N558UA

Part: WINDOW FRAME — UNSECURE (CABIN) · airframe 69,865 hrs · 25,583 cycles

3A INNER WINDOW FRAME FELL OUT. SECURED INNER WINDOW FRAME IN PLACE. SHADE OPERATIONS CHECKED NORMAL.

Part: LIGHT — LOOSE (CABIN) · airframe 69,282 hrs · 25,396 cycles

EMERGENCY EXIT LIGHT STRIP LOOSE ROW 12-12 LT SIDE. LIGHT STRIP AT ROW 12 THRU 13 REINSTALLED & SECURED, OPERATIONS CHECKED GOOD.

Part: RELIEF VALVE — LEAKING (HYDRAULIC SYS) · airframe 69,186 hrs · 25,362 cycles

HYD FLUID RUNNING OUT OF FS COMPARTMENT JUST FWD FOR APU DOORS. FOUND PRESSURE RELIEF VALVE ABOVE HORIZONTAL STAB LT SIDE LEAKING BETWEEN FITTING & VALVE HOUSING.

Part: HEADSET — FAULTY (COCKPIT) · airframe 68,843 hrs · 25,243 cycles

NR 01 BOOM MIKE IS DEFECTIVE.(01=CAPT, 02=1ST OFF, 03=1ST OBS). SPARE MINITEL USED. REPLACED HEAD SET OPERATION CHECKED NORMAL

Part: CIRCUIT CARD — FAILED (LT A/C PACK) · airframe 68,603 hrs · 25,165 cycles

LEFT PACK ISSUE, FLT DIVERTED. CABIN TEMPERATURE DIFFICULT TO CONTROL. PRESSURIZATION FLUCTUATES ALSO ON RT PACK ONLY. REPLACED M284 FLOW CONTROL CARD AND PACK OVERHEAT SWITCH ON RT PACK. OPERATIONAL CHECK GOOD ON GROUND.

Part: CIRCUIT CARD — FAILED (TEMP) · airframe 68,594 hrs · 25,162 cycles

CABIN AND FLT DECK TEMP WENT FULL COLD AFTER TAKEOFF. TURNING TRIM AIR OFF, STABILIZED TEMPS. REPLACED M284 FLOW CONTROL CARD & PACK OVERHEAT SWITCH ON RT PACK. OPS CHECKED GOOD ON GROUND. TURNING TRIM AIR OFF STABILIZED TEMPS. REPLACED TEMP BULB, REPLACED OF CRACKED DUCT. RAN LEFT PACK, OPS NORMAL.

Part: BLADE — BENT (NR 2 ENGINE) · airframe 68,508 hrs · 25,134 cycles

ON WALK AROUND, NR 2 ENGINE BLADE FOUND BENT AT LOCATION MID SPAN AREA. FOUND AREA WITHIN LIMITS. BEND IS SMOOTH AND CONTOUR.

Part: INDICATOR — FAULTY (FUEL QTY) · airframe 68,394 hrs · 25,102 cycles

COCKPIT AND WING FUEL PANELS HAVE NO POWER, FUEL QTY BITE STATUS MESSAGE ON EICAS. REPLACED FQIS PROCESSOR DUE TO SEVERAL FAULTS. FOUND RT WING QTY GAUGE SHORTED. REPLACED RT FUEL QTY INDICATOR AT REFUELING PANEL AND OPS CHECKED GOOD.

Part: STRUT — OUT OF ADJUST (NLG) · airframe 68,366 hrs · 25,091 cycles

NOSE WHEEL HAS A VERTICAL OSCILLATION DURING TAXI ABOVE 10 KNOTS. FOUND STRUT "X" DIMENSION HIGH, ADJUSTED TO PROPER LEVEL IAW AMM 12-51-02.

Part: PANEL — DAMAGED (NR 1 NACELLE) · airframe 68,018 hrs · 24,982 cycles

FAIRING AFT OF NR 1 ENGINE, UNDER WING HAS DAMAGE. DAMAGE IS TO ENGINE AFT FAIRING PANEL MEASURES 1.25" LONG BY 1" DEEP. FAIRING REMOVED AND REPAIRED. INSTALLED AND SEALED PANEL.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 67,848 hrs · 24,929 cycles

DURING DESCENT AND APPROACH, ELECTRICAL FIRE ODOR IN COCKPIT, NO ODOR IN CABIN. NO DEFECTS NOTED. AMM 05-51-56.

Part: STABILIZER — DAMAGED (LEFT) · airframe 67,599 hrs · 24,855 cycles

LEFT STABILIZER HAS DAMAGE. REPAIRED IAW ECRA 5510-02283 FROM STEP 1 THRU 9.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 67,498 hrs · 24,822 cycles

LEFT AFT OVERWING EMERGENCY LIGHT INOP. REPAIRED L562 LIGHT ASSY FOR BROKEN CONTACT-TAB REPLACED M10770 BATTERY CHARGER FOR NO OUTPUT FROM PIN 9. LEFT AFT OVERWING EMERGENCY LIGHT, OPS CHECK OK.

Part: OXYGEN MASK — DEFECTIVE (COCKPIT) · airframe 67,403 hrs · 24,792 cycles

OXYGEN MASK DEFECTIVE AT1.(1=CAPT,2=1ST OFF,3=1ST OBS) SWAPPED CAPT AND 1ST OBSERVER O2 MASK OPS CHECKS 1ST OBSERVER SEAT PLACED INOP. REPLACED OBSERVERS MASK. LEAK AND OPS CHECK NORMAL.

