N550UA

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 85,023 hrs · 24,447 cycles

RT ENG SN 726726 HAD AUDIBLE COMPRESSOR STALL DURING ENG START AT STARTER CUT OUT AT APPROXIMATELY 47 -48%. VISUALLY INSPECTED NR 2 ENG CHIP DETECTORS & PERFORMED BORE INSPECTION OF ENG VIA PLUGS AP 2 & AP 8. NO ABNORMALITIES FOUND BY INSPECTION.

Part: ENGINE — OVERTEMP (RIGHT) · airframe 85,023 hrs · 24,447 cycles

RIGHT ENG SN 726726, DURING ENG START EGT EXCEEDED START LIMITS, MAX EGT FROM EXCEEDANCE PAGE REPORTED TO BE 552 FOR ONE SECOND IAW JRH 2-5-62 FIG 1. EXCEEDANCE IS IN AREA A WHICH REQUIRES VISUAL INSPECTION IAW AMM 72-00-00 PAGE 686U PARA 16. PERFORMED VISUAL INSPECTION OF NR 2 ENG INTAKE & EXHAUST SECTIONS. FOUND NO ABNORMALITIES.

Part: SKIN — DENTED (FUSELAGE) · airframe 84,304 hrs · 24,271 cycles

DENT IN FUSELAGE SKIN REPAIR BS 775 & 2" ABOVE STRINGER 17L. REMOVED EXISTING FUSELAGE SKIN REPAIR BS 775 ABOVE STRINGER 17L. TRIMMED ADDITIONAL DAMAGE & INSTALLED NEW REPAIR DOUBLER & TRIPLER BETWEEN BS 743 - 786 & STRINGER 14L - 18L IAW ECRA 5300-01917 AS AN INTERIM REPAIR.

Part: REPAIR — DENTED (FUSELAGE) · airframe 84,304 hrs · 24,271 cycles

DENT IN FUSELAGE SKIN REPAIR BS 775 & 2 INCHES ABOVE STRINGER 17L. REMOVED EXISTING FUSELAGE SKIN REPAIR BS 775 ABOVE STRINGER 17L. TRIMMED ADDITIONAL DAMAGE & INSTALLED NEW REPAIR DOUBLER & TRIPLER BETWEEN BS 743 - 786 & STRINGER 14L - 18L IAW ECRA 5300-01917 AS AN INTERIM REPAIR. INTERIM REPAIR REQUIRES ADDITIONAL FAA APPROVAL BEFORE 5-23-2016.

Part: SKIN — DENTED (FUSELAGE) · airframe 84,304 hrs · 24,271 cycles

DENT IN FUSELAGE EXTERIOR REPAIR BS 608.5 & 1 IN BELOW STRINGER 16L. REMOVED EXISTING REPAIR DOUBLER AT BS 608.5, STRINGER 16L. INSTALLED NEW REPAIR DOUBLER AT BS 596 - 620 & STRINGER 15L - 18L. THIS IS A CAT A REPAIR. THE SKIN REPAIR BETWEEN BS 596 - 620 & STRINGER 15L - 18L RECEIVED 1ST & 2ND APPROVAL. THE INSPECTION THRESHOLD FOR THIS REPAIR IS 50100 PTC A NEW FAA APPROVAL FINDING COMPLIANCE WITH 14CFR 26 .43 D & 25.571 IS REQUIRED BEFORE THE ACFT REACHES 50,100 PTC FOR THE ACFT TO REMAIN AIRWORTHY AFTER THAT TIME. CONTACT ENGINEERING AFTER ACFT COMPLETES 48100 BUT BEFORE 49100 PTC FOR DISPOSITION IAW ECRA 5331-01892.

Part: ALTIMETER — FAULTY (COCKPIT) · airframe 84,303 hrs · 24,270 cycles

2 ELEC ALTIMETER FLUCTUATES WITH NORMAL OR ALTERNATE STATIC SELECTED. POS, 01=CAPT, 02=F-0. FO ALTIMETER STICKS WHEN CLIMBING & JUMPS WHEN LEVEL. SWITCHED ADC, NO HELP. REPLACED FO`S ALTIMETER IAW MM34-13-01, OPERATIONS CHECKED GOOD.

Part: RADIO ALTIMETER — MALFUNCTIONED (COCKPIT) · airframe 83,434 hrs · 24,056 cycles

CTR RADAR ALTIMETER FLAG CYCLES INOPERATIVE. RESET CTR RADIO ALTIMETER, OPERATION TESTED OK IAW MM 34-33-00.

Part: BPCU — FAULTY (ELECTRICAL SYS) · airframe 83,384 hrs · 24,044 cycles

CREW REPORTED THAT 1.5 HRS INTO FLT, FLT ATTD REPORTED NO PWR TO AFT GALLEY. AT 2.0 HRS INTO FLT BOTH LT & RT UTILITY BUSSES TRIPPED OFF. IAW FIM CREW CYCLED UTILITY BUS SWITCHES ALL PWR RESTORED & OPERATIONS NORMAL. REPLACED BPCU IAW MM24-41 -03, SHOOK OUT WIRES BEHIND BPCU, RAN ENGS & LOADED GALLEY BUSSES. UNABLE TO DUPLICATE UTILITY BUS TRIP. RAN RECIRCULATING FANS ALSO.

Part: RELAY — FAULTY (LT ENGINE) · airframe 83,276 hrs · 24,019 cycles

LT ENG PROBE HEAT STATUS MESSAGE. IAW FIM 30-34-00 & WDM 30-34-11 PG 2. REPLACED RELAY K10337 LT ENG OUT RELAY, MESSAGE CLEAR, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,273 hrs · 24,018 cycles

EMERGENCY EXIT LIGHT STRIP IN FRONT OF AFT LAVATORY INOPERATIVE, ONE STRIP ONLY. ONE LIGHT STRIP ONLY IN FRONT OF AFT LAVATORY INOPERATIVE REST ILLUMINATE OKAY. REPLACED LIGHT ASSEMBLY, CHECKED OK.

Part: RELAY — FAILED (LT ENGINE) · airframe 83,273 hrs · 24,018 cycles

LT ENG PROBE HEAT STATUS MESSAGE. REPLACED K10308. IDLE RUN BOTH ENGS FOR 10 MINUTES. NO STATUS MESSAGES DISPLAYED.

Part: FEEDER CABLE — FAULTY (CABIN) · airframe 83,239 hrs · 24,010 cycles

EMERGENCY EXIT LIGHT FROM SEAT 37 - 40 & BY FWD AFT LAVATORY DOES NOT WORK. REPLACED FEEDER CABLE & LIGHT STRIP EMERGENCY EXIT LIGHT FROM SEAT 37-40 WORKS. THE STRIP BY THE AFT FWD LAVATORY DOES NOT WORK. DEFERRAL FOR LAST LIGHT ASSEMBLY MADE IAW MEL3351C.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,239 hrs · 24,010 cycles

EMERGENCY EXIT LIGHT STRIP IN FRONT OF AFT LAVATORY INOPERATIVE. ONLY ONE LIGHT STRIP IN FRONT OF AFT LAVATORY INOPERATIVE, REST ILLUMINATE OK PARTS 560-0806 36262-4.

Part: STATUS MESSAGE — ACTIVATED (COCKPIT) · airframe 83,231 hrs · 24,006 cycles

PWR XFER UNIT STATUS MESSAGE. COMPLIED WITH MEL 3161B. PLEASE FOLLOW FIM 29-22-00, FIG 104 FOR TROUBLE SHOOTING PURPOSE.

Part: CONTROLLER — FAULTY (BLEED AIR SYS) · airframe 83,162 hrs · 23,990 cycles

LT ENG BLEED AIR SURGES AT LOW POWER SETTINGS, WILL NOT OPEN ENG ANTI ICE AT IDLE. DUCT PRESS. REPLACED NR 1 ENG HIGH STAGE PILOT CONTROL. RAN ENG, OPERATED NORMAL. OPERATIONS CHECK OF ENG ANTI ICE VLV CHECKED GOOD.

Part: BLEED VALVE — MALFUNCTIONED (APU) · airframe 83,156 hrs · 23,989 cycles

APU BLEED VLV CYCLES CLOSED UNCOMMANDED.

Part: HYDRAULIC LINE — CRACKED (THRUST REVERSER) · airframe 83,011 hrs · 23,951 cycles

HYD PUDDLE UNDER NR 2 ENG PYLON SAIL TAIL. HYD FLUID DROPS COMING FROM SAIL TAIL. FOUND NR 2 ENG REVERSER HYD RETURN LINE WITH A 1-16" CRACK IAW ITEM 935 IPC 29-11-51-046, BUT ITEM NUMBER NOT LISTED. REPLACED NR 2 ENG REVERSER HYD RETURN LINE PN 316N3100-35. ROUTED CRACKED LINE TO SHOP 322. R & R TAG R92864, INSTALLED NEW LINE & SECURED. LEAK CHECKED GOOD.

Part: FILTER — DEFECTIVE (APU) · airframe 83,010 hrs · 23,950 cycles

APU BLEED AIR SURGES. REPLACED APU SURGE VLV ELEMENT FILTER IAW AMM, OPERATIONS CHECKED NORMAL.

Part: LIGHT — LOOSE (CABIN) · airframe 82,996 hrs · 23,947 cycles

EMERGENCY LIGHT STRIP ON FLOOR NEAR 1B IS LOOSE & COMING UP. SECURED LIGHT STRIP BY ROW 1AB, OK FOR SERVICE.

Part: BLADE — NICKED (NR 2 ENGINE) · airframe 82,996 hrs · 23,947 cycles

NR 2 ENG FAN HAS A DIME SIZE KNICK. IAW MM72-31-02 FOR ALLOWABLE DAMAGE LIMITS. BLENDED NR 3 BLADE & NR 2 ENG IAW AMM 72-31-02, BLEND WITHIN AMM LIMITS.

Part: PUMP — FAULTY (FUEL SYSTEM) · airframe 82,957 hrs · 23,937 cycles

LT AFT BOOST PUMP LOW PRESS LT ON, SW ON, EICAS MESSAGE LT AFT FUEL PUMP DISPLAYED. CB OUT. REPLACED LT AFT BOOST PUMP IAW 28-22-03, LEAK & OPERATIONS CHECKED OK.

Part: STRAP — MISSING (SLIDE RAFT) · airframe 82,823 hrs · 23,905 cycles

'D' RING STRAP MISSING FROM SLIDE AT DOOR 1L. REPLACED DOOR 1L SLIDE RAFT IAW AMM, OPERATIONS CHECKED GOOD.

Part: ISOLATION VALVE — FAILED (LT ENGINE) · airframe 82,806 hrs · 23,900 cycles

DURING RT ENGINE START, APU DUCT PRESSURE AT 10 PSI, CYCLED LT ENGINE BLEED, PRESSURE RECOVERED BUT AT RT ENGINE START GETTING MAX 15% N2 WITH APU PNEU PRESSURE. REPLACED ISOLATION VALVE IAW MM, ACP TWO NORMAL STARTS.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 82,307 hrs · 23,773 cycles

LT ELEV PCU STATUS. UNABLE TO CLEAR MESSAGE. CYCLED BREAKERS, CYCLED ALT HYD SWITCHES & RAN ELEVATORS. MESSAGE DID NOT CLEAR, APPLIED MEL 2721D. PARTS 643-9091 MR27314 C1283/SFO/03OCT.

Part: COVER — UNSECURE (CABIN) · airframe 82,207 hrs · 23,747 cycles

EMERGENCY FLOOR LIGHTING BY FWD CLOSET IS COMING UP. SECURED THE EMERGENCY EXIT LIGHT COVER FIRST CLASS CLOSET.

