N292UX

Part: FUSE — BLOWN (CABIN) · airframe 32,318 hrs · 45,273 cycles

UPPER CEILING FORWARD EMERGENCY LIGHT INOPERATIVE. (FLT 6678) REPLACED FUSE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,318 hrs · 45,273 cycles

FORWARD CABIN OVERHEAD EMERGENCY LIGHT INOP. (FLT 5768) RELAMPED EMERGENCY LIGHT.

Part: FUSE — BLOWN (CABIN) · airframe 32,281 hrs · 45,225 cycles

CEILING EMERGENCY LIGHT INOP. (FLT 5885) REPLACED FUSE.

Part: ROD — CORRODED (AILERON TAB) · airframe 32,295 hrs · 45,241 cycles

LEFT AILERON TRIM TAB RODS CORRODED. (C CHECK) REPLACED ROD ENDS PER AMM.

Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 32,627 hrs · 45,707 cycles

MAIN DOOR THRESHOLD CRACKED. (C-CHECK) REPLACED THRESHOLD PLATE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 32,627 hrs · 45,707 cycles

STRINGERS 18 AND 19 CORRODED. (C-CHECK) REPAIRED STRINGERS PER SRM.

Part: RIB — CRACKED (LT WING) · airframe 32,627 hrs · 45,707 cycles

FORWARD LEFT WING SPAR INBOARD RIB CRACKED. (C-CHECK) REPAIRED PER SRM.

Part: RIB — CRACKED (LT WING) · airframe 32,295 hrs · 45,241 cycles

LEFT WING RIB ON FRAME 21 CRACKED. (C CHECK) REPAIRED PER SRM.

Part: CHANNEL — CRACKED (LT NACELLE) · airframe 32,295 hrs · 45,241 cycles

LEFT NACELLE CHANNEL CRACKED. (C CHECK) REPLACED CHANNEL PER SRM.

Part: SUPPORT — CRACKED (TE FLAP) · airframe 32,295 hrs · 45,241 cycles

RIGHT NACELLE FLAP FORWARD INBOARD CORNER CRACKED. (C CHECK) REPLACED SIDE SUPPORT PER SRM.

Part: ROD — CORRODED (NLG DOOR) · airframe 32,627 hrs · 45,707 cycles

NOSE GEAR RIGHT AFT GEAR DOOR ROD CORRODED. (C-CHECK) REPLACED ROD.

Part: ROD END — OUT OF ADJUST (RT MLG) · airframe 31,325 hrs · 43,940 cycles

FLT 5553 - RIGHT MAIN GEAR DISAGREE LIGHTS ON AFTER GEAR RETRACTION. ADJUSTED RIGHT MLG ACTUATOR ROD END.

Part: CARTRIDGE — MALFUNCTIONED (APU FIRE BOTTLE) · airframe 30,496 hrs · 42,881 cycles

APU FIRE BOTTLE "INOP" LIGHT IS ON. FLIGHT 5783. REPLACED APU FIRE BOTTLE AND CARTRIDGE IAW MM 26-22-01. OPS TEST GOOD. P/N 899170-1, S/N OFF 15840EK, P/N 897776-01, S/N OFF 57597.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 29,529 hrs · 41,574 cycles

FLT 5544 - EMERGENCY LIGHT TRACK LIGHT IS INOP. RESECURED WIRING AT LIGHT. OPS CHECK GOOD.

Part: TERMINAL — CORRODED (DC GENERATOR) · airframe 29,194 hrs · 41,128 cycles

THE RIGHT DC CONTACTOR TERMINALS ARE CORRODED. REPLACED THE RIGHT DC CONTACTOR IAW MM 24-30-03.

Part: BUSS BAR — CORRODED · airframe 29,194 hrs · 41,128 cycles

BUS BAR ATTACH POINT NEAR K0135 AREA SHOWS SIGNS OF CORROSION. REPLACED FEED PROTECTION RELAY AND ASSOCIATED BUS BARS IAW EMB 120 AMM 24-52-00.

