 hrs · 14,082 cycles

FWD PIT FRAME STA 600, LT EACH DENT STR 24L. MAJOR REPAIR ACCOMPLISHED. TRIMMED OUT DAMAGE, ACP HFEC INSP, NO CRACK FOUND. FABRICATE AND INSTALL REPAIR PER REO-G10763, REV B,

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,124 hrs · 21,665 cycles

CORROSION ON FLOORBEAM STA 324 RBL 37. MAJOR REPAIR ACCOMPLISHED. TRIMMED OUT UPPER CHORD AND INSTALLED REPAIR PARTS PER ECRA 5310-05474, NEED TO ACCOMPLISH PERMANENT REPAIR ON OR BEFORE 12 MONTHS, CONTACT PLANNING AFTER 10 MO BUT BEFORE 11 MO FOR PERM REPAIR.

Part: GATE — GOUGED (L2 DOOR) · airframe 61,124 hrs · 21,665 cycles

L2 DOOR LWR GATE HAS A GOUGE NEAR THE CENTER BOTTOM. REMOVED AND REPLACED LWR DOOR GATE ON LP 9964609.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 61,124 hrs · 21,665 cycles

FLOORBEAM STA 365 FROM RBL 20 TO RBL 50 PREVIOUSLY BLENDED OUT- NEED TO REMOVE PAINT TO CHECK THICKNESS. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED UPPER CORD, INSTALLED REPAIR PARTS PER ECRA 5310.05482.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,124 hrs · 21,665 cycles

CORROSION ON DOUBLER AT STA 1681 UPPER DECK PLATE AFT WET AREA RBL 47. REMOVED AND REPLACED DOUBLER ON AFT PRESSURE DECK PER ECRA 5330-04227 ON LP 9964993.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,427 hrs · 14,082 cycles

AFT PIT FRAME DENTED STA 1400, STR 26L. MAJOR REPAIR ACCOMPLISHED. TRIMMED OUT DAMAGE, ACP HFEC INSP, NO CRACK FOUND. FABRICATE REPAIR ANGLE PER REO- G10758, REV B, AND UA EVA-50516.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,124 hrs · 21,665 cycles

CORROSION ON CABIN FLOORBEAM STA 1661 RBL 3. REMOVED CORRODED UPPER CHORD AND INSTALLED REPAIR PARTS PER SRM ON LP 9965002.

Part: GATE — CORRODED (R2 DOOR) · corrosion level 2 · airframe 61,124 hrs · 21,665 cycles

R2 DOOR LOWER GATE CORRORED AT LOWER FWD SIDE. REMOVED AND INSTALLED NEW SERVICEABLE R2 LOWER GATE.

Part: FLOORBEAM — CORRODED (BS 310) · airframe 61,124 hrs · 21,665 cycles

FLOORBEAM BS 310 AT RBL 37 CORRODED TOP SURFACE. ACCOMPLISHED REPAIR PER ECRA 5310-05477.

Part: FLOORBEAM — CORRODED (BS 310) · corrosion level 2 · airframe 61,124 hrs · 21,665 cycles

FLOORBEAM BS 310 RBL 37 CORRODED TOP SURFACE. ACCOMPLISHED REPAIR PER ECRA 5310-05477.

Part: SHIM — MIGRATED (RT WING SPAR) · airframe 61,124 hrs · 21,665 cycles

RT WING REAR SPAR UPPER TERMINAL FITTING HAS SHIM MIGRATION. TRIMMED SHIM AND SEALED REF ECRA 5720.02276.

Part: FLOORBEAM — CORRODED (BS 377) · corrosion level 2 · airframe 61,124 hrs · 21,665 cycles

CABIN FLOORBEAM STA 377 RBL 45 TOP SURFACE CORRODED. MAJOR REPAIR ACCOMPLISHED. COMPLETED CABIN FLOORBEAM REPAIR AT STA 377 REF ECRA 5310.05476.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 61,124 hrs · 21,665 cycles

CABIN FLOORBEAM AT BS 1640 RBL 6-14 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION AT STA 1640 AND INSTALLED FLOORBEAM REPAIR PER ECRA 5310.05480.

Part: FLOORBEAM — CORRODED (BS 310) · corrosion level 2 · airframe 61,124 hrs · 21,665 cycles

REF NR 9964934, CABIN FWD ENTRY FLOORBEAM STA 310 AT RBL 37 HAS CORROSION ON TOP SURFACE. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM STA 310 AT RBL 37 IAW ECRA 5310-05477. ACCOMPLISH PERMANENT REPAIR WITHIN 363 DAYS ON OR BEFORE 04 APR 13. WORK ACCOMPLI SHED ON SCAL LP 9964934 PLANNING TO CONTACT ENGINEERING AFTER 04 FEB 13 BUT BEFORE 04 MAR 13 FOR PERMANENT REPAIR.

