N533UA

Part: STRUCTURE — DAMAGED (LT WING) · airframe 71,053 hrs · 26,108 cycles

LEFT WING L/E DISBOND. ACCOMPLISHED INTERIM REPAIR PER ECRA 5741-01202.

Part: ENGINE — SHUTDOWN (NR 1) · airframe 70,584 hrs · 25,948 cycles

NR 1 ENGINE IFSD. EPCS MSGS (S SVA OR FCU- EEC,P SVA OR FCU-EEC) ECS-MSG (L ENG LOW N1, L FUEL ON SOL, L ENG OIL PRESS. L ENG SEC CONT, L ENG PRI CONT) CHECKED CHIP DETECTORS AND ENGINE EXHAUST NO METAL FOUND. CREW COMMENTED FUEL CUTOFF LEVER NEVER MOVED TO CUTOFF. REPLACED NR 1 ENGINE MAIL OIL FILTER PER MM. NO METAL OR DEBRIS FOUND.

Part: LIGHT — BROKEN (CABIN) · airframe 70,553 hrs · 25,937 cycles

FLOOR EEL LIGHT STRIP INOP AT SEAT ROWS 8-11 LEFT. REPLACED BROKEN STRIP WITH NEW STRIP, APPROX 3FT IN LENGTH, OPS GOOD.

Part: BATTERY — FAULTY (MAIN) · airframe 70,464 hrs · 25,904 cycles

BATTERY CHARGER MESSAGE. REPLACED MAIN BATTERY AND THE CHARGER. MESSAGE CLEARED, GROUND OPS CHECK OK.

Part: FEEDER CABLE — FAILED (GENERATOR) · airframe 70,233 hrs · 25,822 cycles

APU AUTO SHUTDOWN A SECOND TIME. DID NOT ATTEMPT RESTART PROG. GENERATOR INOP AFTER APU REPLACEMENT. DOES NOT COME ONLINE. APU PNEU OK, ONLY ELECTRICALLY INOP. TROUBLESHOT SYSTEM, RAN APU GEN WOULD COME ONLINE APPROX 5 T0 10 SEC THEN DROP OFF SWAPPED APU GCU WITH LEFT ENG GCU SAME RESULTS RETURNED GCU'S TO ORIGINAL POSITIONS. REMOVED AND REINSTALLED GENERATOR FEEDER WIRES IAW WDM24-21-41. OPS CHECKED OK.

Part: CIRCUIT BREAKER — DAMAGED (P6-3 PANEL) · airframe 69,959 hrs · 25,719 cycles

CIRCUIT BREAKER C-14 ON P6-3 PANEL, LABELED "115 VAC BUS L SECT 2", TOP IS SHEARED OFF. MAINT TEXT: CORRECTION: SHOULD READ "SECT 1". REPLACED CIRCUIT BREAKER C313 (WDM 24-51-11). OPERATIONAL TEST OF P11-3 POWER MM TASK 24-50-00-715-003, EICAS DISPLAYS AND LIGHTING FUNCTIONS OK.

Part: BALLAST — DEFECTIVE (LAVATORY) · airframe 69,748 hrs · 25,650 cycles

FLIGHT ATTENDANT REPORTED SMOKE ODOR INSIDE AFT FORWARD LAV. REPLACED BALLAST IN AFT FORWARD LAV, NO DAMAGE FOUND OTHER THAN BALLAST, CHECKED ASSOCIATED WIRING OK. REPLACED BULBS NO HELP. MIRROR LIGHT INOP, DOME LIGHTS OPS GOOD. SEE PTT 7602003 FOR CORRECTIVE ACTION. PLEASE SIGN THIS ITEM OFF, OPBLM.

Part: BALLAST — ODOR (LAVATORY) · airframe 69,748 hrs · 25,650 cycles

FLIGHT ATTENDANT REPORTED SMOKE ODOR INSIDE FWD LAV. REPLACED BALLAST IN FWD LAV, NO DAMAGE FOUND OTHER THAN BALLAST, CHECKED ASSOCIATED WIRING OK.

