N298SW

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,994 hrs · 43,208 cycles

FORWARD EMERGENCY LIGHTS DON'T STAY ON VERY LONG. (FLT 7755) REPLACED FORWARD EMERGENCY LIGHT BATTERY PACK. P/N D366-04-001, S/N OFF 915/03-91.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,580 hrs · 42,709 cycles

EMERGENCY LIGHTS ARE OUT AT ROW 6. (FLT 6452) REPLACED EMERGENCY LIGHTING BATTERY PACK NEAR ROW 6.

Part: SERVO — MALFUNCTIONED (AUTOPILOT SYS) · airframe 29,532 hrs · 40,171 cycles

ELEVATOR CONTROL JAMMED ON FFOD CHECKS. (FLT 6258) REPLACED ELEVATOR AUTO PILOT SERVO. P/N 622-5734-002, S/N OFF 8286.

Part: BEAM — CORRODED (PAX DOOR) · airframe 29,453 hrs · 40,072 cycles

CORROSION ON PASSENGER DOOR AT HORIZONTAL BEAM NEAR FORWARD HINGE ATTACH POINT. (C CHECK) REPLACED BEAM PER SRM.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 29,453 hrs · 40,072 cycles

SURFACE CORROSION UNDERNEATH THE LAV FLOOR BOARD. (C CHECK) REPLACED RIGHT OUTBOARD CORNER BUTT STRAP.

Part: SUPPORT — CRACKED (COCKPIT) · airframe 29,453 hrs · 40,072 cycles

CAPTAINS WINDOW HORIZONTAL SUPPORT CRACKED. (C CHECK) REPLACED SUPPORT PER SRM.

Part: STRINGER — CRACKED (LT WING) · airframe 29,453 hrs · 40,072 cycles

LEFT WING NR 10 STRINGER CRACKED. (C CHECK) REPAIRED PER SRM.

Part: STRINGER — CRACKED (RT WING) · airframe 29,453 hrs · 40,072 cycles

RIGHT INBOARD WING STRINGER CRACKED. (C CHECK) REPAIRED PER SRM.

Part: SKIN — CHAFED (NACELLE) · airframe 29,453 hrs · 40,072 cycles

RIGHT NACELLE WEBBED SKIN CHAFED. (C CHECK) REPLACED SKIN PER SRM.

Part: SKIN — CHAFED (NACELLE) · airframe 29,453 hrs · 40,072 cycles

LEFT AND RIGHT NACELLE WEBBED SKIN CHAFED. (C CHECK) REPLACED SKINS PER SRM.

Part: BUSHING — WORN (CABIN DOOR) · airframe 29,226 hrs · 39,804 cycles

MAIN CABIN DOOR HANDLE IS HARD TO OPEN AND CLOSE. (FLT 7761) REPLACED BUSHINGS IN BOTH TRANSLATION BELL CRANKS AND ADJUSTED ECCENTRICS PER AMM.

Part: SOLENOID VALVE — MALFUNCTIONED (FEATHERING SYS) · airframe 29,085 hrs · 39,618 cycles

NR 2 PROPELLER FEATHERED INADVERTENTLY AND THEN CAME OUT OF FEATHER. (FLT 6638) REPLACED RIGHT ENGINE FEATHER SOLENOID VALVE, REPAIRED GROUNDING WIRE TERMINAL, CLEANED CONNECTORS AT TORQUE SIGNAL CONDITIONER. ADJUSTED HALF TURN ON PCU CONTROL ROD.

Part: WIRE — LOOSE (CABIN) · airframe 27,768 hrs · 37,863 cycles

FLT 7774 - RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. RESECURED WIRE.

Part: UPLOCK HOOK — MISRIGGED (MLG DOOR) · airframe 26,952 hrs · 36,829 cycles

FLT 5739 - GEAR DISAGREEMENT INDICATION ILLUMINATED. RIGGED UPLOCK HOOK AND ROLLER.

