N578UA

Part: MICROPHONE — BROKEN (COCKPIT) · airframe 68,006 hrs · 23,877 cycles

CAPT HAND MIC BROKEN. REPLACED CAPT HAND MIC, OPERATIONS CHECKED GOOD.

Part: GIRT BAR — OUT OF POSITION (R4 DOOR) · airframe 67,853 hrs · 23,826 cycles

CATERING FOUND GIRT BAR PULLED OUT OF RETAINERS. SECURED GIRT BAR AT DOOR 4R IAW AMM.

Part: PACKING — LEAKING (SPEED BRAKES) · airframe 67,645 hrs · 23,752 cycles

NR 10 SERVO VALVE ON SPEED BRAKE ACTUATOR LEAKING. FOUND PACKING LEAKING FROM PLUG PORT. REPLACED PACKING, NO LEAKS NOTED.

Part: INLET — CONTAMINATED (APU) · airframe 67,615 hrs · 23,742 cycles

SMOKE REPORT IN AFT GALLEY WITH SMOKE ALARM GOING OFF IN AFT FWD LAVATORY WHILE AT GATE. EVENT OCCURRED RUNNING BOTH PACKS OFF THE AIR START UNIT AS APU IS ON DEFERRAL. SHUT OFF PACKS & SMOKE DISSIPATED. FOUND MELTED PLASTIC DEBRIS IN APU INLET. CLEANED APU INLET AREA OF PLASTIC DEBRIS. REACTIVATED APU. ACP APU BURNOUT. NO SMOKE IN CABIN NOTED AFTER 2 HR BURNOUT.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 67,577 hrs · 23,732 cycles

ODOR IN COCKPIT OF PLASTIC, DISSIPATES WITH LT PACK OFF.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 67,559 hrs · 23,725 cycles

STRONG PLASTIC ODOR IN FLT DECK, DURING DESCENT & LANDING. CHECKED NR 1 ENGINE INLET, NO EVIDENCE OF DEBRIS INGESTION, OPENED LT PAC (193HL) & RAM AIR INLET DUCT, NO DEBRIS FOUND PRIOR TO HEAT EXCHANGERS. CLEANED COCKPIT TEMP BULB & SENSOR, ENTERED LT NOSE TUNNEL, CLEANED DUCT AIR TEMP SENSOR, DUCT AIR TEMP BULB & DUCT OVERHEAT SWITCH INOP LT PACK. LEFT PACK GROUND OPERATED, NO ODOR FOUND AFTER SENSORS AND LT NOSE TUNNEL, HEAT EXCHANGERS CHECKED.

Part: CONNECTOR — DAMAGED (OXYGEN BOTTLE) · airframe 67,167 hrs · 23,605 cycles

CREW OXYGEN BOTTLE CONNECTION THREAD DAMAGED. R & R CREW OXYGEN BOTTLE IAW AMM 12-15-08, OPS CHECKED GOOD.

Part: SKIN — DAMAGED (BS 761 S18R) · airframe 67,167 hrs · 23,605 cycles

EVIDENCE OF DEEP BLENDING ON FUSELAGE EXTERIOR BS 761 AND 1 INCH ABOVE S18R. FOUND TO OUT OF LIMITS IAW SRM. INSTALLED EXTERNAL REPAIR DOUBLER IAW SRM 53-00-01 REPAIR 2.

Part: ARMREST — BROKEN (SEAT ROW 20D) · airframe 66,944 hrs · 23,529 cycles

ARM REST ASSY AT 20D IS BROKEN. SECURED 20A ARMREST END CAP. OK TO CONTINUE.

Part: ANGLE — CORRODED (BS 1410-1420) · corrosion level 2 · airframe 66,817 hrs · 23,485 cycles

DURING HMV-3, CORROSION WAS FOUND ON THE AFT CARGO DOORWAY LOWER SILL OUTBOARD ANGLE BETWEEN BS 1410 AND 1420. CORROSION WAS REMOVED IAW ECRA 5310-05405 AND EVA 81334. NO FURTHER ACTION REQUIRED.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 66,817 hrs · 23,485 cycles

DURING HMV3 , A CHAFING GOUGE WAS FOUND AT THE LEFT I/B MAIN FLAP UPPER SURFACE APPROXIMATELY MFS 298 TO 300.

Part: ACTUATOR — MALFUNCTIONED (RUDDER TRIM) · airframe 66,183 hrs · 23,299 cycles

RUDDER TRIM & PEDALS DISPLACED AT FULL LEFT. UNABLE TO RECENTER WITH TRIM KNOB. REPLACED RUDDER TRIM ACTUATOR, OPS CHECKS OKAY. FULL TRIM RIGHT AND LEFT.

Part: BLADE — DAMAGED (NR 1 ENGINE FAN) · airframe 65,956 hrs · 23,217 cycles

ON ARRIVAL WALK AROUND FOUND TWO FAN BLADES DAMAGED BY FOD IN NR 1 ENGINE FAN. REPLACED TWO SETS OF FAN BLADES ON NR 1 ENGINE PER MM 72-31-02. REPLACED BLADE NR 1 AND MATE NR 19 AND REPLACED NR 31 AND MATE NR 13, DIS NR 2189 SENT.

Part: CONTACT — DIRTY (CONTROL PANEL) · airframe 65,287 hrs · 22,971 cycles

TWO BULBS INOP APU FIRE CONTROL PANEL. CLEANED SWITCH CONTACTS, OPS NORMAL.

