N218SW

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,480 hrs · 48,752 cycles

FLT 5732 - EMERGENCY OVERHEAD LIGHT AT ROW 9BC INOP. RELAMPED.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 34,370 hrs · 48,599 cycles

FLT 5879 - EMERGENCY EXIT LIGHTS OUT. REPLACED AFT BATTERY PACK PN D366-04-001, SN ON 1199, SN OFF 77Y.

Part: BALLAST — LEAKING (LAVATORY) · airframe 34,170 hrs · 48,338 cycles

AFTER TAKEOFF, SMELL OF SMOKE IN FLIGHT DECK; LAV SMOKE DETECTOR ACTIVATED (FLT 5538). REPLACED LEAKING LAV LIGHT BALLAST.

Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 34,064 hrs · 48,220 cycles

FLT 5562 - EMERGENCY EXIT SIGN ROW 6A UNINTELLIGIBLE. REPLACED SIGN ASSEMBLY.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 33,619 hrs · 47,629 cycles

FUSELAGE FRAME BEHIND CAPTS DV WINDOW IS CRACKED. (FOUND AT C-CHECK) REPLACED CRACKED FRAME IAW SRM 51-10-02 PAR 3.

Part: SWITCH — DAMAGED (AUTOFEATHER SYS) · airframe 33,138 hrs · 46,971 cycles

FLT 5538 - LEFT AUTO-FEATHER SYSTEM FAILED. REPLACED PIN 1 ON AUTO-FEATHER TEST SWITCH. OPS CHECKS GOOD.

Part: SIGNAL COND UNIT — MALFUNCTIONED (ENGINE TORQUE) · airframe 33,125 hrs · 46,951 cycles

FLT 5098 - RECEIVED AN AUTO FEATHER AURAL WARNING ON TAKEOFF. REPLACED NR 2 ENGINE TORQUE SIGNAL CONDITIONER IAW EMB MM 77-11-01. OPS CHECK GOOD.

Part: UNKNOWN — SMOKE · airframe 33,125 hrs · 46,951 cycles

FLT 5706 - DURING CLIMB-OUT, THE LAV SMOKE DETECTOR ACTIVATED. NO VISIBLE SMOKE REPORTED. INSPECTED AND RAN BOTH PACK SYSTEMS WITH NO DISCREPENCIES NOTED. OPS CHECK GOOD.

Part: UNKNOWN — SMOKE (CABIN) · airframe 33,117 hrs · 46,942 cycles

THE LAV SMOKE ALARM WENT OFF AFTER TAKEOFF, FLIGHT NR 5748. INSPECTED AND OPERATED PACKS IN ALL MODES. COULD NOT DUPLICATE ANY DISCREPANCIES.

Part: BATTERY — FAULTY (SMOKE DETECTOR) · airframe 32,926 hrs · 46,672 cycles

FLT 5474 - LAV SMOKE DETECTOR ACTIVATED INFLIGHT. REPLACED LAV SMOKE DETECTOR BATTERY. OPS CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 32,418 hrs · 45,986 cycles

EMERGENCY EXIT SIGN AT ROW 9 IS INOP. REPAIRED EXIT SIGN WIRING. OPS CHECK GOOD.

Part: SMOKE DETECTOR — ACTIVATED (LAVATORY) · airframe 32,219 hrs · 45,718 cycles

FLT 5541 - LAV SMOKE DETECTOR SOUNDED WHEN APU WAS STARTED. OPERATED BOTH PACKS WITH NO DEFECTS NOTED.

Part: WIRE — INOPERATIVE (CABIN) · airframe 32,182 hrs · 45,662 cycles

FORWARD FLOOR EMERGENCY LIGHTS ARE INOP. REPAIRED WIRING AT FORWARD FLOOR LIGHTING STRIP.

Part: PULLEY — WORN (AILERON CONTROL) · airframe 30,786 hrs · 43,692 cycles

AILERON CONTROLS BIND IN CENTERED POSITION. REPLACED OUTBOARD AILERON PULLEYS ON LEFT AND RIGHT WINGS IAW MM 27-00-00.

Part: A/C PACK — ODOR (RIGHT) · airframe 30,585 hrs · 43,402 cycles

RIGHT PACK GIVES SLIGHT OVERHEATED ODOR IMMEDIATELY AFTER TAKEOFF. OPERATED RIGHT PACK FOR SEVERAL MINUTES AND COULD NOT DUPLICATE. OPERATIONAL CHECKS GOOD.

