N596UA

Part: LIGHT — ILLUMINATED (L2 DOOR SLIDE) · airframe 72,625 hrs · 19,017 cycles

L2 DOOR SLIDE DISARMED, HOWEVER SLIDE LIGHT WILL NOT EXTINGUISH. CYCLED THE ARMING LEVER, LIGHT WENT OUT.

Part: TRANSMISSION — MALFUNCTIONED (TE FLAP) · airframe 72,598 hrs · 19,012 cycles

CREW REPORTS, TE FLAP DISAGREE, LT AND EICAS, WHEN SELECTING FLAPS 20 . FLAPS STUCK BETWEEN 15 AND 20 DEG. SELECTING ALT FLAPS HAD NO EFFECT. LANDED FLAPS 20 AT 170KTS. EMERGENCY DECLARED. FOUND TORQUE INDICATOR POPPED ON NR 1 FLAP TRANSMISSION. REMOVED AND REPLACED LT OUTBOUND FLAP O/B TRANSMISSION IAW AMM TASK 27-51-17-424-020. OPS CHECK GOOD.

Part: CONTACT — DIRTY (L2 DOOR SLIDE) · airframe 72,593 hrs · 19,011 cycles

L2 DOOR SLIDE LIGHT REMAINS ILLUMINATED WITH DOOR DISARMED. CLEANED CONTACT ARM AND DISARM DOOR. SLIDE LIGHT WORKED OK.

Part: LIGHT — UNKNOWN (R2 DOOR) · airframe 72,421 hrs · 18,977 cycles

#2R MED EXTERIOR EMERGENCY LIGHT INOP CYCLED A/C POWER. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,421 hrs · 18,977 cycles

#4L MED EXTERIOR EMERGENCY LIGHT INOP RELAMPED #4L EXTERIOR EMERGENCY LIGHT. OPS CHECK GOOD.

Part: LEVER — DIRTY (R4 DOOR) · airframe 72,007 hrs · 18,898 cycles

DOOR 4R WILL NOT DISARM. CLEAN AND INSPECTED DOOR 4R SLIDE DISARM LEVER IRW 52-11-00-862- 077. NO FAULTS NOTED OK TO CONTINUE.

Part: LEVER — DIRTY (R4 DOOR ARMING) · airframe 71,977 hrs · 18,892 cycles

THE R4 DOOR WILL NOT DISARM, CLEANED AND OPERATED THE DOOR SLIDE DISARM LEVER, NO FAULTS FOUND. OK TO CONTINUE

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,977 hrs · 18,892 cycles

L2 DOOR EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. REPLACED THE LAMP. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,565 hrs · 18,813 cycles

EXTERIOR EMERGENCY LIGHTS AT THE L2 AND R2 DOORS INOPERATIVE REPLACED THE LAMPS, CLEANED CONTACTS AND SECURED LAMPS. OPS CHECKED GOOD IAW AMM 33-51-06-962-001-001.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,565 hrs · 18,813 cycles

THE LEFT OVERWING EXTERIOR EMERGENCY LIGHT FOUND INOPERATIVE. REPLACED THE LAMPS AND CLEANED CONTACTS, OPS CHECKED GOOD IAW AMM 33-51-06-962-054-001.

Part: PUMP — FAULTY (NR 1 ENGINE) · airframe 71,544 hrs · 18,808 cycles

LEFT ENG VALVE LIGHT ILLUM DURING ENG START NO FUEL FLOW. REPLACED FUEL PUMP REF AMM 73-11-01. ACCOMPLISHED ACCELERATION TIME TEST REF JRH 2-5-64. TIME TEST PASSED. FUEL FLOW WAS NORMAL AT IDLE (1.09), FLT IDLE (1.49) AND 95% TO (1.39 EPR FUEL FLOW AT 13.6K). OTHER ENG PARAMETERS WERE NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,395 hrs · 18,779 cycles

DURING 2SVC FOUND EMERGENCY LIGHTS AT ROW 5-7L TO BE INOP. REPLACED SEAT 6 AND SEAT 7 P1 CONNECTORS REF SWPM 20-610-28 AND REPLACED M10567 BATTERY PACK REF AMM-33-51-07-902-001. OPS CK GOOD. ACP INSP OK FOR SVC OPS CHK GOOD REF AMM 33-51-07.

Part: OVEN — SMOKE (GALLEY) · airframe 71,273 hrs · 18,756 cycles

F/A REPORTED AFT GALLEY MIDDLE OVEN SMOKING REMOVED CONTENTS AND SECURED OVEN COMPLIED WITH A FUNCTIONAL TEST OF THE AFT GALLEY MIDDLE OVEN BOTH WITH CONTENTS IN THE OVEN AND NO CONTENTS IN THE OVEN. RAN THE OVEN FOR APPROXIMATELY FIVE MINUTES EACH TIME AND NO EVIDENCE OF SMOKE WAS DETECTED. REF AMM 25-32-98-700-801C2.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 70,996 hrs · 18,702 cycles

2L DOOR SLIDE ARMED LITE INOP. RELAMPED 2L DOOR SLIDE LIGHT. OPS CHECK NORMAL.

Part: ENGINE — FIRE (NR 2) · airframe 70,492 hrs · 18,602 cycles

DURING TAXI FLAMES WERE REPORTED TO BE EMANATING FROM THE NR 2 ENGINE TAILPIPE.. THE ENGINE WAS SHUTDOWN. EMERGENCY WAS DECLARED. PERFORMED STEP 6 & 7 FROM NTSB. PERFORMED GVI OF NR 2 ENGINE AND SURROUNDING AREA FOR EVIDENCE OF FIRE DAMAGE. FOUND NO EVIDENCE OF FIRE OR DAMAGE TO THE NR 2 ENGINE. FDR, CVR, AND SLIDES WERE REMOVED AND FDAU WAS UPLOADED TO PCMIA CARD.

Part: HANDLE — BINDING (L2 DOOR) · airframe 70,492 hrs · 18,602 cycles

AFTER EMERGENCY EVACUATION, FLIGHT ATTENDENT REPORTED THE L2 DOOR WAS DIFFICULT TO OPEN AND DEPLOY SLIDE. REPORTEDLY THE DOOR HANDLE JAMMED ABOUT 45-60 DEGREES AND DOOR WOULD NOT OPEN UNTIL FORCED TO OPEN IN WHICH THE SLIDE FINALLY DEPLOYED.

Part: DOOR — NO TEST (R2) · airframe 70,492 hrs · 18,602 cycles

AFTER EMERGENCY EVACUATION THE R-2 DOOR HANDLE JAMMED ABOUT 45 INCHES AND DOOR FAILED TO OPEN AND SLIDE FAILED TO DEPLOY. FLIGHT ATTENDENT SAID SHE TRIED THE HANDLE SEVERAL TIMES AND THE HANDLE KEPT JAMMING AT 45 INCHES AND DOOR WOULD NOT OPEN.

Part: SWITCH — DIRTY (L2 DOOR) · airframe 70,482 hrs · 18,600 cycles

DOOR 2L SLIDE LIGHT ON WITH DOOR OPEN AND DISARM CLEANED DEBRIS OF SWITCH OPS CKS NORMAL. OK TO CONTINUE.

Part: OVEN — FAULTY (GALLEY) · airframe 69,780 hrs · 18,465 cycles

MID GALLEY OVEN 507 SMOKING AND SPARKING. TURNED OFF AND SMOKE DISSIPATED. REMOVED AND REPLACED OVEN AT POS 507, OPS CK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (TE FLAPS) · airframe 68,950 hrs · 18,305 cycles

TE FLAP DISAGREE MESSAGE WHEN FLAPS SELECTED TO 20 STUCK 17. ACCOMPLISHED OPERATIONAL CHECK UP FLAP SYSTEM HYDRAULICALLY AND ALT ELECTRIC SYSTEM IAW AMM-27-51-00-715-001 AND AMM-27-51-00- 715-167. BOTH SYSTEMS OPERATED NORMALLY IAW AMM WITH NO FAULTS OR MESSAGES NOTED. NO PRIOR HISTORY.

Part: FLOORBEAM — CORRODED (BS 1682) · airframe 68,371 hrs · 18,189 cycles

CORROSION ON TOP OF MAIN CABIN FLOORBEAM AT BS 1682 RBL 48 BETWEEN PRESSURE DECK AND FLOORBEAM. REMOVED CORROSION ON TEE IAW SRM 51-10-02 PARA 15 FIG 1. TEE CAP FOUND TO BE 100% MATERIAL LOSS AND OUT OF LIMITS IAW SRM 53-00-51. REMOVED AND REPLACED UP PER TEE IAW EC/RA 5310-06 948.

Part: FLOOR SUPPORT — CRACKED (BS 1200) · airframe 68,371 hrs · 18,189 cycles

INTERCOSTAL CRACKED AT BS 1200 BL 0 AT FWD ATTACH UPPER. REMOVED AND REPLACED IAW SRM 51-40-02 PAR 4 FIG 3.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 67,247 hrs · 17,964 cycles

TRAILING EDGE FLAP DISAGREE EICAS MSG WHILE TRANSITIONING FROM 15 - 20 DEGREES. FLAPS STOPPED AT 16 - 17 DEGREES, FLIGHT LEVEL 6000 FT, 180 KTS. RAN CHECKLIST. FLAPS MOVED ELECTRICALLY TO 20 DEGREES. UNABLE TO DUPLICATE, OPERATIONS CHECK OK IAW MM 27-51-00-501.

Part: FLAP — MALFUNCTIONED (WING) · airframe 67,247 hrs · 17,964 cycles

TE FLAP DISAGREE EICAS MSG WHILE TRANSITIONING FROM 15 - 20 DEG, FLAPS STOPPED AT 16- 17 DEG, FL 6000 FT, 180 KTS. RAN CHECKLIST, FLAPS MOVED ELECTRICALLY TO 20. ACCOMPLISHED FIM, NO DISCREPANCIES, UNABLE TO DUPLICATE. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,278 hrs · 16,806 cycles

POSITION LIGHT 2 IS OUT, 1=R WHITE, 2=R GREEN, 3=R WHITE & GREEN, 4=L WHITE, 5=L RED, 6=L WHITE & RED. OTBD GREEN NAV LT INOPERATIVE. ONE GREEN BLUB INOPERATIVE.

Part: OVEN — DIRTY (GALLEY) · airframe 61,143 hrs · 16,781 cycles

FIRST CLASS GALLEY 413 RT OVEN HAD SPILLED CARAMEL IN IT THAT CAUSED SMOKE TO FILL GALLEY, FIRE HAZARD. NEED THOROUGH CLEANING OR OVEN CHANGE. REPLACED RT OVEN IN FIRST CLASS GALLEY. OPERATIONS CHECKED OK.

Part: DOOR SEAL — LOOSE (R1 DOOR) · airframe 59,410 hrs · 16,452 cycles

1R PRESS LEAK NOISE SECURED, CLEANED & LUBED DOOR 1R SEAL. VISUALLY INSP DOOR 1R EXTERIOR, ALL NORMAL.

Part: RELAY — FAILED (FUEL SYSTEM) · airframe 59,367 hrs · 16,444 cycles

AIRCRAFT DOES NOT ACCEPT FUELING. REPLACED FUELING POWER TRANSFER RELAY K357. OPERATIONS CHECKED OKAY.

Part: CIRCUIT BREAKER — DAMAGED (EXTINGUISH SYS) · airframe 58,859 hrs · 16,347 cycles

CIRCUIT BREAKER AT HOT BATTERY BUS DC BATTERY BUS LOC H1 MISSING HALF OF CIRCUIT BREAKER. REPLACED LT ENG BTL1 CIRCUIT BREAKER IAW WDM 26-21-11 & SQUIB TESTED GOOD.

Part: FILTER — DIRTY (AC BAY) · airframe 58,473 hrs · 16,273 cycles

SMELL FROM PACKS ON TAKEOFF, DIRTY MUSTY SMELL. TURNED OFF RT RECIRCULATOR TO TRY TO CLEAR. REPLACED BOTH RECIRCULATOR FAN FILTERS IAW AMM.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 58,278 hrs · 16,235 cycles

FWD LAVATORY SMOKE DETECTOR SOUNDS CONTINUOUSLY.

