N567UA

Part: AUDIO PANEL — DEFECTIVE (COCKPIT) · airframe 69,494 hrs · 25,412 cycles

FIRST OFFICER`S MIC BUTTON STICKS AFTER TRANSMITTING FROM PTT SWITCH ON AUDIO SELECTOR PANEL. REPLACED PANEL, TESTED OKAY.

Part: HYDRAULIC LINE — LOOSE (RT MLG) · airframe 69,269 hrs · 25,339 cycles

RAMP REPORTED RT MLG SHOW SIGN OF FLUID LEAK. TIGHTENED RT MLG GEAR DOOR ACTUATOR RETURN HYD LINE, NO LEAK FOUND.

Part: B-NUT — LOOSE (RT MLG ACTUATOR) · airframe 69,258 hrs · 25,335 cycles

AT DEPARTURE TIME THERE IS FLUID ON THE UNDERSIDE OF THE AIRCRAFT. LOOSE UNION & B NUT ON RT MLG ACTUATOR. SECURED B NUT & UNION, CLEANED MLD DOOR & BOTTOM OF FUSELAGE.

Part: SIGN — UNSECURE (CABIN) · airframe 68,848 hrs · 25,199 cycles

CUSTOMER SERVICE REPORTS THAT THE EXIT SIGN ABOVE DOOR 2L FELL DOWN WHEN THE DOOR WAS OPENED. SECURED EXIT SIGN.

Part: BATTERY — DEFECTIVE (MAIN) · airframe 68,852 hrs · 25,200 cycles

MAIN BATTERY CHARGER EICAS STATUS MESSAGE CAN'T CLEAR. REPLACED MAIN BATTERY IAW MM 24-31-01 & RELAY K10424.

Part: INLET BULLET — CRACKED (NR 2 ENGINE) · airframe 68,835 hrs · 25,194 cycles

NR 2 ENG INLET CONE, TWO CRACKS RADIATING FROM TWO SEPARATE BOLTS GREATER THAN .5" IN LENGTH, IN ADDITION TO SEVERAL AREAS OF DELAM. IAW AMM 72-31-01. R & R NR 2 ENG COMPRESSOR INLET CONE IAW AMM 72-31-01, OK TO CONTINUE.

Part: CAP — UNSECURE (CABIN) · airframe 68,822 hrs · 25,189 cycles

EMERGENCY LIGHT STRIP COMING UP AT ROW 12ABC. SECURED EMERGENCY EXIT LIGHT CAP.

Part: SEAL — LEAKING (SLIDING WINDOW) · airframe 68,387 hrs · 25,040 cycles

F/O SLIDING WINDOW HAS PRESSURE LEAK-HIGH PITCHED SQUEAL. INSPECTED AND CLEANED ENTIRE SEAL AND SILL F/O SLIDING WINDOW AND PRESSURIZED TO 6 PSI. NO DEFECTS OR LEAKS NOTED.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 68,009 hrs · 24,933 cycles

CREW REPORTS HEARING & FEELING A SLIGHT VIBRATION (LIKE LOUD LAV MOTOR FLUSHING), FOLLOWED BY LT ENGINE OIL FILTER EICAS MESSAGE. CREW FOLLOWED QUICK REFERENCE HANDBOOK & REDUCED THROTTLE & LIGHT REMAINED ILLUMINATED. AS CREW STARTED ENGINE SHUTDOWN PROCEDURE ENGINE SHUT ITS SELF DOWN. REPLACED NR 1 ENGINE, AUDIO CONTROL PANEL ENGINE RUN NO LEAKS NOTED.

Part: ENGINE — SHUTDOWN (NR 1) · airframe 68,009 hrs · 24,933 cycles

NR 1 ENGINE INFLIGHT SHUTDOWN.

Part: LIGHT — UNSECURE (ROW 11) · airframe 67,548 hrs · 24,797 cycles

EMERERGENCY LIGHT LOOSE ROW 11. SECURED EMERGENCY LIGHT TO FLOOR, OK TO CONTINUE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 54,508 hrs · 19,974 cycles

AFT PIT FRAME DENTED STA 1420, BETWEEN STR 25L AND 24L. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF FRAME AND FABRICATED A REPAIR J-ANGLE AND INSTALLED PER SRM 53 00-07, REPAIR 5 PER SRM 53-00-07.

Part: LIGHT — DAMAGED (CABIN) · airframe 67,152 hrs · 24,683 cycles

EMERGENCY LIGHT AT ROW 11 IS BUCKLED. SECURED LIGHT AT ROW 11. ACFT OK TO CONTINUE.

Part: WHEEL — VIBRATION (NLG) · airframe 66,995 hrs · 24,634 cycles

NOSE WHEEL SHIMMY ON TAKEOFF. REPLACED LEFT AND RIGHT NOSE WHEEL ASSY.

Part: COVER — UNSECURE (EMERGENCY LIGHT) · airframe 67,000 hrs · 24,636 cycles

EMERGENCY EXIT FLOOR LIGHTING STRIP IS COMING UP AT ROW 12. SECURED EMERGENCY LIGHT COVER.

Part: MEDICAL KIT — UNSERVICEABLE (COCKPIT) · airframe 66,163 hrs · 24,350 cycles

NO SAFETY WIRE ON BP CUFFS OF EMERGENCY MEDKIT IN COCKPIT. PLACED ON DF REF MEL 2564H. REPLACED COCKPIT EMERGENCY MEDKIT.

