N236SW

Part: SIGN — UNSECURE (CABIN) · airframe 38,023 hrs · 49,946 cycles

EMERGENCY EXIT SIGN UNSECURE. FLT#7418 REPLACED EMERGENCY EXIT SIGN. PN 10-1301-15

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 37,785 hrs · 49,667 cycles

CABIN DE-PRESSURIZED IN AUTO MODE. FLT#5625 REPLACED ELECTRO-PNEUMATIC OUTFLOW VALVE IAW AMM. PN 2091G010800, SN ON 440, SN OFF 336

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,196 hrs · 48,806 cycles

EMERGENCY LIGHT ABOVE MAIN CABIN DOOR BURNED OUT. (FLT 7391) RELAMPED EMERGENCY LIGHT.

Part: SIGN — BROKEN (CABIN) · airframe 36,786 hrs · 48,320 cycles

RIGHT FLOOR LEVEL EMERGENCY EXIT SIGN AT ROW 6 IS BROKEN. (FLT 7390) REPLACED RIGHT FLOOR LEVEL EMERGENCY EXIT SIGN AT ROW 6.

Part: ACTUATOR — FAILED (TE FLAP) · airframe 36,686 hrs · 48,192 cycles

OUTBOARD FLAP WOULD NOT COME UP AFTER TAKEOFF. (FLT 7790) REPLACED LEFT INBOARD FLAP ACTUATOR AND WIRE W602-0014-22 IAW AMM AND WDM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,686 hrs · 48,192 cycles

CEILING EMERGENCY LIGHTING BURNED OUT. (FLT 6442) RELAMPED EMERGENCY LIGHT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,677 hrs · 48,180 cycles

CORROSION ON FLOORBEAM AT PAX DOOR ENTRY WAY. (C-CHECK) REPLACED LEFT FLOOR OMEGA BEAM TOP BUTT STRAP IAW SRM.

Part: BEARING — FAILED (RT PROPELLER) · airframe 36,459 hrs · 47,902 cycles

RIGHT PROPELLER HUB LEAKING OIL. INSPECTED AND FOUND RIGHT PROPELLER NR 4 BEARING RACE FAILURE CAUSING DAMAGE TO RIGHT PROPELLER HUB. REPLACED RIGHT PROPELLER HUB AND ACTUATOR. P/N OFF: 782501-8 S/N OFF: 1785.

Part: BOLT — SHEARED (MLG ACTUATOR) · airframe 35,057 hrs · 46,197 cycles

AFTER TAKEOFF, THE RIGHT MAIN GEAR WOULD NOT COME UP. (FLT 7795) REPLACED RIGHT MLG ACTUATOR ATTACH BOLT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,572 hrs · 45,600 cycles

MAIN CABIN DOOR INTERIOR EMERGENCY LIGHT IS OUT. (FLT 5587) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,340 hrs · 45,318 cycles

FORWARD OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4469) RELAMPED EMERGENCY LIGHT.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 34,065 hrs · 44,967 cycles

MAIN CABIN DOOR IS DIFFICULT TO OPEN. (FLT 7767) LUBED ROLLERS AND HINGE POINT.

Part: WIRE — BROKEN (CABIN) · airframe 34,052 hrs · 44,954 cycles

EMERGENCY EXIT SIGN ON OVERHEAD BIN DOOR NEAR ROW 9 IS OUT. (FLT 7797) REPAIRED BROKEN WIRE FOR EMERGENCY EXIT OVERHEAD LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,414 hrs · 44,158 cycles

EMERGENCY LIGHTING FROM ROWS 1 TO 6 IS OUT. (FLT 7797) REPLACED NR 2 ELBP.

Part: FRAME — CRACKED (LT NACELLE) · airframe 33,414 hrs · 44,158 cycles

LEFT ENGINE FRAME NR 1 CRACKED AT OUTBOARD TORSION MOUNT ATTACH POINT. (C-CHECK) REPLACED LEFT ENGINE FRAME NR 1.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,185 hrs · 42,679 cycles

ONE WHITE EMERGENCY LIGHT AT ROW 5 INOP. (FLT 6302) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,744 hrs · 42,152 cycles

EMERGENCY LIGHT OVER ROW 7 INOP. (FLT 7806) RELAMPED EMERGENCY LIGHT.