Part: SMOKE DETECTOR — MALFUNCTIONED (FWD LAVATORY) · airframe 58,274 hrs · 16,234 cycles

FORWARD LAVATORY SMOKE DETECTOR SOUNDS CONTINUOUSLY. REMOVED CONNECTOR FROM SMOKE DETECTOR, COVERED PLUG IAW AWD 26-14-11 2A, D42. REPLACED DETECTOR, SYSTEM OPERATIONS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,262 hrs · 16,231 cycles

RT AFT EMERGENCY LIGHT INOPERATIVE. REPLACED LAMPS, OPS CHECKED GOOD.

Part: GENERATOR — FAULTY (APU) · airframe 58,114 hrs · 16,201 cycles

APU SHUTDOWN WHEN ELECTRICAL LOAD WAS PLACED ON. APU AUTOSHUTDOWN, DID NOT HAVE TIME TO BITE ECU. BPCU SHOWS CT LOOP GROUNDED, UNDER FREQ TRIP AND APU GEN PMC WIRING. REPLACED APU GENERATOR.

Part: HANDLE — BINDING (COCKPIT WINDOW) · airframe 57,999 hrs · 16,172 cycles

CAPTAIN`S SLIDING WINDOW HANDLE STUCK IN LOCKED POSITION. FOUND AFT WINDOW TRACK TRIM STUCK. REPOSITION TRIM. CAPTAIN SLIDING WINDOW HANDLE, OPS NORMAL. OK TO CONTINUE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,928 hrs · 16,150 cycles

DURING 2 SVC, FOUND LT OVERWING LIGHT NOT ILLUMINATED. REPLACED LAMP, CHECKED OK.

Part: LINE — UNSECURE (HYD SYSTEM) · airframe 57,510 hrs · 16,071 cycles

THREE INCH ROUND PUDDLE OF FLUID ON GROUND BETWEEN AFT TIRES RIGHT SIDE. SECURED HYD LINE TO TILT ACTUATOR ON RIGHT MAIN GEAR. PRESSURIZED HYD SYS NO ACTIVE LEAKS FOUND. ALL THREE HYD QTY'S FULL.

Part: FIRE LOOP — OUT OF POSITION (LT ENGINE) · airframe 57,298 hrs · 16,031 cycles

LEFT ENGINE FIRE LOOP 2 EICAS. REPAIR- :PERFORMED FIM 26-11-00-10 1 FOUND LOOP TOUCHING CLAMP. NO OTHER DEFECTS NOTED. BITE CHECK OK. LOOP RES 6.02K OHMS.

Part: FAN — NOISY (COCKPIT) · airframe 57,298 hrs · 16,031 cycles

AIR NOISE IN COCKPIT IS VERY LOUD. RIGHT RECIRC FAN NOISY, NEED TROUBLESHOOTING PER MAINT TIP. NO TIME, HAS HISTORY.

Part: CAP — MISSING (L2 WINDOW WIRE) · airframe 57,058 hrs · 15,985 cycles

L2 WINDOW HT WIRES-CAPS MISSING. REPLACED CAP

Part: SKIN — DAMAGED (BS 265) · airframe 57,020 hrs · 15,977 cycles

CROWN SKIN BS 265 RBL 8 AND RBL 11. REPAIRED REF ECRA 5311-01578, AND PTT 0206066.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 57,020 hrs · 15,977 cycles

FLOORBEAM BS 365 CORRODED FROM RBL 11 TO 63. INSTALLED NEW SECTION TEE REPAIR WITH ANGLE DOUBLERS PER ECRA 5310-05536 AND EA 121306 IR. MAJOR REPAIR.

Part: FRAME — DENTED (BS 1540) · airframe 57,020 hrs · 15,977 cycles

AFT CARGO BS 1540 RBL 7.5 FRAME HAS DENT UNDER FLOOR SUPPORT. CUT OUT DAMAGE ON FRAME, FABRICATED & INSTALLED DOUBLER. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 749.5) · airframe 57,020 hrs · 15,977 cycles

FUSELAGE SKIN BS 749.5 HAS SEVERAL DENTS & GOUGES. SKIN BS 750-755 STR 16L REPAIRED IAW ECRA5330-04394. MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 1220) · airframe 57,020 hrs · 15,977 cycles

AFT CARGO BAY FRAME BS 1220 ABOVE STRINGER 27R SIDE PLATE FASTENER ATTACH HOLE IS ELONGATED. FRAME REPAIRED IAW ECRA5360- 01240. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 610-630) · airframe 57,020 hrs · 15,977 cycles

FWD CARGO LOWER AFT CORNER BEAR STRAP DOUBLER CORRODED BS 610-630 S26R. REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER IAW EC RA5330-04384.

Part: SKIN — GOUGED (BS 282 S17R) · airframe 57,020 hrs · 15,977 cycles

FUSELAGE SKIN BS 282 S17R HAS A THREE INCH LONG VERTICAL GOUGE. BLENDED DAMAGE, FOUND OUT OF LIMITS PERFORMED REPAIR WITH DOUBLER IAW SRM 53-00-01 FIG 201 REPAIR 3 SHEET 4 TABLE 1, 2, 3. THIS REPAIR IS CAT B PER TABLE 4 SRM 53-00-01 REPAIR 3.

Part: FLOORBEAM — CORRODED (BS 1680) · corrosion level 2 · airframe 57,020 hrs · 15,977 cycles

CABIN FLOORBEAM BS 1680, LBL 12 HAS CORROSION. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER ECRA 5330-04259.

Part: FRAME — DAMAGED (BS 1240) · airframe 57,020 hrs · 15,977 cycles

AFT CARGO BAY FRAME BS 1240 ABOVE S27R, SIDE PLATE ATTACH FASTENER HOLE ELONGATED. CUTOUT DAMAGE AND INSTALLED L ANGLE REPAIR DOUBLER PER ECRA 5360-01239. MAJOR REPAIR.

Part: SKIN — DENTED (BS 297) · airframe 57,020 hrs · 15,977 cycles

DENT UPPER SKIN 2 6.5 INCH FWD OF BS 297. CUT OUT DENT, FABRICATED AND INSTALLED DOUBLER ON UPPER FUSELAGE SKIN AT BS 265 TO 275 RBL 4 TO RBL 16.

Part: FLOOR PANEL — DAMAGED (BS 1510) · airframe 57,020 hrs · 15,977 cycles

AFT CARGO FLOOR SPLICE EXFOLIATED AT BS 1510. REPLACED AFT CARGO FLOOR PANEL SPLICE.

Part: FLOOR SUPPORT — CORRODED (BS 680-700) · corrosion level 2 · airframe 57,020 hrs · 15,977 cycles

FORWARD CARGO BAY FLOOR SUPPORT BETWEEN BS 680 - 700 CORRODED. REMOVED, FABRICATED AND INSTALLED NEW FLOOR SUPPORT. MAJOR REPAIR

Part: DOOR — DENTED (CARGO BAY) · airframe 10,278 hrs · 2,818 cycles

AFT PIT CARGO DOOR IS DENTED ON LOWER FWD EDGE. ACCOMPLISHED HFEC REF 757 NDT PAT 6 51-00-19. CHECKED THE DENT PER 52-30-01 FOUND WITHIN LIMITS OF MM A OVER Y= 37.5 NO ACTION NEEDED OK TO ARCHIVE. AFT CARGO DOOR LWR FWD CORNER DENT REPAIRED.

Part: ATTACH FITTING — DAMAGED (FUSELAGE) · airframe 57,020 hrs · 15,977 cycles

MAJOR REPAIR AFT CARGO STA 1540 RBL 7 FLOOR SUPPORT ATTACH CLIP 146N5443-14 REQUIRES REPLACEMENT DUE TO FRAME REPAIR DAMAGE REMOVED DAMAGE SUPPORT ATTACH CLIP 146N5443-14 AT STA 1540 RBL 7. FABRICATED NEW SUPPORT CLIP IAW BOEING DWG146N5443-14, APPLIED PROTECTIVE FINISHED IAW SRM 51-20-01, INSTALLED NEW CLIP PER BOEING DWG 146N1018 & SRM 51-40.

Part: SUPPORT BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,020 hrs · 15,977 cycles

STA 1661 TO 1681 BL 0 SUPPORT P/N 146N5650-1 CORRODED. REMOVED AND REPLACED SUPPORT BEAM IAW SRM.

Part: SHUTOFF VALVE — FAILED (BLEED AIR SYS) · airframe 57,020 hrs · 15,977 cycles

NR 2 ENGINE HPSOV FAILED HEALTH CHECK ON TASKCARD 5R36I5053. 535053 REMOVED & REPLACED NR 2 ENGINE HPSOV IAW 36-11-07. PERFORMED HEALTH CHECK ON CARD 5S365S068-NO DEFECTS NOTED. PERFORMED LEAK CHECK IAW 36-11-07-NO LEAKS NOTED IAW AMM 36-11-09.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,020 hrs · 15,977 cycles

PASSENGER CABIN BS 1712 RBL 50 WL 208 UPPER SURFACE OF SUBFLOOR HAS SMALL AREA OF BARE METAL. MAJOR REPAIR ACCOMPLISHED: REMOVED CORR BY BLENDING OUT DAMAGE, OUT OF LIMITS IAW 53-00-51. REPAIRED AREA BY FAB REP AIR DOUBLER AND FILLER PER ECRA 5330-04259.

Part: FASTENER — UNSECURE (CABIN SEAT) · airframe 57,020 hrs · 15,976 cycles

THE 9ABC ENTIRE ROW OF SEATS CAME LOOSE FROM TRACK. SECURED FASTENERS AT SEAT 9ABC.

Part: CHILLER — INOPERATIVE (FWD GALLEY) · airframe 56,945 hrs · 15,955 cycles

FWD GALLEY CHILLER NR C11 INOPERATIVE. CHILLER HAS NO COOL AIR. REPLACED GALLEY CHILLER, OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (FIRE LOOP) · airframe 56,907 hrs · 15,945 cycles

LEFT ENGINE FIRE LOOP 2 EICAS. PER TOMC DIRECTION CYC CB'S B21 AND B21, NO HELP, EICAS MSG REMAINS. CLEAN ALL FIRE LOOP CONNECTORS ON NR 1 ENGINE, LEFT ENGINE FIRE LOOP 2 MESSAGE GONE. FIRE TESTED NORMAL.

Part: HYDRAULIC LINE — LEAKING (LT MLG) · airframe 56,780 hrs · 15,913 cycles

HYD LEAK, LEFT MLG TRUCK POSN PRESS LINE, HOLE IN LINE APPROX 4" FROM TOP CONNECTION. REMOVED LINE, CAPPED HYD CONNECTIONS, BAGGED AND TAGGED CLAMP ASSY HARDWARE AT LOCATIONS REMOVED. REPLACED LEFT GEAR TRUCK POSITION LINE, BLED LINE, NO LEAKS.

Part: CAP — MISSING (CABIN) · airframe 56,780 hrs · 15,913 cycles

EMERGENCY FLOOR LIGHT STRIP END CAP IS MISSING BY SEAT 1B, 8C, 11C AND 12C. INSTALLED NEW CAP AND SECURED.

Part: LINE — LEAKING (BRAKE SYSTEM) · airframe 56,746 hrs · 15,900 cycles

PIN HOLE LEAK ON LEFT GEAR NR 2 FORWARD BRAKE LINE, SOLID LINE THAT MATES TO FLEX LINE TO BRAKE ASSY. REPLACED HYD LINE (PCN 170-3680). OPS AND LEAK CHECK BRAKE SYSTEM. LEAK CHECK OKAY.

Part: WIRE — DAMAGED (LANDING GEAR) · airframe 56,721 hrs · 15,890 cycles

WIRING ISSUES. REMOVED DAMAGED WIRING AND INSTALLED NEW WIRES THRU NEW CONDUIT AND TERMINATED IN D40442P TO TB211. NEED TO SECURE CONDUIT AND CONNECTOR D40442P. SECURED CONNECTOR D40442P AND CONDUIT FROM CONNECTOR TO FWD JUNCTION BOX.

Part: FIRE LOOP — OUT OF POSITION (LT ENGINE) · airframe 56,652 hrs · 15,872 cycles

AFTER ENGINE START LEFT ENGINE FIRE LP 2 WILL NOT CLEAR. CHECKED ALL ENGINE FIRE LOOPS. REROUTED SEVERAL LOOPS THAT WERE TOUCHING METAL, MESSAGE CLEARED AND FIRE TEST GOOD.

