N536UA

Part: APU — DEFECTIVE (APU BAY) · airframe 75,155 hrs · 27,412 cycles

HOT OIL SMELL IN PACK WITH APU RUNNING. DEBRIEFED FLT CREW, OIL SMELL ONLY WHEN APU SUPPLYING AIR. INOPERATIVE APU SHUTOFF VLV. REPLACED APU IAW AMM 49-2 1-01. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — DIRTY (RT SQUIB) · airframe 74,369 hrs · 27,184 cycles

RT ENG SQUIB TEST ONE FAILS TO TEST. CLEANED CONNECTOR ON SQUIB, TESTED OK TEN TIMES.

Part: HYDRAULIC LINE — LEAKING (LT ENGINE) · airframe 73,420 hrs · 26,882 cycles

LT ENG LEAKING FLUID ABOUT 1 - 2 DROPS EVERY 5 - 6 SECONDS. REPLACED DEPLOY HOSE ON NR 1 ENG WITH TEMPORARY LINE IAW GPM 01-0-13-003. REPLACED TEMPORARY HOSE WITH PERMANENT HOSE FOR REVERSER DEPLOY. LEAK & OPERATIONS CHECKED GOOD.

Part: INDICATION SYS — MALFUNCTIONED (FUEL SYSTEM) · airframe 73,331 hrs · 26,857 cycles

5 MIN AFTER TAKEOFF LT FUEL QTY BLANKED, RT FUEL QTY ALREADY DEFERRED SO NO QTY INDICATED, FUEL QTY INDICATOR STATUS.

Part: COVER — UNSECURE (L1 DOOR) · airframe 73,320 hrs · 26,853 cycles

WINDOW FRAME PLASTIC COVER AT 1L & 2R LOOSE. SECURED WINDOW FRAME PLASTIC COVERING AT L1 & 2R DOOR, AIRCRAFT OK TO CONTINUE.

Part: SMOKE GOGGLES — DAMAGED (COCKPIT) · airframe 73,286 hrs · 26,844 cycles

CAPT`S SMOKE GOGGLES NEED REPLACEMENT, ELASTIC SHOT. INSTALLED CAPT`S MISSING SMOKE GOGGLES.

Part: LAMP — INOPERATIVE (ROW 12ABC) · airframe 72,966 hrs · 26,730 cycles

ROW 12 ABC, NO SMOKE & SEAT BELT SIGN INOPERATIVE. REPLACED LAMPS, LIGHT OPS OKAY.

Part: CAP — MISSING (CABIN) · airframe 72,654 hrs · 26,620 cycles

FLOOR EMERGENCY LIGHT SYSTEM MISSING SEVERAL END CAPS. REPLACED EMERGENCY LIGHT SYSTEM END CAPS.

Part: WINDOW — DISLODGED (SEAT 26A) · airframe 72,593 hrs · 26,597 cycles

WINDOW FELL OUT OF FRAME, SEAT 26A. REINSTALLED WINDOW FRAME AT SEAT 26A, OPS CHECKED GOOD.

Part: SEAL — OBSTRUCTED (R1 DOOR) · airframe 72,582 hrs · 26,593 cycles

SQUEAL IN R1 DOOR ENDING AT TOP OF CLIMB. INSPECTED R1 DOOR SEAL, CLEANED DEBRIS FROM SEAL & PRESSURIZE ACFT TO 3 PSI IAW MM, NO SQUEAL NOTED.

Part: CABLE — DISCONNECTED (OVERWING SLIDE) · airframe 72,229 hrs · 26,478 cycles

DURING C-CHECK, RT OVERWING ESCAPE SYS LUBE, SLIDE RELEASE CABLE FOUND NOT ATTACHED TO THE SLIDE PACK & PACK COVER WAS UNLACED INSIDE SLIDE COMPARTMENT. R & R RT OVERWING SLIDE.

Part: CABLE — DETACHED (OVERWING SLIDE) · airframe 72,229 hrs · 26,478 cycles

DURING C-CHECK, LEFT OVERWING ESCAPE SYS LUBE, SLIDE RELEASE CABLE FOUND NOT ATTACHED TO SLIDE PACKED. R & R LT OVERWING ESCAPE SLIDE.

Part: STOP FITTING — LOOSE (EXIT DOORWAY) · airframe 72,229 hrs · 26,478 cycles

RT FWD EMERGENCY EXIT CUTOUT, FWD UPPER DOOR STOP PAD LOOSE. REINSTALLED LOOSE DOOR STOP PAD ON THE RT FWD EMER EXIT CUTOUT IAW DWG 144N8641.

Part: SKIN — DENTED (BS 755) · airframe 72,229 hrs · 26,478 cycles

RAMP REPORTED A DENT LEFT FUSELAGE SKIN BS 755 S15-16L. AFT OF DOOR 2L. MEASUREMENTS ARE 1.5" WIDTH X 1.75" LENGTH, .070" DEEP. A-Y=21.4 CONT OF AMIS ITEM 0672022. ACP A INTERIM REPAIR BURMISH OUT ALL SHARP EDGES AND DENT IS SMOOTH AND FREE FROM SHARP CREASES GOUGES AND CRACK. ACP A NTM PART 6-51-00-19. APPLIED PRIMER, ALODINE AND PAINT. AN EXAMINATION OF THE DENT IS REQUIRED EVERY 300 HOURS AND A PERMANENT REPAIR IS MADE AT OR BEFORE THE NEXT 'C' CHECK. REPAIRED SKIN DAMAGE AT STA 755 BETWEEN 15L AND 17L BY. INSTALLED DOUBLER.

