N583SW

Part: COMPUTER — SMOKE (AUTOPILOT) · airframe 32,005 hrs · 43,927 cycles

WHEN FO TOGGLED ON AUTOPILOT, GOT A TRIM FAIL AND AUTOPILOT FAIL ON MAP AND SMOKE OUT OF GLARESHIELD ABOVE FOS FCP. DECLARED EMERGENCY. REPLACED FCP AND AUTOPILOT COMPUTER. PERFORMED OPS CHECK OF AUTOPILOT SYS. TESTED OK. IAW AMM.

Part: BULKHEAD — CRACKED · airframe 31,952 hrs · 43,849 cycles

LT HYDRAULIC RESERVOIR FORWARD BULKHEAD OTBD SIDE IS CRACKED. REPAIRED LT FORWARD HYDRAULIC BAY BULKHEAD IAW ETD.

Part: STRUCTURE — CRACKED (RT MLG DOOR) · airframe 31,487 hrs · 43,140 cycles

RIGHT MAIN GEAR DOOR INBD AFT TOP REAR CRACKED. INSTALLED INTERNAL AND EXTERNAL DOUBLER WITH THE ADDITION OF FILLER AT UPPER AFT AREA OF RT INBD AFT GEAR DOOR IAW ETD.

Part: LIGHT — LOOSE (CABIN) · airframe 31,460 hrs · 43,109 cycles

FLOOR LEVEL EMERGENCY LIGHT LOOSE. SECURED THE LIGHT.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,419 hrs · 43,050 cycles

ROW 1 EMERGENCY LIGHT INOPERATIVE. REPLACED BULB AND HOUSING ASSY IAW AMM.

Part: TIRE — HOT (RT MLG) · airframe 30,879 hrs · 42,269 cycles

OUTBOARD TIRE ON RT MLG IS EXCESSIVELY HOT. BURNING ODOR AND SMOKE COMING FROM TIRE. INSPECTED NR 3 AND 4 WHEEL ASSY BRAKE AND WHEEL SPEED TRANSDUCERS IN REF TO AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,982 hrs · 41,010 cycles

EMERGENCY LIGHT IN FRONT OF 2A BURNED OUT. FLT#5305 RELAMPLED, PN 10-1307-3, PN 24-1411-5.

Part: SENSOR — FAILED (NLG) · airframe 29,388 hrs · 40,188 cycles

LOST NOSE WHEEL STEERING AND BOTH PEDAL AND TILLER DID NOT WORK FOR TAXI BACK. REPLACED NLG WOW SENSOR IAW AMM.

Part: SIGN — MISSING (CABIN) · airframe 28,892 hrs · 39,491 cycles

EMERGENCY EXIT SIGN AT 6A MISSING. (FLT 5304) REPLACED THE EMERGENCY EXIT SIGN AT SEAT 6A.

Part: SERVO — FAILED (RUDDER) · airframe 28,726 hrs · 39,272 cycles

AFTER TAKEOFF, WITH YAW DAMPER ENGAGED, RUDDER WENT HARD LEFT. (FLT 5357) PERFORMED VISUAL INSPECTION AND CHECKED RUDDER SERVO CABLE TENSION, RUDDER SERVO CLUTCH TORQUE FOUND TO BE WITHIN LIMITS. REPLACED RUDDER SERVO IAW AMM, AUTO PILOT OPS CHECKS GOOD AT THIS TIME. PN-622-5734-002 S/N ON-10043 S/N OFF-6528

Part: FIRE WARNING — FALSE ACTIVATION (CARGO BAY) · airframe 28,633 hrs · 39,117 cycles

RECEIVED A WARNING INDICATION FOR THE CARGO SMOKE/FIRE. DISCHARGED EXTINGUISHER. AFTER LANDING AIRPORT FIRE CREW DETERMINED NO FIRE I REPLACED CARGO FIRE BOTTLES IAW AMM.

Part: WIRE — BROKEN (CABIN) · airframe 28,551 hrs · 39,010 cycles

EMERGENCY EXIT SIGN ON OVERHEAD BIN ABOVE SEAT 9B DOES NOT ILLUMINATE. (FLT 6280) REPAIRED BROKEN WIRE.

