N188SW

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 42,067 hrs · 51,578 cycles

FORWARD PORTION OF EMERGENCY LIGHT FLOOR STRIP INOPERATIVE. REPLACED FORWARD EMERGENCY LIGHT BATTERY, OPERAIONAL CHECK GOOD.

Part: ACTUATOR — INOPERATIVE (TE FLAPS) · airframe 41,936 hrs · 51,413 cycles

BOTH OUTBOARD FLAPS WILL NOT MOVE. REMOVED AND REPLACED RIGHT OUTBOARD FLAP AND LEFT NACELLE FLAP ACTUATOR IAW EMB MM 27-50-04. OPERATIONAL CHECK GOOD IAW 27-50-00.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAP) · airframe 41,916 hrs · 51,388 cycles

FLAP DISAGREEMENT AT 45 DEGREES OUTBOARD PAIR AT 25 DEGREES AND FLASHING. REPLACED CANNON PLUG ON LEFT OUTBOARD FLAP ACTUATOR IAW WM 20-50-01 AND REPLACED LEFT NACELLE FLAP ACTUATOR IAW MM 27-50-08. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (OUTBOARD FLAP) · airframe 41,839 hrs · 51,293 cycles

RETRACTED FLAPS FROM 15 TO UP AND GOT A DISAGREEMENT ON THE OUTBOARD PAIR, PROBLEM CLEARED AFTER APPROX 1 MIN. LANDING IN SLC, SELECTED FLAPS 45 AND GOT A DISAGREEMENT ON THE OUTBOARD PAIR. PROBLEM CLEARED AFTER LANDING. REPLACED RIGHT OUTBOARD FLAP ACTUATOR, OPERATIONAL CHECK GOOD IAW 27-50-09.

Part: ACTUATOR — MALFUNCTIONED (OUTBOARD FLAP) · airframe 41,831 hrs · 51,283 cycles

FLAP CONTROL FAULT OUTER FLAPS STUCK 2 BARS. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR IAW 27-50-09. OPERATIONAL CHECK GOOD.

Part: CONTROL LEVER — FAULTY (COCKPIT) · airframe 41,831 hrs · 51,283 cycles

FLAP CONTROL FAULT WITH OUTBOARD FLAPS STUCK AT 7 DEGREES. REMOVED AND REPLACED FLAP SELECTOR LEVER AND CLEANED OUTBOARD FLAP CANNON PLUGS IAW 27-50-00. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — MALFUNCTIONED (TE FLAPS) · airframe 41,779 hrs · 51,221 cycles

UPON RETRACTING FLAPS AFTER DEPARTURE, GOT FLAP CONTROL FAULT. FOUND MOISTURE IN BOTH OB FLAP ACTUATOR CONNECTOR PLUGS, CLEANED AND REINSTALLED CONNECTOR PLUGS. OPERATIONAL CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,078 hrs · 50,369 cycles

LIGHT BULB OUT ON ESCAPE PATH LIGHTING. RELAMPED AND REPLACED SOCKET IAW 33-51-01. OPS CHECK GOOD.

Part: WIRE — BROKEN (TRIM SWITCH) · airframe 41,072 hrs · 50,363 cycles

FIRST OFFICER'S ELECTRIC TRIM WHEN PUSHED FORWARD, SETS OFF THE TRIM FAIL WARNING. REPAIRED WIRE AT TRIM SWITCH.

Part: PICKUP — MALFUNCTIONED (TORQUE METER) · airframe 41,015 hrs · 50,296 cycles

RIGHT TORQUE GAUGE WOULD ONLY RESPOND TO 20 PERCENT. RIGHT ENGINE FEATHERED. ABORTED TAKEOFF. REPLACED THE TORQUE METER PICK-UP PROBE IAW 77-11-02. OPERATIONAL CHECK GOOD. P/N: 4002-0000-02.

Part: SPAR CAP — CRACKED (LT NACELLE) · airframe 40,976 hrs · 50,251 cycles

LEFT WING LOWER SURFACE OUTBOARD OF LEFT NACELLE FUEL LEAKING NEAR SKIN JOINT. FOUND WING LOWER FORWARD SPAR CRACK CRACKED. REPAIRED SPAR CAP IAW EMB SRM 57-20-05.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 40,762 hrs · 49,995 cycles

OUTBOARD FLAP PAIR CAUSES DISAGREEMENT ON FLAP RETRACTION AFTER TAKEOFF. FIXES ITSELF AND RETRACTS FLAPS AFTER ABOUT 2 SECS, HAPPENED ON 3 FLIGHTS. REMOVED AND REPLACED FLAP CONTROL UNIT. OPS CHECK GOOD IAW EMB MM 27-50-06.

Part: CONTROL PANEL — MALFUNCTIONED (STALL WARNING) · airframe 40,564 hrs · 49,770 cycles

STALL WARNING LIGHT ON MAP ILLUMINATED IN FLIGHT. TURNED OFF SYSTEM 2 WARNING SWITCH, STILL WON`T RESET, NO LIGHT ON LOWER PANEL BUT MAP LIGHT STAYS ILLUMINATED. REMOVED AND REPLACED STALL WARNING CONTROL PANEL. OPS CHECK GOOD.