Part: FRAME — CORRODED (FUSELAGE) · airframe 29,194 hrs · 41,128 cycles

LOWER FUSELAGE BELLY FRAME 23 SHOWS SIGNS OF CORROSION. COMPLIED WITH REPAIRS AT FRAME 23 IAW IC2007-120/07298 AND CPM 51-11-0.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,194 hrs · 41,128 cycles

CORROSION FOUND ON FUSELAGE FLOOR FRAME AT AFT PAX DOOR HINGE. COMPLIED WITH REPAIR OF FLOOR FRAME IAW EMB 120 SRM 51-10-02 PG 3 SECTION 3B.

Part: STRINGER SPLICE — CRACKED (RT NACELLE) · airframe 28,817 hrs · 40,613 cycles

RIGHT NACELLE INBOARD SIDE WHEEL WELL CLOSE OUT STRINGER SPLICE IS CRACKED AT FRAME NR 10, FOUND AT C-CHECK. REPLACED NACELLE INBOARD SIDE WHEEL WELL CLOSE OUT STRINGER SPLICE AND STRINGER PER EMB 120 SRM 51-40-02.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 28,095 hrs · 39,557 cycles

FORWARD FLOOR TRACK LIGHT IS MISSING RED LENS COVER. REINSTALLED RED LENSE COVER TO FLOOR TRACK LIGHT ASSEMBLY. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,056 hrs · 39,503 cycles

FLOOR LEVEL EMERGENCY LIGHTS FORWARD OF ROW 3 INOP. REPLACED FORWARD ELBP WITH SERVICEABLE UNIT.

Part: HANDSET — SMOKE · airframe 28,023 hrs · 39,458 cycles

ON TAXI OUT, FLIGHT ATTENDANTS HANDSET STARTED SMOKING. REPLACED FLIGHT ATTENDANTS HANDSET. OPS CHECK GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 27,039 hrs · 38,014 cycles

ODOR IN COCKPIT. NO SMOKE. REPLACED APU SHUNT R005 AND APU FEEDER PROTECTION RELAY K0152 IAW EMB 120 MM 24-52-0. OPERATIONAL CHECKS GOOD.

Part: CONNECTOR — DIRTY (TE FLAPS) · airframe 26,870 hrs · 37,768 cycles

AFTER TAKEOFF RETRACTING FLAPS CONTROL FAULT ON OUTBOARD PAIR, RETURNED TO SFO. CLEANED TRACKS AND CONNECTORS FOR OUTBOARD FLAPS. OPERATIONAL CHECKS GOOD.

Part: RELAY — MALFUNCTIONED (ELECTRICAL SYS) · airframe 26,767 hrs · 37,624 cycles

OVERHEATING SMELL IN COCKPIT WITH APU ON. REPLACED FEEDER PROTECTION RELAY AND SWITCH. OPERATIONAL CHECKS GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 26,749 hrs · 37,600 cycles

OVERHEATING ODOR IN FLIGHT DECK ON THE GROUND.INSPECTED APU BLEED DUCTING FOR SIGNS OF OIL. OPERATIONAL CHECKS NORMAL. NO ODORS EVIDENT.

Part: SIGN — BROKEN (CABIN) · airframe 26,440 hrs · 37,147 cycles

LOWER EMERGENCY EXIT SIGN AT SEAT 6A IS BROKEN. REPLACED EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD.

Part: RELAY — FAILED (APU) · airframe 26,246 hrs · 36,883 cycles

ELECTRICAL SMELL FROM GENERATOR CONTROL PANEL. REPLACED APU FEEDER PROTECTION RELAY IAW MM 24-00-00. OPERATIONAL CHECKS GOOD.

Part: ACTUATOR — LEAKING (RT WING) · airframe 25,459 hrs · 35,713 cycles

TOTAL LOSS OF ALL HYD FLUID ON THE BLUE SYSTEM. REPLACED RIGHT NACELLE ACTUATOR IAW MM 27-50-00.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 24,515 hrs · 34,302 cycles

FLOOR EMERGENCY LIGHTS, 4 LIGHTS INOP, FIRST 2 RED, FIRST 2 WHITE LIGHTS. REPLACED FWD ELBP. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,453 hrs · 34,205 cycles

RED EMERGENCY LIGHT BY THE MAIN CABIN DOOR INOP. REPLACED RED EMERGENCY LIGHT BY MAIN CABIN DOOR. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAP) · airframe 23,789 hrs · 33,182 cycles

ON APPROACH, FLAP DISAGREEMENT. REPLACED LT NACELLE FLAP ACTUATOR. OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,906 hrs · 30,351 cycles

FIRST OVERHEAD EMERGENCY CABIN LIGHT INOPERATIVE. RELAMPED FIRST OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.