Part: LATCH — LACK OF LUBE (COCKPIT) · airframe 56,570 hrs · 15,847 cycles

REPEAT WRITE UP. AFTER PRESSURE CYCLE, CAPTS WINDOW BINDS AND WILL NOT UNLOCK. PRESSURIZED AC, VERIFIED WINDOW HARD TO UNLATCH. LUBED LATCHES, REPRESSURIZED AC. WINDOW UNLATCHES NORMALLY AFTER PRESSURIZED AND OPENS NORMALLY.

Part: APU — FAULTY (APU BAY) · airframe 56,473 hrs · 15,824 cycles

APU FAULT FAILED TO START FIRST ATTEMPT. ACCMP'D BITE ON ECU, HAD ABORTED START. STARTER CIRCUIT FAULT. CREW STARTED APU ON SECOND TRY. START CONTACTOR, E-STARTER, START RELAY, ECU AND APU BAT CHRGR HAS BEEN REPLACED. HISTORY INDICATES THAT APU ESN 60227 WAS REMOVED FROM ACFT 5439 FOR SAME CHRONIC REASON & PASSED TEST CELL DIAG. HOWEVER PREVIOUS VISIT HAD IGV LINKAGE PROB. REPLACE APU. REPLACED APU PER TOD MM, OPS CHECK AND LEAK CHECK OKAY.

Part: CONTACTOR — FAULTY (APU) · airframe 56,455 hrs · 15,819 cycles

APU FAULT ON FIRST START ATTEMPT ECS FAULT MSG WAS "A-C START CIRCUIT". REPLACED APU CRANK CONTACTOR. REPLACED APU STARTER MOTOR. ERASED ALL FAULT MSGS ON ECS BOX AND FAULT MSG ON EICAS APU PAGE. APU STARTED SUCCESSFULLY ON 1ST AND 2ND TRIES AT GATE IN SFO.

Part: HINGE — LOOSE (R3 DOOR) · airframe 56,435 hrs · 15,812 cycles

DOOR 3R DISARMING FLAP LOOSE. REPLACED HINGE ASSY, OP CHECKS NORMAL.

Part: APU — INOPERATIVE · airframe 56,433 hrs · 15,811 cycles

APU WILL NOT START.

Part: DOOR — OBSTRUCTED (CABIN) · airframe 56,453 hrs · 15,818 cycles

DOOR 3L NOT ARMING CORRECTLY. CHECKED NR 3 ENTRY DOOR OPERATION AND ARMING AND DISARMING. DOOR FOUND TO OPERATE NORMALLY. CLEANED DEBRIS FROM DOOR ARMING AREA, DOOR OPS CHECKS NORMAL.

Part: ENGINE — FIRE (APU) · airframe 56,328 hrs · 15,781 cycles

APU IS BLOWING SMOKE OUT EXHAUST. ACFT WAS INSPECTED FOR FIRE DAMAGE. SHUT DOWN APU, HAD FIRE IN TAIL PIPE, TRIED RESTART TO BLOW OUT NO LUCK. FIRE DEPT SHOT WATER IN TAIL PIPE TO EXTINGUISH FLAMES, NO FIRE ALARM, DECIDED TO BLOW FIRE BOTTLE DUE SOME SMOKE OUT OF APU DOOR VENT AS PRECAUTION BEFORE FIRE DEPT OPENED COWLING. REMOVED AND REPLACED APU FIRE BOTTLE AND BOTTLE CARTRIDGE IAW AMM 26-22-01. SQUIB TESTED NORMAL.

Part: GIRT BAR — DIRTY (L4 DOOR SLIDE) · airframe 56,060 hrs · 15,702 cycles

DOOR 4L DOOR ARMING LEVER DOES NOT LINE UP W INDICATOR. CLEANED GIRT BAR AREA CHECKED LINKAGE REPOSITION LANYARD POS CHECKED NORMAL

Part: HEAT SHIELD — LOOSE (LT PYLON) · airframe 55,982 hrs · 15,674 cycles

LT ENG PYLON TITANIUM HEAT SHIELD RIVETS LOOSE AND HANGING OUT. REPLACED RIVETS.

Part: HEAT SHIELD — LOOSE (RT PYLON) · airframe 55,982 hrs · 15,674 cycles

RT ENG PYLON TITANIUM HEAT SHIELD RIVET MISSING. REPLACED LOOSE RIVETS.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 55,798 hrs · 15,629 cycles

EMERGENCY LIGHTS INOPERATIVE FROM SEATS 8 TO 12. RECONNECTED LIGHT .

Part: HYDRAULIC SYSTEM — OVERSERVICED (RIGHT) · airframe 55,716 hrs · 15,605 cycles

RIGHT HYD OVERFILL STATUS MESSAGE, WITH RIGHT HYD SYS SERVICED TO 1.22. TRANSFERRED HYD FLUID FROM RIGHT TO LEFT. OK FOR SERVICE. CORRECTED SERVICE CONDITION.

Part: BOLT — MISSING (NR 5 SLAT) · airframe 55,550 hrs · 15,570 cycles

FOUND NR 5 LEADING EDGE SLAT AUXILIARY TRACK ARM FORWARD BOLT MISSING. REPLACED MISSING HARDWARE PER IPC 27-81-11-005 AND MM 27-81-00. GROUND OPERATION NORMAL.

Part: IDG — FAULTY (NR 1 ENGINE) · airframe 55,150 hrs · 15,455 cycles

LEFT GENERATOR OFF ON TOUCHDOWN. REPLACED NR 1 ENG IDG. OP & LEAK CHECK OKAY.

Part: GCU — MALFUNCTIONED (POSIT 24) · airframe 55,004 hrs · 15,411 cycles

THERE IS A HYDRAULIC LEAK IN THE LT GEAR WHEEL WELL AREA. REPLACED HMG SHUTOFF VALVE PER AMM. PRESSURIZED AND NO LEAKS NOTED. AFTER REPLACING HMG OP CHECK FAILED (DID NOT TEST). RPL'D HYD MOTOR GENERATOR CONTROL UNIT PER MM AND ACP'D OPERATIONAL CHECK PER MM. OPS OKAY.

Part: ACTUATOR — FAULTY (NR 1 ENGINE) · airframe 54,914 hrs · 15,384 cycles

STATUS MSG: "L ENG PRI CONT". EPCS MSG: P SVA OR FCU-EEC. CLEARED MSG, RAN NR 1 ENG AT IDLE, NO MSG. REPLACED NR 1 ENG SVA PER MM. SEE FAULT ISOL 71 FIG 109. ACCOMPLISHED TEST 14 AND 15 SEE JRH 2-5-92 AND JRH 2-5-64 AND JRH 2-5-35. NO MSG. TAKEOFF POWER CHECK, OKAY.

Part: SCREW — MISSING (TE FLAP CANOE) · airframe 54,909 hrs · 15,383 cycles

TWO ADJACENT SCREWS MISSING LEFT WING INBD MOST FLAP ASS'Y CANOE OTBD SIDE TOP AFT. REPLACED MISSING SCREWS ON INBD FLAP INBD FLAP CANOE 2EA.

Part: CONNECTOR — DIRTY (LT ENGINE) · airframe 54,865 hrs · 15,370 cycles

LEFT ENGINE WOULD NOT START. COMPLIED WITH MEL. CLEANED CONNECTOR. RAN ENGINE TWICE, OPS CHECK OKAY.

Part: UNKNOWN — ODOR (CABIN) · airframe 54,530 hrs · 15,273 cycles

ELECTRICAL BURNING ODOR REPORTED MID GALLEY AREA BY FA'S. TURNED BOTH UTIL BUSSES OFF & CONTD. INSPECTED GALLEY AREA INCLUDING GALLEY EQUIPMENT, AND ASSOCIATED WIRING, INSPECTED LAVS AND LAV AREA INCLUDING VENT FANS, LAV MOTORS ETC. RAN ENGINES, PACKS, HYDRAULICS AND INSPECTED CABIN AREA FOR DUPLICATE ODOR AND OR BURNT WIRING, COULD NOT DUPLICATE, NO DEFECTS OBSERVED.

Part: CIRCUIT CARD — FAULTY (FIRE DETECTION) · airframe 54,418 hrs · 15,245 cycles

DUCT LEAK STATUS MSG DISPLAYED, UNABLE CLEAR. ACP'D BITE OF FIRE DETECTION SYSTEM AND FOUND POWER SUPPLY CARD BAD, REPLACED CARD FROM AIRCRAFT 5677. TESTS NORMAL.

Part: GENERATOR — LEAKING · airframe 54,391 hrs · 15,235 cycles

HYDRAULIC MOTOR GENERATOR LEAKING. REPLACED HMG, LEAK CKS OKAY.

Part: CHARGER — DEFECTIVE (APU) · airframe 54,053 hrs · 15,137 cycles

APU BLEED PRESS SHOWS 0 TO MAX OF 4 PSI. SELECTED BLEED SWITCH TO OFF VALVE CLOSED NORMALLY. AFTER A REVIEW OF HISTORY AND TROUBLESHOOTING, FOLLOWED SERVICE TIP 49-11-00 PAGE 200A. ECU MSG. REVERSE FLOW. REPLACED APU BATTERY CHARGER PER AMM, CHK'D GOOD. APU STARTED AND RAN NORMAL, PNEUMATICS OPS. NORMAL, SHUT DOWN CHK'D. ECU NO MSG'S. REACTIVATED SYSTEM PER MEL 3611G.

Part: SENSOR — MALFUNCTIONED (BLEED AIR SYS) · airframe 54,028 hrs · 15,129 cycles

NO DUCT PRESSURE WITH APU RUNNING AND BLEED OPEN. TRIED RE-SETTING CB'S -NO HELP. SCV, ECU AND FLOW SENSING MODULE REPLACED 06 DEC 11. REPLACED APU INLET PRESSURE (P2) SENSOR PER MM. RAN APU AND DUCT PRESSURE READS 35 PSI, MOTORED NR 2 ENGINE AND APU DUCT PRESSURE READS NORMAL.

Part: ECU — MALFUNCTIONED (BLEED AIR SYS) · airframe 53,997 hrs · 15,116 cycles

LOW PNEUMATIC PRESSURE 5 PSI. UNABLE TO REVIVE AIR PRESSURE. ONLY 5PSI. NEED GROUND START. REPLACED ECU PER MM SINCE IT WOULDN'T RESET AFTER LAMP TEST. REPLACED FLOW SENSE MODULE PER MM AS PER FIM AND WIRING CHECKS WERE GOOD.

Part: REPAIR — DEBONDED (RUDDER) · airframe 53,960 hrs · 15,106 cycles

RUDDER LEFT UPPER SURFACE OLD REPAIR IS DISBONDING AND BREAKING OFF. AREA APPROX 4 INCHES BY 5 INCHES. COMPLIED WITH EVA-81567 AND MADE TEMP REPAIR WITH SPEEDTAPE.REFER TO SM-09-13-25-01-JD FOR PERMANENT REPAIR.

Part: OVEN — NOISY (GALLEY) · airframe 53,808 hrs · 15,062 cycles

CREW REPORTS FWD GALLEY OVEN (R12) FAN MAKING NOISE. NEEDS NEW OVEN- C-B PULLED AND COLLARED AND DOOR PLACARD. OVEN (028-9005) ITEM NR 1 OF IPC. OVEN OPS CHK OK NOISE LEVEL NORMAL PER LAXMM.

Part: OXYGEN BOTTLE — LOW (CABIN) · airframe 53,757 hrs · 15,047 cycles

CREW COMMENTS: USED OXYGEN BOTTLE LOCATED AT 1A. SERVICE BOTTLES TO FULL. 3 EACH BOTTLES USED 2 FWD AND 1 AFT.

Part: WIRE — EXPOSED (MICROPHONE) · airframe 53,744 hrs · 15,043 cycles

CAPTAIN'S HAND MIC HAS BARE WIRES EXPOSED. REPLACED MIC, OPS OKAY.

