N271YV

Part: PROXIMITY SENSOR — OUT OF ADJUST (LT MLG) · airframe 43,666 hrs · 59,242 cycles

ON TAKEOFF THE LT MLG WOULD NOT RETRACT. FLT 5449 ADJUSTED LT MLG UPLOCK PROX SENSOR. SWUNG GEAR SEVERAL TIMES. NO FURTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,314 hrs · 58,828 cycles

EMERGENCY LIGHT IN CEILING ABOVE ROW 2 IS BURNED OUT. FLT#5315 RELAMPED.

Part: PROXIMITY SENSOR — OUT OF ADJUST (RT MLG) · airframe 43,244 hrs · 58,744 cycles

RT MAIN GEAR SHOWS DISAGREEMENT ON RED GREEN LIGHT ON "A" SYSTEM ON GROUND. FLT#7388 ADJUSTED PROXIMITY SENSOR. COULD NOT DUPLICATE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,134 hrs · 58,617 cycles

MIDDLE OVERHEAD EMERGENCY LIGHT BURNED OUT. FLT#7402 RELAMPED.

Part: LATCH — LOOSE (NLG DOOR) · airframe 43,084 hrs · 58,557 cycles

AFTER BRINGING GEAR UP FELT A VIBRATION FROM THE NOSE. FLT#7409 SECURED LATCH ON LT NG DOOR. RAN DOOR OPEN & CLOSED MULTIPLE TIMES, DOOR STAYED LATCHED.

Part: WIRE — BROKEN (CABIN) · airframe 42,245 hrs · 57,537 cycles

EMERGENCY LIGHT IN ROW 9 ON THE LEFT SIDE DOES NOT ILLUMINATE. (FLT 5315) REPAIRED BROKEN WIRES FOR WHITE EMERGENCY FLOOR LIGHT AT ROW 9, IAW WDM.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 42,072 hrs · 57,331 cycles

STRONG SMELL COMING FROM LEFT VENT TO SMELL GOES AWAY WITH LEFT RECIRCULATING FAN OFF. (FLT 7779) REPLACED FAN IAW AMM, P/N: AE1209AA0 SNON: 00520 SNOFF: 214

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,874 hrs · 57,107 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 6 IS BURNED OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,751 hrs · 56,969 cycles

WHITE OVERHEAD EMERGENCY LIGHT AT ROW 9 IS OUT. (FLT 6212) RELAMPED EMERGENCY LIGHT.

Part: HYDRAULIC LINE — FAILED (RT MLG) · airframe 41,704 hrs · 56,905 cycles

AFTER SELECTING LANDING GEAR DOWN, GREEN HYDRAULIC SYSTEM RESERVOIR RAPIDLY WENT EMPTY AND PRESSURE WENT TO ZERO. (FLT 5356) REPLACED THE RIGHT GEAR OUTER DOOR HYDRAULIC ACTUATOR UP LINE IN REFERENCE TO CRJ AMM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,556 hrs · 56,734 cycles

CABIN FLOOR SUPPORT T JUST AFT OF PASSENGER DOOR CUTOUT HAS CORROSION. (C-CHECK) REPLACED CABIN FLOOR SUPPORT T JUST AFT OF PASSENGER DOOR CUTOUT IN REFERENCE TO SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,556 hrs · 56,734 cycles

FUSELAGE FRAME 13 HAS TWO CRACKS AT UPPER DV WINDOW SEAL HEIGHT. (C-CHECK) REPAIRED FUSELAGE FRAME 13 UPPER DV WINDOW SEAL HEIGHT IN REFERENCE TO EMB ETD AND EMB SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,534 hrs · 56,709 cycles

PASSENGER DOOR ENTRY WAY LEFT SIDE OMEGA BEAM AT FRAME 14 HAS CORROSION. (C-CHECK) REPAIRED PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,569 hrs · 55,559 cycles

NR 1 EMERGENCY FLOOR LIGHT AT ROW 8 IS OUT. (FLT 7804) RELAMPED EMERGENCY LIGHT.

Part: ALTIMETER — STICKS (COCKPIT) · airframe 40,366 hrs · 55,307 cycles

FIRST OFFICER'S ALTIMETER STICKS AND STAYS AT VARIOUS INCORRECT ALTITUDES. (FLT 7812) REPLACED FIRST OFFICER'S ALTIMETER IN REFERENCE TO AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,496 hrs · 54,190 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 1 IS OUT. (FLT 6358) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,496 hrs · 54,190 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 6 IS OUT. (FLT 5112) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,496 hrs · 54,190 cycles

AFT EMERGENCY LIGHTS ARE OUT. (FLT 5352) REPLACED AFT EMERGENCY LIGHTS BATTERY PACK, P/N D366-04-001, S/N OFF 1043-02/92.

Part: KEELBEAM — CRACKED (RT NACELLE) · airframe 39,332 hrs · 53,978 cycles

RIGHT NACELLE OUTBOARD KEEL BEAM DENTED AND CRACKED WHERE THE GEAR DOOR ACTUATOR ARM CONTACTS. (SERVICE) REPLACED DAMAGED AREA OF KEEL BEAM PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,053 hrs · 53,618 cycles

ROW 8 FLOOR EMERGENCY LIGHTS NOT WORKING. (FLT 7760) RELAMPED EMERGENCY LIGHT.