Part: RELAY — FAULTY (APU INLET) · airframe 81,930 hrs · 23,677 cycles

AUXILIARY POWER UNIT DOOR STATUS MESSAGE AFTER AUXILIARY POWER UNIT STARTED AFTER LANDING. VERIFIED THAT DOOR DOES NOT BIND. DOOR OPERATIONS CHECKED OK. ERASED BITE MEMORY. REPLACED RELAY K 176 AUXILIARY POWER UNIT INLET DOOR RELAY IAW WWDM 49-61-14. OPERATIONS CHECKED GOOD.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 81,892 hrs · 23,667 cycles

THE CAPTAINS O2 MASK HARNESS SECURING HOSE HAS AIR LEAK. SWAPPED O2 MASK WITH 1ST OBSERVERS SEAT. 1ST OBSERVERS SEAT INOPERATIVE IAW MEL. CAPTAIN'S MASK OPERATION CHECKED. PN 649-0148, REPLACED 1ST OBSERVERS MASK ASSEMBLY.

Part: BLEED AIR SYS — MALFUNCTIONED (APU) · airframe 23,585 hrs · 23,585 cycles

AFTER LT ENGINE START, APU PRESSURE DROPPED TO ZERO. REPLACED APU CHECK VALVE IAW MM 49-11-00. LEAK CHECKED, RAN ENGINES TWICE AT 5 MINUTE IDLE RUN VERIFIED NO EICAS MSGS, ALL INDICATIONS NORMAL.

Part: BULB — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 81,425 hrs · 23,550 cycles

LT WING EMERGENCY EXIT LIGHT ON STROBING. REPLACED BULB.

Part: MICROPHONE — BROKEN (COCKPIT) · airframe 81,430 hrs · 23,551 cycles

F/O MICROPHONE BROKEN. REPLACED.

Part: WIRE — BROKEN (MIC JACK) · airframe 81,177 hrs · 23,486 cycles

F/O'S HAND MICROPHONE INOPERATIVE. FOUND BROKEN WIRE AT HANDSET JACK, REPAIRED, OPS OK.

Part: CLAMP — BROKEN (APU DUCT) · airframe 80,968 hrs · 23,435 cycles

LEFT SIDE APU FLEX DUCT INBD CLAMP BROKEN. INSTALLED NEW CLAMP, LEAK CHECKED OK.

Part: LIGHT — UNKNOWN (CABIN) · airframe 80,961 hrs · 23,432 cycles

EXIT LIGHT FLICKERS AT ROW 21A. COULD NOT DUPLICATE ON GROUND. ACCOMPLISHED OPS TEST IAW AMM. EMERGENCY EXIT SIGNS ALL WORK NORMALLY.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 80,961 hrs · 23,432 cycles

APU AUTO SHUTDOWN. FOUND APU OVERSERVICED CAUSING HOT OIL TEMP. SERVICED OIL TO PROPER LEVEL, OPS GOOD.

Part: SENSOR — FAULTY (COCKPIT TEMP) · airframe 80,923 hrs · 23,421 cycles

FLIGHT DECK TEMP SLOWLY RISES TO HOT WITH FLIGHT DECK TEMP SWITCH IN AUTO. OK IN OFF POSITION. SUP: USED OPTION 1 TURNED OFF TRIM SWITCH AND OFF LIGHT ON TRIM VALVE AT 00. REPLACED DUCT AIR TEMP SENSOR AND OPS CHECKED.

Part: WINDOW FRAME — LOOSE (R2 DOOR) · airframe 80,862 hrs · 23,407 cycles

WINDOW ON 2R DOOR HAS LOOSE FRAME. SECURED DOOR WINDOW FRAME.

Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 80,642 hrs · 23,347 cycles

HYD LEAK IN 'C' SYS. REPLACED O-RING OTBD SPOILER RIGHT SIDE, OPS CHECKED. LEAK CHECK NORMAL NR 12 SPOILER.

Part: SKIN — DENTED (BS 1710 S13-14R) · airframe 77,426 hrs · 22,482 cycles

AFT FUSELAGE SKIN DENTED BS 1710, S13-14R. DENT FOUND TO BE OUT OF LIMITS PER SRM 53-00-01. CUT OUT DAMAGED AREA AND FABRICATED A REPAIR DOUBLER AND FILLER IAW REO G12472, REV B AND EVA 72079. MAJOR REPAIR.

Part: HANDSET — DEFECTIVE (INTERPHONE) · airframe 80,549 hrs · 23,319 cycles

FLIGHT CREW INTERPHONE INOP AT DOOR 4. NEED NEW HANDSET. REPLACED FAIL HANDSET, OPS CHECK GOOD.

Part: PRESSURE SWITCH — FAULTY (HYDRAULIC SYS) · airframe 80,439 hrs · 23,289 cycles

AFTER PUSH AND ENG START CENTER HYD PUMP 2 PRESS LIGHT ILLUM WITH SWITCH ON (DEFERRED PER SAMC). REPLACED PRESSURE SWITCH PUMP 2 CENTER, PER AMM, OPS CHECK OKAY.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 80,433 hrs · 23,288 cycles

EEL STRIP FLEX LAMP SECTION DISCONNECTED AT SEAT 12ABC. REPORTED BY FLIGHT CREW. SECTION OF EEL LIGHT FLEX LAMP PER MM. OPS CHECKED NORMAL.

Part: COVER — UNSECURE (EMERGENCY LIGHT) · airframe 80,112 hrs · 23,204 cycles

EMERGENCY LIGHT NEAR CLOSET AT 1L NOT SECURE. SECURED LIGHT COVER, OPS GOOD.

Part: MINITEL — MALFUNCTIONED (COCKPIT) · airframe 79,978 hrs · 23,168 cycles

CAPTAIN'S AUDIO INOPERATIVE. REPLACED BOTH MINITELS, OPS CHECK OKAY.

Part: SWITCH — FAULTY (POWER TRANSFER) · airframe 79,885 hrs · 23,146 cycles

AFTER LANDING, RECEIVED A POWER TRANSFER UNIT STATUS MESSAGE . FOUND PTU INDICATION SWITCH FAULTY. REPLACED SWITCH PER AMM. OPS AND LEAK CHECKED GOOD. NO EICAS MESSAGE DISPLAYED.

Part: EEC — MALFUNCTIONED (RT ENGINE) · airframe 79,770 hrs · 23,113 cycles

RIGHT ENGINE PRI CONT EICAS MESSAGE AFTER START. CREW CONTACTED TOMC. EPCS PAGE SHOWED P PMA-EEC. FAULT WAS ERASED PER TOMC DIRECTION AND DID NOT RETURN WITH ALTERNATE POWER APPLIED TO EEC. UNABLE TO RESTART ENGINE DUE TO APU BLEED ISSUE. NO FAULTS NOW SHOWN ON EPCS PAGE. RAN ENGINE PER MEL, RIGHT ENGINE PRI CONT MESSAGE STILL DISPLAYED. REPLACED EEC PER MM, OPS CHECKED OKAY.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 79,497 hrs · 23,046 cycles

EMERGENCY LIGHT COVER LOOSE. SECURED COVER.

Part: COVER — LOOSE (CABIN) · airframe 79,493 hrs · 23,045 cycles

EMERGENCY EXIT FLOOR LIGHT PROTECTIVE COVER STARTING AT SEAT 8C LOOSE. SECURED EEL PLASTIC LIGHT COVER.

Part: ACTUATOR — LEAKING (SHUTOFF VALVE) · airframe 79,465 hrs · 23,037 cycles

FUELER REPORTED THAT CENTER TANK WOULD NOT ACCEPT FUEL. RIGHT MANUAL FUEL VALVE LEAKING AT MANUAL SHUT OFF KNOB WILL TIGHTEN TO STOP LEAK. VALVE NOT SAFETIED. REPLACED RIGHT CENTER FUELING SHUTOFF VALVE ACTUATOR PER MM.

Part: COMPUTER — FAILED (FCC) · airframe 79,270 hrs · 22,990 cycles

FCC FAIL AFTER SOL REPLACEMENT. WENT BACK WRUNG OUT SERVO FROM FCC. ALL RES CHECKED GOOD SOL CHECKED GOOD NOW. FAILED C F CC ON TEST 7. REPLACED CTR FCC COMPUTER PER MM. RECHECKED PASSES TEST 7 NOW.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 79,205 hrs · 22,973 cycles

OXYGEN MASK DEFECTIVE AT2.(1=CAPT,2=1ST OFF,3=1ST OBS) CREW COMMENTS: F/O OXYGEN MASK HARNESS BLOWN, LEAKS. REPLACED F/O OXYGEN MASK.

Part: PANEL — FAULTY (COCKPIT) · airframe 79,113 hrs · 22,949 cycles

F/O VHF RADIO RIGHT HAS LOUD SIDE TONE. FOUND F/O'S ASP AT FAULT. REMOVED AND REPLACED SAME AMM, OPS CHECKED OK.

Part: RELAY — FAULTY (CARGO DOOR) · airframe 79,103 hrs · 22,946 cycles

FWD CARGO DOOR WILL NOT CLOSE ELECTRICALLY. REPLACED NR 1 CARGO DOOR HINGE PDU LOWER RELAY REF WDM. OPS CHECK OKAY.

Part: LANYARD — UNSECURE (L2 DOOR) · airframe 78,947 hrs · 22,897 cycles

ARMED INDICATOR NOT LIGHTING UP DOOR 2L. SECURED LOOSE LANYARD SLIDE LIGHT AND ARM DISARM, FUNCTION CHECK OKAY.

Part: HSI — MALFUNCTIONED (COCKPIT) · airframe 78,933 hrs · 22,892 cycles

CAPT'S LOWER DISPLAY INTERMITTENTLY BLANKS OUT COMPLETELY THEN RE-APPEARS MAYBE LOOSE CONNECTION. REPLACED CAPT EHSI PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,936 hrs · 22,894 cycles

NO SLIDE ARMED LIGHT 2L. RELAMPED, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 78,925 hrs · 22,889 cycles

THE 2L SLIDE ARM LIGHT INOPERATIVE. REPLACED LIGHT, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EVAC SLIDE) · airframe 78,925 hrs · 22,889 cycles

THE 2L SLIDE ARM LIGHT INOPERATIVE. REPLACED LIGHT, OPS CHECKED GOOD.

Part: LIGHT — UNSECURE (CABIN) · airframe 78,920 hrs · 22,887 cycles

EMERGENCY EXIT FLOOR STRIP FWD CLOSET MISSING. RE-SECURED FLOOR EEL LIGHT, OPS NORMAL.

Part: ACTUATOR — FAILED (OUTFLOW VALVE) · airframe 77,875 hrs · 22,605 cycles

OUTFLOW VALVE FAILS IN MANUAL MODE. NO DOOR MOVEMENT. VERIFIED 28VDC AT PLUG D2338 WITH SWITCH IN CLIMB OR DESC POS. NEEDS NEW ACTUATOR. REMOVED & REPLACED OUTFLOW VALVE ACTUATOR ASSY. OPS CHECKED GOOD.

Part: BOTTLE — LOW PRESSURE (OVERWING SLIDE) · airframe 77,794 hrs · 22,582 cycles

RIGHT OFFWING SLIDE BOTTLE PRESSURE READS ZERO PSI. REPLACED RT OFF WING SLIDE BOTTLE.

Part: BATTERY — FAULTY (MAIN) · airframe 77,801 hrs · 22,585 cycles

MAIN BATTERY CHARGER STS MSG. REPLACED MAIN BATTERY, ALL INDICATIONS NORMAL.

Part: SLIDE — UNWANTED DEPLOY (RT OVERWING) · airframe 77,794 hrs · 22,582 cycles

RIGHT OVERWING SLIDE DEPLOYED. REMOVED, REPLACED RT OFF WING SLIDE BOTTLE PER AMM AND INSTALLATION OF RT SLIDE BOTTLE. REPLACED RT OFF WING SLIDE ASSY PER AMM.

Part: SLIDE — UNWANTED DEPLOY (RT OVERWING) · airframe 77,794 hrs · 22,582 cycles

RIGHT OVERWING SLIDE DEPLOYED. REMOVED & REPLACED RT OFF WING SLIDE ASSY PER AMM.