Part: CONTROLLER — FAULTY (CABIN TEMP) · airframe 64,663 hrs · 22,753 cycles

RIGHT PACK WENT FULL HOT IN AUTO AND STBY-C UNABLE TO STABILIZE CABIN TEMP. TRM AIR OFF FIXED IT. REPLACED ZONE TEMP CONTROL.

Part: CONTROLLER — FAULTY (COCKPIT TEMP) · airframe 64,647 hrs · 22,748 cycles

COCKPIT TEMP FAULTY, RTFL. UNCONTROLLABLE IN AUTO OR MAN OR TRIM AIR SWITCH OFF. REPLACED ZONE TEMP CONTROLLER PCN 563-9027. ALSO REPLACED TS175 AND TS201 SENSORS. COCKPIT TEMP OPS CHECKS GOOD.

Part: GIRT BAR — DAMAGED (L2 DOOR) · airframe 64,427 hrs · 22,676 cycles

L2 DOOR ARM LIGHT IS OUT AFTER PUSH BACK PRIOR TO TAXI. GIRT BAR END FITTING SEPARATED FROM GIRT BAR. OPENED DOOR FOR THE OUTSIDE OF ACFT AND THE FORWARD END OF THE GIRT BAR APPEARS TO BE DAMAGED. ACCOMPLISHED ADJUSTMENT OF L2 DOOR IAW AMM, OPS CHECKED GOOD.

Part: GIRT BAR — DAMAGED (L2 DOOR) · airframe 64,427 hrs · 22,676 cycles

DOOR 2L ARM LIGHT IS OUT AFTER PUSH BACK PRIOR TO TAXI. OPENED DOOR FOR THE OUTSIDE OF ACFT AND THE FORWARD END OF THE GIRT BAR APPEARS TO BE DAMAGED. ACCOMPLISHED ADJUSTMENT OF L2 DOOR IAW AMM, OPS CHECKED GOOD.

Part: FUEL CONTROL — FAULTY (NR 1 ENGINE) · airframe 64,295 hrs · 22,629 cycles

L ENG PRI CONT STATUS. MESSAGE PROG TEXT: - ITEM ROLLED FORWARD. SAMC TEXT: RTBL PER TOMC-SHUT DOWN L ENG, EPCS HITTING (P) FCU-EEC AND (P) 350-20, NO GO PER MEL 7321E. L ENG FCU JUST REPLACED (PTT SEQ.2952005-23 SEA). REPLACED FUEL CONTROL REF MM.

Part: GIRT BAR — OBSTRUCTED (L2 DOOR) · airframe 64,150 hrs · 22,577 cycles

L2 DOOR WILL NOT ARM. CLEANED DOOR SILL AREA, ARMED DOOR THREE TIMES, CHECKED OK.

Part: CRANK ASSY — FAULTY (R1 DOOR GIRT BAR) · airframe 63,713 hrs · 22,447 cycles

DOOR 1R SLIDE LIGHT INOPERATIVE. REPLACED GIRT BAR ACTUATOR CRANK ASSEMBLY LIGHT, OPS CHECKS NORMAL.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 63,153 hrs · 22,236 cycles

IAS DISAGREE, ALT DISAGREE, MACH SPD TRIM, RUDDER RATIO AND ELEV ASSY EICAS MSG DISPLAYED. FLIGHT DIVERTED.

Part: GROUND STUD — LOOSE (CABIN) · airframe 63,122 hrs · 22,224 cycles

FOUND EMERGENCY EXIT LIGHTS NOT WORKING AT SIDE WALL SEAT 21A AND 20F OVERWING EXIT SIGNS. REPAIRED LOOSE GROUND STUD 3804, SYSTEM OP CHECK OK.

Part: CONNECTOR — SHORTED (L4 DOOR SLIDE) · airframe 62,962 hrs · 22,166 cycles

L4 DOOR SLIDE ARM LIGHT IS ON WHEN DOOR SLIDE IS DISARMED. DOOR ARMS AND DISARMS NORMALLY, BUT ARM LIGHT IS ALWAYS ON. REF TO WD25-66-11, L408 PIN C AND PIN 1 TOUCHING (SHORTING). SECURED PIN 1 AND PROVIDED CLEARANCE. ARMED AND DIS-ARMED DOOR SLIDE ARM LIGHT CHECKED GOOD, AND VERIFIED GIRT BAR WORKED OK.

Part: SOCKET — DIRTY (INDICATOR) · airframe 62,579 hrs · 22,017 cycles

ENGINE BOTTLE 1 DISCHARGE LIGHT STILL NOT TESTING CORRECTLY. SWAPPED LIGHT CAPS, PROBLEM STAYS WITH NR 1 BOTTLE, CHECKED SECURITY OF CONNECTORS AT FIRE CONTROL PANEL, ALL SECURE. RETURNED LIGHT CAPS TO ORIGINAL POSITION. CLEANED SOCKET AND PIN CONTACTS ON LIGHT CAP ASSY. OPS CHECKED GOOD. LIGHT TESTED NORMAL.

Part: RIB — MISSING (VERTICAL STAB) · airframe 61,921 hrs · 21,779 cycles

SPLICE ASSY AT UPPER END OF VERTICAL STABILIZER LEADING EDGE PANEL 321BL MISSING INTERNAL RIB.

Part: HANDLE — UNKNOWN (DOOR) · airframe 61,854 hrs · 21,755 cycles

LEFT AFT DOOR HANDLE ISSUE, FLIGHT DIVERTED.

