N564UA

Part: SWITCH — DEFECTIVE (FUEL DOOR) · airframe 69,470 hrs · 25,514 cycles

PREFLIGHT CHECK OF CTR FUEL PUMPS FAILED. CTR PUMP LIGHTS DO NOT ILLUMINATE AFTER 10 SEC. TROUBLE SHOT IAW WDM 28-21-11. R & R S346 FUEL PANEL DOOR OPEN SWITCH. FUEL PUMPS OPERATION IS NORMAL IAW AMM 28-22-00.

Part: UNKNOWN — FAULTY (L4 DOOR) · airframe 69,375 hrs · 25,483 cycles

DOOR 4L ARMED LIGHT IS ON BUT DOOR IS DISARMED. SLIDE INDICATOR OVER DOOR 4L IS DIMLY LIT WHEN DISARMED. VERIFIED GIRT BAR OPERATION NORMAL WHEN ARMING & DISARMING. SWAPPED LIGHT MODULE, NO HELP. NEEDS TROUBLESHOOTING, WHEN ARMED LIGHT TURNS BRIGHT INDICATING ARMED AS SUPPOSED TO.

Part: ACTUATOR — FAILED (RUDDER) · airframe 69,125 hrs · 25,406 cycles

AUTOPILOT ADJUSTMENT TEST FAILS CTR RUDDER SERVO TEST. REPLACED CTR RUDDER ACTUATOR. ACCOMPLISHED TESTS REQUIRED FOR ACTUATOR REPLACEMENT.

Part: SMOKE GOGGLES — FAULTY (COCKPIT) · airframe 68,941 hrs · 25,341 cycles

CAP NEEDS A NEW SMOKE GOGGLE. REPLACED WITH NEW SMOKE GOGGLE

Part: HEADSET — FAULTY (COCKPIT) · airframe 68,851 hrs · 25,308 cycles

CAPT HEADSET MIC IS HOT IN FLT INPH & SERV INPH, REPEAT WRITEUP. REPLACED CAPTS HEADSET, OPERATIONS CHECKED GOOD.

Part: FEEDER CABLE — DAMAGED (CABIN) · airframe 68,829 hrs · 25,299 cycles

EMERGENCY EXIT LIGHT STRIPS INOPERATIVE FROM ROW 8 THRU ROW 12. THE IN TRACK FEEDER CABLE IS OPEN. IN ADDITION, AT LEAST 2 ILLUMINATED STRIPS ARE INOPERATIVE. SPLICED IN FEEDER CABLE & REPLACED TRACK COVER. TESTED IAW AMM 33-51-96, 801, 401. ACCOMPLISHED SAFETY & SECURITY OF EMERGENCY EXIT LIGHT INSTALLATION.

Part: GUIDE VANE — CRACKED (NR 2 ENGINE) · airframe 68,789 hrs · 25,284 cycles

NR 2 ENG FOUND CRACKED GUIDE VANE ON WALK AROUND INSPECTION. ONE EACH ALUMINUM EXIT GUIDE VANE REMOVED FROM THE ONE O'CLOCK POSITION, ENG SN 727114. INSTALL REPLACEMENT VANE DURING NEXT ENGINE SHOP VISIT SINCE ENGINE HAS LESS THAN 500 CYCLES REMAINING TO SHOP VISIT.

Part: SKIN — TORN (NR 2 NACELLE) · airframe 68,014 hrs · 25,027 cycles

NR 2 ENGINE CORE COWL OTBD SKIN HAS A TEAR MEASURING 2.75" LONG AND .5 WIDE. REPLACED NR 2 ENGINE OTBD CORE COWL IAW AMM.

Part: LAMP — INOPERATIVE (L4 DOOR SLIDE) · airframe 67,935 hrs · 25,004 cycles

L4 DOOR SLIDE LIGHT INOPERATIVE. VERIFIED GIRT BAR ENGAGED. REPLACED LAMP LIGHT, ARM LIGHT CHECKED OK.

