N579UA

Part: INVERTER — INOPERATIVE (CABIN) · airframe 67,488 hrs · 23,938 cycles

LAST 8FT OF EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED INVERTER M10831 IAW WDM 33-51-22.

Part: SEAT — UNSECURE (CABIN) · airframe 67,398 hrs · 23,909 cycles

39D SEAT LOOSE FROM FLOOR. SECURED ROW 39DEF IN TRACKS IAW MM 25-25-05.

Part: DOOR — OUT OF SEQUENCE (L2) · airframe 67,341 hrs · 23,895 cycles

CANNOT CLOSE L2 DOOR FROM OUTSIDE, DOOR L2 OUT OF SEQUENCE. REOPENED DOOR FULLY & CLOSED DOOR. OPERATIONS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (TEMP CONTROL) · airframe 67,174 hrs · 23,844 cycles

HISTORY OF FLIGHT DECK TEMPS UNCONTROLLABLE. IAW SVC TIP MM 21-61-100E & PERFORM ALL STEPS OF FIM 21-60-00 FIG.106. CHECKED & INSPECTED FLIGHT DECK ZONE TEMP SENSOR FAN.

Part: FITTING — MISSING (LAVATORY) · airframe 67,088 hrs · 23,809 cycles

LAVATORY RT DRAIN FITTING MISSING REQUIRED GASKET & SEVERAL ATTACH BOLTS ARE BROKEN WITH REMAINING PIECES STILL IN LAVATORY FLOOR. THIS CONDITION WAS PRESENT AT LAVATORY INSTALLATION & ATTACH SCREWS WERE MODIFIED, SHORTENED, TO ALLOW INSTALLATION. IAW IPC 38-31-51-052D DETAIL E, RESTORED SCREW HOLES TO NORMAL, INSTALLED GASKET & JUNCTION PLATE.

Part: FEEDER CABLE — CUT (CABIN) · airframe 66,896 hrs · 23,742 cycles

EMERGENCY EXIT LIGHT STRIP ON FLOOR IN FRONT OF FIRST CLASS CLOSET IS INOPERATIVE WHEN TESTED. REPAIRED CUT EMERGENCY EXIT LIGHT FEEDER AT ROW 1L.

Part: WIRE — MISWIRED (CABIN) · airframe 66,896 hrs · 23,742 cycles

EMERGENCY LIGHT OVER DOOR 1R, INOPERATIVE, WHEN TESTED. EMERGENCY LIGHT ITEM NUMBER IS L27. SWAPPED RT EMERGENCY EXIT DR 1 ASSEMBLY WITH LT. REPLACED POWER SUPPLY M730 THEN BLEW A FUSE. FOUND WIRE PIN 13 SHORTING OUT ON CONNECTOR D66. SEE WDM 33-51-12 PG 5 & SCHEMATIC MANUAL 33-51-01 PG 105 SH2. FOUND WIRES SWAPPED AT CLASS DIVIDER EXIT SIGN L763. CORRECTED WIRES IAW WDM 33-51-12 LIGHTS CHECKED GOOD.

Part: SENSOR — FAULTY (COCKPIT TEMP) · airframe 66,845 hrs · 23,723 cycles

STILL UNABLE TO CONTROL FLIGHT DECK TEMPERATURE IN AUTO. STANDBY MODE NORMAL, WORKS OKAY. DEFER REF MEL 2151G REPLACED FLIGHT DECK ZONE TEMPERATURE SENSOR IAW. OPERATIONS CHECKED NORMAL.

Part: ACTUATOR — LEAKING (MLG DOOR) · airframe 66,668 hrs · 23,661 cycles

FLUID LEAKING FROM LT WHEEL WELL. REPLACED LEFT MAIN GEAR DOOR ACTUATOR IAW MM.

Part: VALVE — INOPERATIVE (CABIN TEMP) · airframe 66,668 hrs · 23,661 cycles

DURING CLIMB PASSING 18000 FT, COCKPIT AND FWD CABIN WENT VERY HOT. CONTINUE HOT UNTIL TRIM AIR OFF. AT CRUISE, WENT BACK TO AUTO AND TEMPS OK. DEACTIVATED TRIM AIR VALVE.

Part: TRACK — DIRTY (COCKPIT WINDOW) · airframe 66,333 hrs · 23,554 cycles

F/O WINDOW WILL NOT OPEN FULLY. CLEANED LOWER TRACK, LUBED ROLLERS, SNUBBER CLEVIS POINTS AND JACK SCREW. OPERATED SEVERAL CYCLES, OPS CHECKED GOOD.