Part: SLIDE — OUT OF POSITION (R4 DOOR) · airframe 61,841 hrs · 21,749 cycles

R4 DOOR SLIDE CASE HITS DOOR FRAME WHEN CLOSING DOOR. ADJUSTED DOOR SLIDE COVER PER AMM.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 61,841 hrs · 21,749 cycles

LIFE VEST AT AFT F/A AND COCKPIT OBSERVERS POSITIONS DO NOT HAVE DATE STAMP ON SERVICEABLE TAG. REPLACED LIFE VESTS PER AMM.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 61,841 hrs · 21,749 cycles

FLOORBEAM STA 1640 HAS CORROSION. FLOORBEAM REPAIRED FROM LBL 10 TO RBL 60, PER CO ECRA 5310-05401.

Part: FRAME — DAMAGED (BS 1540 S26L) · airframe 61,841 hrs · 21,749 cycles

AFT CARGO BAY FRAME, BS 1540 S26L MISDRILLED. FRAME REPAIRED IAW ECRA 5310-05410 AND EVA 81353. MAJOR REPAIR.

Part: FRAME — CORRODED (BS 1360) · airframe 61,841 hrs · 21,749 cycles

AFT CARGO BAY FRAME CORRODED BS 1360, JUST OTBD OF RT TRANSITION PANEL. REPAIRED FRAME PER ECRA 5310-05409 AND EVA 81353. MAJOR REPAIR

Part: SKIN — DENTED (E/E BAY DOOR) · airframe 61,841 hrs · 21,749 cycles

E&E DOOR HAS 3 EACH DENTS IN THE OUTER SKIN FWD SECTION. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED PER CO ECRA 5210-02264.

Part: SKIN — WORN (LT WING TE FLAP) · airframe 61,841 hrs · 21,749 cycles

LEFT INBOARD TRAILING EDGE MAIN FLAP HAS A DEEP WEAR MARK IN THE UPPER SURFACE AT APPROX MFSTA 298. INSTALLED DOUBLER REPAIR PER ECRA5721-01318 AND EVA 81348. MAJOR REPAIR

Part: FITTING — CORRODED (FUSELAGE) · airframe 61,841 hrs · 21,749 cycles

AFT PIT DOOR CUTOUT LWR SILL, L ANGLE BELOW TIE DOWN FITTINGS CORRODED (MARKED). BLENDED OUT VERTICAL LEG OF "T' AND INSTALLED OVERSIZED FASTENERS PER CAL ECRA 5310-05405 AND EVA 81334. CF9075 CREATED FOR EG FOLLOWUP.

Part: SILL — CORRODED (BS 1410-1420) · airframe 61,841 hrs · 21,749 cycles

DURING HMV-3, CORROSION WAS FOUND ON THE AFT CARGO DOORWAY LOWER SILL OUTBOARD CHORD BETWEEN BS 1410 AND 1420. CORROSION WAS REMOVED IAW ECRA 5310-05405 AND EVA 81334.

Part: SKIN — CRACKED (R1 DOOR) · airframe 61,841 hrs · 21,749 cycles

DOOR R1 HAS A CRACK ON INNER SKIN ON EDGE OF LIGHTNING HOLE (MARKED). BLENDED OUT DAMAGE ACCOMP HFEC INSP REF NDT PT 6, 51-00-04, NO CRACKS NOTED. FAB DOUBLER AND INSTALLED REF EC-RA 5210-02266. THIS IS CONSIDERED A MAJOR RPR.

Part: SKIN — DENTED (FUSELAGE) · airframe 61,841 hrs · 21,749 cycles

DENT-BLENDOUT STA 312, STR 23L. MAJOR REPAIR ACCOMPLISHED. BLENDED AREA SMOOTH, ACCOMP HFEC INSP REF NDT PT 6, 51-00-01, NO CRACKS NOTED. INSTALLED RPR SKIN DOUBLER REF EC-RA 5330-04159 AND EVA 81333.

Part: FRAME — DENTED (BS 1420) · airframe 61,841 hrs · 21,749 cycles

AFT PIT BELT FRAME DENTED JUST OTBD OF LEFT TRANSITION PANEL, AT BS 1420. REMOVED & INSTALLED NEW BELT FRAME FROM STR 24L TO 27L.

Part: FLOORBEAM — DAMAGED (BS 984) · airframe 61,841 hrs · 21,749 cycles

LEFT CABIN FLOORBEAM, BS 984, HAS TOOLING MARKS AT INBD END AND FWD UPPER EDGE. REPAIRED PER EC-RA 5310-05 402. DAMAGE REMOVED, TREATED AND PRIMED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,841 hrs · 21,749 cycles

DOOR 1R, FWD CUTOUT HAS CRACKED REVEAL, LOCATED JUST ABOVE UPPER HINGE ARM. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER RPR PER SRM. NDT AFTER DAMAGE CUTOUT REF NDT PT 6, 53-10, NO DAMAGE NOTED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,841 hrs · 21,749 cycles

FLOORBEAM CORRODED AT STA 324 RBL 38 UP TO CREASE BEAM. MAJOR REPAIR ACCOMPLISHED REPAIRED STRAPS AND REPAIRED ANGLES PER EC-RA 5310-05399. THIS IS A CAT B RPR. ALSO REF EVA 81311. N-R 9949355.