Part: COVER — UNSECURE (EMERGENCY LIGHT) · airframe 67,677 hrs · 24,917 cycles

LIGHTING STRIP AT 34F HAS FALLEN OFF. REPLACED EMERGENCY LIGHT COVER FROM SEAT 24 TO 32.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 67,677 hrs · 24,917 cycles

EMERGENCY LIGHT FROM ROWS 28 THROUGH 32 INOPERATIVE. REPLACED FEEDER CABLE FROM SEAT 32. ALL EMERGENCY LIGHTS CHECKED GOOD.

Part: BATTERY — FAULTY (MAIN) · airframe 67,021 hrs · 24,702 cycles

STATUS MSG MAIN BATTERY CHAGER. REPLACED BATTERY AND CHARGER, ALL CHECKS OK NOW. SYSTEM REMOVED AND REPLACED PER MM.

Part: CAP — MISSING (CABIN) · airframe 66,956 hrs · 24,679 cycles

EMERGENCY EXIT LIGHT END CAP MISSING AT 8C AND 40C. REPLACED END CAPS.

Part: CONTROLLER — FAILED (WINDOW HEAT) · airframe 66,403 hrs · 24,491 cycles

WINDOW EICAS MESSAGE DISPLAYED. INOPERATIVE MESSAGE LIGHT DID NOT EXTINGISH WHEN SWITCH WAS RECYCLED TO OFF THEN ON. REPLACED WINDOW HEAT CONTROLLER.

Part: ARM — OUT OF ADJUST (SLIDING WINDOW) · airframe 66,011 hrs · 24,359 cycles

F/O SLIDING WINDOW HANDLE BINDING. ADJUSTED LOWER LINK ARM.

Part: ENGINE — MAKING METAL (NR 1) · airframe 65,730 hrs · 24,264 cycles

REPLACE NR 1 ENGINE REF LM4718 DUE TO EXCESSIVE METAL FOUND IN OIL FILTER AND CHP REF MM 71-00-02 CONFIG 1. REPLACE NR 1 ENGINE REF LM4718 DUE TO EXCESSIVE METAL FOUND IN OIL FILTER AND CHP. REMOVED NR 1 ENGINE.

Part: SEAL — LOOSE (EVAC SLIDE) · airframe 65,730 hrs · 24,264 cycles

DOOR 4R, LOWER AFT SLIDE COVER HAS LOOSE SEAL. SEAL GOES BETWEEN SLIDE COVER AND FLOOR. THIS IS A DUST SEAL AT BOTTOM OF DOOR 4R INNER DOOR SLIDE COVER. INTERIM REPAIR MADE WITH TAPE TO SECURE DUST SEAL TO SLIDE COVER. REPAIR WITHIN 2 CYCLES. REPLACED HARDWARE. RE-SECURED DUST SEAL TO SLIDE COVER.

Part: FAN — INOPERATIVE (E&E BAY) · airframe 65,541 hrs · 24,199 cycles

HAVE EQUIPMENT OVERHEAT, FORWARD EQUIPMENT FAN INOP. ALSO FOUND THAT THE LEFT RECIRC FAN INOP AND CAUSING ABOVE MESSAGE. SUSPECT FAN BAD. REPLACED RELAYS K10509 AND K124 REF WD21-25-04. REPLACED LEFT RECIRC FAN, CHECKS OK.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 65,528 hrs · 24,195 cycles

1ST OFFICER'S WINDSHIELD'S VISIBILITY IS AFFECTED BY DEFECTS, REPLACE FIRST AVAILABLE. DELAMINATED RIGHT SIDE AND ALONG BOTTOM. REPLACED NR 1 RIGHT WINDSHIELD PER MM.