Part: MICROPHONE — INOPERATIVE (COCKPIT) · airframe 66,331 hrs · 23,553 cycles

NR 3 BOOM MICROPHONE IS DEFECTIVE. MICOPHONE WILL NOT TRANSMIT. REPLACED BOOM MIC.

Part: REVEAL — MISSING (SEAT ROW 20ABC) · airframe 66,187 hrs · 23,511 cycles

WINDOW REVEAL AT SEAT ROW 20ABC MISSING. REPLACED WINDOW REVEAL AT PAX SEAT 20A.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,111 hrs · 23,484 cycles

EMERGENCY ESCAPE FLOOR MARKER DIM AT ROW 38-39. REPLACED CHARGERS, OPS CHECKED NORMAL.

Part: LIGHT — DIM (CABIN) · airframe 66,111 hrs · 23,484 cycles

EMERGENCY ESCAPE FLOOR MARKER DIM INOP AT ROW 38-39

Part: SENSOR — FAULTY (R1 DOOR SLIDE) · airframe 65,911 hrs · 23,410 cycles

R1 DOOR SLIDE LIGHT IS ILLUMINATED. REPLACED SENSOR S10216. ARMED AND DISARMED DOOR, SLIDE LIGHT, CHECKED NORMAL.

Part: SOCKET — DIRTY (EMERGENCY LIGHT) · airframe 65,752 hrs · 23,361 cycles

FOUND R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. CLEANED LIGHT BULB SOCKET, OPERATIONS CHECKED NORMAL.

Part: LINER — OUT OF POSITION (L1 DOOR) · airframe 65,574 hrs · 23,309 cycles

L1 DOOR ARM WEDGE DOES NOT AUTOMATICALLY SPRING OUT AND/OR GETS STUCK WHEN ARMING DOOR. LOOSENED UPPER DOOR LINING, MOVES FREELY.

Part: STRUCTURE — TORN (NR 5 SLAT) · airframe 65,517 hrs · 23,293 cycles

ON ARRIVAL AT GATE, FOUND LEFT INBOARD SLAT TRAILING EDGE RIPPED OPEN AND DELAMINATED. REPLACED NR 5 SLAT PER AMM.

Part: HINGE — LACK OF LUBE (L2 DOOR) · airframe 65,509 hrs · 23,290 cycles

L2 DOOR DOOR HINGE IS NOT CLOSING. LUBED HINGE, OPS NORMAL.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR) · airframe 65,509 hrs · 23,290 cycles

L1 DOOR UNABLE TO DISARM AND COULD NOT REMOVE BUSSEL. L1 SLIDE ARMED AND NOT PINNED. ACCOMPLISHED REMOVAL OF DOOR 1L SLIDE BUSSEL. REMOVED L1 DOOR SLIDE COVER. LUBRICATED PIN. OPERATED SMOOTHLY. CHECKED AND ADJUSTED DOOR, OPS CHECKED NORMAL. FEELS LIKE GIRT BAR HITTING THE FLOOR FITTING. CLEANED DEBRIS FROM FLOOR FITTINGS. CYCLED ARMING LEVER. OPS CHECKED GOOD.

Part: PROXIMITY SENSOR — SHORTED (R4 DOOR) · airframe 65,507 hrs · 23,289 cycles

DOOR SLIDE ARMED LIGHT WILL NOT COME ON. TROUBLESHOT AND FOUND WIRE 3682 GROUNDED AND FOUND FWD AND AFT R4 DOOR PROXIMITY SENSORS SHORTED. REMOVED & REPLACED R4 DOOR PROXIMITY SENSORS, OPS CHECKED GOOD IAW AMM 25-66-11 AND WDM 25-66-11.

Part: SKIN — DENTED (BS 418) · airframe 65,507 hrs · 23,289 cycles

FUSELAGE SKIN DENTED BS 418 S17 TO 19R. REPAIRED SKIN IAW SRM 53-00-01. PERFORMED HFEC OF CUTOUT IAW NTM PART 6 51-00-19 NO DEFECT NOTED. MAJOR REPAIR.

Part: LOCK — MISSING (R4 DOOR) · airframe 65,507 hrs · 23,289 cycles

R4 DOOR SLIDING BAR LOCK ASSY MISSING. INSTALLED BAR LOCK ASSY. OPS CHECKED GOOD IAW AMM 25-66-10.

Part: SKIN — DENTED (BS 400 S16L) · airframe 65,507 hrs · 23,289 cycles

FA SEVEN INCH DENT AFT OF L1 DOOR S16L AND BS 400. REPAIRED DENT IAW ECRA 536 1-01053.

Part: SKIN — DENTED (NR 1 NACELLE) · airframe 65,507 hrs · 23,289 cycles

DENT IN NR 1 ENG FWD INLET COWL AT 4 O'CLOCK POSITION. DENT FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM 54-11-01 FIG 101 DETAIL IV. REMOVED DAMAGE & REPAIRED IAW SRM 54-11-01 FIG 201.

