N524UA

Part: COMPRESSOR BLADE — NICKED (NR 2 ENGINE) · airframe 75,224 hrs · 27,689 cycles

NR 2 ENG FAN BLADE HAS LARGE NICK NEEDS TO BE PROPERLY DRESSED. BLENDED BLADES IAW AMM 72-31-02.

Part: FSEU — FAULTY (LE SLAT) · airframe 74,926 hrs · 27,597 cycles

LE SLAT DISAGREE, FLIGHT DIVERTED. R & R FSEU 1 IAW AMM 27-51-01 AS PRECAUTION, OPERATIONS CHECKED GOOD. RAN SLAT & FLAPS IN NORMAL & ALTERNATE OPERATIONS, OPERATIONS CHECKED GOOD. VISUALLY INSPECTED ROTARY ACTUATORS OVERLOAD INDICATORS, ALL NORMAL, OK FOR FLIGHT. PERFORMED TROUBLESHOOTING IAW FIM 27-81-00, 101, FIG 104, BLOCK 1B. NO FAULTS.

Part: ENGINE — MAKING METAL (LEFT) · airframe 74,538 hrs · 27,480 cycles

LT ENG OIL FILTER MESSAGE, FLT DIVERTED. REPLACED NR 1 ENG DUE TO METAL FOUND IN FILTER. NEW ENG SERIAL NUMBER 726695. REMOVED ENG SERIAL NUMBER 727198. IAW AMM & TOD 71-00-02 FOR WORK ACCOMPLISHMENT.

Part: CONTROL PANEL — SHORTED (CABIN LIGHTS) · airframe 74,039 hrs · 27,312 cycles

CABIN LIGHTS KEEP GOING OUT, CONTROL PANEL BY L1 DOOR SEEMS TO HAVE SHORT. REPLACED PANEL WITH PANEL FROM 5413.

Part: GCU — FAILED (NR 1) · airframe 73,203 hrs · 27,061 cycles

LEFT AC BUS FAILURE, RTFL. REPLACED NR 1 GCU.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 73,058 hrs · 27,017 cycles

SIDE WALL LIGHTS AT 8F AND 40A INOP. REPLACED SIDEWALL BALLAST AT 8F AND 40A, OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (CABIN TEMP) · airframe 72,936 hrs · 26,983 cycles

FLT DECK WARMER THAN SELECTED WITH SWITCH ON & TEMP CONTROL IN AUTO. INOPERATIVE LIGHT EXISTING. 82' WITH FLT DECK CONTROLLER IN FULL COLD. PERFORMED FILTER AND SENSOR CLEANING. TEMP CONTROLLER LISTS NO FAULTS. BITE CHECKED GOOD. OPERATED LEFT PACK IN AUTO. OPS CHECKED GOOD. OKAY TO CONTINUE.

Part: INDICATION SYS — FLUCTUATES (FUEL SYSTEM) · airframe 71,620 hrs · 26,551 cycles

REPEAT WRITE UP. CENTER FUEL QTY MIGRATING FROM 16.2 TO 14.5. FQIS SHOWS CODE 76, SEE FIM 28-41 TASK 880 FUEL QTY INDICATION IN CTR TANK FLUCTUATING UP AND DOWN.

Part: FITTING — LEAKING (CTR FUEL TANK) · airframe 71,572 hrs · 26,534 cycles

FUEL LEAKING FROM THE CENTER FUEL TANK RIGHT FORWARD CORNER DRIPPING ONTO THE AIR COND PACK DUCTING. FUEL EXIT FOUND AT LOWER FORWARD OUTBOARD FITTING ABOVE RIGHT AIR COND BAY COMPARTMENT LEAK IS MARKED. REPAIRED FUEL LEAK REF MM. SEALANT APPLIED SEPT 241500.

Part: CONTROL UNIT — LEAKING (CENTER TANK) · airframe 71,251 hrs · 26,424 cycles

FOUND LEFT CENTER TANK FUEL SHUT OFF VALVE CONTROL UNIT LEAKING AFTER VALVE OPENED. LOCATED ABOVE THE APU FUEL SUPPLY PUMP IN LEFT W-W. REPLACED LEFT CENTER SHUTOFF VALVE ACTUATOR, (CONTROL UNIT). PRESSURIZED FUELING MANIFOLD TRANSFERRED FUEL, NO LEAKS.

