N585UA

Part: CHARGER — FAULTY (APU) · airframe 67,352 hrs · 23,707 cycles

APU WILL NOT START, TWO ATTEMPTS. APU CUTS OUT AT ABOUT 3%. NO VOLTAGE SHOWN ON BATTERY SFOMM, ECB SHOWED AUTO SHUTDOWN. BATTERY SHOWED NO VOLTAGE ON START ATTEMPT. ONLY 17V WHILE CHARGING, BATTERY PCN 563-3040.

Part: SPRING — BROKEN (R4 DOOR) · airframe 67,346 hrs · 23,706 cycles

ON R4 DOOR FOUND UPPER HINGE COVER SPRING & RETAINER BROKEN. IAW LM7806 & PTT 3462002. R & R COVER SPRING & RETAINER IAW AMM, OPERATIONS CHECKED NORMAL.

Part: LINE — UNSECURE (L2 DOOR) · airframe 66,551 hrs · 23,442 cycles

SLIDE LANYARD 2L DISLODGED. SECURED STATIC LINE.

Part: OVEN — ODOR (GALLEY) · airframe 66,481 hrs · 23,421 cycles

FIRST CLASS OVEN ON LT SIDE PRODUCED SMOKE AFTER A FEW MINUTES OF USE. INOPERATIVE 1ST CLASS OVEN NR 1 PRECAUTIONARY, FOUND SMALL AMOUNT OF BURNT SPILLED FOOD ON OVEN INSERT. OVEN STILL PRODUCED SMELL WITH INSERT REMOVED. OVEN NR 1 IS NOT TO BE USED. PARTS: 028-9005 8055-01-0000 - OVEN LOB: N

Part: LANYARD — TANGLED (L2 DOOR GIRT BAR) · airframe 66,342 hrs · 23,375 cycles

L2 DOOR WILL NOT ARM. UNTANGLED ESCAPE SLIDE LANYARD ON GIRT BAR.

Part: STRINGER FITTING — GOUGED (BS 728) · airframe 66,144 hrs · 23,316 cycles

MAIN CABIN L2 DOOR AFT DOOR FRAME, INSIDE STRINGER FITTING, GOUGED AT BS 728 AND STR 16L. REMOVED THE L2 DOOR STRINGER FITTING AND FABRICATED A NEW REPLACEMENT FITTING AND INSTALLED IAW ECRA 5311-01623. MAJOR REPAIR

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 66,144 hrs · 23,316 cycles

RT INBD T/E FLAP DELAMINATED ALONG THE EDGEBAND. 12 INCHES INBD FROM THE BODY. AREA REMOVED OF MOISTURE, R & R RT AFT T/E FLAP IAW MM. RIG AND OPS CHECKED GOOD.

Part: SKIN — DAMAGED (FWD CARGO DOOR) · airframe 66,144 hrs · 23,316 cycles

DAMAGE TO FWD CARGO DOOR SKIN 8 INCHES FROM BOTTOM OF DOOR CENTER OF THE DOOR. TRIMMED OUT AND INSTALLED REPAIR DOUBLER ON FWD CARGO DOOR EXTERNAL SKIN IAW SRM 52-30-01 FIG 201 REPAIR 4. MAJOR REPAIR.

Part: STRUCTURE — DAMAGED (BS 518) · airframe 66,144 hrs · 23,316 cycles

LIGHTNING STRIKE BS 518 BETWEEN STR 7L AND 8L.

Part: FLOOR SUPPORT — DAMAGED (BS 1620-1640) · airframe 66,144 hrs · 23,316 cycles

FLOOR SUPPORT DAMAGED BS 1620-1640, RBL 11.05, WL 208.10. FABRICATED FLOOR SUPPORT. R & R FLOOR SUPPORT IAW SRM 51-40-02, PARA FIG 12.

Part: WIRE — CHAFED (RT FIRE LOOP) · airframe 65,939 hrs · 23,253 cycles

RT ENGINE FIRE LOOP 2 STATUS MESSAGE ILLUMINATED BRIEFLY. OPENED COWLING, INSPECTED LOOPS & CONNECTING WIRES FOR DISCREPANCIES. FOUND WIRE BEGINNING TO CHAFE UNDER RT FAN COWL. REPAIR AND REPOSITIONED WIRE. FIRE TEST GOOD & NO FAULT MESSAGE.

Part: STRAP — UNSECURE (L2 DOOR SLIDE) · airframe 65,916 hrs · 23,245 cycles

L2 DOOR SLIDE PACK STRAP NOT SECURED. RESECURED D-RING STRAP.

Part: LANYARD — UNSECURE (L2 DOOR SLIDE) · airframe 65,917 hrs · 23,246 cycles

L2 DOOR SLIDE LANYARD LOOSE. STOWED LANYARD. OK FOR SERVICE.

Part: SLIDE — UNSECURE (L2 DOOR) · airframe 65,900 hrs · 23,240 cycles

CORD HANGING DOWN FROM L2 DOOR SLIDE. REPACKED SLIDE CORD.

Part: FITTING — LOOSE (SEAT ROW 23) · airframe 65,641 hrs · 23,158 cycles

ROW 23 FWD INBD SEAT ATTACH FITTING IS LOOSE. TIGHTENED FITTING IAW AMM.

Part: OXYGEN MASK — FAULTY (COCKPIT) · airframe 65,632 hrs · 23,156 cycles

OXYGEN MASK DEFECTIVE. DIAPHRAM STICKING. NEED STRONG INHALE TO GET O2 TO FLOW. SWAPPED FO'S O2 MASK WITH OBSERVERS POSITION. NEW MASK OPS TEST OK IAW AMM.

Part: LAMP — INOPERATIVE (L2 DOOR SLIDE) · airframe 65,253 hrs · 23,038 cycles

L2 DOOR EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED LAMPS, CHECKED GOOD.

