N284YV

Part: WIRE — LOOSE (CABIN) · airframe 43,480 hrs · 61,202 cycles

EMERGENCY OVERHEAD LIGHT AT ROW 9C DOES NOT ILLUMINATE. FLT 5415 RESECURED WIRE ON BACK OF EMERGENCY LIGHT FIXTURE AT ROW 9C.

Part: COMPUTER — MALFUNCTIONED (TE FLAP) · airframe 43,308 hrs · 60,968 cycles

FLAPS DISAGREE DURING DESCENT. PERFORMED GO-ROUND. RECYCLED FLAPS SEVERAL TIMES & FINALLY ALL FLAP PAIRS CAME DOWN. FLT 5405 REPLACED FLAP CONTROL COMPUTER.

Part: PANEL — CRACKED (RT WING) · airframe 43,372 hrs · 61,048 cycles

RT WING NR 2 FUEL PANEL LEAKING. FOUND LOWER WING STRINGER 10 OTBD FWD CORNER OF PANEL NR 2 CRACKED. C-CHECK REPAIRED RT WING LOWER STRINGER 10 AT PANEL NR 2 IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,202 hrs · 59,341 cycles

EMERGENCY LIGHTS ROW 9C BURNED OUT. (FLT 5415) RELAMPED EMERGENCY LIGHTS.

Part: CONNECTOR — DIRTY (NR 1 ENGINE) · airframe 42,067 hrs · 59,159 cycles

NR 1 ENGINE NP FLUCUATIONS ON TAKEOFF POWER UP BETWEEN 92 AND 96 PERCENT. BOTH ANALOG AND DIGITAL GAUGES SHOWED NP FLUCTUATIONS. (FLT 5415) CLEANED CONNECTOR ON LEFT NP PROBE AND SWAPPED INDICATOR CONNECTOR FROM SIDE TO SIDE. RAN ENGINES AND OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,754 hrs · 58,716 cycles

EMERGENCY OVERHEAD LIGHT AT 9C BURNED OUT. (FLT 6282) RELAMPED EMERGENCY LIGHT.

Part: WIRE HARNESS — FAILED (LANDING GEAR) · airframe 41,696 hrs · 58,625 cycles

AFTER LANDING, LANDING GEAR RIGHT A INDICATION WAS RED. B INDICATION WENT TO RED INTERMITTENTLY, TRIGGERING A LANDING GEAR WARNING. (FLT 6325) REPLACED RIGHT MLG "A" UP HARNESS AND "B" DOWN HARNESS.

Part: SIGN — BROKEN (CABIN) · airframe 41,575 hrs · 58,463 cycles

EMERGENCY EXIT SIGN ADJACENT SEAT 6C BROKEN. (FLT 5365) REPLACED EMERGENCY EXIT SIGN AT SEAT 6C.

Part: SEQUENCE VALVE — OUT OF ADJUST (LANDING GEAR) · airframe 41,447 hrs · 58,280 cycles

LEFT MAIN LANDING GEAR DID NOT RETRACT ON DEPARTURE. (FLT 1300) ADJUSTED SEQUENCE VALVES IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,684 hrs · 58,600 cycles

CAPTAINS WINDSHIELD SIDE POST AT TOP CRACKED COMPLETELY THROUGH SKIN SHEET. (C-CHECK) INSTALLED PERMANENT DOUBLER REPAIR ON LEFT UPPER SIDE DV WINDOW POST SKIN IAW ETD.

Part: SKIN — CRACKED (RT WING) · airframe 41,423 hrs · 58,241 cycles

ON RT WING SKIN LOWER SURFACE FOUND TO HAVE A CRACK EMANATING FROM THE DEFUELING/REFUELING ACCESS OPENING, OUTBOARD AFT CORNER. (C-CHECK) REPAIRED CRACKED SKIN ON RT WING LOWER SURFACE EMANATING FROM THE CORNER OF THE DEFUELING/REFUELING ACCESS CUTOUT, BY INSTALLING A DOUBLER REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,423 hrs · 58,241 cycles

LEFT FLOOR SEAT TRACK HAS CORROSION. (C-CHECK) REMOVED CORROSION FROM LEFT FLOOR SEAT TRACK AND REPLACED FORWARD END OF SEAT TRACK.

Part: STRINGER — CRACKED (LT WING) · airframe 41,423 hrs · 58,241 cycles

LEFT WING NR 2 FUEL RING HAS CRACKED NR 10 STRINGER. (C-CHECK) INSTALLED STRINGER SPLICE REPAIR TO NR 10 STRINGER LEFT WING AT NR 2 FUEL RING IAW SRM.

Part: BOLT — BROKEN (HYDRAULIC SYS) · airframe 41,202 hrs · 57,933 cycles

GREEN HYDRAULIC SYSTEM FAILURE. (FLT 6444) FOUND BROKEN BOLTS AT LEFT AND PACK ENGINE PRESSURE BYPASS POP OUT INDICATOR. REPLACED O-RING ASSEMBLY AND (4) BOLT ASSEMBLIES AT POPOUT ASSEMBLY.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,196 hrs · 56,541 cycles

CORROSION AND CRACK COMING FROM RIVET HOLE AT FRAME 23 FORWARD FUSELAGE RIGHT LOWER SIDE. REPAIRED DAMAGE AT FRAME 23 FORWARD FUSELAGE RIGHT LOWER SIDE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 40,196 hrs · 56,541 cycles

AFT END OF STRINGER 20L LEFT CENTER FUSELAGE HAS CORROSION. REPAIRED AFT END OF STRINGER 20L LEFT CENTER FUSELAGE IN REFERENCE TO SRM.