Part: VANE — BENT (RT ENGINE) · airframe 65,255 hrs · 24,092 cycles

RT ENGINE EXIT GUIDE VANE BENT, AT ONE O'CLOCK LOOKING FWD. REMOVED DAMAGED FAN EXHAUST GUIDE VAN, LOWER RUBBER BASE SEAL AND VANE SEGMENT. REMOVED DAMAGED. UPPER CUT OFF VANE SEGMENT AND SEAL REMAINING AS REQUIRED BY MM.

Part: CONTROL PANEL — FAULTY (POSIT 1) · airframe 65,217 hrs · 24,080 cycles

MODE CONTROL PANEL NEEDS RESET. REPLACED MODE CONTROL PANEL PER MM. PERFORMED CATIII CK PER MM. SYSTEM TESTED OKAY.

Part: ROLLER — WORN (TE FLAPS) · airframe 65,116 hrs · 24,043 cycles

ACFT VIBRATION, DROPPED FLAPS. LEFT INBD AFT FLAP HAS EXCESSIVE PLAY WHEN FULL EXTENDED. AFTER FURTHER INSPECTION SUSPECT TRAILING EDGE FLAP CARRIAGE ROLLERS TO BE WORN. ALSO FOUND BEARINGS, WORN ON THE MID AND OUTER CARRIAGE. FOUND RT WING LOWER TE PANEL SUPPORT RIVETS SHEARED AND LOOSE LOCK FASTENERS. REPLACED RIVETS AND LOCK FASTENERS PER SRM. REPLACED ALL LEFT AND RIGHT INBD SLAT SEALS. TEST FLIGHT ACCOMPLISHED, CHECKED BOTH OVERWING AREAS DURING PITCH, ROLL, ALTITUDE, FLAP SETTINGS, NO HUM OR VIBRATION FELT.

Part: NUT — CRACKED (NR 3 WHEEL) · airframe 65,066 hrs · 24,024 cycles

NR 3 AFT TIRE: ONE TIE BOLT NUT IS CRACKED. REPLACED TIRE.

Part: SERVICE PANEL — LOOSE (HYD SYSTEM) · airframe 65,066 hrs · 24,024 cycles

DURING DESCENT, VERY NOTICEABLE VIBRATION IN FLOOR FROM ROW 20 TO DOORS 2R&L. FOUND HYD SERVICE PANEL LEADING EDGE LATCHES OUT OF ADJUSTMENT. PANEL VERY LOOSE, ADJUSTED LATCHES.

Part: BEARING — WORN (RAM AIR DOOR) · airframe 64,668 hrs · 23,889 cycles

VIBRATION AND HUM IN FLIGHT AT ROWS 10, 11, AND 21. ROWS 11, 22 AND 28 THE NOISE SEEMS TO BE GETTING LOUDER. EARLIER IN DESCENT THE NOISE WAS LESS BUT VIBRATION STILL THE SAME IN ROWS 11, 22 AND 28. FOUND RIGHT RAM AIR HEAT SINK OUTLET DOOR HINGES WORN WITH A LOT OF PLAY. FOUND BEARING WORN. REPLACED WORN PARTS. ACCOMPLISHED RAM AIR SYSTEM TEST. OPS AND INDICATION CHECKED OK. REPLACED RIGHT RAM AIR EXHAUST DOOR ARM ASSY, LINK ASSY AND BEARING DUE TO WEAR. ACCOMPLISHED RAM AIR SYSTEM TEST. CHECKED NORMAL.

Part: BEARING — LACK OF LUBE (L2 DOOR) · airframe 63,805 hrs · 23,584 cycles

DOOR 2L HARD TO OPEN. LUBED TORQUE TUBE BEARING, OPERATED DOOR SEVERAL TIMES, OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (L1 DOOR SLIDE) · airframe 63,509 hrs · 23,479 cycles

L1 DOOR SLIDE ARMED LIGHT INOPERATIVE. RELAMPED, OP CHECKED GOOD.

