N569SW

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 31,942 hrs · 44,385 cycles

EXIT SIGNS AT MAIN CABIN DOOR, ROW NR 1 & FIRST ROW OF FLOOR EMERGENCY LIGHTS DO NOT ILLUMINATE. FLT#5312 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,678 hrs · 44,006 cycles

ENTRY WAY EMERGENCY FLOOD LIGHT IS BURNED OUT. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,563 hrs · 43,823 cycles

EMERGENCY FLOOR LIGHTING NEAR SEAT 3A DOES NOT ILLUMINATE. REPLACED EMERGENCY FLOOR LIGHT NEXT TO ROW 3A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,207 hrs · 43,348 cycles

EMERGENCY LIGHTS AT 2A & 3A DO NOT ILLUMINATE. (FLT 5362) REPLACED 2A AND 3A FLOOR EMERGENCY LIGHT FIXTURES.

Part: WIRE — BROKEN (CABIN) · airframe 31,087 hrs · 43,165 cycles

FRONT 2 RED EMERGENCY FLOOR LIGHTS ARE BROKEN OFF. (FLT 5638) REPAIRED WIRES AT FRONT TWO RED EMERGENCY FLOOR TRACK LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,821 hrs · 42,796 cycles

EMERGENCY OVERHEAD LIGHT AT MAIN CABIN DOOR BURNED OUT. (FLT 5418) RELAMPED EMERGENCY LIGHT.

Part: MODULE — FAILED (NLG STEERING) · airframe 30,778 hrs · 42,739 cycles

AN UNCOMMANDED HARD TURN TO THE RIGHT. FULL LEFT RUDDER WAS INADEQUATE IN RETURNING THE AIRCRAFT TO THE CENTERLINE. (FLT 5444) REPLACED STEERING HYDRAULIC MODULE ASSEMBLY IN REFERENCE TO EMB 120 MM. P/N: 308550-1003 S/N OFF: 0284

Part: FIRE DETECTOR — FAILED (NR 1 ENGINE) · airframe 30,622 hrs · 42,520 cycles

LEFT DETECTOR INOPERATIVE AND ENGINE WW LIGHT. (FLT 5323) REPLACED NR 1 ENGINE ACCESSORY SECTION FIRE DETECTOR.

Part: FIRE LOOP — FAULTY (NR 1 ENGINE) · airframe 30,637 hrs · 42,541 cycles

INFLIGHT NR 1 ENGINE PER INOP ENG/WW LIGHT ILLUMINATED AND REMAINED ON. (FLT 5323) REPLACED NR 1 ENGINE ACCESSORY SECTION DETECTOR (FIRE LOOP) IAW AMM.

Part: DOOR SEAL — DAMAGED (CARGO DOOR) · airframe 30,504 hrs · 42,351 cycles

CABIN WOULD NOT HOLD PRESSURE WITH PACKS IN AUTO/LOW. (FLT 6264) REPLACED CARGO DOOR SEAL AND UPPER RETAINER IAW AMM PN1: 120-23118-001 / PN2: 120-23348-005.

Part: BATTERY — OVERHEATED (MAIN) · airframe 30,326 hrs · 42,081 cycles

BATTERY OVERHEATED IN FLIGHT. HIGHEST TEMPERATURE SEEN ON THE BATTERY TEMPERATURE GAUGE WAS 70°. (FLT 6283) REPLACED MAIN BATTERY IN REFERENCE TO AMM. P/N: 9750W0730-7 S/N OFF: 9009W0003.

Part: RELAY — FAILED (COCKPIT) · airframe 30,141 hrs · 41,824 cycles

CREW SMELLED HOT ELECTRICAL SMELL FROM FIRST OFFICER'S SIDE PANEL. NO SMOKE OBSERVED. (FLT 6233) REPLACED APU FEEDER PROTECTION RELAY IN REFERENCE TO EMB 120 MM.

