N221SW

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,354 hrs · 61,848 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 9 EXIT IS BURNED OUT. FLT 5437 RELAMPED.

Part: WIRE — BROKEN (CABIN) · airframe 43,307 hrs · 61,782 cycles

EMERGENCY FLOOR LIGHT IN GALLEY DOES NOT ILLUMINATE. FLT 5398 FWD TWO RED EMERGENCY FLOOR LIGHTS REPLACED BROKEN WIRE IAW AMM.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 43,148 hrs · 61,567 cycles

MOST FWD RED EMERGENCY FLOOR LIGHT DOES NOT ILLUMINATE. FLT#5365 RE-POSITIONED LAMP IN SOCKET.

Part: UNKNOWN — ODOR · airframe 42,882 hrs · 61,194 cycles

LT PACK PRODUCES BURNING SMELL IN FLIGHT. FLT# 6387 NO FAULT FOUND.

Part: SUPPORT — CRACKED (LT WING) · airframe 42,831 hrs · 61,132 cycles

LT WING INBD NR 2 FUEL PANEL HAS ONE SKIN SUPPORT CRACKED OTBD OF PANEL. C-CHECK REPLACED LT WING SKIN SUPPORT JUST OTBD OF NR 2 FUEL PANEL IAW SRM.

Part: WEB — CRACKED (CABIN DOOR) · airframe 42,831 hrs · 61,132 cycles

MAIN CABIN DOOR UPPER WEBBING IS CRACKED AT BAY 7. C-CHECK NEW UPPER WEBBING INSTALLED ON MAIN CABIN DOOR IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,831 hrs · 61,132 cycles

LT FORWARD WALL SEAT TRACK NEAR THE MAIN CABIN DOOR HAS CORROSION. C-CHECK REPLACED WITH NEW LT FORWARD WALL SEAT TRACK SPLICE NEAR MAIN CABIN DOOR IAW EST.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,831 hrs · 61,132 cycles

THE LT FORWARD FLOOR SEAT TRACK NEAR THE GALLEY HAS CORROSION. C-CHECK REPLACED WITH NEW LT FORWARD FLOOR SEAT TRACK SPLICE NEAR THE GALLEY IAW EST.

Part: CLEAT — CRACKED (LT WING) · airframe 42,831 hrs · 61,132 cycles

LT WING RIB 16 LOWER SECOND MOST FORWARD SKIN CLEAT CRACKED. C-CHECK REPLACED LT WING RIB 16 LOWER SECOND MOST FORWARD SKIN CLEAT IAW SRM.

Part: CLEAT — CRACKED (RT WING) · airframe 42,831 hrs · 61,132 cycles

RT WING UPPER SKIN CLEAT ABOVE THE NR 4 FUEL ACCESS PANEL CRACKED. C-CHECK REPLACED UPPER SKIN CLEAT AT RT WING ABOVE THE NR 4 FUEL ACCESS PANEL IAW SRM.

Part: FRAME — CRACKED (RT NACELLE) · airframe 42,831 hrs · 61,132 cycles

RT INBD NACELLE FRAME CRACKED AS MARKED AT PULLEY CAGE. C-CHECK REPLACED RT INBD NARCELLE PULLEY FITTING AT NACELLE STATION XN 2424.38 IAW SRM.

Part: FRAME — CRACKED (LT NACELLE) · airframe 42,831 hrs · 61,132 cycles

LT INBD NACELLE FRAME CRACKED AS MARKED AT PULLEY CAGE. C-CHECK REPLACED LT INBD NACELLE FRAME FITTING AT PULLEY CAGE IAW SRM.

Part: STRUT — FAILED (NLG) · airframe 42,466 hrs · 60,586 cycles

ON TAKEOFF LANDING GEAR LEVER WOULD NOT RAISE GEAR OR MOVE UP WITHOUT USING DOWN LOCK RELEASE IAW QRH. AURAL WARNINGS CONTINUOUSLY AFTER RAISING GEAR. REPLACED NLG STRUT ASSY IAW AMM. SWUNG GEAR, SYS OPERATES NORMALLY, PN ON: 19730-100-15, SNON: 297, PN OFF: 19730-100-13, SNOFF: 238, PN: 20500-000-02, SNON: 97, SNOFF: 212.

Part: RELAY — FAULTY (ELECTRICAL SYS) · airframe 42,358 hrs · 60,445 cycles

INTERMITTENT ELECTRICAL OVERHEAT SMELL IN THE COCKPIT NEAR RELAY BOXES. (FLT 5609) REPLACED NR 2 FEEDER PROTECTON RELAY. OPS CHECK GOOD. NO ELECTRICAL SMELL IN COCKPIT.

Part: WIRE — BROKEN (CABIN) · airframe 42,147 hrs · 60,136 cycles

EMERGENCY LIGHTS ROWS 2-5 DO NOT ILLUMINATE. (FLT 5366) REPAIRED BROKEN WIRE IN ROW 5.

Part: SERVO — FAILED (ELEVATOR) · airframe 41,731 hrs · 59,554 cycles

WITH AUTOPILOT SELECTED TO THE CAPTAINS SIDE AND AUTOPILOT ENGAGED, AIRCRAFT STARTED A SHALLOW CLIMB AND THEN AN ABRUPT DESCENT ACCOMPANIED BY A TRIM FAIL WARNING. AFTER THE AUTOPILOT WAS DISCONNECTED NORMAL FLIGHT RESUMED. (FLT 5474) REPLACED ELEVATOR AUTOPILOT SERVO. P/N 622-5734-002 S/N ON-3622 S/N OFF-9595.