Part: SKIN — DENTED (FUSELAGE) · airframe 61,841 hrs · 21,749 cycles

SKIN DENT STA 260, STR 22L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SKIN, HFEC INSP REF NDT PT 6, 51-00-01, NO CRACKS NOTED. A .04 INSURANCE CUT REF SRM 53-00-01 RPR 2, AND INSTALLED SKIN DOUBLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,841 hrs · 21,749 cycles

CABIN FLOORBEAM STA 1661 LBL TO LBL HAS SURFACE CORROSION. MAJOR REPAIR ACCOMPLISHED: CORRODED SECTION OF FLOORBEAM UPPER CAP LBL 24 TO LBL 29 WAS CUTOUT AND REPAIR ACCOMPLISHED PER SRM REPAIR 3. WORK WAS ACP ON CAL NR 9949626.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,841 hrs · 21,749 cycles

FLOORBEAM AT STA 345 RBL 2 HAS CORROSION. REMOVED CORROSION, FOUND 2 PERCENT MATERIAL REMOVED WITHIN LIMITS. TREAT AND PRIME AREA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,841 hrs · 21,749 cycles

CREASE BEAM RT SIDE AT STA 755-760 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION. FABRICATED REPAIR PARTS. INSTALLED REPAIR AT STA 755-760, RT SIDE.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 61,440 hrs · 21,607 cycles

THE 1ST OFFICER'S WINDSHIELD'S VISIBILITY IS AFFECTED BY DEFECTS, REPLACE FIRST AVAILABLE. CREW COMMENTS: DELAMINATION LOWER LT CORNER. REPLACED NR 1 RIGHT WINDOW PER MM.

Part: O-RING — LEAKING (FUEL PUMP) · airframe 61,350 hrs · 21,574 cycles

FUEL & OIL LOSS, FLIGHT DIVERTED. ON RIGHT SIDE AS TOTALIZED AND CALCULATED FUEL WAS OFF BY APPROX 5000LBS. REPLACED O-RINGS AT FUEL PUMP TO FUEL CONTROL AND REPLACED CARBON SEAL AT FUEL PUMP.

Part: HINGE FITTING — DAMAGED (RT AILERON) · airframe 60,838 hrs · 21,390 cycles

RIGHT ELEVATOR OTBD HINGE FITTING HAS EVIDENCE OF LIGHTNING STRIKE DAMAGE. REMOVED RT OTBD HINGE FITTING. NEW HINGE ON AOG M1904. REPLACED RT OTBD HINGE FITTING.

Part: SKIN — DAMAGED (BS 206 S27L) · airframe 60,838 hrs · 21,390 cycles

LIGHTENING BURN HOLE IN SKIN STA 206, 6 INCHES ABOVE STR 27L. REMOVED RIVET, HFEC ACP. NO DEFECT NOTED. PERFORMED SOLID RIVET REPAIR PER SRM.

Part: SLIDE — UNSERVICEABLE (R4 DOOR) · airframe 60,779 hrs · 21,366 cycles

NR 4 RT MED SLIDE COVER AFT UPPER PIN LACING IS BROKEN. REPLACED 4R MED SLIDE PER MM.

Part: MECHANISM — DIRTY (R3 DOOR) · airframe 60,779 hrs · 21,366 cycles

CANNOT ARM DOOR 3R. CLEANED AND LUBED SLIDE ARM MECHANISM AT AFT RT DOOR.

Part: BEARING — FAULTY (TE FLAP) · airframe 60,779 hrs · 21,366 cycles

LT INBD MAIN FLAP TRACK FWD ATTACH POINT BEARING PUSHED OUT OF TRACK WITH INBOARD LOAD FROM FLAP HOLDING TRACK AGAINST MOUNTING BRACKET. BEARING IS CAPTURED BY SUPPORT BRACKETS AND CANNOT MOVE FURTHER. REMOVED FITTING REPLACED. REPLACED BEARING PER GNMM. LIGHTNING STRIKE BTWN DOOR CUTOUT AND STA 400 ON LAP JOINT. REMOVED 1 EA. FASTENER, HFEC AFTER FAST. RMV, NO CRACKS FOUND AND INSTALLED FASTENER.

Part: PAN — GOUGED (PAX DOOR) · airframe 60,340 hrs · 21,215 cycles

#1 LEFT MAIN ENTRY DOOR HANDLE PAN GOUGED AT THE 11 TO 12 POSITION. THE DEPTH OF THE GAUGE IS .025" PER DRAWINGS THE SKIN IN THE AREA COULD BE STRETCHED AS THIN AS .045" DURING FORMING. FERRIED TO SFO FOR REPAIR. MAIN ENTRY DOOR 1 LEFT CAM BASKET BEARING WORN. REPLACED ON DOCK WU K2333E PER MM. PRELIMINARY MEASUREMENTS SHOW .047" REMAINING MATERIAL IN RADIUS. AFTER BLENDING MEASUREMENT NOW .035 REMAINING MATERIAL (PARTIAL). OVERALL LENGTH1.5 INCH. WIDTH .093-.125 INCH. ORIGINAL MATERIAL THICKNESS .071 REPLACED DOOR HANDLE ON DOCK WU K2334E.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 58,789 hrs · 20,632 cycles

BIRDSTRIKE TO RT SIDE OF RADOME, RTFL. REPLACED RADOME. ACCOMPLISHED BORESCOPE. NO LIMITING DISTRESS NOTED.