Part: SKIN — GOUGED (LT WING) · airframe 72,229 hrs · 26,478 cycles

LEFT WING INBD MAIN FLAP, OTBD CARRIAGE ATTACHMENT AREA, GOUGE IN SKIN ABOVE FWD OTBD ATTACH FITTING. REPAIRED AREA IAW EA 13 0717 AND ECRA 5750-04568.

Part: BRACKET — CORRODED (BS 1400-1420) · corrosion level 2 · airframe 72,229 hrs · 26,478 cycles

FOUND CORROSION ON MOUNT BRACKET UNDER SEALANT AT ON WEB BETWEEN BS 1400 AND 1420 RBL 24. REMOVED WEB FROM BS 1360-1380 AND 1380-1340, RBL 24-02 AND ATTACHING STRUCTURE IAW SRM 51-40-02. REMOVED CORROSION IAW SRM 51-10-02 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15, FIG 101, DET VI. FABRICATED, LOCATED DRILLED, ANODIZED, PRIMED AND TOPCOATED REPAIR PARTS IAW DWG 146N8522 AND INSTALLED IAW DWG 146N8522. MAJOR REPAIR.

Part: RELAY — MISINSTALLED (E/E BAY) · airframe 72,229 hrs · 26,478 cycles

E & E COMPARTMENT PANEL P33 RELAY K10875 INSTALLED INCORRECTLY IAW TC 297224580 AND AD 2008-11-07. REPAIRED THE MISLOCATED HOLES IN THE E&E COMPARTMENT PANEL P33 RELAY IAW EA 130737 AND ECRA 2400-02175.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,229 hrs · 26,478 cycles

FOUND CORROSION DURING REMOVAL OF AFT CARGO DOOR WEB. REMOVED CORROSION ON LOWER STRUCTURE OF AFT CARGO DOOR CUTOUT, FOUND TO BE WITHIN LIMITS IAW ECRA 5360-01330 AND EA 130794. HFEC IAW EA 130794, STEP 5, NO DEFECTS NOTED.

Part: WIRE — DAMAGED (ELECTRICAL) · airframe 72,229 hrs · 26,478 cycles

WIRE DAMAGED AT BS 1681, WL 200 RBL 044, APPROX 6 INCHES BELOW THE ACCELEROMETER, M10735 BEHIND THE CARGO BAY BULKHEAD. REPAIRED WIRE IAW SWPM 20-10-13 AND WDM 30-11-21 AND GMM 05-30-40.

Part: WIRE — DAMAGED (WINDOW ANTI ICE) · airframe 72,229 hrs · 26,478 cycles

WIRE BUNDLE DAMAGED. WIRES CHAFING ON THE TOP LT FWD SIDE OF THE E2 RACK. REPAIRED WIRES IAW SWPM 20 -10-13, 20-30-12 AND WDM 30-41-11 OPS CHECKED FOR FLIGHT DECK WINDOW ANTI-ICING GOOD IAW AMM 30-41-00.

Part: LATCH — FAILED (OXYGEN MASK DOOR) · airframe 72,229 hrs · 26,478 cycles

DURING PAX O2 DOOR LATCH OPS CHECK, FOUND SEAT ROWS 8L AND 37L WOULD NOT DROP. FURTHER INVESTIGATION FOUND THEM TO BE MECHANICALLY INOPERATIVE. REMOVED THE OXYGEN DOOR LATCH ASSY'S, R & R DOOR LATCH ASSY HOUSING AND REINSTALLED LATCH ASSY'S AT ROWS 8L AND 37L. OPS CHECKED GOOD IAW AMM 35-21-00-501.

Part: STRUCTURE — CORRODED (BS 1440) · corrosion level 2 · airframe 72,229 hrs · 26,478 cycles

AFT CARGO INNER STRUCTURE CORRODED AT BS 1440, RBL 19 AFT OF DOOR CUTOUT. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, FIG 101. REMOVED STRUCTURE IAW SRM 51-40-02. FABRICATED, LOCATED, DRILLED, ALODINED, PRIMED, TOP COATED AND INSTALLED NEW STRUCTURE IAW DWG 146N8522.

Part: SKIN — DAMAGED (BS 1701) · airframe 72,229 hrs · 26,478 cycles

LEFT LOWER FUSELAGE FWD OF BS 1701 HAS DENT. INSTALLED A SKIN REPAIR BETWEEN BS 1685 & 1710 AND S18-21L IAW ECRA 5360-01328. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 755 S15-16L) · airframe 72,229 hrs · 26,478 cycles

A DENT LOCATED AT BS 755 BETWEEN S15-16L. REPAIRED SKIN IAW EA 130704 AND ECRA 5330-04658.

Part: INTERCOSTAL — CORRODED (BS 1681-1701) · corrosion level 2 · airframe 72,229 hrs · 26,478 cycles

AFT CABIN BS 1681-1701 RBL 51 INTERCOSTAL CORRODED ON TOP SURFACE. REPAIRED INTERCOSTAL IAW EA 130756 AND ECRA 5360-01331. R & R THE INTERCOSTAL IAW SRM 51-40-02 AND DWG 146N5300. MAJOR REPAIR.

Part: FLOORBEAM — CRACKED (BS 700) · airframe 72,229 hrs · 26,478 cycles

CABIN FLOORBEAM BS 700, LBL 25 CRACKED IN THE RADIUS OF UPPER TEE. REMOVED DAMAGED AREA OF FLOORBEAM UPPER TEE AT LBL 25, ACCOMPLISHED HFEC OF CUT-OUT & FASTENER HOLES, NO DEFECT NOTED. FABRICATED & INSTALLED REPAIR SPLICE FROM LBL 18 TO LBL 32 IAW ECRA 5310-05536

Part: SKIN — DAMAGED (BS 1393) · airframe 72,229 hrs · 26,478 cycles

SKIN DAMAGED BS 1393, INSTALLED DOUBLER BS 1384-1401 S28L-29R IAW EA 130660 AND ECRA 5360-0 1313.

Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 72,229 hrs · 26,478 cycles

CABIN BS 1681 FLOORBEAM HAS CORROSION LBL 12, RBL4, RBL12, RBL 48 ON FORWARD SIDE OF FLOORBEAM AROUND NUTPLATES. CLEANED CORROSION FROM LBL12 TO RBL 12 AND IT IS WITHIN LIMIT IAW SRM 53-00-51. REPAIRED FLOORBEAM AT RBL 48 IAW SRM 53-60-51.

Part: SLIDE — DAMAGED (RT OVERWING) · airframe 72,229 hrs · 26,478 cycles

RIGHT OVERWING SLIDE LACING HAS COME LOOSE. R & R RT OVERWING SLIDE IAW AMM 25-65-01.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 72,229 hrs · 26,478 cycles

MAIN CABIN AFT WET AREA FLOORBEAM, BS 1640 LBL 9 TO RBL 61 UPPER SURFACE OF TEE CORRODED. REPAIRED CORRODED TEE AT BS 1640 IAW ECRA 5310-05536, REPAIR 3.

Part: CABLE — DETACHED (LT OVERWING) · airframe 72,229 hrs · 26,478 cycles

LEFT OVERWING EMERGENCY ESCAPE SLIDE RELEASE CABLE FOUND NOT ATTACHED TO SLIDE. REPLACED SLIDE.

Part: FLOOR PANEL — CORRODED (BS 1681) · corrosion level 2 · airframe 72,229 hrs · 26,478 cycles

AFT CABIN UPPER FLOOR DECK PLATE AT BS 1681 CORRODED FROM LBL 11 TO RBL 61. REPAIR UPPER DECK PLATE IAW ECRA 5330-04259 REPAIR 2.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,135 hrs · 26,447 cycles

FIRST SECTION OF EMERGENCY LIGHTS IN COACH INOPERATIVE. REPLACED POWER STRIP AND LIGHT SECTION, OP CHECKED OK.

Part: FRAME — DENTED (BS 1420 S25-26L) · airframe 55,800 hrs · 20,477 cycles

AFT CARGO BAY FRAME DENTED BS 1420 S25 & 26L. REPAIRED FRAME IAW SRM 53- 00-07 DETAIL III PG 8. MAJOR REPAIR.

Part: FRAME — DENTED (BS 1480 S26L) · airframe 55,800 hrs · 20,477 cycles

AFT CARGO BAY BS 1480, S26L FRAME DENTED. REPAIRED FRAME IAW SRM 53-00-07 REPAIR 5 TABLE II ZONE 1. MAJOR REPAIR.

Part: FRAME — DENTED (BS 1540 S25-27L) · airframe 55,800 hrs · 20,477 cycles

AFT CARGO BAY BS 1540, BETWEEN S25 & 27L FRAME DENTED. REPAIRED FRAME IAW SRM 53-00-07 REPAIR 5 TABLE II ZONE 1. MAJOR REPAIR.

Part: FRAME — DENTED (BS 1400 S25-26L) · airframe 55,800 hrs · 20,477 cycles

AFT CARGO BAY FRAME DENTED BS 1400 S25-26L. INSTALLED DOUBLER REPAIR PER SRM 53-00-07, REPAIR 5, DETAIL III, PG 208 AND SRM 51-40-02. PER SRM 53-00-07, REPAIR 5, PG 210, TABLE I. MAJOR REPAIR.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 71,950 hrs · 26,389 cycles

EMERGENCY LIGHT ACROSS THE ENTRY DOOR TO THE MID LAVATORY IS INOPERATIVE. RECONNECT EMERGENCY LIGHT, OP CHECKED GOOD.

Part: BLADE — NICKED (NR 1 ENGINE FAN) · airframe 71,847 hrs · 26,359 cycles

NR 2 ENGINE HAS A NICK IN FAN BLADE. BLENDED ONE FIRST STAGE BLADE ON NR 2 ENGINE REF MM.

Part: BUSHING — WORN (NR 7 SPOILER) · airframe 71,761 hrs · 26,329 cycles

NR 7 SPOILER HAT BUSHINGS FOR ROD END ARE WORN. REPLACED WORN SPOILER HAT BUSHINGS P/N ZLS43E NR 7 SPOILER RE-INSTALLED PIN WASHER AND NUT PER MM. ALL CHECKS GOOD AT THIS TIME.

Part: ACTUATOR — FAILED (SPOILER) · airframe 71,761 hrs · 26,329 cycles

REF CH5479, T-S PER FIM.27-09-00 PG126 FIG 105 FAILED BLOCK 14. RESISTANCE CHECK. NEED TO REPLACE 6 & 7 PCA. REMOVED AND REPLACED 6 & 7 PCA PER MM, OP'S CHECK'S GOOD.

Part: SQUIB — NO TEST (COCKPIT) · airframe 71,692 hrs · 26,305 cycles

EMERGENCY ESCAPE SQUIBS IN COCKPIT FAILED TEST. OPS CHECKED EMERGENCY ESCAPE SQUIBS LIGHT TEST. OPS CHECKED GOOD.

Part: FCU — FAILED (NR 1 ENGINE) · airframe 71,612 hrs · 26,279 cycles

NR 1ENG FLAME OUT. REMOVED AND REPLACED FUEL PUMP AS PER AMM, FUEL CONTROL AS PER AMM AND ALSO EEC AS PER MM 73-21-04.

Part: FCU — MALFUNCTIONED (LT ENGINE) · airframe 71,612 hrs · 26,279 cycles

LEFT ENGINE ROLLED BACK AFTER START. FLAMES REPORTED. REPLACED LEFT ENGINE FUEL PUMP, FUEL CONTROL UNIT AND EEC.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,569 hrs · 26,266 cycles

EXTERIOR EMERGENCY LIGHT AT L1 DOOR INOPERATIVE. REPLACED LAMP.

