N544UA

Part: DOOR — FROZEN (APU) · airframe 82,785 hrs · 23,696 cycles

APU WILL NOT START. OPENED INLET DOOR MANUALLY VIA MANUAL DRIVE IAW AMM 49-15-06. FOUND ICE & SNOW STUCK IN INLET ACTUATOR AREA. APU INLET DOOR FROZEN ICED SHUT. RAN APU & MELTED COMPARTMENT. CYCLED APU SEVERAL TIMES, OPERATIONS NORMAL.

Part: BLEED AIR SYS — MALFUNCTIONED (APU) · airframe 82,614 hrs · 23,658 cycles

APU SOV INOPERATIVE. APU BLEED STOPPED WORKING NOT SURE OF SOURCE OR BLEED LEAK. PERFORMED APU PERFORMANCE CHECK, NO FAULT FOUND & PERFORMANCE CHECKED NORMAL IAW DIS 245.

Part: WIRE HARNESS — OUT OF POSITION (COCKPIT) · airframe 82,637 hrs · 23,662 cycles

SPEED BRAKE HANDLE COVER REMOVED FOR ACCESS. WIRE BUNDLE SHOWS EVIDENCE OF WEAR & INTERFERING WITH HANDLE OPERATION. FOUND NO WIRE DAMAGE REPOSITIONED WIRE BUNDLE TO CLEAR HANDLE.

Part: BLEED AIR SYS — INOPERATIVE (APU) · airframe 82,614 hrs · 23,658 cycles

APU BLEED STOPPED WORKING NOT SURE OF SOURCE OR BLEED LEAK.

Part: HOUSING — LOOSE (COCKPIT) · airframe 82,492 hrs · 23,632 cycles

CAPTAIN`S OXY MASK HOUSING LOOSE. SECURED CAPTAIN`S OXY MASK HOUSING, OPERATIONS NORMAL.

Part: MECHANISM — STICKING (L2 DOOR) · airframe 82,454 hrs · 23,623 cycles

DOOR 2L WILL NOT ARM, ACCOMPLISHED.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 82,448 hrs · 23,622 cycles

THE FWD CARGO ACCESS CUTOUT LOWER SECTION 2ND BRACKET ASSEMBLY FROM FWD SHOWS EVIDENCE OF CORROSION ADJACENT TO THE UPPER FASTENER. R & R THE SUPPORT FITTING PN 69-45555-12.

Part: TERMINAL — LOOSE (LIGHT SWITCH) · airframe 82,448 hrs · 23,622 cycles

THE EMERGENCY LIGHT SWITCH PN 2100-7 AT THE L1 DOOR SURROUND AREA JUST ABOVE THE FWD UPPER EDGE OF DOOR CUT OUT ON THE LINING WAS FOUND INOPERATIVE. TROUBLESHOT L1 DOOR EMERGENCY LIGHT SWITCH & FOUND ONE TERMINAL LOOSE. SECURED THE LUG & OPERATIONS CHECKED GOOD IAW AMM 33-51-00-7150-002.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,448 hrs · 23,622 cycles

FWD CARGO ACCESS CUTOUT LOWER SECTION 4TH SUPPORT ASSEMBLY FROM CORROSION AT THE FWD MOUNTING BRACKET & AT THE AFT TIEDOWN FITTING. REMOVED CORROSION AT FWD CARGO ACCESS CUT OUT LOWER SECTION 4TH SUPPORT ASSEMBLY FROM FWD & TIEDOWN IAW 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-30-15. R & R NR 4 SUPPORT BRACKET ASSEMBLY & TIEDOWN IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,448 hrs · 23,622 cycles

MAIN DECK FWD WET AREA FLOOR PANEL SUPPORT AT BS 365 RBL 60 HAS CORROSION. FLOOR SUPPORT FABRICATED IAW DRAWING 141N5162 & REPLACED IAW SRM 51-21-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,448 hrs · 23,622 cycles

CABIN FLOOR SUPPORT ANGLE FASTENER HOLE CORROSION STATION 1032 RBL 64. CREASE BEAM PN 144N5152-2 FABRICATED IAW DRAWING 144N5140 & REPLACED IAW SRM 51-40-01 ON AAR NR SN2339282.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,448 hrs · 23,622 cycles

MAIN CABIN CUSP WEB CORROSION AT STATION 940 RBL70. CUSP WEB FABRICATED IAW DRAWING 144N5140 & REPLACED IAW SRM51-40-02 ON AAR NR SN2339268.

Part: LIGHT — DEFECTIVE (COCKPIT) · airframe 82,446 hrs · 23,621 cycles

CAPT & CTR FLUORESCENT TUBES STROBE AT LOW INTENSITIES. RELAMPED & CHECKED OKAY.

Part: IDG — MALFUNCTIONED (RT ENGINE) · airframe 82,300 hrs · 23,582 cycles

RT GEN DP TRIP ON BPCU. REPLACED NR 2 ENG IDG, OPERATIONS CHECKED NORMAL. NO LEAKS, NO FAULTS, BPCU CHECKED OK, CLEAN & RESET IAW AMM24-11-00-501.

Part: SEALANT — MISSING (WINDSHIELD) · airframe 82,295 hrs · 23,580 cycles

INTERMITTENT HISSING ON WINDSHIELD. SOUNDS SIMILAR TO AN INTENSE RAINSTORM. FOUND CAPTAIN`S SLIDING WINDOW PRESSURE SEAL MISSING SEALANT ON OTBD SIDE. APPLIED FILLET SEAL IAW MM 56-11-53.

Part: ENGINE — OIL CONSUMPTION (NR 1) · airframe 82,295 hrs · 23,580 cycles

NR 1 ENG HIGH OIL CONSUMPTION EXCEEDS LIMIT. MAY CONTINUE IN SERVICE IN NON ETOPS WITH RED LIMIT IAW SAMC APPROVAL & MM 79-00-95. ACCOMPLISHED CHECK IAW MM79-00-95 PG 2 NO EXTERNAL LEAKAGE NOTED OR FROM DRAIN TUBES.

Part: MODULE — FAILED (SPOILER) · airframe 82,191 hrs · 23,555 cycles

DURING ETOPS PRE-DEPARTURE CHECK FOUND "SPOILER" STATUS MESSAGE. FOUND FAULT BALL ON CSEU POWER SUPPLY MODULE 1R M538 & FOUND FAULT BALL ON SPOILER CONTROL MODULE 3L. REPLACED BOTH MODULES IAW AMM, OPERATIONS CHECKED GOOD.

Part: FILTER — DIRTY (CABIN) · airframe 81,920 hrs · 23,490 cycles

ACRID ODOR F/D, FLIGHT DIVERTED. REPLACED CABIN RECIRCULATION FILTERS. IAW AMM 21-25-02. REMOVED & REPLACED BOTH LT & RT CABIN FILTERS AS A PRECAUTION IAW AMM. RAN ENGINES & PACKS & NO SIG.

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 80,761 hrs · 23,214 cycles

HYDRAULIC LEAK. FOUND HYD FLUID POURING OUT OF STRUT DRAIN. INSPECTED PLYON AREA, NO LEAKS FOUND. WE DID NOT OPEN SLIPPER COWL ON TOP OF ENGINE, SUSPECT LEAK IN THAT AREA. FOUND PYLON PRESSURE LINE LEAKING REF IPC29-11-61-001, PG1 ITEM K SEC. LINE ACP 5MIN IDLE LEAK CHECK FITTING GOOD. FLUID STILL DRAINING FROM STRUT DRAIN. REMOVED FROM SAME LINE THE UNION AT "J" BOX, PRESSURE LINE. REPLACED BOTH FITTING AND PRESSURE LINE MOTORED ENGINE NO LEAKS NOTED.

Part: BATTERY — FAULTY (MASTER) · airframe 81,720 hrs · 23,443 cycles

MAIN BATTERY CHARGER EICAS MESSAGE WILL NOT CLEAR. REPLACED MAIN BATTERY IAW MM, CHECKS OK.

Part: ANTENNA — FAILED (TCAS) · airframe 81,610 hrs · 23,415 cycles

TCAS FAIL DURING TEST. LOWER ANTENNA FAILED.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 81,532 hrs · 23,400 cycles

NR 1 ENGINE LEAKING HYD FLUID. REPAIRED THRUST REVERSER PRESSURE LINE IAW GPM1-0-13-028.

Part: WARNING LIGHT — MALFUNCTIONED (RECIRC FAN) · airframe 81,359 hrs · 23,365 cycles

RT RECIRCULATION FAN INOPERATIVE LIGHT ILLUMINATED WHEN SWITCH IS ON. CYCLED CIRCUIT BREAKERS, NO HELP.

Part: FAN — INOPERATIVE (RECIRC) · airframe 81,210 hrs · 23,325 cycles

DURING PRESSURIZATION, LT RECIRCULATION FAN INOPERATIVE AND EICAS MESSAGE SHOWED INTERMITTENTLY. REPLACED LT RECIRCULATION FAN IAW MM, OPS AND LEAK CHECKED OK.

Part: REGULATOR — MALFUNCTIONED (NR 2 ENGINE) · airframe 81,160 hrs · 23,314 cycles

DURING CRUISE, LEFT DUCT PRESSURE AT 29PSI, RIGHT DUCT 7PSI. PACK TEMPS STABLE. REPLACED HIGH STAGE VALVE, HIGH STAGE CONTROLLER, AND CHECKED LINES. LESS THAN 5 PSI OUTPUT. NO INCREASE WITH THROTTLES. REPLACED DUAL PRESSURE INDICATOR. REPLACED PRSOV REGULATOR PER AMM. ALSO REPLACED MISSING PACKING ON PRSOV VALVE, FITTING NEAR LOCK OUT FITTING. RAN ENGINE AT IDLE AND INDICATIONS NORMAL.

Part: ALTIMETER — DAMAGED (FIRST OFFICER'S) · airframe 81,115 hrs · 23,303 cycles

FIRST OFFICER`S ALTIMETER MISSING "SPEED BUG". REPLACED MISSING SPEED BUG ON AIRSPEED INDICATOR.

Part: PUMP — LEAKING (NR 1 ENGINE) · airframe 81,094 hrs · 23,298 cycles

NR 1 ENGINE HYD PUMP LEAKING AT THE SEAM. R & R NR 1 HYD PUMP, OPS AND LEAK CHECKED GOOD.

Part: COMPUTER — FAILED (RIGHT) · airframe 81,068 hrs · 23,292 cycles

RT FCC FAILURE, FLT DIVERTED. WHILE AT FL380, RECEIVED A NO LAND 3 INDICATION AND THE F/O LOST HIS FLIGHT DIRECTOR BARS. SHORTLY THEREAFTER STARTED TO RECEIVE AN UNUSUAL ODOR CROSS BETWEEN ELECTRICAL AND ODOR OF SHOE POLISH. CREW STARTED TO RUN CHECK LIST AND ODOR DISSIPATED, WHILE RUNNING LIST F/A'S ADVISED ODOR IN CABIN. REPLACED RT FCC IAW AMM. TESTED IAW AMM 22 00 02 TEST 1 AND TEST 30. ALL TEST PASSED.

Part: FAN — FAULTY (CABIN) · airframe 80,972 hrs · 23,267 cycles

COCKPIT FWD WINDSHIELD ANTI-FOGGING AIR VERY LOUD. NO OBSTRUCTIONS NOTED. NOISE DECREASES WITH RT RECIRC FAN OFF. ACCOMPLISHED SVC TIP MM 21-22-00, OP CK OF NOISE LEVEL OK. REPLACED RT CABIN AIR RECIRCULATION FAN IAW MM, OPS CHECK OK. NOISE WITHIN LIMITS.

