N575UA

Part: HANDSET — INOPERATIVE (PA SYSTEM) · airframe 68,401 hrs · 25,188 cycles

AFT HANDSET PA INOPERATIVE, REPLACED AFT HANDSET. OPERATIONS CHECKED GOOD. AIRCRAFT OK TO CONTINUE.

Part: LENS — BROKEN (CABIN) · airframe 67,736 hrs · 24,978 cycles

1ST CLASS EMERGENCY EXIT FLOOR LIGHT CLEAR COVER BROKEN & NEEDS TO BE REPLACED. REPLACED EMERGENCY EXIT LIGHT STRIP CLEAR LENS COVER AS REQUIRED.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 67,736 hrs · 24,978 cycles

FLIGHT ATTENDANT REPORTS FLOOR SOFT AT ROW 4. MUSHY FLOOR PANEL FWD CABIN FLOOR. BEGAN REMOVAL OF FLOOR PANEL IN FWD CABIN, ALL SCREWS REMOVED. PANEL LEFT IN PLACE FOR SAFETY. NEW PANEL ON AOG.

Part: CONNECTOR — UNSECURE (FA HANDSET) · airframe 67,666 hrs · 24,959 cycles

4L FLT ATTENDANT HANDSET PHONE DOES NOT RING OR LIGHT UP. RESET CONNECTOR FOR FLT ATTENDANT HANDSET AT 4L HANDSET, OPERATIONS CHECKED GOOD. LIGHT COMES ON & RINGS WHEN CALLED FROM OTHER HANDSET.

Part: CLAMP — UNSECURE (CABIN) · airframe 67,610 hrs · 24,938 cycles

BS 1020 LT SIDE EMERGENCY EXIT LIGHT POWER SUPPLY WIRING CLAMP DISBONDED FROM DUCT ASSEMBLY. SECURED WIRING CLAMP.

Part: BLEED VALVE — FAULTY (APU) · airframe 67,420 hrs · 24,876 cycles

SMELL OF TURBO ENGINE OIL IN CABIN AFTER APU STARTED & PACKS OPERATED AT GATE SFO. APU BLEED VALVE DEF INOPERATIVE IAW MEL PROCEDURE.

Part: SCAVENGE PUMP — FAULTY (ENGINE) · airframe 67,419 hrs · 24,875 cycles

SMOKE IN COCKPIT. AMBER. MAX TEMP 163. EPCS CLEAN PROPLEM WITH OIL SYSTEM. ACCOMPLISHED BLOCK 22 OIL SCAV PUMP REPLACED ON PTT SEQ 4192004. OIL TEMP GOOD ON SCAV PUMP ADJ RUN.

Part: OIL SYSTEM — OVERHEATED (NR 1 ENGINE) · airframe 67,419 hrs · 24,875 cycles

NR 1 ENGINE OIL TEMPERATURE HIGH.

Part: MOTOR — FAULTY (WINDSHIELD WIPER) · airframe 67,414 hrs · 24,873 cycles

FOUND PRESSURE LEAK & SQUEAL AROUND CAPTAINS WINDSHIELD WIPER MOTOR. REPLACED CAPTAINS WIPER MOTOR IAW AMM. LEAK CHECKED AND OPERATIONS CHECKED GOOD.

Part: MOTOR — DEFECTIVE (WINDSHIELD WIPER) · airframe 67,414 hrs · 24,873 cycles

FOUND PRESSURE LEAK & SQUEAL AROUND CAPTAIN`S WINDSHIELD WIPER MOTOR. REPLACED CAPTAIN`S WIPER MOTOR IAW AMM, LEAK CHECKED & OPERATIONS CHECKED GOOD.

Part: HINGE — BROKEN (LAVATORY DOOR) · airframe 67,413 hrs · 24,872 cycles

LAVATORY DOOR AT 2L HINGE BROKEN. DOOR RESECURED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,366 hrs · 24,857 cycles

EMERGENCY LIGHTING FLOOR EMERGENCY EXIT LIGHT STRIP BY DOOR 2L LAVATORY IS INOPERATIVE & PULLED FROM FLOOR. SECURED STRIP BACK IN PLACE & REPLACED COVER.

Part: FASTENER — MISSING (FAIRING) · airframe 67,362 hrs · 24,855 cycles

TWO EACH FASTENERS MISSING FROM RT WING TO BODY FAIRING. REPLACED FASTENER ON RT WING TO BODY PANEL LEADING EDGE. REMAINING MISSING FASTENER IS NOT IN LEADING EDGE OR CORNER OF PANEL. COVERED OPEN HOLE WITH ALUMINUM FOIL TAPE IAW SRM 51-10-05.

Part: CAP — MISSING (CABIN) · airframe 67,335 hrs · 24,845 cycles

FLOOR MOUNTED EMERGENCY EGRESS LIGHTS MISSING ENDCAPS. REPLACED FLOOR MOUNTED EMERGENCY EGRESS LIGHTING END CAPS.

Part: COVER — UNSECURE (EMERGENCY LIGHT) · airframe 67,215 hrs · 24,805 cycles

AFT END OF EMERGENCY LIGHT AFT CABIN COVER COMING OFF. SECURED COVER.

Part: CHARGER — FAULTY (APU) · airframe 66,712 hrs · 24,645 cycles

AUXILIARY POWER UNIT WILL NOT START. PLACARDED AUXILIARY POWER UNIT INOPERATIVE IAW MEL. AUXILIARY POWER UNIT HAS FUEL NO IGNITION. REPLACED BATTERY, VOLTAGE WAS AT 5V & CHARGER NOT CHARGING BATTERY VERY HOT. REPLACED BOTH BATTERY & CHARGER AUXILIARY POWER UNIT HAD NORMAL STARTS & RAN WITH ELECTRIC & PNEUMATIC LOAD FOR 2 HOURS AT GATE.

Part: PLATE — MISSING (DIFFUSER DUCT) · airframe 66,258 hrs · 24,497 cycles

VERY LOUD AIR NOISE FROM AIR DUCTS NEAR DOOR 2. INTERFERES WITH CREW COMMUNICATION. FOUND SECTION OF DIFFUSER DUCT PLATE MISSING, FWD OF PROJECTOR NR 3. INSTALLED MISSING SECTION AND SEALED. NOISE LEVEL CHECKED OKAY.