Part: FASTENER — OUT OF ADJUST (CABIN DOOR) · airframe 38,785 hrs · 53,305 cycles

MAIN CABIN DOOR EXTREMELY HARD TO OPEN. (SERVICE) ADJUSTED HARDWARE, DOOR CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,490 hrs · 52,936 cycles

RIGHT FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: STRINGER — CRACKED (LT WING) · airframe 38,461 hrs · 52,902 cycles

LEFT I/B WING STRINGER NR 10 CRACKED AT 1ST ACCESS HOLE I/B OF NACELLE. (C-CHECK) REPAIRED LEFT I/B WING STRINGER NR 10 AT 1ST ACCESS HOLE I/B OF NACELLE PER SRM.

Part: STRINGER — CRACKED (RT WING) · airframe 38,461 hrs · 52,902 cycles

RIGHT I/B WING NR 8 STRINGER CRACKED BETWEEN RIB NR 8 AND 9. (C-CHECK) REPAIRED STRINGER NR 8 ON THE RIGHT I/B WING BETWEEN RIBS 8 AND 9 PER SRM.

Part: STRINGER — CRACKED (LT WING) · airframe 38,461 hrs · 52,902 cycles

LEFT O/B WING STRINGER NR 10 CRACKED AT RIB NR 16. (C-CHECK) REPAIRED LEFT O/B WING STRINGER 10 AT RIB 16 PER SRM.

Part: A/C PACK — SMOKE (RIGHT) · airframe 38,275 hrs · 52,678 cycles

THE RIGHT PACK SMOKES WHEN USED. (C-CHECK) TROUBLESHOOT AND REPAIR PER AMM.

Part: HYDRAULIC LINE — CRACKED (HYDRAULIC SYS) · airframe 38,257 hrs · 52,647 cycles

EN ROUTE, LOW LEVEL GREEN HYDRAULIC FOLLOWED BY MAIN PUMP OFF. (FLT 6965) REPAIRED HYDRAULIC LINE AT ENGINE DRIVEN PUMP LINE AT ABOVE LEFT ENGINE OIL COOLER PER AMM.

Part: WIRE — NOT SEATED (CABIN) · airframe 37,427 hrs · 51,680 cycles

FLOOR STRIP WHITE EMERGENCY LIGHT AT ROW 8 INOP. (FLT 7737) RE-SEATED WIRES.

Part: FUSE — BLOWN (CABIN) · airframe 37,427 hrs · 51,680 cycles

FLOOR ILLUMINATION EMERGENCY LIGHTS INOP BETWEEN ROWS 6 AND 8. (FLT 6371) REPLACED FUSE XF0033.

Part: DOOR — BINDS (CABIN) · airframe 35,920 hrs · 49,776 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6311) OPERATIONAL CHECK OF DOOR NORMAL.

Part: HMU — MALFUNCTIONED (RT ENGINE) · airframe 35,556 hrs · 49,303 cycles

FLT 6486 - RIGHT ENGINE POWER LOSS. REPLACED HMU.

Part: ANGLE — CORRODED (CARGO DOORWAY) · airframe 35,314 hrs · 49,011 cycles

C-CHECK, MCD ENTRANCE LOWER THRESHOLD ANGLE CORRODED. REPLACED ANGLE.

Part: DOWNLOCK SENSOR — INOPERATIVE (MLG) · airframe 34,798 hrs · 48,365 cycles

FLT 5752 - GEAR DID NOT EXTEND WHEN COMMANDED. REPLACED RIGHT MLG DOWN LOCK SENSORS AND SWUNG GEAR.

Part: SUPPORT — BENT (AILERON SYS) · airframe 34,644 hrs · 48,173 cycles

FLT 5790 - AILERONS BINDING. REPLACED BENT RVDT ROD SUPPORT ON AILERON BELLCRANK.

Part: SERVO — BINDING (ELEVATOR) · airframe 34,644 hrs · 48,173 cycles

FLT 5749 - ELEVATOR BINDING. REPLACED NR 1 STICK PUSHER SERVO, PN 622-5734-002, SN ON 3079, SN OFF 3640.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 34,590 hrs · 48,098 cycles

FLT 5527 - FLOOR EMERGENCY LIGHT STRIP FORWARD RED LIGHT INOP. RELAMPED.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 34,514 hrs · 48,005 cycles

ELECTRICAL SMOKE SMELL IN COCKPIT CORRESPONDING TO AVIDYNE FLIGHTMAX DISPLAY GOING BLANK. PULLED C/B AND SMELL STOPPED. FLT 7782. REPLACED FLIGHTMAX SCREEN. P/N: D98-0000-1-58-G, S/N ON: 1583, S/N OFF: 1562.

Part: STRINGER — DAMAGED (LT NACELLE) · airframe 33,466 hrs · 46,676 cycles

LEFT NACELLE OUTBOARD STRINGER IN WHEEL WELL REQUIRES REPLACEMENT. REPAIRED STRINGER IAW EMB-IC2008-120/03069.