Part: HANDLE — FAULTY (COCKPIT) · airframe 65,675 hrs · 24,177 cycles

ENGINE 1 FIRE HANDLE RED COVER WILL NOT STAY LATCHED CLOSED. REPLACED LEFT ENGINE FIRE CONTROL HANDLE M10443, OPS CHECK GOOD.

Part: PROBE — FAULTY (PITOT HEAT) · airframe 65,582 hrs · 24,140 cycles

TROUBLESHOOT CAPT PITOT HEAT LIGHT PROBLEM. ACCOMPLISHED PROBE HEAT TEST FRONT P61 PANEL. ALL LIGHTS EXTINGUISH EXCEPT CAPT PITOT PROBE LIGHT. SUSPECT PROBE BAD. REPLACED CAPT PITOT PROBE ASSY.

Part: FITTING — FAULTY (TE FLAP) · airframe 65,570 hrs · 24,135 cycles

DURING REWORK OF RIGHT I/B FLAP TORQUE TUBE SLOT DOOR ARM REF CF0580. REMOVED AND REPLACED FITTING PER SRM 51-40-02 AND ECRA5750-04490.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 65,570 hrs · 24,135 cycles

FAB ANT REPAIR DOUBLER AT STA 1393. FAB REPAIR DOUBLER AT STA 1393 PER ECRA5361-01024. THE FUSELAGE SKIN REPAIR INSTALLED BETWEEN BS 1385-1401 & STR 28L-29L.

Part: SKIN — DENTED (FUSELAGE) · airframe 65,570 hrs · 24,135 cycles

SMALL DENT APPROX 12" BELOW & IN LINE WITH FWD EDGE MID LAV SER PANEL REF INBOUND CF9032. REPAIR FUSELAGE SKIN AT STA 700 STR 23L & 24L IAW ECRA 5331-01636. THE FUSELAGE SKIN REPAIR INSTALLED BETWEEN BS 695- 705 & STR 21L-25L.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 65,570 hrs · 24,135 cycles

L-1 DOOR ESCAPE SLIDE FWD CABLE FRAYED. REMOVED & REPLACED L4 DOOR ESCAPE SLIDE IAW AMM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,570 hrs · 24,135 cycles

CABIN FLOORBEAM T-CAP CORRODED STA 1640 RBL 34 TO RBL 60. MAJOR REPAIR ACCOMPLISHED: FABRICATED REPAIR AND INSTALLED WITH CHANNELS AND ANGLES IAW SRM 53-00-51. SCUFF PLATE AND GUTTER REMOVED AND REPAIRED IAW MM 53-13-01.

Part: SPOILER — PUNCTURED (NR 7) · airframe 65,570 hrs · 24,135 cycles

NR 7 SPOILER HAS 5EA PUNCTURES, ALL 5 ARE APPROX 3-8TH INCH DIA, ALL MEASUREMENTS ARE INCHES FROM O/B EDGE X T/E, 8.5X5.25, 11X7, 26.5X13, 57.5X12.5, 61X5.5. ALL DAMAGES ALLOWABLE REF SRM 57-70-01 PG 102, TAPED OVER DAMAGE.

Part: SPOILER — PUNCTURED (NR 5) · airframe 65,570 hrs · 24,135 cycles

NR 5 SPOILER HAS 2EA PUNCTURES BOTH 3-8TH INCH DIA, 11.5" FROM O/B EDGE AND 7" FROM T/E, 59" O/B EDGE 12" FROM T/E.

Part: SPOILER — PUNCTURED (NR 8) · airframe 65,570 hrs · 24,135 cycles

NR 8 SPOILER HAS 2 EA PUNCTURES 1 AT 11.75" FROM O/B EDGE AND 13.0" FROM TE APPROX .5" DIA NR 2 IS AT 69.75"X 7.0" APPROX .3" DIA. FOUND NO DELAM OUTSIDE OF PUNCTURES, APPLIED SPEED TAPE OVER DAMAGED AREAS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,570 hrs · 24,135 cycles

CABIN FLOORBEAM T-CAP CORRODED STA 324 RBL 46. T-CAP MATERIAL LOSS FOUND TO BE OUT OF SRM LIMITS. FABRICATE & INSTALLED T-CAP FROM LBL 7 TO RT SIDE END OF FLOORBEAM PER SRM 53-10-08.

Part: SHAFT — WORN (R4 DOOR) · airframe 65,570 hrs · 24,135 cycles

R-4 DOOR INNER SHAFT P/N 65B1523-3 IS WORN. REPLACED INNER SHAFT.

Part: COLLAR — WORN (R4 DOOR) · airframe 65,570 hrs · 24,135 cycles

R-4 DOOR CLUTCH COLLAR P/N 140N2044 IS WORN. REPLACED CLUTCH COLLAR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,570 hrs · 24,135 cycles

MAIN CABIN FLOORBEAM UPPER CHORD CORRODED, STA 365 RBL 0 TO RBL 62. MAJOR REPAIR ACCOMPLISHED: CORROSION FOUND TO BE OUT OF SRM LIMITS. FABRICATE & INSTALLED UPPER CHORD T-CAP AT STA 365 LBL 11 TO RBL 69 PER SRM 53-00-51 REPAIR 3 FIG 201 SH 1 THRU 6. THE REPAIR MADE TO CABIN FLOOR T-CAP AT STA 365 LBL 11 TO RBL 69 REF NR 44608 IS CATEGORY A PERMANENT REPAIR PER SRM 53-00-51 REPAIR 3 PG 202.