Part: SKIN — DENTED (FUSELAGE) · airframe 66,196 hrs · 24,479 cycles

LEFT FUSELAGE SKIN HAS A DENT 1INCH WIDE BY 0.029 INCH DEEP AT BS 600, S17L. DENT IS WITHIN LIMITS PER SRM 53-00-01. EDDY CURRENT INSPECTION REVEALED NO CRACKS. AREA REPAIRED PER ECRA 53 30-014531 ORIG,

Part: SKIN — DENTED (FUSELAGE) · airframe 66,196 hrs · 24,479 cycles

EXTERNAL FUSELAGE SKIN HAD SEVERAL DENTS BS 600-640 S14-19L. FOUND OUT OF LIMITS. REPAIRED IAW REO EVA G-09691, REV A IAW EVA 40072.

Part: STIFFENER — DAMAGED (LT WING) · airframe 66,196 hrs · 24,479 cycles

LEFT WING PNEUMATIC DUCT, I/B DUCT CLAMP BRACKET LOCATED BEHIND NR 5 SLAT I/B AUX TRACK, WEARING INTO VERTICAL STIFFENER ON FRONT SPAR. REMOVED AND REPLACED DAMAGED FRONT SPAR STIFFENER IAW SRM 51-40-02 AND DWG 112N2002.

Part: SKIN — DENTED (BS 1620) · airframe 66,196 hrs · 24,479 cycles

FUSELAGE SKIN DENTED AT BS 1620 BELOW S18R. AT C CHECK DENT WAS FOUND TO BE OUT OF LIMITS AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-045 12.

Part: SKIN — DENTED (BS 1622) · airframe 66,196 hrs · 24,479 cycles

EXTERIOR FUSELAGE SKIN DENTED AT S 1622 ABOVE S19R. EVALUATED DENT PER SRM 53-00-01, FIG 101 AND FOUND TO BE WITHIN LIMITS. DENT HFEC INSPECTED, NO CRACKS. INSTALLED INTERIM REPAIR IAW ECRA 5330-04512.

Part: SKIN — DENTED (R2 DOOR) · airframe 66,196 hrs · 24,479 cycles

EXTERIOR BOTTOM RIGHT R2 DOOR DENT AND FRESH PAINT MISSING DOWN TO BARE METAL IN L SHAPE. INSTALLED INTERIM REPAIR AT BS 1617 JUST ABOVE S18R PER ECRA 5330-04512.

Part: SKIN — DENTED (R2 DOOR) · airframe 66,196 hrs · 24,479 cycles

BOTTOM R2 DOOR DENTED AND FRESH PAINT MISSING DOWN TO BARE METAL IN SHAPE L. INSTALLED INTERIM REPAIR AT BS 1617 JUST ABOVE S18R PER ECRA 5330-04512.

Part: FLOOR PANEL — DAMAGED (FWD LAVATORY) · airframe 66,196 hrs · 24,479 cycles

FORWARD LAVATORY FLOOR PANEL IS SOFT AND SPONGY. REPAIRED PER CMM 25-40-23 AND CE-50-25-40-01-JD.

Part: WEDGE — DENTED (NR 6 SLAT) · airframe 29,109 hrs · 10,723 cycles

RIGHT WING NR 6 SLAT HAS A SMALL DENT ON THE T/E WEDGE 10 INCHEC FROM OUTBOARD EDGE. MEASURED DENT AND FOUND IT TO BE WITHIN LIMITS OF SRM 57-43-02 DETAIL 3.

Part: WEDGE — DENTED (NR 8 SLAT) · airframe 29,109 hrs · 10,723 cycles

RIGHT WING NR 8 SLAT HAS A SMALL DENT ON THE T/E WEDGE THREE FEET FROM I/B END. MEASURED DENT AND FOUND IT TO BE WITHIN LIMITS OF SRM 57-43-02 DETAIL 3.

Part: SKIN — DAMAGED (BS 470 S24R) · airframe 66,196 hrs · 24,479 cycles

FUSELAGE SKIN DAMAGED BS 470 S24R. REPAIRED IAW SRM 53-00-01 REPAIR 3 TABLE 5.

Part: SKIN — DENTED (BS 440) · airframe 66,196 hrs · 24,479 cycles

DENT ON RIGHT SIDE OF ACFT, APROX 37 INCHES AFT BS 440 AND 13.75 INCHES FROM BOTTOM OF RVSM. INSTALLED CATEGORY B REPAIR IAW SRM 53-00-01 REPAIR 3.

Part: SKIN — DAMAGED (BS 440) · airframe 66,196 hrs · 24,479 cycles

DIMPLE LOCATED AT RIGHT SIDE OF ACFT AT APPROX 28.75 IN BEHIND BS 440 AND 14.5 INCH BELOW RVS BOTTOM.

Part: DIFFUSER — MISINSTALLED (COCKPIT) · airframe 65,994 hrs · 24,408 cycles

EXCESSIVE NOISE IN FLT DECK AND AT ROWS 10-12. AIRFLOW AND NOISE VERYLOUD IN CABIN ROWS 10-12. MT 21-22-00 FOUND 4-5 DECIBLE DROP WITH RT RECIRC FAN BEING TURNED OFF. FOUND ROW 12 SEATS 12A&F TO BE LOUDER THAN NORMAL FROM SIDEWALL RISERS AND OVERHEAD AREA LOUDER THAN REMAINING AC. CLEANED OVERHEAD DUCT. ACCOMPLISHED COMPLETE DUCT CLEAN OF AIRCRAFT REF MT21-22-00. ALSO FOUND DIFFUSER IN COCKPIT ON OVERHEAD PANEL INSTALLED BACKWARDS. REINSTALLED DIFFUSER, COCKPIT CHECKS WITHIN LIMITS.

Part: UNKNOWN — ODOR (CABIN) · airframe 65,797 hrs · 24,337 cycles

EQUIPMENT FAN FAILED CREATED A ELECTRICAL SMELL IN CABIN. BPCU FAULTS AS FOLLOWS LEFT GEN POWER STS UNDER VOLT TRIP, OPPOSITE BUS OVERLOAD AND GCU 58. REF FIM 24-20-00 PAGE 182K STEP BJ RING OUT WIRES FROM L IDG TO GCU AND IDG TO CB C109 .REF WDM 24-21-11 PG1A SHEET2. NO FAULTS FOUND. REINSTALLED GCU AND CONNECTED CB C901, NEEDS OP CHECK.