Part: DOUBLER — UNKNOWN (FUSELAGE) · airframe 61,124 hrs · 21,665 cycles

ANTENNA DOUBLERS AT FUSELAGE STA 1393 AND 1433 REQUIRES FABRICATION AND INSTALLATION REF WC 59745401C. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED DOUBLERS AT STA 1393 AND 1433 REF SRM 53-00-01 REPAIR 3 & WC 5 9745401C. WORK ACCOMPLISHED ON NR 9965167.

Part: OXYGEN BOTTLE — LOW PRESSURE (CABIN) · airframe 60,557 hrs · 21,457 cycles

LG O2 BOTTLE AT SEAT 20C IS LOW PRESSURE. REPLACED 11CU BOTTLE. MASK TO HIGH SIDE.

Part: PANEL — DELAMINATED (VERTICAL STAB) · airframe 58,835 hrs · 20,821 cycles

LT VERTICAL STABILIZER PANEL AT APPROX STA 1770 TO STA 1808 PNL P/N 175N2001-35, FOR REPAIR. STARTED LT VERTICAL STAB PANEL REMOVAL, NEED TO CONTINUE WITH REMOVING PANEL FASTENERS.

Part: RELAY — FAILED (FUEL SYSTEM) · airframe 58,834 hrs · 20,820 cycles

FUEL PROBLEM, FLT DIVERTED. COMPLIED WITH MEL 2822J, CTR TANK QTY 3.8K, CB'S PULLED AND WRAPPED WITH DF STICKER F20 F14, DF STICKER APPLIED OVER RT AND LT LENS COVER. DF555. WORK IN CONJUNCTION WITH DF554 FOR LT CTR PUMP INOP, PREVIOUSLY DEFERRED. COA 507223 WAS JUST RECENTLY ACCOMPLISHED IN GSO. SEE ALSO DF554 FOR LT CTR PUMP. REPLACED RELAY K10872 IN P33 PANEL. CTR FUEL TANK OVERRIDE PUMPS OP CK OK AUTO SHUTOFF TEST OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,666 hrs · 20,756 cycles

EMERGENCY LIGHT INOP OUTSIDE DOOR 4R. REPLACED M10817 EMERGENCY LIGHT POWER SUPPLY UNIT PER MM, EMERGENCY LIGHT TESTED OKAY.

Part: PANEL — PEELING (THRUST REVERSER) · airframe 58,666 hrs · 20,756 cycles

NR 2 ENG RT REVERSER LOWER BIFURCATION PANEL ALBLANTIVE COATING COMING OF FWD 2-3RDS. REPAIRED COATING LARGE AREA REPAIR PER MM.

Part: LINE — LEAKING (FUEL SYSTEM) · airframe 58,329 hrs · 20,628 cycles

FUEL LEAK FROM RT WING DRY BAY DRAINS 4, 2 AND 1. WING AND BELLY WET ON ARRIVAL. FUEL SEEP, NOT A RUNNING LEAK IN AREA OF TANK PLATES AND DRY BAY VENTS. TROUBLESHOT FUEL SYSTEM. FOUND NR 2 ENG FUEL FEED FLEX LINE BAD. LOCATED IN DRY BAY. REPLACED FLEX LINE. PRESSURE CHECK GOOD. SEALED WITH A1-2 B1-2 AT 0400 2-5.

Part: STOWAGE BOX — LEAKING (OXYGEN MASK) · airframe 58,216 hrs · 20,587 cycles

F/O O2 MASK STOWAGE BOX LEAKS. SWAPPED WITH OBSERVERS O2 STORAGE BOX. YELLOW FLOW INDICATOR STICKS WITH YELLOW DISK SHOWING. REPLACED STOWAGE BOX PER MM, OPS CHECK NORMAL.

Part: VALVE — LEAKING (OXYGEN MASK) · airframe 58,216 hrs · 20,587 cycles

OBSERVERS O2 MASK VALVE LEAKS. REPLACED OBSERVERS O2 MASK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,216 hrs · 20,587 cycles

AFT LAV, EMERGENCY LIGHT INOPERATIVE. REPLACED AFT LAV EMERGENCY LIGHT.