Part: MODULE — INOPERATIVE (EDP) · airframe 80,962 hrs · 23,265 cycles

RT HYD SYS PRESSURE LIGHT INOPERATIVE ON OVERHEAD, OK ON EICAS. REPLACED RT EDP SWITCH CIRCUIT MODULE AND MASTER MODULE IAW AMM, OPS CHECKED NORMAL.

Part: STRUCTURE — BROKEN (FUSELAGE) · airframe 80,802 hrs · 23,226 cycles

PLASTIC TRIM AROUND 5 COCKPIT OVERHEAD WARNING LIGHTS IS MISSING OR BROKEN. INSTALLED EMERG DOOR MODULE. CHECKED GOOD.

Part: FIRE LOOP — FAULTY (NR 2 NACELLE) · airframe 80,761 hrs · 23,214 cycles

NR 2 ENGINE HAS A ENG FIRE LP 1 EICAS MESSAGE. LOOP 1 INOPERATIVE. R & R LOWER FWD RT ENGINE DETECTOR-LOOP. CHECKED GOOD.

Part: WIRE — DAMAGED (STICK SHAKER) · airframe 80,572 hrs · 23,167 cycles

WARNING ELEX STATUS MESSAGE WITH IRU'S ALIGNED. REPAIRED WIRES TO RIGHT STALL WARNING STICK SHAKER, AND TESTED OKAY.

Part: UNKNOWN — UNKNOWN (EICAS) · airframe 80,573 hrs · 23,168 cycles

REPLACE LEFT EICAS COMPUTER FOR DF979. REPLACED LEFT EICAS COMPUTER MM, NO HELP. STILL HAS UPPER EICAS CRT LEFT SIDE ERRATIC DISPLAY, OK IN RIGHT POSITION.

Part: SWITCH — FAILED (EFIS DISPLAY) · airframe 80,555 hrs · 23,163 cycles

TOP EFIS DISPLAY INOPERATIVE IN AUTO POSITION, VERIFIED EICAS UPPER DISPLAY INOPERATIVE IN AUTO. REPLACED EICAS DISPLAY SWITCH, RELOAD SOFTWARE OPS AND OPC ON LEFT EICAS PER MM, GROUND OPS CHECKED OK.

Part: FILTER — FAULTY (EQUIPT COOLING) · airframe 80,418 hrs · 23,128 cycles

STATIS MSG KEEPS COMING BACK- EQPT CLG FLOW. EQPT COOLING FILTER. MSG CLEARED.

Part: CAP — MISSING (R2 WINDOW) · airframe 80,355 hrs · 23,110 cycles

HIGH VOLT CAP MISSING COCKPIT WINDOW R2. INSTALLED NEW CAP.

Part: MECHANISM — FAULTY (GIRT BAR) · airframe 80,318 hrs · 23,099 cycles

R4 DOOR SLIDE ARMED LIGHT INOPERATIVE. REPLACED GIRT BAR MECHANISM BEARINGS. ADJUSTED GIRT BAR MECHANISM PER AMM, OPS CHECKED NORMAL.

Part: FILTER — DIRTY (FWD CAB TRIM AIR) · airframe 80,265 hrs · 23,087 cycles

FWD CAB TRIM AIR INOPERATIVE. CLEANED CABIN TEMP SENSOR FILTERS. OPS CHECKED NORMAL.

Part: VALVE — OPEN (POTABLE WATER) · airframe 80,177 hrs · 23,066 cycles

NO POTABLE WATER IN ENTIRE ACFT, FLIGHT DIVERTED. FOUND POTABLE WATER FILL VALVE PARTIALLY OPEN, CYCLED FILL VALVE OPEN AND CLOSED, CHECKED ALL LAVATORIES AND GALLEYS FOR WATER PRESSURE.

Part: GIRT BAR — OUT OF POSITION (R4 DOOR) · airframe 80,059 hrs · 23,031 cycles

SLIDE ARM LIGHTS DOOR 1R 4R INOP. RELAMPED DOOR 1R INDICATOR, OPS CHECKS GOOD. REPOSITIONED GIRT BAR AT DOOR 4R, OPS CHECKS GOOD.

Part: SWITCH — FAULTY (R4 DOOR) · airframe 80,067 hrs · 23,034 cycles

NO SLIDE ARM LIGHT AT 4R WITH DOOR ARMED. CLEANED ARMED SWITCH AND LIGHT, OPS CHECK GOOD.

Part: SENSOR — FAILED (R4 GIRT BAR) · airframe 79,759 hrs · 22,960 cycles

R4 DOOR SLIDE LIGHT DOES NOT ILLUMINATE WHEN ARMED. REPLACED GIRT BAR PROXIMITY SENSORS S10224 AND S10225 IAW WDM 25-66-11 R4 DOOR SLIDE LIGHT CHECKED OK.

Part: CONTACT — DIRTY (DISCHARGE LIGHT) · airframe 79,694 hrs · 22,945 cycles

NR 2 CARGO BOTTLE DISCHARGE LIGHT INOPERATIVE. CLEANED CONTACT, OPS CHECKED GOOD.

Part: BLADE — DAMAGED (NR 1 ENGINE FAN) · airframe 79,516 hrs · 22,897 cycles

NR 1 ENGINE HAS A DAMAGED FAN BLADE. REPAIRED IAW AMM 72-31-02 PAGE 801. INSPECTED AND HFEC PER MM 72-31-02-801. ADDITIONAL .020 BLEND-OUT REQUIRED PER MM 72-31-02-801. C ACCOMPLISHED ADDITIONAL .020 BLEND IAW AMM 72-31-02 PAGE 801.

Part: SLIDER — OUT OF POSITION (GIRT BAR) · airframe 79,456 hrs · 22,879 cycles

DOOR 4R GIRT BAR IS DISLODGED. AFT GIRT BAR SLIDER FOUND COCKED. RE-INSTALLED SLIDER ON GIRT BAR LEAF SPRING. CHECK OPERATION OF GIRT BAR. GIRT BAR & SLIDE LIGHT ARM & DIS-ARMED NORMAL. DOOR OPERATION NORMAL. REMOVED ASSIST BOTTLE PINS & SLIDE PRESSURE BOTTLE SAFETY PIN. CONFIRMED DOOR 4R GIRT BAR SLIDER SPRINGS AND RIVETS IN GOOD CONDITION. SLIDER ENGAGEMENT AND OPERATION GOOD. INDICATION GOOD. CONFIRMED DOOR ASSIST BOTTLE PINS REMOVED, PRESS GOOD. SLIDE BOTTLE PIN REMOVED AND STOWED.

Part: OIL CAP — OUT OF POSITION (APU) · airframe 79,368 hrs · 22,853 cycles

APU FLAMEOUT, FLIGHT DIVERTED. FLAMED OUT WHEN ELECTRIC POWER APPLIED. FOUND APU OIL CAP OFF OIL TANK & OIL QTY AT APPROX 2 QTS. INSPECTED CHIP DETECTOR AND NO METAL NOTED. REMOVED AND REPLACED CHIP DETECTOR AS IT ALSO WAS LEAKING. SERVICED APU OIL QTY TO FULL. APU RAN NORMALLY WITH NO LEAKS NOTED.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 79,232 hrs · 22,816 cycles

RIGHT HYDRAULIC SYSTEM PRESS LIGHT DOES NOT ILLUMINATE WITH PUMPS OFF. REPLACED LIGHT ASSY L3 ON M10050 OVHD AND REPAIRED BROKEN GROUND WIRE ON D3064. LIGHT AND SYSTEM OPS CHECKS GOOD.

Part: MODULE — MALFUNCTIONED (APU) · airframe 79,180 hrs · 22,804 cycles

APU SHUTS DOWN WITH FAULT LIGHT. APU AUTO SHUT DOWN TWICE, NO WORK. REPLACED APU FLOW SENSING MODULE IAW AMM. APU OPS CHECK NORMAL.

Part: CONTROL UNIT — FAULTY (ELECTRICAL SYS) · airframe 79,063 hrs · 22,767 cycles

AFTER BOTH ENGINE START, APPLYING BREAKAWAY POWER, ALL ELEC AND PNEUMATICS DROPPED OFF. ENGS WENT TO IDLE, APU OFF, ATTEMPT TO RESET GEN AND BUSES, NO HELP. ACFT RETURNED TO GATE. REPLACED BPCU ALL ELEC POWER RE-STORED TO AIRCRAFT.

Part: PRESSURE SWITCH — FAULTY (HYDRAULIC SYS) · airframe 78,973 hrs · 22,744 cycles

RT ENGINE DRIVEN HYD PRESS LIGHT EXTINGUISHED WITH ENGINE SHUTDOWN. LOW PRESSURE INDICATION FOR RIGHT ENGINE HYDRAULICS IN DIM MODE. OK IN BRIGHT MODE. REPLACED NR 2 EDP PRESSURE SWITCH.

Part: CONTROL VALVE — FAULTY (APU) · airframe 78,960 hrs · 22,740 cycles

APU SHUTDOWN AT GATE UNABLE TO RESTART. FOUND APU SURGE VALVE SOLENOID DAMAGE. REPLACED APU SURGE VALVE REF MM 49-53-01. BITE CONTROLLER MINIFLAG 9 REMOVED AND REPLACED LOAD COMPRESSOR INLET TEMP SENSOR AS PRECAUTION, APU OPS NORMAL.

Part: TIRE — WORN (MLG) · airframe 78,826 hrs · 22,704 cycles

ON WALKAROUND FOUND NR 3 MAIN TIRE WORN NO TIME LIHMM. REPLACED TIRE PER AMM.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 78,782 hrs · 22,694 cycles

APU FAULT FIRST START. HUNG AT 40PCT. SECOND START OKAY. BIT THE BOX, NO FAULTS OR MESSAGES. STARTED APU TWICE AND START NORMAL. RAN APU FOR AN HOUR WITH A FULL ELECTRICAL LOAD. SHUTDOWN NORMAL. CHECKED CHIP DETECTORS AND DPI'S. NO PROBLEMS FOUND. OIL QUANTITY OKAY.

Part: GIRT BAR — OUT OF ADJUST (R4 DOOR) · airframe 78,712 hrs · 22,678 cycles

DOOR 4 RIGHT WILL NOT ARM. ADJUSTED GIRT BAR SLIDE, OPS OK, ARM LIGHT OK.

Part: REGULATOR — FAULTY (BLEED AIR SYS) · airframe 78,691 hrs · 22,671 cycles

NR 1 ENGINE BLEED FAULTS. LT DUCT PRESS: 45 PSI RIGHT DUCT PRESS: 25 PSI EPR: 1.21 N1: 80% N2: 86% BOTH ENGINES FL390. IN CONSULT WITH TOMC-DEFERRED HPSOV PER THE MEL 3611C. REPLACED HIGH STAGE PILOT PER MM & PRSOV REG PER MM. HIGH POWER RUN OK REF JRH.

Part: VALVE — FAULTY (LT ENGINE) · airframe 78,571 hrs · 22,637 cycles

LEFT ENGINE BLEED LIGHT ILLUMINATED. EICAS MESSAGE ENGINE BLEED VALVE DISPLAYED. LIGHT REMAINS ILLUMINATED AFTER BLEED AIR VALVE CLOSED. SAMC TEXT: FAV 643-9087,FATS 481-0423, FATS PACKING 751-5810. COMPLIED WITH MEL 3611A, PLACARD INSTALLED. REPLACED FAN AIR VALVE, OPS CHECK GOOD.