Part: IGNITER — FAULTY (NR 2 ENGINE) · airframe 71,007 hrs · 26,083 cycles

IGNITION IN POSITION 1 HAD A NO LIGHT OFF STARTING NR 2 ENGINE. STARTED IN BOTH. NORMAL ENGINE START WITH IGNITION IN "BOTH" OK TO DEFER USING MEL 7400C. RPL- :NR 1 & 2 SPARK PLUGS. RAN THE ENGINE OP CHECK OKAY.

Part: THRESHOLD — DAMAGED (CABIN) · airframe 70,788 hrs · 26,010 cycles

AFT GALLEY FLOORBOARD CAME OFF. FLOORBOARD OK. PLASTIC THRESHOLD BETWEEN UNDER CART FLOOR COVER AND GALLEY AREA RUBBER MAT PULLED UP AND TORN. REMOVED DAMAGED THRESHOLD AND SECURED AREA WITH TAPE 20-DAY LIMIT.

Part: LINK — BROKEN (NLG STEERING) · airframe 70,698 hrs · 25,978 cycles

NOSE WHEEL STEERING SUMMING MECHANISM TWO LINKS BROKEN AND BOTH PULLEYS DAMAGED. REPLACED NWSA, NWSB AND LEFT COMPENSATOR LINK.

Part: SUPPORT BRACKET — BROKEN (NLG STEERING) · airframe 70,698 hrs · 25,978 cycles

NOSE WHEEL STEERING UPPER PULLEY SUPPORT BRACKET BROKEN. UPPER LEFT CORNER PULLEY MISSING. REPLACED BRACKET.

Part: BRACKET — DAMAGED (NLG STEERING) · airframe 70,698 hrs · 25,978 cycles

NOSE WHEEL STEERING CABLE ASSY CAME OFF PULLEYS AND IS DAMAGED. REPLACED BRACKET ASSEMBLY PER MM AND PULLEYS.

Part: SKIN — DENTED (FUSELAGE) · airframe 70,067 hrs · 25,757 cycles

RAMP REPORTS DENT AT LEFT FUSE AT STA 755 BET STR 15L + 16L. AFT OF DOOR 2L. MEASUREMENTS ARE 1.5\ WIDTH X 1.75\ LENGTH, .070\ DEEP. A-Y=21.4 CONT OF AMIS ITEM 0672022. ACP A INTERIM REPAIR BURNISH OUT ALL SHARP EDGES AND DENT IS SMOOTH AND FREE FROM SHARP CREASES GOUGES AND CRACK. ACP A NTM PART 6-51-00-19. APPLIED PRIMER, ALODINE AND PAINT AN EXAMINATION OF THE DENT IS REQUIRED EVERY 300 HOURS AND A PERMANENT REPAIR IS MADE AT OR BEFORE THE NEXT C CHECK.

Part: MOTOR — LEAKING (LT HYD SYSTEM) · airframe 69,567 hrs · 25,581 cycles

FLUID LEAKING FROM APU FIRE CONTROL ACCESS DOOR. FOUND LEAK COMING FROM BOTTOM LEFT HYDRAULIC MOTOR OF STAB TRIM BALL SCREW ACTUATOR IPC 27-41-10-001. ITEM 45 PCN 611-9023. LEAK IS 23 DROPS PER MINUTES. WITHIN LIMITS PER MM. ALL HYDRAULIC SYSTEMS ARE FULL.

Part: UNKNOWN — LEAKING (HORIZONTAL STAB) · airframe 68,507 hrs · 25,224 cycles

FLUID LEAKING IN RIGHT HORIZONTAL STAB AREA. LEAK APPEARS TO BE COMING FROM THE RUDDER AREA AND RUNNING DOWN HORIZONTAL STAB AREA. ACCESSED THE RUDDER PCA'S AND CLEANED AREA. CYCLED THE RUDDER THRU FULL TRAVEL SEVERAL TIMES. NO LEAKS NOTED, CHECK WAS INCONCLUSIVE. VISUALLY INSPECTED RUDDER AND THE UPPER AND LOWER RIGHT SIDE OF HORIZONTAL STAB NO EVIDENCE OF LEAK.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 66,973 hrs · 24,656 cycles

SMOKE IN COCKPIT AFTER ENGINE SHUT DOWN. SEEMS AC PACK RELATED. CABIN NORMAL. ACP FAULT ISOLATION PROCEDURE NR 4 OF MM. FOUND NO SMOKE SMELL IN FLIGHT DECK OR CABIN AFTER ENGINE START OR ENGINE SHUTDOWN.

Part: SEAL — MISSING (TE FLAP) · airframe 66,747 hrs · 24,576 cycles

RT WING OTBD FLAP INBD TRACK FAIRING MISSING RIGHT SEAL ON AOG U4388. MUST BE ADDRESSED AT NEXT MAINT OPPORTUNITY PER MM 57-22-99 SEAL RETAINER IS SECURE. REPLACED SEAL.

Part: SEAL — MISSING (TE FLAP) · airframe 66,747 hrs · 24,576 cycles

PAX OBSERVED A PIECE OF FABRIC REMOVE FROM TRAILING EDGE FLAP DURING EXTENSION A-C LEFT. SHOULD BE FIXED NEXT MAINT OPPORTUNITY PER MM. ORD INF- :LT WING I/B FLAP I/B TRACK FAIRING LT SEAL. RPL-:REPLACED SEAL.

