N586UA

Part: SLIDE — UNSECURE (R4 DOOR) · airframe 63,733 hrs · 22,571 cycles

R-4 DOOR SLIDE FELL OUT OF DOOR ONTO THE CATERING TRUCK. REMOVED & REPLACED R4 SLIDE ASSY.

Part: COVER — UNSECURE (EVAC SLIDE) · airframe 63,728 hrs · 22,569 cycles

REPORTED R2 DOOR SLIDE COVER LOOSE. SECURED R2 SLIDE COVER. SLIDE DID NOT FALL OR DISTORT. JUST COVER ON ONE SIDE.

Part: BLADE — CHIPPED (RT ENGINE) · airframe 63,685 hrs · 22,552 cycles

CHIPPED FAN BLADE RIGHT ENGINE. BLADE MARKINGS WORN OFF, LEFT CHIPPED BLADE AT 6 O`CLOCK POSN. BLENDED 2 BLADES ADJACENT TO EACH OTHER REF AMM. BLADES ARE MARKED FOR EDDY CURRENT INSPECTION. DUE TO BLADE REPAIR, NEED EDDY CRNT INSP. CF EDDY CURRENT DUE TO TIME REF AMM 72-31-02 BLADES ARE MARKED. PERFORMED HFEC INSP OF ALL E 2 FAN BLADE LEADING EDGES PER NTM MAN. PART-6-72-31-401 NO DISCREPANT INDICATIONS NOTED.

Part: INSULATION — OUT OF POSITION (R4 DOOR) · airframe 63,441 hrs · 22,464 cycles

DOOR 4R WILL NOT ARM. FOUND INSULATION BINDING UNDER ARM DISARM LEVER. REROUTED AND SECURED INSULATION AND ADJ DOOR ASSY, MED DOOR 4RT, OPS NORMAL.

Part: FEEDER CABLE — INOPERATIVE (CABIN) · airframe 63,431 hrs · 22,459 cycles

EEL LIGHT INOP AT SEAT 8AB. REPLACED FEEDER CABLE, OPS CHECK OKAY.

Part: PLATE — BROKEN (COCKPIT) · airframe 63,415 hrs · 22,452 cycles

FWD AILERON TRIM GUARD ON CTR PEDESTAL BROKEN OFF. REMOVED AND REPLACED RUDDER AILERON TRIM MODULE LIGHT PLATE. ALL LIGHTS AND SWITCHES, OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,370 hrs · 22,439 cycles

EEL STRIP FWD OF 1ST CLASS PARTIALLY INOP. EEL LIGHT STRIP ASSY, CHECKED OKAY.

Part: CABLE — BROKEN (CABIN) · airframe 63,370 hrs · 22,439 cycles

EEL LIGHTING STRIP BROKEN 12 ABC. REPLACED 6 FOOT CABLE AND END CAPS AT ROW 12.

Part: GIRT BAR — DETACHED (R4 DOOR) · airframe 63,252 hrs · 22,397 cycles

MECHANIC REPORTED THE 4R DOOR SLIDE GIRT BAR WAS FOUND DETACHED. MECHANIC RE-ATTACHED BAR TO GIRT AND ATTEMPTED TO CYCLE THE ARM DISARM LEVER AND GIRT BAR FELL OUT AGAIN. INFO FROM OPS WAS THE CATERING PEOPLE HAD PROBLEM OPENING DOOR AND IT APPEARED GIRT CAUGHT ON FLOOR WHILE OPENING DOOR BUT DOOR WAS NOT FULLY OPENED. SECURED SLIDE GIRT BAR AND SKIRT.

Part: DUCT — FAULTED (AFT CABIN) · airframe 62,891 hrs · 22,270 cycles

AFT CABIN WARMER THAN SELECTED WITH SWITCH ON AND TEMP CONTROL IN AUTO INOPERATIVE LIGHT EXISTING. PRESS ECS REC BUTTON AND RECORD ZONE TEMPS. FOUND POSSIBLE OVERHEAD DUCT LEAK AT ROW 14 OR 20. OVERHEAD MONITOR NEEDS TO BE RMV'D FOR FURTHER EVALUATION. AIRFLOW GOOD FWD OF ROW 12, WEAK AFT OF 14. -INF- :NEEDS DUCT REPAIR OR REPLACEMENT RECOMMEND 2 SHIFT FOR FIX. PCN 170-4971. REPLACED DUCT AIR MIX MANIFOLD TEMP SENSOR. OUTLET TEMP SENSORS AND PACK TEMP SENSORS CHECKED GOOD. ACCOMPLISHED INTERIM REPAIR TO DISTRIBUTION DUCT AT ROW 20 ABOVE VIDEO MONITOR TO UPPER PORTION OF PRODUCTION JOINT. ACP PERM RPR. UNABLE TO COOL ENTIRE CABIN. REPLACED TRIM AIR VALVE AS PER AMM, OPS CK IS GOOD AC OK TO CONTINUE.

