N295UX

Part: PCU — FAILED (RT PROPELLER) · airframe 30,946 hrs · 43,793 cycles

ON TAKEOFF, RIGHT NP DROPPED TO 99 PERCENT AND DID NOT RECOVER, ABORTED TAKEOFF. REPLACED RIGHT PCU, P/N 782490-46 S/N ON 980810 S/N OFF 890455.

Part: SIGN — BROKEN (CABIN) · airframe 30,638 hrs · 43,379 cycles

EMERGENCY EXIT SIGN AT 6C BROKEN. FLT 5493. REPLACED SIGN.

Part: ATTACH BRACKET — BROKEN (LT NACELLE FLAP) · airframe 30,258 hrs · 42,861 cycles

LT NACELLE FLAP HAS A CRACKED ATTACH BRACKET. (FLIGHT NR 5480) REPLACED THE LT NACELLE FLAP IAW 27-50-03.

Part: PROBE — CONTAMINATED (TORQUE) · airframe 29,756 hrs · 42,224 cycles

FLT 5732 - THE LEFT ENGINE WENT INTO AUTO-FEATHER WHILE ON GROUND. INSPECTED AND REMOVED MOISTURE FROM TORQUE PROBE. OPS CHECK GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 29,251 hrs · 41,492 cycles

EMERGENCY LIGHT AT ROW 6A IS DAMAGED, FLIGHT NR 5723. REPLACED EXIT SIGN PER MM 33-51-02. OPS CHECK OK.

Part: ROLLER — OUT OF ADJUST (PAX DOOR) · airframe 28,904 hrs · 41,013 cycles

FLT 5584 - MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN. ADJUSTED UPPER AFT ROLLER ON PAX DOOR FRAME. OPS CHECKS GOOD.

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 28,013 hrs · 39,722 cycles

FLT 5774 - MAIN CABIN DOOR GETS JAMMED WHEN TRYING TO OPEN FROM INSIDE. REPLACED THE TOP SHIM STACK ATTACH SCREW AND ADJUSTED GAP TO PROPER CLEARANCES. DOOR OPERATES NORMALLY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,833 hrs · 39,427 cycles

FLOOR LEVEL EMERGENCY LIGHTING IN ROW 9 AND EXIT SIGNS ARE INOP. INSTALLED A SERVICEABLE AFT ELBP. OPS CHECK GOOD.

Part: CONNECTOR — OVERHEATED (WINDSHIELD WIPER) · airframe 27,487 hrs · 38,903 cycles

RIGHT WINDSHIELD WIPER INOP. REPLACED OVERHEATED PINS AT CONTROLLER CONNECTION.

Part: WINDOW — CRACKED (COCKPIT) · airframe 25,416 hrs · 35,914 cycles

CAPTAIN'S SIDE WINDOW HAS CRACK. REPLACED CAPTAIN'S DV WINDOW PANEL IAW EMB 120 MM 56-11-01. OPERATIONAL AND LEAK CHECKS GOOD, PN: 163600-3 SN OFF: 1151

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,162 hrs · 35,503 cycles

FLOOR EMERGENCY LIGHTS ADJACENT GALLEY WILL NOT ILLUMINATE. REMOVED AND REPLACED E-LIGHTING IAW 33-00-00.

Part: SMOKE DETECTOR — CONTAMINATED (LAVATORY) · airframe 24,539 hrs · 34,569 cycles

LAV SMOKE ALARM ACTIVATES WITH SHIP POWER AND WILL NOT RESET. REMOVED MOISTURE FROM LAV SMOKE DETECTOR SENSOR. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,390 hrs · 32,883 cycles

ONE RED EMERGENCY LIGHT ON FLOOR INOPERATIVE. REPLACED RED EMERGENCY LIGHT ON FLOOR. OPERATIONAL CHECK GOOD.

Part: RELAY — FAILED (APU) · airframe 22,101 hrs · 30,920 cycles

SMOKE COMING FROM F/O'S SIDE PANEL. REPLACED OVERHEATED APU FEEDER PROTECTION RELAY. OPERATIONAL CHECK GOOD.

Part: SERVO — MALFUNCTIONED (AUTOPILOT) · airframe 21,527 hrs · 30,016 cycles

AUTOPILOT WANDERS IN PITCH AXIS EXCEEDING COMMAND BARS ABOVE AND THEN BELOW. REMOVED AND REPLACED ELEVATOR SERVO. AUTOPILOT OPERATIONAL CHECK GOOD IAW MM 22-11-00.

