N529UA

Part: SLIDE — UNSERVICEABLE (R4 DOOR) · airframe 75,865 hrs · 27,799 cycles

CABIN DOOR 4R DOOR PRESS IS ZERO. REPLACED DOOR 4R SLIDE IAW AMM 25-66-01. SLIDE PRESS BOTTLE FULL. ACCOMPLISHED SLIDE RENDER SAFE CHECKLIST.

Part: SKIN — DENTED (FUSELAGE) · airframe 75,358 hrs · 27,645 cycles

DENT IN EXTERNAL FUSELAGE SKIN REPAIR BS 1689, STRINGER 20L. EVALUATED DENT, A - Y MEASURED 66 & IS OUT OF LIMITS IAW SRM 53000-01 FIG 101. REPAIRED AREA IAW ECRA 5361-01 071. THE BS 1675 - 1705, STRINGER 19L - 22L.

Part: ENGINE — SHUTDOWN (NR 1) · airframe 75,402 hrs · 27,659 cycles

ON CLIMB OUT FROM 4000 FEET NR 1 ENG HAD A BANG THEN DID AN AUTO SHUTDOWN.

Part: REPAIR — DENTED (FUSELAGE) · airframe 75,358 hrs · 27,645 cycles

DENT IN EXTERNAL FUSELAGE SKIN REPAIR BS 1689, STRINGER 20L. EVALUATED DENT, A - Y MEASURED 66 & IS OUT OF LIMITS IAW SRM 53000-01 FIG 101. REPAIRED AREA IAW ECRA 5361-01 071.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,358 hrs · 27,645 cycles

CORROSION ON TOP OF FRAME ABOVE REPAIR STRAP AT STATION 1480, STRINGER 26R IN AFT CARGO COMPARTMENT. CORROSION ON FRAME BOTTOM FOUND TO BE OUT OF LIMITS. MATERIAL LOSS IS .038. ORIGINAL THICKNESS WAS .063, REMAINING THICKNESS IS .025. USING MIC ID MO1 IAW SRM 53-00-07 FIG 101, REMOVED, FABRICATED & INSTALLED NEW -69 FRAME IAW SRM 51-40-02 PARA 4 & 7 FIG 8 & 12 DWG 14N1030 SHT 10.

Part: STRINGER — DENTED (FUSELAGE) · airframe 75,358 hrs · 27,645 cycles

DENT IN STRINGER 20L AT BS 1689, AFT ACCESSORY COMPARTMENT. CUT OUT DAMAGED SECTION OF STRINGER BETWEEN BS 1673 TO 1708 & FABRICATED STRINGER SECTION, SPLICES & INSTALLED IAW SRM 53-00-03, REPAIR 1, FIG 201 ON NON-ROUTINE 42813. THIS REPAIR IS CONSIDERED CAT A & THE FUSELAGE SKIN INSPECTIONS PROVIDED IN THE MPD ARE SUFFICIENT TO MAINTAIN THE DAMAGE TOLERANCE OF THE INITIAL STRUCTURE WITH THE REPAIR INSTALLED. NO OUTBOUND CF REQUIRED TO CAPTURE FUTURE INSPECTIONS.

Part: SKIN — DAMAGED (RUDDER) · airframe 75,358 hrs · 27,645 cycles

SURFACE MARK LT SIDE OF RUDDER, RUDDER STATION 280. REPAIRED THE LT SIDE OF RUDDER, RUDDER STATION 280 IAW B757 SRM 51-70-04 PARA A FIG 5 & 51-40- 01 REPAIR 1. INSTALLED PLIES IAW SRM 51-70-04 FIG 5. PRIMED & PAINTED IAW AMM 51-21-10-377-039.

Part: FASTENER — DAMAGED (FUSELAGE) · airframe 75,358 hrs · 27,645 cycles

LIGHTING STRIKE JUST AFT OF STATION 405 & BETWEEN STRINGER 22L & 23L. AFTER CHECKING FOUND DAMAGE ON THE LT SIDE & PLACED ON DEFERRAL REF MM 53-30-95 P 601. REMOVED DAMAGED FASTENER & REPLACED WITH BLIND FASTENER IAW MM 53-30-95. RECHECK AT NEXT C CHECK & REPLACE WITH SOLID FASTENER AT HMV. REPAIRED LIGHTNING STRIKE AT BS 405 BETWEEN STRINGER 22L & 23L IAW B757-200 SRM 53-00-01 FG 201 092896 RPR 6 SEC II.

Part: FASTENER — DAMAGED (FUSELAGE) · airframe 75,358 hrs · 27,645 cycles

LIGHTNING STRIKE AT STATION 286 AT STRINGER 26L. AFTER CHECK FOUND DAMAGE ON THE LT SIDE & PLACED ON DEFERRAL. REMOVED BLIND FASTENER, INSTALLED BLIND FASTENER IAW MM 53-30-95. RECHECK AT NEXT C CHECK & REPLACE WITH SOLID FASTENER AT HMV. REPAIRED LIGHTNING STRIKE AT BS 286 STRINGER 24L IAW B757-200 SRM 53-00-01 FIG 201 RPR 6 SECT II. CAT A SOLID RIVET REPAIR INSTALLED WITH NO REPEAT INSPECT REQUIREMENTS.

Part: FASTENER — DAMAGED (FUSELAGE) · airframe 75,358 hrs · 27,645 cycles

LIGHTNING STRIKE AT STATION 327 ON STRINGER 23. AFTER CHECKING FOUND DAMAGE ON THE LT SIDE OF THE AIRCRAFT PLACED ON DEFERRAL IAW MM 53-30-95 P601. REMOVED DAMAGED FASTENER & INSTALLED BLIND FASTENER IAW MM 53-30-95. RECHECK AT NEXT C CHECK & REPLACE WITH SOLID FASTENER AT HMV. REPAIRED LIGHTNING STRIKE AT BS 327 STRINGER 23L IAW B757-200 SRM 53-00-01 FIG 201 RPR 6 SEC II.

Part: ATTACH BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,358 hrs · 27,645 cycles

CORROSION ON MAIN CABIN FLOOR STRUCTURE CREASE BEAM ATTACH BRACKET AT BS 1040 STRINGER 17R. REMOVED CORROSION AT BS 1040 STRINGER 17R AT MAIN CABIN FLOOR STRUCTURE CREASE BEAM ATTACH BRACKET IAW B757-200 SRM 51-10-02 PAR 15 FIG 1. ORIGINAL MATERIAL .063, REMAINING MATERIAL .059, REMOVED .004. WITHIN LIMITS IAW B757- 200 SRM 53-40-13.

Part: FASTENER — DAMAGED (FUSELAGE) · airframe 75,358 hrs · 27,645 cycles

LIGHTING STRIKE AT STATION 337 ON STRINGER 23. AFTER CHECKING FOUND DAMAGE ON THE LT SIDE OF THE AIRCRAFT PLACED ON DEFERRAL. REMOVED DAMAGE FASTENER & REPLACED WITH BLIND FASTENER IAW MM53-30-95. RECHECK AT NEXT C CHECK & REPLACE WITH SOLID FASTENER AT HMV. REPAIRED LIGHTNING STRIKE IAW B757-200 SRM 53-00-01 FG 201 RPR 6 SEC II.

