N584SW

Part: CONNECTOR — INTERMITTENT (RT WING TE FLAPS) · airframe 32,311 hrs · 44,020 cycles

A MAINTENANCE TEST FLIGHT FOR NACELLE FLAP DISAGREEMENT WAS IN PROGRESS. DURING THE TEST FLIGHT THE CREW WAS IN CRUISE CONFIGURATION AND INCREMENTALLY SET THE FLAPS UNTIL THEY WERE FULLY DOWN. UPON MOVING THE FLAPS BACK TO 25 DEGREES THEY EXPERIENCED A FLAP DISAGREEMENT BETWEEN THE NACELLE FLAPS. IN TRYING TO CORRECT THE ISSUE THE ALSO EXPERIENCED A FLAP ASYMMETRY IN THE NACELLE FLAPS. AT THIS POINT IT WAS DECIDED TO HEAD DIRECT TO KHYI FOR AN EMERGENCY LANDING. UPON ARRIVAL AT KHYI MAINTENANCE TROUBLESHOT THE FLAP ISSUE TO A FAULTY CANNON PLUG AT THE RH NACELLE FLAP ACTUATOR. MAINTENANCE REMOVED AND REPLACED THE CANNON PLUG AND PERFORM OPS CHECKS WITH NO DEFECTS NOTED. THE AIRCRAFT THEN PERFORMED ANOTHER MAINTENANCE TEST FLIGHT WITH NO FURTHER DEFECTS NOTED.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 31,834 hrs · 43,667 cycles

FWD TWO RED EMERGENCY LIGHTS INOPERATIVE. REPAIRED THE WIRE FOR THE EMERGENCY LIGHTS AND RELAMPED. OPS CHECKED GOOD.

Part: CONTROL VALVE — FAILED (BRAKE SYS) · airframe 31,505 hrs · 43,157 cycles

WHILE TAXIING AT NORMAL TAXI SPEED WITH ANTI-SKIDS ON, BRAKES FELT SPONGY. FELT LIKE ACFT WOULD NOT COME TO A STOP UNTIL TAXI SPEED IS VERY LOW AND THEN THE BRAKES FINALLY GRAB BRINGING THE ACFT TO A JOLTING STOP. R & R BLUE SYSTEM BRAKE CONTROL VALVE IAW AMM. PN 39651-2, SN ON 305, SN OFF 734.

Part: RELAY — FAILED (ANTI SKID SYS) · airframe 31,268 hrs · 42,827 cycles

FLIGHT IS RETURNING TO DEPARTURE AFTER ANTI-SKID FAILED. REMOVED AND REPLACED ANTI-SKID RELAYS K0255 AND K0021 IAW AMM. OPS CHECKED GOOD.

Part: POTENTIOMETER — INOPERATIVE (RUDDER FEEDBACK) · airframe 31,162 hrs · 42,669 cycles

PEDAL STEERING INOPERATIVE ILLUMINATED AFTER TAKEOFF. REMAINED ILLUMINATED AFTER GEAR RETRACTION. REMOVED AND REPLACED RUDDER FEEDBACK POTENTIOMETER AND OPS CHECKED GOOD IAW AMM. TAXI CHECKED GOOD, NO FURTHER DEFECTS NOTED.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 31,069 hrs · 42,529 cycles

F/A REPORTS FLASHLIGHT INOPERATIVE. R & R F/A FLASHLIGHT BATTERIES. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,048 hrs · 42,496 cycles

LEFT FWD OVERWING EMERGENCY LIGHT IS INOPERATIVE. C-CHECK, R & R LT FWD OVERWING EMERGENCY LIGHT ASSY.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 31,048 hrs · 42,496 cycles

PASSENGER SEAT TRACK IS CORRODED. C-CHECK, R & R SEAT TRACK IAW ETS.

Part: RIB — CRACKED (LT NACELLE) · airframe 31,048 hrs · 42,496 cycles

LT NACELLE FLAP OTBD SIDE RIB STIFFENER CRACKED. C-CHECK, REPLACED OTBD SIDE RIB STIFFENER AT LT NACELLE FLAP IAW SRM.

Part: STRINGER — CRACKED (RT WING) · airframe 31,048 hrs · 42,496 cycles

RIGHT WING STRINGER NR 10 CRACKED AT RIB NR 16, 1ST PANEL OTBD OF NACELLE. C-CHECK, PERFORMED RT WING NR 10 STRINGER REPAIR AT RIB 16 IAW ETD.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 31,018 hrs · 42,449 cycles

IN CABIN EMERGENCY LIGHT AFT LENS IS BROKEN. R & R WITH NEW EMERGENCY TRACK LIGHT AFT LENS IAW AMM.