Part: SMOKE GOGGLES — LOOSE (OBSERVER'S) · airframe 70,271 hrs · 26,094 cycles

OBSERVER SMOKE GOGGLES STRAP TOO LOOSE REPLACED GOGGLES.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 69,941 hrs · 25,977 cycles

DOOR 2L ARM LGT WILL NOT ILLUM. REPLACED LAMP AT SLIDE ARM INDICATOR.

Part: ACTUATOR — LEAKING (NR 1 ENGINE) · airframe 69,834 hrs · 25,938 cycles

NR 1 ENG 2.5 ACT IS LEAKING FUEL FROM WEEP HOLE IN ACT BODY. REPLACED 2.5 BLEED ACT AND RIGGED REF MM. ACP IDLE RUN. NO LEAKS NOTED, OPS CHECKED OKAY.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 69,434 hrs · 25,778 cycles

FLOOR SOFT IN AISLE NEAR 34C AND 35C. FLOOR PANEL AT AISLE ROW 35 - 2" SOFT SPOT, 4" FROM EDGE OF PANEL. ACP'D INTERIM REPAIR PER MM. INSTALLED ALUM METAL 0.071" THICKNESS OVERLAP ON SOFTNESS AREA. REPLACE FLOOR PANEL AT NEXT "C" CHECK.

Part: WIRE — DAMAGED (MLG) · airframe 68,975 hrs · 25,617 cycles

LANDING GEAR ALTERNATE EXTENTION CIRCUIT BREAKER POPPED ON P6-1. REPAIRED DAMAGED WIRE BY SPLICE SP1544 REF WDM32-12-12, WIRE LOCATED IN LEFT MAIN GEAR WHEEL WELL NEAR GEAR DOOR CLOSED SWITCH.

Part: PROBE — FAULTY (FUEL QTY) · airframe 68,700 hrs · 25,517 cycles

FUEL QTY TOTALIZER AND CENTER TANK INDICATORS ARE BLANK. FUEL QTY PROCESSOR FAULTING CTR TANK DENSITOMETER. FOUND FQPU FAULT CODE 76 CTR TANK PROBE 6. REPLACED PROBE #6. AFTER REPLACEMENT NO FAULT CODES NOTED.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 68,331 hrs · 25,366 cycles

CAPTAINS FWD WINDOW DELAMINATED, DELAMINATED AREA IS ON LOWER INBOARD CORNER. DELAMINATION MEASURES 3 INCHES HORIZONTAL INTO CLEAR VIEW AREA AND 4 INCHES VERTICAL INTO CLEAR VIEW AREA. WINDOW NEEDS REPLACEMENT. REPLACED NR 1 WINDOW.

Part: PANEL — FAULTY (AUDIO SYSTEM) · airframe 68,206 hrs · 25,323 cycles

CAPT O2 MASK MIC HOT WITH FLIGHT INTERPHONE SELECTED. REPLACED CAPT AUDIO SEL PANEL & AUDIO ACCESSORY, NO HELP. CONFERRED WITH LM (BRENDEL) WHO SUGGESTED SVC TIP 23-51-00-500A. CREW AGREES THIS WOULD COVER THE DESCRIBED CONDITION. VERIFIED VHF CHANNELS ARE CLEAR WITH NO BLEED OVER. CONDITION COULD ALSO BE HEARD USING THE MINITELS. VERIFIED VHF CHANNELS ARE CLEAR WITH NO BLEED OVER.

Part: SINK — CRACKED (GALLEY) · airframe 67,804 hrs · 25,182 cycles

AFT GALLEY SINK CORNER FOUND CRACKED. MASSIVE AMOUNT OF WATER LEAKING FROM LEFT SIDE OF AFT GALLEY ON DESCENT. WATER 8FT DOWN AISLE. FOUND CRACK IN AFT GALLEY SINK CORNER. CRACK IS IN AFT OUTBD CORNER WHEN LOOKING AFT. NEEDS TO BE WELDED OR REPLACED. -INF- :LM INFO: NEXT STATION, IF UNABLE TO REPAIR, PLZ IDENTIFY PARTS NEEDED AND IPC REFERENCE. INF- :PER IPC 25-30-00B-001R THE SINK IS PART OF THE COUNTERTOP. COUNTER TOP PART NUMBER IS 839217-401. TAKE & POST RVI PIXS OF THE DAMAGED AREA. PICTURES HAVE BEEN TAKEN AND UPLOADED TO RVI SITE. REMOVED COUNTERTOP AND R&R'D TO SHOP R29329 FOR WELDING AND REINSTALLED ON SMC2.