Part: LIGHT — INOPERATIVE (CASBIN) · airframe 28,507 hrs · 38,944 cycles

ONE FLOOR LEVEL WHITE EMERGENCY LIGHT DOES NOT ILLUMINATE. (FLT 5325) REPLACED ONE WHITE FLOOR EMERGENCY LIGHT ASSEMBLY BETWEEN ROW 3 AND 4.

Part: SEAL — FAILED (CARGO DOOR) · airframe 28,469 hrs · 38,883 cycles

PASSING THROUGH 13,200 FT RECEIVED CABIN ALTITUDE LIGHT TRIPLE CHIME, CABIN WAS NOT PRESSURIZING. (FLT 5516) REPLACED GROUND SERVICE PORT SEAL, CARGO DOOR SEAL AND LEFT ACM IAW AMM.

Part: HYDRAULIC LINE — CHAFED (NR 2 ENGINE) · airframe 27,827 hrs · 37,963 cycles

LOSS OF NR 2 HYDRAULIC FLUID. FLUID LEVEL DROPPED TO 0. (FLT 5397) ENGINE DRIVEN HYDRAULIC PUMP PRESSURE LINE CHAFED. REPAIRED IN REFERENCE TO MM.

Part: CONNECTOR — UNSECURE (RT MLG) · airframe 27,474 hrs · 37,506 cycles

LANDING GEAR DOESN'T RAISE WITHOUT PRESSING THE DOWN LOCK RELEASE BUTTON. (FLT 1302) TIGHTENED RIGHT MAIN LANDING GEAR CONNECTOR.

Part: SELECTOR — FAILED (COCKPIT) · airframe 27,474 hrs · 37,506 cycles

SELECTED GEARS DOWN AND ALL 3 GEARS FAILED TO GO DOWN. (FLT 6263) REPLACED LANDING GEAR RELAY BOX AND LANDING GEAR SELECTOR HANDLE. P/N 120-61110-001, S/N OFF 120353 AND P/N 120-38594-501, S/N OFF 257613-313.

Part: SEQUENCE VALVE — OUT OF ADJUST (RT MLG DOOR) · airframe 27,288 hrs · 37,250 cycles

RIGHT MAIN GEAR DOORS DID NOT CLOSE ON GEAR ACTUATION. CLOSED NORMALLY AFTER GEAR CYCLED. (FLT 6417) ADJUSTED RIGHT GEAR FORWARD OUTBOARD DOOR SEQUENCE VALVE PLUNGER IN REFERENCE TO EMB 120 MM.

Part: MODULE — FAILED (LANDING GEAR) · airframe 27,248 hrs · 37,192 cycles

RIGHT MAIN GEAR RED DISAGREEMENT LIGHT STAYED ILLUMINATED WHILE LEFT MAIN GEAR CONTINUOUSLY OSSCILATED UP AND DOWN. (FLT 6397) REPLACED LANDING GEAR MODULE ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,248 hrs · 37,192 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 6 IS OUT. (FLT 6318) RELAMPED EMERGENCY LIGHT.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LT MLG) · airframe 27,203 hrs · 37,124 cycles

DURING GEAR RETRACTION, THE RIGHT MAIN GEAR WOULD NOT COME UP, THEN THE LEFT MAIN GEAR STARTED TO GO DOWN, THEN BACK UP. (FLT 5586) ADJUSTED LEFT MAIN GEAR UNLOCK PROX SENSOR POSITION SCREW AND ADJUSTED THE SEQUENCE VALVE AT LEFT MLG OUTBOARD GEAR DOOR PER EMB 120 MM.

Part: SIGNAL COND UNIT — FAILED (LT ENGINE) · airframe 27,203 hrs · 37,124 cycles

LEFT ENGINE NP DROPPED TO 43 PERCENT AFTER GEAR DOWN. (FLT 6243) REPLACED LEFT TORQUE SIGNAL CONDITIONER IN REFERENCE TO EMB 120 MM. P/N 30005-0000-52 S/N OFF 923

Part: CONTROL HANDLE — FAILED (COCKPIT) · airframe 26,664 hrs · 36,362 cycles

LANDING GEAR WILL NOT EXTEND WHEN GEAR HANDLE IS SELECTED DOWN. MUST BE HELD DOWN UNTIL GEAR IS EXTENDED. (FLT 6389) REPLACED LANDING GEAR HANDLE. PN OFF: 120-38594-501 SN OFF: 120294.