Part: STRINGER — DENTED (FUSELAGE) · airframe 56,621 hrs · 19,990 cycles

STR 16LT IS DENTED AT STA 610. MAJOR REPAIR ACCOMPLISHED: ACP'D ON DOCK WU S1800P. TRIMMED OUT DENTED SECT OF STR & INSTALLED REPAIR STRINGER SECTION WITH FILLER.

Part: SKIN — DAMAGED (NR 5 SLAT) · airframe 56,104 hrs · 19,801 cycles

NR 5 SLAT HAS DAMAGE. NR 5 SLAT DAMAGED DUE TO LAV DOOR DEPARTING ACFT. DRESSED OUT DAMAGE ON NOSE SKIN OF NR 5 SLAT, POTTED DAMAGE ON TOP SKIN AND PREPPED FOR METAL BOND REPAIR. SKIN SURFACE ETCHED AND PRIMER APPLIED, NEEDS PATCH LAID UP AND CURED (REPAIR NR 4). WHILE ACCOMPLISHING METAL BOND OVERLAY, SLAT UPPER SKIN BUCKLED AND IS NOW DISBONDED A TOTAL OF 120 SQ. IN. RPR WAS AT 235 DEG. FOR 30 MI. REPLACED SLAT IAW MM.

Part: CONTROL PANEL — INTERMITTENT (FIRE DETECTION) · airframe 55,063 hrs · 19,424 cycles

RT ENG SQUIB FAILURE, RTFL. ACCOMPLISHED MEL 2620J. FOUND SQUIB OK. CONTROL PANEL SWITCH NR 2 INTERMITTENT. VERIFIED FAULT. REPLACED TEST PANEL. OP CKS GOOD.

Part: WIRE — MISINSTALLED (CHILLER) · airframe 52,837 hrs · 18,575 cycles

CREW REPORTS ODOR IN FLT DECK ON TAXI OUT. FOUND PIN 6 AND PIN 9 (6:DC GROUND, 9: CASE GROUND) HAVE BEEN SWITCHED. NO OTHER DAMAGE NOTED. AIR FILTER WAS NOT RECEIVED WITH UNIT. REPLACED CHILLER.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,476 hrs · 15,935 cycles

EXTERIOR EMERGENCY EXIT LIGHTS OUT AT DOORS 1R & 3R. RELAMPED EXTERIOR EMERGENCY EXIT LIGHTS AT DOORS 1R AND 3R AND OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (STA 1243) · airframe 40,525 hrs · 14,120 cycles

SECTION OF COACH EMERGENCY LIGHTS INOP, REPLACED BATTERY.

Part: FRAME — DENTED (STA 580, STR 24L) · airframe 40,427 hrs · 14,082 cycles

DENT IN FRAME AT STA 580, STR 24L. TRIMMED OUT DAMAGE, ACP HFEC INSP, NO CRACK FOUND. FABRICATE ANGLE REPAIR PER TIMCO REO-G10764 AND UA EVA-50105.

Part: SPLICE — DENTED (STA 1420 FRAME) · airframe 40,427 hrs · 14,082 cycles

FRAME SPLICE AT STA 1420 BETWEEN STR 24L AND 25L IS DENTED ON TOP IN AFT CARGO PIT. TRIMMED OUT DAMAGE, ACP HEFC NDT INSP, NO CRACK FOUND. REPAIR PER TIMCO REO-G10762, REV B, AND UAL EVA 50517.

Part: FRAME — DENTED (FWD PIT STA 600) · airframe 40,427 hrs · 14,082 cycles

FWD PIT FRAME STA 600, LT 2 EACH DENT STR 24L. TRIMMED OUT DAMAGE, ACP HFEC INSP, NO CRACK FOUND. FABRICATE AND INSTALL REPAIR PER TIMCO REO-G10763, REV B, AND UA EVA-50518.

Part: FRAME — DENTED (STA 1400, STR 26) · airframe 40,427 hrs · 14,082 cycles

AFT PIT FRAME DENTED STA 1400, STR 26L. TRIMMED OUT DAMAGE, ACP HFEC INSP, NO CRACK FOUND. FABRICATE REPAIR ANGLE PER TIMCO REO- G10758, REV B, AND UA EVA-50516.

Part: SKIN — DENTED (STA 490, STR 15L) · airframe 40,427 hrs · 14,082 cycles

EXTERNAL FUSELAGE SKIN AT STA 490, STR 15L HAS DENT. REMOVE DAMAGE AND INSTALL REPAIR DOUBLER PER SRM 53-00-01, REPAIR 4, P201. REPAIR IS A CATEGORY A REPAIR.