Part: ANNUNCIATOR — MALFUNCTIONED (TE FLAPS) · airframe 21,483 hrs · 29,676 cycles

RECEIVED A FLAP AND ADVANCE SWS MAP IN FLIGHT WITH ASSOCIATED CONTROL FAULT ON OVERHEAD PANEL INDICATING FAULT IN OUTBOARD PAIR OF FLAPS. REMOVED AND REPLACED FLAP ANNUNCIATOR IAW EMB 120 MM 27-50-05. ALSO REPAIRED DEFECTIVE SPLICE ON LEFT OUTBOARD FLAP ACTUATOR WIRE W502-0026-22. OPS CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 21,417 hrs · 29,578 cycles

ON CLIMBOUT THE OUTBOARD FLAPS INDICATED A SINGLE BAR ASSEMETRY. RETURNED TO FAT. REMOVED AND REPLACED FLAP CONTROL UNIT IAW EMB 120 MM 27-50-00. OPS CHECK GOOD.

Part: ANNUNCIATOR — MALFUNCTIONED (SMOKE DETECTOR) · airframe 21,392 hrs · 29,543 cycles

SMOKE TRIPLE CHIME IN FLIGHT ON FINAL DESCENT. LAV SMOKE DETECTOR LIGHTS FLASHING. NO SMOKE IN CABIN AT ALL, OR LAV. REMOVED AND REPLACED SMOKE DETECTOR ANNUNICATOR PANEL WITH SERVICEABLE PANEL. OPS CHECK GOOD.

Part: SELECTOR — MALFUNCTIONED (TE FLAPS) · airframe 20,918 hrs · 28,814 cycles

ON TOUCHDOWN, FLAPS 45 LANDING AND RECEIVED A CONTROL FAULT ALL LIGHT BARS FLASHING 0, QRH PROCEDURE DID NOT FIX. REPLACED FLAP SELECTOR LEVER ASSEMBLY WITH SERVICEABLE UNIT. FLAPS OPS CHECK GOOD.

Part: SELECTOR — MALFUNCTIONED (TE FLAPS) · airframe 20,882 hrs · 28,756 cycles

AFTER TAKEOFF DURING FLAP RETRACTION, RECEIVED A FLAP DISAGREEMENT ON THE OUTBOARD FLAPS. CYCLED FLAPS PER THE QRH, DISAGREEMENT REMAINED. OVERHEAD PANEL INDICATED OUTBOARDS STUCK AT 2 SEGMENT BARS. REPLACED FLAP SELECTOR WITH SERVICEABLE UNIT. CLEANED AND LUBED FLAP TRACKS. OPS CHECKS GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAP) · airframe 20,793 hrs · 28,633 cycles

FLAP DISAGREEMENT ON DEPARTURE WHEN RETRACTING FROM 15-0. RESELECTED 15 THEN 0 PER QRH TWICE AT DIFFERENT AIR SPEEDS WITH SAME RESULT. FLAP PANEL INDICATION: OUTBOARD SHOWED 2 DOTS, NAC AND INBOARD SHOWED 1 DOT EACH. REMOVED AND REPLACED FLAP COMPUTER WITH A SERVICEABLE UNIT. OPS CHECKS GOOD.

Part: WIRE — DAMAGED (AUTOPILOT SYS) · airframe 20,730 hrs · 28,540 cycles

WITH AUTOPILOT ON FO'S SIDE, THE COMMAND BARS WILL NOT PITCH UP WITH ROCKER SWITCH ON AUTOPILOT CONTROL PANEL. IF GO AROUND BUTTON IS PRESSED, COMMAND BARS WILL NOT PITCH UP. REPAIRED WIRING TO P0144. OPS CHECK GOOD IAW MM 22-10-00.