Part: PIN — BROKEN (CONNECTOR) · airframe 40,460 hrs · 49,625 cycles

F/O'S ELECTRIC TRIM NOSE UP INOP. REPAIRED BROKEN PIN ON J2 PIN 1. RERACKED APC NR 2. OPS CHECK GOOD IAW MM 22-10-00.

Part: ANNUNCIATOR — MALFUNCTIONED (TE FLAPS) · airframe 40,417 hrs · 49,556 cycles

IN FLIGHT, RECEIVED CONTROL FAULT-FLAP, ADVANCED SWS ON MAP, NO LIGHTS ON FLAP PANEL. TRIED TO RESET PER QRH WITHOUT SUCCESS. REPLACED FLAP ANNUNCIATOR. OPS CHECKS GOOD.

Part: HMU — MALFUNCTIONED (LT ENGINE) · airframe 40,405 hrs · 49,544 cycles

ON CLIMBOUT FROM SLC, RECEIVED AN APPARENT AUTOFEATHER ON THE LEFT ENGINE. THE PROP FEATHERED AND TORQUE INDICATED 145 PERCENT. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN. REMOVED AND REPLACED LEFT TSCU, HMU AND EEC. OPS CHECKS GOOD OF ALL SYSTEMS. TSCU P/N: 30005-0000-57, S/N OFF: 855.73-301. HMU P/N OFF: 786390-0, S/N OFF: M80009. EEC P/N OFF: 800414-2-003, S/N OFF: 90049994.

Part: WIRE — DAMAGED (NACELLE FLAPS) · airframe 40,391 hrs · 49,528 cycles

ON TAXI WITH FLAP SELECTOR SET TO 15 DEGREES AFTER 1-2 MINUTES, FLAP & ADV SWS ON MAP POSITION INDICATOR 0 DEGREES OUTBOARD LIGHT BAR 4 LIGHTS NACELLE, INBOARD AND COMD ONE LIGHT BAR. AFTER FIVE MINUTES SYSTEM CORRECTED ITSELF. INSTALLED NEW WIRES TO I/B, O/B & NACELLE FLAP ACTUATORS FROM FUSELAGE P0365. INSTALLED CONNECTORS (NEW) AT ACTUATORS AND AT FUSELAGE P0365. REFERENCE EMB WM 27-51-00. CONTINUITY CHECK SATISFACTORY.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 40,346 hrs · 49,485 cycles

RIGHT INBOARD FLAP WON'T COME UP. REMOVED AND REPLACED FLAP CONTROL UNIT IAW 27-50-06, OPS CHECK GOOD. P/N ON 307500-1007, S/N OFF 0133.

Part: CONNECTOR — DIRTY (TE FLAPS) · airframe 40,346 hrs · 49,485 cycles

ON SELECTING FLAPS 45 DEGREES OUTBOARD FLAPS STAY AT 25 DEGREES WITH FLAP DISAGREEMENT LIGHT. FOUND CONNECTOR TO BOTH INBOARD AND OUTBOARD FLAP ACTUATOR TO BE WET WITH DEICE FLUID. CLEANED ALL 4 CONNECTORS. OPS CHECKED GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 40,190 hrs · 49,304 cycles

FLAP DISAGREEMENT. REMOVED AND REPLACED FLAP CONTROL UNIT IAW MM 27-50-01. OPS CHECK GOOD.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 40,026 hrs · 49,103 cycles

IN FLIGHT, RT OIL PRESSURE DROPPED TO 40 PSID. ON 20 MILE FINAL OIL PRESSURE WENT TO 0. REMOVED AND REPLACED RIGHT ENGINE ASSEMBLY PER EMB 120 MM 71-00-00 AND RII 72-301. RAN ENGINE. OPS AND LEAKS CHECKS GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (STALL WARNING) · airframe 39,969 hrs · 49,040 cycles

STALL WARNING LIGHT WON'T EXTINGUISH ON PANEL. REMOVED AND REPLACED STALL WARNING CONTROL PANEL. OPS TESTED GOOD. P/N: 120-34428-505, S/N OFF: 386792.

Part: INDICATOR — MALFUNCTIONED (MLG) · airframe 39,771 hrs · 48,801 cycles

LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. ALL GREEN LIGHTS REMAINED ILLUMINATED, ALL RED LIGHTS REMAINED ILLUMINATED EXCEPT RIGHT B-LIGHT. TRIED TO CYCLE THE GEAR SEVERAL TIMES. REMOVED AND REPLACED RIGHT A-SYSTEM UP/DOWN HARNESS ASSEMBLY PER EMB120 MM 32-61-01. OPS CHECKS GOOD. P/N: 120-22623-501.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 39,635 hrs · 48,639 cycles

FLAP DISAGREEMENT ON OUTBOARD PAIR WHEN FLAPS 45 DEGREES SELECTED. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR IAW EMB MM 27-50-00. OPS AND LEAK CHECK GOOD.