Part: CAP — MISSING (SLIDING WINDOW) · airframe 67,299 hrs · 24,760 cycles

MISSING 2 CAPS ON F/O SLIDING WINDOW HEATING ELEMENTS. INSTALLED CAPS.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 67,266 hrs · 24,748 cycles

NUMEROUS BULLNOSE EMERGENCY LIGHTS DO NOT ILLUMINATE DURING TESTING. REPLACED FUSE IN POWER SUPPLY AT BS 705 IAW AMM. REPLACED BULBS AISLES 37,38,39,40 IAW AMM, OPS CHECKED GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 67,266 hrs · 24,748 cycles

PROTRUDING DENT IN EXTERIOR FUSELAGE SKIN AT BS 585, 3.5 INCHES ABOVE STR 18L. REPAIRED EXTERIOR FUSELAGE SKIN AT BS 585 3.5 INCHES ABOVE STR 18L IAW TIMCO REO-MO597 AND ECRA 5331 01682 PART 1.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 67,266 hrs · 24,748 cycles

PROTRUDING DENT ON EXTERIOR FUSELAGE REPAIR DOUBLER AT BS 589.5, 1.5" ABOVE STR 18L. HFEC - NO CRACKS NOTED. REPAIRED EXT FUSELAGE SKIN AT BS 589.5, 1.5' ABOVE STR 18L IAW ECRA 5331-01682 PART 1.

Part: SKIN — DENTED (LT HORIZ STAB) · airframe 67,266 hrs · 24,748 cycles

LEFT HORIZONTAL STAB LWR SKIN HAS 2 DENTS AT FS STA 155 .849 -14. REPAIRED 2 DENTS ON LEFT HORIZONTAL STAB LOWER SKIN AT FS STA 155. CUT OUT SKIN, REPAIRED IAW B757-200 SRM 51-70-10 REPAIR 4 FIGURES 201 AND 209.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 67,266 hrs · 24,748 cycles

MAIN CABIN FLOOR SUPPORT WEB UPPER ATTACH ANGLE HAS A CRACK ABOUT 1' LONG, BS 1590 BL 0. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED MAIN CABIN FLOOR SUPPORT WEB UPPER ATTACHMENT ANGLE BS 1590 BL 0 IAW B757-200 SRM 51-40-02 PARA 4 AND 7D, FIG 8 AND 12.

Part: SUPPORT — BROKEN (FUSELAGE) · airframe 67,266 hrs · 24,748 cycles

BS 1380 RBL 45 STR 18 INSIDE, JUST FORWARD OF AFT CARGO DOOR, CEILING SUPPORT IS BROKEN. REPAIRED AFT CARGO COMPARTMENT CEILING SUPPORT AT BS 1380 RBL 45 STR 18 IAW ECRA 5315-01058 AND TIMCO NR 20797.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,266 hrs · 24,748 cycles

CABIN FLOORBEAM ATT STA 1640 UPPER CAP IS CORRODED FROM BL-0 8' LEFT AND 12' RIGHT. NOTE - PREVIOUS REPAIR IN PLACE. MAJOR REPAIR ACCOMPLISHED. HFEC NO CRACKS NOTED. REPLACED CABIN FLOORBEAM 1640 UPPER CAP LBL 12 TO RBL 55 AND REPAIRED FLOORBEAM.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 67,266 hrs · 24,748 cycles

EMERGENCY LIGHTING, LIGHT OVER RIGHT SIDE OVERWING, EXIT SIGN FORWARD OF L2 DOOR IS INOP. RESEATED CONNECTOR AT POWER SUPPLY AT STA 985R IAW B757 AMM. OPS CHECKED GOOD IAW B757 AMM. EMERGENCY LIGHTING OVER RIGHT SIDE OVERWING, EXIT SIGN FORWARD OF L2 DOOR OPS CHECKS GOOD IAW B757 AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 67,266 hrs · 24,748 cycles

SEAT TRACKS LIGHT BROKE BS 530 LBL 1.2. REMOVED AND REPLACED SEAT TRACK LIGHT AT BS 530 LBL 12 IAW B757 AMM 33-51-11, OPS CHECK GOOD.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 67,266 hrs · 24,748 cycles

LIGHTNING STRIKE ON AFT CARGO DOOR SKIN BS 1435 AND 20.5 INCHES ABOVE BOTTOM OF DOOR. REPAIRED LIGHTNING STRIKE DAMAGE ON AFT CARGO DOOR SKIN BS 1435 AND 20.5 INCHES ABOVE BOTTOM OF DOOR IAW B757-200 SRM 52-30-01 FIG 201 REPAIR ACCOMPLISHED.

Part: SKIN — DENTED (FUSELAGE) · airframe 67,266 hrs · 24,748 cycles

PROTRUDING DENT ON EXTERIOR FUSELAGE REPAIR DOUBLER AT BS 592, 1.5" STR 18L. REPAIRED BY REPLACING DOUBLER IAW ECRA 5331-01682.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,266 hrs · 24,748 cycles

BS 1640 RBL 7 TO RBL 60 HAS SOME SCRIBE MARKS AND CORROSION ON NUMEROUS HOLES. MAJOR REPAIR ACCOMPLISHED. HFEC NO CRACKS. REPLACED UPPER CAP OF FLOORBEAM AND REPAIRED IAW ECRA 5365-01071 AND TIMCO NR 20472.

Part: SKIN — DENTED (FUSELAGE) · airframe 67,266 hrs · 24,748 cycles

DENT IN FUSELAGE SKIN BS 1697.25, 1 INCH BELOW STR 20L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FUSELAGE SKIN AT BS 1681 TO BS 1720 STR 18L TO STR 21L IAW EC-RA 5361-01033. WORK ACCOMPLISHED ON TIMCO NR 20011.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 67,266 hrs · 24,748 cycles

LIGHTNING STRIKE AFT CARGO DOOR SKIN BS 1435, 20.5 INCHES ABOVE BOTTOM OF DOOR. REPAIRED LIGHTNING STRIKE DAMAGE ON THE AFT CARGO DOOR SKIN BS 1435 AND 20.5 INCHES ABOVE BOTTOM OF DOOR IAW SRM.