Part: SPRING — DAMAGED (LIGHT PANEL) · airframe 65,318 hrs · 24,183 cycles

FLIGHT ATTENDANT REPORTED THE AFT EMERGENCY LIGHT SWITCH SPRING IS SPRUNG. REPLACED EVAC PANEL. OPS CHECK OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,950 hrs · 24,045 cycles

EMERGENCY AISLE PATH LIGHTING STRIP INOP AT SEAT ROW 40C. REMOVED AND REPLACED THE FLOOR AISLE PATH LIGHT STRIP AT ROW 40C, COMPLIED WITH OPERATIONAL CHECK OF AISLE PATH LIGHT SYSTEM AT ROW 40, OP CHECKS OKAY.

Part: LIGHT — INOPERATIVE (SEAT ROW 40C) · airframe 64,945 hrs · 24,043 cycles

EMERGENCY AISLE PATH LIGHT INOPERATIVE AT SEAT ROW 40C. EMERGENCY FLOOR LIGHT END CAP MISSING. INSTALLED END CAP.

Part: INVERTER — FAULTY (ELECTRICAL SYS) · airframe 64,853 hrs · 24,013 cycles

STANDBY POWER TEST GENERATES A 'STBY INVERTER' STATUS MSG. REPLACED STATIC INVERTER AS PER MM, OPS CHECK NORMAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 64,287 hrs · 23,804 cycles

EXT BOTTOM RIGHT DOOR 2R DENT AND FRESH PAINT MISSING DOWN TO BARE METAL. DENT IS FWD OF D4R S17 AND 18 FWD OF STA 1640 AFT OF 1596. 2.25W X .046 DEEP. ACCOMPLISHED VISUAL INSP REF ECRA PART 1. ACCOMPLISHED PART 3. PERMANENT REPAIR REF SRM. PER ECRA 5330-04280.

Part: LANYARD — MISROUTED (L3 DOOR) · airframe 63,325 hrs · 23,479 cycles

DOOR 3 LEFT LANYARD IS ON WRONG SIDE. ROUTED LANYARD CORRECTLY.

Part: BOLT — MISSING (R1 DOOR) · airframe 63,072 hrs · 23,389 cycles

DURING DOOR 1 RT SLIDE CHANGE FOUND GATE ROD END BOLT MISSING. INSTALLED BOLT, WASHERS, BUSHING AND NUT. ADJUSTING NUT WAS TIGHT, NO RIG REQUIRED.

Part: HEAT EXCHANGER — RUPTURED (AC BAY) · airframe 63,041 hrs · 23,377 cycles

PRESSURIZATION LOSS, RTFL LEFT SECONDARY HEAT EXCHANGER HAS RUPTURED. REPLACED RUPTURED HEAT EXCHANGER ON LEFT PACK AND DAMAGED CONDITIONED AIR DUCT & COUPLING BOOT ON RT PACK REPAIR ACCOMPLISHED.

Part: DOOR — OPEN (COCKPIT) · airframe 62,715 hrs · 23,258 cycles

COCKPIT DOOR OPENED ON FINAL APPROACH BY ITSELF. NO PRIOR PROBLEMS DURING FLT. ACCOMPLISHED ELECTRIC STRIKE SYSTEM TEST AS PER MM. NO FAULTS NOTED. SYS CKS NORMAL.

Part: STRUCTURE — CRACKED (R2 DOOR) · airframe 62,110 hrs · 23,048 cycles

FERRY FROM SEA TO SFO FOR REPAIR BY SFO. DOOR 2R UPPER HINGE CUTOUT IS CRACKED APPROXIMATELY 0.28". ACP WALK AROUND OF ACFT. MED 2R. UPPER HINGE CUT OUT CRACK APPROX 9-32 OF AND INCH. MAJOR REPAIR-DOUBLER INSTALLED PER SRM 52-10-02 REPAIR 1 AND UA-EVA-81495 DUE TO EDGE MARGIN ON ONE FASTENER. AMIS ITEM CREATED TO RECEIVE NEW 8100-9 WITHIN 24 MONTHS. RPR ACPD ON OV WU E8863H.

Part: GIRT BAR — DIRTY (L1 DOOR SLIDE) · airframe 61,747 hrs · 22,910 cycles

THE 1R DOOR WILL NOT ARM HANDLE IS JAMMED. FOUND DEBRIS IN GIRT AREA, ARMING OPS CHECKED GOOD.

Part: CONTROL UNIT — FAULTY (CABIN) · airframe 61,708 hrs · 22,893 cycles

DURING FLIGHT, F/A REPORTED THAT DURING TAXI OUT CABIN LOST ALL LIGHTS & VIDEO TWICE-REPEAT. REPLACED BPCU. TAXI AIRCRAFT WITH FLT CREW SETUP OF LT ENGINE ONLY. SYSTEM CHECKS GOOD.

Part: SKIN — DENTED (HORIZ STAB) · airframe 61,364 hrs · 22,766 cycles

LT HORIZONTIAL STAB HAS A DENT ON THE UNDERSIDE, APPROX STA 195 MEASURES 1.25 X 1.25. DENT LOCATED AT STA 193.249- 10.34" AFT OF PANEL L/E- REF SRM 55-10-01 PG 104 DETAIL IV A=1", Y= .022", A OVER Y = 45.45. PANEL LOCATED 2.375" FROM PREVIOUS REPAIR & 1.25" FROM DENT LOCATED AT STA 191.249. ACCOMPLISHED TAP TEST AND HFEC OF AREA. NO DELAM OR CRACKS NOTED. REF NDT MANUAL 51-00-19 PART 6 FOR HFEC. ACCOMPLISH A REPTITIVE INSPECTION VISUAL AND TAP TEST AT EVERY 3SV TO ENSURE NO ADDITONAL DAMAGE PRESENT. ACCOMPLISH PERMANENT REPAIR PER SRM. PER UA-EVA-81190 TO BE REPAIRED BY NEXT A11 CHECK.

