N551UA

Part: DOOR SEAL — TORN (CARGO DOOR) · airframe 83,251 hrs · 24,032 cycles

FWD CARGO DOOR PRESSURIZATION SEAL TORN, AT LOWER AFT RADIUS. REPAIRED DOOR SEAL.

Part: REGULATOR — FAULTY (BLEED AIR SYS) · airframe 83,213 hrs · 24,024 cycles

LOW LT ENG DUCT PRESS AT THROTTLE UP, RT DUCT PRESS NORMAL. LT BLEED & LT PACK EICAS MESSAGES. REPLACED BOTH HIGH STAGE PILOT & PRSOV REGULATOR IAW MM 36-11-08, MM 36-11-19 ON LT ENG. RAN ENG BOTH DUCT PRESS NORMAL NO BLEED OFF LIGHT ILLUMINATED. NO EICAS MESSAGE NOTED.

Part: ACTUATOR — LEAKING (LT AILERON) · airframe 83,158 hrs · 24,015 cycles

HYD LEAK LT OTBD WING NEAR AIL. REPLACED LT INBD PCA ACTUATOR.

Part: ACTUATOR — LEAKING (LT AILERON) · airframe 83,158 hrs · 24,015 cycles

FOUND LT AILERON INBD ACTUATOR LEAKING 75 DROPS PER MINUTE AT THE ACTUATOR ROD TO CASE SEAL OR FITTING UPPER HALF. REPLACED LT WING INBD AILERON ACTUATOR.

Part: PROBE — MALFUNCTIONED (PITOT/STATIC SYS) · airframe 83,059 hrs · 23,992 cycles

CREW REPORTS CAPTAIN`S PITOT HEAT LIGHT ILLUMINATED WITH ASSOCIATED EICAS MESSAGE DISPLAYED, WOULD NOT RESET. REPLACED CAPTAIN'S PITOT PROBE IAW AMM 34-11-01 P401. PERFORMED PITOT LEAK TEST IAW AMM 34-11 -01 P501, CHECKED GOOD.

Part: PANEL — DAMAGED (OVERWING EXIT) · airframe 82,841 hrs · 23,940 cycles

LT FWD OVERWING EXIT SURROUND PANEL MISSING 4 INCHES AT LOWER FWD END. REPLACED DAMAGED PANEL.

Part: PANEL — DAMAGED (OVERWING EXIT) · airframe 82,632 hrs · 23,881 cycles

RT FWD OVERWING EXIT SURROUND PANEL MISSING 3 INCHES AT LOWER FWD END.

Part: AUDIO PANEL — FAULTY (COCKPIT) · airframe 82,823 hrs · 23,935 cycles

OXYGEN MASK AUDIO IS WEAK. ROBBED OXYGEN MASK & AUDIO CONTROL PANEL FROM OBSERVER POSITION TO CAPTAIN'S POSITION, FOUND O2 MASK GND GOOD, BUT SWAPPED O2 MASK & AUDIO CONTROL PANEL. PERFORMED OPERATION TEST AMM IAW 35-11-00, 35-11-51 & 23-51-01 FOR AUDIO CONTROL PANEL. GND CHECKED GOOD.

Part: COVER — CRACKED (CABIN) · airframe 82,771 hrs · 23,921 cycles

AFT CABIN 2 FT SECTION OF EMERGENCY EXIT LIGHT COVER CRACKED. REPLACED EMERGENCY EXIT LIGHT COVER IN AFT CABIN.

Part: TRIM PANEL — DAMAGED (CABIN) · airframe 82,632 hrs · 23,881 cycles

RT FWD OVERWING EXIT SURROUND PANEL MISSING 3 INCHES AT LOWER FWD END. IAW ECRA#2500-03171 INTERIM REPAIR IS ACCEPTABLE FOR 4 DAYS AT TERMINATION OF DAYS FLYING 26OCT2013. REPLACE OR REPAIR TRIM PCN 170-1314 OR 170-0962 OUT OF STOCK SYSTEM. NO ROUGH EDGES & TAPE REPAIR WILL NOT AFFECT PASSENGER ERGONOMICS.

Part: COVER — UNSECURE (CABIN) · airframe 82,637 hrs · 23,882 cycles

COVER FELL OF EXIT PATH LIGHTING. SECURED EMERGENCY EXIT LIGHT COVERING.

Part: TRIM PANEL — DAMAGED (CABIN) · airframe 82,632 hrs · 23,881 cycles

LT FWD OVERWING EXIT SURROUND PANEL MISSING 4 INCHES AT LOWER FWD END. IAW ECRA#2500-03171 INTERIM REPAIR IS ACCEPTABLE FOR 4 DAYS AT TERMINATION OF DAYS FLYING 26OCT2013. REPLACE OR REPAIR TRIM PCN 170-1314 OR 170-0962 OUT OF STOCK SYSTEM. NO ROUGH EDGES & TAPE REPAIR WILL NOT AFFECT PASSENGER ERGONOMICS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,632 hrs · 23,881 cycles

EMERGENCY LIGHT AT STOWBIN 38C INOPERATIVE. RELAMPED, OPERATIONS CHECKED GOOD.

Part: LIGHT — INTERMITTENT (HYDRAULIC SYS) · airframe 82,527 hrs · 23,854 cycles

RT CTR ELECTRIC HYD PUMP OVERHEAT LIGHT INTERMITTENT WHEN TESTING. SWAPPED KORRY LENS, NO HELP. CHANGED MEL 2932F COMPLIED WITH MEL REQUIREMENTS. CAP ASSEMBLY PCN IS 563-3679, REPLACED LIGHT BASE, OPERATIONS CHECKED GOOD.

Part: BATTERY — FAULTY (APU) · airframe 82,476 hrs · 23,840 cycles

APU NO START, 2 ATTEMPTS WITH FAULT BOTH TIMES. APU VERY SLOW TO SPOOL, ABORTS AT 19 PERCENT ON 3 TRIES. REPLACED APU BATTERY, WAS READING LOW VOLTAGE 21 BEFORE START & 11 VOLTS DURING START. REPLACED APU BATTERY IAW AMM, CHECKED GOOD. APU STARTS & RUNS NORMALLY.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 82,468 hrs · 23,837 cycles

APU WILL NOT START, HANGS AT 28%. START ABORT MESSAGE. REPLACED APU.

Part: COVER — MISSING (CABIN) · airframe 82,470 hrs · 23,838 cycles

COVER ON EXIT LT MISSING AT DOOR 4R. REPLACED LENS COVER SECURE.

Part: ACTUATOR — MALFUNCTIONED (APU) · airframe 82,456 hrs · 23,832 cycles

APU DOOR FAULT, APU NO START. DOOR WOULD NOT OPEN, MESSAGE ON BOX DOOR ACTUATOR. APU CONSIDERED INOPERATIVE DUE TO DOOR ACTUATOR MESSAGE DEFERRAL. REPLACED APU AIR INTAKE DOOR ACTUATOR IAW MM, OPERATIONS CHECKED NORMAL..

Part: PROXIMITY SWITCH — FAULTY (FUEL SYSTEM) · airframe 82,419 hrs · 23,822 cycles

CENTER FUEL PUMPS NOT TESTING CORRECTLY, NO CENTER LT OR RT FUEL PUMPS LIGHT ON TEST. ADJUSTED FUELING PNL PROX SW.

Part: LIGHT — LOOSE (CABIN) · airframe 82,416 hrs · 23,821 cycles

EMERGENCY EXIT LIGHTS STRIP LOOSE AT ROW 40. RELAMPED EMERGENCY EXIT LIGHT AT ROW 40 IAW AMM.

Part: RELAY — FAILED (FUEL SYSTEM) · airframe 82,377 hrs · 23,813 cycles

RT CENTER TANK FUEL PUMPS AUTOMATIC SHUT OFF SYSTEMS INOPERATIVE. IAW AUTOMATIC SHUT OFF FUNCTIONAL TEST THE RT CENTER FUEL AUTOMATIC FUNCTION SHUT OFF IN 4 SECONDS, THE LIMIT IS 15 PLUS OR MINUS 3 SECONDS. REPLACED RT OVERRIDE PUMP AUTOMATIC SHUT OFF TIME DELAY RELAY K10871 IAW WDM 28-22-11. OPERATIONS CHECKED TO BE ACCOMPLISHED IN SMC3.

Part: COVER — DAMAGED (CABIN) · airframe 82,361 hrs · 23,807 cycles

EMERGENCY EXIT LIGHT TRACK COVER DAMAGED FROM ROW 9 THRU 21. INSTALLED NEW EMERGENCY EXIT LIGHT TRACK COVER, OPERATED EMERGENCY LIGHTS, OPERATIONS NORMAL.

Part: IDG — DISCONNECTED (NR 2 ENGINE) · airframe 82,213 hrs · 23,766 cycles

NO DRIVE LIGHT FOR RT ENGINE DRIVE DISC WITH ENGINE SHUTDOWN. RT IDG DISCONNECTED & INOPERATIVE IAW MEL. R&R NR 2 ENGINE IDG IAW MM.

Part: INTERFACE UNIT — FAULTY (NR 2 ENGINE) · airframe 82,182 hrs · 23,756 cycles

NR 2 ENGINE APPROXIMATELY IDLE RPM HIGH, NR 2 READS 75. REPLACED NR 2 PDIU. ACCOMPLISHED SUCCESSFUL BITE TEST & ENGINE APPLIED IDLE TEST IAW JRH 2-500-2. ALL PARAMETERS NORMAL.

Part: SOLENOID — LEAKING (APU) · airframe 82,151 hrs · 23,748 cycles

APU INOPERATIVE DUE TO OIL LEAK. INSTALLED NEW DE-OILER SOLENOID IAW AMM. NO PACKING AT GEARBOX. NEED PCN 750-1183, NOT AT SANMM. PART IS MARKED FOR NEXT STATION. COMPLIED IAW MEL 4911E. REPLACED WITH NEW SEAL. OPERATIONS & LEAK CHECKED GOOD.

Part: CONNECTOR — DIRTY (RT EEC) · airframe 82,098 hrs · 23,736 cycles

RT ENGINE SEC CONT MESSAGE ON EICAS. CLEANED ELECTRICAL CONNECTIONS ON RT HAND ELECTRONIC ENGINE CONTROL. CREW RAN ENGINES, EICAS MESSAGE CLEARED.

Part: VALVE — STUCK (NR 2 ENGINE) · airframe 82,034 hrs · 23,717 cycles

NR 2 ENGINE FUEL VALVE STUCK OPEN. REPLACED FUEL DISTRIBUTION VALVE PER MM. OPERATIONS & LEAK CHECKED OK. NO WHITE SMOKE AFTER ENGINE RUN UP.

Part: VALVE — STUCK (FUEL SYSTEM) · airframe 82,034 hrs · 23,717 cycles

NR 2 ENGINE FUEL VALVE STUCK OPEN. REPLACED DISTRIBUTION VALVE IAW MM. OPERATIONS & LEAK CHECKED OK. NO WHITE SMOKE AFTER ENGINE RUN UP.

Part: LIGHT — LOOSE (CABIN) · airframe 81,818 hrs · 23,661 cycles

EMERGENCY LIGHT STRIP LOOSE NEAR ROW 40. SECURED EMERGENCY EXIT LIGHT STRIP CONNECTIONS & REPLACED MISSING COVER. TESTED OKAY.

Part: PDIU — MALFUNCTIONED (NR 2 ENGINE) · airframe 81,702 hrs · 23,632 cycles

IDLE DESCENT ENG PARAMETERS SPLIT EPR .84-.86 N1 34-42 EGT 304-323 N2 71-76 FF .7-1.2. HAD S AND P PDIU MESSAGE ON EICAS PDIU GROUND TESTED OK. REPLACED PDIU NR 2. RAN ENGINE, CHECKED OK.

Part: LANYARD — UNSECURE (RT DOOR SLIDE) · airframe 81,668 hrs · 23,623 cycles

RIGHT SERVICE DOOR FWD EVAC SLIDE ARM LEVER DIFFICULT TO POSITION. FOUND THAT LANYARD CAME OUT OF GIRT UNDER GIRT BAR. SECURED LANYARD, OPS CHECKED NORMAL.

Part: LANYARD — OBSTRUCTED (R1 GIRT BAR) · airframe 81,662 hrs · 23,621 cycles

DOOR LIGHT AT 1R DOES NOT COME ON OR SHOW ARMED. FOUND THAT THE LANYARD ON GIRT WAS SNAGGING GIRT LATCHING MECHANISM. SECURED LANYARD PROPERLY OPERATIONALLY CHECKED FUNCTION OF THE ARMING MECHANISM AND INDICATION LIGHT. ALL FOUND TO BE WORKING NORMALLY.

Part: PRESSURE SWITCH — INOPERATIVE (HYD SYSTEM) · airframe 81,321 hrs · 23,538 cycles

LEFT HYD SYS PRESSURE LIGHT SHOULD BE ON, BUT ISN`T. LIGHT TESTED OK. FOUND LT HYD SYSTEM PRESSURE SWITCH FAILED. R & R PRESSURE SWITCH LEAK AND OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,261 hrs · 23,521 cycles

EMERGENCY LIGHTS NOT SECURED AT LAST ROW OF SEATS ABEAM AFT LAVATORY. EMERGENCY LIGHT AT 40C INOPERATIVE, ONLY LAST SECTION INOPERATIVE, ABOUT 10 INCHES. LIGHT DISCONNECTED AT 40C AISLE FLOOR, ENTIRE ACFT NORMAL.

Part: GCU — FAULTY (APU GENERATOR) · airframe 81,169 hrs · 23,499 cycles

UNABLE TO GET ELECTRICAL POWER ON LINE APU GEN. REPLACED GENERATOR CONTROL UNIT AS PRECAUTIONARY FOR LOG 2. REPLACED BPCU AS PRECAUTIONARY FOR LOG 2.

Part: GENERATOR — FAULTY (APU) · airframe 81,169 hrs · 23,499 cycles

APU WILL NOT PICK UP EMECTRIC. REPLACED GENERATOR APU IAW AMM. R & R IAW MM 24-21-01-040.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 81,150 hrs · 23,496 cycles

EMERGENCY LIGHT BY 40C LOOSE. REPLACED EMERGENCY LIGHT COVER. OPS CHECKED OK.

