N232SW

Part: SIGN — FRACTURED (EMERGENCY LIGHTS) · airframe 29,347 hrs · 41,537 cycles

FLT 7816 - LIGHT "EXIT" SIGN NEXT TO MAIN DOOR FIXTURE IS BROKEN. REPLACED MAIN DOOR LIGHTED "EXIT" SIGN.

Part: TARGET — OUT OF ADJUST (LT MLG) · airframe 28,782 hrs · 40,854 cycles

LEFT MAIN WOULD NOT RETRACT. FOUND TARGET BACKED OFF ON LEFT GEAR. ADJUSTED TARGET.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,749 hrs · 40,813 cycles

EMERGENCY LIGHT STRIP HAS TWO LIGHT BULBS NOT WORKING. FLIGHT 3581. REPLACED EMERGENCY LIGHTING BATTERY PACK NR 1. OPS CHECK GOOD. P/N D366-04-001, S/N OFF 1164.

Part: ACTUATOR — LEAKING (TE FLAPS) · airframe 28,710 hrs · 40,769 cycles

RIGHT HYDRAULIC QUANTITY WENT TO ZERO ON TAXI OUT AFTER SELECTING FLAPS. REPLACED RIGHT NACELLE FLAP ACTUATOR IAW MM 27-50-00. P/N 343100-1001, S/N OFF 235.

Part: STRINGER — CRACKED (LT WING) · airframe 28,492 hrs · 40,480 cycles

FOUND STRINGER 10 AT RIB 9 TO BE CRACKED INSIDE LT IB NR 1 FUEL PANEL. PERFORMED REPAIR TO STRINGER 10 AT RIB 9 IAW SRM 57-20-03.

Part: SENSOR — FAILED (A/C PACK) · airframe 28,160 hrs · 40,038 cycles

DURING CRUISE, FLIGHT ATTENDANT REPORTED A BURNING SMELL IN THE CABIN FOLLOWED BY AN INTERMITTENT RIGHT "DUCT OVERHEAT" LIGHT ON OVERHEAD PANEL. FLIGHT 3628 - REPLACED RIGHT PACK TEMP SENSOR FOR AUTO CONTROL. OPS CHECK GOOD IAW 21-60-04.

Part: WIRE — FAILED (GALLEY LIGHTS) · airframe 28,000 hrs · 39,817 cycles

FLT 5570 - ELECTRICAL SMOKE REPORTED IN THE GALLEY AREA. REPAIRED GALLEY LIGHT WIRING AND REPLACED LIGHT BULB IAW MM 33-21-05. OPS CHECK GOOD.

Part: SIGN — MISSING (CABIN) · airframe 27,803 hrs · 39,570 cycles

PAX DOOR EMERGENCY EXIT SIGN IS MISSING. INSTALLED SERVICEABLE EXIT SIGN.

Part: BUSHING — BINDING (PAX DOOR TQ TUBE) · airframe 27,154 hrs · 38,726 cycles

FLT 3664 - MAIN CABIN DOOR HANDLE IS VERY DIFFICULT TO OPEN AND CLOSE. REPLACED CENTER ROD TORQUE TUBE BUSHINGS. OPS CHECK GOOD IAW MM 52-11-05.

Part: UNKNOWN — SMOKE (CABIN) · airframe 26,889 hrs · 38,374 cycles

FLT 5749 - ON DESCENT, THE CABIN FILLED WITH SMOKE AND THE LAV SMOKE DETECTOR WENT OFF. RAN AIRCRAFT TO FLIGHT CONFIGURATION WITH ENGINES AND PACKS TO FULL POWER. COULD NOT DUPLICATE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 26,758 hrs · 38,196 cycles

FLT 5473 - AFT EMERGENCY LIGHTS NOT WORKING. REPLACED AFT ELBP. OPS CHECK GOOD AT THIS TIME.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 26,696 hrs · 38,114 cycles

FLT 3708 - SEVERAL EMERGENCY LIGHTS IN THE CABIN ARE INOP. REPLACED AFT ELBP IAW 33-50-02. LIGHTING OPS CHECK GOOD AT THIS TIME.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 26,413 hrs · 37,792 cycles

FORWARD EMERGENCY LIGHTS DO NOT ILLUMINATE, FLIGHT NR 3696. REMOVED AND REPLACED ELBP 1 AND 3. OPS CHECK GOOD. NR 3 P/N D366-04-001, S/N ON 1121, OFF 1268/08-96, NR 1 P/N D366-04-001, S/N ON 489 OFF 794/10-90.