Part: LIGHT — INOPERATIVE (FIRE HANDLE) · airframe 53,739 hrs · 15,042 cycles

SEVERAL LIGHTS INOP ENG 2 FIRE HANDLE. RELAMPED ENG 2 FIRE HANDLE AND OP CHECKED.

Part: LINK — OUT OF ADJUST (COCKPIT) · airframe 53,739 hrs · 15,042 cycles

CAPTAIN'S SLIDING WINDOW WON'T UNLOCK. ADJUSTED LINK ARM.

Part: GCU — FAULTY (LEFT) · airframe 53,435 hrs · 14,951 cycles

L GEN DRIVE LIGHT IS NOT ILLUMINATED WHEN IT SHOULD BE LIGHT TESTS OKAY. COMPLIED WITH MEL 2411E. REPLACED LEFT GEN CNTRL UNIT, OPS NORMAL.

Part: PUMP — FAULTY (FUEL SYSTEM) · airframe 53,187 hrs · 14,880 cycles

LT AFT FUEL BOOST PUMP ISSUE, FLIGHT DIVERTED. LT AFT MAIN TANK FUEL PUMP FAILED LOW PRESS LIGHT AND EICAS MSG. REPLACED LT AFT MAIN FUEL BOOST PUMP. OPS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (ELEVATOR) · airframe 53,125 hrs · 14,859 cycles

R ELEV PCU STATUS MSG. RESET CBS, NO HELP. REPLACED PCU MONITOR MODULE, NO HELP. SUSPECT THE RT ELEVATOR PCU. COMPLETED OP CK OF ELEVATOR FLIGHT CONTROLS PER FIM. NO MESSAGE NOTED AT THIS TIME. OK FOR SERVICE.

Part: CARBON SEAL — LEAKING (NR 1 ENGINE) · airframe 53,107 hrs · 14,854 cycles

NR 1 ENG HIGH OIL CONSUMPTION EXCEEDS LIMIT. HOC TROUBLESHOOTING STARTS ON PAGE 117. ACP HOC TROUBLESHOOTING REF MM 71-05-00. OBSERVED RUNNING OIL LEAK FROM BREATHER PORT DURING ENG RUN. ALL OTHER ACCESSORY DRAINS CHECKED OK. REPLACED DE-OILER CARBON SEAL PER MM. RAN ENG NO LEAKS.

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 53,063 hrs · 14,841 cycles

NR 2 FUEL SPAR VALVE ISSUE, RTFL. RIGHT FUEL SPAR VALVE LIGHT ON WITH EICAS 30 MINUTES INTO FLIGHT AND REMAINS ON. RT ENG PARAMETERS ALL NORMAL, FUEL FLOW MATCHES LEFT ENGINE. MAINT TEXT: SEE PTT SEQ #0632003 FOR WIRING CHECK INFO. NO WIRING DEFECTS FOUND BETWEEN CUTOFF-RUN SWITCH AND R SPAR FUEL SHUTOFF VALVE V26. REPLACED NUMBER TWO ENGINE FUEL SHUTOFF VALVE, SPAR VALVE, ACTUATOR AFTER COMPLETING WIRING CHECK OK PER MM. FOUND RIGHT ENGINE SPAR VALVE CB TRIPPED ON P6 PANEL. ACCOMPLISHED WIRING CHECK FROM R SPAR FUEL SHUTOFF VALVE (V26) CONNECTOR D2022, PINS 2, 5, AND 6, TO R FUEL CUTOFF-RUN SWITCH S3. CHECKED OK-NO SHORTS TO GROUND, SHORTS TO SHIELD, OR PIN-TO-PIN SHORTS. SHOOK WIRING AT CONNECTOR-NO DISCREPANCIES.

Part: HYDRAULIC LINE — FAULTY (NLG) · airframe 53,035 hrs · 14,833 cycles

L HYD SYS PRESS AND RSVR LIGHT ON EICAS AND L HYD QTY 0.18 RF. REPLACED NLG DOOR HYD LINE AND SERVICED SYSTEM, LEAK CHECK GOOD.

Part: HEADSET — DEFECTIVE (COCKPIT) · airframe 52,932 hrs · 14,800 cycles

NR 1 PILOT'S HEADSET IS DEFECTIVE. (O1=CAPT,O2=1ST OFF, O3=1ST OBS). CREW COMMENTS: ATC REPORTS MICROPHONE ON HEADSET IS SCRATCHY. REPLACED HEADSET, OUTBOUND CAPT REPORTS MICROPHONE OPS NORMAL DURING PREFLIGHT CHECKS.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 52,932 hrs · 14,800 cycles

ONE BULB IN 'LOCK FAIL' LIGHT ON FWD OVERHEAD PANEL IS BURNED OUT. RELAMPED OVERHEAD LIGHT.

Part: FAN — NOISY (COCKPIT) · airframe 52,932 hrs · 14,800 cycles

RIGHT RECIRC FAN NOISE INTERFERES WITH COCKPIT COMMUNICATIONS. APPLY MEL 2125A.

Part: DISPLAY — DEFECTIVE (ACARS) · airframe 52,847 hrs · 14,779 cycles

ACARS DIMMER SWITCH INOP. UNABLE TO SEE SCREEN. INSTALLED NEW ACARS DISPLA Y UNIT PER MM, OPS CHECKS GOOD.

Part: WIRE — DAMAGED (RT MLG) · airframe 52,716 hrs · 14,743 cycles

ANTI-SKID EICAS, FLIGHT DIVERTED. FOUND WIRE W4910-2501-20 AND W4910-2502-20 DAMAGED AND GROUNDED. REMOVED CONBOX COVER AT RIGHT MLG JUNCTION BOX WHERE WIRES ARE DAMAGED. HARD FAULT ON ANTI-SKID CONTROL UNIT FOR ANTI-SKID XDUCER 4 WD 32-42-11 PG 3 SHEET 4. INSTALLED NEW WIRES DOWN TO R MLG FWD JUNCTION BOX J3. INSTALLED PINS INTO CONNECTOR D40442P. NEED TO COMPLETE INSTALLATION BY TERMINATING WIRES INTO TERMINAL BLOCK TB211. REPAIRED WIRES W4910-2501-20, W4910-2502-20. OPS

Part: SEAL — DEFORMED (E/E BAY DOOR) · airframe 52,668 hrs · 14,726 cycles

LOUD NOISE FROM NOSE OF ACFT AT 14000'. FOUND FWD E/E DOOR SEAL DEFORMED AND DOOR LOOSE.

Part: STRUCTURE — DAMAGED (ENTRY DOOR) · airframe 52,550 hrs · 14,692 cycles

MAIN ENTRY DOOR 2R UPPER HINGE CUTOUT IS CRACKED. FERRIED IN FROM SEA FOR DOOR 2R UPPER HINGE CRACKED. MAIN ENTRY DOOR 2R UPPER HINGE CUTOUT IS CRACKED OVER .25 INCH. REPAIR IS DONE. EG WILL HAVE 8100-9. CONT INSTL INTERNAL MECH THEN RIG AND CLOSE UP TO ACP*. REPAIRED 2R MED HINGE CUTOUT PER UA-EVA-81021A. REF SFOOV WRITE UP Y1170H.

Part: FAN — INOPERATIVE (E&E BAY) · airframe 52,473 hrs · 14,670 cycles

COOLING FAN IN THE RACK FOR RADAR TR UNIT INOP. REPLACED FAN.

Part: TRANSCEIVER — FAULTY (WX RADAR) · airframe 52,473 hrs · 14,670 cycles

WX FAIL RD BOTH ND'S SHORT FINAL APPROACH. REPLACED TRANSCEIVER.

Part: TRANSCEIVER — FAULTY (WX RADAR) · airframe 52,445 hrs · 14,663 cycles

WX RADAR SHOWS A LOT OF GROUND RETURN UPPER 1-3 OF SCREEN 160NM RANGE FL390 MIDDLE OF SCREEN. REPLACED WEATHER RADAR TR UNIT IAW AMM, CKS OKAY.

Part: LAMP — INOPERATIVE (GALLEY) · airframe 52,331 hrs · 14,632 cycles

GALLEY HOT PLATE LIGHT INOPERATIVE AT DOOR-1R FWD-CABIN FWD GALLEY. RELAMPED, OPS CHECKED OKAY.

Part: TRANSCEIVER — OUT OF TOLERANCE (CABIN) · airframe 51,173 hrs · 14,289 cycles

AFT EMERGENCY TRANSCEIVER OUT OF TIME IAW RUNOUT DATE. REPLACED AFT EMERGENCY TRANSCEIVER.

Part: CONNECTOR — CORRODED (SLIDE TEST PANEL) · airframe 51,173 hrs · 14,289 cycles

GREEN LIGHT ON TEST PANEL P61 FOR R EMER ESCAPE OVER WING SLIDE. TRIED NEW TEST RELAY K10487 AND HUNG NEW SQUIB, NO HELP. SHAKING WIRES ON P79 PANEL CAUSES LIGHT TO FLICKER. FOUND MOISTURE & CORROSION IN CONNECTOR D4083 0P & J ON P79 PANEL. CLEANED CONNECTOR, D4083 AND BOTH TEST SW P61 PANEL. OPS CKS OK AND LIGHT STAYS OFF BOTH TESTS FUNCTION OK.

Part: RELAY — FAULTY (R1 DOOR SLIDE) · airframe 51,130 hrs · 14,275 cycles

RIGHT SIDE EMERGENCY ESCAPE GREEN LIGHT ON SQUIB TEST PANEL ON AFTER MX ADJUSTED DOOR R1 SLIDE COVER. REPLACED RT SLIDE TEST RELAY K10487 AND ACCOMPLISHED SQUIB TEST PER MM, CHECKED OKAY.

Part: FAN — FAULTY (NR 1) · airframe 50,844 hrs · 14,197 cycles

STATUS MSG AFT EQUIP COOLING FAN 1. REPLACED FAN ASSY. WORKS FINE.

Part: BLEED VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 50,682 hrs · 14,148 cycles

STARTING RT ENG WITH LT ENG RUNNING LT ENG BLEED VALVE OPENED AND APU BLEED VALVE CLOSED. REPLACED RELAY K10281, NO HELP. REPLACED K10554 TO FIX SIMILAR BLEED FAULT. REPLACED NR 1 ENG PRSOV STARTED RT ENG, LT ENG RUNNING, BOTH ENG BLEED SW IN (OPEN), AND APU BLEED SWITCH IN (OPEN). MOTORED RT ENG TO 28 PERCENT, N2 BEFORE FUEL ON. ALSO ACCOMPLISHED CROSSBLEED START IAW JRH 2-5-1. LT ENG STARTING RT ENG.

Part: LIGHT — INOPERATIVE (ENGINE OVERHEAT) · airframe 50,642 hrs · 14,138 cycles

RT ENGINE OVERHEAT LIGHT INOPERATIVE. REPLACED RT ENG OVERHEAT LIGHT BASE ASSY AND OP CHECKED IAW MM. TEST PASSED.

Part: RADAR — FAILED (WX SYSTEM) · airframe 50,475 hrs · 14,090 cycles

WEATHER RADAR FAILED, DISPLAYED ON HSI. WHEN IN WEATHER RADAR TEST. ANTENNA AND RT DISPLAYED. REPLACED SCANNER ASSY. CHECKS OK.

Part: CONTROL VALVE — INOPERATIVE (LT A/C PACK) · airframe 50,456 hrs · 14,085 cycles

DUE TO HISTORY OF LT PACK FLOW CONTROL VALVE NOT CLOSING, REPLACE LT PACK FLOW CONTROL VALVE. REPLACED LT FLOW CONTROL & SHUTOFF VALVE, OP CKD GOOD.

Part: ELT — OUT OF TOLERANCE (ESCAPE RAFT) · airframe 50,325 hrs · 14,049 cycles

REPLACED ELT ON RAFT NR1 AND RAFT NR 2 IAW AMM ON TASK CARD 2355N00700.

Part: FLOOR PANEL — CORRODED (BS 1681) · airframe 50,325 hrs · 14,049 cycles

MAIN CABIN AFT PRESSURE DECK AT BS 1681 AND RBL 38 IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REPAIRED MAIN CABIN DECK AT 1681 IAW EA. ITEM IS CONSIDERED A PERMANENT REPAIR WITH NO FURTHER ACTION REQUIRED IAW EG.