Part: LIGHT — UNSECURE (CABIN) · airframe 39,840 hrs · 56,075 cycles

FLT 6240, TRANSPARENT EMERGENCY FLOOR LIGHTING STRIP IN FRONT OF GALLEY HAS FALLEN OFF. SECURED EMERGENCY FLOOR LIGHTING STRIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,728 hrs · 55,916 cycles

FLOOR EMERGENCY EXIT LIGHT AT ROW NINE IS OUT. (FLT 5523) RELAMPED EMERGENCY LIGHT.

Part: LINKAGE — LACK OF LUBE (CABIN DOOR) · airframe 39,377 hrs · 55,432 cycles

MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN AND CLOSE. (FLT 5348) CLEANED AND LUBED PASSENGER DOOR LINKAGE AND CAMS.

Part: MECHANISM — OBSTRUCTED (CABIN DOOR) · airframe 39,377 hrs · 55,432 cycles

CABIN DOOR HARD TO OPEN. (FLT 5362) REMOVED EXCESSIVE GREASE FROM MAIN CABIN DOOR HANDLE INSIDE MECHANISM, AND LUBED MAIN CABIN DOOR HANDLE LINKAGE.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 39,377 hrs · 55,432 cycles

MAIN CABIN DOOR VERY DIFFICULT TO OPEN FROM INSIDE AND OUTSIDE. (FLT 6332) OPEN CENTER PANEL OF MAIN DOOR AND LUBED AS NEEDED.

Part: CONTROL UNIT — FAILED (LT PROPELLER) · airframe 39,371 hrs · 55,422 cycles

LEFT PROPELLER FEATHERS. (FLT 5460) REPLACED LEFT ENGINE PROPELLER CONTROL UNIT. P/N:782490-46 S/N OFF:980616

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,517 hrs · 54,230 cycles

TWO FLOOR EMERGENCY LIGHTS AT ROW 8 ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,976 hrs · 53,485 cycles

MIDDLE EMERGENCY LIGHTS DO NOT ILLUMINATE. (FLT 6423) REPLACED CENTER ELBP. P/N 0366-04-001, S/N ON 1319, S/N OFF 1128-09/95

Part: FUSE — BLOWN (CABIN) · airframe 37,976 hrs · 53,485 cycles

OVERWING EMERGENCY EXIT SIGNS NOT ILLUMINATING. (FLT 6493) REPLACED A BLOWN FUSE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,667 hrs · 53,031 cycles

EMERGENCY LIGHTS AT ROW 9 ARE OUT. (FLT 6818) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,667 hrs · 53,031 cycles

FLOOR LEVEL AND ROW 9 EMERGENCY LIGHTS ARE OUT. (FLT 6660) REPLACED NR 1 AND 3 ELBP'S. NR 1 P/N D366-04-001, S/N OFF 1159, NR 3 P/N D366-04-001, S/N OFF 1043.

Part: STRINGER — CRACKED (RT WING) · airframe 37,793 hrs · 53,227 cycles

RIGHT WING STRINGER NR 8 CRACKED AT 1ST ACCESS PANEL INBOARD OF NACELLE. (C-CHECK) REPAIRED STRINGER NR 8 ON RIGHT WING BETWEEN RIBS 8 AND 9 PER SRM.

Part: RCCB — BURNED (COCKPIT) · airframe 36,804 hrs · 51,847 cycles

SMELL OF ELECTRICAL SMOKE IN FIRST OFFICER'S SIDE PANEL. (FLT 6317) REPLACED RIGHT LANDING LIGHT RCCB.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 36,710 hrs · 51,697 cycles

MAIN CABIN DOOR HARD TO OPEN. (FLT. 6317) LUBRICATED MAIN CABIN DOOR.

Part: HOT WATER POT — FAULTY (GALLEY) · airframe 36,710 hrs · 51,697 cycles

ELECTRICAL SMELL FROM HOT WATER JUGS IN GALLEY. (FLT 4553) REMOVED AND REPLACED HOT JUGS.

Part: HANDLE — LACK OF LUBE (CABIN DOOR) · airframe 36,616 hrs · 51,554 cycles

MAIN CABIN DOOR HARD TO OPEN. (FLT 6450) LUBRICATED DOOR HANDLE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 36,599 hrs · 51,530 cycles

EMERGENCY EXIT SIGN AT 6A INOP. (FLT 6824) REPLACED LIGHT ASSEMBLY.

Part: WIRE — BROKEN (CABIN) · airframe 36,270 hrs · 51,072 cycles

FLOOR EMERGENCY LIGHT INOP. (FLT 6449) REPAIRED BROKEN WIRE.

Part: WIRE — BROKEN (CABIN) · airframe 36,170 hrs · 50,929 cycles

EMERGENCY FLOOR LIGHT INOP. (FLT 6417) REPAIRED BROKEN WIRE.