Part: CONNECTOR — DIRTY (HYD SYSTEM) · airframe 81,150 hrs · 23,496 cycles

LEFT ENGINE HYD PUMP LOW PRESSURE LIGHT INOPERATIVE. CLEANED CONNECTOR. OPS CHECKED OK.

Part: WIRE — BROKEN (SOCKET) · airframe 81,083 hrs · 23,483 cycles

APU BLEED INOPERATIVE. VERIFIED BLEED VALVE CLOSED. APU ELECT OK. COULD NOT GET APU VALVE TO OPEN WITH SWITCH. NO VALVE LIGHT NO EICAS MESSAGE CHANGED RELAYS K23, K24, K25, K10201 AND K10280, NO HELP. REPLACED APU BLD VALVE. NO HELP. TRIED NEW APU CONTROLLER, ALSO NO HELP. REINSTALL PREVIOUS CONTROLLER. SUSPECT BAD APU BLD SWITCH. SWAPPED OUT BLEED PANEL IN COCKPIT WITH PANEL FROM ANOTHER ACFT TO CONFIRM SWITCH IS GOOD, NO HELP. CHECKED GROUNDS FROM VALVE CONNECTOR, CHECK GOOD. UNABLE TO GET POWER TO VALVE PIN. REPAIRED BROKEN WIRE AT SOCKET POSITION 55 OF D40570J. APU BLEED VALVE, OPS CK OK.

Part: EEC — FAILED (NR 1 ENGINE) · airframe 80,555 hrs · 23,328 cycles

LEFT ENG FAILURE ON TAXI IN. MAINT TEXT: DEBRIEFED CREW, AFTER ROLL OUT ON TO TAXI WAY UPPER EICAS FAILURE MSGS RELATED TO NR 1 ENGINE ROTATION DECREASING AND EGT RISING RAPIDLY, CAPT SHUT DOWN ENGINE. BOTH S SVA OR FCU-EEC AND P SVC OR FCU-EEC MESSAGES ON EPCS PAGE. REF SEQ NUMBERS 5552008, 5552007 FOR REPLACEMENT OF NR 1 FUEL PUMP AND FUEL CONTROL UNIT. R&R NR 1 ENG EEC REF UAL AMM 73-21-04. OPS CHECK GOOD, REF AMM 71-00-59.

Part: CONNECTOR — LOOSE (FCU) · airframe 80,552 hrs · 23,327 cycles

EICAS STATUS; LEFT ENG PRI CONT FOUND FWD CONNECTOR LOOSE, CHECK MESSAGES PER FIM 73-21-00 PG 131 FOR EPSC MESSAGES NONE NOTED, IDLE RAN ENG NR 1 NO FAULTS NOTED, RAN ENG AT HIGH POWER NO FAULTS, ACCOMPLISHED ACCELERATION TIME TEST PER JRH2-5-64. ALL PASSED AND WITHIN LIMITS AND NO FAULTS NOTED. THE CONNECTOR LOOSE ON FCU.

Part: SUPPORT BRACKET — DETACHED (CABIN) · airframe 80,548 hrs · 23,326 cycles

SEAT 40D LIFE VEST POUCH SUPPORT BRACKET IS DETACHED FROM THE SEAT. SECURED BRACKET.

Part: LIGHT — UNKNOWN (CABIN) · airframe 80,536 hrs · 23,323 cycles

EMERGENCY LIGHTS INOPERATIVE FROM SEAT ROWS 20 TO 27 AND 37 TO 40. TESTED LIGHTS USING FIM 33-51-00 PG 107 AND AMM 33-51-00. ALL LIGHTS WORK NORMAL.

Part: UNKNOWN — UNKNOWN (GENERATOR) · airframe 80,493 hrs · 23,309 cycles

EICAS MESSAGES, RIGHT GENERATOR DRIVE LIGHT DID NOT ILLUMINATE WITH ENGINE SHUTDOWN. OPERATED DISCONNECT PROCEDURE AND RECONNECTED GENERATOR SYSTEM, ALL BACK TO NORMAL.

Part: SEAL — LEAKING (NR 2 ENGINE) · airframe 80,477 hrs · 23,305 cycles

NR 2 ENG OIL CONSUMPTION CONTINUES TO INCREASE THE DEOILER ROTATING RING AND SEALS HAVE BEEN REPLACED. NOW CHECK FOR OIL LEAKS PER MM 79-00-95 PG 201 AND MM71-05-00 FIG 109. IF NO LEAKS FOUND ON VISUAL CHECKS RUN ENG AT 80% N1 FOR MINIMUM OF 10 MINUTES WITH BAGS ON DRAIN. IF UNABLE TO RUN, PERFORM STATIC LEAK CHECKS PER MM 71-08-00 FIG 102. FOUND EDP DRIVE SEAL LEAKING. REPLACED PER MM 72-61-02 PG 401 AND MM 29-11-05.

Part: BLADE — NICKED (NR 1 ENGINE) · airframe 80,477 hrs · 23,305 cycles

SEVERAL BLADES IN INLET OF NR 1 ENGINE HAVE NICKS IN THEM. BLENDED BLADES PER 72-31- 02. PERFORMED HFEC INSPECTION OF BLADES REF NDT MANUAL PT 6 72-31-401, NO CRACK INDICATIONS.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 80,474 hrs · 23,304 cycles

EMERGENCY FLOOR LIGHTING LOOSE ROW 40. REPLACED DAMAGED EMERGENCY LIGHT TRACK COVER AND EMERGENCY LIGHT ILLUMINATION, TESTED GOOD.

Part: LIGHT — UNSECURE (ROW 40C) · airframe 80,470 hrs · 23,303 cycles

EMERGENCY LIGHT BY 40C IS COMING APART. SECURED EMERGENCY LIGHT, LIGHT OPS NORMAL.

Part: BLADE — DAMAGED (NR 2 LPT) · airframe 80,432 hrs · 23,291 cycles

NR 2 ENGINE LPT FAN BLADE HAS A NICK APPROXIMATELY 4 INCHES FROM LEADING EDGE BLADE TIP. ACCOMPLISHED EDDY CURRENT IAW NDTM 72-31-401, NO CRACKS DETECTED.

Part: UNKNOWN — UNKNOWN (TRIM SYSTEM) · airframe 80,402 hrs · 23,279 cycles

AIRCRAFT HAS POOR TRIM QUALITIES. 0 RUDDER TRIM WINGS LEVEL EVEN POWER LEVEL FUEL REQ OVER 1 RIGHT AILERON TRIM. THE ELEVATOR POSITION SHOWS RT ELEVATOR LOWER THAN LEFT. POOR TRIM WITH AND WITHOUT AUTO-PILOT, PER CREW. CHECKED ELEVATOR POSITION FOR BEING SPLIT, ON SPLIT FOUND. NO FAULTS FOUND ON PCU(S). CHECKED EACH HYD SYSTEM, NO FAULTS FOUND. MM 27-20-00 PAGE 902,3A.

Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 80,386 hrs · 23,272 cycles

RIGHT HYDRAULIC SYS INDICATES 3200PSI. NORMAL IS 3000. REMOVED AND REPLACED RIGHT ELECTRIC HYDRAULIC PUMP IAW MM. OPS AND LEAK CHECKED GOOD.

Part: ACTUATOR — FAULTY (ELEVATOR) · airframe 80,244 hrs · 23,229 cycles

STATUS MSG ELEV ASYM T-S PER FIM 27-09-00 FIG 106. REMOVED AND REPLACED ASYMMETRY LIMITER ACTUATOR IAW AMM, OPS CHECK GOOD. P/N 1846T100-3 SN 872 TT 1499375.

Part: ADC — FAULTY (NR 2) · airframe 80,239 hrs · 23,227 cycles

F/O ELEC ALTIMETER WRONG. SELECT ALTN STATIC FIXES PROB SEE LOG BOOK FOR READINGS. CREW COMMENTS: F/O ALTM 80 FT HIGHER THAN CAPTS. CORRECTS USING ALTN AIR DATA. REPLACED RIGHT AIR DATA COMPUTER REF AMM. ACCOMPLISHED SELF TEST AND MCDP TEST 30, ALL NORMAL.

Part: WIRE — SHORTED (FUEL SYSTEM) · airframe 80,059 hrs · 23,177 cycles

NR 2 SPAR VALVE LIGHT REMAINS LIT AT ALL TIMES. ENGINE DOES NOT START, NO FUEL FLOW. NO POWER ON ONE SIDE OF ENGINE 2 SPAR VALVE CB ON P6-1 PANEL. AFTER CHANGING CIRCUIT BREAKER WILL NOT STAY IN. SUSPECT VALVE IS ALSO BAD. HUNG NEW SPAR VALVE ACTUATOR, SPARE VALVE CB TRIPS, ALSO TRIPS WITH CONNECTOR REMOVED FROM ACTUATOR. NR 2 ENGINE FUEL CONTROL SW. SELECTED TO RUN, CB STAYED IN, & SPA. CONNECTOR D42342J DISCONNECTED CB STAYS IN. FOUND CONTINUITY TO GRD ON PIN 6 OF CONNECTOR D2022 WITH CONNECTOR D42342J DISCONNECTED. FOUND WIRE W3484-1007-18 SHORTED TO GROUND AT OLD SPLICE REPAIR. CUT OUT DAMAGED WIRE & SPLICED IN NEW WIRE.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 80,059 hrs · 23,177 cycles

BACKGROUND LIGHT INOPERATIVE FOR MASTER CONTROL PANEL. REPLACED AFCS MODE CONTROL PANEL. OPS CHECKED GOOD.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 79,968 hrs · 23,153 cycles

EMERGENCY LIGHT AFT CABIN MISSING END CAP AND DAMAGED. REPLACED END CAP AND SECURED EMERGENCY LIGHT.

Part: DISPLAY — FAULTED (EICAS) · airframe 79,904 hrs · 23,132 cycles

TOP CRT BLURRY. REMOVED AND REPLACED UPPER EICAS DISPLAY - RAN EICAS BITE TEST, CHECKED OKAY.

Part: MODULE — FAULTY (CONTROL PANEL) · airframe 79,556 hrs · 23,044 cycles

RIGHT FLT CONTROL CUTOFF WONT STAY IN. REPLACED RIGHT FLIGHT CONTROL SWITCH MODULE ON P-61 PNL. SWITCH OP'S CHECK GOOD.

Part: FLUID — LEAKING (NR 2 ENGINE) · airframe 79,295 hrs · 22,974 cycles

RAMP REPORTED NR 2 ENGINE HAS OIL LEAKING OUT BOTTOM OF COWLING. CLEANED OFF EXCESSIVE OIL GRD RAN ENGINE FOR 5 MIN IDLE RUN. NO ACTIVE LEAKS NOTED, OK FOR SERVICE.

Part: RELAY — FAULTY (FUEL SYSTEM) · airframe 79,270 hrs · 22,966 cycles

CTR R FUEL PUMP EICAS WILL NOT DISPLAY FOR GROUND CHECK PER AFM. REPLACED K10871, RIGHT OVERRIDE PUMP SO TIME DELAY RELAY. SYSTEM OPS CHECKED OKAY.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 79,156 hrs · 22,936 cycles

APU BOTTLE DISCHARGE LIGHT INOPERATIVE. REPLACED LIGHT ASSY, OP CHECKED GOOD.

Part: WIRE — BROKEN (LIGHT) · airframe 79,104 hrs · 22,920 cycles

P6 PANEL CIRCUIT BREAKER LIGHT WIRE IS BROKEN. INSTALLED END CAP ON BROKEN WIRE AND SECURED. AREA LIGHT BENEATH P61 INOPERATIVE.

Part: TRANSCEIVER — FAILED (WX RADAR SYS) · airframe 79,099 hrs · 22,919 cycles

WEATHER RADAR TILT INOPERATIVE. ONLY SHOWING GROUND RETURNS ON BOTTOM LEFT OF SCREEN. REPLACED R/T PER MM 34-43-01. OPS CHECK GOOD TILT WORKS.

Part: SPEAKER — DEFECTIVE (COCKPIT) · airframe 79,033 hrs · 22,900 cycles

FIRST OFFICERS OXYGEN MASK MICROPHONE WILL NOT TRANSMIT TO FIRST OFFICER SPEAKER. SWAPPED ASP WITH 1ST OBS NO HELP. REPLACED F/O'S OXYGEN MASK, NO HELP. REPLACED AUDIO ACCESS UNIT, NO HELP. TROUBLESHOT DOWN TO BAD F/O'S SPEAKER. BOX FOR F/O'S OXYGEN MASK WAS ALSO REPLACED, NO HELP. NOT MR UNIT. ADJUSTED, SYSTEM CKS NORMAL.

Part: MONITOR — ACTIVATED (HYDRAULIC SYS) · airframe 78,978 hrs · 22,887 cycles

RIGHT HYDRAULIC SYSTEM 'RSVR' LIGHT INOPERATIVE. NEED MORE TROUBLESHOOTING. INF- :383-23 CRW REPORT NORMAL OPS OF HYD SYSTEM PRESS INDICATION, AND AFTER ENGINE START THE RTT HYD RSVR PRESS EICAS MSG WAS NOT DISPLAYED. THIS ITEM CREATED AS PART OF DF695. REPLACED MONITOR UNIT SEQ# 9782007.

Part: CONTROL VALVE — FAULTY (LT ENGINE) · airframe 78,952 hrs · 22,882 cycles

LEFT ENGINE STARTER EICAS ON DURING LEFT ENGINE START ATTEMPT. START VALVE ONLY OPENS PARTIALLY, ACP'D MANUAL START PER MEL. PARTS: 643-5284 MR80126 (VALVE) RPL START CONTROL VALVE PER AMM AND DRY MOTOR JRH 2-5-9. OP CHK GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 78,741 hrs · 22,821 cycles

TWO SMALL DENTS BELOW FWD CARGO DOOR SILL AREA IS 1 INCH BY 1 INCH PER BOTH AT .075 DEPTH. A-Y DIMENSION = 14. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR DOUBLER PER ECRA 5330-04331.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,741 hrs · 22,821 cycles

SKIN DENTS CLOSE TO DOUBLER AT STA 580 AND STR 29R. MAJOR REPAIR ACCOMPLISHED: REMOVED DOUBLER, CUT OUT SKIN DAMAGE, FABRICATED AND INSTALLED ALL REPAIR PARTS PER ECRA 5330-04331.