Part: RELAY — FAILED (LANDING GEAR) · airframe 26,592 hrs · 36,260 cycles

FLT 5511, ON FIRST GEAR EXTENSION ATTEMPT, ALL LANDING GEAR REMAINED UP. REPLACED LANDING GEAR RELAY BOX ASSEMBLY.

Part: PCU — FAILED (LEFT) · airframe 26,556 hrs · 36,212 cycles

LEFT NP DROPPED BELOW 97 PERCENT. (FLT 5583) REPLACED LEFT ENGINE PCU ASSEMBLY. P/N OFF 782490-46, S/N OFF 900654

Part: GOVERNOR — FAILED (RIGHT) · airframe 26,556 hrs · 36,212 cycles

RIGHT NP OSCILLATED AS LOW AS 97.3 PERCENT. (FLT 1310) REPLACED RIGHT PROPELLER OVERSPEED GOVERNOR.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,145 hrs · 35,624 cycles

EMERGENCY LIGHTS WILL NOT STAY ON IN THE CABIN. (FLT# 5330) REPLACED ALL EMERGENCY LIGHT BATTERY PACKS. P/N D366-04-001 S/N OFF 971/05-91 P/N D366-04-001 S/N OFF 178/08-86 P/N D366-04-001 S/N OFF 1076/06-92.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,922 hrs · 35,328 cycles

FORWARD RED EMERGENCY LIGHT ON FLOOR STRIP IS OUT. (FLT 6297) RELAMPED EMERGENCY LIGHT.

Part: STRINGER — CRACKED (RT WING) · airframe 24,726 hrs · 33,609 cycles

RIGHT WING STRINGER 10 CRACKED AT RIB 5. (C-CHECK) REPAIRED PER SRM.

Part: BEAM — CORRODED (FLOORBOARD) · airframe 24,726 hrs · 33,609 cycles

FLOORBOARD BEAM AFT OF ENTRY IS CORRODED. (C-CHECK) REPAIRED PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,831 hrs · 32,345 cycles

FORWARD EMERGENCY LIGHT INOPERATIVE. (FLT 6568) RELAMPED EMERGENCY LIGHT.

Part: WIRE — BROKEN (CABIN) · airframe 23,129 hrs · 31,351 cycles

ONE RED FLOOR EMERGENCY ESCAPE PATH LIGHT OUT AT SEAT 1A. (FLT 6063) REPAIRED WIRE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,404 hrs · 30,300 cycles

CEILING EMERGENCY LIGHT AT ROW 3 INOP. (FLT 6275) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,120 hrs · 29,895 cycles

EMERGENCY LIGHT AT FORWARD DOOR INOP. (FLT 6299) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,689 hrs · 29,291 cycles

ROW 9 EMERGENCY LIGHT INOP. (FLT 6311) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,389 hrs · 28,838 cycles

EMERGENCY FLOODLIGHT INOP. (FLT 6468) RELAMPED EMERGENCY LIGHT.

Part: WHEEL — CRACKED (LT MLG) · airframe 20,992 hrs · 28,301 cycles

FLT 6099 - LEFT MAIN INNER WHEEL CRACKED. REPLACED BOTH TIRES ON LEFT MAIN GEAR.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 20,938 hrs · 28,241 cycles

FLT 6341 - FLOOR STRIP EMERGENCY LIGHT LENSE MISSING. REPLACED LENSE.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 20,880 hrs · 28,165 cycles

FLT 6185 - FORWARD FLOOR EMERGENCY LIGHT INOP. REPAIRED BROKEN WIRE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 20,583 hrs · 27,755 cycles

FLT 5584 - EMERGENCY EXIT LIGHT AT ROW 6A INOP. RELAMPED.

Part: SIGN — MISSING (EMERGENCY LIGHT) · airframe 20,503 hrs · 27,624 cycles

FLT 5448 - EXIT SIGN ON MCD BULKHEAD MISSING. REPAIRED EXIT SIGN FIXTURE AND INSTALLED A NEW PLACARD EXIT SIGN.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 19,906 hrs · 26,845 cycles

FLT 5458 - OVERHEAD EMERGENCY LIGHT EXIT ROW 9 B AND C INOP. RELAMPED.

Part: SWITCH — MALFUNCTIONED (LT A/C PACK) · airframe 18,546 hrs · 25,069 cycles

FLT 3708 - RECEIVED A "SMOKE" AURAL WARNING WITH SMOKE IN THE CABIN. REPLACED LEFT PACK SELECTOR SWITCH. OPS CHECK GOOD.