Part: PAINT — DAMAGED (FLOORBEAM) · airframe 65,507 hrs · 23,289 cycles

PAINT ABRASION UPPER SURFACE AFT MAIN CABIN FLOORBEAM BS 1600. REPAIRED FLOORBEAM IAW ECRA 5310-05538.

Part: TIRE — DAMAGED (NR 1 MLG) · airframe 65,298 hrs · 23,214 cycles

NR 1 MLG TIRE HAS A SPLIT NUT ON THE WHEEL ASSY. REPLACED NR 1 FWD TIRE & WHEEL ASSY PER AMM.

Part: SMOKE DETECTOR — FALSE ACTIVATION (FWD LAVATORY) · airframe 64,947 hrs · 23,098 cycles

FLIGHT ATTENDANT REPORTS AFT FWD LAVATORY SMOKE DETECTOR ALARMING. REPLACED SMOKE DETECTOR PER AMM. CHECKED GOOD. NO SIGN OF SMOKE OR FIRE FROM LAVATORY AND TRASH CONTAINER. DETECTOR SENSOR FAILURE.

Part: LENS — DEFECTIVE (FIRE BOTTLE) · airframe 64,415 hrs · 22,932 cycles

WHEEL WELL FIRE LIGHT NOT TESTING. LOG SHOULD SAY APU BOTTLE DISCHARGE LIGHT. REPLACED APU BOTTLE DISCHARGE LENSE TESTED OKAY.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 64,162 hrs · 22,837 cycles

DOOR 1L SLIDE ARMED LIGHT WENT OUT DURING TAXI OUT. RELAMPED LIGHT ASSY. DOOR SLIDE OPERATION NORMAL.

Part: MECHANISM — WORN (R1 DOOR) · airframe 63,152 hrs · 22,482 cycles

MAIN ENTRY DOOR 1 RIGHT TRIGGER MECH WORN. REPLACED TRIGGER MECH.

Part: MODULE — FAULTY (LEFT) · airframe 62,955 hrs · 22,414 cycles

ELEVATOR FEEL STATUS MESS ON TAKEOFF ROLL. DUE REPEAT, RECOMMEND TO ACP SVC TIP MM. PITOT LEAK CHECK AND POSSIBLY WILL NEED ELEVATOR FEEL COMP REPLACED.

Part: PUMP — FAILED (RT HYD SYSTEM) · airframe 62,792 hrs · 22,358 cycles

RT ENG HYD PUMP OVERHEAT LIGHT ILLUMINATED ON TAKEOFF. CREW SELECTED ENG PUMP SWITCH TO OFF AND LIGHT WENT OUT. FLIGHT DIVERTED. REPLACED RT ENG HYD PUMP ASSY PER AMM. ALSO REPLACED RH SYS CASE DRAIN AND PRESS FILTERS PER AMM. NO LEAKS NOTED.

Part: HYDRAULIC LINE — LEAKING (THRUST REVERSER) · airframe 62,601 hrs · 22,297 cycles

FLUID DRIPPING FROM NR 1 ENGINE. FOUND THRUST REVERSER RETURN LINE ITEM 565, IPC 29-11-51 LEAKING ON NR 1 ENGINE PYLON. REPLACED LINE, OPS CHECKS NORMAL.

Part: LANYARD — UNSECURE (L2 DOOR SLIDE) · airframe 62,426 hrs · 22,230 cycles

L2 DOOR WILL NOT ARM. SECURED SLIDE BUSSEL. DOOR ARMING OPERATION NORMAL.

Part: BRACKET — DEBONDED (CABIN) · airframe 62,117 hrs · 22,119 cycles

FOUND BRACKET DISBONDED FROM INSIDE OF CENTER AIR DUCT AT ROW 11 WHERE DUCT ASSY IS SAGGING. REMOVED NOZZLE ASSY AND REPLACED BRACKETS. NOZZLE ASSY NEEDS TO BE RE-INSTALLED AFTER REPAIR REF MM PER ORDLE. ACCOMPLISHED REPAIR OF LOWER SURFACE, WAS ABLE TO REMOVE SOME OF THE SAGGING. REINSTALLED NOZZLE AND BRACKETS.

Part: HANDLE — DETACHED (SLIDING WINDOW) · airframe 61,941 hrs · 22,049 cycles

F/O'S SLIDING WINDOW HANDLE FELL OFF. REPLACE WITH CONFIGURATION HARDWARE TO SECURED HANDLE. OP'S NORMAL.