Part: BOTTLE — READS LOW (R3 DOOR SLIDE) · airframe 58,706 hrs · 20,598 cycles

DOOR 3R SLIDE PRESSURE IS IN THE RED. SLIDE CHECKS WITHIN LIMITS. NFF.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,258 hrs · 20,432 cycles

LEFT AND RIGHT MID CABIN EMERGENCY EXIT LIGHTS INOP (INSIDE AND OUTSIDE). RELAMPED LT AND RT MID CABIN EMERGENCY EXIT LIGHTS, OPS CHECK OKAY, WORK WAS ACCOMPLISHED ON NR 2175N00010.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,258 hrs · 20,432 cycles

LEFT FWD OVERWING EXIT EMERGENCY LIGHT INOPERATIVE. RELAMPED FWD OVERWING EMERGENCY EXIT LIGHT, OPS OKAY. WORK WAS ACP ON PEMCO NR 2175N0008.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 58,029 hrs · 20,345 cycles

AFT EMERGENCY FLOOR LIGHTING DISCONNECTED. INTERIM REPAIR MADE WITH TAPE. SMALL SECTION OF EMERGENCY LIGHT LENS CRACKED AND PEALING UP. WILL NEED NEW SECTION OF LENSE. INSTALLED NEW BASE AND LENS COVER AS REQUIRED.

Part: HOUSING — CRACKED (PCU)

DURING NDT INSP IT WAS NOTED THAT THE BLOCKING AND RELIEF VALVE HOUSING IS CRACKED.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHT) · airframe 57,106 hrs · 20,007 cycles

EXTERIOR EMERGENCY LIGHT AT DOOR 2L WILL NOT ILLUMINATE. REPLACED POWER SUPPLY M733. RANG OUT WIRING FROM POWER SUPPLY CONNECTOR D72, PIN 9 TO LIGHT L35 =P. WIRE CHECKED GOOD. L35 =G TO GROUND CHECKED OK. REPLACED LAMP AND OPERATION CHECK OKAY.

Part: WARNING LIGHT — FALSE ACTIVATION (PAX DOOR) · airframe 56,322 hrs · 19,731 cycles

DOOR OVERHEAD LIGHT & EICAS, FLT DIVERTED. CREW REPORTS AFT RT ENTRY DOOR OVERHEAD LIGHT AND EICAS. HANDLE CREPT UP AND WILL NOT STOW. NO PRESSURE LEAKS NOTED. OPENED DOOR AND INSPECTED DOOR SEALS, ROLLERS AND STOPS ALL CHECKED GOOD. ALSO INSPECTED DOOR ARMING MECHANISM AND CYCLED DOOR SEVERAL TIMES. OPENS, CLOSES AND ARMS CORRECTLY. THE SAMC CONTROLLER AND MANAGER CONCURR THAT THE AIRPLANE CAN BE RELEASED BACK TO SERVICE.

Part: WIRE — LOOSE (CABIN) · airframe 56,024 hrs · 19,618 cycles

MAIN CABIN DOOR R1 GIRT BAR WARNING LIGHT INOP. REPAIRED LOOSE WIRE AT SWITCH S10216. OPS CHECKS GOOD.

Part: TUBE — OBSTRUCTED (SMOKE DETECTOR) · airframe 56,024 hrs · 19,618 cycles

AFT CARGO COMPARTMENT SMOKE DETECTOR TUBES NOT CLEAR AND PLACARDS TORN. PULLED SMOKE DETECTOR TUBES CLEAR AND INSTALLED PLACARDS AS REQUIRED.

Part: SLIDE — DEFECTIVE (L1 DOOR) · airframe 56,024 hrs · 19,618 cycles

MAIN CABIN DOOR L1 SLIDE AFT LACING PARACHUTE AND PIN KNOT LOOSE. RE-INSTALLED NEW PARACHUTE IN SAFETY THREAD.

Part: SNUBBER — FAULTY (DOOR 4R) · airframe 56,024 hrs · 19,618 cycles

MAIN CABIN DOOR 4R DOOR SNUBBER INDICATION LOW. INSTALLED NEW DOOR SNUBBER AND COUNTER BALANCE, LWR AND UPR CAM PLATE BEARINGS AND INTERCOSTAL BEARINGS HOUSE BEARINGS. REINSTALLED DOOR. ADJUST AND OPS NORMAL.

Part: HARNESS — FRAYED (EVAC SLIDE) · airframe 56,024 hrs · 19,618 cycles

MAIN CABIN R4 DOOR SLIDE HARNESS LOWER FRAYED. REPLACED THE SLIDE HARNESS.

Part: BEARING — CORRODED (L4 DOOR) · airframe 56,024 hrs · 19,618 cycles

MAIN CABIN DOOR 4L LWR FWD GATE TORQUE TUBE CAM BEARING CORRODED. INSTALLED NEW BEARING.

Part: BEARING — CORRODED (R1 DOOR) · airframe 56,024 hrs · 19,618 cycles

MAIN CABIN DOOR R1 TORQUE TUBE BEARINGS CORRODED. INSTALLED 2 EA NEW BEARINGS P/N B54200.

Part: CONNECTOR — CORRODED (EVAC SLIDE) · airframe 56,024 hrs · 19,618 cycles

AFT CARGO COMPT RIGHT OFFWING SLIDE CYLINDER CONNECTOR BACKSHELL CORRODED. CLEANED BACKSHELL.

Part: CONNECTOR — CORRODED (EVAC SLIDE) · airframe 56,024 hrs · 19,618 cycles

AFT PIT LEFT OFFWING SLIDE CYLINDER CONNECTOR BACKSHELL CORRODED. CLEANED BACKSHELL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,545 hrs · 18,280 cycles

SLIDE LIGHT INOP AT DOOR 2R. LAMP INOPERATIVE. REPLACED LAMP. CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,545 hrs · 18,280 cycles

SLIDE LIGHT INOP AT DOOR 4R. FOUND LAMP INOPERATIVE. REPLACED LAMP. OP CHECKS GOOD.