Part: WARNING SYSTEM — ACTIVATED (BLEED AIR SYS) · airframe 78,565 hrs · 22,636 cycles

LEFT ENGINE BLEED LIGHT ILLUMINATED EICAS MSG ENGINE BLEED VALVE DISPLAYED. LIGHT REMAINS ILLUMINATED AFTER BLEED AIR VALVE CLOSED. FAV 643-9087, FATS 481-0423, FATS PACKING 751-5810. COMPLIED WITH MEL 3611A, PLACARD INSTALLED.

Part: VALVE — FAILED (APU) · airframe 78,333 hrs · 22,572 cycles

APU AUTO SHUTDOWN. TIGHTEN INLET TEMPERATURE SENSOR IAW AMM 49-6103. REPLACED APU SURGE VALVE. OPS CHECK NORMAL, NO LEAKS NOTED. APU START NORMAL. NO AUTO SHUT DOWN NOTED.

Part: BATTERY — FAULTY (APU) · airframe 78,306 hrs · 22,566 cycles

APU AUTO SHUTDOWN. PERFORMED BITE CHECK ON APU CONTROLLER, NO FAULTS NOTED. PERFORMED VISUAL INSPECTION OF APU AND EXHAUST TAIL PIPE, NO DEFECTS NOTED. DURING APU START BATTERY VOLTS DROP TO 15V AND 36 AMPS. REPLACED BATTERY PER AMM. RAN APU THREE TIMES, OPS CHECKED NORMAL.

Part: UNKNOWN — UNKNOWN (CARGO DOOR) · airframe 78,296 hrs · 22,563 cycles

RAMP REPORTED FWD CARGO DOOR UNABLE TO OPEN ELECTRICALLY. FWD CARGO DOOR DOES NOT OPEN ELECTRICALLY. MANUAL OPERATION OK. DOOR CLOSES ELECTRICALLY. REPLACED THE LAMP, CHECKS GOOD. NO FAULTS PER PSEU, REPLACED K10411 AND K10412, NO 28VDC D41136P, PIN 7, 28VDC 41188J PIN7. NEED HARNESS.

Part: CONNECTOR — DAMAGED (LT ENGINE BLEED) · airframe 78,291 hrs · 22,562 cycles

LEFT ENG BLEED OFF, AFTER ENG START. DURING TROUBLESHOOTING REMOVED RELAYS K10645 AND K10453 AND REMOVED CONNECTOR D5138J. MEGGARED X2 OF K10453 TO GROUND AND 130M OHMS. DISCONNECTED CONNECTOR D1098 AT DISC AS1140 (FIREWALL DISC) FOUND PIN AND SOCKET IN POSITION 1 TO BE BURNED OR CORRODED. FOUND 70-130 MEG OHM SHORT AT D1098J, APPEARS TO BE HYD FLUID CONTAMINATION. REPLACED BURNED PINS. OP CHECKED NORMAL ON ENGINE RUNS.

Part: PILOT VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 78,213 hrs · 22,545 cycles

DURING DESCENT LEFT DUCT PRESS CONTINUALLY PULSATES BETWEEN 20-35 PSI. N1 IS 68% STAB AT IDLE. NECESSARY TO LOCK HIGH STG SYSTEM CLOSED TO ISOLATE IF PROBLEM EXIST IN HIGH STG SYS OR PRSOV. LOCKED HIGH STG PER MEL AND ACCOMP HIGH POWER RUN AND NO FLUX NOTED AT ANY POWER SETTING WITH OR WITHOUT USERS. PACKS ON OR OFF. PNEU SYSTEM MARRIED AND STABLE. CHECKS GOOD.

Part: DAU — FAULTY (COCKPIT) · airframe 78,209 hrs · 22,543 cycles

AIRCRAFT IS NOT SENDING ECM DATA. DFDAU NEEDS TO BE REPLACED. REPLACED DFDAU, AND LOADED SOFTWARE.

Part: LAMP — INOPERATIVE (DOOR SLIDE) · airframe 77,930 hrs · 22,470 cycles

R1 AND R2 DOOR SLIDE ARM LIGHTS NOT ON WHEN DOOR ARMED. RELAMPED , CHECKED OKAY.

Part: PRESSURE SWITCH — INOPERATIVE (RT HYD PUMP) · airframe 77,922 hrs · 22,467 cycles

RT HYD PUMP PRESSURE SWITCH NOT FUNCTIONING. REPLACED RT PRESSURE SWITCH, OPS CHECKED GOOD.

Part: SOCKET — DIRTY (R1 DOOR SLIDE) · airframe 77,827 hrs · 22,437 cycles

R1 DOOR ARM LIGHT INTERMITTENT. CLEANED LIGHT ASSY & LIGHT GROUND CHECKED NORMAL.

Part: REGULATOR — FAULTY (POSIT 1) · airframe 77,771 hrs · 22,419 cycles

TROUBLESHOT WIRE RUN FOR LEFT ENG BLEED PRSOV VALVE AND LT INDICATION. CHECK WIRES AT PIN 2 AND 3 AT D5138J FOR SHORTS TO D1098P NO SHORTS FOUND. PIN 2 TO GRD AT D1098J OK. PIN 1 TO GRD AT D1098J NO SHORTS FOUND. RAN LEFT ENG PRSOV VALVE INDICATED OPEN WITH LFT DUCT PRESS AT 18PSI BUT LT REMAIN ON WHICH SHOULD HAVE INDICATED OFF WITH VALVE OPEN. REPLACED PRSOV REGULATOR AND THE HIGH PRESSURE SHUTOFF VALVE PER AMM. LEAK AND OPS CHECKED PER JRH 2-5-16, OPS NORMAL

Part: LIGHT — UNKNOWN (CABIN) · airframe 77,776 hrs · 22,420 cycles

WITH OVERHEAD PANEL SWITCH ON, MULTIPLE EMERGENCY LIGHTS EXTINGUISH . ALL OTHER LIGHTS AND INDICATORS NORMAL.

Part: MODULE — FAULTED (APU FLOW CONTROL) · airframe 77,762 hrs · 22,417 cycles

APU AUTO SHUT DOWN TWICE WITH FAULT LIGHT ON. APU ECU HAD 3 START ABORTED FAULTS, 1 REVERSE FLOW FAULT. CLEAR ECU FAULTS. AIRCRAFT WAS STARTING ENGINES IN A 40 MPH TAIL WIND. PULLED BACK TO GATE. AFTER CLEARING FAULTS APU STARTED NORMALLY. APU INLET DOOR ACTUATOR PULLED AND SAFETIED. DID NOT ACCOMPLISH PARA. B ACFT DOOR OPEN. REPLACED FLOW CONTROL MODULE. NO FAULTS OR SHUTDOWNS NOTED.

Part: ACTUATOR — MALFUNCTIONED (RUDDER TRIM) · airframe 77,753 hrs · 22,415 cycles

RUDDER TRIM INOPERATIVE UNTIL 22000 FT. REPLACED RUDDER TRIM ACTUATOR PER MM, SYSTEM CHECK OKAY.

Part: PILOT VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 77,546 hrs · 22,350 cycles

CREW REPORTED NR 2 HIGH STAGE VALVE OPEN AND HIGH STAGE LIGHT ON AFTER TAKEOFF. FLIGHT 505 RETURNED TO FIELD. TROUBLESHOT PER FIM 36-10-00 FOUND HI STAGE PILOT OVER PRESSURE SENSOR TRIP A 85 PSI SHOULD TRIP 1 125-165PSI, REPLACED HI STAGE PILOT PER MM 36-11-08.

Part: COMPUTER — MALFUNCTIONED (GROUND PROX) · airframe 77,199 hrs · 22,253 cycles

TOO LOW TERRAIN CALLOUT MULTIPLE TIMES CLIMBING THRU 16000 TO 18000. REPLACED EGPWS COMPUTER PER AMM. OPS CHECKED NORMAL.

Part: INDICATOR — INOPERATIVE (FUEL TEMP) · airframe 76,632 hrs · 22,096 cycles

FUEL TEMPERATURE INDICATOR IS INOPERATIVE. SUSPECT BAD TEMP SENSOR.

Part: BLADE — DAMAGED (ENGINE FAN) · airframe 76,533 hrs · 22,067 cycles

NR 2 ENGINE FAN BLADE NR 16 HAS SMALL NICK ON LEADING EDGE OF FAN BLADE AREA 2. NICK MEASURES 0.020 DEEP. NO CRACK OR TEAR VISIBLE. ACCOMPLISHED BLADE REPAIR PER MM. ACCOMPLISHED EDDY CURRENT INSPECTION PER NDT. NO DEFECTS.

Part: BLADE — DAMAGED (NR 2 ENGINE FAN) · airframe 76,544 hrs · 22,070 cycles

NR 2 ENGINE FAN BLADE NR 15 HAS SMALL NICK ON LEADING EDGE OF FAN BLADE AREA 2. EXTENT OF DAMAGE DETERMINED TO BE WITHIN 25 HOUR FLYBACK LIMITS PER AMM. NICK MEASURES 0.020 IN DEPTH. NO TEAR OR CRACK VISIBLE. CARRIED FORWARD PER AMM. ACP'D BLADE REPAIR PER MM. ACCOMPLISHED EDDY CURRENT INSPECTION PER NDT. NO DEFECTS.

Part: PANEL — DAMAGED (ENGINE) · airframe 76,319 hrs · 22,002 cycles

APPEARS TO BE SOME KIND OF DELAMINATION INSIDE BOTH ENGINES AHEAD OF RVS BLOCKER DOORS. BOTH OUTER LOWER FAN EXIT LINER PANEL COATING MISSING BELOW 30 PERCENT OF PANEL, OK PER TOM C ENGINE CONTROLLER AND MM. TO BE REPAIRED NEXT 'A' CHECK. REPAIRED BOTH ENGINES PER MM.

Part: COVER — LOOSE (L2 DOOR) · airframe 80,050 hrs · 23,029 cycles

SLIDE PACK COVER LOOSE DOOR 2L. SECURED BUSTLE.

Part: ENGINE — MAKING METAL (NR 1) · airframe 76,161 hrs · 21,960 cycles

NR 1 ENGINE VIBRATION, RTFL. LEFT ENGINE, SHORTLY AFTER TAKEOFF ALL ENG PARAMETERS DECREASED AND ENGINE SHUTDOWN. RETURNED TO DEPARTURE. ON ARRIVAL AT GATE, NO EXTERNAL LEAKS, MAIN CHIP DETECTOR HAS METAL PARTICLES. REPLACED NR 1 ENGINE.

Part: SPRING — MISSING (LT MLG UPLOCK) · airframe 75,945 hrs · 21,902 cycles

LEFT MAIN LANDING GEAR UPLOCK ASSY MISSING AFT SPRING. REPLACED SPRING PER MM.

Part: INDICATOR — INOPERATIVE (FUEL SYSTEM) · airframe 75,874 hrs · 21,878 cycles

NR 2 FUEL QTY INDICATOR AT FUELING PANEL INOP. F-D IND OK. REPLACED NR 2 FUEL PANEL INDICATOR, OPS CHK'D NORMAL.

Part: SWITCH — FAULTY (ELEVATOR) · airframe 75,714 hrs · 21,837 cycles

ELEVATOR C HYD PRESS STATUS ON SHUTDOWN. CHRONIC SUPPLEMENTAL DATA UPDATE REPLACED S10002 IAW FIM, SYSTEM OPS CKS NORMAL.

Part: PILOT VALVE — MALFUNCTIONED (LT ENGINE) · airframe 75,673 hrs · 21,826 cycles

LEFT ENGINE HIGH STAGE EICAS ILLUMINATED DURING CLIMB, RETURNED TO FIELD, REPLACED LEFT ENG HIGH STAGE PILOT VALVE PER MM. ACCOMPLISHED HIGH POWER PNEU BLEED SHIFT OPS CHECKS. OPS CHECKED GOOD, NO FAULTS NOTED.