Part: RCCB — ODOR (COOLING FAN) · airframe 29,972 hrs · 41,593 cycles

LEFT PACK SMELLS BURNT. (FLT 5380) REPLACED RCCB FOR LEFT GROUND COOLING FAN IN REFERENCE TO AMM. P/N SM600BA50N1

Part: PLACARD — BROKEN (CABIN) · airframe 29,502 hrs · 40,906 cycles

RIGHT OVERWING LOWER EMERGENCY PLACARD BROKEN. (FLT 5348) REPLACED RIGHT OVERWING LOWER FORWARD EMERGENCY EXIT PLACARD LIGHT ASSEMBLY IN REFERENCE TO EMB 120 MM.

Part: WIRE — BROKEN (CABIN) · airframe 29,359 hrs · 40,704 cycles

EMERGENCY EXIT SIGN ON OVERHEAD STORAGE BIN AT ROW 9 DOES NOT ILLUMINATE. (FLT 6767) REPAIRED BROKEN WIRE ON EMERGENCY EXIT LIGHT AT ROW 9 OVERHEAD BIN.

Part: WIRE — BROKEN (CABIN) · airframe 29,290 hrs · 40,625 cycles

EMERGENCY EXIT SIGN OVER SEAT 9B DOES NOT ILLUMINATE. (FLT 5586) REPAIRED BROKEN WIRE AT EMERGENCY EXIT SIGN OVER 9B.

Part: WIRE — UNSECURE (EXIT SIGN) · airframe 29,189 hrs · 40,483 cycles

OVERHEAD EMERGENCY EXIT SIGN AT ROW 9 IS OUT. (FLT 5432) RE-SECURED WIRING ON EMERGENCY EXIT SIGN.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 28,836 hrs · 39,976 cycles

PASSENGER CABIN FLOOR SUPPORT T BRACKET JUST AFT OF PASSENGER DOOR ENTRANCE HAS CORROSION AT FRAME 16. (C-CHECK) REPLACED PASSENGER CABIN FLOOR SUPPORT T BRACKET PER SRM.

Part: RIB — CRACKED (RT WING) · airframe 28,836 hrs · 39,976 cycles

RIGHT OUTBOARD WING NOSE RIB 20 CRACKED AT RIVET HOLE. (C-CHECK) REPLACED IN REFERENCE TO SRM.

Part: RIB — CRACKED (RT WING) · airframe 28,836 hrs · 39,976 cycles

RIGHT OUTBOARD WING NOSE RIB 21 CRACKED AT TOP RIVETS. (C-CHECK) REPLACED PER SRM.

Part: WIRE HARNESS — FAILED (RT MLG) · airframe 28,583 hrs · 39,623 cycles

LANDING GEAR LEVER FAILED TO RAISE AND LOCKED IN DOWN POSITION. FOLLOWED QRH PROCEDURE AND LANDING GEAR HANDLE RAISED. (FLT 5432) REPLACED RIGHT MAIN LANDING GEAR AIR/GROUND SWITCH HARNESS.

Part: WIRE — BROKEN (CABIN) · airframe 28,294 hrs · 39,235 cycles

RED EMERGENCY FLOOR LIGHT AT ROW 2 BROKEN. (FLT 6222) REPAIRED BROKEN WIRE FOR THE FLOOR EMERGENCY RED LIGHT AT ROW 2.

Part: WIRE — DISCONNECTED (CABIN) · airframe 28,230 hrs · 39,154 cycles

EMERGENCY LIGHTS ON CABIN FLOOR ARE OUT. (FLT 5362) RECONNECTED EMERGENCY FLOOR LIGHT WIRE.

Part: SOCKET — DEFECTIVE (CABIN) · airframe 28,177 hrs · 39,072 cycles

EMERGENCY LIGHT NEXT TO 2A LIGHT WILL NOT ILLUMINATE. (FLT 6501) REPLACED FORWARD FLOOR EMERGENCY LIGHTING STRIP LAMP SOCKET.

Part: WIRE — DAMAGED (CABIN) · airframe 28,130 hrs · 39,002 cycles

ONE RED LIGHT IS OUT ON FORWARD MOST FLOOR EMERGENCY LIGHT STRIP. (FLT 5375) REPAIRED WIRING AT FORWARD FLOOR LEVEL EMERGENCY LIGHT.