Part: BEARING — WORN (R4 DOOR) · airframe 65,570 hrs · 24,135 cycles

R-4 DOOR BUTTERFLY HANDLE BEARING HOUSING HAS IMPROPER HARDWARD AND WORN BEARING. REMOVED EXISTING HARDWARE AND REPLACED WITH NEW HARDWARE, P/N BACB30LH3-5, P/N NAS1149DO3 16J, AN P/N BACN1CYR3CD PER SRM AND REPLACED BEARING P/N M81934-1-06C014 PER BSOPM 20-50-03.

Part: MOUNT — GOUGED (R4 DOOR) · airframe 65,570 hrs · 24,135 cycles

R-4 DOOR ESCAPE SLIDE UPPER MOUNTS GOUGED. REMOVED AND REPLACED SLIDE MOUNTS, P/N 416N2201U42 AND 416N2201Y40.

Part: LIGHT — LOOSE (CABIN) · airframe 65,331 hrs · 24,041 cycles

EMERGENCY LIGHT STRIP IN FRONT OF LAV AT DOOR 2L IS PULLED LOOSE. CHECKED EMERGENCY ESCAPE LIGHTING IN FRONT OF MID LAV DOOR. FOUND STRIP SECURE AND OPERATIONAL.

Part: BRACKET — MISSING (FUSELAGE) · airframe 65,221 hrs · 24,000 cycles

CREW FOUND FIRE EXTINGUISHER BRACKET MISSING. REPLACED FIRE EXTINGUISHER AND BRACKET.

Part: SWITCH — FAULTY (LE SLAT) · airframe 64,178 hrs · 23,660 cycles

FSEU 1 SHOWS SLAT LOSS FAULT. REPLACED FSEU 1, NO HELP. RE-INSTALLED ORIGINAL UNIT. FLAPS AND SLATS ARE LOCKED IN NORMAL AND ALTERNATE MODES. REF FIM 27-81-00, SUSPECT A SLAT POSITION TRANSMITTER OR A SLAT LOSS POSITION SENSOR. ACCMP'D TROUBLESHOOTING PER FIM 27-81-00 UP TO FIG 105 (SHEET 3) BLOCK 4. PIN 7 AT D41 828P IS 1 OHM NEED TO CONT TO BLK 43 MOST LIKELY NEEDS NEW SLAT LOSS SENSING SWITCH S10338. REPLACED INBD SLAT B LOSS SWITCH AND RESET TRIGGER AT SLAT #9.

Part: COVER — DAMAGED (CABIN) · airframe 64,163 hrs · 23,655 cycles

EMERGENCY FLOOR PATH LIGHTING DAMAGED NEAR DOOR 4L. REPLACED DAMAGED SECTION OF CLEAR TRACK COVER.

Part: MOTOR — FAULTY (WINDSHIELD) · airframe 64,140 hrs · 23,647 cycles

CAPTAINS WINDSHIELD WIPER CAME OUT OF PARKED UNCOMMANDED. VIBRATNG AND FLOATING AT BOTTOM. FOUND MOTOR SHAFT WITH PLAY AND WIPER ARM SPLINE BUSHING WORN AND NOT ENOUGH WIPER ARM PRESSURE.REPLACED WIPER MOTOR PER MM. REPLACED WIPER ARM AND BLADE PER MM. ADJUSTED SYSTEM PER MM, OPS CHECK GOOD.

Part: ACCESSORY UNIT — MALFUNCTIONED (AUDIO SYSTEM) · airframe 64,139 hrs · 23,646 cycles

F/O O2 MASK DOES NOT TRANSMIT VOICE ON FLT INPH TO F/O SPEAKER. REPLACED AUDIO ACC UNIT AND RESEATED PIN 5 & 6 ON CONNECTOR D337 AUDIO SELECTOR PNL (F/O'S )SYSTEMS GRD CHECKS NORMAL.

Part: CABLE — STICKS (PARKING BRAKE) · airframe 64,113 hrs · 23,640 cycles

PARKING BRAKE HANDLE STICKS. PARKING BRAKE EICAS MSG DISPLAYED WHEN RELEASED. TROUBLESHOT DEFECTIVE PARKING BRAKE CABLE SYSTEM PER FIM 32-44-00. FOUND ALL COMPONENTS INTACT. SUSPECT DEFECTIVE CABLE ASSEMBLY. REMOVED ALL ATTACHING HARDWARE TO PARKING BRAKE CABLE. CABLE REPLACED.

Part: LIGHT — UNSECURE (ROW 11) · airframe 63,466 hrs · 23,397 cycles

EMERGENCY LIGHT AT ROW 11 LOOSE. RESECURED LIGHT, OPS CHECKED GOOD.

Part: LIGHT — UNSECURE (ROW 12) · airframe 63,451 hrs · 23,391 cycles

EMERGENCY LIGHT LOOSE ROW 12. RESECURED EMERGENCY LIGHT.