Part: SKIN — CRACKED (LT NACELLE) · airframe 31,018 hrs · 42,449 cycles

LT ENGINE NACELLE OTBD SIDE FWD OF FWD COWL DOOR SKIN CRACKED. REPAIRED DAMAGED SKIN ON LT ENGINE NACELLE OTBD SIDE FWD OF FWD COWL DOOR SKIN BY MEANS OF A DOUBLER REPAIR IAW ETD.

Part: WIRE — OVERHEATED (WINDSHIELD HEAT) · airframe 31,018 hrs · 42,449 cycles

WIRE SHOWS SIGNS OVERHEATING IN RIGHT DC RELAY BOX, W208-0240-2, FOR WINDSHIELD HEAT. REPLACED WIRE W208-0240-2 IN RT DC RELAY BOX IAW WM.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 31,018 hrs · 42,449 cycles

EMERGENCY EXIT SIGN AT 6A IS BROKEN. REPLACED EXIT SIGN.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,954 hrs · 42,359 cycles

FLOOR EMERGENCY LIGHT AT ROW 5 IS INOPERATIVE, REPLACED THE LAMPS.

Part: SIGN — LOOSE (CABIN) · airframe 30,504 hrs · 41,739 cycles

SMALL VERTICAL EMERGENCY EXIT SIGN AT 6C IS LOOSE. FLT 6221 TIGHTENED SIGN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,010 hrs · 41,055 cycles

FWD OVERHEAD EMERGENCY LIGHT AT ROW 2 DOES NOT ILLUMINATE. FLT 5442 RELAMPED.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 29,889 hrs · 40,895 cycles

LT WING NR 1 FUEL ACCESS PANEL FWD STRINGER 10 CRACKED. REPAIRED LT WING NR 1 FUEL PANEL FWD STRINGER 10 IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,611 hrs · 39,153 cycles

ONE WHITE FLOOR EMERGENCY LIGHT AT ROW 3 IS BURNED OUT. (FLT 5541) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,320 hrs · 38,743 cycles

EMERGENCY OVERHEAD LIGHT AT EXIT ROW 9 BURNED OUT. (FLT 5312) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,320 hrs · 38,743 cycles

EXIT ROW SEATS 9 B&C EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 5339) RELAMPED EMERGENCY LIGHT.

Part: COMPUTER — FAILED (AHRS) · airframe 28,263 hrs · 38,654 cycles

AIRCRAFT BEGAN YAWING AFTER YAW ENGAGED. (FLT 5336) REPLACED THE CAPTS AHRS COMPUTER AND BOTH AUTO-PILOT COMPUTERS. PN-622-6190-204 S/N ON-2667 S/N OFF-3072, P/N-622-8315-402 S/N ON-2469 SN OFF-1178, P/N-622-8315-402 SN ON-2581 SN OFF-2415.

Part: PRESSURE SWITCH — FAILED (LT ENGINE) · airframe 27,812 hrs · 38,015 cycles

LEFT ENGINE AIR INLET DEICE FAILED IN FLIGHT IN ICING CONDITIONS. (FLT 5317) REPLACED LEFT ENGINE AIR INLET DEICE BOOT PRESSURE SWITCH.

Part: CLAMP — LOOSE (AC BAY) · airframe 27,366 hrs · 37,397 cycles

LEFT PACK OVERHEATING SMELL ON DESCENT. (FLT 5437) TIGHTENED A LOOSE CLAMP FOR LEFT PACK TEMPERATURE INLET CONTROL VALVE.

Part: APU — FAULTY (APU BAY) · airframe 26,959 hrs · 36,810 cycles

SMOKE IN THE CABIN. (FLT 5447) REPLACED APU ASSEMBLY.

Part: SWITCH — OUT OF POSITION (RAM AIR VALVE) · airframe 26,847 hrs · 36,656 cycles

SMOKE MAP LIGHT AND AURAL WARNING SOON AFTER LEFT PACK FAIL. (FLT 5322) REPOSITIONED RAM AIR INLET VALVE SWITCH TO CLOSED POSITION.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 26,847 hrs · 36,656 cycles

RECEIVED A CABIN ALT MESSAGE. (FLT 5616) REPLACED THE ELECTRONIC CONTROLLER AND TRIPLE INDICATOR IN REFERENCE TO EMB 120 AMM. P/N 22201T011400 S/N OFF 241 P/N 72015900-1410 S/N OFF 1754.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,514 hrs · 36,170 cycles

FLT 5614, NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,120 hrs · 34,201 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 9 IS OUT. (FLT 6426) RELAMPED EMERGENCY LIGHT.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 24,180 hrs · 32,856 cycles

FORWARD FUSELAGE STRINGER 18 IS CORRODED. (C-CHECK) REPAIRED FORWARD FUSELAGE STRINGER 18 PER SRM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 24,165 hrs · 32,836 cycles

CAPTAINS DIRECT VISION WINDOW IS CRACKED. (C-CHECK) REPLACED LEFT SIDE DIRECT VISION WINDOW.