Part: PCA — LOOSE (ELEVATOR) · airframe 62,115 hrs · 22,976 cycles

FOUND LT ELEVATOR MIDDLE PCA REACTION LINK AND PCA ACTUATION ROD EXTREMELY LOOSE. FOUND LT ELEVATOR MIDDLE PCA REACTION LINK AND PCA ACTUATION ROD EXTREMELY LOOSE REF: PTT 1152007. REPLACED LT ELEVATOR MIDDLE PCA PER MM 27-31-05.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 61,659 hrs · 22,807 cycles

NOISE IN COCKPIT VERY LOUD ON DESCENT REGARDLESS OF RECIRC FAN BEING ON OR OFF. COMPLIED WITH MEL, ACP STEP 6 OFF. THE FLOW AND VELOCITY FAILED. FLOW WAS 437 CFM SHOULD BE BELOW 375 CFM. VELOCITY WAS 5009 FPM SHOULD BE BELOW 3430 FPM.

Part: LIGHT — UNSECURE (CABIN) · airframe 61,212 hrs · 22,626 cycles

CREW REPORT: EMERGENCY EXIT FLOOR LIGHTING LOOSE AT 13C. SECURED LIGHT STRIP.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 61,198 hrs · 22,622 cycles

1ST OFFICER'S FIXED SIDE-AFT WINDOW'S VISIBILITY IS AFFECTED BY DEFECTS. REPLACE FIRST AVAILABLE. CREW COMMENTS: WINDOW R3 HAS 2 DELAM BUBBLES SIZE OF A CHILDS HAND. REPLACED WINDOW PER MM.

Part: SENSOR — INOPERATIVE (R3 DOOR) · airframe 61,070 hrs · 22,577 cycles

F/A REPORTED DOOR 3R SLIDE ARMED LIGHT INOP. VERIFIED GIRT BAR ENGAGEMENT CORRECT AND DOOR ARMS CORRECTLY. ONLY LIGHT INOP. NEEDS LIGHT SOCKET ASSY, (PCN 561-2342) NIS AT MCO. WILL NEED TIME TO DISASSEMBLE OVERHEAD DOOR LINER TO REPLACE SWITCH ASSY L408. REPLACED LIGHT ASSY, NO HELP. TRIED ANOTHER LIGHT ASSY ALSO NO HELP. SUSPECT POSSIBLE PROX SW. PROX SW NOT AVAIL LAS. SHOULD READ DOOR 3 RIGHT. REPLACED THE REAR GIRT BAR PROX SENSOR, OPS CHECKED OKAY.

Part: SEAL — DAMAGED (L4 DOOR SLIDE) · airframe 60,965 hrs · 22,537 cycles

DOOR 4L DOOR SLIDE REMOVED FOR SEAL REPAIR. SAME DOOR SLIDE RE-INSTALLED REF AMM.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 60,960 hrs · 22,535 cycles

CORROSION ON AFT PRESSURE DECK LEADING EDGE AT BS 1681 RBL 3 THRU RBL 34. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION AND CUT OUT DAMAGED AREA. FABRICATED NEW REPAIR PARTS AND INSTALLED PERMANENT REPAIR IAW SRM.

Part: FLOORBEAM — CORRODED (BS 324) · airframe 60,960 hrs · 22,535 cycles

CORROSION ON TOP OF FLOORBEAM AT STA 324 RBL 51- RBL 55. ACCOMPLISHED REPAIR OF FLOOR BEAM IAW PD57-53-093 AND EVA 80627.