Part: MECHANISM — LACK OF LUBE (PAX DOOR) · airframe 26,771 hrs · 36,598 cycles

FLT 5710 - PASSENGER DOOR DIFFICULT TO OPEN. CLEANED AND LUBE LOCKING MECHANISM.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 26,170 hrs · 35,822 cycles

EMERGENCY EXIT LIGHT AT ROW 9C INOP. FLIGHT 5561. REPLACED BULBS AS REQUIRED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 26,084 hrs · 35,705 cycles

UNDER FLOOR CROSSMEMBER AT ROW 9 MIDDLE RT CTR AREA IS CORRODED. (FOUND AT C-CHECK) REPLACED UNDER FLOOR CROSS MEMBER AT ROW 9 IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 26,084 hrs · 35,705 cycles

CENTER FRAME UNDER FLOOR BOARD AT ROW 10 HAS SURFACE CORROSION. (FOUND AT C-CHECK) REPLACED CENTER FRAME UNDER FLOOR BOARD AT ROW 10 IAW SRM 51-40-02.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 26,084 hrs · 35,705 cycles

PAX DOOR FRAME IS CRACKED UNDER AFT LOWER STOP. (FOUND AT C-CHECK) REPAIRED FRAME UNDER LOWER AFT STOP ON PAX DOOR IAW SRM 52-10-02.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 25,931 hrs · 35,512 cycles

RECEIVED CARGO SMOKE MESSAGE UPON APU START UP. REPLACED FORWARD CARGO SMOKE DETECTOR IAW EMB 120 MM 26-15-01. OPS CHECK GOOD.

Part: CONNECTOR — DIRTY (FIRE WARNING) · airframe 25,765 hrs · 35,279 cycles

CARGO FIRE "WARN" LIGHT STAYS ON AND WILL NOT TEST CORRECTLY. INSPECTED AND CLEANED CONNECTORS ON BOTH LEFT AND RIGHT CARGO FIRE BOTTLES. OPS CHECK GOOD.

Part: B-NUT — LOOSE (APU) · airframe 25,752 hrs · 35,267 cycles

WITH APU BLEED ON, THE CABIN SMELLS LIKE FUEL. TIGHTENED FUEL NOZZLE MANIFOLD B-NUT. NO LEAKS NOTED.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 25,720 hrs · 35,229 cycles

FLT 3619 - EMERGENCY EXIT SIGN AT ROW 9 IS INTERMITTENT. REPAIRED WIRING ON EMERGENCY LIGHT AT ROW 9. OPS CHECK GOOD.

Part: PLACARD — MISSING (EMERGENCY EXIT) · airframe 25,685 hrs · 35,187 cycles

FLT 3592 - EMERGENCY EXIT PLACARD MISSING FROM PAX DOOR AREA. REPLACED EMERGENCY EXIT SIGN. OPS CHECK GOOD.

Part: SIGNAL COND UNIT — MALFUNCTIONED (RT ENG TORQUE) · airframe 23,278 hrs · 32,301 cycles

ON CLIMB-OUT, RIGHT TORQUE WENT TO 118 PERCENT. REPLACED SIGNAL CONDITIONING UNIT IAW 77-11-01 AND TORQUEMETER PICKUP PROBE P/N 3116942-01 IAW 77-11-02 IAW 71-00-00. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENC Y LIGHT) · airframe 23,195 hrs · 32,205 cycles

FOUND FORWARD EMERGENCY LIGHT BATTERY PACK IS DEAD. REPLACED FORWARD EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 23,195 hrs · 32,205 cycles

FOUND EMERGENCY EXIT ROW LIGHT/SIGN ON 9B OVERHEAD BIN WILL NOT ILLUMINATE. REPAIRED WIRE ON EMERGENCY EXIT LIGHT AT ROW 9B/C OVERHEAD BIN. OPERATIONAL CHECKS GOOD.

Part: VALVE — FAILED (LT ENGINE) · airframe 22,485 hrs · 31,270 cycles

LEFT ENGINE DUCT LEAKAGE LIGHT AND DUCT LEAK ON MAP. PRECAUTIONARY ENGINE SHUT DOWN. RETURNED TO FIELD.REPLACED LEFT DEICE PRESSURE VALVE.

Part: SUPPORT — CRACKED (PAX DOOR STEP) · airframe 22,400 hrs · 31,138 cycles

PAX DOOR STEPS FORWARD SUPPORT FRAME CRACKED AT LOWER END, DISCOVERED DURING C-CHECK INSPECTION. NEW SUPPORT FRAME INSTALLED IAW SRM 120 51-10-02 ALSO IAW RII 52-800-1000.