Part: SERVO — JAMMED (RUDDER) · airframe 31,405 hrs · 41,740 cycles

RUDDER UNCONTROLLABLE IN FIXED POSITION ON TAKEOFF ROLL. (FLT 7773) REPLACED RUDDER SERVO AND RUDDER SERVO MOUNT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,727 hrs · 40,882 cycles

FOUND ELBP (CENTER) TO BE INOP DURING OPS CHECK OF THE EMERGENCY LIGHTS. (FLT 7766) REPLACED ELBP (CENTER) IAW AMM 33-50-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,422 hrs · 40,500 cycles

RIGHT EXTERIOR AFT EMERGENCY LIGHT INOP. (FLT 7813) RELAMPED EMERGENCY LIGHT.

Part: WIRE — CORRODED · airframe 29,668 hrs · 39,476 cycles

DURING C-CHECK, RIGHT INBOARD FLAP WELL WIRE SPLICE CORRODED. REPLACED WIRE SPLICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,180 hrs · 40,210 cycles

C-CHECK, SEAT TRACKS CORRODED. REPLACED PER AMM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 30,180 hrs · 40,210 cycles

C-CHECK, STRINGERS IN AREA UNDER FORWARD PASSENGER DOOR ACTUATOR CORRODED. REPAIRED PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 29,407 hrs · 39,129 cycles

FLT 5411 - ONE RED FLOOR EMERGENCY EXIT PATH LIGHT INOP AT ROW 9. INSTALLED NEW LIGHT FIXTURE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 29,284 hrs · 38,970 cycles

FLT 5798 - WHITE FLOOR EMERGENCY LIGHT INOP AT ROW 6. RELAMPED.

Part: MODULE — FAILED (MLG SELECTOR) · airframe 28,999 hrs · 38,585 cycles

FLT 5495 - LANDING GEAR DID NOT RETRACT AFTER TAKEOFF. REPLACED LANDING GEAR HANDLE SELECTOR CONTROL PANEL MODULE.

Part: ACTUATOR — BYPASSING (NLG) · airframe 28,984 hrs · 38,565 cycles

FLT 5509 - LANDING GEAR VERY SLOW TO RETRACT. REPLACED NOSE GEAR ACTUATOR.

Part: PCU — MALFUNCTIONED (LEFT) · airframe 28,926 hrs · 38,499 cycles

NP CONTINUOUS L 102.0, R 101.6-101.3 ON APPROACH, 30% TORQUE. (FLT 7762)REPLACED LEFT PROPELLER CONTROL UNIT.

Part: PCU — DEFECTIVE (RIGHT) · airframe 28,890 hrs · 38,455 cycles

IN ALL PHASES OF FLIGHT, AND AT SEVERAL DIFFERENT TORQUE SETTINGS, IF CONDITION LEVERS ARE MAX RPM, NP IS 101.5 PERCENT TO 102.5 PERCENT RT SIDE. FLT 7768. REPLACED RIGHT PCU. P/N: 782490-46, S/N ON: 981074, S/N OFF: 950741.

Part: LIGHT — BROKEN (CABIN) · airframe 28,574 hrs · 38,079 cycles

EMERGENCY LIGHT STRIP IN AFT CABIN IS BROKEN. REINSTALLED LIGHT STRIP. OPS CHECK GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (ROW 7) · airframe 28,345 hrs · 37,760 cycles

THE O2 MASK AT ROW 7 DROPPED IN FLIGHT. (FLIGHT NR 5473) INSPECTED AND RESTOWED O2 MASKS AS REQUIRED.

Part: A/C PACK — ODOR (LEFT) · airframe 28,058 hrs · 37,382 cycles

THE LT PACK FAILED AND A BURNING SMELL WAS NOTED. (FLT 5476) INSPECTED AND WASHED LT PACK HEAT EXCHANGER ASSEMBLY. OPS CHECK GOOD AT THIS TIME.

Part: CONNECTOR — CONTAMINATED (PROP SYNC) · airframe 27,906 hrs · 37,162 cycles

FLT 3605 - RIGHT PROP NP WAS FLUCTUATING IN FLIGHT. INSPECTED AND CLEANED OIL FROM RIGHT PROP SYNC PICK-UP SENSOR CONNECTOR. OPS CHECK GOOD IAW EMB 120 MM 61-24-00.