Part: RIB — CRACKED (LT NACELLE FLAP) · airframe 21,135 hrs · 29,395 cycles

LEFT NACELLE FLAP 3RD UPPER RIB SUPPORT (FROM OUTBOARD) CRACKED. DISCOVERED DURING A-CHECK INSPECTION. REMOVED AND REPLACED LEFT NACELLE FLAP WITH SERVICEABLE UNIT. REF MM 27-50-03.

Part: COMPUTER — MALFUNCTIONED (AUTO PILOT) · airframe 20,497 hrs · 28,395 cycles

AUTOPILOT ON CAPT'S SIDE DOES NOT PASS FIRST FLIGHT OF DAY CHECKS. REPLACED NR 1 AUTOPILOT COMPUTER. OPS CHECKED GOOD.

Part: ACTUATOR — MALFUNCTIONED (LT NACELLE) · airframe 20,362 hrs · 28,207 cycles

ON TAXI IN TO GATE, FLAP RETRACTION CAUSED DISAGREEMENT - NACELLE FLAPS LAGGING. REMOVED AND REPLACED LT NACELLE ACTUATOR IAW MM 27-50-08. OPS CHECKS GOOD.

Part: COMPUTER — FAULTY (AUTOPILOT SYS) · airframe 20,147 hrs · 27,896 cycles

CAPTAIN'S COMMAND BARS ON THE FLIGHT DIRECTOR ALWAYS INDICATE ABOUT 4 DEGREES TOO LOW. REPLACED APC-65B COMPUTER. OPS CHECK GOOD IAW MM 22-11-00.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 20,104 hrs · 27,834 cycles

YAW ENGAGED, RUDDER TRIM AT 6, WHEN AUTO-PILOT ENGAGED, PLANE YAWED LEFT AND RIGHT HARD MOMENTARILY. REMOVED AND REPLACED F/O'S APC 65B IAW MM 22-10-02. OPS CHECK GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (AUTOPILOT) · airframe 20,074 hrs · 27,794 cycles

WITH YAW ENGAGED AND RUDDER IN TRIM, THEN ENGAGED AUTO PILOT AND AIRPLANE YAWED AND BALL JUST WENT .5 SCALE TO LT, HAPPENED ON BOTH SIDES. REMOVED AND REPLACED AUTOPILOT CONTROL PANEL IAW MM 22-10-04. OPS CHECK GOOD.

Part: ACTUATOR — OUT OF ADJUST (LT MLG) · airframe 18,202 hrs · 24,955 cycles

ON TAKEOFF, THE LEFT MAIN GEAR WOULD NOT RETRACT ALL THE WAY. CYCLED GEAR BUT DID NOT CLEAR PROBLEM. RETURNED TO FIELD. ADJUSTED ACTUATOR LENGTH PER MM 32-32-10 AND ADJUSTED PROX SENSORS TARGET PER MM 32-61-01. GEAR RETRACTIONS AND INDICATIONS CHECK GOOD.

Part: FRAME — CRACKED (NR 2 NACELLE) · airframe 18,038 hrs · 24,675 cycles

RT ENGINE FRAME NR 1 CRACKED AT OB TORSION MOUNT WEB. DISCOVERED DURING C-CHECK, C/W SB 120-54-0036 PART 11 FRAME ONE REPLACEMENT.

Part: COMPARATOR — MALFUNCTIONED (NR 1) · airframe 17,935 hrs · 24,508 cycles

AT 70 PERCENT NP, CAPTAIN'S AHARS GOES BLANK, THEN RETURNS WITH HDG FLAG AND COMPASS CARD 30 DEGREES OFF THE HEADING. RETURNED OT SAN. REPLACED NR 1 AHC-85. PERFORMED REORIENTATION PROCEDURE. RAN LEFT AND RIGHT ENGINES THROUGH 70 PERCENT NP, AUX GENS ON AND OFF, CAPTAIN'S EHSI AND EADI CHECK GOOD. OPS CHECKS GOOD, COMPASS CARDS AND HEADING MATCH SIDE TO SIDE.

Part: WIRE — BROKEN (CABIN) · airframe 17,670 hrs · 24,140 cycles

EXIT SIGN ON ROW 9 OVERHEAD BIN INOP. REPAIRED BROKEN WIRE FOR EMERGENCY EXIT SIGN AT ROW 9 OVERHEAD. OPS CHECK GOOD. NO OTHER DEFECTS NOTED.

Part: LATCH — BROKEN (LT MLG DOOR) · airframe 17,670 hrs · 24,140 cycles

LEFT MAIN GEAR RED LIGHT REMAINED ON AFTER GEAR RETRACTION AND RECYCLE. RETURNED TO SAN. LEFT GEAR FORWARD INBOARD DOOR LATCH BROKEN. REPLACED LATCH AND CYCLED DOORS. OPS CHECK GOOD.