Part: LIGHT — INOPERATIVE (LAVATORY) · airframe 69,768 hrs · 25,656 cycles

FLIGHT ATTENDANT REPORTED SMOKE ODOR INSIDE AFT FWD LAV. REPLACED BALLAST IN AFT FWD LAV, NO DAMAGE FOUND OTHER THAN BALLAST, CHECKED ASSOCIATED WIRING OK. MIRROR LIGHT INOP, DOME LIGHTS OPS GOOD.

Part: SWITCH — FAULTED (SPOILERS) · airframe 69,598 hrs · 25,603 cycles

EICAS MESSAGE 'SPOILERS' DISPLAYED. SPOILERS LIGHT ILLUMINATED WITH SPEED BRAKE LEVER SELECTED TO DOWN. FOUND SPOILER CONTROL MODULE 3 LEFT (M532) FAULTING FAULTBALL PCA, WILL NOT RESET. JUMPED PINS 2 AND 3 ON RIGHT HYR PRESSURE SWITCH. MESSAGE AND FAULTBALL CLEARED. REPLACED RIGHT HRD PRESSURE SWITCH REF MM 29-11-17. MESSAGE ON EICAS CLEARED AND FAULTBALL CLEARED. LEAK AND OPS CHECKED GOOD.

Part: WIRE — CHAFED (STARTER) · airframe 69,126 hrs · 25,424 cycles

DURING TAXI STARTER CUTOUT MESSAGE FLICKERED AND LIGHT FLICKERED. STARTER VALVE ASSY PER MM 80-11-02. SECURED CHAFED WIRING AT CONNECTOR D5024 IAW WD80-11-11. RAN ENG, OP CHECKED OK.

Part: ENGINE — MAKING METAL (NR 2) · airframe 69,024 hrs · 25,389 cycles

NR 2 ENGINE COMPRESSOR STALL IN FLIGHT. ENG RECOVERED AND CONTINUED OPERATING. IMMEDIATE PRECEDING STALL, ENGINE POWER WAS STEADY HIGH POWER (CRUISE OR CLIMB). CREW COMMENTS: DURING CRUISE AT FL380 EPR ROLLED BACK TO ZERO FOLLOWED CHECKLIST ENGINE RECOVERED SAMC TEXT: REF AMM 71-05-00 FIG 103 PAGE 104 FOR TROUBLESHOOTING. NR 2 ENGINE METAL IN TAILPIPE. ENGINE REPLACED.

Part: DUCT — DIRTY (COCKPIT) · airframe 68,865 hrs · 25,339 cycles

EXCESSIVE COCKPIT NOISE. CLEANED ALL FLIGHT DECK DISTRIBUTION DUCTING IAW AMM. ACCOMPLISHED RIGHT RECIRC FAN CHECK RT RECIRC FAN CHECKS GOOD. FLIGHT DECK GROUND NOISE LEVEL CHECK IS OK.

Part: TRANSMITTER — FAULTY (FUEL SYSTEM) · airframe 68,865 hrs · 25,339 cycles

NR 2 ENG FUEL FLOW TRANS 5433-2, ESN 727259, NR 2 ENG FUEL FLOW TRANSMITTER IS NOT SENDING ACCURATE DATA (ECM SHIFT) ON THIS ENGINE. REPLACE THE FUEL FLOW TRANSMITTER, MR73318, (PCN 480-9280). REPLACED FUEL FLOW TRANSMITTER ON NR 2 ENG. REPLACED FUEL DIST VALVE.

Part: ENGINE — HUNG START (LEFT) · airframe 68,345 hrs · 25,154 cycles

HUNG START ON LEFT ENGINE. SECOND START UNSATISFACTORY. 3RD ATTEMPT MADE WITH IGNITION IN BOTH. ENGINE HANGS AT 60% N2 AND WILL NOT ACCELERATE TO IDLE. NO LIMITS EXCEEDED. STARTER CUTOUT WAS NORMAL. REFER TO MM 73-21-00 FIG 111 ON PG125 FOR FAULT ISOLATION. FAULT REPEATED AFTER SECURING SVA ELECTRICAL CONNECTORS (3456001). STARTED LEFT ENGINE ON ING1, ING2 AND IN BOTH POSITION, THREE GOOD STARTS, NO FAULTS, NO MESSAGES, PERFORMED ACCELERATION CHECK PER JRH, OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: GIRT BAR — OBSTRUCTED (R4 DOOR) · airframe 68,068 hrs · 25,061 cycles