Part: FASTENER — DAMAGED (FUSELAGE) · airframe 75,358 hrs · 27,645 cycles

LIGHTNING STRIKE AT STATION 420 JUST BELOW STRINGER 22. AFTER CHECKING FOUND DAMAGE ON THE LT SIDE OF THE AIRCRAFT PLACED ON DEFERRAL IAW MM 53-30-95 P601. REMOVED DAMAGED FASTENER & INSTALLED BLIND FASTENER IAW MM 53-30-95. RECHECK AT NEXT C CHECK & REPLACE WITH A SOLID FASTENER AT HMV. REPAIRED LIGHTNING STRIKE IAW B757-200 SRM 5 0928963-00-01 FG 201 RPR 6 SEC II.

Part: FASTENER — DAMAGED (FUSELAGE) · airframe 75,358 hrs · 27,645 cycles

LIGHTNING STRIKE DAMAGE AT LT FUSELAGE STATION 202.3 & STRINGER 24. REMOVED DAMAGE FASTENER & INSTALLED BLIND FASTENER IAW MM 53-30-95. RECHECK AT C CHECK & REPLACED WITH A SOLID FASTENER AT HMV. REPAIRED LIGHTNING STRIKE AT BS 202 BETWEEN STRINGER 22L & 23L. INSTALLED SOLID RIVET REPAIR IAW B757 SRM 53-00-01 FIG 201 REPAIR 6.

Part: FITTING — CRACKED (FUSELAGE) · airframe 75,358 hrs · 27,645 cycles

MAIN CABIN BS 1080 RBL SPLICE FITTING AT INBD CHORD LOCATION IS CRACKED. R & R SPLICE FITTING IAW B757-200 SRM 51-40-02 PARA 7 FIG 12, PN 144N5215U 1, PO 428680 1.

Part: FASTENER — DAMAGED (FUSELAGE) · airframe 75,358 hrs · 27,645 cycles

LIGHTNING STRIKE AT STATION 370 ON STRINGER 23L. AFTER CHECKING FOUND DAMAGE ON THE LT SIDE OF THE AIRCRAFT PLACED ON DEFERRAL. REMOVED DAMAGED FASTENER & INSTALLED BLIND FASTENER IAW MM 53-30-95. RECHECK AT NEXT C CHECK & REPLACE WITH SOLID FASTENER AT HMV. REPAIRED LIGHTNING STRIKE AT BS 370 STRINGER 23L IAW B757-200 SRM 53-00-01 FIG 201 RPR 6 SEC II.

Part: FASTENER — DAMAGED (FUSELAGE) · airframe 75,358 hrs · 27,645 cycles

LIGHTNING STRIKE DAMAGE AT LT FUSELAGE STATION 600 AT STRINGER 17. REMOVED DAMAGE FASTENER & INSTALLED BLIND FASTENER IAW MM 53-30-95. RECHECK AT C CHECK & REPLACE WITH SOLID FASTENER AT HMV. REPAIRED LIGHTNING STRIKE AT BS 600 STRINGER 17L IAW B757-200 SRM 53-00-01 FIG 201 RPR 6 SECT II, CAT A SOLID RIVET REPAIR WITH NO REPEAT INSPECTION REQUIREMENTS.

Part: FASTENER — DAMAGED (FUSELAGE) · airframe 75,358 hrs · 27,645 cycles

LIGHTNING STRIKE AT STRINGER 26L AT STATION 273. REMOVED DAMAGED FASTENER, INSTALLED BLIND FASTENER IAW MM53-30-95. RECHECK AT NEXT C CHECK & REPLACED WITH SOLID FASTENER AT HMV. REPAIRED LIGHTNING STRIKE AT BS 273 AT STRINGER 24L. INSTALLED SOLID RIVET REPAIR IAW B757 SRM 53 -00-01 FIG 201 RPR 6 SECTION II, NDT IAW 757NTM PART 6 51-00-16 244916, NO CRACK FOUND.

Part: FASTENER — DAMAGED (FUSELAGE) · airframe 75,358 hrs · 27,645 cycles

LIGHTNING STRIKE AT STATION 330 ON STRINGER 23L. AFTER CHECK FOUND DAMAGE ON THE LT SIDE OF THE AIRCRAFT PLACED ON DEFERRAL. REMOVED DAMAGED FASTENER & REPLACED WITH BLIND FASTENER IAW MM53-30-95. RECHECK AT NEXT C CHECK & REPLACE WITH SOLID FASTENER AT HMV. REPAIRED LIGHTNING STRIKE AT BS 330 STRINGER 23L IAW B757-200 SRM 53-00-01 FG 201 RPR 6 SEC II.

Part: FASTENER — DAMAGED (FUSELAGE) · airframe 75,358 hrs · 27,645 cycles

LIGHTNING STRIKE AT STATION 332, BETWEEN STRINGERS 24L & 25L. REMOVED DAMAGE FASTENER & REPLACED WITH BLIND FASTENER IAW MM 53-30-95. RECHECK AT C CHECK & REPLACE WITH SOLID FASTENER AT HMV. REPAIRED LIGHTNING STRIKE AT BS 332 STRINGER 24L IAW B757-200 SRM 53-00-01 FIG 201 RPR 6 SECT II, CAT A SOLID RIVET REPAIR.

Part: FASTENER — DAMAGED (FUSELAGE) · airframe 75,358 hrs · 27,645 cycles

LIGHTNING STRIKE AT STATION 360 JUST BELOW STRINGER 23L. AFTER CHECKING FOUND THE DAMAGE ON THE LT SIDE OF THE AIRCRAFT PLACED ON DEFERRAL IAW MM 53-30 -95 P601. REMOVED & REPLACE WITH SOLID FASTENER AT HMV. REPAIRED LIGHTNING STRIKE AT BS 360 STRINGER 23L IAW B757-200 SRM 53-00-01 FG 201 RPR 6 SEC II.

Part: FASTENER — DAMAGED (FUSELAGE) · airframe 75,358 hrs · 27,645 cycles

06 JAN MCO CFQ LIGHTING STRIKE AT STATION 293.5 ON STRINGER 24L. AFTER CHECKING FOUND DAMAGE TO BE ON THE LT SIDE OF THE AIRCRAFT PLACED ON DEFERRAL. REMOVED DAMAGED FASTENER & INSTALLED BLIND FASTENER IAW MM 53-30-95. RECHECK AT NEXT C CHECK & REPLACE WITH SOLID FASTENER AT HMV. REPAIRED LIGHTNING STRIKE AT BS 293.5 STRINGER 24L. INSTALLED SOLID RIVET REPAIR IAW 757SRM 53-00-01 FIG 201 REPAIR 6 SEC II. HFEC IAW 757 NTM PART 6 51-00-16 NO DEFECTS NOTED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 75,358 hrs · 27,645 cycles

LIGHTNING STRIKE AT STATION 580 ON STRINGER 18. AFTER CHECKING FOUND DAMAGED ON THE LT SIDE OF THE AIRCRAFT. REPAIRED LIGHTNING STRIKE NOTED AT STATION 580, DETERMINED LOCATION TO BE AT STATION 460 ABOVE STRINGER 21L. INSTALLED SOLID FASTENER IAW 757 SRM 53-00-01 FIG 201 REPAIR 6, 244916HFEC IAW NDT B757 NTM PART6 53-00-16, NO DEFECTS NOTED.