Part: STRINGER — CRACKED (LT WING) · airframe 24,180 hrs · 32,856 cycles

CRACKED STRINGER IN LEFT WING THROUGH NR 2 FUEL PANEL. (C-CHECK) PERFORMED STRINGER SPLICE REPAIR AT LEFT WING NR 10 STRINGER BETWEEN RIBS 9 & 7 PER SRM.

Part: SPAR CAP — CRACKED (LT WING) · airframe 24,180 hrs · 32,856 cycles

LEFT WING FORWARD SPAR CAP INBOARD OF NACELLE CRACKED AT HI-LOK. (C-CHECK) REPAIRED LEFT WING AUX SPAR PER EMBRAER TECHNICAL DISPOSITION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,065 hrs · 32,707 cycles

MAIN CABIN EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: WIRE — BROKEN (CABIN) · airframe 23,860 hrs · 32,429 cycles

AFT FLOOR LEVEL EMERGENCY LIGHT IS OUT. (FLT 6473) REPAIRED BROKEN WIRE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,566 hrs · 32,008 cycles

WHITE EMERGENCY LIGHT AT SEAT 11 A FLOOR LEVEL INOPERATIVE. (FLT 6917) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,520 hrs · 31,943 cycles

LAST FLOOR LEVEL EMERGENCY LIGHT ON LEFT SIDE BURNT OUT. (FLT 6385) RELAMPED EMERGENCY LIGHT.

Part: WIRE — OUT OF POSITION (COCKPIT) · airframe 23,122 hrs · 31,373 cycles

FLIGHT DECK STARTED TO SMELL STRONGLY OF ELECTRONICS, NO SMOKE IN EVIDENCE. (FLT 6854) REPAIRED AND REPOSITIONED WIRE BEHIND OVERHEAD ELECTRICAL PANEL.

Part: WIRE — LOOSE (CABIN) · airframe 21,709 hrs · 29,366 cycles

EMERGENCY LIGHT OVER THE PASSENGER DOOR IS INTERMITTENT. (FLT 6282) RESEATED CONNECTOR WIRE.

Part: AHRS — MALFUNCTIONED (COCKPIT) · airframe 20,990 hrs · 28,297 cycles

CAPTAINS EADI SCREEN WENT BLANK FOR 10 SEC, THEN SCREEN CAME BACK ON WITH RED FLAGS AND BANK AT 30°, EVEN IN LEVEL FLIGHT. (FLT 6490) REPLACED THE PILOTS AHC85 AHRS COMPUTER AND ORIENTED IAW AMM 34-21-00.

Part: WIRE — BROKEN (CABIN) · airframe 20,606 hrs · 27,734 cycles

FOUR FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOP. (FLT 6455) REPAIRED BROKEN WIRE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 20,941 hrs · 28,235 cycles

STRINGER 19 CORRODED. (C-CHECK) REPAIRED PER SRM.

Part: TERMINAL — UNSECURE (GALLEY LIGHT) · airframe 20,152 hrs · 27,087 cycles

FLT 6339 - ELECTRICAL ODOR COMING FROM GALLEY AREA. RESECURED LOOSE TERMINAL CONNECTOR TO THE BULB.

Part: ROD END — BINDING (RT ELEVATOR) · airframe 19,708 hrs · 26,514 cycles

FLT 7808 - ELEVATOR TRIM BINDS IN FLIGHT. REPLACED ROD ENDS ON LEFT AND RIGHT ELEVATOR TRIM CONTROL RODS.

Part: ENGINE — OVERSPEED (RIGHT) · airframe 19,565 hrs · 26,314 cycles

FLT 5700 - RIGHT NP WENT TO 103 PERCENT DURING TAKE OFF. ACCOMPLISHED ENGINE RUNS, UNABLE TO DUPLICATE.