Part: WINDOW — CRACKED (COCKPIT) · airframe 32,934 hrs · 46,003 cycles

FLT 5510 - COCKPIT LEFT SIDE WINDOW IS CRACKED. REPLACED SIDE WINDOW IAW MM 56-11-01.

Part: STOP FITTING — BINDING (PAX DOOR) · airframe 31,781 hrs · 44,425 cycles

FLT 5477 - MAIN CABIN DOOR WILL NOT OPEN. REPLACED TOP AFT STOP BOLT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,747 hrs · 44,379 cycles

FUSELAGE FRAME IS CRACKED FORWARD OF INSTRUMENT PANEL BELOW CAPTAINS WINDSCREEN, DISCOVERED AT C-CHECK. REPLACED FUSELAGE FRAME BELOW CAPTAINS WINDSCREEN IAW SRM 120 51-10-02 PG 3 SEC 3A.

Part: COUNTERWEIGHT — MIGRATED (LT AILERON) · airframe 31,747 hrs · 44,379 cycles

LEFT AILERON OUTBOARD LEAD WEIGHT HAS MIGRATED OUT DUE TO CORROSION AND IS RUBBING ON BEARING SUPPORT, DISCOVERED AT C-CHECK. REPLACED LEFT AILERON LEAD WEIGHT IAW EMB 120 MM 27-00-00 AND 51-61-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,747 hrs · 44,379 cycles

LEFT SIDEWALL FORWARD SEAT TRACK IS CORRODED, DISCOVERED AT C-CHECK. REPLACED THE LEFT SIDEWALL SEAT TRACK IAW EMB SERVICE LETTER EST-186/96 AND MM 20-10-03.

Part: FRAME — CRACKED (CARGO DOOR) · airframe 31,747 hrs · 44,379 cycles

CARGO DOOR FORWARD SIDE FRAME HAS CRACK ON TOP CORNER, DISCOVERED AT C-CHECK. REPLACED FRAME IAW SRM 51-10-02.

Part: DOOR FRAME — CRACKED · airframe 31,747 hrs · 44,379 cycles

PAX DOOR FORWARD SIDE OF INTERNAL FRAME IS CRACKED, DISCOVERED AT C-CHECK. REPAIRED PAX DOOR INTERNAL FRAME IAW SRM 52-10-02 FIG 203 PG 208.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,747 hrs · 44,379 cycles

RIGHT SIDEWALL FORWARD SEAT TRACK IS CORRODED, DISCOVERED AT C-CHECK. SPLICED IN A NEW SECTION OF TRACK IAW EMB SERVICE LETTER EST-186/96 AND MM 20-10-03.

Part: TORQUE TUBE — CORRODED (MAIN PAX) · airframe 31,747 hrs · 44,379 cycles

PAX DOOR INTERCONNECT TORQUE TUBE INBOARD BEARING BOSS IS CORRODED, DISCOVERED AT C-CHECK. REPLACED PAX DOOR INTERCONNECT TORQUE TUBE BEARING BOSS IAW EMB 120 MM 52-11-00.

Part: STRINGER — CRACKED (RT WING) · airframe 31,747 hrs · 44,379 cycles

RIGHT FORWARD STRINGER IN NR 1 FUEL BAY OF RIGHT WING IS CRACKED, DISCOVERED AT C-CHECK. REPAIRED RIGHT FORWARD STRINGER IN NR 1 FUEL BAY IAW EMB 120 SRM 57-20-03 FIG 202.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 31,747 hrs · 44,379 cycles

PAX DOOR INTERNAL STRUCTURE CRACKED AT FORWARD NR 4 STOP, DISCOVERED AT C-CHECK. REPAIRED INTERNAL PAX DOOR STRUCTURED STOP IAW SRM 52-10-02 FIG 203 PG 208.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,119 hrs · 43,590 cycles

LEFT HYDRAULIC BAY OUTBOARD FRAME HAS A CRACK IN IT, DISCOVERED DURING SERVICE CHECK INSPECTION. REPLACED OUTBOARD FRAME IAW EMB SRM 51-40-02.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 30,922 hrs · 43,365 cycles

CO PILOT'S WINDSHIELD SHATTERED AFTER THE LANDING ROLL. REPLACED FIRST OFFICER'S WINDSHIELD IAW EMB 120 AMM REF 56-10-01, P/N NP-151311-2, S/N OFF 03119H2956.

Part: AUTOPILOT SYS — OVERHEATED · airframe 30,241 hrs · 42,533 cycles

(TRIM FAIL) WARNING AND TRIM LIGHT ON AUTOPILOT PANEL ILLUMINATE ON CLIMB WITH AUTOPILOT ENGAGED ON FIRST OFFICER'S SIDE. REPLACED AUTOPILOT TRANSFER BOX DUE TO OVERHEATED AND CORRODED PINS ON CONNECTER. OPERATIONAL CHECKS GOOD.

