N571UA

Part: GIRT BAR — STUCK (R4 DOOR) · airframe 68,387 hrs · 25,194 cycles

DOOR 4R WON'T ARM. UNSTUCK GIRT BAR & CYCLED 4R ARM DISARM HANDLE SEVERAL TIMES. NO TROUBLE NOTED, INDICATION NORMAL.

Part: PLUG — LOOSE (SPOILER ACTUATOR) · airframe 68,264 hrs · 25,149 cycles

HYD FLUID LEAKING FROM LT WING OTBD SPOILER ACTUATOR. FOUND UPPER PLUG ON ACTUATOR LOOSE. SECURED & LEAK CHECKED. NO LEAKS NOTED.

Part: SKIN — DELAMINATED (RT WING) · airframe 67,749 hrs · 24,961 cycles

RIGHT WING T/E BETWEEN INBD AND OTBD FLAP HAS AREA OF DELAMINATION. REMOVED DAMAGE REPAIR REF SRM 51-70-10, REF ALSO SRM 57-53-01.

Part: CONTROL PANEL — DAMAGED (COCKPIT) · airframe 67,306 hrs · 24,819 cycles

FLIGHT DECK WET WITH HIGH HUMIDITY. REPLACED VHF COMM 1 & 2 CONTROL PANELS IAW AMM. REPLACED ADF CONTROL PANEL IAW AMM. REPLACED RT EFIS CONTROL PANEL IAW AMM. REPLACED ILS CONTROL PANEL IAW AMM. UNITS REPLACED DUE TO FOGGING IN DISPLAYS. ALL TEST REFERENCED PASSED.

Part: FRAME — GOUGED (FUSELAGE) · airframe 67,208 hrs · 24,789 cycles

A GOUGE AT STA 1640, ABOVE STR 9L. REPAIRED GOUGE AT BS1640 FRAME UPPER FLANGE APPROX 1.25" ABOVE STR 9L.

Part: SKIN — DENTED (FUSELAGE) · airframe 67,208 hrs · 24,789 cycles

DENT ON FUSELAGE SKIN AT BS 270 STR 21-22R. REPAIRED DENT AT FUSELAGE SKIN AT 270 STR 21R-22R IAW SRM 53-00-01, FIG 201, REPAIR 3.

Part: SKIN — DENTED (RT APU DOOR) · airframe 67,208 hrs · 24,789 cycles

RT APU DOOR FWD EDGE MEMBER HAS A DENT 24 INCHES AFT OF FWD EDGE. REPAIRED RT APU DOOR FWD EDGE IAW SRM 51-70-11. NDT INSPECTED CUTOUT IAW NTM 51-00-19 AND 16 NO DEFECTS NOTED.

Part: SKIN — DENTED (FUSELAGE) · airframe 67,208 hrs · 24,789 cycles

IAW CF9083 & CF9084. DENTS AT BS 1490 & 1495 BETWEEN STRINGER 22L & 23L. CUTOUT & REPAIRED DENTS AT BS 1490 & 1495 AT STRINGER 22L - 23L IAW SRM 53-00-01 FIG 201 REPAIR 3. REPAIR ACCOMPLISHED IAW SRM 53-0 0-01 FIG 201 REPAIR 3.

Part: SKIN — DENTED (BS 1601) · airframe 67,208 hrs · 24,789 cycles

DENT ON LOWER EXTERIOR FUSELAGE SKIN JUST FWD OF REPAIR DOUBLER AT BS 1601, S30R. REPAIRED DAMAGE ON LOWER EXTERIOR FUSELAGE SKIN AT BS 1595-1615 S29-30R IAW SRM 53-00-01, REPAIR 2, FIG 201.

Part: SKIN — DENTED (BS 1495) · airframe 64,333 hrs · 23,800 cycles

ON WALK AROUND, FOUND A DENT AT BS 1495 BETWEEN S22-23L. DENT MEASURES 2.5" WIDE, 3.5" LONG AND 3-32 (.09375) DEEP. CUTOUT AND REPAIRED SKIN.

Part: SKIN — DENTED (BS 520 S24L) · airframe 67,208 hrs · 24,789 cycles

FUSELAGE SKIN HAS PROTRUDING DENT BS 520 STR 24L. REPAIRED DENT IN FUSELAGE SKIN AT BS 520, STR 24L IAW SRM 53-00-01, FIG 201, REPAIR 2. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 552) · airframe 67,208 hrs · 24,789 cycles

EXTERNAL SKIN HAS A LIGHTNING STRIKE AT BS 552 FIVE INCHES BELOW S28R. REPAIRED SKIN IAW SRM 53-30-01, FIG 1 AND SRM 53-00-01, FIG 101. NDT INSPECTION IAW NTM PN 6 51-00-16, NO DEFECTS NOTED.

Part: SKIN — DAMAGED (BS 480) · airframe 67,208 hrs · 24,789 cycles

EXTERNAL SKIN HAS INDICATION OF LIGHTNING STRIKES AT BS 480, STR 25R. REPAIRED SKIN IAW SRM 53-00-01, FIG 201.

Part: SKIN — DAMAGED (BS 211) · airframe 67,208 hrs · 24,789 cycles

LIGHTNING STRIKE AT BS 211 EIGHT INCHES LEFT OF BL 0. REPAIRED SKIN IAW SRM 53-00-01, FIG 201.

Part: SKIN — DAMAGED (BS 220) · airframe 67,208 hrs · 24,789 cycles

LIGHTNING STRIKE AT BS 220 7.5" LT OF BL 0. REPAIRED SKIN IAW SRM 53-00-01, FIG 201.