Part: ATTACH FITTING — CRACKED (LT WING) · airframe 22,400 hrs · 31,138 cycles

2 CLEATS CRACKED INSIDE LT WING NR 5 FUEL CELL, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LT WING CLEATS AT NR 5 FUEL CELL IAW SRM 120 51-10-02 PG 3 SEC 3A ALSO IAW RII 28-900-1000.

Part: SKIN — CRACKED (FUSELAGE) · airframe 22,400 hrs · 31,138 cycles

CRACK ON LT FUSELAGE SKIN CLEAT JUST ABOVE AND FORWARD OF FORWARD CARGO DOOR TRACK, DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN CLEAT IAW SRM 51-10-02 PG 3 SEC 3H AND RII 53-800-1000.

Part: ARM — CORRODED (STEP ACTUATOR) · airframe 22,400 hrs · 31,138 cycles

CENTER PAX DOOR STEP ACTUATOR ARM CORRODED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CENTER PAX DOOR STEP ACTUATOR ARM WITH SERVICEABLE ARM IAW 57-13-00.

Part: BOSS — CORRODED (PAX DOOR) · airframe 22,400 hrs · 31,138 cycles

PAX DOOR INTERCONNECT MID TORQUE TUBE AFT BOSS CORRODED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED PAX DOOR INTERCONNECT MID TORQUE TUBE ASSY IAW 32-13-00.

Part: SUPPORT FITTING — CORRODED (PAX DOOR STEP) · airframe 22,400 hrs · 31,138 cycles

PAX DOOR LOWER STEP SUPPORT FITTING CORRODED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LOWER STEP SUPPORT FITTING IAW SRM 120 51-10-03 PG 3 SEC 3A ALSO IAW 52-800-1000.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 20,970 hrs · 29,182 cycles

AFT EMERG LIGHT ON FLOOR STRIP INOP. REPAIRED WIRE AT CONNECTOR. OPERATIONAL CHECK GOOD.

Part: HEAT EXCHANGER — SMOKE (RT A/C PACK) · airframe 20,779 hrs · 28,921 cycles

RIGHT PACK FILLS CABIN WITH SMOKE INFLIGHT. LAV SMOKE DETECTOR WENT OFF INFLIGHT. REPLACED RIGHT HEAT EXCHANGER IAW EMB 120 MM 21-50-03 AND REPLACED BATTERY FOR LAV SMOKE DETECTOR. OPERATIONAL CHECK GOOD.

Part: APU — SMOKE · airframe 20,762 hrs · 28,896 cycles

SMOKE ALARM IN LAV WENT OFF WITH NO VISIBLE SMOKE. REPLACED APU IAW 49-00-02 EMB MM. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (SMOKE DETECTOR) · airframe 20,742 hrs · 28,863 cycles

FOUND LAV SMOKE DETECTOR KEEPS BEEPING ON THE GROUND. REPLACED LAV SMOKE DETECTOR WITH A NEW BATTERY, OPERATIONAL CHECK GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 20,676 hrs · 28,767 cycles

LAVATORY SMOKE DETECTOR SOUNDED INFLIGHT THREE TIMES. REPLACED LAVATORY SMOKE DETECTOR. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (SMOKE DETECTOR) · airframe 19,223 hrs · 26,848 cycles

LAV SMOKE DETECTOR WILL NOT SILENCE. NO VISIBLE SMOKE. REPLACED LAV SMOKE DETECTOR BATTERY. OPERATIONAL CHECK GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 18,749 hrs · 26,220 cycles

SMOKE ALARM IN LAV GOES OFF INTERMITTENTLY. NO SMOKE OR FIRE NOTED. REPLACED SMOKE ALARM WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 18,566 hrs · 25,996 cycles

EXIT SIGN TO LOWER RIGHT OF F/A SEAT BROKEN. REPLACED LIGHT RECEPTACLE FOR EMERGENCY LIGHT AT F/A SEAT. OPERATIONAL CHECK GOOD.

Part: TRIM SWITCH — MALFUNCTIONED (COCKPIT) · airframe 17,659 hrs · 24,845 cycles

RECEIVED ORAL (TRIM FAIL) FOLLOWED BY AP DISCONNECT. REMOVED AND REPLACED PILOTS TRIM SWITCH IAW MM 22-10-10, OPERATIONAL CHECK GOOD.