Part: FUEL LINE — MISINSTALLED (NR 2 ENGINE) · airframe 66,741 hrs · 24,573 cycles

NR 2 ENGINE MAIN FUEL LINE QUICK DISCONNECT IMPROPERLY CONNECTED. REMOVED & REPLACED THE NR 2 MAIN FUEL LINE AND QUICK DISCONNECT IAW MM. NO LEAKS NOTED PER B757 AMM.

Part: LANYARD — MISROUTED (L1 GIRT BAR) · airframe 66,741 hrs · 24,573 cycles

L1 DOOR GIRT BAR CHAIN LANYARD NOT ROUTED PROPERLY. SUPPLEMENTAL DATA UPDATE DISCONNECTED AND RMV'D AND CONNECTED L1 DOOR SLIDE GIRTBAR LANYARD CHAIN PROPERLY IAW UAL W-C 5R5211010 ON NON ROUTINE 3121N00088 BY EMP 720049.

Part: QUICK DISCONNECT — MISINSTALLED (NR 1 ENGINE) · airframe 66,741 hrs · 24,573 cycles

NR 1 ENGINE MAIN FUEL LINE QUICK DISCONNECT IMPROPERLY CONNECTED. RESECURED NR 1 ENGINE MAIN FUEL LINE QUICK DISCONNECT IAW AMM ON NR 3121N002 39.

Part: HOSE — KINKED (L2 DOOR SLIDE) · airframe 66,741 hrs · 24,573 cycles

DURING TEST OF DOOR 2 LEFT SLIDE DEPLOYMENT ON ROUTINE TASK CARD 5R251S061, THE SLIDE DEPLOYED PROPERLY AND WITHIN THE ALLOTED TIME PER THE TASK CARD BUT THE AFT INFLATION HOSE KINKED. SUPPLEMENTAL DATA UPDATE REPORTING SDR AND INSTALLED REJECT FOLLOW UP TAG ON SLIDE. ON ROUTINE TASK CARD 5R251S015. REMOVED AND REPLACED THE NUMBER 2 LT SLIDE.

Part: FILTER — FAULTED (LT ENGINE) · airframe 66,685 hrs · 24,552 cycles

L ENG FUEL FILTER EICAS, RTFL SAMC TEXT: ACP CHECK OF MAIN FUEL FILTER PER MM. ALSO ACP TEST OF FUEL FILTER INDICATION SYSTEM PER MM. REPLACED FUEL PUMP FILTER PER MM. EXAMINATION OF FUEL FILTER SHOWED NO ABNORMAL FINDINGS. REPLACED DIFFERENTIAL PRESSURE SWITCH PRECAUTIONARY. RAN ENGINE, NO DISCREPANCIES NOTED OR STATUS MESSAGES GENERATED.

Part: LIGHT — BROKEN (CABIN) · airframe 66,380 hrs · 24,451 cycles

EEL PATH LIGHTING INOP FROM ROWS 8 THRU ROWS 12. FLOOR EMERGENCY LIGHT STRIPE BROKEN IN REAR OF AISLE. MOST SECTIONS IN COACH DO NOT TEST. REPLACED LIGHT STRIP, LIGHTS CHECK GOOD.

Part: LIGHT — UNSECURE (SEAT 13ABC) · airframe 65,305 hrs · 24,050 cycles

EMERGENCY LIGHTS AT 13ABC ARE COMING UP TRIPPING HAZARD. SECURED EMERGENCY PATH LIGHT STRIP COVER TO TRACK

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,555 hrs · 23,774 cycles

FWD PIT FRAME CRACKED WHERE GUIDE MOUNTS TO JACKSCREW FWD END. REPLACED SUPPORT STRINGER.

Part: PANEL — PUNCTURED (WTB FAIRING) · airframe 62,072 hrs · 22,844 cycles

FOUND WTB FAIRING PANEL 194CR PUNCTURED. REMOVED PANEL. REPLACED THREE BAD NUT PLATES ON AIRCRAFT STRUCTURE. SUMP DRAIN LINE DISCONNECTED TO REMOVE PANEL. PANEL NEEDS REPAIR OR REPLACE. CONNECTED SUMP DRAIN LINE AND REPLACED PANEL.

Part: MODULE — FAULTY (EMERGENCY LIGHT) · airframe 62,030 hrs · 22,827 cycles

PER CREW: ALL THE EMERGENCY LIGHTS ARE ON IN CABIN WITH AIRCRAFT POWERED AND EMERGENCY LIGHT SWITCH IN ARMED POSITION. SUPPLEMENTAL DATA UPDATE REPLACED EMERGENCY LIGHT MODULE M731 AND BATTERY IAW MM. OPS TESTED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 62,030 hrs · 22,827 cycles

EMERGENCY LIGHTS AROUND DOORS 1L AND 1R ILLUMINATED. COCKPIT EMERGENCY LIGHT SWITCH NO CHANGE. REPLACED M731 POWER SUPPLY AND BAT M731 NEXT TO FWD OVERHEAD MONITOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,102 hrs · 21,325 cycles

DOOR NR 1 LT EMERGENCY EXIT LIGHT INOP (EXT). RELAMPED, CHECKS GOOD.

Part: FUEL CONTROL — MALFUNCTIONED (LT ENGINE) · airframe 57,928 hrs · 21,265 cycles

LEFT ENGINE SHUTDOWN BY ITSELF AFTER START. REPLACED FUEL CONTROL UNIT.

Part: BEARING — CORRODED (R3 DOOR) · airframe 56,402 hrs · 20,695 cycles

THE 3R DOOR HARD TO ARM & DISARM. INTERNAL BEARING RUSTED AND SIEZED. REPLACED BEARING. DOOR OPS NORMALLY.

