N187SW

Part: CONTROL PANEL — MALFUNCTIONED (STALL WARNING) · airframe 41,583 hrs · 50,898 cycles

STALL WARNING ON MAP WILL NOT CLEAR. REMOVED AND REPLACED STALL WARNING PANEL. OPERATIONAL CHECK GOOD. P/N: 120-84428-505, S/N OFF: 1200034R.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 41,462 hrs · 50,753 cycles

LEFT WING UPPER AFT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIPS IAW SRM 57-20-07, 51-40-05, 52-25-00, 51-40-02.

Part: RIB — CRACKED (RT WING) · airframe 41,462 hrs · 50,753 cycles

RIGHT WING FORWARD RIB 20 CRACKED AT TOP TWO SPOTS. DISCOVERED DURING C-CHECK INSPECTION. RIGHT WING FORWARD RIB 20 REPLACED IAW 51-25-00, 51-40-05, 51-40-02, 51-22-00.

Part: BRACKET — CRACKED (LT WING) · airframe 41,476 hrs · 50,769 cycles

LEFT WING UPPER 3RD FROM FRONT SKIN SUPPORT BRACKET IS CRACKED AT RIB 22. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP IAW SRM 57-20-07, 51-40-05, 51-25-00, 51-40-02.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 41,462 hrs · 50,753 cycles

LEFT WING UPPER AFT SKIN SUPPORT BRACKET CRACKED AT RIB 23. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLAMP IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,462 hrs · 50,753 cycles

FRAME 15 IN BELLY CRACKED FRAME AT AFT AIR STAIR ACTUATOR. DISCOVERED DURING C-CHECK INSPECTION. FRAME REPAIRED IAW EMB 120 SRM 53-00-04 PG 201-204.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 41,462 hrs · 50,753 cycles

LEFT WING UPPER 2ND FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT IAW SRM 57-20-07, 51-40-05, 51-25-00, AND 51-40-02.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 41,462 hrs · 50,753 cycles

RIGHT WING RIB 24 LOWER 2ND FROM FRONT SKIN SUPPORT BRACKET CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED CRACKED BRACKET IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.

Part: RIB — CRACKED (RT WING) · airframe 41,462 hrs · 50,753 cycles

RIGHT WING FORWARD RIB 19 CRACKED AT TWO SPOTS. DISCOVERED DURING C-CHECK INSPECTION. RIGHT WING FORWARD RIB 19 REPLACED IAW EMB 120 SRM 51-40-07, 51-40-04, 51-40-05, 51-22-00, AND 51-40-07, AND CONTINUATION SHEET 1 AND 2.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 41,462 hrs · 50,753 cycles

RIGHT WING UPPER AFT SKIN SUPPORT BRACKET CRACKED AT RIB 23. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.

Part: BRACKET — CRACKED (LT WING) · airframe 41,476 hrs · 50,769 cycles

LEFT WING UPPER 2ND FROM LAST SKIN SUPPORT BRACKET CRACKED. DISCOVERED DURING C-CHECK INSPECTION. SKIN SUPPORT REMOVED AND REPLACED IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.

Part: RIB — WORN (RT WING) · airframe 41,462 hrs · 50,753 cycles

RIGHT WING LEADING EDGE INBOARD OF NACELLE, OUTBOARD ATTACH POINT RIB WORN THROUGH. DISCOVERED DURING C-CHECK INSPECTION. RIB REPAIRED IAW EMB 120 SRM 51-70-05 FIG 1.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 41,462 hrs · 50,753 cycles

RIGHT WING UPPER FORWARD SKIN SUPPORT BRACKET CRACKED AT RIB 21. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 41,462 hrs · 50,753 cycles

LEFT WING UPPER 3RD FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT IAW SRM 57-20-07, 51-40-05, 51-25-00, AND 51-40-02.

Part: STRUCTURE — CRACKED (WING TO BODY) · airframe 41,462 hrs · 50,753 cycles

LEFT ZONE 193 LOWER FLANGE WING TO FUSELAGE IS CRACKED IN THREE LOCATIONS. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE IAW EMB 120 SRM 53-20-13 PG 205-206 FIG 202.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 41,462 hrs · 50,753 cycles

RIGHT WING UPPER 3RD FROM FRONT SKIN SUPPORT BRACKET AT RIB 23 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 52-40-05, 51-40-02.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 41,462 hrs · 50,753 cycles

RIGHT WING UPPER 2ND FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 21. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.