Part: PROXIMITY SENSOR — MALFUNCTIONED (LT MLG) · airframe 39,584 hrs · 48,581 cycles

LANDING GEAR WOULD NOT EXTEND NORMALLY, GEAR EXTENDED USING ELECTRICAL OVERRIDE PROCEDURE.FOUND LEFT MAIN GEAR 'A' DOWN LOCK PROX SENSOR INOP. REPLACED MAIN "A" HARNESS IAW EMB120 MM 32-61-01. OPS CHECK GOOD. P/N: 120-22623-501

Part: FRAME — CRACKED (LT NACELLE) · airframe 39,536 hrs · 48,501 cycles

LT ENGINE FRAME 1 CRACKED. DISCOVERED DURING C-CHECK. REMOVED & REPLACED FRAME 1 PER SB 120-54-0036 WITH NEW P/N 120-0351-003.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 39,536 hrs · 48,501 cycles

RIGHT WINDSHIELD POST CRACKED. DISCOVERED DURING C-CHECK. COMPLIED WITH SB120-53-0072.

Part: FRAME — CRACKED (RT NACELLE) · airframe 39,536 hrs · 48,501 cycles

RT ENGINE FRAME 1 CRACKED. DISCOVERED DURING C-CHECK. REMOVED & REPLACED FRAME 1 PER SB 120-54-0036 WITH NEW P/N 120-0351-004.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 39,320 hrs · 48,242 cycles

CREW REPORTS THE LEFT OUTBOARD FLAP IS SLOW DEPLOYING TO 45 DEGREES. REMOVED FAULTY FLAP ACTUATOR ON LEFT OUTBOARD FLAP AND REPLACED WITH A SERVICEABLE UNIT AS REQUIRED BY EMB MM 27-50-09. OPS CHECK GOOD. NO LEAKS NOTED.

Part: INDICATOR — FAILED (HSI) · airframe 38,773 hrs · 47,603 cycles

CAPTAIN'S HSI FAILURE AFTER TAKEOFF, WENT VERY DIM, THEN BLACK. A MINUTE OR SO LATER IT CAME SLOWLY ON THEN IT WENT SLOWLY BLACK AGAIN. NO FLAGS. REPLACED RELAYS K0395 AND K0397. NR 1 EHSI OPS CHECK GOOD IAW MM 34-22-00. AUX GEN 1 AND 2 OPS CHECK GOOD IAW MM 24-31-00. RELAYS REPLACED IAW MM 24-52-04. P/N OFF: M83536/33-003L.

Part: INDICATOR — MALFUNCTIONED (ATTITUDE) · airframe 38,611 hrs · 47,404 cycles

CAPTAIN'S ATTITUDE INDICATOR INDICATED APPROX 15 DEGREES BANK TO THE LT WITH WINGS LEVEL. ATTITUDE RESET HAD NO EFFECT. ATTITUDE DISPLAY WAS ILLUMINATED ON THE MAP. RETURNED OT SLC. REMOVED AND REPLACED NR 1 AH85 IAW 34-25-00. COMPLIED WITH OPS CHECK AS REQUIRED. OPS CHECK GOOD.

Part: RELAY — MALFUNCTIONED (HSI) · airframe 38,556 hrs · 47,325 cycles

FIRST OFFICER'S EHSI WENT BLANK ON TAKEOFF GOING THROUGH 500 FT. RETURNED TO SFO. INSTALLED KNOWN SERVICEABLE RELAYS AT K0394 AND K0396. NR 2 EHSI SCREEN REMAINED UNAFFECTED BY AUX GENERATOR POWER TRANSFERS. HEADING INDICATION CHECKS GOOD.

Part: STRINGER — CRACKED (RT WING) · airframe 38,556 hrs · 47,325 cycles

RIGHT WING LOWER STRINGER 10 IS CRACKED. FOUND DURING C-CHECK INSPECTION. COMPLIED WITH SB120-57-0037, REPLACEMENT OF STRINGERS NR 8 AND 10, LOWER RIGHT SIDE.

Part: INDICATOR — ERRATIC (LT ENGINE) · airframe 38,515 hrs · 47,264 cycles

ERRATIC T6 INDICATIONS, FLUCTUATING AS MUCH AS 100 PERCENT, ON THE LT ENGINE. ALL OTHER GAUGES REMAINED NORMAL. NO SURGING OF ENGINE HEARD OF FELT. REPLACED NR 1 T6 INDICATOR. RAN ENGINE. ALL INDICATIONS NORMAL.

Part: RCCB — MALFUNCTIONED (RT PROPELLER) · airframe 38,515 hrs · 47,264 cycles

INFLIGHT ''RIGHT INOP'' PROP DEICE LIGHT ILLUMINATED, TIMER 1 AND TIMER 2, COLD AND NORM. FAILS 1:30 IN NORM AND ;35 IN COLD. RETURNED TO THE FIELD. REMOVED AND REPLACED RCCB CB0226 IAW EMB 120 MM 24-52-05. OPS CHECK OF LEFT AND RIGHT PROPELLER DEICE GOOD.