Part: GIRT BAR — DIRTY (R3 DOOR) · airframe 56,128 hrs · 20,600 cycles

THE 3R WILL NOT ARM. CLEANED AND LUBED 3R GIRT BAR FITTING, OPS CHECKED NORMAL.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 56,109 hrs · 20,590 cycles

BS 1440 STR 26L HAS DAMAGE. ACCOMPLISHED MAJOR REPAIR AT GSO--RPR WAS RPL ON PTT#8002108 PER SRM 53 -00-07 RPR 5. THIS IS A RPR IN ZONE 1 AND IS CAT B RPR AND REQUIRES SUPPLEMENTAL INSPECTIONS STARTING AT 50,000 TOTAL FLIGHT CYCLES AND 12,000 FC THERE AFTER. INSPS ARE BOTH VISUAL AND NDT PER SRM 53-00-07 RPR 5 TABLE II. CURRENT PTC IS 20477. ON NR 46109 -INF- : REPAIR ACCMPLSHED PER SRM 50-00-07 TABLE II ZONE 1. REQUIRING REINSPECTION AT 50,000 CYCLES & REPEAT AT 12,000 CYCLES. THIS IS CAT B REPAIR. EC 50-5330-036SA -A CREATED TO ACCMPLSH INSP'S. DTA 03-184 WILL TRACK REPAIR.

Part: WIRE — NICKED (LAVATORY) · airframe 56,035 hrs · 20,557 cycles

PAX REPORTED RECEIVING A ELECTRIC SHOCK IN MID LAV. FOUND VERY TINY NICK ON DOOR SWITCH WIRE, GROUNDING TO LAV STRUCTURE. REPAIRED WIRE.

Part: SKIN — DAMAGED (BS 1700 S19-20L) · airframe 55,800 hrs · 20,477 cycles

DOUBLER INSTALLED STA 1700 STR 19 TO 20L. SUPPLEMENTAL , REPAIR ACCOMPLISHED: REMOVED EXISTING REPAIR DOUBLER AND VERIFIED ALL DAMAGE REMOVED BY HFEC INSPECTION. FABRICATED AND INSTALLED A NEW DOUBLER AND STRUCTURAL FILLER.

Part: FRAME — DAMAGED (BS 1681) · airframe 55,800 hrs · 20,477 cycles

RT FRAME REPAIR WAS ACP'D BS 1681, WL-209. ACCOMPLISHED MAJOR, PER EVA MOC1-8433 REVA. AFTER DTA, THIS REPAIR IS CONSIDERED TO BE A CAT 'A' TIME LIMITED REPAIR. THIS REPAIR MUST BE REPLACED PER REVISED EVA-40093, NO LATER THAN NEXT HMV CURRENTLY SCHEDULED 06JUN08 AND REPAIR IS TO BE RE-INSPECTED AT EACH 'C' CHK PER EVA INSTRUCTIONS.

Part: FRAME — DENTED (BS 1480 S26L) · airframe 55,800 hrs · 20,477 cycles

AFT PIT STA 1480, STR 26L FRAME DENTED. AFT PIT STA 1480, STR 26L FRAME DENTED. REPAIRED FRAME DENTS IAW S RM 53-00-07 RPR 5 TABLE II ZONE 1.THIS REPAIR MUST BE REINSPECT ED STARTING AT 50000 TOTAL FLIGHT CYCLES AND 12000FC THERE AFTER .

Part: FRAME — DENTED (BS 1540 S25-27L) · airframe 55,800 hrs · 20,477 cycles

AFT PIT STA 1540, BETWEEN STR 25L AND 27L FRAME DENTED (3 EA DENTS). AFT PIT STA 1540, BETWEEN STR 25L AND 27 L FRAME DENTED (3 EA DENTS) REPAIRED FRAME DENTS IAW S RM 53-00-07 RPR 5 TABLE II ZONE 1.THIS REPAIR MUST BE REINSPECT ED STARTING AT 50000 TOTAL FLIGHT CYCLES AND 12000FC THERE AFTER.

Part: STRUCTURE — CRACKED (RT WING LE) · airframe 55,800 hrs · 20,477 cycles

CRACK INDICATION UNDER FLAKING TEFLON PAINT ON UPPER SURFACE OF THE RT WING FIXED LEADING EDGE BELOW NR 10 SLAT. REMOVED DAMAGED AREA APPLIED A PRE-PREG FIBERGLASS REPAIR IAW SRM 57-41-01 AND 51-70-07

Part: WIRE — DETERIORATED (SMOKE DETECTOR) · airframe 55,800 hrs · 20,477 cycles

"R" LAV SMOKE DETECTOR WIRE DETERIORATED. REPLACED BOTH WIRES FOR SMOKE DETECTOR IN "R" LAV. OPS CHECKED GOOD.

Part: SKIN — DENTED (L1 DOOR) · airframe 55,800 hrs · 20,477 cycles

DOOR L1 HAS SKIN DENT LWR MID AREA OF SKIN ABOVE GATE. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA. ACCOMPLISHED HFEC. NO CRACK INDICATED. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: SKIN — DAMAGED (R2 DOOR) · airframe 55,800 hrs · 20,477 cycles

DOOR 2R UPPER HINGE ARM CUTOUT REQUIRES DOUBLER TO BE INSTALLED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. ACCMP'D HFEC. PERFORMED INSURANCE CUT. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: SKIN — DAMAGED (L2 DOOR) · airframe 55,800 hrs · 20,477 cycles

DOOR 2L UPPER HINGE ARM CUT OUT REQUIRES DOUBLER TO BE INSTALLED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. ACCMP'D HFEC. PERFORMED INSURANCE CUT. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: SLIDE — READS LOW (R1 DOOR) · airframe 55,800 hrs · 20,477 cycles

DOOR R1 SLIDE PRESSURE LOW. REPLACED SLIDE R1, PRESSURE OK.