Part: FASTENER — DAMAGED (FUSELAGE) · airframe 75,358 hrs · 27,645 cycles

LIGHTNING STRIKE AT STATION 480 BETWEEN STRINGER 20 & 21L. AFTER CHECKING FOUND THAT THE DAMAGE WAS ON THE LT SIDE OF THE AIRCRAFT & IN THE RVSM AREA. REMOVED DAMAGE FASTENER & INSTALLED BLIND FASTENER IAW MM 53-30-95 & WITHIN RVSM SMOOTHNESS IAW SRM 51-10-01. RECHECK AT C CHECK & REPLACE WITH SOLID FASTENER AT HMV. REPAIRED STRIKE AT BS 480 STRINGER 20L IAW B757-200 SRM 53-00-01 FG 201 RPR 6 SEC II.

Part: FASTENER — DAMAGED (FUSELAGE) · airframe 75,358 hrs · 27,645 cycles

LIGHTNING STRIKE BETWEEN STATION 452 AT STRINGER 25L. THERE ARE TWO RIVETS TOGETHER AT THE SAME PLACE. AFTER CHECKING FOUND DAMAGE TO BE ON THE LT SIDE OF THE AIRCRAFT PLACED ON DEFERRAL IAW MM 53- 30-95 P601. REMOVED DAMAGED FASTENER & REPLACED WITH BLIND FASTENER IAW MM 53-30-95. RECHECK AT NEXT C CHECK & REPLACE WITH SOLID FASTENER AT HMV. EVALUATED LIGHTNING STRIKE AT STATION 452 STRINGER 21L, FOUND SOLID FASTENER PREVIOUSLY INSTALLED IAW 757SRM 53-00-01 FIG 201 REPAIR 6.

Part: FASTENER — DAMAGED (FUSELAGE) · airframe 75,358 hrs · 27,645 cycles

LIGHTNING STRIKE AT STATION 565 ON STRINGER 18L. THERE ARE TWO RIVER SIDE BY SIDE. AFTER CHECKING FOUND DAMAGE ON THE LT SIDE PLACED ON DEFERRAL IAW MM 53-30-95 P 601. REMOVED DAMAGE FASTENER & REPLACED WITH BLIND FASTENER IAW MM 53-30-95. RECHECK AT NEXT C CHECK & REPLACE WITH A SOLID FASTENER AT HMV. REPAIRED LIGHTNING STRIKE IAW B757-200 SRM 53-00-01 FIG 201 RPR 6 SECT II. CAT A SOLID RIVET REPAIR WITH NO REPEAT INSPECT REQUIREMENT.

Part: PRESSURE SWITCH — FAULTY (HYDRAULIC SYS) · airframe 75,041 hrs · 27,561 cycles

LT ENG HYD PUMP PRESS LIGHT NOT ON WITH PUMP OFF. R & R LT ENG HYD PUMP PRESS IAW AMM 29-11-17-401, OPERATIONS CHECKED GOOD.

Part: ACTUATOR — STUCK (RUDDER TRIM) · airframe 74,855 hrs · 27,504 cycles

ON CLIMB OUT RUDDER TRIM STUCK AT 1.0 LEFT & WOULDN'T TRIM. FREED UP AFTER RT INPUT. RUDDER TRIM ON GND IS INOPERATIVE, NO MOVEMENT. REPLACED RUDDER TRIM ACTUATOR & UPPER ARM ASSEMBLY.

Part: TRIM SYSTEM — MALFUNCTIONED (RUDDER) · airframe 74,855 hrs · 27,504 cycles

ON CLIMB OUT RUDDER TRIM STUCK AT 1.0 LT & WOULDN'T TRIM FURTHER. FREED UP AFTER RT INPUT. RUDDER TRIM ON GND IS INOPERATIVE, NO MOVEMENT.

Part: CONNECTOR — DEFECTIVE (COCKPIT) · airframe 74,576 hrs · 27,406 cycles

OXYGEN MASK DEFECTIVE AT FIRST OFFICER`S. MIC INOPERATIVE, ADJUSTED MIC CONNECTOR. O2 MASK MIC OPERATED NORMALLY AT GATE.

Part: FLUID — LEAKING (UNKNOWN) · airframe 74,205 hrs · 27,282 cycles

FLUID STREAM BENEATH TAIL CONE ON LT SIDE.

Part: MODULE — FAULTY (AUTOPILOT SYS) · airframe 73,991 hrs · 27,205 cycles

UPON DOING TESTS FOR CSEU FOUND LT STAB TRIM & ELEVATOR ASSEMBLY LIMIT MODULE (SAM) FAULT B ALL ON COMPUTER UNABLE TO CLEAR. R&R LT SAM IAW AMM, ALL TESTED GOOD.

Part: CONNECTOR — DAMAGED (FUEL SYSTEM) · airframe 73,986 hrs · 27,204 cycles

DURING TROUBLESHOOTING FOUND CONNECTOR D42316P PINS 3 & 4 LOCKS DAMAGED. REPLACED D42316P IAW WDM HOOKUP CHART & WDM 26-18-11, WDM 78-34-11,WDM 29-11-11,WDM 28-4 1-21,WDM 28-22-21,WDM 74-31-11.

Part: LINE — KINKED (FUEL SYSTEM) · airframe 73,318 hrs · 26,991 cycles

NR 2 ENGINE FUEL CONTROL AIR-OIL COOLER CLOSED LINE ON INBD SIDE OF FUEL CONTROL IS KINKED. KINKED LINE IAW MM.

Part: SWITCH — DAMAGED (SPEED BRAKES) · airframe 72,596 hrs · 26,769 cycles

DURING TROUBLESHOOTING OF AUTO SPEED BRAKE SYSTEM, FOUND AUTO SPEEDD BRAKE ARMING ROLL PIN PIVOT OFF SWITCH BRACKET DAMAGED. REPLACED SWITCH, OPS CHECK OK IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,453 hrs · 26,725 cycles

LAST CABIN EMERGENCY LIGHT INOPERATIVE. INSTALLED NEW LIGHT AND OPS CHECKED SATISFACTORY.