Part: SIGNAL COND UNIT — MALFUNCTIONED (ENG TORQUE) · airframe 30,394 hrs · 43,123 cycles

ON TAKEOFF, THE "AUTOFEATHER" SYSTEM WOULD NOT ARM. ABORTED T/O. REPLACED LEFT ENGINE TORQUE SIGNAL CONDITIONER. OPERATIONAL CHECKS GOOD. S/N OFF: 4713.

Part: CONTROL UNIT — FLUCTUATES (PROPELLER) · airframe 30,254 hrs · 42,920 cycles

RIGHT PROPELLER (NP) FLUCTUATING (ANALOG AND DIGITAL) ERRATICALLY AFTER TAKEOFF. REPLACED RIGHT PROP CONTROL UNIT IAW EMB-120 MM 61-21-00 AND C/W RII 61-900-1003. OPERATIONAL CHECKS GOOD.

Part: UNKNOWN — SMOKE (CABIN) · airframe 30,109 hrs · 42,725 cycles

ON GROUND WITH PACKS ON AUTO LOW GOT SMOKE COMING FROM THE VENTS. POWERED AIRCRAFT DOWN AND BACK UP. SMOKE CLEARED AND PACKS OPS CHECK GOOD.

Part: A/C PACK — ODOR · airframe 30,019 hrs · 42,599 cycles

PACKS FAILED AND SET OFF FIRE DETECTOR IN LAV AND THE CABIN HAD A BAD PACK SMELL. REMOVED EXCESS OIL ON RIGHT ENGINE AND CLEANED BOTH HEAT EXCHANGERS. OPERATIONAL CHECKS GOOD.

Part: A/C PACK — ODOR (LEFT) · airframe 29,932 hrs · 42,470 cycles

LEFT PACK STINKS AND SMOKES WHILE INFLIGHT IN AUTO/LOW. DRAINED LEFT ENGINE OIL TO PROPER LEVEL. OPERATIONAL CHECKS GOOD.

Part: RIB — CRACKED (LT WING) · airframe 30,164 hrs · 42,789 cycles

LEFT WING RIB 20 SHEAR CLIP UNDER 2ND AFT FROM FORWARD SPAR IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SHEAR CLIP UPPER 2ND FROM FORWARD SPAR AT RIB NR 2 PER EMB 120 SRM 51-40-02 AND RII 28-900-1000.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 30,164 hrs · 42,789 cycles

COCKPIT BELOW LEFT DV WINDOW FRAME 10 CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPAIRED FRAME NR 10 BELOW LEFT DV WINDOW PER SRM 53-00-04 AND RII 53-800-1000.

Part: SUPPORT — CRACKED (LT NACELLE) · airframe 30,164 hrs · 42,789 cycles

LEFT NACELLE OUTBOARD SUPPORT JUST FORWARD OF HYD BAY FIREWALL IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPAIRED OUTBOARD SUPPORT HALF FRAME FORWARD OF HYD BAY FIREWALL IN LEFT NACELLE PER SRM 54-20-04 FIG 201 AND RII 54-900-1000.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 29,836 hrs · 42,336 cycles

CLIMBING OUT, HAD AN ODOR OF SMOKE AND LAV SMOKE DETECTOR CAME ON. RETURNED TO FIELD. REMOVED EXCESS OIL FROM APU AND LT ENGINE AND SERVICED TO PROPER LEVELS. PERFORMED ENGINE AND APU BLEED CHECKS. UNABLE TO DUPLICATE DISCREPANCY.

Part: RELAY — MALFUNCTIONED (AUTOFEATHER SYS) · airframe 29,315 hrs · 41,591 cycles

AURAL TAKEOFF WARNING "AUTO FEATHER" ON CLIMB-OUT WITH AUTO FEATHER ARMED. REPLACED RELAY'S K0162 FEATHER SOLENOID RELAY NR 1 AND K0163 ELECTRIC FEATHER RELAY 1 ALSO TIGHTENED LOOSE CONNECTORS AT LT ENGINE TORQUE SIGNAL CONDITIONER. OPERATIONAL CHECKS GOOD, PN 1 ON/OFF M83536/2217, PN 2 ON/OFF MS1401-27.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 29,213 hrs · 41,439 cycles

FORWARD EMERGENCY LIGHTS WILL NOT TEST. INSTALLED SERVICEABLE ELBP. OPERATIONAL CHECKS GOOD.

Part: STALL WARNING — FALSE ACTIVATION · airframe 28,290 hrs · 40,104 cycles

ON TAKEOFF AT 100 KTS, RECEIVED STALL PUSHER, NO SHAKER. REPLACED STALL WARN TEST PANEL. INSPECTED STALL VANES AND SIDE SLIP. ALL CHECKED GOOD.