Part: SKIN — DENTED (BS 702) · airframe 67,266 hrs · 24,748 cycles

LOWER FUSELAGE SKIN BS 702 HAS A SHARP DENT BETWEEN S28-29R. HFEC INDICATES NO CRACKS. REPAIRED SKIN IAW SRM 53-00-01 FIG 201. DENT FOUND OUT OF ALLOWABLE LIMITS IAW SRM 53-00-01 FIG 101 DETAIL III.

Part: SKIN — DENTED (FUSELAGE) · airframe 67,266 hrs · 24,748 cycles

FUSELAGE SKIN DENTED JUST BELOW FORWARD PASSENGER WINDOW ON LEFT SIDE. ACCOMPLISHED INSPECTION IAW ECRA 5300-01 46 PART 2. FASTENER SECURE AND NO CRACKS PRESENT. REMOVED FASTENERS AT DENTED AREA STR 15L BS 398, IAW SRM 51-40-02, FOUND DAMAGE TO BE CONTAINED TO S15L DENTED, REPAIRED DAMAGE STRINGER IAW SRM 53-00-03 FIG 201.

Part: WEDGE — DENTED (NR 2 SLAT) · airframe 67,266 hrs · 24,748 cycles

NR 2 SLAT TRAILING EDGE WEDGE UPPER SURFACE DENTED. REPAIRED DENT IAW SRM 51-70-10, REPAIR 3 & 4 FIGURE 201. MAJOR REPAIR.

Part: WEDGE — DENTED (NR 2 SLAT) · airframe 67,266 hrs · 24,748 cycles

NR 2 SLAT TRAILING EDGE WEDGE UPPER SURFACE DENTED. REPAIRED DENT IAW SRM 51-70-10, REPAIR 3 AND REPAIR 4 FIGURE 201. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,266 hrs · 24,748 cycles

THIS ITEM IS RII FOR MAJOR REPAIR FOR FLOORBEAM T-CAP. REPAIR ACCOMPLISHED PER ECRA 5330-04259 AND INSPECTED. CABIN FLOORBEAM UPPER CAP AT STA 1681 HAS CORROSION ON UPPER SKIN FROM BL 0 30" RIGHT. REPLACED CABIN FLOORBEAM CAP AT STA 1681 AND REPLACE DOUBLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,266 hrs · 24,748 cycles

CORROSION ON FLOORBEAM BS 364.5 RBL 31. MAJOR REPAIR ACCOMPLISHED. FOUND TO BE OUT OF LIMITS PER SRM 53-00-51 FIG 101 REMOVED & REPLACED FLOORBEAM REPAIR T-CAP LBL 10 TO RBL 65 IAW ECRA 5310-05536, REPAIR 3, FIG 2 AND 3.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,266 hrs · 24,748 cycles

BS 1681 RBL 50 TO 55, CORROSION ON PRESSURE DECK RUNNING UNDER GALLEY FITTING. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION ON DOUBLER FOUND TO BE OUT OF LIMITS IAW ECRA 5330-04259. REMOVED AND REPLACED DOUBLER IAW ECRA 5330-04259.

Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 67,266 hrs · 24,748 cycles

CABIN FLOORBEAM UPPER TEE AT BS 1681 HAS CORROSION FROM BL 0 - RBL 30 . REPLACED CABIN FLOORBEAM TEE.

Part: SKIN — DAMAGED (BS 760, S2L) · airframe 67,266 hrs · 24,748 cycles

LIGHTNING STRIKE AT BS 760, STR 2L. ACCOMPLISHED REPAIR IAW EVA 805 28 AND EA PD57-53-074.

Part: CONTACTOR — DIRTY (GIRT BAR) · airframe 67,252 hrs · 24,741 cycles

L2 DOOR WILL NOT ARM. CLEANED CONTACTS FOR SLIDING ARMING INDICATOR. VISUAL INSPECTION ACCOMPLISHED GIRT BAR ASSY. OPERATED DOOR SEVERAL TIMES ARM DISARM. OP CHECKED OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,208 hrs · 24,725 cycles

EMERGENCY LIGHT AT 6B INOPERATIVE. RELAMPED EMERGENCY LIGHT IN STOW BIN AT SEAT 6B.

Part: LIGHT — LOOSE (CABIN) · airframe 67,208 hrs · 24,725 cycles

EMERGENCY LIGHT STRIP ON FLOOR BY 12C IS LOOSE. TAPE EEL STRIP TO CABIN FLOOR.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 66,380 hrs · 24,443 cycles

BROKEN WIRE HANGING DOWN AT SEAT 27D. SECURED LOOSE CONNECTOR AT SEAT 27D.

Part: SMOKE GOGGLES — DEFECTIVE (COCKPIT) · airframe 66,316 hrs · 24,419 cycles

OBSERVER SMOKE GOGGLES HEAD BAND ELONGATED. REMOVED AND REPLACED SMOKE GOOGLES.

Part: TARGET — DIRTY (ENTRY DOOR) · airframe 66,178 hrs · 24,370 cycles

LEFT AFT ENTRY DOOR EICAS CAME ON DURING APPROACH. CLEANED AND LUBED DOOR TARGET AND PROXIMITY SWITCH. OPS CHECK DOOR. NO EICAS MESSAGE. OPS CHECK GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (L4 DOOR HANDLE) · airframe 65,835 hrs · 24,247 cycles

L4 DOOR HANDLE UNSECURE, FLT DIVERTED. COMPLETED CHECK OF ADJUSTMENT OF DOOR 4L. REMOVED SLIDE AND LINING OF DOOR TO CHECK SAFETY AND SECURITY OF LINKAGES DOOR ADJUSTMENT CHECKED OKAY. VERIFIED DOOR ADJUSTMENT GOOD. DOOR CLOSES AND OPENS NORMAL. ARMING MECHANISM CK'S GOOD

Part: CHECK VALVE — WORN (APU) · airframe 65,732 hrs · 24,210 cycles

APU CHECK VALVE IS WORN. INSTALLED SERVICEABLE APU CHECK VALVE. COMPLETED INSTALLATION OF APU CHECK VALVE IAW AMM 36-11-11.