Part: SMOKE DETECTOR — FAULTY (EQ COOLING) · airframe 60,960 hrs · 22,535 cycles

EQUIPMENT COOL SMOKE DETECTOR - REPLACED EQUIP COOL SMOKE DETECTOR ON TASKCARD.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 60,960 hrs · 22,535 cycles

CORROSION ON TOP OF FLOORBEAM AT STA 1640 RBL 8 - RBL 50. ACCOMPLISHED COA SMC002 ON TASKCARD 2487N00201.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 60,691 hrs · 22,428 cycles

EMERGENCY ESCAPE LIGHTING STRIP END CAP MISSING AT 6B. REPLACED EMERGENCY LIGHT STRIP BLACK END CAP. ALL EMERGENCY LIGHTS WORKED NORMAL.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 59,959 hrs · 22,158 cycles

CABIN EMERGENCY LIGHTS INOP ON O/H BIN BULL NOSE. 1AB, 2CD, 6AB, 11AB, 20DEF, 21ABC, 23DEF, LT OVERWING EXIT. PUSHED CB AND CHARGED BATTERY. OPS CHECK GOOD.

Part: WIRE — BURNED (CABIN) · airframe 59,690 hrs · 22,052 cycles

FOUND FWD CLOSET LIGHT SWITCH S10578 DAMAGED. OPENING UP FWD CLOSET FOR ACCESS TO BURNED WIRES. FOUND 5VAC WITH CB FOR CLOSET LIGHT PULLED. CHECKING BETWEEN P34 AND CLOSET CONNECTOR FOR SHORT. REPLACED SIDEWALL LIGHT AT ROW 1ABC, LIGHT OPS NORMAL. FOUND POWER WIRE AT LIGHT ASSY PULLED OUT. REPLACED WIRE AND LIGHT ASSY. REPLACED WIRE W3576-0037-2 2 IN CLOSET.

Part: UNKNOWN — ODOR (CABIN) · airframe 59,351 hrs · 21,925 cycles

ACRID OIL SMELL IN CABIN, FLT DIVERTED. FERRIED IN FOR APU CHANGE OIL SMELL IN CABIN AND PACK BURNOUTS. WILL REPLACE APU AND ACCOMPLISH LM ITEMS. REPLACED APU IAW MM.

Part: UNKNOWN — ODOR (CABIN) · airframe 59,335 hrs · 21,919 cycles

SMOKE IN CABIN, FLIGHT DIVERTED. APU PNEUMATICS HAS STRONG OIL ODOR IN FLIGHT DECK AND CABIN. FOUND APU OIL SMELL VERY NOTICEABLE WITH RT PACK ON. ISOLATED RT AND LT ENGINE BLEEDS NO OIL SMELL DETECTED IN FD OR CABIN. HIGH POWER RUN CHECKED GOOD WITH ENGINE BLEEDS. INSPECTED APU AND PACK COMPARTMENTS NO VISIBLE OIL LEAKS NOTED. REMOVED APU DUCT AT APU COMPARTMENT FOUND DRY. APU SWITCH PLAC. THIS APU HAS NO HISTORY OF OIL USAGE AND IAW THE ABOVE STATEMENT THAT APU DUCT WAS FOUND DRY PLEASE VERIFY THAT APU IS PUTTING OIL IN PACK SYS BEFORE REPLACING APU.

Part: CHILLER — FAULTY (GALLEY) · airframe 58,538 hrs · 21,610 cycles

CREW REPORTS ELECTRICAL ODOR IN CABIN AROUND ROWS 28-34. INVESTIGATE AND REPORT FINDINGS TO SAMC. CHECKED ALL CABIN, GALLEY AND LAV LIGHTS. CHECKED ALL GALLEY EQUIP AND FOUND AFT GALLEY CHILLER CAUSING ODOR. PULLED CHILLER CBS AND INOP PER MEL. INSTALLED CHILLER REF MM. BLUE LIGHT IS FLASHING AND FAULT LIGHT COMES ON AFTER 4 MIN 16 SEC. PER CHART MM LP CUTOUT FAULT. SUSPECT BAD CHILLER FROM STOCK. REPLACED AFT CHILLER. OPS CHECKS GOOD. INSPECTED WIRING TO CHILLER-NO DEFECTS NOTED-RAN CHILLER FOR 30 MINUTES-NO ODOR NOTED-POWER INDICATION LIGHT IN AFT GALLEY NEVER FLICKED ON OR OFF AS IT DID WITH PREVIOUS CHILLER.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,027 hrs · 21,406 cycles