Part: FRAME — DENTED (BS 1420) · airframe 55,800 hrs · 20,477 cycles

AFT PIT FRAME DENTED STA 1420 S25L TO 26L. REPAIRED FRAME IAW SRM 53- 00-07 DETAIL III PG 8 FRAME FALLS UNDER THE INSPECTION REQUIRMENTS OF SRM 53-00-07 RPR 5 TABLE II ZONE 3. INSPECTIONS TO BEGIN 1 2000 FLIGHT CYCLES AFTER INSTALLATION AND 11000 FLIGHT CYCLES T HERE AFTER. INSPECTIONS ARE BOTH VISUAL AND NDT. PTC CURRENTLY

Part: FRAME — DENTED (BS 1400 S25-26L) · airframe 55,800 hrs · 20,477 cycles

AFT PIT FRAME DENTED STA 1400 S25L TO 26L. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR.

Part: HOUSING — CORRODED (L4 DOOR HANDLE) · airframe 55,800 hrs · 20,477 cycles

DOOR 4L HANDLE BOX CORRODED AROUND INSERTS AND INTERNAL AREA FOR HANDLE ASSY GOUGED. REPLACED HANDLE BOX.

Part: FRAME SPLICE — DAMAGED (FUSELAGE) · airframe 55,800 hrs · 20,477 cycles

AFT PIT STA 1520 BETWEEN STR 22R AND STR 25R FRAME SPLICE HAS TOOL MARKS. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED FRAME SPLICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,800 hrs · 20,477 cycles

FLOORBEAM AT STA 365 RBL 5R MAIN CABIN. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED T-CAP. FABRICATED AND INSTALLED NEW T-CAP.

Part: FLOORBEAM — CORRODED (BS 365) · airframe 55,800 hrs · 20,477 cycles

CORROSION ON FLOORBEAM AT STA 365 RBL 5R MAIN CABIN. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED T-CAP. FABRICATED NEW T-CAP & INSTALLED.

Part: DISPLAY — FAILED (COCKPIT) · airframe 55,559 hrs · 20,401 cycles

AFTER AIRCRAFT ARRIVED, RAMP PLUGGED GROUND POWER IN AND CREW NOTICED AN ACRID ODOR, FOUND UPPER CENTER EICAS CRT SCREEN BURNED UP AND RECEPTACLE ON AIRCRAFT BURNED PINS AND RUBBER INSULATION BURNED.

Part: DISPLAY — DEFECTIVE (COCKPIT) · airframe 55,559 hrs · 20,401 cycles

AFTER AIRCRAFT ARRIVED, RAMP PLUGGED GROUND POWER IN AND CREW NOTICED AN ACRID ODOR, FOUND UPPER CENTER EICAS CRT SCREEN BURNED UP AND RECEPTACLE ON AIRCRAFT BURNED PINS AND RUBBER INSULATION BURNED. BPCU BITE SHOWS EXT PWR OVR VOLT TRIP. REPLACED CRT AND REPT PINS. ALL CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 54,765 hrs · 20,112 cycles

NR 2R DOOR EMERGENCY LIGHT BURNED OUT. REPLACED BURNED OUT LAMP. SYSTEM OPS CHECKED NORMALLY.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 54,227 hrs · 19,903 cycles

WINDOW EICAS MSG DISPLAYED POSITION 2. CAPT'S SLIDING WINDOW (L2) DELAMINATING BOTTOM CENTER OF WINDOW.

Part: BATTERY — DISCHARGED (CABIN) · airframe 52,865 hrs · 19,420 cycles

EMERGENCY LIGHTS INOP AT THE FOLLOWING LOCATIONS: AISLE EXIT SIGN ON CEILING PANEL AT ROW 13, EXIT SIGN OVER RIGHT OVERWING HATCHES, EXIT SIGN AT LWR FWD CORNER OF RT FWD OW HATCH, EXIT SIGN AT LWR FWD CORNER OF LT AFT OW HATCH, & RT AFT OVERWING SLIDE LIGHT ON EXTERIOR OF ACFT. REPLACED BATTERY PACK FOR POWER SUPPLY M10568.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,865 hrs · 19,420 cycles

EEL STRIP IN FRONT OF FWD AFT LAV INOPERATIVE. REPLACED EEL STRIP.

Part: CHARGER — FAULTY (BATTERY) · airframe 52,680 hrs · 19,352 cycles

EICAS WHITE STATUS MSG "MAIN BAT CHGR" DISPLAYED. WILL NOT CLEAR. [06-14-07] REPLACED MAIN BATTERY AND CHARGER PER UA ENGINEERING SPECIFICATIONS.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 52,144 hrs · 19,175 cycles

NR 2 AFT CARGO COMPARTMENT SMOKE DETECTOR INOPERATIVE. [SUP 05-08-07] REPLACED AFT CARGO SMOKE DETECTOR.

Part: SKIN — DAMAGED (BS 600-640) · airframe 51,471 hrs · 18,933 cycles

LEFT FUSELAGE SKIN STA 600-640 STR 16L-17L IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. REPAIRED LEFT FUSELAGE SKIN STA 600 REPAIR ACP STA 600-640 STRINGER - LOCATION OF REPAIR BS 602-642 STR 17L.

Part: SKIN — DENTED (BS 1700) · airframe 48,192 hrs · 17,729 cycles

A 2 INCH GOUGE AND DENT AT DOOR 3L, 2 FEET AFT AND BELOW DOOR AT STA 1700. INSTALLED REPAIR DOUBLER PER SRM 53-00-01.

Part: SWITCH — SHORTED (LAVATORY DOOR) · airframe 47,204 hrs · 17,344 cycles

ELECTRICAL SMOKE SMELLED, WHITE SMOKE SEEN BRIEFLY IN AFT LAV. REPLACED DOOR LOCK SWITCH.