Part: DOOR — DENTED (L2) · airframe 51,045 hrs · 17,745 cycles

SMALL DENT LOWER RIGHT CORNER DOOR 2L. A PERMANENT REPAIR HAS BEEN REPAIRED PER UA-EVA-71342 A AND APPROVED VIA FAA FORM 8100-9 31 MARCH 2008 SR 1-795555670

Part: SKIN — DAMAGED (FUSELAGE) · airframe 51,045 hrs · 17,745 cycles

LEFT FUSELAGE SKIN AT STA 1715 STR 15L & I-16A HAS DAMAGE. LT FUSELAGE SKIN REPAIR AT BS 1715 S15L & I-16A IS TIME LIMITED REPAIR. APPROVED VIA FAA FORMS 8100-9 PER EVA UA-EVA-71357 A A CATEGORY "B" REPAIR PER PARAGRAPH "E" MUST BE ACP BY 31MAR10

Part: SKIN — DAMAGED (BS 305-320) · airframe 49,624 hrs · 17,239 cycles

TWO EACH MISSING FASTENERS NEAR STR 0 AT ABOUT STA 305 AND 320 NEED BLIND RIVETS INSTALLED TO FILL HOLES. MAJOR REPAIR ACCOMPLISHED. INSTALLED BLIND RIVETS AND INSPECTED 2 EACH RIVETS FOR VERIFICATIONS. NO DEFECTS FOUND AND A/C WAS RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (BS 440-600) · airframe 49,624 hrs · 17,239 cycles

SIX BURNS IN SKIN BETWEEN STA 440 AND 600, AND BETWEEN STR 2R AND 3R. MAJOR REPAIR ACCOMPLISHED. ACFT OPENED UP AND DISCOVERED 70 HITS, MANY SEVERE. WORKING FASTENER REPLACED & ACCOMPLISHED BURNISHING REPAIRS. REPAIRED 6EA BURNED AREAS AT STA 454,480,490,517,536,592 BETWEEN STR 2R AND 3R.

Part: SKIN — DAMAGED (BS 420-440 S2-3R) · airframe 49,624 hrs · 17,239 cycles

TWO BURNS IN SKIN BETWEEN STA 420 AND 440, AND BETWEEN STR 2R AND 3R. MAJOR REPAIR ACCOMPLISHED. ACFT OPENED UP AND DISCOVERED 70 HITS, MANY SEVERE. WORKING FASTENER REPLACED & ACCOMPLISHED BURNISHING REPAIRS.

Part: LATCH — DAMAGED (ESCAPE RAFT BIN) · airframe 49,242 hrs · 17,094 cycles

LATCH AND CATCH FOR RAFT BIN BROKE. RAFT AND ELT REMOVED FOR REPAIR.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 48,976 hrs · 17,005 cycles

FLAPS WILL NOT RETRACT OR EXTEND. INSPECTED FLAP AND LEADING EDGE FOR DAMAGE AND NO DEFECTS NOTED. OPERATIONAL CHECK WAS GOOD. REPLACED NR 1 FLAP SLAT ELECTRONIC UNIT.

Part: CONTROL PANEL — MALFUNCTIONED (RUDDER TRIM) · airframe 48,502 hrs · 16,838 cycles

RUDDER TRIM INTERMITTENT TWICE DURING FLIGHT. WORKED AFTER SEVERAL SHORT RE-ATTEMPTS. [08-07-07] REMOVED AND REPLACED RUDDER TRIM ACTUATOR AND RUDDER TRIM CONTROL PANEL

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,315 hrs · 16,768 cycles

FLOOR MOUNTED ESCAPE PATH LIGHT STRIP INOP AT MID LAV. [06-22-07] RECONNECTED LAMP TO FWD POWER CABLE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,315 hrs · 16,768 cycles

EXT EMERGENCY EXIT LIGHT INOP DOOR 4R. RELAMPED EMERGENCY LIGHT.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 47,877 hrs · 16,618 cycles

ELECTRICAL BURNING ODOR IN COCKPIT & CABIN, DISSIPATED QUICKLY, TURNED OFF RIGHT RECIRCULATION FAN. [06-14-07] CONDUCTED TROUBLESHOOTING TO IDENTIFY WHETHER SOURCE OF ODOR COULD BE FWD E&E COMP OR PNEUMATICS. RAN PACKS SEVERAL HRS ALSO RT FAN UNABLE TO DUPLICATE. ROOT CAUSE COULD NOT BE ESTABLISHED.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 46,784 hrs · 16,245 cycles

DOOR 1L PRESSURE BOTTLE OUT OF GREEN.

Part: UNKNOWN — ODOR (CABIN) · airframe 46,554 hrs · 16,152 cycles

SMOKE ODOR IN ROW 22 INFLT AND ON TAXI IN. INSPECTED CABIN LIGHTING, GALLEYS, LAVS,PITS AND RAN PACKS ON GROUND NO ABNORMAL SMELL NOTED AT THIS TIME. ROOT CAUSE OF SMOKE COULD NOT BE DETERMINED AT THIS TIME.

Part: INDICATOR — FAILED (R1 DOOR SLIDE) · airframe 46,218 hrs · 16,021 cycles

SLIDE LIGHT INOP DOOR 1R. CHECKED GIRT BAR SWITCH AREA TO BE FREE OF DEBRIS AND THAT SWITCHES ARE SECURE. THE ROOT CAUSE LIES IN A BLOWN LT SLIDE LIGHT INDICATOR ASSY. REPLACED SLIDE LIGHT ASSY.

Part: O-RING — LEAKING (ESCAPE SLIDE)

NEEDLE IN RED (LOW). PRESSURE GAGE FITTING LEAKING. REPLACED O-RING.