Part: MODULE — FAULTY (RIGHT) · airframe 77,685 hrs · 22,556 cycles

CREW REPORTS STAB TRIM EICAS MSG. REPLACED RT STAB TRIM POSITION MODULE PER MM, OP CHECKED OK. PERFORMED MCDP GND TEST 65 STAB TRIM OP CHECKED OK. PERFORMED MCDP GND TEST 30 PER MM 22-00-03 FIG 117, OP CHECKED OKAY.

Part: CLAMP — UNSECURE (WASTE LINE) · airframe 77,464 hrs · 22,495 cycles

BLUE WATER LEAKING FROM A PLUG LEFT SIDE OF NOSE UNDER FORWARD LAV. SECURED THREE LOOSE CLAMPS ON F-C LAV DUMP LINE. FILLED AND DUMPED LAV A FEW TIMES, NO LEAKS.

Part: FRAME — DAMAGED (BS 231.25) · airframe 77,426 hrs · 22,482 cycles

FRAME AT BS 231.25 DAMAGED. REPAIRED FRAME IAW PD 57-53-013 AND ECRA 5213-01044. MAJOR REPAIR.

Part: SUPPORT BEAM — WORN (NR 2 NACELLE) · airframe 77,426 hrs · 22,482 cycles

NR 2 ENGINE INBD FAN COWL SUPPORT BEAM INSTALLATION WEB WORN. REPAIRED NR 2 ENG INBD ENG COWL SUPPORT WEB IAW ECRA 5450-01968. MINOR REPAIR.

Part: FIREWALL — WORN (NR 1 NACELLE) · airframe 77,426 hrs · 22,482 cycles

NR 1 ENGINE PYLON FIREWALL OTBD SIDE FAN COWL SUPPORT BEAM INSTALLATION WEB WORN. COMPLETED REPAIR OF NR 1 ENGINE PYLON FIREWALL OTBD SIDE AT PPS 125 IAW EA 57-54- 001 AND ECRA 5450-01966.

Part: WEB — CORRODED (BS 1360 S27L) · corrosion level 2 · airframe 77,426 hrs · 22,482 cycles

AFT CARGO BAY BILGE AREA WEB AT BS 1360 STR 27 LT HAS CORROSION, FABRICATED AND INSTALLED NEW WEB PER SRM 53-60-04 AND 51-40-05.

Part: SHEAR TIE — CORRODED (BS 1320 S27-28L) · corrosion level 2 · airframe 77,426 hrs · 22,482 cycles

SHEAR TIE CORRODED AT BS 1320 BETWEEN STRINGERS 27 AND 28L, AFT CARGO BAY. REMOVED AND REPLACED SHEAR TIE IAW SRM. MAJOR REPAIR.

Part: SHEAR TIE — CORRODED (BS 1350 S27-28L) · corrosion level 2 · airframe 77,426 hrs · 22,482 cycles

SHEAR TIE CORRODED AT BS 1320 BETWEEN 27 AND 28L IN AFT CARGO. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-40-02. MAJOR REPAIR

Part: WEB — CORRODED (BS 1360 S27L) · corrosion level 2 · airframe 77,426 hrs · 22,482 cycles

AFT CARGO BAY BILGE AREA WEB AT BS 1360 STR 27L HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: FABRICATED AND INSTALLED NEW WEB.

Part: SKIN — DENTED (BS 1595 S15-16R) · airframe 77,426 hrs · 22,482 cycles

FUSELAGE SKIN DENTED BS 1595 STR 15-16R. EVALUATED DENT AND FOUND OUT OF SRM LIMITS. CUT OUT DAMAGE AND ACCOMP NDT OF CUT OUT AND OPEN HOLES COMMON TO REPAIR REF NDTM 51-00-19 (PART 6). FABRICATED AND INSTALLED EXTERNAL DOUBLER REPAIR REF SRM 53-00-01 REPAIR NR 3. MAJOR REPAIR.

Part: SKIN — DENTED (BS 1595) · airframe 77,426 hrs · 22,482 cycles

FUSELAGE SKIN DENTED BETWEEN BS 1600-1620 AT STR 15R-16R. DENT LOCATION AT 1510, APPROX DENT CORRECTLY LOCATED AT BS 1595. CORRECTED LOCATION DUE TO ERROR DURING INITIAL EVALUATION. EVALUATED DENT AND FOUND OUT OF SRM LIMITS. CUT OUT DAMAGE AND ACCOMP NDT OF CUT OUT AND OPEN HOLES COMMON TO REPAIR REF NDTM 51-00-19 (PART 6). FABRICATED AND INSTALLED EXTERNAL DOUBLER REPAIR REF SRM 53-00-01 REPAIR NR 3.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 77,426 hrs · 22,482 cycles

FLOORBEAM AT BS 1640 CORRODED AT BL 0. REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF SRM LIMITS. REMOVED FLOORBEAM UPPER TEE FROM LBL 9.5 TO RBL 68. ACCOMPLISHED NDT OF TRIMMED EDGE AND EXISTING FASTENER HOLES AND HOLES COMMON TO REPAIR. NO CRACKS FOUND. FABRICATED AND INSTALLED REPAIR TEE, FILLERS AND ANGLES REF ECRA 5360- 01205. MAJOR REPAIR

Part: FLOORBEAM — CORRODED (BS 1340) · corrosion level 2 · airframe 77,426 hrs · 22,482 cycles

FLOORBEAM AT BS 1640 CORRODED AT BL 0. REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF SRM LIMITS. REMOVED FLOORBEAM UPPER TEE FROM LBL 9.5 TO RBL 68. ACCOMPLISHED NDT OF TRIMMED EDGE AND EXISTING FASTENER HOLES AND HOLES COMMON TO REPAIR. NO CRACKS FOUND. FABRICATED AND INSTALLED REPAIR TEE, FILLERS AND ANGLES REF ECRA 5360-01205. MAJOR REPAIR

Part: DOOR — OUT OF POSITION (OXYGEN MASKS) · airframe 77,426 hrs · 22,482 cycles

A & K LAV O2 MASK DOORS DID NOT OPEN DURING MASK DROP. CONNECTED QUICK DISCONNECT FOR A LAV O2 MASK DOOR. REPOSITIONED O2 MASK DOOR OF K LAV BOTH LAV O2 MASK DOORS OPEN IAW MM.

Part: FLOOR SKIN — CORRODED (BS 1700-1718) · corrosion level 2 · airframe 77,426 hrs · 22,482 cycles

CORROSION ON PRESSURE DECK AT BS 1700 - 1718 AT RBL 50. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. ACCOMPLISHED HFEC PER NTM, NO DEFECTS NOTED. FABRICATED AND INSTALLED DOUBLER PER ECRA 5360-01206 AND PEMCO EA PT57-53-012.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,426 hrs · 22,482 cycles

AFT CARGO COMPARTMENT STA 1620, STR 28L - 29L FRAME CORRODED. REMOVED FASTENERS AND SHEAR TIE PER SRM, REMOVED CORROSION PER SRM, ACCOMPISHED NDT FOR MAT THICKNESS PER NTM. ORIG THICKNESS .063, REMOVED .004" TO .059"; WITHIN LIMITS PER SRM, TREATED AND PRIMED PER SRM. RE-INSTALLED SHEAR TIE AND FASTENERS PER SRM.

Part: SKIN — DENTED (FUSELAGE) · airframe 77,426 hrs · 22,482 cycles

EXTERNAL FUSELAGE DENTED AT BS 681 AND STRINGER S-26L. MAJOR REPAIR ACCOMPLISHED. REMOVED GOUGE FROM DENT & FOUND DAMAGE OUT OF SRM LIMITS. CUT OUT DAMAGE AND ACCOMPLISHED HFEC OF CUT-OUT & OPEN HOLES COMMON TO THE REPAIR. NO CRACKS. FABRICATED & INSTALLED EXTERNAL DOUBLER & FILLER REPAIR REF SRM 53-00-01 REPAIR 3.

Part: SKIN — DAMAGED (BS 680 S25L) · airframe 77,426 hrs · 22,482 cycles

FUSELAGE SKIN AT BS 680 STR 25L HAS RIVET DAMAGED BY LIGHTNING STRIKE. REPAIR ACCOMPLISHED IAW SRM REPAIR 3. FABRICATED & INSTALLED EXTERNAL DOUBLER AND FILLER REPAIR.

Part: SKIN — DAMAGED (BS 681 S26L) · airframe 77,426 hrs · 22,482 cycles

FUSELAGE SKIN DENTED AT BS 681 STRINGER 26L. REMOVED GOUGE FROM DENT & FOUND DAMAGE OUT OF SRM LIMITS. CUT OUT DAMAGE AND ACCOMPLISHED HFEC OF CUT-OUT & OPEN HOLES COMMON TO THE REPAIR. NO CRACKS. FABRICATED & INSTALLED EXTERNAL DOUBLER & FILLER REPAIR REF SRM 53-00-01 REPAIR 3.

Part: BATTERY — FAULTY (MAIN) · airframe 77,287 hrs · 22,439 cycles

MAIN BATTERY CHARGER STATUS MESSAGE AT DEPARTURE. REPLACED MAIN BATTERY AND MAIN BATTERY CHARGER PER AMM, OPS CHECK OK.

Part: LAMP — INOPERATIVE (L2 DOOR SLIDE) · airframe 77,122 hrs · 22,389 cycles

DOOR 2L ARMED, BUT SLIDE ARM LIGHT IS OFF, PER CREW. RELAMPED SLIDE ARMED LIGHT. OPS GOOD.

Part: DOOR — DELAMINATED (LT MLG) · airframe 76,867 hrs · 22,312 cycles

LEFT MLG STRUT ATTACHED LOWER DOOR, FWD OUTBOARD LOWER EDGE IS DELAMINATED 10 INCHES LONG VERTICAL AND 2 INCHES LONG HORIZONTAL ALONG LOWER EDGE, SKIN IS SPLIT ALONG EDGE. ACCOMPLISHED TAP TEST OF DELAMINATION, CLEANED AREA APPLIED TAPE IAW ECRA 5280-01485. REMOVED LT STRUT DOOR AND REPAIRED.

Part: SENSOR — FAULTED (APU BLEED) · airframe 76,711 hrs · 22,266 cycles

APU HAS LOW BLEED AIR AT ENGINE START AND SURGING. REPLACED SURGE VALVE AND LOAD COMPRESSOR INLET TEMP SENSOR PER MM. OPERATED NORMAL ON ENGINE START.

Part: ACTUATOR — FAULTY (ENGINE) · airframe 76,711 hrs · 22,266 cycles

BLEED TRACK CHECK MESSAGE WITH ASSOCIATED STATUS MESSAGES 276-22 & 276-26. CURRENTLY 2.5 BLEED SEEMS TO BE WORKING OK, JUST MESSAGES. WITHIN 50 FLT HRS, COMPLISHED TROUBLESHOOTING PER MM 71. ACCOMPLISHED NR 1 ENGINE FAULT ISOLATION FOR EPCS MESSAGES 2.5 BLEED-EEC, SVA FB, 351-25, 276- 22, AND 276-26 PER 71. NO DEFECT FOUND ON WIRING FROM EEC TO SVA AND 2.5 BLEED ACTUATOR. RESISTANCE CHECK OF SVA AND 2.5 ACT CHECKED GOOD PER 71-EPCS MSG INDEX PG 178 AND PG 180, FIG 115. ACCOMPLISHED CHECK OF 2.5 BLEED ACTUATOR LINKAGE PER MM. CHECKED GOOD. REPLACED 2.5 BLEED ACTUATOR PER MM AND ADJUSTED PER MM.

Part: CONTROL VALVE — NOISY (A/C PACK) · airframe 76,711 hrs · 22,266 cycles

LOUD AIR NOISE IN COCKPIT EVEN WITH RECIRCULATION OFF, MUCH LOUDER INFLT THAN ON GROUND. REPLACED LT PACK FLOW CONTROL AND SHUTOFF VALVE PER SERVICE TIP AND MM. LOW AND DEEP PITCHED SOUND HEARD WITH RECIRCULATION FANS OFF GONE.