Part: WIRE — DAMAGED (EXIT SIGN) · airframe 27,983 hrs · 38,797 cycles

LIGHTED EMERGENCY EXIT ROW SIGN AT ROW 9 IS OUT. (FLT 6336) REPLACED WIRE AT ROW 9 LIGHTED EMERGENCY SIGN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,744 hrs · 38,465 cycles

ROW 1 FLOOR EMERGENCY LIGHT HAS A RED LIGHT OUT. (FLT 6426) RELAMPED EMERGENCY LIGHT.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 26,809 hrs · 37,143 cycles

MAIN CABIN DOOR HANDLE DIFFICULT TO OPEN. (FLT 6903) LUBED MAIN CABIN DOOR.

Part: SWITCH — DIRTY (CABIN DOOR) · airframe 26,657 hrs · 36,927 cycles

F/A'S MAIN CABIN DOOR BUTTON STUCK, NOT ALLOWING THE DOOR TO OPEN. (FLT 6846) CLEANED FORWARD DOOR SWITCH AT FLIGHT ATTENDANTS PANEL.

Part: DISPLAY — SMOKE (COCKPIT) · airframe 26,558 hrs · 36,792 cycles

SMOKE FROM DISPLAY. (FLT 6765) INSTALLED SERVICEABLE DISPLAY.

Part: SEAL — LACK OF LUBE (CABIN DOOR) · airframe 26,479 hrs · 36,688 cycles

MCD DIFFICULT TO OPEN AND CLOSE. (FLT 6418) LUBRICATED MCD SEAL.

Part: STRINGER — CRACKED (LT WING) · airframe 25,794 hrs · 35,772 cycles

LEFT NR 2 FUEL PANEL AFT STRINGER 81 IS CRACKED. (C-CHECK) REPAIRED PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,363 hrs · 35,141 cycles

EMERGENCY LIGHT AT ROW 9 ON THE FLOOR INOP. (FLT 6174) RELAMPED EMERGENCY LIGHT.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 23,249 hrs · 32,137 cycles

FLT 6254 - LEFT EXIT SIGN BROKEN. REPLACED SIGN.

Part: ROLLER — BINDING (PAX DOOR) · airframe 23,206 hrs · 32,079 cycles

FLT 7793 - MAIN CABIN DOOR HARD TO OPEN AND CLOSE. ADJUSTED DOOR RODS AND UPPER DOOR ROLLERS.

Part: SHIM — OUT OF ADJUST (CABIN DOOR) · airframe 23,154 hrs · 32,002 cycles

FLT 6066 - MAIN CABIN DOOR DIFFICULT TO OPEN. REPOSITIONED SHIMS.

Part: MECHANISM — BINDING (PAX DOOR) · airframe 22,532 hrs · 31,175 cycles

FLT 5611 - FA REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN. CLEANED AND LUBED DOOR MECHANISM.

Part: LANDING GEAR — SLUGGISH · airframe 22,480 hrs · 31,101 cycles

FLT 5579 - GEAR TOOK OVER 30 SECONDS TO RETRACT. REPLACED LANDING GEAR BOX.

Part: LANDING GEAR — HUNG UP · airframe 22,406 hrs · 31,003 cycles

FLT 7779 - LANDING GEAR WOULD NOT COME UP ON FIRST ATTEMPT. OPERATION CHECKS NORMAL.

Part: ENGINE — SLUGGISH (RIGHT) · airframe 22,366 hrs · 30,956 cycles

FLT 7790 - RIGHT ENGINE VERY SLOW TO SPOOL UP ON TAKEOFF; RECEIVED AN AUTOFEATHER AURAL WARNING WITH SWITCHES IN CORRECT POSITION. COMPLETED RIGHT ENGINE TRIM ADJUSTMENTS.

Part: FRAME — CRACKED · airframe 22,662 hrs · 31,350 cycles

C-CHECK, CABIN FRAME AFT TOP SIDE OF GASPER IS CRACKED. REPAIRED PER SRM.

Part: STRINGER — CRACKED (RT WING) · airframe 22,662 hrs · 31,350 cycles

C-CHECK, RIGHT INBOARD WING OUTBOARD PANEL STRINGER NR 8 CRACKED. REPAIRED PER SRM.