Part: FILTER — DIRTY (HYD SYSTEM) · airframe 17,061 hrs · 23,247 cycles

GREEN HYDRAULIC FILTER LIGHT ILLUMINATED ON TAKEOFF. ALL SYSTEM INDICATORS NORMAL. RETURNED TO SFO. INSTALLED NEW HYDRAULIC RETURN FILTER ON GREEN SYSTEM. PRESSURIZED SYSTEM. OPS CHECKS GOOD.

Part: DEICE SYSTEM — MALFUNCTIONED (WING) · airframe 16,647 hrs · 22,624 cycles

LEFT OUTBOARD WING DEICE BOOT INOP LIGHT IN ICING CONDITIONS. RETURNED TO SFO. RE-CHECKED INFLATION OF LEFT AND RIGHT OUTBOARD WING BOOTS. FOUND GOOD. SWAPPED LEFT AND RIGHT OUTBOARD WING BOOT PRESSURE SWITCHES FOR TROUBLESHOOTING. RAN ENGINES. OPERATIONAL CHECK OF DEICE SYSTEM GOOD.

Part: COMPUTER — FAULTY (COCKPIT) · airframe 16,573 hrs · 22,523 cycles

ON TAKEOFF THE FIRST OFFICER'S EADI AND EHIS WENT OUT. SAME OCCURRED ON LANDING. REPLACED K0394, K0396 AND NR 2 DPU. RAN AIRCRAFT AND CYCLED AUXILLARY GENERATORS ON LINE SEVERAL TIMES. EFIS SYSTEMS OPERATIONAL CHECK GOOD IAW MM 34-23-00.

Part: WIRE HARNESS — DEFECTIVE (RT MLG) · airframe 16,512 hrs · 22,431 cycles

RIGHT MAIN B-GREEN LANDING GEAR INDICATION REMAINS ILLUMINATED WITH GEAR UP. RETURNED TO SFO. REMOVED AND REPLACED UPLOCK HARNESS AND SENSOR. SWUNG GEAR SEVERAL TIMES, ALL CHECKS GOOD IAW EMB 120 32-61-01.

Part: COMPARATOR — FAILED (COCKPIT) · airframe 16,407 hrs · 22,270 cycles

UPON APPLICATION OF TAKEOFF POWER CAPTAIN'S SIDE ATTITUDE INDICATOR BECAME INOPERATIVE SHOWING NO HORIZON INFORMATION AND DISPLAYING ATT FLAG. REPLACED CAPTAIN'S AHC-85. OPS CHECK GOOD IAW EMB120 MM 34-25-00.

Part: RELAY — FAULTY (E/E BAY) · airframe 16,212 hrs · 21,992 cycles

EFIS & ATT INDICATIONS WHEN POWER LEVER ADVANCED FOR TAKEOFF WITH RIGHT AUX GEN OFF. COULD NOT DUPLICATE DPU FAILURE. RAN ENGINE AND HAD SCREENS FLASH. DPU FAIL CAME UP FOR APPROXIMATELY 3-5 SECONDS. THIS IS NORMAL. REPLACED RELAYS K0119, K0227 AND K0029. OPS CHECK GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 4,154 hrs · 5,669 cycles

ON TAKEOFF ROLL AURAL WARNING ''AUTO FEATHER''. SWITCH WAS ON AND TESTED ON TAXI CHECK.COULD NOT DUPLICATE DURING RUNUP. OPS CHECK GOOD.

Part: PROP HEAT — INTERMITTENT (LT PROP) · airframe 15,239 hrs · 20,595 cycles

CREW REPORTS LEFT PROP HEAT FAILS INTERMITTENTLY INFLIGHT. RETURNED TO PDX. MAINTENANCE FOUND THE PROP HAD BEEN STRUCK BY LIGHTNING. REMOVED AND REPLACED LEFT BULKHEAD ASSEMBLY, DID NOT FIX PROBLEM. P/N ON 784784-1, S/N ON 960443, S/N OFF 9202318. REMOVED AND REPLACED ALL PROP BLADES IAW MM 61-13-04.

Part: SWITCH — OUT OF ADJ (FWD DOOR) · airframe 15,230 hrs · 20,583 cycles

FORWARD DOOR LIGHT ILLUMINATED DURING TAKEOFF ROLL. ABORTED AND RETURNED TO GATE. ADJUSTED BOTH FORWARD DOOR SWITCHES. OPS CHECKS GOOD.

Part: SENSOR — FAILED (ELEVATOR TRIM) · airframe 14,333 hrs · 19,335 cycles

TAKEOFF ''TRIM'' AURAL WARNING ON TAKEOFF ROLL WITH TRIM SET AT 32. ABORTED TAKEOFF. REMOVED AND REPLACED RIGHT ELEVATOR PROXIMITY TRIM SENSOR AND ADUSTED IAW EMB 120 MM 27-32-00. OPS CHECKS NORMAL.