Part: SPLICE — CORRODED (CIRCUMFERENTIAL) · airframe 40,138 hrs · 13,850 cycles

AFT PIT STA 1400 LBL 18 CIRCUMFERENTIAL SPLICE IS CORRODED. DAMAGE CAUSED BY TYPICAL STA 1400 PIT CORROSION. FABRICATED CIRCUMFRENTIAL SPLICE STRAP AND REPLACED CORRODED STRAP.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,138 hrs · 13,850 cycles

AFT PIT STA 1360 AT STR 26L FRAME INBD FLANGE IS DENTED. INSTALLED NESTED J-ANGLE REPAIR.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,138 hrs · 13,850 cycles

AFT CARGO PIT SHEAR TIE CORRODED AT BS 1340 AND RBL 27. DAMAGE CAUSED BY TYPICAL AFT PIT CORROSION. REPLACED SHEAR TIE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,138 hrs · 13,850 cycles

CREASE NEAR BELLY SKIN CENTERLINE AT BS 1420 (EXTERIOR). SKIN DOUBLER REPAIRS AND STRINGER REPAIRS WERE ACCOMPLISHED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,138 hrs · 13,850 cycles

STA 1400 SHEAR CLIP SEVERELY CORRODED. DAMAGE CAUSED BY TYPICAL STA 1400 PIT CORROSION. REPLACED SHEAR TIE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,138 hrs · 13,850 cycles

CREASE NEAR BELLY CENTERLINE AT BS 1385 (EXTERIOR). SKIN DOUBLER REPAIRS AND STRINGER REPAIRS WERE ACCOMPLISHED.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,138 hrs · 13,850 cycles

AFT PIT STA 1620, FRAME IS DENTED AT STR 25L ON INBD FLANGE. INSTALLED NESTED J-ANGLE REPAIR.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,138 hrs · 13,850 cycles

STA 1400 FRAME SHEAR TIE BETWEEN STR 29R AND 30R IS SEVERELY CORRODED. DAMAGE CAUSED BY TYPICAL STA 1400 PIT CORROSION. REPLACED SHEAR TIE.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,138 hrs · 13,850 cycles

AFT PIT STA 1620 FRAME IS DENTED ON INBD FLANGE AT STR 25R. INSTALLED NESTED J-ANGLE REPAIR.

Part: SHEAR TIE — CORRODED (FUSLEAGE) · airframe 40,138 hrs · 13,850 cycles

AFT PIT FRAME SHEAR TIE IS CORRODED AT STA 1400 BETWEEN STRINGERS 27L AND 28L. DAMAGE CAUSED BY TYPICAL STA 1400 PIT CORROSION. REPLACED SHEAR TIE.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,138 hrs · 13,850 cycles

AFT PIT STA 1560 AT STR 26L FRAME IS DENTED ON INBD FLANGE. INSTALLED NESTED J-ANGLE REPAIR.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,138 hrs · 13,850 cycles

AFT PIT FRAME SHEAR TIE IN BILGE AREA IS CORRODED AT STA 1400 BETWEEN STR 28L AND 29L. DAMAGE CAUSED BY TYPICAL STA 1400 PIT CORROSION. REPLACED SHEAR TIE.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,138 hrs · 13,850 cycles

AFT PIT STA 1580 AT STR 26L FRAME IS DENTED ON INBD FLANGE. INSTALLED NESTED J-ANGLE REPAIR.

Part: FRAME — DENTED (FUSLAGE) · airframe 40,138 hrs · 13,850 cycles

AFT PIT STA 1480 FRAME IS DENTED ON INBD FLANGE AT STR 26L. INSTALLED NESTED J-ANGLE REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,138 hrs · 13,850 cycles

FLOORBEAM UPPER CAP IS CORRODED AT STA 365, RBL 16-73. SUPPLEMENTAL DATA UPDATE TYPICAL FLOORBEAM CORROSION DAMAGE. MAJOR REPAIR ACCOMPLISHED. REPAIRED USING NEW T-CAP SECTION AND SPLICE ANGLES.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 40,138 hrs · 13,850 cycles

FUSELAGE AT FRAME STA 640, FWD SHEAR TIE IS CRACKED AT STR 16L. SUPPLEMENTAL DATA UPDATE SHEAR TIE CRACKED DUE TO IMPACT DAMAGE. MAJOR REPAIR ACCOMPLISHED. SHEAR TIE WAS FABRICATED AND REPLACED.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 40,138 hrs · 13,850 cycles

SHEAR TIE HAS ELONGATED HOLES STA 620, BETWEEN STR 16L AND 17L. SUPPLEMENTAL DATA UPDATE SHEAR TIE FOUND DAMAGED DURING REPLACEMENT OF PREVIOUS REPAIR IN THE AREA. MAJOR REPAIR ACCOMPLISHED. SHEAR TIE REPLACEMENT WAS FABRICATED AND INSTALLED.