Part: RIB — CRACKED (LT WING) · airframe 22,662 hrs · 31,350 cycles

C-CHECK, LEFT OUTBOARD WING OUTBOARD OF NACELLE, RIB NR 16 LOWER CLIP CRACKED. REPLACED PER SRM.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 22,662 hrs · 31,350 cycles

C-CHECK, FLOOR EMERGENCY LIGHTS LOOSE AND INOP AT 2A. REPAIRED BROKEN WIRES AND REINSTALLED FLOOR EMERGENCY LIGHTS AT 2A.

Part: LIGHT — MISSING (CABIN) · airframe 22,211 hrs · 30,739 cycles

FORWARD EMERGENCY LIGHT MISSING, PULLED OUT (FLT 5456). INSTALLED LIGHT ASSEMBLY.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 21,819 hrs · 30,233 cycles

MAIN CABIN DOOR IS DIFFICULT TO OPEN. (FLIGHT NR 5561) LUBED PAX DOOR ROLLERS AND CONTACT POINTS. OPS CHECK GOOD.

Part: STRINGER — CRACKED (RT WING) · airframe 20,874 hrs · 28,962 cycles

RIGHT WING FUEL PANEL INBOARD OF NACELLE IS LEAKING FUEL. FOUND STRINGER NR 10 BETWEEN RIB 8 AND 9 ON RIGHT WING TO BE CRACKED. COMPLIED WITH STRINGER REPAIR PER EMB SRM 57-20-03.

Part: SIGN — MISSING (CABIN) · airframe 20,768 hrs · 28,813 cycles

FLT 5746 - FORWARD EXIT SIGN IS MISSING. INSTALLED MISSING EXIT SIGN. OPS CHECK GOOD.

Part: FIREWALL — CRACKED (LT NACELLE) · airframe 20,117 hrs · 27,958 cycles

LEFT ENGINE FORWARD FIREWALL IS CRACKED AT 12:00 POSITION. REPAIRED IAW EMB120 SRM 51-70-00.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 19,998 hrs · 27,824 cycles

FLT 3680 - EMERGENCY LIGHT LENS BELOW FA SEAT IS MISSING. INSTALLED NEW LENS.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 19,657 hrs · 27,375 cycles

FLIGHT ATTENDANT REPORTS THAT 4 FLOOR EMERGENCY LIGHTS DO NOT WORK, FLIGHT NR 5572. REPLACED EMERGENCY BATTERY PACK.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 19,048 hrs · 26,525 cycles

FIRST OFFICERS WINDSHIELD DAMAGED FROM JET BLAST. REPLACED FIRST OFFICERS WINDSHIELD IAW EMB MM 56-10-01.

Part: FRAME — CRACKED (PAX DOOR) · airframe 19,414 hrs · 27,006 cycles

PAX DOOR IS CRACKED AT FRAME 5 ON THE AFT SIDE, DISCOVERED AT C-CHECK. NEW FRAME INSTALLED IAW SRM 120 51-10-02 PG 3, SEC 3 A.

Part: WINDOW — SCRATCHED (CABIN) · airframe 19,373 hrs · 26,957 cycles

PAX WINDOW 11BC HAS TWO HEAVY SCRATCHES ON THE OUTER PANE, DISCOVERED AT C-CHECK. REPLACED PAX WINDOW AT 11BC IAW AMM 56-20-00.

Part: ATTACH FITTING — CORRODED (PAX DOOR) · airframe 19,373 hrs · 26,957 cycles

PAX DOOR FORWARD AND AFT CAM LINK ATTACH HARDWARE IS CORRODED, DISCOVERED AT C-CHECK. REPLACED HARDWARE AT PAX DOOR CAM LINKS AND BUSHINGS IAW 52-11-03.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 19,414 hrs · 27,006 cycles

PAX DOOR IS CRACKED AT AFT LOWER CORNER, DISCOVERED AT C-CHECK. REPLACED CRACKED BRACKET ON PAX DOOR AFT LOWER CORNER IAW EMB 120 SRM 51-10-02 AND 51-40-02.