Part: NUT PLATE — DEFECTIVE (NR 1 PYLON) · airframe 72,445 hrs · 26,722 cycles

SCREW STICKING OUT ON NR 1 PYLON OUTBOARD SIDE. MAINT TEXT: FWD FAIRING, AFT SECTION, LOWER OUTBD CORNER HAS 1 SCREW STICKING OUT, SEE FIG 1, AMM 54-52-00 PAGE 2. NEEDS NUT PLATE REPLACED. SCREW IS ON TRAILING EDGE 1 SCREW UP FROM CORNER. CF FOR REPAIR REF AMM 54- 52-01 PARA 1E WITHIN 5 FLT CYCLES.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 72,442 hrs · 26,721 cycles

FLOORBEAM TEE BS 1640 UPPER SIDE HAS CORROSION LBL 10 TO RIGHT OTBD SIDE. INSTALLED NEW SECTION OF TEE IAW ECRA 5310-05526, REPAIR 3. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 622) · airframe 72,442 hrs · 26,721 cycles

LIGHTNING STRIKE BS 622, BETWEEN STR 27L AND 26L. CUTOUT DAMAGED SKIN, AND INSTALLED DOUBLER REPAIR PER EA 130281 AND ECRA 5330-04489. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 345) · corrosion level 2 · airframe 72,442 hrs · 26,721 cycles

FORWARD PASSENGER COMPARTMENT BS 345 RBL 11 FLOORBEAM HAS UPPER SURFACE CORROSION AROUND FASTENER HOLE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. INSTALLED REPAIR ANGLE.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 72,442 hrs · 26,721 cycles

FORWARD WET AREA FLOORBEAM HAS CORROSION AROUND FASTENER HOLES BS 365 RBL 4 - 42. REMOVED CORROSION AND VERIFIED USING 10X MAGNIFY GLASS IAW SRM 51-10-2. FOUND OUT OF LIMITS IAW SRM 53-0051 PG 103, 104 FIG 101. REPAIR FLOORBEAM TEE BS 365 LBL 10 TO RBL 70 IAW ECRA 5310-05536. MAJOR REPAIR.

Part: WEDGE — DENTED (NR 1 SLAT) · airframe 72,442 hrs · 26,721 cycles

LEFT WING NR 1 SLAT TRAILING EDGE WEDGE AT 38 INCH INBOARD FROM OUTBOARD EDGE AND 4 INCH, FWD OF TRAILINGE EDGE IS DENTED. DENT IS WITHIN LIMITS BUT DUE TO BEING IN EXCESS OF 2 INCH IN DIAMETER, REQUIRES REPAIR SRM 57-43-01 FIG101 SHEET 4 NOTEJ AND FIG101 SHEET 5 DETAIL III. FABRICATED DOUBLER.

Part: WEDGE — DENTED (NR 3 SLAT) · airframe 72,442 hrs · 26,721 cycles

LEFT WING NR 3 SLAT TRAILING EDGE WEDGE UPPER SURFACE 40. 5 INCHES FROM OUTBOARD EDGE AND 5.25 INCHES FROM TRAILING EDGE HAS A SMALL DENT. MARKED, EVALUATED AND MEASURED DENT ON NR 3SLAT 40.5 FROM OUTBOARD EDGE, DENT MEASURES A=.700 AND Y=.011=63, WITHIN LIMITS IAW SRM 57-43-02, NDT FOR DELAMINATED AND NO DEFECTS NOTED.

Part: FLOOR SUPPORT — CORRODED (BS 1640) · corrosion level 2 · airframe 72,442 hrs · 26,721 cycles

MAIN CABIN FLOOR SUPPORT BS 1640 RBL 50 UPPER SURFACE HAS CORROSION AT FASTENER HOLE. REMOVED AND REPLACED FLOOR SUPPORT BS 1640-1620 IAW DWG 146N5664-3 ORG.

Part: SKIN — DELAMINATED (NR 3 SLAT) · airframe 72,442 hrs · 26,721 cycles

NR 3 SLAT, 9 INCH FROM THE INBOARD END AND AND 6.5 INCH FWD OF TRAILING EDGE, AREA OF DELAMINATED. THE AREA ON THE UNDERSIDE SAME LOCATION THERE IS AREA OF DELAMINATED MAJOR REPAIR ACCOMPLISHED: EVALUATED DELAMINATED ON NR 3 SLAT AND FOUND TO BE OUT OF LIMITS IAW SRM 57-43-02 AND 51-10-02. REMOVED DAMAGE, VERIFIED MATERIALS, POTTED CORE, APPLIED BOEGEL, APPLIED ADHESIVE PRIMER, FAB DOUBLER, BONDED DOUBLER, TAP TEST GOOD. RESTORED PRIMER, FINISH.

Part: SKIN — DENTED (NR 3 SLAT) · airframe 72,442 hrs · 26,721 cycles

LEFT WING NR 3 SLAT TRAILING EDGE WEDGE UPPER SURFACE 7.0 INCHES FROM INBOARD EDGE AND 3.5 INCHES FROM TRAILING EDGE HAS A SMALL DENT. FOUND OUT OF LIMITS IAW 57-43-02, NDT CHECK FOR DELAMINATION, NO CRACKS NOTED. REMOVED DAMAGE, FABRICATED DOUBLER SRM 51-70-10. MAJOR REPAIR

Part: INTERCOSTAL — CORRODED (BS 333-344) · corrosion level 2 · airframe 72,442 hrs · 26,721 cycles

FWD WET AREA INTERCOSTAL BS 333-344 RBL 56 IS CORRODED ON TOP AND LOWER SURFACE. FOUND CORROSION TO BE 110%. REMOVED AND INSTALLED NEW INTERCOSTAL PER DWG 141N5160 & SRM 51-40-02&51-40-05. MAJOR REPAIR.

Part: SILL — CORRODED (BS 1661-1681) · corrosion level 2 · airframe 72,442 hrs · 26,721 cycles

R4 DOOR CUTOUT LOWER SILL IS CORRODED BS 1661- 1681, RBL 57, WL 208. INSTALLED NEW SILL IAW DWG 146N5230, 146N8722, AND SRM 51-40- 02. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 460) · airframe 72,442 hrs · 26,721 cycles

LIGHTNING STRIKE AT BS 460 BETWEEN S20-21L. FOUND DAMAGE WAS ON THE LEFT SIDE AND IN THE RVSM AREA. INSTALLED SOLID FASTENER PER SRM 51-40-02.

Part: VALVE — LEAKING (NR 2 ENGINE) · airframe 72,368 hrs · 26,694 cycles

FUEL LEAKING FROM NR 2 ENGINE AFT AREA, DISTRIBUTION VALVE. NR 2 ENGINE OPENED FAN, CORE AND T/R COWLS FOR REPLACEMENT OF FUEL DISTRIBUTION VALVE REF MM.

Part: BRACKET — BROKEN (NR 2 ENG FAN LIN) · airframe 72,277 hrs · 26,660 cycles

NR 2 ENGINE FAN EXIT LINER SEGMENTS AT 12 THRU 2 O'CLOCK POSITIONS APPEAR TO HAVE DAMAGE. REMOVED TWO LINER'S, AT 1 & 2 O'CLOCK POSITIONS, FOUND FOUR BRACKETS BROKEN. REMOVED FOUR BROKEN BRACKETS & REPLACED. COMPLETED INSTALLATION OF 2 FAN EXIT CASE LINERS.

Part: LIGHT — BROKEN (ROW 20 ABC) · airframe 70,412 hrs · 26,022 cycles

EMERGENCY EXIT ROW 20 ABC EXIT LIGHT FRAME BROKEN DIFFUSER FELL OUT. INTERIM REPAIR MADE GOOD FOR 4 CYCLES. REPLACED DIFFUSER.