Part: WIRE — BROKEN (CABIN) · airframe 36,070 hrs · 50,777 cycles

TWO RED FLOOR EMERGENCY LIGHTS INOP. (FLT 6085)REPAIRED WIRE AND REPLACED LIGHT ASSEMBLY.

Part: FASTENER — LOOSE (DOOR) · airframe 35,996 hrs · 50,673 cycles

FORWARD DOOR HANDLE DIFFICULT TO OPERATE. (FLT 6687) SECURED LOOSE HARDWARE AT INNER HANDLE TORQUE TUBE ROD ENDS.

Part: CABLE — CORRODED (RUDDER TRIM) · airframe 35,851 hrs · 50,457 cycles

RUDDER TRIM FROZE INFLIGHT. (FLT 6821) REPLACED RUDDER TRIM ACTUATOR CABLE.

Part: STRINGER — CRACKED (NACELLE) · airframe 35,612 hrs · 50,139 cycles

SHEET METAL DAMAGE TO DOUBLER AT RIGHT INBOARD MAIN LANDING GEAR FORWARD DOOR. (SERVICE CK) REPLACED CRACKED INBOARD NACELLE STRINGER PER SRM.

Part: SIGNAL COND UNIT — FAILED (RT PROPELLER) · airframe 35,397 hrs · 49,822 cycles

FLT 6645 - AFTER LANDING, RIGHT PROP WENT INTO UNCOMMANDED FEATHER. REPLACED TQ SIGNAL CONDITIONER.

Part: ALTIMETER — INACCURATE (COCKPIT) · airframe 35,311 hrs · 49,711 cycles

FIRST OFFICERS ALTIMETER READING DIFFERS BY 120 TO 200 FEET. (FLT 5714) REPLACED FIRST OFFICERS ALTIMETER.

Part: SWITCH — DIRTY (LT ENGINE) · airframe 35,134 hrs · 49,468 cycles

LEFT ENGINE FEATHERS UNCOMMANDED. (FLT 6200)CLEANED MICROSWITCHES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,865 hrs · 49,078 cycles

ROW 6 CEILING EMERGENCY LIGHT INOP. (FLT 6642) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — BROKEN (CABIN) · airframe 34,118 hrs · 48,036 cycles

FLT 6312 - BOTH RED EMERGENCY FLOOR LIGHTS AT FORWARD ENTRANCE INOP. REPLACED RED LIGHT ASSEMBLY.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,334 hrs · 48,333 cycles

POST ANGLES CRACKED AT FRAME 10 AND 12 UNDER LEFT DV WINDOW. (C-CHECK) REPAIRED PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,334 hrs · 48,333 cycles

FRAMES CRACKED NEXT TO ACM ACCESS DOORS. (C CHECK) REPAIRED PER SRM.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 33,873 hrs · 47,723 cycles

FLT 6536 - CAPTAINS WINDSHIELD CRACKED. REPLACED PER AMM, PN NP-151311-1, SN OFF 01200H3559.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 33,506 hrs · 47,232 cycles

FLT 5406 - EXIT LIGHT ROW 9CDE IS BROKEN. SECURED COVER.

Part: PCU — MALFUNCTIONED (LEFT) · airframe 32,713 hrs · 46,174 cycles

FLT 5415 - AFTER ROLLOUT LEFT PROP WOULD GO TO FEATHER. REPLACED LEFT PCU, P/N 782490, S/N ON: 960232, S/N OFF: 861240.

Part: STRINGER — CRACKED (LT NACELLE) · airframe 32,232 hrs · 45,527 cycles

FIRST LEFT SIDE FUEL PANEL INBOARD OF NACELLE HAS A CRACKED STRINGER AT FRAME 8, RIB 9. PERFORMED REPAIR ON STRINGER PER EMB 120 SRM 57-20-03.

Part: ELECTRICAL SYS — MALFUNCTIONED · airframe 32,014 hrs · 45,223 cycles

AFTER SELECTING THE GEAR DOWN, THE ELECTRICAL SYSTEM TRANSFERRED TO EMERGENCY MODE. (FLIGHT #5719)INSPECTED AND OPERATED THE AUXILLARY GENERATOR TRANSFERRING AND ELECTRICAL EMERGENCY SYSTEMS. SWUNG GEAR MULTIPLE TIMES. NO DISCREPENCIES NOTED.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 30,515 hrs · 43,184 cycles

FLT 5620 - OXYGEN MASKS AT ROW 5 DROPPED. RESTOWED MASKS AND SECURED PANEL AT ROW 5. NO DISCREPANCIES NOTED.

Part: SKIN — CORRODED (ELEVATOR TAB) · airframe 30,493 hrs · 43,147 cycles

LEFT ELEVATOR TRIM TAB HAS CORROSION IN BETWEEN SKIN, FOUND AT C-CHECK. REPLACED LEFT ELEVATOR TRIM TAB IAW EMB 120 MM 27-32-01.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 30,437 hrs · 43,076 cycles

FLT 5415 - EMERGENCY LIGHTS ON FLOOR LIGHTING STRIP ARE INOP. REPAIRED BROKEN WIRE ON FLOOR LIGHTING STRIP. OPS CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,108 hrs · 42,594 cycles

EMERGENCY LIGHTS AFT OF ROW 6 ARE INOPERATIVE. REPLACED AFT ELBP PER MM 33-50-02, OPS CHECK GOOD, P/N - D366-04-001, S/N OFF - 1252.