Part: STRINGER — CRACKED (LT WING) · airframe 19,414 hrs · 27,006 cycles

LEFT WING NR 2 FUEL PANEL FORWARD STRINGER IS CRACKED, DISCOVERED AT C-CHECK. REPAIRED STRINGER IAW SRM 120 57-20-03, FIG 202, PG 206 TO 211.

Part: FRAME — CRACKED (PAX DOOR) · airframe 19,414 hrs · 27,006 cycles

PAX DOOR IS CRACKED AT FRAME NR 3 DISCOVERED AT C-CHECK. DOUBLER INSTALLED IAW SRM 120 52-10-02.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 19,414 hrs · 27,006 cycles

LEFT DV WINDOW HORIZONTAL SUPPORT BRACKET IS CRACKED, DISCOVERED AT C-CHECK. REPLACED SUPPORT BRACKET BEHIND LEFT DV WINDOW IAW EMB 120 SRM 51-10-02/51-40-02.

Part: BOSS — CRACKED (PAX DOOR) · airframe 19,373 hrs · 26,957 cycles

PAX DOOR HAS CRACKED LOCKING MECHANISM BOSS BETWEEN FRAMES 4 AND 5, DISCOVERED AT C-CHECK. REPLACED LOCKING MECHANISM BOSS IAW 52-11-03.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 18,178 hrs · 25,375 cycles

DETECTED ODOR OF SMOKE ON SHORT FINAL. COULD NOT DUPLICATE DISCREPANCY. LUBRICATED RAM AIR CHECK VALVES. OPERATIONAL CHECKS GOOD.

Part: LINE — BURST (HYD SYSTEM) · airframe 16,908 hrs · 23,672 cycles

INFLIGHT RECIEVED GREEN HYD SYSTEM RESERVOIR LOW LEVEL AND LOW PRESSURE IMMEDIATELY FOLLWED BY MAIN PUMP LOW PRESSURE AND AUTOMATIC ENGAGEMENT OF THE ELECTRIC PUMP. REPLACED BURST MAIN PRESSURE LINE IAW MM 20-10-04. OPERATIONAL CHECK GOOD.

Part: ROLLER — BINDING (PAX DOOR) · airframe 16,345 hrs · 22,891 cycles

MAIN CABIN DOOR HARD TO OPEN AND CLOSE. REPLACED FLAT SPOTTED CAM ROLLERS PER EMB MM 52-00-00. OPERATIONAL CHECK GOOD.

Part: BALLAST — SMOKE (CARGO LIGHTS) · airframe 15,151 hrs · 21,333 cycles

ON TAXI OUT, SMELLED SMOKE IN CABIN/COCKPIT THEN RECEIVED BAGGAGE COMPARTMENT FIRE/SMOKE INDICATION. REPLACED LIGHT BALLASTS AS NEEDED. OPERATIONAL CHECK GOOD.

Part: LATCH — BACKED OUT (PAX DOOR) · airframe 14,983 hrs · 21,120 cycles

MAIN CABIN DOOR WON'T OPEN. DOOR CAPTURE LATCH HAD BACKED OUT. REMOVED LATCH, CLEANED AND REINSTALLED. OPERATIONAL CHECK GOOD.

Part: COMPUTER — INTERMITTENT (STALL WARNING) · airframe 14,658 hrs · 20,700 cycles

STALL WARNING SYSTEM 2 FAILS INTERMITTENTLY ON GROUND AND IN FLIGHT. REPLACED NR 2 STALL COMPUTER. OPERATIONAL CHECK GOOD. P/N: C-81806-1, S/N OFF: 342.

Part: BATTERY PACK — INTERMITTENT (EMERGENCY LIGHT) · airframe 14,508 hrs · 20,492 cycles

FA REPORTS EMERGENCY LIGHTS FROM ROW 9 AFT WORK INTERMITTENTLY. REPLACED AFT CABIN EMERGENCY LIGHT BATTERY PACK.