Part: SKIN — DAMAGED (BS 1380-1390) · airframe 75,613 hrs · 21,810 cycles

EXTERNAL FUSELAGE SKIN CREASED BETWEEN BS 1380 TO 1400 AND STR 27-28R. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SKIN AND FABRICATED A REPAIR DOUBLER, STRUCTURAL FILLER, AND FILLER AND INSTALLED PER REO G14379, REV. C.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 75,613 hrs · 21,810 cycles

EXTERNAL FUSELAGE SKIN CREASED BETWEEN BS 1380 TO 1400 AND STR 27R-28R. REMOVED DAMAGED SKIN AND FABRICATED A REPAIR DOUBLER, STRUCTURAL FILLER, AND FILLER AND INSTALLED BETWEEN BS 1380 TO 1390 AND AFT CARGO DOOR FORWARD LOWER CORNER OF CUTOUT PER REO G14379, REV C.

Part: ANGLE — CORRODED (BS 1862) · corrosion level 2 · airframe 75,613 hrs · 21,810 cycles

AFT FUSELAGE INTERNAL ABOVE CONSTANT BOX UPPER BULKHEAD, LOWER ANGLE, JUST BELOW APU DUCT IS CORRODED AT BS 1862, AND RBL 17 TO RBL 19. REMOVED BS 1862.7 LATERAL STRUCTURE AND REMOVED CORROSION BETWEEN RBL 10 AND RBL 17 ON UPPER SURFACE OF THE HORIZONTAL FLANGE PER REO G14404, REV. A .

Part: ARM — OUT OF ADJUST (L1 DOOR) · airframe 75,613 hrs · 21,810 cycles

L1 DOOR UPPER FORWARD TORQUE TUBE ROLLER IS HITTING HARD ON THE UPPER FWD LATCH CAM AND NEARLY FALLING OUTSIDE OF CAM, FALSE LATCHING. ADJUSTED GUIDE ARM AND OPS CHECK GOOD.

Part: SLIDE — UNSERVICEABLE (CABIN) · airframe 75,613 hrs · 21,810 cycles

LT OVERWING SLIDE IS UNRAVELED. RMV'D & RPLC'D LT OVERWING SLIDE PER MM ON NON ROUTINE 29126.

Part: NOSE COWL — DENTED (NR 2 ENGINE) · airframe 75,613 hrs · 21,810 cycles

RAMP REPORTED DENT IN NR 2 ENG NOSE COWL 6 O'CLOCK POSITION. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE SKIN PER SRM. FABRICATED REPAIR DOUBLERS AND INSTALLED PER SRM.

Part: NOSE COWL — DENTED (NR 2 ENGINE) · airframe 75,613 hrs · 21,810 cycles

NR 2 ENGINE NOSE COWL HAS A DENT ON LEADING EDGE AT 5:00 POSITION. MAJOR REPAIR ACCOMPLISHED. EVALUATED DENT LIMITS AND FOUND OUT OF LIMITS PER SRM. CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLERS AND INSTALLED PER SRM ON NON ROUTINE 29135.

Part: FUEL/OIL COOLER — LEAKING (NR 1 ENGINE) · airframe 75,358 hrs · 21,733 cycles

NR 1 ENG HIGH OIL CONSUMPTION EXCEEDS LIMIT. REPLACED NR 1 ENGINE FUEL OIL HEAT EXCHANGER PER MM, OPS & LEAK CHECK OKAY.

Part: AMU — FAULTY (ACARS) · airframe 75,358 hrs · 21,733 cycles

ACARS NO COMM. RESET BREAKER, NO HELP. REPLACED ACARS MANAGEMENT UNIT M172 PER AMM, OPS CHECK NORMAL.

Part: GENERATOR — INOPERATIVE (APU) · airframe 75,353 hrs · 21,732 cycles

CREW REPORTS APU GEN INOPERATIVE. REPLACED APU GENERATOR PER MM. ACCOMPLISHED SUCCESSFUL OPERATIONAL CHECK.

Part: SHIELD — OUT OF POSITION (LT MLG) · airframe 75,190 hrs · 21,686 cycles

LT MLG TRUCK BEAM SHIELD FOUND HANGING DOWN. SHIELD REMOVED & PLACED IN LOB. NO DAMAGE TO BEAM. LOWER SURFACE OF THE BEAM MUST BE INSPECTED FOR DAMAGE BEFORE SHIELD IS REPLACED. INSTALLED NEW SHIELD AND HARDWARE.

Part: LIGHT — INOPERATIVE (VHF COMM) · airframe 75,190 hrs · 21,686 cycles

VHF2 BACK LIGHT INOPERATIVE. REPLACED VHF2 PER MM. OPS CHECKED PER MM. NO FAULT NOTED CHECKED OK.

Part: SOFTWARE — OUTDATED (EICAS COMPUTER) · airframe 75,133 hrs · 21,672 cycles

DUE TO SOFTWARE EICAS DISAGREE AFTER LEFT EICAS COMPUTER REPLACEMENT REF CF722, REINSTALLED ORIGINAL LEFT EICAS COMPUTER. LEFT FICAS COMPUTER INOPERATIVE. NEW EICAS COMPUTER SOFTWARE WAS NOT CURRENT. REINSTALLED OLD EICAS COMPUTER.

Part: COMPUTER — FAULTY (LT EICAS) · airframe 75,133 hrs · 21,672 cycles

LOWER EICAS DISPLAY DISTORTED. OPERATION NORMAL ON ALTERNATE COMPUTER. REPLACED LEFT EICAS COMPUTER.

Part: WINDOW — UNSECURE (CABIN) · airframe 74,441 hrs · 21,465 cycles

WINDOW FRAME BETWEEN ROWS 24 & 25F IS LOOSE. SECURED LOOSE WINDOW TRIM.

Part: TRANSCEIVER — FAULTY (HF COMM) · airframe 74,307 hrs · 21,422 cycles

RT HF INOPERATIVE. REPLACED TRNSVR, COUPLER DUE NO TXMT ONLY RCV. PERFORMED OPERATIONAL 5540 FREQ 5X5, NO FAULTS. CHECKS OK ON GRND.

Part: EEC — FAULTY (NR 2 ENGINE) · airframe 74,199 hrs · 21,392 cycles

DUE TO BURNED PINS FOUND ON NR 2 ENG EEC ALTERNATOR STATOR EEC STATOR NEEDS TO BE REPLACED. REPLACED NR 2 ENG EEC STATOR PER MM. STILL NEEDS IDLE LEAK CHECK TEST NR 3. FOUND BURNT PINS AT EEC ALTERNATOR. HARNESS TO CONNECTOR IS BAD, FASTER TO CHANGE ENGINE THAN HARNESS OR TEMP REPAIR TO HARNESS. ENG AVAILABLE.

Part: ENGINE — VIBRATION (NR 2) · airframe 74,149 hrs · 21,374 cycles

DUE TO NR 2 ENGINE VIBRATIONS FELT BY CREW. PRIOR TO HIGH POWER RUN, REPLACED MAIN OIL FILTER, NO DEFECTS FOUND, OIL TANK SERVICED TO FULL.

Part: LANYARD — OUT OF POSITION (R1 DOOR) · airframe 74,006 hrs · 21,338 cycles

F/A REPORTS 1R DOOR WILL NOT ARM. FOUND LANYARD BELOW GIRT BAR. REPOSITONED DOOR AND OP CHECKS OKAY.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 73,971 hrs · 21,327 cycles

EVIDENCE OF HYDRAULIC FLUID ON TAIL SECTION OF AIRCRAFT. AFT FUSELAGE TAIL CONE HAS FLUID SPRAYED (APPEARS TO BE OIL NOT HYD) PREDOMINANTLY ON RIGHT. ACCMP'D CLEANED RESIDUAL OIL. RAN APU, NO ACTIVE LEAKS NOTED. LEAKING LINE ID BY MIDS. P/N BACH8C06EE0274B. LINE FROM BULKED FITTING TO RATIO CHARGER REMOVED LEFT SYS CENTER LINE. ITEM 300 SEAL, ON SHELF WHERE LINE ATTACHES. HELD ON BY TY WRAP AROUND BOOT. PANEL 324CL HAS ONE FASTENER THAT SPINS (NUTPLATE BROKEN). ALL OTHER FASTENERS ON PANEL ARE REMOVED. SECURED FASTNER REINSTALLED PANEL. REPLACED LINE PER IPC. ACCOMPLISHED RUDDER RATIO TEST PER MM AND RUDDER DEFLECTION. LEAK CHECK GOOD. ALL PANELS SECURED. L-C-R HYD RESEVOIRS WERE DEPRESSURIZED & VLV PINNED OPEN FOR RUDDER RATIO CHGR HYD HOSE RPLCMNT. REMOVED PINS. RESV PRESSURIZED.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 73,870 hrs · 21,298 cycles

CORROSION AFT PIT JUST INSIDE OF DOOR LEFT SIDE, AROUND FLOOR FITTINGS. REMOVED CORRODED AREA OF 'Z' ANGLE. REPAIRED WITH SPICED IN NEW SECTION OF 'Z' ANGLE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,870 hrs · 21,298 cycles

NR 2 MED EXT EMERGENCY LIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,870 hrs · 21,298 cycles

NR 2 MED EXT EMERGENCY LIGHT INOP, VOLTAGE AT SOCKET. BATTERY PACK NO HELP. NO VOLTAGE AT SOCKET. REPLACED LIGHT ASSY, CHECKS OK PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,870 hrs · 21,298 cycles

NR 2 MED (LT) EMERGENCY EXIT LIGHT INOP (EXTERIOR). RELAMPED, OPERATES NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,870 hrs · 21,298 cycles

4L DOOR EMERGENCY EXIT LIGHT (EXTERIOR). RELAMPED, OPERATES NORMAL.

Part: FUEL CELL — LEAKING (RT WING) · airframe 73,585 hrs · 21,210 cycles

RIGHT WING DRY BAY DRAIN HOLE 4 LEAKING STEADY STREAM OF FUEL WITH 30K IN CENTER TANK. AIRCRAFT DEFUELED AND CENTER TANK FUEL TRANSFERRED INTO WING TANKS. CENTER TANK IS EMPTY. LEAK OUT DRY BAY DRAIN HOLE NR 4 HAS STOPPED SUSPECT LEAK IS IN WALL OF CENTER TANK. REPAIRED RIGHT HAND DRY BAY FUEL LEAK IAW GNMM.

Part: SEAL — LEAKING (FUEL CELL) · airframe 73,585 hrs · 21,210 cycles

FUEL LEAK. OPENED,VENTED AND GAINED ACCESS TO DRY BAY. REPAIRED RIGHT HAND DRY BAY FUEL LEAK IAW GNMM. LEFT CTR FUEL TANK ACCESS PANEL 531AB HAS A LOOSE SEAL. REPLACED SEAL. FILLED CENTER TANK AND NO LEAKS NOTED FROM 1400 TO 1900.

Part: COMPUTER — FAULTY (LEFT EICAS) · airframe 73,582 hrs · 21,209 cycles

LEFT EICAS COMPUTER FAILED. INOP'D AND PLACARDED PER MEL. REPLACED LT EICAS COMPUTER PER MM. ALSO, REPLACED SWITCHING MODULE M10417 PER MM, OPS CHKS GOOD.