Part: BEARING — WORN (R1 DOOR) · airframe 50,325 hrs · 14,049 cycles

R1 DOOR TORQUE TUBE COCKING ROD END BEARING WORN. REPLACED IAW MM ON WOO-34NR1.

Part: GATE — CORRODED (L1 DOOR) · airframe 50,325 hrs · 14,049 cycles

L1 DOOR LOWER GATE CORRODED. ACCOMPLISHED REPAIR IAW WOO-37 NRI.

Part: FLOORBEAM — CORRODED (STA 1706 RBL 52) · airframe 50,325 hrs · 14,049 cycles

MAIN CABIN AFT PRESSURE DECK AT BS 1706 AND RBL 52 IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REPAIRED AFT FLOOR SUPPORT DECK AT STA 1706 IAW EA 57-53-066. THIS A PERMANENT REPAIR AND REQUIRES NO FURTHER ACTION.

Part: FLOORBEAM — CORRODED (BS 1861) · airframe 50,325 hrs · 14,049 cycles

FLOORBEAM AT STATION 1681 ON RBL 38 CORRODED ON UPPER AND LOWER SURFACE OF FWD SIDE OF TEE. MAJOR REPAIR ACCOMPLISHED: REPAIRED FLOORBEAM AT STA 1681 PER EA 57-53-066. THIS IS A PERMAMENT REPAIR WITH NO FURTHER ACTION REQUIRED.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 50,325 hrs · 14,049 cycles

RT INBD MAIN FLAP UPPER SURFACE HAS A 1.2" LONG GOUGE, .26' IN WIDTH AND A DEPTH OF .022 INCORPORATING 2 EA FASTENERS. THIS GOUGE IS LOCATED 77 INCHES FROM INBD EDGE AND 15. 5 INCHES FWD OF T/E. THIS GOUGE IS LOCATED 77 INCHES FROM INBD EDGE AND 15. 5 INCHES FWD OF T/E. REPAIRED IAW EA PD- 57-57-(035) AND EVA 80387.

Part: HOUSING — OUT OF TOLERANCE (R1 DOOR SNUBBER) · airframe 50,325 hrs · 14,049 cycles

R-1 DOOR SNUBBER SUPPORT HOUSING RUBBING AGAINST TRIGGER. REPLACED ON JOB CARD 5R52I1811 AND WOO-47NRO.

Part: BEARING — WORN (R4 DOOR) · airframe 50,325 hrs · 14,049 cycles

R4 DOOR COCKING ROD END BEARING WORN. SUPPLEMENTAL DATA UPDATE REPLACED THE COCKING ROD END BEARING PER CMM.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 50,325 hrs · 14,049 cycles

MAIN CABIN FLOOR HAS CORROSION AT BS1640 BETWEEN RBL 0 AND RBL 56 UNDER NUT CLIPS ON TOP OF HAT CHANNEL SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED: AFTER CORROSION REMOVAL FOUND MATERIAL LOSS BEYOND LIMITS. REPLACED NEW T-CHORD AND STRAPS AND ANGLES. AREA TREATED AND PRIMED.

Part: SEAT TRACK — BROKEN (BS 747) · airframe 50,325 hrs · 14,049 cycles

SEAT TRACK CROWN AT BODY STATION 747 AT RBL 24 IS BROKEN. REPAIRED PER SRM ON WOO 146 NRO, CARD 2355N00388.

Part: GATE — CORRODED (R4 DOOR) · airframe 50,325 hrs · 14,049 cycles

4-R DOOR LOWER GATE CORRODED.

Part: BEARING — FROZEN (R4 DOOR) · airframe 50,325 hrs · 14,049 cycles

R4 DOOR TRIGGER MECH BEARING NOT MOVING, FROZEN. ACCOMPLISHED ON WOO 32NR1.

Part: LIFTER — WORN (L2 DOOR GIRTBAR) · airframe 50,325 hrs · 14,049 cycles

L2 DOOR GIRT BAR LIFTERS WORN FWD AND AFT.

Part: FLOORBEAM — CORRODED (BS 1661) · airframe 50,325 hrs · 14,049 cycles

MAIN CABIN FLOORBEAM T-CAP CORRODED AT BS 1661 AND LBL 15. MAJOR REPAIR ACCOMPLISHED: REPAIRED FLOORBEAM T-CAP AT STA 1661 LBL15 SRM.

Part: PUMP — FAULTY (HYD SYSTEM) · airframe 50,325 hrs · 14,049 cycles

LEFT HYD SYS QTY DROPPED ON APPROACH. SHOWS .35RF. REMOVED AND REPLACED LEFT PTU IAW AMM. REMOVED AND REPLACED AILERON SERVO ACTUATOR IAW MANUFACTURER REPLACED AILERON SERVO PRESSURE AND RETURN LINES IAW AMM, LEAK CHECK GOOD.

Part: SWITCH — FAILED (ENGINE OIL) · airframe 50,233 hrs · 14,022 cycles

STATUS MESSAGE ENGINE OIL PRESSURE INDICATED 138. REPLACED LOW OIL PRESSURE WARNING SWITCH, RAN LT ENG PRESSURE AT IDLING INDICATION, NO HELP. REPLACED SCAVENGE OIL PUMP. RAN ENGINE AND ADJUSTED OIL PRESSURE THREE TURNS CLOCKWISE. LEAK AND OPS CHECKS OKAY.

Part: PUMP — LEAKING (NR 1 ENGINE OIL) · airframe 50,193 hrs · 14,009 cycles

EXCESSIVE OIL DRIPPING FROM NR1 ENG COWL. RAN ENG AND FOUND A PIN HOLE IN THE FWD OTBD SECTION OF THE OIL PUMP SPRAYING OIL. APPROX 1 IN FWD OF THE SCAVENGE OUT LINE. REPLACED LUBE AND SCAVENGE PUMP. RAN NR1 ENG, NO LEAKS NOTED. FOUND LT RUDDER PCA LEAKING FROM FWD END. REPLACED ACTUATOR.

Part: POWER CABLE — SEPARATED (L2 DOOR) · airframe 50,164 hrs · 14,001 cycles

UNABLE TO PIN DOOR 2L EMERGENCY POWER ASSIST BOTTLE. FOUND CABLE SERRATED, PLATES OUT OF ADJUSTMENT. ADJUSTED DOOR ASSIST RESERVOIR CABLE TERMINAL AND SERRATED PLATES TO CORRECT POSITION IAW MM. SAFETY PINS NOW FIT CORRECTLY. ACCOMPLISHED RII OF CABLE PLATES AND ATTACHING HARDWARE SECURED.

Part: CONTROL VALVE — FAULTY (CABIN TEMP) · airframe 50,121 hrs · 13,986 cycles

CAN NOT CONTROL CABIN TEMPERATURE. REPLACED TEMP CONTROL VALVE. ALL OPS NORMAL.

Part: LIGHT — LOOSE (ROW 13 ABC) · airframe 50,111 hrs · 13,984 cycles

EMERGENCY LIGHT STRIP 13 ABC LOOSE. SECURED STRIP.

Part: FSEU — FAULTY (NR 2) · airframe 49,978 hrs · 13,948 cycles

TWO STATUS MESSAGES WARN ELEX AND FLAP-SLAT STATUS NOT ABLE TO CLEAR. NO BITE ON NR 2 FSEU. NR 1 AND 2 FSEU SHOW NO DATA FROM FSEU NR 2. REPLACED NR 2 FSEU. ALL TESTS NORMAL.

Part: BRACKET — OUT OF ADJUST (DOOR 3R) · airframe 49,974 hrs · 13,947 cycles

DOOR 3R WILL NOT OPEN. FOUND RETRACTABLE DOOR MECHANISM STOP BRACKET LOOSE AND JAMMING THE BOTTOM OF THE RETRACTABLE DOOR PREVENTING THE DOOR FROM DISARMING. ADJUSTED AND SECURED THE STOP BRACKET PER MM. DOOR ARMING FUNCTION, OPS CHKS GOOD.

Part: MODULE — FAULTY (AIR FLOW SENSOR) · airframe 49,807 hrs · 13,894 cycles

NO DUCT PRESSURE FROM APU. LOW AIR PRESSURE FROM APU. APU PRESSURE RETURNED TO NORMAL. REOPENED BY ORD MM FOR: LOW BLEED PRESSURE PROBLEM RETURNED. REPLACED APU AIR FLOW SENSOR MODULE. APU DUCT PRESSURE CONSTANT NOW AT 28 PSI. OPERATES BOTH PACKS AND DRY MOTORS ENGINES TO START.

Part: RELAY — FAULTY (GALLEY) · airframe 49,374 hrs · 13,761 cycles

FOUND GALLEY 4B BREAKER POPPED IN COCKPIT PRIOR TO ENG RUNS. RESET BREAKER AND IT WAS POPPED AGAIN AFTER RUNS COMPLETED. REPLACED CB C743 AND RELAY K10136. NO HELP. CB POPPING AFTER 10 SECONDS. SUSPECT M227 AFT GALLEY ELCU. REPLACED LT AFT GALLEY PWR ELEC PWR CONTROL RELAY, OPS CHECKS OK.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 49,328 hrs · 13,748 cycles

L HYD SYS LOSS, RTFL. LT GEAR DOWN LOCK ACTUATOR PRESS FLEX LINE LEAKING. R & R LINE AFTER HYD SYS SERVICED, RAN SYS WITH LT ENG PUMP AND ELEC PUMP. RESTORED ALTERNATE FLAPS SWITCH TO NORMAL AND CYCLED FLAPS AND PRIMARY FLT CONTROLS SEVERAL TIMES. CLOSED ALL GEAR DOORS AND CLEANED UP FLUID. ACFT IS READY FOR SERVICE.

Part: REGULATOR — MALFUNCTIONED (BLEED AIR SYS) · airframe 49,038 hrs · 13,669 cycles

LT PACK & ENG BLEED ISSUES, RTFL. LT PACK WOULD NOT OPERATE NORMALLY AND CREW NOTICED LT ENG BLEED WOULD COME ON. WHILE ACCOMPLISHING PNEUMATIC HEALTH CHECK, FOUND PRSOV REGULATOR BAD, REPLACED PRSOV REGULATOR.

Part: VALVE — FAULTY (LT BLEED SYS) · airframe 48,918 hrs · 13,639 cycles

LEFT ENGINE BLEED OFF LIGHT ILLUMINATED WITH LT ENG BLEED OFF EICAS MESSAGE WITH ENG RUNNING, BLEED SWITCH ON & ISOLATION VALVE CLOSED. PACK ON WITH DUCT PRESSURE ZERO. BLEED LIGHT STAYS ON WITH THROTTLES ADVANCED ABOVE 41 PERCENT N1. RECORD DUCT PRESSURE WHEN ADVANCED. LT ENGINE BLEED OFF EICAS. FOLLOWED PROCEDURE, LIGHT OUT MOMENTARY THEN BACK ON. PRESS ZERO. DEFERRED BLEED INOP, CLOSED. REPLACED FAN AIR TEMP SENSOR. RAN NR 1 ENGINE DUCT PRESSURE 20 PSI AT IDLE. BLEED LIGHT OPERATES NORMALLY.

Part: CIRCUIT CARD — DEFECTIVE (COCKPIT) · airframe 48,791 hrs · 13,604 cycles

LEFT ENG BLEED VALVE OFF LIGHT ON WITH POWER AT IDLE IN DESCENT. RESET PER CHECKLIST OK. REPLACED LT ENG N2 SPEED CARD. RAN ENG ALL PRESSURES AND INDICATIONS NORMAL.

Part: SPOILER SYS — FAULTY (NR 9) · airframe 48,647 hrs · 13,565 cycles

SPOILER MESSAGE AND EXCESSIVE RUDDER TRIM. 6 UNITS RT RUDDER TRIM REQ IN CLB-4 UNITS IN CRZ TO KEEP A-C LVL IN ROLL CONTINUED, 0 UNITS OF RUDDER PRODUCES PRONOUNCED LEFT ROLL RATE. NEGATIVE ROLL STABILITY. CHECKED RUDDER CHANGER RIGGING, YAW DAMPER SUMMING LINKAGE SHEAR RIVETS, AND RUDDER TRIM CONTROL SYSTEM TEST. REPLACED NR 9 SPLOILER, OPS CHECKED NORMAL, NO FAULTS.