Part: RIB — CRACKED (PAX DOOR) · airframe 26,140 hrs · 37,479 cycles

PAX DOOR TORQUE TUBE FORWARD ATTACH RIB IS CRACKED, DISCOVERED AT C-CHECK. REPLACED CRACKED RIB PER SRM 51-40-02.

Part: SUPPORT — CRACKED (LT NACELLE) · airframe 25,514 hrs · 36,675 cycles

FOUND LEFT NACELLE WHEEL WELL LOWER SUPPORT FRAME (STRINGER NR 1) IS CRACKED, DISCOVERED DURING ROUTINE INSPECTION. REPLACED LOWER OUTBOARD SUPPORT FRAME IAW EMB 120 SRM 51-10-02.

Part: OIL COOLER — MALFUNCTIONED (LT ENGINE) · airframe 24,194 hrs · 34,896 cycles

SHUTDOWN LEFT ENGINE AND DIVERTED TO CDC AFTER LOSS OF OIL PRESSURE. REPLACED LINE ON LEFT ENGINE OIL COOLER.

Part: WIRE — BROKEN (RT MLG) · airframe 24,042 hrs · 34,715 cycles

AT ALTITUDE STARTED LOSING PRESSURIZATION IN AUTO MODE. SWITCHED TO MAN AND ALSO HAD NO CONTROL. FORCED FULL 2000FPM DOWN. REPAIRED BROKEN WIRING AT RIGHT MLG SHOCK STRUT. OPERATIONAL CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 22,740 hrs · 33,014 cycles

FOUND CENTER EMERGENCY LIGHTS INOP. REPLACED ELBP IAW AMM 33-50-02, OPERATIONAL CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,541 hrs · 32,767 cycles

ROW 9 OVERHEAD LIGHT INOP. REPLACED EXIT LAMP ASSY IAW33-60-00. OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,719 hrs · 31,664 cycles

ONE FLOOR LEVEL EMERGENCY LIGHT FAILS TO ILLUMINATE. RELAMPED ONE FLOOR LEVEL EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 21,638 hrs · 31,545 cycles

FORWARD BULB INOPERATIVE ON EMERGENCY TRACK LIGHTING. REPAIRED BROKEN WIRE AS REQUIRED. OPERATIONAL CHECK GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (STALL WARNING) · airframe 21,188 hrs · 30,891 cycles

ON FFOD STALL WARNING TEST, PUSHER IS INOP ON BOTH SIDES AND POPS BOTH PUSHER CIRCUIT BREAKERS (D31 & D32). REMOVED AND REPLACED THE STALL WARNING CONTROL PANEL. SYSTEMS BOTH CHECK GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 20,758 hrs · 30,224 cycles

RED FLOOR LIGHTING MISSING AT EXIT 9B AND 9C. INSTALLED NEW RED EMERGENCY LIGHTING FLOOR RECEPTACLE IAW EMB 120 MM 33-52-01. READJUSTED EMERGENCY FLOOR LIGHTING COVER AND REPAIRED SECOND FORWARD RED LAMP. OPERATIONAL CHECK GOOD IAW 33-51-00.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 20,657 hrs · 30,065 cycles

EMERGENCY FLOOR LIGHTING SYSTEM HAS ONE BULB INOPERATIVE. REMOVED AND REPLACED BROKEN SPLICE WITH NEW ENVIRONMENTAL SPLICE, OPERATIONAL CHECKS GOOD.

Part: RELAY — FAULTY (EMERGENCY LIGHT) · airframe 20,361 hrs · 29,574 cycles

EMERGENCY FLOOR LIGHT (RED) BULB AT MAIN CABIN DOOR DOES NOT ILLUMINATE. REMOVED AND REPLACED RELAY K00913. OPERATIONAL CHECK GOOD.