DOOR 4R WILL NOT ARM. REMOVED DEBRIS FROM GIRT BAR RECEPTICAL.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,113 hrs · 24,704 cycles

AFT CARGO COMPARTMENT BS 1360 BETWEEN STRINGERS S-29R - S-28R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION & FOUND MATERIAL LOSS OUT OF LIMITS. REMOVED CORRODED SHEAR TIE & ACP NDT OF HOLES COMMON TO REPAIR. FABRICATED AND INSTALLED NEW SHEAR TIE FROM 0.050\ 7075 T6 MATERIAL REF SRM 51-40-02.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 67,113 hrs · 24,704 cycles

AFT CARGO DOOR CUTOUT AREA BETWEEN BS 1380-1440 AT RBL 21 EXTRUSION PN 146N5391U24 FOUND CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION & FOUND MATERIAL LOSS OUT OF LIMITS OF SRM. REPLACED CORRODED EXTRUSION WITH NEW REF SRM 51-40-06 & SRM 51-40-02.

Part: CONTROL UNIT — INOPERATIVE (RAT) · airframe 66,984 hrs · 24,657 cycles

DURING RAT CHECK, RAT WILL NOT RETRACT USING MANUAL GROUND SWITCH. RANGOUT RAT BLADE INDEX & RAT STRUT INDEX SWITCHES OK, FOUND RAT CONTROL INOP, REPLACED PER MM, OPS CHECK GOOD.

Part: HANDLE — OBSTRUCTED (R3 DOOR) · airframe 66,919 hrs · 24,635 cycles

THE 3R MED ARMING PLACARD NOT CORRECT POSITION WHEN ATTD DISARMED DOOR. FLIGHT ATTENDENT REPORTED THAT THE ARMING HANDLE WOULD NOT GO PASS THE ARMING PLACARD. REMOVED BOTTLE CAP FROM UNDER SLIDE GRIT BAR SLIDE ARMS AND DISARMS NORMALLY.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 66,754 hrs · 24,573 cycles

FLASHLIGHT AT 3L RED LIGHT NOT FLASHING. REPLACED BATTERY PACK. OPS OKAY.

Part: APU — LEAKING · airframe 65,730 hrs · 24,183 cycles

CREW WAS REPORTING STRONG OIL-HYD SMELL IN FWD PART OF CABIN AND COCKPIT. PRIOR TO ENGINE RUN FOR TROUBLESHOOTING, ACP A DETAILED VISUAL INSP OF NR 1 ENGINE EXTERNALS FOR ANY EVIDENCE OF OIL OR HYD LEAKS. ACCOMPLISHED NO LEAKS NOTED. PNEUMATIC DUCTS CONTAMINATED WITH OIL OR HYD FLUID NEEDS CLEANING EYES & THROAT IRRITATION. FOUND OIL LEAK FROM APU THAT IS THE SOURCE OF THE CABIN SMELL. AREA HAS BEEN CLEANED, OK TO DEFER THE APU INOP PER MEL. AFTER CONVERSATIONS WITH MECH'S & OPB RPL APU PER AMM. APU HAS OVER 6,500 CYCLES. ACCOMPLISH PACK BURNOUT PER MM TO DETERMINE COCKPIT-CABIN AIR QUALITY IS ACCEPTABLE AFTER SOURCE OF SMELL IS CORRECTED. REPLACE RECIRCULATION FILTERS.

Part: PACKING — PINCHED (FUEL SYSTEM) · airframe 65,721 hrs · 24,180 cycles

ON WALK AROUND FOUND FUEL LEAKING FROM LEFT ENGINE OPENED FAN COWLS, SUSPECT FUEL COMING FROM FUEL OIL COOLER DRAIN. NR 2 ENGINE FUEL LEAKING FROM FCU FILTER HOUSING. FOUND FUEL FILTER COVER PACKING PINCHED. REPLACED PACKING, ALSO FUEL FILTER PER MM. IDLE LEAK CHECKED GOOD. REPLACED FILTER AND O-RINGS, LEAK CHECK GOOD. WORKING LOG2 ADF BEARING POINTER...DDK 0930.