Part: LIGHT — BURNED OUT (ROW 9BC) · airframe 27,926 hrs · 39,563 cycles

OVERHEAD EMERG LIGHT ROW 9BC IS BURNED OUT. INSTALLED NEW BULB, OPERATIONAL CHECK GOOD.

Part: RECEPTACLE — LOOSE (EMERGENCY LIGHT) · airframe 26,945 hrs · 38,045 cycles

FA REPORTS OVERHEAD EMERGENCY LIGHT BY ROW 9 EXIT ROW INOP. RESECURED TERMINAL AT LIGHT RECEPTICAL. OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,945 hrs · 38,045 cycles

AFT CEILING EMERGENCY LIGHT INOP. RELAMPED AFT CEILING EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 26,620 hrs · 37,549 cycles

EXIT ROW LIGHT ROW 9 DOES NOT ILLUMINATE. REPAIRED WIRING INSIDE OVERHEAD BIN AT ROW 9. OPS CHECK GOOD.

Part: BELLCRANK — BROKEN (PAX DOOR) · airframe 26,193 hrs · 36,882 cycles

MAIN CABIN DOOR WON'T OPEN OR CLOSE. REPLACED BROKEN BELLCRANK. OPERATIONAL CHECKS GOOD IAW 52-11-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,182 hrs · 36,864 cycles

AFT OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP. OPERATIONAL CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 26,123 hrs · 36,767 cycles

F/A REPORTS RED FLOOR EMERGENCY LIGHT BURNT OUT. REPLACED BULB FOR FLOOR EMERGENCY LIGHT AS REQUIRED, OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,049 hrs · 36,654 cycles

EMERGENCY FLOOR LIGHTING INOP AT ROW 8A-2 WHITE LIGHTS, NUMEROUS RED LIGHTS, & MAIN CABIN DOOR FLOOR EMERGENCY EXIT SIGN. REPLACED LAMPS AS NECESSARY, OPERATIONAL CHECKS GOOD.

Part: APU — SMOKE (APU BAY) · airframe 25,813 hrs · 36,301 cycles

ON INITIAL POWER UP AFTER STARTING APU AND TURNING ON PACKS BOTH PACK FAIL LIGHTS ILLUMINATED & LAV SMOKE ALARM SOUNDED. F/A NOTED SMOKE SMELL IN CABIN. COULD NOT DUPLICATE PAC FAIL. NO DISCREPANCIES IN AIR CONDITIONING SYSTEM, GASPER FANS, APU BLEED, CROSS BLEED. OPERATIONAL CHECK GOOD. NO FURTHER BURNING SMELL.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 25,681 hrs · 36,126 cycles

EMERGENCY LIGHT NEXT TO GALLEY, ONE LIGHT IN STRIP INOPERATIVE. REPAIR BROKEN WIRE AS REQUIRED. OPERATIONAL CHECK GOOD.

Part: BATTERY — INOPERATIVE (SMOKE DETECTOR) · airframe 25,354 hrs · 35,638 cycles

SMOKE DETECTOR SOUNDED INFLIGHT, F/A REPORTED NO INDICATION OF SMOKE IN LAV. INSPECTED DETECTOR AND INSTALLED SERVICEABLE BATTERY. FOUND NO EVIDENCE OF SMOKE/FIRE IN LAV OR SURROUNDING AREA.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 25,050 hrs · 35,180 cycles

STALL WARNING WILL NOT CLEAR ON MAP. REPLACED STALL WARN PANEL PER MM 27-34-08. OPERATIONAL CHECK OK. P/N: 120-34428-505.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 24,921 hrs · 34,980 cycles

OVERHEAD BIN ROW 9 EXIT ROW LIGHT INOPERATIVE. REPLACED SPLICE IN GROUND WIRE AT EXIT LIGHT ASSY AT ROW 9. OPERATIONAL CHECK OK PER MM 33-50-00.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 24,678 hrs · 34,604 cycles

AFT OVERHEAD POD LIGHT INOP IN MAIN CABIN. REPLACED BULB IN AFT EMERGENCY LIGHT IN MAIN CABIN. OPERATIONAL CHECK GOOD.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 23,286 hrs · 32,390 cycles

LEFT DV WINDOW AFT BRACKET CRACK FRAME 12/13 DAMAGE OUT OF LIMITS. DISCOVERED DURING C-CHECK. REPLACED BRACKET AT FRAME 12/13 CENTER OF LEFT DV WINDOW PER SRM 51-40-00.