Part: SMOKE — DETECTED (CABIN) · airframe 17,247 hrs · 24,331 cycles

DURING CRUISE, AFTER SETTING CRUISE POWER AND PACKS TO NORM CABIN FILLED WITH SMOKE. LAV SMOKE ALARM ACTIVATED. RAN RIGHT PACK ON GROUND FOR SEVERAL MINUTES, PACK OPERATES NORMAL. COULD NOT DUPLICATE DISCREPANCY.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 16,904 hrs · 23,909 cycles

RIGHT AFTER TAKEOFF TRIM FAIL LIGHT ILLUMINATED ON MAP AND TRIM LIGHT ON FCP AND SINGLE CHIME. ALL LIGHTS WENT OUT WHEN AUTOPILOT WAS SWITCHED TO FIRST OFFICER'S SIDE. ALL ILLUMINATED AGAIN WHEN SWITCHED BACK TO CAPTAIN'S SIDE. REMOVED AND REPLACED APC NR 1 WITH SERVICEABLE UNIT. OPS CHECK GOOD IAW MM 22-10-00.

Part: HYDRAULIC SYSTEM — LOW (LT (GREEN)) · airframe 16,395 hrs · 23,280 cycles

LEFT (GREEN) HYDRAULIC SYSTEM LOW LEVEL LIGHT ILLUMINATED. QUANTITY GAUGE READ ZERO. (MADE EMERGENCY LANDING DEN) SERVICED HYDRAULIC SYSTEMS. RAN ENGINES, SWUNG GEAR AND OPERATED ALL GREEN HYDRAULIC SYSTEM COMPONENTS. OPS CHECKS GOOD.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 16,167 hrs · 22,987 cycles

CAPTAINS FLIGHT DIRECTOR COMMAND BARS PITCH UP ABRUPTLY IN FLIGHT TO 20 DEGREES AND NOSE UP AND 20 DEGREES LEFT AND RIGHT TURN. INSTALLED SERVICEABLE AUTOPILOT COMPUTER ON CAPTS SIDE. OPS CHECK GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 15,762 hrs · 22,428 cycles

RT FRAME 9 CRACKED BY FO'S O2 STORAGE BOX, UPPER RADIUS. (DISCOVERED DURING C-CHECK INSPECTION) COMPLIED WITH SERVICE BULLETIN NR 120-53-0073 IAW EMB SRM 51-40-00 THRU 51-40-08.

Part: BRACKET — CRACKED (COCKPIT WINDOW) · airframe 15,762 hrs · 22,428 cycles

CRACKED BRACKET AT CAPTAIN'S DV WINDOW AFT FRAME. (DISCOVERED DURING C-CHECK INSPECTION)REMOVED AND REPLACED CAPTAIN'S DV WINDOW AFT FRAME BRACKET WITH A SERVICEABLE UNIT IAW EMB SRM 51-10-02.

Part: CLIP — CRACKED (RT WING) · airframe 15,762 hrs · 22,428 cycles

RIGHT OUTBOARD WING, STATION 15, LOWER WING CLIP (FWD OF MIDDLE CLIP) CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED LOWER WING SUPPORT CLIP (FWD OF MIDDLE CLIP) OF RIGHT OUTBOARD WING RIB 15 PER MM 28-10-00.

Part: CHANNEL — CRACKED (NACELLE) · airframe 15,762 hrs · 22,428 cycles

BLUE HYDRAULIC PACK LOWER SUPPORT CHANNEL CRACKED IB EDGE. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED LOWER SUPPORT CHANNEL WITH SERVICEABLE UNIT FOR BLUE HYDRAULIC PACK.

Part: CLIP — CRACKED (RT WING) · airframe 15,762 hrs · 22,428 cycles

RIGHT OUTBOARD WING, STATION 15, LOWER WING CLIP (MIDDLE) CRACKED AT FWD END. (DISCOVERED DURING C-CHECK INSPECTION)REMOVED AND REPLACED RIGHT OUTBOARD WING, STATION 15, LOWER WING MIDDLE CLIP WITH A SERVICEABLE UNIT IAW EMB SRM 51-40-01 & 51-40-02.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 15,709 hrs · 22,335 cycles

FORWARD EMERGENCY LIGHTS INOP. REMOVED AND REPLACED FWD EMERGENCY BATTERY PACK IAW 33-50-02. OPS CHECKS GOOD.