EXTERIOR FUSE EMERGENCY EXIT LIGHTS INOP AT 1 RT MED 2 LT MED AND RT OVERWING EXIT FWD POSITIONS. REPLACED LAMPS P/N 767, OPS GOOD

Part: WATER HEATER — OVERHEATED (LAVATORY) · airframe 57,586 hrs · 21,230 cycles

FWD AFT LAV SMOKE DETECTOR WENT OFF (REPEAT). HOT IRON TYPE ODOR EMANATING FROM THAT LAV. UPDATE-CREW TURNED OFF WATER HEATER AND RAN ALL HOT WATER OUT OF HEATER. ODOR HAS NOW DISSIPATED. NO SMOKE WAS SEEN. SMOKE DETECTOR OK. WATER HEATER OVERHEATING. ITEM DEFERED.

Part: SMOKE DETECTOR — FAULTY (AFT LAVATORY) · airframe 57,572 hrs · 21,225 cycles

FWD AFT LAV SMOKE DET ALARMING AND WILL NOT RESET. REPLACED FWD AFT LAV SMOKE DETECTOR, OPS CHECKS OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,543 hrs · 21,211 cycles

EXIT LIGHT AT DOOR 1R BY THE LINEN DISPOSAL COMP. IS IN-OP. REPLACED EXIT LIGHT, OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,543 hrs · 21,211 cycles

EXIT LIGHT AT DOOR 1R BY THE LINEN DISPOSAL COMP IS INOP. REPLACED EXIT LIGHT, OPS CHECKS GOOD.

Part: SMOKE GOGGLES — DAMAGED (COCKPIT) · airframe 57,055 hrs · 21,017 cycles

ALL FLIGHT DECK SMOKE GOGGLES HAVE SCRATCHED LENS. REPLACED SMOKE GOGGLES, 3EA.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 57,055 hrs · 21,017 cycles

CAPTAIN'S O2 MASK LEAKS. REPLACED CAPTAIN'S O2 MASK. OP TEST OKAY.

Part: WIRE — DAMAGED (RT WING) · airframe 55,592 hrs · 20,449 cycles

RIGHT WING L/E, OUTBOARD OF NR 2 ENG PYLON WIRE DAMAGED. REPLACED WIRE W4026-4501 PER BSPMS 20-10-13, 20-35-19, 20-10-15, AND CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,592 hrs · 20,449 cycles

RIGHT AFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK AT M10568 AND OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 55,215 hrs · 20,301 cycles

NR 2 RT MED EXTERIOR EMERGENCY EXIT PATH LIGHT INOP. REPLACED LAMP, OPS GOOD. P/N BULB 767.

Part: OXYGEN MASK — DEFECTIVE (COCKPIT) · airframe 54,285 hrs · 19,934 cycles

PILOTS O2 MASK HAS DEFECTIVE AIRFLOW. REPLACED MASK & OP CHECKS OK.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 54,025 hrs · 19,841 cycles

CAPT O2 MASK HAS CONSTANT FLOW WHEN IN USE. FOUND MASK LEAKING. REPLACED CAPT OXYGEN MASK. LEAK & OPS TEST OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,870 hrs · 19,426 cycles

DOOR 4 LEFT OUTSIDE EMERGENCY LIGHT INOP. *S/D* LAMP INOP. RELAMPED LIGHT BULB AND OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,378 hrs · 19,237 cycles

EXT EMERGENCY EXIT LIGHT INOP DOOR 2R, RELAMPED.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 51,934 hrs · 19,071 cycles

TRAILING EDGE FLAP DISAGREE BETWEEN 25 AND 30. PERFORMED SEVERAL FLAP DEPLOYMENTS, NO DISAGREE NOTED AT ANY SETTING OR BETWEEN SETTINGS, UNABLE TO DUPLICATE ON GROUND, NO HISTORY OR REPEATS SINCE ORIGINAL WRITE UP.