Part: SUPPORT BRACKET — CORRODED (RT WING) · airframe 41,462 hrs · 50,753 cycles

RIGHT WING UPPER 2ND FROM FRONT SKIN SUPPORT BRACKET AT RIB 20 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 51-40-05, 51-40-02.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 41,462 hrs · 50,753 cycles

RIGHT WING UPPER 4TH FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-40, 51-40-05, AND 51-40-02.

Part: PROXIMITY SWITCH — FAULTY (LT & RT ELEVATOR) · airframe 40,904 hrs · 50,096 cycles

FIRST FLIGHT AURAL WARNING TRIM CHECK FAILS. REMOVED LEFT AND RIGHT ELEVATOR TRIM PROX SWITCHES HAND SHAKE CONNECTORS AND REPLACED WITH ENVIRONMENTAL SPLICE CONNECTORS IAW EMB 120 WMM 20-21-00 AND 31-52-00, OPS CHECKED GOOD.

Part: SHUTOFF VALVE — MALFUNCTIONED (LT ENGINE) · airframe 40,838 hrs · 50,023 cycles

SMOKE IN COCKPIT AND CABIN WITH BOTH PACKS OFF. REMOVED AND REPLACED LT ENGINE PRESSURE REGULATOR SHUT OFF VALVE WITH SERVICEABLE UNIT IAW MM 36-10-04. OPS CHECKS GOOD AT THIS TIME.

Part: ANNUNCIATOR — MALFUNCTIONED (TE FLAPS) · airframe 40,790 hrs · 49,951 cycles

FLAP CONTROL FAULT, DISAGREE, AND ASYM MESSAGE OVERHEAD FLAP AND ADVANCED SWS ON MAP STAY ON. INSTALLED A SERVICEABLE FLAP ANNUNCIATOR IAW 27-50-05. OPS CHECK GOOD. REMOVED AND REPLACED FLAP CONTROL UNIT. P/N OFF: 347200-1001, SN OFF: 0194.

Part: LIGHT — SHORTED (LT OVERWING) · airframe 40,406 hrs · 49,494 cycles

EMERGENCY EXIT LIGHTS AT 6A AND 6C OVERWING EXIT AND THE MIDDLE CEILING LIGHT AS WELL AS FOUR OR FIVE FLOOR LEVEL LIGHTS DO NOT ILLUMINATE OR JUST BARELY LIGHT UP. FOUND SHORT AT LEFT OVERWING EMERGENCY EXIT FLOOD LIGHT. RECONNECTED, REPOSITIONED TERMINALS AND REPLACED INSULATION BOOT. OPS CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 40,107 hrs · 49,130 cycles

CONTROL FAULT WITH FLAP AND ADVANCED SWS IN FLIGHT INBOARD FLAPS FLASHING. CLEARED WITH RESET IAW QRH. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR AND REPLACED FCU IAW 27-80-08. OPS AND LEAK CHECKS GOOD. PN: 320300-1005 SN OFF: 0885

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 40,072 hrs · 49,095 cycles

ON APPROACH INTO SLC WE SELECTED FLAPS 15 AND GOT THE ''CONTROL FAULT'' WITH THE ''FLAP'' AND ''ADVANCED SWS'' ON THE MAP. QRH PROCEDURE CORRECTED PROBLEM.REMOVED AND REPLACED FLAP CONTROL UNIT IAW MM 27-50-06. OPS CHECK GOOD.

Part: BRACKET — CRACKED (FLAP ROLLER) · airframe 40,072 hrs · 49,095 cycles

RT INBOARD FLAP ROLLER BRACKET IS CRACKED. REPLACED RT INBOARD FLAP OUTBOARD GAP PANEL ROLLER BRACKET. CHECKS GOOD.

Part: WIRE HARNESS — UNSERVICEABLE (MLG) · airframe 39,582 hrs · 48,490 cycles

WHEN LANDING GEAR LEVER WAS MOVED DOWN, RIGHT RED TRANSITION -A- LIGHT STAYED ON, RIGHT GREEN -A- LIGHT DID NOT COME ON. REMOVED AND INSTALLED SERVICEABLE WIRE HARNESS. OPS CHECK GOOD ON GEAR SWING IAW EMB MM 32-61-01. P/N OFF/ON 120-22623-501.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 39,582 hrs · 48,490 cycles

INFLIGHT FLAP CONTROL FAULT INDICATION WOULD NOT CLEAR. RETURNED TO FIELD. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR. OPS AND LEAK CHECKS GOOD IAW MM 27-50-09.