Part: COMPUTER — MALFUNCTIONED (AUTO-PILOT) · airframe 20,229 hrs · 27,778 cycles

FD FLAG CAPT SIDE, FOS FD ERATIC WILL NOT CAPTURE AUTOPILOT, EITHER SIDE. DOES NOT TEST ON GROUND. REPLACED CAPT APC 65B AUTOPILOT COMPUTER. OPS CHECK GOOD IAW MM 22-10-00. PN ON 622-8315-402 SN ON 3332 OFF 131.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 20,011 hrs · 27,432 cycles

ON LEVEL OUT AFTER CLIMB YOKE SHOOK FORWARD QUICKLY WITH SINGLE CHIME ALERT AND NO OTHER INDICATIONS. REPEATED ON DESCENT INITIATION. BOTH TIMES AP ON. CHECKED SYSTEM. FOUND NO FAULTS WITH AOA NR 1 OR AOA NR 2 OR SIDE SLIP. ALL SYSTEM TEST POINTS CHECK GOOD. REMOVED AND REPLACED THE STALL WARNING COMPUTER AS A PRECAUTION IAW MM 27-34-03. SYSTEM OPS CHECKS GOOD WITH NO FAULTS FOUND.

Part: FRAME — CRACKED (RT NACELLE) · airframe 18,946 hrs · 25,845 cycles

FOUND CRACKS IN FRAME NR 1 ON RIGHT NACELLE. FOUND DURING ENGINE CHANGE. COMPLIED WITH S/B 120-54-0036, INSTALLED NEW FRAME NR 1.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 18,847 hrs · 25,673 cycles

PRESSURIZATION WAS WORKING IN MANUAL MODE AT FL230. AUTOMATIC MODE WAS DEFERRED. DURING CRUISE THE CABIN CLIMBED INSTANTLY TOWARD CRUISE ALTITUDE AND WAS THERE WITHIN 10 SECONDS. THE MASKS DROPPED. INITIATED EMERGENCY DESCENT AFTER ATC CLEARANCE 5 MINUTES LATER. INSTALLED PNEUMATIC OUTFLOW VALVE IAW 21-30-00. INSTALLED ELECTRO-PNEUMATIC VALVE IAW 21-30-00. PRESSURIZED AIRCRAFT, ALL CHECKS OK AT THIS TIME.

Part: WARNING LIGHT — FALSE ACTIVATION (PAX DOOR) · airframe 18,847 hrs · 25,673 cycles

FORWARD DOOR WARNING ACTIVATED DURING TAKEOFF ROLL. ABORTED TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. FORWARD DOOR WARNING CHECKS GOOD.

Part: FRAME — CRACKED (RT WING LE) · airframe 18,309 hrs · 24,860 cycles

RIGHT INBOARD LEADING EDGE INBOARD FRAME CRACKED, MARKED. DISCOVERED DURING C-CHECK. REPLACED RIGHT INBOARD LEADING EDGE FRAME.

Part: SENSOR — MALFUNCTIONED (LAVATORY) · airframe 18,221 hrs · 24,702 cycles

ON TAKOFF, AT 90 KAIS, TRIPLE CHIME SMOKE ALARM MAP SMOKE LIGHT ON MAP. ABORTED TAKEOFF. REPLACED LAV SMOKE SENSOR WITH A SERVICEABLE UNIT. OPS CHECKS GOOD.

Part: INDICATOR — DEFECTIVE (COCKPIT) · airframe 16,990 hrs · 22,781 cycles

ON TAKEOFF, AT ABOUT 60 KIAS, GOT AN AURAL WARNING - HIGH SPEED. ABORTED TAKEOFF. REPLACED CAPTAIN'S AIRSPEED INDICATOR PER EMB MM 34-12-01. OPS CHECKS GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 16,975 hrs · 22,753 cycles

HIGH SPEED AURAL WARNING SOUNDED ON TAKEOFF. PERFORMED PITOT STATIC CHECK IAW MM 34-12-00. HIGH SPEED WARNING SOUNDED AT CORRECT TIME. COULD NOT DUPLICATE. CHECKS GOOD AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 16,876 hrs · 22,649 cycles

TRIPLE CHIME HIGH SPEED WARNING SOUNDED ON TAKEOFF (ABORTED TAKEOFF). HOOKED UP PITOT STATIC SET, RAN UP AND DOWN 5 TIMES, COULD NOT DUPLICATE. OPS CHECKS GOOD.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 16,759 hrs · 22,520 cycles

DURING TAKEOFF ROLL, TRIPLE CHIME FOLLOWED BY SMOKE ON MAP, FOLLOWED BY LAVATORY SMOKE ALARM.RAN AIRCRAFT UP TO STATIC POWER WITH PACKS ON. COULD NOT DUPLICATE SMOKE ALARM ON MAP PANEL OR BY LAVATORY ALARM. OPS CHECK GOOD.