Part: VALVE — FAULTED (CABIN TEMP) · airframe 62,642 hrs · 22,189 cycles

HARD TO CONTROL COCKPIT, FWD CABIN, AND AFT CABIN TEMP. TROUBLESHOT PER FIM 21-60-00 PG130. REPLACED TRIM AIR MODULATOR VALVE PER MM 21-61-07.

Part: FEEDER CABLE — INOPERATIVE (EMERGENCY LGIHTS) · airframe 62,570 hrs · 22,162 cycles

EMERGENCY LIGHTS INOPERATIVE ROW 8A-12A. REPLACED BROKEN FEEDER CABLE, OPS CHECKED NORMAL.

Part: POWER CABLE — DISCONNECTED (SMOKE DETECTOR) · airframe 62,471 hrs · 22,130 cycles

AFT LAV SMOKE DETECTOR GREEN POWER LIGHT IS NOT ILLUMINATED. FOUND POWER CORD DISCONNECTED. RECONNECTED POWER CORD, PERFORMED TEST. TESTED OK. OPS NORMAL.

Part: KNOB — OUT OF POSITION (CABIN TEMP) · airframe 62,336 hrs · 22,084 cycles

KNOBS FOR AFT CABIN TEMP AND RT PACK ARE REVERSED. PLACED KNOBS IN CORRECT POS.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 62,155 hrs · 22,030 cycles

LEFT EICAS COMPUTER STATUS MESSAGE CAME ON AT POWER CHANGE. WILL NOT CLEAR, CYCLED 'LT EICAS ' CIRCUIT BREAKER, OPS NOW SATISFACTORY.

Part: OXYGEN BOTTLE — USED (SEAT 5AB) · airframe 61,889 hrs · 21,939 cycles

LARGE O2 BOTTLE 5AB USED, REPLACED O2 ROW 5A.

Part: OXYGEN BOTTLE — USED (ROW 20A) · airframe 61,889 hrs · 21,939 cycles

SMALL O2 BOTTLE USED FROM ROW 20ABC, REPLACED O2 ROW 20A.

Part: GIRT BAR — LACK OF LUBE (R4 DOOR) · airframe 61,867 hrs · 21,929 cycles

R4 DOOR IS CLOSED BUT WILL NOT ARM, ADJUSTED AND LUBED GIRT BAR MECHANISM PER AMM 52-11-25. SLIDE ARMS AND DISARMS NORMALLY.

Part: CIRCUIT CARD — FAULTY (RIGHT) · airframe 61,864 hrs · 21,927 cycles

POWER TRANSFER EICAS MESSAGE. REPLACED CIRCUIT CARD S10246, PTU MESSAGE CLEARED, OP CHECKED OKAY.

Part: D-RING — OUT OF ADJUST (L2 DOOR) · airframe 60,679 hrs · 21,524 cycles

RAFT SLIDE SURV KIT ATTACH 'D' RING 2L NEEDS ADJ REPAIRED "D" RING ATTACH POINT PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,604 hrs · 21,501 cycles

CORROSION ON FLOORBEAM AT STA 1640 BL 0 - RBL 62. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION & FOUND BLEND OUT OF SRM LIMITS. CUT OUT DAMAGED UPPER CHORD SECTION OF FLOORBEAM FROM LBL 10 TO RIGHT END OF FLOORBEAM REF PEMCO EA PD57-53-231 & SRM 53-00-51 FIG 201 REPAIR 3. FABRICATED AND INSTALLED NEW FLOORBEAM UPPER CHORD, ANGLES, STRAPS & FILLERS PER EA & SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,604 hrs · 21,501 cycles

AFT DECK AREA AT STA 1681 FLOORBEAM AT RBL 32 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION & FOUND BLEND OUT OF LIMITS OF SRM. CUT OUT DAMAGED AREA & ACP NDT OF OF OPEN HOLES COMMON TO REPAIR AREA FOR CRACKS. NONE FOUND. ACP INSURANCE CUT. FABRICATED & INSTALLED TWO REPAIR ANGLES, A STRAP & FILLER REPAIR PER EA PD57-53-227.

Part: PRESSURE DECK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,604 hrs · 21,501 cycles

CORROSION ON PRESSURE DECK AT STA 1715 - 1720 AT RBL 20-62. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION & FOUND BLEND OUT OF LIMITS OF SRM. REMOVED FASTENERS IN REPAIR AREA & ACP NDT OF OPEN HOLES. NO CRACKS FOUND. FABRICATED & INSTALLED EXTERNAL DOUBLER REPAIR ON AFT DECK UPPER PLATE REF PEMCO EA PD 57-53-232 & SRM 53-60-51 & UA EVA-81489.