Part: ACTUATOR — FAULTY (MLG) · airframe 19,500 hrs · 26,234 cycles

FLT 5711 - RIGHT MAIN GEAR WOULD NOT RETRACT. REPLACED RIGHT MAIN GEAR ACTUATOR, P/N 1959-000-07, S/N ON 685, S/N OFF: B118.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 18,832 hrs · 25,331 cycles

BAGGAGE SMOKE "WARN" ON GLARESHIELD. (FLIGHT NR 3610) REPLACED AFT CARGO SMOKE DETECTOR IAW AMM 26-15-01. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 18,584 hrs · 25,012 cycles

FLIGHT ATTENDANT REPORTS THAT SEVERAL EMERGENCY EXIT SIGNS ARE INOP. FLIGHT 5408 - REPLACED THE MIDDLE ELBP. OPS CHECK GOOD.

Part: TIRE — FAILED (MLG) · airframe 18,270 hrs · 24,566 cycles

FLT 5780 - NR 1 MAIN TIRE FOUND FLAT AFTER LANDING. REPLACED NR 1 AND NR 2 MAIN WHEEL ASSEMBLIES PN 3-1446-1, SN/OFF 0695, PN 3-1446-1, SN/OFF 1267.

Part: BEARING — CORRODED (FLAP ACTUATOR) · airframe 18,185 hrs · 24,435 cycles

FOUND AT C-CHECK, RIGHT OUTBOARD FLAP ACTUATOR ROD END BEARING AND BOLT IS CORRODED. REPLACED ACTUATOR ROD END AND BOLT IAW CMM 25-50-23.

Part: STRINGER — CRACKED (LT WING) · airframe 18,185 hrs · 24,435 cycles

LEFT WING AREA NEAR THE NR 2 FUEL PANEL HAS A LEAKING RIVET, FOUND AT C-CHECK. REPAIRED STRINGER 10 IAW EMB 120 SRM 57-20-03.

Part: BOLT — CORRODED (FLAP ACTUATOR) · airframe 18,185 hrs · 24,435 cycles

RIGHT INBOARD FLAP ACTUATOR ROD END BEARING AND BOLT IS CORRODED, FOUND AT C-CHECK. REPLACED ACTUATOR ROD END AND BOLT IAW CMM 27-50-23.

Part: HYDRAULIC LINE — LEAKING (GREEN SYSTEM) · airframe 16,604 hrs · 22,268 cycles

LOST GREEN SYSTEM HYDRAULIC FLUID. REPLACED BAD SECTION OF HYDRAULIC PRESSURE LINE IN LEFT OUTBOARD NACELLE. SERVICED HYDRAULIC FLUID TO PROPER LEVEL. OPS AND LEAK CHECKS ARE GOOD.

Part: INVERTER — MALFUNCTIONED (NR 1 STATIC) · airframe 16,505 hrs · 22,144 cycles

BOTH CAPTAIN AND FIRST OFFICER RECEIVED YELLOW HEADING FLAGS. THEN RED HEADING FLAG. BOTH EHSI'S WERE BETWEEN 50-70 DEGREES OFF OF COMPASS. RETURNED TO SLC, REPLACED NR 1 STATIC INVERTER IAW MM 24-20-01. OPS CHECK GOOD.

Part: STRINGER — CRACKED (RT WING) · airframe 16,219 hrs · 21,765 cycles

RT WING IB FIRST PANEL FROM NACELLE HAS SEVERAL LEAKING RIVETS . FOUND STRINGER 8 CRACKED BETWEEN RIBS 7 AND 8. C/W STRINGER 8R REPAIR IAW SRM 57-20-03 AND IAW RII 57-900-1000.

Part: SERVO — MALFUNCTIONED (FLT DIRECTOR) · airframe 14,441 hrs · 19,601 cycles

FLIGHT DIRECTOR WILL NOT FOLLOW COMMAND BARS (+10 TO -5 DEG DISCREP INFLIGHT). REPLACED ELEVATOR PRIMARY SERVO IAW 22-10-05. OPERATIONAL CHECK GOOD.

Part: FCU — MALFUNCTIONED (T/E FLAP) · airframe 14,047 hrs · 19,142 cycles

CONTROL FAULT ON FCP DURING FLAP EXTENSION. REPLACED FLAP CONTROL UNIT, OPERATIONAL CHECK GOOD.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 13,847 hrs · 18,859 cycles

SEGMENT OF EMERGENCY EXIT LIGHTS FAIL TEST. CLEANED CONNECTOR FOR CENTER EMERGENCY LIGHTS BATTERY PACK, OPERATIONAL CHECK GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,732 hrs · 18,711 cycles

FWD "E" LIGHTS GO OUT DURING OPERATIONAL CHECK AFTER THREE SECONDS. REPLACED FORWARD EMERGENCY LIGHT BATTERY IAW MM 33-50-02. OPERATIONAL CHECK GOOD.