Part: SKIN — DAMAGED (BS 208) · airframe 67,208 hrs · 24,789 cycles

LIGHTNING STRIKE AT BS 208, 8.5" LEFT OF BL 0. REPAIRED SKIN IAW SRM 53-00-01, FIG 2, 01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,934 hrs · 24,719 cycles

EMERGENCY LIGHT OUTSIDE OF MID LAVATORY INOPERATIVE. REPLACED EMERGENCY LIGHT ASSY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,928 hrs · 24,716 cycles

EEL OUTSIDE OF MID LAV INOP. MID LAV EEL STRIP INOPERATIVE.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 66,708 hrs · 24,645 cycles

SOFT SPOT II AISLE FLOOR ROW 39. FOUND DELAM AREA MEASURED 22" ACROSS. PERFORMED INTERIM REPAIR REF AMM 53-00-99 PG 801. OVERLAY TAPED AND FASTENER HOLES PICKED UP ADJACENT TO DELAM AREA.

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS) · airframe 66,708 hrs · 24,645 cycles

ENGINE DUCT PRESSURES SPLIT DURING TAKEOFF OR CLIMB. REPLACED NR 1 ENGINE PRSOV IAW AMM & REPLACED NR 1 ENG PRSOV REGULATOR IAW AMM.

Part: SMOKE DETECTOR — NOISY (LAVATORY) · airframe 65,977 hrs · 24,396 cycles

L1 DOOR SQUEAL IS EXTREMELY LOUD AND UNBEARABLE FOR FLIGHT ATTENDANTS. DURING PRESSURIZATION FOR TROUBLESHOOTING, SQUEAL COMING FROM THE FWD LAV. REMOVED AND REPLACED FWD LAV SMOKE DETECTOR IAW AMM 26-14-01. SMOKE DETECTOR OPS CHECKED GOOD. REPRESSURIZED, SQUEAL GONE. OK TO CONTINUE.

Part: BOTTLE — LOW PRESSURE (OXYGEN SYS) · airframe 65,844 hrs · 24,352 cycles

AFT O2 BOTTLE WAS USED PRESSURE IS LOW. PRESSURE IS LOW. REMOVED BOTTLE AND INSTALLED STICKER TO BRACKET.

Part: PIN — BROKEN (EMERGENCY LIGHTS) · airframe 65,469 hrs · 24,221 cycles

EMERGENCY LIGHT STRIP ON FLOOR AT C12 LOOSE WIRES. FWD OF ROW 12 EMER FLOOR STRIP INOP. CONNECTOR PIN BROKEN. REMOVED AND SOLDERED POWER STRIP AS PER INTERIM REPAIR METHOD II AMM. ACCEPTABLE FOR SERVICE FOR A PERIOD NOT TO EXCEED 45 DAYS. INSTALLED NEW EEL STRIP SECTION, ROW 12, OPS CHECKS OKAY.

Part: O-RING — LEAKING (FUEL SYSTEM) · airframe 65,319 hrs · 24,171 cycles

FUEL LEAK RIGHT WING, IN THE MLG FWD TRUNNION AREA. REPLACED O-RINGS ON SHUT-OFF VALVE ACTUATOR, REF MM 28-21-1.

Part: CONTROL VALVE — FAULTY (RT WING) · airframe 65,311 hrs · 24,167 cycles

RIGHT WING SHUTOFF VALVE WILL NOT OPEN. COMPLIED WITH MEL. REPLACED RIGHT WING CONTROL VALVE IAW AMM.

Part: ACTUATOR — LEAKING (SPOILER) · airframe 65,291 hrs · 24,159 cycles

HYD FLUID LEAKING FROM RIGHT OUTBOARD WING UNDER NUMBER 12 SPOILER AREA. REMOVED NR 12 SPOILER ACTUATOR. MEASUREMENT FROM BOTTOM OF LOCKNUT TO PCA ROD IS .326 REF MM 27-61-02 STEP 2F.5 +VIEW C HARDWARE AND OLD ACTUATOR IN COCKPIT. ACP. RII INSPECTION OF SPOILER ACTUATOR ATTACH POINTS, NO DEFECTS NOTED, REF GMM 09-25-0 5. ACP RII TO VERIFY CORRECT. FINISHED REPLACED NR 12 SPOILER ACT TO END.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,730 hrs · 23,949 cycles

FOUND AFT EMEGENCY LIGHT NOT WORKING. REPLACED EMERGENCY LIGHT.

Part: GUARD — FAULTY (EMERGENCY LIGHTS) · airframe 64,467 hrs · 23,857 cycles

EMERGENCY LIGHTS SWITCH COVER DOES NOT ARM SWITCH WHEN CLOSED. REPLACED P5 PANEL EMERGENCY LIGHT SWITCH GUARD.

Part: FILTER — FAULTED (LT ENGINE) · airframe 64,000 hrs · 23,691 cycles

LEFT ENGINE OIL FILTER EICAS AND STATUS MESSAGE AFTER ENGINE START, OIL TEMP 69C. RETURNED TO BLOCKS, REPLACED MAIN OIL FILTER AND PER MM 79-21-05 P 401, AND OIL FILTER DIFFERENTIAL PRESSURE SWITCH PER MM 79-35-01 P 401.

Part: OIL SYSTEM — OVERSERVICED (NR 1 ENGINE) · airframe 63,925 hrs · 23,667 cycles

NR 1 ENG HIGH OIL CONSUMPTION EXCEEDS LIMIT, CHECKED OVER ENGINE AND COULD FIND NO EVIDENCE OF ANY LEAKS. REVIEW OF OIL SERVICE HISTORY AND SUSPECT THE PREVIOUS STATION DID NOT CORRECTLY SERVICE THE ENGINE. ENGINE IS OPERATING WELL WITHIN LIMITS.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 63,715 hrs · 23,594 cycles

EMERGENCY LIGHT INOPERATIVE ROW 8 TO 12. FOUND LOOSE CONNECTOR. SECURED CONNECTOR. SYSTEM OPS CHECKED NORMAL.