Part: PANEL — UNSECURE (L1 DOOR) · airframe 76,630 hrs · 22,242 cycles

DOOR 1L ARMED WEDGE INDICATOR BINDING ON DOOR PANELING. SECURED MID DOOR TRIM PANEL SCREW FWD SIDE. NR 1 LEFT MAIN ENTRY DOOR. SLIDE ARMING FUNCTION, OPS NORMAL.

Part: SQUIB — NO TEST (LT OVRWING SLIDE) · airframe 76,625 hrs · 22,240 cycles

LEFT BOTTLE PRESSURE FOR EMERGENCY ESCAPE SQUIB FAILS TEST. REPLACED LEFT OVERWING SLIDE PRESSURE BOTTLE PER MM, PASSED SQUIB TEST. UNIT INSTALLED PER AMM AND IS NOW OPERATIONAL.

Part: TRANSMITTER — FAULTY (LE FLAP) · airframe 76,414 hrs · 22,177 cycles

T/E FLAP ASYM FSEU NR 1 SHOW LEFT FLAP TRANSMITTER WIRING FAULT. RPLC'D FLAP POSITION TRANSMITTER PER MM. TESTED TRANSMITTER PER MM. NO DISCREPANCIES NOTED. SECURED CANNON PLUG ON FLAP TRANSMITTER.

Part: EEC — FAULTY (ENGINE) · airframe 76,414 hrs · 22,177 cycles

NO REVERSE ABOVE IDLE REVERSE BOTH ENGINES. ON EPCS SHOWED P & S 2.5 BLEED-EEC, P351-25, S351-25, P350-22. CHECK WIRES FROM 2.5 BLEED TO EEC NO FAULTS FOUND. REPLACED EEC AND TESTED ON ENGINE RUN. BOTH ENGINES REVERSED AND INTERLOCK RELEASED ALLOWING REVERSE POWER.

Part: WIRE — BROKEN (HYDRAULIC SYS) · airframe 76,277 hrs · 22,138 cycles

POWER XFER UNIT MSG. WHILE LT ENG IS RUNNING PTU VLV DOES NOT SHUT. REF SYS SCHEMATIC 29-00-05. FOUND 3 BROKEN WIRES, PINS 1, 3, & 4 ON CONNECTOR D6240 FOR LT ENG HYD PRESS SWITCH. REPLACED CONNECTOR REF WDM29-22-11 PG 1. STILL NEEDS OPS CHECK. ACP OPS CHECK PER MM. CKS OKAY, RUN BOTH ENGINES, CHECKS OKAY.

Part: ECU — FAULTY (POSIT 'A') · airframe 76,226 hrs · 22,127 cycles

APU SURGES WITH SINGLE PACK OPERATION. ECU BITE INDICATES ECU FAULT. REPLACED ECU IAW MM. OPERATED BOTH PACKS ONE AT A TIME AND TOGETHER WITH NO SURGES.

Part: ARM — BROKEN (WINSHIELD WIPER) · airframe 76,169 hrs · 22,107 cycles

WINDSHIELD WIPER LINKAGE BROKEN ON FIRST OFFICER'S WINDOW. REPLACED F/O'S WIPER ARM AND BLADE IAW AMM.

Part: MODULE — FAULTY (ELEVATOR) · airframe 76,032 hrs · 22,059 cycles

STATUS MSG 'ELEV ASYM' DISPLAYED. FOUND BOTH SRM'S HAD ELV ASSY ACT FAULT BALLS (CONT OF AMIS ITEM 0322003). BOTH SRM RESET MSG BY ITSELF. PERFORM BOTH SRM TEST AND YAW DAMPER TEST AND RUDDER RATIO TEST ALL PASS, N FAULT IN HIS MCDP. GRD TEST MCDP TEST 8,65,68. ELEV SERVO, STAB TRIM, ELEV SUR TEST RESPECTIVELY PER MM. ALL TEST PASSED, DUE TO REPEAT W-U OF ELEV ASYM FAULT. SUGGEST TO REPLACE R-SRM. PCN 481-9025 FOR PRECAUTIONARY. PART ON ORDER. REPLACED R-SRM. GRD TEST PER MM 27-09-00. MCDP GRD TEST 1, 30, 65 AND 68. ALL PASSED, NO MAIN MSG OR STATUS. RETURN AC BACK TO AUTO PILOT PER MM 22-10-00 PG 203.

Part: SLIDE — DISLODGED (R3 DOOR) · airframe 75,960 hrs · 22,039 cycles

R3 DOOR SLIDE FELL DOWN ON DOOR SILL. DOOR SLIDE INSTALLED PER AMM. INSPECTED INSTALLATION PER AMM. OBSERVED ALL STEPS OF INSTALLATION FOLLOWED PROPERLY. DOOR ARMING AND DISARMING OBSERVED TO BE WORKING PROPERLY.

Part: NONE — NONE (NONE) · airframe 75,807 hrs · 21,997 cycles

DOOR 1L ENTRY HANDLE RISES INFLIGHT APPROX 2 INCHES". PERFORMED DOOR LATCHING INSPECTION PER AMM. ALL CHECKED GOOD. CHECKED DOOR LOCKING AND GIRT BAR OPERATION ALL CHECKS GOOD.

Part: CIRCUIT BREAKER — MALFUNCTIONED · airframe 75,085 hrs · 21,789 cycles

APU FLAMED OUT WHEN PACKS TURNED OFF FOR ENGINE START. RERACKED CIRCUIT BREAKER. RAN NR 1 ENGINE WITH APU, NO FAULTS WITH APU. OKAY.

Part: SKIN — DEBONDED (RT WING TE FLAP) · airframe 75,078 hrs · 21,786 cycles

OUTBOARD CORNER OF RT INBOARD TRAILING FLAP HAS A PREVIOUS REPAIR TO THE TRAILING EDGE THAT IS DISBONDED. DAMAGE IS TO THE RT MAIN FLAP INBD TRAILING EDGE FLAP. PANEL DELAM OUT OF LIMITS. REPAIR PATCH DIMENSIONS ARE 16.5" BY 8". DISBOND EXTENDS 10" FROM O/B EDGE. COMPLETED INSTALLING TE WEDGE AND PAINTED TO MATCH.

Part: CIRCUIT BREAKER — TRIPPED (FUELING VALVE) · airframe 75,034 hrs · 21,774 cycles

ACFT WILL NOT TAKE FUEL, FOUND C-B OUT A9 FUELING VALVES ON THE P34 PANEL MAIN E&E BAY. FLT DECK. P6-1 PANEL C-B E6 FOR FUELING VALVES POPPED.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 74,963 hrs · 21,747 cycles

DAMAGE FOUND LT SIDE OF FUSELAGE FWD OF DOOR 2L. APPROX STA 636 BELOW FLOOR LEVEL STRINGER S-17 DAMAGE APPROX 1.4375 X 0.875 PUNCTURE THRU SKIN. ACP INSPECTION OF SURROUNDING AREA INSIDE AND OUT, NO FURTHER DAMAGE NOTED. INSTALLED INTERIM RPR WITH ALUMINUM FOIL TAPE PER SAMC DIRECTION FOR THE PURPOSES OF NON-PRESSURIZED FERRY FLT. ACCMPL'D FUSELAGE REPAIR AT BS 636 BELOW STR 17L PER SRM 53-00- REPAIR 3. THE DAMAGE CUTOUT AREA IS WITHIN 20 INCHES OF AN EXISITING DOUBLER AND THE REQUIRED REPAIR DOUBLER THICKNESS WILL EXCEED THE MAXIMUM ALLOWABLE THICKNESS FOR A CAT 'B' REPAIR PER SRM REPAIR 3. REPAIR ACP PER UA EVA 81295.

Part: TRANSCEIVER — FAULTY (WEATHER RADAR) · airframe 74,739 hrs · 21,680 cycles

RADAR UNRELIABLE, FLIGHT DIVERTED. WX RETURNS ERRATIC ON WXR DISPLAY. CREW COMMENTS: WX RADAR NOT PAINTING ACTUAL WX. REPLACED WXR TRANCEIVER PER MM. RELOCATED ACFT TO ORD SCENIC PAD AND PERFORMED AN OPERATIONAL TEST PER MM, SYSTEM PAINTED AND TESTED NORMAL.

Part: SEAL — DAMAGED (AC BAY) · airframe 74,571 hrs · 21,626 cycles

COCKPIT AIR TEMP WENT TO 92 DEG AFTER LANDING. LOW VOLUME & HOT AIR OUT OF DUCTS. TRIM AIR & C NO. REPLACED SEAL BETWEEN REHEATER & TURBINE, SECURED AS REQ'D IN MM. RAN PACKS, NO LEAKS, LT PACK OPERATES NORMAL, COOLS COCKPIT.

Part: HOUR METER — FAILED (APU) · airframe 74,554 hrs · 21,620 cycles

APU HOUR METER IS STUCK AT 338.0. REPLACED APU HOUR METER PER MM. CHECKED OKAY.

Part: START VALVE — FAILED (LEFT) · airframe 74,554 hrs · 21,620 cycles

LEFT STARTER VALVE EICAS & LT VALVE LIGHT ON OVERHEAD PANEL DURING START. NO ROTATION WITH GOOD APU. START VALVE MUST BE MANUALLY OPENED AND CLOSED. REPLACED START VALVE, OPS CHECKED OKAY.

Part: ELEVATOR SYSTEM — MALFUNCTIONED · airframe 74,517 hrs · 21,612 cycles

CREW REPORTS ELEVATOR FEEL EICAS STATUS MESSAGE. DID NOT FIND ANY PITOT STATIC LEAKS, EICAS MESSAGE "ELEVATOR FEEL" DID NOT DISPLAY, AND STANDBY AIRSPEED INDICATOR WAS INDICATING NORMALLY. SYSTEM IS OK.

Part: SEAL — DAMAGED (SLIDING WINDOW) · airframe 74,406 hrs · 21,577 cycles

CAPT SLIDING WINDOW LEAKING AT 5 O'CLOCK POSITION. WHEN PRESSING ON GLASS NOISE PITCH CHANGES. REPLACED CAPT NR 2 WINDOW PRESSURE SEAL. APPLIED SEALANT PER MM. SEALANT APPLICATION IS CF PER MM. A/C PRESSURIZED TO 4 PSID. NO SQUEAL.

Part: WIRE — CHAFED (FUEL SYSTEM) · airframe 74,234 hrs · 21,528 cycles

WHEN FUELING BOTH DC FUEL CONTROL AND FUEL PANEL CB POPPED. RESET AND POPPED WHEN FUEL DOOR OPENED. REMOVED FUELING PANEL AND REPAIRED CHAFING WIRING BEHIND PANEL. REINSTALLED AND OPS CHECK GOOD.

Part: APU — FAULTY · airframe 74,214 hrs · 21,521 cycles

APU STARTED AND RAN NORMALLY FOR 3 MINUTES THEN QUIT AGAIN. CHIP DET AND OIL FILTER CHECKS GOOD. REPLACED APU PER AMM.

Part: SHUTOFF VALVE — FAULTY (NR 2 BLEED) · airframe 74,201 hrs · 21,517 cycles

DURING TAXI, NR 2 ENGINE BLEED WOULD NOT OPEN UP WITH DEMAND. BOOSTED ENGINE, NO HELP. NO LOW STAGE EITHER. REPLACED HIGH STAGE PILOT IN REFERENCE TO MM, NO HELP. REPLACED HPRSOV WHICH HELPED, IN REFERENCE TO MM. NO LEAKS NOTED.

Part: VALVE — UNSECURE (FUEL CELL) · airframe 73,995 hrs · 21,462 cycles

UNWANTED FUEL TO CENTER FUEL TANK DURING FUELING. SECURED BOTH CENTER TANK FILL VALVES CLOSED AND CHECKED OKAY.