Part: COMPUTER — INTERMITTENT (STALL WARNING) · airframe 14,212 hrs · 20,113 cycles

F/O STALL WARNING CAME ON INFLIGHT, AURAL WARNING, LIGHT ON MAP. REMOVED AND REPLACED NR 2 STALL WARNING COMPUTER WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD IAW MM 27-34-04.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 14,052 hrs · 19,915 cycles

EXIT LIGHT ON OVERHEAD BIN-ROW 9 IS INOPERATIVE. REPAIRED BROKEN WIRE. OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 13,997 hrs · 19,849 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 9 INOPERATIVE. REPAIRED BROKEN WIRE. OPERATIONAL CHECK GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (STALL WARNING) · airframe 12,908 hrs · 18,393 cycles

STALL WARNING SYSTEM TEST NR 2 BUTTON LIGHT OUT, AFTER TEST BUTTONS PUSHED, BOTH SIDES STMI WARN RED LIGHT ON MAP STAYS ON. REPLACED STALL WARNING CONTROL PANEL. STALL WARNING 1 AND 2 OPERATIONAL CHECK GOOD. PN: 120-34428-505, S/N OFF: 120473.

Part: WIRE — BROKEN (CABIN) · airframe 12,753 hrs · 18,182 cycles

ONE EMERGENCY LIGHT IS INOP (LEFT SIDE OF AISLE).REPLACED BROKEN WIRE. OPS CHECK GOOD.

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 11,451 hrs · 16,559 cycles

UPON FLAP RETRACTION AFTER TAKEOFF, FLAPS HAD DISAGREEMENT. IB WOULD NOT RETRACT INITIALLY. AFTER APPROXIMATELY 1 MIN, IB FLAPS RETRACTED. AFTER LANDING, FLAPS WOULD NOT RETRACT BEYOND 5-10 DEGREES WITH DISAGREEMENT ALL FLAPS. REMOVED AND REPLACED FCU IAW EMB MM 27-50-06. OPS CHECK GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 11,119 hrs · 16,160 cycles

EXIT ROW LIGHT BELOW DOOR AT SEAT 6A BROKEN. REMOVED AND REPLACED EXIT LIGHT ASSY AT SEAT 6A. OPS CHECK GOOD. PN: 10-1301-15

Part: PROXIMITY SENSOR — BROKEN (LEFT MLG) · airframe 10,700 hrs · 15,603 cycles

GNS AFIS FUNCTION DOES NOT RECORD OFF OR ON TIMES AND CREW HAD TO USE THE DOWNLOCK RELEASE BUTTON TO RETRACT THE GEAR. INSPECTED LANDING GEAR SYSTEM. FOUND LEFT MLG GROUND PROX SENSOR TO BE BROKEN. REMOVED AND REPLACED PROXIMITY SENSOR WITH A SERVICEABLE UNIT AND ACCOMPLISHED NUMEROUS GEAR SWINGS WITH NO FURTHER DEFECTS. OPS CHECK GOOD. VERIFIED CORRECT OUT, OFF, ON AND IN TIMES. GNS OPS CHECK GOOD.

Part: WIRE — CHAFED (NAV LIGHT) · airframe 10,116 hrs · 14,757 cycles

NAV LIGHT CIRCUIT BREAKER POPPED. RETURNED TO GEG. FOUND CHAFED WIRES IN RIGHT SIDE LEADING EDGE. REPAIRED WIRES AS REQUIRED AS PER EMB MM 33-00-00. LIGHT OPS CHECK GOOD.

Part: TORQUE SENSOR — MALFUNCTIONED (RIGHT ENGINE) · airframe 9,644 hrs · 14,028 cycles

ABOVE V1, AFTER FLAP & GEAR RETRACTION, THE RT ENGINE FEATHERED. TQ READ ZERO, ALL OTHER PARAMETERS NORMAL. POWER LEVER WAS BROUGHT TO FLIGHT IDLE, CONDITION LEVER FEATHER, ENGINE WAS LEFT RUNNING AND A SINGLE ENGINE LANDING WAS PERFORMED. REPLACED RT PROP ASSEMBLY IAW EMB120 MM 61-10-03. COMPLIED WITH RIGHT ENGINE BOROSCOPE INSPECTION PER P&W MM. COMPLIED WITH OVERTORQUE FORM ST72-334. ALL INSPECTIONS FOUND TO BE FREE OF DISCREPANCIES. REPLACED RT ENGINE TORQUE SENSOR WITH SERVICEABLE UNIT. PERFORMED ENGINE RUN-UP, TORQUE CHECKS GOOD, ALL OTHER PARAMETERS NORMAL. PN OFF 3116942-01 SN OFF 7537.