Part: ENGINE — VIBRATION (NR 1) · airframe 65,253 hrs · 23,038 cycles

NR 1 ENGINE VIBRATION. LEFT ENGINE VIBRATION INDICATES 1.2. VIBRATION CAN BE FELT AND HEARD THROUGH ACFT. IT DOES NOT VARY WITH THROTTLES, ACFT SPEED OR ALTITUDE. TROUBLESHOT PER FIM 71-05-0 FIG 107. REPLACED NR 1 ENGINE PER MM TOD 71-00-02 CON FIG 1.

Part: LIGHT — LOOSE (CABIN) · airframe 65,225 hrs · 23,031 cycles

EMERGENCY LIGHT LOOSE ROW 22. SECURED LIGHT.

Part: GROUND STUD — LOOSE (EMERGENCY LIGHT) · airframe 65,027 hrs · 22,969 cycles

DURING NR 2 SERVICE CHECK, FOUND EMERGENCY LIGHT OUTSIDE L1 DOOR INOPERATIVE. REPLACED LAMPS AND REPLACED CHARGER ASSY, NO HELP. FOUND BAD LIGHT ASSEMBLY AND BAD GROUND FROM ASSEMBLY. FOUND LOOSE GROUND STUD NUT AT GD499 REF WDM 33-51-12, SECURED GROUND STUD NUT. LIGHT CHECKED GOOD.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 63,821 hrs · 22,572 cycles

DAMAGE FOUND TO FORWARD CARGO DOOR SKIN ABOUT 8 INCHES UP FROM BOTTOM CENTER DOOR. DEFECTION OF ABOUT 3 INCHES IN CIRCUMFERENCE WITH A GOUGE AT THE CENTER. .031 IN DEPTH .031 IN WIDTH AND .093 LENGTH. REPAIRED IAW SRM 52-30-01 AND ONLY SMALL SMOOTH DENT REMAINS WITH NO CREASE. NO CRACKS NOTED.

Part: LANYARD — UNSECURE (L2 DOOR) · airframe 63,538 hrs · 22,466 cycles

STRAP HANGING FROM SLIDE PACK AT 2L. FOUND LANYARD PULLED OUT OF POUCH RE-INSTALLED LANYARD.

Part: LIGHT — FAULTY (EVAC SLIDE) · airframe 63,521 hrs · 22,459 cycles

DOOR LEFT SLIDE LIGHT DOES NOT ILLUMINATE.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 63,409 hrs · 22,421 cycles

DOOR 1R NO SLIDE ARM LIGHT. LIGHT NOT WORKING DOOR CLOSED AND ARMED MEL COMPLIED WITH. RELAMPED, CHECKED OKAY.

Part: GIRT BAR — OBSTRUCTED (PAX DOOR) · airframe 62,985 hrs · 22,290 cycles

PASSENGER DOOR EVACUATION SLIDE ARM LEVER DIFFICULT TO MOVE. ACCOMPLISHED STATIC LINE EXCESS LENGTH ADJUSTMENT PER MM 25-66-01-400A. FOUND STATIC LINE WAS RUBBING ON GIRT BAR CAM LOCK. SLIDE ARMS AND DISARMS OK NOW. ARM LIGHT CORRECT. SLIDE PRESSURE CORRECT.

Part: SWITCH — DIRTY (EVAC SIGNAL HORN) · airframe 61,990 hrs · 21,962 cycles

CREW REPORTS EMERGENCY EVAC SIGNAL HORN WENT OFF SEVERAL TIMES DURING CLIMB. CLEANED PRESS TO TEST SWITCH AND ACCOMPLISHED PER MM, SYSTEM OPS CHECKED OKAY.

Part: SEAL — LEAKING (L2 DOOR) · airframe 61,735 hrs · 21,882 cycles

INBOUND CREW REPORTS DOOR 2L HAS LOUD SQUEAL. THIS LEAK IS BECOMING CHRONIC AND PREVIOUS LM3088 CALLOUT REQUEST DOOR SEAL RPL. APPLIED REN TO DOOR SEAL AREAS THAT LEAKED. PRESSURIZED AIRCRAFT NO LEAKS AND OR SQUEALS.

Part: ROD — OUT OF POSITION (PAX DOOR) · airframe 61,409 hrs · 21,755 cycles

PASSENGER ENTRY-SERVICE DOORS L CTR NOISE FROM AIR LEAK (PROG TEXT: ACCOMPLISH CHRONIC REVIEW). FOUND UPPER AND LOWER GATE DIAPHRAGM SEAL NYLON RODS OUT OF RETAINERS. RE-INSTALLED RODS SEALS GATE CORNERS AND PRESSURIZED AND LEAKED CHECK, OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,412 hrs · 21,756 cycles

RIGHT WW RED UNSAFE LIGHT INOP. RELAMPED, NO HELP. VERIFIED NO POWER AT SOCKET SWITCH NOT AT SEAMM. REPLACED LAMP AND SECURED WIRING.

Part: WIRE — BROKEN (R1 DOOR SLIDE) · airframe 61,281 hrs · 21,708 cycles

SLIDE LIGHT EXTINGUISHED IN CRUISE DOOR 1R. ALL OTHER ARMING INDICATIONS NORMAL. REPLACED LIGHT ASSSY, NO HELP. SUSPECT GIRT BAR PROXIMITY SWITCHES. FOUND WIRE W3682-B-PA BROKEN IN SIDE WALL APPROXIMATELY 24 INCHES DOWN. OBSERVED CORROSION ON BROKEN END. REPLACED R1 DOOR GIRT BAR AND LIGHT L404 REF WDM. REPLACED R1 DOOR GIRT BAR PROXIMITY SENSOR S10216. SLIDE ARMED LIGHTT COMES ON WHEN ARMED AND OFF WHEN DISARMED, CHECKED OKAY. SPLICED NEW WIRES IN PER GNMM, RAN TO DOOR SWITCH.