Part: O-RING — UNKNOWN (PROPELLER) · airframe 27,830 hrs · 37,062 cycles

FLT 5747 - THE RIGHT PROPELLER NP EXCEEDED 100 PERCENT. REPLACED RIGHT PROP TRANSFER TUBE O-RINGS. OPS CHECKS GOOD PER AMM 61-00-00.

Part: PCU — OUT OF ADJUST (RIGHT) · airframe 27,623 hrs · 36,788 cycles

FLT 5504 - ON CLIMB-OUT, RIGHT NP INCREASED TO 104 PERCENT. ADJUSTED PROPELLER PCU IAW HAMILTON STANDARD 61-22-00. OPS CHECK GOOD.

Part: BUSHING — BINDING (PAX DOOR) · airframe 27,245 hrs · 36,316 cycles

FLT 3726 - PAX DOOR IS HARD TO OPEN AND CLOSE FROM INSIDE AIRCRAFT. REPLACED INTERMEDIATE TORQUE TUBE BUSHINGS IN PAX DOOR IAW 52-11-00. OPS CHECK GOOD.

Part: STOP — OUT OF ADJUST (PAX DOOR) · airframe 26,722 hrs · 35,620 cycles

FLT 5774 - MAIN CABIN DOOR IS DIFFICULT TO OPEN. ADJUSTED MAIN CABIN DOOR BACKSTOPS IAW MM 52-11-00.

Part: SUPPORT BRACKET — CRACKED (PAX DOOR) · airframe 26,390 hrs · 35,156 cycles

CRACK ON PAX DOOR AFT SIDE NEAR 4TH SHIM STOP, DISCOVERED AT C-CHECK. REPLACED PAX DOOR AFT MID CLEAT SUPPORT BRACKET IAW 120 SRM 51-10-02 PG 3, SEC 3.

Part: STRINGER — CRACKED (RT WING) · airframe 26,390 hrs · 35,156 cycles

RIGHT WING, NR 2 FUEL PANEL, FORWARD STRINGER IS CRACKED, FOUND AT C-CHECK. APPLIED STRINGER SPLICE SECTION IAW SRM 120 57-20-03.

Part: ANNUNCIATOR — MALFUNCTIONED (TE FLAPS) · airframe 24,532 hrs · 32,559 cycles

OUTBOARD FLAPS FAILED TO RETRACT FULLY ON DEPARTURE. RETURNED TO SFO. REMOVED MOISTURE FROM LEFT OUTBOARD FLAP ACTUATOR CONNECTOR AND REPLACED FLAP COMPUTER AND ANNUNCIATOR WITH SERVICEABLE UNITS. OPERATIONAL CHECKS GOOD. FLAP COMPUTER PN ON 347200-1001 OFF 0061.

Part: ACTUATOR — MALFUNCTIONED (T/E FLAP) · airframe 24,532 hrs · 32,559 cycles

ON DEPARTURE, HAD A FLAP DISAGREEMENT. RETURNED TO RDD. REPLACED LEFT NACELLE FLAP ACTUATOR IAW EMB 120 MM 27-50-03 AND RII 27-900-1005. OPERATIONAL CHECKS GOOD.

Part: APU — SMOKE · airframe 24,344 hrs · 32,333 cycles

APU BLEED CAUSING SMOKE IN CABIN. REMOVED AND REPLACED APU IAW RII 49-300-1000. OPERATIONAL CHECKS GOOD.

Part: UNKNOWN — SMOKE (CABIN) · airframe 24,286 hrs · 32,251 cycles

APU BLEED CAUSING SMOKE IN THE CABIN. INSPECTED BLEED AIR DUCT ON APU. UNABLE TO DUPLICATE DISCREPANCY. OPERATIONAL CHECKS GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 23,628 hrs · 31,356 cycles

EMERGENCY EXIT LIGHTS AT ROW 9 EXIT INOP. REPLACED AFT EMERGENCY BATTERY ASSY. OPERATIONAL CHECK GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 23,617 hrs · 31,340 cycles

LAV SMOKE DETECTOR SOUNDS INTERMITTENTLY. REPLACED FAULTY DETECTOR. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (LAVATORY) · airframe 23,470 hrs · 31,141 cycles

SMOKE DET IN LAV SOUNDS CONTINIOUSLY. REPLACED BATTERY IN LAV. OPERATIONAL CHECK GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 23,470 hrs · 31,141 cycles

LAV SMOKE DETECTOR GOES OFF. REPLACED DETECTOR. OPERATIONAL CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 23,432 hrs · 31,100 cycles

FO WINDSHIELD CRACKED RIGHT SIDE. REPLACED RIGHT WINDSHIELD IAW 56-10-01, PN NP-151311-2 SN OFF 96026H2228.