Part: PULLEY — CRACKED (RT AILERON) · airframe 18,250 hrs · 24,696 cycles

RIGHT AILERON O/B PULLY IS CRACKED, FOUND AT C-CHECK. REPLACED PULLY IAW EMB 120 MM 27-00-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,250 hrs · 24,696 cycles

LEFT FLOOR SEAT TRACK AFT AREA IS CORRODED, FOUND AT C-CHECK. REPLACED SEAT TRACK AFT PORTION IAW EMB 120 MM 53-01-05.

Part: WIRE — BURNED (COOLING FAN) · airframe 17,992 hrs · 24,350 cycles

FLT 5522 - SMOKE IN THE FLIGHT DECK AND CABIN WITH LEFT PACK ON. REPLACED RCCB, WIRE W206-0051-10 AND LEFT GROUND COOLING FAN. CHECKS GOOD.

Part: WIRE — DAMAGED (GROUND FAN) · airframe 17,857 hrs · 24,173 cycles

FOUND RCCB FOR LEFT GROUND FAN WITH DAMAGED WIRES. REPAIRED WIRES AND REPLACED RCCB IAW 24-34-01. GROUND FAN OPS CHECKS GOOD.

Part: CONNECTOR — DISCONNECTED (ELT) · airframe 17,439 hrs · 23,620 cycles

ELT TOGGLE SWITCH HAS A RED LIGHT BLINKING. RECONNECTED ELT CONNECTOR IAW MM 25-61-03. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 15,508 hrs · 20,995 cycles

EMERGENCY EXIT LIGHTS IN ROW 9 INOP. REPLACED AFT ELBP. OPERATIONAL CHECKS GOOD.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 15,334 hrs · 20,803 cycles

BOTH FORWARD RED EMERGENCY LIGHTS ARE INOP. RELAMPED BOTH FORWARD RED EMERGENCY LIGHTS. OPERATIONAL CHECKS GOOD, PN: DL3071BPZ.

Part: SIGN — MISSING (CABIN) · airframe 15,274 hrs · 20,718 cycles

EXIT SIGN PORTION OF EMERGENCY EXIT SIGN AT LOWER MAIN CABIN DOOR IS MISSING. REPLACED EMERGENCY EXIT SIGN AT LOWER MAIN CABIN DOOR. OPERATIONAL CHECKS GOOD IAW 33-00-00.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 14,806 hrs · 20,081 cycles

AILERONS WERE EXTREMELY STIFF TO MOVE BOTH LEFT AND RIGHT AFTER TAKEOFF. REPLACED APP 65. OPERATIONAL CHECKS GOOD.

Part: SERVO — MALFUNCTIONED (RUDDER TRIM) · airframe 14,430 hrs · 19,590 cycles

WITH AUTOPILOT ENGAGED RUDDER TRIM GETS STICK WHEN TRIMING LEFT OR NOSE RIGHT RUDDER TRIM. REPLACED RUDDER SERVO IAW MM 22-10-05. OPERATIONAL TESTS GOOD, PN 622-5734-002, SN ON 1G7X SN OFF 8027.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 14,279 hrs · 19,386 cycles

AFT EMERGENCY LIGHTS INOP. REPLACED AFT EMERGENCY BATTERY. OPERATIONAL CHECKS GOOD IAW 33-50-02.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 13,899 hrs · 18,917 cycles

ONE RED FLOOR LEVEL EMERGENCY EXIT LIGHT INOP. RELAMPED FLOOR LEVEL RED EMERGENCY LIGHT, OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (RUDDER) · airframe 13,372 hrs · 18,191 cycles

RT RUDDER JAMMED ON TAKEOFF. REPLACED BLUE SYSTEM ACTUATOR IAW MM 27-22-02. OPERATIONAL CHECK GOOD.

Part: ACM — SMOKE (ACM BAY) · airframe 13,134 hrs · 17,903 cycles

"AFTER SHUT DOWN, POSITIONED PACK FROM LOW TO NORM, OVERWHELMING SMELL OF SMOKE IN COCKPIT. REMOVED AND REPLACED ACM (TURBINE). OPERATIONAL CHECK GOOD.