Part: GCU — MALFUNCTIONED (RIGHT) · airframe 73,972 hrs · 21,454 cycles

EICAS MESSAGE RIGHT IDG TEMP SENSOR DISPLAYED AFTER PARKING AIRCRAFT FROM REPOSITIONING. BIT BPCU, MESSAGE IDG-OIL OUT BULB-WIRING, REPLACED RIGHT GCU. REPLACED RT IDG PER MM. RAN ENG, OPS CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (BLEED AIR SYS) · airframe 73,958 hrs · 21,449 cycles

L ENG BLEED LIGHT NOT ON WITH ENGINE SHUT DOWN. REPLACED PRSOV PER MM. JUMPED PINS ON CONNECTOR-STILL NO LIGHT WITH BLEED OFF. RAN ENGINE PER JRH AND FOUND DUCT PRESSURE TO READ ABOVE 15 PSI WHEN OPEN AND ZERO WHEN CLOSED.

Part: CONTROLLER — FAULTY (APU FUEL) · airframe 73,958 hrs · 21,449 cycles

ON APU START, GOT A FAULT LIGHT. CONTROLLER SHOWING FUEL SOLENOID FAULT. SOLENOID MAY HAVE TO BE ROBBED FROM FCU OR FROM APU SHOP. REPLACED APU FUEL CONTROL UNIT PER MM.

Part: MODULE — FAULTY (NR 2) · airframe 73,885 hrs · 21,429 cycles

R FLT CONT STATUS MSG. FLT CONT POWER SUPPLY 2R FAULTBALL WILL NOT RESET. REPLACED MODULE 2R AND MSG CLEARED.

Part: RIVET — DAMAGED (FUSELAGE) · airframe 73,765 hrs · 21,392 cycles

LT FUSE AT STA 680 STR 25L HAS RIVET DAMAGED BY LIGHTNING STRIKE. MAJOR REPAIR ACCOMPLISHED: REMOVED RIVET AND INSTALLED CHERRYMAX RIVET PER MM. NEEDS TO BE RE-INSPECTED AT C CHECK AND REPLACED AT HMV. ** MF7573 CREATED TO MONITOR ** MAJOR REPAIR OF FUSELAGE SKIN WITH CHERRYMAX RIVET WILL REQUIRE RII INSPECTION USING METHOD NR 2. ACP INSPECTION OF FUSELAGE SKIN REPAIR IN REF TO CF496.

Part: LINK — OUT OF TOLERANCE (NR 7 FLAP TRACK) · airframe 73,765 hrs · 21,392 cycles

NR 7 FLAP TRACK AFT FAIRING ATTACH POINT BEARINGS TO LINK ROD AND LINKAGE HAVE EXCESSIVE AXIAL PLAY - BEARINGS HAVE FAILED. REPLACED ADJUSTMENT LINK AND INSTALLED WASHER IN SUPPORT LINK.

Part: ANTENNA — DAMAGED (VHF SYSTEM) · airframe 73,765 hrs · 21,392 cycles

NR 1 VHF -UPPER- ANTENNA LEADING EDGE HAS ALL FINISH ERODES AND A CRACK FROM SIDE TO SIDE OPEN IN LEADING EDGE ABOUT .5 INCH ABOVE VENT HOLE. REPLACED ANTENNA USING GEL GASKET.

Part: PCA — FAULTY (ELEVATOR) · airframe 73,516 hrs · 21,315 cycles

P ELEV PCU STATUS MSG. TEST OK PER MEL. FOUND RIGHT CENTER SYSTEM ELEVATOR PCA FAULTING, REPLACED PCA PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,401 hrs · 20,990 cycles

EMERGENCY EXIT SIGN L809 INOP DURING TEST. REPLACED BATTERY AT M10699 REF MM. OPS CHECKED OK.

Part: FAIRING — DISCONNECTED (LT WING TE FLAP) · airframe 72,218 hrs · 20,940 cycles

LEFT WING L/E OF FLAP FAIRING OTBD OF LEFT ENG IS NO LONGER CONNECTED TO WING. INSTALLED BOLTS. FAIRING SECURE.

Part: ACTUATOR — FAULTY (ELEVATOR) · airframe 71,986 hrs · 20,874 cycles

ELEVATOR ASYMMETRY STATUS MESSAGE ON TAXI IN. REPEAT WU. RT STAB TRIM MODULE SHOWS LIMIT ASYMMETRY ACTUATOR. SAM BOX PREVIOUSLY REPLACED. REPLACED ELEVATOR ASYMMETRY ACTUATOR. OPS NORMAL.

Part: MODULE — FAULTY (POSITION 1) · airframe 71,920 hrs · 20,852 cycles

ELEV ASYM STATUS MSG CAME ON. REPLACED LEFT STCM PER 27-09-00 BECAUSE MODULE PREVIOUSLY INSTALLED HAD ALL FAULT BALLS DISPLAYED & WOULD NOT RESET. NEW UNIT TESTED OK. THEN PERFORMED AUTOPILOT ADJ TEST PER MM.

Part: MODULE — FAULTY (ELEVATOR CONTROL) · airframe 71,916 hrs · 20,851 cycles

STATUS MESSAGE: "ELEV ASYM" REPLACED STAB TRIM-AIR LOCK-ASYM-MODULE PER MM, GROUND CHECK NORMAL.

Part: CIRCUIT CARD — FAULTY (RT A/C PACK) · airframe 71,623 hrs · 20,771 cycles

RIGHT PACK FLOW CONTROL VALVE IS NOT GOING INTO HIGH FLOW, EITHER ON THE GROUND OR IN AIR MODE WITH RIGHT RECIRC FAN OFF. REPLACED RIGHT PACK FLOW CONTROL CARD.

Part: HOSE — DIRTY (RT RECIRC) · airframe 71,445 hrs · 20,711 cycles

COCKPIT AIR NOISE STILL TOO LOUD WORSE ON THE GROUND. CREW REPORTED MOST INFLIGHT NOISE COMING FROM UPPER WINDSHIELD VENTS. RT RECIRCULATION FAN IS INOPERATIVE. CLEANED SCAT HOSE AND RESEATED DIFFUSER IAW MM. ACCOMPLISHED BY AMT NR 600486 AND INSP NR Q848 ON WORKCARD NR 2377N00003.

Part: CONTROL VALVE — FAULTY (CABIN AIR) · airframe 71,433 hrs · 20,704 cycles

AIR NOISE IN THE COCKPIT IS LOUD. CFM IS 380 (SHOULD BE 375 OR LESS) AND FPM IS 4380 (SHOULD BE 3430 OR LESS). AIR CONDITIONING OUTLET DUCTS REQUIRE CLEANING. ONLY 8DB DIFFERENCE WHEN USING JUST 1 PACK. REPLACED LT FLOW CONTROL VALVE. BOTH ENGINES IDLE AND PACKS RUNNING COCKPIT 75 DB. BOTH ENGINE 1.4 EPR AND PACKS ON COCKPIT 80 DB. 1 DB DIFF WITH RT RECIRC ON. FWD LAV 77 DB. REPLACED LT PACK FLOW CONTROL VALVE.

Part: CONTROL PANEL — FAULTY (VHF AUDIO) · airframe 71,295 hrs · 20,658 cycles

LT SIDE OF CAPT VHF AUDIO PANEL DOES NOT ILLUMINATE. REPLACED CONTROL PANEL. OPS NORMAL.

Part: SYMBOL GENERATOR — FAILED (LEFT) · airframe 71,286 hrs · 20,654 cycles

REF LOG 1 FLAG TRU HEADING DISPLAYED. REPLACED LT SYMBOL GENERATOR. OPS NORMAL.

Part: SELECTOR — FAILED (CABIN PRESSURE) · airframe 71,251 hrs · 20,643 cycles

CABIN ALTITUDE CONTROL INOP IN MAN. REPLACED CABIN PRESS SELECTOR. CHECKED OK.

Part: LINE — OUT OF POSITION (R1 DOOR GIRT BAR) · airframe 70,821 hrs · 20,512 cycles

DOOR 1R DIFFICULT TO ARM AND SLOWLY CREEPS INTO DISARMED POSITION. FOUND SLIDE STATIC LINE UNDER SLIDE GRIT BAR. RESTOWED STATIC LINE IN POUCH PER SERVICE TIP. DOOR ARMS AND DISARMS PROPERLY.

Part: SERVICE PANEL — CORRODED (LAVATORY SERVICE) · airframe 70,755 hrs · 20,493 cycles

CORROSION AROUND FWD LAV SERVICE PANEL. FWD LAV SERVICE PANEL AFT INBD CORNER SEPARATED FROM FUSELAGE. INSPECTED INTERIOR AND FOUND INTERNAL STRUCTURE OF SERVICE PANEL CORRODED. NDT ON EXTERNAL SKIN SHOWS EXCESSIVE MAT LOSS DUE TO CORR RMVL. MAPPING AREA TO FORWARD TO EG. HAVE NEW PAN, MFG'G CLIPS TO INSTALL. REPAIRED IAW C7 TO WU L0364H.

Part: ACTUATOR — LEAKING (NR 5 SPOILER) · airframe 70,479 hrs · 20,422 cycles

RUNNING HYDRAULIC LEAK LT WING AT DEPT. FLUID STREAMING OUT OF INBOARD FLAP CANOE. SUSPECT NR 5 SPOILER ACTUATOR IS LEAKING. REPLACED NR 5 SPOILER ACTUATOR PER AMM. ADJUSTED PER AMM. OPS CHECK AND LEAK CHECK GOOD.

Part: CAP — MISSING (COCKPIT WINDOW) · airframe 70,460 hrs · 20,416 cycles

TWO HIGH VOLTAGE CAPS MISSING FROM COPILOT'S SLIDING WINDOW (HEAT TERMINALS). INSTALLED TAPE PER UA-EVA. CAPS TO BE REPLACED WITHIN 100 HOURS.

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 70,388 hrs · 20,400 cycles

DOOR 2R SLIDE PACK FALLING OFF. SECURED LOWER CENTER STRAP TO SLIDE COVER. DOOR OPENS AND CLOSES OK. SLIDE ARMS AND DISARMS OKAY.

Part: CONTROL VALVE — INOPERATIVE (PTU) · airframe 70,135 hrs · 20,325 cycles

POWER TRANSFER UNIT STATUS MESSAGE WILL NOT CLEAR. FOUND PTU CONTROL VALVE MOTOR NOT GOING TO OPEN POSITION. REPLACED PTU CONTROL VALVE AND PRESSURE SWITCH S10246. PTU SYS CKS OK.

Part: GENERATOR — MALFUNCTIONED (APU) · airframe 69,809 hrs · 20,238 cycles

APU WILL NOT STAY ON BUSS. REPLACED APU GENERATOR IAW MM, OPS AND OUTPUT OF GEN NORMAL.

Part: BEARING — WORN (DOOR 3R) · airframe 69,661 hrs · 20,197 cycles

DOOR 3R CANNOT CLOSE, UPPER AFT GUIDE FITTING IS DAMAGED, UPPER AFT GUIDE ROLLER HITS FITTING ON SIDE AND ROLLER IS DAMAGED. FOUND GUIDE ARM BRG WORN. REPLACED GUIDE ARM AND UPPER AFT LATCH BRG. BLENDED DMG ON GUIDE FITTING. RIGGED DOOR IAW AMM. DOOR OPERATION AND SLIDE OPERATION NORMAL.

Part: ACTUATOR — FAULTY (RUDDER TRIM) · airframe 69,529 hrs · 20,155 cycles

NO RUDDER TRIM, RTFL. REPLACED RUDDER TRIM ACTUATOR, OP CHECK NORMAL.

Part: STATIC LINE — OUT OF POSITION (EVAC SLIDE) · airframe 69,245 hrs · 20,077 cycles

DURING INVESTIGATING MED 4L LOOSE BUSTLE, FOUND SLIDE STATIC LINE LAYING ON THE FLOOR AND BUSTLE REMOVED. SECURED STATIC LINE OF DOOR 4L PER SERVICE-TIP.

Part: TRIM PANEL — FAILED (COCKPIT) · airframe 69,148 hrs · 20,050 cycles

RUDDER TRIM INDICATOR ON PEDESTAL NOT WORKING. REPLACED INDICATOR RUDDER TRIM PANEL, OP CHECKS OKAY.