Part: SKIN — DENTED (FUSELAGE) · airframe 78,741 hrs · 22,821 cycles

SKIN DENTS AT STA 611 AND STR 29R NEAR ANTENNAS. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED ALL REPAIR PARTS PER ECRA 5330-04331.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,741 hrs · 22,821 cycles

THREE LIGHTNING STRIKES ON FUSELAGE SKIN ZONE 123. INSPECTED STRIKES PER MM 53 -30-95 P601. DAMAGE WITHIN PARAMETERS LISTED PAGE 602 PAR 5B. OK FOR SERVICE. APPROX STA 500 LEFT SIDE AFT OF EE DOOR., SURFACE BURN, 1-32ND DIA. NO CRACKS DETECTED. STA 620 LEFT SIDE OPPOSITE OF FWD CARGO DOOR. AFT EDGE, SURFACE BURN 3-32ND DIA, NO CRACKS DETECTED. APPROX STA 729 LEFT SIDE AFT OF LAV SVC PANEL, SURFACE BURN 3-32ND DIA, NO CRACKS DETECTED. INSTALLED SOLID FASTENERS FOR PERM REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,741 hrs · 22,821 cycles

UPPER FUSELAGE EXTERNAL SKIN HAS BLENDED AREA AT STA 1448 AND STR 2R. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER ECRA 5330-04330.

Part: SKIN — DENTED (FUSELAGE) · airframe 78,741 hrs · 22,821 cycles

SKIN DENT LEFT SIDE AFT FUSELAGE AT STA 1620, BETWEEN STR 16L AND 14L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SKIN, FABRICATED & INSTALLED REPAIR PARTS PER ECRA.

Part: GATE — CORRODED (R1 DOOR) · corrosion level 2 · airframe 78,741 hrs · 22,821 cycles

R-1 DOOR UPPER GATE HAS CORROSION LP 9980671. DOOR GATE FOUND OUT OF LIMITS, REMOVED AND REPLACE UPPER DOOR GATE PER MM 52-11-38.

Part: GATE — CORRODED (R1 DOOR) · corrosion level 2 · airframe 78,741 hrs · 22,821 cycles

R-1 DOOR LOWER GATE HAS CORROSION. DOOR GATE WAS FOUND OUT OF LIMITS, REMOVED AND REPLACED LOWER DOOR GATE PER MM 52-11-38.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,741 hrs · 22,821 cycles

DEEP CORROSION ON STRINGER 26L BETWEEN STA 860 AND 879 IN THE FWD CARGO. LP 9982431. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION AND INSTALLED REPAIR PARTS PER SRM 53-00-03.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,741 hrs · 22,821 cycles

CABIN FLOORBEAM STA 1680 HAS CORROSION AT RBL 12. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED AREA, INSTALLED REPAIR PARTS PER SRM 53-60-51 AND ECRA 5330-04259.

Part: ARM — CORRODED (L1 DOOR) · airframe 78,741 hrs · 22,821 cycles

CABIN DOOR L-1 HINGE ARM ASSEMBLY HAS CORROSION. REMOVED AND REPLACED L-1 DOOR HINGE ARM ASSY AND RIGGED DOOR PER AMM 52-11-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,741 hrs · 22,821 cycles

DEEP CORROSION ON CABIN FLOORBEAM UPPER SURFACE STA 1640, LBL 8 TO RBL 60. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION, INSTALLED REPAIR PARTS PER ECRA 5352-01070.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,741 hrs · 22,821 cycles

UPPER LEFT FUSELAGE SKIN BLEND OUT AT STA 1460 ABOVE STR 8L. OPENED RIVET HOLE TO .254 ACCOMPLISHED HFEC AND INSTALLED SOLID RIVET PER ECRA 5330-04327.

Part: ACTUATOR — LEAKING (THRUST REVERSER) · airframe 78,741 hrs · 22,821 cycles

NR 1 ENGINE T/R FOUND O/B HALF CENTER T/R ACTUATOR LEAKING. REMOVED AND REPLACED NR 1 T/R CENTER ACTUATOR REF MM NR 9983852.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,741 hrs · 22,821 cycles

MULTIPLE LIGHTNING STRIKES IN FUSELAGE ZONE 123 (BETWEEN WL 148.5 - WL 208 AND STA 540 -STA 845). INSPECTED STRIKES PER MM 53 -30-95. DAMAGE WITHIN PARAMETERS OF PAR 6A PAGE 602. REPLACED DAMAGE FASTENERS WITH CHERRY MAX AT 5 LOCATIONS. (STA 617, STA 657, STA 677, STA 795, STA 845). INSTALLED SOLID FASTENERS AT LIGHTNING STRIKES PER SRM 53-00-01 FIG 201.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,741 hrs · 22,821 cycles

DEEP CORROSION FOUND ON CABIN FLOORBEAM UPPER SURFACE STA 365 RBL 1 TO RBL 58. TRIMMED OFF UPPER FLANGE INSTALLED REPAIR PARTS PER ECRA 5310-05536.

Part: VALVE — FAULTED (LT BLEED) · airframe 78,712 hrs · 22,814 cycles

LEFT BLEED TROUBLE, ACCOMPLISHED HEALTH CHECK OF PRSOV AND REPLACED SOURCE AIR SWIVEL FITIING. SWIVEL LOOSE WHILE 'B' NUT SEIZED. IDLE OPS CHECKED AND FOUND NR 1 BLEED PRESS FLUCTUATES BETWEEN 12-15 PSI. REPLACED CONTROL PRESSURE SENSE LINES, SOLID AND FLEX LINES. PERFORMED NR 1 ENG RUN, APPLIED PNEUMATIC LOAD, OPS CHECKED NORMAL.

Part: VALVE — FAILED (BLEED SYSTEM) · airframe 78,712 hrs · 22,814 cycles

LEFT BLEED TROUBLE. ACCOMPLISHED HEALTH CHECK OF PRSOV AND REPLACED SOURCE AIR SWIVEL FITTING, SWIVEL LOOSE WHILE B NUT SEIZED. IDLE OPS CHECKED AND FOUND NR 1 BLEED PRESSURE FLUTUATES BETWEEN 12-15 PSI. REPLACED HIGH STAGE PILOT VALVE PER AMM 36-11-08.

Part: SHUTOFF VALVE — FAULTY (APU BLEED) · airframe 78,706 hrs · 22,811 cycles

APU BLEED VALVE WILL NOT OPEN. REMOVED AND REPLACED APU SHUTOFF VALVE, OPS OK.

Part: REGULATOR — FAULTY (PNEUMATIC SYS) · airframe 78,706 hrs · 22,811 cycles

ZERO PNEUMATIC PRESSURE FROM LEFT ENGINE. REMOVED AND REPLACED PRSOV CONTROLLER NR 1 ENG, GROUND RAN. OPS CHECKED GOOD.

Part: CONTROLLER — FAULTY (PNEUMATIC SYS) · airframe 78,706 hrs · 22,811 cycles

ZERO PNEUMATIC PRESSURE FROM LEFT ENGINE. REMOVED AND REPLACED PRSOV CONTROLLER NR 1 ENG. GROUND RAN, OPS CHECKED GOOD.

Part: CONTROLLER — FAULTY (BLEED SYS) · airframe 78,706 hrs · 22,811 cycles

IN DESCENT, LT DUCT PRESSURE 8 RIGHT 22. REPLACED PRSOV CONTROLLER.

Part: IGNITER — FAULTY (RT ENGINE) · airframe 78,699 hrs · 22,809 cycles

NO START ON RT ENG IN IGNITER 2 OK IN BOTH. SECOND START ATTEMPT IN BOTH HAD A NORMAL START. IGNITER 2 INOPERATIVE ON RT ENGINE. NR 2 IGNITER ON RT ENGINE INOPERATIVE. REPLACED BOTH IGNITER PLUGS, OPS CHECKED OKAY.

Part: BLEED VALVE — FAULTY (LT ENGINE) · airframe 78,675 hrs · 22,802 cycles

LEFT ENGINE BLEED VALVE OFF LIGHT ILLUMINATED ON DESCENT STAYED ON THROUGH LANDING AND TAXI IN. SUPPLEMENTAL DATA, REPLACED NR 1 PRSOV VALVE PER MM. DURING ENG RUN LEFT BLEED INTERMITTENT, BLEED WOULD FLUCTUATE UNTIL DEMAND PLACED ON SYSTEM THEN BLEED STABILIZED FOR A FEW SECONDS, THEN BLEED WOULD SHUTOFF, WITH BLEED OFF LIGHT ILLUMINATED. ACCOMPLISHED BLEED HEALTH CHECK, FOUND PRSOV REGULATOR INOPERATOVE. REPLACED REGULATOR, OPS OK.

Part: COMPUTER — FAULTED (AUTOPILOT) · airframe 78,483 hrs · 22,742 cycles

RIGHT AUTOPILOT INOPERATIVE. WILL NOT ENGAGE. NO LAND 3. SUSPECT RIGHT FCC. REPLACED RT FCC. MCDP TEST 01 AND 30, OK. REF MM.

Part: LINE — WORN (HYD SUPPLY) · airframe 77,686 hrs · 22,523 cycles

HYDRAULIC SUPPLY LINE WORN APPROX .020 DEEP LOC IN RT PYLON AT STA 180.8. REMOVED DAMAGE SECTION OF HYD SUPPLY LINE. INSTALLED HYD SUPPLY LINE REF IPC 29-11-61 AND GNMM 1-0-0-006.

Part: TRANSCEIVER — MALFUNCTIONED (WX RADAR SYS) · airframe 77,436 hrs · 22,450 cycles

WEATHER RADAR SYS HAS UNCODED FAULT. RADAR WEAK. DID NOT PANT ANY RETURNS FOR CELLS WE HAD TO DV8 ARND. IN MAX MID AND NORM. ITEM HAS HISTORY. REPLACED WEATHER RADAR TRANSCEIVER. TESTED DISPLAY NORMAL WITH NO FAILURE MESSAGES.

Part: CONTROL VALVE — LEAKING (TE FLAPS) · airframe 77,412 hrs · 22,441 cycles

HYD FLUID LEAKING FROM VALVE TRAILING EDGE PWR DRIVE LEFT WHEEL WELL SPRAY OUT WHEN FLAP ARE GOING UP. REMOVED AND REPLACED LEFT CONTROL VALVE MODULE IAW AMM, LEAK CHECK GOOD, OPS CHECK GOOD.

Part: ACTUATOR — LEAKING (RT AILERONS) · airframe 77,394 hrs · 22,434 cycles

RT WING OTBD AILERON ACTUATOR LEAKING HYD FLUID AT FLANGE AREA. REPLACED RT OTBD AILERON ACTUATOR, OPS CHECKED OKAY.

Part: REGULATOR — FAULTY (BLEED SYSTEM) · airframe 77,224 hrs · 22,382 cycles

LEFT ENGINE BLEED VALVE DOES NOT CLOSE WITH SWITCH OFF. DUCT PRESSURE DROPS 5 PSI WITH SWITCH OFF. REPLACED PRSOV REGULATOR REF AMM. RAN ENGINE OPEN AND CLOSED PRSOV SEVERAL TIMES, OP CHECKED GOOD.

Part: DUCT — CRACKED (RECIRC FAN) · airframe 77,106 hrs · 22,351 cycles

RIGHT RECIRCULATION FAN IS OBNOXIOUSLY LOUD, IT IS HARD TO COMMUNICATE WITH IT ON. REPLACED DUCT, LEAK CHECK NORMAL.

Part: DUCT — CRACKED (PNEUMATIC SYS) · airframe 77,106 hrs · 22,351 cycles

PNEUMATIC DUCT THAT CONNECTS BETWEEN TEE DUCT AND LT GROUND CONNECTION IS CRACKED AT MATING SURFACE. REPLACED DUCT, LEAK CHECK NORMAL.

Part: DUCT — CRACKED (PNEUMATIC SYS) · airframe 77,106 hrs · 22,351 cycles

PNEUMATIC DUCT FWD OF APU CHECK VALVE IN RT PACK BAY IS CRACKED AT FLANGE MATING SURFACE. INSTALLED DUCT. LEAK CHECKED NORMAL.

Part: WIRE HARNESS — DAMAGED (CARGO DOOR) · airframe 76,612 hrs · 22,203 cycles

AFT CARGO DOOR ELECTRICAL HARNESS ATTACHED TO INSIDE OF DOOR HAS DAMAGED OUTER STAINLESS STEEL BRAIDING. PCN 562-1068 AOG Z6815. REPLACED HARNESS, DOOR OPS AND LIGHTS GOOD.

Part: ROTARY ACTUATOR — FAULTY (CARGO DOOR) · airframe 76,612 hrs · 22,203 cycles

AFT CARGO DOOR WILL NOT OPEN ELECTRICALLY OR MANUAL. SUSPECT DRIVE MOTOR. GRINDING POPPING NOISE WHILE TRYING TO DRIVE OPEN. LOWER INTERNAL DOOR ROD END BOLTS REMOVED TO REMOVE BAGGAGE. LOWER INTERNAL DOOR ROD END BOLTS REINSTALLED AND SECURED. DOOR CLOSED AND LATCHED. ACFT IS IN A DEFERABLE CONDITION. REF PLACARD 5230D FOR DEFERRAL IF NECESSARY. PCN 564-9028 ON AOG H1158. FOUND AFT CARGO DOOR, AFT ROTARY ACTUATOR LOCKED UP INTERNALLY. BOTH FWD AND AFT ROTARY ACTUATORS REMOVED. AOG'S: H3563 & K3617.

Part: BLADES — DAMAGED (COMPRESSOR) · airframe 76,125 hrs · 22,062 cycles

FOUND FAN BLADE TIP WITH MINOR CURL LESS THAN .125". BLENDED BLADE. INSPECTED USING HFEC, NO CRACKS NOTED.

Part: ACTUATOR — MALFUNCTIONED (SLATS) · airframe 76,124 hrs · 22,062 cycles

L/E SLAT DISAGREE EICAS, FLIGHT DIVERTED. MESSAGE DISPLAYED & LEADING EDGE LIGHT ILLUMINATED. FLAP INDICATOR NEEDLES STOPPED AT ONE HALF UNIT WITH NO SPLIT. FLAP HANDLE IN UP POSITION. CREW REPORTED NO ABNORMAL VIBRATION OR FLT CONTROL PROBLEMS. CREW FOLLOWED QRH 90.6. AIRSPEED LIMITED TO 240 KTS AND WAS NOT EXCEEDED. PER FLT MANUAL, ACFT LIMITED TO FL200. MANUFACTURER REP OBSERVED LEADING EDGES WERE NOT FULLY RETRACTED DURING FLIGHT. REPLACED NR 5 SLAT ROTARY ACTUATOR. REF AMIS 1252011.