Part: ACTUATOR — INOPERATIVE (RUDDER) · airframe 22,611 hrs · 30,036 cycles

ON TAKEOFF, RUDDER JAMMED. REPLACED RUDDER BLUE SYSTEM ACTUATOR IAW MM 27-22-00. OPERATIONAL CHECK GOOD.

Part: SERVO — BINDING (AILERONS) · airframe 22,406 hrs · 29,792 cycles

ROUGHNESS IN CONTROL YOKE WHEN MOVING AILERONS FROM CENTER TO THE LT. REPLACED AILERON AUTO-PILOT SERVO IAW 22-10-05. OPERATIONAL CHECK GOOD.

Part: SMOKE — DETECTED (LAVATORY) · airframe 22,197 hrs · 29,526 cycles

LAV SMOKE DETECTOR WENT OFF IN FLIGHT, F/A NOTICED SMOKEY ODOR. INSPECTED LAVATORY AND GALLEY LIGHT ASSYS. NO DEFECTS NOTED. ALSO INSPECTED CARGO AREA. NO PROBLEMS FOUND. NO SMOKE ODOR FOUND PRESENT.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 21,761 hrs · 28,973 cycles

ROW 9 EMERGENCY LIGHT BULB IS INOPERATIVE. REPLACED BULB AT ROW 9, FORWARD RED, EMERGENCY LIGHT AT FLOOR TRACK. OPERATIONAL CHECK GOOD.

Part: SMOKE — DETECTED (CABIN) · airframe 21,506 hrs · 28,596 cycles

F/A REPORTED LIGHT SMOKE AND BURNING SMELL DURING DESCENT IN BOTH AUTO & LOW. RAN RIGHT AND LEFT PACKS ON GROUND FROM APU BLEED. NO SMOKE NOTED AT THIS TIME.

Part: ACM — SMOKE · airframe 21,391 hrs · 28,461 cycles

ON DESCENT, WITH BLEED AND PACKS SELECTED ON AUTO AND LOW, RIGHT PACK FAIL INDICATION, SLIGHT SMELL OF SMOKE IN FLIGHT DECK AND CABIN. REMOVED AND REPLACED RIGHT ACM IAW EMB 120 MM 21-50-05, OPERATIONAL CHECK GOOD.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 21,151 hrs · 28,146 cycles

MAIN CABIN DOOR VERY DIFFICULT TO OPEN. LUBRICATED MAIN DOOR.

Part: LIGHT — LOOSE (CABIN) · airframe 21,030 hrs · 28,007 cycles

ONE EMERGENCY LIGHT ROW 9 CAME LOOSE. REPLACED DAMAGED RED EMERGENCY FLOOR LAMP IN ROW 9 IAW 33-50-00. OPERATIONAL CHECK GOOD.

Part: HEADSET — SMOKE (INTERPHONE) · airframe 20,828 hrs · 27,761 cycles

F/A REPORTS SMOKE COMING FROM INTERPHONE IN AFT GALLEY. REPLACED AFT ATTENDANT HEADSET IAW MM 23-41-01. OPERATIONAL CHECK GOOD.

Part: LIGHT — SMOKE (CABIN) · airframe 20,710 hrs · 27,619 cycles

MIDDLE STORM LIGHT SMOKES AT THE LEADS WHEN OPERATED. REPLACED MIDDLE STORM LIGHT IAW 33-21-02, OPERATIONAL CHECK GOOD. P/N 10-21C22-513, S/N OFF 151.

Part: BALLAST — SMOKE (LAV LIGHT) · airframe 20,540 hrs · 27,422 cycles

DURING PASSENGER DEPLANING, MOMENTARILY SMELLED SMOKE AND NOTICED C/B A30 POPPED. REPLACED LAV LIGHT BALLAST AND RESET BREAKER A30, OPERATIONAL CHECK GOOD.

