N269UE

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 30,098 hrs · 33,242 cycles

FLAPS HAD RT INBOARD FLAP ASYMMETRY WHEN SET FOR LANDING AND FAILED TO RETRACT AFTER LANDING (RT AND LT INBOARD). RE-RACKED FLAP CONTROL UNIT. PERFORMED FUNCTIONAL CHECK OF FLAP SYSTEM. CYCLED FLAPS SEVERAL TIMES. NO DISCREPANCIES NOTED.

Part: TERMINAL — BROKEN (NR 1 GEN WIRE) · airframe 30,098 hrs · 33,242 cycles

DURING THE TAKEOFF RUN THE NR 1 GEN OFF BUS LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED. ATTEMPTED RESET PER QRH WITH NO SUCCESS. FOUND BROKEN WIRE ON NR 1 GENERATOR. REPLACED WIRE EYELET WITH SERVICEABLE UNIT AND CONNECTED TO NR 1 GENERATOR. RAN RT ENGINE, APPLIED LOAD TO NR 1 GENERATOR AND PARALLELED GCU TO 28.50 VDC. OPS CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 30,056 hrs · 33,167 cycles

CONTROL FAULT ON INBOARD FLAPS AFTER TRYING TO RAISE FLAPS. REMOVED AND REPLACED FLAP CONTROL UNIT. FLAPS FUNCTIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (LT TE FLAPS) · airframe 30,005 hrs · 33,100 cycles

AFTER FLAP RETRACTION ON LANDING, THE INBOARD PAIR OF FLAPS REMAINED AT 25 DEGREES. THERE WERE NO CONTROL FAULTS OR DISAGREEMENT WARNINGS. AFTER RESETTING THE SYSTEM, THE FLAPS RETRACTED. REPLACED LEFT INBOARD FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-00. OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 29,586 hrs · 32,454 cycles

ON TAKEOFF GOT TRIPLE CHIME EEC WARNING. ABORTED TAKEOFF. SUSPECT LEFT EEC THE CULPRIT, LOWER NP THAN RT ON FFOD. INSPECTED CANNON PLUGS AND WIRING FOR CHAFING ON LT ENGINE EEC. RAN ENGINE FOR TRIM CHECK AND TAXIED AIRCRAFT. COULD NOT DUPLICATE. OPS CHECK GOOD. NO DEFECTS NOTED.

Part: DUCT — LEAKING (LT WING) · airframe 29,385 hrs · 32,148 cycles

AT ABOUT 50 KTS ON TAKEOFF ROLL, TRIPLE CHIME DUCT LEAK RED LIGHT ON MAP AND DUCT LEAKAGE ON LEFT SIDE OVERHEAD. ABORTED TAKEOFF. LIGHTS REMAINED ON FOR ONLY 10-15 SECONDS, THEN WENT OUT. INSTALLED SERVICEABLE LEFT WING BLEED LINE. OPS CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (T/E FLAP) · airframe 29,218 hrs · 31,905 cycles

LEFT OUTBOARD FLAP DEPLOYED APPROXIMATELY 3 DEGREES (UNCOMMANDED) WHILE FLAP HANDLE IS IN ZERO POSITION. ANALOG INDICATOR SHOWS ZERO DEGREES. FLAP ON MAP ILLUMINATED, ASYMMETRY ON FLAP PANEL INDICATOR ILLUMINATED. REPLACED LEFT OUTBOARD FLAP ACTUATOR PER EMB 120 27-50-00. OPS CHECKS GOOD.

Part: EEC — MALFUNCTIONED (NR 1 ENGINE) · airframe 29,218 hrs · 31,905 cycles

ABORTED TAKEOFF IN FAT DUE TO LEFT EEC FAILURE. RAN NR 1 ENGINE IAW 71-00-00. RAN WITHIN PARAMETERS. OPS CHECKS GOOD AT THIS TIME. NO OTHER DEFECTS NOTED.

Part: CONNECTOR — DIRTY (LT & RT EEC) · airframe 29,078 hrs · 31,665 cycles

WHILE IN POSITION FOR TAKEOFF, RECEIVED AN AURAL WARNING ENGINE CONTROLS AND MOMENTARY RED EEC LIGHT. CLEANED P1 CONNECTOR OF LEFT AND RIGHT EEC'S. PERFORMED ENGINE RUNS. NO DISCREPANCIES FOUND.

Part: DOOR — DEPARTED (A/C PACK) · airframe 28,753 hrs · 31,178 cycles

RIGHT AIR CONDITIONING PACK DOOR DEPARTED WHILE IN FLIGHT. REPLACED PACK DOOR IAW SRM 120 51-10-02.