Part: COMPUTER — FAILED (EICAS) · airframe 73,582 hrs · 21,209 cycles

RIGHT EICAS COMPUTER FAILED. CYCLED J29 TO RESTORE AND EICAS RETURNED, FAILED AGAIN MINUTES LATER. REPLACE EICAS COMPUTER. ASSURE EQUIP COOLING AIRFLOW TO COMPUTER AND THAT COOLING METERING PLATES NOT CLOGGED. REPLACED RT EICAS COMPUTER PER MM, OPS CHKS GOOD. ALSO INSPECTED COOLING PLATES NO CLOGS NOTED AIRFLOW IS GOOD.

Part: NUT PLATE — DAMAGED (ELEVATOR) · airframe 73,554 hrs · 21,199 cycles

DAMAGED NUT PLATE ON RT ELEVATOR PCU ACCESS PANEL 345DB FWD OTBD SIDE. ONE NUT PLATE ON BLADE PANEL AFT OF PANEL 345DB. DAMAGED NUT PLATES REPLACED AND PANELS REINSTALLED.

Part: MECHANISM — LACK OF LUBE (R3 DOOR) · airframe 73,524 hrs · 21,186 cycles

DOOR 3R DIFFICULT TO ARM AND DISARM. SUPPLEMENTAL DATA UPDATE REMOVED LINER AND LUBED ARMING MECHANISMS. OPS OKAY.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 73,517 hrs · 21,184 cycles

NR 2 ENG HOC, RTFL. REPLACED ENGINE

Part: LIGHT — UNSECURE (CABIN) · airframe 73,454 hrs · 21,165 cycles

EEL LIGHTS AT ROW 18 REMOVED. SECURED EEL LIGHTS AT ROW 18, TEST OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,445 hrs · 21,161 cycles

AFT LAV EEL STRIP INOP. REPLACED AFT LAV EEL STRIP.

Part: UNKNOWN — FAILED (HMG) · airframe 73,454 hrs · 21,165 cycles

FAILS HMG OPERATIONAL TEST. HMG OPS CHK GOOD PER CORRECTED JOB CARD 5-5010-B.

Part: YAW DAMPER — LEAKING (ELEVATOR) · airframe 73,317 hrs · 21,114 cycles

FLUID DRIPPING FROM ELEV CTRL ACCESS DOOR AND BOTH SIDES OF TAIL CONE. FOUND LEFT YAW DAMPER LEAKING AT 5-10 DROPS PER MINUTE, WITHIN LINE MAXIMUM DISPATCH LIMITS, CARRY FORWARD LEAKAGE LIMITS PERMIT CONTINUED AIRCRAFT OPERATION FOR A MAXIMUM OF 75 FLT HOURS, CONFERRED WITH SFOLM. REPLACED LT YAW DAMPER SERVO, OPS CHECKED GOOD. NO LEAKS NOTED.

Part: COMPUTER — FAULTY (WX RADAR SYS) · airframe 73,168 hrs · 21,073 cycles

WEATHER RADAR SHOWS YELLOW AND RED CELLS AT THE 40MILE. IN AUTO TILT OK IN MANUAL, REPEAT ITEM. WX AUTO TILT FUNCTION CONTROL BY EGPWS PER MM. REPLACED EGPWS COMPUTER PER MM. WX CHECKED OKAY.

Part: FLOW DIVIDER — LEAKING (APU FUEL) · airframe 73,062 hrs · 21,041 cycles

FUEL LEAKING FROM APU DRAIN MAST. FOUND DRAIN FOR FUEL FLOW DIVIDER LEAKING ONLY WHEN APU NOT RUNNING AT 10 DROPS EVERY 14 SECONDS. LIMIT FOR STATIC LEAK ON THIS DRAIN IS 1 DROP PER SECOND. APU OK FOR SERVICE TO NEXT MAINT OP FOR FLOW DIVIDER CHANGE. REPLACED FUEL FLOW DIVIDER VALVE PER MM. OPS CHECK AND LEAK CHECK ACCOMPLISHED.

Part: DRIVE UNIT — MALFUNCTIONED (WX RADAR) · airframe 72,885 hrs · 20,991 cycles

WX RADAR AUTO TILT SHOWS EXCESS GROUND RETURN. INBOUND CREW DESCRIBED WX RADAR DISPLAY AS OK BUT NOT FOLLOWING TRACK OF A-C IN AUTO MODE NOR RESPONDING CORRECTLY IN MANUAL MODE. REPLACED DRIVE UNIT.

Part: CONTROL PANEL — MALFUNCTIONED (WX RADAR) · airframe 72,868 hrs · 20,987 cycles

RECEIVED EXCESSIVE GROUND CLUTTER IN AUTO AND NEEDED 3 UP IN MAN PER INBD CREW RADAR OPS OK IN MANUAL. REPLACED WEATHER RADAR CONTROL PANEL AND OPS CHECKED PER MM, TEST WAS GOOD.

Part: HYDRAULIC SYSTEM — LEAKING (NR 2 DRAIN) · airframe 72,672 hrs · 20,932 cycles

HYD DRIP 7 DROPS PER MINUTE FROM LT PYLON STRUT DRAIN NR 2. OPENED PYLON CAP AND CHECKED FOR LEAKS ALONG LT STRUT DRAIN. NONE NOTED, AREA DRY. FOLLOWED NR 2 STRUT DRAIN TOP TO BOTTOM. NO LEAKS NOTED. EXERCISED LT RVSR. NO LEAKS NOTED. RAN ENGINE FOR 10 MINUTES USING LT EDP TO EXERCISE HYD USERS. NO LEAKS NOTED. CLOSED UP PYLON. RETURNED ACFT TO NORMAL. RECHECKED WITHIN 25 HRS PER MM. OK, NO LEAKS FOUND WITH PUMPS RUNNING, AREA DRY.

Part: FAN — FAULTY (CABIN AIR) · airframe 72,613 hrs · 20,914 cycles

POSSIBLE BALLAST NOISE IN OVHD BAG AREA ROW 21DEF. MADE INOPERATIVE IAW MEL 2161J. VALVE CONFIRMED CLOSED, CB AND COLLARD. FOUND FAN IN AFT CABIN TRIM AIR TEMP SENSOR MAKING RUBBING NOISE.

Part: TRANSCEIVER — FAULTY (WX RADAR SYS) · airframe 72,577 hrs · 20,903 cycles

IN AUTO TILT RADAR PAINTS GROUND AT 40 MILES IN ALL RANGE SETTINGS HALF OF DISPLAY IS GROUND. REPLACED WX TRANSCEIVER IAW AMM. PERFORMED WX RADAR OPS TEST IAW AMM, ALL TESTS PASS.

Part: START VALVE — FAULTY (LT ENGINE) · airframe 72,367 hrs · 20,837 cycles

NR N2 -ROTATION- ON ENG START LT ENG START. NR1 ENGINE STARTED MANUALLY, NO TIME TO TROUBLESHOOT. START VALVE HAS BEEN REPLACED. PLEASE SEE SVC TIP AND FIM TO TROUBLESHOOT. T/S PER FIM, NO FAULTS. CHECKED VOLTAGE TO START VALVE. EXERCISED START SWITCH, ALL OK. REPLACED START VALVE MM. OPS NORMAL.

Part: CIRCUIT CARD — FAULTY (LT A/C PACK TEMP) · airframe 72,352 hrs · 20,832 cycles

EICAS MESSAGE 'L PACK TEMP'. PACK INOP LIGHT ON. LIGHT EXTINGUISHING WHEN STBY SELECTED. OPERATED NORM IN STBY. APPLIED MEL 2151G. REPLACED FLOW CONTROL CARD ASSY, NO HELP. REPLACED LOW LIMIT CONTROL VALVE ON LT PACK.

Part: CONTROL VALVE — MALFUNCTIONED (COCKPIT TEMP) · airframe 72,352 hrs · 20,832 cycles

COCKPIT TEMP UNCONTROLLABLE WITH LT PACK INSTBY. COCKPIT TEMP TOO HOT WITH LT PACK IN STBY NORMAL, TOO COLD WITH STBY COLD. TRIM AIR ON-OFF HAD NO EFFECT. REPLACED TEMP CONTROL VALVE LT PACK. TEMP VALVE ERRATIC ON EICAS. FOUND D2966 PIN 1 IS GROUNDED AND OPEN. REPLACED COMP SENSOR TS41 AND CK WIRING FROM SENSOR TO LT PACK CONTROLLER CHECKS OK . REPLACED PACK LOW LIMIT CONTROL VALVE IAW MM & SENSOR TS5133, ON LT PACK, NO HELP. ALSO TEMP CONTROL VALVE, NO HELP. REPLACED PACK OVHT SWITCH IAW MM, NO HELP. REPLACED STANDBY CONTROLLER, FAILED LAMP TEST. REPLACED STANDBY CONTROLLER AND OP CHECKED GOOD.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 72,317 hrs · 20,823 cycles

RADOME STOVED IN DUE TO BIRDSTRIKE. ACCOMPLISHED BIRDSTRIKE INSPECTION. REPLACED RADOME IAW MM.

Part: START VALVE — FAILED (LT ENGINE) · airframe 72,317 hrs · 20,823 cycles

"LEFT ENGINE STARTER" EICAS MESSAGE. LT ENG START VALVE FAILED TO OPEN. COMPLIED WITH MEL 8000C. DEFERRED. REPLACED START VALVE IAW MM.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 72,248 hrs · 20,798 cycles

STA 1060 RT FRAME T-CHORD DAMAGED. MAJOR REPAIR ACCOMPLISHED: INSTALLED ANGLE REPAIR TO RT WHEEL WELL FAIRING SUPPORT STRUCTURE AT STA 1060 PER SRM.

Part: STRUCTURE — DAMAGED (WNG-BDY FAIRING) · airframe 72,247 hrs · 20,797 cycles

RAMP REPORTED RIGHT WING TO BODY FAIRING PANEL NR 198AR DAMAGE, AFT LOWER CORNER OF PANEL DAMAGE 7" BY 8". PICTURES OF DAMAGE ARE ON RVI SIGHT. FABRICATED HORIZONTAL EXTRUDED CHORD & SENT FOR HEAT TREATMENT. DOUBLER ANGLE REPAIR IAW SRM & GNMM. CHORD ANGLES INSTALLED. INSTALLED NEW FAIRING SUPPORT AND ATTACH CLIPS. REF DWG 149N7553 AND 1497550. REPAIRED DAMAGE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,185 hrs · 20,775 cycles

EMERGENCY LIGHT AT DOOR 2 RT AND 2 LT EXTERIOR SLIDE LIGHTS INOP. REPLACED EMERGENCY LIGHT POWER SUPPLY AT L2 DOOR. OPS CK GOOD IAW AMM.

Part: AUDIO PANEL — FAULTY (NR 1) · airframe 72,153 hrs · 20,764 cycles

CAPTS AUDIO SELECT PANEL NR1 MIC SWITCH INTERMITTENT. ALL ON LIGHTS IN MIKE SELECTOR SWITCHES INOP. BACKGROUND LIGHTING FOR PANEL IS ALSO INOP. REPLACED CAPTAIN'S AUDIO CONTROL PANEL IAW MM. PROBLEM RECURRED. REPLACED CAPTAIN'S AUDIO SELECTOR PANEL IAW MM. LIGHTING OPS CHECKS OK.

Part: IRU — FAULTY (RIGHT) · airframe 72,131 hrs · 20,757 cycles

NO LAND 3 IN ASA AFTER ADIRU ALIGNED. MCDP TEST 30 FAILED "ADC-I RU R" WITH INTERMITTENT NR2 IVSI INOP. FLAG IN VIEW. NEW IVSI AND ADC, NO HELP. NEW IRU CORRECTED PROBLEM. ORIGINAL IVSI AND ADC REINSTALLED--ALL UNITS TEST OK.