Part: ACARS — INOPERATIVE (COCKPIT) · airframe 70,113 hrs · 25,926 cycles

CREW REPORTED ACARS INOPERATIVE. DISPLAY UNIT IS DEAD. REPLACED ACARS CDU IAW MM, OPS CHECKED NORMAL.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 69,728 hrs · 25,796 cycles

FWD SIDE OF DOORWAY 4R, ACCESS PANEL SUPPORT ABOUT LOWER HINGE ARM IS CRACKED APPROX 11-16 IN LENGTH. REMOVED WEBBING. CUT OUT DAMAGED WEB AND MANUFACTURED WEB, AND JOINT DOUBLER. CONT. INSTALLING WEB REPAIR ALSO STARTED TO INSTALL FORMED CLOSURE WEB. INSTALLED NEW FORMED CLOSURE WEB REPAIR. FINISHED INSTALLING REPAIR DOUBLER.

Part: UNKNOWN — ODOR (CABIN) · airframe 69,694 hrs · 25,784 cycles

NOTICED STRONG ELEC ODOR IN ENTIRE ACFT DURING TAXI FROM HANGAR WITH APU RUNNING. FOUND ODOR COMING FROM APU COMPARTMENT. RPLACED GENERATOR AND APU STARTER. RAN APU AND ENG(S) WITH BLEEDS ON, NO ODOR NOTED.

Part: LIGHT — DAMAGED (CABIN) · airframe 69,547 hrs · 25,731 cycles

EMERGENCY ESCAPE LIGHT END CAPS MISSING 6B, 8C & 1L. REPLACED MISSING END CAPS AT 1L, 6B & 8C WITH (PCN .

Part: MODULATING VALVE — MALFUNCTIONED (AC BAY) · airframe 67,446 hrs · 24,955 cycles

FLT DECK TEMP WENT FULL HOT ON CLIMBOUT. STANDBY NO HELP. TRIM AIR OFF REGAINED CONTROL. AFTER FUTHER TROUBLESHOOTING FOUND SYSTEM NEEDS TRIM AIR VALVE 643-9023 CONFLICTING WITH OTHER WORK. RPL FLT DECK TRIM AIR MODULATING VLV.

Part: ACTUATOR — MALFUNCTIONED (FUEL SYSTEM) · airframe 67,333 hrs · 24,910 cycles

LEFT ENGINE FLAMED OUT AFTER IT HAD BEEN STABILIZED AT IDLE. DURING NEXT START ATTEMPT, ENGINE REACHED 30 PERCENT N2 THEN FLAMED OUT WITH LT ENG FUEL VALVE EICAS MESSAGE. REPLACED LT SPAR VALVE ACTUATOR.

Part: CONNECTOR — BROKEN (PT2-T2 PROBE) · airframe 67,276 hrs · 24,889 cycles

CONNECTOR D4886 FOR EEC PT2-TT2 PROBE FOUND BROKEN. CONNECTOR 420-2182 ON AOG Q1367. BACKSHELL 585-4997 ON AOG F1326. REPLACED FAILED CONNECTOR AT PT2-T2 PROBE. OPS CHECKED GOOD. NO FURTHER ACTION REQUIRED.

Part: SKIN — DENTED (BS 602-623) · airframe 67,094 hrs · 24,818 cycles

EXTERNAL FUSELAGE SKIN DENTED AT APPROX STA 602 AND STA 623, BETWEEN STR 15L-16L, DENTS ARE WITHIN LIMITS OF SRM 53-00-01 AND FOUND TO BE CRACK FREE BY HFEC. OK TO ARCHIVE.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,017 hrs · 24,789 cycles

STA 700 FLOORBEAM CRACKED FWD FACE TO UPPER CHORD RADIUS AT LBL 24.75 AND LBL 45.5. MAJOR REPAIR ACCOMPLISHED: REPAIRED ON SMB W-US C1389M AND S8433M, PER EVA 80930 AND SRM 53-00-51 FIG 201, RPR.3. CUT DAMAGE, HFEC CUTOUT AND HOLES, INSTALLED DOUBLERS, FILLERS & STRAPS. ID WITH EVA #.

Part: CIRCUIT CARD — NO TEST (FIRE DETECTION) · airframe 65,981 hrs · 24,410 cycles

REPLACE FIRE OVERHEAT LOGIC TEST CARD NR 1 FOR LT ENG FIRE TEST DUE TO FAILED FIRE TEST (FIRE HANDLE DID NOT ILLUMINATE AND NO EICAS FOR LT ENG FIRE). CARD WAS SWAPPED WITH RT ENG LOGIC CARD NR2 AND PROBLEM FOLLOWED. ALL CARDS ARE BACK IN ORIGINAL POSITIONS. REF WD26-11-11 ITM M10224 PCN 481-9094. REPLACED M10224 CIRCUIT CARD IAW MM 26-10-01, OPS CHECKED NORMAL.

Part: FEEDER CABLE — LOOSE (EMERGENCY LIGHT) · airframe 65,772 hrs · 24,329 cycles

EXIT ROW LIGHTING IS LOOSE ABEAM SEATS 1AB. REPLACED EMERGENCY POWER FEEDER CABLE AT 1L. OPERATES NORMALLY.

Part: FEEDER CABLE — FAULTY (EMERGENCY LIGHT) · airframe 65,772 hrs · 24,329 cycles

EXIT ROW LIGHTING IS LOOSE ABEAM SEATS 1AB. REPLACED EMERGENCY LIGHT POWER FEEDER CABLE AT 1L. OPERATES NORMALLY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,627 hrs · 23,903 cycles

4 LEFT EMERGENCY EXIT LIGHT INOPERATIVE. RELAMP OPS CHECKS OK. 4L EMERGENCY EXIT EXTERIOR LIGHT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,627 hrs · 23,903 cycles

AFT CARGO EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED LAMP PN 767 AND CLEANED CORROSION. REPLACED LAMP AND CLEANED CORROSION. OPS NORMAL.

Part: SKIN — DELAMINATED (NR 6 SLAT) · airframe 61,218 hrs · 22,559 cycles

NR 6 LEADING EDGE SLAT IS DELAMINATING ON UPPER SURFACE IN AREA OF PREVIOUS REPAIR. DETERMINED THAT AREA IS BEYOND LINE REPAIRABLE LIMITS. DAMAGED SLAT REMOVED, INSTALLATION. COMPLETED INSTALLATION OF SLAT. INSPECTED INSTALLATION AND RIG OF NR 6 LE SLAT. ALL CHECKS WERE GOOD.

Part: PACKING — DEFECTIVE (HYDRAULIC PUMP) · airframe 60,972 hrs · 22,454 cycles

LEFT HYD LEAK IN FLIGHT. FLIGHT DIVERTED. REPLACED LT ENG DRIVEN HYD PUMP BLEEDER PLUG PACKING. SERVICED LT HYD SYSTEM TO FULL. EDP TESTS GOOD. NO LEAKS, NO MSG ON ECS, EPCS EICAS.