Part: PRESSURE PANEL — DAMAGED (FUSELAGE) · airframe 40,138 hrs · 13,850 cycles

AFT PRESSURE DECK HAS DAMAGE AT STA 1681 TO 1691, RBL 29 TO RBL 56. SUPPLEMENTAL DATA UPDATE DAMAGE CAUSED BY TYPICAL FLOOR CORROSION UNDER THE GALLEY AREA. MAJOR REPAIR ACCOMPLISHED. REMOVED EXISTING REPAIRS AND INSTALLED NEW DOUBLERS ON THE AFT PRESSURE DECK WEB.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 40,138 hrs · 13,850 cycles

FLOORBEAM T-CAP IS DAMAGED AT STA 1640, BL-0 TO RBL 61. SUPPLEMENTAL DATA UPDATE EXISTING REPAIR REQUIRED MODIFICATION. ORIGINAL DAMAGE CAUSED BY TYPICAL FLOORBEAM CORROSION. MAJOR REPAIR ACCOMPLISHED. REMOVED EXISTING REPAIR AND INSTALLED NEW T-CAP SECTION WITH SPLICE ANGLES AND STRAPS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,138 hrs · 13,850 cycles

FWD CABIN FLOORBEAM HAS CORROSION AROUND FASTENERS AT STA 324, RBL 51 TO RBL 52, BEAM UPPER CAP. DAMAGE DUE TO CORROSION. MAJOR REPAIR ACCOMPLISHED. DAMAGE WAS BLENDED. ANGLE REPAIR WAS INSTALLED.

Part: PROXIMITY SENSOR — MALFUNCTIONED (L1 DOOR GIRT BAR) · airframe 39,425 hrs · 13,586 cycles

DOOR 1L SLIDE LIGHT WILL NOT COME ON WHEN DOOR IS ARMED. REPLACED DEFECTIVE GIRT BAR PROXIMITY SENSOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,060 hrs · 11,384 cycles

SKIN CREASED LEFT SIDE OF FUSELAGE STA 1725, STR 19L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: CARBON SEAL — FAILED (ENGINE) · airframe 32,863 hrs · 11,304 cycles

HAZE AND NON-ELECTRICAL SMELL IN CABIN AT FLT 360 AFTER FA'S TURNED ON MOVIE SYSTEM. ATTENDANTS HAS TURNED OFF GALLEY POWER, VIDEO SYSTEM AND LIGHTS IN CABIN AND DID NOT SEEM TO HELP. SMELL AND HAZE WAS ONLY SLIGHT IN FLIGHT DECK. LINE TROUBLE SHOOTING TO ELIMINATE THE APU AS THE OIL SOURCE THE SUBJECT ENGINE WAS REPLACED AND SENT TO THE ENGINE SHOP FOR REPAIR. INSPECTION SHOWED THAT OIL FROM THE NR 3 AFT CARBON SEAL HAD ENTERED THE GAS PATH THROUGH THE 10TH OR 14TH STAGE BLEED DUCT. THE ROOT CAUSE IS A FAILED 2/3 CARBON SEAL CAUSING HIGH GEARBOX BREATHER PRESSURE AND THE LEAKAGE PAST THE NR 3 AFT CARBON SEAL.

Part: CARBON SEAL — FAILED (ENGINE) · airframe 32,831 hrs · 11,292 cycles

AFT LAV SMOKE DETECTOR ALARM ON AND A BLUISH SMOKE IN CABIN WITH SMELL OF OIL. CABIN WAS CLEARED BUT SMOKE RETURNED. FOLLOWING LINE TROUBLE SHOOTING TO ELIMINATE THE APU AS THE OIL SOURCE THE SUBJECT ENGINE WAS REPLACED AND SENT TO THE ENGINE SHOP FOR REPAIR. INSPECTION SHOWED THAT OIL FROM THE NR 3 AFT CARBON SEAL HAD ENTERED THE GAS PATH THROUGH THE 10TH OR 14TH STAGE BLEED DUCT. THE ROOT CAUSE IS A FAILED 2/3 CARBON SEAL CAUSING HIGH GEARBOX BREATHER PRESSURE AND THE LEAKAGE PAST THE NR 3 AFT CARBON SEAL.

Part: OIL SYSTEM — OVERTEMP (LEFT) · airframe 29,518 hrs · 10,098 cycles

ON DESCENT WITH POWER AT IDLE, LEFT OIL TEMPERATURE REDLINED TILL LANDING.

Part: REGULATOR — CORRODED (EVAC SLIDE)

DURING SHOP OVERHAUL OF SLIDE REMOVED FOR EXPIRATION OF TIME THE REGULATOR BODY AREA WAS FOUND TO BE BADLY CORRODED. *S/D* REPLACED REGULATOR.

Part: SURGE VALVE — MALFUNCTIONED (APU)

APU PNUEMATICS INOP. *S/D* REPLACED APU SURGE CONTROL VALVE. MOTORED ENGINES AND DUCT PRESSURE NORMAL.

Part: WIRE — DEFECTIVE (CABIN)

SECTION OF EEL SYSTEM FROM NUMBER TWO LEFT DOOR TO FIRST OVERWING EXIT DOOR WAS INOP. FOUND DEFECTIVE CABLE. REPAIRED CABLE, GROUND CHECK WAS GOOD.

Part: LIGHT — FAILED (CABIN)

EMERGENCY EGRESS LIGHTING IN FRONT OF AFT LAV INOP. REPLACED EMERGENCY EGRESS LIGHT ASSEMBLY, OPERATION CHECKS NORMAL.

Part: LIGHT STRIP — INOPERATIVE (CABIN)

EMERGENCY ESCAPE LIGHTING STRIP IN FRONT OF LAVATORY 108 INOP. REPLACED EMERGENCY ESCAPE LIGHTING STRIP AT LAVATORY 108, OPERATION CHECKS NORMAL.

Part: ASSIST BOTTLES — DISCHARGED (2 RT, 4 LT/RT)

DOOR ASSIST BOTTLES FOR NR 2 RT, NR 4 LT AND NR 4 RT WERE FOUND FLAT. REPLACED DOOR ASSIST BOTTLES AND ISOLATED CAUSE AS MATERIAL DEFECT. UAL HAS A RECOVERY PLAN AND IS CORRECTING.