Part: RELAY — MALFUNCTIONED (MLG) · airframe 39,320 hrs · 48,167 cycles

DURING FLIGHT, RIGHT MAIN ''A'' GREEN LIGHT ILLUMINATED. GEAR WOULD NOT EXTEND - ALL THREE GEAR RED LIGHTS ILLUMINATED EXCEPT RIGHT ''A'' RED WITH HANDLE DOWN. AFTER 5 MINUTES THE PROBLEM FIXED ITSELF AND THE GEAR LOWERED NORMALLY. REPLACED LANDING GEAR RELAY BOX IAW 32-31-02. OPS CHECK GOOD.

Part: CONNECTOR — CONTAMINATED (FLAP ACTUATOR) · airframe 38,822 hrs · 47,578 cycles

CONTROL FAULT ON INBOARD FLAPS DURING FLAP RETRACTION. CLEANED CONNECTOR ON FLAP INBOARD ACTUATORS ON BOTH SIDES. RAN SEVERAL TIMES. NO FAULTS AT THIS TIME.

Part: WIRE HARNESS — MALFUNCTIONED (RT MLG) · airframe 38,712 hrs · 47,435 cycles

ON TAKEOFF FROM PSP, THE RT GEAR GREEN SYS A LIGHT REMAINED ON. UPON PUTTING GEAR DOWN AT LAX, THE GEAR DID NOT COME DOWN. PERFORMED ELECTRIC OVERRIDE QRH PROCEDURE AND THE GEAR CAME DOWN OK. REMOVED RIGHT A-HARNESS, REPAIRED AND REINSTALLED IAW 32-60-00. PERFORMED GEAR SWING A-GATE LIGHT FOR RIGHT GEAR, OPS CHECK GOOD.

Part: ANNUNCIATOR — MALFUNCTIONED (COCKPIT) · airframe 38,712 hrs · 47,435 cycles

AFTER LANDING AT PSP THE INBOARD FLAPS WOULD NOT RETRACT. REPLACED FLAP ANNUNCIATOR WITH A SERVICEABLE UNIT. OPS CHECK GOOD.

Part: SWITCH — LACK OF LUBE (CABIN DOOR) · airframe 38,701 hrs · 47,419 cycles

FORWARD DOOR LIGHT ILLUMINATED INFLIGHT. LUBED FORWARD DOOR MICROSWITCHES. OPS CHECK GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 38,104 hrs · 46,724 cycles

FLOOR LIGHTING IN FRONT OF GALLEY NOT WORKING. REPAIRED BROKEN WIRE. OPS CHECK GOOD.

Part: WIRE — BURNED (ELECTRICAL SYS) · airframe 37,610 hrs · 46,101 cycles

WIRE AT CANNON PLUG J0958 PIN F ON RIGHT SIDE DC RELAY BOX IS BURNED AND NEEDS TO BE REPLACED. REMOVED AND REPLACED WIRE W208-0064 AT CANNON PLUG J0958 PIN F WITH A NEW WIRE 1 GAUGE LARGER AND PERFORMED OPERATIONAL CHECK AS PER MM 30-40-00. OPS CHECK GOOD.

Part: TORQUE TUBE — CORRODED (PAX DOOR) · airframe 37,610 hrs · 46,101 cycles

NR 2 AND NR 3 PASSENGER DOOR STEP RODS FOUND CORRODED DURING INSPECTION. REMOVED AND REPLACED NR 2 AND NR 3 PASSENGER DOOR STEP TORQUE TUBES IAW EMB MM 52-10-03.

Part: ACTUATOR — CORRODED (PAX DOOR) · airframe 37,610 hrs · 46,101 cycles

PASSENGER DOOR STEP ACTUATOR ARM FOUND CORRODED. REMOVED AND REPLACED PASSENGER DOOR STEP ACTUATOR ARM WITH NEW. OPS CHECK GOOD.