Part: ACTUATOR — INTERMITTENT (RUDDER TRIM) · airframe 69,101 hrs · 20,035 cycles

RUDDER TRIM INTERMITTENT. ACTUATOR FOUND FAULTY. REPLACED RUDDER TRIM ACTUATOR. OPS CHECKS OKAY.

Part: THRESHOLD — CRACKED (CARGO DOORWAY) · airframe 68,799 hrs · 19,955 cycles

RAMP REPORTS AFT CARGO DOORWAY THRESHOLD PLATE HAS CRACK. REMOVED AFT CARGO DOORWAY THRESHOLD, WELDED CRACKS PER REPAIR SPECIFIED AND REINSTALLED THRESHOLD.

Part: SCAVENGE PUMP — LEAKING (NR 2 ENGINE) · airframe 68,659 hrs · 19,916 cycles

NR 2 ENGINE REQUIRED 8 QUARTS UPON ARRIVAL. ENG LEAK CHECK REVEALED A HOLE IN OIL PUMP CASE. REMOVING PUMP AWAITING PART, 615-9009 ON AOG K6781. REPLACED LUBE AND SCAV PUMP. RAN ENG AND ADJUSTED THE PRES TRIM VALVE. OPS ARE NORMAL.

Part: LAMP — INOPERATIVE (SLIDE LIGHT) · airframe 68,649 hrs · 19,914 cycles

1L SLIDE LIGHT WILL NOT ILLUMINATE WHEN SLIDE IS ARMED. RELAMPED, CHECKS OK.

Part: IDG — LEAKING (LEFT) · airframe 72,086 hrs · 20,902 cycles

LT ENGINE IDG OVER TEMP DRAIN LINE LEAKING ONE DROP PER SECOND STATIC. REPLACED IDG IAW MM. RAN ENGINE AT IDLE POWER FOR 5 MINUTES, OPS CKS GOOD. NO LEAKS NOTED.

Part: SENSOR — FAULTED (APU) · airframe 68,249 hrs · 19,803 cycles

APU ALTITUDE NO START. APU HANGS BETWEEN 0-22 PERCENT DURING START. 0 EGT 23 PERCENT RPM IAW APU COLD START PROCEDURE. REPLACED APU BATTERY. REQUIRES APU HIGH ALT START BEFORE ACFT CAN BE ETOPS. APU ALTITUDE NO START. APU ROTATES BUT NO EGT INDICATIONS DURING START NEED TO T-S AND RPR. R & R P2 INLET SENSOR. APU IN-FLT START FAILED AGAIN 3X. REPLACED IGNITION EXCITER AND IGNITER PLUG. DID NOT REPLACE IGNITER CABLE DUE TO NO STOCK IN BOS. OPS CK'D GOOD. INBD CREW ACCMP'D SUCCESSFUL ALTITUDE START.

Part: BEARING — CORRODED (L1 DOOR) · airframe 68,150 hrs · 19,776 cycles

MED 1L HARD TO ARM. FOUND DOOR ARM HANDLE SHAFT BEARINGS CORRODED & SEIZED. NEED 2 EA 760-1478 BEARINGS, ON AOG Y2735, 4-6 HRS TO REPLACE BEARINGS AND RE-ASSEMBLE DOOR. REPLACED BEARINGS, DOOR ARMING HANDLE BEARINGS LUBED DOOR ARMING LINKAGES OPS NORMAL.

Part: ACTUATOR — STICKING (RUDDER TRIM) · airframe 68,136 hrs · 19,772 cycles

RUDDER TRIM FAILED TO TRIM IN EITHER DIRECTION. TRIM FROZEN UNTIL CONTROL KNOB EXERCISED A LOT. FOUND RUDDER TRIM ACTUATOR STICKING. REPLACED RUDDER TRIM ACTUATOR. RUDDER TRIM. OPS CK NORMAL.

Part: ACTUATOR — FAULTY (RUDDER TRIM) · airframe 68,013 hrs · 19,736 cycles

RUDDER TRIM FAILED TO TRIM IN EITHER DIRECTION. REPLACED RUDDER AILERON PANEL. REPLACED RUDDER AILERON PANEL. RUDDER TRIM FROZEN AGAIN. REPLACED RUDDER TRIM ACTUATOR. OP CHKS NORMAL.

Part: CONTROL PANEL — FAULTY (AUTOPILOT SYS) · airframe 67,575 hrs · 19,617 cycles

MCDP SHOWS NO LAST FLT FAULTS. NO FAULTS TEST 30. PASSES TEST 04 THAT INCLUDES SELECTING THE HDG SEL SWITCH. REPLACED AFCS MODE CONTROL PANEL AND PERFORMED CAT III CHECK, OP CHECKED OKAY. ACFT OK FOR CAT III SVC.

Part: CONTROLLER — MALFUNCTIONED (NR 2 ENGINE) · airframe 67,518 hrs · 19,600 cycles

RT ENG ANALOG N2 MESSAGE ON STATUS PAGE. RT ENG BLD PSI DROPPED TO 0 FOR 5 SEC. NOW NORMAL. REPLACED NR 2 ENG PMA. COMPLETED ENGINE RUN. PER TEST 3 ALL INDICATIONS NORMAL. RT ENG ANALOG N2 MSG DIDN'T RETURN DURING OR AFTER RUN.

Part: GIRT BAR — OUT OF ADJUST (EVAC SLIDE) · airframe 67,402 hrs · 19,559 cycles

DOOR 1L WILL NOT ARM PROPERLY SLIDE PACK APPEARS LOOSE. ADJUSTED GIRT BAR, OPS CHECK OKAY.

Part: COVER — MISSING (CABIN) · airframe 67,366 hrs · 19,550 cycles

EVAC COMMAND BUTTON MISSING SAFETY COVER AT 2L. REPLACED EVAC AND THRESHOLD LIGHT ASSY AT DOOR 2L. CHECKS OKAY.

Part: SEAL — LEAKING (STARTER) · airframe 67,142 hrs · 19,477 cycles

HIGH OIL CONSUMPTION. ACP HOC AND FOUND STARTER DRIVE SEAL LEAKING. REMOVED STARTER AND FOUND INNER CAVITY SURFACE DAMAGED AND UPPER MATING SURFACE PARTIALLY MIGRATED. STARTER MODULE REPAIRED.

Part: ACTUATOR — LEAKING (AILERON) · airframe 67,050 hrs · 19,449 cycles

RIGHT WING UNDER AND NEAR RIGHT AILERON IS WET WITH HYDRAULIC FLUID. REPLACED RT WING INBOARD AILERON ACTUATOR. VERIFICATION FLIGHT CONFIRMS NORMAL OPERATION.

Part: SEAL — LEAKING (NR 2 ENGINE) · airframe 66,955 hrs · 19,421 cycles

NR 2 ENG HIGH OIL CONSUMPTION EXCEEDS LIMIT. FOUND NR 2 ENG STARTER DRIVE SEAL LEAKING. REPLACED SEAL. IDLE LEAK CHECKED GOOD.

Part: START VALVE — FAULTY (RT ENGINE) · airframe 66,804 hrs · 19,375 cycles

CREW REPORTS: DURING RT ENGINE START, NORMAL STARTER CUTOUT BUT HAD START VALVE LIGHT REMAINED ILLUMINATED, FOLLOWED FM PROCEDURE, S-DWN ENGINE. START VALVE LIGHT INOP 'D. STARTER CUTOUT NORMAL & DUCT PRESS RECOVERS NORMAL. REPLACED STARTER CONTROL VALVE, OP OK.

Part: START VALVE — FAULTY (NR 1 ENGINE) · airframe 66,629 hrs · 19,328 cycles

LT STARTER CUTOUT EICAS AND START VALVE LIGHT ON. REPLACED NR 1 ENGINE START VALVE. CHECKED AND SHOOK WIRING TO START VALVE. NO FAULTS FOUND. RAN ENGINE, ALL NORMAL. OPS CHECKED GOOD.

Part: ACTUATOR — FAULTY (RUDDER TRIM) · airframe 66,392 hrs · 19,260 cycles

RUDDER TRIM KNOB DID NOT WORK IN FLT, WORKED OK ON GND. REPLACED RUDDER TRIM ACTUATOR. OP CHECKED GOOD, NO FAULTS.

Part: FEEDER CABLE — DEFECTIVE (CABIN) · airframe 66,410 hrs · 19,265 cycles

EEL LAMP AT FWD CLOSET INOPERATIVE. REPLACED FWD CLOSET FLOOR EEL POWER FEEDER CABLE.

Part: START VALVE — FAULTY (RT ENGINE) · airframe 66,364 hrs · 19,249 cycles

WHEN STARTING RIGHT ENGINE STARTER SWT POPPED OUT OF GRND AND CB ENG RT START CONTROL POPPED. REPLACED ENGINE START VALVE. RAN ENGINE START VALVE OPERATES OK ENG RAN OK.

Part: SLIDE — UNSERVICEABLE (CABIN)

PRESSURE READING LOW. VERY SLOW LEAK AT BALL STEM O-RING. RESERVOIR ASSY WAS REPLACED WITH STOCK BOTTLE. O-RING WILL BE REPLACED AT VALVES TIME OF OVERHAUL.

Part: SLIDE — LOW PRESSURE (R3 DOOR) · airframe 65,902 hrs · 19,113 cycles

DOOR 3R SLIDE PRESSURE IN THE RED BAND. PRESSURE CHECKED TO WITHIN LIMITS. SLIDE TO BE REPLACED WITHIN 25 HOURS. REPLACED DOOR 3RH SLIDE.

Part: PUMP — FAULTY (HYDRAULIC SYS) · airframe 65,536 hrs · 19,012 cycles

CREW REPORT: CENTER ELECT 2 PUMP PRESS LIGHT ILLUMINATED. REPLACED PUMP ASSY AND PRESSURE AND CASE DRAIN FILTERS. LEAK AND OPS CHECK OKAY.

Part: FILTER — DEFECTIVE (E&E BAY) · airframe 64,933 hrs · 18,843 cycles

EQUIP COOLING EICAS MSG DURING TAXI OUT. REPLACED EQ COOLING AIR FILTER, NO MESSAGE.

Part: BYPASS VALVE — FAULTY (OIL SYSTEM) · airframe 64,658 hrs · 18,760 cycles

NR 2 ENG HOC. REPLACED FUEL OIL HEAT EXCHANGER AND BYPASS VALVE. ACCOMPLISHED LEAK CHECK OF NR 2 ENGINE FUEL OIL HEAT EXCHANGER AND BYPASS VALVE. NO LEAKS NOTED.

Part: HEAT EXCHANGER — LEAKING (NR 2 ENGINE) · airframe 64,658 hrs · 18,760 cycles

NR 2 ENG HOC REPLACED FUEL OIL HEAT EXCHANGER AND BYPASS VALVE. ACCOMPLISHED LEAK CHECK OF NR 2 ENGINE FUEL OIL HEAT EXCHANGER AND BYPASS VALVE. NO LEAKS NOTED.

Part: FLAP — MALFUNCTIONED (WING) · airframe 64,536 hrs · 18,721 cycles

FLAPS FAILED TO MOVE. T/E LIGHT ILLUMIN EICAS MESSAGE 'T/E FLAP DISAGREE' DISPLAYED. FLAPS OPERATE NORMALLY ALTERNATE SYS. REPLACED NR 2 FSEU WITH DIGITAL MODEL. ALL ADJUSTMENTS CHECK GOOD. REPLACED NR 8 FLAP TRANSMISSION AND INSTALLED NEW JACKSCREW. OPS CHECK GOOD.

Part: OIL SYSTEM — MALFUNCTIONED (NR 2 ENGINE) · airframe 64,222 hrs · 18,628 cycles

NR 2 ENGINE OIL PRESSURE LOSS. FLIGHT DIVERTED.