Part: BATTERY — DISCHARGED (CABIN) · airframe 9,400 hrs · 13,652 cycles

DURING F/A PREFLIGHT EMERGENCY LIGHTS COME ON THEN GO DARK. TEST FAILED. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT 5BC. OPS CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (ELEVATOR TAB) · airframe 8,345 hrs · 11,986 cycles

CLIMBING TO FLIGHT LEVEL 200 AT APPROXIMATELY 18,000 FT, ELEVATOR TRIM WHEEL FROZE. UNABLE TO MOVE THE WHEEL UNTIL DESCENDED BELOW APPROXIMATELY 12,000 FT BELOW THAT ALTITUDE THE TRIM FUNCTIONED NORMALLY. REMOVED AND REPLACED BOTH LEFT AND RIGHT ELEVATOR TRIM TAB LINEAR ACTUATORS IAW MM 27-32-02. ADJUSTED TRIM TAB CABLE TENSIONS IAW MM 27-00-01. OPS CHECK GOOD.

Part: ACTUATOR — FAULTY (T/E FLAP) · airframe 8,004 hrs · 11,470 cycles

WHILE IN CRUISE, FLAP AND ASYMMETRY AND CONTROL FAULT WARNINGS. POSITIVE ROLL TO THE RIGHT. OUTBOARD PAIR OF LIGHTS FLASHING. MEGGED-OUT ALL WIRES TO FCU. FOUND NO DISCREPANCIES. UPON RETRACTION TEST FOUND LEFT OUTBOARD FLAP ACTUATOR TO EXTEND AND THEN RETRACT 2 DEGREES, THEN EXTEND A LITTLE MORE THEN RETRACT 2 DEGREES, ALL THE WAY DOWN ON EXTENSION CYCLE. REPLACED LEFT OUTBOARD FLAP ACTUATOR IAW 27-50-09. CYCLED FLAPS 5 TIMES. OPS CHECK GOOD.

Part: FCU — FAULTY (T/E FLAP) · airframe 8,000 hrs · 11,463 cycles

WHILE EN ROUTE GOT FLAP WARNING ASYMMETRY ASSOCIATED WITH CONTROL FAULT AND ADVANCED SWS. FLAP PAIR LIGHT BARS ON OUTBOARD PAIR SHOW ASYMMETRY WARNING, ONLY ONE LIGHT SEGMENT. THERE WERE NO CONTROL PROBLEMS OR ROLL TENDENCIES. PERFORMED SYSTEM SELF-DIAG TEST USING VERSION II ANNUNCIATOR FOUND OUTBOARD EXTEND SOLENOID TO BE STUCK OPEN. CHECKED ACTUATORS IAW 27-50-00. NO FAULTS FOUND. REMOVED AND REPLACED FCU IAW MM 27-50-06. CLEARED FAULT. OPS CHECK GOOD. P/N: 347200-1001, S/N OFF: 0222.

Part: BEARING — FAILED (AILERON) · airframe 7,811 hrs · 11,178 cycles

RIGHT AILERON INBOARD HINGE BEARING IS FALLING APART. REMOVED AND REPLACED INBOARD HINGE BEARING IAW MM 20-40-00.

Part: BUSHING — WORN (T/E FLAP) · airframe 7,811 hrs · 11,178 cycles

LEFT NACELLE FLAP INBOARD HINGE POINT BUSHINGS HAVE PLAY, INBOARD AND OUTBOARD. REMOVED AND REPLACED BUSHINGS IAW SRM 54-20-02. (P/N 120-39902-005)

Part: BOOT — DAMAGED (RIGHT WING) · airframe 7,811 hrs · 11,178 cycles

OUTBOARD LEFT WING AND OUTBOARD RIGHT WING LEADING EDGE DEICERS FAILED SIMULTANEOUSLY AT FL200. SYSTEM OPERATED NORMALLY FOR 10 MINUTES PRIOR TO FAILURE. BOTH TIMERS 1 AND 2 RESULTED IN FAILURES AS PER QRH. INSPECTED AND FOUND HOLE IN RIGHT BOOT - OUTER TOP AREA. REPAIRED WITH BFG DEICER PATCH. OPERATIONALLY CHECKS GOOD. LIGHTS AND FUNCTION OF INFLATION OK.