Part: FUEL CONTROL — LEAKING (NR 1 ENGINE) · airframe 63,461 hrs · 23,502 cycles

NR 1 ENGINE HAS FUEL LEAK. FUEL LEAKING FROM TOP COVER ON FUEL CONTROL. RMV'D FUEL CONTROL PER AMM. REPLACED FUEL CONTROL.

Part: GUARD — OUT OF ADJUST (COCKPIT) · airframe 62,350 hrs · 23,097 cycles

EMERGENCY EXIT LIGHT SWITCH IN COCKPIT IS VERY TOUCHY, NEEDS ADJUSTMENT. ADJUSTED GUARD ASSY. SYSTEM OP CHECK OK.

Part: SKIN — DENTED (FUSELAGE) · airframe 61,795 hrs · 22,878 cycles

EXTERNAL FUSELAGE BETWEEN BS 520 AND BS 540, BETWEEN STR 29L AND STR 28L HAS A DENT. MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT THE DAMAGED SKIN AND FABRICATED A REPAIR DOUBLER AND INSTALLED PER TIMCO REO 2 0284. PER UAL EVA 81196, THE FUSELAGE SKIN REPAIR BETWEEN BS 525 - BS-555, AND STR 26L AND 28L HAS RECEIVED FIRST STAGE APPROVAL FOR STATIC STRENGTH 085625 ONLY, AND A NEW FAA 8100-9 MUST BE ISSUED AND DTA INFORMATION INCORPORATED IN THE AIRPLANE MAINTENANCE PROGRAM BEFORE 08AUG2013. THE AIRCRAFT WILL BECOME UNAIRWORTHY IF A NEW FAA 8100-9 IS NOT ISSUED ON OR BEFORE 08AUG2013.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 61,795 hrs · 22,878 cycles

FUSELAGE DAMAGE AREA OF STA 500, 520 STR 17L,18L ON LEFT SIDE OF FUSELAGE APPROX 10 FT FROM DOOR 1L AT FLOOR LEVEL. MAJOR REPAIR ACCOMPLISHED: INTERIM RPR DONE PER BOEING MSG REQUIRED PERM RPR BY GSO. FUSELAGE SKIN REPAIRED WITH DOUBLER-FILLER REPAIR PER REO G138 42, REV D ON NON ROUTINE 20001. CREATED CF9079 PER EVA 81204 FOR 24 MONTH DTA.

Part: STRINGER — DAMAGED (BS 500-520 S17L) · airframe 61,795 hrs · 22,878 cycles

STRINGER 17L FROM BS 500 TO 520 HAS OUT OF ROUND HOLES. MAJOR REPAIR ACCOMPLISHED: R & R STRINGER 17L SECTION FROM BS 476 TO 583 PER REO G13842, REV. D.

Part: FRAME — DAMAGED (BS 1680) · airframe 61,795 hrs · 22,878 cycles

MAJOR REPAIR ACCOMPLISHED: FRAME AT BS 1680 RH HAS SMALL CUT IN THE FWD. FACE OF FRAME JUST BELOW FLOORBEAM T-CAP. MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT DAMAGE AND FABRICATED A REPAIR ANGLE, STRAP, AND FILLER, AND INSTALLED PER REO G13883, REV. B.

Part: SKIN — DAMAGED (BS 500-520) · airframe 61,795 hrs · 22,878 cycles

BS 500 - 520 LT BETWEEN S17-18L HAS INCURRED DAMAGE TO SKIN. MAJOR REPAIR ACCOMPLISHED: FABRICATED REPAIR DOUBLER AND FILLER PER REO G13842, REV. D.

Part: SWITCH — MISWIRED (EMERGENCY LIGHT) · airframe 61,795 hrs · 22,878 cycles

EMERGENCY LIGHTS INOPERATIVE. REWIRED EMERGENCY LIGHT SWITCHES PER WDM AND OPS CHECKED GOOD PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,795 hrs · 22,878 cycles

RH AFT OVERWING EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT PER MM AND OPS CHECKED GOOD.

Part: FLOORBEAM — CORRODED (BS 1681) · airframe 61,795 hrs · 22,878 cycles

FLOORBEAM AT BS 1681, RBL 37 - RBL 42 CORRODED. REMOVED DAMAGED TEE ENTIRE LENGTH BETWEEN RBL 60 TO LBL 60. FABRICATED A REPLACEMENT TEE ANGLE AND FILLERS AND ASSOCIATED REPAIR PARTS PER REO G 13868, REV. C AND INSTALLED

Part: FRAME — BROKEN (BS 520 S17-18L) · airframe 61,795 hrs · 22,878 cycles

MAIN CABIN STA 520 FRAME AND CHORD IS BROKEN OUT BETWEEN STR 17L AND STR 18L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED FRAME & CHORD SECTION AND REPLACED FRAME SECTION AND FABRICATED A DOUBLER PER DWG 143N1027, REV. A, AND A NEW FAILSAFE PER DWG 143N1026, REV. B, AND INSTALLED PER DWG 143N1004 AND 143N1005 .

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 61,795 hrs · 22,878 cycles

EMERGENCY ESCAPE LIGHTS DO NOT ILLUMINATE DURING TEST 1 OF THE ELECTRICAL SYSTEM SQUIB AND PRESSURE SWITCH TEST AS FOUND IN AMM AND ROUTINE JIC 5R 25I9050. PERFORMED ELECTRICAL SYSTEM SQUIB AND PRESSURE SWITCH TEST 1 PER MM. OPS CHECKED NORMAL.

Part: PUSHROD — OUT OF ADJUST (R4 DOOR GIRT BAR) · airframe 61,795 hrs · 22,878 cycles

R-4 DOOR FAILED MIDWAY CHECK. ADJUSTED R-4 DOOR GIRT BAR CRANK PUSH RODS PER MM AND DOOR MIDWAY OPS CK GOOD ON NON ROUTINE 21146 BY MECH-110236 AND INSP QC031.