Part: DOOR FRAME — CRACKED (NACELLE) · airframe 23,286 hrs · 32,390 cycles

LEFT GEAR, FORWARD OUTBOARD DOOR NACELLE FRAME CHANNEL DENTED AND CRACKED BY DOOR TENSIONER. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED LEFT GEAR, FORWARD OUTBOARD DOOR NACELLE FRAME CHANNEL BY DOOR TENSIONER WITH A SERVICEABLE UNIT IAW SRM 51-10-02. OPS CHECKS GOOD.

Part: CLIP — CRACKED (RT NACELLE) · airframe 23,286 hrs · 32,390 cycles

RIGHT NACELLE FLAP WELL, OUTBOARD SKIN SUPPORT CLIP IS CRACKED OUT OF LIMITS. DISCOVERED DURING C-CHECK INSPECTION. REPLACED SKIN SUPPORT CLIP OUTBOARD IN RIGHT NACELLE FLAP WELL PER SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 23,286 hrs · 32,390 cycles

FRAME 13 ON LEFT SIDE FLOOR PROP DOUBLER IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT FLOOR PROP SUPPORT CLIP AT FRAME 13 PER SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (T/E FLAP) · airframe 23,138 hrs · 32,164 cycles

LEFT OUTBOARD FLAP, INBOARD ROLLER SUPPORT BRACKET IS CRACKED. DISCOVERED DURING LINE INSPECTION, INSTALLED SERVICEABLE BRACKET AND OPERATED FLAPS. OPS CHECKS GOOD. P/N: 120-21940-001

Part: FLAP TRACK — CRACKED (T/E FLAP) · airframe 23,008 hrs · 31,946 cycles

RIGHT OUTBOARD FLAP, OUTBOARD FLAP TRACK ON WING, IS CRACKED AT BOTTOM AFT RADIUS. DISCOVERED DURING LINE INSPECTION. REMOVED AND REPLACED RIGHT OUTBOARD FLAP OUTBOARD AFT TRACK IAW EMB 120 MM 57-53-04. PN ON 120-33047-004.

Part: LANDING GEAR — MALFUNCTIONED (LEFT) · airframe 21,644 hrs · 29,878 cycles

LT MAIN GEAR WOULD NOT RETRACT UNTIL 5TH LANDING GEAR CYCLE. RETURNED TO PDX. SWING GEAR COULD NOT GET TO DUPLICATE. CHECKED GAP ON HOOK IAW 32-32-10 CHECK GOOD. ADJUSTED TARGET IAW MM 32-61-01 AND ADJUSTED GEAR DOOR SEQUENCE VALVE (INBOARD AND OUTBOARD) IAW MM 32-32-04. SWUNG GEAR SEVERAL TIMES. SYSTEM CHECKS GOOD.

Part: LANDING GEAR — MALFUNCTIONED (LT & RT) · airframe 21,641 hrs · 29,873 cycles

UPON GEAR RETRACTION, WE GOT A GEAR DISAGREEMENT ON BOTH MAIN GEAR WITH LOUD VIBRATION. CYCLED GEAR 3 TIMES. DID NOT CORRECT IT. RETURNED TO RDM. PERFORMED GEAR SWING. SYSTEM OPS CHECK GOOD. COULD NOT DUPLICATE DISCREPANCY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 21,556 hrs · 29,762 cycles

FOUR LIGHTS ON FLOOR LEVEL EMERGENCY LIGHTING STRIPS FAIL TO ILLUMINATE. INSTALLED SERVICEABLE EMERGENCY LIGHT BATTERY FOR CENTER SECTION. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 21,330 hrs · 29,426 cycles

EMERGENCY LIGHTS FROM ROW 9 AND AFT ARE INOP. REPLACED AFT BATTERY PACK FOR EMERGENCY LIGHTS. OPS CHECK GOOD.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 21,078 hrs · 29,061 cycles

FORWARD DOOR LIGHT WITH TRIPLE CHIME ON BEGINNING OF TAKEOFF ROLL. ABORTED TAKEOFF. ADJUSTED FORWARD DOOR MICROSWITCH. OPS CHECK GOOD.