Part: ACTUATOR — MALFUNCTIONED (SPOILERS) · airframe 61,112 hrs · 21,647 cycles

SPOILERS EICAS MESSAGE, RTFL CLEANED NR 6 SPOILER PCA CONNECTOR. SWAPPED 1L & 3L SPOILER CONTROL MODULES. OPS CHECKED GOOD IAW MM 27-61-00.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 61,110 hrs · 21,645 cycles

AFT CARGO DOOR FRAME AT BS 1380 AND RBL 20 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED EXISTING CORROSION AND FABRICATED A REPAIR ANGLE, AND PLUGGED 2 EACH OVERSIZED HOLES AND INSTALLED REPAIR PER REO G14321, REV A, AND EC-RA 5310-05424 ON NON ROUTINE 28367. PER EC-RA 5310-05424, A NEW 8100-9 MUST BE ISSUED, AFTER ANALYSIS WITHIN 24 MONTHS 08562505DEC2011. THIS AIRCRAFT WILL BECOME UNAIRWORTHY UNLESS A NEW FAA FORM 8100-9 IS ISSUED ON OR BEFORE 05DEC2013.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,110 hrs · 21,645 cycles

MAIN CABIN FLOORBEAM IS CORRODED AT STA 310.5 RBL 50. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF T-CAP AND FABRICATED A NEW T-CAP SECTION, REPAIR ANGLES AND STRAPS PER REO G14282, REV A AND EC-RA 5310-05423 ON NON ROUTINE 27866. THIS IS A CATEGORY A PERMANENT REPAIR.

Part: SKIN SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,110 hrs · 21,645 cycles

AFT CARGO COMPARTMENT SKIN SPLICE CORRODED BS 1398 - BS 1402, STR 26L - STR 26R. MAJOR REPAIR ACCOMPLISHED. FOUND SKIN SPLICE OUT OF LIMITS PER SRM BETWEEN STRINGERS 28L-29L, 29L-30, AND 30-29R AFTER CORROSION REMOVAL. REMOVED SHEAR TIES AND FABRICATED A NEW SKIN SPLICE ON N-R 28399 PER BACO DWG 146N3300 AND RE-INSTALLED SPLICE, STRAPS, AND SHEAR TIES ON NON ROUTINE 28167. THIS IS A CAT A, 085625 PERMANENT REPAIR.

Part: FITTING — GOUGED (FUSELAGE) · airframe 61,110 hrs · 21,645 cycles

MAIN CABIN L-2 DOOR AFT DOOR FRAME, INSIDE STRINGER FITTING GOUGED AT BS 728 AND STR 16L. MAJOR REPAIR ACCOMPLISHED. REMOVED THE L-2 DOOR STRINGER FITTING, P/N 143N8348-9, AND FABRICATED A NEW REPLACEMENT FITTING AND INSTALLED PER REO G14319, REV C AND EC-RA 5310-05425 ON NON ROUTINE 28282. PER EC-RA, THIS REPAIR IS INTERIM CATEGORY C, AND REQUIRES REPLACEMENT IN 24 MONTHS OR 3, 000C, 085625 WHICHEVER OCCURS FIRST. CURRENT PTC IS 21645C. OSTF IS P2591.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,110 hrs · 21,645 cycles

AFT CABIN EMERGENCY LIGHT MOUNTED ON FLOOR INOP. REMOVED AND REPLACED AFT CABIN EMERGENCY FLOOR LIGHT PER MM AND OPS CHECK GOOD PER MM ON NON ROUTINE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,110 hrs · 21,645 cycles

FLOORBEAM CORRODED STA 324, RBL 45-RBL 62, T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF T-CAP AND FABRICATED A NEW T-CAP, REPAIR ANGLES AND STRAPS AND INSTALLED AT BS 324 AND RBL 45- RBL 62 PER REO G14229, REV B AND UAL EVA 81564 ON NON ROUTINE 27774.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 61,110 hrs · 21,645 cycles

EXTERNAL FUSELAGE SKIN DOUBLER HAS A DENT AT BS 610 BETWEEN STR 16L TO STR 17L. MAJOR REPAIR ACCOMPLISHED. REMOVED PREVIOUS BARN DOOR SKIN SPLICE REPAIR, AND FABRICATED A NEW SKIN SECTION AND SPLICE DOUBLERS AND FILLERS AND INSTALLED PER TIMCO REO G14217, REV A AND UAL EVA 81561 ON NON ROUTINE 27224. TOTAL ADDED WEIGHT FOR THIS REPAIR IS .943 LBS. A NEW CF9 WILL BE GENERATED FOR 24 MONTH DTA PER 085625UAL EVA 81561.

Part: SWITCH — FAULTY (COCKPIT) · airframe 61,110 hrs · 21,645 cycles

RAT SWITCH NEEDS SHEAR WIRE. SAFETIED RAT SWITCH ON FLIGHT STATION OVERHEAD P11 PANEL PER MM ON NON ROUTINE 27209.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,110 hrs · 21,645 cycles

MAIN CABIN SHEAR WEB DOUBLER, AFT PRESSURE DECK PLATE CORRODED AT BS 1680, RBL 58. MAJOR REPAIR ACCOMPLISHED. REMOVED CORRODED DOUBLER BETWEEN RBL 45 TO RBL 52 AND FABRICATED AND INSTALLED A NEW REPAIR DOUBLER PER REO G14236, REV C AND UAL EVA 81559 ON NON ROUTINE 28084.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,110 hrs · 21,645 cycles

FLOORBEAM CORRODED AT BS 365 BL 0 - RBL 62, T-CAP. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF T-CAP AND FABRICATED A NEW REPAIR T-CAP AND SPLICE ANGLES AND INSTALLED PER SRM, REPAIR 3 ON NON ROUTINE 27775.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,110 hrs · 21,645 cycles

MAIN CABIN FLOORBEAM T-CAP HAS EXFOLIATION CORROSION BS 1640, RBL 58.2. MAJOR REPAIR ACCOMPLISHED. T-CAP CORROSION WAS FOUND TO BE OUT OF LIMITS PER SRM. REMOVED DAMAGED SECTION OF FLOORBEAM AND FABRICATED AND INSTALLED REPAIR CHORD, ANGLES, AND STRAPS PER SRM, REPAIR 3 ON NON ROUTINE 28078.