Part: FLOORBEAM — BROKEN (BS 500L) · airframe 61,795 hrs · 22,878 cycles

MAIN CABIN FLOORBEAM AT BS 500L IS BROKEN OFF FROM LBL 45 TO THE END OF THE BEAM. REMOVED DAMAGED SECTION OF FLOORBEAM AND FABRICATED A REPLACEMENT FLOORBEAM SEGMENT, REPAIR CHANNELS, REPAIR ANGLES, AND DOUBLERS AND INSTALLED PER REO G1385 9, REV.

Part: FRAME — BROKEN (FUSELAGE) · airframe 61,795 hrs · 22,878 cycles

MAIN CABIN STA 500L FRAME & CHORD IS BROKEN OUT BETWEEN STR 17L & STR 18L. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED FRAME & CHORD & REPLACED WITH NEW FRAME SECTION, PN 143N1024-29, AND FABRICATED FRAME CHORD, PN 143N1026-35 AND FRAME DOUBLER, PN 143N1027-1 PER BACO DWG 143N1024, 143N1026, AND 143N1027 AND INSTALLED PER BACO DWG 143N1004 ON NON ROUTINE 20004.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,795 hrs · 22,878 cycles

MAIN CABIN FLOORBEAM T-CAP UPPER SURFACE CORRODED AT BS 322, RBL 41-50. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS PER SRM. BLENDED DAMAGED AREA AND FABRICATED REPAIR ANGLES AND FILLER AND INSTALLED PER TIMCO REO G13891, REV B ON NON ROUTINE 20495. PER UAL-EVA-81179, THIS REPAIR HAS RECEIVED FIRST STAGE APPROVAL FOR STATIC STRENGTH ONLY 085625A NEW FAA 8100-9, SHOWING COMPLIANCE TO 14 CFR 25.571 AND 26.43(D), MUST BE ISSUED BEFORE 02AUG2013. THE AIRPLANE WILL BECOME UNAIRWORTHY IF A NEW FAA 8100-9 IS NOT RECEIVED ON OR BEFORE 02AUG2013.

Part: SKIN — DENTED (FUSELAGE) · airframe 61,795 hrs · 22,878 cycles

THERE ARE 3 DENTS LOCATED APPROX STA 442 & AFT BTWN STR LT 17 + 18. MAJOR REPAIR ACCOMPLISHED: 1ST DENT IS 1.25" IN DIAMETER & .015" DEPTH STA 441.75. 2ND DENT IS 2.0" IN DIAMETER & .015" DEPTH STA 444. 3RD DENT IS 3.0 INCH IN DIAMETER & .031" DEPTH STA 446. THE FIRST DENT IS NOT WITHIN LIMITS FOR PROXIMITY TO SKIN JOINTS (3.0IN) OF SRM. REMOVED SECTION OF FUSELAGE SKIN AT BS 440L AND BETWEEN STR 17L TO STR 18L. FABRICATED AND INSTALLED A REPAIR DOUBLER AND FILLER PER REO G13845, REV B. BUTT JOINT NOT AFFECTED AND NO LOOSE FASTENERS. ACP HFEC INSP AND FOUND NO CRACKS. PERMANENT REPAIR TO BE ACCOMPLISHED AT NEXT HMV3 CURRENTLY SCHEDULED FOR JULY 2011^02NOV.

Part: FLOORBEAM — BROKEN (FUSELAGE) · airframe 61,795 hrs · 22,878 cycles

MAIN CABIN FLOORBEAM STA 520L IS BROKEN OFF FROM LBL 65 TO THE END OF THE BEAM LT SIDE. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED END OF FLOORBEAM & PERFORMED HFEC ON TRIM OUT PER NDT 6-51-00-19 WITH NO CRACK INDICATIONS FOUND. FABRICATED, LOCATED, DRILLED AND INSTALLED A REPAIR DOUBLER AND TWO EACH STRUCTURAL FILLERS PER REO-G13880 REV A ON NON ROUTINE 20003. THIS IS A CATEGORY 'A' REPAIR PER BACO 8100-9 AND 085625SRM 51-00-06.

Part: SHEAR TIE — BROKEN (FUSELAGE) · airframe 61,795 hrs · 22,878 cycles

MAIN CABIN STA 500L FRAME TO SKIN SHEAR TIES ARE BROKEN FROM STR 17L TO STR 20L. MAJOR REPAIR ACCOMPLISHED: FABRICATED AND INSTALLED 2 EACH SHEAR TIES AT BS 500 FRAME, BETWEEN STR 17L AND 20L PER BACO DWGS 140N2006, 140N2001 AND 140N2002 AND SRM ON NON ROUTINE 20007.

Part: SHEAR TIE — BROKEN (FUSELAGE) · airframe 61,795 hrs · 22,878 cycles

MAIN CABIN FRAME TO SKIN SHEAR TIES AT BS 520L ARE BROKEN FROM STR 17L TO STR 20L. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SHEAR TIES AND REPLACED WITH NEW SHEAR TIES, P-N 140N2002-53 AND 140N2002-5 5 PER BACO DWG 140N2002 AND INSTALLED PER SRM ON NON ROUTINE 20008.

Part: STRINGER — BROKEN (FUSELAGE) · airframe 61,795 hrs · 22,878 cycles

MAIN CABIN STRINGER 18L IS BROKEN OUT BETWEEN STA 500L TO 520L. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED STRINGER 18L FROM BS 440 TO BS 660 LT SIDE PER SRM ABD BAC DWG 143N3300. (STRINGER P-N 143N3110-46).