Part: ACTUATOR — MALFUNCTIONED (ELEVATOR TAB) · airframe 29,481 hrs · 41,554 cycles

ON CLIMB-OUT WITH AUTOPILOT ENGAGED, HAD TRIM FAIL AURAL WARNING AND AUTOPILOT DISENGAGED. BOTH CAPT AND FO EXPERIENCED SPRINGBACK IN THE TRIM WHEEL. REPLACED LEFT AND RIGHT ELEVATOR TRIM TAB ACTUATORS IAW MM 27-32-02. OPERATIONAL CHECKS GOOD, LEFT SN OFF 302388.

Part: SELECTOR — MALFUNCTIONED (TE FLAPS) · airframe 27,989 hrs · 39,217 cycles

ANNUNCIATOR "FLAPS TOO LOW" SOUNDS ON SHORT FINAL WITH FLAPS. REPLACED FLAP HANDLE IAW MM 27-50-00. OPERATIONAL CHECK GOOD.

Part: CONTACTOR — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 27,730 hrs · 38,813 cycles

EMERGENCY LIGHTS STAY ON AFTER FA'S TEST. REPLACED EMERGENCY BUSS CONTACTOR NR 2 K0519. OPERATIONAL CHECK GOOD.

Part: SENSOR — OVERHEATED (PITOT HEAT) · airframe 26,989 hrs · 37,699 cycles

DURING FLIGHT STRONG ELECTRICAL BURNING ODOR NOTED BY BOTH CREW MEMBERS, ON GROUND IN LAX ODOR SEEMS TO BE ISOLATED TO COCKPIT AREA AND AUX PITOT STATIC HEAT IS NOW INOPERATIVE. INSTALLED NEW OVER CURRENT SENSOR IAW MM 30-33-00. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAP) · airframe 26,737 hrs · 37,321 cycles

FLAPS NACELLE DISAGREEMENT. REPLACED LEFT NACELLE ACTUATOR PER MM 27-50-00. OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 26,191 hrs · 36,502 cycles

FLOOR EMERGENCY LIGHT AT FORWARD END INOPERATIVE. REPAIRED BROKEN WIRE ON FORWARD (RED) FLOOR EMERGENCY LIGHT, OPERATIONAL CHECK GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (ELEVATOR) · airframe 25,554 hrs · 35,497 cycles

ON FFOD CHECKS NO TRIM AURAL WARNING. REPAIRED WIRING AT ELEVATOR TRIM PROX SENSORS AND ADJUSTED PER MM. OPERATIONAL CHECK GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,290 hrs · 35,120 cycles

LEFT AFT FLOOR SEAT TRACK CORRODED, MARKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED LEFT AFT FLOOR SEAT TRACK AS NEEDED.

Part: FRAME — CRACKED (RT NACELLE) · airframe 25,309 hrs · 35,149 cycles

RT NACELLE FRAME NR 1 CRACKED INBOARD AND OUTBOARD AT TORSION BAR MOUNTS. DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT NACELLE FRAME IAW 120 SB 120-54-0036 AND RII. PART II COMPLIED WITH.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,290 hrs · 35,120 cycles

RIGHT AFT SIDEWALL SEAT TRACK CORRODED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED RIGHT AFT SIDEWALL SEAT TRACK AS NEEDED.

Part: RIB — CRACKED (LT WING LE) · airframe 25,309 hrs · 35,149 cycles

LT INBOARD LEADING EDGE RIB HAS A SMALL CRACK. DISCOVERED DURING C-CHECK INSPECTION. DOUBLER REINFORCEMENT ADDED AT AFFECTED AREA OF LT LEADING EDGE RIB IAW EMB120 SRM 51-10-02 PG 2 SEC 2B.

Part: SUPPORT — DAMAGED (LT MLG WW) · airframe 25,309 hrs · 35,149 cycles

CRACKED VERTICAL SUPPORT ON INBOARD SIDE OF LEFT WHEEL WELL WHERE ENGINE CABLES RUN THROUGH. REPLACED VERTICAL SUPPORT AT INBOARD SIDE OF LEFT NACELLE IAW SRM 120 51-10-02 PG 2 SEC 2B.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 25,309 hrs · 35,149 cycles

RIGHT HYDRAULIC RESERVOIR LOWER SUPPORT CHANNEL CRACKED AT INBOARD END. DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT HYDRAULIC RESERVOIR LOWER SUPPORT CHANNEL AT INBOARD IAW EMB120 SRM 51-10-02 SEC 2 ITEM C.

Part: SUPPORT — CRACKED (COCKPIT WIDOW) · airframe 25,309 hrs · 35,149 cycles

CAPTAIN'S DV WINDOW AFT SUPPORT CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED SUPPORT BRACKET IAW 120 SRM 51-10-02 PAR 3. P/N: 120-12545-001.

Part: ACTUATOR — FAILED (LT FLAP) · airframe 25,140 hrs · 34,874 cycles

FLAP DISAGREEMENT AFTER RETRACTING FLAPS DURING AFTER-LANDING CHECK. REPLACED LEFT NACELLE ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-00. OPS CHECKS GOOD, LEAK CHECK GOOD.

Part: WARN PANEL — FAULTY (COCKPIT) · airframe 24,992 hrs · 34,639 cycles

STALL WARNING SYSTEM 2 FAILS TO TEST NORMALLY; STALL WARNING LAMP ILLUMINATES, WILL NOT EXTINGUISH ON MAP. REMOVED AND REPLACED STALL WARNING PANEL IAW 27-00-00, OPS CHECK OK. P/N 120-34428-505.