Part: LINK — CORRODED (PAX DOOR) · airframe 37,610 hrs · 46,101 cycles

PASSENGER DOOR PUSH-PULL LINKS CORRODED (FORWARD AND AFT). REMOVED AND REPLACED PASSENGER DOOR FORWARD AND AFT PUSH-PULL LINKS IAW EMB MM 52-11-03.

Part: PCU — MALFUNCTIONED (RUDDER) · airframe 37,473 hrs · 45,940 cycles

ON TAKEOFF, COULD NOT MOVE RUDDER PAST HALF TRAVEL TO THE RIGHT. TURNING BLUE SYSTEM OFF MADE NO DIFFERENCE. UPON LANDING FULL TRAVEL WAS RESTORED. REPLACED RUDDER PCU. INFLIGHT FUNCTIONAL TEST OF RUDDER SYSTEM NORMAL. FLIGHT TEST OK.

Part: SUPPORT — WORN (ELEVATOR TRIM) · airframe 37,153 hrs · 45,571 cycles

THE ELEVATOR TRIM FORWARD QUADRANT IDLER SPROCKET SUPPORT HAS CHAIN TRACKS WORN IN IT. REMOVED DAMAGED SUPPORT AND INSTALLED NEW IAW EMB SRM 51-40-02.

Part: TRIM TAB — OUT OF ADJUST (ELEVATOR) · airframe 36,939 hrs · 45,324 cycles

ON DESCENT INTO EKO, TRIM FAIL WARNING WENT OFF. AFTER A/P DISCONNECT, AIRCRAFT PITCHED UP AT 230 KTS WITH ELEVATOR TRIM AT FULL NOSE DOWN STOP. AIRCRAFT NOT UNDER NORMAL CONTROL UNTIL SLOWED BELOW 200 KTS. ADJUSTED RT ELEVATOR TRIM TAB AS REQUIRED TO RECEIVE TRIM EXPECTED.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 36,890 hrs · 45,261 cycles

ON DEPARTURE, AIRCRAFT WOULD NOT PRESSURIZE AT ALL. MANUAL CONTROLLER WOULD NOT FUNCTION. RETURNED TO ELKO. REMOVED AND REPLACED AUTO PRESSURIZATION CONTROLLER IAW EMB MM 21-30-01. AUTO PRESSURIZATION OPS CHECKS GOOD IAW EMB MM 21-30-00.

Part: STRINGER — CRACKED (LT WING) · airframe 36,749 hrs · 45,106 cycles

STRINGER NR 8 CRACKED AT LEFT WING NR 2 FUEL PANEL. REPAIRED STRINGER CRACK IAW EMB SRM 57-20-03.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 3,875 hrs · 4,454 cycles

AUTO FEATHER WARNING ON TAKE OFF ROLL.RAN BOTH ENGINES W/AUTO FEATHER ARMED. APPLIED 60% TORQUE. NO AUTO FEATHER WARNINGS. OPS CHECK GOOD.

Part: VALVE — FAILED (A/C BAY) · airframe 35,163 hrs · 43,287 cycles

RIGHT PACK FAILED DURING CLIMB. APPROXIMATELY 1 MINUTE LATER, THE LAV SMOKE DETECTOR STARTED BEEPING AND THE FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. WITH RECIRCS AND GASPERS OFF, THE CABIN SLOWLY CLEARED. REMOVED LEFT AND RIGHT RAM AIR VENTILATION VALVES AND LEFT HEAT EXCHANGER SPRAYER (H2O) DUCT WITH SERVICEABLE UNITS IAW MM 21-26-01 & 21-51-02. OPS CHECK GOOD. VALVE P/N ON LT 120-42193-001, LT P/N OFF 120-21588-001, DUCT P/N ON RT 120-42193-002, RT P/N OFF 120-21588-002.

Part: TUBE — BROKEN (HYD SYSTEM) · airframe 34,873 hrs · 42,954 cycles

LEFT HYDRAULIC SYSTEM (GREEN) LOW RESERVOIR PRESSURE, LOW LEVEL, MAIN PUMP LOW PRESS LIGHTS ON. RETURNED TO SLC REPAIRED BROKEN MAIN HYDRAULIC PUMP PRESSURE TUBE AT LEFT HYDRAULIC COMPARTMENT FIRE WALL IAW EMB 120 MM 20-10-04. OPS AND LEAK CHECKS GOOD.