Part: ACTUATOR — JAMMED (RUDDER PEDAL) · airframe 11,596 hrs · 15,848 cycles

DURING CLIMBOUT BOTH, CAPTAIN AND FIRST OFFICER'S, RIGHT RUDDER PEDAL WAS JAMMED. REMOVED AND REPLACED BLUE SYSTEM ACTUATOR ON RUDDER IAW MM 27-22-02. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB) · airframe 10,967 hrs · 14,985 cycles

INFLIGHT AND ON APPROACH RECEIVED FLAP CONTROL FAULT. REPLACED HSTCU AS REQUIRED PER CRJ MM 27-41-01. OPERATIONAL CHECK GOOD.

Part: LEVER — MALFUNCTIONED (FLAP SELECTOR) · airframe 10,947 hrs · 14,961 cycles

FLAP CONTROL FAULT DURING FLIGHT. REPLACED FLAP CONTROL HANDLE. OPERATIONAL CHECK GOOD.

Part: HANDSET — SMOKE (CABIN) · airframe 10,947 hrs · 14,961 cycles

SMOKE FROM FLIGHT ATTENDANT`S HANDSET. REMOVED AND REPLACED FLIGHT ATTENDANT'S HANDSET.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 10,578 hrs · 14,428 cycles

EMERGENCY LIGHTS WILL NOT STAY ILLUMINATED DURING TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW 33-50-01. OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (E/E BAY) · airframe 10,469 hrs · 14,278 cycles

AP DISCONNECTED, ASSOCIATED WITH -FD- ANNUNCIATOR ON CAPTAIN'S EADI AND -ERRATIC BEHAVIOR- FROM F/O'S FLIGHT DIRECTOR DISPLAY, IT DISCONNECTED WHILE AP WAS ON F/O'S COMPUTER. INSTALLED SERVICEABLE AHRS COMPUTER ON CAPTAINS SIDE. AUTOPILOT AND AHRS OPS CHECK GOOD PER 34-21-00.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 10,398 hrs · 14,175 cycles

CAPTAIN'S AUTOPILOT DISENGAGES DUE TO FD FLAG. REMOVED AND REPLACED NR 1 & 2 AUTOPILOT COMPUTERS.

Part: WIRE — CHAFED (AUTOPILOT) · airframe 10,335 hrs · 14,090 cycles

DURING AUTO PILOT FIRST FLIGHT OF THE DAY CHECKS, THE FIRST OFFICER'S AUTO PILOT DISCONNECTS ITSELF DURING TEST. INSPECTED AND FOUND CHAFED WIRE. REPAIRED WIRE AS REQUIRED. OPS CHECK GOOD, REPOSITIONED WIRING.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 10,335 hrs · 14,090 cycles

EMERGENCY LIGHT OUT ON FLOOR STRIP. REMOVED AND REPLACED LIGHT BULB ON EMERGENCY LIGHT FLOOR STRIP.

Part: CIRCUIT CARD — FAILED (RUDDER TRIM) · airframe 10,304 hrs · 14,047 cycles

RUDDER TRIM WHEEL, IN CLIMB AND CRUISE, VIBRATES AND FEELS RATCHETY. RETENSIONED RUDDER TRIM CABLE CIRCUIT AS REQUIRED REFERENCING MM 27-00-01 AND COMPLETED RII CARD 27-314. OPS CHECK GOOD.

Part: CONTROL CABLE — DAMAGED (RUDDER TRIM) · airframe 9,941 hrs · 13,594 cycles

DURING FLIGHT RUDDER TRIM JAMMED AND WOULD NOT TURN LEFT OR RIGHT. REMOVED AND REPLACED FORWARD RUDDER TRIM CABLES WITH NEW SERVICEABLE CABLES AND TENSIONED IAW EMB 120 MM 27-00-01.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 9,816 hrs · 13,435 cycles

FORWARD SECTION OF EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED FORWARD ELBP. OPS CHECKS GOOD.

Part: SMOKE — DETECTED (COCKPIT) · airframe 9,595 hrs · 13,151 cycles

ON THE GROUND, CABIN AND COCKPIT FILLED UP WITH SMOKE WITH APU RUNNING. RAN BOTH PACKS INDEPENDANTLY, NO SMOKE NOTED. RAN BOTH PACKS IN MAN AND AUTO, NO SMOKE. PACKS OPERATE NORMALLY.