Part: SERVO — MALFUNCTIONED (AUTOPILOT) · airframe 13,722 hrs · 18,698 cycles

WITH AUTOPILOT SELECTED TO EITHER SIDE "TRIM FAIL" ON MAP AND THEN TRIM STARTED TO ROLL FORWARD. REPLACED ELEVATOR TRIM SERVO MOTOR IAW MM 22-10-05.

Part: SOCKET — SMOKE (SEAT LIGHT) · airframe 13,396 hrs · 18,292 cycles

SIDEWALL LIGHT ABOVE SEAT 6A EMITS SMOKE, STRONG ELECTRICAL ODOR AND BURN MARK IN CEILING PANEL. REPLACED LIGHT FIXTURE IN CEILING ABOVE SEAT 6A. OPERATIONAL CHECK GOOD.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 12,961 hrs · 17,732 cycles

"SMOKE" LIGHT ON THE MAP ILLUMINATED DURING FLIGHT AS WELL AS THE SMOKE LIGHT AND ALARM IN THE REAR OF THE CABIN. ALL LIGHTS AND ALARMS CEASED AFTER ABOUT 4 MINUTES. FLIGHT ATTENDANT REPORTED NO ODOR OF SMOKE OR FIRE INDICATION IN THE LAV OR CABIN AREA. NO SMOKE DETECTED IN THE COCKPIT. OPERATIONAL CHECK LAV SMOKE DETECTOR WITH NO DEFECTS.

Part: SEAL — DIRTY (PAX DOOR) · airframe 12,961 hrs · 17,732 cycles

MAIN CABIN DOOR IS DIFFICULT TO OPEN OR CLOSE. REMOVED FOD FROM AROUND DOOR SEAL. NO OTHER DEFECTS FOUND. CYCLED DOOR SEVERAL TIMES. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — FAILED (TE FLAP CONTROL) · airframe 12,267 hrs · 16,768 cycles

FLAP CONTROL FAULT. REPLACED CONNECTOR ON LEFT AND RIGHT OUTBOARD ACTUATOR. OPERATIONAL CHECK GOOD IAW MM 27-50-00.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 12,178 hrs · 16,650 cycles

SELECTING FLAPS TO 15 DEGREES GOT A CONTROL FAULT. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR IAW MM 27-50-09. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (OUTBOARD FLAP) · airframe 12,118 hrs · 16,572 cycles

REPEATED FLAP CONTROL FAULTS (APPROX 5) DURING CLIMB, CRUISE, DESCENT. REPLACED LEFT FLAP OUTBOARD FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-00. OPERATIONAL CHECK GOOD.

Part: ANNUNCIATOR — MALFUNCTIONED (TE FLAPS) · airframe 12,053 hrs · 16,493 cycles

REPEATED FLAP CONTROL FAULTS DURING FLIGHT. REMOVED AND REPLACED ANNUNCIATOR WITH SERVICEABLE UNIT IAW 27-50-10. OPERATIONAL CHECK GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 11,080 hrs · 15,159 cycles

EMERGENCY EXIT ROW LIGHTING IN ROW 6 INTERMITTENT, BOTH SIDES. REPAIRED WIRING BEHIND (EXIT) SIGN AT ROW 6A. OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 10,998 hrs · 15,019 cycles

RIGHT HAND FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED IAW MM 33-52-01, OPERATIONAL CHECK GOOD.

Part: CONNECTOR — DIRTY (TE FLAPS) · airframe 10,772 hrs · 14,686 cycles

AT 500 FT, FLAP AND ADVANCED SWS LIGHTS ON MAP ILLUMINATED. CLEANED AND RE-SAFETIED FLAP CONNECTORS. OPERATIONAL CHECK GOOD.

Part: SELECTOR — MALFUNCTIONED (TE FLAPS) · airframe 10,676 hrs · 14,546 cycles

DURING FLAP RETRACTION, RECEIVED CONTROL FAULT MESSAGE NUMEROUS TIMES. WOULD NOT RESET. REMOVED AND REPLACED FLAP SELECTOR LEVER ASSY WITH SERVICEABLE. OPS CHECK GOOD.

Part: CONTROL HANDLE — MALFUNCTIONED (TE FLAPS) · airframe 10,365 hrs · 14,120 cycles

ON APPROACH GOT A CONTROL FAULT ON THE OUTBOARD FLAPS WHEN SELECTING 15 DEGREES. ALSO GOT 2 CONTROL FAULTS ON THE OUTBOARD FLAPS WHILE IN CRUISE. REPLACED FLAP SELECTOR HANDLE. OPS CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 10,320 hrs · 14,058 cycles

CAPTAIN REPORTS OUTBOARD FLAPS HAD CONTROL FAULT MESSAGE DISPLAYED 2 TIMES IN A ROW. REMOVED AND REPLACED FLAP CONTROL UNIT AS REQUIRED. SYSTEM OPS CHECKS GOOD.