Part: DISPLAY — INOPERATIVE (COCKPIT) · airframe 60,268 hrs · 22,181 cycles

LOST POWER TO CAPTAIN'S DISPLAY SCREEN.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 58,170 hrs · 21,408 cycles

DOOR 2L RT EMERGENCY FLASHLIGHT IS INOP. BATTERY INOP. REPLACED BATTERY, OPS GOOD.

Part: MOTOR — MALFUNCTIONED (CABIN PRESSURE) · airframe 57,358 hrs · 21,131 cycles

FLIGHT DIVERTED DUE TO A CABIN PRESSURIZATION PROBLEM. REPLACED AC MOTOR ASSY AND NR 2 AUTO PRESSURE CONTROLLER, OPS CHECKED GOOD, NO REPEATS.

Part: SQUIB — NO TEST (EMER ESCAP DOOR) · airframe 56,819 hrs · 20,941 cycles

EMERGENCY ESCAPE TEST 2 GREEN LIGHT DOES NOT TEST. RT MASTER CONTROL VALVE SQUIB FOR RT OFF WING ESCAPE DOOR INOP. REPLACED RT MASTER CONTROL VALVE SQUIB FOR RT OFF WING ESCAPE DOOR. OPS CHECKED NORMAL.

Part: WIRE — OUT OF POSITION (GIRT BAR) · airframe 56,747 hrs · 20,915 cycles

DOOR 4L DOOR SLIDE ARM LIGHT DOES NOT COME ON WHEN ARMED, POPS C-B. FOUND WIRES AT GIRT BAR SWITCH CONTACTING GROUND. REPOSITIONED WIRES CORRECTLY, OPS CHECKED OK.

Part: FRAME — DAMAGED (BS 1681) · airframe 56,745 hrs · 20,914 cycles

AIRCRAFT RECEIVED DAMAGE TO THE BS 1681 FRAME AT WL 210, NEAR THE THRESHOLD AT DOOR 4R. ACCOMPLISHED MAJOR REPAIR AT GSO.

Part: LIGHT — BROKEN (4R DOOR) · airframe 56,745 hrs · 20,914 cycles

R-4 DOOR SURROUND PANEL (BLACK) EMERGENCY LIGHT BROKEN. REMOVED AND REPLACED R4 DOOR SLIDE LIGHT.

Part: SKIN — GOUGED (TE FLAP) · airframe 56,746 hrs · 20,914 cycles

RT INBOARD FLAP VANE UPPER EXTERNAL SURFACE IS GOUGED AT OUTBOARD END OF VANE. ACCOMPLISHED MAJOR REPAIR AT GSO.

Part: SWITCH — BROKEN (4L DOOR) · airframe 56,745 hrs · 20,914 cycles

L-4 DOOR SURROUND PANEL, EMERGENCY SWITCH TEST IS BROKEN. FOUND DAMAGE TO EMER LIGHT TEST SWITCH. REPLACED EMER LIGHT TEST SWITCH, OPS CHECKED NORMALLY.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,745 hrs · 20,914 cycles

CREW REPORT: A CREASE ON THE LOWER FUSELAGE AFT OF THE AFT GALLEY DRAIN IS ABOUT A FOOT LONG. ACCOMPLISHED MAJOR REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 56,745 hrs · 20,914 cycles

AFT PIT FRAME DENTED AT STR 26L STA 1420 ON INBOARD FLANGE. ACCOMPLISHED MAJOR REPAIR AT GSO.

Part: FRAME SPLICE — DAMAGED (FUSELAGE) · airframe 56,745 hrs · 20,914 cycles

AFT PIT STA 1520 BETWEEN STR 24R AND 25R FRAME SPLICE HAS TOOL MARKS. ACCOMPLISHED MAJOR REPAIR AT GSO.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 56,745 hrs · 20,914 cycles

DOOR R1 FAILS MIDWAY CHECK. FOUND GRIT BAR OUT OF ADJUSTMENT. ADJUSTED GIRT BAR. CHECKS NORAMALLY.

Part: GATE — DAMAGED (L1 DOOR) · airframe 56,745 hrs · 20,914 cycles

L1 DOOR LOWER GATE HAS HOLE IN INSIDE LIP. INSTALLED FILL WELD REPAIR.

Part: ARM — DAMAGED (L2 DOOR HINGE) · airframe 56,745 hrs · 20,914 cycles

L-2 DOOR UPPER HINGE ARM CUT OUT IS DAMAGED. ACCOMPLISHED MAJOR REPAIR AT GSO.

Part: STRUCTURE — DAMAGED (R2 DOOR) · airframe 56,745 hrs · 20,914 cycles

R-2 DOOR UPPER HINGE ARM CUTOUT IS DAMAGED. ACCOMPLISHED MAJOR REPAIR AT GSO.

Part: FRAME — DENTED (FUSELAGE) · airframe 56,745 hrs · 20,914 cycles

FWD PIT AT STA 600, STR 24L FRAME IS DENTED ON INBOARD FLANGE. ACCOMPLISHED MAJOR REPAIR AT GSO.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 56,745 hrs · 20,914 cycles

AFT CARGO COMP ANTENNA DOUBLER FWD LT FASTENER NUT PLATE HAS EXFOLIATION CORROSION. REMOVED CHANNEL ASSY. FABRICATED & INSTALLED NEW RADIUS FILLER. MAJOR REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 56,745 hrs · 20,914 cycles

AFT PIT AT STA 1600, APPROX STR 26L, FRAME DENTED ON INBOARD FLANGE. ACCOMPLISHED MAJOR REPAIR AT GSO.

Part: FRAME — DENTED (FUSELAGE) · airframe 56,745 hrs · 20,914 cycles

AFT PIT FRAME DENTED JUST OUTBOARD OF STR 26L AT STA 1440, INBOARD FLANGE. ACCOMPLISHED MAJOR REPAIR AT GSO.

Part: FRAME — DENTED (FUSELAGE) · airframe 56,745 hrs · 20,914 cycles

AFT PIT AT STA 1540, APPROX AT STR 26L, FRAME DENTED ON INBOARD FLANGE. ACCOMPLISHED MAJOR REPAIR AT GSO.

Part: LANYARD — BROKEN (EVAC SLIDE) · airframe 56,745 hrs · 20,914 cycles

LEFT OVERWING SLIDE SAFETY PIN STRING BROKEN. THIS PIN KEEPS SLIDE FROM UNRAVELING. REMOVED AND REPLACED LT OVERWING SLIDE.

Part: FRAME — DENTED (FUSELAGE) · airframe 56,745 hrs · 20,914 cycles

AFT PIT AT STA 1500, APPROX AT STR 26L FRAME DENTED ON INBOARD FLANGE. ACCOMPLISHED MAJOR REPAIR AT GSO.

Part: SUPPORT — CRACKED (JACKSCREW) · airframe 56,745 hrs · 20,914 cycles

LEFT O/B FLAP I/B SIDE TRACK, FWD LWR JACK SCREW SUPPORT CRACKED. ACCOMPLISHED MAJOR REPAIR AT GSO.

Part: FRAME — DENTED (FUSELAGE) · airframe 56,745 hrs · 20,914 cycles

AFT PIT FRAME HAS 2 EACH DENTS ON INBOARD FLANGE BETWEEN STR 25L AND 26L AT STA 1400. ACCOMPLISHED MAJOR REPAIR AT GSO.