Part: FLOORBEAM — CORRODED (366) · airframe 61,795 hrs · 22,878 cycles

MAIN CABIN FLOORBEAM TEE ATTACH SPLICE CHANNEL CORRODED, BS 366, RBL 56. MAJOR REPAIR ACCOMPLISHED: REMOVED HAT CHANNEL AND FABRICATED A NEW HAT CHANNEL PER BAC DWG 141N5162, REV D AND INSTALLED PER SRM.

Part: FLOORBEAM — CORRODED (BS 366) · airframe 61,795 hrs · 22,878 cycles

MAIN CABIN FLOORBEAM TEE UPPER SURFACE CORRODED BS 366, RBL 5-RBL 56. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF TEE AND FABRICATED AND INSTALLED REPAIR ANGLES AND STRAPS PER SRM ON NON ROUTINE 20493.

Part: CUSP WEB — CORRODED (BS 1400-1420) · airframe 61,795 hrs · 22,878 cycles

MAIN CABIN RT CUSP WEB FROM BS 1400 TO 1420 CORRODED. MAJOR REPAIR ACCOMPLISHED: RT CUSP WEB CORRODED BEYOND LIMITS PER SRM. FABRICATED AND HEAT TREATED A NEW WEB AND INSTALLED PER SRM.

Part: CUSP WEB — CORRODED (BS 1420-1440) · airframe 61,795 hrs · 22,878 cycles

MAIN CABIN RT CUSP WEB FROM BS 1420 TO 1440 CORRODED. MAJOR REPAIR ACCOMPLISHED: RT CUSP WEB WEB CORRODED OUT OF LIMITS PER SRM. FABRICATED AND HEAT TREATED A NEW WEB PER BAC DWG 146N5590 AND INSTALLED PER SRM ON NON ROUTINE 20412.

Part: PAN — GOUGED (R1 DOOR) · airframe 61,795 hrs · 22,878 cycles

R-1 DOOR HANDLE PAN IS GOUGED. REMOVED DAMAGED DOOR PAN AND REPLACED WITH SERVICEABLE HANDLE PAN PER SRM ON NON ROUTINE 20933.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 61,795 hrs · 22,878 cycles

AFT GALLEY FLOORBEAM TEE CORRODED AT BS 1640, RBL 54. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF FLOORBEAM. FABRICATED TWO REPAIR ANGLES PER DWG BAC 5602 AND TWO FILLERS AND A STRAP PER SRM. INSTALLED PER SRM ON NON ROUTINE 20584.

Part: SLIDE — BROKEN (LT OVERWING) · airframe 61,795 hrs · 22,878 cycles

LT OVERWING SLIDE PACKBOARD IS BROKEN AND SEPARATING FROM THE CORNER. REMOVED LT OVERWING SLIDE AND INSTALLED A SERVICEABLE SLIDE PER MM ON NON ROUTINE 20922.

Part: HARNESS — WORN (R1 DOOR SLIDE) · airframe 61,795 hrs · 22,878 cycles

MAIN CABIN R-1 DOOR SLIDE HARNESS IS WORN, TORN AT LOWER BRACKET. REMOVED AND REPLACED MAIN CABIN R-1 DOOR SLIDE HARNESS PER MM.

Part: RADOME — DAMAGED (NOSE) · airframe 61,795 hrs · 22,878 cycles

RADOM DIVIDER STRIPS MISSING IN SPOT R AND SURFACE IS CHIPPED TO EXPOSE COMPOSITE MATERIAL 14 SPOTS. REPLACED AND ADJUSTED RADOME IAW MM.

Part: HARNESS — FRAYED (L4 DOOR SLIDE) · airframe 61,795 hrs · 22,878 cycles

MAIN CABIN L-4 DOOR SLIDE HARNESS IS WORN-FRAYED AT LOWER FITTING. REMOVED AND REPLACED MAIN CABIN L-4 DOOR SLIDE HARNESS PER MM.

Part: DUCT — OBSTRUCTED (A/C SYSTEM) · airframe 61,795 hrs · 22,878 cycles

EXCESSIVE NOISE LEVELS ON FLIGHT DECK, HAVE BEEN FOUND TO BE CAUSED BY DEBRIS BLOCKING AIR CONDITIONING OUTLETS THROUGHOUT THE A/C SYSTEM. DIFFUSER PLATE INSTALLED IN THE OUTBOARD OUTLETS SHOWN IN THE ABOVE REFERENCED IPC AND AMM TRAP THE DEBRIS AND BECOME BLOCKED. REMOVED DEBRIS FROM OUTLETS AND FLEX HOSES IAW MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,795 hrs · 22,878 cycles

MAIN CABIN FLOORBEAM AT STA 1660 CORRODED AROUND FLOORBOARD MOUNT HOLES BL 0 TO LBL 30. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS OF SRM. ORIGINAL MATERIAL THICKNESS IS .125, REMOVED .011, AND REMAINING MATERIAL THICKNESS IS .1 14. ALODINED AND PRIMED PER SRM ON NON ROUTINE 20414.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,787 hrs · 22,876 cycles

FUSELAGE DAMAGED BY JETWAY, APPROXIMATELY 10FT FROM DOOR 1L AT FLOOR LEVEL, 2.5 TO 3.5 FEET LONG, 8 TO 12 IN WIDE.

Part: LIGHT — UNSECURE (CABIN) · airframe 61,590 hrs · 22,797 cycles

EMERGENCY LIGHTING FLOOR STRIP AT ROW 13ABC IS COMING UP. RE-SECURED STRIP COVER TO FLOOR CHANNEL, LIGHT OPS GOOD. ROW 13 IS BULKHEAD FEED TO STRIP CAUSING SLIGHT RISE IN CARPET. NO DEFECTS NOTED. OK PER SMF MM.