Part: MODULE — NO TEST (TE FLAP) · airframe 64,155 hrs · 18,604 cycles

TRAILING EDGE FLAP ASYMMETRY ON FINAL APP BETWEEN 15 & 20. FOUND THE NR 8 JACKSCREW STOP OUT OF RIG. PERFORMED A COMPLETE RE-RIG OF RT OUTBOARD FLAP. ACP FIM 27-51-60, FAILED DEPRESS MODULE OPS CHECK FOR UNCOMMANDED MOTION. REPLACED MODULE MR 27597 ON CARD 33130. HAND ROLLED FLAPS IAW FIM 27-51-00, NO BINDING NOTED THROUGH FULL RANGE OF MOTION. ACP INSP OF RT OB FWD & AFT FLAP TRACKS AND ROLLERS, NO BINDING, FLAT SPOTS OR SIGNS OF WEAR NOTED, ADJUSTED LESA & LESB (SLAT FOLLOW UP) TO IN LIMITS. ACP FLAP-SLAT RIG CHECKED ALL GOOD. CHECKED WIRING FROM FSEU-1 AND FSEU-2 (ALL GOOD). NO INDICATOR POP NOTED ON ALL TRANSMISSION OR FLAP DISAGREE MESSAGES.

Part: SUPPORT — DEFECTIVE (TE FLAP) · airframe 64,086 hrs · 18,578 cycles

FOUND "T/E FLAP TT SPRT" INBOARD BRG OUTER RACE SPINNING DURING OPS CHECK, LOCATED BETWEEN NR 5 AND NR 6 XMISSION. REPLACED TORQUE TUBE BEARING SUPPORT ASSY WITH NEW, OPS CHECK GOOD.

Part: TRANSMISSION — FAULTY (TE FLAP) · airframe 64,034 hrs · 18,567 cycles

FLAP DISAGREE ON APPROACH. FLAPS STUCK ON 20 UNITS. TROUBLESHOOT T/E FLAP DISAGREE. FOUND NR 6 FLAP TRANSMISSION OIL IS BLACK AS VIEWED THROUGH SIGHT GLASS. DRAINED AND REPLACED WITH NEW OIL. LAB ANALYSIS INDICATED ACCEPTABLE LEVELS OF CARBON COMPOUND, OK. REMOVED NR 8 TRANSMISSION BALL SCREW ASSY. INSTALLED NEW NR 8 T/E FLAP TRANS.

Part: WARNING SYSTEM — MALFUNCTIONED (TE FLAP) · airframe 64,034 hrs · 18,567 cycles

FLAP DISAGREE ON APPROACH. FLAPS STUCK ON 20 UNITS. SFOLM TUNG INSPECTED ALL OVERLOAD INDICATORS ON FLAP TRANSMISSION GEAR BOXES AND FOUND OK. OPS CHECKED GOOD IN NORMAL AND ALTERNATE MODE INCLUDING FSEU TEST.

Part: TRANSMITTER — FAULTY (TE FLAP) · airframe 64,009 hrs · 18,559 cycles

IN ALTERNATE FLAPS - INDICATORS SPLIT AT FLAPS 1. LT INDICATION MOVES TO 1 NORMALLY, RT INDICATOR JUMPS TO ABOUT 15 THEN NEEDLES STAY SPLIT UNTIL LEADING EDGES AND TRAILING EDGES GET TO POSITION 1, THEN INDICATIONS ARE WITHIN LIMITS.

Part: TRANSMITTER — INACCURATE (TE FLAP) · airframe 64,009 hrs · 18,559 cycles

IN ALTERNATE FLAPS - INDICATORS SPLIT AT FLAPS 1. LT INDICATION MOVES TO 1 NORMALLY, RT INDICATOR JUMPS TO ABOUT 15 THEN NEEDLES STAY SPLIT UNTIL LEADING EDGES AND TRAILING EDGES GET TO POSITION 1, THEN INDICATIONS ARE WITHIN LIMITS. RT FLAP AND RT SLAT O/B XMITTERS WERE BOTH SLAVED IN. T/S WIRES FROM FSEU 2 TO FLIGHT DECK ROTARY SWITCH AND ARMING SWITCHES, CKS GOOD. RELAY K10244 CHANGED. REMOVED ALL 3 FSEU 'S AT SAME TIME AND SLAVED IN KNOWN GOOD UNITS. SLAVED IN KNOWN GOOD FLAP. WIRING HAS BEEN RUNG FROM FSEU'S TO RT FLAP & SLAT, LT FLAP & SLAT AND PDU FLAP & SLAT XMITTERS. ALL ARE GOOD & COMPARABLE TO OPPOSITE SIDE. RELAY K10244 CHANGED.

Part: SKIN — DENTED (FUSELAGE) · airframe 64,006 hrs · 18,558 cycles

AFT FUSELAGE DENTED STA 1710, STR 13-14R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED AREA AND FABRICATED A REPAIR DOUBLER AND FILLER.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 64,006 hrs · 18,558 cycles

LT FORWARD OVERWING ESCAPE HATCH CUTOUT CORRODED AT LOWER FORWARD CORNER. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION AND FOUND MATERIAL REMAINING IS OUT OF LIMITS. REMOVED DAMAGE AND FABRICATED REPAIR DOUBLER AND INSTALLED.

Part: SKIN — DENTED (FUSELAGE) · airframe 64,006 hrs · 18,558 cycles

DENT ON FUSELAGE SKIN AT STA 1711 BETWEEN S15R AND S16R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,006 hrs · 18,558 cycles

CABIN STA 365, RBL 45 FLOOR SUPPORT BEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION. FABRICATED & INSTALLED DOUBLER AND SHIM REPAIR.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 64,006 hrs · 18,558 cycles

CABIN: STA 365, RBL 25 SEAT TRACK SPLICE STRAP CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRAP AND FILLER.

Part: CABLE — FAULTY (RT ESCAPE HATCH) · airframe 64,006 hrs · 18,558 cycles

RT OVERWING ESCAPE HATCH(S) OFFWING MANUAL BACKUP CABLE CHECK FAILED. REPLACED RT OVERWING EXIT PRESSURE BOTTLE MANUAL BACKUP CABLE AND ADJUSTED.

Part: CABLE — FAULTY (ESCAPE HATCH) · airframe 64,006 hrs · 18,558 cycles

RT OVERWING ESCAPE HATCH (S) OFFWING MANUAL BACKUP CABLE CHECK FAILED. REPLACED RT OVERWING EXIT PRESSURE BOTTLE MANUAL BACKUP CABLE AND ADJUSTED.

Part: SKIN — DAMAGED (FWD CARGO DOOR) · airframe 64,006 hrs · 18,558 cycles

FWD CARGO PIT DOOR SKIN AFT LWR CORNER IS CRACKED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF SKIN. INSTALLED DOUBLER & FILLER REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,006 hrs · 18,558 cycles

CRACK ON FRAME, FWD OF R-2 DOOR CUTOUT, BS 665, STR 11R. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW WEB (P/N 143N8388).

Part: SKIN — CRACKED (FWD CARGO DOOR) · airframe 64,006 hrs · 18,558 cycles

FWD CARGO PIT DOOR SKIN AFT LWR CORNER IS CRACKED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF SKIN. INSTALLED DOUBLER & FILLER REPAIR.

Part: DOOR FRAME — DAMAGED (FWD CARGO DOOR) · airframe 64,006 hrs · 18,558 cycles

FWD CARGO PIT DOOR HAS DAMAGE TO LOWER AFT CORNER. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED FRAME CORNER & INSTALLED NEW FRAME CORNER (P-N 143N6618).

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,006 hrs · 18,558 cycles

CRACK ON FRAME, FWD OF R-2 DOOR CUTOUT, BS 665, STR. 12R. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED WEB AND INSTALLED NEW WEB.

Part: GATE — CORRODED (R4 DOOR) · airframe 64,006 hrs · 18,558 cycles

DOOR 4R LWR GATE CORRODED AND MISSING PIECES. REPLACED LOWER GATE.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,006 hrs · 18,558 cycles

AFT PIT BS 1400, LT SIDE STR 24L, FRAME INBOARD FLANGE DENTED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR.

Part: STRUCTURE — OUT OF TOLERANCE (R2 DOOR) · airframe 64,006 hrs · 18,558 cycles

DOOR R2 REQUIRES DOUBLER AT UPPER HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,006 hrs · 18,558 cycles

AFT CARGO COMPT, FRAME AT BS 1500 LT AND STR 25L HAS A DENT AT INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,006 hrs · 18,558 cycles

AFT PIT BS 1420LT, STR 24L, FRAME INBOARD FLANGE DENTED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,006 hrs · 18,558 cycles

AFT PIT, BS 1440LT, STR 23-25L, FRAME INBOARD FLANGE DENTED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED FRAME SECTION AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,006 hrs · 18,558 cycles

AFT CARGO COMPT FRAME AT BS 1580 AND STR 26R HAS 2 DENTS AT FRAME INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED FRAME SECTION AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,006 hrs · 18,558 cycles

AFT CARGO COMPT, FRAME AT BS 1480 LT AND STR 26L HAS A DENT AT INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,006 hrs · 18,558 cycles

FWD PIT AT STA 600, STR 23L FRAME DENTED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 64,006 hrs · 18,558 cycles

CORROSION ON UPPER T-CAP WHERE IT ATTACHES TO RT CUSP AT BS 1640. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED & INSTALLED A NEW SECTION OF T-CAP.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 64,006 hrs · 18,558 cycles

CABIN, BS 365, RBL 30, T-CAP SPLICE CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED OLD SPLICE STRAP, FABRICATED & INSTALLED A NEW STRAP SPLICE.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 64,006 hrs · 18,558 cycles

CABIN, BS 365, RBL 5, T-CAP SPLICE CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED STRAP SPLICE. FABRICATED & INSTALLED A NEW STRAP SPLICE.

Part: BYPASS VALVE — LEAKING (WING) · airframe 63,838 hrs · 18,512 cycles

FOUND LEADING EDGE BYPASS VALVE (V10059) LEAKING, CRACKED CASTING. CRACK (FATIGUE) IN CASTING. REPLACED LEADING EDGE BYPASS VALVE.

Part: MONITOR — LOOSE (VIDEO SYSTEM) · airframe 63,453 hrs · 18,405 cycles

VIDEO MONITOR IN BACK CABIN IS LOOSE.

Part: FILTER — CLOGGED (AIR SUPPLY) · airframe 62,960 hrs · 18,266 cycles

EQ COOLING HORN SOUNDED & OVERHEAT LIGHT IS ON. *S/D* AIR SUPPLY FILTER CLOGGED, NO AIR FLOW. REPLACED FILTER AND CLEANED SENSOR, SYS CHECKED NORMALLY.

Part: GIRT BAR — FAULTY (R3 DOOR) · airframe 62,678 hrs · 18,188 cycles

DOOR 3R NOT ARMING. REMOVED SLIDE AT DOOR 3R, LUBED ARMED, DISARMED BEARINGS AND OPS CHECKED SLIDE OPERATION.

Part: BOTTLE — LEAKING (EVAC SLIDE) · airframe 62,578 hrs · 18,158 cycles

DOOR 1 LEFT SLIDE PRESSURE IS ONE NEEDLE OUT OF THE GREEN BAND. PRESSURE LEAK IN SLIDE BOTTLE. REPLACED SLIDE ASSY.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 62,367 hrs · 18,100 cycles

EXTERIOR EMERGENCY LIGHT INOP AT DOOR 4R. RELAMPED. OPS CHK'D GOOD.

Part: LANYARD — OUT OF POSITION (1R DOOR SLIDE) · airframe 61,677 hrs · 17,920 cycles

DOOR 1R WILL NOT ARM. FOUND LANYARD WRAPPED AROUND GIRT BAR. REPOSITIONED LANYARD, DOOR OPS NORMAL.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 61,234 hrs · 17,795 cycles

LEFT LAMP INOP IN FLT DECK DOOR (LOCK FAIL) INDICATOR. BULB OUT (BURNED OUT). REPLACED BULB, OPS CHECKS OK.