Part: RUDDER PEDAL — BINDING (COCKPIT) · airframe 34,873 hrs · 42,954 cycles

RIGHT RUDDER PEDAL BINDS AND IS NOISY WITH FORWARD MOVEMENT. APPLIED LUBRICANT TO RUDDER TRIM ACTUATOR CLUTCH MECHANISM. OPS CHECK GOOD.

Part: RUDDER PEDAL — OUT OF ADJ (COCKPIT) · airframe 34,536 hrs · 42,576 cycles

FOS RUDDER PEDALS WILL NOT EXTEND FULL FORWARD. ADJUSTED RIGHT RUDDER PEDAL ADJUSTEMENT CRANK AS NECESSARY. OPS CHECK GOOD.

Part: CONNECTOR — FAILED (LT ENGINE EEC) · airframe 34,436 hrs · 42,463 cycles

LEFT EEC FAILED ON TAKEOFF ROLL. ABORTED TAKEOFF. FOUND CANNON PLUG P5 ON LEFT EEC WITH FAULT. REMOVED AND REPLACED LEFT EEC HARNESS IAW EMB 120 MM 73-21-00, OPS CHECK GOOD. P/N ON 3115911-01, S/N ON AA4313, S/N OFF AA3712.

Part: EEC — MALFUNCTIONED (LT ENGINE) · airframe 34,308 hrs · 42,313 cycles

LEFT EEC FAILED ON TAKEOFF ROLL. ABORTED TAKEOFF. CLEANED ALL CANNON PLUGS AND GROUND RAN LEFT ENGINE. OPS CHECK GOOD.

Part: ACTUATOR — CONTAMINATED (TE FLAPS) · airframe 34,177 hrs · 42,167 cycles

FLAP DISAGREEMENT ON FINAL WITH FLAPS 45 DEGREES. CLEANED GLYCOL FROM THE FLAP ACTUATORS ON BOTH OUTBOARD AND INBOARD PAIRS. FLAPS OPS CHECK GOOD.

Part: EEC — FAILED (LEFT) · airframe 34,112 hrs · 42,091 cycles

LEFT EEC FAILED ON TAKE OFF ROLL. ABORTED AS REQUIRED. DEFERRED PER MEL 73-21-1. PERFORMED RUN UP OF NUMBER ONE ENGINE IAW MM 71-00-00. COULD NOT DUPLICATE. OPS CHECKS GOOD.

Part: STARTER GEN — FAILED (APU) · airframe 34,070 hrs · 42,047 cycles

''APU GEN OFF BUS'' LIGHT ON IN FLIGHT. RESET AS PER QRH. RESET FOR APPROXIMATELY 10 SECONDS THEN ''OFF BUSS''CAME ON AGAIN. RETURNED TO FIELD. REMOVED AND REPLACED APU STARTER/GENERATOR IAW 24-30-00. OPS CHECK GOOD.P/N: 23080-015 S/N ON: 98543 S/N OFF: 96115

Part: DUCT — LEAKING (LT ENGINE) · airframe 33,438 hrs · 41,298 cycles

DUCT LEAK INDICATION, QRH REQUIRES, INFLIGHT SHUT DOWN OF LEFT ENGINE. DUCT LEAK LIGHT EXTINGUISHED AFTER APPROX 3 MINUTES. CHECKED ALL DUCTS FOR LEAKS ON LT SIDE. FOUND LEAKS ON FLANGE OF ''''Y'''' DUCT. ALSO COMPLIED WITH SB 120-36-0015. REPLACEMENT OF THERMAL SWITCHES ON PNEUMATIC DUCTS. OPS CK OF PNEUMATIC SYSTEM. NO LEAKS DETECTED.

Part: WARNING LIGHT — ILLUMINATED (LT ENGINE) · airframe 33,411 hrs · 41,268 cycles

ABORTED TAKEOFF DUE TO ''''ENGINE CONTROL'''' WARNING. LEFT ENGINE EEC REVERTED TO MANUAL. RETURNED TO THE GATE. RAN ENGINE AND PERFORMED OPS CHECKS OF EEC''S WITHOUT A FAILURE. OPS CHECKS GOOD IAW MM 71-00-00.

Part: CONTROLLER — MALFUNCTIONED (PROP FEATHER) · airframe 33,411 hrs · 41,268 cycles

AUTO FEATHER DID NOT ARM ON TAKEOFF ROLL. ABORTED TAKEOFF. RAN ENGINE FOR AUTO FEATHER CHECK BUT COULD NOT DUPLICATE. OPS CHECKS GOOD.