Part: DOOR — DAMAGED (LT MLG DOOR) · airframe 61,173 hrs · 22,654 cycles

MAIN GEAR INBD DOOR HEAT SHIELDS HAVE DAMAGE. LT MAIN GEAR STRUT DOOR LWR FWD L/E HAS FOD DAMAGE WITH A SECTION OF L/E PREVIOUS REPAIR BROKEN OFF AT AREA FROM OUTER SKIN TO INNER SKIN WIDE & ABOUT 5" IN LENGTH WITH CORE POTTING MATERIAL GOUGED OUT. REMOVED LT STRUT DOOR & ROUTED TO SHOP FOR REPAIR. R&R R45044. PER SHOP 23DOOR 113N8107-435P, REPAIR IS COMPLETE.

Part: LIGHT — BOWED (CABIN) · airframe 61,064 hrs · 22,609 cycles

EMERGENCY LIGHT STRIP BOWING AT AISLE 13. CHECKED EEL TRACK LIGHTING. ROW 13 IS BULKHEAD FEED TO STRIP CAUSING SLIGHT RISE IN CARPET. NO DEFECTS NOTED. OK PER SMFMM.

Part: SWITCH — MALFUNCTIONED (LT MLG) · airframe 60,979 hrs · 22,577 cycles

LANDING GEAR MONITOR CAME BACK ON ECS MESSAGE PAGE GEAR DOOR MSG DISPLAYED AND PSEU BITE CHECK FAULTS LEFT MLG DOOR CLOSED SENSOR S10242. REPLACED LEFT MAIN GEAR DOOR LOCKED SWITCH S10371, GROUND CHECKED OKAY.

Part: FLOOR SUPPORT — DAMAGED (BS 1660-1680) · airframe 60,814 hrs · 22,514 cycles

CABIN FLOOR CTR LINE, STA 1660 TO 1680 FLOOR STRUCTURE CHANNEL EXFOLIATED. MAJOR REPAIR ACCOMPLISHED: REPLACED WITH NEW FLOOR CHANNEL ON NON ROUTINE WRITE UP K6718C.

Part: STRINGER — CORRODED (BS 1460-1480) · airframe 60,814 hrs · 22,514 cycles

AFT PIT BILGE AREA FUSELAGE STRINGER 29R IS EXFOLIATED FROM STA 1460 TO 1480. ACCOMPLISHED REPAIR IAW EVA-80565A ON OV WU H3917T.

Part: SKIN — DENTED (BS 442) · airframe 59,948 hrs · 22,183 cycles

DENT AFT OF 1L IN LIGHT BLUE STRIPE. 3 DENTS LOCATED APPROX STA 442 AND AFT, BETWEEN STRINGER LT 17 & 18. DENTS 1.25" ROUND X .015"D, 2"ROUND X .015" D, AND 3"ROUND X .031"D. 1ST DENT L/E .5 IN FROM BUTT STRAP REAR ATTACH FASTENER. EXTERNAL VISUAL INSP ACCOMPLISHED AND FOUND TO BE FREE OF ANY SHARP CREASE, CRACKS, GOUGES, OR LOOSE FASTENERS. EVA 80271 TO BE ACCOMPLISHED WITHIN 2 FLT CYCLES. ACCOMPLISHED EXTERNAL HFEC. NO CRACKS FOUND. VISUAL AND HFEC ACCOMPLISHED ON EXTERIOR AND INTERIOR. NO CRACKS FOUND. INSP ACP HFEC REF: CF674 AND CF675 AND FOUND NO CRACKS. IAW EVA-80271 CREATED CF0678 FOR PERMANENT REPAIR WITHIN 100 HRS.

Part: TERMINAL BLOCK — FAULTY (WINDOW HEAT) · airframe 59,467 hrs · 22,006 cycles

FLIGHT DECK WINDOWS 1L AND 1R NEED TO BE REPLACED DUE TO LOOSE TERMINAL BLOCKS AT J5. OPENED CIRCUIT BREAKERS FOR BOTH WINDSHIELD CHANGES. REPLACED 1L & 1R WINDSHIELDS. OK FOR SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,409 hrs · 21,984 cycles

DOOR 2L UPPER DOOR HINGE CUTOUT HAS A 1-8TH INCH CRACK AT BASE OF RADIUS. 1-8TH INCH ABOVE THE CRACK THERE APPEARS TO BE A TEAR IN THE CUTOUT. REPAIRED CRACK TO UPPER HINGE CUTOUT ON DOOR 2 LT, AWAITING REV OF EVA FOR FINAL SIGN OFF. CURRENT EVA UA-EVA-70740-A. ACCOMPLISHED REPAIR PER UA- EVA-80049. HFEC TO BE ACP AT NEXT CK AND IF NO CRACKS ARE FOUND, REPAIR IS TO BE CONSIDERED PERMANENT.

Part: LIGHT — BURNED OUT (DOOR 1L SLIDE) · airframe 58,199 hrs · 21,509 cycles

1L SLIDE LIGHT BURNED OUT. REPLACED LIGHT ASSY. OPS OK.

Part: LIGHT — SHORTED (CABIN) · airframe 57,978 hrs · 21,423 cycles

FLOOR EEL LIGHTING INOP FROM ROW 31 AFT AND IN FRONT OF LAV DOOR. REPLACED MAIN LINE NO HELP, NEW SIDEWALL INVERTER NO HELP, JUMPERED FEEDER CABLE NO HELP, HOOKED UP EXISTING FEEDER CABLE. USED NEW BATTERY & BATTERY CHARGER, NO HELP. LOWER SIDEWALL PANEL IS REMOVED AT SEAT 33ABC. REPLACED SHORTED EEL LAMP. REPLACED BATTERY PACK M735. EMERGENCY LIGHTS CHECK OKAY.

Part: SQUIB — NO TEST (RT OVRWG SLIDE) · airframe 56,151 hrs · 20,718 cycles

TEST 1 FAILED FOR RT OVERWING SLIDE SQUIB. CYCLE RIGHT GROUND ENABLE HANDLE ON P79 AND BOTH SYSTEM, SQUIB TESTED OK.