Part: UNKNOWN — MALFUNCTIONED (FUEL TRANSFER) · airframe 39,803 hrs · 13,870 cycles

LANDED UNDER AMBER ALERT DUE TO A FUEL TRANSFER PROBLEM. UNEXPLAINABLE FUEL TRANSFER FROM RIGHT MAIN TANK TO CENTER TANK. MAINTENANCE ACCOMPLISHED INTERNAL LEAK CHECK OF SYSTEM BY PRESSURIZING FUEL FEED AND FUELING MANIFOLDS USING AIRCRAFT BOOST PUMPS. AFTER SEVERAL HOURS NO LEAKS (UNCOMMANDED TRANSFER) OCCURED.

Part: O-RING — LEAKING (FILLER VALVE)

LOW PRESSURE ON CYLINDER. O-RING LEAK AT FILLER VALVE FITTING. REPLACED O-RING.

Part: INDICATOR — LEAKING (RAFT BOTTLE)

LOW BOTTLE PRESSURE. PRESSURE LOSS WAS DUE TO LEAKAGE FROM PRESSURE GAUGE WINDOW. PRESSURE GAUGE WAS REPLACED.

Part: CAP — INSTALLED (OIL DRAIN) · airframe 34,879 hrs · 12,181 cycles

RETURNED TO FIELD DUE TO SMOKE IN THE CABIN. A YELLOW PROTECTIVE CAP WAS LT ON THE DEOILER OVERBOARD BREATHER TUBE AFTER ENGINE INSTALLATION. AT ENGINE START, THE EXISTENCE OF THE CAP ALLOWED THE INTERNAL OIL PRESSURE TO BUILD UP SUFFICIENTLY TO UNSEAT SEVERAL OF THE BEARING CARBON SEALS RESULTING IN A LARGE OIL LOSS (> 7QTS.). AFTER REMOVING THE CAP & PERFORMING SEVERAL ENGINE RUNS, THE AIRCRAFT WAS CLEARED FOR SERVICE. SMOKE IN THE CABIN OCCURRED SHORTLY AFTER TAKEOFF. AC RETURNED TO FIELD AND ENGINE REMOVED. UPON DISASSEMBLY LARGE AMOUNTS OF OIL WERE STILL FOUND IN HPC DRUM CAVITIES AND SEALS LEAKED. ALL SEALS REPLACED.

Part: ODOR — DETECTED (LAVATORY) · airframe 29,716 hrs · 10,303 cycles

ELECTRICAL SMELL COMING FROM BOTH AFT LAVS.

Part: STATOR — FAILED (RT ENGINE)

AFTER CLIMBOUT FROM EWR, RIGHT ENGINE WENT TO IDLE THRUST. FLT DIVERTED TO SYR. *S/D* METAL WAS FOUND IN TAILPIPE. THE ENGINE WAS REPLACED. SHOP FINDINGS WERE A HPC STATOR FAILURE.

Part: REGULATOR — CORRODED (EVAC SLIDE)

DURING SHOP OVERHAUL OF SLIDE REMOVED FOR EXPIRATION OF TIME THE REGULATOR BODY AREA, SPRING AND PISTON WERE FOUND TO BE CORRODED. REPLACED REGULATOR.

Part: LAMP — FAILED (CABIN)

DOOR 4L EXTERIOR EMERGENCY LIGHT INOP. REPLACED LAMP, CHECKS GOOD.

Part: SURGE VALVE — MALFUNCTIONED (APU)

APU AUTO SHUTDOWN AT DEPARTURE. *S/D* REPLACED SURGE CONTROL VALVE, OPERATIONAL CHECK GOOD.

Part: CONNECTOR — DIRTY (APU)

APU ALTITUDE START FAILED AT ALTITUDE LEVEL 350, FAULT LIGHT ILLUMINATED. SUPPLEMENTAL DATA UPDATE, FOUND THE TORQUE MOTOR CANNON PLUG CONNECTOR DIRTY AND LOOSE. CLEANED AND SECURED CANNON PLUG. REPLACED THE FUEL CONTROL UNIT, THE IGNITION EXCITER BOX AND IGNITER AS PRECAUTION. SYSTEM CHECKED OK WITH APU TESTER. APU ALTITUDE START IS OPERATING NORMALLY.

Part: YAW DAMPER — MALFUNCTIONED (E/E COMPT)

TUNING NR 1 HF CAUSES RIGHT YAW DAMPER INOP, ACCOMPANIED WITH EICAS MESSAGE.

Part: CONTROL MECH — OUT OF ADJUST (LT SPOILER)

GROUND SPOILER ON THE LEFT WING IS FLOATING IN CRUISE, ESPECIALLY THE OUTBOARD AFT EDGE.