Part: INVERTER — MALFUNCTIONED · airframe 10,165 hrs · 13,858 cycles

PILOT REPORTS SEVERAL AUTO PILOT FAILURES ON BOTH SIDES WITH ASSOCIATED FD AND OTHER FLAGS. REMOVED AND REPLACED NR 1 INVERTER DUE TO POSSIBLE A/C POWER PROBLEMS TO AHRS AND AUTOPILOT COMPUTERS. OPS CHECK OF INVERTER AND A/P GOOD. REF EMB MM 120 24-21-01.

Part: FDAU — MALFUNCTIONED (COCKPIT) · airframe 9,928 hrs · 13,553 cycles

ON DEPARTURE, SMOKE EMITTED FROM FDAU CB ON OVERHEAD PANEL, CEASED WHEN CIRCUIT BREAKER WAS OPENED. REPLACED FDAU CB. SPLICED IN WIRE NR WE01-0023-22 ON RIGHT HAND SIDE. REMOVED AND REPLACED FDAU. SYSTEM OPS CHECK GOOD.

Part: CONTACTOR — FAILED (EMERGENCY LIGHT) · airframe 9,726 hrs · 13,297 cycles

EMERGENCY LIGHT CIRCUIT BREAKER POPPED. REPLACED EMERGENCY BUS CONTACTOR K0028. OPS CHECKS GOOD.

Part: STRUCTURE — CRACKED (LT NACELLE) · airframe 9,445 hrs · 12,949 cycles

LT ENGINE NACELLE DECK CRACKED BY ENGINE DRIVEN HYD LINE. (DISCOVERED DURING E005 INSPECTION) REPAIRED LEFT ENGINE NACELLE DECK CRACK IAW IC 2003-120/3178 2A AND SRM 51-40-00.

Part: CONTROL HANDLE — FAULTY (COCKPIT) · airframe 9,251 hrs · 12,714 cycles

CREW REPORTS MULTIPLE FLAP FAILURES WITH CONTROL FAULTS.REMOVED AND REPLACED FLAP HANDLE IAW MM 27-50-00. OPS CHECK GOOD.

Part: HYDRAULIC LINE — BROKEN (HYD SYSTEM) · airframe 9,090 hrs · 12,525 cycles

LOST ALL GREEN SYSTEM HYDRAULIC PRESSURE AND FLUID ENROUTE FROM CDC TO SLC. REPLACED BROKEN HYDRAULIC LINE AT LEFT RESERVOIR FOR ENGINE DRIVEN HYDRAULIC PUMP. FLUSHED SYSTEM & REPLACED ENGINE DRIVEN HYDRAULIC PUMP IAW 29-10-00. OPS AND LEAK CHECKS GOOD.

Part: LANDING GEAR — CONTAMINATED (MAINS) · airframe 7,807 hrs · 10,925 cycles

ON DEPARTURE OUT OF CPR, LANDING GEAR WOULD NOT RETRACT AND HAD RT MLG DISAGREEMENT. PERFORMED QRH AND GEAR EXTENDED. RETURNED TO CPR. INSPECTED LANDING GEAR DUE TO ICE ACCUMULATION. PERFORMED GEAR SWINGS IAW MM 32-30-00. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 7,469 hrs · 10,458 cycles

ABORTED TAKEOFF DUE TO A RED FLAG ON THE FIRST OFFICER'S RMI. RETURNED TO THE GATE. REMOVED AND REPLACED FO'S RMI IAW 34-26-01. OPS CHECK GOOD IAW MM 34-21-00 AND USED NAV 402 TEST SET TO VERIFY VOR STATION INDICATION.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 7,517 hrs · 10,521 cycles

FRAME 13, LOWER RIGHT HAND ANGLE AND CHANNEL CRACKED. FOUND DURING C CHECK INSPECTION. REMOVED CRACKED ANGLE AND CHANNEL. FABRICATED NEW ANGLE AND SPLICED IN A SECTION OF THE CHANNEL. INSTALLED BOTH IAW EMB SRM 51-70-05 AND 51-40-02.

Part: STIFFENER — CRACKED (RT NACELLE) · airframe 7,505 hrs · 10,503 cycles

RIGHT NACELLE AFT SIDE OF HYDRAULIC BULKHEAD HAS A CRACKED HORIZONTAL STIFFENER. FOUND ON C-CHECK INSPECTION. FABRICATED AND INSTALLED A DOUBLER IAW SRM 51-00-00 AND 51-40-02.