Part: SKIN — DAMAGED (HORIZ STAB) · airframe 61,364 hrs · 22,766 cycles

LT HORIZONTIAL STAB HAS A DENT UNDERSIDE, APPROX STA 192 MEASURES 3 X 1.375. FOUND ON ARRIVAL. DENT LOCATED STA 191.249- 8.5\ AFT OF PANEL L/E- REF SRM 55-10-01 PG 104 DETAIL IV A=1.25\, Y=.032\ A OVER Y = 39.06 DENT LOCATED 4.625\ FROM PREVIOUS REPAIR AND 1.25\ FROM DENT AT STA 193.249. ACCOMPLISHED TAP TEST AND HFEC OF AREA. NO DELAM OR CRACKS NOTED. REF NDT MANUAL 51-00-19 PART 6 FOR HFEC. ACCOMPLISH A REPETATIVE INSPECTION VISUAL AND TAP TEST AT EVERY 3SV TO ENSURE NO ADDITIONAL DAMAGE PRESENT. ACCMP PERMANENT REPAIR PER SRM. TO BE REPAIRED BY NEXT A11 CHECK.

Part: SKIN — DENTED (HORIZ STAB) · airframe 61,364 hrs · 22,766 cycles

LT HORIZONTAL STAB HAS A DENT, UNDER SIDE APPROX STA 135. MEASURES 2.25 X 1.375. FOUND ON ARRIVAL. DENT LOCATED AT STA 135.249- 12.25\ AFT OF PANEL L/E- REF SRM 55-10-01 PG 104 DETAIL IV A=1.5\ , Y=.025\ A OVER Y =60. ACCMP'D TAP TEST AND HFEC OF AREA NO DELAM OR CRACKS NOTED REF NDT MANUAL. ACCOMPLISH PERMANENT REPAIR PER SRM BY THE NEXT (A11) CHECK.

Part: SEAL — LEAKING (DOOR HINGE) · airframe 61,335 hrs · 22,752 cycles

CREW REPORTS LOUD NOISE AT DOOR 2R. CHECKED DOOR 2R SEAL & SEALING AREA. FOUND ALL IN SERVICEABLE CONDITION. PRESSURIZED ACFT TO 4.5 PSID. HAD AUDIBLE LEAK AT LOWER HINGE AREA. CHECKED & FOUND VOID IN SEALANT AT FWD O.B. CORNER OF HINGE CAVITY CASTING WHERE IT ATTACHES TO FUSELAGE. CLEANED PASSAGE OF VOID WITH SOLVENT & PIPE CLEANER. INJECTED BMS95 SEALANT INTO OUTER HOLE UNTIL IT WAS VISIBLE FROM INSIDE ACFT. PRESSURIZED AIRCRAFT, NO AUDIBLE LEAK NOTED AT DOOR 2R.

Part: ACM — MALFUNCTIONED (LEFT) · airframe 60,892 hrs · 22,595 cycles

HEAVY VIBRATION AND NOISE IN CRUISE FL 410 WITH RT PACK STANDBY NORMAL AND LT PACK RETURNED TO AUTO. LT ACM WAS REPLACED. RIGHT PACK PUTS OUT VERY LOW AIR FLOW. WILL NOT HOLD CABIN PRESSURE WITH LT PACK OFF. FOUND RT PACK BAY FLEX CONNECTOR PARTIALY DISCONNECTED BETWEEN SUPPLY DUCT TO AIR CHECK VALVE. REPOSITIONED FLEX CONNECTOR & SECURED. LEAK CHECKED CONNECTOR & PACK BAY. PACK OPS NORMAL. DUE TO EXCESSIVE VIBRATION ON 2 CONSECUTIVE FLTS, ACCOMPLISH TEST FLIGHT WITH AN EG CREW AFTER TROUBLESHOOTING AND REPAIRS ARE COMPLETE. NEED A VERIFICATION TEST FLIGHT DUE TO LM 8834. PREVIOUS REPORTED AIRFRAME VIBRATION, LT PACK COULD NOT MAINTAIN CAB PRESSURE, LOUD NOISE IN FLIGHT DECK. VIBRATION AND CYCLING NOTED OVER WING AREA. ACCOMPLISH TEST FLIGHT 9919. OK TO ADD 1 CYCLE PER OPBLM. TEST FLIGHT GOOD.

Part: FLEX HOSE — OUT OF POSITION (ACM) · airframe 60,885 hrs · 22,594 cycles

LOUD NOSE & MAIN GEAR NOISE. STARTED AT 17500 290 KTS. CONSTANT AIRFRAME VIBRATION NOISE. NOISE WENT AWAY WHEN THROTTLE PULLED BACK, IT WAS LIKE A MOTOR GOING ON AND OFF. AIRCRAFT WILL NOT HOLD PRESSURE WITH ONLY LEFT PACK ON. RIGHT PACK HOLDS PRESSURE BY ITSELF. RIGHT PACK PUTS OUT VERY LOW AIR FLOW. WILL NOT HOLD CABIN PRESSURE WITH LEFT PACK OFF. FOUND RT PACK BAY FLEX CONNECTOR PARTIALLY DISCONNECTED BETWEEN SUPPLY DUCT TO COND AIR CHECK VALVE (RT PACK SUPPLY AIR TO MIX MANIFOLD). REPOSITIONED FLEX CONNECTOR AND SECURED. LEAK CHECKED CONNECTOR AND PACK BAY, GOOD. PACK OPERATION NORMAL. TEST FLT, NO NOISE FOUND.

Part: MODULE — FAULTY (COCKPIT) · airframe 60,880 hrs · 22,592 cycles

GEAR DISAGREE LIGHT ILLUM. DEBRIEFED CREW AND NOTED GEAR AMBER LIGHT ILLUMINATED WITH ASSOCIATED GEAR DISAGREE EICAS MSG. THIS HAPPENS 3X DURING GEAR CYCLES ON FINAL AND GO-AROUND. PSEU SHOWS FAULTS 421,422 ,423,424. FIM SHOWS REPLACE LANDING GEAR LEVER ASSY M937 AVAIL SFO 170-0698. REPLACED LANDING GEAR LEVER MODULE M937, PER MM. SWUNG GEAR PER MM, SYSTEM CKS GOOD.