Part: LIGHT — LOOSE (FIRE BOTTLE) · airframe 51,782 hrs · 19,016 cycles

NR 2 CARGO FIRE BOTTLE DISCHARGE LIGHT INOP. INDICATOR LIGHT LOOSE. SECURED LIGHT ASSY, GROUND CHECKS OK.

Part: ACTUATOR — FAULTY (RUDDER TRIM) · airframe 51,778 hrs · 19,015 cycles

RUDDER TRIM FAILED TO TRIM IN EITHER DIRECTION. CREW COMMENTS: RUDDER TRIM INTERMITTENT. RUDDER TRIM ACTUATOR FAILURE, TRANSMITTER ISSUE. REPLACED RUDDER TRIM ACTUATOR, OPS CHECKED GOOD.

Part: O-RING — LEAKING (SLIDE BOTTLE)

LOW BOTTLE. FOUND LEAK AT THE CENTER O-RING OF THE TANK. REPLACED O-RING ON CENTER SHAFT.

Part: SLIDE — LOW PRESSURE (L4 DOOR) · airframe 51,286 hrs · 18,837 cycles

DOOR 4L SLIDE PRESSURE IS ON LOW END OF GREEN BAND. REPLACED SLIDE ASSY.

Part: STRAP — BROKEN (GIRT BAR) · airframe 50,365 hrs · 18,516 cycles

NR 1 LEFT MED SLIDE GIRT BAR STRAP BROKEN RIVETS. 10-9-07 REPLACED LT MAIN ENTRY DOOR SLIDE.

Part: LANDING GEAR — MALFUNCTIONED · airframe 50,223 hrs · 18,463 cycles

GEAR DOWN AND LANDING GEAR ALTN EXTEND C/B (F5) ON P6 PANEL TRIPPED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,959 hrs · 18,375 cycles

INTERIOR OVERWING EEL LIGHTS INOPERATIVE, ONE ON EACH SIDE OF A-C. REPLACED EEL PWR SUPPLY. OP CK GOOD.

Part: UNKNOWN — UNKNOWN (FUEL TANK) · airframe 49,382 hrs · 18,164 cycles

DURING FLIGHT CENTER FUEL TANK QTY ROSE FROM 0 TO 1300 AND RIGHT WING DOWN 2K LESS THAN LEFT WING. [06-20-07] AT DISPATCH TIME, FUELER COULD NOT OPEN RIGHT WING FILL VALVE FOUND RT WING FUEL FILL VALVE STUCK IN THE OPEN POSITION. REPLACED VALVE AND OPS CHECKED NORMAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,761 hrs · 13,899 cycles

TWO DENTS LT FUSELAGE AT STA 606, STR 15L AND 16L. REMOVED 4 EA EXISTING REPAIRS AND INSTALLED DOUBLER REPAIR PER EVA IMC-30171.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,760 hrs · 14,607 cycles

FRAME AT STA 1420 IS DENTED BETWEEN STR 25-26L. MAJOR REPAIR ACCOMPLISHED. FRAME REPAIR DOUBLER INSTALLED.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,760 hrs · 14,607 cycles

FRAME AT STA 1500 DENTED ABOVE STR 25L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,760 hrs · 14,607 cycles

FRAME AT STATION 1400 DENTED ABOVE STR 25L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: WEB — CRACKED (FUSELAGE) · airframe 39,760 hrs · 14,607 cycles

FLIGHT DECK FLOOR WEB CRACKED ON VERTICAL LEG AT FIRST FASTENER AFT OF STA 199 BULKHEAD ON RT SIDE OF AIRCRAFT. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW WEB.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,760 hrs · 14,607 cycles

AFT CABIN FLOORBEAM AT BS 1640 IS CORRODED RBL 18 THRU 58. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW T-CAP AND REPAIR STRAPS.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 39,760 hrs · 14,607 cycles