Part: CLIP — CRACKED (RT NACELLE) · airframe 7,517 hrs · 10,521 cycles

RIGHT NACELLE INBOARD AND OUTBOARD FRAME 17 CLIPS CRACKED AT BOTTOM RIVET HOLES. FOUND DURING C CHECK INSPECTION. STOP-DRILLED CRACKS AND INSTALLED REPAIR DOUBLERS ON THE FRAMES IAW EMB SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 7,505 hrs · 10,503 cycles

FRAME 13 LEFT AND RIGHT SIDES OF STEP INTO COCKPIT CRACKED INSIDE AND OUTSIDE OF VERTICAL BRACE. FOUND ON C-CHECK INSPECTION. REMOVED ANGLES, FABRICATED AND INSTALLED A NEW ANGLES AND A DOUBLERS IAW SRM 51-00-00 AND 51-40-02.

Part: FRAME — CRACKED (LT & RT NACELLE) · airframe 7,505 hrs · 10,503 cycles

LEFT AND RIGHT NACELLE INBOARD AND OUTBOARD EXHAUST MOUNTS HAVE INTERNAL FRAME CRACKS AT NUTPLATES. FOUND ON C-CHECK INSPECTION. STOP-DRILLED CRACKS AND INSTALLED A REPAIR DOUBLERS ON FRAMES IAW EMB SRM 51-70-05.

Part: BRACKET — CRACKED (RT WING) · airframe 7,505 hrs · 10,503 cycles

SMALL LOWER BRACKET AT RIB 15 IN RIGHT FUEL CELL IS CRACKED. CRACK IS ON INBOARD SIDE OF FRAME. FOUND ON C-CHECK INSPECTION. REMOVED AND REPLACED CRACKED SKIN CLIP IAW EMB SRM 51-40-02.

Part: CLIP — CRACKED (LT NACELLE) · airframe 7,505 hrs · 10,503 cycles

LEFT NACELLE OUTBOARD SIDE FRAME 17 CLIP CRACKED. FOUND ON C-CHECK INSPECTION. FABRICATED AND INSTALLED DOUBLER IAW EMB120 SRM 51-40-02.

Part: STIFFENER — CRACKED (LT NACELLE) · airframe 7,505 hrs · 10,503 cycles

LEFT NACELLE AFT SIDE OF HYDRAULIC BULKHEAD APPEARS TO HAVE A CRACKED VERTICAL STIFFENER. FOUND ON C-CHECK INSPECTION. FABRICATED AND INSTALLED DOUBLER IAW SRM 51-70-05 AND 51-40-02.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 7,517 hrs · 10,521 cycles

COCKPIT LEFT SIDE, JUST AFT OF DIRECT VISION WINDOW, FOUND CRACK IN INTERCOSTAL. FOUND DURING C CHECK INSPECTION. FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 51-00-00 & 51-40-02.

Part: BRACKET — CRACKED (RT WING) · airframe 7,505 hrs · 10,503 cycles

LOWER BRACKET AT RIB 16 APPEARS TO BE CRACKED ALONG OUTBOARD, AFT AREA OF BRACKET. RIGHT FUEL CELL. FOUND ON C-CHECK INSPECTION. REMOVED CRACKED CLIP AND FABRICATED NEW CLIP AND INSTALLED NEW SKIN CLIP IAW EMB SRM 51-40-02.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 6,151 hrs · 8,857 cycles

ABORTED TAKEOFF DUE TO ERRONEOUS TRIM WARNING, ALTHOUGH TRIM WAS SET IN THE GREEN. PERFORMED TRIM WARNING FUNCTIONAL CHECK IAW 27-32-00. OPS CHECK GOOD.

Part: ACCESS PANEL — MISSING (APU) · airframe 6,213 hrs · 8,936 cycles

APU ACCESS PANEL MISSING UPON ARRIVAL AT SLC. INSTALLED SERVICEABLE PANEL ASSEMBLY AS NEEDED. P/N ON 145-33351-401.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 6,031 hrs · 8,709 cycles

ON CLIMB THROUGH 16,000 FEET, ALT WARNING LIGHT CAME ON. QRH ACCOMPLISHED. MANUAL MODE WOULD NOT HOLD ALT LOW OR AUTO MODE. REMOVED AND REPLACED PRESSURIZATION AUTO CONTROLLER. OPS CHECKS GOOD. S/N ON 478, S/N OFF 437.

Part: LATCH — UNLATCHED (FUEL DOOR) · airframe 4,636 hrs · 6,686 cycles

ABORTED TAKEOFF AND RETURNED TO GATE BECAUSE SERVICE DOOR LIGHT CAME ON. RESECURED FUEL DOOR LATCH. OPS CHECK GOOD.