Part: DUCT — OBSTRUCTED (COCKPIT) · airframe 63,267 hrs · 23,326 cycles

ABNORMAL NOISE & VIB IN FLT DECK. FOUND DEBRIS IN CENTER DIST DUCTING. DUCTING HAS BEEN CLEANED FROM ROW 40 FWD TO ROW 30. NEED TO COMPLETE DUCT CLEANING FROM ROW 30 FWD. REMOVED LARGE DEBRIS ITEMS, FROM FLT DECK MAIN DIST DUCT AT TEMP BULB (WITH HOLE MULTIFOLD PAPER TOWEL, AND FLT DECK LEFT AFT EYEBALL DOWNSTREAM OF OVERHEAD Y DUCT. NOISE DB OK PER SVC TIP.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 63,262 hrs · 23,323 cycles

CREW REPORTED OIL SMELL. ACP SMOKE OR FUMES PER FIM. REMOVED ENGINE AND AIR CONDITIONING DISTRIBUTION DUCTS FOR PRESENCE OF OIL. NO INDICATION OF OIL INSIDE OF THE DUCTS. NEED TO PERFORM ENG RUN FOR BLEED PRESS SPLIT. BLEED SHIFT OCCURS ON BOTH ENGS AT 80% N2. LT ENG PRECOOLER TEMP ABOUT 30 DEG HIGHER AT IDLE. AS POWER INCREASES, PRECOOLER TEMP REACHES 310 DEG AS LT BLEED DROPS. STRONG OVHT SMELL OCCURS DUE TO PACK OVERTEMP. RT BLEED APPROX 180DEG. LT BLD PRESS 25 PSI AND FALLING VS RT. SUSPECT FAMV FAILURE. ACCOMPLISHED OIL SMELL TASK. PILOT VALVE OVER TEMP SENSOR AND FAN AIR VALVE REPLACED. PERFORMED HIGH POWER RUN, OPS CHECK NORMAL. MEASURED COCKPIT NOISE LEVELS USING SIMPSON SOUND METER GRD ENGS RUNNING 2 PACS ON = 72DB, TAKEOFF = 88DB, CLIMB=85DB, CRUISE = 82DB NOISE LEVEL INCREASE TO 90DB WHEN ADJUSTING CABIN TEMPS TO COLD TO WARM. REPLACED LEFT PACK FLOW CNTL VALVE (P/N S210T130-608 / DASH# 187).

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 63,262 hrs · 23,323 cycles

CAPTAIN'S WINDSHIELD'S VISIBILITY IS AFFECTED BY DEFECTS, REPLACE FIRST AVAILABLE. CREW COMMENTS: U SHAPED DELAMINATION BUBBLE WINDOW 1L LOWER RT CORNER. REPLACED CAPT'S WINDSHIELD PER MM.

Part: SELECTOR — FAULTY (COCKPIT) · airframe 63,250 hrs · 23,319 cycles

NOISE IN CABIN. REPLACED-: FLIGHT DECK ZONE TEMPERATURE SELECTOR & ZONE TEMPERATURE CONTROLLER IAW MM. REPLACED FLIGHT DECK ZONE TEMPERATURE SENSOR IAW MM FLT DECK NOISE CHECKED GOOD. DUE TO HISTORY OF LOUD COCKPIT NOISES AND UNCONTROLLABLE COCKPIT TEMPERATURES. NEED TO REPLACE FLT COMP TRIM AIR VLV. REPLACED FLT COMP TRIM AIR VALVE (P/N 398786-5 - DASH# 350 - POSIT 1). OPS AND LEAK CK OK.

Part: CHARGER — FAULTY (MAIN BATTERY) · airframe 63,240 hrs · 23,314 cycles

MAIN BATTERY CHARGER STATUS MESSAGE WILL NOT CLEAR. BATTERY CHARGER, OP CHECKS OKAY.

Part: SKIN — PUNCTURED (AILERON) · airframe 62,446 hrs · 23,018 cycles

AIRCRAFT ENCOUNTERED MODERATE HAIL STRIKE ON GROUND IN DENVER. RT WING AILERON UPPER SURFACE HAS NUMEROUS PUNCTURES TO COMPOSITE SKIN. WILL CONTINUE TO MAP OUT AND EVAL DAMAGE. RT AILERON NEEDS TO BE REMOVED ACCOUNT OF DAMAGE. REMOVED RT AILERON & REPLACED.

Part: SIGN — OUT OF POSITION (CABIN) · airframe 62,406 hrs · 23,003 cycles

CREW REPORT: RIGHT SIDE OVERWING EXIT SIGN FELL DOWN NEEDS REPAIR. RE-INSTALLED SIGN.

Part: WIRE — LOOSE (TERMINAL BLOCK) · airframe 62,268 hrs · 22,955 cycles

AFTER ENG START NOTICED MESSAGE SAYING LEFT ENG 655 DEGREE OVERTEMP. FOUND SEVERAL CONNECTOR NUTS AT TERMINAL BLOCK APPROX 1 FULL TURN LOOSE. RETORQUED AS AND ACCOMPLISHED RESISTANCE CHECK OF EACH THERMOCOUPLE. ALL CHECKED OK. ALL ENG STARTS NORMAL.

Part: COVER — UNSECURE (EMERGENCY LIGHT) · airframe 61,734 hrs · 22,764 cycles

EMERGENCY STRIP LIGHTING NEAR SEAT 13C TRIP HAZARD. SECURED TRACK COVER.