Part: PRESSURE DECK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,604 hrs · 21,501 cycles

CORROSION ON PRESSURE DECK FROM 1681-1686 LBL 18 - RBL 62. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION FROM AFT DECK PLATE P/N 146N5318-10 AND FOUND BLEND OUT OF LIMITS OF SRM. ACP NDT FOR CRACKS & PERFORMED INSURANCE CUT ALL PER PEMCO EA57-53-228. ACP NDT OF OPEN HOLES COMMON TO REPAIR. FABRICATED & INSTALLED REPAIR DOUBLER, FILLER, SHIMS & COUNTER SUNK REPAIR WASHERS PER EA & UA-EVA-81487.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,604 hrs · 21,501 cycles

BS 1420-1446 FUSELAGE SKIN REPAIR INCORPORATING AIRFONE ANTENNA DOUBLER REPAIR BETWEEN STRINGERS S-29L & S-30 RECEIVED FIRST STAGE APPROVAL FOR STATIC STRENGTH ONLY. THIS REPAIR WAS ACP PER EA PD57-53-229 & UA-EVA 81494 ON N-R 3550N00031 WITHOUT DEVIATION. REMOVED EXISTING REPAIR DOUBLER & ACP NDT OF OPEN FASTENER HOLES IN REPAIR AREA & ACP INSURANCE CUT. FABRICATED & INSTALLED AN EXTERNAL DOUBLER REPAIR REF PEMCO EA PD57-53-229 & UA EVA-81494.

Part: PCA — LEAKING (RT ELEVATOR) · airframe 60,604 hrs · 21,501 cycles

RT ELEVATOR O/B PCA SHOWS EVIDENCE OF LEAKAGE. REMOVED & REPLACED RT ELEVATOR O/B PCA IAW B757 AMM, OPS CHECK GOOD. NO LEAKS NOTED.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 60,604 hrs · 21,501 cycles

DUE TO A MAJOR REPAIR OF THE BS 324 FLOORBEAM UPPER CHORD DURING HMV 3 VISIT, AN INITIAL FIRST STAGE APPROVAL WAS RECEIVED. THIS REPAIR MUST RECEIVE A NEW 8100-9 SHOWING COMPLAINCE TO 14CFR 25.571 AND 26.43(D) AND DTA INCORPORATED INTO THE AIRCRAFT MAINTENANCE PROGRAM WITHIN 24 MONTHS FROM NOV 3RD 2011 FOR THIS REPAIR TO REMAIN VALID AND AIRCRAFT TO REMAIN AIRWORTHY.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,604 hrs · 21,501 cycles

CORROSION ON FLOORBEAM AT STA 323 RBL 40.5 AND 60.0. MAJOR REPAIR ACCOMPLISHED: CORROSION AT STA 324 RBL 40.5 AND 60 REPAIRED PER INSTRUCTIONS ON EA PD57-53-225 AND UA EVA 81467 WITHOUT DEVIATION. CF CREATED FOR DTA.

Part: SKIN — DENTED (R4 DOOR) · airframe 60,604 hrs · 21,501 cycles

DOOR 4 RIGHT OUTER SKIN HAS A SMALL DENT AT THE FWD EDGE ADJACENT TO THE 3RD DOOR STOP FROM THE BOTTOM. MEASURED DENT AND FOUND TO BE WITHIN LIMITS IAW B757 SRM. NDT HFEC PERFORMED ON DENT AREA IAW B757 NDTM PART 6 AND FOUND NO CRACKS. TREATED, PRIMED AND PAINTED IAW B757 MM. MARKED DENT ON DOOR 4 RIGHT IAW NMOP 002-001-15.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,604 hrs · 21,501 cycles

CORROSION ON FLOORBEAM AT STA 365.25 RBL 5 TO RBL 65. MAJOR REPAIR ACCOMPLISHED: CORROSION IS BEYOND LIMITS PER B757 SRM. REMOVED PART AND FABRICATED A NEW CHORD REPAIR ANGLE 2&3, REPAIR STRAP 4 & 5 IAW B757 SRM. TREATED AND PRIMED ALL PARTS IAW B757 AND TOP COATED IAW B757.

Part: COLLAR — CRACKED (FUSELAGE) · airframe 60,604 hrs · 21,501 cycles

NUMEROUS HI-LOK FASTENER COLLARS CRACKED UNDER DOOR 4 LEFT INTERCOSTALS AT STA 1620-1660. INSTALLED NEW HI-LOK COLLARS. NR 355ON00582.

Part: COLLAR — BROKEN (FUSELAGE) · airframe 60,604 hrs · 21,501 cycles

MAIN CABIN BETWEEN BS 1340 - 1360, STR 17R HAS 1 EA BROKEN HI-LOK COLLAR UPPER SIDE. REMOVED & REPLACED BROKEN HI-LOK COLLAR BY AMT 601259.

Part: COLLAR — BROKEN (FUSELAGE) · airframe 60,604 hrs · 21,501 cycles

MAIN CABIN BETWEEN BS 1440 - 1460, STR 17R HAS 3 EA BROKEN HI-LOK COLLARS. REMOVED & REPLACED BROKEN HI-LOK COLLARS.