AFT CABIN SHEAR WEB HAS AREA OF CORROSION AT APPROX BS 1681 THRU 1699 RBL 44 THRU 54. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW WEB.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,760 hrs · 14,607 cycles

AFT CABIN FLOORBEAM AT STA 1661, RBL 54 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,760 hrs · 14,607 cycles

MAIN CABIN AT STA 365, RBL 45 TO RBL 60, FLOORBEAM HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,760 hrs · 14,607 cycles

CABIN STATION 365, CL TO RBL 15 FLOOR SUPPORT HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP AND L-ANGLE REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,760 hrs · 14,607 cycles

EXTERNAL FUSELAGE SKIN HAS 2 LIGHTNING STRIKES JUST BELOW FWD CARGO DOOR STA 582 AND 529 AT STR 27R, DEPTH WAS MEASURED TO BE .100. INSTALLED DOUBLER REPAIR.

Part: APU — MALFUNCTIONED · airframe 39,270 hrs · 14,427 cycles

APU ON AT GATE FOR 3 MIN. PUT BOTH PACKS ON NOTICED BLUE-OIL SMOKE IN COCKPIT & CABIN. REPLACED APU. STAT-O-SEALS FAILED IN THE DRIVEN COMPRESSOR MODULE. RUBBER WAS EXTRUDED AND TORN FROM BOLT HEAD AND SHAFT. NO LOOSE BOLTS NOTED. SEALING FUNCTION COMPROMISED ON BACKSHROUD INNER DIAMETER BOLT CIRCLE.

Part: WEB — CORRODED (THRESHOLD) · airframe 37,761 hrs · 13,899 cycles

AFT PIT CARGO DOOR CUTOUT THRESHOLD SILL WEB CORRODED UNDER THRESHOLD PLATE. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED WEB REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,761 hrs · 13,899 cycles

TWO DENTS LT FUSELAGE AT STA 606, STR 15L AND 16L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: WEB — CORRODED (THRESHOLD) · airframe 37,761 hrs · 13,899 cycles

AFT PIT CARGO DOOR CUTOUT THRESHOLD SILL WEB CORRODED UNDER THRESHOLD PLATE. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED WEB REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,419 hrs · 12,270 cycles

DENT ON FRAME-SKIN SPLICE AT STA 1620 FWD OF NR 3L ENTRY DOOR AT FLOOR LEVEL. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR ACCOMPLISHED.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 29,939 hrs · 11,017 cycles

FUSELAGE SKIN AND STRINGER DAMAGED STA 780, STR 16 LT. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER SPLICE AND DOUBLER.

Part: IDG — FAILED (NR 2)

CREW DIVERTED TO DEN DUE TO LOSS OF NUMBER 2 GENERATOR. *S/D* THE IDG STATOR ASSEMBLY HAD SHIFTED WHICH CAUSED A CRACK IN A CONTROL CURRENT TRANSFORMER CONNECTION INTERNAL TO THE GENERATOR. REPLACED NUMBER 2 INTEGRATED DRIVE GENERATOR.

Part: TUBE — FAILED (SLIDE)

DURING THE SHOP OVERHAUL OF AN EVACUATION SLIDE REMOVED FOR TIME EXPIRATION IT FAILED THE PROOF TEST. THERE WAS A SEAM SEPARATION OF OVER 8 FEET ON THE LEFT TOP TUBE STARTING AT THE UPPER INTERNAL BULKHEAD AND GOING DOWN TOWARD THE SLIDE FOOT IN THE CROUCH AREA. SLIDE SENT TO VENDOR FOR INVESTIGATION AND REPAIR.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY EXIT GREEN LIGHTS INOP AT LEFT AND RIGHT REAR SERVICE DOORS. WHITE EMERGENCY EXIT LIGHT INOP AT LEFT REAR SERVICE DOOR. REPLACED BATTERY, CHECKS OK.