Part: LIGHT — FAULTY (CABIN) · airframe 61,653 hrs · 22,735 cycles

BEFORE CABIN CREW MOD STARTED, FOUND EMERGENCY LIGHT STRIP IN FRONT OF THE MID LAV AT STATION 740 IS NOT WORKING. REPAIRED EMERGENCY LIGHT STRIP.

Part: CHARGER — FAULTY (APU) · airframe 61,635 hrs · 22,727 cycles

MAIN BATTERY CHARGER STATUS MSG. INOP APU SWAP APU BATTERY CHARGER WITH MAIN BATTERY CHARGER. MR24321 OFF 61 ON 312. REPLACED MAIN BATTERY CHARGER. OP CHECKS GOOD, MESSAGE CLEARED.

Part: WIRE HARNESS — CHAFED (FUEL PANEL) · airframe 61,297 hrs · 22,601 cycles

FUELER REPORTS WIRE BUNDLE CHAFING IN SIDE FUEL PANEL DOOR, FWD SIDE. FOUND WIRE W1500-0068-20 WORN THRU INSULATION. NO STRANDS OF WIRE BROKEN. REPAIRED WIRE PER SWPM. OPS CHECKED GOOD.

Part: GIRT BAR — OBSTRUCTED (L2 DOOR) · airframe 61,179 hrs · 22,555 cycles

CREW REPORTS DOOR 2L IS HARD TO DISARM. FOUND DEBRIS IN GIRT BAR PAWLS, CLEANED CYCLED ARMING LEVER SEVERAL TIMES, OPS CHECKS NORMAL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 60,048 hrs · 22,116 cycles

EMERGENCY LIGHT STRIP INOP AT AFT LAV. RECONNECTED STRIP, OP CHECKS OKAY.

Part: LIGHT — FAULTY (CABIN) · airframe 60,048 hrs · 22,116 cycles

WITH ATTND PANEL SWITCH ON, TRACK MOUNTED EXIT INDICATORS AT 2 (FWD=1, MID FWD=2, MID AFT=3, AFT=4) MAIN CABIN AREA EXTIN. ALL OTHER LIGHTS NORMAL. LIGHT STRIP ON FLOOR BY SEAT 13C INOP. LIGHT STRIP AT 13C IS HALF INOP, LIGHT STRIPS ON BOTH SIDE OF THIS LOCATION AND BOTH SIDES OF EMERGENCY EXIT OK. ORANGE EMERGENCY LIGHT STRIPS OPERATE NORMALLY. REPLACED EMERGENCY LIGHT STRIP PN 36262-4, OP CK OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,747 hrs · 22,009 cycles

STOW BIN EMERGENCY LIGHT INOPERATIVE AT SEAT 6C. RELAMPED.

Part: BULB — OUT OF POSITION (SMOKE DETECTOR) · airframe 59,709 hrs · 21,993 cycles

FWD AFT SMOKE DETECTOR NOT POWERED. BULB APPEARS BE MISSING. ALIGNED BULB WITH CUTOUT, OK.

Part: HOSE — BROKEN (OXYGEN MASK) · airframe 59,707 hrs · 21,992 cycles

OXYGEN MASK HOSE DEFCTIVE AT2(1=CAPT, 2=1ST OF, 3= 1ST OBS). HOSE ON HEADBAND BROKEN. REPLACED MASK ASSY WITH OBSERVERS, OP CKS OK.

Part: SWITCH — LEAKING (RT ENGINE) · airframe 59,661 hrs · 21,978 cycles

FUEL LEAKING FROM RT ENG. REPLACED NR2 ENG FUEL PUMP FILTER DIFFERENTIAL PRESSURE SWITCH.

Part: ROTARY ACTUATOR — MALFUNCTIONED (NR 11 LE SLAT) · airframe 59,315 hrs · 21,851 cycles

L/E SLAT DISAGREE MSG, RTFL. FOUND NR11 L/E ROTARY ACTUATOR OVERLOAD SPRING POPPED. ACTUATOR IS LOOSE AT MOUNTING FLANGE. REPLACED NR 11 L/E ROTARY ACTUATOR. OPS CKS NORMAL. NO MESSAGES NOTED.

Part: COVER — DAMAGED (EMERGENCY LIGHTS) · airframe 58,765 hrs · 21,637 cycles

20C 21C FLOOR PLASTIC COVERED EMERGENCY EXIT LIGHT PAX TRIP INTERIM REPAIR MADE WITH CLEAR TAPE TO SECURE PLASTIC COVER. EMERGENCY LIGHT WORKS NORMAL.

Part: ELECTRONIC UNIT — INTERMITTENT (LE SLAT) · airframe 58,546 hrs · 21,549 cycles

L/E SLAT DISAGREE AND EICAS MSG, RTFL. ACCOMPLISHED FIM BITE PROCEDURE, ALL NORMAL. NR 1 FSEU SHOWED INTERMITTENT NR 1 SLAT, ALL CLEARED. OPERATED FLAPS - SLAT HYD AND ELEC 3 TIMES ALL NORMAL. PER ABOVE MM OK FOR NORMAL SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,925 hrs · 21,303 cycles

EMERGENCY LIGHT STRIP AT MID LAV INOPERATIVE. REPLACED. OPS NORMAL.