Part: FAN — ODOR (RT RECIRCULATION) · airframe 65,714 hrs · 24,176 cycles

RT RECIRCULATION FAN HAS ODOR, RTFL. REMOVED RT RECIRCULATION FAN AND LT & RT RECIRCULATION FILTERS FOR INSPECTION. NO BURNING ODOR FOUND. REPLACED FILTERS AND RT FAN PER MM.

Part: UNKNOWN — ODOR (CABIN/COCKPIT) · airframe 65,714 hrs · 24,175 cycles

CREW REPORTED JUST AFTER ROTATION, FLIGHT ATTENDANT AT DOOR 2L DETECTED AN ACRID ODOR, THIS ODOR MOVED FORWARD TO DOOR 1L, AND THEN WAS NOTICED IN COCKPIT. CREW TURNED OFF BOTH UTILITY BUSSES AND ODOR DISSIPATED. TURNED ON BOTH UTILITY BUSSES, TURN ALL LIGHTS GALLEY EQUIPMENT, BOTH PACKS, VIDEO SYSTEM FOR OVER 30 MINS. NO ODOR NOTED. ALSO INSPECTED E/E COMPARTMENT FOR ANY EVIDENCE OF ELECTRIC ODOR, NONE NOTED. FOUND NO FAULTS OR EICAS MESSAGES PERTAINING TO THE ELECTRICAL SYSTEM, ALSO FOUND NO POPPED CIRCUIT BREAKERS.

Part: SLAT — SEPARATED (WING) · airframe 63,488 hrs · 23,353 cycles

L/E SLAT SKIN SEPARATION, FLIGHT DIVERTED. CREW REPORTS FAA INSPECTOR SAW A PIECE OF SHEETMETAL DEPART THE LEFT WING LEADING EDGE INBOARD OF NR 1 ENG. HONEYCOMB MATERIAL IS EXPOSED. REPLACED THE NR 5 LEADING EDGE SLAT. FIXED LEADING EDGE PANEL REPAIRED ALSO. REPAIR HAS BLIND FASTENERS. RE-INSPECTED, NO DEFECTS NOTED.

Part: OVEN — SMOKE (GALLEY) · airframe 61,482 hrs · 22,575 cycles

SMOKE FROM FWD OVEN. PIECE OF PAPER IN FWD OVEN CAUGHT ON FIRE. F/A DISCHARGED FIRE EXTINGUISHER IN FWD GALLEY.

Part: RIB — CRACKED (LE SLAT)

NR 6 T/E SLAT DAMAGED. INBOARD RIB CRACKED SKIN DENTED. REPLACED T/E PER SM 50-57-56-01-JD. REPLACED END RIB INBOARD SIDE REF DOC 114N3002. REPAIRED DENT PER 71883A EVA.

Part: BOTTLE — LOW

LOW BOTTLE. LEAKING AT FILL VALVE. REPLACED FILL VALVE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 56,716 hrs · 20,773 cycles

EMERGENCY EXIT LIGHTS OUT AT DOOR 2L (3EA) AND 1 EA FWD OF DOOR 2R. REPLACED BATTERY PACK AND CHARGER AT DOOR 2L. OP CHK GOOD.

Part: SHEAR TIE — OUT OF TOLERANCE (FUSELAGE) · airframe 56,062 hrs · 20,518 cycles

EXISTING FASTENER HOLE WAS FOUND LOCATED TOO FAR AFT. THE FASTENER IS COMMON TO THE SIDE LINK FITTING (012N8887), SHEAR TIE FITTING (112N7017) AND THE TENSION CLIP (012N8886). THIS FASTENER LOCATION WAS LOCATED AT THE FACTORY 85625 DURING OEM ASSEMBLY AND THE 112N7009-14 DRAG FITTING WAS MODIFIED TO MAKE ROOM FOR THE FASTENER. ACCOMPLISHED MAJOR REPAIR.