Part: COMPUTER — MALFUNCTIONED (NR 1 AUTOPILOT) · airframe 24,910 hrs · 34,516 cycles

CAPTAIN'S AUTOPILOT WILL CLIMB AND DESCEND 100 FT WHEN IN LEVEL FLIGHT. SWITCHED TO F/O'S AUTOPILOT. NO DISCREPANCIES. COULD NOT DUPLICATE. REPLACED NR 1 APC FOR TROUBLESHOOTING SYSTEM. OPS CHECKS GOOD IAW 22-10-00.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAP) · airframe 24,233 hrs · 33,474 cycles

NACELLE FLAPS DISAGREE WHEN SELECTED UP FROM 45 DEGREES. REMOVED AND REPLACED LEFT NACELLE ACTUATOR IAW EMB 120 MM 27-50-00 RII 27-307. ALL OPS CHECKS GOOD.

Part: COMPUTER — FAILED (STALL WARNING) · airframe 23,464 hrs · 32,280 cycles

LEFT STALL WARNING SYSTEM FAILED INFLIGHT WITH ASSOC WARNING ON MAP, AND RED LIGHT ILLUMINATED ON STALL SYSTEM PANEL. FOLLOWED QRH AND TURNED OFF LEFT STALL SYSTEM. REPLACED NUMBER 1 STALL WARNING COMPUTER. OPS CHECK GOOD.

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 23,061 hrs · 31,655 cycles

ON TAXI OUT, UPON SELECTING FLAPS 15 RECEIVED A CONTROL FAULT. INSTALLED SERVICEABLE FLAP SELECTOR AND FLAP CONTROL UNIT. GROUND OPS CHECK GOOD. P/N: 120-64207-615, S/N OFF: 148978-304, S/N ON: 120237.

Part: RELAY — MALFUNCTIONED (MLG) · airframe 22,804 hrs · 31,266 cycles

GEAR WOULD NOT RETRACT, ONLY THE RED INTRANSIT LIGHTS CAME ON, GEAR STAYED DOWN AND LOCKED. THE HANDLE WOULD MOVE OK BUT THE GEAR DID NOTHING. RETURNED TO PDX. REMOVED AND REPLACED RELAY BOX, CONDUCTED GEAR SWINGS 15 TIMES. ALL CHECKS GOOD IAW EMB 120 MM 32-32-00.

Part: WIRE — CHAFED (LT ELEV TRIM) · airframe 22,703 hrs · 31,115 cycles

AFTER TAKEOFF RECEIVED A TRIM FAIL AURAL WARNING AND THE TRIM FAIL LIGHT ON THE MAP CAME ON AND CONTINUED FOR APPROXIMATELY 5 MINUTES. RETURNED TO LAX. INSPECTED ELEVATOR TRIM WIRING ON TOP OF TAIL. FOUND CHAFED WIRE TO LEFT PROXIMITY SENSOR AND CORRODED CONNECTOR TO RIGHT SENSOR. REPAIRED WIRE AND REPLACED CONNECTORS. OPS CHECK GOOD.

Part: WIRE — DAMAGED (RT STARTER/GEN) · airframe 22,336 hrs · 30,575 cycles

RIGHT MAIN GENERATOR FAILED TO RESET ITSELF ON TAKEOFF ROLL. ABORTED TAKEOFF. REPAIRED WIRE TO RIGHT STARTER/GENERATOR. CLEANED ALL TERMINALS AND CANNON PLUGS. TAXIED ACFT. OPS CHECK GOOD.

Part: ENGINE — POWER LOSS (NR 2) · airframe 22,215 hrs · 30,393 cycles

LARGE SPLIT IN POWER LEVERS ON TAKEOFF ROLL AND AT 100 FT NR 2 NP DROPPED TO ABOUT 50 PERCENT, THE TQ STAYED AT 100 PERCENT. ON DOWNWIND, TQ DROPPED TO 0 PERCENT, NP INCREASED TO 100 PERCENT. WE FEATHERED NR 2 AND RETURNED TO IPL. INSPECTED NR 2 ENG WIRING & CANNON PLUGS. COULD NOT DUPLICATE SQUAWK. REPLACED K0161 RELAY WITH SERVICEABLE UNIT FOR TROUBLESHOOTING. RAN AIRCRAFT. AUTO FEATHER CHECKS GOOD. OPS CHECKS GOOD.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 21,534 hrs · 29,293 cycles

LEFT BRACKET FRAME 12 CRACKED AFT OF PILOT'S DIRECT VISION WINDOW. REPLACED LEFT BRACKET FRAME 12 AFT OF PILOT'S DV WINDOW IAW MM 53-40-02.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 21,534 hrs · 29,293 cycles

RIGHT HYDRAULIC RESERVOIR SUPPORT BRACKET CRACKED. REMOVED AND REPLACED RIGHT HYDRAULIC PACK LOWER SUPPORT BRACKET IAW SRM 51-40-02 AND 51-10-02-3A.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 21,420 hrs · 29,095 cycles

DURING TAKEOFF ROLL, RECEIVED A HIGH SPEED TRIPLE CHIME AND AURAL WARNING. ABORTED TAKEOFF. CYCLED CIRCUIT BREAKER. GROUND OPS CHECK GOOD.