Part: SLIDE — RUPTURED (R1 DOOR) · airframe 49,571 hrs · 18,271 cycles

TUBE RUPTURED DURING OVERPRESSURE (PROOF) TEST. TEST PRESSURE WAS AT 3.41 PSI FOR FIVE MINUTES. INFLATABLE FAILED OVERPRESSURE TEST DUE TO SEAM FAILURE. INFLATABLE WAS BEYOND REPAIR PER CMM. SLIDE WAS SENT TO OEM FOR INFLATABLE REPLACEMENT.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,262 hrs · 15,159 cycles

INBD CAP OF FRAME AT STA 1681 WL 209 IS EXFOLIATED. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED REPAIR IAW EVA MOCI-8433A.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 40,300 hrs · 14,798 cycles

LEFT AFT OFF-WING EMERGENCY SLIDE LIGHT AFT OF AFT OVERWING EXIT HATCH INOPERATIVE. RELAMPED LIGHT.

Part: FRAME — CORRODED (FUSELAGE) · airframe 37,457 hrs · 13,716 cycles

CABIN AFT FRAME STATION 1681 STRINGER 17R RBL 57 I/B CAP EXFOLIATED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 37,457 hrs · 13,716 cycles

FORWARD CABIN FLOOR STATION 365 BL 0 THROUGH RBL 65 UPPER T-CAP IS GOUGED AND CORRODED. MAJOR REPAIR ACCOMPLISHED. SPLICED IN REPAIR CAP.

Part: CAP — CORRODED · airframe 37,457 hrs · 13,716 cycles

CABIN FLOOR BEAM STATION 324 UPPER CAP CORRODED RBL40 TORBL60. MAJOR REPAIR ACCOMPLISHED.SPLICED IN NEW CAP.

Part: FRAME — CORRODED (FUSELAGE) · airframe 37,457 hrs · 13,716 cycles

AFT PIT STATION 1480 FRAME UPPER CHORD HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 37,457 hrs · 13,716 cycles

AFT CABIN PRESSURE DECK CORRODED AT STATION 1684 RBL 52 IN. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: SKIN — DENTED · airframe 37,457 hrs · 13,716 cycles

LEFT HAND UPPER FORWARD FUS SKIN DENTED, STATION 606 TO STATION 612, BETWEEN STRINGER 16 AND STRINGER 17L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.DOUBLER AND FILLER INSTALLED.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 37,457 hrs · 13,716 cycles

CREASE BEAM WEB CORRODED AT STATION 1020, RBL 80, WL208, FWD END OF WEB. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB.

Part: CREASE BEAM — CORRODED · airframe 37,457 hrs · 13,716 cycles

MID CABIN BODY STATION 1022 LEFT HAND CREASE BEAM WEB CORRODED ON UPPER SURFACE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.CREASE BEAM REPLACED.

Part: FRAME — GOUGED (FUSELAGE) · airframe 37,457 hrs · 13,716 cycles

AFT PIT STATION 1520 STRINGER 23R TO 25R, FRAME UPPER CHORD AFT EDGE HAS GOUGES FROM CONTACT WITH SIDEWALL PANEL SCREWS. MAJOR REPAIR ACCOMPLISHED. FRAME SPLICE REPLACED.

Part: FRAME — DENTED · airframe 37,457 hrs · 13,716 cycles

AFT PIT FRAME 1440 DENT ABOVE STRINGER 26L. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER REPAIR.

Part: DUCT — LOOSE (A/C DISTRIBUTION) · airframe 31,507 hrs · 11,520 cycles

OVERHEAD AIR CONDITIONING DUCT BLOCKED. *S/D* AIRCRAFT WAS FOUND WITH 5 SECTIONS OF OVERHEAD DUCT PULLED AWAY FROM CEILING SUPPORTS. 2 SECTIONS FROM MONITOR NR 2 TO ROW 10 HAD SUPPORT BRACKET FAILURES. THREE ADDITIONAL DUCT SECTIONS FAILED BETWEEN ROWS 15 THROUGH 24. THE SUPPORTS ON THESE DUCTS PULLED THROUGH THE DUCTING MATERIAL. NEW DUCT SECTIONS AND BRACKETS HAVE BEEN INSTALLED.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 30,181 hrs · 11,029 cycles

DIVERTED TO CLE DUE TO SMOKE IN THE COCKPIT. *S/D* A VISUAL INSPECTION OF THE RECIRCULATION AND EQUIPMENT COOLING FANS WAS PERFORMED. THE FANS WERE OPERATED (ONE AT A TIME) WITH NO SMOKE OR SMELL. THE PACKS WERE THEN RUN OFF EACH ENGINE INDIVIDUALLY AND OFF THE APU WITH NO SMOKE OR SMELL NOTED.

Part: VALVE — FROZEN (SLIDE BOTTLE)

DURING THE SHOP OVERHAUL OF AN EVACUATION SLIDE REMOVED FOR EXPIRATION OF TIME, THE UNIT FAILED TO FLAT FIRE. MECHANIC PULLED THE FIRING LINE WITH A FORCE OF 20 LBS AND THE BOTTLE VALVE DID NOT OPEN. THE BOTTLE VALVE MANUFACTURER (CARLTON) HAS THE VALVE, (P/N 61199-107) (S/N 2136), UNDER INVESTIGATION.

Part: BULB — FAILED (CABIN)

DOOR 4R EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT, OPERATION CHECKS NORMAL.

Part: SLIDE — LEAKING (DOOR 2R)

DOOR 2 RT SLIDE RETURNED TO SHOP FOR TIME CONTROLLED OVERHAUL. LOWER INFLATION TUBE IS LEAKING AT THE SEAMS AND THERE IS CORROSION IN BOTH ASPIRATORS AND ON THE CHECK VALVES. RETURNED TO VENDOR FOR REPAIR.