Part: FLAP SYSTEM — OUT OF ADJUST (TE FLAPS) · airframe 29,781 hrs · 42,162 cycles

FLAPS WOULD NOT RETRACT PROPERLY ON TAKEOFF. OUTBOARD PAIR REMAINED 2 LIGHT BARS DOWN WITH FLAP DISAGREEMENT INDICATION, RETURNED TO LAX. REPLACED LEFT WING TRAILING EDGE FAIRING ADJACENT TO OUTBOARD FLAP. OPS CHECK GOOD.

Part: CONTROL LEVER — MALFUNCTIONED (TE FLAPS) · airframe 29,708 hrs · 42,064 cycles

AFTER TAKEOFF, A FLAP DISAGREEMENT APPEARED. THE OUTBOARD FLAPS DID NOT RETRACT AND THE DISAGREEMENT REMAINED. RETURNED TO LAX, CLEANED CONNECTORS ON OUTBOARD FLAP ACTUATORS. REPLACED FLAP CONTROL HANDLE IAW 27-50-00. OPS CHECKS GOOD.

Part: A/C PACK — SMOKE (LEFT) · airframe 28,804 hrs · 40,679 cycles

LEFT PACK FAILED AND BLEW SMOKE INTO COCKPIT ON GROUND. SECURED CLAMP ON LEFT ACM INLET. OPERATIONAL CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,672 hrs · 39,047 cycles

FLOOR LEVEL FORWARD RED TRACK EMERGENCY LIGHTS INOP. REPLACED FLOOR LEVEL RED TRACK EMERGENCY LAMPS AS REQUIRED.

Part: SKIN — CRACKED (WINDSHIELD) · airframe 27,366 hrs · 38,590 cycles

FOUND LEFT WINDSHIELD POST SKIN CRACKED IN 2 PLACES. COMPLIED WITH SB 120-53-0072 REV 0 21 FEB 00, LEFT SIDE PART V, SEE RII 53-301.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 26,198 hrs · 36,915 cycles

ONE RED FLOOR EMERGENCY LIGHT AT OVERWING EXITS INOP. REPAIRED WIRES TO RED FLOOR EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (AILERON TRIM TAB) · airframe 25,165 hrs · 35,325 cycles

AILERON TRIM VERY STIFF IN FLIGHT. REMOVED AND REPLACED AILERON TRIM TAB ACTUATOR ASSY IAW EMB 120 MM 27-12-01. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 24,060 hrs · 33,690 cycles

FORWARD EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD EMERGENCY BATTERY PACK IAW MM 33-50-02. OPERATIONAL CHECK GOOD. P/N 366-04-001, S/N OFF 1240/07-96.

Part: WIRE — FAILED (EMERGENCY LIGHT) · airframe 23,735 hrs · 33,158 cycles

ONE RED LIGHT ON EMERGENCY LIGHT STRIP IS BURNED OUT. REPAIRED WIRES TO RED LIGHT AT FORWARD FLOOR EMERGENCY LIGHTS, OPERATIONAL CHECK GOOD.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT) · airframe 23,637 hrs · 33,010 cycles

FLOOR LEVEL TRACK LIGHTS INOPERATIVE AT GALLEY. REPLACED MIDDLE POSITION EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT) · airframe 23,637 hrs · 33,010 cycles

SEVERAL EMERGENCY LIGHTS INOPERATIVE. INSTALLED NEW EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD.

Part: SUPPORT BRACKET — CRACKED (COCKPIT WINDOW) · airframe 23,558 hrs · 32,896 cycles

FRAME 12 SUPPORT BRACKET AT PILOT'S DV WINDOW CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INTERCOSTAL AFT OF PILOT'S DV WINDOW AT FS 3900 (BETWEEN FRAME 12, 13) PER EMB 120 SRM 51-40-02.

Part: SKIN — CORRODED (FUSELAGE) · airframe 23,558 hrs · 32,896 cycles

AT RIB 15A IN PAX DOOR ENTRANCE AFT OF PAX DOOR AFT ACTUATOR RIB CLIP IS CORRODED THROUGH TO SKIN. P/N 120-09800-001. DISCOVERED DURING C-CHECK INSPECTION. REMOVED FRAME SHEAR AT FRAME 15A. INSTALLED FRAME 15A SHEAR TIE BETWEEN STRINGER 18L - 19L.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 23,558 hrs · 32,896 cycles

STRINGER 18L AT FS 482(5) APPROX CORRODED OUT OF LIMITS PER EMB 120 SRM 53-00-03; APPROX 3 INCH AREA. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPLACEMENT STRINGER SECTION 18L AND SPLICE DOUBLERS 2 EA PER EMB 120 SRM 53-00-00.