Part: SLIDE — FAULTY (L1 DOOR) · airframe 56,062 hrs · 20,518 cycles

L-1 MED EVAC SLIDE HANDLE DOESN'T FULLY ENGAGE. HANDLE ONLY MOVES TWO-THIRDS TRAVEL IN ARM DIRECTION. OVERHEAD ANNUNCIATOR DOESN'T TURN ON EITHER. FOUND SLIDE PACKED WAS NOT IN CORRECT SHAPE, THUS CAUSING THIS PROBLEM. REPLACED SLIDE ASSY, OPS CHECKED NORMALLY.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,062 hrs · 20,518 cycles

FOUND DENT AND WEAR MARKS ON FUSELAGE. ACCOMPLISHED MAJOR REPAIR.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 56,062 hrs · 20,518 cycles

COACH CLASS EEL FWD AND AFT SECTIONS INOP. REPLACED FEEDER CABLE.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 56,062 hrs · 20,518 cycles

EEL FIRST CLASS AND MID LAV INOP. RESEATED CONNECTORS.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,062 hrs

OVERHEAD EMERGENCY LIGHT AT CLASS DIVIDE CURTAIN IS INOP. REPLACED FUSE.

Part: FIRE LOOP — BROKEN (NR 1 NACELLE) · airframe 56,062 hrs · 20,518 cycles

NR 1 ENG PYLON DUCT LEAK LOOP TS5260 IS BROKEN. REPLACED LOOP TS5260, REF MM26-18-01. OPS CHECKS NORMAL PER MM 26-18-01.

Part: FRAME — DAMAGED (BS 1620 S26R) · airframe 56,062 hrs · 20,518 cycles

AFT PIT FUSELAGE STA 1620 FRAME AT STR 26R. ACCOMPLISHED A MAJOR REPAIR AT GSO.

Part: FRAME — DENTED (BS 1460 S26L) · airframe 56,062 hrs · 20,518 cycles

AFT LOWER CARGO COMPARTMENT FUSELAGE FRAME DENTED AT BS 1460 AT STR 26L, INBOARD FLANGE. ACCOMPLISHED A MAJOR REPAIR AT GSO.

Part: PAN — DAMAGED (L2 DOOR HANDLE) · airframe 56,062 hrs · 20,518 cycles

DOOR 2L DOOR HANDLE PAN GOUGED AND HAS LIGHTNING STRIKES (3 EA). ACCOMPLISHED A MAJOR REPAIR AT GSO.

Part: SKIN — DAMAGED (R2 DOOR) · airframe 56,062 hrs · 20,518 cycles

DOOR 2R UPPER HINGE ARM CUTOUT REQUIRES DOUBLER. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED A MAJOR REPAIR AT GSO.

Part: FRAME — GOUGED (BS 1520 S22-24R) · airframe 56,062 hrs · 20,518 cycles

AFT PIT FRAME GOUGED NUMEROUS PLACES AT BS 1520 BETWEEN STR 22R AND STR 24R. ACCOMPLISHED A MAJOR REPAIR AT GSO.

Part: INSERT — CORRODED (R4 DOOR HANDLE) · airframe 56,062 hrs · 20,518 cycles

R4 DOOR HANDLE BOX INSERTS CORRODED. ACCOMPLISHED A MAJOR REPAIR AT GSO.

Part: SKIN — DAMAGED (BS 1420 S26L) · airframe 56,062 hrs · 20,518 cycles

AFT PIT FUSE STA 1420 AT STR 26L HAS DAMAGE. ACCOMPLISHED A MAJOR REPAIR.

Part: FRAME — DENTED (BS 1480 S25-26L) · airframe 56,062 hrs · 20,518 cycles

AFT LOWER CARGO PIT, FUSELAGE FRAME UPPER CHORD DENTED AT BS 1480 BETWEEN STR 25L-26L. ACCOMPLISHED A MAJOR REPAIR AT GSO.

Part: FRAME — DAMAGED (BS 1520 S24-26R) · airframe 56,062 hrs · 20,518 cycles

AFT PIT FRAME AT BS 1520R, STR 24.5R - 26R HAS DAMAGE. ACCOMPLISHED MAJOR REPAIR AT GSO.

Part: FRAME — DENTED (BS 1440 S25-26L) · airframe 56,062 hrs · 20,518 cycles

AFT LOWER CARGO COMPARTMENT, FUSELAGE FRAME DENTED ON INBOARD FLANGE, BS 1440, AT STR 25L-26L. ACCOMPLISHED MAJOR REPAIR AT GSO.