Part: ANNUNCIATOR — MALFUNCTIONED (TE FLAPS) · airframe 19,856 hrs · 28,789 cycles

ON LANDING EXTENDING FLAPS TO 25 DEGREES, GOT CONTROL FAULT ON OUTBOARD FLAPS. REPLACED FLAP ANNUNICIATOR. OPS CHECKS GOOD. S/N OFF: 0171.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 19,341 hrs · 27,999 cycles

WHEN FIRST POWER UP A/C RECEIVED A CONTROL FAULT ON FLAP. REPLACED FLAP CONTROL UNIT PER MM 27-50-00. OPS CHECK OK.

Part: BRACKET — CRACKED (LT WING) · airframe 19,208 hrs · 27,794 cycles

LEFT INBOARD WING, BRACKET CRACKED AT RIB STATION 8 AFT LOWER OUTBOARD ACCESS PANEL, MARKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED BRACKET AT RIB STATION NR 8 AFT OF OUTBOARD FUEL ACCESS PANEL PER SRM 51-40-02. NO LEAKS AT THIS TIME.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 19,208 hrs · 27,794 cycles

FRAME 12 BRACKET BEHIND PILOT'S DV WINDOW IS CRACKED AT FLANGE HOLE. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INTERCOSTAL AT FRAME NR 12 BEHIND PILOT'S DV WINDOW PER EMB120 SRM 51-40-02.

Part: SEQUENCE VALVE — OUT OF ADJUST (LT MLG) · airframe 18,464 hrs · 26,641 cycles

UPON SELECTING GEAR DOWN RIGHT MAIN EXTENDED NORMALLY, NOSE GEAR ABOUT 5-10 SECONDS LATER, LEFT MAIN INDICATED RED LIGHTS ONLY THEN NORMAL AFTER 45 SECONDS TO 1 MINUTE, THE GEAR WAS FELT THUD COINCIDING WITH GEAR DOWN INDICATION. ADJUSTED LEFT OUTBOARD SEQUENCE VALVE. OPS CHECKS GOOD.

Part: PUMP — FAILED (LT ENGINE) · airframe 16,663 hrs · 23,888 cycles

GREEN SYSTEM MAIN HYDRAULIC PUMP FAILED ON TAKEOFF. ELECTRONIC PUMP TOOK OVER. COMPLIED WITH QRH. RETURNED FOR NORMAL LANDING AT SFO. REPLACED LEFT ENGINE MAIN HYDRAULIC PUMP. RAN ENGINE. OPS & LEAK CHECK GOOD.

Part: CONNECTOR — DIRTY (FLAP ACTUATOR) · airframe 16,025 hrs · 22,913 cycles

RECEIVED FLAP CONTROL FAULT ON TAXI WHEN FLAPS 15 IS SELECTED. COMPLIED WITH QRH PROCEDURES AND PROBLEMS STILL EXISTED. CLEANED CANNON PLUG ON OUTBOARD FLAP ACTUATOR. POWERED DOWN SYSTEM. REMOVED FCU. CHECKED CONNECTIONS, REINSTALLED FCU. OPERATED FLAP SYSTEMS THROUGH ALL MODES OF OPERATIONS. NO DEFECTS NOTED.

Part: SWITCH — OUT OF ADJUST (PAX DOOR) · airframe 15,686 hrs · 22,367 cycles

FORWARD DOOR LIGHT ILLUMINATED ON TAKEOFF. RETURNED TO MRY. ADJUSTED FORWARD DOOR LOWER MICROSWITCH. OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (T/E FLAP) · airframe 15,415 hrs · 22,002 cycles

WHEN SETTING FLAPS TO 15 DEGREES FOR TAKEOFF, FLAP/CONTROL FAULT ILLUMINATED AND WILL NOT RESET. REPLACED THE FLAP COMPUTER WITH A SERVICEABLE UNIT. OPS CHECK OF FLAP SYSTEM IS NORMAL.