Part: LIGHT — LOOSE (CABIN) · airframe 65,647 hrs · 24,182 cycles

EMERGENCY LIGHT STRIP LOOSE AT ROW 13. FOUND CHAP STICK UNDER FLOOR LIGHT TRACK. REMOVED CHAP STICK AND SECURED LIGHT TRACK.

Part: THERMOCOUPLE — OPEN (NR 3 EGT) · airframe 64,155 hrs · 23,682 cycles

FOUND NR 2 ENGINE EGT THERMOCOUPLE T4.9 PROBE AT 10 O'CLOCK POSITION OPEN. REPLACED THERMOCOUPLE PROBE PER AMM.

Part: BLADES — DAMAGED (ENGINE FAN) · airframe 64,056 hrs · 23,643 cycles

FAN BLADES ON NR 2 ENGINE ARE DAMAGE. ACCOMPLISHED BLEND REPAIR ON FAN BLADE LE TIP.

Part: LEG ASSY — DISLODGED (SEAT 32 ABC) · airframe 63,507 hrs · 23,448 cycles

SEATS 32 ABC LOOSE FROM FLOOR REINSTALLED INBD LEG. CHECKED LOCK, SECURE ON OTBD LEG.

Part: PANEL — DELAMINATED (THRUST REVERSER) · airframe 63,394 hrs · 23,399 cycles

NR 1 ENG THRUST REVERSER OUTBOARD COWL UPPER BIFURCATION PANEL INNER (NON PERFORATED) AND OUTER (PERFORATED) SKINS BOTH DELAMINATED FROM L/E TO T/E AND FROM SIDE TO SIDE TOTAL AREA OF DELAM IS BETWEEN 680 AND 700 SQ INCHES, EXCEEDS LIMITS OF MM. INSTALLED REPAIR PER AMM.

Part: GATE — CRACKED (L2 DOOR) · airframe 63,394 hrs · 23,399 cycles

MAIN ENTRY DOOR 2 LEFT LOWER GATE CRACKED AFT END LAST HINGE RIVET. REMOVED & REPLACED LOWER GATE PER MM. ACCOMPLISHED RIG CHECK PER MM.

Part: SUPPORT BRACKET — CRACKED (NR 1 NACELLE) · airframe 63,392 hrs · 23,398 cycles

NR 1 ENGINE PYLON FUEL SHUT OFF WIRE CONDUIT SUPPORT BRACKET CRACKED ALMOST SEPARATED. REMOVED AND REPLACED BRACKET.

Part: BLOWOUT PANEL — LOOSE (NR 2 NACELLE) · airframe 63,392 hrs · 23,398 cycles

INLET COWL NR 2 ENG 6:00 POSITION BLOW OUT OVER PRESSURE PANEL FORWARD EDGE HANGING DOWN, FWD PIVOT PINS AND BUSHINGS WORN. REPLACED BUSHINGS AND PIVOT PINS.

Part: DUCT — CRACKED (NR 1 INLET) · airframe 63,392 hrs · 23,398 cycles

NR 1 ENGINE INLET COWL ANTI ICE DUCT CRACKED AT 3:00 POSITION ON AFT BULKHEAD. REPLACED DUCT. LEAK & OPS CHECKED GOOD.

Part: SEAL — TORN (L2 DOOR) · airframe 63,234 hrs · 23,338 cycles

NEED TO SMOOTH REN AREA AT 2L ENTRY DOOR UPPER MIDDLE SECTION AND ACCOMPLISH PRESSURE CHECK OF DOOR SEAL. SMOOTHED REN AREA AT 2L ENTRY DOOR. PRESSURIZED ACFT, STILL LEAKS. NOTICED HOLE AT MIDDLE HINGE ASSY AND SEAL TORN ON FRAME (MKD WITH TAPE). SUSPECT LEAK COMING FROM THERE AND TRAVELING UPWARDS. REN AREA STILL NEEDS TO BE PAINTED. APPLIED SEALANT TO FWD SIDE OF DOOR 2L UPPER HINGE CAVITY FUSELAGE SIDE PER SFOOV 109207.

Part: BATTERY — FAULTY (MASTER) · airframe 62,903 hrs · 23,219 cycles

MAIN BATTERY CHARGER MSG AFTER PREVIOUS CLEARING OF SAME MESSAGE. REPLACED SHIPS BATTERY, CHECKED NORMAL.

Part: SMOKE GOGGLES — UNKNOWN (COCKPIT) · airframe 62,720 hrs · 23,153 cycles

F/O NEEDS A NEW PAIR OF SMOKE GOGGLES. REPLACED SMOKE GOOGLES.

Part: OXYGEN MASK — IMPROPER PART (CABIN) · airframe 62,616 hrs · 23,115 cycles

WRONG O2 HOSE AND BAG 1ST CLASS AREA. INSTALLED CORRECT MASK.

Part: B-NUT — LOOSE (YAW DAMPER) · airframe 62,599 hrs · 23,107 cycles

HYD LEAK ON RT SIDE OFF FUSELAGE JUST AFT OF RT ELEVATOR. SECURED 'B' NUT CONNECTION ON THE LEFT YAW DAMPER SERVO. ACCMP'D HYD SYSTEM GENERAL EXTERNAL LEAK CHECK IAW MM, ALL CHECKS GOOD.