Part: LANYARD — OUT OF RIG (R1 GIRT BAR) · airframe 71,545 hrs · 20,589 cycles

WHITE SLIDE INDICATOR LIGHT AT 1R IS INTERMITTENT. TAKES SEVERAL ARMINGS TO GET LIGHT ON. ROUTED LANYARD AT GIRT BAR AND CLEANED AND LUBRICATED SLIDER FITTINGS. VERIFIED SAFETY AND SECURITY OF GIRT BAR AND FITTINGS.

Part: ACTUATOR — FAULTY (RUDDER RATIO) · airframe 71,338 hrs · 20,523 cycles

RUDDER RATIO ISSUES. REPLACED RUDDER RATIO ACTUATOR. OPS NORMAL.

Part: STARTER — FAILED (LT ENGINE) · airframe 71,036 hrs · 20,433 cycles

LT ENGINE NO START SPARKS REPORTED BY GROUND. REPLACED STARTER AND VALVE IAW MM. OPS NORMAL.

Part: VALVE — FAULTY (APU) · airframe 70,917 hrs · 20,394 cycles

INSUFFICIENT APU BLEED PRESSURE TO START ENGINES ONLY 15 PSI. REPLACED APU SHUTOFF VALVE (PN 2790598-101 - SN 146), NO HELP. REPLACED FLOW SENSING MODULE, NO HELP. REPLACED APU SURGE VALVE. APU BLEED PRESSURE NORMAL.

Part: ACTUATOR — FAULTY (LT ENGINE) · airframe 70,631 hrs · 20,311 cycles

SPAR VALVE EICAS AND L SPAR VALVE LT. WHEN ENG WAS FAILING, THE ENG VAL LIGHT WAS FLICKERING. REPLACED LT ENGINE SPAR VALVE ACTUATOR, OPS NORMAL.

Part: GUARD — LOOSE (EMERGENCY LIGHT) · airframe 70,164 hrs · 20,185 cycles

EMERGENCY LIGHT TEST COVER IS LOOSE AT DOOR 2L. SECURED LOOSE EMERGENCY LIGHT SWITCH GUARD AT DOOR 2L.

Part: CHARGER — FAILED (EMERGENCY LIGHT) · airframe 69,847 hrs · 20,096 cycles

SLIDE EMERGENCY LIGHT AT DOOR 2 LEFT DOES NOT ILLUMINATE. REPLACED POWER SUPPLY AND BATTERY PACK AT POSITION M733. WORKS NORMALLY

Part: ELEVATOR — DAMAGED (LH POSITION) · airframe 69,826 hrs · 20,090 cycles

LEFT ELEVATOR LWR SURFACE DAMAGED. PUNCTURE DAMAGE MEASURES .75 X .5" LOCATED 83" FROM INBD EDGE OF ELEVATOR AND 15" AFT OF LEADING EDGE. APPLIED INTERIM REPAIR. TAPE APPLIED TO DAMAGED AREA. MUST HAVE PERMANENT REPAIR WITHIN 300 FLT HRS. PER SHOP, DAMAGE IS TOO CLOSE TO SCREW HOLE, ELEVATOR WILL HAVE TO BE R&R TO SHOP. REPLACED LT ELEVATOR.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 69,816 hrs · 20,088 cycles

HYD FLUID LEAKING FROM NR 2 PYLON DRAIN. FOUND ENG DRIVEN PUMP CASE DRAIN FILTER RETURN LINE FWD FROM MODULE CHAFING ON A PRESS LINE IN PYLON. REPLACED LINE AND LEAK CK OK.

Part: IDG — FAILED (LT GENERATOR) · airframe 69,732 hrs · 20,057 cycles

EICAS MSG L GEN OFF DISPLAYED. GEN OFF LGT ILLUM & FAILED TO RESET. GEN RESET THEN RETRIPPED. RAN CHECKLIST-NO HELP. REPLACED IDG, OPS CK NORMAL.

Part: TRANSMITTER — FAILED (LT ENGINE) · airframe 69,661 hrs · 20,034 cycles

LT ENG OIL LOSS, RTFL. REPLACED ESN AND OIL QUANTITY TRANSMITTER.

Part: ACTUATOR — FAULTY (ELEVATOR) · airframe 69,570 hrs · 20,004 cycles

REMOVED ELEVATOR LT INBD PCU ACTUATOR AND HYD LINES FORE ACTUATOR. REPLACED ELEVATOR LT INBD ACTUATOR. REINSTALLED HYD LINES.

Part: NOSE COWL — DENTED (NR 2 ENGINE) · airframe 69,470 hrs · 19,974 cycles

RAMP REPORTED DENT IN NR 2 ENG NOSE COWL 6 O'CLOCK POSITION. EVALUATED DENT APPROX DIMENSIONS ARE 3.5 IN L X 2 IN W .090 DEPTH BEYOND ALLOWABLE LIMITS. APPEARS TO BE PREVIOUS REPAIR. IAW UA-EVA-73731 PERFORMED EDDY CURRENT (HFEC) INSP. NO DEFECTS NOTED. NO CRACKS FOUND. INSP TO BE REPEATED EVERY A CHECK UNTIL PERMANENT REPAIR IS ACCOMPLISHED BY NEXT C6 CHECK.

Part: ACTUATOR — FAULTY (OUTFLOW VALVE) · airframe 69,378 hrs · 19,951 cycles

CABIN PRESSURIZATION OUTFLOW VALVE WILL NOT CLOSE IN MANUAL MODE. REPLACED FAULTY OUTFLOW VALVE ACTUATOR, OPS CK NORMAL.

Part: PUMP — LEAKING (NR 1 ENGINE) · airframe 69,072 hrs · 19,867 cycles

FOUND NR 1 ENG DRIVEN HYDRAULIC PUMP LEAKING AT MATING SURFACE. PUMP FOUND LEAKING. REPLACED NR 1 ENG DRIVEN HYD PUMP. ACCOMPLISHED CHECK, NO LEAKS NOTED.

Part: CLAMP — WORN (LT WING) · airframe 68,451 hrs · 19,688 cycles

BLOCK CLAMP THAT SUPPORTS 3 HYD TUBES INSIDE LT WING PANEL 511KT IS WORN TO THE POINT THAT THE LOWER 2 TUBES ARE ALMOST TOUCHING. CLAMP FOUND WORN. REPLACED BLOCK CLAMP.

Part: ANTI-ICE VALVE — DEFECTIVE (RT WING) · airframe 67,761 hrs · 19,504 cycles

RIGHT WING ANTI ICE VALVE LIGHT OUT. REPLACED RT WING ANTI-ICE VALVE, LEAK CHECK AND OPS CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (LT ENGINE) · airframe 67,642 hrs · 19,470 cycles

STATUS L ENG PRI. POSSIBLE BAD SVA. SUGGEST CHECK SVA RESISTANCE. EPCS MSG'S P SVA OR FCU-EEC AND S SVC OR FCU-EEC. REPLACED NR 1 ENG SVA ACTUATOR. ACP HIGH POWER RUN. OP CHECK NORMAL.

Part: FCU — FAULTY (LT ENGINE) · airframe 67,642 hrs · 19,471 cycles

L ENG SURGE, RTFL. REPLACED FCU. RAN ENGINE. ALSO RAN TWO TIMES AT 1.39 EPR FOR THREE MINUTES EACH TIME. ALL PARAMETERS STEADY.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 67,466 hrs · 19,422 cycles

NR 1 ENG HYD PUMP LEAKING FROM SPLIT FLANGE. REPLACED PUMP, ONE MOUNT NUT AND PRESSURE FITTING. LEAK CHECKED OKAY.

Part: IMPELLER — OUT OF TOLERANCE (FUEL PUMP) · airframe 67,404 hrs · 19,403 cycles

RT AFT PUMP OUT OF TOLERANCE. PERFORMED RESISTANCE CHECK OF REPLACEMENT PUMP. CHECKS OKAY. REPLACED MOTOR IMPELLER.

Part: HANDLE — OUT OF ALIGNMENT (PAX DOOR) · airframe 66,365 hrs · 19,109 cycles

CREW REPORTS AFT LEFT DOOR WILL NOT ARM PROPERLY. MAINTENANCE FOUND DOOR ARMED WITH HANDLE IN MID POSITION . WILL NOT DISARM OR HANDLE WILL NOT GO TO DOOR CLOSED POSITION. FOUND DOOR OUT OF SEQUENCE INSPECTED EMERGENCY EGRESS SYSTEM NO DEFECTS NOTED. RE-INSTALLED SLIDE AND OP CHECKED DOOR AND SLIDE OPERATION. OPERATION NORMAL AND DOOR INDICATION NORMAL.

Part: CYLINDER — CORRODED (RT MLG) · airframe 66,014 hrs · 19,003 cycles

RT MLG OUTER CYLINDER HAS HEAVY CORROSION AT AND JUST ABOVE GLAND NUT THREADS. GEAR REMOVED FROM ACFT, SEPARATED INNER FROM OUTER CYLINDER, & ROUTED OUTER CYL TO SHOP. OPEN

Part: PROBE — FAULTY (PITOT/STATIC SYS) · airframe 66,008 hrs · 19,000 cycles

F/O PITOT STATIC HEAT INOP. REPLACED RELAYS K310, K103 09 AND K178, NO HELP. PROBE REMOVED FOR REPLACEMENT. F/O'S PITOT PROBE NEEDS TO BE RESEALED DUE TO PROBE REPLACEMENT. SEALED F/O PITOT PROBE. NEED TO PERFORM CHECK OF PROBE TO COMPLETE F/O'S PROBE REPLACEMENT AND INSTALLATION. CHECKS OK BUT, FAILS STEP 15 ONLY, ALL OTHER STEPS OK. F/O PIT OT LIGHT STAYS ON WITH ENGINE RUN SIMULATION. REVIEWED RUN SIMULATION. OP F/O PITOT, OP CHECKS OKAY.

Part: PCU — FAULTY (ELEVATOR TRIM) · airframe 65,987 hrs · 18,992 cycles

ELEVATOR PITCH CONTROL HAS ABOUT ONE HALF INCH PLAY AND ALSO PULSATES WHEN YOU PULL BACK ON THE STICK. SUSPECT ELEV PCA, FOUND THE RT CENTER ELEVATOR PCU AT FAULT. PCU PLANESIDE WORKING REPLACEMENT. BITE TEST REPORTED RT ELEVATOR PCU FAULT MAINTENANCE AND STATUS MESSAGE. TROUBLESHOT FAULT WITH FIM 27-31-00 PG 119. ALSO, PERFORMED BITE 31-41-00. STARTED REMOVAL OF PCU. REPLACED CENTER SYSTEM ACTUATOR. LEAK CK GOOD.

Part: IDG — FAULTY (RT ENGINE) · airframe 65,895 hrs · 18,971 cycles

EICAS MSGS R GEN DRIVE LIGHT DID NOT ILLUM WITH ENG SHUTDOWN. REPLACED IDG. RAN ENG, OPS CHECK OK.

Part: ACTUATOR — FAULTY (DEFUEL VALVE) · airframe 65,079 hrs · 18,741 cycles

RT MAIN TANK TRANSFERRED INTO C TANK. REPLACED RT DEFUEL VALVE ACTUATOR.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 64,396 hrs · 18,565 cycles

INOP OVERWING LT EXIT LIGHT (INTERIOR). REPLACED BALLAST.