Part: SIGNAL COND UNIT — MALFUNCTIONED (LEFT) · airframe 33,298 hrs · 41,138 cycles

EXPERIENCED ''''AUTO FEATHER'''' AURAL WARNING DURING EARLY PHASE OF TAKEOFF ROLL. ABORTED TAKEOFF. A/C WAS CONFIGURED CORRECTLY AND AUTO FEATHER SYSTEM TESTED PROPERLY. REMOVED AND REPLACED LEFT TORQUE SIGNAL CONDITION IAW MM 77-11-01. OPS CHECKS GOOD AT THIS TIME. P/N ON: 30005-0000-52, S/N ON: 1331, S/N OFF: 4065.

Part: CONNECTOR — FAILED (FLAP ACTUATOR) · airframe 32,656 hrs · 40,383 cycles

CONTROL FAULT INFLIGHT WOULD NOT RESET. RETURNED TO SLC RAN FLAPS ON GROUND FAILED ON RIGHT OUTBOARD. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR CANNON PLUG PER MM 27-51-00 AND 50-50-00, OPS CHECKS GOOD. (P/N MS3476612201) ON.

Part: CONTROLLER — MALFUNCTIONED (TE FLAP) · airframe 32,586 hrs · 40,302 cycles

IN CLIMBOUT OF SLC AND CRUISE FLIGHT FLAP CONTROL FAULT ON NACELLE FLAP ILLUMINATED AND WOULD NOT CLEAR. RETURNEDTO SLC. REPLACED NUMBER ONE AND NUMBER TWO NACELLE FLAP ACTUATORS IAW MM 27307, OPS CHECK GOOD. LEAK CHECK GOOD. (P/N 3082001007) (S/N 0164) ON, (S/N 0091) OFF.

Part: CONTROLLER — MALFUNCTIONED (TE FLAP) · airframe 32,586 hrs · 40,302 cycles

CONTROL FAULT NACELLE FLAP RETURNED TO SLC PERFORMED OPERATIONAL TEST OF FLAPS IAW MM 275000501, NO DEFECTS NOTED. INSPECTED LT AND RT NACELLE FLAPS FOR CONDITION AND SECURITY, CHECKED OK. INSPECTED LT AND RT NACELLE FLAP ACTUATORS FOR CONDITION AND SECURITY, CHECKED OK. REMOVED FLAP COMPUTER, INSPECTED CONNECTOR, OK. OHMD AND MEGD NACELLE FLAP ACTUATOR WIRING LT AND RT FOR CONTINUITY AND BREAKDOWN, CHECKED OK. REINSTALLED FCU, ACTUATORS, CONNECTORS AND ALL PANELS OPENED. REMOVED FOR ACCESS, PERFORMED FLAP ACTUATOR TIME TRAVEL CHECK IAW MM 275000 AND REPEATED FLAP OPERATIONAL CHECK IAW MM 275000. ALL CHECKS GOOD. UNABLE TO DUPLICATE PROBLEM.

Part: CONNECTOR — DIRTY (LANDING GEAR)

RED TRANSIT LIGHT A WOULD NOT EXTINGUISH ON RETRACTION. RETURNED TO SLC. CLEANED CORRODED CANNON PLUGS ON LEFT GEAR CANNON PLUGS. OPS CHECK GOOD.

Part: WINDSHIELD — FAILED (RT COCKPIT)

FIRST OFFICERS WINDSHIELD OUTER PANE SHATTERED CLIMBING THROUGH 20,000 FEET. RETURNED TO SLC. REMOVED AND REPLACED RIGHT WINDSHIELD. NO EVIDENCE OF OTHER DAMAGE.

Part: DRAIN — OUT OF POSITION (RT PNEU SYST)

RIGHT DUCT LEAK LIGHT CAME ON ABOUT 25 MILES OUTSIDE OF TWF. FOLLOWED QRH AND AFTER THREE MINUTES SHUT DOWN RIGHT ENGINE. THE LIGHT WENT OUT AFTER ENGINE SHUT DOWN. RETURNED TO TWF. REPOSITIONED PNEUMATIC PRESSURE REGULATOR OVERBOARD DRAIN TUBE. ALSO, PERFORMED CHECK OF PNEUMATIC SYSTEM FOR ONE HOUR 45 MINUTES. OPS CHECKS GOOD IAW EMB 120 MM 36-00-00 AND 36-20-00.