Part: VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 76,031 hrs · 22,033 cycles

CB POPPED Q27 R HI STG SW OVER. REPLACED RIGHT ENG HIGH STAGE PILOT & SERVICE TIP.

Part: WIRE — DISCONNECTED (THRUST REVERSER) · airframe 75,973 hrs · 22,010 cycles

L REV ISLN VAL' MESSAGE NOT DISPLAYED DURING NR 1 ENGINE AUTO RESTOW CHECK. REF A-CHECK JOB CARD 5-5501. FOUND WIRE W3386-2521B-20 REMOVED FROM D5014 AND CAP & STOWED (CONT OF AMIS ITEM 9732002). INSTALLED CONTACT ON WIRE AND REPLACED IN CONNECTOR, THRUST REV OP TEST - ENG NOT RUNNING OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,973 hrs · 22,010 cycles

DOOR 2R EMERGENCY EXIT LIGHT IS INOP. CLEANED SOCKET & RELAMPED. CHECKS NORMAL.

Part: CARBON SEAL — LEAKING (NR 2 ENGINE) · airframe 75,957 hrs · 22,004 cycles

EVIDENCE OF OIL LEAK NR 2 ENG. NR 2 ENGINE RUN FOR APPROXIMATELY 5 MINUTES, NO LEAKS NOTED. ONE HOUR AFTER HIGH POWER BAG CHECK. IDG DRIVE PAD DRAIN STARTED LEAKING 60 DROPS PER MIN STATIC. DRAINED IDG AND STARTED DISCONNECTING FOR REMOVAL. REPLACED DRIVE SEAL AND RAN ENGINE AT IDLE, NO LEAKS NOTED AFTER RUN. DUE TO OIL CONSUMPTION TRENDING UP. AIRCRAFT TO REMAIN NON-ETOPS FOR AT LEAST 4 OIL SERVICES OR A POSITIVE FIX. NOTIFY DISPATCH FOR DEFERRAL. DUE TO IDG DRIVE SEAL AND DEOILER SEAL REPLACED ON NR 2 ENG, ACFT TO REMAIN NON-ETOPS AS STATED IN ABOVE TEXT.

Part: STRUCTURE — MISSING (TE FLAP) · airframe 75,881 hrs · 21,976 cycles

BOTH INBD FLAPS ELEPHANT EARS MISSING. PARTS NOT AVAILABLE MCO. -INF- :PARTS ORDERED AT MCO. 28 EA BACB30NN3K14, 2 EA 113N2038-7, 2 EA 113N2038-8, 1 EA 113N2037- 9SP, 1 EA 113N2037-10SP, AND 2 EA 113N2039-1. RPL- :INSTALLED, ADJUSTED AND OPS CHECKED PER BOEING DWG 113N1781. ALL CHECKS GOOD.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 75,831 hrs · 21,957 cycles

DURING DESCENT LEFT DUCT PRESSURE OSCILLATED BETWEEN 5PSI & 30PSI. RIGHT PRESSURE WAS STEADY. REPLACED HIGH STAGE PILOT VALVE AND PRSOV REGULATOR VALVE. RAN ENGINE AT IDLE, NO FLUCTUATION VISIBLE.

Part: ECU — UNKNOWN · airframe 75,734 hrs · 21,931 cycles

APU NO START. NO MESSAGES FOUND ON BOX. STARTED FIRST TIME AND SEVERAL MORE TIMES, COULD NO DUPLICATE ON GROUND. FOUND NO FAULTS ON ECU & FIRST ATTEMPT FAILED, REPLACED ECU PER MM.

Part: TERMINAL — DAMAGED (WINDOW HEAT) · airframe 75,549 hrs · 21,879 cycles

FOUND CAPTS WINDOW HEAT TERMINAL J1 WILL NOT REACH TORQUE. REMOVED AND REPLACED WINDSHIELD REF MM.

Part: PLACARD — MISSING (SEAT 34C) · airframe 75,549 hrs · 21,879 cycles

SEAT 34C 'LIFE VEST UNDER SEAT' PLACARD MISSING. INSTALLED ON TRAY TABLE. INSTALLED CORRECT PLACARD.

Part: RELAY — FAULTY (APU) · airframe 75,522 hrs · 21,872 cycles

APU WON'T START. REPLACED APU CRANK CONTACT OR RELAY PER MM. APU START NORMAL.

Part: EEC — FAULTY (NR 1 ENGINE) · airframe 75,426 hrs · 21,842 cycles

STATUS MSGL ENG SEC CONTL ENG PRI CONT REPLACED NR 1 ENG EEC PER AMM. RAN ENG TO VERIFY. ALL OPS NORMAL. NO MESSAGES ADVISED LM ENG CONTROLLER, NO VERIFICATION FLIGHT REQUIRED FOR ETOPS A/C.

Part: SWITCH — FAULTY (FUEL CUTOFF) · airframe 75,385 hrs · 21,825 cycles

WITH ENOUGH PRESSURE APPLIED, RIGHT FUEL CUTOFF SWITCH CAN BE INADVERTANTLY SELECTED OFF WHILE ENGINE IS RUNNING. NEEDS REPLACEMENT PER MM. PART ON AOG X5995. PCN 564-0213. RT FUEL CONTROL SW DOES NOT STAY IN THE RUN-LOCKED POSITION. INSPECTED SWITCH, FOUND OK SWITCH ACTION NORMAL.

Part: PRESSURE SWITCH — FAULTY (APU) · airframe 75,198 hrs · 21,770 cycles

APU AUTO SHUTDOWN AT GATE WITH ELEC LOAD BUT NO AIR LOAD .CHRONIC. REPLACED GENERATOR OIL FILTER DIFFERENTAL PRESSURE SWITCH PER AMM. STARTED APU TWICE AND APPLIED ELEC AND PNEU LOAD. APU RUNS OKAY.

Part: CONTROL UNIT — FAULTY (SPOILER SYSTEM) · airframe 75,085 hrs · 21,736 cycles

WHILE TROUBLESHOOTING LOG 1 SPOILER MESSAGE, FOUND 2R SPOILER CONTROL MODULE WITH PCA FAULT BALL. PER FIM AND MM 27-61-99-101, NR 3 AND NR 10 SPOILER PAIR PCA'S NEED TO BE REPLACED, NEEDS TWO PCA'S 643-9104. CONFERRED WITH OPBLM. THE 3 AND 10 SPOILERS LOCKED IN DOWN POSITION. AC IN CAT I, RETURN TO CAT III AFTER REPLACEMENT. WITH THE NEW -200 SCM INSTALLED PLEASE IDENTIFY WHICH PCA IS AT FAULT AND REPLACE ONLY FAULTY PCA. ALSO CHECK RVDTS FOR CORRECT SETTINGS PRIOR TO REPLACING A PCA. FOUND RVDT NR 3 -8.257 NR 10 -8.171. LIMIT -8.013 +- .050. ADJ 3 TO -8.011 10 TO -8.012. ADJ SOLID NO FLUX WHEN ADJ CONNECTOR HOOKED UP. FOUND 2R SCM -200 IN ANOTHER LANGUAGE. NEED TO REPLACE AND ACP OPS CHECK. REPLACED 2R SCM, GND CHECK OK PER MM. NO MSG'S AND NO FAULT BALLS. RETURNED AC BACK TO CAT III STATUS, GND CHECK OK PER AMM.

Part: MODULE — LEAKING (FLAP SLAT SYS) · airframe 75,019 hrs · 21,718 cycles

SLAT AND FLAP DEPRESSURIZATION MODULE LEAKS WITH PRESSURE ON AFTER FLAPS ARE STOWED. REMOVED & INSTALLED NEW MODULE AND CONNECTED HYDRAULIC LINES. REPLACED FLAP SLAT DEPRESSURIZATION MODULE. LEAK CHECKED GOOD. OPS CHECKED GOOD.

Part: CAP — FAULTY (APU OIL) · airframe 75,011 hrs · 21,713 cycles

RELEASE LEVER ON APU OIL CAP LOCKING MECHANISM IS MISSING. CAP CAN BE REMOVED WITH TOOLS FOR OIL SERVICE AND IS SECURE WHEN REINSTALLED. REPLACED APU OIL CAP WITH SERVICEABLE UNIT.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 74,977 hrs · 21,703 cycles

HYDRAULIC FLUID DRIPPING FROM RUDDER. FOUND HYD LINE ON UPPER RUDDER ACTUATOR RT SIDE LEAKING AT FWD END. REMOVED UPPER RUDDER PCA PRESSURE LINE. NEW HOSE ASSY ON EXPEDITE P/N AS115-06-0184 OSTF Z5024. REPLACED HOSE ASSY, NO LEAKS.

Part: AILERON — DENTED (LT WING) · airframe 74,912 hrs · 21,681 cycles

NUMEROUS DENTS WITH POSSIBLE 2 PUNCTURES TO THE LT AILERON. APPROXIMATELY 18 INCHES OUTBOARD OF THE INBOARD EDGE.

Part: SOCKET — MISSING (FUEL SYSTEM) · airframe 74,894 hrs · 21,674 cycles

LEFT CTR BOOST PUMP INOP. CTR L FUEL PUMP EICAS MSG AND NO TRANSFER INTO LEFT MAIN FUEL MAN. MAINT TEXT: OPB AND DD REFUSAL USING MEL 2822G LEFT CENTER PUMP INOP DUE PAYLOAD PENALTY AND ETOPS CRITICAL. TRANSFERED FUEL FROM MAIN TO CENTER TANKS, BOTH CENTER PUMPS INTERMITTENT WHEN TRYING TO TRANSFER BACK TO MAIN. WHILE PERFORMING CHK PER WD FOUND SOCKETS B3, B2 FROM RELAY K10872 MISSING. SUGGEST WORKING ITEM EG5768 TO CHK REST OF WIRING DUE TO GSO PERFORMING WIRING COA. USE WD 28-22-11 PG 3.1A SHEETS 1 THRU 3. SUGGEST DISCONNECTING S10010 & S10011 CONNECTORS & THEN TRYING COCKPIT CTR PUMP SWITCHES. ACCMP'D FIM 28-22-00 CTR PUMPS OPERATE NORMAL.

Part: WIRE — BROKEN (AUTOPILOT SYS) · airframe 74,819 hrs · 21,652 cycles

AUTOPILOT & A-P DISC LIGHT ON, LINE THRU (HDG HLD, HDG SEL, LNAV LOC, B-CRS) ON EADI, & EICAS MSG 'AUTOPILOT DISC' DISPLAYED WITH 1 AUTOPILOT SYSTEM ENGAGED IN CMD. OPS NORMAL WITH (L OR C) A-P SYS SELCTED (1=L, 2=C ,3=R) CREW COMMENTS: WITH CAPT FLT DIR OFF FO FD BARS ARE REMOVED FROM VIEW AND VNAV-LNAV REVERTS TO HDG-VS. WITH SAMC TEXT: ALSO WITH RIGHT A. RPL FCC R AND RH FMC, NO HELP. FOUND WIRE AT SOCKET 4 OF K2068 RELAY BROKEN. REPLACED SOCKET AND REINSTALLED. ACP CATIII TEST PER MM, TEST PASSED. RETURNED TO CATIII STATUS.

Part: PILOT VALVE — FAULTY (BLEED AIR SYS) · airframe 74,529 hrs · 21,555 cycles

UNABLE TO COOL AC ON GROUND WITH ENGINE BLEEDS ONLY ON IDLE. R 8 PSI, L 15 PSI. AC NORMAL IN FLT. PER MEL REPLACED HI STAGE PILOT PER AMM.

Part: CONTROLLER — FAULTY (FLIGHT DECK) · airframe 74,423 hrs · 21,516 cycles

FLT DECK WARMER THAN SELECTED WITH SWITCH ON & TEMP CONTROL IN AUTO. INOP LIGHT EXISTING. PRESS ECS REC BUTTON AND RECORD ZONE TEMPS. PROG TEXT: ACCOMPLISH CHRONIC REVIEW. -CHRONIC. PROCEDURE 1 USED ON MEL 2161E. REPLACED ZONE TEMP CONTROLLER. CHECKS OKAY PER MM.

Part: CONTROLLER — INOPERATIVE (AC PACK) · airframe 74,364 hrs · 21,500 cycles

FLT DECK TEMP CONTROLLER INOP. TEMP VARIED BTWN 92 AND 61. CREW REPORTED STBY SYSTEM WORKED WHEN SWITCHED OVER. REPLACED LEFT PACK TEMP CONTROLLER PER AMM, OPS CHECK NORMAL.

Part: SHUTOFF VALVE — FAULTY (AC BAY) · airframe 74,364 hrs · 21,500 cycles

LOUD WHISTLING NOISE WRT RECIRC OR BOTH PACKS ON. AIR NOISE TOO LOUD INTERF W COCKPIT COM. COMPLIED WITH MEL. CK SOUND & AIRFLOW LEVELS AT START & END TO COMPARE IMPROVEMENT. SUGGEST ACP STEP-4 OF ABOVE SVC TIP. IF NO FAULTS FOUND SUGGEST REPLACE LT PACK FLOW CONTROL & S-O VLV. ADDITIONALLY CHECK CONN AT L PACK TEMP VLV. REPLACED LEFT PACK FLOW CONTROL & S-O VLV PER MM, OPS CHECK OK.

Part: PRESSURE SWITCH — FAULTY (HYD SYSTEM) · airframe 74,152 hrs · 21,441 cycles

CREW REPORTED THE LEFT ELEC HYD PUMP LOW PRESSURE LIGHT IS FLICKERING ON-OFF. ALSO EICAS MESSAGE LEFT ELECT HYD PUMP IN-OP IN VIEW BUT IS INTERMITTANT WITH ALL PUMPS OFF TOO. PERFORMED WIRING CHECKS IAW LM8436. REPLACED LT HYD SYS PRESSURE SWITCH S27 AND RAN ENGINES WITH NO FAULTS.