Part: SILL — CORRODED (FUSELAGE) · airframe 60,744 hrs · 22,541 cycles

CORROSION FOUND ON OUTER CHORD OF LOWER MAIN SILL OF THE AFT CARGO DOOR BS 1440 TO BS 1460 AT STRINGER 27R. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE & ACP NDT OF EXISTING FASTENER HOLES COMMON TO THE CHORD. REF NDT MANUAL 51-00-16 PART 6. NO DEFECTS. FABRICATED & INSTALLED REPAIR ANGLE NEAR BS 1450 REF EA PD57-53-125.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 60,742 hrs · 22,540 cycles

AFT CARGO PIT PRODUCTION SPLICE CORRODED AT STR 29L AT STA 1465, SPLICE GOES FROM STA 1453 TO STA 1465. MAJOR REPAIR ACCOMPLISHED: REMOVED CORRODED STRINGER PRODUCTION SPLICE. FABRICATED & INSTALLED REPLACEMENT STRINGER SPLICE BETWEEN BS 1453 -1465 AT STRINGER 29L REF SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,742 hrs · 22,540 cycles

CORROSION ON FRAME AT STA 1420, BETWEEN S-30 AND STR 28L. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION FROM THE FRAME. ACP NDT OF FASTENER HOLES & BLENDED AREA REF NDT MANUAL. FABRICATED & INSTALLED REPAIR DOUBLER, ATTACH ANGLE, REPAIR STRINGER CLIP AND SHEAR TIE REF EA PD57-53-123 & UA EVA-80835.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 60,742 hrs · 22,540 cycles

MED R4 CREASE BEAM (HOCKEY STICK) CRACKED AT STA 1681 RBL. REMOVED DAMAGE AT BS1683 & BS 1639. ACP NDT OF CHORD & FASTENER HOLES REF NDT MANUAL, NO DEFECTS. FABRICATED & INSTALLED DOUBLER REPAIR AT BS 1683 & ANGLE REPAIR AT BS 1639 REF EA PD57- 53-118 & UA-EA 80842.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 60,742 hrs · 22,540 cycles

CORROSION AT STA 324 PREVIOUS REPAIR RBL 52 - 70 CORR. MAJOR REPAIR ACCOMPLISHED: REPAIRED PER DETAILED INSTRUCTIONS ON EA PD57-53-116 AND UAL EVA 80818 WITHOUT DEVIATION.

Part: RAM AIR TURB — DEFECTIVE (HYDRAULIC SYS) · airframe 60,742 hrs · 22,540 cycles

RAT FAILED OPS CHECK ON TC 5R29I3046, FOUND FILTERS CONTAMINATED, FILTER REPLACEMENT REQUIRED. REMOVED AND INSTALLED NEW RAT HYDRAULIC PUMP IAW B757 MM, OPS CHECK OKAY. REMOVED AND REPLACED NEW FILTER ELEMENT UNTO RAM AIR TURBINE PUMP, LEAK CHECK OKAY IAW B757 MM.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 60,742 hrs · 22,540 cycles

AFT CARGO PIT FLOOR PAN JUST INBOARD OF CARGO DOOR HAS SEVERAL AREAS OF EROSION AT FLOOR PAN EDGES AND THROUGH OUT PAN. STARTED FLOOR PANEL REMOVAL FOR CORROSION EVALUATION. REMOVED PRODUCTION SPLICE AND STRINGER CLIP IAW B757 SRM. NEW SPLICE HEAT TREATED LOCATED AND DRILLED PER SRM. TREATED AND PRIMED IAW 757 SRM. INSTALLED PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,742 hrs · 22,540 cycles

CORROSION AT STA 563 ON STR 27R IN FWD CGO BILGE AREA (WITHIN 20 INCHES OF THE CARGO DOOR, CORR TASK #C53-119-02). MAJOR REPAIR ACCOMPLISHED: REPLACED PRODUCTION STRINGER SPLICE AT STA 560, STR 27R PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,742 hrs · 22,540 cycles

CORROSION AT STA 365 FROM RBL 20 - 56 ON FLOORBEAM (CORR TASK #CP53-222-01I). MAJOR REPAIR ACCOMPLISHED: REPLACED T-CAP STA 365 FROM RBL 00 TO RBL 65, BRACKETS AT RBL 00, 10, 55, AND INTERCOSTALS AT RBL 56 AND 65 ON PEMCO NR 2537N00148.

Part: FEEDER CABLE — BURNED (GALLEY) · airframe 60,742 hrs · 22,540 cycles

GALLEY POWER FEEDER CABLES BURNED AND BROKEN AT PREVIOUS SPLICE STA 1600-1620, STR 3R. REPAIRED THE AMP COPPER, ALUMINUM SPLICE OF THE POWER FEEDER WIRES FOR GALLEY G4A.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 60,742 hrs · 22,540 cycles

CORROSION ON INTERCOSTAL BOTH SECTIONS UNDER R4 DOOR. MAJOR REPAIR ACCOMPLISHED: CORROSION OUT OF LIMITS, REPLACED INTERCOSTAL STA 1640 - 1660 PER SRM.

Part: FLOOR SUPPORT — DAMAGED (BS 1408) · airframe 60,742 hrs · 22,540 cycles

AFT CARGO RT FLOOR SUPPORT DAMAGED BY OLD FLOORBOARD REPAIR. APPROX RBL 22, STA 1408. MAJOR REPAIR ACCOMPLISHED: REMOVED STRINGER FROM STA 1345 - 1445 RBL 16.10 IAW B757-200 SRM. RECEIVED "Z" ANGLE EXTRUSION AND FABRICATED NEW FLOOR SUPPORT, LOCATED AND DRILLED IAW SRM. TREATED AND PRIMED RH FLOOR SUPPORT & INSTALLED IAW SRM. DAMAGE ALSO FOUND AT APPROX RBL 19, STA 1405 TO 1418.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,742 hrs · 22,540 cycles

AFT CABIN FLOORBEAM CORRODED AT STA 1660, RBL 3 TO RBL 5. REPLACED FLOORBEAMS FROM RBL 3 TO RBL 24 PER SRM. ACP ON PEMCO NR 2537N00118, BY MECH AND INSPECTOR.

Part: STRUCTURE — DAMAGED (ELEVATOR) · airframe 60,652 hrs · 22,506 cycles

CREW REPORT: LEFT ELEVATOR TRAILING EDGE BY FUSELAGE SMALL AREA OF DAMAGE. SAMC TEXT: DAMAGE IS 8 INCHES FROM INBD EDGE OF LEFT ELEVATOR, THE DAMAGE IS A DENT .625 INCHES DEEP AND 1.750 INCHES WIDE ON THE TRAILING EDGE. ELEVATOR EDGE IS CRUSHED AT DAMAGE LOCATION. ACCOMPLISHED REPAIR PER SRM. ACP PER AMT. PAINTED TO MATCH.