Part: SIGN — MISSING (CABIN) · airframe 67,880 hrs · 25,209 cycles

L SIDE OVERWING EXIT SIGN COVER MISSING. INSTALLED NEW OVERWING EXIT SIGN COVER ON LEFT SIDE.

Part: LIGHT — NOT SEATED (CABIN) · airframe 67,214 hrs · 24,967 cycles

L EMER ESCAPE SQUIB TEST LIGHT DOES NOT TEST. RESEATED LIGHT BULB, TESTED NORMAL.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 67,057 hrs · 24,904 cycles

FOUND EEL LIGHT STRIP NOT WORKING IN FRONT OF THE FWD AFT LAV DOOR. REPLUG EEL LIGHT TO STRIP. OPS CHECK LIGHTING EEL LIGHT WORKS FINE.

Part: SWITCH — SHORTED (LAVATORY DOOR) · airframe 67,027 hrs · 24,895 cycles

FWD AFT LAV DOOR SWITCH SHORTED CAUSING SMOKE IN AFT CABIN PRIOR TO DEPARTURE. REPLACED LAV DOOR SWITCH ASSY WIRES WERE NOT DAMAGED. ONLY THE MICRO SWITCH WAS DAMAGED. OPS TESTED AFTER RE-ASSEMBLY WITH NEW SWITCH. CHECKED GOOD AFTER MULTIPLE CYCLES (SWITCH CONTROLS THE FLUORESCENT LIGHTS)

Part: WINDOW — MALFUNCTIONED (COCKPIT) · airframe 65,066 hrs · 24,157 cycles

CAPT WINDOW CAME OPEN 2INCHES WITH HANDLE LOCKED. OPERATED WINDOW AND CHECKED ADJUSTMENT. WINDOW FOUND IN PERFECT WORKING ORDER. OK FOR CONTINUED SERVICE AT THIS TIME. OPS CHECKS NORMAL.

Part: CARTRIDGE — NO TEST (ESCAPE SLIDE) · airframe 63,463 hrs · 23,534 cycles

LT ESCAPE SLIDE SQUIB DOES NOT TEST. CARTRIDGE WILL NOT TEST. REPLACED MASTER CONTROL VALVE SQUIB.

Part: BEARING — MIGRATED (R2 DOOR) · airframe 63,463 hrs · 23,534 cycles

MED 2 RT BODY TORQUE TUBE LOWER BEARING HAS MIGRATED UP ON LOWER HINGE LINK SHAFT. (SERPENTINE PLATE) REPAIRED ON DOCK WU K7660C BY 116743 REMOVED DOOR, REPAIRED BRG, INSTALLED DOOR, OPS CK'D DOOR.

Part: CONNECTOR — FAULTED (SQUIB) · airframe 59,684 hrs · 22,043 cycles

NR 1 L FIRE BOTTLE WILL NOT TEST. ACCOMPLISHED LEFT ENGINE EXTINGUISHER BOTTLE SQUIB TEST CIRCUIT TEST. RANG OUT WIRING FROM M32 SQUIB TEST PANEL TO LEFT SQUIB CONNECTOR D2188 ON BOTTLE 1, B17. CHECKED GOOD. CONNECTOR D2188 ON SQUIB CHECKED GOOD. REPLACED SQUIB TEST PANEL M32 DUE TO BAD SWITCH S1. TESTED GOOD.

Part: ROD — BROKEN (R1 DOOR) · airframe 58,089 hrs · 21,480 cycles

UNABLE TO DISARM DOOR 1R, FOUND LOWER GATE ACTUATING ROD BROKEN AND CORRODED AT LOWER ROD END BEARING.

Part: WINDOW — OVERHEATED (COCKPIT) · airframe 57,999 hrs · 21,442 cycles

STRONG ELECTRICAL ODOR IN FLT DECK, GOT WORSE DURING DESCENT. ODOR WAS COMING FROM NR 1 LT WINDSHIELD. WINDOW HEAT TERMINAL BLOCK MELTED. REPLACED NR 1 LT WINDOW, REPLACED WIND HEAT CONTROL UNIT FOR WINDOW 1L AS PRECAUTION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,454 hrs · 21,242 cycles

EXTERIOR EMERGENCY LIGHT INOP AT DOOR 4R. CAUSE, LAMP INOP. RELAMPED ASSY, OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 56,974 hrs · 21,061 cycles

EXTERIOR EMERGENCY EXIT LIGHT INOP AT DOOR 2L. RELAMPED EMERGENCY LIGHT.