Part: SUPPORT — CRACKED (JACKSCREW) · airframe 56,745 hrs · 20,914 cycles

RIGHT O/B FLAP I/B TRACK FWD LWR JACKSCREW SUPPORT CRACKED. ACCOMPLISHED MAJOR REPAIR AT GSO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,190 hrs · 20,716 cycles

EMERGENCY EXIT SIGN LIGHT OUT AT 15A OVERWING LOCATION.

Part: TRIM SYSTEM — INOPERATIVE (RUDDER) · airframe 55,941 hrs · 20,624 cycles

RUDDER TRIM INOP IN BOTH DIRECTIONS IN ACCENT, CRUISE AND DESCENT. RUDDER TRIM INTERMITTENT ON TESTING. REPLACED RUDDER TRIM ACTUATOR

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,701 hrs · 20,536 cycles

AISLE EMERGENCY LIGHTS INOP ROWS 27, 31 & 34.

Part: LIGHT — INOPERATIVE (ESCAPE SLIDE) · airframe 55,701 hrs · 20,536 cycles

EMERGENCY SLIDE LIGHT INOP AT DOOR 4R.

Part: LIGHT — INOPERATIVE (L4 DOOR SLIDE) · airframe 55,701 hrs · 20,536 cycles

EMERGENCY SLIDE LIGHT INOP AT DOOR 4L.

Part: LIGHT — INOPERATIVE (ROW 7-13) · airframe 55,701 hrs · 20,536 cycles

EEL LIGHTS INOP ROWS 7-13. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: LIGHT — INOPERATIVE (GALLEY) · airframe 55,701 hrs · 20,536 cycles

EEL LIGHT INOP AT FWD GALLEY CART STOWAGE.

Part: LAMP — INOPERATIVE (EMERENCY LIGHTS) · airframe 55,701 hrs · 20,536 cycles

EEL LAMPS INOP ROW 31 TO AFT GALLEY.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 55,701 hrs · 20,536 cycles

EEL LIGHTS INOP ROWS 7-13. 11-01-07 REPLACED EEL LEAD IN CABLE.

Part: LIGHT — BROKEN (CABIN) · airframe 52,945 hrs · 19,514 cycles

CABIN FLOOR EEL LIGHTS AT FWD ENTRY BROKEN. REPAIRED EEL LIGHTS AT FWD ENTRY.

Part: LIGHT — BROKEN (LAVATORY) · airframe 52,945 hrs · 19,514 cycles

CABIN FLOOR EEL LIGHTS AT AFT LAV BROKEN. REPAIRED EEL LIGHT AT AFT LAV.

Part: STRUCTURE — CRACKED (R2 DOOR) · airframe 52,372 hrs

MAIN ENTRY DOOR 2R IS CRACKED AT THE FWD 3RD FROM TOP STOP CUTOUT. REPLACED WITH A NEW MAIN ENTRY CABIN DOOR. REMOVED DOOR SENT TO SHOP FOR EVALUATION. ROOT CAUSE OF CRACK IS STILL UNDER INVESTIGATION.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 51,949 hrs · 19,151 cycles

LEFT ENGINE PUMP PRESSURE LIGHT ILLUMINATED. REPLACED NR 1 ENG HYDRAULIC PUMP (EDP). REPLACED NR 1 ENG. HYDRAULIC PUMP (EDP).

Part: APU — FAILED (APU BAY) · airframe 50,854 hrs · 18,733 cycles

RETURNED TO DEN DUE TO INOPERATIVE GEN & LOSS OF APU EN ROUTE. APU NO START DUE TO LOW OIL PRESSURE. APU GENERATOR HOUSING CRACKED AT 12:00 POSITION. APU SHARES OIL SYS WITH GEN. LOSS OF OIL FROM CRACKED GEN HOUSING CAUSED INSUFFICIENT OIL LEVEL IN APU RESULTING IN LOW OIL PRESSURE SHUTDOWN DURING ALTITUDE START ATTEMPT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,961 hrs · 18,046 cycles

EMERGENCY EXIT LIGHT ABOVE ROW 16 LT INOP. REPLACED BATTERY PACK AT POWER SUPPLY LOC, M10699 (ROW 23DEF).

Part: ODOR — DETECTED (COCKPIT) · airframe 47,606 hrs · 17,564 cycles

DIVERTED TO ORD UNDER AMBER ALERT DUE TO AN ELECTRICAL SMELL IN THE FLIGHT DECK. REPLACED FAN.

Part: EADI — BURNED (COCKPIT) · airframe 45,574 hrs · 16,819 cycles

ELECTRICAL ODOR IN FLIGHT DECK AND EADI BLANKING OUT. REPLACED EADI. REMOVED UNIT HAD CAPACITOR A3C31 FOUND TO BE BURNED & CRACKED. SHOP REPLACED CAPACITOR AND BURNED-IN CRT.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 42,456 hrs · 15,699 cycles

FRAME DAMAGED AT FUSELAGE STA.1681 AT WL210.

Part: TURBINE BLADES — FAILED (LT ENGINE) · airframe 39,948 hrs · 14,742 cycles

WHILE CLIMBING THROUGH 14000 FT LEFT ENGINE EXPERIENCED A COMPRESSOR STALL. ENGINE SELF RECOVERED AND CLIMB CONTINUED TO FL260. EGT REDLINED, THROTTLE RETARDED TO IDLE. ENGINE WAS REMOVED FOR METAL IN THE TAILPIPE, IT HAD A NORMAL ECM TREND PLOT. AT ENGINE TEARDOWN, A STAGE 2 TURBINE BLADE FAILURE WAS FOUND TO BE THE CAUSE.

Part: RELAY — INTERMITTENT (EXTERNAL POWER) · airframe 39,337 hrs · 14,502 cycles

RIGHT HYDRAULIC QUANTITY INDICATES ZERO. RIGHT HYDRAULIC PRESS NORMAL. TROUBLESHOT TO 115 V AC GROUND SERVICE TRANSFER BUS RELAY K102. RELAY WAS INTERMITTENT, K102 RELAY WAS REPLACED AND SYSTEM CHECKED NORMAL.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 38,084 hrs · 14,046 cycles

FORWARD GALLEY FLOOR LOWER CUTOUT STRINGER 17R TEAR STRAP HAS EXCESSIVE BLENDOUT OF DAMAGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED OUTER SKIN DOUBLER.

Part: RUDDER — DELAMINATED · airframe 38,084 hrs · 14,046 cycles

PREVIOUS REPAIR DELAM ON RUDDER TRAILING EDGE RS 245.00 SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REMOVED DELAM REPAIR AND INSTALLED NEW REPAIR PLIES.

Part: FRAME — CORRODED · airframe 38,084 hrs · 14,046 cycles

AFT CABIN #4RH DOOR AFT LOWER FRAME HAS EXCESSIVE MATERIAL REMOVED JUST ABOVE FLOOR LEVEL BECAUSE OF CORROSION REMOVAL AT STATION 1681.5 RBL 60. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.FABRICATED AND INSTALLED INTERNAL REPAIR ANGLE.