Part: STRINGER SPLICE — GOUGED (FUSELAGE) · airframe 61,110 hrs · 21,645 cycles

MAIN CABIN - FUSELAGE STRINGER SPLICE GOUGED IN INNER U-CHANNEL RADIUS'S, UPPER AND LOWER, AT BS 783 AND STRINGER 16L SPLICE. MAJOR REPAIR ACCOMPLISHED: REMOVED STRINGER SPLICE AND ATTACH ANGLE, LOCATED AND DRILLED NEW STRINGER SPLICE, P/N 143N3800U13, AND INSTALLED PER SRM ON NON ROUTINE 28328.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,110 hrs · 21,645 cycles

MAIN CABIN SPLICE IS CORRODED AT BS 365 AND RBL 45. MAJOR REPAIR ACCOMPLISHED. REMOVED SPLICE AND FABRICATED A NEW REPAIR SPLICE AND SHIM PER REO G14273, REV A, AND UAL EVA 81560 AND INSTALLED ON NON ROUTINE 27862.

Part: SKIN — CRACKED (L4 DOOR) · airframe 61,110 hrs · 21,645 cycles

L4 DOOR INTERNAL SKIN HAS A CRACK 9 INCHES FROM FWD EDGE OF DOOR. MAJOR REPAIR ACCOMPLISHED. BLENDED OUT DAMAGE PER SRM AND FOUND TO BE OUT OF LIMITS. FORMED REPAIR DOUBLER AND SHIM AND INSTALLED PER SRM ON NON ROUTINE 2 7569.

Part: GATE — CORRODED (L2 DOOR LOWER) · corrosion level 2 · airframe 61,110 hrs · 21,645 cycles

L2 DOOR LOWER GATE IS CORRODED ON BOTTOM EDGE. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION BY BEAD BLASTING PER SM-09-13-25-10-JD AND ACCOMPLISHED ALL FINAL CORROSION PREVENTATIVE TREATEMENT, PRIME AND TOP COATED ON NON ROUTINE 27578.

Part: GATE — CRACKED (L2 DOOR LOWER) · airframe 61,110 hrs · 21,645 cycles

MAIN CABIN L2 DOOR LOWER GATE IS CRACKED. REMOVED LOWER GATE & SEAL RETAINERS, WELD REPAIRED GATE AND REINSTALLED ON NON ROUTINE 27474.

Part: SKIN — CRACKED (R4 DOOR) · airframe 61,110 hrs · 21,645 cycles

R4 DOOR INTERNAL SKIN CRACKED JUST ABOVE LOWER HINGE ARM. MAJOR REPAIR ACCOMPLISHED. BLENDED OUT DAMAGE PER SRM, FOUND TO BE OUT OF LIMITS. FORMED REPAIR DOUBLER AND FILLER PER SRM AND ALODINED AND PRIMED AND INSTALLED PER SRM ON ROUTINE 27592.

Part: FLOOR PANEL — DEFECTIVE (CABIN) · airframe 60,650 hrs · 21,460 cycles

FLOOR IS SOFT ROW 12. MAINT TEXT: PULLED UP CARPET SOFT AREA IS A REMNANT PIECE CUT AND LAYED IN WITHOUT SCREWS OR HOLES FOR SCREWS. USED METAL OVER LAY REPAIR PER MM. PANEL NUMBER 754.1822 HAS NO SCREWS OR HOLES ON FRONT EDGE. PANEL IS PROPER CONFIG. INF-:PANEL IS 170-4260. PANEL ON AOG J5432. PARTS: 170-4260 15F6866-682.

Part: SOCKET — DIRTY (COCKPIT) · airframe 60,498 hrs · 21,411 cycles

RIGHT MAIN WHEEL WELL UNSAFE LIGHT WILL NOT ILLUMINATE. NO POWER AT LIGHT SOCKET SUSPECT SWITCH S10370, PCN 561-6602, NOT STOCK SEAMM. CLEANED LIGHT SOCKET.

Part: JUMPER — DEFECTIVE (CABIN) · airframe 60,498 hrs · 21,411 cycles

EMERGENCY EXIT FLOOR LIGHT IS INOP FROM SEAT ROW 8 TO SEAT ROW 12. REPLACED JUMPER AT SEAT ROW 12. OPS CHECKS GOOD.

Part: GUARD — MISSING (FIRE PROTECTION) · airframe 60,313 hrs · 21,345 cycles

SECONDARY PLASTIC GUARD MISSING ON CARGO FIRE BOTTLE DISCH SWITCHES. PER EVA-81163 THIS IS AN ACCEPTABLE CONDITION FOR A PERIOD OF 10 DAYS. AS A RESULT, CARGO COMPARTMENT FIRE EXTINGUISHER 2 IS INOP PER MEL 2623A.

Part: STRIP — BUCKLED (CABIN) · airframe 60,012 hrs · 21,238 cycles

EXIT FLOOR PATH STRIP BUCKLED AT 12C. SECURED STRIP.

Part: CONTACT — DIRTY (CARGO BAY) · airframe 59,498 hrs · 21,050 cycles

AFT CARGO FIRE NO TEST LIGHT WORKS. REPLACED LOGIC CARD PER MM, NO HELP. CLEANED CONTACTS ON LIGHTED SWITCH, OPS NORMAL.

Part: FEEDER CABLE — DEFECTIVE (CABIN) · airframe 59,379 hrs · 20,999 cycles

EEL LIGHTING INOP, INTERMITTENT BETWEEN MID LAV AND OVERWING EXIT. REPLACED EEL LIGHT FEEDER CABLE AT OVERWING AREA. OPS TESTED NORMAL.

Part: CABLE — DEFECTIVE (CABIN) · airframe 59,351 hrs · 20,987 cycles

BEFORE CABIN CREW PERFORMED CABIN MOD CHECK, FOUND EEL LIGHT STRIP NOT WORKING IN FRONT OF THE FWD AFT LAVATORY DOOR. DEFERRED PER MEL. NEED LIGHTING CABLE ASSY. (560-0812). NO PARTS SMF. REPAIRED EEL LIGHTS IN FRONT OF FWD AFT LAV. OPS CHKS GOOD.