Part: STRUCTURE — LEAKING (LT WING) · airframe 37,861 hrs · 46,454 cycles

LEFT OUTBOARD FLAP ACTUATOR REMOVED DUE TO FUEL CONTAMINATION ON FLAP FROM FUEL LEAK. REPAIRED LEAK IN FUEL CELL & INSTALLED ACTUATOR IAW 28-10-00 & 27-50-00.

Part: PROXIMITY SENSOR — FAILED (RT MLG) · airframe 37,426 hrs · 45,926 cycles

RIGHT MAIN LANDING LIGHT REMAINS ILLUMINATED. RETURNED TO SLC. REPLACED RIGHT MAIN LANDING GEAR B CHANNEL DOWNLOCK PROXIMITY SENSOR IAW 32-61-01. SWUNG LANDING GEAR 4 TIMES, OPERATIONS NORMAL.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 36,851 hrs · 45,250 cycles

TRIPLE CHIME HIGH SPEED WARNING ON TAKEOFF. ABORTED TAKEOFF. CHECKED BOTH AIRSPEED INDICATOR HIGH SPEED WARNINGS AND FOUND BOTH TO BE OPERATING AND NORMAL. OPS CHECK GOOD AT THIS TIME.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 36,814 hrs · 45,209 cycles

CARGO DOOR LIGHT CAME ON DURING TAKEOFF (ABORTED). CARGO DOOR MICRO SWITCH FOUND TO BE OVER CENTERED. ADJUSTED SWITCH, OPS CHECKS GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 36,814 hrs · 45,209 cycles

HIGH SPEED AURAL WARNING ACTIVATED AT 80 KTS ON TAKEOFF ROLL. OPERATED TEST PER MM 34-12-01. NO DISCREPANCIES NOTED ON GROUND.

Part: CONTROL BOX — MALFUNCTIONED (LANDING GEAR) · airframe 36,734 hrs · 45,115 cycles

AFTER TAKEOFF FROM JAC LANDING GEAR DID NOT RETRACT. HANDLE WENT UP BUT NO GEAR, HAD ALL LIGHTS - A & B, RED AND GREEN. SAME ON 2ND TRY PER MX CONTROL. RIGHT MAIN GEAR DOES NOT FULLY RETRACT ON FIRST TRY. CYCLED GEAR AND RETRACTION SUCCESSFUL. REMOVED AND REPLACED LANDING GEAR RELAY BOX IAW EMB MM 32-31-02. CYCLED GEAR SEVERAL TIMES. OPS CHECK GOOD. ADJUSTED RIGHT MLG ACTUATOR IAW 32-32-10. ALSO REPLACED LANDING GEAR RELAY BOX. S/N OFF: 120124, S/N ON 120230.

Part: ACTUATOR — MALFUNCTIONED (T/E FLAP) · airframe 36,682 hrs · 45,056 cycles

FLAP DISAGREEMENT UPON RETRACTING FLAPS ON CLIMBOUT. PERFORMED QRH AND WORKED NORMAL FOR THE REMAINDER OF THE FLIGHT. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR IAW 27-50-00. OPS CHECK GOOD.

Part: CONTROL BOX — INTERMITTENT (LANDING GEAR) · airframe 36,682 hrs · 45,056 cycles

LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. FOUND LANDING GEAR OVERNIGHT PINS INSTALLED IN GEAR. REMOVED GEAR PIN. GEAR WOULD RETRACT AND DEPLOY NORMALLY. FOUND GEAR TO HAVE INTERMITTENT INDICATION PROBLEM. REMOVED AND REPLACED LANDING GEAR CONTROL BOX AND RELAY.

Part: PIN — DEFECTIVE (FLAP ACTUATOR) · airframe 36,511 hrs · 44,867 cycles

AFTER TAKEOFF FLAPS WOULD NOT COMPLETELY RETRACT. A FLAP DISAGREEMENT RESULTED. DID QRH PROCEDURE, IT DID NOT CLEAR. RETURNED TO LAND. AFTER LANDING FLAPS RETURNED OK. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR CONNECTOR PIN. CYCLED FLAPS NUMEROUS TIMES. OPS CHECK GOOD. P/N: MS3476L12-10S.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 36,511 hrs · 44,867 cycles

HIGH SPEED AURAL WARNING ON TAKEOFF. ABORTED TAKEOFF. REMOVED AND REPLACED NR 1 AIRSPEED INDICATOR. OPS CHECK GOOD IAW 34-12-01.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 36,499 hrs · 44,853 cycles

FLAP DISAGREEMENT OUTBOARD AFTER TAKEOFF. FLAPS RETRACTED AFTER QRH PROCEDURE. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR. OPS CHECKS GOOD. LEAK CHECKS GOOD IAW MM 27-50-09.