Part: WIRE — DISCONNECTED (CABIN) · airframe 15,312 hrs · 21,823 cycles

EMERGENCY POD LIGHT IN 6A IS INOP. FERRIED UNDER SPECIAL FLIGHT PERMIT FORM MOD TO SFO. FOUND BOTH WIRES NOT CONNECTED TO THE SOCKET ON OVERHEAD EMERGENCY LIGHT ASSEMBLY SEAT 6A. RECONNECTED WIRES. OPS CHECK GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,389 hrs · 21,954 cycles

RIGHT SIDE UPPER SEAT TRACK HAS SIGN OF CORROSION AT SCREW HOLES AND NEEDS REPLACED. REMOVED AND REPLACED RIGHT SIDE UPPER SEAT TRACK WITH NEW AS REQUIRED IAW EMB120 MM 53-01-04.

Part: FRAME — CRACKED (RT NACELLE) · airframe 15,389 hrs · 21,954 cycles

RIGHT ENGINE FRAME NR 1 CRACKED. REPLACED RIGHT FRAME NR 1 IAW SB 120-54-0036 REV 02.

Part: FRAME — CRACKED (LT NACELLE) · airframe 15,389 hrs · 21,954 cycles

LEFT ENGINE FRAME NR 1 CRACKED. REPLACED LEFT FRAME NR 1 IAW SB 120-54-0035 REV 02.

Part: COMPUTER — FAULTY (NR 2) · airframe 15,258 hrs · 21,732 cycles

AFTER DEPARTURE FIRST OFFICER'S EHSI DISPLAY WENT BLANK. RETURNED TO LAX. REMOVED AND REPLACED NR 2 HPU74 WITH SERVICEABLE UNIT. OPS CHECK GOOD.

Part: ACCESS PANEL — LOOSE (WING) · airframe 14,360 hrs · 20,358 cycles

STRONG FUEL SMELL IN AIRCRAFT WITH AIR CONDITIONER TURNED ON DURING ENGINE OPERATION.FOUND LOOSE SCREWS ON LEFT INBOARD WING FUEL CELL ACCESS PANEL CAUSING FUEL TO ENTER PACK AREA DURING ENGINE OPERATIONS. SECURED ACCESS PANEL AND RAN ENGINES WITH PACKS OPERATING. NO FURTHER SMELL NOTED. OPS AND LEAK CHECK GOOD.

Part: ACTUATOR — LEAKING (T/E FLAP) · airframe 13,917 hrs · 19,722 cycles

LOST ALL HYDRAULIC BLUE SYSTEM FLUID. LOW PSI, LOW RESERVOIR WARNING LIGHTS. MAIN PUMP LOW PRESSURE INDICATION FOR BLUE SYSTEM. RETURNED TO SFO. REPLACED LEFT NACELLE FLAP ACTUATOR PER MM 27-50-00 AND CHECKED BLUE SYSTEM HYDRAULIC FILTERS. ALL CHECKS GOOD.

Part: INVERTER — MALFUNCTIONED (E/E BAY) · airframe 12,132 hrs · 17,111 cycles

GYRO AND COMPUTER ON ADI (BOTH), HEADING ON BOTH HSI. RETURNED TO FAT. FOUND DISCREPANCY TO CLEAR WITH NUMBER ONE INVERTER TURNED OFF. REPLACED NUMBER ONE INVERTER. OPS CHECKS GOOD AT THIS TIME. P/N ON: PC251-1C, S/N: 6074, S/N OFF: 8356.

Part: GYRO — FAILED (COCKPIT) · airframe 12,114 hrs · 17,082 cycles

AT TAKEOFF, FIRST OFFICER''S GYRO AND COMPUTER FLAGS CAME OUT. LOST FIRST OFFICER''S ATTITUDE INDICATOR AND HEADING. RETURNED TO LAX. REPLACED NUMBER ONE INVERTER. OPS CHECKS GOOD. S/N: 8356, S/N OFF: 7164.

Part: COMPUTER — FAILED (AHRS) · airframe 11,864 hrs · 16,733 cycles

CO-PILOT AHRS MALFUNCTIONING INCLUDING TCAS AND AUTO PILOT. RETURNED TO SFO. REPLACED NUMBER TWO AHRS COMPUTER AND REINITIALIZED SYSTEM. OPS CHECKS GOOD. P/N ON: 622-6190-204, S/N: 1103, S/N OFF: 2096.