Part: PANEL — FAULTY (CABIN) · airframe 56,082 hrs · 20,693 cycles

TEST 1 RT OVERWING SLIDE WON'T TEST. REPLACED SQUIB TEST PANEL AND RT OVERWING SQUIB, CHECKS OKAY. INSTALLATION CHECKS GOOD.

Part: SHIM — MISSING (L4 DOOR) · airframe 55,313 hrs · 20,420 cycles

L4 DOOR EMERGENCY POWER BOTTLE LINKS MISSING SHIMS - WASHERS - BINDING TRIGGER LEVER. REPLACED HARDWARE.

Part: SKIN — DENTED (FUSELAGE) · airframe 55,313 hrs · 20,420 cycles

SEVERAL SKIN DENTS STA 600 AND STR 14L- 19L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: ROLL PIN — DAMAGED (R1 DOOR) · airframe 53,784 hrs · 19,833 cycles

NR 1 RIGHT MAIN ENTRY DOOR EMERGENCY POWER TRIGGER LOOSE. REPLACED ROLL PIN.

Part: SQUIB — DIRTY (NR 2 ENGINE) · airframe 52,217 hrs · 19,241 cycles

L ENG NUMBER 2 SQUIB TEST FAIL. SUPPLEMENTAL DATA UPDATE CAUSE, SWITCH S2 WAS DIRTY. CLEANED SWITCH S2 ON M32 PANEL, RESET CIRCUIT BREAKER C786 ON P6 PANEL, SQUIB TEST OK.

Part: SQUIB — NONE (ESCAPE SLIDE) · airframe 51,874 hrs · 19,108 cycles

RIGHT NUMBER ONE EMERGENCY ESCAPE SLIDE DOES NOT TEST ON SQUIB PANEL. TESTED SQUIB 20 TIMES, OPS CHECKS GOOD EVERY TIME.

Part: SIGN — MISSING (CABIN) · airframe 51,401 hrs · 18,949 cycles

RIGHT OVERWING EXITS EMERGENCY EXIT SIGN MISSING. LATCHING MECHANISM NOT WORKING PROPERLY CAUSING THE SIGN TO FALL OUT/OFF. MADE AN INTERIM REPAIR AND INSTALLED A NEW EMERGENCY EXIT SIGN.

Part: OXYGEN MASK — FAULTY (COCKPIT) · airframe 51,349 hrs · 18,932 cycles

CAPTAIN'S O2 MASK WILL NOT DEFLATE & MIC IS INOP. REPLACED CAPT O2 MASK, OPS CHECKED NORMALLY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,413 hrs · 18,589 cycles

FLOOR EEL LIGHTS INOP ROW 9-22. REPLACED BATTERY ON POWER SUPPLY

Part: ENGINE — SHUTDOWN (NR 1) · airframe 50,308 hrs · 18,553 cycles

FLIGHT DIVERTED DUE TO NR 1 ENGINE FOR INFLIGHT SHUTDOWN.

Part: WARNING MESSAGE — ILLUMINATED · airframe 49,166 hrs · 18,142 cycles

THE -L ELEV PCU- STATUS MESSAGE RECEIVED. [08-07-07] FOUND LT INBOARD ELEVATOR POWER CONTROL UNIT FAULTING. REPLACED LT INBD PCU.

Part: UNKNOWN — ODOR (CABIN) · airframe 49,113 hrs · 18,126 cycles

F/A REPORTS STRONG RUBBER BURN ODOR BY DOOR 3R. [07-03-07] FOUND BAD BALLAST FOR AFT GALLEY CEILING LIGHT, DISCONNECTED CONNECTOR AND TIED BACK. BALLAST M10808. FOUND NO OTHER PROBABLE SOURCE IN AREA. PACKS OPERATING NORMAL WITH NO HISTORY OF ODORS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 48,967 hrs · 18,066 cycles

BOTH FWD & AFT LEFT WING EXTERIOR OVERWING AND ROW 2CD BULLNOSE EXIT EMERGENCY LIGHTS ARE INOPERATIVE. RELAMPED EMERGENCY LIGHTS.

Part: WATER HEATER — FAILED (LAVATORY) · airframe 48,820 hrs · 18,011 cycles

NO H2O PRESSURE TO LAVS OR GALLEYS. 1:10 INTO FLT AFT LAV H2O HEATER. AFT LAV, LAV 'R', LAV IS WHERE ACRID ODOR WAS COMING FROM. FOUND WATER HEATER OVERTEMP CONDITION TRIPPED CIRCUIT BREAKER INSIDE HEATER. LAV IS WHERE ACRID ODOR WAS COMING FROM. CB ON PNL P37 WAS COLLARED. ALL OTHER WATERHEATERS HAVE BEEN REACTIVATED. WATER SERVICE PANEL HAD VALVE PARTIALLY OPEN. RESET CB HEATER AND SYSTEM WAS CHECKED NORMAL.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,156 hrs · 14,833 cycles

AFT PIT STA 1420 FRAME DENTED AT STR 25L. DENT CUTOUT AND J ANGLE REPAIR INSTALLED.

Part: TEAR STRAP — CORRODED (FUSELAGE) · airframe 40,156 hrs · 14,833 cycles

AFT PIT TEAR STRAP EXFOLIATED FWD AND AFT SIDE OF STA 1400 BETWEEN STR 27L AND 28L. SPLICE STRAP REPLACED.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,156 hrs · 14,833 cycles

AFT PIT STA 1580 FRAME DENTED AT STR 25R. DAMAGED WAS CUTOUT AND FRAME J ANGLE REPAIR WAS ACCOMPLISHED.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,156 hrs · 14,833 cycles

AFT PIT STA 1340 FRAME DENTED AT STR 25R. TYPICAL AFT PIT FRAME DENT DAMAGE DUE TO CARGO LOADING. FRAME CAP REPAIRED USING "J" ANGLE REPAIR.