Part: LANYARD — UNSECURE (R4 DOOR) · airframe 61,240 hrs · 21,783 cycles

DOOR 4R WILL NOT ARM. SECURED LANYARD AT BOTTOM OF DOOR 4R. ARMING GOOD.

Part: RING — OUT OF POSITION (GIRT BAR) · airframe 60,932 hrs · 21,663 cycles

UNABLE TO ARM DOOR. FOUND D-RING NOT STOWED, STOWED D-RING. CYCLED DOOR AND ARMS NORMALLY.

Part: PLACARD — IMPROPER PART (CABIN) · airframe 60,799 hrs · 21,615 cycles

ALL COACH SEATS AND BULKHEAD SEATS IN FIRST CLASS HAVE THE WRONG SEAT BELT AND LIFE VEST PLACARDS. REPLACED ALL BUT ROW 40 ON THE LEFT SIDE AND ROW 32 THROUGH 40 ON THE LEFT. INSTALLED REMAINING PLACARDS FROM ROW 32 TO 40.

Part: PLACARD — IMPROPER PART (CABIN) · airframe 60,807 hrs · 21,619 cycles

ALL COACH SEATS AND BULKHEAD SEATS IN FIRST CLASS HAVE THE WRONG SEAT BELT AND LIFE VEST PLACARDS. REPLACED ALL BUT ROW 40 ON THE LEFT SIDE AND ROW 32 THROUGH 40 ON THE LEFT. CREATED INTERIM REPAIR REF GNMM ON REMAINING ROWS, PLACARD PCN 781-1202 IS NEEDED. AFTER FURTHER ANALYSIS, IT HAS BEEN DETERMINED THIS IS NOT AN SDR REPORTABLE EVENT.

Part: FRAME — CORRODED (BS 1460 S28-29L) · airframe 60,610 hrs · 21,539 cycles

CORROSION ON FRAME AT BS 1460 INBD OF STR 28R & BETWEEN STR 29R - 28L. ACCOMPLISHED PERMANENT REPAIR PER EA PD57-53-166 AND EVA 81175.

Part: SILL — CORRODED (BS 1380-1440) · airframe 60,610 hrs · 21,539 cycles

AFT CARGO CORROSION, CARGO DOOR SILL AREA FROM STA 1380 TO STA 1440 SEVERAL AREAS. ACCOMPLISH PERMANENT RPR PER EA PD57-53-167 AND EVA 81174.

Part: FRAME — CORRODED (BS 1680 S29L/R) · airframe 60,610 hrs · 21,539 cycles

CORROSION ON FRAME AT STA 1680 29L - 29R. MAJOR REPAIR ACCOMPLISHED: REPAIRED FRAME AT STA 1680 STR 29L - 29R PER EA PD57-53-159 AND EVA 81158.

Part: FRAME — CORRODED (BS 1620 S29-30R) · airframe 60,610 hrs · 21,539 cycles

CORROSION ON FRAME AT BS 1620 BETWEEN STR 29R-30. REPAIRED PER EAPP 57-53-160.

Part: FLOORBEAM — GOUGED (BS 1640) · airframe 60,610 hrs · 21,539 cycles

FLOORBEAM AT BS 1640 RT OUTBOARD HAS A GOUGE ON TOP. REPAIRED PER EA PD 57-53-153.

Part: LEAD — DAMAGED (EMERGENCY LIGHTS) · airframe 60,610 hrs · 21,539 cycles

EMERGENCY LIGHTS INOPERATIVE UPON ARRIVAL BETWEEN ROWS 24 AND 27. REPLACED LEAD IN CABLE IAW AMM, OPS CHECKED GOOD.

Part: FLOORBEAM — CORRODED (BS 1660) · airframe 60,610 hrs · 21,539 cycles

FLOORBEAM AT BS 1660 CORRODED APPROX 12 INCHES LEFT & RIGHT OF BL 0 ON TOP SURFACE. ACCOMPLISHED ON TASK CARD 2808N00106.

Part: FLOORBEAM — CORRODED (BS 324) · airframe 60,610 hrs · 21,539 cycles

CORROSION ON FLOORBEAM AT STA 324, RBL 40 - 60. CUT OUT DAMAGE . ACCOMPLISHED NDT OF CUT & FASTENER HOLES COMMON TO REPAIR PER NDT MANUAL. FABRICATED & INSTALLED SPLICE ANGLES, STRAPS & FLOORBEAM REF EA PD57-53-152 & UA EVA-81030. MAJOR REPAIR

Part: PAN — GOUGED (L2 DOOR) · airframe 60,610 hrs · 21,539 cycles

DOOR 2L HAS GOUGE IN HANDLE PAN. REMOVED AND REPLACED HANDLE PAN IAW SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,610 hrs · 21,539 cycles

FUSELAGE HAS LIGHTNING STRIKE DAMAGE. ACCOMPLISHED PERMANENT REPAIR IAW SRM 53-00-01 RPR 6.