Part: FRAME — CRACKED (RT WING) · airframe 20,961 hrs · 28,884 cycles

RIGHT INBOARD LEADING EDGE INBOARD FRAME CRACKED AT UPPER AND LOWER TERMINATION. REPAIRED RIGHT INBOARD LEADING EDGE INBOARD PER SRM 51-30-01, 51-10-02.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 20,355 hrs · 28,002 cycles

JUST AFTER ROTATION, TRIPLE CHIME AUTOPILOT WITH ASSOCIATED AUTOPILOT FAIL RED MAP INDICATION AND TRIPLE CHIME TRIM FAIL WITH ASSOCIATED TRIM FAIL MAP LIGHT. RAN QRH, RETURNED TO PSP. COMMAND BARS ON CAPTAIN'S SIDE STUCK 15 DEGREES DOWN AND 30 DEGREES RIGHT. OPS CHECK GOOD AT THIS TIME. COULD NOT DUPLICATE AUTOPILOT PROBLEM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 19,475 hrs · 26,699 cycles

FOUR EMERGENCY EXIT FLOOR LIGHTS INOP. RECONNECTED FLOOR EMERGENCY LIGHTING CONNECTOR.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 19,418 hrs · 26,616 cycles

LEFT SIDE DV WINDOW FRAME IS CRACKED. COMPLIED WITH SB 120-53-0072 STEPS 2.1 THROUGH 2.7 - INSTALLATION OF NEW DOUBLERS AND REPLACEMENT RIVETS.

Part: SWITCH — DIRTY (PAX DOOR) · airframe 19,394 hrs · 26,583 cycles

FORWARD DOOR LIGHT ILLUMINATED ON TAKEOFF. RETURNED TO GATE. REMOVED TRASH FROM DOOR MICROSWITCH. RESET BREAKER AND REPLACED BULBS. OPS CHECK GOOD.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 19,394 hrs · 26,583 cycles

DURING TAKEOFF ROLL, CABIN PRESSURIZED UP TO 2000+ PER MIN THEN UPON POWER REDUCTION DROPPED TO -2000 RAPIDLY. REPLACED ELECTRO PNEUMATIC OUTFLOW VALVE IAW RII CARD 21-302. OPS CHECK GOOD.

Part: ACTUATOR — WORN (AILERON TAB) · airframe 19,411 hrs · 26,606 cycles

RIGHT AILERON TRIM TAB ACTUATOR, ROD ATTACH FITTING SLOPPY/WORN AS MARKED. REMOVED AND REPLACED AILERON TRIM TAB ACTUATOR WITH SERVICEABLE ACTUATOR IAW EMB120 MM 27-11-00.

Part: BEARING — WORN (T/E FLAP) · airframe 19,411 hrs · 26,606 cycles

LEFT NACELLE FLAP INBOARD HINGE BEARING WORN. REPLACED HINGE ARM IAW 120 SRM 51-10-02, PAGE 3 SECTION 3A.

Part: ROD END — WORN (FLAP ACTUATOR) · airframe 19,411 hrs · 26,606 cycles

RIGHT NACELLE FLAP ACTUATOR ROD END WORN. REPLACED RIGHT NACELLE FLAP ACTUATOR ROD END IAW 27-50-08.

Part: CONTROL CABLE — WORN (ELEVATOR) · airframe 19,411 hrs · 26,606 cycles

RIGHT INBOARD AND OUTBOARD ELEVATOR CABLES WORN FORWARD OF WING BOX. REPLACED RIGHT INBOARD AND OUTBOARD ELEVATOR CONTROL CABLES IAW EMB120 MM 27-00-01.

Part: CONTROL CABLE — WORN (RUDDER) · airframe 19,411 hrs · 26,606 cycles

RIGHT INBOARD AND OUTBOARD RUDDER CONTROL CABLES WORN FORWARD OF WING BOX AT CABIN AREA. REPLACED RIGHT INBOARD AND OUTBOARD RUDDER CONTROL CABLES IAW EMB120 MM 27-00-01.

Part: BOSS — ELONGATED (AILERON) · airframe 19,411 hrs · 26,606 cycles

LEFT AILERON 2ND FROM INBOARD END HINGE POINT ELONGATED. REPLACED BOSS IAW 120 SRM 51-10-02.

Part: CONTROL CABLE — WORN (AILERON) · airframe 19,411 hrs · 26,606 cycles

RIGHT AND LEFT AILERON CONTROL CABLES (UPPER AND LOWER) WORN AT WING. REPLACED AILERON CONTROL CABLES IAW EMB120 MM 27-00-01.

Part: ROLLER — WORN (T/E FLAP) · airframe 19,411 hrs · 26,606 cycles

REMOVE AND REPLACE ALL RIGHT WING FLAP ROLLERS FOR WEAR. REMOVED AND REPLACED ALL RIGHT WING FLAP ROLLERS IAW EMB120 MM 27-50-12.

Part: RIVET — LOOSE (T/E FLAP) · airframe 19,411 hrs · 26,606 cycles

RIGHT NACELLE FLAP INBOARD BEARING ARM HAS LOOSE RIVETS. REMOVED AND REPLACED RIVETS IAW EMB120 SRM 51-40-02.