Part: DOOR — NOT LATCHED (RT EMER EXIT)

AIRCRAFT WOULD NOT PRESSURIZE IN AUTO. RETURNED TO SLC. FOUND REAR RIGHT EMERGENCY EXIT AUTO HANDLE PANEL OPEN. CLOSED PANEL. OPS CHECK GOOD DURING GROUND PRESSURIZATION RUN.

Part: AHC — FAILED (LEFT)

AFTER TAKEOFF IN 30 DEGREE RIGHT TURN THE YAW, TCAS AND CAPTAIN, GYRO FAILED. THEN ON APPROACH BACK INTO SLC FLAPS RIGHT INBOARD FAILED. INSTALLED NEW AHC-85 ON CAPTAINS SIDE AND ORIENTATED. OPS CHECKS GOOD. CLEANED FLAPS, CANNON PLUGS AND INSPECTED FLAPS. CHECKS GOOD.

Part: THRESHOLD — CORRODED (PAX DOORWAY)

THE PASSENGER DOOR THRESHOLD ATTACH BRACKET HAS INTERGRANULAR CORROSION. INSTALLED A SERVICEABLE THRESHOLD BRACKET ASSEMBLY, CHECKS GOOD.

Part: DME ANTENNA — CORRODED (FUSELAGE)

FORWARD AND AFT DME ANTENNAS NEED REPLACEMENT DUE TO CORROSION. REPLACED FORWARD AND AFT DME ANTENNAS AS REQUIRED, OPS CHECK GOOD.

Part: STRAP — CORRODED (FUSELAGE)

LEFT FORWARD BUTT STRAP IN FRONT OF PASSENGER DOOR HAS CORROSION. DRILLED OUT THE CORRODED BUTT STRAP IN FRONT OF THE PASSENGER DOOR AND DRILLED AND INSTALLED A NEW BUTT STRAP.

Part: STRAP — CORRODED (FUSELAGE)

MOST FORWARD CENTER, WIDE BUTT STRAP HAS CORROSION. REMOVED AND REPLACED THE MOST FORWARD CENTER WIDE BUTT STRAP WITH NEW.

Part: SEAT TRACK — CORRODED (CABIN)

RIGHT LOWER SEAT TRACK (FORWARD SECTION) HAS SEVERAL AREAS OF CORROSION. INSTALLED NEW SEAT TRACK AFTER DRILLING AND FITTING TO PROPER POSITION.

Part: SEAT TRACK — CORRODED (CABIN)

LEFT LOWER SEAT TRACK (FORWARD SECTION) HAS SEVERAL AREAS OF CORROSION. REPLACED LEFT LOWER SEAT TRACK.

Part: SKIN — CORRODED (FUSELAGE)

AFT DME ANTENNA HOLE IN FUSEALAGE FOR COAX HAS SOME CORROSION. REMOVED ALL CORROSION, FABRICATED TWO DOUBLER OUT OF .50 2024-T3 AND INSTALLED AT AFT DME ANTENNA HOLE AREA.

Part: ANTENNA — CORRODED (NR 2 MARKER)

NR 2 MARKER BEACON ANTENNA NEEDS REPLACEMENT DUE TO CORROSION. REPLACED NR 2 MARKER BEACON ANTENNA.

Part: SEAT TRACK — CORRODED (CABIN)

CABIN RIGHT UPPER SEAT TRACK FORWARD SECTION HAS SEVERAL AREAS OF CORROSION. DRILLED AND INSTALLED NEW SEAT TRACK AS REQUIRED.

Part: SEAT TRACK — CORRODED (GALLEY)

SMALL FORWARD GALLEY MOUNT SEAT TRACK CORRODED. REPLACED SMALL FORWARD GALLEY MOUNT SEAT TRACK.

Part: SEAT TRACK — CORRODED (CABIN)

CABIN LEFT UPPER SEAT TRACK FORWARD SECTION HAS AREAS OF CORROSION. FIT, DRILLED AND INSTALLED NEW SEAT TRACK AS REQUIRED.