Part: LIGHT — LOOSE (CABIN) · airframe 57,407 hrs · 21,102 cycles

FLOOR EMERGENCY LIGHT STRIP AT SEAT 14 RIPPED UP. TRACK & LIGHT STRIP ARE DAMAGED. SECURED EMERGENCY LIGHT AND NEW COVER.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 55,920 hrs · 20,514 cycles

EEL LIGHTS IN FWD SECTION OF COACH ARE INOP. REPLACED POWER PACK M10567. 563-1046 & 563-1188.

Part: INDICATOR — FAULTY (ALTIMETER) · airframe 55,297 hrs · 20,271 cycles

F/O ALTIMETER INDICATION. FLIGHT DIVERTED. ALTIMETER CAME BACK AFTER DESCENT CYCLING CB W SAM DID NOT FIX PROBLEM. FOUND INDICATOR TO BE FAULTING, REPLACED AND TESTED.

Part: SPRING — OUT OF ADJUST (GIRT BAR) · airframe 54,598 hrs · 20,012 cycles

UNABLE TO DISARM DOOR 2L ON ARRIVAL. ADJUSTED LEAF SPRING ON FWD SIDE OF GIRT BAR.

Part: SPRING — OUT OF ADJUST (GIRT BAR) · airframe 54,598 hrs · 20,012 cycles

UNABLE TO DISARM DOOR 2L ON ARRIVAL. ADJUSTED LEAF SPRING ON FWD SIDE OF GIRT BAR.

Part: WIRE — DAMAGED (R2 DOOR) · airframe 54,509 hrs · 19,975 cycles

SLIDE LIGHTS ABOVE ALL CABIN DOORS ARE INOP. REPAIRED WIRE AT DOOR R2. ALL MED'S OPS CHECKS GOOD.

Part: WIRE — DAMAGED (CABIN) · airframe 54,509 hrs · 19,975 cycles

SLIDE LIGHTS ABOVE ALL CABIN DOORS ARE INOP. REPAIRED WIRE AT DOOR R2. ALL MED'S, OPS CHECKS GOOD.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 54,508 hrs · 19,974 cycles

AFT PIT SHEAR TIE BETWEEN S28R AND 27R IS CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED SHEAR TIE AND FABRICATED & INSTALLED A NEW SHEAR TIE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 54,508 hrs · 19,974 cycles

AFT PIT SHEAR TIE BS 1400, BL 0, CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED SHEAR TIE AND FABRICATED A NEW SHEAR TIE.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 54,508 hrs · 19,974 cycles

AFT PIT SKIN DOUBLER BS 1400, LBL 18 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED STRAP SKIN DOUBLER AND FABRICATED & INSTALLED A NEW DOUBLER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 54,508 hrs · 19,974 cycles

AFT PIT SHEAR TIE BS 1400, LBL 18 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED SHEAR TIE. FABRICATED & INSTALLED A NEW SHEAR TIE.

Part: FRAME — DENTED (FUSELAGE) · airframe 54,508 hrs · 19,974 cycles

AFT PIT FRAME DENTED STA 1420, BETWEEN STR 25L AND 24L. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF FRAME AND FABRICATED & INSTALLED A REPAIR J-ANGLE.

Part: FRAME — DENTED (FUSELAGE) · airframe 54,508 hrs · 19,974 cycles

AFT PIT FRAME STA 1580 AT STR 25R IS DENTED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED J-ANGLE DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 54,508 hrs · 19,974 cycles

AFT PIT STA 1600 AT STR 25R IS DENTED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 54,508 hrs · 19,974 cycles

AFT PIT FRAME DENTED STA 1540, BETWEEN STR 25L - 24L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 54,508 hrs · 19,974 cycles

AFT PIT STA 1580 AT STR 25L FRAME IS DENTED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 54,508 hrs · 19,974 cycles

AFT PIT FRAME DENTED STA 1400, BETWEEN STR 25L AND 24L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 54,508 hrs · 19,974 cycles

AFT PIT BS 1520 AT STR 25L, FRAME DENTED AT INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME FLANGE AND REPAIRED FRAME WITH J-SECTION ANGLE.

Part: FRAME — DENTED (FUSELAGE) · airframe 54,508 hrs · 19,974 cycles

AFT PIT FRAME IS DENTED STA 1480 AT STR 24L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF INBOARD FLANGE AND INSTALLED A REPAIR J-ANGLE.

Part: FRAME — DENTED (FUSELAGE) · airframe 54,508 hrs · 19,974 cycles

AFT PIT FRAME IS DENTED STA 1440, BETWEEN STR 25L AND 24L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF INBOARD FLANGE, AND REPAIRED WITH J-ANGLE SECTION.

Part: FRAME — DENTED (FUSELAGE) · airframe 54,508 hrs · 19,974 cycles

AFT PIT FRAME STA 1520 AT STR 25L IS DENTED. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME BY CUTTING OUT DAMAGED SECTION OF FLANGE AND REPAIRING WITH J-ANGLE SECTION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,146 hrs · 19,826 cycles

NR 4 RT MAIN ENTRY DOOR (EXT) EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY LIGHT. OPERATES NORMAL.