Part: CONTROL CABLE — WORN (AILERON TAB) · airframe 19,411 hrs · 26,606 cycles

AILERON TRIM CABLES WORN. REPLACED ALL AILERON TRIM CABLES IAW EMB120 MM 27-00-01.

Part: BUSHING — WORN (ELEVATOR) · airframe 19,411 hrs · 26,606 cycles

RIGHT ELEVATOR OUTBOARD HINGE BUSHING WORN. REMOVED AND REPLACED RIGHT ELEVATOR OUTBOARD HINGE BEARING ASSEMBLY AND SHIMMED IAW MM 27-31-02.

Part: BEARING — WORN (T/E FLAP) · airframe 19,411 hrs · 26,606 cycles

LEFT OUTBOARD FLAP INBOARD BEARING ON MOVEABLE CHANNEL WORN. REPLACED OUTBOARD FLAP INBOARD BEARING.

Part: BEARING — WORN (AILERON) · airframe 19,411 hrs · 26,606 cycles

LEFT AILERON QUADRANT ASSEMBLY WORN AT PIVOT PIN. REPLACED LEFT AILERON QUADRANT BEARINGS IAW EMB120 MM 27-11-05.

Part: LINK — WORN (FLAP ACTUATOR) · airframe 19,411 hrs · 26,606 cycles

RIGHT OUTBOARD FLAP ACTUATOR ATTACHMENT LINK WORN. REPLACED ATTACHMENT LINK IAW 27-50-00.

Part: CONTROL CABLE — WORN (RUDDER) · airframe 19,411 hrs · 26,606 cycles

LEFT AND RIGHT OUTBOARD AND INBOARD RUDDER CABLES IN TAIL WORN AT PRESSURE SEAL. REPLACED RUDDER CABLES IAW EMB120 MM 27-00-01.

Part: CONTROL CABLE — WORN (ELEVATOR) · airframe 19,411 hrs · 26,606 cycles

LEFT AND RIGHT INBOARD AND OUTBOARD ELEVATOR CABLES WORN IN TAIL AREA. REPLACED AFT ELEVATOR CABLES IAW EMB120 MM 27-00-01.

Part: FLAP TRACK — WORN (T/E FLAP) · airframe 19,411 hrs · 26,606 cycles

LEFT INBOARD FLAP, INBOARD STATIONARY TRACK WORN. REPLACED LEFT INBOARD FLAP INBOARD STATIONARY TRACK. P/N: 120-33041-003.

Part: ROLLER — WORN (T/E FLAP) · airframe 19,411 hrs · 26,606 cycles

REMOVE AND REPLACE ALL LEFT WING FLAP ROLLERS FOR WEAR. REMOVED AND REPLACED ALL LEFT WING FLAP ROLLERS IAW EMB120 MM 27-50-12.

Part: DUCT — LEAKING (RT ENGINE) · airframe 18,919 hrs · 25,908 cycles

RIGHT ENGINE DUCT LEAK IN FLIGHT. SHUT ENGINE DOWN AS PER QRH.RESECURED DRAIN TUBING CUP AT RIGHT ENGINE DEICER PRESSURE REGULATING VALVE. PERFORMED RUN UP. OPS CHECK GOOD IAW MM 30-10-06.

Part: ACTUATOR — WEAK (T/E FLAP) · airframe 3,843 hrs · 5,514 cycles

MULTIPLE FLAP DISAGREEMENT WHEN SET TO 45 DEGREES. NORMAL LANDING FLAPS 25 DEGREES. INSPECTED FLAP TRACKS FOR BROKEN/LOOSE HARDWARE, ALL OK. OPERATED ON GROUND, CHECK OK. LUBED ROLLERS CLEANED TRACKS, GROUND OPS GOOD. FOUND LEFT OUTBOARD FLAP ACTUATOR TO BE WEAK. REPLACED LEFT OUTBOARD FLAP IAW CHAPT 27-50-00 EMB MM. CLEARED ALL FLAP FAULTS. SYSTEM OPS CHECKS GOOD.

Part: SMOKE — DETECTED (LT PACK) · airframe 17,662 hrs · 24,078 cycles

LEFT PACK INFLIGHT SET OFF LAV SMOKE DETECTOR. RETURNED TO PDX. REPOSITIONED RAM AIR DOOR SWITCH TO CORRECT POSITION. OPS CHECKS GOOD. SECURED PANEL AND CONTROL KNOB.