Part: SKIN — DAMAGED (BS 1080 S8R) · airframe 60,610 hrs · 21,539 cycles

FUSELAGE STA 1080 STR 8R SKIN HAS LIGHTNING DAMAGE. MAJOR REPAIR. REPAIRED PER SRM. REPAIRED IAW PWI E-88 T1437.

Part: FLOORBEAM — CORRODED (BS 365) · airframe 60,610 hrs · 21,539 cycles

CORROSION ON FLOOR BEAM AT STATION 365 RBL 60. MAJOR REPAIR. AFTER BLENDING CORROSION FOUND FLOORBEAM TO BE OUT OF LIMITS PER SRM. REMOVED DAMAGE IAW SRM, FABRICATED REPAIR PART ANGLES. FABRICATED STRAP & BEAM. INSTALLED ALL PARTS IAW SRM 53-00-51.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,610 hrs · 21,539 cycles

FLOORBEAM AT STA 1660 HAS CORROSION APPROXIMATELY 12 INCHES LEFT AND RIGHT OF BL ON TOP SIDE. MAJOR REPAIR ACCOMPLISHED: RMV'D PREVIOUS REPAIR, FABBED AND INSTALLED T-CHORD, ANGLES AND STRAPS STA 1660, LBL 10 - RBL 02 PER SRM ON PEMCO NR 2808N00106.

Part: OXYGEN BOTTLE — MISSING (CABIN) · airframe 60,519 hrs · 21,507 cycles

OXYGEN BOTTLE MISSING - USED AT AFT CABIN. REPLACED O2 BOTTLE.

Part: COLLAR — LACK OF LUBE (NLG STEERING) · airframe 60,487 hrs · 21,498 cycles

NOSE GEAR STEERING USING FOOT PEDDLES PRODUCES APPROX 1 DEGREE LEFT WITH FULL LEFT INPUT AND APPROXIMATELY 8 DEGREES RT WITH FULL INPUT. INSPECTED NLG, NO DEFECTS NOTED. FOUND STEERING COLLAR WITH INSUFFICIENT LUBRICATION. ACCOMPLISHED GEAR LUBE AND RIG CHECK PER MM. STEERING OPERATION NORMAL. ACCOMPLISHED ACFT TAXI AND VERIFIED NORMAL STEERING RESPONSE.

Part: LIGHT — INOPERATIVE (L1 DOOR SLIDE) · airframe 59,374 hrs · 21,100 cycles

SLIDE LIGHT DOOR 1L DID NOT ILLUMINATE. OTHER INDICATIONS NORMAL. REINSTALLED SLIDE RAFT LANYARD. CHECKED NORMAL AT THE GATE.

Part: TRANSMITTER — FAULTY (HYD RESERVIOR) · airframe 58,861 hrs · 20,914 cycles

LOST LT HYD SYS QTY, FLIGHT DIVERTED. RAN BOTH ENGINES, OPERATED THRUST REVERSER, CYCLED ALL FLIGHT CONTROLS. OPENED GEAR DOORS, PINNED GEARS AND CYCLED LANDING GEAR HANDLE. NO ACTIVE LEAKS NOTED. AT INITIAL SERVICE NOTED ERRATIC QTY INDICATIONS. DRAINED RESERVIOR AND RESERVICED. SUSPECT RESERVIOR QTY TRANSMITTER. REPLACED TRANSMITTER.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 57,860 hrs · 20,542 cycles

ACFT HAS EXPERIENCED LIGHTNING STRIKE. ACCOMPLISHED CK. FOUND 68 STRIKES TO FUSE SKIN & FAIRINGS. STRIKES ARE ON FASTENER HEADS; NO TWO ADJACENT FASTENERS AFFECTED. FAIRING DAMAGE IS SPEED TAPED. NO HOLES OR BURN THROUGHS. ACCOMPLISH FULL LIGHTNING STRIKE CHECK IAW MM. INSTALLED DOUBLER REPAIR BS 1080 S8R IAW SRM. INSTALLED 13 BLIND RIVETS. REMAINING AREAS INSPECTED AND REPAIRED IAW SRM.