Part: STRUCTURE — DAMAGED (NR 6 SLAT) · airframe 53,428 hrs · 19,555 cycles

ON INBOUND RECEIVING INSPECTION, A TEAR WAS FOUND ON THE NR 6 SLAT, RT INBOARD IN THE UPPER INBOARD CORNER OF THE TRAILIING EDGE WEDGE. THE TEAR GOES FROM THE TRAILING EDGE 3.3 INCHES INTO THE WEDGE. THE TEAR GOES COMPLETELY THROUGH THE WEDGE, BOTH FACES AND THE HONEYCOMB. REPLACED NR 6 SLAT. INSPECTED NR 6 SLAT FOR SAFETY AND SECURITY. OPS CHECKS GOOD.

Part: SCAVENGE PUMP — LEAKING (ENGINE) · airframe 53,130 hrs · 19,457 cycles

OIL PRESSURE PROBLEM. FLIGHT DIVERTED. *S/D* LUBE & SCAVENGE PUMP FAILING. CHANGED LUBE & SCAVENGE PUMP-HIGH POWER RUNS ACCOMPLISHED WITH LEAK CHECKS, ALL NORMAL.

Part: FAN — FAILED (LEFT) · airframe 52,217 hrs · 19,118 cycles

EMERGENCY DESCENT DUE TO LEFT PACK FAILURE. FLIGHT DIVERTED. FOUND EQUIPMENT COOLING VALVE STUCK IN OPEN POSITION-FAILING HULL CHECK. REPLACED EQ COOLING VALVE, ALSO REPLACED POSITIVE PRESSURE RELIEF AND OUTFLOW VALVE ACTUATOR AS PRECUATIONARY.

Part: GIRT BAR — OBSTRUCTED · airframe 51,190 hrs · 18,743 cycles

FOUND STATIC LINE OUT OF POCKET INTERFERING WITH GIRT BAR AND DOOR SEAL. FLT ATT STUFFED PAPER TOWELS UNDER SLIDE COVER AND JAMMED SLIDE BUSTLE LOOSE. AFTER REMOVAL OF COVER FOUND DOOR WOULD NOT ARM. FOUND STATIC LINE OUT OF POCKET INTERFERING WITH GIRT BAR AND DOOR SEAL. STOWED STATIC LINE. CLEANED SEAL AND DOOR SILL AREA. PRESSURIZED AIRCRAFT, NO LEAKS FOUND.

Part: STATIC LINE — OUT OF POSITION (R4 DOOR) · airframe 51,190 hrs · 18,743 cycles

FOUND STATIC LINE OUT OF POCKET INTERFERING WITH GIRT BAR AND DOOR SEAL.

Part: CONTROL MODULE — MALFUNCTIONED (SPOILER SYS) · airframe 49,896 hrs · 18,256 cycles

RTFL DUE TO SPOILERS LIGHT ON DURING CLIMB ON EICAS AND OVERHEAD. FOUND A MALFUNCTIONING SPOILER CONTROL MODULE. REPLACED SCM PER UA EG SPECIFICATIONS. SYSTEM CHECKS GOOD. NO LIGHT OR MESSAGE PRESENT.

Part: CHARGER — INOPERATIVE (MAIN BATTERY) · airframe 49,571 hrs · 18,126 cycles

MAIN BATTERY CHARGER WILL NOT ERASE ON ECS MSG. [08-08-07] REPLACED MAIN BATTERY AND MAIN BATTERY CHARGER

Part: HINGE — CRACKED (PAX DOOR) · airframe 49,367 hrs · 18,056 cycles

THE 2R MED PASS DOOR CRACKED AT UPPER HINGE. [08-07-07] MAJOR REPAIR ACCOMPLISHED. REPAIRED 2R MED UPPER HINGE.

Part: SKIN — CRACKED (DOOR) · airframe 49,367 hrs · 18,056 cycles

NR 2 LT MED FWD DOOR FRAME (ON DOOR) UPPER HINGE CUTOUT SKIN IS CRACKED AT CUTOUT LWR RADIUS. [08-07-07] MAJOR REPAIR ACCOMPLISHED PER ENGINEERING SPECIFICATION. CRACK ROUTED OUT AND TREATED BARE EDGE.

Part: SMOKE DETECTOR — FAILED (AFT CARGO) · airframe 49,367 hrs · 18,056 cycles

AFT CARGO SMOKE DETECTOR CHECK FAILS CHECK. [08-07-07] REPLACED NR 1 DETECTOR.

Part: LIGHT — INOPERATIVE (ESCAPE SLIDE) · airframe 38,658 hrs · 14,106 cycles

EXTERIOR EMERGENCY SLIDE LIGHT INOP AT DOOR 4L. REPLACED LAMP NR 767.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,825 hrs · 13,091 cycles

EMERGENCY SLIDE LIGHT OUTSIDE AFT CARGO DOOR INOPERATIVE. RELAMPED.

Part: CREASE BEAM — DAMAGED (FUSELAGE) · airframe 35,372 hrs · 12,923 cycles

MID CABIN BS 612 CREASE BEAM LEFT SIDE, TOOLING DAMAGE ON BOTTOM OF HORIZONTAL FLANGE. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED AREA AND INSTALLED 2 EACH UPPER AND LOWER REPAIR ANGLES.

Part: SKIN — DENTED · airframe 35,372 hrs · 12,436 cycles

DENT LEFT SIDE OF A/C BETWEEN STRINGER 14 & 15 AT STATION 1615. A OVER Y IS 32. DIA 3-64 BY 1.5 INCHES. HFEC ACCOMPLISHED/NO CRACKS NOTED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED DOUBLER AND TRIPLER REPAIR.