Part: FEEDER CABLE — DAMAGED (CABIN) · airframe 56,974 hrs · 21,061 cycles

EEL LIGHTING POWER FEED CABLE BURNT AND ARCHING AT ROW 18. EEL LIGHTS INTERMITTENT, 8 FOOT SECTION. REPLACED POWER FEEDER CABLE.

Part: SCREW — MISSING (LIGHT RECEPTACLE) · airframe 56,974 hrs · 21,061 cycles

EXTERIOR EMERGENCY EXIT LIGHT INOP AT DOOR 4R. REPLACED MISSING SCREWS. OPS CHECKS GOOD.

Part: LIGHT — FAULTY (R3 DOOR) · airframe 56,783 hrs · 20,990 cycles

SLIDE ARMED LIGHT ABOVE DOOR 3R IS ILLUM WHEN SLIDE IS DISARMED.

Part: LIGHT — FAULTY (CABIN) · airframe 56,783 hrs · 20,990 cycles

THE EMERGENCY LIGHTS ON THE LEFT SIDE OF AIRCRAFT ARE ON. LIGHTS OVER THE DOORS. PERFORMED RESET OF EMERGENCY LIGHT SYSTEM, ALL CHECKED OK AFTER RESET.

Part: SWITCH — DIRTY (SLIDE LIGHT) · airframe 56,783 hrs · 20,990 cycles

SLIDE ARMED LIGHT ABOVE DOOR 3R IS ILLUM WHEN SLIDE IS DISARMED. FOUND DIRTY SWITCH. CLEANED SWITCH, OPS CHECKED GOOD.

Part: LIGHT — FAULTY (CABIN) · airframe 56,783 hrs · 20,990 cycles

THE EMERGENCY LIGHTS ON THE LEFT SIDE OF AIRCRAFT ARE ON. LIGHTS OVER THE DOORS.

Part: SUPPORT BRACKET — CRACKED (RT WING FLAP) · airframe 56,130 hrs · 20,741 cycles

RIGHT WING OUTBOARD FLAP INBOARD JACK SCREW FWD JACKSCREW SUPPORT BRACKET INBOARD LWR RADIUS ABOVE BORE LUG CRACKED. RT WING OTBD FLAP INBD JACK SCREW FWD JACK SCREW SUPPORT BRACKET INBD LOWER RADIUS ABOVE BORE LUG CRACKED. REMOVED AND REPLACED FLAP JACKSCREW SUPPORT BRACKET.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,130 hrs · 20,741 cycles

R2 DOOR UPPER HINGE CUTOUT TRIMMED ALL THE WAY UP TO BEND LINE OF FRAME REQUIRES REPAIR. FOUND NO CRACKS ON FRAME AFTER NDT INSPECTION, INSTALLED REPAIR DOUBLER AS A PRECAUTIONARY.

Part: FRAME — DENTED (BS 540 S26-27L) · airframe 56,130 hrs · 20,741 cycles

FORWARD PIT FRAME AT STA 540 BETWEEN STR 26L AND 27L HAS DENT. MAJOR REPAIR ACCOMPLISHED. REMOVED EXISTING PRODUCTION SPLICE BETWEEN STR 23L-26L AND FABRICATED A NEW PRODUCTION SPLICE AND STRINGER CLIPS AND REPLACED SHEAR TIE -664 ABOVE STR-24L,

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,130 hrs · 20,741 cycles

MID CABIN EEL LIGHT BAR AT MID LAV INOPERATIVE. 11-01-07 REPLACED LIGHT BAR, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (L2 DOOR SLIDE) · airframe 56,130 hrs · 20,741 cycles

L2 DOOR SLIDE LIGHT IS INOPERATIVE. 11-01-07 REMOVED AND REPLACED SLIDE LIGHT ASSY.

Part: SUPPORT — CRACKED (R2 DOORWAY) · airframe 56,130 hrs · 20,741 cycles

CABIN R2 DOOR FWD CUTOUT AREA AT 680 STR 12R DOOR SUPPORT STRUCTURE CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED CRACKED WEB.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,130 hrs · 20,741 cycles

L2 DOOR UPPER HINGE CUTOUT IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. DOOR 2L UPPER HINGE CUTOUT TRIMMED ALL THE WAY UP TO BEND LINE OF FRAME. DRILLED, TRIMMED, FITTED AND INSTALLED REPAIR DOUBLER.