Part: GCU — FAULTY (LEFT) · airframe 57,849 hrs · 20,540 cycles

LEFT GENERATOR DRIVE ILLUMINATED, RTFL CREW ACCOMPLISHED DISCONNECT OF LT GEN. FOUND LT IDG OIL QTY LOW. RECONNECTED & SERVICED PER MM. LEFT IDG REQUIRED 5 PINTS OF OIL AT SERVICE. REPLACED LT GCU PRECAUTIONARY. ACP HIGH POWER RUN ALL INDICATIONS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,836 hrs · 19,816 cycles

EMERGENCY FLOOR LIGHT AT AFT LAV IS IN-OP. REPLACED EMERGENCY LIGHT SECTION AT AFT LAV. PCN 560-3325. OPS CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,414 hrs · 19,659 cycles

EXT EMERGENCY LIGHT AT D00R 2R INOPERATIVE. RELAMPED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,414 hrs · 19,659 cycles

EXT EMERGENCY LIGHT AT DOOR 3R INOPERATIVE. RELAMPED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,414 hrs · 19,659 cycles

EXT EMERGENCY LIGHT AT DR 1R INOPERATIVE. RELAMPED.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 55,067 hrs · 19,513 cycles

SCRIBE INSPECTION IDENTIFIED 1 SCRIBE OUT OF LIMITS AT STA 780, 56 INCHES LONG BETWEEN STR 4R AND 10R, .0077. DEEP. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIRS ARE COMPLETED.

Part: CYLINDER — CORRODED (RT MLG) · airframe 54,712 hrs · 19,373 cycles

RIGHT MLG OUTER CYL HAS CORROSION AT GLAND NUT. REMOVED OUTER CYLINDER AND ROUTED TO SHOP. SHOP 134 ACCOMPLISHED REPAIR.

Part: CYLINDER — CORRODED (RT MLG) · airframe 54,712 hrs · 19,373 cycles

RIGHT MLG INNER CYL HAS CORROSION ON INSIDE NEAR TOP OF CYL ON FWD SIDE. REMOVED INNER CYLINDER AND ROUTED TO SHOP. SHOP 134 PERFORMED REPAIR.

Part: SKIN — BULGED (FUSELAGE) · airframe 54,685 hrs · 19,364 cycles

EXT FUSE SKIN IS BULGED JUST FWD OF BUTT SPLICE AT FRAME STA 1640 BETWEEN STR 28R AND 29R (REF OV WU D9344 X). DENT HFEC BEFORE ANY REWORK. NO CRACKS FOUND. DENT STRAIGHTENED. HFEC INSPECTED. NO CRACK INDICATION NOTED. AREA PAINTED.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 54,685 hrs · 19,364 cycles

FLOOR SOFT AT ROWS 9-10. REMOVED AND REPLACED FLOORBOARD AT ROWS 9-10 ON WU K6774D BY AMT'S.

Part: SKIN — DENTED (FUSELAGE) · airframe 54,685 hrs · 19,364 cycles

DENT LOCATED NEAR DOOR 2L BELOW AND TO THE LEFT OF THE 2L MAIN ENTRY DOOR. POSSIBLE CONTACT FROM JETWAY. DENT LOCATED ON DOUBLER FWD OF DOOR. FWD OF WING ILLUMINATION LIGHT. DOUBLER SKIN DENT DEPTH IS 0.040 AND AREA IS 2 IN. COLD WORKED SKIN ON STRINGER AREA DENT. CHECKED & RECORDED SIZED & DEPTH IS 0.020 AND AREA IS 1.625. NDT NO CRACKS ON WU K6773D BY AMT'S DOUBLER SKIN DENT AND STRINGER DENT ARE WITHIN LIMITS RESPECTIVELY.

Part: SLIDE — MISINSTALLED (RT OVERWING) · airframe 54,685 hrs · 19,364 cycles

RIGHT OVERWING SLIDE PACK NOT INSTALLED CORRECTLY INSIDE PACK COMPARTMENT, NOT INSTALLED INSIDE AFT SUPPORT BRACKETS. ACCMP ON WU K6818D.

Part: GUARD — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,047 hrs · 19,130 cycles

EMERGENCY LIGHTS SWITCH GUARD INOPERATIVE. REPAIRED GUARD.

Part: LIGHT — INOPERATIVE (LAVATORY) · airframe 53,733 hrs · 19,010 cycles

K-LAV EEL LIGHT BAR IS INOP. REPLACED K-LAV LIGHT BAR, OPS CHECKS GOOD.

Part: FITTING — MISSING (R2 DOOR) · airframe 52,377 hrs · 18,480 cycles

MED 2 RT EMER TRIGGER MECH. MISSING ADJUSTMENT SAFETY CLIP. REPLACED SAFETY CLIP.

Part: MECHANISM — WORN (R1 DOOR) · airframe 52,377 hrs · 18,480 cycles

MED 1 RT EMER. TRIGGER MECH. WORN. REPLACED EMERGENCY TRIGGER.