Part: TRANSPONDER — MALFUNCTIONED (E/E BAY) · airframe 21,382 hrs · 29,037 cycles

AFTER TAKEOFF, TRANSPONDER NR 1 REPORTED DIAG WITH NO ASSOCIATED NUMBER. ATC REPORTED NO ALTITUDE READOUT. SWITCHED TO NR 2 TRANSPONDER AND HAD NO REPLY LIGHT OR ALT INFORMATION AS REPORTED BY ATC. RETURNED TO PDX. RERACKED NR 1 TDR94 TRANSPONDER. INSPECTED CONNECTIONS. NO DEFECTS NOTED. OPS CHECKED NR 1 TRANSPONDER OK. REMOVED NR 2 TDR94 AND CAD62 AND CLEANED CONNECTIONS. OPS CHECKED SYSTEM. SYSTEM TESTS GOOD.

Part: BOOT — FAILED (HORIZ STAB) · airframe 20,816 hrs · 28,179 cycles

LEFT AND RIGHT OUTBOARD STAB DEICE BOOTS FAILED INFLIGHT, BOTH TIMERS. REPLACED BAD LEFT STABILIZER DEICE BOOT PER MM 30-10-00. DEICE SYSTEM OPS CHECK GOOD.

Part: BOOT — DAMAGED (HORIZ STAB) · airframe 20,824 hrs · 28,193 cycles

OUTBOARD LEFT AND RIGHT STABILIZER DEICE BOOTS FAILED INFLIGHT, BOTH TIMERS. INSTALLED PATCH ON LEFT OUTBOARD STAB DEICE BOOT. OPS CHECK GOOD.

Part: EEC — MALFUNCTIONED (NR 2 ENGINE) · airframe 19,043 hrs · 25,619 cycles

NUMBER TWO EEC DROPPED OFF LINE (AURAL WARNING, RED EEC LIGHT ILLUMINATED, MANUL LIGHT) DURING TAKEOFF. ABORTED TAKEOFF. NUMBER TWO NP REMAINED AT 80 PERCENT UNTIL EEC WAS TURNED OFF. DEFERRED PER MEL 73-21-1, MC 0179. INSPECTED, CLEANED AND OHMED RIGHT ENGINE EEC SYSTEM. PERFORMED GROUND RUNS WITH NO DEFECTS NOTED. SYSTEM OPS NORMAL AT THIS TIME. PLACARD REMOVED.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 19,043 hrs · 25,619 cycles

ON TAKEOFF FUEL AMBER LIGHT ILLUMINATED ON MAP. OVERHEAD RIGHT SIDE LOW PRESSURE LIGHT ILLUMINATED. BOTH RIGHT FUEL PUMPS CAME ON. LOW PRESSURE LIGHT REMAINED ILLUMINATED. RIGHT FRONT PUMP WILL NOT SHUT OFF. ABORTED TAKEOFF. REPLACED RELAY K0103 AND SECURED WIRES TO RIGHT FRONT FUEL BOOST PUMP SWITCH. CLEANED AND RE-SECURED RIGHT ENGINE FUEL LOW PSI SWITCH CANNON PLUG. OPS CHECK GOOD AT THIS TIME.

Part: WINDSHIELD — MALFUNCTIONED (COCKPIT) · airframe 19,279 hrs · 25,970 cycles

EN ROUTE AT 22,000 FT NOTED SMOKE COMING FROM FORWARD PORTION OF GLARESHIELD. DIVERTED TO LAX. AFTER A DETAILED INSPECTION OF WIRING AND COMPONENTS LOCATED UNDER GLARESHIELD FOUND GROUND WIRE ON LT WINDSHIELD HEATING BLOCK TO HAVE BEEN ARCING AT THE TERMINAL TO LUG ATTACH POINT. REPLACED LUG ON GROUND WIRE (G1). UPON REINSTALLATION ON HEATING BLOCK DISCOVERED HEATING BLOCK TO HAVE BEEN DAMAGED. SECURED GROUND WIRE (G-1) IN HEATING BLOCK AND DEFERRED LT WINDSHIELD HEAT PER MEL 30-40-1. SECURED CB TO PREVENT INADVERTANT OPERATION DEFERRED. 02/05/01 R&R LT WINDSHIELD IAW EMB 120 MM 56-10-01. OPS CHECKS GOOD. 02/12/01 R&R LT WINDSHIELD HEAT RCCB. OPS CHECKS GOOD.

Part: TAIL CONE — OUT OF POSITION (FUSELAGE) · airframe 18,671 hrs · 25,106 cycles

ELEVATOR CONTROL BINDING IN MIDDLE OF THROW. FOUND ELEVATOR CONTACTING RIGHT SIDE OF TAIL CONE AT MID THROW. REPOSITIONED AND SECURED TAIL CONE. CHECKS OK.