Part: SKIN — DAMAGED (NR 1 PYLON) · airframe 56,130 hrs · 20,741 cycles

NR 1 PYLON NAC STA 140 OUTBOARD SIDE SKIN FASTENER HOLE ELONGATED THRU SKIN AND DOUBLER. 11-01-07 MAJOR REPAIR ACCOMPLISHED. REAMED HOLES 1, 2, AND 3 TO BE TRUE ROUND AND CONCENTRIC. ACCOMPLISHED HFEC. INSTALLED FASTNERS IN HOLES 2 AND 3. MACHINED FREEZE PLUGS WITH 75T6 AND 15-5PH AND INSTALLED FREEZE PLUGS AND FASTNERS IN HOLE 1.

Part: SKIN — CANNING (BS 218-228 S16L) · airframe 56,130 hrs · 20,741 cycles

FOUND EXTERNAL FUSELAGE AT STA 218 TO 228 STRINGER 16L IS OIL CANNING.

Part: SHEAR TIE — CORRODED (BS 1700 S28-29R) · airframe 56,130 hrs · 20,741 cycles

AFT PIT STA 1700 BETWEEN STR 28R AND 29R SHEAR TIE HAS CORROSION.

Part: FRAME — DENTED (BS 1360 S26R) · airframe 56,130 hrs · 20,741 cycles

FOUND AFT PIT STA 1360 STR 26R MAIN FRAME HAS DENT.

Part: FRAME — DENTED (BS 1340) · airframe 56,130 hrs · 20,741 cycles

AFT PIT FRAME DENTED AT STA 1340 LT AND RT SLOPE AREAS. 10-26-07 MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE AREA AND FABRICATED AND INSTALLED AN APPROVED REPAIR.

Part: CREASE BEAM — DAMAGED (BS 1405-1420) · airframe 56,130 hrs · 20,741 cycles

RT CREASE BEAM HAS CORROSION ON WEB UPPER SURFACE AND SEVERAL RIVET HEADS AT STA 1405-1420 FOUND OUT OF LIMITS. 10-26-07 MAJOR REPAIR ACCOMPLISHED. RIVET HEADS AT STA 1405-1420 FOUND OUT OF LIMITS. REMOVED DAMAGE AREA AND FABRICATED REPAIR AND INSTALLED PER SRM.

Part: FLAPPER VALVE — STUCK (MID LAVATORY) · airframe 55,334 hrs · 20,460 cycles

FLIGHT DIVERTED DUE TO ALL LAVATORIES NEED SERVICING. MID LAV TOILET FLAP STUCK. SERVICED MID LAV FLAPPER TO UNSTUCK POSITION.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 55,065 hrs · 20,359 cycles

RIGHT AFT SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOP. [06-22-07] RELAMPED.

Part: CYLINDER — CORRODED (RT MLG) · airframe 54,896 hrs · 20,296 cycles

RIGHT MLG OUTER CYLINDER JUST ABOVE INNER THREADS FOR GLAND NUT IS HEAVILY CORRODED.

Part: BULB — FAULTY (ESCAPE SLIDE) · airframe 54,831 hrs · 20,273 cycles

NUMBER 1 SQUIB TEST FAILURE FOR LEFT EMERGENCY ESCAPE SLIDE. CLEANED AND RELAMPED BULB. [SUP 06-06-07] CLEANED AND RELAMPED BULB. ACCOMPLISHED SQUIB TEST SEVERAL TIMES ON P61 PANEL. TESTED OK.

Part: DUCT — LOOSE (LT ENGINE) · airframe 54,271 hrs · 20,070 cycles

RTFL DUE TO SIGNIFICANT VIBRATION IN LEFT ENGINE AFTER TAKEOFF. COULD NOT ADVANCE POWER W/O VIBRATION INCREASING. 3RD STAGE LPT BLADE FRACTURED. THE 3RD STAGE LPT BLADES AND VANES WERE SULFIDED. DURING DISASSEMBLY A BOLT FOR THE OUTER DUCT WAS FOUND FRACTURED. THE LOOSE DUCT REDUCED AIRFLOW TO THE BLADES AND THE ON-GOING BLADE SULFIDATION CAUSED THE FAILURE OF BLADE.

Part: BOTTLE — LEAKING (EVAC SLIDE) · airframe 53,616 hrs · 19,826 cycles

LOW BOTTLE PRESSURE. BOTTLE LEAKING AROUND GLASS ON GAUGE. REPLACED GAUGE

Part: O-RING — LEAKING (ESCAPE SLIDE) · airframe 53,312 hrs · 19,705 cycles

LOW BOTTLE PRESSURE. FUSIBLE PLUG O-RING LEAKING. REPLACED O-RING.