Part: SWITCH — FAILED (RT STABILIZER)

RIGHT INBOARD STABILIZER BOOT FAILS. RETURNED TO FIELD. REPLACED PRESSURE SWITCH FOR RIGHT INBOARD STABILIZER. OPS CHECKS GOOD.

Part: STRAP — CORRODED (CABIN)

CORROSION ON CENTER AFT OMEGA BEAM BUTT STRAP EXCEEDS 10 PERCENT OF STRAP THICKNESS. REMOVED THE CORROSION PORTION OF THE BUTT STRAP AND INSTALLED NEW MATERIAL IAW SRM 51-40-02.

Part: TQ SIGNAL COND — FAILED (RT ENGINE)

ON INITIAL CLIMB, RIGHT TORQUE GAUGE FLUCTUATED DRAMATICALLY WITH NO ACCOMPANING YAW. THIS WAS FOLLOWED BY RIGHT PROPELLER INADVERTENT AUTO FEATHER. RETURNED TO PSP. CHANGED TORQUE SENSOR AND TORQUE SIGNAL CONDITIONER. RAN RIGHT ENGINE, OPS CHECKS GOOD.

Part: PROP HEAT — INOPERATIVE (NR 1 ENGINE)

LEFT PROPELLER HEAT INOP LIGHT ILLUMINATED. RETURNED TO FIELD. RESET CIRCUIT BREAKER ON LEFT PROPELLER HEATER. GROUND RAN NR 1 ENGINE, ALL OPS NORMAL.

Part: PRSSSURE SWITCH — FAILED (LT ENGINE)

LEFT ENGINE AIR INLET INOP LIGHT ILLUMINATED IN FLIGHT. RETURNED TO FIELD. REMOVED AND REPLACED LEFT ENGINE AIR INLET DE-ICE PRESSURE SWITCH, OPS CHECKS GOOD.

Part: DE-ICE MONITOR — MALFUNCTIONED (E/E COMPT)

DURING TAKEOFF ROLL, PRIOR TO ROTATION MAP DE-ICE LIGHT ILLUMINATES AS WELL AS OVERHEAD BOOTS PROPELLER AND ENGINE AIR LIGHT REMAIN ON. REPLACED DE-ICE MONITOR PERFORM OPS CHECKS GOOD. ALL DE-ICE SYSTEMS WITH BOTH ENGINE RUNNING AT HIGH POWER SETTING, OPS CHECKS GOOD AT THIS TIME.

Part: PRESS LINE — FAILED (GREEN HYD SYST)

GREEN HYDRAULIC SYSTEM FAILED IN-FLIGHT. WHEN EMERGENCY GEAR EXTENSION PROCEDURE WAS ATTEMPTED, GEAR WOULD NOT LOWER. GEAR DOORS WOULD NOT OPEN. ABNORMAL LANDING GEAR SEQUENCE WAS PERFORMED IN ORDER NUMEROUS TIMES. GEAR DOORS WERE NOTED CLOSED. REPLACED HYDRAULIC PRESSURE LINE AT GREEN SYSTEM PACK. SERVICED GREEN HYDRAULIC SYSTEM. OPERATED ELECTRIC AND ENGINE DRIVEN PUMPS. FOUND PRESSURE GOOD. REMOVED ALL FOUR FILTERS AT GREEN RESERVOIR. FOUND NO METAL CONTAMINATION ON FILTERS OR IN FLUID. CYCLED GEAR IN NORMAL CONDITION. ALL CHECKS GOOD. PERFORMED NUMEROUS EMERGENCY EXTENSIONS AND ALL CHECKD GOOD. NO LEAKS NOTED FROM LINE.

Part: PROX SWITCH — OUT OF ADJUST (LANDING GEAR)

AFTER TAKEOFF, RECEIVED RED LANDING GEAR LIGHTS. GREEN EXTINGUISHED. CYCLED GEAR 9-10 TIMES. RECEIVED COMBINATION OF A AND/OR B-SYSTEM RED LIGHTS ON ALL THREE GEARS. ADJUSTED PROXIMITY SWITCH TARGETS ON BOTH MAIN GEARS. OPERATIONAL CHECKS WERE GOOD.