Part: VALVE — FAULTY (ENGINE ANTI-ICE) · airframe 64,158 hrs · 18,503 cycles

EICAS MSG ENG ANTI-ICE DISPLAYED AND ENG ANTI-ICE VALVE LIGHT REMAINED ILLUM WITH SWITCH OFF. POSITION 2. CREW COMMENTS: VALVE LIGHT TOOK 30 SEC TO EXTINGUISH. VALVE DID CLOSE. REPLACED NR 2 ENG TAI VALVE.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 63,945 hrs · 18,449 cycles

DOOR 1L SLIDE PRESSURE NEEDLE INDICATES LOW. PRESSURE BELOW DISPATCH LIMITS. REPLACED SLIDE ASSEMBLY.

Part: START VALVE — STICKING (NR 1 ENGINE) · airframe 63,262 hrs · 18,268 cycles

CREW REPORT: LEFT START VALVE FAILED TO OPEN WITH EICAS MESSAGE. START VALVE INOP- SOLENOID CLOGGED, HARDWARE (INTERNAL) DAMAGED. REPLACED START VALVE AND OPS CHECKED OK.

Part: STARTER — FAULTY (NR 1 ENGINE) · airframe 63,085 hrs · 18,225 cycles

COULD NOT START NR 1 ENGINE. RTBL. *S/D* STARTER FAILURE. REPLACED MAIN ENGINE STARTER AND REPLACED STARTER VALVE AND SERVICED MAIN ENGINE STARTER PER. RAN UP ENGINE ALL INDICATIONS NORMAL AND NO LEAKS DETECTED AFTER ENGINE RUN. NO OTHER DEFECTS NOTED.

Part: PANEL — SHORTED (FIRE TEST) · airframe 62,822 hrs · 18,155 cycles

RT ENGINE OVHT LIGHT ON CENTER PEDESTAL INOP DURING FIRE TEST. *S/D* SHORT IN ENG FIRE TEST PANEL. REPLACED ENG FIRE PANEL ON PEDESTAL, GROUND CHECK NORMAL.

Part: SEAL — LEAKING (BYPASS VALVE) · airframe 62,635 hrs · 18,103 cycles

OIL LEAKING FROM LEFT ENGINE. *S/D* NR 5 DRAIN LEAKING, SEALS BAD. REPLACED FUEL OIL HEAT EXCHANGER AND BYPASS VALVE AND SEALS, ENG RUNS ARE DRY.

Part: BLADES — DAMAGED (RT ENGINE) · airframe 62,635 hrs · 18,103 cycles

RIGHT ENGINE, BLADE 10 IS 'TORN' AT END. BADLY DAMAGED. *S/D* UNKNOWN FOD DAMAGE. REPLACED NR 2 ENG 1ST STAGE FAN BLADES 10 AND 28, ACCOMPLISHED ENG RUNS, SATISFACTORY.

Part: LOCK — WORN (GIRT BAR) · airframe 62,535 hrs · 18,073 cycles

DOOR 1R SLIDE LIGHT WILL NOT COME ON. FOUND LOCK ASSY WORN. REPLACED AFT GIRT BAR LOCK ASSY. AND ADJUST RECEIVER, SUSPECT WORN. LOCK, CHECKED SEVERAL TIMES AND LIGHT COMES ON.

Part: PCU — DEFECTIVE (LEFT) · airframe 62,518 hrs · 18,068 cycles

WHILE TROUBLESHOOTING DF053 WITH A RT ELEVATOR PCU MESSAGE, GOT LT PCU MESSAGE ON EICAS. TROUBLESHOT MESSAGE DOWN TO LT ELEVATOR RT PCU BAD. REPLACED PCU, OPS CHECKED GOOD.

Part: HYDRAULIC LINE — BENT (LT WING) · airframe 62,456 hrs · 18,050 cycles

DURING TAXI FLIGHT CONTROL CHECK, WHEN MOVING TO LEFT WING DOWN, APPROX HALF WAY FROM NEUTRAL TO FULL LWD, AN ADDITIONAL 3-4 LBS OF PRESSURE REQUIRED. NEUTRAL TO FULL RWD NO ADDITIONAL PRESSURE IS REQUIRED, PER CREW. BENT HYD LINE HITTING AILERON PUSH ROD. REPLACE LINE OPERATION CHECK. PUSH ROD CLEAR LINE NO LEAKS. AILERON OPS NORMAL.

Part: LAMP — INOPERATIVE (EMEGENCY LIGHTS) · airframe 62,455 hrs · 18,049 cycles

EXTERIOR EMERGENCY LIGHT ON AFT CARGO DOOR INOP. *S/D* LAMP INOP. RELAMPED EXT LIGHT OF AFT CARGO.

Part: FRAME — DENTED (FUSELAGE) · airframe 62,453 hrs · 18,048 cycles

FWD PIT AT STA 520 BETWEEN STR 25L AND 26L FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE. INSTALLED DOUBLER REPAIR.

Part: STRINGER SPLICE — MISMANUFACTURED (RT WING) · airframe 62,453 hrs · 18,048 cycles

RIGHT WING UPPER STRINGER SPLICES 757-3503 -8 AND -10 HAVE SHORT EDGE MARGIN (WINGLET MOD). ACCOMPLISHED MAJOR REPAIR AT GSO-TRIMMED -8 STR SPLICE PER REO-G12358. NDT INSP PER PT 6, 51-00-19. NO DEFECTS NOTED. ROTO PEENED PER REO AND SRM 51-20-13. INSTALLED 757-3503-10 SPLICE PER REO N-R 30599.

Part: FITTING — CRACKED (NR 1 PYLON) · airframe 62,453 hrs · 18,048 cycles

NR 1 PYLON "DELTA" FITTING CRACKED ON OUTBOARD SIDE. ACCOMPLISHED MAJOR REPAIR AT GSO. REPLACED DELTA FITTING PER SRM 51-40-02. LEAK CHECKED ALL LINES PER MM 29-00-98, LEAK CHECKS GOOD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,453 hrs · 18,048 cycles

EXTERNAL FUSELAGE SKIN CORRODED UNDER FWD AIRPHONE ANTENNA LOC BS 1390. ACCOMPLISHED A MAJOR REPAIR AT GSO. REPAIR PER REO G12355 AND EVA 71616. THIS REPAIR HAS RECEIVED ONLY 1ST STAGE APPROVAL PENDING FATIGUE AND DTA EVALUATION BY BOEING TO SHOW COMPLIANCE WITH 14CFR 25.571 AND 26.43D. AIRPLANE MUST BE REMOVED FROM SERVICE ON 28MAY09 UNLESS A NEW 8100-9 IS ISSUED FINDING COMPLIANCE WITH 14CFR 25.571 AND 26.43D.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,453 hrs · 18,048 cycles

CABIN, PREVIOUS REPAIR ON END OF SEAT TRACK BS 377.7 IS CORRODED, APPROX RBL 40. ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED DAMAGE AND FABRICATED REPAIR IAW REO G12351 REV B.

Part: STRUCTURE — CRACKED (L2 DOOR) · airframe 62,453 hrs · 18,048 cycles

L2 DOOR UPPER HINGE ARM CUTOUT HAS A CRACK. ACCOMPLISHED MAJOR REPAIR AT GSO. REPAIRED PER MM 52-11-87 AND SRM 51-40-02.

Part: STRUCTURE — CRACKED (R2 DOOR) · airframe 62,453 hrs · 18,048 cycles

R2 DOOR UPPER HINGE ARM CUTOUT HAS A CRACK. ACCOMPLISHED MAJOR REPAIR AT GSO. REPAIRED FRAME IAW MM 52-11-87 AND SRM 51-40-02.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 62,453 hrs · 18,048 cycles

CABIN RT BETWEEN BS 1420 AND 1440 AT STR 17R CORROSION. ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED AND REPLACED WEB IAW SRM 53-60-13.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,453 hrs · 18,048 cycles

CABIN FLOORBEAM AT STA 377.7, AT LBL 62 IS CORRRODED. ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW 53-00-98 FIG 825.

Part: CREASE BEAM — CORRODED (BS 1000) · airframe 62,453 hrs · 18,048 cycles

MAIN CABIN CREASE BEAM AT STA 1000 LBL 71 IS CORRODED. MAJOR REPAIR ACCOMPLISHED, REMOVED AND REPLACED WEB.

Part: STRUCTURE — CHAFED (R4 DOOR) · airframe 62,453 hrs · 18,048 cycles

DOOR R4 DOUBLER AFT AND BELOW HANDLE BOX CHAFED. MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGE. FABRICATED AND INSTALLED DOUBLER REPAIR.

Part: SEAL — BROKEN (SLIDE RAFT) · airframe 62,453 hrs · 18,048 cycles

AFT FWD LOWER CEILING SLIDE RAFT ELT SEAL IS BROKEN. UNKNOWN DAMAGE. REPLACED ELT.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,453 hrs · 18,048 cycles

CABIN RT BETWEEN STA 1400 AND 1420 AT STR 17R CORROSION. ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED AND REPLACED WEB IAW SRM 53-60-13.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,453 hrs · 18,048 cycles

MAIN CABIN FLOORBEAM STA 324 CORRODED. ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 53-00-98 PG 842 AND SRM 51-40-02.

Part: APU — UNKNOWN · airframe 62,350 hrs · 18,016 cycles

APU FAILED TO START. FAULT LIGHT ILLUMINATED AND EICAS MSG APU FAULT DISPLAYED. APU HAD OVER 6,000 CYCLES AND WAS REPLACED.

Part: CONNECTOR — DAMAGED (ENGINE) · airframe 62,112 hrs · 17,949 cycles

EICAS MSG 'R ENG SEC CONT' DISPLAYED. FOUND CONNECTOR FAILED. REPLACED CONNECTOR AND BACKSHELL.

Part: PCU — LEAKING (RUDDER) · airframe 61,637 hrs · 17,822 cycles

ON PREFLIGHT, FOUND FLUID LEAKING DOWN RIGHT SIDE OF TAILCONE. FOUND INTERNAL HYD FAILURE OF LT RUDDER PCU. REPLACED LT RUDDER PCU.

Part: FAN — BURNED (RT RECIRC) · airframe 61,471 hrs · 17,769 cycles

ELECTRICAL BURNING ODOR IN FRONT HALF OF CABIN DURING PUSHBACK. RT RECIRC FAN BEARING FAILURE. REPLACED FAN.

Part: CONTROL PANEL — SHORTED (FIRE WARNING SYS) · airframe 61,349 hrs · 17,734 cycles

AFT CARGO FIRE SYS SWITCH LT DOES NOT ILLUMINATE DURING TEST. ASSOC EICAS MSG DOES DISPLAY. CARGO FIRE TEST PANEL SHORT. REPLACED CARGO FIRE TEST PANEL. ALL OPS CHECKS ARE GOOD.

Part: SWITCH — FAULTY (FIRE WARNING SYS) · airframe 61,249 hrs · 17,706 cycles

CARGO FIRE (RED AFT) ARM SW LIGHT INOPERATIVE. REPLACED SWITCH ASSY.

Part: OXYGEN BOTTLE — READS HIGH (CABIN) · airframe 60,762 hrs · 1,757 cycles

O2 BOTTLES OVER 15ABC LOW PSI. REPLACED O2 BOTTLE.

Part: WIRE HARNESS — DAMAGED (LEFT IDG) · airframe 59,775 hrs · 17,264 cycles

RTFL DUE TO LEFT GENERATOR DISCONNECTION. ACCOMPLISHED TROUBLESHOOTING OF EICAS MESSAGE DISPLAY AND GENERATOR DRIVE LIGHT ILLUMUNATION. DISCONNECTED GENERATOR DRIVE. REPLACED AND SERVICED IDG. FOUND BACK SIDE WIRE HARNESS ELECTRICAL PLUG FOR LT IDG CAME APART. REPLACED D5132 CONNECTOR FOR LT ENGINE IDG.