Part: STRINGER — CRACKED (LT NACELLE) · airframe 20,014 hrs · 26,782 cycles

LEFT NACELLE EXHAUST CRADLE STRINGER CRACKED INBOARD SIDE. ITEM FOUND AT C-CHECK. REPLACED LEFT HAND NACELLE EXHAUST CRADLE STRINGER INBOARD SIDE PER SRM 51-40-00.

Part: INDICATOR — FAILED (RADO ALTIMETER) · airframe 19,869 hrs · 26,581 cycles

BUZZING SOUND AND SMOKE FROM LEFT SIDE INSTRUMENT PANEL. PULLED CIRCUIT BREAKER ON RADIO ALTIMETER, NOISE STOPPED. REPLACED RADIO ALTIMETER WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 19,558 hrs · 26,186 cycles

DURING TAXI-IN, RECEIVED SPORADIC TRIPLE CHIME TAKEOFF TRIM WITH TRIM IN GREEN BAND. PERFORMED TEST AFTER SHUT DOWN AND DID NOT PASS. RERACKED AURAL WARNING UNIT AND RESET AURAL WARNING CB. OPS CHECKS GOOD.

Part: WIRE — BROKEN (STALL WARNING) · airframe 19,169 hrs · 25,716 cycles

NO STICK SHAKER RIGHT SIDE. REPAIRED BROKEN WIRE. OP CHECK OK.

Part: SHAFT — DAMAGED (YOKE) · airframe 18,573 hrs · 25,015 cycles

TRIED TO MOVE YOKE TO THE LT AND IT WAS BOUND UP AND WOULD NOT GO TO THE LT. REPLACED BELLCRANK SHAFT IAW MM 31-30-10. OPS CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (RUDDER) · airframe 17,609 hrs · 23,778 cycles

RIGHT RUDDER LIMITED TO APPROXIMATELY 1/3 OF FULL TRAVEL DURING INITIAL CLIMB. RUDDER WORKS CORRECTLY WITH BLUE SYSTEM SWITCH TURNED OFF. REMOVED AND REPLACED BLUE SYSTEM RUDDER ACTUATOR IAW EMB 120 MM 27-22-02. OPS CHECK GOOD IAW EMB MM 27-20-00. NO DEFECTS NOTED. S/N OFF 0671.

Part: SEAL — CONTAMINATED (EMERGENCY EXIT) · airframe 17,525 hrs · 23,685 cycles

AIRCRAFT DID NOT PRESSURIZE ON TAKEOFF. TRIED BOTH AUTO AND MANUAL. RETURNED TO SLC. CLEANED DEBRIS FROM THE SEAL AROUND THE LEFT OVERWING EXIT. PRESSURIZED THE AIRCRAFT. BOTH AUTO AND MANUAL PRESSURE CHECKS GOOD.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 17,456 hrs · 23,608 cycles

PAX 02 MASKS DEPLOYED IN FLIGHT CLIMBING THROUGH 8,000 FEET. NOTICED DELTA-P WAS AT 7,000 FT AND THE CABIN WAS LESS THAN ZERO. REMOVED AND REPLACED ALTITUDE CONTROLLER IAW MM 21-30-01. OPS CHECK GOOD, NO DEFECTS NOTED.

Part: ACTUATOR — LEAKING (NACELLE FLAP) · airframe 17,432 hrs · 23,578 cycles

UPON DEPLOYING FLAPS 15 DEGREES, FLAPS DISAGREEMENT LIGHT CAME ON, FOLLOWED BY LOW LEVEL LIGHT FOR RT/BLUE HYDRAULIC PUMP, LOW PRESS, MAIN PUMP LOW PRESS AND ELECTRIC PUMP LIGHT. UPON POSTFLIGHT, FOUND SIGNIFICANT FLUID LEAK. REMOVED AND REPLACED RIGHT NACELLE FLAP ACTUATOR IAW EMB 120 MM 27-50-00. REPLACED RT ENGINE DRIVEN PUMP AND ALL FOUR FILTERS IAW EMB120 MM 29-10-00. OPS AND LEAK CHECK GOOD.

Part: BATTERY — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 17,421 hrs · 23,566 cycles

EMERGENCY LIGHTS EXIT LIGHT ARE INOP ABOVE 5C AND 5A. REMOVED AND REPLACED NR 2 MID EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-02. OPS CHECK GOOD.