Part: WIRE — SHORTED (RT MLG WW) · airframe 14,769 hrs · 21,164 cycles

FDAU AND DFDR LIGHTS CAME ON IN FLIGHT. CIRCUIT BREAKER FOR FDAU FOUND POPPED AND SMELLED SMOKE AT THE SAME TIME. FOUND W501-0018-22 SHORTING TO GROUND FROM LEFT AILERON RIVET INSIDE WHEEL WELL. REPAIRED WIRE IAW WM 20-00-00. OPS CHECK OF FDAU AND DFDR GOOD IAW MM 31-30-00.

Part: PRESSURE SWITCH — MALFUNCTIONED (DEICE BOOT) · airframe 14,643 hrs · 21,012 cycles

MIDDLE RIGHT WING DEICE BOOT LIGHT CAME ON INFLIGHT, BOTH TIMERS. RETURNED TO SLC. REMOVED AND REPLACED THE PRESSURE SWITCH FOR THE RIGHT MIDDLE WING DEICER. RAN THE ENGINES AT ALL POWER SETTINGS. NO FAULTS NOTED AT THIS TIME. P/N OFF: 211C117-183, S/N OFF: U08021A.

Part: WIRE HARNESS — MALFUNCTIONED (RT ENGINE EEC) · airframe 14,499 hrs · 20,803 cycles

ON CLIMBOUT THE RT ENGINE TQ STARTED TO FLUCTUATE 5 PERCENT TO 20 PERCENT. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN AND RETURNED TO THE FIELD. REPLACED RIGHT ENGINE EEC ELECTRICAL WIRING HARNESS IAW PW MM 22-01-10. ALL OPS CHECKS GOOD. P/N: 3115911-01 SN OFF: AR4013.

Part: RELAY — FAILED (INVERTER) · airframe 13,540 hrs · 19,514 cycles

NR 1 INVERTER FAILED DURING CLIMBOUT. FOLLOWED QRH PROCEDURE BUT INVERTER WOULD NOT RESET. RETURNED TO SLC. REMOVED AND REPLACED RELAY K0001 IAW WM 24-20-00. OPS CHECKS GOOD.

Part: OIL SYSTEM — LOW (LT ENGINE) · airframe 12,988 hrs · 18,855 cycles

AFTER TAKEOFF, AT ABOUT 1500 AGL, THE LEFT ENGINE OIL AURAL WARNING CAME ON. CONCURRENTLY HEARD RCCB'S CLICKING AND THE OIL NEEDLE FLUCTUATED. RETURNED TO DEN. ADDED 4 QUARTS OF OIL AND COMPLIED WITH ST72-344. NO DEFECTS NOTED. LEAK CHECK GOOD.

Part: SWITCH — OUT OF ADJUST (PAX DOOR) · airframe 12,882 hrs · 18,728 cycles

FORWARD DOOR RED LIGHT ON OVERHEAD PANEL CAME ON AT START OF TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO THE GATE. ADJUSTED MICROSWITCHES ON FORWARD DOOR AS NEEDED. OPS CHECK GOOD.

Part: PRESSURE SWITCH — FAILED (RT ENGINE) · airframe 12,307 hrs · 18,046 cycles

RIGHT SIDE ENGINE AIR INLET DEICE BOOT FAILED, AMBER LIGHT. RE-ATTEMPTS AT DIFFERENT POWER SETTINGS, ALL FAILED. RETURNED TO DENVER. INSTALLED SERVICEABLE RT ENGINE AIR INLET PRESSURE SWITCH. OPS CHECK GOOD.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 12,247 hrs · 17,985 cycles

RIGHT NACELLE FLAP WOULD NOT RETRACT AFTER LANDING. REPLACED RIGHT NACELLE FLAP ACTUATOR. OPS CHECK GOOD.

Part: VENTURI — BLOWN (RT A/C PACK) · airframe 10,889 hrs · 16,010 cycles

INFLIGHT, WHEN PACKS (A/C) ARE SELECTED TO NORM, A BURNING PACK ODOR OCCURS. INSPECTED A/C PACKS. FOUND RIGHT VENTURI BLOWN OUT. REPLACED WITH SERVICEABLE UNIT. RAN BOTH PACKS. NO DISCREPANCIES NOTED AT THIS TIME.