Part: INDICATOR — FAILED (COCKPIT) · airframe 3,777 hrs · 5,401 cycles

ON TAKEOFF, PASSING THROUGH 80 KNOTS RIGHT NP GAUGE FLUCTUATED FROM 100 PERCENT DOWN TO 50 PERCENT A FEW TIMES. ABORTED TAKEOFF. REPLACED RIGHT NP INDICATOR WITH SERVICEABLE UNIT. OPS CHECK GOOD. S/N ON B939, S/N OFF 105AB.

Part: WARNING SYSTEM — ILLUMINATED (PROP DEICE SYS) · airframe 3,777 hrs · 5,401 cycles

PROP DEICE FAILURE IN BOTH CYCLES. CIRCUIT BREAKER TRIPPED. FOLLOWED QRH PROCEDURES. PROP STILL FAILED. RETURNED TO LAX. RAN DEICE SYSTEM IAW 20-10-00. ALL CHECKS OK AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 3,706 hrs · 5,296 cycles

WHILE APPLYING TAKEOFF POWER RAN BOTH ENGINES. COULD NOT DUPLICATE. CHECKED ENGINE CONTROL CHIME WITH EECS OFF. CHECK GOOD.

Part: FILTER — FAILED (SCAV) · airframe 3,611 hrs · 5,155 cycles

ALT 400 FEET WE ENCOUNTERED WAKE TURBULENCE WITH AN UNCOMMANDED LEFT ROLL. THE WAKE TURBULENCE PERSISTED AND IN ORDER TO REGAIN STABILITY CONTROL AND CLIMB ABOVE IT, I ADDED POWER. I OBSERVED 132 PERCENT TORQUE WHEN I REDUCED THE POWER TO LIMITS. THE OVERTORQUE LASTED FOR 2-3 SECONDS. THE ACTION WAS TAKEN TO ENSURE SAFETY OF LIGHT AND TO REGAIN POSITIVE RATE OF CLIMB. RETURNED TO SMX. COMPLIED WITH INSPECTION OF NUMBER ONE AND NUMBER TWO ENGINES SCAVENGE FILTERS RGB CHIP DETECTORS. REPLACED NUMBER ONE AND NUMBER TWO SCAVENGE FILTERS. NO DEFECTS NOTED. PERFORMED ENGINE POWER ASSURANCE RUNS. OPS CHECK GOOD. NO LEAKS NOTED.

Part: RUDDER PEDAL — OUT OF ADJ (COCKPIT) · airframe 3,137 hrs · 4,470 cycles

WHEN CAPTAIN PUT FEET ON RUDDER PEDALS RUDDER PEDALS MOVED ALMOST FULL TRAVEL FOWARD. READJUSTED THEM AND HAD NO FURTHER PROBLEMS. CHECKED CABLE AT RUDDER PEDAL ADJUST HANDLE DRIVE SHAFT, FOUND GOOD. REINSTALLED CABLE RUDDER PEDALS, FULLY ADJUSTED WITH NO SLIPPAGE. UNABLE TO DUPLICATE SQUAWK.

Part: GENERATOR — FAILED (RT MAIN) · airframe 3,045 hrs · 4,334 cycles

RIGHT MAIN GENERATOR FAILURE AFTER TAKEOFF. SYSTEM TRANSFERRED TO EMERGENCY MODE WITH APU ONLINE. RETURNED TO ACV. REPLACED RIGHT MAIN GENERATOR IAW EMB 120 MM 24-30-01. OPS CHECKS GOOD ON GROUND. (P/N 23080-013) (S/N 7370) ON, (S/N 6851) OFF.

Part: ACTUATOR — LACK OF LUBE (ELEVATOR TRIM) · airframe 1,667 hrs · 2,386 cycles

ELEVATOR TRIM BINDS AND SUDDENLY RELEASES IN DSC MODE. RATE GREATER THAN 1500 RPM. LUBED BOTH LEFT AND RIGHT TRIM ACTUATORS, OPS CHECK GOOD ON THE GROUND.

Part: SENSOR — INTERMITTENT (RT MLG)

RIGHT MAIN GEAR A INTRANSIT LIGHT WOULD NOT EXTINGUISH ON GEAR RETRACTION. CYCLED GEAR TWICE WITH SAME RESULTS.. RETURNED TO PSP. TROUBLESHOOTING OF RIGHT MAIN GEAR A INTRANSIT. FOUND RIGHT GEAR PROXIMITY SENSOR INTERMITTENT. INSTALLED SERVICEABLE PROXIMITY SENSOR PER MM 326101. OPS CHECKS GOOD.