Part: FRAME — WORN (FUSELAGE) · airframe 38,084 hrs · 14,046 cycles

AFT PIT FRAME AT 1480 3 INCHES BELOW STRINGER 26R UPPER FLANGE ON FRAME HAD WEAR MARK. MAJOR REPAIR ACCOMPLISHED. FABRICATED A TWO PLY STRAP THAT WAS INSTALLED ON UNDERSIDE OF FRAME.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,084 hrs · 14,046 cycles

CABIN FLOORBEAM STA 310 RBL 40 HAS EXCESSIVE MATERIAL LOSS FROM CORROSION REMOVAL. MAJOR REPAIR ACCOMPLISHED. INSTALLED TWO STRAPS REPAIRS ON EACH SIDE OF T-FLANGE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,084 hrs · 14,046 cycles

CABIN FLOORBEAM UPPER FLANGE HAS CORROSION STATION 324 RBL 50 TO 60. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP AND ANGLE REPAIR.

Part: CHANNEL — CORRODED · airframe 38,084 hrs · 14,046 cycles

CABIN FLOOR SUPPORT CHANNEL HAD EXCESSIVE CORROSION ON UPPER SURFACE BETWEEN STATION 310 AND 324 RBL 40" STRINGER 17R. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW OUTSIDE CENDER NEW CHANNEL INTERCOSTAL FLOOR SUPPORT.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,084 hrs · 14,046 cycles

STATION 695 RIGHT HAND INBOARD CABIN SEAT TRACK CORRODED AT SPLICE. MAJOR REPAIR ACCOMPLISHED. REPLACED TRACK.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 38,084 hrs · 14,046 cycles

CABIN FLOOR INTERCOSTAL BETWEEN STATION 324.5 AND 345 HAD EXCESSIVE MATERIAL REMOVED DURING CORROSION CLEAN UP, 3 RBL AND AT STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,084 hrs · 14,046 cycles

CABIN FLOOR SEAT TRACK SUPPORT BETWEEN STATION 365 TO 415 RBL 48 STRINGER 17R HAD EXCESSIVE MATERIAL REMOVED DURING CORROSION CLEAN UP. MAJOR REPAIR ACCOMPLISHED. REMOVED COMPLETE SECTION OF SEAT TRACK SUPPORT AND INSTALLED NEW PART.

Part: INTERCOSTAL — CORRODED · airframe 38,084 hrs · 14,046 cycles

CABIN BODY STATION 400 WL 208 RBL40, FLOORBEAM INTERCOSTAL TOP SURFACE DAMAGED FROM EXCESSIVE MATERIAL LOSS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 38,084 hrs · 14,046 cycles

CABIN FLOOR INNER CREASE BEAM CHORD AT STATION 760 RBL 65 STRINGER 17R HAD EXCESSIVE MATERIAL REMOVED DURING CORROSION CLEAN UP. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLES AND STRAP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,084 hrs · 14,046 cycles

FLOORBEAM CORRODED, STATION 365 RBL 618. MAJOR REPAIR ACCOMPLISHED. ANGLE REPAIR INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,084 hrs · 14,046 cycles

CABIN FLOOR UPPER T-CAP UPPER SURFACE CORRODED STATION 365 RBL 10 STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP AND L-ANGLE REPAIR.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 38,084 hrs · 14,046 cycles

CABIN FLOORBEAM MATERIAL REMOVED EXCEEDS LIMITS STATION 345 RBL 61. MAJOR REPAIR ACCOMPLISHED. TOP T-CAP SPLICED.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 38,084 hrs · 14,046 cycles

CABIN DOOR 2 LEFT LOWER CREASE BEAM CORRODED, STATION 663-754 WATERLINE 208, STRINGER 17 LEFT. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 38,084 hrs · 14,046 cycles

MID CABIN RIGHT HAND CREASE BEAM WEB EXFOLIATED BETWEEN STATION 940-944 STRINGER 17 RIGHT, WATERLINE 208. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM WEB.

Part: PNEUMATIC SYST — SMOKING (CABIN)

CREW REPORTED TWO AFT SMOKE DETECTORS SOUNDING INTERMITTENTLY. *S/D* MAINTENANCE DETERMINED THAT THE CAUSE OF SMOKE IN CABIN WAS A RESULT OF PNEUMATIC SYSTEM OIL CONTAMINATION FROM THE APU. THE SUSPECT APU WAS REPLACED IN ORD ON 12/3/98. PACK BURNOUT WAS ACCOMPLISHED TO EXPEL RESIDUAL OIL IN PNEUMATIC SYSTEM. APU HAS BEEN RETURNED TO SHOP FOR ANALYSIS.

Part: APU — FOD (APU COMPT)

OIL LIKE ODOR DETECTED IN REAR CABIN AREA. THE ODOR WAS NOT STRONG OR PUNGENT, BUT IT DID SET OFF THE AFT LAV SMOKE DETECTORS. *S/D* THE APU WAS REPLACED DUE TO CONTAMINATED PNEUMATICS. DURING DISASSEMBLY AND SHOP INSPECTION OF THE APU A PLASTIC BAG WAS FOUND IN THE INLET.

Part: SEAL — COAKED (NR 2 ENGINE)

FLIGHT DIVERTED TO TLH DUE TO SMOKE IN THE COCKPIT AND CABIN. *S/D* AFTER ENGINE DISASSEMBLY, EVIDENCE SHOWED OIL HAD GONE THROUGH THE HPC OF THE NUMBER 2 ENGINE. THIS CAUSED SMOKE TO PASS THROUGH THE RIGHT ENGINE BLEED. THE NUMBER 2 ENGINE WAS REPLACED.

Part: MATERIAL — LEAKING (EXCAPE SLIDE)

SLIDE FAILED AIR RETENTION DURING SHOP TEST. *S/D* UNIT WAS SENT TO THE VENDOR FOR EVALUATION AND REPAIR. THE SLIDE LEAKED DUE TO POROSITY OF THE INFLATABLE MATERIAL, AND WAS BEYOND REPAIR.

Part: FLAP LIGHT — ILLUMINATED (TE FLAPS)

TRAILING EDGE FLAP LIGHT CAME ON WHEN MOVING FLAP HANDLE FROM 20 TO 25 DEGREES FLAP POSITION. FLAP INDICATOR REMAINED AT 20 DEGREES. A/C LANDED SFO UNDER AMBER ALERT. *S/D* THE CAUSE OF THIS DISCREPANCY WAS NOT FOUND. TROUBLESHOOTING AND OPERATIONAL CHECKS WERE ACCOMPLISHED PER APPLICABLE MMS AND NO DISCREPANCIES WERE NOTED.

Part: SLIDE REGULATOR — CORRODED (CABIN)

DURING OVERHAUL OF SLIDE, INFLATION REGULATOR FAILED. REGULATOR AND ASPIRATORS SHOWED SIGNS OF HEAVY CORROSION. DISASSEMBLY OF REGULATOR REVEALED FOD WAS PREVENTING NORMAL OPERATION OF THE REGULATOR.