Part: RELAY — FAULTED (GROUND SERVICE) · airframe 48,380 hrs · 13,491 cycles

BEFORE DISPATCH SEVERAL STATUS MESSAGES APPEARED ON EICAS-MAIN BATTERY CHARGER, EXH NR1 AFT EQUIP WITH FLUCTUATION OF CTR HYD QTY. COMMON 115 VOLT AC FOR ABOVE SYS IS A2 PHASE OF 115V AC GROUND SVC BUSS. WD 24-51-52. FOUND TWO LUGS ON GROUND SERVICE TRANSFER RELAY A3 & B3 SEPARATED FROM MOUNTING BASE. REPLACED RELAY. RAN ENGINE IAW JRH. OPERATED SYS WITH GRND POWER & APU POWER. SYS OPERATED NORMAL.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 48,380 hrs · 13,490 cycles

LEFT HYD FLUID LOSS, FLIGHT DIVERTED. FOUND EVIDENCE OF METAL IN PUMP. ACP'D SYS FLUSH FOUND NR 1 EDP LEAKING FROM DRAIN. REPLACED NR1 EDP. LEAK CHECKED LT EDP DUE TO REPLACEMENT. RAN ENG. NO LEAKS AT EDP AND FILTER MODULES.

Part: LENS — BROKEN (CABIN) · airframe 48,355 hrs · 13,482 cycles

FLOOR EMERGENCY LIGHT LENS BROKEN ROW 13. NEEDS NEW LENS ASSY. TAPED EDGES OF LENS TO HOLD DOWN. EMERGENCY LIGHT STILL VISIBLE AND SECURE. REPLACED EMERGENCY LIGHT TRACK COVER.

Part: BLADES — MISSING (COMPRESSOR) · airframe 48,241 hrs · 13,447 cycles

WHILE INSPECTING 14TH STAGE BLADES THRU AP7. NOTICED 13TH STAGE BLADES HAS 2 BLADES WITH MISSING MATERIAL AT T/E AND TIP. APPEARS TO BE OVER THE .250 MAX IN IN BOTH DIRECTIONS. CF IS FOR NR 2 ENG S-N 726525. CONTACTED SAMC ENG CONTROLLER & ENGINEER AND BOTH AGREED FOR A 4 CYCLE FLYBACK WITH REVENUE. REPLACED ENGINE.

Part: PUMP — LEAKING (NR 1 ENGINE) · airframe 48,135 hrs · 13,414 cycles

NR 1 ENGINE HYD PUMP (EDP) LEAKING HYD FLUID FROM SHAFT SEAL AT 12 DROPS PER MINUTE DURING IDLE RUN. REPLACED NR 1 EDP, LEAK CHECK OPS TEST OKAY.

Part: PANEL — CORRODED (LAV SERVICE) · airframe 48,129 hrs · 13,413 cycles

CORROSION ACB BULK CARGO AREA AT LAV SERVICE PANEL PAN AROUND DUCT UNDER TANK. REPLACED LAV SERVICE PANEL. ACFT PRIMARY STRUCTURE IS OK. WORK WAS ACP ON PEMCO NR 2012N00376 AND INSP BY QC 802.

Part: WIRE — DAMAGED (E&E BAY) · airframe 48,129 hrs · 13,413 cycles

E+E BAY UNDER FLOOR AFT OF P-31 AND P-32 PANELS, WIRES HAVE SIGNS OF ARCING. ACP SMC003 CUT OUT ARCH DAMAGE AND SPLICED WIRE TOGETHER WITH COLD SHRINK SLEEVE.

Part: STRUCTURE — UNKNOWN (DOOR 4L & R) · airframe 48,129 hrs · 13,413 cycles

DOOR 4 LT & RT DOOR STOP TEE CLIP. ACP COA 506902 ON TASK CARD 5C0690201 BY INSP Q816. NO CRACKS FOUND.

Part: GENERATOR — INOPERATIVE (APU) · airframe 47,823 hrs · 13,317 cycles

APU GENERATOR WILL NOT COME ONLINE. APU GENERATOR INOPERATIVE. A-C TO BE REROUTED TO HNL FOR FIX. REPLACED GEN WITH GEN FROM SPARE APU, OPS CHECK GOOD.

Part: LIGHT — LOOSE (ROW 12) · airframe 47,813 hrs · 13,314 cycles

EMERGENCY LIGHT STRIP AT ROW 12 LOOSE. SECURED LIGHT STRIP.

Part: VALVE — FAULTY (POSITION 1) · airframe 47,727 hrs · 13,293 cycles

LT BLEED SHOWS PRESSURE WITH SWITCH SELECTED OFF. COMPLIED WITH MEL. PRSOV LOCKED CLOSED. REPLACED LT PRSOV VALVE, NO HELP. REPLACED HIGH STAGE PILOT VALVE. REPLACED LT ECS BLEED CONFIGURATION CARD (P/N 285N0006-12 / SERIAL 97). SYSTEM OPS CHECKS NORMAL.

Part: SHUTOFF VALVE — FAILED (APU) · airframe 47,091 hrs · 13,126 cycles

APU BLD AIR DUCT PRESS LO APPROX 18 PSI FOR LT ENGINE START. PROBLEM RELATED TO LOW PNEUMATIC DUCT PRESSURE. NR 1 ENGINE PRSOV WOULD NOT CLOSE. REPLACED PRSOV AND APU PNEUMATICS OP CHECK OK.

Part: TRANSMITTER — FAULTY (OIL PRESSURE) · airframe 46,816 hrs · 13,043 cycles

NR 2 ENG OIL PRESS LIGHT ON OR FLUCTUATING. OIL PRESS INDICATES NORMAL RANGE. RT ENG OIL PSI FLUCTUATED 114-176 PSI FIRST TEN MINUTES OF FLIGHT. REPLACED MAIN OIL PRESSURE TRANSMITTER. RAN ENG, OPS AND LEAKED CHECKED NORMAL ON GROUND.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,738 hrs · 13,021 cycles

EMERGENCY EVACUATION LIGHT ON FLOOR FWD OF LT CLOSET INOP. NEEDS LIGHT STRIP AND POWER CABLE. TAPED THE LIGHT STRIP SO ALL ARE INTACT TOGETHER. LIGHT ASSY & PWR CABLE REPAIRED AND TEST OKAY.

Part: SKIN — LEAKING (FUSELAGE) · airframe 46,737 hrs · 13,020 cycles

PRESSURE LEAK AT STA 1620 LT CROWN AREA. SKIN LAP, FWD AND 12" ABOVE RT AFT STATIC PORT FOUND TO BE LEAKING DURING PRESSURIZATION CK. SEALED SKIN LAP ON OV WU E 5819H. SKIN LAP AFT OF UPPER TCAS ANT FOUND TO BE LEAKING DURING PRESSURIZATION CHECK SEALED SKIN LAP ON OV WU E5816H. THE CAUSE OF THE MOISTURE IN CROWN AREA IS MOIST CABIN AIR MIGRATING THROUGH GAPS OF BLANKETS & CONTACTING COLD FUSELAGE SKIN. TO RESOLVE THE ISSUE, DRY EXCESS MOISTURE & REINSTALL BLANKETS. PAY ATTENTION TO SEALING GAPS WHERE BLANKETS OVERLAP. RESTORED AIRCRAFT TO NORMAL. WORK ACP ON DOCK WU E5813H . ALL CEILING INSULATION GAPS SEALED.

Part: SKIN — LEAKING (FUSELAGE) · airframe 46,737 hrs · 13,020 cycles

WHILE ENROUTE, FLIGHT CREW REPORTS WATER DRIPPING AND ICE FORMATION OVERHEAD AND AT BOTTOM OF DOORS. FOUND CROWN PANEL LAP JOINT AT STA 1620 LT SIDE OF VERT STAB HAS PRESSURIZATION LEAK. PRESSURE CHECK FOUND 3 LEAK TOP OF FUSELAGE. WILL CLEAN AND RESEAL. REPLACED BLANKETS AS NEED FOR THE ENTIRE LENGTH OF CROWN. ALL CEILING INSULATION GAPS SEALED.

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS) · airframe 46,624 hrs · 12,991 cycles

CREW REPORTS AFTER ENG START, THE LEFT BLEED WOULD NOT CLOSE. SHUTDOWN NR 1 ENG, CYCLED LT BLEED CONTROL CB AND RESTARTED ENG, NO HELP. OPERATED ENGINE AND FOUND THAT LEFT PRSOV WOULD OPEN WITH SWITCH SELECTED TO OFF. REPLACED LEFT PRSOV. OPERATED ENGINE, PRSOV OPERATES OKAY.

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS) · airframe 46,449 hrs · 12,939 cycles

LEFT ENG BLEED WILL NOT CLOSE. REPLACED LEFT ENG PRSOV. OPS NORMAL.

Part: REGULATOR — FAULTY (POSITION 1) · airframe 46,350 hrs · 12,910 cycles

L ENG BLEED WILL NOT CLOSE. REPLACED LEFT ENGINE PRSOV WITH ENGINE HIGH STAGE VALVE. NO HELP. REPLACED HIGH STAGE VALVE WITH PRSOV VALVE. SUSPECT LEFT ENGINE PRSOV REGULATOR. LEFT ENG PRSOV REGULATOR REMOVED. REPLACED PRSOV REGULATOR. ACCOMPLISHED IDLE RUN, CHECKS GOOD.

Part: SHUTOFF VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 46,281 hrs · 12,886 cycles

LEFT ENG START NORM, RT ENG START ONLY 5 PSI. FOUND LT ENG PRSOV NOT CLOSE WITH ENG RUNNING AND SWITCH OFF. REPLACED NR 1 PRSOV, STARTED AND RAN NR 1 ENG AND THEN STARTED NR 2 ENG. NORMAL ENG START ON BOTH ENGINES.

Part: VALVE — FAULTY (APU) · airframe 46,269 hrs · 12,880 cycles

CREW REPORTS APU DUCT PRESS DROPS TO BELOW 10 PSI ON NR 2 ENG START. REPLACED APU SURGE VALVE. OPS CHECK OKAY.

Part: EXCITER — DEFECTIVE (APU) · airframe 46,205 hrs · 12,857 cycles

APU HARD TO START. BITE BOX FAULTS NO LIGHT LRU IGNITER LOST. REPLACED IGNITER, LEAD AND EXCITER. ACCOMPLISHED SEVERAL START WITH NO FAULTS DISPLAYED.

Part: FIRE LOOP — FAULTY (RT ENGINE) · airframe 46,048 hrs · 12,803 cycles

R ENG OH LP 1 STATUS MSG AT TOP OF DESCENT. FOUND TS5256A OVHT LOOP 1 OPEN. NEEDS NEW LOOP. REPLACED UPPER RIGHT FAN FIRE LOOP, CHECKS OKAY.

Part: BLEED VALVE — INTERMITTENT (LT ENGINE) · airframe 46,042 hrs · 12,800 cycles

L ENGINE BLEED VALVE INTERMITTENT WHEN APU VALVE SELECTED ON. REPLACED NR 1 ENG PRSOV AND PRSOV REGULATOR, RAN ENG. OP CHECK GOOD.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 46,002 hrs · 12,787 cycles

CAPTAIN'S O2 MASK MICROPHONE NOT HEARD ON SPEAKER. SWAPPED CAPT ACP WITH 1ST OBS ACP. AUDIO FUNCTIONS AT CAPT ACP NOW CHECK GOOD. REPLACED FIRST OBS AUDIO SELECT PANEL, OPS CHECKED GOOD.

Part: ACTUATOR — MALFUNCTIONED (SPOILERS) · airframe 45,914 hrs · 12,755 cycles

SPOILERS EICAS MSG. SCM 3R SHOWS MODULE AND PCA FAULTS. DEACTIVATED SPOILERS 4 AND 9. CHRONIC RE-ACTIVATED. REPLACED NR 9 SPOILER ACTUATOR. OPS AND LEAK CHECK GOOD. ALSO WENT BACK AND CHECKED LVDT VOLT ON 4 STILL GOOD.