Part: PACKING — MISINSTALLED (FILTER HOUSING) · airframe 53,147 hrs · 19,645 cycles

LEFT ENGINE SHUTDOWN. LOSS OF OIL PRESSURE. LUBE AND SCAVENGE PUMP, PART NUMBER MR79232-168, FAILED. CAUSE OF FAILURE WAS DUE TO BOM DAMAGE. HARD OBJECT FLOWING DOWN FROM THE OIL SCAVENGE LINE CAUSED A SUDDEN STOPPAGE OF THE OIL SCAVENGE GEARS, PART NUMBERS 5009048 AND 5009049. THE INTERCONNECTING SPLINE SHAFT, PART NUMBER 5007416, SUFFERED AN IMMEDIATE TORQUE FRACTURE EVENT AS THE PRIMARY INPUT DRIVE SHAFT WAS ROTATING AT APPROXIMATELY 3,100 RPM UNDER UNLIMITED TORQUE AT THE MOMENT THE BOM STOPPED THE OIL SCAVENGE GEAR ROTATION. THE OIL PRESSURE GEARS, WHICH ARE LOCATED BEHIND THE OIL SCAVENGE GEARS, CEASED ROTATION WHEN THE INTERCONNECTING SPLINE SHAFT FAILED.

Part: WEDGE — DELAMINATED (NR 6 SLAT)

SLAT HAS DAMAGED DELAMINATED T/E WEDGE. WEDGE REPLACED.

Part: SKIN — DELAMINATED (NR 6 SLAT) · airframe 47,766 hrs · 17,679 cycles

SLAT NR 6 TRAILING EDGE WEDGE DEPARTED THE AIRCRAFT. LEADING EDGE PANELS DAMAGED AFT OF THE NR 6 SLAT. DELAMINATION OF SLAT'S TRAILING WEDGE (INDUSTRY PROBLEM). WEDGE DAMAGED LEADING EDGE PANELS PRIOR TO DEPARTURE. NEW NR 6 LEADING EDGE SLAT INSTALLED. LEADING EDGE PANELS REPAIRED.

Part: ASPIRATOR — DENTED (SLIDE BOTTLE)

LOW BOTTLE PRESSURE. FOUND DURING ASPIRATOR INSPECTION THAT BOTH ASPIRATORS HAD DENTED BARRELS. LOW BOTTLE PRESSURE: CYLINDER ASSEMBLY TEMPERATURE WAS STABILIZED AND GAGE NEEDLE WAS OBSERVED IN CENTER OF GREEN BAND. CYLINDER ASSEMBLY WAS LEAK CHECKED. NO LEAKS DETECTED. ASPIRATORS BARRELS DENTED. NO EXTERNAL SLIDE DAMAGE OBSERVED. SLIDE FOLDING PROCEDURE OBSERVED TO HAVE BEEN CORRECTLY PERFORMED PER AIR CRUISER CMM 25-66-02. IT IS ASSUMED SLIDE PACK WAS OVER-COMPRESSED DURING PACKING PROCEDURE.

Part: SENSOR — DIRTY (4R DOOR SLIDE) · airframe 45,365 hrs · 16,779 cycles

DOOR 4R SLIDE ARMED LIGHT INOP. ANOMALIE WAS CAUSED BY DIRT OR DEBRIS ON PROXIMITY SENSORS WHICH AFFECTED THE POSITION AND THEREFORE INDUCTANCE NECESSARY FOR SYSTEM OPERATION. CORRECTIVE ACTION CONSISTED OF CLEANING AND ADJUSTMENT OF THE GIRT BAR PROXIMITY SWITCHES/SENSORS.

Part: VALVE — DISCHARGED (ESCAPE SLIDE)

LOW BOTTLE PRESSURE. PRESSURE RELIEF VALVE DEFECTIVE. PRESSURE GAUGE WAS REPLACED WHICH INCLUDED REPLACEMENT OF PRESSURE RELIEF VALVE. OSV, WINSLOW, HAS ADDED ULTRASONIC LEAK DETECTION TO BOTTLE INSPECTION PROCESS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 42,070 hrs · 15,588 cycles

SKIN DAMAGED AT STA 470 AT STR 23 RT. MAJOR REPAIR - FILLER AND DOUBLER INSTALLED.