Part: SERVO — MALFUNCTIONED (RUDDER) · airframe 9,551 hrs · 13,099 cycles

STICKING IN RUDDER PEDALS. REPLACED RUDDER SERVO IAW MM 22-10-05. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,199 hrs · 12,609 cycles

EMERGENCY EXIT ROW 6C LIGHT OUT. INSTALLED SERVICEABLE BULB AT 6C EMERGENCY EXIT OVERHEAD LIGHT. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,168 hrs · 12,566 cycles

EMERGENCY EXIT OVERHEAD LIGHT INOP. REPLACED BULB FOR RIGHT EMERGENCY LIGHT EXIT OVERHEAD. OPS CHECK GOOD.

Part: ANGLE — CRACKED (RT NACELLE) · airframe 7,695 hrs · 10,719 cycles

ANGLE ON FIRE WALL FWD OF RT HYDRAULIC PACKAGE CRACKED JUST ABOVE GROUND SERVICE PORTS. DISCOVERED DURING C-CHECK. FABRICATED REPAIR, STOP DRILLED CRACK, AND INSTALLED REPAIR IAW EMB SRM 51-70-06 & 51-40-02.

Part: FRAME — CRACKED (LT NACELLE) · airframe 7,695 hrs · 10,719 cycles

LT OB NACELLE 1/2 FRAME CRACKED AT RIVET AT APPROX FRAME 18. DISCOVERED DURING C-CHECK. FABRICATED AND INSTALLED DOUBLER OVER CRACK IAW EMB120 SRM 51-00-00 AND 51-40-02.

Part: FRAME — CRACKED (RT NACELLE) · airframe 7,695 hrs · 10,719 cycles

RT NACELLE OB SIDE 1/2 FRAME AT APPROX FRAME 18 IS CRACKED AT RIVET. DISCOVERED DURING C-CHECK. STOP-DRILLED CRACK AND INSTALLED A REPAIR DOUBLER ON FRAME IAW EMB SRM 51-70-05 AND 51-40-02.

Part: FRAME — CRACKED (LT NACELLE) · airframe 7,695 hrs · 10,719 cycles

LT NACELLE IB SIDE 1/2 FRAME AT APPROX FRAME 18 IS CRACKED AT RIVET. DISCOVERED DURING C-CHECK. FABRICATED AND INSTALLED DOUBLER TO CRACKED AREA IAW EMB SRM 51-00-00 AND 51-40-02.

Part: FRAME — CRACKED (RT NACELLE) · airframe 7,695 hrs · 10,719 cycles

RT NACELLE IB SIDE 1/2 FRAME AT APPROX FRAME 18 IS CRACKED AT RIVET. DISCOVERED DURING C-CHECK. FABRICATED AND INSTALLED DOUBLER TO CRACKED AREA IAW EMB SRM 51-00-00 AND 51-40-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 7,695 hrs · 10,719 cycles

LEFT AND RIGHT SIDES OF ANGLES AT FRAME 13 BELOW JUMPSEAT CUTOUT ARE CRACKED. DISCOVERED DURING C-CHECK. FABRICATED AND INSTALLED IB & OB SIDE DOUBLERS ON LT & RT FRAME 13. CRACKS STOP-DRILLED IAW SRM 51-70-05 AND 51-40-02.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 7,695 hrs · 10,719 cycles

AFT, MIDDLE BUTT STRAP HAS CORROSION. DISCOVERED DURING C-CHECK. REMOVED AND REPLACED BUTT STRAP IAW EMB SRM 51-40-02.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 7,624 hrs · 10,631 cycles

EMERGENCY LIGHTS AFT OF ROW 7 ARE INOP. REPLACED BATTERY PACK. OPS CHECKS GOOD.

Part: LEAD — DEFECTIVE (RT PROPELLER) · airframe 7,187 hrs · 10,097 cycles

RIGHT PROPELLER DEICE FAILED IN FLIGHT ON TIMERS 1 AND 2. RETURNED TO SLC. REMOVED AND REPLACED FULL SET OF DEICE LEADS ON RIGHT PROP IAW MM 30-60-00. OPS CHECKS GOOD.

Part: SWITCH — OUT OF ADJUST (FUEL DOOR) · airframe 6,362 hrs · 9,083 cycles

SERVICE DOOR LIGHT INTERMITTENT ON TAKEOFF ROLL. ADJUSTED FUEL SERVICE DOOR SWITCHES. OPS CHECK GOOD.