Part: SENSOR — FAULTY (R1 DOOR SLIDE) · airframe 59,205 hrs · 20,938 cycles

DOOR 1R SLIDE ARMED LIGHT DOES NOT ILLUMINATE. SLIDE ARM LIGHT INOPERATIVE. CONFIRMED GIRT BAR ENGAGEMENT NORMAL. LIGHT IS OK, SUSPECT ONE OF THE SENSORS TO BE AT FAULT.

Part: SENSOR — FAULTED (R1 DOOR SLIDE) · airframe 58,981 hrs · 20,856 cycles

THE SLIDE ARMED LIGHT AT DOOR 1R IS NOT ON WHEN DOOR IS ARMED. CLEANED LED CONTACTS IN LENS CAP. SLIDE ARM LT CK'S NORMAL. LIGHT NOW WORKING NORMAL AFTER SLIDE ARMED, INTERMITTANT OPERATION. REPLACED LIGHT ASSY WITH BASE. CONFIRMED LIGHT WIRED CORRECTLY, NO HELP. SUSPECT PROX SENSORS FOR GIRT BAR OR SHORT IN WIRE. . OPERATED DOOR ARMING 30 CYCLES, OPS CHK NORMAL. INSPECTED GIRT BAR AND SENSORS, NO DEFECTS FOUND. CONFIRMED WITH INBOUND CREW DOOR OPERATED NORMALLY.

Part: LIGHT — DAMAGED (CABIN) · airframe 58,522 hrs · 20,687 cycles

EMERGENCY LIGHT STRIP DAMAGED AT 13A. REPLACED DAMAGED SECTION OF EMERGENCY LIGHT STRIP. CHECKED OK.

Part: SKIN — DENTED (BS 1660) · airframe 58,063 hrs · 20,517 cycles

MAJOR REPAIR. BS 1660 SKIN DENT. THIS CF CAN BE CLEARED. NEW 8100-9 IAW 14CFR26.43(D) AND 25.571 RECD 17NOV09. EC 50-5330-002SB & EQ 7728 TO MONITOR.

Part: LAMP — INOPERATIVE (FIRE HANDLE) · airframe 57,679 hrs · 20,376 cycles

L ENG FIRE HANDLE LIGHT OUT. RELAMPED FUEL SHUT-OFF HANDLE, TESTS OKAY.

Part: SKIN PANEL — DAMAGED (NR 6 SLAT) · airframe 57,010 hrs · 20,138 cycles

FOUND ON ARRIVAL, RT WING NR 6 L/E SLAT UPPER PANEL HAS DAMAGE & DELAMINATION. HOLE DIMENSION IS APPROX 17 INCHES LONG BY 8 INCHES WIDE. AREA OF DELAMINATION IS APPROX 30 INCHES LONG BY 12 INCHES WIDE. INSTALLED NR 6 L/E SLAT & COMPLETED STEPS THRU 3F(12)(G) OF MM. RIGGED NR 6 SLAT GAPS AT INTERMEDIATE AND RETRACTED POS. COMPLETED RIGGING AND INSTALLATION OF NR 6 SLAT, OPS CHECKS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,131 hrs · 19,804 cycles

EVACUATION LIGHT AT RT 4 DOOR INOPERATIVE. RELAMPED.

Part: CONTACT — OUT OF ADJUST (EMERGENCY LIGHT) · airframe 56,131 hrs · 19,804 cycles

EXT EVAC LIGHT AT L4 DOOR INOPERATIVE. ADJUSTED GROUND CONTACT ON LIGHT ASSY. OPS NORMAL.

Part: SKIN — DENTED (LT WING) · airframe 56,111 hrs · 19,797 cycles

DENT ON UNDERSIDE OF LEADING EDGE LT WING BET FUSE & PYL. POSSIBLE BIRD STRIKE. MARKED AND TAPED PER SRM, 7.5L X 3.25W DEPTH 16TH OF AN INCH. MEETS UNDER 10 PERCENT LIMIT. REPAIRED DENT.

Part: LANYARD — FAULTY (R1 DOOR SLIDE) · airframe 56,100 hrs · 19,793 cycles

UNABLE TO ARM DOOR 1R. RESTOWED SLIDE LANYARD.

Part: LIGHT — FAULTY (CABIN) · airframe 53,651 hrs · 18,853 cycles

EEL LIGHT AT 'S' LAV PARTIALLY LIT. REPLACED 'S' LAV LIGHT AND OPS CHECK GOOD.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 53,651 hrs · 18,853 cycles

EEL FLOOR LIGHT AT SEAT ROWS 9 THROUGH 12 INOP. RESEATED CONNECTION AT FEEDER FOR EEL FLOOR LIGHTS, ROW 9-12. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 53,327 hrs · 18,722 cycles

THE 4L DOOR EMERGENCY EVACUATION EXTERIOR FUSE LIGHT INOP. REPLACED LAMP, OPS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,327 hrs · 18,722 cycles

FOUND EMERGENCY LIGHT SHORT STRIP IN FRONT FWD AFT LAV NOT WORKING. REPLACED SHORT EMERGENCY LIGHT ASSY IN FRONT OF AFT LAV.

Part: LIGHT — DAMAGED (CABIN) · airframe 53,279 hrs · 18,702 cycles

SECONDARY BARRIER DIFFICULT TO LATCH EXIT PATH LIGHTS INTERFERING. REPAIRED EXIT PATH LIGHTING STRIP. CHECKS OKAY.

Part: SLIDE — UNSERVICEABLE (L4 DOOR)

LOW BOTTLE, IN RED BAND. NO LEAK FOUND. BOTTLE WENT OUT IN LOWER GREEN "GO" BAND. TOP OFF AND REWEIGH.