Part: SEAL — LEAKING (EMERGENCY EXIT) · airframe 14,193 hrs · 19,131 cycles

FLIGHT ATTENDANT REPORTS LOUD RUSHING AIR AT SEAT 6A EXIT DOOR, UNABLE TO PRESSURIZE AIRCRAFT. RETURNED TO PDX.. CLEANED SEAL ON LEFT OVER WING EMERGENCY EXIT. REINSTALLED DOOR AND PRESSURIZED AIRCRAFT. CHECKS GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 14,048 hrs · 18,950 cycles

MAIN CABIN DOOR EMERGENCY EXIT LIGHT BROKE OFF. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IAW MM 33-51-02. OPS CHECK GOOD.

Part: LATCH — FAILED (REFUEL DOOR) · airframe 13,501 hrs · 18,198 cycles

DOOR LIGHT ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AND REPLACED SINGLE POINT REFUELING ACCESS DOOR CAMLOC IAW MM 28-00-00. OPS CHECK GOOD.

Part: LT PACK — FAILED (ACM BAY)

LEFT PACK FAILED ON CLIMB THROUGH 700 FOLLOWED BY SMOKE LIGHT ON MAP PANEL AND SMOKE AURAL WARNING. RETURNED TO SFO. REMOVED AND REPLACED LEFT AIR CYCLE MACHINE WITH SERVICEABLE UNIT IAW MM 215005, OPS CHECKS GOOD AT THIS TIME. (P/N 22045402) ON, (S/N 87303) ON, (S/N 100534) OFF.

Part: WINDSHIELD — FAILED (LT COCKPIT)

LEFT WINDSHIELD SHATTERED CLIMBING THROUGH 12000 FT. REMOVED AND REPLACED LEFT WINDSHIELD IAW MM 56-10-01. NO EVIDENCE OF ANY OTHER DAMAGE.

Part: SKIN — LIGHTNING STRIKE (LT ELEVATOR)

AIRCRAFT TOOK A LIGHTNING STRIKE WHILE AIRBORNE. RETURNED TO RDM. RDM, INSPECTED AIRCRAFT PER MM 05-50-01 AND FOUND LIGHTNING STRIKE TO LEFT ELEVATOR. NO OTHER DAMAGE FOUND. RELEASED AIRCRAFT FOR SPECIAL FLIGHT.

Part: HMU — MALFUNCTIONED (LT ENGINE)

FSD - LEFT ENGINE DID NOT MAKE POWER, ABORTED TAKEOFF, RETURNED TO GATE. REPLACED HMU. (X)

Part: CONTROL CABLE — WORN (RT AILERON)

AILERON CONTROL CABLES ARE WORN. REMOVED AND REPLACED AILERON CONTROL CABLES. (X)

Part: CONTROL CABLE — WORN (LT AILERON)

AILERON CONTROL CABLES ARE WORN. REMOVED AND REPLACED AILERON CABLES. (X)

Part: SWITCH — DIRTY (NLG STEERING)

FSD - AFTER LANDING, UNABLE TO STEER NOSEWHEEL BY TILLER OR RUDDER PEDALS. MAINTENANCE FOUND PROXIMITY SWITCHES STICKING. CLEANED AND OPERATES NORMALLY. (M)

Part: TORQUE SENSOR — FAILED (RT ENGINE)

SPI - CREW REPORTED RT TORQUE GAUGE INOPERATIVE (READS ZERO). THEY RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED RT TORQUE SENSOR. OPS CHECK WAS GOOD. (X)

Part: TQ SIG COND — FAILED (RT ENGINE)

OSH - CREW ABORTED TAKEOFF WHEN RT ENGINE TORQUE GAUGE WENT INOP AND THE ENGINE AUTOFEATHERED. MAINTENANCE REPLACED THE TORQUE GAUGE (TORQUE SIGNAL CONDITIONER) AND PERFORMED SATISFACTORY ENGINE RUNS.

Part: RETRACT MECH — MALFUNCTIONED (TE FLAPS)

ORD - THE CREW ELECTED AN AIR TURN BACK AFTER THE FLAPS STUCK IN THE 15 DEGREE POSITION. AFTER AN UNEVENTFUL LANDING, MAINTENANCE CHECKED THE FAULT SYSTEM IN THE MX MODE OF THE FLAP COMPUTER AND CLEARED FAULTS PER BRASKA MM CH27-50-00. OPS CHECK OF FLAPS COULD NOT DUPLICATE PROBLEM.