Part: SENSOR — CORRODED (ELEVATOR TAB) · airframe 28,734 hrs · 31,148 cycles

TAKEOFF TRIM AURAL WARNING OCCURRED DURING INITIAL PART OF TAKEOFF ROLL. TRIM WAS SET IN THE MIDDLE OF THE GREEN BAND. INSPECTED WIRING AND CLEANED CORROSION AT ELEVATOR TRIM SENSORS. OPERATED SYSTEM, COULD NOT DUPLICATE.

Part: FCU — MALFUNCTIONED (T/E FLAP) · airframe 28,761 hrs · 31,190 cycles

INBOARD FLAPS DID NOT RETRACT AFTER LANDING. REMOVED AND REPLACED FLAP CONTROL UNIT WITH SERVICEABLE. CYCLED FLAPS SEVERAL TIMES. NO DISCREPANCIES NOTED. OPS CHECK GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 28,734 hrs · 31,148 cycles

ABORTED 3 STATIC TAKEOFFS FOR T/O TRIM AURAL WARNING. TRIM SETTING WAS IN GREEN BAND 30 PERCENT TO 35 PERCENT. CYCLED TRIM WHEEL, THEN NORMAL TAKEOFF. TESTED TRIM AURAL WARNING AT VARIOUS SETTINGS. ALL CHECKS GOOD AT THIS TIME.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 28,602 hrs · 30,954 cycles

AURAL TRIM INDICATION WITH TRIM IN THE GREEN ON THE TAKEOFF ROLL. RESET AURAL WARNING COMPUTER. OPS CHECK GOOD.

Part: SEQUENCE VALVE — MALFUNCTIONED (NLG WW) · airframe 28,272 hrs · 30,458 cycles

LANDING GEAR WOULD NOT COME DOWN AFTER SELECTING GEAR LEVER DOWN. ALL RED A & B LIGHTS, EXCEPT LEFT MAIN A LIGHT, STAYED ON. LT MAIN GREEN A LIGHT WAS ALSO ILLUMINATED. ON THE GO-AROUND THE GEAR EXTENDED AND GOT NORMAL GREEN LIGHTS EXCEPT LEFT MAIN A LIGHT REMAINED OFF FOR ABOUT 10 SECONDS. UPDATE 11/5: ON APPROACH SELECTED GEAR DOWN WITH NO RESPONSE. GEAR DOORS REMAINED CLOSED. STARTED TO FOLLOW QRH PROCEDURE, ELECTRICAL OVERRIDE, WHEN GEAR FINALLY CAME DOWN. REMOVED AND REPLACED LANDING GEAR CONTROL BOX WITH SERVICEABLE UNIT. OPS CHECK GOOD. UPDATE: 11/5: REMOVED AND REPLACED SEQUENCE VALVE IN NOSE BAY. SYSTEM OPS CHECK GOOD AS PER EMB MM 32-30-00.

Part: PUMP — DEFECTIVE (RT ENGINE) · airframe 28,168 hrs · 30,302 cycles

DURING CLIMB TO 16000 FT NR 2 ENGINE TORQUE FLUCTUATED THEN RAPIDLY DROPPED TO 11 PERCENT TQ. OTHER ENGINE INDICATIONS WERE NORMAL. PERFORMED PRECAUTIONARY ENGINE SHUT DOWN. REMOVED AND REPLACED RIGHT ENGINE HMU AND FUEL PUMP IAW MM 73-21-00. OPS AND LEAK CHECK GOOD. HMU P/N ON: 3035659 S/N ON: 49502 P/N OFF: 78639040 S/N OFF: M80363, PUMP P/N ON: 5009984C S/N ON: 136 P/N OFF: 3117075-01 S/N OFF: 1940

Part: SWITCH — MALFUNCTIONED (PASSENGER DOOR) · airframe 27,961 hrs · 29,974 cycles

FORWARD DOOR ACTUATOR LT ON IN FLIGHT. LIGHT EXTINGUISHES ON THE GROUND. COULD NOT GET MAIN CABIN DOOR OPEN NORMALLY ON GROUND. USED EMERGENCY OVERRIDE. REMOVED AND REPLACED PASSENGER DOOR SWITCH AT FLIGHT ATTENDANT'S STATION. SYSTEM OPS CHECK GOOD.