Part: CONTROL UNIT — FAULTY (HYD PUMP) · airframe 74,152 hrs · 21,441 cycles

LT HYD ELEC PUMP. REPLACED LEFT ELCU, OPS CHECKED GOOD.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 74,152 hrs · 21,441 cycles

NUMEROUS TIMES IN CLIMB AND CRUSE, LEFT ELEC HYD PUMP LOW PRESSURE LIGHT AND EICAS LT HYD ELEC. DUE TO PREVIOUS HISTORY REPLACE LT ELECT PUMP. REPLACED LEFT ELEC HYD PUMP AND FILTERS.

Part: PUMP — FAULTY (HYD SYSTEM) · airframe 74,145 hrs · 21,439 cycles

LEFT HYD ELECTICAL PUMP EICAS CAME ON AGAIN WITH LOW PRESSURE LIGHT IN SWITCH. TURNED OFF PER CHECKLIST. REPLACED L-ELEC HYD PUMP PRESSURE SWITCH. ALSO CHECKED ALL DELTA P'S. NONE WERE POPPED PRESSURIZED SYS, ALL PARAMETERS NORMAL. RAN GEAR DOORS UP AND DOWN AND CYCLED ALL FLIGHT CONTROLS ALL NORMAL.

Part: STARTER — FAILED (APU) · airframe 74,140 hrs · 21,436 cycles

APU WILL NOT START. STARTER WOULD NOT ENGAGE CHECKED FADEC. FOUND REVERSE FLO MESSAGE CLEARED. STILL NO START. APU DID NOT START 4 TIMES, APU NOT CRANKING. REPLACED APU STARTER PER AMM AND REPLACED APU CRANK CONTACTOR PER AMM. DID APU BITE TEST AND RAN APU TWICE WITH NORMAL START PER AMM.

Part: PRINTER — FAILED (COCKPIT) · airframe 74,120 hrs · 21,427 cycles

ACARS PRINTER FAILED. REPLACED ACARS PRINTER, OPS CHECKED GOOD.

Part: VALVE — OUT OF TOLERANCE (AC SYSTEM) · airframe 74,102 hrs · 21,421 cycles

INTERMITTENT THUMPING NOISE IN COCKPIT WHEN EITHER LEFT OR RIGHT PACK TURNED ON OR OFF. RECIRC OFF DOESN'T HELP. LEFT A-C PACK FLOW CONTROL VALVE, UPPER SUPPORT ROD ASSY FOUND TO BE WORN OUT. SUSPECT CAUSE OF HUMMING SOUND WHEN PACK IS TURNED ON. REPLACED SUPPORT ROD. ALSO FOUND GROUND AIR SERVICE FLAPPER STUCK IN OPEN POSITION. REPAIRED VALVE. NO ABNORMAL NOISES NOTED. NOISE LEVEL WITHIN LIMITS.

Part: APU — MALFUNCTIONED · airframe 73,195 hrs · 21,154 cycles

APU STARTED THEN SHUTDOWN FOR UNKNOWN REASON WILL NOT RESTART. ACCOMPLISHED APU BITE AND FOUND INLET DOOR FAULT. CYCLED APU DOOR CIRCUIT BREAKER C05 AND CONT CIRCUIT BREAKER C05 E6 PANEL. APU START AND OPS NORMAL.

Part: PRESSURE SWITCH — FAILED (HYD RESERVOIR) · airframe 72,598 hrs · 20,984 cycles

LEFT HYD RESERVOIR OVERHEAD LIGHT AND EICAS LOW RESERVOIR PRESSURE. REPLACED LEFT HYD RESERVOIR PRESSURE SWITCH AND LT RESERVOIR VENT VALVE. IDLE RUN NR1 ENGINE WITH ENGINE BLEED. ALL SYS LIGHTS CHECK NORMAL.

Part: LINE — LEAKING (RT ENGINE FUEL) · airframe 72,444 hrs · 20,938 cycles

FUEL CONTROL LINE LEAKING ON RT ENGINE. PARTS ON AOG. REPLACED LEAKING RIGID LINE TO FUEL CONTROL PER MM.

Part: PRESSURE SWITCH — FAULTY (HYD PUMP) · airframe 72,159 hrs · 20,854 cycles

AC MOTOR PUMP - WITH LOW PRESS LIGHT ILLUMINATED AND EICAS MESSAGE 'C HYD ELEC 2' DISPLAYED AND EICAS MESSAGE 'HYD SYS MAINT' WAS NOT DISPLAYED. REPLACED THE PRESSURE SWITCH, S100016, FOR THE ACMP, C2 IN THE CENTER HYD SYS. CREW COMMENTS: C HYD ELEC 2 CAME ON TWICE FOR APPROX 4 SEC EACH TIME, AOG DID NOT COME IN. REPLACED PRESSURE SWITCH S100016. LEAK CHECK OK, NO MESSAGES OR FAULTS FOUND.

Part: CONTROL VALVE — FAULTY (STARTER) · airframe 72,150 hrs · 20,852 cycles

LEFT ENG OH LP 1 STATUS MESSAGE. REPLACED STARTER AND REPLACED STARTER CONTROL VALVE PER MM. MOTORED ENGINE, NO LEAKS NOTED. RAN ENGINE. CHECKS NORMAL, NO MESSAGES.

Part: GASKET — FAULTY (CHECK VALVE) · airframe 71,944 hrs · 20,790 cycles

VERY NOTICEABLE PRESSURIZATION SURGE AT ABOUT 600'. REPLACED SEAL ON CHECK VALVE RT PACK BEFORE DIST DUCT. LEAK AND OPS CK GOOD. WHILE TROUBLESHOOTING LOG 2, FOUND SECTION OF GASKET MISSING FROM FWD MATING SURFACE OF CONDITIONED AIR CHECK VALVE ATTACH POINT. REPLACED GASKET PER MM. OPS AND LEAK CHECKS OK. ALSO REPLACED ISOLATION VALVE PER MM AS A PRECAUTION. OPS AND LEAK CHECKS OKAY.

Part: ELEVATOR — LOOSE (ELEVATOR) · airframe 71,539 hrs · 20,659 cycles

CONTROL COLUMN HAS A BUMP WHEN CYCLING ELEVATORS FROM NOSE DOWN TO UP. FOUND F/O'S AFT ELEVATOR QUADRANT LOOSE ON TORQUE SHAFT. SETTING UP TO START DISASSEMBLY OF F-O QUADRANT. REMOVED FASTENERS, APPLIED INSTRUCTION FROM MM 27-31-70 REPAIR 8-1. HOLES WERE ROUND AND WITHIN TOLERANCE PER FIG 601. NO CRACKS PER 757 NDT. MCDP CHECK REVEALED FAULT RUDDER SERVO-FCC. PULLED AND SECURED BREAKER E18 L FCC SERVO. REPLACED ARGS ELECTRO HYD SERVO VALVE. OPS CHECKS GOOD. TROUBLESHOT LT ELEVATOR PCU STATUS MESSAGE. REPLACED OTBD PCU ON LT ELEVATO, OPS & LEAK CHECKED GOOD. MESSAGE WENT AWAY. PERFORMED AUTOPILOT CAT-III AUTOLAND TEST PER MM. TEST PASSED, NO FAULTS. RETURNED AC TO CAT-III STATUS.

Part: PCU — FAULTY (LT ELEVATOR) · airframe 71,539 hrs · 20,659 cycles

LEFT ELEVATOR PCU STATUS MESSAGE. ACP BLOCK 1 LT PCU MESSAGE RETURNED, NO TIME TO TROUBLESHOOT. ACCOMPLISHED FIM TO BLOCK 11. INSPECTION WIRE WAS NOT ABLE TO GO THROUGH INSPECTION HOLE. ALSO ACCOMPLISHED DIODE CHECK IN PCA TS5206. ONE DIODE FAILED RINGOUT CHECK-FAILURE OF DIFFERENTIAL PRESSURE SENSOR IN PCA. REPLACED OUTBOARD PCU ON LT ELEVATOR. OPS CHECKED, LEAK CHECKED GOOD. MESSAGE WENT AWAY.

Part: CONNECTOR — MISINSTALLED (HF SYSTEM) · airframe 70,845 hrs · 20,460 cycles

NR1 HF WEAK AND SCRATCHY IN REC-XMIT UNABLE TO USE. NEEDS MORE TIME. REPLACED HF-L ANTENNA COUPLER, NO HELP. TDR CHECK OF ANTENNA CABLES FROM E & E TO ANTENNA CHECKS GOOD. CHECKED CONNECTIONS IN COUPLER AND ANTENNA AREA. REPLACED LT AND RT HF COAX CABLE CONNECTORS AT COUPLER IAW GNMM. UNABLE TO OPS CHECK DUE TO STRUCTURE IN FRONT OF ACFT. REQUEST CREW OPS CHECK ON OTBD FLIGHT. ACFT TAXIED AND GOOD VOICE COMMUNICATIONS ON BOTH HF RADIOS. 59-220 CONNECTORS ON EACH-COUPLER FOUND IMPROPERLY INSTALLED. ALL OPS NORMAL AFTER REPLACEMENT.

Part: CONTROL VALVE — FAULTY (LEFT ENGINE) · airframe 70,758 hrs · 20,436 cycles

LEFT ENG STARTER EICAS ON START. NO ROTATION. CYCLED D19, NO HELP. ACCMP'D MANUAL START. REPLACED STARTER CONTROL VALVE PER MM. OPS CHECKS NORMAL.

Part: SKIN — DAMAGED (BS 972 S3R) · airframe 70,308 hrs · 20,308 cycles

LIGHTNING STRIKE, STA 972 STR 3R. MAJOR REPAIR ACCOMPLISHED: WILL REQUIRE REPAIR IAW SRM REPAIR 2. DRILLED OUT STRINGER FASTENERS AND STARTED MFG REPAIR DOUBLER. REMOVED DAMAGED AREA FOR REPAIR. DOUBLER STILL NEEDS TO BE COUNTERSUNK, TRIMMED, PRIMED AND INSTALLED WET. FINISHED DOUBLER, COUNTERSUNK HOLES. MFG'D FILLERS. INSTALLED DOUBLER IAW SRM, REPAIR 2. SEALED, PRIMED AND PAINTED DOUBLER.

Part: ACTUATOR — FAULTY (RUDDER TRIM) · airframe 70,200 hrs · 20,274 cycles

RUDDER TRIM FAILED TO TRIM IN EITHER DIRECTION. SAMC TEXT: AFTER CONSULTING SFOEG SUGGEST RPL RUDDER TRIM ACTUATOR. REPLACED AIL & RUDDER TRIM CONTROL MODULE, NO HELP. NEEDS FURTHER T-S. REPLACED RUDDER TRIM ACTUATOR. OP CKS GOOD. INSPECTED ACTUATOR INSTALLATION FOR SAFETY, SECURITY AND PROPER INSTALLATION. OBSERVED PROPER OPERATION AND INDICATION. NO LEAKS.

Part: ACTUATOR — FAILED (RUDDER TRIM) · airframe 70,042 hrs · 20,229 cycles

RUDDER TRIM FAILED TO TRIM IN EITHER DIRECTION. CREW COMMENTS: INTERMITTENTLY INOPERATIVE. REPLACED RUDDER TRIM ACTUATOR. ACCOMPLISHED TRIM TEST, ALL OPERATIONS AND INDICATIONS NORMAL. DURING RUDDER TRIM INDICATION TEST NOTICED RUDDER TRIM INDICATOR IN THE PEDESTAL PANEL INDICATION ARROW STICKS. EICAS INDICATION NORMAL. REPLACED RUDDER TRIM INDICATOR. OPS CK NORMAL. EICAS RUDDER POSITION INDICATION NORMAL.

Part: VALVE — SHORTED (MLG DOOR ACT) · airframe 70,039 hrs · 20,227 cycles

LANDING GEAR ALTERNATE EXTENSION MOTOR CONTINUED TO RUN. PULLED C-B TWICE AND RESET BOTH TIMES MOTOR RAN AGAIN. PULLED AND LT PUMP BREAKER OUT. REPLACED RT GEAR DOOR ACTUATOR UNLOCK SOLENOID SHORTED. ALL OPS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,039 hrs · 20,227 cycles

LT EXTERIOR EMERGENCY EVACUATION LIGHT AFT OF WING INOPERATIVE. REPLACED BATTERY M735 AND CKD OK.

Part: LAMP — INOPERATIVE (MLG INDICATOR) · airframe 70,039 hrs · 20,227 cycles

RIGHT MLG WHEEL WELL UNSAFE LIGHT INOPERATIVE. REPLACED LAMP, OPS GOOD.

Part: CONNECTOR — FAULTY (APU) · airframe 69,683 hrs · 20,115 cycles

APU INOP. REPLACED BAD ELEC CONNECTOR TO APU SHUTOFF VALVE ACTUATOR. ALL OPS NORMAL. APU STARTS AND RUNS NORMALLY. FOUND DEFECTIVE CONNECTOR, OPS CHECKED SYS, ALL CHECKS GOOD.

Part: CONTROL VALVE — FAULTY (LT A/C PACK) · airframe 69,117 hrs · 19,955 cycles

LEFT PACK OFF LIGHT AND EICAS MESSAGE NOT ON WITH PACK SELECTED OFF, IAW CREW. REPLACED FLOW CONTROL AND SHUTOFF VALVE. OPS GOOD.

Part: IDG — FAULTY (NR 1) · airframe 68,950 hrs · 19,906 cycles

EICAS MSG L GEN DRIVE DISPLAYED.GEN DRIVE LGT ILLUM. GEN DRIVE DISCONNECTED. CREW COMMENTS: L GEN DRIVE LIGHT ON. APU OK. FOUND L ENG IDG WITH MULTIPLE HOLES, DIFF PRESS INDICATOR POPPED. DRAINED IDG OIL, SMELLED NO EVIDENCE OF FUEL. MOTORED ENGINE TO ENSURE IDG DISCONNECTED. INSPECTED AREA AROUND IDG AND COWLING, NO OTHER DEFECTS FOUND. REPLACED NR 1 IDG LEAK & OPS CHKD NORMAL.

Part: IDG — FAULTY (NR 1) · airframe 68,944 hrs · 19,904 cycles

EICAS MSGS L GEN DRIVE LGT DID NOT ILLUM WITH ENG SHUTDOWN. REPLACED NR1 ENG IDG. FLEW ONE SEGMENT AND FOUND L ENG IDG WITH MULTIPLE HOLES, DIFF PRESS INDICATOR POPPED. DRAINED IDG OIL, SMELLED NO EVIDENCE OF FUEL. MOTORED ENGINE TO ENSURE IDG DISCONNECTED. INSPECTED AREA AROUND IDG AND COWLING, NO OTHER DEFECTS FOUND. REPLACED NR1 ENG IDG.