Part: SKIN — DAMAGED (L2 DOOR) · airframe 56,062 hrs · 20,518 cycles

DOOR 2L UPPER HINGE ARM CUTOUT REQUIRES DOUBLER. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED A MAJOR REPAIR AT GSO.

Part: FRAME — GOUGED (FUSELAGE) · airframe 56,062 hrs · 20,518 cycles

AFT PIT FRAME GOUGED NUMEROUS PLACES AT BS 1520 BETWEEN STR 22R THRU STR 24R. ACCOMPLISHED MAJOR REPAIR AT GSO.

Part: HINGE PIN — BROKEN (EVAC SLIDE) · airframe 56,062 hrs · 20,518 cycles

L1 DOOR SLIDE LOWER LATCH ASSY HINGE PIN IS BROKEN. UNKNOWN DAMAGE. REPLACED L1 DOOR SLIDE ASSY.

Part: STRUCTURE — CRACKED (L2 DOOR) · airframe 56,062 hrs · 20,518 cycles

DOOR 2L UPPER HINGE ARM CUTOUT REQUIRES DOUBLER. ACCOMPLISHED MAJOR REPAIR AT GSO.

Part: INSERT — CORRODED (R4 DOOR) · airframe 56,062 hrs · 20,518 cycles

R4 DOOR HANDLE BOX INSERTS CORRODED. REMOVED AND REPLACED HANDLE BOX ASSY.

Part: STRUCTURE — DAMAGED (R2 DOOR) · airframe 56,062 hrs · 20,518 cycles

DOOR 2R UPPER HINGE ARM CUTOUT REQUIRES DOUBLER. ACCOMPLISHED MAJOR REPAIR AT GSO.

Part: PULLEY — CRACKED (ELEVATOR) · airframe 56,062 hrs · 20,518 cycles

CABIN CEILING AREA ELEVATOR CONTROL CABLE PULLEY CRACKED OB SIDE BETWEEN BS 333 AND BS 350 L4L. STRESS FRACTURE. REPLACED ELEVATOR CONTROL CABLE PULLEY.

Part: SLIDE — DISENGAGED (R1 DOOR) · airframe 55,961 hrs · 20,478 cycles

SLIDE AT DOOR 1R IS DISENGAGED FROM DOOR. REINSTALLED SLIDE.

Part: SKIN — DELAMINATED (NR 6 SLAT) · airframe 55,467 hrs · 20,283 cycles

RTFL WITH A DELAMINATING NR 6 SLAT. POSSIBLE BIRD STRIKE. THE RT WING LE AREA INBOARD OF THE ENGINE DELAMINATION AND MISSING MATERIAL. AREA OF DAMAGE IS APPROX 1 FOOT LONG BY 6" WIDE. THIS DAMAGE IS TO THE NR 6 SLAT. REPLACED THE NR 6 LE SLAT

Part: WARNING LIGHT — ILLUMINATED (MLG) · airframe 55,160 hrs · 20,166 cycles

AFTER DEPARTURE "GEAR DISAGREE" INDICATION WAS DISPLAYED ON EICAS. MESSAGE WAS DISPLAYED FOR APPROX 15 MIN UNTIL AIRCRAFT ENCOUNTERED SLIGHT TURBULENCE AND CAUSED MESSAGE TO CLEAR AND AMBER "GEAR" LIGHT TO EXTINGUISH.

Part: SEAL — LEAKING (STARTER DRIVE) · airframe 53,981 hrs · 19,753 cycles

NR 1 ENGINE HIGH OIL CONSUMPTION EXCEEDS LIMITS. [08-07-07] REPLACED NR 1 ENG STARTER DRIVE SEAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,828 hrs · 19,704 cycles

EMERGENCY LIGHT STRIP INOPERATIVE IN FRONT OF AFT LAV. [06-22-07] REPLACED EMERG LIGHT STRIP OPS CK GOOD.