Part: FASTENER — LOOSE (FUEL PANEL) · airframe 6,035 hrs · 8,698 cycles

ABORTED 2 TAKEOFFS FOR FLICKERING DOOR LIGHT, NO CHIME. TAXIED BACK. ONE FASTENER ON FUEL DOOR WAS LOOSE. RESECURED FUEL PANEL DOORS AS NEEDED.

Part: RELAY — FAILED (ELECTRICAL SYS) · airframe 5,618 hrs · 8,129 cycles

NR 2 INVERTER INOP LIGHT ILLUMINATED INFLIGHT, FAILED RESET. REPLACED AC DISABLE/TRANSFER RELAY K0002. OPS CHECK GOOD.

Part: DOOR — UNLATCHED (SERVICE DOOR) · airframe 4,580 hrs · 6,554 cycles

SERVICE DOOR LIGHT CAME ON TAKEOFF ROLL. FOUND OUTBOARD FORWARD THUMB LATCH OPEN. SECURED LATCH. OPS CHECK GOOD.

Part: FUEL DOOR — UNLATCHED (RT WING) · airframe 4,396 hrs · 6,258 cycles

ABORTED TAKEOFF DUE TO DOOR WARNING LIGHT (SERVICE DOOR). FOUND OUTBOARD FUEL DOOR LATCH OPEN. SECURED. GROUND CHECKS GOOD.

Part: RUDDER — VIBRATION (TAIL) · airframe 4,173 hrs · 5,907 cycles

RUDDER HAS A VIBRATION WITH YAW AND/OR RUDDER ON AND OFF. SEEMS TO LESSEN AS RUDDER TRIM APPROACHED ZERO. INSPECTED RUDDER AND RUDDER TRIM IAW EMB 120 MM 27-21-00 PG 601. NO DEFECTS NOTED. AIRCRAFT IS OK FOR RETURN TO SERVICE. ALL PANELS ARE CLOSED.

Part: HYDRAULIC LINE — CHAFED (HYD SYSTEM) · airframe 4,173 hrs · 5,907 cycles

ON APPROACH RECIEVED A GREEN (LEFT) SYTEM LOW LEVEL LIGHT GAUGE SHOWED TOP OF YELLOW ARC. A FEW MINUTES LATER RECEIVED A LOW PRESSURE LIGHT. THEN A FEW MINUTES LATER RECEIVED A MAIN PUMP LOW PRESSURE LIGHT WITH THE ELEC HYDRAULIC PUMP ON LIGHT. THE HYDRAULIC FLUID LEVEL GAUGE DID SHOW A SLOW DECREASE IN FLUID LEVEL THE ENTIRE TIME. LANDED NORMALLY WITH GAUGE SHOWING IN MIDDLE OF YELLOW ARC. ELEC PUMP RAN EMTPY APPROXIMATELY 5 MINUTES AFTER LANDING. TROUBLESHOT SYSTEM FOR LEAKS. FOUND CHAFED LINE AT GREEN HYD SYTEM MAIN ENGINE DRIVEN PUMP PRESSURE LINE. REMOVED AND REPAIRED LINE TO SERVICEABLE CONDITION. OPS CHECK GOOD. NO LEAKS NOTED. ALL HYDRAULIC SYSTEMS AND EQUIPMENT OPS CHECK GOOD.

Part: HANDLE — FAILED (TE FLAPS) · airframe 3,716 hrs · 5,266 cycles

WHEN FLAPS SELECTED TO 15 DEGREES DURING APPROACH, FLAP SELECTOR HANDLE DID NOT DROP FULLY INTO DETENT. FLAPS DID NOT MOVE. REPLACED FLAP SELECTOR HANDLE PER MM 27-50-00 OPS CHECK GOOD. PN ON 120-42642-507 SN ON 148478-304 SN OFF 120336

Part: SWITCH — FAILED (RT WING)

DURING CLIMB-OUT, MIDDLE RIGHT WING LIGHT ON THE LEADING EDGE OVERHEAD ICE PANEL ILLUMINATED. RETURNED TO SEA. REMOVED AND REPLACED RIGHT WING MIDDLE DE-ICE PRESSURE SWITCH IAW MM 301005. OPS CK GOOD, SN ON: 0115 SN OFF: 0497.