Part: SWITCH — INTERMITTENT (PAX DOOR) · airframe 36,499 hrs · 44,853 cycles

CABIN DOOR STAYS HYDRAULICALLY PRESSURIZED INTERMITTENTLY AND WILL NOT OPEN. FLIGHT ATTENDANT CABIN DOOR BUTTON NEEDED TO BE TOGGLED TO RELEASE PRESSURE. REMOVED AND REPLACED CABIN PASSENGER DOOR CONTROL SWITCH AT F/A STATION. OPS CHECKS GOOD IAW MM 52-10-00.

Part: ROLLER — WORN (T/E FLAP) · airframe 36,378 hrs · 44,722 cycles

ON CLIMBOUT FLAP DISAGREEMENT, WOULD NOT FIX ITSELF. RAN QRH PROCEDURE. RESET FLAPS TO 15 DEGREES, THEN BACK TO 0. FLAP DISAGREEMENT WENT OUT. REMOVED AND REPLACED RT WING O/B FLAP O/B ROLLER WITH NEW ROLLER. OPS CHECK GOOD AT THIS TIME.

Part: GROUND WIRE — LOOSE (LT MLG WW) · airframe 36,271 hrs · 44,601 cycles

LEFT GEAR WELL EMITTED A SHOWER OF SPARKS WHEN THE LEFT ELECTRIC HYDRAULIC PUMP WAS TURNED ON. FABRICATED AND INSTALLED DOUBLER OVER ARC-WELDED HOLE AND RE-ATTACHED GROUND FOR HYDRAULIC PUMP IAW SRM 51-70-06 AND 51-40-02.

Part: SMOKE — DETECTED (CABIN) · airframe 35,908 hrs · 44,173 cycles

SMELL OF SMOKE IN COCKPIT WHILE AIRCRAFT ON THE GROUND.CHECKED AVIONIC COMPARTMENT, BATTERY COMPARTMENT AND HYDRAULIC COMPARTMENT AND FOUND NO DISCREPANCIES. SMELLED NO SMOKE OR BURNED MATERIALS.

Part: CONNECTOR — CONTAMINATED (TE FLAPS) · airframe 35,908 hrs · 44,173 cycles

FLAP DISAGREEMENT WHEN FLAPS BROUGHT UP FROM 15 DEGREES ON TAKEOFF (HAPPENED REPEATEDLY) THEN GOES AWAY. CLEANED OUTBOARD FLAP ACTUATOR CANNON PLUGS. TESTED FLAP. NO FAULTS.

Part: BATTERY — DISCHARGED (CABIN) · airframe 35,893 hrs · 44,156 cycles

EMERGENCY EXIT SIGN WILL NOT ILLUMINATE ROW 9.REMOVED AND REPLACED NR 3 EMERGENCY BATTERY PACK.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 4,138 hrs · 4,792 cycles

FLAP DISAGREEMENT WHEN SELECTING 45 DEGREES. CLEANED MOISTURE FROM RIGHT OUTBOARD CANNON PLUG (INSTALLED FLAP ACTUATOR TEST BOX). NO FAULTS NOTED ON ALL FLAP ACTUATORS. REINSTALLED FECU. SECURED DOORS. OPERATED FLAPS SEVERAL TIMES. OPS CHECK GOOD.

Part: TIRE — FAILED (MLG) · airframe 35,467 hrs · 43,667 cycles

LEFT OUTBOARD MAIN TIRE BLEW ON LANDING. (SLC) FOUND NR 1 BRAKE HAD LOCKED UP DUE TO POOR CONDITIONS. REMOVED AND REPLACED THE NR 1 BRAKE ASSEMBLY IAW A/C MM 32-41-05. PN ON 2-1661 SN ON 0055 SN OFF 1466. ALSO REMOVED AND REPLACED THE NR 1 MAIN WHEEL ASSY. OPS CHECKED GOOD IAW 32-44-02. PN ON 3-1446-1 SN ON 2716 SN OFF 0152.

Part: FCU — MALFUNCTIONED (T/E FLAPS) · airframe 34,851 hrs · 42,966 cycles

IN DESCENT THROUGH 18,000 FLAP/ADV SWS LIGHT ILLUMINATED AS WELL AS CONTROL FAULT INBOARD FLAP LIGHTS (2ND FROM TOP) FLASHING (QRH PROCEDURE UNSUCCESSFUL). CAPT AUTOPILOT DISCONNECTED. TRY TO RE-ENGAGE AND AC PITCHED NOSE DOWN AT RAPID RATE. REMOVED AND REPLACED THE FLAP CONTROL COMPUTER IAW MM 27-50-06. OPERATED THE FLAPS, COULD NOT DUPLICATE THE PROBLEM AFTER FECU REPLACMENT OPS CHECKS GOOD. P/N ON 307500-1007, S/N ON 0102, S/N OFF 0193. OPERATED THE NR 1 AUOTPILOT SYSTEM IAW MM 22-10-00. COULD NOT DUPLICATE THE PROBLEM. NO PITCH TENDANCIES NOTED AT THIS TIME.

Part: CONTROL UNIT — MALFUNCTIONED (FLAP) · airframe 34,817 hrs · 42,926 cycles

FLAP DISAGREEMENT ON INBOARD FLAPS DURING TAXI IN. REMOVED FLAP CONTROL UNIT AND RE-RACKED. OPS CHECK OK.