Part: VALVE — LEAKING (DEICE SYSTEM) · airframe 27,626 hrs · 29,471 cycles

DURING CLIMB OUT, DUCT LEAK LIGHT ILLUMINATED FOR RIGHT ENGINE. COMPLIED WITH QRH, NO CHANGE. CLOSED BLEEDS, ALSO THE PACKS. THE LIGHT DID NOT EXTINGUISH UNTIL POWER ON THE RIGHT ENGINE WAS PULLED TO FLIGHT IDLE. RETURNED TO MEDFORD. GAINED ACCESS TO ALL DUCT WORK ASSOCIATED WITH RIGHT DUCT LEAK INDICATION SYSTEM. FOUND RIGHT DE-ICE PRESSURE REGULATING VALVE TO BE LEAKING. REPLACED VALVE IAW MM 30-10-06. OPS CHECKS GOOD. PN ON 38E96-6A SN ON RF1918.

Part: TERMINAL — FAILED (WINDSHIELD) · airframe 27,626 hrs · 29,471 cycles

RIGHT WINDSHIELD REPORTED NOT FUNCTIONING & BURN SMELL NOTED IN COCKPIT. FOUND BURNED POWER TERMINAL ON RIGHT WINDSHIELD. REMOVED AND REPLACED RIGHT WINDSHIELD PER MM 56-10-01. REMOVED & REPLACED POWER WIRE PER WM 30-41-00. WINDSHIELD HEAT OPS CHECK GOOD. NP151311-2 SN ON 9914H3022 SN OFF 97219H2979.

Part: RECEPTACLE — MELTED (COFFEEMAKER) · airframe 27,626 hrs · 29,471 cycles

ON CLIMB OUT FROM EUGENE, NOTICED BURNING SMELL LIKE BURNING RUBBER IN FLIGHT DECK. SMELL CONTINUED, COULD NOT ISOLATE. NO VISABLE SMOKE. DIVERTED TO PDX. RAN AIRCRAFT FOR 30 MINUTES, COULD NOT DUPLICATE. FOUND FORWARD COFFEE POT ELECTRICAL RECEPTACLE MELTED. SUSPECT THIS IS ORIGIN. REMOVED AND REPLACED RECEPTACLE IAW CMM 25-00-00. OPS CHECK GOOD.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 26,977 hrs · 28,504 cycles

WHEN SELECTING FLAPS 15 DEGREES AND 25 DEGREES AIRCRAFT ROLLS TO THE RIGHT WITH NO FLAP WARNING INDICATIONS. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR. OPS CHECK GOOD. P/N: 320300-1007, S/N ON: 0706, S/N OFF: 0931.

Part: ACTUATOR — FAULTY (RT FLAP) · airframe 26,897 hrs · 28,381 cycles

EN ROUTE AT FL230 CONTROL FAULT LIGHT ILLUMINATED, WOULD NOT RESET. WEIGHTED FLAP AVERAGE WAS ZERO. LANDED WITH 0 DEGREES FLAPS. FOUND RIGHT HAND OUTBOARD FLAP ACTUATOR EXTERNAL READING AT 820-R. REMOVED AND REPLACED ACTUATOR. OPS CHECKS ACTUATOR IAW 27-50-00 RI I 27-307 P/N ON 3203001007, S/N ON 0315, S/N OFF 0971. REMOVED AND REPLACED FLAP ANNUNCIATOR. OPS CHECK GOOD. P/N ON 3069001005, S/N ON 0037, S/N OFF 0010. FOUND INCORRECT (SOFTWARE LEVEL) FCU INSTALLED, REMOVED AND REPLACED OPS CHECK GOOD WITH NO FAULT FOUND ON GROUND IAW. P/N ON 307500-1007, S/N ON 0092, S/N OFF 0181.

Part: SWITCH — OUT OF ADJ (FUEL DOOR) · airframe 26,798 hrs · 28,237 cycles

SERVICE DOOR LIGHT ILLUMINATED AGAIN ON TAKEOFF ROLL. REMOVED AND REPLACED SERVICE DOOR LIGHT INDICATOR. INSPECTED SERVICE DOOR MICROSWITCH WIRING FOUND TO BE NORMAL. ADJUSTED OUTBOARD FUEL DOOR MICROSWITCH. OPS CHECK GOOD.

Part: REGULATOR VALVE — LEAKING (RT ENGINE) · airframe 26,740 hrs · 28,155 cycles

RIGHT ENGINE INFLIGHT SHUTDOWN DUE TO LOW OIL PRESSURE LIGHT ON MAP AND OIL PRESSURE GAUGE BELOW 40 PSI. REMOVED AND REPLACED RIGHT ENGINE OIL PRESSURE REGULATING VALVE ASSEMBLY IAW P&W MM 72-01-50, PAGE 418. PERFORMED ENGINE RUNS AS REQUIRED. OPS CHECK GOOD. NO LEAKS NOTED. VALVE (P/N ON: 3105732-01) (P/N OFF: 3108007) (HOUSING P/N: 3105735).