Part: SEAL — LEAKING (COCKPIT WINDOW) · airframe 61,620 hrs · 22,763 cycles

CHRONIC FLIGHT DECK NOISE. AIR LEAK FOUND AT THE AFT SIDE OF THE FIRST OFFICERS SLIDING WINDOW. REPLACED RT NR 2 WINDOW SEAL. AIRCRAFT WILL NEED TO BE PRESSURIZED AND NR 2 RT WINDOW LEAK CHECKED. LEAK CHECK IS GOOD. CABIN AIR RISER DUCTS DISCONNECTED FROM MAIN DUCT FROM AFT CABIN THRU FWD CABIN. RECONNECTED RISER DUCTS. CLEANED DISTRIBUTION DUCT AND GASPER HOUSING AND TUBES. ACP CLEANING OF CENTER DIFFUSER AND ALL GASPER TUBES AND HOUSING, MOST SCREENS WHERE CLOGGED WITH DEBRIS BEFORE CLEANING. ENTIRE ACFT CABIN NEEDS TO CLEANED. CLEANED COMPLETE CABIN DUCTING AND GASPER TUBING.

Part: SEAL — DEFECTIVE (R2 DOOR) · airframe 61,565 hrs · 22,741 cycles

DOOR 2R WHISTLING NOISE AT CRUISE. FOUND UPPER GATE SEALING SURFACE IRREGULAR FROM PREVIOUS "REN" REWORK. SMOOTHED AREAS INTO CORNERS. FOUND DIAPHRAGM SEAL MIGRATED OUT FROM NYLON RETAINING ROD IN BOTH CORNERS OF UPPER GATE AND FWD CORNER OF LOWER GATE. WILL REQUIRE DIAPHRAGM SEAL REINSTALLATION. REPLACED DOOR 2 RIGHT PRESSURE SEAL. PRESSURIZED TO 4 POUNDS, NO LEAKS.

Part: SEALANT — MISSING (THRESHOLD) · airframe 61,438 hrs · 22,689 cycles

THERE APPEARS TO BE A LARGE LEAK IN THE PRESSURE CABIN. OUTFLOW VALVE ALMOST FULLY CLOSED. REPAIRED THRESHOLD ON DOOR 1R AND 2R ACCOUNT OF NO SEALANT BEHIND THRESHOLD PLATE ACCOMPLISHED LEAK CHECK'S UP TO 4 PSI AND NO LEAKS NOTED ON DOORS OR THRESHOLDS AFTER REPAIRS.

Part: SKIN — DENTED (FUSLEAGE) · airframe 61,211 hrs · 22,602 cycles

RAMP REPORTS DENT AFT AND BELOW DOOR 4LT MAJOR REPAIR ACCOMPLISHED: INSPECTED AREA IAW SRM AND FOUND TO BE OUT OF LIMITS. DENT MEASURES 1-32 " IN DEPTH, 3 QTR " TALL AND 1 1-2 " WIDE, DENT MEASURES 18 3-4 " FROM STA 1720 (PRESSURE BULKHEAD) AND 11 1-2 " FROM THE FLOOR LINE AND 1-4 " FROM THE NEXT RIVET, INSPECTED THE AFFECTED AREA FROM THE INSIDE, NO DAMAGE FOUND. IN REF TO EVA 73071. MF5133 CREATED TO MONITOR. REF TO EVA AND SRM EXTERNAL DOUBLER REPAIR EST 2-3 SHIFT SLOT. LM INFO: *20HR SLOT RQSTD*. ARC: FOUND DENT TO BE OUT OF LIMITS. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER IAW SRM.

Part: LIGHT — INOPERATIVE (MID LAV) · airframe 61,211 hrs · 22,602 cycles

MID LAV EMERGENCY LIGHTING STRIP INOP. REPAIRED EMERGENCY LIGHTING STRIP AT MID LAV IAW MM. OPS CHECKS GOOD.

Part: SKIN — DAMAGED (BS 630 S14-19L) · airframe 61,211 hrs · 22,602 cycles

LEFT FUSELAGE SKIN STA 630, STR 14L TO STR 19L SKIN DOUBLER REPAIR WAS INSTALLED 22JUN10. MAJOR REPAIR ACCOMPLISHED DOUBLER MODIFIED AND STRAP INSTALLED IAW EA PD57-53-075 ON NR 2429N00115.

Part: BUTT JOINT — CORRODED (BS 1400) · airframe 61,211 hrs · 22,602 cycles

CORROSION FOUND AT BUTT JOINT AFT CARGO STA 1400 AT LBL 3 BETWEEN STRINGER 29L AND RBL 2.5 OTBD OF STRINGER 30. BUTT JOINT AT AFT CARGO STA 1400 AT LBL 3 BETWEEN STRINGER 29L AND RBL 2.5 OTBD OF STRINGER 30 HAD CORROSION AND WAS REPAIRED IAW EVA 80534.

Part: SKIN — DAMAGED (BS 310-530) · airframe 61,211 hrs · 22,602 cycles

6 LIGHTNING STRIKES FOUND ON INSP, ON UPPER FUSELAGE BETWEEN STA 310.5 AND 530. MAJOR REPAIR ACCOMPLISHED: REPAIRED IAW MM NR 2429 N00117, EA PD57-53-088, EA PD57-53-080, NR 2429N00862. & EA PD57-53-079, NR 2429N00863.

Part: STRUCTURE — OUT OF TOLERANCE (STA 395, STR 2R) · airframe 61,211 hrs · 22,602 cycles

EXT FUSELAGE REPAIR DOUBLER AND STRINGER REPAIR ACCOMPLISHED AT STA 395, STR 2R, IAW EA PD57-53-079. DURING HMV, 3 JAN 2011.

Part: PRESSURE PANEL — CORRODED (STA 1682, RBL 56) · airframe 61,211 hrs · 22,602 cycles

PRESSURE DECK HAS CORROSION AT STA 1682, RBL 56 TO RBL 33. MAJOR REPAIR ACCOMPLISHED: INSTALLED FILLER AND DOUBLER IAW EA PD57-53-072.

Part: CREASE BEAM — CORRODED (BS 1020, STR 17L) · airframe 61,211 hrs · 22,602 cycles

CORROSION ON CREASEBEAM AND ANGLE BRACKET AT BS 1020, STR 17L. INSTALLED SPLICE IAW EA PD57-53-076.