Part: COMPUTER — FAULTED (NR 1) · airframe 60,578 hrs · 22,479 cycles

CREW REPORTED ELEVATOR FORCES ABNORMALLY HEAVY. RT SYSTEM ELEV PCA AT LT ELEVATOR (OTBD) IS LEAKING AT ROD END. OPERATED AILERONS. NO LEAKS NOTED. SUSPECT COLD SOAK LEAK. UNABLE TO DETERMINE IF LEAK IS FROM LT INBD OR LT OTBD PCA DUE TO RESIDUAL HYD FLUID MIGRATED TO MOST OF COMPARTMENT. REPLACED RT SYSTEM LEFT ELEVATOR PCA PER MM. ELEVATOR FEEL COMPUTER LEAKING AT CENTER MATING SURFACE. REMOVED & REPLACED ELEVATOR FEEL COMPUTER. REPLACED ELEVATOR FEEL ACTUATOR PER MM. FAILED TEST. ACCOMPLISH NEUTRAL SHIFT OVERRIDE MECHANISM TEST AND FEEL UNIT OVERRIDE TEST PER MM. COMPLETED TEST DOWN TO PARA P. TESTED NORMAL.

Part: BRACKET — INOPERATIVE (HANDSET) · airframe 60,467 hrs · 22,436 cycles

INTERPHONE HANDSET DOOR 1L WON'T STAY SECURED. DOOR 1L HANDSET IS SECURE. DOOR 4L HANDSET INTERIM SECURED TO CRADLE. HANDSET IS CONSIDERED INOP. REPLACED CUP ASSEMBLY, OPS OKAY.

Part: FEEDER CABLE — FAULTY (EMERGENCY LIGHTS) · airframe 60,079 hrs · 22,291 cycles

EMERGENCY LIGHT STRIP AT 14ABC DAMAGED. EMERGENCY LIGHTS ARE INOP FROM ROW 9 TO ROW 14. EMERGENCY LIGHT PULLED UP AND CUT IN HALF AY ROW 14. REPLACED CABLE ASSY AND 2 EACH LAMPS AND FLOOR TRACK TOP HOUSING AND OP CHECKS GOOD.

Part: ACTUATOR — FAULTY (ELEVATOR) · airframe 59,959 hrs · 22,250 cycles

HEAVY ELEVATOR CONTROL FORCES NEEDED. IAW THE FLIGHT CREW ELEVATOR NEEDED MORE PRESSURE THEN NORMAL TO MOVE. REPLACED ELEV FEEL ACTUATOR IAW MM, LEAK CHECK AND TEST GOOD.

Part: CONTROL COLUMN — STIFF (ELEVATORS) · airframe 59,635 hrs · 22,130 cycles

STICK FORCES VERY HEAVY. PITCH CONTROL ON GROUND TEST AND DURING LANDING FLARE OUT VERY HEAVY. ACCOMPLISHED ELEVATOR FEEL SYSTEM FORCES TEST PER MM. CHECKED WITHIN LIMITS.

Part: FAN — MALFUNCTIONED (E/E COOLING) · airframe 59,065 hrs · 21,923 cycles

EQUIP COOLING STATUS MESSAGE ACCOMPANIED W-HOT ODOR. NR1 E&E COOLING FAN MAKING EXCESSIVE NOISE DURING OPERATION. REPLACED COOLING FAN. ALSO CHANGED COOLING FILTER.

Part: EXTINGUISHER — LEAKING (FWD) · airframe 58,395 hrs · 21,677 cycles

FWD H2O FIRE EXTINGUISHER LEAKING. REPLACED H20 FIRE EXT FWD POSITION AT DOOR 1 LT.

Part: EXTINGUISHER — LEAKING (AFT) · airframe 58,395 hrs · 21,677 cycles

AFT H2O FIRE EXTINGUISHER LEAKING. REPLACED FIRE EXTINGUISHER.

Part: WIRE — OPEN (CHILLER) · airframe 58,110 hrs · 21,572 cycles

GALLEY CHILLER INOP AT R1 DOOR GALLEY G1B. C/B C3023 ON P37 PANEL WAS TRIPPED. C/B RESET BUT WOULD TRIP AFTER APROX 10 SEC. WITH C.B FOR CHILLER ON FWD GALLEY SW PANEL OPEN, C3023 STAYS IN. RANG OUT WIRES FROM CHILLER TO C/B YS8C001, NO DISCREPANCIES NOTED. WITH CONNECTOR OFF OF CHILLER, AND YS8C001 IN, C.B C3023 STAYS IN. CHECKED VOLTAGE ON EACH PHASE TO CHILLER, ALL 3 PHASES OK. REPLACED CHILLER PER MM. WIRING CKS PER WDM. WHEN RINGING OUT CHILLER, FOUND PHASE A AND B SHORTED. AFTER REMOVAL OF CHILLER RECHECKED FOR SHORTED WINDINGS AND NO SHORTS NOTED. POSSIBLE CONNECTOR SHORT, MAY HAVE BEEN DISTURBED ENOUGH DURING REMOVAL TO REMOVE SHORT. CHILLER WILL BE TAGGED WITH REJECT FOLLOW UP TAG.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 58,048 hrs · 21,549 cycles

SMALL SECTION OF EMERGENCY STRIP AT LOCATION 14C HAS A CRACK IN PLASTIC LENS. INTERIM REPAIR, TAPED THE CRACK SECTION OF EMERGENCY STRIP PLASTIC COVER, SYS OPS CKS NORMAL. R & R BROKEN SECTION. OPS CHECK ACCOMPLISHED EMERGENCY EXIT LIGHTS. SYS CHECKS OK.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,440 hrs · 21,301 cycles

FLOOR EMERGENLCY LIGHT INOP ROW 9 THRU 15. REPLACED EMERGENCY LIGHT POWER INVERTER M10827. FLOOR EMERGENCY LIGHTS ROWS 9 - 15 CK OK.