Part: ACTUATOR — FAILED (T/E FLAPS) · airframe 34,716 hrs · 42,807 cycles

FLAP DISAGREEMENT ON OUTBOARD FLAPS WHEN SELECTING FLAPS 45 DEGREES. REPLACED LEFT OUTBOARD FLAP ACTUATOR. FLAP OPS CHECKS GOOD. P/N ON 3203001007, S/N ON 0738, S/N OFF 850.

Part: CONNECTOR — CONTAMINATED (TE FLAPS) · airframe 34,256 hrs · 42,274 cycles

FLAP DISAGREEMENT ON SELECTION OF FLAP 45 DEGREES (OUTBOARD FLAPS WOULD NOT EXTEND BEYOND LAST LIGHT BAR ON FLAP ANNUNCIATOR PANEL). FOUND GLYCOL IN LEFT OUTBOARD CANNON PLUG. CLEANED PLUG. OPS CHECK GOOD.

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 34,198 hrs · 42,209 cycles

CONTROL FAULT ON ARRIVAL INTO SLC. INBOARD FLAPS DO NOT EXTEND. TRIED RESET BUT DIDNT WORK. REMOVED AND REPLACED ACTUATOR ON LEFT WING INBOARD SIDE FLAP, IAW EMB MM 27-50-09. OPS AND LEAKS CHECKS GOOD. PN ON: 320300-1005 SNON: 0139 SNOFF: 0838

Part: CONNECTOR — CONTAMINATED (TE FLAPS) · airframe 34,200 hrs · 42,212 cycles

FLAP CONTROL FAULT OR FLAP WARNING INDICATOR WITH ASSOCIATED ADVANCED SWS AND FLAP ON MAP ILLUMINATED INFLIGHT. ALSO GREEN LIGHTS FLASH ON INBOARD PAIR. IT WILL RESET, BUT INDICATES COME BACK AFTER FEW MINUTES. REMOVED AND CLEANED ALL CANNON PLUGS IN FLAP WELLS. PERFORMED OPERATION CHECKS IAW 27-50-00. ALL CHECKS SATISFACTORY.

Part: ROLLER — FAILED (TE FLAPS) · airframe 33,981 hrs · 41,966 cycles

FLAP DISAGREEMENT (OUTBOARD) WHEN SELECTING FLAPS FROM 25 TO 45 SETTING. REMOVED AND REPLACED LEFT OUTBOARD FLAP ROLLERS IAW EMB120 MM 27-50-13. OPS CHECK GOOD.

Part: CONNECTOR — CONTAMINATED (TE FLAPS) · airframe 33,981 hrs · 41,966 cycles

FLAP DISAGREEMENT WHEN SELECTING FLAPS FROM 25 TO 45 SETTING (OUTBOARD). INSPECTED FLAP AND FOUND DEICE FLUID ON LEFT OUTBOARD AND LEFT INBOARD FLAPS CANNON PLUGS. CLEANED PLUGS. RAN FLAPS. OPS CHECK GOOD AT THIS TIME.

Part: WARNING LIGHT — ILLUMINATED (SERVICE DOOR) · airframe 33,790 hrs · 41,754 cycles

DOOR (SERVICE) LIGHT ON TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. DEFERRED DOOR WARNING SYSTEM. SLC - REPAIRED DOOR IAW 51-70-01. OPS CHECKS WARNING SYSTEM CHECKED GOOD.

Part: INDICATOR — MALFUNCTIONED (TE FLAPS) · airframe 33,743 hrs · 41,697 cycles

AFTER SELECTING FLAPS 15 DEGREES ON TAXI CHECK, INBOARD FLAPS STOPPED AT 10 DEGREES. CYCLED FLAPS SEVERAL TIMES AFTER CLEARING FAULTS. NO FAULTS DETECTED AT ANY POSITION. OPS CHECKS GOOD.

Part: SWITCH — FAILED (E/E BAY DOOR) · airframe 33,737 hrs · 41,689 cycles

SERVICE DOOR LIGHT ILLUMINATED ON TAKEOFF ONLY. ABORTED TAKEOFF. REMOVED AND REPLACED AVIONICS DOOR MICRO SWITCH AND ADJUSTED IAW MM 52-73-02. OPS CHECKS GOOD.

Part: ACTUATOR — FAILED (RT MLG) · airframe 33,395 hrs · 41,304 cycles

RIGHT MAIN GEAR WOULD NOT RETRACT. CYCLED TWICE, NO LUCK. RETURNED TO SLC. REPLACED RIGHT MAIN GEAR HYDRAULIC ACTUATOR IAW 32-11-00, 32-21-00, 32-30-00 RII 32-302. P/N ON: 19595-000-07, S/N: T00067, S/N OFF: B45.