Part: HOUSING — CRACKED (FLAP XMISSION) · airframe 61,211 hrs · 22,602 cycles

FOUND NR 3 FLAP TRANSMISSION HOUSING CRACKED AT TOP MOUNTING BOLTS. R & R LT WING NR 3 FLAP TRANSMISSION AND OPS CHECKED IAW MM. TRANSMISSION DAMAGED DURING FLAP MOVEMENT. OPEN

Part: STOWAGE BOX — OUT OF TOLERANCE (OXYGEN SYSTEM) · airframe 61,211 hrs · 22,602 cycles

CREW O2 MASK STOWAGE BOX OUT OF TOLERANCE. INSTALLED CREW O2 MASK STOWAGE BOX ON TASKCARD 5R35I2193.

Part: LIGHT — INOPERATIVE (ROW 22) · airframe 61,211 hrs · 22,602 cycles

EMERGENCY LIGHTING INOP FROM ROW 22 TO LAV K. REPAIRED EMERGENCY LIGHTING FROM ROW 22 TO LAV K AND PERFORMED OPS CHECK IAW MM.

Part: SKIN — DAMAGED (STA 760, STR 2L) · airframe 61,211 hrs · 22,602 cycles

LIGHTNING STRIKE AT STA 760, STR 2L. ACCOMPLISH REPAIR IAW EVA 805 28. EA PD57-53-074. RII ACCOMPLISHED, NO DEFECTS NOTED.

Part: FLOORBEAM — CORRODED (STA 1682, RBL 25) · airframe 61,211 hrs · 22,602 cycles

FLOORBEAM AT STA 1682, RBL 25 HAS CORROSION. INSTALLED STRAP ANGLES AND FILLERS IAW EA PD57-53-072.

Part: LIGHT — INOPERATIVE (CARGO BAY) · airframe 61,211 hrs · 22,602 cycles

EMERGENCY LIGHT INOP AT AFT LEFT CARGO COMPT. REMOVED AND REPLACED LAMP AT AFT LEFT EXT EMERGENCY LIGHT ASSY. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,333 hrs · 22,264 cycles

SECTION OF EMERGENCY LIGHTING INOP AT AFT LAV. INSTALLED SERVICEABLE EMEGENCY LIGHT STRIP.

Part: RELAY — BURNED (APU) · airframe 59,990 hrs · 22,140 cycles

DUE TO APU WILL NOT START ISSUES AND PLANNED APU REPLACEMENT ON 20AUG10 IN SFO. PRECAUTIONARY, REPLACE APU CRANK CONTACTOR RELAY. FOUND WIRE HARNESS FROM FIRE WALL TO STARTER BURNED. ALSO FOUND DAMAGE TO HARD LINES ON APU, AND STARTER BURNED. OPERATIONS AND LEAK CHECK GOOD.

Part: VALVE — MALFUNCTIONED (CABIN TEMP) · airframe 59,496 hrs · 21,962 cycles

CREW COMMENTED COCKPIT-UNABLE TO CONTROL IN AUTO-TOO HOT-MANUAL. FLT DECK WARMER THAN SELECTED WITH SWITCH ON & TEMP CONTROL IN AUTO. INOP LIGHT EXISTING. PRESS ECS REC BUTTON AND RECORD ZONE TEMPS. ACP LOG1 ON NON ROUTINE CARD NR 2162N00004. R & R FIT BECK AIR TRIM VALVE. OPS CKD NORMAL AND NO LEAK FOUND.

Part: SKIN — DAMAGED (BS 617-677) · airframe 59,496 hrs · 21,962 cycles

FUSELAGE DAMAGE TO SKIN APPROX STA 617 TO 677 AT WL 208 TEAR APPROX 9 IN LONG. MAJOR REPAIR ACCOMPLISHED: INSTALLED SKIN AT STA 630 AND STRINGER 17L TO 19L IAW UA-EVA-73889. PWI 6951 AND EA PD57-53-041. REPAIR IS A CATEGORY "C" INTERIM REPAIR AND MUST BE REPLACED OR MODIFIED TO A CAT A OR B REPAIR ()WITHIN 24 MONTHS OF 22 JUN 10, NOT TO EXCEED 3000 FLIGHT CYCLE S FROM PTT 59,496 PER THIS EA.

Part: TILLER — BINDING (NLG STEERING) · airframe 59,272 hrs · 21,878 cycles

TILLER STEERING - STEERING FORCES ARE HIGH. PEDAL NWS NO RESPONSE. TILLER FORCES VERY HIGH. ADJUSTED TILLER INDICATOR AND RIG SYSTEM. DUE TO LOG 2 TILLER STEERING AND RUDDER PEDAL NWS NO RESPONSE, NEED TO ACCOMPLISH TAXI TEST. OPS NORMAL. AFTER COMPLETION OF NLG STEERING GRIPE SAFETIED QUICK DISCONNECT HANDLES.

Part: COMPUTER — FAULTY (EICAS) · airframe 59,270 hrs · 21,877 cycles

LOST ALL PRESSURIZATION AT 6000'. LT EICAS TEST SHOWS 1 INTERNAL FAULT. REPLACED LEFT EICAS COMPUTER, TESTS OKAY. NO FAULTS NOTED.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 59,172 hrs · 21,839 cycles

DURING EXTERNAL CHECK FOUND HYD LEAK AT THE PRESSURE HYD LINE FROM THE RIGHT BRAKE STABILIZER CONTROL BMS UNIT. REPLACED RIGHT HYD HORIZONTAL STAB TRIM CONTROL LINE P/N 271N6482-1116. OPS CHECK HORIZONTAL STAB. OPS CHECK NORMAL, NO LEAKS NOTED.