Part: O-RING — LEAKING (EVAC SLIDE)

LOW BOTTLE PRESSURE. LEAKING AT BURST DISK O-RING. REMOVED & REPLACED O-RING.

Part: BOTTLE — READS LOW (L1 DOOR SLIDE) · airframe 55,161 hrs · 20,390 cycles

DOOR 1L SLIDE PSI LOW. EVACUATION SLIDE BOTTLE PRESS (LOW, ZERO) AT DOOR 1. REPLACED DOOR MOUNTED SLIDE RAFT REF MM 25-66-01.

Part: FUEL/OIL COOLER — FAILED (LT GENERATOR) · airframe 53,691 hrs · 19,805 cycles

LOST LT GENERATOR. FUEL COOLED OIL COOLER REPLACED. UNIT SO FAR PASSING TEST. ONLY RAN 100 PSI BUT NO LEAKS DETECTED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,578 hrs · 19,369 cycles

EXTERIOR EMERGENCY LIGHT BY DOOR 2L AND LT OVERWING ESCAPE HATCH FWD LIGHT INOP. FOUND BULBS INOP. RELAMPED BULBS, ALL OPS TEST NORMAL.

Part: VIDEO UNIT — ODOR (CABIN) · airframe 51,325 hrs · 18,921 cycles

F/A REPORTS ACRID ODOR AND HAZE FROM VIDEO SYSTEM PROG. VIDEO SYSTEM WAS CLEANED AND RETESTED WITH NO SMELL, NO REPEATS.

Part: SENSOR — FAULTY (R2 DOOR SLIDE) · airframe 51,190 hrs · 18,870 cycles

FOUND DOOR 2R SLIDE LIGHT INDICATOR INOP. FOUND A WEAK PROX SENSOR. REPLACED PROX SENSOR 585-3162 AT DOOR 2R AT AFT POSITION.

Part: LAMP — INOPERATIVE (EXTERIOR) · airframe 51,125 hrs · 18,847 cycles

EXTERIOR EMERGENCY LIGHTS INOP AT DOOR 4L AND 4R. FOUND LAMP INOPERATIVE. REPLACED LAMP, CHECKED OK.

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 50,649 hrs · 18,666 cycles

THE 1L DOOR ASSIST BOTTLE NOT IN GREEN BAND. REPLACED DOOR ASSIST BOTTLE 1L DUE TO CHRONIC LEAKING.

Part: TRIM SYSTEM — OUT OF RIG (RUDDER) · airframe 50,402 hrs · 18,575 cycles

RUDDER TRIM OUT OF LIMITS. FOUND RUDDER RIG OFF SLIGHTLY. RE-RIGGED ENTIRE RUDDER SYSTEM AND STANDBY RUDDER LVDT. NO HISTORY SINCE ORIGINAL.

Part: LIGHT — DAMAGED (CABIN) · airframe 48,853 hrs · 17,994 cycles

FOUR EEL LIGHTING END CAPS MISSING THROUGHOUT CABIN. [08-17-07] REPLACED MISSING END CAPS.

Part: WARNING MESSAGE — ILLUMINATED · airframe 45,645 hrs · 16,832 cycles

LEFT AUX PITOT MESSAGE AND LIGHT CAME ON DURING CLIMBOUT. RELAY REPLACED WITH NEW UNIT WHICH TRIGGERED FAULTS WITHIN RELAY OR AT RELAY CONNECTIONS. A DIFFERENT RELAY WAS INSTALLED AND WIRING CHECKED. NO FURTHER FAULTS SINCE THE LAST REPLACEMENT.

Part: RADAR — FAILED (WX SYSTEM) · airframe 41,663 hrs · 15,387 cycles

WEATHER RADAR FAILED JUST AFTER TAKEOFF. FLIGHT DIVERTED DUE TO THUNDERSTORMS. MAINTENANCE REPLACED THE RADAR ANTENNA ASSY (P/N 2041444-0401). THE COMPONENT SHOP TESTING DID NOT REVEAL ANY FAILURES, HOWEVER THE AZIMUTH GEAR ASSY WAS FOUND WITH WATER CONTAMINATION. THE GEAR ASSY WAS DRIED AND THE ANTENNA DRIVE ASSY OPERATIONALLY CHECKED GOOD. THE AIRCRAFT HAS FLOWN WITHOUT RADAR PROBLEMS SINCE 9 JULY.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,654 hrs · 14,609 cycles

RT EXT FUSELAGE AT STA 595 AND STR 8R, REPAIR DOUBLER AREA DAMAGED, CUTOUT CORNERS HAVE INSUFFICIENT RADII. *S/D* REMOVED EXISTING REPAIR DOUBLER, ENLARGED CUTOUT TO PROPER CUTOUT SPECIFICATIONS, AND INSTALLED REPAIR DOUBLER.

Part: STRAP — CORRODED (FUSELAGE) · airframe 39,654 hrs · 14,609 cycles

AFT PIT AFT STA 1400L BETWEEN STR 28L AND 29L, PRODUCTION SPLICE PLATE CORRODED. SPLICE STRAP REMOVED AND REPLACED.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,654 hrs · 14,609 cycles

AFT PIT FRAME DENTED UPPER FLANGE AT STA 1420, STR 26L.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,654 hrs · 14,609 cycles

AFT PIT FRAME DENTED ON UPPER FLANGE STA 1400 AND STR 26L. INSTALLED NESTED J ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,654 hrs · 14,609 cycles

AFT PIT FRAME DENTED ON UPPER FLANGE AT STA 1520 AND STR 26L. INSTALLED NESTED J ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,654 hrs · 14,609 cycles

AFT PIT FRAME DENTED UPPER FLANGE AT STA 1500 AND STR 26L. INSTALLED J ANGLE REPAIR DOUBLER.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,654 hrs · 14,609 cycles

AFT PIT FRAME DENTED AT UPPER FLANGE AT STA 1440, STR 26L. REPAIRED FRAME WITH J ANGLE REPAIR SECTION.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 39,654 hrs · 14,609 cycles

AFT PIT BETWEEN STA 1180L AND STA 1200L AT STRINGER 17L, CREASE BEAM WEB HAS CORROSION. REPLACED CREASE BEAM WEB.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,654 hrs · 14,609 cycles

STATION 1380 LBL 19, INTERNAL SKIN DOUBLER CORRODED BEYOND LIMITS IN AFT PIT.