Part: WIRE — BURNED (AFT WATER HEATER) · airframe 68,891 hrs · 19,891 cycles

NO WATER IN AFT GALLEY AFTER 4 HOURS OF FLIGHT. FOUND CB C4262 FOR AFT WATER HEATERS POPPED AND BURNED SPLICES SP273,SP269,SP1842. CONFIGURED WIRES IAW WDM 30-71-21 PG 2. NO OTHER DAMAGE FOUND, TESTED WATER HEATERS. COMPRESSOR PRESSURE GOOD.

Part: ACTUATOR — MALFUNCTIONED (ELEV ASYM LIMIT) · airframe 68,721 hrs · 19,839 cycles

ELEVATOR ASYM MESSAGE DISPLAYED, IAW CREW. ACTUATOR FOUND FAULTY. REPLACED ACTUATOR M10048, OP CHECKS OK AND NO MESSAGES.

Part: CABLE — FAULTY (EMERGENCY LIGHTS) · airframe 68,658 hrs · 19,820 cycles

EMERGENCY EVACUATION FLOOR LIGHT AT THE FWD CLOSET IS IN-OP. REPLACED LEAD IN CABLE. OPS CHECKS GOOD.

Part: WEDGE — MISSING (LE SLAT) · airframe 68,335 hrs · 19,727 cycles

A SECTION OF RIGHT INBOARD SLAT TRAILING EDGE WEDGE IS MISSING. INSTALLED NEW NR 6 SLAT. ACCOMPLISHED INSPECTION OF NR 6 SLAT INSTALLATION. ACCOMPLISHED TEST OF L/E SLAT INSTALLATION. OP CHECKS GOOD.

Part: SCAVENGE PUMP — FAULTY (ENGINE) · airframe 68,319 hrs · 19,724 cycles

DURING CRUISE OIL QUANTITY LEFT ENG 19, RIGHT ENG 09. RAN ENGINE QUANTITY DROP APPROX 10 QT. NO EVIDENCE OF A LEAK. FILLED OIL TANK TO FULL. ALL OTHER INDICATIONS NORMAL. REPLACED OIL QUANTITY TRANSMITTER. FIVE MINUTE IDLE LEAK CHECK OKAY, AND OPERATIONAL TEST-OIL QUANTITY INDICATING SYSTEM OKAY. REOPENED ON 06NOV09 DUE TO SAME PROBLEM ON HI POWER RUN. REPLACED LUBRICATION AND SCAVENGE OIL PUMP. ACCOMPLISHED RUN TEST. ALL PARAMETERS WITHIN LIMITS AND LEAK CHECKS GOOD.

Part: CABLE — DEFECTIVE (EMERGENCY LIGHT) · airframe 68,187 hrs · 19,691 cycles

EMERGENCY EEL LIGHTING FROM SEAT ROW 9 TO SEAT ROW 12 IS INOP. REPLACED EEL POWER JUMPER CABLE AT SEAT ROW 9. EEL OP CHECKS OKAY.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 68,122 hrs · 19,671 cycles

LEFT ENG BLEED VALVE STUCK CLOSED. REPLACED PRSOV VALVE, BLEED OPS CHECKS NORMAL.

Part: LINE — RUPTURED (HYD SYSTEM) · airframe 67,939 hrs · 19,617 cycles

LOST LEFT HYD SYSTEM QTY DECREASED TO .24. TOWED BACK TO GATE AND FOUND FLEX LINE FOR NLG DOOR ACT RUPTURED. REPLACED HOSE AND SERVICED HYD, OP CHECK GOOD, NO LEAKS.

Part: MODULE — FAULTY (ELEVATOR) · airframe 67,937 hrs · 19,616 cycles

ELEV ASYM MSG, RTFL. REPLACED LEFT CSEU AND RT SAM. REPLACED ELEVATOR ASYM ACTUATOR (P/N S251N206-2 - S/N 56), OPS CHECK OK. NO MESSAGES DISPLAYED.

Part: SKIN — BENT (LT WING TE FLAP) · airframe 67,714 hrs · 19,551 cycles

LEFT WING OUTBOARD TRAILING EDGE FLAP LOWER SKIN IS BENT NEAR THE INBOARD FLAP TRACK. FOUND FLAP SUPPORT TRACK LOOSE WITH MISSING BOLTS. INSTALLED & SECURED MISSING BOLTS AFT FLAP TRACK INBOARD SIDE LT OUTBOARD MID FLAP REF IPC 57-53-10 051 VIEW-N. CYCLED FLAPS FULL DOWN, UP, CHECKED OK. NO OTHER DAMAGE NOTED. RECONTOURED SKIN BUT WILL NEED ADDITIONAL WORK. INSP'D LWR WING SKIN WITH HFEC. REMOVED DAMAGED SKIN, INSPECTED STRUCTURE, MFG NEW SKIN, INSTALLED ON WU L8685M.

Part: FEEDER CABLE — FAILED (CABIN) · airframe 67,701 hrs · 19,547 cycles

EEL LIGHTS INOP AT SEAT 21ABC-33ABC. REPLACED POWER FEEDER STRIP IN EEL TRACK, P/N 5878-1. OPERATES NORMALLY.

Part: SELECTOR PANEL — FAULTY (VHF COMM) · airframe 67,683 hrs · 19,542 cycles

VHF R STILL BROKEN. REPLACED R VHF FREQUENCY SELECT PANEL, COMM CHECKS ARE GOOD.

Part: SKIN — MISSING (APU INLET DOOR) · airframe 67,623 hrs · 19,527 cycles

DAMAGE WAS FOUND AT APU INLET AREA. LOOKED AT DAMAGE, ENTIRE INNER SKIN OF APU INLET DOOR IS MISSING PROBABLY BETTER TO REPLACE INLET ASSY. REPLACED APU INLET DOOR. OPS CHECK GOOD.

Part: APU — SPARKS (APU BAY) · airframe 67,594 hrs · 19,519 cycles

AFTER PARKING AT GATE GROUND CREW INFORMED FLIGHT CREW APU STARTED THROWING SPARKS OUT THE EXHAUST. CHECKED ALL MAG PLUGS NO METAL FOUND. INSPECTED TAIL CONE, NO DEFECTS NOTED. ONE TIME FLIGHT TO HNL FOR CHANGE. REPLACED APU ASSY, LEAK AND OPS CHECKED OKAY.

Part: CARBON SEAL — LEAKING (NR 2 ENGINE) · airframe 67,535 hrs · 19,497 cycles

NR 2 ENG HIGH OIL CONSUMPTION EXCEEDS LIMIT. ACCOMPLISHED RUN AT 80 PERCENT FOUND OIL LEAK FROM STARTER DRAIN 60 DROPS A MIN. REPLACED NR 2 ENG STARTER DRIVE CARBON SEAL. RERAN ENG, NO LEAKS. SECURED FAN COWLS.

Part: FUEL CONTROL — FAULTY (FUEL SYSTEM) · airframe 67,353 hrs · 19,444 cycles

RT MAIN FUEL TANK INDICATION BEFORE FUELING PROCESSOR SHOWED NO PRESENT FAULTS AND SELF TEST PASSED. AFTER FUELING SELF TEST SHOWS "CT DENS CONTAMINATED OR RESISTOR G" AND "RM DENS CONTAMINATED OR RESISTOR G" AND "CT COMP CONTAMINATED OR RESISTOR G" AND "RM COMP CONTAMINATED OR RESISTOR G". REPLACED RT DENSITOMETER. REPLACED FUEL QUANTITY PROCESSOR (PRECAUTIONARY). REPLACED COMPENSATOR. OPS CHECK GOOD. BITE CHECK GOOD.

Part: HEAT EXCHANGER — LEAKING (OIL SYSTEM) · airframe 67,210 hrs · 19,395 cycles

FUEL OIL HEAT EXCHANGER LEAKING. AFTER REPLACEMENT OF NR 2 FUEL OIL HEAT EXCHANGER RAN NR 2 ENG LEAKING 24 DROPS A MIN. BAD FROM STOCK. REPLACED FUEL OIL HEAT EXCHANGER. LEAK CHECKS GOOD.

Part: IDG — LEAKING (NR 2 ENGINE) · airframe 67,210 hrs · 19,395 cycles

RIGHT GEN 'FIELD OFF' LIGHT ILLUM WITH FIELD OFF SW PRESSED. REPLACED NR 2 ENG IDG, OPS CHECKED ALL INDICATIONS NORMAL, NO LEAKS NOTED.

Part: EEC — FAULTY (NR 2 ENGINE) · airframe 66,927 hrs · 19,310 cycles

NR 2 ENGINE HUNG START BEFORE STARTER CUTOUT. HUNG 49 % BOTH STARTS EGT APP RED LINE EGT ABOUT 476. NO EXCEEDENCE. HUNG START ENGINE WILL NOT ACCELERATE PAST 49 % N2 WITH EGT CLIMBING. MESSAGE 275-25 EEC; REPLACED NR 2 ENGINE EEC. FOUND PIN-3 ON D5024- SHORTED TO SHIELD & GROUND WITH D1074P DISCONNECTED FROM FIREWALL, PIN-6 ALSO HI-RES SHORT-GND D5024 INTERMITMENT. D5024 IS DISASSEMBLED AT NR 2 START VALVE. RECHECKED ABOVE FAULTS & FOUND NO SHORTS TO GROUND. REASSEMBLED D5024 & TESTED AGAIN OK. SECURED DISCONNECTED CONNECTORS. FOUND NR 2 ENG START SWITCH SOMETIMES STICKS IN GND POS WITH NO POWER APPLIED. REPLACED NR 2 START SWITCH. ACP 3 SUCCESSFUL ENGINE STARTS WITH NORMAL CUTOUT.

Part: ACTUATOR — LEAKING (SPOILER) · airframe 66,699 hrs · 19,236 cycles

EVIDENCE OF HYD LEAK O/B OF NR 2 ENG. FOUND NR 11 SPOILER WET. RAN UP AND DOWN SEVERAL TIMES, NO LEAKS NOTED. TO BE RE-CHECKED WITHIN 75 HRS. REPLACED PCA ACTUATOR, HYD LEAK FIX BUT FAIL ON SYNCHRONOUS TEST. REPLACED RVDT AND OPS CHECKED.

Part: MOUNT — SHEARED (NR 1 ENGINE) · airframe 66,304 hrs · 19,126 cycles

NR 1 ENG LOWER ISOLATION PACK BOLT SHEARED OFF AND LAYING ON UNISON RING. TRIED TO REMOVE SHEARED BOLT FROM MOUNT UNABLE TO ACP. SHIM PACK AND SHEARED BOLT HEAD PACKAGED AND ON FLIGHT DECK. REPLACED NR 1 ENG LOWER FWD ENG MOUNT. ACP'D INSP OF FWD ENG MOUNT INSTALLATION. SAFETY AND SECURITY GOOD. NO DEFECTS FOUND. NOTE: NOSE COWL WAS NOT REMOVED, SAME ESN CAME DOWN AND UP AFTER FWD MOUNT WORK. ENG RUN - LK CHECK OKAY. ACCMP'D VERIFICATION FLIGHT DUE TO ENGINE POS 01 REMOVAL AND REINSTALLATION. ITEM CLEARED.

Part: ACTUATOR — FAULTY (SPOILER) · airframe 66,271 hrs · 19,116 cycles

EXCESSIVE RUDDER TRIM. VERY SLOW TO EXTEND. CREW REPORTED FELT MORE LIKE A SPOILER FLOAT, NOT AN ENGINE VIBRATION. THE NR 2 FLT SPOILER WAS FOUND TO BE LAGGING IN OPERATIONAL TIME IN COMPARISON TO THE REMAINING FLT SPOILERS AND THE NR 10 FLT SPOILER WAS FOUND TO HAVE EXCESSIVE LEAKAGE & THEREFORE REPLACED. NR 2 SPOILER ACTUATOR ALSO REPLACED. VERIFICATION TEST FLIGHT CONFIRMS NORMAL OPERATION OF FLIGHT CONTROLS.

Part: FEEDER CABLE — DEFECTIVE (CABIN) · airframe 65,819 hrs · 18,985 cycles

EEL LIGHT IS INOP IN FWD CABIN FLOOR ADJ TO COAT CLOSET SHORT SECTION. REPLACED POWER FEEDER CABLE. EEL LIGHT OP CHECKS OK.

Part: COMPRESSOR — DAMAGED (NR 1 ENGINE) · airframe 65,373 hrs · 18,864 cycles

NR 1 & NR 2 ENGINE FOD. CREW REPORTED, WALK-AROUND AFTER ARRIVAL IN JAC, FOUND FOD DAMAGE TO THE NR 1 & NR 2 ENGINES. ACP A BORESCOPE INSPECTION WITH NO LIMITING DEFECTS NOTED. REPLACED COMPLETE FAN SET ON BOTH ENGINES.

Part: ENGINE — FOD (NR 1) · airframe 65,373 hrs · 18,864 cycles

NR 1 & 2 ENGINE FOD.

Part: ENGINE — FOD (NR 2) · airframe 65,373 hrs · 18,864 cycles

NR 1 & NR 2 ENGINE FOD.

Part: COUPLING — BROKEN (BLEED AIR SYS) · airframe 65,107 hrs · 18,787 cycles

R BLEED DUCT LEAK. RTFL. FOUND BROKEN FUSED COUPLING ON DUCT IN WING LEADING EDGE JUST ABOVE PYLON. REPLACED COUPLING AND DUCT SEAL. LEAK CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,879 hrs · 18,725 cycles

EEL LIGHTS AFT OF ROW 31 INOP. EXIT SIGN INOP OVER DOOR 4R. AISLE LIGHTS INOP ROWS 27 & 31, SLIDE LIGHT INOP DOOR 4R. REPLACED BATTERY PACK & POWER SUPPLY AT POSITION M10817.

Part: IDG — FAULTY (NR 1 ENGINE) · airframe 64,690 hrs · 18,675 cycles

LT GEN CAME OFF LINE 2 TIMES, SPOKE TO SAM, DURING RUN UP IS WHEN GEN CAME OFF AT =40% N1. REPLACED NR 1 IDG.