Part: WARNING LIGHT — ILLUMINATED (RIGHT ENGINE) · airframe 17,601 hrs · 23,981 cycles

RIGHT DUCT LEAK LIGHT ILLUMINATED PRIOR TO TAKEOFF. CLOSED RIGHT BLEED VALVE AND LIGHT REMAINED ILLUMINATED FOR MORE THAN 3 MINUTES. SHUT DOWN RIGHT ENGINE. LIGHT REMAINED ILLUMINATED FOR FOUR MINUTES, UNTIL POWER DOWN. ABORTED TAKEOFF. RAN RIGHT ENGINE AND APU BLEEDS AND INSPECTED BLEED AIR DUCT FROM ENGINE NACELLE TO CROSSBLEED VALVE. NO LEAKS NOTED. INSPECTED DUCT LEAK SENSORS ALONG SAME AREA. NO DISCREPANCIES FOUND. OPS CHECK GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 17,535 hrs · 23,895 cycles

ON TAKE OFF ROLL, GOT TRIM AURAL WARNING WITH TRIM SET IN GREEN RANGE. ABORTED TAKEOFF. PERFORMED AURAL WARNING RESET PROCEDURES, CHECKS GOOD IAW MM 31-63-00

Part: UNKNOWN — ODOR (COCKPIT) · airframe 17,535 hrs · 23,895 cycles

RETURNED TO PDX WITH ELECTRICAL ODOR IN CABIN. FAS HANDSET INOP. FOUND STRONG ELECTRICAL SMELL TO BE COMING FROM FAS HANDSET. REPLACED FAS HANDSET ASSEMBLY PER MM 23-30-00. OPS CHECK GOOD. INSPECTED WIRING BEHIND FAS HANDSET, NO DISCREPANCIES NOTED

Part: WARNING LIGHT — FALSE ACTIVATION (WING DEICE) · airframe 17,479 hrs · 23,820 cycles

RIGHT INBOARD WING DEICE LIGHT ILLUMINATES ERRONEOUSLY. ABORTED TAKEOFF. MEL 30-10-1, MC 2762 RAN RIGHT INBOARD WING DEICE BOOTS. COULD NOT DUPLICATE AT THIS TIME. OPS CHECK GOOD.

Part: FLAP — ACTIVATED (TE FLAPS) · airframe 16,348 hrs · 22,178 cycles

FLAP DISAGREEMENT BOTH OUTBOARD SEGMENTS WHEN FLAPS SELECTED. DIVERTED TO RDD FROM ACV DUE TO RUNWAY RESTRICTIONS. INSPECTED FLAPS, CLEANED ACTUATOR CANNON CONNECTORS, LUBRICATED ROLLERS, FLAPS OPS CHECKS NORMAL.

Part: EEC — FAILED (RT ENGINE) · airframe 16,329 hrs · 22,147 cycles

RIGHT EEC FAILED DURING TAKEOFF, ABORTED IMMEDIATELY AT 40 KNOTS. CONNECTED EEC BREAKOUT BOX TO EEC FOUND SENSORS TO BE WITHIN PARAMETERS. CLEANED CANNON PLUGS AND REINSTALLED. RAN RIGHT ENGINE IAW MM 710000, BUT COULD NOT DUPLICATE DISCREPANCY. RIGHT ENGINE EEC, OPS CHECKS GOOD.

Part: LOCK — LOOSE (REFUELING DOOR) · airframe 15,791 hrs · 21,413 cycles

SERVICE DOOR ILLUMINATED INFLIGHT. RETURNED TO SFO. SECURED LOOSE CAMLOCK ON REFUELING DOOR, CHECKS GOOD.

Part: CONTROL CABLE — WORN (RT ELEVATOR)

BOTTOM RIGHT ELEVATOR CABLE SHOWING SIGNS OF WEAR AT BELLCRANK. WEAR CAUSED BY A SCREW BECOMING LODGED BETWEEN QUADRANT AND CABLE. EMBRAER MM IPC 27-31-00 ITEM 210 OF SECTION B PAGE 0 DATED JAN 10/87 SHOWS LOCATION OF QUADRANT. INSTALLED NEW CABLE ON RIGHT ELEVATOR LOWER SIDE IAW MM 27-00-01.

Part: EXHAUST PIPE — CRACKED (LEFT)

LEFT EXHAUST PIPE HAS APPROXIMATE 8 INCH CRACK AT BREATHER TUBE. ALSO, THERMAL BLANKETS SCORCHED. INSTALLED LEFT EXHAUST PIPE WITH SERVICEABLE UNIT PER MM 78-00-00. REPLACED THERMAL BLANKETS AS REQUIRED.