Part: RECEPTACLE — DAMAGED (ACTUATOR) · airframe 45,899 hrs · 12,750 cycles

SPOILER EICAS MESSAGE ILLUM AT FLAPS 15 THRU LANDING. FOUND M535, 3R MOD, APL 757 SHELF 3R SCM FAULT- 27-61-16 M535 OR WIRING, INTERMITTENT, PH DESCENT. ALL OTHER MOD'S NO FAULTS. FOUND RECEPTACLE ON M309 DAMAGED DURING DEACTIVATION PER MEL. LT ACT, NR 4. DE-ACTIVATED SPOILER PAIR PER 4 & 9 PER MEL. REPLACED 3R SCM AND OPS CHECKS GOOD. RE-ACTIVATED SYS SECURED NR 4 & 9 PCA CONNECTORS SYS OPS CHECKS NORMAL.

Part: EXCITER — FAULTED (LT ENGINE) · airframe 45,711 hrs · 12,691 cycles

LEFT ENGINE NR 1 IGNITION SYSTEM INOPERATIVE. AUDIBLE IGNITION CHECKED GOOD. REPLACED NR 1 IGN PLUG PRECAUTIONARY. STARTED ENGINE 4X AND IGNITION TIMES VARY FROM 3-10 SECS EACH TIME BUT LIT OFF OKAY. IF PROBLEM PERSIST, MAY WANT TO SUSPECT POSSIBLE FUEL START NOZZLE ATOMIZATION SPRAY.

Part: CAP — DAMAGED (CABIN) · airframe 45,655 hrs · 12,673 cycles

EEL LIGHT AT SEAT 34A DAMAGED. REPLACED EEL LIGHT END CAP. TESTED EEL LIGHT NORMAL.

Part: SENSOR — INOPERATIVE (RT PACK) · airframe 45,632 hrs · 12,667 cycles

RT PACK OUTPUT TEMPS ARE ERRATIC IN MANUAL MODE. IN N POS: 118 DEGREES, IN W POS: 62 DEGREES. REPLACED STBY PACK OUT TEMP SENSOR, NO HELP. STBY MODE INOP. OK AUTO. REPLACED TS 199 RT PACK TEMP SENSOR. SYSTEM OPS CHECKS NORMAL. ACCOMPLISHED BITE OF L-H PTC, FOUND PACK TEMP SENSOR FAULT. REPLACED LT PACK TEMP SENSOR AND ACP BITE A SECOND TIME AND ALL OK, NO FAULTS NOTED.

Part: PUMP — LEAKING (LT ENGINE) · airframe 45,594 hrs · 12,653 cycles

LEFT ENGINE HYDRAULIC PUMP LEAKING COPIOUS AMOUNTS OF FLUID ON GROUND. REPLACED LEFT ENGINE HYDRAULIC PUMP. NO LEAKS DETECTED. OP CKS OKAY.

Part: VALVE — FAULTY (BLEED AIR SYS) · airframe 45,536 hrs · 12,638 cycles

LEFT ENGINE DUCT PRESSURE FLUCTUATES. PRESSURE FLUCTUATES BETWEEN 15 AND 30. NORMAL PSI IS 26-29. REPLACED HIGH STAGE VALVE AND HIGH STAGE PILOT AND ACCOMPLISHED PNEUMATIC TEST, ALL NORMAL. ACCOMPLISHED TEST, BLEED SHIFT OK.

Part: IGNITER — FAULTY (NR 1 ENGINE) · airframe 45,453 hrs · 12,618 cycles

NR 1 ENGINE HUNG START BEFORE STARTER CUTOUT. THRUST LEVER ADVANCE NOT ATTEMPTED. REPLACED NR 1 ENGINE LOWER IGNITER PLUG. IGNITION SYSTEM OPS CHECKED NORMAL. RAN ENGINE USING IGNITION SYSTEM 1 AND 2. EVERYTHING IS NORMAL.

Part: BLEED VALVE — FAULTY (LEFT) · airframe 45,408 hrs · 12,606 cycles

LEFT BLEED AIR PRESS FLUCTUATING FROM 20 TO 40 PSI DURING DESCENT. TROUBLESHOT PER MM. UNABLE TO DETECT ANY FAILURE MODES. REPLACED PRSOV AS A PRECAUTION.

Part: SHUTOFF VALVE — FAILED (BLEED AIR SYS) · airframe 45,388 hrs · 12,602 cycles

LEFT ENG BLEED ANNUNCIATOR CYCLED ON OFF THREE TIMES. REPLACED PRSOV AND PRSOV REGULATOR. OP CHECK OKAY.

Part: FUEL CONTROL — FAULTY (APU) · airframe 45,154 hrs · 12,532 cycles

APU FAILED TO START. FAULT LIGHT ILLUM AND EICAS MSG. APU FAULT DISPLAYED. NO MSG ON BOX. ONE AUTO EVENT 35 PERCENT 770 DEG. HOOKED TESTER UP COULD NOT GET TO FAULT. DOOR CIRCUIT NEVER FAILED. CHECKED INLET FOR BLOCKAGE OKAY. NO SPIKE VOLT FROM CHARGER. REPLACED THE FUEL CONTROL AND STARTER.

Part: BOTTLE — FAULTY (L3 DOOR ASSIST) · airframe 44,722 hrs · 12,399 cycles

DOOR 3L CANNOT BE ARMED, LEVER STUCK HALFWAY. NEED 3L DOOR ASSIST BOTTLE. REPLACED OVERCENTER SPRING ASSY AND DOOR ASSIST BOTTLE. OPS CHECK NORMAL.

Part: MECHANISM — LACK OF LUBE (DOOR 3R ARMING) · airframe 44,721 hrs · 12,398 cycles

DOOR 3R WILL NOT ARM. SPLIT UPPER AND LOWER CABLES FOUND PROBLEM IN UPPER CABLE. DISASSEMBLING DOOR LINER FOR ACCESS TO UPPER CABLE. LUBED AREAS OF DOOR ARMING MECHANISM. ARMING MECHANISM NOW ARMS FREELY. OPS CHECK OF DOOR ARMING AND DISARMING IS GOOD.

Part: LEAD — FAILED (LT ENGINE) · airframe 44,604 hrs · 12,366 cycles

LEFT ENG NO START IN NR 2 POSITION. WORKED IN BOTH. REPLACED IGNITION EXCITER, AND PLUG, NO HELP. REPLACED LEAD, OPS CHECK NORMAL.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 44,349 hrs · 12,290 cycles

NR 1 ENGINE COMPRESSOR STALL ON ENGINE RUNUP, ENGINE SHUT DOWN, PER CREW. SAMC FLETCH PROG TEXT: - ITEM ROLLED FORWARD. SAMC TEXT: COMPRESSOR STALL AT APPROX 40 PERCENT, SHUTDOWN, PER CREW. INSPECTED ENGINE UNISON RINGS, CHIP DETECTORS AND BOROSCOPED FOR FOD INGESTION (SNOW SLUDGE) LPC AND HPC NO DEFECTS FOUND. RAN ENGINE TO CRUISE POWER WITHOUT INCIDENT.

Part: CARBON SEAL — LEAKING (NR 2 ENGINE) · airframe 44,287 hrs · 12,275 cycles

NR 2 ENG HIGH OIL CONSUMPTION. REPLACED NR 2 ENG DE-OILER CARBON SEAL. ACP 5 MIN IDLE RUN, NO LEAKS NOTED.

Part: VALVE — FAULTY (AC BAY) · airframe 43,862 hrs · 12,157 cycles

LEFT PACK OFF ON GROUND AT GROUND IDLE. LIGHT OUT WHEN POWER ADVANCED. REPLACED HI-STAGE VALVE & CONTROLLER. GROUND CHECK GOOD.

Part: VALVE — FAULTY (LT AC PACK) · airframe 43,862 hrs · 12,157 cycles

LEFT PACK OFF ON GROUND AT GROUND IDLE. LIGHT OUT WHEN POWER ADVANCED. REPLACED HI-STAGE VALVE & CONTROLLER. GROUND CHECK GOOD.

Part: VALVE — FAULTY (LT AC PACK) · airframe 43,862 hrs · 12,157 cycles

LEFT PACK OFF ON GROUND AT GROUND IDLE. LIGHT OUT WHEN POWER ADVANCED. REPLACED HI-STAGE VALVE & CONTROLLER. GROUND CHECK GOOD.

Part: VALVE — DEFECTIVE (APU) · airframe 43,726 hrs · 12,119 cycles

APU BLEED INOP. REPLACED CAPU SURG VALVE, OPS CHECKED OK. BLEED OK PSI AT ENG START RECOVERY AND PACK OPERATION NORMAL.

Part: VALVE — DEFECTIVE (APU) · airframe 43,726 hrs · 12,119 cycles

APU BLEED INOP. REPLACED APU SURGE VALVE, OPS CHECKED OK. BLEED OK PSI AT ENG START RECOVERY AND PACK OPERATION NORMAL.

Part: CONTROLLER — DEFECTIVE (APU) · airframe 43,720 hrs · 121,187 cycles

APU START FAILED TWICE. APU DOOR STATUS MESSAGE. APU INOP WON'T START. REPLACED APU CONTROLLER FOR TROUBLESHOOTING.

Part: ACTUATOR — FAULTY (APU) · airframe 43,720 hrs · 121,187 cycles

APU START FAILED TWICE. APU DOOR STATUS MESSAGE. APU INOP, WON'T START. REPLACED INLET DOOR ACTUATOR.

Part: SHUTOFF VALVE — FLUCTUATES (BLEED AIR SYS) · airframe 43,628 hrs · 12,087 cycles

LEFT DUCT PRESSURE FLUCTUATED 20 PSI DURING DESCENT WITH POWER JUST ABOVE IDLE. REPLACED HPSOV. TESTED AND NO LEAK DETECTED.

Part: VALVE — FAULTY (NR 1 ENGINE) · airframe 43,580 hrs · 12,074 cycles

NR 1 ENGINE HUNG START BEFORE STARTER CUTOUT. THRUST LEVER ADVANCE NOT ATTEMPTED. REPLACED 14TH STG CONVERTER VALVE AND ONE FAILED 8TH STG VSV RUNNER GUIDE BLOCK.

Part: SHUTOFF VALVE — FAULTY (LT ENGINE) · airframe 43,517 hrs · 12,053 cycles

LEFT ENG SLOW TO SPOOL, SUSPECT PRSOV NOT FULLY CLOSED. FLT DECK OVERHEAD INDICATED VALVE OPEN, WHEN IT SHOULD BE CLOSED. REPLACED PRSOV, ENGINE STARTED NORMAL TWO ATTEMPTS.

Part: SHUTOFF VALVE — FAILED (LT ENGINE) · airframe 43,458 hrs · 12,037 cycles

LEFT ENG BLEED VLV WILL NOT COMPLETELY CLOSE WHEN SW IS PLACED IN THE OFF POSITION. HISTORY. REPLACED PRSOV VALVE. LEAK CHECKED. RAN 5 MINUTES AND BLEED OPEN AND CLOSED NORMAL.

Part: START VALVE — FAULTY (NR 1 ENGINE) · airframe 43,361 hrs · 12,013 cycles

LT START VALVE WON'T ENGAGE CIRCUIT BREAKER POPPED. RPL NR1 ENG START VALVE. MOTORED ENGINE, START CONTROL CB STAYED IN AND START VALVE OPS AND LEAK CHECKED GOOD.

Part: STARTER — FAULTY (APU) · airframe 43,123 hrs · 11,952 cycles

APU FAILED TO START. FAULT LGT ILLUM AND EICAS MSG. APU FAULT DISPLAYED. ADDITIONAL START ATTEMPTS UNSUCCESSFUL. CREW COMMENTS: 4 ATTEMPTS UNSUCCESSFUL. EGT ROSE TO 790 RPM 21. AUTO SHUTDOWN. REMOVED & REPLACED APU STARTER. OP CHECKS GOOD.

Part: CONTROL UNIT — NO TEST (HMG) · airframe 43,090 hrs · 11,942 cycles

HMG DOES NOT TEST. REPLACED HYDRAULIC MOTOR GENERATOR CONTROL UNIT. OP CHECKS OKAY.

Part: IDG — FAILED (RIGHT) · airframe 43,090 hrs · 11,942 cycles

THE R GEN DRIVE LIGHT ON WITH ASSOCIATED EICAS DURING TAXI OUT. VERIFIED GEN BAD. GEN OIL SMELLED BURNED. REPLACED RT ENG IDG. OPS NORMAL.