Part: COLLAR — BROKEN (FUSELAGE) · airframe 60,604 hrs · 21,501 cycles

HI-LOK FASTENER MISSING THE COLLAR AT STA 1420-1440 STR 17R. REMOVED & REPLACED BROKEN HI-LOK COLLAR.

Part: COLLAR — CRACKED (FUSELAGE) · airframe 60,604 hrs · 21,501 cycles

HI-LOK COLLAR CRACKED AT BS 1600 STR 17L CREASE BEAM. REMOVED & REPLACED BROKEN HI-LOK COLLAR.

Part: COLLAR — BROKEN (FUSELAGE) · airframe 60,604 hrs · 21,501 cycles

MAIN CABIN BETWEEN BS 1380 - 1400, STR 17R HAS 13 EA BROKEN COLLARS UPPER SIDE. REMOVED & REPLACED BROKEN HI-LOK COLLARS BY AMT 601259.

Part: COLLAR — BROKEN (FUSELAGE) · airframe 60,604 hrs · 21,501 cycles

MAIN CABIN BETWEEN BS 1422, STR 17R HAS 1 EA BROKEN HI-LOK COLLAR. REMOVED & REPLACED BROKEN HI-LOK COLLAR.

Part: COLLAR — BROKEN (FUSELAGE) · airframe 60,604 hrs · 21,501 cycles

MAIN CABIN BETWEEN BS 1380 - 1400, STR 17R HAS 1 EA BROKEN HI-LOK COLLAR UNDER WEB. REMOVED & REPLACED BROKEN HI-LOK COLLAR BY AMT 601259.

Part: COLLAR — BROKEN (FUSELAGE) · airframe 60,604 hrs · 21,501 cycles

HI-LOK FASTENERS COLLARS BROKEN ON CREASE BEAM AT STA 1340 - 1360 AT STR 17R. REMOVED & REPLACED BROKEN HI-LOK COLLARS.

Part: COLLAR — BROKEN (FUSELAGE) · airframe 60,604 hrs · 21,501 cycles

MAIN CABIN BETWEEN BS 1400 - 1420, STR 17R HAS 5 EA BROKEN H-LOK COLLARS UNDER WEB. REMOVED & REPLACED BROKEN HI-LOK COLLARS REF SRM.

Part: FASTENER — MISSING (FUSELAGE) · airframe 60,604 hrs · 21,501 cycles

MAIN CABIN BETWEEN BS 1440 RT FLOORBEAM TO FRAME ATTACH POINT HAS 5 EA FASTENERS MISSING. REMOVED & REPLACED BROKEN HI-LOK COLLARS.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 60,604 hrs · 21,501 cycles

LOWER FUSELAGE AT BS 512 BETWEEN STR 28R AND STR 29R IS DENTED AND GOUGED. DENT IS WITHIN LIMITS IAW B757 SRM 53-00-01. GOUGE WAS REMOVED BY DRILLING A .187 DIAMETER HOLE IAW B757 SRM 53-00-01. HFEC INSPECTION REVEALED NO DAMAGE IAW B757 NDTM PART 6 51-00-19. ENLARGED HOLE AND INSTALLED RIVET IAW B757 SRM 53-00-01. TREATED AND PRIMED AREA IAW B757 MM 51-21-04. MARKED REPAIR IAW GNMM 1-0-1-07.

Part: SKIN — GOUGED (RT NACELLE) · airframe 60,386 hrs · 21,422 cycles

SMALL HALF INCH BLEMISH AND POSSIBLE CRACK ON RIGHT NACELLE AFT CORE COWL 10 O'CLOCK POSITION. .375L X .0310D X .5W. PIXS POSTED. OUT OF SRM LIMITS. REPAIRED BLEMISH AT 10 O'CLOCK POSITION NO CRACKS FOUND. CHECKED IAW SRM.

Part: DUCT — DIRTY (CABIN) · airframe 60,357 hrs · 21,409 cycles

ABSOLUTELY NO AIR FLOW FROM CEILING OVERHEAD DISTRIBUTION NOZZLE STARTING AT ROW 30. REFERENCE PREVIOUS HISTORY OF LITTLE TO NO AIRFLOW IN AFT CABIN. CLEANED AFT CABIN OVHD DISTRIBUTION DUCT AND ALL SIDEWALL VENT RISERS USING SIDEWALL DIFFUSER CLEANING TOOL. AIRFLOW TO AFT CABIN GOOD.

Part: STRAP — BROKEN (FLOORBEAM) · airframe 59,730 hrs · 21,180 cycles

ON POST FLT WALK AROUND SCRATCHES ON SIDE OF FUSELAGE LEFT SIDE 10' FWD OF DOOR 2L AT FLOOR LEVEL. ALSO IN NLG TUNNEL FOUND 2 FLOORBEAM STRAPS BROKEN BEAM 365-25 & 377.7. BLENDED SCRATCHES.