Part: LANYARD — OUT OF POSITION (EVAC SLIDE) · airframe 52,072 hrs · 18,205 cycles

DOOR 1R SLIDE WILL NOT ARM. SECURED LANYARD IN PROPER POSITION. ARMED DOOR SEVERAL TIMES, CKS GOOD.

Part: SKIN — DENTED (BS 1660) · airframe 51,964 hrs · 18,164 cycles

EXTERNAL FUSELAGE SKIN DENTED AT STA 1660 AND BETWEEN STR 26L-27L AT LAV SERVICE DOOR CUTOUT. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE. FABRICATED AND INSTALLED FILLER, DOUBLER AND TRIPLER.

Part: SKIN — DENTED (FUSELAGE) · airframe 51,964 hrs · 18,164 cycles

EXTERNAL FUSELAGE STA 1680 BETWEEN STR 27L AND 28L DENTED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER REPAIR.

Part: LANYARD — OUT OF POSITION (R1 DOOR) · airframe 51,685 hrs · 18,065 cycles

DOOR 1R DIFFICULT TO ARM -"ARMED" LIGHT STAYS ON. PROPERLY STOWED LANYARD THAT WAS TANGLED IN GIRT BAR. OPERATED ARMING HANDLE SEVERAL TIMES, ALL OK.

Part: DOOR — OBSTRUCTED (R3 DOOR) · airframe 51,640 hrs · 18,047 cycles

DOOR 3R WILL NOT ARM. CLEARED D RING STRAP FROM DOOR SILL, ARMS OK.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 51,601 hrs · 18,031 cycles

HIGH INTENSITY FLASHLIGHT AT DOOR 2, LT SIDE IS INOP, PER FLIGHT ATTENDENT. REPLACED AND CHECKED.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 50,383 hrs · 17,599 cycles

THE 1R DOOR WILL NOT ARM. DEBRIS UNDER GIRT BAR. CLEANED DEBRIS UNDER GIRT BAR. DOOR ARMS/DISARMS NORMALLY.

Part: LIGHT — INOPERATIVE (R4 DOOR) · airframe 50,059 hrs · 17,492 cycles

DOOR NR 4R SLIDE LIGHT INOP. RELAMPED. OPS CHECKED OK.

Part: DOOR — OBSTRUCTED (L1) · airframe 50,016 hrs · 17,474 cycles

DOOR 1L DOES NOT DISARM. FOUND FOD UNDER DOOR. REMOVED SCREW FROM UNDER AFT GATE AREA, DISARMS NORMALLY.

Part: LANYARD — OUT OF POSITION (DOOR 1R GIRT BAR) · airframe 49,721 hrs · 17,371 cycles

CANNOT GET DOOR 1R TO ARM. FOUND LANYARD HANGING DOWN, CAUSING INTERFERENCE. RESTOWED LANYARD, OPS CHECKED GOOD.

Part: LANYARD — OUT OF POSITION (EVAC SLIDE) · airframe 49,624 hrs · 17,336 cycles

THE 1R SLIDE HAS LANYARD HANGING DOWN. STOWED LANYARD.

Part: LANYARD — LOOSE (R1 DOOR SLIDE) · airframe 49,339 hrs · 17,235 cycles

DOOR 1R SLIDE PACK HAS HANGING LANYARD. SECURED LOOSE SLIDE PACK LANYARD.

Part: LANYARD — OUT OF POSITION (R1 DOOR SLIDE) · airframe 48,789 hrs · 17,050 cycles

DOOR 1R UNABLE TO ARM SLIDE. FOUND GIRT BAR LANYARD INTERFERENCE. REPOSITIONED GIRT BAR LANYARD. DOOR FUNCTIONS NORMALLY.

Part: CABLE — FAULTY (CABIN) · airframe 48,629 hrs · 16,994 cycles

DURING ENGINE START ELECTRICAL POWER WAS LOST AND FLT ATTENDANT REPORTED THAT SEVERAL EEL FLOOR STRIPS WERE NOT ILLUMINATED WHEN EMERGENCY LIGHTS CAME ON. AFTER POWER UP STRIPS NEAR ROWS 9-13 AND 24-31 WERE INOP. REPLACED BROKEN POWER EXT AT ROW 14 AND SYSTEM CHECKS NORMALLY,

Part: GIRT BAR — FAULTY (R1 DOOR) · airframe 48,520 hrs · 16,951 cycles

DOOR 1R WON'T DISARM AND SLIDE LT IS ON.

Part: LIGHT — FAULTY (3R DOOR SLIDE) · airframe 48,419 hrs · 16,910 cycles

SLIDE LIGHT AT 3R NOT LIT UP.

Part: FIRE LOOP — FAULTY (NR 2) · airframe 48,107 hrs · 16,800 cycles

STATUS MSG R ENG FIRE LOOP 2.

Part: LANYARD — OUT OF POSITION (R1 DOOR SLIDE) · airframe 47,343 hrs · 16,521 cycles

DOOR 1R WILL NOT ARM.

Part: WIRE — MISINSTALLED (DOOR 1R SLIDE) · airframe 47,100 hrs · 16,435 cycles

DOOR 1R SLIDE LIGHT REMAINS ON WHEN DOOR IS DISARMED. [08-07-07] WIRED LIGHT ASSY CORRECTLY. LIGHT OPERATES NORMALLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,790 hrs · 16,320 cycles

EMERGENCY EXIT SLIDE LIGHT INOP AT DOOR 4R. [SUP 06-06-07] RELAMPED.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 46,793 hrs · 16,322 cycles

SMOKE AND FUMES IN THE COCKPIT. [06-14-07] ON PREFLT CHECK WHEN FLT CREWS TURNED ON WINDOW HEAT, ACRID ODOR NOTICED. FOUND 1L WINDOW POWER TERMINAL BURNED & ASSOCIATED TERMINAL CAP MELTED. NOTICED CAPT'S FLOOD LIGHTS WERE INOP, WHEN FLOOD LIGHT RHEOSTAT TURNED TO FULL BRIGHT, ODOR REAPPEARED. ISOLATED FAULT DOWN TO CAPTAINS & CENTER PANEL FLOODLIGHT CONTROL UNIT, WHICH IS LOCATED BEHIND PANEL NEAR RUDDER. RESET LIGHT BREAKERS, LIGHT WORKED NORMAL & NO SIGN OF SMOKE OR ODOR WITH C.BREAKER FOR CAPTS NR 1 FRONT WINDOW HEAT OPEN AND DEFFERED. REPLACED WINDOW AND WINDOW HEAT CONTROLLER, PRECAUTIONARY.