Part: PRESS REG VALVE — MALFUNCTIONED (RT ENGINE)

DUCT LEAK LIGHT ILLUMINATED ON RIGHT ENGINE. RETURNED TO FIELD. REMOVED AND REPLACED RIGHT PRESSURE REGULATOR VALVE IAW MM 30-10-00. RAN RIGHT ENGINE. PRESSURE REGULATOR VALVE OPS CHECKS NORMAL WITH NO LEAKS NOTED AND NO DUCT LEAK LIGHTS.

Part: B-NUT — LOOSE (RT ENGINE)

DUCT LEAK LIGHT ILLUMINATED. SHUTDOWN RIGHT ENGINE AND RETURNED TO FIELD. FOUND B-NUT FITTING LOOSE ON 18 PSI REGULATOR. TIGHTENED FITTING AND RAN ENGINE TO TAKEOFF POWER. NO DUCT LEAK LIGHT NOTED AND OPS CHECKS GOOD.

Part: WIRE — OUT OF POSITION (RT ENGINE)

ON CLIMBOUT, DUCT LEAK LIGHT FOR RIGHT ENGINE ILLUMINATED, IT STAYED ON FOR MORE THAN 3 MINUTES. SHUT DOWN RIGHT ENGINE PER QRH AND RETURNED TO RNO. INSPECTED A/C RIGHT ENGINE BLEED AIR SYSTEM, FOUND SUSPECT TEMP SENSOR WIRE TO BE IN CLOSE PROXIMITY TO BLEED AIR LINE. SECURED WIRE WITH A/C WIRE BUNDLE, RAN A/C 10 MIN USING BLEED AIR SYSTEM, COULD NOT DUPLICATE. CHECKS GOOD.

Part: CLIPS — CRACKED (RT WING)

RT WING RIB 15 HAS THREE CRACKED WING SUPPORT CLIPS ON UPPER SURFACE AND FOUR CRACKED WING SUPPORT CLIPS ON LOWER SURFACE. REMOVED AND REPLACED SEVEN WING SUPPORT CLIPS, THREE ON UPPER AND FOUR ON LOWER SURFACE ON RIB 15 RT WING, IAW EMB SRM 51-30-00, 51-40-00 AND EMB SB 120-57-0031 PART 1.

Part: CLIPS — CRACKED (RT WING)

RT WING RIB 22 HAS THREE CRACKED CLIPS ON UPPER SURFACE. REMOVED AND REPLACED THREE WING SUPPORT CLIPS ON UPPER SURFACE RIB 22 OF RT WING IAW EMB SRM 51-30-00 AND 51-40-00 AND EMB SB 120-57-0031 PART 1.

Part: CLIPS — CRACKED (RT WING)

RT WING RIB 16 HAS TWO CRACKED WING SUPPORT CLIPS ON UPPER SURFACE AND CRACKED WING SUPPORT CLIPS ON LOWER SURFACE. REMOVED AND REPLACED FIVE WING SUPPORT CLIPS, TWO ON UPPER SURFACE AND THREE ON LOWER SURFACE, RIB 16 RT WING IAW EMB SRM 51-30-00, 51-40-00 AND EMB SB 120-57-0031 PART 1.

Part: CLIPS — CRACKED (RT WING)

RT WING RIB 20 HAS THREE CRACKED WING SUPPORT CLIPS ON UPPER SURFACE. REMOVED AND REPLACED THREE WING SUPPORT CLIPS ON UPPER SURFACE OF RIB 20 ON RT WING, IAW EMB SRM 51-30-00 AND EMB SB 120-57-0031 PART 1.

Part: CLIPS — CRACKED (RT WING)

RT WING RIB 21 HAS FOUR CRACKED SUPPORT CLIPS ON UPPER SURFACE. REMOVED AND REPLACED FOUR WING SUPPORT CLIPS ON UPPER SURFACE OF RIB 21 ON RT WING, IAW EMB SRM 51-30-00, 51-40-00 AND EMB SB 120-57-0031 PART 1.

Part: EEC CONNECTOR — DIRTY (RT ENGINE)

RIGHT ENGINE EEC (ELECTRONIC ENGINE CONTROL) FAILED AND WOULD NOT RESET. DEFERRED PER MEL 73-21-1. ABORTED TAKEOFF. INSPECTED WIRING. CLEANED CANNON PLUG AND RAN AIRCRAFT. OPERATIONALLY CHECKS GOOD.