Part: CHILLER — FAULTY (GALLEY) · airframe 59,595 hrs · 21,128 cycles

CREW REPORTS FLIGHT ATTENDANT IN FORWARD GALLEY SMELLED AN ACRID ODOR. CREW TURNED OFF THE LIGHTS FOR THE FORWARD GALLEY AND THE SMELL DISSIPATED. DEBRIEFED CABIN CREW UPON ARRIVAL TURNED OFF GALLEY LIGHTS AND CHILLER SMELL DISSIPATED. FOUND WATER IN CHILLER AND DUCTS DUE DRAIN CLOGGED. STRONG ACRID ODOR IN CHILLER COMPARTMENT DF CHILLER INOP.

Part: STRUCTURE — DAMAGED (RT NLG DOOR) · airframe 59,102 hrs · 20,943 cycles

RT FWD NLG DOOR HAS 3 EA HOLES FROM LIGHTNING. REMOVED RT AFT NOSE GEAR DOOR FOR ACCESS TO LIGHTNING STRIKE DAMAGE. ACCOMPLISHED REPAIR PER SRM AND GNMM.

Part: VALVE — LEAKING (NR 1 ENGINE) · airframe 58,671 hrs · 20,784 cycles

FUEL LEAKING FROM NR 1 ENG TURBINE CASE ABOVE FUEL DIVERTER VALVE. FUEL IS DRIPPING FROM M FLANGE ABOVE FUEL DISTRIBUTION VALVE. WHILE BORO COMBUSTOR. FUEL NOT DRIPPING FROM SPRAY END. FUEL IS IN COLD SIDE BETWEEN CASE AND OUTER LINER. RAN ENG STILL LEAKS. NEED TO GO IN WITH FLEX SCOPE AND TRY TO ID POSSIBLE BAD NOZZLE ON BULKED SIDE. REPLACED FUEL DIST VLV NR 2 ENG, NO HELP. WENT BACK IN LOWER IGNITER PLUG FOUND FUEL DRIPPING FROM NOZZLE AROUND 6 O'CLOCK ONE DOWN FROM LOWER IGNITER, HOLE. DISCONNECTED NOZZLE LINE. FUEL COMING FROM LINE FROM DIST VALVE. RAN ENG NO LEAK RUNNING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,139 hrs · 20,582 cycles

RIGHT LAV EMERGENCY LIGHT STRIP INOPERATIVE. REPLACED EMERGENCY LIGHT STRIP IN FRONT OF K LAV. OPS CHECKED GOOD.

Part: LAMP — FAULTY (EMERGENCY LIGHT) · airframe 57,482 hrs · 20,332 cycles

P62 PANEL S10035 EMERGENCY LIGHT TEST SWITCH NOT TURNING ON EMERGENCY LIGHTS. REPLACED EXTERNAL EMERGENCY LIGHT LAMP, OPS GOOD.

Part: COVER — BROKEN (EMERGENCY LIGHTS) · airframe 57,423 hrs · 20,312 cycles

EMERGENCY LIGHT STRIP AT FWD AFT LAV BROKEN. REPLACED MISSING EMERGENCY TRACK COVER.

Part: SKIN — PEELING (RT ELEVATOR) · airframe 57,264 hrs · 20,258 cycles

RIGHT ELEVATOR UPPER SURFACE SKIN PEELING BACK. ACCOMPLISHED INTERIM REPAIR. COMPLETED REPAIR AT 1730 REFINISH. REPAIR ACCOMPLISHED PER MM. THIS REPAIR IS OKAY TO CONTINUE UNTIL CCH. ACCOMPLISHED PER SFOEG.

Part: GUARD — OUT OF TOLERANCE (DOOR) · airframe 57,258 hrs · 20,256 cycles

DOOR 1 EVAC ALARM SWITCH COVER DOES NOT SPRING CLOSED. REPLACED SWITCH GUARD.

Part: BATTERY — FAULTY (MASTER) · airframe 56,228 hrs · 19,879 cycles

MAIN BATTERY CHARGER EICAS. MAIN BATTERY HOT. MAIN BATTERY NOT CHARGING. R & R MAIN SHIPS BATTERY AND BATTERY CHARGER.

Part: ATTACH ANGLE — CORRODED (CARGO BAY) · airframe 56,069 hrs · 19,817 cycles

FOUND CORROSION, AFT PIT FLOOR, CARGO NET TIE DOWN, JUST FWD OF CARGO DOOR OPENING. STARTED REMOVING CORROSION PANEL, CARGO FITTING TIE DOWN OK, NEED TO REMOVE FLOOR PANEL FOR ACCESS TO 'Z' ANGLE. REPLACED 'Z' ANGLE AND SPLICE ANGLES FROM STA 1440-1480. REPLACED 'Z' ANGLE FROM STA 1310-1380. REPLACED 'Z' ANGLE STA 1380-1440. REPLACED TIE DOWN AND REINSTALLED FLOOR PANEL.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 56,010 hrs · 19,797 cycles

LAST SECTION OF EMERGENCY LIGHT IN AFT CABIN DOESN'T LIGHT UP AND THE LAST 8 IN OF COVER IS MISSING. SECURED LOOSE CONNECTOR. OPS CHECK OK.