Part: BRACKET — CRACKED (NACELLE) · airframe 23,558 hrs · 32,896 cycles

RIGHT HYDRAULIC PACK RESERVOIR, RIGHT LOWER MOUNTING BOLT BRACKET CRACKED INSIDE. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INBOARD SIDE OF RIGHT HYDRAULIC PACK VERTICAL MOUNT BRACKET PER SRM 51-40-02.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 23,558 hrs · 32,896 cycles

RIGHT FRAME 13 FLOOR PROP CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED RIGHT FLOOR PROP AT FRAME 13 IAW SRM 53-10-10.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 23,558 hrs · 32,896 cycles

LEFT FRAME 13 FLOOR PROP CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED FRAME 13 FLOOR PROP ON LEFT SIDE IAW SRM 53-10-10.

Part: WIRE — BROKEN (CONTROL COLUMN) · airframe 23,345 hrs · 32,562 cycles

FIRST OFFICER'S STALL WARNING SHAKER INOP. REPAIRED BROKEN WIRE NEAR SHAKER CONNECTOR ON CONTROL COLUMN OF FIRST OFFICER'S SIDE. OPS CHECKS GOOD.

Part: FAN — FAILED (CABIN) · airframe 23,252 hrs · 32,416 cycles

DURING DESCENT, EXPERIENCED A BURST OF SMOKE COMING FROM THE PACKS AND INTO THE COCKPIT AND CABIN. THE SMOKE SUBSIDED AFTER TURNING OFF THE RECIRC AND GASPER FANS. AFTER DEPLANING THE PASSENGERS, TRIED TURNING ON THE FANS AND THE SMOKE STARTED AGAIN. REPLACED LEFT RECIRC FAN. OPS CHECK GOOD. NO SMOKE NOTED.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT) · airframe 23,156 hrs · 32,267 cycles

ONE STRIP OF FLOOR EMERGENCY LIGHTING INOP. REMOVED MIDDLE ELBP AND INSTALLED SERVICEABLE UNIT. OPS CHECK GOOD.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 22,802 hrs · 31,756 cycles

CENTER CABIN SECTION (ROWS 4-7) EMERGENCY LIGHTS; FLOOR, SIDE AND CEILING; WILL INTERMITTENTLY FAIL BY DIMMING OUT AFTER ILLUMINATING FOR SEVERAL SECONDS DURING TEST. REMOVED AND REPLACED MID BATTERY PACK IAW 33-50-02. OPS CHECK GOOD. S/N OFF: 1076/06-92.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,641 hrs · 31,514 cycles

EMERGENCY LIGHTS WILL NOT TEST ROW 6 OVERHEAD; FLOOR BETWEEN ROW 3 AND 6. REMOVED AND REPLACED MIDDLE BATTERY PACK WITH A SERVICEABLE UNIT. OPS CHECK GOOD.

Part: WIRE — BROKEN (STICK SHAKER) · airframe 22,490 hrs · 31,260 cycles

F/O'S STICK SHAKER IS INOP. REPAIRED BROKEN WIRE AT SERVO SHAKER. OPS CHECK OKAY.

Part: WIRE — BROKEN (STALL WARNING) · airframe 22,152 hrs · 30,747 cycles

FIRST OFFICER STALL TEST HAS A PUSHER BUT NO SHAKER. REPAIRED BROKEN WIRE TO F/O'S SHAKER. OPS CHECK GOOD.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 21,425 hrs · 29,607 cycles

EMERGENCY LIGHTS AT ROW 6 DOOR, AND FLOOR LIGHTS BETWEEN ROW 3 AND 6, FOUND INOPERATIVE DURING F/A PREFLIGHT CHECKS. REPLACED ROW 6 EMERGENCY LIGHTS FUSE. OPS CHECK GOOD.

Part: BATTERY — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 21,181 hrs · 29,277 cycles

EMERGENCY LIGHTS DO NOT ILLUMINATE ON FLOOR STRIP ROWS 2 TO 6, KNEE LEVEL EXIT SIGNS AT ROW 6 AND OVERHEAD ROW 6. REMOVED AND REPLACED CENTER EMERGENCY LIGHTS BATTERY PACK. OPERATIONAL CHECK GOOD.

Part: BRACKET — DAMAGED (LT MLG DOOR) · airframe 20,589 hrs · 28,382 cycles

LEFT OUTBOARD MAIN GEAR DOOR OPENED IN FLIGHT ON LEFT MAIN GEAR. REPLACED AFT HINGE BRACKETS ON LEFT NACELLE OUTBOARD FORWARD DOOR WITH SERVICEABLE UNITS. STRAIGHTENED DOOR SKIN. INSPECTED LATCH MECHANISM AND FOUND TO BE SERVICEABLE. OPS CHECK GOOD.

Part: LATCH — FAILED (LG DOOR) · airframe 20,372 hrs · 28,065 cycles

LEFT SIDE FORWARD OUTBOARD GEAR DOOR CAME UNLATCHED IN FLIGHT. LATCHED OK, BUT HAPPENED 2X. REPLACED LANDING GEAR DOOR LATCH PIN AS REQUIRED. OPS CHECK GOOD.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 19,875 hrs · 27,332 cycles

CARGO UPPER FWD LATERAL STOP MOUNT PAD POSSIBLE CRACK (POSITION NR 1). FABRICATED AND INSTALLED DOUBLER AT POSITION NR 1, UPPER FWD LATERAL STOP MOUNT OF CARGO DOOR PER SRM 52-30-02 AND RII 52-301.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 19,875 hrs · 27,332 cycles

CARGO DOOR AFT TRACK TOP MOUNT SUPPORT CRACKED. REPLACED TOP SUPPORT WITH SERVICEABLE UNIT FOR CARGO DOOR AFT TRACK.