Part: PRESSURE PANEL — DAMAGED (CABIN FLOOR) · airframe 35,372 hrs · 12,923 cycles

AFT CABIN PRESSURE DECK WEB, STA 1681 - RBL 50 TO 52, HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. REPAIRED DECK WITH FILLER AND DOUBLER.

Part: PDU — FAILED (L/E SLAT) · airframe 32,733 hrs · 11,973 cycles

LEADING EDGE DISAGREE EICAS MESSAGE AND LIGHT ILLUMINATED. FAILURE OF THE LEADING EDGE SLAT POWER DRIVE UNIT, (PDU), CAUSED THE LEADING EDGE SLAT AND TRAILING EDGE FLAP SYSTEMS TO SHUTDOWN AND PRODUCE THE LEADING EDGE DISAGREE EICAS MESSAGE. REPLACED THE LEADING EDGE SLAT PDU AND OPERATIONALLY CHECKED THE SYSTEM GOOD.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 30,471 hrs · 11,117 cycles

DIVERSION DUE TO AUTOBRAKES DISARMED AND ANTISKID EICAS ILLUMINATED.

Part: UNKNOWN — ODOR (CABIN) · airframe 30,256 hrs · 11,043 cycles

STRONG BURNED RUBBER ODOR ON TAKEOFF ROLL AT 100 KTS. UNABLE TO DUPLICATE ODOR ON GROUND.

Part: WEB — CRACKED (NR 2 PYLON) · airframe 29,672 hrs · 10,836 cycles

NR 2 PYLON WEB IS CRACKED OUT OF THE FORWARD RIGHT HAND CUTOUT, ABOVE THE FORWARD MOUNT, AT THE ONE OCLOCK POSITION. MANUFACTURED AND INSTALLED DOUBLERS. MAJOR REPAIR ACCOMPLISHED.

Part: WEB — CRACKED (NR 1 PYLON) · airframe 29,672 hrs · 10,836 cycles

NR 1 PYLON WEB CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLERS TO THE AFFECTED AREA. MAJOR REPAIR ACCOMPLISHED.

Part: ACTUATOR — FAILED (NLG) · airframe 29,020 hrs · 10,588 cycles

NOSE GEAR FAILED TO EXTEND ON APPROACH. GEAR EXTENDED WITH ALTERNATE SYSTEM. *S/D* REPLACED NOSE GEAR UPLOCK ACTUATOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,203 hrs · 9,950 cycles

EMERGENCY SLIDE LIGHT AT DOOR 2 RIGHT IS INOPERATIVE. *S/D* SLIDE LIGHT WAS RELAMPED.

Part: IDG — FAILED (RIGHT)

RIGHT GENERATOR FAILED. RETURNED TO DEN. *S/D* REPLACED RIGHT INTEGRATED DRIVE GENERATOR (P/N 729825 DASH 770), AIR-OIL HEAT EXCHANGER AND FUEL-OIL COOLER. RIGHT INTEGRATED DRIVE GENERATOR DIFFERENTIAL FAILED DUE TO CONTAMINATION. UNIT WAS CONTAMINATED WITH MINERAL OIL.

Part: PANEL — DAMAGED (NR 1 LE SLAT)

NR 1 SLAT, FIXED LEADING EDGE, AUXILIARY SPAR, AND LOWER ACCESS PANELS DAMAGED. *S/D* AIRCRAFT TOWED INTO SERVICE TRUCK. MAJOR REPAIR NR 090 REPLACED THE NR 1 SLAT (P/N 114N4002-147A), AND REPAIRED DAMAGE TO FIXED LE, AUXILIARY SPAR, AND LOWER ACCESS PANELS PER APPLICABLE SRM SECTIONS.

Part: PSEU — DEFECTIVE (NLG)

RETURNED TO FIELD AT LAX UNDER AMBER ALERT DUE TO A NOSE GEAR INDICATION PROBLEM. *S/D* PSEU WAS GIVING FALSE SIGNALS. NOSE DOWN LOCK SYSTEM 1 AND 2 WAS OUT OF ADJUSTMENT. READJUSTED NOSE DOWN LOCK SYSTEM 1 AND 2.

Part: EXTINGUISHER — LOW PRESSURE (APU)

APU BOTTLE DISCHARGE LIGHT ON. APU INOP. *S/D* APU FIRE EXTINGUISHER WAS FOUND TO HAVE LOW PRESSURE. REPLACED THE APU FIRE EXTINGUISHER AND RELATED SQUIB PER 757MM 26-22-01. PERFORMED OPERATIONAL CHECK AFTER REPLACEMENT PER SAME 757 MM AND FOUND THAT SYSTEM CHECKED OK.

Part: BULB — FAILED (CABIN)

EMERGENCY LIGHT OUTSIDE DOOR NR 2 LEFT INOP. REPLACED LAMP.

Part: BULB — FAILED (CABIN)

EXTERIOR EMERGENCY EGRESS LIGHT AT DOOR 2L INOPERATIVE. RELAMPED EXTERIOR EMERGENCY EGRESS LIGHT AT DOOR 2L. OPERATION CHECKS NORMAL.

Part: EEL — INOPERATIVE (NR 2 DOOR)

DOOR NR 2 EXTERIOR EEL LIGHT INOP. RELAMPED OPS CHECKS OK.