Part: BOTTLE — LOW (CREW OXYGEN) · airframe 55,863 hrs · 19,746 cycles

CREW O2 LOW. 1340, BEFORE SERVICING. SERVICED TO NORMAL.

Part: SKIN — DENTED (BS 617 S17L) · airframe 55,200 hrs · 19,492 cycles

MIN DENT ON FUSELAGE LOCATED AT STA 617 CREASE BEAM (I.D. STR 17) (FWD OF DOOR 2L). MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE, ACP HEFC INSP ON CUTOUT, NO CRACK FOUND, ACP REPAIR. MAJOR REPAIR.

Part: SLIDE — DISLODGED (RT OVERWING) · airframe 55,200 hrs · 19,492 cycles

RT OVERWING SLIDE ASSY UNPACKED. REMOVED AND REPLACED RT OVERWING SLIDE ASSY.

Part: SKIN — GOUGED (BS 463) · airframe 55,200 hrs · 19,492 cycles

EXTERNAL SKIN GOUGED, FWD OF MAIN EQUIPMENT CTR ACCESS DOOR, BS 463. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. ACP HFEC INSP. FABRICATED & INSTALLED DOUBLER REPAIR.

Part: STRUCTURE — DELAMINATED (THRUST REVERSER) · airframe 55,200 hrs · 19,492 cycles

NR 2 ENG REVERSER UPPER BI-FURCATION IS DELAMINATED. APPROX 300 SQUARE INCHES FWD END GOING AFT (MARKED) ACCOMPLISHED TIME LIMITED BACK SHEET REPAIR IAW MM-78-31-93. REPAIR INSTALLED MEASURES APPROX 280 SQ INCHES. IAW MM PG 803: REPAIR TO BE RE-CHECKED AT NEXT C-CHECK. IF C-CHECK FINDS FURTHER DELAMINATION BUT LESS THAN 330 SQ INCHES, FOUND PANEL DISBONDING BEYOND REPAIRED DOUBLER. MEASURED DISBONDED AREA EQUAL TO 380 SQ INCHES . BI-FURCATION PANEL NEEDS TO BE REPLACED IN SMB 094972 CURRENT CF9046 PERMITS TO RE-CF ADDITIONAL 300 HRS TO ALLOW TIME TO HAVE SPARE AVAILABLE. ENGINE CONTROLLER HAS BEEN CONTACTED. OK TO CREATE ANOTHER CF TO ACTIVE THE 300 HRS REPAIR LIMIT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,200 hrs · 19,492 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. LAMP FOUND DEFECTIVE. RELAMPED R2 DOOR EXIT LIGHT. OPS CHECK OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,200 hrs · 19,492 cycles

R1 DOOR EXTERIOR SLIDE EMERGENCY LIGHT IS INOP. RELAMPED R1 DOOR EXT SLIDE EMERGENCY LIGHT AND OPS CHECK.

Part: OXYGEN MASK — DEFECTIVE (COCKPIT) · airframe 54,961 hrs · 19,404 cycles

#2 OXYGEN MASK MIKE IS INOP. SUPPLEMENTAL DATA UPDATE MASK ASSY FOUND DEFECTIVE. REPLACED 1ST OFFICER'S OXY MASK ASSY. OP CHKS NORMAL.

Part: MONITOR — FAULTY (AFT CABIN) · airframe 54,824 hrs · 19,355 cycles

BURNING RUBBER ODOR NOTED IN AFT CABIN. FOUND COMING FROM 2ND TO LAST OVERHEAD MONITOR. DEACTIVATED OVERHEAD VIDEO SYS. REPLACED MONITOR AFT 2ND TO LAST AND CHECKED OKAY.

Part: SLIDE — READS LOW (DOOR 3R) · airframe 53,809 hrs · 18,960 cycles

ESCAPE SLIDE PRESSURE AT DOOR 3R IS LOW. SLIDE NEEDS TO BE REPLACED. REPLACED DOOR SLIDE 4R.

Part: GIRT BAR — OBSTRUCTED (L3 DOOR) · airframe 52,725 hrs · 18,544 cycles

DOOR 3L WILL NOT ARM. REMOVED TRASH FROM GIRT BAR.

Part: LANYARD — OUT OF POSITION (L3 DOOR) · airframe 51,915 hrs · 18,232 cycles

DOOR 3L WON'T ARM. *S/D* REMOVED LANYARD AROUND GIRT BAR AND REPOSITIONED.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 50,866 hrs · 17,826 cycles

DOOR 2L SLIDE DISLODGED FROM MOUNT. REINSTALLED DOOR 2L SLIDE.