Part: DOOR SEAL — UNSECURE (CARGO BAY) · airframe 10,765 hrs · 15,836 cycles

AFTER DEPARTURE FROM BOI CLIMBING THROUGH 20,000 FEET LOST PRESSURIZATION. FLIGHT ATTENDANT HEARD LOUD NOISE COMING FROM CARGO AREA. RETURNED TO BOI. FOUND CARGO DOOR SEAL NOT SECURED. INSTALLED SEAL IAW MM 52-30-01. PRESSURIZATION CHECK OK. OK FOR SERVICE.

Part: ACTUATOR — JAMMED (ELEVATOR TRIM) · airframe 10,480 hrs · 15,428 cycles

AT FL250 WITH AUTOPILOT ENGAGED THE YELLOW TRIM LIGHT ON AUTOPILOT PANEL ILLUMINATED. DISCONNECTED THE AUTOPILOT AND MANUALLY MOVED THE TRIM WHEEL AND FOUND IT TO BE JAMMED. TRANSFERRED AUTOPILOT TO CAPTAIN SIDE AND THE SAME OCCURRED. DISCONNECTED AUTOPILOT AND FOUND TRIM STILL JAMMED. DECLARED AN EMERGENCY AND CONTINUED TO YUM. UPON DESCENT DID NOT TOUCH TRIM PER QRH. REPLACED BOTH ELEVATOR TRIM TABS ACTUATORS. RIGGING AND OPS CHECKS GOOD. SWAPPED OUT FDR. LEFT ACT P/N: 5299, S/N ON: 824, S/N OFF: 738, RIGHT ACT P/N: 5299, S/N ON: FA339, S/N OFF: 743.

Part: REGULATOR — FAILED (DEICE SYSTEM) · airframe 10,116 hrs · 14,879 cycles

LEADING EDGE ICE PROTECTION TIMER 1 FAILED IN FLIGHT BOTH LIGHT AND HEAVY. RETURNED TO SBA. INSTALLED SERVICEABLE 18 PSI REGULATOR FOR NUMBER TWO SIDE IAW 30-1-00. RAN ENGINE ON GROUND FOR 20 MINUTES. OPS CHECK GOOD. SN ON B2423

Part: REGULATOR — FAILED (DEICE SYSTEM) · airframe 10,057 hrs · 14,786 cycles

THREE MINUTES AFTER TAKE OFF, LEFT DUCT LEAK LIGHT ILLUMINATED. FOLLOWED QRH PROCEDURE 6:39 LIGHT REMAINED ILLUMINATED. AFTER 3 MINUTES, SHUT DOWN ENGINE (LEFT). LIGHT EXTINGUISHED AT THAT TIME. RESTARTED LEFT ENGINE WITH LEFT BLEED/PACK OFF. RETURNED TO LAX FOR A NORMAL LANDING. FOUND LEFT ENGINE DEICE PRESSURE REGULATOR TO BE DEFECTIVE. REPLACED LEFT DEICE PRESSURE REGULATOR WITH SERVICEABLE UNIT. EXTENSIVE INSPECTION OF LEFT ENGINE DUCT SYSTEM FOUND EVERYTHING ELSE GOOD. PERFORMED EXTENSIVE ENGINE RUN WITH NO FURTHER PROBLEMS NOTED. SN OFF UNKNOWN SN ON RF962.

Part: ENGINE — LACK OF LUBE (LEFT) · airframe 9,852 hrs · 14,474 cycles

OIL PRESS ''ONE'' LIGHT CAME ON WITH AURAL WARNING AT 70 KNOTS. ABORTED TAKEOFF. INSPECTED LEFT ENGINE AND FOUND TO BE ONE AND ONE HALF QUARTS LOW ON OIL. ADDED OIL AND GROUND RAN ENGINE. OIL PRESSURE OK. NO WARNING LIGHT OR AURAL WARNING. RETURN TO SERVICE.