Part: FIREWALL — CRACKED (FUSELAGE) · airframe 19,875 hrs · 27,332 cycles

LEFT SIDE APU FIREWALL HAS SMALL CRACK AT LARGE CANNON PLUG TOP, RIGHT MOUNT SCREW. STOP-DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-10-00.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 19,412 hrs · 26,616 cycles

ABORTED TAKEOFF DUE TO TRIM AURAL WARNING. TRIM WAS IN THE GREEN RANGE AT 38 DEGREES CG. CHECKED TRIM WARNING SYSTEM. OPS CHECKS GOOD.

Part: WIRE HARNESS — DEFECTIVE (LT MLG) · airframe 18,757 hrs · 25,623 cycles

AFTER GEAR HANDLE WAS MOVED UP, ALL GREEN LIGHTS STAYED ON AND ALL RED LIGHTS ILLUMINATED EXCEPT A-LEFT MAIN GEAR. GEAR WOULD NOT RETRACT. PDX SWAPPED LEFT MAIN A & B SENSOR LEADS PER SNL 20-32-0015. SWUNG GEAR. DEFERRED RED B-LIGHT IAW MEL 32-60-1A. GEAR OPS CHECK GOOD. FOUND B-UPLOCK PROX TO BE OPERATIONAL. HOWEVER, FOUND A-UPLOCK TO BE INOP. REPLACED A-UPLOCK PROX HARNESS PER MM 32-61-01. ALL GEAR INDICATIONS CHECK GOOD ON GEAR SWING.

Part: PRESSURE SWITCH — MALFUNCTIONED (RT ENGINE) · airframe 18,525 hrs · 25,306 cycles

RIGHT ENGINE AIR INLET BOOT FAILED AT 17,000 FT, -5 DEGREES CELSIUS. RECYCLED MULTIPLE TIMES. FINALLY WORKED DURING DESCENT WITH POSITIVE TEMPS. BOOT CYCLE WAS VISIBLE BUT MAP LIGHT INDICATED FAILURE.REPLACED RIGHT ENGINE DEICE PRESSURE SWITCH IAW MM 30-20-03. RAN FOR SEVERAL MINUTES WITHOUT FAULT. P/N: 211C117-183 S/N ON: S50860A S/N OFF: S30815A

Part: CONNECTOR — CONTAMINATED (RT FLAP ACTUATOR) · airframe 18,011 hrs · 24,516 cycles

FLAP DISAGREEMENT WARNING AFTER SELECTION OF FLAPS 45. OUTBOARD FLAP PAIR INDICATES 2 BAR DISAGREEMENT. COMPUTER FAULT CODES SHOWING RIGHT OUTBOARD FLAP NOT RESPONDING. FOUND MOISTURE IN RIGHT OUTBOARD FLAP ACTUATOR CANNON PLUG, CLEANED MOISTURE. OPS CHECKED GOOD OF FLAP SEVERAL TIMES.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 17,226 hrs · 23,354 cycles

EMERGENCY EXIT SIGNS AT ROWS 5 AND 6 DO NOT ILLUMINATE. INSTALLED SERVICEABLE MIDDLE BATTERY PACK IAW 33-50-00. OPS CHECK GOOD. S/N ON 1335, S/N OFF 1089.

Part: FASTENER — LOOSE (FUEL DOOR) · airframe 17,226 hrs · 23,354 cycles

SERVICE DOOR WARNING LIGHT ON TAKEOFF ROLL. TAKEOFF ABORTED. INBOARD FUEL DOOR CAM LOCK LOOSE. RESECURED, OPS CHECK GOOD.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 16,972 hrs · 23,011 cycles

AT APPROXIMATELY 60 KNOTS ON TAKEOFF FIRST OFFICERS EADI AND EHSI BOTH WENT BLANK FOR APPROXIMATELY 3 - 5 SECONDS. RED DPU FAIL ON EADI. AFTER CALLING ABORT (30 KNOTS) SCREENS RELIT. REMOVED AND REPLACED FIRST OFFICERS DPU. P/N 622-7711-003, S/N OFF 7032, S/N ON 2774. OPS CHECK NORMAL.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 16,941 hrs · 22,962 cycles

ON BEGINNING OF TAKEOFF ROLL, A SINGLE CHIME SOUNDED AND THE ATTITUDE DISPLAY MAP LIGHT ILLUMINATED WITH ASSOCIATED PIT AND ROLL FLAGS ON THE CAPTS EHSI. ABORTED TAKEOFF. REORIENTED NR 1 AHRS COMPUTER. GROUND CHECKS GOOD.

Part: CONNECTOR — CONTAMINATED (NR 2 PITOT HEAT) · airframe 16,707 hrs · 22,624 cycles

NR 2 PITOT HEAT FAILED IN FLIGHT, AUTO PILOT FAILED, HIGH SPEED WARNING WENT OFF WHEN FIRST OFFICER'S AIRSPEED FLUCTUATED. EN ROUTE FROM MRY TO LAX. DIVERTED TO SBA. FOUND CONTAMINATION OF WATER IN NUMBER TWO PITOT CANNON PLUG. DRIED WATER AND CLEANED CONTAMINATION. OPERATED NUMBER TWO PITOT HEAT, OPS CHECK GOOD. TESTED AUTOPILOT SYSTEM. COULD NOT DUPLICATE. OPS CHECK GOOD.