Part: CONTACT — DIRTY (EXTERIOR) · airframe 49,620 hrs · 17,385 cycles

EXTERIOR EMERGENCY LIGHT INOP AT DOOR 1R AND DOOR 4R. LIGHT ASSY CONTACTS DIRTY. CLEANED LIGHT ASSY CONTACTS, OPS CHECKED OK.

Part: GIRT BAR — OBSTRUCTED (DOOR 1L) · airframe 49,530 hrs · 17,351 cycles

DOOR 1L WON'T ARM. FOUND VELCO D-RING NOT SECURED AND CAUGHT IN DOOR GIRT BAR. RESECURED D-RING, DOOR ARMS/DISARMS NORMALLY.

Part: FAN — SMOKE (LT RECIRCULATION) · airframe 49,439 hrs · 17,319 cycles

THERE IS SMOKE IN THE COCKPIT, PACKS WERE OFF AND GROUND AIR WAS ON. TURNED OFF UTILITY BUSS AND RECIRCULATION FANS. SMOKE WENT AWAY. FOUND BAD PART OUT OF STOCK (INSTALLATION OF CABIN AIR RECIRCULATION FAN (LEFT) ) BEARING FAILURE. REINSTALLED CABIN AIR RECIRCULATION FAN (LEFT)

Part: SOCKET — CORRODED (EMERGENCY LIGHTS) · airframe 48,180 hrs · 16,843 cycles

EXTERIOR EMERGENCY LIGHTS AT DOORS 1R & 4R ARE INOP.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 47,393 hrs · 16,546 cycles

ESCAPE PATH LIGHTING INOPERATIVE FROM ROW 9 TO 13. SECURED EEL CONNECTION AT 13A. NO COMPONENTS REPLACED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,249 hrs · 16,496 cycles

EXTERIOR EMERGENCY LIGHTS INOP AT DOORS 2L, 4L AND 4R.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,249 hrs · 16,496 cycles

EEL LIGHTS INOP FROM ROW 9 - ROW 12. RECONNECTED.

Part: TRACK — DIRTY (DOOR 3L ARMING) · airframe 46,913 hrs · 16,379 cycles

F/A REPORTED DOOR 3L WAS HARD TO ARM, ARMING LEVER VERY STIFF. [08-08-07] REMOVED DEBRIS FROM ARMING TRACK. OPERATION IMPROVED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,815 hrs · 16,340 cycles

SLIDE LIGHT AT 4L BURNT OUT. OPERATED ARM AND DISARM HANDLE AT DOOR 3L. SLIDE LIGHT CAME ON WHEN ARMED AND WENT OFF WHEN DISARMED. COULD NOT DUPLICATE PROBLEM.

Part: GIRT BAR — CONTAMINATED (4R DOOR) · airframe 44,439 hrs · 15,470 cycles

FWD GIRT AT DOOR 4R HAS COME LOOSE, RAFT IS FALLING SLIGHTLY AND CAN`T GET GIRT TO ALIGN PROPERLY TO ENGAGE. FWD GIRT AT DOOR 4R HAS COME LOOSE, SLIDE RAFT FELL OUT OF POSITION SLIGHTLY. COULD NOT GET GIRT TO ALIGN PROPERLY TO ENGAGE. FOUND GIRT BAR NOT ENGAGED ON FWD SIDE. CLEANED DEBRIS FROM AREA

Part: INDICATOR — FAILED (AIRSPEED) · airframe 43,951 hrs · 15,290 cycles

RETURNED TO IAD DUE TO THE CAPTAIN AIRSPEED INDICATION PROBLEM. ATTRIBUTED TO A FAILED MACH AIR SPEED INDICATOR. REPLACED INDICATOR.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 39,650 hrs · 13,730 cycles

AFT PIT STA 1420 RBL 26, CARGO DOOR THRESHOLD T-CAP REPAIR FILLER CORRODED AT THRESHOLD FORMING HORN. INSTALLED NEW T CAP AND REPLACED FILLER.

Part: DOOR FRAME — CORRODED (R4 DOOR) · airframe 39,647 hrs · 13,729 cycles

DOOR R4 FWD FRAME AT STA 1645 IS CORRODED. REPAIR CONSISTED OF REMOVING CORROSION AND INSTALLING 0.032 REPAIR DOUBLER AS OUTLINED IN REPAIR DOCUMENT.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 39,647 hrs · 13,729 cycles

AFT PIT LWR BILDGE, BETWEEN STA 1440-1460, STRINGER 29L IS CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED SECTION OF CORRODED STRINGER AND SPLICED IN NEW STRINGER SECTION.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,647 hrs · 13,729 cycles

AFT PIT FRAME DENTED STA 1420 BETWEEN STR 25 & 26 LEFT. DAMAGE WAS CUTOUT OF FRAME AND REPAIR ANGLES INSTALLED.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,647 hrs · 13,729 cycles