Part: SKIN — DAMAGED · airframe 38,020 hrs · 14,060 cycles

RIGHT HAND APU COMPT. DOOR EXTERNAL SKIN DAMAGED AROUND FORWARD LATCH CUTOUT. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,020 hrs · 14,060 cycles

EXTERNAL FUSE IS DENTED APPROX AFT OF DOOR 4R 12 INCHES AND ABOVE EMERGENCY LIGHT. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.

Part: SKIN — DAMAGED · airframe 38,020 hrs · 14,060 cycles

AFT PIT FRAME HAS DENT AT STATION 1580 BELOW STRINGER 25R 2EA. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. DOUBLER INSTALLED.

Part: SKIN — DAMAGED · airframe 38,020 hrs · 14,060 cycles

APU COMPT RIGHT HAND DOOR EXTERNAL SKIN DAMAGED AT 2ND FROM THE LATCH CUTOUT. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. DOUBLER INSTALLED.

Part: SKIN — DAMAGED · airframe 38,020 hrs · 14,060 cycles

EXTERNAL FUSELAGE LOWER SKIN DAMAGED STATION 781 BL 0. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.

Part: SKIN — CORRODED · airframe 38,020 hrs · 14,060 cycles

FORWARD PIT FUSELAGE SKIN HAS EXCESSIVE MATERIAL REMOVED AT STATION 606 BETWEEN STRINGER 19L AND 20L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,020 hrs · 14,060 cycles

FORWARD CABIN FLOORBEAM AT STATION 365, RBL9 HAS EXCESSIVE MATERIAL LOSS, MAJOR REPAIR ACCOMPLISHED. REINFORCING REPAIR INSTALLED.

Part: SKIN — DENTED · airframe 38,020 hrs · 14,060 cycles

FUSE SKIN HAS DENT WITH GOUGES AT STATION 620 S16L TO S17L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIRED DOUBLER INSTALLED.

Part: SKIN — DAMAGED · airframe 38,020 hrs · 14,060 cycles

APU COMPT RIGHT HAND DOOR EXTERNAL SKIN DAMAGED AT 2ND FROM FORWARD LATCH CUTOUT. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.

Part: SKIN — DAMAGED · airframe 38,020 hrs · 14,060 cycles

APU COMPT RIGHT HAND DOOR EXTERNAL SKIN DAMAGED AT AFT LATCH CUTOUT. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. DOUBLER INSTALLED.

Part: FRAME — DENTED · airframe 38,020 hrs · 14,060 cycles

AFT PIT FRAME AT STATION 1420 AND STRINGER 26L IS DENTED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REINFORCING REPAIR INSTALLED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,020 hrs · 14,060 cycles

LEFT HAND FUSELAGE STATION 1478 STRINGER 25L IS CREASED. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.

Part: FRAME — DENTED · airframe 38,020 hrs · 14,060 cycles

AFT PIT FRAME AT STATION 1420 STRINGER 26L DENTED. MAJOR REPAIR ACCOMPLISHED.REPAIR ANGLE FABRICATED AND INSTALLED UNDER FRAME.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 38,020 hrs · 14,060 cycles

AFT PIT STATION 1473 STRINGER 25L REPAIR HAS FASTENER ON UPPER FLANGE NO EDGE MARGIN. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER REPAIR.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 38,020 hrs · 14,060 cycles

EXT FUSELAGE DOUBLER AT STATION 1480 STRINGER 25L REQUIRES REMOVAL TO FACILITATE INSTALLATION OF 25L STRINGER. MAJOR REPAIR ACCOMPLISHED. DOUBLER INSTALLED.

Part: FRAME — CORRODED · airframe 38,020 hrs · 14,060 cycles

AFT PIT STATION 1480 AT STRINGER 22-23 RIGHT FRAME CORRODED AT APU GROUND WIRE CONNECTION. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. DAMAGED REMOVED. FILLER REPAIR DOUBLER AND FAIL SAFE CHORD INSTALLED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,020 hrs · 14,060 cycles

AFT PIT FUSELAGE FRAME STATION 1440 ABOVE STRINGER 25 LEFT IS CRACKED IN INBOARD CHORD FLANGE. MAJOR REPAIR ACCOMPLISHED. DAMAGE REMOVED. FRAME REPAIR INSTALLED.