Part: WARNING HORN — ACTIVATED (COCKPIT) · airframe 18,457 hrs · 24,797 cycles

DURING TAKE OFF ROLL, TAKE OFF AURAL WARNING ''AUTO FEATHER''. ABORTED TAKEOFF. ON SAME SYSTEM DURING TAXI CHECKED GOOD. REPLACED AUTO FEATHER SYSTEM ARM REALY K0161. OPS CHECKED GOOD ON GROUND RUN.

Part: SWITCH — LOOSE (COCKPIT) · airframe 18,471 hrs · 24,819 cycles

CAPTS TRIM SWITCH ON YOKE LOOSE, CAUSING CIRCUIT BREAKER TO POP. RETURNED TO FIELD. RESECURED SWITCH. OPS CHECK GOOD.

Part: SENSOR — OUT OF ADJ (ELEVATOR TRIM) · airframe 18,289 hrs · 24,594 cycles

ABORTED TAKEOFF ROLL, DUE TO TRIM AURAL WARNING, TRIM WAS SET IN GREEN BAND. ADJUSTED ELEVATOR TRIM PROXIMITY SENSORS IAW EMB 120 MM 27-32-00, OPS CHECKS GOOD.

Part: STRUCTURE — DAMAGED (LT WING) · airframe 18,129 hrs · 24,348 cycles

DAMAGE FOUND ON LEFT WING TIP. OUTBOARD STATIC WICK BRACKET BROKEN AND JAMMED IN LEFT AILERON CAUSING IT NOT TO MOVE. REPAIRED LEFT WING TIP IAW SRM 51-70-02. REPLACED STATIC WICK AND REINSTALLED WING TIP. AILERON OPS CHECKS GOOD.

Part: SWITCH — OUT OF ADJ (CARGO DOOR) · airframe 18,107 hrs · 24,315 cycles

CARGO LIGHT ILLUMINATED ON CLIMBOUT. RETURNED TO FAT. ADJUSTED FORWARD CARGO DOOR MICROSWITCH. OPS CHECKS GOOD.

Part: PROBE — FAILED (RT ENGINE) · airframe 17,748 hrs · 23,814 cycles

NH INDICATIONS VARY WITH EEC OFF FROM 48 - 85 PECENT IN CRUISE. RETURNED TO SFO. REPLACED BOTH NH GAUGE AND NH PROBE ON RIGHT ENGINE. OPS CHECKS GOOD ON ENGINE RUN. NH GAUGE P/N ON: SEDL0C29M, S/N ON: 1321, S/N OFF: 156.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 17,590 hrs · 23,581 cycles

UPON GEAR RETRACTION, RIGHT MAIN GEAR RED LIGHTS REMAINED ILLUMINATED AND VIBRATION WAS FELT FROM NOSE. CYCLED GEAR TWO MORE TIMES TO NO EFFECT AND RETURNED TO MOD. SWUNG GEAR ON JACKS BUT COULD NOT DUPLICATE RIGHT MAIN LIGHTS ON. OPS CHECKS GOOD.

Part: PROXIMITY SWITCH — DIRTY (RT MLG) · airframe 17,550 hrs · 23,521 cycles

LANDING GEAR DISAGREEMENT LIGHT ON RIGHT MAIN AND THE RIGHT ANTISKID SHOWS INOP. RETURNED TO LAX. CLEANED RIGHT LANDING GEAR PROX SWITCHES AND INSPECTED RIGHT BRAKE ANTISKID. PERFORMED OPS CHECK OF LANDING GEAR SWING, OPS CHECKS GOOD.

Part: CONNECTOR — DIRTY (OUTFLOW VALVE)

AIRCRAFT WILL NOT PRESSURIZE IN MANUAL. RETURNED TO PDX. REMOVED AND CLEANED CONNECTIONS AND TUBES ON PNEUMATIC VALVE AND REFERENCE FITTING MANUAL SYSTEM, OPS CHECKS GOOD. VERIFIED AUTO PRESSURIZATION SYSTEM DEFERRED AND MAINTENANCE ACTIONS COMPLIED WITH IAW MEL 21311A.

Part: SWITCH — FAILED (RT MLG)

INFLIGHT UPON GEAR RETRACTION, NEEDED TO USE DN LOCK RELEASE OVERRIDE TO BRING GEAR HANDLE UP. UPON FLAP RETRACTION, TRIPLE CHIME AURAL WARNING FLAP ANNUNCIATED CONTINUIOUSLY. AGAIN WHEN THE AUTO FX SWITCH WAS TURNED OFF, WARNINGS CONTINUED. RETURNED TO PSP. PERFORMED GEAR SWING. FOUND GEAR WOULD NOT SWING WITHOUT OVERRIDE BUTTON. WITH NLG PROX SENSOR SLAVED IN AND TARGETED, GEAR SWINGS OK. REPLACED SENSOR, BUT SWING CHECKS BAD. CHECKED HARNESS WITH A NEW SENSOR AND CHECK OK. CHECKED TARGET THROUGH PROX SENSOR, TARGET NOT USEABLE. REPLACED RIGHT UPLOCK PROXIMITY SWITCH. OPS CHECKS GOOD.