Part: PRESSURE PANEL — DAMAGED (FUSELAGE) · airframe 64,584 hrs · 18,644 cycles

AFT PRESSURE DECK BS 1681.8 AT RBL 42" AND RBL 52" HAS CORROSION DAMAGE. MAJOR REPAIR ACCOMPLISHED. REMOVED PREVIOUSLY INSTALLED REPAIR DOUBLER-TRIPLER. FABRICATED A NEW REPAIR DOUBLER.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 64,584 hrs · 18,644 cycles

LAV K SMOKE DETECTOR WILL NOT RESET.

Part: WIRE — CHAFED (CABIN) · airframe 64,584 hrs · 18,644 cycles

WIRE BUNDLES AND COAX HAVE CHAFING, 1 EA BROKEN WIRE, NOT SECURED UNDER MAIN CABIN FLOOR STA 996 TO 1180, LBL 48. SECURED WIRE BUNDLES AND COAX UNDER MAIN CABIN FLOOR AT BS 996-1180, LBL 48 PER BSWPM 20-10-42. OPS CHECK OF HYDRAULIC RESERVOIR TEMP GOOD AND OPS CHECK OF SPOILER CONTROL MODULE 3R WIRING GOOD.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,584 hrs · 18,644 cycles

AFT PIT FRAME DENTED STA 1520, RBL 8 TO RBL 9. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED J-ANGLE DOUBLER REPAIR.

Part: SWITCH — FAILED (CREW O2) · airframe 64,584 hrs · 18,644 cycles

THE O2 SYSTEM FAILS ALTITUDE SWITCH, OPS CHECKS. REPLACED ALTITUDE PRESSURE SWITCH, OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,584 hrs · 18,644 cycles

LAV K FLOOR PATH LIGHT STRIP INOP. REPLACED FLOOR PATH LIGHT STRIP.

Part: REPAIR — DENTED (FUSELAGE) · airframe 64,584 hrs · 18,644 cycles

SKIN REPAIR DENTED STA 610, STA 620, STR 15L TO 16L. MAJOR REPAIR ACCOMPLISHED. REMOVED EXISTING REPAIR DOUBLER AND ACP'D SCRIBE LINE INSPECTIONS PER 757-53A0092 S/B AND ACP'D HFEC PER 757 NDT 6-51-00-19 AND 6-51-00-16, NO INDICATIONS NOTED. FABRICATED A NEW SKIN, DOUBLERS, TRIPLERS, FILLERS, AND STRUCTURAL FILLERS PER TIMCO REO-G12490 REV A AND UAL EVA 72120.

Part: SKIN — DENTED (FUSELAGE) · airframe 64,584 hrs · 18,644 cycles

LWR FUSELAGE SKIN IS DENTED NUMEROUS PLACES, STA 233 - 236, STR 24L TO 26L. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SKIN AND FABRICATED A REPAIR DOUBLER AND INSTALLED.

Part: RESERVOIR — LOW PRESSURE (L2 DOOR) · airframe 64,584 hrs · 18,644 cycles

DOOR 2L EMERGENCY POWER RESERVOIR PRESSURE IS LOW. REMOVED AND REPLACED THE L -2 DOOR EMERGENCY POWER RESERVOIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,584 hrs · 18,644 cycles

AFT PIT FRAME DENTED STA 1460, STR 25L TO 24L. MAJOR REPAIR ACCOMPLISHED. CUTOUT DAMAGED SECTION OF PIT FRAME AND INSTALLED DOUBLER REPAIR. THIS ALSO INCLUDES DAMAGE NEAR STR 26L-25L.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 64,584 hrs · 18,644 cycles

AFT PIT FRAME UPPER FLANGE DENTED BETWEEN STR 26L AND 25L AT STA 1460. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF PIT FRAME AND INSTALLED DOUBLER REPAIR. THIS ALSO INCLUDES DAMAGE NEAR STR 26L-25L. REPAIRED WITH SMC022.

Part: WIRE — BROKEN (CABIN) · airframe 64,584 hrs · 18,644 cycles

TWO EEL EXIT IDENTIFIERS HAVE BROKEN WIRES. REPLACED 2 EA EEL IDENTIFIERS, 1 EA SEAT ROW 15 LT AND RT. OPS CHECKS GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 64,584 hrs · 18,644 cycles

TWO EEL EXIT IDENTIFIERS HAVE BROKEN WIRES. REPLACED 2 EA EEL IDENTIFIERS, 1 EA SEAT ROW 15 LT AND RT. OPS CHECKS GOOD.

Part: FITTING — CRACKED (L4 DOOR) · airframe 64,584 hrs · 18,644 cycles

MAIN CABIN L-4 DOOR TORQUE BOX AREA, AT BS 1645 AND STR 11L, EMERGENCY POWER ASSIST CABLE MECHANISM FITTING CRACKED. REPLACED EMERGENCY POWER ASSIST CABLE MECHANISM FITTING.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,584 hrs · 18,644 cycles

AFT PIT FRAME DENTED STA 1540 AT STR 25R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,584 hrs · 18,644 cycles

AFT PIT FRAME DENTED STA 1540 STR 22R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF PIT FRAME AND INSTALLED DOUBLER REPAIR.

Part: CIRCUIT BREAKER — BROKEN (EMERGENCY ESCAPE) · airframe 64,584 hrs · 18,644 cycles

CIRCUIT BREAKER P6C5 "EMER ESCAPE SYS" IS BROKEN. REPLACED P6 C5 CIRCUIT BREAKER FOR EMERGENCY ESCAPE SYSTEM. CONTINUITY CHECKS GOOD. OPS CHECKS GOOD.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,584 hrs · 18,644 cycles

AFT PIT FRAME DENTED STA 1420, STR 25L TO 24L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,584 hrs · 18,644 cycles

AFT PIT FRAME DENTED STA 1580, STR 26R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,584 hrs · 18,644 cycles

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

Part: FRAME — DENTED (FUSELAGE) · airframe 64,584 hrs · 18,644 cycles

AFT PIT FRAME DENTED STA 1520 AT STR 21L - 22L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED FRAME SECTION AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,584 hrs · 18,644 cycles

AFT PIT FRAME DENTED AT STA 1500, STR 25L TO 24L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF PIT FRAME AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,584 hrs · 18,644 cycles

AFT PIT FRAME DENTED STA 1360, STR 25R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED A DOUBLER REPAIR.

Part: GATE — CORRODED (R4 DOOR) · airframe 64,584 hrs · 18,644 cycles

DOOR 4R LWR GATE CORRODED. INSTALLED NEW GATE.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,584 hrs · 18,644 cycles

AFT PIT FRAME DENTED STA 1340, STR 25L TO 24L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED FRAME SECTION AND INSTALLED DOUBLER REPAIR.

Part: GATE — CORRODED (L2 DOOR) · airframe 64,584 hrs · 18,644 cycles

DOOR 2L LWR GATE CORRODED. INSTALLED NEW GATE.

Part: GATE — CORRODED (L4 DOOR) · airframe 64,584 hrs · 18,644 cycles

DOOR 4L, LWR GATE CORRODED. INSTALLED NEW GATE.

Part: STRUCTURE — DAMAGED (R2 DOOR) · airframe 64,584 hrs · 18,644 cycles

DOOR 2R NEEDS REPAIR DOUBLER UPPER HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: STRUCTURE — DAMAGED (L2 DOOR) · airframe 64,584 hrs · 18,644 cycles

DOOR 2L NEEDS REPAIR DOUBLER AT UPPER HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: VIDEO UNIT — SMOKE (CABIN) · airframe 64,554 hrs · 18,634 cycles

SMOKE DETECTED AT MID GALLEY LAV. SMOKE COMING OUT OF VIDEO SYSTEM CONTROL UNIT DURING PREFLIGHT. STOPPED WHEN POWER TURNED OFF. REPLACED VIDEO CONTROL UNIT. OP CHECKS OKAY.

Part: FLAPPER VALVE — DAMAGED (CABIN PRESSURE) · airframe 64,445 hrs · 18,604 cycles

CREW REPORT: COCKPIT TEMP 90F - CABIN NORMAL. PRESSURIZATION IRREGULAR ON DESCENT DUE TO EXISTING PROBLEM. CABIN CLIMBED TO 8000FT. FOUND CONDITIONED AIR CHECK VALVE FLAPPER DAMAGED. REPLACED FLAPPER.

Part: IDG — MALFUNCTIONED · airframe 64,267 hrs · 18,558 cycles

RIGHT GEN DRIVE LIGHT NOT ILLUMINATED AT GATE. REPLACED IDG, ALL OPS CHECKS NORMAL.

Part: FILTER — FAULTY (RECIRC SYS) · airframe 64,129 hrs · 18,520 cycles

MUSTY SMELL IN CABIN. WHILE TROUBLESHOOTING FOUND LEFT FILTER NEW AND ALL DUCTS CLEAN. RIGHT RECIRC FILTER IS FAULTY. REPLACED RT RECIRC FILTER.

Part: GIRT BAR — OBSTRUCTED (L2 DOOR) · airframe 64,027 hrs · 18,495 cycles

DOOR 2L WILL NOT ARM. FOUND LANYARD CAUGHT IN GIRT BAR. STOWED LANYARD. DOOR OPERATES NORMALLY.

Part: SCAVENGE PUMP — LEAKING (ENGINE OIL) · airframe 63,892 hrs · 18,457 cycles

OILY ODOR NOTICED ON DESCENT. SCAVENGE PUMP SEAL LEAKING. REPLACED G-B OIL SCAVENGE PUMP REPLACED LUBRICATION AND SCAVENGE PUMP ACCOMPLISHED LT PACK BURNOUT PER SVC TIP 79-00-95. OPERATION AL AND LEAK CHECK GOOD. OIL ODOE NO LONGER PRESENT AT ANY POWER SETTING. REACTIVATED HIGH STAGE BLEED.

Part: LIGHT — FAULTY (CABIN) · airframe 63,826 hrs · 18,439 cycles

NO SLIDE LIGHTS ON FWD DOORS. REPLACED LIGHT ASSEMBLY INDICATOR. ALL OKAY.

Part: SHUTOFF VALVE — FAULTY (APU) · airframe 67,491 hrs · 19,483 cycles

APU BLEED VALVE WON'T OPEN. REMOVED AND REPLACED APU SHUTOFF VALVE. OPS AND LEAK CHECKED GOOD.

Part: FAN — ODOR · airframe 63,621 hrs · 18,381 cycles

SMELL OF OIL IN CONDITIONED AIR IN DESCENT UNTIL ENGINE SHUTDOWN AT GATE. *S/D* RAN BOTH ENGINES AT IDLE AND HIGH POWER, WITH PACKS ISOLATED. NO SMOKE OR FUMES NOTED PER FIM 21-00-01. NOTED MUSTY ODOR WITH LEFT RECIRCULATION FAN, REPLACED FILTER, OPS CHECKED GOOD.

Part: LANYARD — UNSECURE (DOOR SLIDE) · airframe 63,365 hrs · 18,307 cycles

DOORS 2L AND 2R WON'T ARM. *S/D* LANYARD LOOSE, CAUSING INTERFERENCE. SECURED LANYARD, DOOR ARMS/DISARMS NORMALLY.

Part: PRESSURE SWITCH — FAULTY (HYD PTU) · airframe 63,305 hrs · 18,288 cycles

POWER TRANSFER UNIT STATUS MSG DISPLAYED. PRESSURE SWITCH S10246 FAULTY. REPLACED PRESSURE SWITCH S10246, OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (ROWS 8 - 13) · airframe 63,256 hrs · 18,272 cycles

EMERGENCY EXIT LIGHT ROW 8-13 INOP. EEL STRIP DAMAGED. REPLACED EEL STRIP AT ROWS 12 AND 13, OPS CHECKED GOOD.

Part: GIRT BAR — OBSTRUCTED (L2 DOOR) · airframe 63,188 hrs · 18,255 cycles

THE 2L WILL NOT ARM. DEBRIS UNDER GIRT BAR. CLEANED DEBRIS FROM UNDER GIRT BAR. DOOR ARMS/DISARMS NORMALLY.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 63,107 hrs · 18,229 cycles

CABIN ALTITUDE CONTROL PANEL WHEN SELECTED TO MANUAL "AUTO OFF" LIGHT DOES NOT COME ON. CONTROLLER IS FAULTY. REPLACED CABIN PRESSURE SELECTOR AND AUTOMATIC PRESSURE CONTROLLER 2. OPS CHECK OK.

Part: ACTUATOR — FAULTY (NR 2 ENG SVA) · airframe 62,276 hrs · 17,991 cycles

LOWER EICAS R ENG PRI CONT WARNING ILLUM. FOUND NR 2 ENG SVA FAILURE. REPLACED NR 2 ENG SVA

Part: CONTROLLER — FAILED (WINDSHIELD HEAT) · airframe 61,238 hrs · 17,707 cycles

RETURNED TO FIELD DUE TO A CRACKED WINDSHIELD. FOUND HEAT CONTROLLER FAILED CAUSING OVERHEATING OF WINDSHIELD, CRACKING. REPLACED WINDOW HEAT CONTROLLER AND FO'S WINDSHIELD.

Part: SENSOR — FAULTY (A/C PACK) · airframe 61,098 hrs · 17,668 cycles

FLIGHT DIVERTED DUE TO PACK PROBLEM. RIGHT PACK TEMP INDICATOR FAILURE. REPLACED RT PACK TEMP SENSOR NR 2, NO REPEATS.

Part: ENGINE — OIL CONSUMPTION · airframe 60,655 hrs · 17,538 cycles

OIL CONSUMPTION TRENDING UP.

Part: UNKNOWN — UNKNOWN (GENERATOR) · airframe 59,977 hrs · 17,337 cycles

RTFL DUE TO A GENERATOR PROBLEM. EICAS MESSAGE FOR RIGHT GENERATOR DRIVE DISPLAYED WHILE CLIMB OUT AT 10000 FT. THE ROOT CAUSE OF THIS ACTION BY THE PILOT WAS DUE TO ILLUMINATION OF GENERATOR DRIVE LIGHT AS A RESULT OF A DISCONNECTED GENERATOR DRIVE.

Part: LANYARD — MISLOCATED (R1 DOOR) · airframe 59,876 hrs · 17,307 cycles

DOOR 1R WAS HARD TO ARM. A CHORD WITH A HOOK IS ON THE GALLEY FLOOR.