Part: WARNING LIGHT — ILLUMINATED (HYD SYSTEM) · airframe 16,627 hrs · 22,502 cycles

AFTER TAKEOFF GREEN SYSTEM HYDRAULIC FILTER LIGHT AND HYDRAULIC MAP LIGHT ILLUMINATED AFTER GEAR RETRACTION. RETURNED TO LAX. REMOVED GREEN SYSTEM ENGINE PUMP RETURN FILTER AND INSPECTED NO PARTICLES NOTED. INSTALLED NEW FILTER AND RESET BYPASS INDICATOR PIN. RUN UP FOR OPS AND LEAK CHECK GOOD.

Part: AFCS — FAILED (TRIM) · airframe 16,500 hrs · 22,313 cycles

SHORTLY AFTER TAKEOFF HAD AN ELECTRIC TRIM FAILURE. CONTINUED TO LAX. ELECTRIC TRIM SYSTEM OPS CHECK GOOD. COULD NOT DUPLICATE DISCREPANCY.

Part: COMPUTER — MALFUNCTIONED (AHRS) · airframe 15,994 hrs · 21,572 cycles

WHEN ENGAGED ON CAPTAIN''S SIDE, AUTOPILOT COMMENCES A RIGHT TURN AWAY FROM COMMAND BARS (FLIGHT DIRECTOR). WORKED FINE EN ROUTE HOWEVER, ONCE DESCENT INITIATED AIP WOULD NOT RESPOND TO FLIGHT DIRECTOR. F/O''S SIDE APPEARS TO FUNCTION NORMALLY. DIVERTED FROM ACV TO SFO. REPLACED NUMBER ONE AHRS COMPUTER AND RE-INITIALIZED. AUTOPILOT SYSTEM OP CHECKS GOOD IAW MM 22-11-00. P/N ON: 6226190-204, S/N ON: 967, S/N OFF: 714,

Part: BEARING — LOOSE (LT MLG DOOR)

LEFT MAIN LANDING GEAR WOULD NOT RETRACT, BOTH RED A AND B LIGHTS STAYED ON. INSPECTED LEFT FOWARD GEAR DOOR AND FOUND OUTBOARD DOOR FOWARD BEARING LOOSE, ALLOWING DOOR TO BE LOOSE AT DOOR SEQUENCE VALVE. REMOVED AND REPLACED LOOSE BEARING AS NEEDED AND ADJUSTED SEQUENCE VALVE TARGET IAW MM 528100. GEAR SWUNG AS NEEDED, OPS CHECK GOOD.

Part: UNKNOWN

LEFT ENGINE INLET DE-ICE BOOT FAILS AFTER 2 MINUTES. RETURNED TO FIELD. FOUND SIGNIFICANT AIR LEAKAGE AT LEFT PRESSURE REGULATOR VALVE FITTING. SECURED LOOSE FITTING. OPS CHECKS GOOD PER MM 30-10-00.

Part: UNKNOWN

MIDDLE LEFT WING, INBOARD RIGHT WING AND INBOARD LEFT STABILIZER BOOTS FAILED IN FLIGHT. RETURNED TO SEA. REMOVED AND REPLACED LEFT MIDDLE WING DE-ICE PRESSURE SWITCH IAW MM30-10-05. REMOVED AND REPLACED INBOARD WING AND STABILIZER EJECTOR VALVE IAW MM30-10-0. REMOVED AND REPLACED MIDDLE WING EJECTOR IAW MM 30-10-04. RAN ENGINES AND OPS CHECK DE-ICE BOOTS ON GROUND.

Part: ENGINE — MALFUNCTIONED (RIGHT)

INADVERTENT AUTOFEATHER AT 1200 FEET. TORQUE WENT TO 146 PERCENT ON LEFT ENGINE. RETURNED TO LAX. INSTALLED SERVICEABLE LEFT ENGINE IAW MM 71-00-00. CHANGED LEFT PROPELLER ALSO. CAUSE OF AUTOFEATHER UNKNOWN UNTIL FURTHER TEARDOWN OF COMPONENTS COMPLETED.

Part: RETRACT MECH — MALFUNCTIONED (NLG DOOR)

LEFT NOSE LANDING GEAR DOOR REMAINED OPENED AFTER GEAR RETRACTION. RETURNED TO PSP. LATCHED GEAR DOOR AND CHECKED DOORS FOR SECURITY. FOUND DOORS SECURE.

Part: AHRS COMPUTER — FAILED (COCKPIT)

ABOUT 30 MINUTES AFTER FIRST OFFICERS EADI FAILED, PIT YELLOW FLAG ON CAPTAIN AND FIRST OFFICERS AND A/P STARTED PITCHING UP AND HAD TO BE DISCONNECTED. FIVE MINUTES LATER, HDG YELLOW FLAG AND WE HAD 10 FT-15 FT DIFFERENCE FROM CAPTAINS TO FIRST OFFICER'S HEADING INDICATORS. DIVERTED FROM SFO TO FAT. REPLACED FIRST OFFICER'S AHRS COMPUTER. FIRST OFFICER'S AND CAPTAIN'S AHRS SYSTEM TESTS NORMALLY PER MM 34-21-00. BOTH A/P AND FD SYSTEMS TEST NORMALLY PER MM 22-11-00.