Part: SEAT — UNSECURE (ROW 13) · airframe 51,542 hrs · 18,145 cycles

F/A REPORTS ROW 13 SEATS D, E, F ARE NOT SECURE TO FLOOR. SECURED SEAT TO TRACK. NO RECENT MTX ACTIVITY IN THIS AREA FOR THIS A/C.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,461 hrs · 18,116 cycles

EXTERIOR EMERGENCY LIGHTS FOR DOORS 2LT & 4LT ARE INOP. RE-LAMPED DOORS 2L AND 4L, OPS CHECKED NORMAL.

Part: GIRT BAR — OBSTRUCTED (L2 DOOR) · airframe 51,048 hrs · 17,969 cycles

DOOR 2L WON`T ARM AND DISARM PROPERLY. FOUND STATIC LINE TANGLED IN GIRT BAR. FREED LINE AND STOWED, OPS NORMAL.

Part: STRAP — OUT OF POSITION (EVAC SLIDE) · airframe 50,413 hrs · 17,752 cycles

STRAP HANGING OUT OF SLIDE PACK AT 2L. SECURED D-RING STRAP.

Part: GIRT BAR — UNRELIABLE (L2 DOOR) · airframe 49,025 hrs · 17,266 cycles

DOOR 2L WILL NOT ARM.

Part: LIGHT — LOOSE (CABIN) · airframe 48,863 hrs · 17,208 cycles

EMERGENCY LIGHT STRIP LOOSE AT 12C.

Part: WARNING SYSTEM — ACTIVATED (RT ENGINE) · airframe 48,686 hrs · 17,148 cycles

EICAS MESSAGE - R ENGINE FIRE LOOP 2.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,350 hrs · 17,028 cycles

EEL LIGHT INOP ROW 14ABC. REPLACED BATTERY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,675 hrs · 16,780 cycles

EXTERIOR EMERGENCY LIGHT AT 1R, 4R & 4L ARE INOPERATIVE. [07-27-07] RELAMPED.

Part: OXYGEN SYSTEM — LEAKING (CREW O2) · airframe 47,372 hrs · 16,667 cycles

CREW O2 PRESSURE APPEARS TO HAVE A SLOW LEAK. STARTED OUT WITH 1640 PSI NOW READS 1600 PSI AFT. [06-20-07] REMOVED BOTTLE AND SVC'D TO 1650PSI. NOTED THAT LEAK WAS EVIDENT AT BOTTLE AFTER CYCLING SHUTOFF VALVE SEVERAL TIMES, NO LEAK NOTED. REPLACED CREW O2 BOTTLE.

Part: CONTROLLER — ERRATIC (COCKPIT) · airframe 46,198 hrs · 16,229 cycles

1ST OFFICER'S SIDE WINDOW HEAT INOP LIGHT IS COMING ON AND GOING OFF. *S/D* RANG OUT ALL WIRES, ALL RESISTANCES WERE WITHIN RANGE. REPLACED WINDOW HEAT CONTROLLER AS PRECAUTION.

Part: SKIN — BULGED (FUSELAGE) · airframe 38,980 hrs · 13,604 cycles

AFT LAV SERVICE AREA STA 1700 HAS BULGING SKIN. CORROSION DAMAGE AT THE AFT LAV SERVICE DOOR DUE TO FLUID LEAKAGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,980 hrs · 13,604 cycles

FWD PIT STA 580 AND BETWEEN STR 24L AND 25L, FRAME HAS DENT. INSTALLED "J" ANGLE REPAIR ON TOP OF FRAME.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 38,980 hrs · 13,604 cycles

SHEAR TIE CORRODED BEYOND LIMITS AT STA 1400. INSTALLED NEW SHEAR TIE.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,980 hrs · 13,604 cycles

AFT PIT FRAME DENTED AT STA 1320 NEAR STR 26L AT INBOARD FLANGE. REPAIRED FRAME WITH INNER NESTED J-ANGLE.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,980 hrs · 13,604 cycles

AFT PIT FRAME DENTED STA 1420 BY STR 26L. REPAIRED FRAME WITH NESTED "J" ANGLE REPAIR.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 38,980 hrs · 13,604 cycles

SHEAR TIE IS CORRODED BEYOND LIMITS AT STA 1400 BETWEEN STR 30 AND 29R. REPLACED SHEAR TIE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 38,980 hrs · 13,604 cycles

FRAME WEB CORRODED OUT OF LIMITS AT STA 1400 RT BETWEEN STR 28R AND 29R. REPLACED FRAME SECTION.

Part: SILL — CORRODED (FUSELAGE) · airframe 38,980 hrs · 13,604 cycles

AFT CARGO DOOR SILL FS 1380 TO 1440 IS CORRODED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,980 hrs · 13,604 cycles

MAIN CABIN AT BS 1661 FLOORBEAM CORRODED BETWEEN BL 0 AND LBL 1. FABRICATED & INSTALLED STRAP REPAIR TO UPPER CHORD.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 38,980 hrs · 13,604 cycles

MAIN CABIN AT STA 1640 & RBL 8 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED "J" ANGLE REPAIR.