Part: FAN — FAILED (GASPERS) · airframe 9,679 hrs · 14,221 cycles

AN ELECTRICAL SMELL WAS PRESENT AT SEATS 2A AND 3A WHEN THE GASPER FANS EYEBALLS WERE TURNED OPEN. DEFERRED THE GASPER FAN. MEL 21-24-1 PRI ''C'' DUE:10/19/00 SMOKE (SMALL DEGREE) IN CABIN. LAVATORY ALARM WAS ACTIVATED AND FLIGHT ATTENDANT NOTICED NO SMOKE OR FIRE FROM LAVATORY. SEAT 2A NOTICED SMELL OF SMOKE FROM GASPER VALVE. DECLARED AN EMERGENCY AND DIVERTED TO MRY. NO SMOKE OR FIRE ENSUED. REMOVED AND REPLACED GASPER FAN IAW MM 21-24-03, OPS CHECKS GOOD. P/N ON: EVAC-523C2, S/N: 805, S/N OFF: 212.

Part: WARNING SYSTEM — ACTIVATED (OIL INDICATOR) · airframe 9,520 hrs · 13,998 cycles

AFTER STATIC TAKEOFF PASSING THROUGH 70 KNOTS, TRIPLE CHIME AND AURAL ''OIL'' HEARD AT APPROXIMATELY 40 PSI. ABORTED TAKEOFF AND OIL PRESSURE RETURNED TO GREEN RANGE (60 + PSI). DISCONNECTED CANNON PLUGS P0943 AND P0308, INSPECTED AND MEGGED WIRING ASSOCIATED WITH NUMBER ONE ENGINE OIL PRESSURE INDICATIONS AND WARNING SYSTEMS. DISCONNECTED AND CLEANED OIL LINES TO AND FROM THE LOW OIL PRESSURE SWITCH. TAXIED AC AT 70 KTS. COULD NOT DUPLICATE DISCREPANCY FOR LEAK CHECK.

Part: WARNING SYSTEM — ACTIVATED (OIL SYSTEM) · airframe 9,333 hrs · 13,716 cycles

UPON ROTATION, LEFT ENGINE AURAL ''OIL'' OCCURRED WITH NO CORRESPONDING LOW OIL PRESSURE INDICATION. APPROXIMATELY 10 SECONDS LATER, OIL PRESSURE BEGAN FLUCTUATING WITHIN THE GREEN ARC WITH NO FURTHER AURAL WARNINGS. RETURNED TO SBP. OIL LEVELS SATISFACTORY. NO LEAKS. RUN-UP SHOWS OIL PRESSURE STEADY AND IN THE ''''''''''''''''GREEN ARC''''''''''''''''.

Part: NUT — LOOSE (RT ENGINE HUB) · airframe 9,175 hrs · 13,474 cycles

RIGHT ENGINE HUB RETAINING NUTS LOOSE, FOUND DURING INSPECTION. REPLACED RT ENG PROP WITH SERVICEABLE UNIT. RII 61-301PN ON: RFC11M16A SN: 857876 SN OFF: 885659 PN ON: RFC11M16A SN: 8880996A SN OFF: 888144 PN ON: RFC11M16A SN: 887900 SN OFF: 868626 PN ON: RFC11M16A SN: 869414 SN OFF: 888659 PN ON; 784784-1 SN: 270 SN OFF: 418PN ON: 790201-3 SN: 920614 SN OFF: 881226PN ON: 782501-6 SN: 326 SN OFF: 175

Part: LIGHT — DAMAGED (CABIN) · airframe 9,055 hrs · 13,300 cycles

EMERGENCY LIGHT EXIT SIGN AT ROW NINE SMASHED AND TWO EXIT ROW SIGNS AT ROW NINE ARE INOP. REPLACED LOWER EXIT SIGN AT ROW 9BC AND PERFORMED OPS CHECK OF ALL LIGHTS. OPS CHECKS GOOD.

Part: CONTROL HANDLE — MALFUNCTIONED (TE FLAPS)

AFTER TAKEOFF, WHEN FLAPS SELECTED UP, INBOARD FLAP PAIRS IN DISAGREEMENT WITH OUTBOARD AND NACELLE. QUICK REFERENCE HANDBOOK PROCEDURE INEFFECTIVE. OPERATES NORMAL ON GROUND AFTER RETURNING TO SJC. REPLACED FLAP CONTROL HANDLE AND RERACKED FLAP CONTROL UNIT. OPS CHECKS GOOD.

Part: FCU — MALFUNCTIONED (TE FLAPS)

AFTER TAKEOFF AND FLAP RETRACTION, FLAP DISAGREEMENT COULD NOT FIX. RETURNED TO SFO. REPLACED FCU, OPS CHECKS GOOD.