Part: JUMPER — DISCONNECTED (EMERGENCY LIGHTS) · airframe 46,790 hrs · 16,320 cycles

FLOOR MOUNTED ESCAPE PATH LIGHTING INOP FROM ROW 9 TO 13. RECONNECTED JUMPER CABLE.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 46,297 hrs · 16,138 cycles

EMERGENCY LIGHTS INOP ROW 9 THRU ROW 13. FOUND POWER STRIP DISCONNECTED. RECONNECTED STRIP AND LIGHTS ILLUMINATE CORRECTLY.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 45,451 hrs · 15,826 cycles

PUNCTURE ON LEFT SIDE OF FUSELAGE 5.5 FT FWD OF DOOR 2L APPROX 6 INCHES ABOVE FLOORLINE. FULL DAMAGE MEASURES 3.5 INCHES WITH A PUNCTURE LIMIT OF ABOUT 2.75 INCHES. MAJOR REPAIR ACCOMPLISHED. THE SKIN WAS FOUND PUNCTURED BUT NO INTERNAL STRUCTURE WAS DAMAGED. A PRE-EXISTING REPAIR WAS LOCATED AFT OF DENT. CUTOUT DAMAGE AND FABRICATED REPAIR DOUBLER. ATTACHED STRUCTURAL ANALYSIS VERIFIED THAT STATIC STRENGTH OF SKIN IS RESTORED.

Part: LANYARD — DISLODGED (3R DOOR SLIDE) · airframe 44,660 hrs · 15,507 cycles

DOOR 3R SLIDE LANYARD FALLING OUT. MORE THAN ALLOWABLE SLACK TO LANYARD WITHIN ITS POUCH COULD HAVE INADVERTENTLY ALLOWED IT GET SNAGGED BY A GALLEY SERVICING EQUIPMENT. STOWED LANYARD TO SLIDE & GIRT BAR.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 43,834 hrs · 15,186 cycles

EEL LIGHTS INOP ROWS 9-16. REPLACED LEAD-IN CABLE FROM INVERTER TO EEL TRACK CABLE.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 43,834 hrs · 15,186 cycles

EEL LIGHTS INOP ROWS 9-16. REPLACED LEAD-IN CABLE FROM INVERTER TO EEL TRACK CABLE.

Part: LANYARD — TANGLED (ESCAPE SLIDE) · airframe 43,295 hrs · 14,986 cycles

NR 4 RT MED SLIDE STATIC LINE AND D-RING L ANYARD TANGLED. WRAPPED AROUND GIRT BAR.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,532 hrs · 13,651 cycles

EXTERNAL FUSELAGE SKIN AT BS 758, STRINGER 16L IS DENTED. REPAIR DOUBLER AND TRIPLER WERE INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,532 hrs · 13,651 cycles

CABIN FLOORBEAM CAP CORRODED AT BS 324, RBL 60-64 UPPER SURFACE. FLOORBEAM WAS REPAIRED USING REPAIR ANGLES AND STRAP.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,532 hrs · 13,651 cycles

AFT PIT STA 1540 RIGHT SIDE FRAME HAS DENT ABOVE STR 26R, UPPER FLANGE. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,532 hrs · 13,651 cycles

FWD PIT STA 540 LEFT SIDE, FRAME HAS DENT ABOVE STR 25L UPPER FLANGE INTO RADIUS. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR.

Part: FRAME — DENTED (FUSLAGE) · airframe 39,532 hrs · 13,651 cycles

FWD PIT LEFT SIDE STA 660 FRAME HAS DENT ABOVE STR 25L UPPER FLANGE. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 39,532 hrs · 13,651 cycles

AFT CABIN SHEAR WEB IS CORRODED AT STA 1681 TO 1720 AROUND DRAIN ATTACH FASTENER HOLES RBL 48. CORROSION WAS REMOVED AND A DOUBLER REPAIR INSTALLED.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,532 hrs · 13,651 cycles

FWD PIT RIGHT SIDE STA 660 FRAME HAS DENT BETWEEN STR 25R AND 26R, UPPER FLANGE. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,532 hrs · 13,651 cycles

FRAME AT STA 1440 ABOVE STR 25L DENTED. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,532 hrs · 13,651 cycles

FRAME AT STA 1460 ABOVE STR 25L IS DENTED. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,532 hrs · 13,651 cycles

DENT ON FRAME STA 1580, JUST ABOVE STR 23L, AFT PIT. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,532 hrs · 13,651 cycles

FWD PIT FRAME STA 600 ABOVE STR 25L IS DENTED ON UPPER FLANGE. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,532 hrs · 13,651 cycles

AFT PIT HAS DENTED FRAME, STA 1520, ABOVE STR 25L, DENT IS IN UPPER FWD RADIUS OF UPPER FLANGE. DENT DAMAGE IN FRAME WAS TRIMMED OUT. REPAIR ANGLE WAS INSTALLED.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,532 hrs · 13,651 cycles

FWD PIT LEFT SIDE STA 640 FRAME HAS A DENT ABOVE STR 25L - 26L, UPPER FLANGE. FRAME DENT WAS ROUTED OUT AND DAMAGE REMOVED. INSTALLED ANGLE DOUBLER.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,532 hrs · 13,651 cycles

AFT PIT STA 1480, FRAME HAS DENT ABOVE STR 26L, UPPER FLANGE. DENT DAMAGE WAS TRIMMED OUT AND A DOUBLER ANGLE REPAIR WAS INSTALLED.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,532 hrs · 13,651 cycles