Part: LEVER — FAULTY (R1 DOOR SLIDE) · airframe 52,598 hrs · 19,262 cycles

DOOR 1R DISARM LEVER HARD TO DISARM. CREW REPORTS LEVER MOVED FORCEFULLY TO DISARM AND HEARD UNUSUAL NOISE, DOOR APPEARS TO BE DISARMED. CLEANED DEBRIS AND ICE FROM GIRT BAR SENSOR AREA. ARM LEVER NOW NORMAL. NO COMPONENTS REPLACED.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 52,573 hrs · 19,254 cycles

FOUND EMERGENCY LIGHT STRIP ON FLOOR IN FRONT OF FIRST CLASS CLOSET INOP. PROBLEM WAS TRACED TO THE FEEDER CABLE AND BROKEN PINS ON THE WALL. REPLACED FEEDER CABLE AND LIGHT STRIP.

Part: LIGHT — LOOSE (CABIN) · airframe 51,926 hrs · 19,010 cycles

EEL LIGHT INOP BY ROW 1. REINSTALLED LOOSE EEL LIGHT STRIP.

Part: JUMPER — FAULTY (EMERGENCY LIGHT) · airframe 51,926 hrs · 19,010 cycles

EEL LIGHTS INOP FROM ROW 9 TO ROW 13. REPLACED MALE TO MALE JUMPER.

Part: WARNING MESSAGE — ILLUMINATED (SLATS) · airframe 50,708 hrs · 18,551 cycles

ON APPROACH THE CREW RECEIVED A LEADING EDGE SLAT DISAGREE MESSAGE.

Part: BLADE — FAILED (COMPRESSOR) · airframe 43,921 hrs · 16,043 cycles

LEFT ENGINE COMPRESSOR STALL AND SURGE WHILE IN STEADY CLIMB CONFIGURATION. SHOP TEARDOWN CONFIRMED A HPT STAGE 2 BLADE FAILURE. BLADES OF THIS PART NUMBER HAVE BEEN BEING REMOVED FROM ENGINES DURING ENGINE SHOP VISITS SINCE MAY 2003. THE REMOVAL OF THE REMAINDER OF THESE BLADES IS EXPECTED TO BE COMPLETED IN 2005.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 42,132 hrs · 15,434 cycles

EMERGENCY LIGHTS INOP, OUTSIDE OF AFT CARGO DOOR, AISLE LIGHT AT ROW 25, EXIT SIGN ON CEILING PANEL AT ROW 16. REPLACED EMERGENCY BATTERY CHARGER AND BATTERY PACK.

Part: SWITCH — FAILED (NR 1 ENGINE) · airframe 40,052 hrs · 14,638 cycles

A/C RECEIVED NR 1 ENGINE OIL FILTER BYPASS MESSAGE. DELTA PRESSURE SWITCH AND OIL FILTER REPLACED.

Part: FRAME — DENTED (FUSELAGE) · airframe 37,265 hrs · 13,599 cycles

AFT PIT FUSELAGE FRAME INNER FLANGE DENTS STATION 1380 STRINGER 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR ON FLANGE.

Part: FRAME — DAMAGED · airframe 37,265 hrs · 13,599 cycles

AFT PIT FRAME BODY STATION 1620 ABOVE STRINGER 26R EDGE DAMAGED FROM DRILL START. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.DOUBLER REPAIR APPLIED TO WEB AND INBD CAP.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 37,265 hrs · 13,599 cycles

LEFT HAND CREASE BEAM WEB AT BODY STATION 1020-1023 HAS EXCESSIVE MATERIAL LOSS AFTER REMOVAL OF CORROSION. MAJOR REPAIR ACCOMPLISHED. CREASE BEAM WEB REPLACED.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 37,265 hrs · 13,599 cycles

LEFT HAND CREASE BEAM WEB AT BODY STATION 1020-1023 HAS EXCESSIVE MATERIAL LOSS AFTER REMOVAL OF CORROSION. MAJOR REPAIR ACCOMPLISHED. CREASE BEAM WEB REPLACED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,265 hrs · 13,955 cycles

CABIN FLOORBEAM AT STATION 365 RBL 43 HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. EXCESSIVE MATERIAL WAS REMOVED AND A STRAP REPAIR APPLIED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,265 hrs · 13,599 cycles

CABIN FLOOR SUPPORT AT STATION 365 RBL 45 HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. FILLER AND DOUBLER INSTALLED.