Part: LIGHT — SMOKE (COCKPIT) · airframe 16,451 hrs · 22,416 cycles

CAPTAIN'S FLOODLIGHT SMOKES WHEN THE LIGHT IS ON. REPLACED CAPTAIN'S FLOODLIGHT FIXTURE WITH SERVICEABLE UNIT.

Part: WIRE — MISSING (CABIN) · airframe 16,356 hrs · 22,286 cycles

FORWARD EMERGENCY LIGHT EXIT SIGN DOES NOT ILLUMINATE. FOUND WIRE MISSING FROM REAR TERMINAL BLOCK. REINSTALLED WIRE FOR FORWARD EMERGENCY LIGHT WITH NEW HARDWARE. COMPLIED WITH OPS CHECK OF LIGHT AND FOUND OK.

Part: PROXIMITY SENSOR — FAULTY (ELEVATOR TAB) · airframe 15,253 hrs · 20,998 cycles

DURING TAKEOFF, TRIM AURAL WARNING SOUNDED. TAKEOFF WAS ABORTED. TRIM SETTING WAS 34. EVEN WITH TRIM IN MIDDLE OF GREEN BAND, AURAL WARNING SOUNDED. REMOVED AND REPLACED BOTH RIGHT AND LEFT ELEVATOR TRIM TAB PROX SENSORS. OPS CHECKS GOOD.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 15,330 hrs · 21,086 cycles

BOTH CENTER CROSS BEAMS ADJACENT TO CENTER OMEGA BEAM AT LAV AREA HAVE DEEP PITTING AND INTERGRANULAR CORROSION. REMOVED AND REPLACED BOTH CENTER CROSS BEAMS IAW SRM 51-40-02.

Part: BUTT STRAP — CORRODED (FUSELAGE) · airframe 15,330 hrs · 21,086 cycles

RIGHT SIDE BUTT STRAP A BEAM LAV HAS DEEP PITTING AND INTERGRANULAR CORROSION. REMOVED AND REPLACED RIGHT SIDE BUTT STRAP IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,281 hrs · 21,031 cycles

RIGHT SIDE SEAT TRACK IN FORWARD CABIN AREA HAS CORROSION AROUND SEVERAL SCREWS. REMOVED AND REPLACED RIGHT SIDE FORWARD FLOOR SEAT TRACK IAW 53-01-05.

Part: BUTT STRAP — CORRODED (FUSELAGE) · airframe 15,281 hrs · 21,031 cycles

CENTER BUTT STRAPS A BEAM LAV HAVE DEEP PITTING AND INTERGRANULAR CORROSION. REMOVED AND REPLACED (2) CENTER BUTT STRAPS IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,281 hrs · 21,031 cycles

CENTER OMEGA BEAM AT BUTT STRAP SPLICE A BEAM LAV HAS VISIBLE CORROSION EXTENDING MORE THAN 10 PERCENT INTO MATERIAL. REMOVED AND REPLACED THE CENTER OMEGA BEAM IAW SRM 51-40-02.

Part: SMOKE — DETECTED (CABIN) · airframe 14,435 hrs · 20,025 cycles

DUE TO REPORT OF SMOKE IN THE LAV AREA AND SMOKE DETECTOR GOING OFF CONTINUOUSLY FOR THREE MINUTES INFLIGHT, INSPECT CABIN FOR SOURCE OF SMOKE AND CORRECT ANY DISCREPANCIES. LAV SMOKE DETECTOR ALARM SOUNDED DURING CRUISE. F/A AND PAX SMELLED SMOKE. ALARM SOUNDED AROUND 3 MINUTES. SMOKE SMELL WENT AWAY DURING DESCENT. INSPECTED AIRCRAFT FOR ELECTRICAL AND HEAT DAMAGE OR SIGNS OF MALFUNCTION THAT WOULD CAUSE SMOKE OR SMELL OF SMOKE IN CABIN, NONE FOUND. OPERATIONAL CHECK OF ALL LOCAL SYSTEMS CHECKS GOOD.