Part: STRINGER — DAMAGED · airframe 38,020 hrs · 14,060 cycles

CABIN FUSELAGE STRINGER 16L HAS DAMAGE FROM BODY STATION 603 TO BODY STATION 606. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED · airframe 38,020 hrs · 14,060 cycles

AFT PIT FUSELAGE FRAME IS DENTED AT STATION 1460 STRINGER 25 LEFT. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED AREA MFG AND INSTALLED REPAIR DOUBLER.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 38,020 hrs · 14,060 cycles

AFT CABIN FLOOR DECK HAS 5 LOCATIONS OF EXCESSIVE MATERIAL REMOVED RBL 5, RBL 12, RBL 45, RBL 48, RBL 52, AT STATION 1682. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIRS.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 38,020 hrs · 14,060 cycles

CABIN FLOOR SUPPORT STATION 660 TO 680 FLOOR SUPPORT ANGLE IS CRACKED 3 PLACES. MAJOR REPAIR ACCOMPLISHED, REPLACED ANGLE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,020 hrs · 14,060 cycles

CABIN STATION 725 RBL 63 AFT EDGE OF DR 2R FLOOR SUPPORT IS CORRODED AT TOP SURFACE. MAJOR REPAIR ACCOMPLISHED. REPLACED CHANNEL.

Part: STRINGER — GOUGED · airframe 38,020 hrs · 14,060 cycles

AFT PIT FRAME AT STATION 1520, FRAME SPLICE HAS 3 AREAS OF DAMAGE FROM SIDEWALL PANEL SCREWS-SCREWS GOUGED INTO FRAME SPLICE STRINGER 24R. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPLACED SPLICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,020 hrs · 14,060 cycles

AFT CABIN STA 1640 FLOORBEAM UPPER SURFACE HAS CORROSION AROUND N-P HOLES RBL 1 TO RBL 53. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP AND FLANGE CUTOUT REPAIR.

Part: FRAME — DENTED · airframe 38,020 hrs · 14,060 cycles

FWD PIT FRAME DENTED AT STA 660 STR 24R. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPAIRED WITH FRAME DOUBLER.

Part: SLIDE — DEPLOYED (DOOR 1R)

NUMBER 1 RIGHT DOOR SLIDE DEPLOYED. *S/D* INADVERTENT DEPLOYMENT DUE TO HUMAN ERROR. DEPLOYMENT WAS NORMAL. SLIDE WAS REPLACED.

Part: ACTUATOR — BROKEN (LT MLG)

RETURNED TO DEN DUE TO LOSS OF LEFT HYDRAULIC SYSTEM. NORMAL LANDING. *S/D* LEFT MLG TRUCK POSITION ACTUATOR BLEED PLUG CAME LOOSE, CAUSING FLUID LOSS. ACTUATOR REPLACED. AIRCRAFT TO BE TESTED FOR PROPER FUSE OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

ALL EMERGENCY LIGHTS IN AFT GALLEY AREA ARE INOP, AND EEL LIGHTS IN BULLNOSE ABOVE SEATS 30C AND 34C ARE INOP. REPLACED POWER SUPPLY BATTERY AT M10817.

Part: WINDOW — NOT LATCHED (LT COCKPIT)

CAPTAIN'S WINDOW UNLATCHED AT 100 KNOTS ON TAKEOFF ROLL. ABORTED TAKEOFF. *S/D* WINDOW APPEARED CLOSED AND LOCKED. CAPTAINS SLIDING WINDOW CLOSING/LOCKING MECHANISM, OPS CHECKS NORMAL.

Part: BLADES — FAILED (RT ENGINE)

DURING GEAR RETRACTION DETECTED A LOUD REPORT ACCOMPANIED BY AIRCRAFT SHAKING. SHORTLY AFTER, HEARD TWO ADDITIONAL BANGS ALONG WITH JERKING. EGT BEGAN TO RISE, RETURNED RIGHT ENGINE TO IDLE. RE-APPLICATION OF POWER TO RIGHT ENGINE RESULTED IN CONTINUED COMPRESSOR STALL. ENGINE RETURNED TO IDLE, AIRCRAFT RETURNED TO FIELD. 9TH STAGE BLADE FAILURE. REPLACED ENGINE.

Part: EEL INVERTER — INOPERATIVE (CABIN)

EMERGENCY ESCAPE PATH LIGHTING INOP FROM ROW NR 9 THROUGH NR 16. REPLACED INVERTER, CHECKS OK.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO DOOR)

ABORTED TAKEOFF AT 70 KNOTS DUE TO CARGO PIT FIRE INDICATION. NO EVIDENCE OF FIRE FOUND. REPLACED CARGO SMOKE DETECTOR, SYSTEM OP CHECKS OK.