Part: PLATE — CORRODED (FUSELAGE) · airframe 37,265 hrs · 13,599 cycles

AFT CABIN DECK PLATE HAS EXCESSIVE MATERIAL LOSS AT STATION 1681 RBL 9.5-RBL 14. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: PLATE — CORRODED (FUSELAGE) · airframe 37,265 hrs · 13,599 cycles

AFT CABIN DECK PLATE CORRODED AT STA 1681 RBL 22.5 TO RBL 52. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 37,265 hrs · 13,599 cycles

CABIN FLOORBEAM BODY STATION 640 LBL 4 TO LBL 17 HAS EXCESSIVE MATERIAL REMOVED DUE TO GOUGE IN CENTER O/B BEAM. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP AND NESTED ANGLE REPAIR.

Part: FRAME — CORRODED (FUSELAGE) · airframe 37,265 hrs · 13,599 cycles

AFT CARGO COMP STATION 1480 FUSE FRAME ABOVE STRINGER 22R HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,265 hrs · 13,599 cycles

CABIN FLOORBEAM BODY STATION 440 UPPER SURFACE HAS EXCESSIVE MATERIAL LOSS DUE TO REMOVAL OF CORROSION AT RBL 4 TO RBL 5.5. MAJOR REPAIR ACCOMPLISHED. STRAP REPAIR INSTALLED.

Part: FRAME — DENTED (FUSELAGE) · airframe 37,265 hrs · 13,599 cycles

AFT PIT FRAME STATION 1420 DENTED ABOVE STRINGER 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND STRAP.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 37,265 hrs · 13,599 cycles

MID CABIN FLOOR BODY STATION 960-984 RBL 65-72 CREASE BEAM UPPER EXCESSIVE MATERIAL LOSS DUE TO CORROSION REMOVAL. MAJOR REPAIR ACCOMPLISHED. CREASE BEAM WEB REPLACED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 37,265 hrs · 13,599 cycles

AFT CARGO COMPARTMENT CIRCUMFERENTIAL FRAME AT BODY STATION 1520 LBL 16 CORRODED. MAJOR REPAIR ACCOMPLISHED. REPAIR STRAP INSTALLED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 37,265 hrs · 13,599 cycles

FORWARD NOSE COMP STATION 231.25 RBL 4 FRAME UPPER CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP.

Part: WIRE — BROKEN (LEFT)

RETURNED TO IAD DUE TO PARTIAL ELECTRICAL FAILURE. TERMINAL LUGS L2 (PHASE B) AND L3 (PHASE C) WERE FOUND BROKEN AT LEFT GENERATOR CIRCUIT BREAKER C901. LOSS OF PHASE B AND PHASE C AT L GEN CB CAUSED PARTIAL ELECTRICAL FAILURE. THE WIRE TERMINALS WERE REPLACED.

Part: TUBE — LEAKING (SLIDE)

SLIDE FAILED AIR RETENTION TEST DURING SHOP VISIT. *S/D* POROSITY CAUSED SEAM LEAK. UNIT WAS SENT TO VENDOR FOR EVALUATION AND REPAIR.

Part: STARTER — FAILED (APU)

APU WOULD NOT START. *S/D* REPLACED STARTER PER MM 49-41-01, OPS CHECKED GOOD.

Part: INTER LOCK — ENGAUGED (RT THROTTLE)

THE RIGHT THROTTLE LEVER STICKS AT MID POSITION. TAKEOFF THRUST NOT ACHIEVED. ABORTED TAKEOFF AT 65 KNOTS. *S/D* ABORTED TAKEOFF AT65 KTS. RT THROTTLE STUCK ABOUT HALFWAY. LT THROTTLE OK, (FOUND INTER-LOCK ENGAGED).

Part: BATTERY PACK — DISCHARGED (CABIN)

EEL LIGHTING GOES OFF AFTER 7 SECONDS WITH MASTER SWITCH IN FLIGHT DECK AND AGAIN WITH AFT ATTENDANT PANEL TURNED ON. REPLACED BATTERY PACK AND LIGHTS CHECK NORMAL.

Part: EEL LAMP — INOP (CABIN)

EMERGENCY ESCAPE PATH LIGHTING INOP AT ROW NR 16. RELAMPED. CHECKS O.K.

Part: EEL LAMP — FAILED (CABIN)

EMERGENCY ESCAPE PATH LIGHTING INOP ROW NR 16. RELAMPED, CHECKS OK.