Part: FEEDER CABLE — FAULTY (EMERGENCY LIGHT) · airframe 58,909 hrs · 21,739 cycles

FLOOR MOUNTED EMERGENCY LIGHT AT FWD CLOSET DOES NOT ILLUMINATE. REPLACED POWER CABLE FROM WALL.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 58,909 hrs · 21,739 cycles

EMERGENCY EXIT LIGHT STRIP LIFTED UP AT SEAT 13C. PUT EEL TRACK IN PLACE WITH DOUBLE BACK TAPE.

Part: ACTUATOR — FLUCTUATES (NR 1 BLEED VALVE) · airframe 58,299 hrs · 21,495 cycles

NR1 ENG FLUX, FLIGHT DIVERTED. REPLACED NR 1 ENGINE 2.5 BLEED ACTUATOR. ALSO ACP JRH TESTS 2-5-70 AND 2-5-71 AT 87% N1 ALL PARAMETERS STABLE. REPLACED EEC AND ACP'D ENG RUN.

Part: WINDOW — DAMAGED (COCKPIT) · airframe 58,121 hrs · 21,424 cycles

RH FWD WINDSHIELD SHATTERED. FWD RT WINDSHIELD SHATTERED BUT STILL IN PIECE. REPLACED NR 1R WINDSHIELD.

Part: LINE — LEAKING (HJYDRAULIC SYS) · airframe 57,888 hrs · 21,331 cycles

LT HYD QTY EICAS, RTFL. FOUND BOTH LINES DAMAGED AND LEAKING TO LT MLG DOWNLOCK ACTUATOR. REMOVED BOTH LINES FROM LT MLG DOWNLOCK ACTUATOR. BENCH CHECKED LINES AND FOUND ONE LINE BAD. OTHER LINE OKAY FOR SERVICE. REPLACED BAD LINE. HYD FLUID LEAKING FROM NR1 ENG AFT PYLON. SECURED B-NUT ON REV ISO VALVE IN NR 1 PYLON. LEAK CHECKED OK. REVERSER OPS CHECKED OKAY.

Part: LIGHT — UNSECURE (CABIN) · airframe 57,449 hrs · 21,143 cycles

ROW 12 AND 13 EMERGENCY FLOOR LIGHTING COMING UP. SECURED LIGHTS.

Part: LUG — BROKEN (ELECTRICAL SYS) · airframe 57,445 hrs · 21,141 cycles

PWR LOSS EICAS MSGS, RTFL. FOUND TERMINAL LUG BROKEN. REPLACED LUG AND SHRINK TUBING, OPERATION NORMAL.

Part: MICROPHONE — INOPERATIVE (COCKPIT) · airframe 57,169 hrs · 21,027 cycles

FIRST OFFICER O2 MASK MICROPHONE INOPERATIVE. MOVED O2 MASK BOX FROM 1ST OBSERVERS SEAT TO F/O SEAT.

Part: LIGHT — UNSECURE (CABIN) · airframe 55,790 hrs · 20,505 cycles

EXIT PATH LIGHTING ON FLOOR BETWEEN ROW 9 & 15 LOOSE. SECURED EEL.

Part: LIGHT — INOPERATIVE (LAVATORY) · airframe 53,935 hrs · 19,787 cycles

AFT LAV FLOOR EEL LIGHT INOP. REPLACED LIGHT ASSY. CHECKED OKAY.

Part: SPRING — BROKEN (EVAC SLIDE) · airframe 53,170 hrs · 19,505 cycles

NR 1 DOOR SLIDE ARM LEVER COVER SPRING BROKEN. DOES NOT STOW CORRECTLY. REPLACED COVER, FUNCTIONS CORRECTLY.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 52,513 hrs · 19,259 cycles

DOOR 1R EMERGENCY LIGHT INOP. SUPPLEMENTAL DATA UPDATE CAUSE, FOUND BROKEN WIRE AT LIGHT L30. REPAIRED WIRE AT L30 AND REPLACED POWER SUPPLY M730. OPS CHECKED NORMALLY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,505 hrs · 19,257 cycles

DOOR 1L EMERGENCY LIGHT INOPERATIVE. SUPPLEMENTAL DATA UPDATE, CAUSE LAMP IS INOP. RELAMPED ASSY, OPS CHECKED OK.

Part: LIGHT — UNSECURE (CABIN) · airframe 51,849 hrs · 19,027 cycles

EEL AT 13C NOT SECURED TO FLOOR. SECURED EEL TRACK TO FLOOR.

Part: FIRE LOOP — INTERMITTENT (RT NACELLE) · airframe 51,725 hrs · 18,983 cycles

RIGHT ENGINE LOOP 2 FIRE DETECTION INOPERATIVE. PROBLEM WAS INTERMITTENT FROM DAY ONE..HARD TO DIAGNOSE. AFTER SEVERAL WEEKS ON THE WATCH LIST, THE ISSUE NEVER RETURNED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,077 hrs · 18,753 cycles

EMERGENCY LIGHTS DOORS 1R & 4R EXTERIOR ARE INOP. 11-01-07 RELAMPED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,077 hrs · 18,753 cycles

CABIN EEL INOP ABOVE SEAT ROW 11 ABC.

Part: SWITCH — FAULTY (EMERGENCY LIGHTS) · airframe 50,834 hrs · 18,659 cycles

AFT SECTION EEL LIGHTS REMAIN ON. 10-19-07 ON T/S FOUND NOSE GEAR TEST SWITCH INTERMITTENT. REPLACED NOSE EMERGENCY TEST LIGHT SWITCH.

Part: LIGHT — UNSECURE (ROW 13ABC) · airframe 50,646 hrs · 18,590 cycles

EMERGENCY LIGHT STRIP ON FLOOR AT ROW 13ABC STICKS UP.

Part: UNKNOWN — ODOR (GALLEY) · airframe 50,163 hrs · 18,424 cycles

ACFT RETURN TO BLOCK DUE TO BURNING ODOR FROM AFT GALLEY AREA.