Part: PCU — FAILED (RT ENGINE)

RIGHT ENGINE AUTO FEATHERED ON CLIMB-OUT. RETURNED TO SFO. REMOVED AND REPLACED PCU IAW MM 61-21-00. ALSO, CHANGED TORQUE SIGNAL CONDITIONER. CHANGED RIGHT ENGINE DUE TO OVER-TORQUE.

Part: TIMER — FAILED (LEFT WING DEICE)

MIDDLE LEFT WING LEADING EDGE DEICE BOOT INOP BOTH TIMERS. RETURNED TO PDX. RAN ENGINES AND OPS CHECKS GOOD ON GROUND. COULD NOT DUPLICATE PROBLEM.

Part: ACTUATOR — FAILED (LT MLG)

LEFT MAIN LANDING GEAR WOULD NOT RETRACT. RETURNED TO SMF. REMOVED AND REPLACED LEFT MAIN LANDING GEAR ACTUATOR IAW EMB 120 MM 32-32-10. OPS CHECK GOOD.

Part: RADOME — BIRDSTRIKE (FWD FUSELAGE)

SBA - BIRDSTRIKE ON NOSE DURING APPROACH REPORTED. MAINTENANCE INSPECTED AREA FOR DAMAGE. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: RADOME — DELAMINATED (NOSE)

FAT - EN ROUTE FAT TO MRY, WEATHER RADAR REPORTED PAINTING FALSE RETURNS. WEATHER CONDITIONS EN ROUTE REQUIRED AIRCRAFT TO RETURN TO STATION. MAINTENANCE REPLACED RADOME ASSEMBLY. WEATHER RADAR OPERATIONAL CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (M)

Part: RADOME — BIRD STRIKE (FWD FUSELAGE)

SMF - BIRD STRIKE ON LEFT NOSE AREA REPORTED. MAINTENANCE INSPECTED AREA FOR DAMAGE. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (X)

Part: HI SPEED WARNING — ACTIVATED (COCKPIT)

LAX - HIGH SPEED WARNING ON TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY ON GROUND. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED FOR TEST FLIGHT. NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ENGINE — LOW OIL (LEFT)

SFO - LEFT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED AFTER TAKEOFF. CREW SECURED LEFT ENGINE AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED LEFT ENGINE WITH FOUR QUARTS OIL. LEAK AND OPERATIONAL CHECKS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ENGINE — LOW OIL QTY (LEFT)

FAT - LOW OIL PRESS WARNING ON LEFT ENG ON CLIMB-OUT REPORTED. AIRCRAFT RETURNED TO STATION. MAINTENANCE ADDED FOUR QUARTS OF OIL TO LEFT ENGINE. OIL PRESSURE INDICATION OPERATES NORMAL. INSPECTED ENGINE FOR LEAKS. NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: PRESSURE SWITCH — FAILED (LT ENGINE)

SFO - LEFT FUEL FILTER LIGHT ILLUMINATED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE DEFFERED INDICATING SYSTEM PER MEL 73-33-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY REPLACING LEFT ENGINE FUEL FILTER LIGHT SWITCH. (M)

Part: TRANSDUCER — DIRTY (LANDING GEAR)

FAT - BRAKE WARNING LIGHT ILLUMINATED DURING TAXI ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE UNABLE TO DUPLICATE DISCREPANCY. DEFERRED ANTI-SKID AS PRECAUTION. AIRCRAFT RELEASED FOR SERVICE. MX SUBSEQUENTLY CLEARED DEFERRAL BY INSPECTING AND CLEANING WHEEL SPEED TRANSDUCER CONNECTORS AND MECHANICAL ENGAGEMENTS. (M)

Part: CONTROL CABLE — WORN (RT WING AILERON)

DURING A 1600-HOUR CONTROL CABLE INSPECTION, FOUND RIGHT WING UPPER AILERON CABLE, PN 120-27655-031, WORN WITH BROKEN STRANDS WHERE CABLE PASSES THROUGH NYLON GROMMET ON BOTH INBOARD AND OUTBOARD NACELLE STRUCTURE.

Part: CONTROL CABLE — WORN (LT WING AILERON)

DURING A 1600-HOUR CONTROL CABLE INSPECTION, FOUND LEFT WING LOWER AILERON CABLE, PN 120-27655-007, WORN WITH BROKEN STRANDS WHERE CABLE PASSES THROUGH NYLON GROMMET ON BOTH INBOARD AND OUTBOARD NACELLE STRUCTURE.

Part: CONTROL CABLE — WORN (LT WING AILERON)

DURING A 1600-HOUR CONTROL CABLE INSPECTION, FOUND LEFT WING LOWER AILERON CABLE, PN 120-27655-005, WORN WITH BROKEN STRANDS WHERE CABLE PASSES THROUGH NYLON GROMMET ON BOTH INBOARD AND OUTBOARD NACELLE STRUCTURE.

Part: CONTROL CABLE — WORN (RT WING AILERON)

DURING A 100-HOUR CONTROL CABLE INSPECTION, FOUND RIGHT WING LOWER AILERON CABLE, PN 120-27655-029, WORN WITH BROKEN STRANDS WHERE CABLE PASSES THROUGH NYLON GROMMET ON BOTH INBOARD AND OUTBOARD NACELLE STRUCTURE.