Part: ACTUATOR — LEAKING · airframe 61,023 hrs · 17,733 cycles

DISPATCH REPORTS LOSS OF LEFT GEN INFLIGHT. APU GEN ONLINE. RECURRED ON FLT 116-16JAN FOUND FUEL LEAK FROM NR 1 2.5 BLD ACT. REPLACED LT IDG, NR 1 ENG FUEL/OIL COOLER AND 2.5 BLEED ACTUATOR.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 59,147 hrs · 17,206 cycles

FLOOR MOUNTED EMERGENCY ESCAPE PATH LIGHT INOP AT AFT LAV. RESECURED CONNECTOR FROM LIGHT STRIP TO POWER CABLE.

Part: SENSOR — STUCK (CABIN TEMP) · airframe 58,704 hrs · 17,086 cycles

CABIN TEMPERATURE DIFFICULT TO CONTROL, CANNOT WARM UP THE CABIN & COCKPIT. INSPECTED AND CLEANED CABIN AND FLT DECK TEMP SENSORS AND EVALUATE TEMP CONTROL SYSTEM AS REQUIRED. REPAIRED LARGE AIR LEAK AT JOINT BETWEEN ACM AND PREHEATER IN LT PACK. REPLACED RT PACK AC COMP OUT SENSOR AND RT PACK TEMP SENSOR PACK OUT TEMPS NOW WITHIN LIMITS. DURING T/S FOUND RT PACK STUCK IN LOW FLOW.

Part: CHARGER — FAULTY (MAIN BATTERY) · airframe 58,509 hrs · 17,030 cycles

MAIN BATTERY CHARGER STATUS MESSAGE DISPLAYED. [06-20-07] REPLACED A FAULTY BATTERY CHARGER.

Part: BOTTLE — READS LOW (R1 DOOR SLIDE) · airframe 58,440 hrs · 17,008 cycles

LOW BOTTLE PRESSURE. WATER TESTED FOR 10 MINUTES AND NO LEAK WAS FOUND. REPLACED WITH A STOCK BOTTLE AND TOPPED OFF OLD BOTTLE AND PUT BACK IN STOCK.

Part: SKIN — CORRODED (RT WING) · airframe 58,440 hrs · 17,008 cycles

RIGHT UPPER WING SKIN HAS NUMEROUS AREAS OF EXFOLIATION CORROSION FROM FRONT SPAR TO AFT SPAR C-T FUSELAGE. [SUP 06-06-07] RT WING UPPER SURFACE AT FILLET FAIRING MATING SURFACES BETWEEN FRONT SPAR TO REAR SPAR HAS NUMEROUS AREAS BLENDED EXCEEDING SRM. WORK ACCOMPLISHED PER UA ENGINEERING EVALUATION AND RECOMMENDED REPAIR.

Part: SKIN — CORRODED (LT WING) · airframe 58,440 hrs · 17,008 cycles

LEFT UPPER WING SKIN CORRODED AT MID SPAR C-T FUSELAGE. [SUP 06-06-07] PERFORMED DETAILED VISUAL INSPECTION OF THE LT FWD TRUNNION FUSE PINS FOR LOOSE FUSE PINS AND CORROSION ON ADJACENT STRUCTURE. WORK ACCOMPLISHED PER UA ENGINEERING EVALUATION AND RECOMMENDED REPAIR.

Part: SLIDE — LOW PRESSURE (R4 DOOR) · airframe 57,400 hrs · 16,703 cycles

THE 4R DOOR SLIDE PRESSURE READS LOW. REPLACED DOOR SLIDE.

Part: PIN — INSTALLED (EVAC SLIDE) · airframe 54,457 hrs · 15,885 cycles

SLIDE SAFETY PIN WAS PREVIOUSLY INSTALLED AND NOT REMOVED BEFORE FLT. SAFETY PIN WAS ROUTINELY INSTALLED PRIOR TO RII INSPECTION OF SLIDE RAFT FOR DOOR 1R. THE SAFETY PIN WAS NOT REMOVED AS PER UA OPERATING PROCEDURE BEFORE FLIGHT. REQUIRES FURTHER TRAINING OF INVOLVED AMTS TO ENSURE SECURING PIN IN SAFETY POUCH BEFORE SLIDE RAFT INSTALLATION. DOES NOT APPEAR TO BE PROBLEM WITH HARDWARE.

Part: SKIN — DAMAGED (TE FLAP) · airframe 53,527 hrs · 15,611 cycles

RIGHT HAND TRAILING EDGE MAIN INBD FLAP HAS PREVIOUS REPAIR COMING OFF TOP SIDE OF FLAP ACCOMPLISHED INTERIM REPAIR PER EVA UA-EVA-60124 WITH NEW PATCH RIVETED AND COVERED WITH SPEED TAPE ON TOP OF INBD MIDFLAP. MUST INSPECT EVERY 3SV. PERMANENT REPAIR MUST BE MADE BY PTT 53,827 (300 FLT HRS). FLAP ROUTED TO SHOP FOR REPAIR. REMOVED UPPER RT FLAP SKIN PANEL AND REPLACED.

Part: A/C PACK — SMOKE (LEFT) · airframe 52,394 hrs · 15,281 cycles

AFTER TAKEOFF 1ST OFFICER NOTICED SMOKE FROM VENT SLIT BEHIND REAR WINDOW. COCKPIT NOTICED SMOKE & ODOR RISING FROM SIDE WINDOW VENTS DURING T-O ROLL AND C-O. TURNED OFF LEFT PACK, SMOKE DISSIPATED. NO ODOR WAS DETECTED IN MAIN CABIN. MAINTENANCE VERIFIED NORMAL PACK OPERATION. SMOKE AND ODOR WAS PROBABLY DUE TO GAS PATH WASH PERFORMED ON THE ENGINE.

Part: SMOKE — DETECTED (CABIN) · airframe 51,338 hrs · 14,950 cycles

DIVERTED DUE TO SMOKE IN THE CABIN & COCKPIT. MODERATE SMOKE AND FUMES OF ELECTRICAL TYPE IN CABIN AND COCKPIT. FLIGHT DIVERTED TO DTW. INSPECTED GALLEYS, CABIN, CARGO PITS AND BOTH E&E BAYS FOR ELECTRICAL RELATED PROBLEMS. FOUND AUDIO ACCESSORY UNIT WITH STRONG ELECTRICAL SMELL. CAPT AND FO WRITE-UP ALSO GENERATED SAYING UNABLE TO COMMUNICATE WITH FLT ATTENDANTS ON SERVICE INTERPHONE. REPLACED AUDIO ACCESSORY MR23505-59 UNIT CHECKED GOOD. TWO CIRCUIT BOARD FAILURES OCCURRED WITHIN THE AUDIO ACCESSORY UNIT. BOARD A1 HAD RESISTOR R1 AND CAPACITOR C2 FAILURE. BOARD A2 HAD A FAILURE OF RESISTOR R1. RESISTOR SPECIFICATIONS (R1) FOR BOTH BOARDS IS P/N RL42S100GTX (10 OHM 2WATT). CAPACITOR SPECIFICATION

Part: CABLE — SHORTED (EMERGENCY LIGHT) · airframe 42,321 hrs · 12,415 cycles

EEL LIGHTING OUT AT SEAT 23 TO 31. REPLACED TRACK FEEDER CABLE.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 40,617 hrs · 11,971 cycles

CABIN FLOOR STRUCTURE CHANNEL BETWEEN STATION 365.25 AND 377.7 RBL 12 STR 17R CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED CHANNEL AND INSTALLED NEW PART.

Part: FRAME — DENTED · airframe 40,617 hrs · 11,971 cycles

FWD PIT FRAME CAP DENTED. STA 540 STR 24L. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,617 hrs · 11,971 cycles

CABIN FLOORBEAM CORRODED, STA 365, RBL 6. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED SPLICE, ANGLE AND STRAP REPAIR.

Part: SHEAR TIE — CRACKED · airframe 40,617 hrs · 11,971 cycles

AFT PIT FRAME TO SKIN SHEAR TIE CRACKED. STA 1300 BETWEEN STR 20L - 21L. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW SHEAR TIE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,617 hrs · 11,971 cycles

CABIN FLOOR BEAM UPPER T-CAP CORRODED, STA 324, RBL 45. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP ANGLE REPAIR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 40,617 hrs · 11,971 cycles

LT CABIN FLOOR CREASE BEAM INBOARD ANGLE CORRODED STA 680 TO 740, DOOR 2L. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM ANGLE, STA 663 TO 754.

Part: WEB — CORRODED (FUSELAGE) · airframe 40,617 hrs · 11,971 cycles

CABIN FLOOR BEAM SHEAR WEB CORRODED, STA 1680, RBL 52. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR STA 1680 TO 1686, RBL 46 TO RBL 55.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 40,617 hrs · 11,971 cycles

FUSELAGE RT SIDE CREASE BEAM HAS CORRODED FASTENERS. STA 1420 - 1440. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM WEB.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 40,617 hrs · 11,971 cycles

FUSELAGE RT CREASE BEAM CORRODED, STA 1420. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,617 hrs · 11,971 cycles

CABIN FLOOR BEAM CORRODED, STA 1520, STR 27L. MAJOR REPAIR ACCOMPLISHED. INSTALLED INTERNAL ANGLE REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,617 hrs · 11,971 cycles

CABIN FLOORBEAM UPPER CAP CORRODED, STA 310, RBL 38, STR 17R. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR AND L-ANGLE DOUBLER.

Part: PUMP — FAILED (LT ENGINE) · airframe 39,650 hrs · 11,697 cycles

LEFT ENGINE HYDRAULIC PUMP FAILED. TOWED TO THE GATE WITHOUT INCIDENT. REPLACED PUMP, CHANGED FILTERS.

Part: VALVE — FAILED (RT ENGINE) · airframe 35,953 hrs · 10,699 cycles

REJECTED T/O AT 50 KNOTS. RIGHT ENGINE EPR ROLLED BACK FROM 1.2 TO 1.1. WHILE ACCOMPLISHING AN ENGINE RUN TO TROUBLESHOOT THE PROBLEM, AT 1.1 EPR 14TH STAGE BLEED VALVE SOUNDED LIKE IT WAS OPEN. THE 14TH STAGE CONVERTER VALVE WAS REPLACED (CONVERTER VALVE IS THE CONTROLLING ITEM FOR THE BLEED VALVE).

Part: VALVE — FAILED (LT ENGINE)

DIVERTED TO SFO DUE TO A BLEED VALVE PROBLEM. *S/D* LEFT ENGINE BLEED SYSTEM WAS CLOSING OFF DUE TO TEMPERATURE. LEFT ENGINE FAN AIR MODULATING VALVE TEMPERATURE SENSOR AND LEFT ENGINE AIR BLEED OVERTEMP SENSOR REPLACED. NO PNEUMATIC WRITE-UPS SINCE DIVERSION.

Part: DUCT — FAILED WELD (NR 2 ENGINE)

FOUND EXCESSIVE LEAK ON NUMBER TWO ENGINE PNEUMATIC SUPPLY DUCT DURING MAINTENANCE INSPECTION. *S/D* DUCT FAILED IN BALL JOINT WELD. REPLACED PNEUMATIC DUCT.

Part: INLET — BLOCKED (RT FUEL PUMP)

DURING CLIMBOUT, RIGHT FUEL PUMP ALTERNATED ON AND OFF. *S/D* INTERMITTENT PUMP OPERATION DUE TO PARTIAL BLOCKAGE OF PUMP INLET. BLOCKAGE CAUSED BY IN TANK DEBRIS.

Part: IDG — FAILED (LT ENGINE)

LEFT GENERATOR FAILED, IDG DRIVE DISCONNECTED ACCOMPANIED WITH INCREASED VIBRATION. *S/D* FOUND INTEGRATED DRIVE GENERATOR FAILED. REPLACED GENERATOR, CHECKS OK.

Part: EEL LAMP — FAILED (CABIN)

EMERGENCY EXIT LIGHT INOP AT ROW 17. RELAMPED. CHECKS O.K.