Part: SWITCH — FAILED (REFUEL DOOR) · airframe 16,412 hrs · 22,008 cycles

SERVICE DOOR LIGHT WILL NOT EXTINGUISH. ABORTED TAKEOFF.REPLACED REFUELING RECEPTACLE DOOR MICROSWITCH WITH SERVICEABLE UNIT, OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 16,058 hrs · 21,463 cycles

EMERGENCY LIGHTS WOULD NOT TEST PROPERLY. REMOVED AND REPLACED FORWARD, MID AND AFT ELBP'S IAW 33-50-02. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,067 hrs · 20,039 cycles

ONE EMERGENCY LIGHT INOP AT ROW 7 FLOOR. REPLACED ONE EMERGENCY AISLE MONITOR UNIT AT ROW 7 FLOOR (P/N 10-1307-3). GROUND CHECK NORMAL.

Part: WIRE — BROKEN (TAIL CONE) · airframe 14,853 hrs · 19,738 cycles

TAKEOFF AURAL WARNING TRIM WITH TRIM IN GREEN ARC. ABORTED TAKEOFF. FOUND BROKEN WIRE FOR RIGHT HAND SENSOR AT TAIL CONE. RECONNECTED PER WIRING MANUAL 20-21-00 AND CHECKED RIGGING OF RIGHT HAND SENSOR PER MM 27-32-00. OPS CHECK GOOD.

Part: SEAL — OBSTRUCTED (CARGO DOOR) · airframe 14,765 hrs · 19,624 cycles

DEPARTED SEA, PRESSURIZATION FAILED, WENT TO MANUAL PRESSURIZATION, STILL UNCONTROLLABLE. RETURNED TO SEA. CLEANED CABIN DOOR SEAL AND CHECKED CARGO DOOR SEAL. CHECKED OUTFLOW VALVES FOR OBSTRUCTIONS. PRESSURIZATION CHECKS GOOD DURING GROUND OPS IAW MM 21-30-00. COULD NOT DUPLICATE SQUAWK.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 14,655 hrs · 19,491 cycles

PRESSURIZATION SYSTEM INOP IN AUTO AND MANUAL. RETURNED TO PDX. REPLACED PRESSURIZATION CONTROLLER PER MM 21-31-01. OPS CHECKS GOOD IN AUTO MODE ON GROUND. PN ON: 22201T011400 SNON: 191 SNOFF: 152. REPLACED PNEUMATIC OUTFLOW VALVE PER RII 21-303 . PN ON: 2093K010800 SNON: 144 SNOFF: 159. OPS CHECKS GOOD MANUAL MODE ON GROUND.

Part: LOCK — UNSECURE (FUEL DOOR) · airframe 14,369 hrs · 19,121 cycles

RED DOOR WARNING DURING TAKEOFF ROLL. ABORTED AND RETURNED TO GATE. SECURED CAMLOCK ON INBOARD FUEL DOOR. OPS CHECKS GOOD.

Part: LOCK — LOOSE (FUEL QTY DOOR) · airframe 14,369 hrs · 19,121 cycles

DOOR LIGHT ON MAP, SERVICE OVERHEAD LIGHT ILLUMINATED ON ROTATION. RETURNED TO PDX. FOUND FUEL QUANTITY DOOR CAMLOCK LOOSE. RESECURED AS NEEDED, OPS CHECKS GOOD.

Part: CONNECTOR — DIRTY (TE FLAPS) · airframe 13,889 hrs · 18,486 cycles

AFTER TAKEOFF, FLAP DIASGREEMENT, LEFT OUTBOARD PAIR DID NOT RETRACT. CYCLED FLAPS BUT THEY WOULD NOT RESET. RETURNED TO MRY. CHECKED ALL FOUR FLAP BEARINGS AND REMOVED AND CLEANED CANNON PLUG. OPS CHECKED FOUR TIMES AND COULD NOT DUPLICATE.