Part: SHUTOFF VALVE — FAULTY (LT ENGINE) · airframe 43,048 hrs · 11,929 cycles

LEFT ENGINE BLEED VALVE WILL NOT CLOSE WHEN SWITCH IS MOVED TO THE OFF POSITION. DUCT PRESS RISES WHEN THROTTLES WERE ADVANCED. REMOVED AND REPLACED PRSOV. OP CHECKS AND LEAK CHECKS GOOD.

Part: COVER — LOOSE (CABIN) · airframe 42,686 hrs · 11,833 cycles

EMERGENCY FLOOR LIGHTING STRIP AT 13C IS PEELING BACK. SECURED LOOSE PLASTIC COVER ON TRACK.

Part: IDG — FAULTY (RT ENGINE) · airframe 42,616 hrs · 11,817 cycles

RT IDG DRIVE LIGHT AND MESSAGE ON TAXI OUT. DISCONNECTED IDG PER SAM. RETURN TO GATE. IDG IS OUT OF TOLERANCE. REPLACED RT ENGINE IDG. OP CHK'D GOOD ON ENGINE RUN. NO LEAKS, NO FAULTS.

Part: SCAVENGE PUMP — LEAKING (NR 1 ENGINE) · airframe 42,527 hrs · 11,794 cycles

FOUND OIL LEAKED FROM LUBE SCAVENGE PUMP HOUSING ON NR 1 ENG. FOUND OIL LEAKING FROM PUMP. REPLACED LUBE-SCAVENGE PUMP.

Part: INVERTER — FAULTY (EMERGENCY LIGHTS) · airframe 42,038 hrs · 11,659 cycles

EEL LIGHTS IN AISLE LAST SECTION ARE INOP FOUND BAD INVERTER. FOUND AFTER BATTERY HAD TIME TO CHARGE LIGHTS OPS CK GOOD.

Part: CONTROL MODULE — MALFUNCTIONED (SPOILERS) · airframe 45,857 hrs · 12,738 cycles

EICAS SPOILERS LIGHT WITH SPOILERS UP OR DOWN. REPLACED NR 3 RT SPOILER CONTROL MODULE ACCOUNT OF SHOWING HARD FAIL FAULT.

Part: HEAT EXCHANGER — LEAKING (LT ENGINE) · airframe 40,478 hrs · 11,243 cycles

LEFT ENGINE OIL LEAK OUT OF LIMITS. LEAK FROM NR 5 DRAIN. FOUND LEAK AT FUEL OIL HEAT EXCHANGER. REMOVED NR 1 ENG FUEL OIL HEAT EXCHANGER AND BYPASS VLV. REPLACED, LEAK CHECKED AND ENGINE RUNS WERE GOOD.

Part: FEEDER CABLE — SHORTED (EMERGENCY LIGHTS) · airframe 40,460 hrs · 11,238 cycles

EEL LIGHTS STRIP INOP FROM ROW 31 TO 34. FOUND A SHORT IN THE EEL STRIP. REPLACED EEL LIGHT STRIPS, OPS CHECKS OK.

Part: CONTROL MODULE — MALFUNCTIONED (SPOILERS) · airframe 40,377 hrs · 11,216 cycles

EICAS SPOILERS MSG ON UPPER EICAS AND ON OVERHEAD PANEL. REPLACED SPOILER CONTROL MODULE- M535 WAS FAULTING GROUND TEST.

Part: LIGHT — UNSECURE (CABIN) · airframe 40,222 hrs · 11,181 cycles

EXIT PATH LIGHTING NOT SECURED TO FLOOR AT ROW 13 ABC. CAUSE, UNKNOWN. SECURED EEL LIGHT TO FLOOR TRACK.

Part: LIGHT — MISSING (CABIN) · airframe 38,893 hrs · 10,792 cycles

DOOR 3R LIGHT BULB INSERT NEXT TO EXIT LIGHT MISSING. INSTALLED NEW LIGHT ASSY.

Part: BATTERY PACK — LOOSE (EMERGENCY LIGHTS) · airframe 38,864 hrs · 10,786 cycles

CEILING EEL EXIT LIGHT OUT AT OVERWING POSITION. FOUND BATTERY PACK LOOSE. SECURED LOOSE BATTERY PACK AT SEAT 23DEF.

Part: LIGHT — UNSECURE (STRIP AT ROW 13) · airframe 38,342 hrs · 10,624 cycles

STRIP OF EMERGENCY LIGHTS BUNCHED UP AT ROW 13. 10-30-07 RE-SECURED LIGHT.

Part: HOSE — DEFECTIVE (COCKPIT) · airframe 37,840 hrs · 10,484 cycles

OXYGEN MASK HOSE DEFECTIVE AT 2 (1=CAPT, 2=1ST OF, 3= 1ST OBS).

Part: INDICATION SYS — MALFUNCTIONED (COCKPIT) · airframe 37,700 hrs · 10,447 cycles

CREW REPORTED GEAR HANDLE TO OFF THEN EICAS DOORS & GEAR DISAGREE. ALSO HAD HOT RUBBER ODOR IN COCKPIT. PERFORMED TROUBLESHOOTING OF PSEU INPUTS AND TARGET TESTED OK. NO INBOARD STATUS MESSAGE. CREW CYCLED HANDLE AND SYSTEM OPERATED OK. NO PREVIOUS HISTORY ON RECORD. NO FLIGHT FAULTS. NO OTHER MAINTENANCE SYSTEM MESSAGE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,831 hrs · 10,196 cycles

EXTERIOR EMERGENCY EXIT LIGHT OUT AT DOOR 2L. [06-22-07] RELAMPED.

Part: GENERATOR — FAILED (NR 2) · airframe 36,808 hrs · 10,190 cycles

FLIGHT DIVERTED DUE TO LOSS OF NR 2 GENERATOR. [08-07-07] RT GENERATOR DRIVE DISC LIGHT ILLUMINATED WITH EICAS MSG. REPLACED RIGHT GCU. RESET DRIVE DISC AND SERVICED IDG AS PRECAUTIONARY.

Part: GIRT BAR — DIRTY (L2 DOOR) · airframe 36,646 hrs · 10,139 cycles

DOOR 2L WILL NOT ARM. [06-14-07] REMOVED DEBRIS FROM GIRT BAR AREA, SECURED COSMETIC SEAL.

Part: STRAP — LOOSE (R1 DOOR) · airframe 36,319 hrs · 10,037 cycles

DOOR 1R WILL NOT ARM. [06-14-07] FOUND "D" RING STRAP LOOSE, RESECURED. DOOR ARMING OPERATION PUT BACK TO NORMAL.

Part: CHAIN — MISROUTED (L1 DOOR) · airframe 36,144 hrs · 9,982 cycles

MED 1LH HARNESS LATCH CHAIN MISROUTED OVER HARNESS FITTING. [06-14-07] ACCOMP'D ROUTINE JC'S TO RESTORE DOOR AND SLIDE TO NORMAL SAFE CONDITION. REROUTED CHAIN TO CORRECT POSITION.

Part: COVER — DAMAGED (CABIN) · airframe 35,729 hrs · 9,865 cycles

EEL STRIP COVER IS DAMAGED JUST FWD OF AFT FWD LAV APPROX 1.500 FT DAMAGED. REPLACED 25' SECTION OF EEL STRIP COVER.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,729 hrs · 9,865 cycles

AFT RT OVERWING EXIT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED.

Part: WIRE — DAMAGED (LAV SMOKE DETECT) · airframe 35,607 hrs · 9,830 cycles

LAV SMOKE DETECTOR LEFT CIRCUIT BREAKER WILL NOT RESET. FOUND WIRE CONNECTING LEFT LAV SMOKE DETECTOR SHORTED AROUND METAL GASPER DUCT BETWEEN CIRCUIT BREAKER AND DISC. REPAIRED WIRING TO FIX CIRCUIT BREAKER.

Part: A/C PACK — VIBRATION · airframe 34,329 hrs · 9,464 cycles

WITH BOTH PACKS ON LOUD RUMBLE AND VIBRATION HEARD AND FELT IN FIRST CLASS. REPLACED EQUIPMENT COOLING OVERBOARD AIR SHUTOFF (MOTOR OPERATED) EXHAUST VALVE. NO RE-OCURRENCE OF THIS PROBLEM NOTED SINCE THEN.

Part: WIRE — BURNED (INSTRUMENT PANEL) · airframe 30,835 hrs · 8,459 cycles

FOUND BURNED WIRES BEHIND CONNECTOR D40496 UNDER THE P37 PANEL. FIVE WIRES WERE FOUND DAMAGED WITHIN THE P37 PANEL IN THE VICINITY OF CONNECTOR D40496J ON AIRCRAFT 5596. FOUR WIRES WERE BURNT THROUGH AND ONE WIRE HAD INSULATION DAMAGE PRESENT UPON WIRE BUNDLE INSPECTION.

Part: BATTERY — INOPERATIVE (DOORS 1R) · airframe 29,036 hrs · 7,921 cycles

EMERGENCY EXIT LIGHTS AT DOOR 1R INOPERATIVE. REPLACED BATTERY PACK AT M730. REPLACED BATTERY PACK AT M730.

Part: APU — INOPERATIVE (APU BAY) · airframe 29,002 hrs · 7,913 cycles

RETURNED TO THE FIELD AT SFO AFTER THE APU WOULD NOT START AT TOP OF CLIMB. APU WAS REMOVED FROM AIRCRAFT AND TESTED IN APU TEST CELL. NO FAULT FOUND WITH APU S/N 61832. PASSED ALL TEST AND RETURNED TO SERVICE. AFTER APU REPLACEMENT, MECHANIC FOUND APU BATTERY LOW AND APU BATTERY CHARGER CIRCUIT BREAKER BROKEN. APU BATTERY WAS REPLACED AND OPERATION CHECKED OK.

Part: CONNECTOR — DISCONNECTED (ROW 16 ABC) · airframe 25,201 hrs · 6,833 cycles

EMERGENCY EXIT LIGHT INOP ABOVE SEAT 16ABC. FOUND DISCONNECTED CONNECTOR UNDER OVERHEAD SEALING PANEL. RECONNECTED.

Part: DOOR — WILL NOT TEST (OVERWING SLIDE) · airframe 23,687 hrs · 6,415 cycles

LEFT OVERWING SLIDE COMPARTMENT DOOR FAILED TO OPEN ON PNEUMATIC DEPLOYMENT TEST. NITROGEN SUPPLY REGULATOR USED FOR THE TEST WAS NOT CONFIGURED TO QUICKLY PROVIDE PRESSURE TO THE ACTUATOR TEST PORT. THE SUBSEQUENT, SUCCESSFUL, PNEUMATIC TEST WAS PERFORMED WITH A REGULATOR CONFIGURED TO QUICKLY DELIVER NITROGEN AT 1500 PSI TO THE ACTUATOR TEST PORT. AMM 25-65-00/501 'OFF-WING ESCAPE SYSTEM - ADJUSTMENT/TEST' HAVE INSTRUCTIONS TO QUICKLY APPLY PRESSURE TO 1500 PSI. THE CARRIAGE WILL NOT TURN OUT IF THE PRESSURE RELEASE IS SLOW.

Part: COMPUTER — FAILED (ELEVATOR) · airframe 14,295 hrs · 3,884 cycles

LANDING FLARE CONTROL PRESSURE TWICE THE NORMAL EFFORT (PITCH PRESSURE EXTREMELY HIGH). FAILURE OF THE ELEVATOR FEEL COMPUTER CAUSED THE EXTRA FORCE REQUIRED TO OPERATE THE CONTROL COLUMN. REPLACED THE ELEVATOR FEEL COMPUTER.

Part: ENGINE — BIRD STRIKE (NR 2)

RETURNED TO ABQ, ACCOUNT OF BIRD STRIKE TO NR 2 ENGINE ON TAKEOFF. *S/D* ACCOMPLISHED BIRD STRIKE INSPECTION. IDENTIFIED DAMAGE TO THE FAN BLADES AND INLET AREA. NO INTERNAL DAMAGE FOUND ON BORESCOPE. REPLACED DAMAGED FAN BLADES AND REPAIRED FAN INLET.