Part: SWITCH — FAULTY (APU) · airframe 59,045 hrs · 17,067 cycles

APU WOULD NOT START. STARTED APU BY PULLING THE REMOTE FIRE INDICATION. [08-08-07] REPLACED APU FIRE SHUT DOWN SWITCH.

Part: SIGN — INOPERATIVE (CABIN) · airframe 58,784 hrs · 16,996 cycles

CEILING EMERGENCY EXIT SIGN AT OVERWING DOORS IN INOP. [06-22-07] REPLACED BATTERY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,784 hrs · 16,996 cycles

EMERGENCY EXIT LIGHT AT 25ABC IS INOPERATIVE. REPLACED LAMP.

Part: GIRT BAR — FAULTY (R4 DOOR) · airframe 57,383 hrs · 16,589 cycles

DOOR 4 RIGHT DISARM OPERATION FAILS CHECK WHEN ATTEMPTING TO OPEN FROM OUTSIDE. THE GIRT BAR DOES NOT DISENGAGE. NOTE: CONDITION OCCURS WHEN OPENING SLOWLY IN ARMED POSITION. THE DISCREPANCY WAS TAKEN CARE OF BY CABLE ADJUSTMENT. NO COMPONENT NEEDED TO BE REPLACED.

Part: UNKNOWN — UNKNOWN (CABIN PRESSURE) · airframe 56,024 hrs · 16,215 cycles

LOSS OF CABIN PRESSURE DURING FLIGHT. CABIN PRESSURIZATION PROBLEM DURING FLT, MASKS IN CABIN DID NOT DEPLOY. PERFORMED CONTROLLER BITE TEST, RESET CONTROLLER AND CHECKED ACFT PRESSURIZATION. ALL INDICATIONS NORMAL.

Part: PUMP — MALFUNCTIONED (FUEL SYS) · airframe 54,926 hrs · 15,930 cycles

RETURN TO THE FIELD FOR CYCLING BLEED AND FUEL PUMP. LT ENG SPEED CARD & LT ENG ANALOG N2 STATUS MSG DISPLAYED. REPLACED SPEED CARD, CLEARED MSG, RAN ENGINE NO HELP. EXAMINED CIRCUIT FROM EEC ALT. CON. TO EICAS COMPUTERS AND STBY INDICATOR FOR CONTINUITY AND SHORTS, ALL CHKD NORMAL REPLACED EEC ALT, ACP ENGINE RUN, AND FINALLY OPS CHECKED NORMAL.

Part: GENERATOR — FAILED (APU) · airframe 53,935 hrs · 15,652 cycles

APU ELECTRICAL INOP. AIRCRAFT LOG INDICATED THAT THE APU GENERATOR HAD A BPCU GENERATOR TRIP MESSAGE DUE TO A DIODE FAILURE. THE APU GENERATOR WAS REMOVED AND REPLACED, OPS CHECK OK. SHOP FINDINGS INDICATED THAT THE UNIT HAS BEEN OPERATING FOR TEN YEAR AND HAVE FAILED DUE TO NORMAL WEAR AND DIODE FAILURE.

Part: LIGHT — NO TEST (DOOR 2R SLIDE) · airframe 52,061 hrs · 15,125 cycles

DOOR 2R SLIDE LIGHT NOT ILLUMINATED WITH DOOR ARMED PER CREW. REPLACED.

Part: CABLE — INOPERATIVE (STA 1076) · airframe 51,141 hrs · 14,850 cycles

EMERGENCY PROXIMITY LIGHTS INOPERATIVE. REPLACED CABLE AT STA 1076 AND JUMPER WIRE AT STA 880 TO 902.

Part: WARNING LIGHT — ILLUMINATED (LT GENERATOR) · airframe 50,847 hrs · 14,760 cycles

RETURNED TO FIELD DUE TO THE LEFT GENERATOR DRIVE LIGHT. SHOP FINDINGS INDICATED THAT NO FAULT WAS FOUND. THE IDG OIL PRESSURE SWITCH WAS REPLACED PRECAUTIONARY.

Part: SKIN — DENTED (FUSELAGE) · airframe 45,283 hrs · 13,204 cycles

AFT EXT FUSELAGE SKIN UNDER CARGO PIT DOOR AT STA 1420 STR 28R IS DENTED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 45,283 hrs · 13,204 cycles

FWD FUSELAGE SKIN DENTED AFT OF L2 DOOR. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED DOUBLER, TRIPLER AND FILLER REPAIR.

Part: RELAY — BURNED (AFT PIT P-70) · airframe 44,383 hrs · 12,957 cycles

GROUND CREW REPORTED SMOKE IN AFT PIT. SMOKE FROM DUCTING AND FORWARD WALL AREA. CAUSE APPEARS TO BE A STUCK AFT CARGO HEATER RELAY. STUCK RELAY ALLOWED HEATER TO OVERHEAT TO POINT WHERE SILICONE WRAPPED HEATER RIBBON MELTED, CAUSING SMOKE. MELTING OF RIBBON WIRE CAUSED OPEN CIRCUIT, ALLOWING HEATER TO SHUT DOWN. RELAY K10083 PER WDM 21-44-11. RELAY, HEATER AND FAN REPLACED.

Part: ENGINE — BIRD INGESTION (NR 2) · airframe 41,807 hrs · 12,252 cycles

A/C EXPERIENCED BIRD STRIKE IN THE NR 2 (RIGHT) ENGINE. UPDATE ROOT CAUSE DETERMINED TO BE AN 8-12 LB. CANADAN GOOSE. EWR DOES HAVE A WILDLIFE MITIGATION PROGRAM; HOWEVER, DISCUSSIONS ARE CONTINUING TO IMPROVE THEIR PROGRAM.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,716 hrs · 11,692 cycles

FUSELAGE HAD MULTIPLE DENTS ON EXISTING REPAIR DOUBLER AND ADJACENT TO THE REPAIR DOUBLER BETWEEN STATION 615 AND 645 AND STRINGER 15L TO 19L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND TRIPLER AND FILLERS.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,716 hrs · 11,692 cycles

CENTER AC DISTRIBUTION BAY LWR BILGE LWR FRAME AT STATION 880 AT STRINGER 30 HAS HEAVY CORROSION. MAJOR REPAIR ACCOMPLISHED.REPLACED SHEAR TIES.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,716 hrs · 11,692 cycles

CABIN FLOOR STRUCTURE FLOOR BEAM UPPER T-CAP AT STATION 324 STRINGER 17R 38 RBL TO 63 RBL HAD EXCESSIVE MATERIAL REMOVED IN PROCESS OF CORROSION CLEAN UP. MAJOR REPAIR ACCOMPLISHED. REMOVED SECTION OF T-CAP FROM 9 LBL TO 63 RBL AND INSTALLED REPLACEMENT T-CAP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,716 hrs · 11,692 cycles

CABIN FLOORBEAM AT STATION 365 STRINGER 17R HAD EXCESSIVE MATERIAL REMOVED DURING CORROSION CLEAN UP BETWEEN RBL 10 OUT TO 64 RBL ON THE UPPER T-CAP SURFACE. MAJOR REPAIR ACCOMPLISHED. REPLACEMENT T-CAP INSTALLED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,716 hrs · 11,692 cycles

AFT PIT FRAME HAS CORROSION STATION 1480 RBL 25. MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME CAP STRAP.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 39,716 hrs · 11,692 cycles

CABIN FLOOR STRUCTURE OUTER CREASE BEAM HAD EXCESSIVE CORROSION ON UPPER SURFACE AT STATION 736 RBL 64 STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. REMOVED COMPLETE SECTION OF CREASE BEAM AND INSTALLED NEW SECTION.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 39,716 hrs · 11,692 cycles

CABIN FLOOR STRUCTURE INTERCOSTAL SUPPORT AT STATION 720 TO 740 RBL 62 STRINGER 17R HAD EXCESSIVE CORROSION ON UPPER SURFACE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 39,716 hrs · 11,692 cycles

RIGHT HAND FUSELAGE SKIN AT STATION 532 STRINGER 17R, HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. DOUBLER INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,716 hrs · 11,692 cycles

RIGHT HAND CABIN FLOOR FRAME, STATION 1640, RBL 55, WL 208 HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 39,716 hrs · 11,692 cycles

APU FIREWALL BULKHEAD REPAIR AT STATION 1885 WORN DUE TO CONTACT WITH RIGHT HAND DOOR HOOK. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW DOUBLER.

Part: CIRCUIT BOARD — DEFECTIVE (WARNING SYSTEM) · airframe 32,565 hrs · 9,802 cycles

AT APPROX 130 KT, MASTER WARNING AND CONFIG LIGHTS ILLUMINATED ACCOMPANIED BY FLAPS EICAS MESSAGE. T/O WAS ABORTED. *S/D* SHOP TESTED THE SUBJECT T/O CONFIG WARNING CARD AND FOUND AN INTERMITTENT FAILURE. REPLACED T/O CONFIG WARNING MODULE M620.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 32,565 hrs · 9,802 cycles

AFTER TAKEOFF NOTICED CENTER HYDRAULIC QUANTITY DECREASING. SECURED CENTER HYDRAULIC PUMPS AT .72 QUANTITY. *S/D* REPLACED NR 2 CENTER AC MOTOR PUMP.

Part: SENSE MODULE — MALFUNCTIONED (APU)

APU DUCT PRESSURE LOW AT ENGINE START, APU INOP. *S/D* SURGE CONTROL VALVE REPLACEMENT, DID NOT HELP. REPLACED PNUEMATIC FLOW SENSING MODULE, AND OPERATION OF APU BACK TO NORMAL.

Part: SCAVENGE PUMP — FAILED (APU)

APU AUTO SHUTDOWN IN AIR. DIVERTED TO HNL. *S/D* THE APU MAIN ELECTRICAL HARNESS WAS THE SUSPECT CAUSING THE AUTO SHUTDOWN. UPON CHECKING THE APU IN THE SHOP, THE GENERATOR SCAVENGE PUMP HAD FAILED AND WAS FOUND IN BAD CONDITION. THE PUMP BUSHINGS WERE LOOSE, CAUSING OIL PRESSURE FLUCTUATIONS AND THE OIL LEVEL TO DROP WITH SUBSEQUENT AUTO SHUTDOWNS. THE GENERATOR SCAVENGE PUMP WAS REPLACED, AND THE APU TESTED OK AND WAS RETURNED TO SERVICE.

Part: COMPRESSOR — FAILED (RT ENGINE)

DURING TAKEOFF EXPERIENCED THREE COMPRESSOR STALLS FROM RIGHT ENGINE. AIRCRAFT RETURNED TO FIELD. *S/D* STALLS WERE THE RESULT OF HIGH PRESSURE COMPRESSOR DAMAGE DUE TO A FAILED 9TH STAGE BLADE. ENGINE REPLACED.

Part: SKIN — CRACKED (RT TE FLAP)

RIGHT INBOARD MAIN FLAP, TRAILING EDGE FLAP, HAS A CRACK IN THE SKIN AND SPAR. RIGHT AFT FLAP TRAILING EDGE REMOVED AND REPLACED. ASSEMBLY SENT TO SHOP FOR ANALYSIS AND REPAIR.

Part: EEL CONNECTOR — DIRTY (CABIN)

EEL INOPERATIVE ON ROWS 24ABC TO 32ABC. CLEANED AND DRIED MOISTURE FROM LAMP CONNECTION AT ROW 24. CHECKS OKAY.