Part: ACTUATOR — MALFUNCTIONED (FLAPS) · airframe 13,889 hrs · 18,486 cycles

FLAP ASYMMETRY AFTER TAKEOFF. RETURNED TO MRY. MX COMPUTER SHOWED (LT LVDT IMP FLR ), PERFORMED CONTINUITY CHECK FROM FCU TO LEFT OUTBOARD ACTUATOR IAW MM 27-51-00, OPS CHECKS GOOD. REPLACED OUTBOARD FLAP ACTUATOR IAW 27-50-09, OPS CHECKS GOOD. (P/N 3430001007) ON, (S/N 0253) ON, (S/N 0555) OFF.

Part: COVER — LEAKING (RT ENGINE) · airframe 12,876 hrs · 17,117 cycles

THROUGH 10,000 FEET ON CLIMBOUT RIGHT ENGINE DUCT LEAK LIGHT, THREE CHIME AND AURAL WARNING OCCURRED. FOLLOWED QRH PROCEDURE, RIGHT ENGINE WAS SHUTDOWN IN FLIGHT. WARNINGS WENT AWAY AFTER APPROXIMATELY TWO MINUTES, LANDED SINGLE ENGINE AFTER RETURNING TO SFO. REINSTALLED COVER CUP ON DEICE PRESSURE REGULATOR, OPS CHECKS GOOD.

Part: BOOT — FAILED (LT ENG INLET)

LEFT ENGINE AIR INLET BOOT FAILED IN FLIGHT. RETURNED TO SEA. INSTALLED UNIVERSAL INLET IAW MM 30-20-00.

Part: OIL SYST — REQD SERVICE (RT ENGINE)

ON DEPARTURE, RIGHT OIL PRESSURE FLUCTUATED BETWEEN 50 AND 35 PSI CAUSING AN AURAL WARNING AND LIGHT. RETURNED TO FIELD. CREW SERVICED OIL. GROUND RAN ENGINE AT 100 PERCENT AND CRUISE POWER. ALL OIL SYSTEM INDICATION CHECKS GOOD.

Part: CONTROL CABLE — WORN (RT AILERON)

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

Part: EEC — MALFUNCTIONED (RT ENGINE)

SPW - RIGHT ENGINE OVERTORQUED FOR APPROXIMATELY 10 SECONDS. MAINTENANCE COMPLETED OVERTORQUE INSPECTION AND REPLACED EEC. (M)

Part: TQ SENSOR — LOOSE (LT ENGINE)

SPI - LEFT TORQUE FLUCTUATES 30 TO 40 PERCENT. MAINTENANCE INSPECTED AND FOUND NH SENSOR LOOSE AND HMU SENSOR LOOSE. TIGHTENED AS REQUIRED. OPERATIONAL CHECK GOOD. TEST FLIGHT SATISFACTORY. (M)

Part: UPLOCK ACTUATOR — MALFUNCTIONED (LT MLG)

SPW - LEFT MAIN A AND B SYSTEMS RED LIGHTS REMAINED ILLUMINATED AFTER RETRACTION. CREW MADE AN AIR TURNBACK AND LANDED UNEVENTFULLY. MAINTENANCE SWAPPED MLG UPLOCK ACTUATORS. TEST FLIGHT SATISFACTORY. (X)

Part: NP SENSOR — LOOSE (RT ENGINE)

CIU - CREW REPORTED A 30 PERCENT TORQUE LOSS ON RT ENGINE WITH EEC ON. THEY MADE AN AIR TURN-BACK AND LANDED UNEVENTFULLY. MAINTENANCE TIGHTENED RT NP SENSOR. OPS CHECK WAS GOOD. (X)

Part: START CONTACTOR — FAILED (RT COCKPIT)

SUX - CREW REPORTED A 'HOT' SMELL COMING FROM COPILOT'S SIDE PANEL (PANEL WAS HOT). MAINTENANCE REMOVED AND REPLACED APU START CONTACTOR AND ASSOCIATED ELECTRICAL CONNECTORS WHICH HAD BEEN DAMAGED BY HEAT. OPS CHECK WAS GOOD. (X)

Part: LATCH PIN — WORN (COPILOT SEAT)

ORD - CREW REPORTED CO-PILOT'S SEAT SLID AFT ON TAKEOFF ROLL. MAINTENANCE REMOVED AND REPLACED SEAT LATCH PINS. OPS CHECK WAS GOOD. (X)