Part: SHEAR TIE — CORRODED (FRAME) · airframe 40,156 hrs · 14,833 cycles

BS 1400 AFT PIT FRAME SHEAR TIE CORRODED BETWEEN STR 27L & 28L. DAMAGE CAUSED BY CORROSION. REPLACED FRAME SECTION AND CORRODED SHEAR TIES.

Part: LIGHT — DETERIORATED (CABIN) · airframe 40,156 hrs · 14,833 cycles

EMERGENCY EVACUATION LIGHT STRIP AT LAV AREA DETERIORATED. REPLACED LIGHT STRIP.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,156 hrs · 14,833 cycles

EXTERNAL FUSELAGE STA 736.5 BETWEEN STR 27L AND 28L INTERCOSTAL FASTENER HAS STATIC DISCHARGE HOLE OUT OF LIMITS. REMOVED DAMAGE AND FABRICATED REPAIR DOUBLER FOR SKIN.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,156 hrs · 14,833 cycles

MAIN CABIN STA 324 RS FLOORBEAM CORRODED FROM RBL 40 TO CUSP. REMOVED CORROSION DAMAGE AND INSTALLED FLOORBEAM REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,156 hrs · 14,833 cycles

MAIN CABIN STA 365 FLOORBEAM CORRODED FROM RBL 26 TO RBL 0. REMOVED DAMAGE, FABRICATED AND INSTALLED REPLACEMENT FLOORBEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,156 hrs · 14,833 cycles

STA 365 RBL 58 TO 63 FLOORBEAM CORRODED. REMOVED CORROSION AND INSTALLED REPAIR TO FLOORBEAM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 40,156 hrs · 14,833 cycles

AFT CARGO PIT STA 1620 RBL 3 INTERCOSTAL WEB HAS CORROSION. REMOVED CORROSION, FABRICATED AND INSTALLED NEW INTERCOSTAL WEB.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,156 hrs · 14,833 cycles

MAIN CABIN FLOOR SUPPORT CORRODED STA 1660 TO 1680 AT RBL 50 TO 55. TYPICAL FLOOR CORROSION. REMOVED DAMAGE AND REPLACED THE FLOOR SUPPORT.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 40,156 hrs · 14,833 cycles

FRAME AT BS 1400 STR 26L IS DAMAGED. CARGO PIT FRAME DAMAGE DUE TO CARGO HANDLING. FRAME SECTION REPLACED.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,156 hrs · 14,833 cycles

AFT PIT STA 1440 FRAME DENTED AT STR 25L. INSTALLED J ANGLE REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,156 hrs · 14,833 cycles

RIGHT FWD FUSELAGE DENTED AND SCRATCHED APPROX 1 FT AFT OF JACKING POINT. REMOVED EXISTING TIME-LIMITED SKIN DOUBLER AND REPLACED WITH NEW DOUBLER AND FILLER REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,156 hrs · 14,833 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT STA 1640 TO 1660 LBL 50 TO LBL 55. TYPICAL FLOOR STRUCTURE CORROSION. REPLACED FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,156 hrs · 14,833 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT STA 1660 TO 1680 LBL 50 TO LBL 55. TYPICAL FLOOR STRUCTURE CORROSION. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 40,156 hrs · 14,833 cycles

PUNCTURED HOLE IN FUSELAGE AT STA 1862 UPPER LT SIDE. PUNCTURE DAMAGE. FABRICATED & INSTALLED REPAIR DOUBLER AND FILLER.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,721 hrs · 13,960 cycles

FUSELAGE BS 600L, STRINGER 14L-19L SKIN DENTED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED SKIN SPLICE REPAIR.

Part: ACTUATOR — WORN (SLATS) · airframe 35,239 hrs · 13,016 cycles

WHILE PLACING FLAPS IN UP POSITION, LEADING EDGE SLAT DISAGREE INDICATION CAME ON. INHIBITED SLAT MOVEMENT DUE TO FAULTED NR 11 LEADING EDGE SLAT ACTUATOR. REMOVED AND REPLACED THE SUBJECT LEADING EDGE SLAT ACTUATOR WITH NEW SERVICEABLE ACTUATOR

Part: ACTUATOR — WORN (SLAT) · airframe 35,238 hrs · 13,015 cycles

SLAT DISAGREE INDICATION CAME ON AFTER TAKE-OFF. INHIBITED SLAT MOVEMENT DUE TO FAULTED NR 11 LEADING EDGE SLAT ACTUATOR. REMOVED AND REPLACED THE SUBJECT LEADING EDGE SLAT ACTUATOR WITH NEW SERVICEABLE ACTUATOR

Part: WINDOW — CRACKED (RT COCKPIT)

DIVERTED TO JAX DUE TO CRACKED F/O WINDOW.

Part: FAN — FOD (E & E COMPT)

DIVERTED TO CLE DUE TO AN EQUIPMENT OVERHEAT INDICATION. *S/D* THE OVERHEAT INDICATION WAS TO REMOVE DEBRIS FROM THE EQUIPMENT COOLING FANS. THE SOURCE OF THIS DEBRIS IS PRESENTLY UNDER INVESTIGATION.

Part: O-RING — TORN (LT ENGINE)

LANDED MCI UNDER AMBER ALERT DUE TO LOSS OF LEFT HYDRAULIC FLUID. *S/D* FLUID LEAKING AT TORN O-RING FOUND ON ENGINE HYDRAULIC LINE QUICK DISCONNECT FITTING. REPLACED O-RING.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHT INOP AT RIGHT HAND FORWARD OVERWING DOOR. REPLACED DEFECTIVE LIGHT ASSEMBLY, OPERATION CHECKS NORMAL.