AFT PIT FRAME DENTED STA 1440, STR 26L. FRAME DENT WAS TRIMMED OUT AND J ANGLE REPAIR INSTALLED.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,647 hrs · 13,729 cycles

AFT PIT FRAME DENTED STA 1560, STR 26L. FRAME DENT WAS TRIMMED OUT AND J ANGLE REPAIR INSTALLED.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,647 hrs · 13,729 cycles

FWD PIT FRAME DENTED STA 600, STR 24L. FRAME DENT WAS TRIMMED OUT AND J ANGLE REPAIR INSTALLED.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,647 hrs · 13,729 cycles

AFT PIT FRAME DENTED STA 1560, STR 26R. FRAME DENT WAS TRIMMED OUT AND J ANGLE REPAIR INSTALLED.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,647 hrs · 13,729 cycles

AFT PIT FRAME DENTED STA 1540, STR 26L. FRAME DENT WAS TRIMMED OUT AND J ANGLE REPAIR INSTALLED.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,647 hrs · 13,729 cycles

AFT PIT FRAME DENTED STA 1460, STR 26L. FRAME DENT WAS TRIMMED OUT AND J ANGLE REPAIR INSTALLED.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,647 hrs · 13,729 cycles

AFT PIT FRAME DENTED STA 1480, STR 25L. FRAME DENT WAS TRIMMED OUT AND J ANGLE REPAIR INSTALLED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,647 hrs · 13,729 cycles

CIRCUMFERENTIAL FRAME SHEAR TIE CORRODED AT STA 1460, BETWEEN STR 27L AND 28L. FABRICATED AND INSTALLED A NEW SHEAR TIE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,647 hrs · 13,729 cycles

FLOORBEAM AT STA 324, RBL CORRODED. FLOORBEAM TEE WAS TRIMMED TO REMOVE CORROSION AND REPAIR ANGLES AND STRAPS WERE SPLICED TO REPAIR THE FLOORBEAM UPPER CAP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,647 hrs · 13,729 cycles

FLOORBEAM AT STA 1640, RBL 60 IS CORRODED. FLOORBEAM WAS BLENDED TO REMOVE CORROSION AND REPAIR STRAP INSTALLED ON THE FLOOR BEAM UPPER CAP.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,647 hrs · 13,729 cycles

CIRCUMFERENTIAL FRAME SHEAR TIE CORRODED AT STA 1480 + 3 INCHES LEFT OF STR 30. FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,647 hrs · 13,729 cycles

AFT CABIN FLOORBEAM UPPER CAP IS CORRODED AT STA 1661 RBL 60. CORROSION WAS REMOVED AND A STRAP REPAIR WAS INSTALLED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,921 hrs · 12,473 cycles

DOOR 1R EMERGENCY EXTERIOR LIGHT INOPERATIVE. RELAMPED, OPS CHECK NORMAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 35,101 hrs · 12,187 cycles

DENT AFT AND LOWER OF DOOR 3R. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.

Part: HEATER — OVERHEATED (WATER) · airframe 25,588 hrs · 8,732 cycles

ELECTRICAL ODOR IN FORWARD CABIN DUE TO WATER HEATER OVERHEATING.

Part: HANDLE — BROKEN (LIFE RAFT DOOR)

AT DEPARTURE CHECK, FLIGHT CREW DISCOVERED AFT RAFT OPEN LOCK HANDLE BROKEN. *S/D* CAUSE NOT DETERMINED. ACCOMPLISHED INTERIM REPAIR. OPERATIONAL CHECK OF HANDLE WITH INTERIM REPAIR OK. REPLACED HANDLE AT NEXT MAINTENANCE OPPORTUNITY.

Part: LIGHT — INOPERATIVE (CABIN)

EEL LIGHT STRIP INOP AT AFT LAV LT AISLE. REPLACED EEL STRIP.

Part: LIGHT — INOPERATIVE (CABIN)

EEL LIGHTS INOP ROWS 1 AND 2. INSTALLED NEW LIGHT STRIP, OPS CHECKS NORMAL.

Part: WIRE — SEVERED (CABIN)

EMERGENCY EXIT LIGHTING AT THE MID LAV AREA INOP. REPAIRED SEVERED PIGTAIL ON EMERGENCY EXIT LIGHT, OPERATION CHECKS NORMAL.

Part: AIR DISTR — ODOR (CABIN)

ODOR NOTICED MAIN CABIN DURING POWER CHANGES. MOST NOTICEABLE DURING TRANSITION FROM CRUISE TO IDLE.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS ROW 16L, 18L INOP. EMERGENCY EGRESS LIGHTING ROWS 16-23 INOP. BATTERY PACK FAILED. REPLACED BATTERY PACK. OPERATION CHECKS NORMAL.

Part: LAMP — FAILED (CABIN)

EMERGENCY LIGHT ROW 24R INOP. RELAMPED EMERGENCY LIGHT ROW 24R, OPERATION NORMAL.