Part: SEQUENCE VALVE — DIRTY (LT MLG)

LEFT MAIN GEAR WOULD NOT RETRACT AFTER TAKEOFF. CYCLED GEAR THREE TIMES WITH NO CHANGE. RETURNED TO SMX. INSPECTED LEFT GEAR DOORS SEQUENCE VALVES FOR RIGGING, FOUND GOOD. CLEANED HEAVY GRIME FROM SEQUENCE VALVE. SWUNG GEAR SIX TIMES AND OPS CHECKS GOOD.

Part: FILTER — DIRTY (GREEN HYD SYST)

GREEN HYDRAULIC FILTER LIGHT CAME ON AFTER TAKEOFF. RETURNED TO SLC. REPLACED GREEN SYSTEM PRESSURE AND RETURN FILTERS. NO VISIBLE CONTAMINATION FOUND (RETURN PIN WAS POPPED). RAN BOTH HYDRAULIC SYSTEMS 15 MINUTES AND ALL CHECKS GOOD.

Part: ACTUATOR — FAILED (RUDDER)

AFTER DEPARTURE RIGHT RUDDER PEDALS REFUSED FURTHER MOVEMENT BEYOND NEUTRAL POSITION. RETURNED FOR LANDING. REPLACED GREEN SYSTEM RUDDER ACTUATOR IAW MM 27. OPS CHECKS GOOD.

Part: WATER SEPARATOR — MALFUNCTIONED (LT DE-ICE SYST)

ON CLIMB-OUT, LEFT DUCT LEAK LIGHT CAME ON. FOLLOWED QRH AND SHUT THE LEFT ENGINE DOWN. REPLACED LEFT DE-ICE WATER SEPARATOR.

Part: MECHANISM — OUT OF ADJUST (CARGO DOOR)

CARGO DOOR LIGHT ILLUMINATED ON TAKEOFF, MEL 52-70-1. RETURNED TO FIELD. INSTALLED NEW HARDWARE AND ADJUSTED MICROSWITCH ARM AS REQUIRED, OPS CHECKS GOOD.

Part: CONTROL BOX — MALFUNCTIONED (LT MLG)

LEFT LANDING GEAR WOULD NOT INITIALLY EXTEND. CYCLED GEAR HANDLE AND GEAR THEN EXTENDED. REPLACED LANDING GEAR CONTROL BOX SWING LANDING GEAR 25 TIMES. COULD NOT DUPLICATE PROBLEM. CHECKS GOOD.

Part: SWITCH — OUT OF ADJUST (FUEL DOOR)

AFTER TAKEOFF SERVICE DOOR LIGHT ILLUMINATED AND RETURNED FOR LANDING. READJUSTED FUEL DOOR MICROSWITCH. CLOSED DOOR AND SERVICE DOOR LIGHT REMAINS EXTINGUISHED. OPS CHECKS GOOD.

Part: RETRACT MECH — ICED UP (RT MLG)

RIGHT MAIN GEAR WILL NOT COME UP, TRIED TO CYCLE 3 TIMES. RETURNED TO FIELD. CLEANED SNOW AND ICE FROM GEAR WELL AREA, CYCLED GEAR 15 TIMES AND SYSTEM OPS CHECKS GOOD.

Part: LATCH — NOT SECURED (LT MLG DOOR)

LEFT GEAR DOOR REMAINED OPEN ON DEPARTURE. RETURNED TO FIELD. INSPECTED LATCH AND ROLLER, SECURED LATCH.

Part: NP INDICATOR — MALFUNCTIONED (LT PROPELLER)

LEFT NP INDICATION WENT TO ZERO, BOTH DIGITAL AND ANALOG. RETURNED TO THE FIELD. REPLACED NP INDICATOR. PERFORMED OPS CHECKS, CHECKS GOOD.

Part: STUBSHAFT BOLT — FAILED (NR 1 ENGINE)

AFTER TAKEOFF, NR 1 ENGINE FAILED. RETURNED FOR LANDING. INSTALLED SERVICEABLE ENGINE ASSEMBLY IAW MM 71-00-00. PERFORMED ALL APPLICABLE ENGINE RUNS, OPS CHECKS GOOD WITH NO LEAKS NOTED. *S/D* ENGINE SHUTDOWN AS RESULT OF FAILURE OF BOLTS ON ENGINE STUBSHAFT.

Part: ENGINE — FAILED (NR 1)

AFTER TAKEOFF, NR 1 ENGINE FAILED. RETURNED FOR LANDING. INSTALLED SERVICEABLE ENGINE ASSEMBLY IAW MM 71-00-00. PERFORMED ALL APPLICABLE ENGINE RUNS. OPS CHECKS GOOD WITH NO LEAKS NOTED.