Part: SEQUENCE VALVE — FAILED (RT MLG) · airframe 33,296 hrs · 41,189 cycles

RIGHT MAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RECYCLED LANDING GEAR TWICE. ON SECOND RETRACTION GEAR HESITATED, THEN CAME UP. CONTINUED TO SLC. REMOVED AND REPLACED RIGHT MLG INBOARD SEQUENCE VALVE. SWUNG GEAR. OPS AND LEAK CHECKS GOOD IAW MM 32-32-04. P/N ON: 120-32943-001, S/N: 1777, S/N OFF: 225.

Part: EEC — FAILED (ENGINE) · airframe 32,933 hrs · 40,784 cycles

LEFT EEC FAILED ON TAKEOFF ROLL. ABORTED TAKEOFF, CHECKED EEC SYSTEM. TROUBLESHOOTING FOUND VARYING RESISTANCE ON T18 WIRING. REPLACED LT EEC WIRE HARNESS 720110. ENGINE GROUND RUN GOOD (P/N 3039368) (S/N 8N175) ON, (S/N AA4313).

Part: ROLLER — CONTAMINATED (LT MLG)

LEFT MAIN GEAR FAILED TO RETRACT. REMOVED LARGE CHUNK OF ICE FROM UPLOCK ROLLER. TEST FLEW AIRCRAFT AND OPERATED GEAR 3 TIMES WITH NO PROBLEMS,

Part: WARNING — ACTIVATED (LANDING GEAR)

ON CLIMB-OUT THROUGH 23,000 FT, AURAL LANDING GEAR WARNING SOUNDED WITH ASSOCIATED LIGHT ON MAP AND REPEATED AURAL WARNINGS. RETURNED TO SLC. CHECKED ALL LANDING GEAR WARNINGS AND FOUND ALL WORKING NORMAL. BOTH EEC'S WERE DEFERRED AND SUSPECT THAT UPPER POWER LEVER MICROSWITCH WAS BEING TRIGGERED. ALL CHECKS GOOD. UNABLE TO DUPLICATE DISCREPANCY.

Part: REGULATOR — FAILED (RT ENGINE)

RIGHT ENGINE DUCT LEAK LIGHT CAME ON DURING DESCENT. SHUT ENGINE DOWN ACCORDING TO QRH PROCEDURES. REMOVED AND REPLACED RIGHT DE-ICE PRESSURE REGULATOR. RUN UP CHECKS GOOD ON DUCT LEAK. NO LEAKS FOUND.

Part: HMU — MALFUNCTIONED (LT ENGINE)

TORQUE ON LEFT ENGINE FLUCTUATED AND THEN DROPPED OFF TO 26 PERCENT TORQUE ACCOMPANIED BY FUEL FLOW FLUCTUATION. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN. RETURNED TO SLC. REMOVED AND REPLACED LEFT ENGINE HMU IAW RII 73-301 AND MM 73-21-00. OPS CHECKS GOOD.

Part: FITTING — DAMAGED (LT PNEUMATIC SYS)

AT 11,000 FEET WE GOT A DUCT LEAK LIGHT. AFTER DOING QUICK REFERENCE HANDBOOK AND WAITING 3 MINUTES THE LIGHT REMAINED ON. BEFORE GETTING ENGINE SHUT DOWN THE LIGHT EXTINGUISHED. RETURNED TO SLC. REMOVED AND REPLACED DAMAGED FITTING TO INLET OF LEFT AIR PRESSURE REGULATOR PER EMB 120 MM 20-10-04. ALSO, REMOVED AND REPLACED LEFT PRESSURE REGULATOR VALVE PER EMB 120 MM 30-10-06. RAN LEFT ENGINE FOR 20 MINUTES HIGH POWER SETTING WITH PACKS ON. OPS CHECK GOOD WITH NO LEAKS NOTED.

Part: ACTUATOR — FAILED (RT TE FLAP)

FLAP ASYMMETRY AFTER TAKEOFF UPON FLAP RETRACTION. RETURNED TO EKO. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR.

Part: FILTER — CONTAMINATED (BLUE HYD SYST)

HYDRAULIC FILTER BLUE SYSTEM LIGHT ILLUMINATED. RETURNED TO SLC. REPLACED BLUE SYSTEM RETURN FILTERS. OPS AND LEAKS CHECKS GOOD.

Part: CONTROL UNIT — FAILED (TE FLAPS)

FLAP FAULT INBOARD FLAPS. ASYMMETRY FAULT INBOARD PAIR DID NOT RESPOND. REPLACED FLAP CONTROL UNIT WITH SERVICEABLE PART. OPS CHECKS GOOD.

Part: RELAY — FAILED (DC ELECT SYST)

FO'S ATTITUDE HEADING INDICATOR FAILED IN FLIGHT. RETURNED TO SLC. REPLACED EMERGENCY BATTERY RELAY BOX.

Part: FLUX DETECTOR — FAILED (RIGHT)

NUMBER 2 AHRS FAILURE IN FLIGHT, NO GYRO ON FO SIDE. RETURNED TO SLC. MEL 12-30-98. REMOVED AND REPLACED NUMBER 2 RIGHT FLUX DETECTOR AND ADJUSTED SYSTEM. WORK DONE IAW MM 34-21-03. OPS CHECKS GOOD.