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,610 hrs · 27,948 cycles

EXIT ROW SIGNS AT 6A AND 6C DO NOT ILLUMINATE CONTINUOUSLY WHEN EMERGENCY LIGHTS SWITCH IS TURNED ON AT FLIGHT ATTENDNATS PANEL. REPLACED ELBP AT ROW 6. OPS CHECKS GOOD. P/N ON,OFF: D366-04-001, S/N ON: 1137, S/N OFF: 1169.

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 26,071 hrs · 27,192 cycles

CONTROL FAULT WHEN FLAPS WERE SELECTED 45 DEGREES. RERACKED FCU. OPS CHECKS GOOD IAW 27-00-00.

Part: FAN — FAILED (LEFT)

SMOKE IN COCKPIT. RETURNED TO FAT. REPLACED LEFT RECIRCULATION FAN. OPS CHECKED GOOD WITH NO DISCREPANCIES AND NO SMOKE.

Part: PACK — FAILED (RIGHT)

RIGHT PACK FAILED AT 21,600 RESULTING IN LOSS OF CABIN PRESS DUE TO DEFERRED LEFT PACK. RETURNED TO LAS. RUN AND LEAKS CHECK OF RIGHT PACK. BLOWS STRONG, COULD NOT GET IT TO FAIL. OPS CHECKS GOOD.

Part: SWITCH — SHORTED (INST PANEL)

FLT 5271 - TPA-PNS - AIRCRAFT WAS ON APPROACH TO PNS WHEN THE CREW SMELLED AND SAW A SMALL AMOUNT OF SMOKE COMING FROM BEHIND THE CAPT'S INSTRUMENT PANEL. MAINTENANCE DISCOVERED THAT THE CAPT'S PUSH TO CANCEL BUTTON HAD SHORTED OUT. ITEM WAS DEFERRED PER MEL 31-50-3 AND AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE CAPT'S PUSH TO CANCEL SWITCH WAS REMOVED AND REPLACED. (M)

Part: BULB — FAILED (LT EXTERIOR)

FLT 5558 - JAX-GNV - CREW FOUND EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: MECHANISM — JAMMED (PAX DOOR)

AIRSHUTTLE 5271 - TPA-PNS - WHILE ON THE GROUND IN TPA, THE CREW FOUND THE CABIN DOOR LATCH TO BE JAMMED. MAINTENANCE LUBED THE LATCHING MECHANISM, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONTROL MODULE — FAILED (LANDING GEAR)

RDD - LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR MAINTENANCE. REPLACED LANDING GEAR CONTROL MODULE. LANDING GEAR OPERATION NORMAL DURING GEAR SWING. AIRCRAFT RETURNED TO SERVICE. (X)

Part: PROX SENSOR — OUT OF ADJUST (LT MLG)

SFO - LEFT MLG 'A' AND 'B' SYSTEM INTRANSIT LIGHTS ILLUMINATED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE ADJUSTED LEFT MLG 'A' AND 'B' SYSTEM DOWNLOCK PROXIMITY SENSORS. LANDING GEAR POSITION INDICATIONS NORMAL DURING GEAR SWING. AIRCRAFT RETURNED TO SERVICE. (X)

Part: SERVICE DOOR — UNSECURED (RT WING)

FAT - SERVICE DOOR WARNING INDICATION RECEIVED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE RESECURED CAMLOCK ON FUEL SERVICE DOOR. DOOR WARNING SYSTEM OPERATIONALLY CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. (X)

Part: CONNECTOR — DIRTY (LT ENGINE)

FAT - AFTER TAKEOFF, LEFT ENGINE OIL LOW PRESSURE AURAL WARNING ACTIVATED WITH REPORTED FLUCTUATION OF LEFT ENGINE OIL PRESSURE INDICATION OF FROM 30 PSI TO 60 PSI. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE INSPECTED OIL PRESSURE INDICATION SYSTEM, CLEANED ELECTRICAL CONNECTOR AT LEFT ENGINE OIL PRESSURE TRANSMITTER AND SERVICED ENGINE WITH OIL (1 QUART). PERFORMED ENGINE GROUND RUN. OIL PRESSURE INDICATION NORMAL. AIRCRAFT RETURNED TO SERVICE. (X)

Part: DOOR WARN — MALFUNCTION (FWD DOOR)

SFO - FORWARD DOOR WARNING LIGHT FAILS TO EXTINGUISH. MAINTENANCE DEFERRED DOOR WARNING SYSTEM PER MEL 52-70-1. AIRCRAFT RETURNED TO SERVICE. (Z)