Part: GIRT BAR — FAULTY (R1 DOOR) · airframe 49,810 hrs · 18,295 cycles

DOOR 1R MAY NOT BE DISARMED ACCORDING TO F/A'S.

Part: STRIP — TORN (CABIN) · airframe 49,775 hrs · 18,282 cycles

EXIT PATH LIGHTING STRIP IS TORN AND A TRIPPING HAZARD AT 13ABC & 29ABC. [06-22-07] SECURED COVERS. LIGHTS OP NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,553 hrs · 18,191 cycles

EMERGENCY SLIDE LIGHT ON EXTERIOR OF AFT CARGO DOOR, EMERGENCY AISLE LIGHT IN STOW BIN BULLNOSE AT LEFT ROW 26 & EMERGENCY OVERHEAD EXIT SIGN AT ROW 15-16 ARE INOPERATIVE. REPLACED BATTERY PACK FOR POWER SUPPLIES.

Part: CIRCUIT BREAKER — TRIPPED · airframe 48,798 hrs · 17,931 cycles

DOOR GIRT BAR C/B TRIPS AFTER DOORS ARMED. FOUND DOOR ARM LIGHT SOCKET MISALIGNED WITH RECEPTICAL HOLE BEHIND UPPER TRIM PANEL, FORCING LUGS TOGETHER AND SHORTING OUT CAUSING CIRCUIT BREAKER TO POP. STRAIGHTENED LUGS AND REALIGNED SOCKET, CB STAYS IN, BUT ARM LIGHT STAYS ON, SUSPECT SENSOR BAD (CAUSED BY SHORTED WIRES ON LIGHT ASSY)

Part: PUMP — FAILED (HYD SYSTEM) · airframe 47,522 hrs · 17,435 cycles

DIVERTED DUE TO LOSS OF LEFT ENGINE ELECTRICAL AND HYDRAULIC PUMP. L HYD ENG DRIVEN PUMP EICAS MSG OFF. REPLACED LEFT HYDRAULIC ENGINE DRIVEN PUMP.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,879 hrs · 14,590 cycles

AFT PIT FRAME CORRODED AT BS 1300 BL 0 TO RBL 3. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FILLER & ANGLE REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,879 hrs · 14,590 cycles

LEFT FUSE SKIN IS DENTED AT STA 610-625, STR 15L-17L. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW PARTIAL SKIN PNL WITH DOUBLER SPLICES.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,879 hrs · 14,590 cycles

FRAME DENTED AND CRACKED AT BS 1480 BETWEEN STR 25L AND 26L AFT PIT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER & FILLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,879 hrs · 14,590 cycles

FUSELAGE FRAME DENTED AT BS 1520 STR 26L AFT PIT. MAJOR REPAIR ACCOMPLISHED. FABRICATED, INSTALLED DOUBLER & FILLER REPAIR.

Part: FAILSAFE — CRACKED (FRAME) · airframe 39,879 hrs · 14,590 cycles

FAILSAFE ANGLE CRACKED AT STA 1300 ABOVE STR 21L AT LWR END OF ANGLE IN RADIUS IN AFT PIT. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,879 hrs · 14,590 cycles

AFT PIT FRAME INNER FLANGE DENTED AT STA 1420 ABOVE STR 25L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,879 hrs · 14,590 cycles

AFT PIT FRAME INNER FLANGE DENTED 3 PLACES WITHIN 7.5 INCHES FROM JUST INBOARD OF STR 26L TO JUST ABOVE STR 26L AT STA 1400. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER & FILLER REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,879 hrs · 14,590 cycles

DENT ON FUSELAGE SKIN AT STA 1417, BETWEEN STRINGERS 27R & 28R. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER & FILLER REPAIR.

Part: PITOT TUBE — OBSTRUCTED (AIRSPEED) · airframe 38,331 hrs · 14,088 cycles

CAPTAINS AIRSPEED INDICATOR FAILED TO ADVANCE PAST 80 KNOTS. RUDDER RATIO AND MACH SPEED TRIM MESSAGES ILLUMINATED. MECHANIC FOUND LARGE BUG NESTING INSIDE CAPTS PITOT PROBE. ( RESTRICTING RAM PRESSURE). REMOVED AND CLEANED OUT BUG. THE BUG WAS LIKELY INSERTED BY A MUD DAUBER DURING LAYOVER. ACCOMPLISHED LOW RANGE PITOT STATIC CK. RUDDER RATIO AND MACH SPEED MESSAGES ALL RELATED TO CLOGGED PITOT.

Part: BULB — FAILED (3R DOOR)

DISCOVERED SLIDE LIGHT INOP WHEN ARMING DOOR 3R. LIGHT BULB INOP. RELAMPED, OPERATED NORMAL.

Part: CARD-FIRE DET — MALFUNCTIONED (RT ENGINE)

RIGHT ENGINE FIRE OVERHEAT AMBER LIGHT AND EICAS DID NOT COME ON WHEN TESTED. *S/D* THE RIGHT FIRE DETECTION CARDS, LOOP 1 OR LOOP 2, WERE FOUND FAULTY. REPLACED LOOP 1 AND 2 FIRE DETECTION CARDS. FUNCTIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY EGRESS LIGHTING INOP ROWS 16 TO 23. REPLACED BATTERY PACK, OPERATION CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY ESCAPE LIGHTS INOP BETWEEN ROWS 16 AND 32. REPLACED BATTERY PACK AT ROW 19, OPERATION CHECKS NORMAL.

Part: EEL INVERTER — FAILED (CABIN)

EMERGENCY LIGHT INVERTER INOP AT OVERWING LOCATION. REPLACED INVERTER. TESTS OK.

Part: LOCK PIN — INSTALLED (NLG)

UNABLE TO RAISE NOSE GEAR WHEN GEAR RETRACTED. REMOVED DOWNLOCK PIN FROM NOSE LANDING GEAR.