Part: TIMER — FAILED (RT ENG DEICE)

RIGHT ENGINE INLET DEICE FAILED INFLIGHT. RETURNED TO SEA. REMOVED AND REPLACED RIGHT ENGINE INLET DEICE TIMER. GROUND RUN, OPS CHECKS GOOD.

Part: SWITCH — FAILED (RT HORIZ STAB)

RIGHT OUTBOARD STABILIZERS FAIL ON BOTH TIMERS. RETURNED TO FAT. REPLACED RIGHT OUTBOARD STABILIZER PRESSURE SWITCH, OPS CHECKS GOOD.

Part: PROX SENSOR — FAILED (NLG)

SBA - LANDING GEAR FAILED TO RETRACT ON DEPARTURE. AIRCRAFT RETURN TO STATION WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NOSE GEAR SHOCK ABSORBER PROXIMITY SENSOR. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURN TO SERVICE. (M)

Part: ENGINE — OVERTEMP (LT/RT)

SFO - POSSIBLE ENGINE OVERTEMP AND OVER TORQUE REPORTED ON BOTH ENGINES DURING STALL WARNING ACTIVATION WHILE AIRCRAFT WAS IN HOLDING PATTERN. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT REMAINS IN SFO MAINTENANCE. (M)

Part: AIR DISTRIBUTION — ODOR (CABIN)

LAX - SMOKE SMELL IN CABIN REPORTED. MAINTENANCE DEFERRED COOLING SYSTEM PER MEL 21-51-2. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY PERFORMING OPERATIONAL CHECK. UNABLE TO DUPLICATE DISCREPANCY. SWAPPED GROUND COOLING FANS FOR TROUBLESHOOTING. (M)

Part: FAN — FAILED (CABIN)

FAT - ELECTRICAL ODOR REPORTED FROM RIGHT PACK. MAINTENANCE DEFERRED RIGHT PACK PER MEL 21-51-2. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY REPLACING RIGHT GROUND COOLING FAN. OPERATIONAL CHECK SATISFACTORY. (M)

Part: CONTROL BOX — FAILED (COCKPIT)

LAX - INTRANSIT A-LIGHTS REMAIN ILLUMINATED WHEN GEAR RETRACTED. MAINTENANCE REPLACED CONTROL BOX. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY — DISCHARGED (CABIN)

SMX - EMERGENCY LIGHT AT ROW 4 FORWARD THROUGH GALLEY FAIL TO ILLUMINATE. MAINTENANCE DEFERRED EMERGENCY LIGHTING PER MEL 33-50-1. OPENED DMI 77715. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY REPLACING EMERGENCY LIGHT BATTERIES. OPERATIONAL CHECK SATISFACTORY. (M)

Part: TIRE — FAILED (RT MLG)

SFO - BOTH RT MAIN TIRES BLEW OUT ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE FOUND DAMAGE TO INBOARD AFT GEAR DOOR, PROXIMITY SENSOR, HYDRAULIC BAY DOOR, AND NACELLE. REPLACED BOTH TIRES AND WHEEL ASSEMBLIES. AIRCRAFT FERRIED TO FAT FOR FURTHER REPAIRS. REPAIRED GEAR DOORS, REPLACED BROKEN PROXIMITY SENSOR. INSPECTED NACELLE, FOUND DENTS TO BE WITHIN LIMITS. OPERATIONAL CHECK OF LANDING GEAR SYSTEM SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)

Part: DOOR LATCH — OBSTRUCTED (AVIONICS BAY)

FAT - SERVICE DOOR LIGHT CAME ON DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE REMOVED RUBBER TRIM PIECE FROM AVIONICS BAY DOOR LATCH. SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: RETRACTION JACK — OUT OF ADJUST (RT MLG)

SFO - RIGHT MAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO FAT. MAINTENANCE ADJUSTED RIGHT MAIN LANDING GEAR RETRACTION JACK AND UPLOCK PROXIMITY SENSOR. SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: PROXIMITY SENSOR — OUT OF ADJUST (RT MLG)

SFO - RIGHT MAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO FAT. MAINTENANCE ADJUSTED RIGHT MAIN LANDING GEAR RETRACTION JACK AND UPLOCK PROXIMITY SENSOR. SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CABLE — FRAYED (LT AILERON)

DURING A 1600 HOUR CONTROL CABLE INSPECTION, FOUND LEFT WING LOWER AILERON CABLE, P/N 12027655-005, WORN WITH BROKEN STRANDS AT WING STATION Y2902 WHERE CABLE PASSES THROUGH NYLON GROMMET, P/N PE49068-505, AT OUTBOARD NACELLE STRUCTURE. IT APPEARS THAT THE CABLE ROUTING THROUGH THE NACELLE ALLOWS FOR THE CABLE TO RUB CONTINUOUSLY ON THE BULKHEAD GROMMET CAUSING PREMATURE WEAR OF THE CABLE ASSEMBLY.