Part: FIREWALL — GOUGED (NR 2 PYLON) · airframe 39,654 hrs · 14,609 cycles

NR 2 PYLON I/B FIREWALL BULKHEAD IS GOUGED.

Part: FLOORBEAM — CORRODED (FUSLEAGE) · airframe 39,654 hrs · 14,609 cycles

CABIN FLOORBEAM STA 324 AND RBL 53 HAS CORROSION. REMOVED DAMAGED T CAP SECTION AND INSTALLED NEW SECTION SPLICED WITH DOUBLERS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,654 hrs · 14,609 cycles

FUSELAGE SKIN HAS LIGHTNING STRIKE DAMAGE. DAMAGED SKIN WAS CUTOUT AND A DOUBLER REPAIR WAS INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,654 hrs · 14,609 cycles

CABIN FLOORBEAM STA 1640 HAS CORROSION RBL 44 TO 52, UPPER CAP. CORRODED SECTION REMOVED AND A FLOORBEAM DOUBLER REPAIR WAS INSTALLED.

Part: FLOORBEAM — BUCKLED (CARGO BAY) · airframe 39,654 hrs · 14,609 cycles

CARGO PIT FLOOR JUST IN FRONT OF DOORWAY IS SEVERELY BUCKLED.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,309 hrs · 13,771 cycles

EXTERNAL FUSELAGE SKIN HAS SEVERAL DENTS AT BS 600-640, AND STR 14L TO 19L. MAJOR REPAIR ACCOMPLISHED. INSTALLED SKIN SPLICE DOUBLER REPAIR.

Part: STATOR — FAILED (NR 1 ENGINE) · airframe 30,934 hrs · 11,374 cycles

NUMBER 1 ENGINE COMPRESSOR STALL. FOUND 10TH STAGE STATOR FAILED. THIS STATOR HAD THE NEW GOLD/NICKEL BRAZE MATERIAL AS PER PWA SERVICE BULLETIN. STATOR HAD 470 CYCLES SINCE 100 PERCENT VANE REPLACEMENT.

Part: ENGINE — VIBRATION (LEFT) · airframe 29,678 hrs · 10,904 cycles

LEFT ENG VIB IND FLUCTUATES BETWEEN 1.0 & 1.5 IN CRUISE AT 350. VIB FELT THROUGHOUT AIRCRAFT AND INCREASES INVERSELY WITH THROTTLE. FOUND METAL IN THE TAILPIPE.

Part: SKIN — DENTED (FUSELAGE) · airframe 29,140 hrs · 10,734 cycles

FUSELAGE DENTED STA 1688-1701, STR 18R. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND TRIPLER.

Part: ELEVATOR — FLUTTERED (WING)

FLIGHT DIVERTED TO ORD UNDER AMBER ALERT DUE TO A CONTROL FLUTTER PROBLEM. CONCURRENT REPORTING OF UNITED'S FINDINGS TO FAA IS ONGOING THROUGH UNITED'S FLIGHT SAFETY DEPARTMENT. ACTIONS ACCOMPLISHED PRIOR TO SUCCESSFUL TEST FLIGHT INCLUDE REPLACEMENT OF NUMEROUS ELEVATOR HINGE BEARINGS, ELEVATOR REACTION LINK BEARINGS, REACTION LINKS, AND REPLACEMENT OF ELEVATOR PCA'S. RE-RIGGING OF THE ELEVATOR SYSTEM AND RE-TENSION OF THE ELEVATOR CONTROL CABLES WERE ALSO ACCOMPLISHED.

Part: PUMP — OVERHEATED (NR 2 HYD SYS)

LANDED UNDER AMBER ALERT DUE TO A NR 2 HYDRAULIC SYSTEM FAILURE. S/D, THE PARTING SURFACE OF THE ENGINE DRIVEN PUMP FAILED WHEN THE PUMP OVERHEATED, ALLOWING FLUID TO LEAK. CAUSE OF OVERHEAT IS UNKNOWN BUT MOST LIKELY A RESULT OF A FAILED SHAFT BEARING. THE PUMP WAS REPLACED.

Part: WIRE — FAILED (LE FLAP)

RETURNED TO FIELD AT ORD UNDER AMBER ALERT DUE TO A LEADING EDGE ASYMMETRY LIGHT. *S/D* FOUND A WIRE ASSOCIATED WITH THE LEADING EDGE SLAT SYSTEM SHORTING TO GROUND WHICH CAUSED THE SYSTEM FAULT AND SHUTDOWN. REPLACED THE WIRE AND RETURNED AIRCRAFT TO SERVICE WITHOUT FURTHER INCIDENT.

Part: WARNING — ACTIVATED (FLAP SYST)

DIVERTED TO PHX UNDER AMBER ALERT DUE TO FLAP/SLAT PROBLEM. *S/D* CHECKS OF THE SYSTEM DID NOT REVEAL A ROOT CAUSE, AND PROBLEM COULD NOT BE DUPLICATED. SYSTEM OPERATIONALLY CHECKED OK.

Part: SWITCH — FAILED (COCKPIT)

OXYGEN MASKS DEPLOYED ON TOUCH DOWN. *S/D* RECEPTICLE ON S119 ALTITUDE PRESSURE SWITCH WAS FOUND DETACHED FROM SWITCH BODY. REPLACED S119 AND PERFORMED CALIBRATION CHECK PER MM 35-21-00.

Part: LIGHT — INOPERATIVE (CABIN)

FLOOR EEL LIGHT INOP AT ROW 13. RECONNECTED EEL LIGHT STRIP.

Part: CHARGER — INOPERATIVE (CABIN)

EEL LIGHTS AT ROW 19 THROUGH 24 DO NOT COME ON. REPLACED CHARGER M10770. SYSTEM CHECKS OK.

Part: BATTERY — DISCHARGED (CABIN)

FLASHLIGHT AT DOOR 1L INOP, BATTERY DEAD. REPLACED BATTERY.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHT AT ENTRY DOOR 2L INOP. REPLACED BATTERY AND CHARGER AT DOOR 2L, OPERATION CHECKS NORMAL.

Part: BATTERY — DISCHARGED (CABIN)

CEILING EMERGENCY EGRESS LIGHTING AT OVERWING POSITION INOP. REPLACED BATTERY PACK, OPERATION CHECKS NORMAL.