Part: RELAY — ODOR (COCKPIT) · airframe 12,918 hrs · 17,923 cycles

STRONG ELECTRICAL SMELL COMING FROM UNDERNEATH FIRST OFFICERS SHELF. THE SHELF IS ALSO VERY HOT. FOUND AP FEEDER PROTECTION RELAY WARM. REPLACED APU FEEDER PROTECTION RELAY. OPS CHECK OF APU AND GENERATOR GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 11,346 hrs · 15,730 cycles

FIRST OFFICER''S TRIM FAIL WARNING ANNUNCIATED DURING TAKEOFF. TAKEOFF ABORTED. AUTO PILOT RED MAP LIGHT ANNUNCIATED AS WELL. REPLACED F/O''S APC-65B WITH SERVICEABLE UNIT. OPS CHECKS GOOD ON GROUND. (P/N 622-8315-402), (S/N 32445) ON, (S/N 2947) OFF.

Part: CONTROL BOX — MALFUNCTIONED (MLG) · airframe 11,133 hrs · 15,430 cycles

ON APPROACH, PUT GEAR DOWN, LEFT DISPLAYED RED LIGHTS ONLY. NOSE AND RIGHT DISPLAYED NO RED OR GREEN LIGHTS. GEAR MADE A LOUD RACKET AND VIBRATION. RECYCLED GEAR UP AND BACK DOWN. GEAR EXTENDED NORMALLY WITH 6 GREEN LIGHTS. REPLACED LANDING GEAR CONTROL BOX. CYCLED GEAR MANY TIMES. OPS CHECKS NORMAL. S/N ON: 120282, S/N OFF: 120271.

Part: GENERATOR — FAILED (AUX SYSTEM)

AUXILLARY GENERATORS NUMBER ONE AND NUMBER TWO BOTH FAILED IN FLIGHT, WOULD NOT RESET. RETURNED TO LAX. RAN ENGINES, FOUND RIGHT AUXILLARY GENERATOR WORKING NORMAL.

Part: INVERTER — FAILED (NR 1&2)

DUAL INVERTER FAILURE. RETURNED TO PSP. REMOVED AND REPLACED NUMBER 1 AND NUMBER 2 INVERTERS. OPS CHECKS GOOD AT THIS TIME.

Part: UPLOCK HOOK — OUT OF ADJUST (LT MLG)

WHEN LANDING GEAR IS RETRACTED THE GEAR COMES UP AND THE DOORS CLOSE BUT THE LEFT MAIN GEAR UNSAFE LIGHT STAYS ILLUMINATED. RETRACTED LANDING GEAR AND CHECKED CLEARANCE OF ROLLER AND UPLOCK HOOK. ADJUSTED CLEARANCE IAW MM 32-61-01. LANDING GEAR OPS CHECKS GOOD.

Part: STRAP — CORRODED (CABIN)

RT FLOOR BUTT STRAP IN GALLEY/LAVATORY AREA HAS CORROSION. REPLACED BUTT STRAP WITH NEW ASSEMBLY AS REQUIRED PER SRM.

Part: STRAP — CORRODED (CABIN)

CENTER FLOOR BUTT STRAP IN GALLEY/LAVATORY AREA HAS CORROSION. REPLACED BUTT STRAP WITH NEW ASSEMBLY AS REQUIRED PER SRM.

Part: WARNING LIGHT — ILLUMINATED (LT EEC)

ON TAKEOFF ROLL, LEFT EEC FAILURE WARNING ILLUMINATED AND AURAL WARNING SOUNDED. WITH CONDITION LEVERS IN MININUM, LEFT RPM WAS 90 PERCENT UNTIL THE EEC WAS TURNED OFF, THEN LEFT RPM WAS NORMAL. ABORTED TAKEOFF. MEL 23-21-1. TROUBLESHOT SYSTEM. OHMED WIRES AND CHECKED PROBES IAW MM 76-10-00. RAN ENGINE THROUGH ALL PARAMETERS AND COULD NOT DUPLICATE PROBLEM AT THIS TIME.

Part: PCU — MALFUNCTIONED (RT ENGINE)

ON CLIMBOUT, RT TORQUE GAUGE FLUCTUATES 80 PERCENT TO 105 PERCENT BOTH IN DIGITAL AND ANALOG WITH EEC'S IN MANUAL. REMOVED AND REPLACED RT ENGINE PCU. ALL GROUND RUNS AND LEAKS CHECKS IAW MM 61-00-00.