Part: ARMING LEVER — OBSTRUCTED (R1 DOOR SLIDE) · airframe 59,610 hrs · 17,236 cycles

UNABLE TO ARM 1R SLIDE. FOUND AN OVEN TIMER KNOB LODGED IN AND OBSTRUCTING ARMING OF SLIDE. REMOVED OBJECT AND DOOR 1R SLIDE ARMS GOOD.

Part: LANYARD — OUT OF POSITION (R1 DOOR SLIDE) · airframe 59,531 hrs · 17,210 cycles

GIRT BAR WILL NOT ENGAGE DOOR 1R.

Part: SLIDE — LOW PRESSURE (DOOR) · airframe 53,655 hrs · 15,562 cycles

LOW BOTTLE PRESSURE. [SUP 06-06-07] NO LEAK FOUND, WATER TESTED FOR 15 MIN. TOPPED OFF BOTTLE PRESSURE AND LET SIT FOR 24 HOURS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,784 hrs · 16,993 cycles

DOOR R1 EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. [SUP 06-06-07] REPLACED BATTERY PACK.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 58,432 hrs · 16,893 cycles

EEL STRIP AT MID LAV INOPERATIVE. SECURED EEL CONNECTION. OPS CHECK GOOD.

Part: ENGINE — INOPERATIVE (NR 1) · airframe 58,196 hrs · 16,827 cycles

DIVERTED FLIGHT DUE TO LOSS OF NR 1 ENGINE. LEFT ENGINE FAILED INFLT FL330 N2 ZERO OIL PRESSURE. ENGINE WINDMILLING INSPECTION. CREW REPORTED ENGINE WINDMILLED FOR 40 MINS WITH ZERO OIL QTY INDICATED. CONDUCTED OIL FILTER AND MAG PLUGS INSP AND NO CONTAMINATION WAS FOUND. FILTER REPLACED. REPLACED EEC ALTERNATOR AND STATOR. ROOT CAUSE ATTRIBUTED TO A FAILED ROTOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,149 hrs · 16,510 cycles

EEL LIGHTS INOP FROM MID LAV TO ROW 16. TROUBLESHOT INOPERATIVE EEL LIGHT, FOUND BAD CONNECTION - SECURED SAME.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,149 hrs · 16,510 cycles

EEL LIGHT INOP AT SEATS 10 DEF AND 34 DEF BULLNOSE. LAMP WAS FUSED. REPLACED LAMP.

Part: IRU — FAILED (COCKPIT) · airframe 56,395 hrs · 16,299 cycles

CTR IRS FAULT LT ON TAXI . SWAPPED RIGHT AND CENTER NAV UNITS TO HELP WITH TROUBLESHOOTING. THE UNIT ON RIGHT POSITION WAS FOUND TO BE NOT WORKING, THE UNIT IN CENTER POSITION WAS WORKING. REPLACED RT IRU. ACP ALL TESTS AFTER THAT, ACFT RESORTED BACK TO CAT 3 STATUS.

Part: HOUSING — LEAKING (SLIDE GAUGE)

THE GAUGE BOTTOM HOUSING WAS LEAKING.

Part: ODOR — DETECTED (CABIN) · airframe 53,244 hrs · 15,451 cycles

RETURN TO FIELD DUE TO SMOKE AND ELECT SMELL IN CABIN. FOUND RIGHT RECIRC FAN INOP LIGHT ILLUMINATED. REPLACED FAN, OPS CHECK OK.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 46,301 hrs · 13,462 cycles

LEFT FUSELAGE SKIN IS DAMAGED AT BS 760 TO BS 780, BETWEEN STR 15L AND 16L. MAJOR REPAIR ACCOMPLISHED. JETWAY DAMAGE. EXISTING DOUBLERS REMOVED AND AREA, NDT INSPECTED. NO DEFECTS NOTED. PERMANENT DOUBLER REPAIR INSTALLED.

Part: SENSOR — FAILED (LAVATORY 'K') · airframe 41,361 hrs · 12,093 cycles

FIRE IN THE LEFT AFT LAV UNDER THE SEAT SHROUD. LIQUID LEVEL SENSOR FAILED INTERNALLY CAUSING A FIRE THAT DAMAGED THE SENSOR ITSELF ALONG WITH THE TOILET SEAT SHROUD AND A NEARBY AIR VENT. REPLACED LIQUID LEVEL SENSOR, TOILET SHROUD, AND VENT ASSEMBLY AND RETURNED LAVATORY TO SERVICE.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 40,792 hrs · 11,955 cycles

AFT CABIN PRESSURE DECK CORRODED STATION 1680 TO STA 1683, RBL 42 TO RBL 53. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND TRIPLER REPAIR.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 40,792 hrs · 11,955 cycles

AFT PRESSURE DECK STA 1692 RBL 5.5 & STA 1694 RBL 7.25 CORRODED. MAJOR REPAIR ACCOMPLISHED. BLENDED CORROSION AND INSTALLED DOUBLER REPAIR.

Part: TRACK — DAMAGED · airframe 40,792 hrs · 11,955 cycles

RH IB SEAT TRACK FLANGE DOME NUT MISSING AND HOLE ELONGATED. STA 1050, RBL 24. MAJOR REPAIR ACCOMPLISHED.INSTALLED REPAIR ANGLE ON SEAT TRACK FLANGE.

Part: FRAME — DAMAGED · airframe 40,792 hrs · 11,955 cycles

FRAME INNER FLANGE DAMAGED. STA 1640 AT FLOOR BEAM. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER REPAIR.

Part: BEAM — CORRODED · airframe 40,792 hrs · 11,955 cycles

CABIN FLOOR BEAM UPPER CAP CORRODED. STA 365 RBL 10 - RBL 40. MAJOR REPAIR ACCOMPLISHED.INSTALLED SPLICE AND ANGLE REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,792 hrs · 11,955 cycles

CABIN FLOORBEAM CORRODED, STA 310, RBL 40 TO 44. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,792 hrs · 11,955 cycles

FUSELAGE SKIN DENTED, STA 583 STR 26R TO 27R. MAJOR REPAIR ACCOMPLISHED. TRIPLER REPAIR INSTALLED.

Part: FRAME — GOUGED (FUSELAGE) · airframe 40,792 hrs

AFT PIT FRAME GOUGED, STA 1500, RBL 13. MAJOR REPAIR ACCOMPLISHED. INSTALLED INTERNAL DOUBLER STRAP REPAIR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 40,792 hrs · 11,955 cycles

CABIN FLOOR CREASE BEAM WEB CORRODED, STA 742, RBL 62. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM WEB.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 40,792 hrs · 11,955 cycles

DOOR 2R CUT OUT CREASE BEAM IB CHORD CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED IB CHORD OF CREASE BEAM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,792 hrs · 11,955 cycles

AFT PIT FUSELAGE FRAME CORRODED, STA 1520, STR 27L. MAJOR REPAIR ACCOMPLISHED. INSTALLED INTERNAL ANGLE REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,792 hrs · 11,955 cycles

CABIN FLOOR BEAM CORRODED ON UPPER SURFACE OF CAP, STA 324, RBL 8 STR 17R. MAJOR REPAIR ACCOMPLISHED. INSTALLED TWO NESTED ANGLES BELOW UPPER CAP WITH FILLER.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 40,792 hrs · 11,955 cycles

CREASE BEAM INBOARD CHORD STA 733-755, LBL 63 STR 17L CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED INNER CHORD.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 40,792 hrs · 11,955 cycles

AFT SIDE OF FRAME OB CREASE BEAM TEE ANGLE CRACKED IN RADIUS, STA 902-903, STR 17R. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLES.

Part: CLIP — CRACKED (FUSELAGE) · airframe 40,792 hrs · 11,955 cycles

FRAME CLIP AT STA 1300 STR 21L CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW CLIP.

Part: WEB — CORRODED (STA 968) · airframe 40,792 hrs · 11,955 cycles

RH MID CABIN STA 968.5 TO 969.5 RH CREASE BEAM WEB UPPER SURFACE CORRODED. MAJOR REPAIR ACCOMPLISHED.REPLACED CREASE BEAM WEB.

Part: SEQUENCE VALVE — FAILED (NLG) · airframe 37,619 hrs · 11,076 cycles

UNABLE TO RETRACT GEAR DOORS. NOISE CONFIRMED GEAR DOORS NOT UP. CYCLED GEARS, NO HELP. FOUND NOSE GEAR DOORS WOULD NOT CLOSE. REPLACED NOSE GEAR DOOR SEQUENCE VALVE.

Part: SPUR GEAR — FAILED (COOLING FAN) · airframe 34,662 hrs · 10,295 cycles

APU INOP. SUPPLEMENTAL DATA UPDATE REPLACED APU. FOUND STARTER AND COOLING FAN IDLER DRIVE GEAR BROKEN IN GEARBOX. GEARBOX HOUSING HAS DAMAGE AND WILL PROBABLY BE SCRAPPED.

Part: IDG — FAILED (LT GENERATOR) · airframe 33,505 hrs · 10,005 cycles

LEFT GENERATOR FAILED 10 MINUTES AFTER DEPARTURE. *S/D* REPLACED IDG. SHOP FINDINGS, THE ROTOR FAILED TEST. UPON FURTHER TESTING AN OPEN CIRCUIT WAS FOUND IN THE EXCITER ROTOR. ALSO, THE UNIT WAS FOUND TO BE LEAKING AT THE TERMINALS. THE TERMINAL SEALS WERE REPLACED ALONG WITH THE ENTIRE ROTOR ASSEMBLY.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,448 hrs · 9,987 cycles

FUSELAGE DENT AT FS 760 AND STR 15. DAMAGE MEASURES 3 INCHES LONG, 1.75 INCHES WIDE AND .187 INCHES DEEP. SUPPLEMENTAL DATA UPDATE SKIN, CHANNEL, AND STRINGER WERE REPAIRED PER STRUCTURAL REPAIR MANUAL.

Part: ENGINE — MALFUNCTIONED (NR 2)

THE NR 2 ENGINE WAS SHUTDOWN ON CLIMB-OUT DUE TO LOSS OF POWER AND HIGH EGT. AIRCRAFT RETURNED TO ABQ. PROBABLE ROOT CAUSE FOUND TO BE THE DISPATCH OF THE AIRCRAFT PER MEL PROCEDURES WITH EEC MAINTENANCE SWITCH IN THE AUTO POSITION AND THE SECONDARY CHANNEL IN CONTROL. WHILE GOING THROUGH 22K FEET THE EEC HAD AN IN-RANGE SECONDARY PB SENSE FAILURE. THIS TRIGGERED A SERIES OF EVENTS THAT RESULTED IN AN ENGINE EGT OVERTEMP. THIS WAS JOINTLY INVESTIGATED BY SFOEP AND UA FLIGHT SAFETY, WITH ASSISTANCE FROM PWA AND BOEING. THE ENGINE WAS REPLACED.

Part: PANEL — DEFECTIVE (DOOR 1 L)

EMERGENCY EVACUATION GOING OFF WITHOUT BEING SELECTED. *S/D* REPLACED PASSENGER COMPARTMENT EMERGENCY EVACUATION SIGNAL PANEL AT DOOR 1L, CHECKED OK.

Part: ENGINE — BIRD STRIKE (LEFT)

AIRCRAFT RETURNED TO FIELD DUE TO A LEFT ENGINE BIRD STRIKE. *S/D* BORESCOPED HPC 6TH, 11TH, 15TH AND 17TH STAGE, FOUND NO LIMITING DISTRESS. REPLACED FOUR DAMAGED FAN BLADES AND THEIR PAIRS. ENGINE RUN VIBRATION CHECKED OK.

Part: DOOR — NOT LATCHED (LT SLIDE DOOR)

RETURNED TO BOS DUE TO LEFT OVERWING SLIDE DOOR INDICATION. *S/D* INSPECTED PER MM 25-65-00 AND FOUND SLIDE DOOR AFT LATCH NOT LOCKED. RESET ROUND CRANK HANDLE AND SLIDE DOOR LATCHES PER MM 25-65-00.

Part: BEARING — FAILED (RT ENGINE)

DIVERTED TO LAS DUE TO AN OIL INDICATION LIGHT ON THE RIGHT ENGINE. *S/D* METAL WAS FOUND IN THE MAIN OIL FILTER AND ON ALL CHIP DETECTORS. THIS WAS CAUSED BY A FAILED BUMPER BEARING. ENGINEERING HAS CREATED TASKS TO REPLACE THE BUMPER BEARINGS.

Part: SWITCH — FAILED (CABIN)

AIRCRAFT RETURNED TO GATE AFTER EMERGENCY LIGHTS AFT OF WING CAME ON, THEN WENT OUT. REPLACED SWITCH AT DOOR 4L AND TESTED OK.

Part: STRAP — MISSING (3R DOOR)

DOOR 3R MISSING D-RING ATTACH STRAP FOR SURVIVAL KIT. *S/D* REPLACED ATTACH STRAP.

Part: SLIDE — CUT (1 R DOOR)

DURING SHOP OVERHAUL OF SLIDE REMOVED FROM DOOR 1R FOR TIME EXPIRATION, A CUT WAS FOUND ON THE SLIDING SURFACE. SLIDE/RAFT WAS SENT TO THE VENDOR FOR REPAIR.

Part: FUEL CONTROL — MALFUNCTIONED (LT ENGINE)

TOP OF DESCENT, LEFT ENGINE VALVE LIGHT ACTIVATED. NO RESPONSE WITH THROTTLE MOVEMENT. RESTARTED LEFT ENGINE. DURING SHORT FINAL APPROACH AGAIN NO RESPONSE FROM LEFT ENGINE. TAXIED TO GATE ON ONE ENGINE. O-RINGS USED TO SEAL THE MINIMUM PRESSURE SHUTOFF VALVE (MPSOV) AGAINST THE FUEL CONTROL HOUSING WERE DAMAGED. FCU WAS REPLACED. OPERATION CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT AND AISLE EMERGENCY ESCAPE LIGHTS OPERATION INTERMITTENT. REPLACED BATTERY PACKS M10817 AND M10818, OPERATION CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS AT DOOR 3L AND FLOOR LIGHTS AT ROWS 16 THROUGH 23, 32 THROUGH 38, CYCLE ON AND OFF INTERMITTENTLY. REPLACED M10818 BATTERY CHARGER AND BATTERY PACK, OPERATION CHECKS NORMAL.