Part: STRAP — CORRODED (SKIN) · airframe 38,980 hrs · 13,604 cycles

AFT PIT STA 1400 TEAR STRAP BETWEEN STRINGERS 28R & 29R CORRODED. FABRICATED & INSTALLED TEAR STRAP.

Part: SKIN — DENTED (STA / STR 17) · airframe 37,060 hrs · 12,957 cycles

SKIN IS DENTED AT STA 618 BELOW STR 17L. MAJOR REPAIR ACCOMPLISHED. JETWAY DAMAGE. DOUBLER REPAIR INSTALLED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 35,560 hrs · 12,451 cycles

AFT PIT INTERCOSTAL HAS CORROSION STA 1500 TO 1513 STR 30R TO STR 29R. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW PART PER SRM 51-40-02 & BOEING DWG 146N5451.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 35,560 hrs · 12,451 cycles

SHEAR TIE HAS CORROSION, STA. 1628 TO STA 1620, AND STR 29L AND 28L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 35,560 hrs · 12,541 cycles

AFT PIT WEB ON AFT SIDE OF STA 1540, AND AT STR 29R AND 29L HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 35,560 hrs · 12,451 cycles

AFT PIT, STA 1520 & STR 29R AND 29L, SHEAR TIE HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 34,228 hrs · 11,977 cycles

EMERGENCY LIGHTS ARE INOP AT EXTERIOR AT DOOR 4L AND EEL LIGHTS, EXIT SIGN AND BULLNOSE LIGHTS BETWEEN ROWS 20-30. RELAMPED AT DOOR 4L AND RESEATED CONNECTORS ON POWER SUPPLIES.

Part: MOUNT — CHAFED · airframe 11,457 hrs

#1 ENGINE FORWARD MOUNT CHAFED. AFT SIDE OF FWD ISOLATOR BEARING JOURNAL. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW FWD MOUNT.

Part: GENERATOR — INOPERATIVE (ENGINE) · airframe 30,383 hrs · 10,582 cycles

DIVERTED DUE TO GENERATOR INOP AND APU FAILED TO START. NO EICAS STATUS MESSAGES FOR THE APU. NORMAL START ACCOMPLISHED ON THE GROUND.

Part: IDG — FAILED (NR 2 ENGINE) · airframe 29,009 hrs · 10,069 cycles

NR 2 IDG FAILED. REPLACED NUMBER 2 INTEGRATED DRIVE GENERATOR (IDG).

Part: PACK — FAILED (LEFT)

DIVERTED TO JFK DUE TO CABIN DECOMPRESSION. AIRCRAFT DIVERTED DUE TO THE LOSS OF THE RT PNEUMATIC SYSTEM. THE LT PACK WAS INOP ON TAKEOFF. THE LT ACM WAS REPLACED AND A PNEUMATIC HEALTH CHECK WAS PERFORMED ON BOTH ENGINES. THE RT ENGINE WAS FOUND WITH A BAD HIGH PRESSURE CONTROLLER (3399004-7U1) AND THE 490 AND FAN AIR TEMP SENSORS WERE REPLACED AS A PRECAUTIONARY.

Part: CONTROL MODULE — FAILED (LANDING GEAR)

DIVERTED TO IAD DUE TO A GEAR UNSAFE LIGHT INDICATION. FOUND INTERNAL OPEN IN LANDING GEAR LEVER CONTROL MODULE BETWEEN PINS 6 AND 7. REPLACED MODULE.

Part: ENGINE — MALFUNCTIONED (NR 2)

DURING TAKEOFF, THE NUMBER 2 ENGINE EGT EXCEEDED 645 DEGREES FAHRENHEIT, REACHING A PEAK OF 664 DEGREES FOR 20 SECONDS. *S/D* ENGINE REPLACED DUE TO HISTORY OF HIGH EGT.

Part: BEARING — SPALLED (LT ENGINE)

LEFT ENGINE OIL FILTER BYPASS INDICATION ILLUMINATED AND OIL TEMPERATURE, PRESSURE AND QUANTITY REMAINED NORMAL. OIL PRESSURE BEGAN TO RISE AND THEN DROPPED TO ZERO. ENGINE WAS SHUTDOWN, TEMP AND QUANTITY REMAINED STEADY. GROUND INSPECTION FOUND METAL IN THE SCREEN AND ON CHIP DETECTORS. ENGINE WAS REMOVED AND SHOP FOUND NUMBER ONE BEARING SPALLED.