FRAME DENTED STA 1340, ABOVE STR 25R. DAMAGE TO THE FRAME WAS TRIMMED OUT AND A J-ANGLE DOUBLER REPAIR WAS INSTALLED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 39,532 hrs · 13,651 cycles

STRINGER 16L AT BS 758 IS CRACKED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,532 hrs · 13,651 cycles

EXTERNAL FUSELAGE AT BS 274 BETWEEN STR 21L AND 22L HAS IMPROPER FASTENER INSTALLED, COUNTERSUNK CHERRY MAX RIVET. MAJOR REPAIR ACCOMPLISHED. REMOVED BLIND RIVET AND CUT OUT SKIN DAMAGE AND INSTALLED DOUBLER AND FILLER.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,532 hrs · 13,651 cycles

EXTERNAL FUSELAGE SKIN HAS BLIND FASTENER INSTALLED AT APPROX BS 746 BETWEEN STR 24L AND STR 25L. MAJOR REPAIR ACCOMPLISHED. REMOVED BLIND FASTENERS, CUT OUT SKIN DAMAGE AND INSTALLED DOUBLER AND FILLER.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,532 hrs · 13,651 cycles

AFT PIT FLOOR THRESHOLD SUPPORT UPPER AND LOWER SURFACE CORRODED AT STA 1380 TO 1440 RBL 20. DAMAGE CAUSED BY CORROSION IN DOOR CUTOUT AREA AT THE AFT PIT THRESHOLD SUPPORT. PART WAS REPLACED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,532 hrs · 13,651 cycles

AFT CABIN FLOORBEAM IS CORRODED AROUND FASTENERS AT APPROXIMATELY BS 1661 RBL 58. DAMAGE CAUSED BY FLOORBEAM CORROSION IN WET AREAS OF THE CABIN. NEW T-CAP WAS FABRICATED AND INSTALLED TO REPLACE THE DAMAGED PORTION OF THE FLOORBEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,532 hrs · 13,651 cycles

CABIN FLOORBEAM CAP AT FS 365 RBL 33 CORRODED AT EXISTING REPAIR. DAMAGE TO THE FLOOR BEAM CAUSED BY TYPICAL CORROSION. REMOVED THE EXISTING REPAIR AND FABRICATED NEW T-CAP SPLICED INTO EXISTING TEE CAP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,520 hrs · 12,625 cycles

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

Part: HOSE — FAILED (LT HYD SYS)

LANDED DEN UNDER AMBER ALERT DUE TO LOSS OF LEFT HYDRAULIC SYSTEM. RT MLG UPLOCK FLEX HOSE WAS LEAKING AT SWAGED FITTING AT ACTUATOR. REPLACED FLEX HOSE.

Part: SENSOR — FAILED (DOOR 1L)

DOOR 1L AND 3R ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS INOP. *S/D* REPLACED BOTH PROXIMITY SENSORS AT 3R DOOR AND CLEANED PROXIMITY SENSORS AT 1L DOOR, OP CHECK OK.

Part: SWITCH — FAILED (LT SLATS)

LANDED LAX UNDER AMBER ALERT DUE TO LEADING EDGE SLAT ASYMMETRY. *S/D* FAILURE OF ONE OF TWO INBOARD LEADING EDGE SLAT LOSS SWITCHES CAUSED THE EICAS MESSAGE, LIGHT AND SHUTDOWN OF THE LEADING EDGE SLAT SYSTEM. REPLACED BOTH INBOARD SLAT LOSS SWITCHES AND RETURNED AIRCRAFT TO SERVICE WITHOUT FURTHER INCIDENT. FAILURE OF THESE SWITCHES IS A KNOWN 757 INDUSTRY WIDE PROBLEM. UNITED IS CORRECTING THE PROBLEM VIA COA 504070 DURING HEAVY MAINTENANCE VISITS ON ALL EFFECTIVE 757 AIRCRAFT.

Part: DISARM LIGHT — MALFUNCTIONED (DOOR 1L SLIDE)

DOOR 1 LEFT EMERGENCY ESCAPE SLIDE LIGHTS REMAIN ILLUMINATED IN THE ARMED AND DISARMED POSITION. *S/D* CYCLED DOOR ARM HANDLE SEVERAL TIMES AND FOUND LIGHT TO OPERATE NORMAL.

Part: FIRE DETECTOR — FAILED (LT ENGINE)

LEFT ENGINE HAD FIRE LP2 INDICATION. *S/D* FOUND LOWER CORE NUMBER 2 LOOP FAULTED. REPLACED THE DETECTOR ASSEMBLY AND THE SYSTEM OPERATIONALLY CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN)

EEL LIGHTS IN FIRST CLASS AND BY FORWARD COAT CLOSET INOP. REPLACED BATTERY.

Part: TUBE — WORN (SLIDE)

DURING SHOP OVERHAUL OF SLIDE/ RAFT REMOVED FOR TIME EXPIRATION, IT WAS FOUND THAT THE LOWER TUBE RELIEF VALVE HAD WORN A HOLE INTO THE LOWER TUBE. THE HOLE WAS REPAIRED WITH AN OUTSIDE PATCH.

Part: CIRCUIT BREAKER — TRIPPED (E/E BAY)

APU WOULD NOT START AT DEN. FOUND C1391 CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER AND ACCOMPLISHED FIVE NORMAL STARTS, OPERATIONS CHECK NORMAL.

Part: FUEL SHUT VALVE — MALFUNCTIONED (RT ENGINE)

RIGHT ENGINE FLAMED OUT DURING START AND SPAR VALVE AND ENGINE VALVE LIGHTS ILLUMINATED ON PEDESTAL DURING EVENT. *S/D* NO DESCREPENCY NOTED DURING TROUBLESHOOTING. REPLACED PRECAUTIONARY ENGINE FUEL SHUTOFF VALVE ASSEMBLY.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHT AT MID-CABIN INOPERABLE. SLIDE LIGHT ON CARGO DOOR INOPERATIVE. REPLACED BATTERY PACK. OPERATION CHECKS NORMAL.