Part: CONNECTOR — DIRTY (SMOKE DETECTOR) · airframe 7,486 hrs · 10,690 cycles

BAGGAGE SMOKE/FIRE EXTINGUISHER WILL NOT SOUND AURAL SMOKE WARNING WHEN TESTING. CLEANED CANNON PLUG ON CARGO COMPARTMENT DETECTOR ASSEMBLY. OPS CHECK GOOD AT THIS TIME.

Part: INDICATOR — MALFUNCTIONED (RT ENG TORQUE) · airframe 6,814 hrs · 9,695 cycles

TORQUE FLUCTUATIONS RIGHT ENGINE ON TAKEOFF ROLL. ABORTED AND RETURNED TO GATE. REPLACED RIGHT ENGINE TORQUE GAUGE. OPS CHECK GOOD.

Part: BRUSH BLOCK — FAILED (RT PROP) · airframe 6,490 hrs · 9,207 cycles

RIGHT PROP INOP LIGHT ILLUMINATED ON TIMER 1 & 2. RETURNED TO FIELD. REPLACED RT ENGINE BRUSH BLOCK. OPS CHECK GOOD 30-60-00, 71-00-00. UPDATE BOI: REMOVED AND REPLACED RIGHT ENGINE OIL DEICE PRESSURE SWITCH IAW EMB120 MM 79-00-00. OPS CHECK IAW EMB120 MM 30-60-00. P/N: 1153P0013-01, S/N ON: 1061, S/N OFF: 0504.

Part: BOOT — CONTAMINATED (ENGINE INLET) · airframe 6,194 hrs · 8,773 cycles

BOTH ENGINE AIR INLET DEICE BOOTS FAILED ON CLIMBOUT. RETURNED TO FIELD. PURGED MOISTURE FROM LEFT AND RIGHT INLET BOOT TUBING. PERFORMED RUNUP. NO FAILURE DURING TEST.

Part: CONNECTOR — CONTAMINATED (TE FLAPS) · airframe 5,573 hrs · 7,920 cycles

IN FLIGHT AT FLIGHT LEVEL 230 ELEVATOR TRIM BECAME VERY ERRATIC. DISCONNECTED TRIM AND AUTOPILOT. TRIM WHEEL BECAME VERY HARD TO TURN. REMOVED MOISTURE FROM LEFT AND RIGHT ELEVATOR TRIM ACTUATORS. CYCLED ELEVATOR TRIM FULL TRAVEL. OPS CHECK GOOD.

Part: STRUT — DISCHARGED (NLG) · airframe 4,748 hrs · 6,709 cycles

GEAR DOOR NOT RETRACT NORMALLY, MUST USE DOWNLOCK RELEASE. SERVICED NOSE STRUT ASSEMBLY WITH NITROGEN IAW MM 12-13-04. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,403 hrs · 6,229 cycles

LINE RIGHT FORWARD EMERGENCY LIGHT INOP, FOUND CENTER ELBP LOW VOLTAGE. REMOVED AND REPLACED CENTER ELBP, OPS CHECK GOOD P/N ON D36604001, S/N 104, S/N OFF 178.

Part: DOOR — NOT LATCHED (FUEL SERVICE)

RETURNED TO LAS DUE TO SERVICE DOOR LIGHT. FOUND FUEL DOOR NOT LATCHED PROPERLY. FUELER LATCHED DOOR, CHECKS GOOD. MEL 52-70-1. INSPECTED ALL SERVICE DOORS AND LATCHES. ALL FOUND GOOD. SERVICE DOOR LIGHT SYSTEM FOUND TO BE WORKING NORMAL.