Part: AHRS — FAILED (NR 2)

NR 2 AHRS FAILED 20 MINUTES AFTER DEPARTURE. REINITIALIZED BEFORE LANDING. RETURNED TO SLC. REPLACED NR 1 INVERTER IAW MM 24-22-00, OPS CHECK GOOD.

Part: WIRE HARNESS — FAILED (LANDING GEAR)

LANDING GEAR FAILED TO EXTEND AFTER SEVERAL ATTEMPTS WITH LANDING GEAR CONTROL LEVER. HYDRAULIC PRESSURE NORMAL. USED ELECTRIC OVERRIDE TO EXTEND GEAR. RETURNED TO LAX. REPLACED RIGHT GEAR PROXIMITY SENSOR HARNESS AND CYCLED GEAR SEVERAL TIMES, OPS CHECKS GOOD.

Part: BUTT STRAP — CORRODED (LAVATORY)

CORROSION ON BUTTS STRAPS UNDER LAVATORY. REPLACED RIGHT BUTT STRAP AND SPLICED IN NEW BUTT STRAP UNDER LAVATORY.

Part: BULKHEAD STRAP — CORRODED (FUSELAGE)

CORROSION ON BUTT STRAP ALONG LEFT BULK HEAD UNDER GALLEY. REPLACED LEFT BUTT STRAP SILL.

Part: SEAT TRACK — CORRODED (CABIN)

LEFT FORWARD INBOARD SEAT TRACK HAS CORROSION BEYOND LIMITS. REMOVED AND REPLACED BAD PORTION OF SEAT TRACKS ON LEFT FORWARD SEAT TRACK.

Part: ACTUATOR — FAILED (LT TE FLAPS)

ON MISSED APPROACH BROUGHT FLAP SELECTOR UP AND GOT FLAP ASYMMETRY. MADE A NO FLAP LANDING. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR IAW MM 27-00-00. OPS CHECKS GOOD AT THIS TIME.

Part: CONNECTOR — DIRTY (AHRS COMPUTER)

INFLIGHT NUMBER ONE AHRS FAILED ADI WENT TO 90 DEGREES UP, HDG OSCILLATED AT 210 DEGREES. WHEN AHRS FAILED HDG'S WERE WITHIN 5 DEG OF EACH OTHER. RETURNED TO LAX. REMOVED NUMBER ONE AHRS COMPUTER, CLEANED CONNECTOR, REINSTALLED AND REINITIALIZED. ALL CHECKS GOOD.

Part: RELAY — FAILED (PITOT HEAT)

AUXILIARY PITOT HEAT FAILS IN-FLIGHT AFTER 8 OR 9 MINUTES. RETURNED TO SLC. REMOVED AND REPLACED K0093 RELAY. AUXILIARY PITOT CHECKS GOOD.

Part: ACTUATOR — FAILED (RT MLG)

RIGHT MAIN GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO CDC. FOUND ROD END ON RIGHT GEAR ACTUATOR WORN AND FROZEN. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR ACTUATOR PER MM 32-11-00.

Part: AHS — FAILED (RT COCKPIT)

COPILOTS AHS FAILS INFLIGHT. DIVERTED TO BFL. INSTALLED SERVICEABLE AHC85 IN COPILOT SIDE, OPS CHECKS GOOD.

Part: FLUX DETECTOR — FAILED (NR 2)

NR 2 ADI FAILED INFLIGHT. REMOVED AND REPLACED NR 2 FLUX DETECTOR, OPS CHECKS GOOD.

Part: AHRS COMP — FAILED (NR 2)

ADI AND HSI FAILURE INFLIGHT. REMOVED AND REPLACED NR 2 AHRS COMPUTER. COMPLIED WITH ORIENTATION PROCEDURES. SYSTEM GROUND TESTS NORMAL. RAN AIRCRAFT FOR 30 MINUTES, SYSTEM TESTS GOOD.

Part: AHARS COMP — MALFUNCTIONED (NR 2)

ATTITUDE AND HEADING FAILURE INFLIGHT. RIGHT SIDE COULD NOT DUPLICATE. RERACKED NR 2 AHRS COMPUTER PER EMB AHRS INITIALIZATION AND ORIENTATION PROCEDURE.

Part: PROX SENSOR — MALFUNCTIONED (RT MLG)

GEAR FAILED TO EXTEND NORMALLY, USED ELECTRIC OVERRIDE FOR GEAR EXTENSION, ABNORMAL LIGHT INDICATIONS A-SYSTEM RT MAIN GEAR. REPLACED RT AIR/GROUND PROXIMITY SENSOR PER MM 32-01-01. LANDING GEAR FUNCTION CHECKS GOOD.

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

LANDING GEAR WOULD NOT EXTEND OR RETRACT WITHOUT USING ELECTRICAL OVERRIDE. RT GEAR UPLOCK PROXIMITY SENSOR NEEDED ADJUSTMENT. ADJUSTED AND OPS CHECK GOOD. CYCLED GEAR TWELVE TIMES.