Part: CONTROL PANEL — FAILED (AUTOPILOT SYS) · airframe 41,719 hrs · 59,536 cycles

WHILE LEVEL AT 17,000 FEET, THE AUTOPILOT BEGAN TO PITCH UP AND DOWN, THEN THE NOSE ABRUPTLY PITCHED DOWN AND THERE WAS A "TRIM FAIL" MESSAGE. (FLT 5457) REPLACED AUTO PILOT CONTROL PANEL. OPS CHECK GOOD AT THIS TIME. P/N: 622-6684-006 S/N ON: 440 S/N OFF: 1519

Part: SIGN — MISSING (CABIN) · airframe 41,245 hrs · 58,879 cycles

LOWER EMERGENCY EXIT SIGN AT ROW 9 IS MISSING. (SERVICE) REPLACED THE LOWER EMERGENCY EXIT SIGN AT ROW 9.

Part: ACTUATOR — FAILED (LT MLG) · airframe 41,205 hrs · 58,822 cycles

LEFT MAIN LANDING GEAR WOULD NOT EXTEND. PERFORMED AGO AROUND AND LEFT MAIN GEAR LOCKED INTO PLACE. (FLT 6347) REPLACED LEFT MAIN LANDING GEAR ACTUATOR IN REFERENCE TO AMM. P/N: 19595-000-07 S/N OFF: B66.

Part: MODULE — FAILED (LANDING GEAR) · airframe 41,172 hrs · 58,779 cycles

LEFT MAIN GEAR WOULD NOT EXTEND. PERFORMED QRH PROCEDURE AND GEAR DID EXTEND. (FLT 5409) REPLACED LANDING GEAR MODULE ASSEMBLY. P/N: 120-38594-001 S/N OFF: 120148

Part: OUTFLOW VALVE — OBSTRUCTED (CABIN PRESSURE) · airframe 40,666 hrs · 58,055 cycles

CABIN PRESSURE WAS CLIMBING, CREW INITIATED DESCENT TO 10,000 FEET. (FLT 5371) REMOVED DEBRIS FROM ELECTRO PNEUMATIC OUTFLOW VALVE.

Part: MODULE — FAILED (NLG) · airframe 40,188 hrs · 57,377 cycles

UPON GEAR RETRACTION NOSE GEAR HUNG AND DID NOT RETRACT. RECYCLED GEAR AND GEAR OPERATED NORMALLY. (FLT 1352) REPLACED LANDING GEAR MODULE ASSEMBLY. PN: 120-38594-002 SN OFF: 120275.

Part: LENS — MISSING (EXIT SIGN) · airframe 40,102 hrs · 57,256 cycles

EMERGENCY EXIT SIGN LENS COVER AT SEAT 6A IS MISSING. (FLT 6414) REPLACED EMERGENCY EXIT SIGN ASSEMBLY AT SEAT 6A.

Part: WIRE — BROKEN (CABIN) · airframe 39,120 hrs · 55,889 cycles

FLOOR LEVEL RED EMERGENCY LIGHT AT ROW 2A IS OUT. (FLT 5381) REPAIRED WIRE AT NR 1 FLOOR LEVEL RED EMERGENCY LIGHT.

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 38,655 hrs · 55,271 cycles

SMOKE COMING FROM COFFEEMAKERS. (FLT 6516) REPLACED BOTH HOT JUGS.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 38,214 hrs · 54,676 cycles

MAIN CABIN DOOR HARD TO OPEN. (FLT 7026) LUBED MCD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,811 hrs · 54,101 cycles

AFT OVERHEAD EMERGENCY LIGHT OUT. (FLT 6673) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,699 hrs · 53,959 cycles

MAIN CABIN DOOR EMERGENCY LIGHTS ARE OUT. (FLT 6618) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,543 hrs · 53,730 cycles

FORWARD EMERGENCY FLOOR LIGHT IS OUT. (FLT 6750) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,750 hrs · 52,593 cycles

EMERGENCY LIGHTS OUT IN CABIN. (FLT 6195) REMOVED AND REPLACED AFT CABIN EMERGENCY LIGHT BATTERY PACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,492 hrs · 52,242 cycles

ENTRY EMERGENCY LIGHT INOP. (FLT 6660) RELAMPED EMERGENCY LIGHT.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 36,593 hrs · 52,379 cycles

CORROSION ON LEFT BUTT STRAP NEAR LEFT OUTBOARD SEAT TRACK. (C-CHECK) INSTALLED NEW BUTT STRAP.

Part: SUPPORT — CORRODED (ELEVATOR TAB) · airframe 36,593 hrs · 52,379 cycles

RIGHT ELEVATOR TRIM TAB HINGE POINTS HAVE CORROSION. (C-CHECK) REPLACED RIGHT ELEVATOR TRIM TAB SUPPORT.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,593 hrs · 52,379 cycles

STRINGER 18 CORRODED. (C-CHECK) REPAIRED PER SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,593 hrs · 52,379 cycles

SEAT TRACK HAS CORROSION. (C-CHECK) REPLACED SEAT TRACK.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,593 hrs · 52,379 cycles

STRINGER 19 CORRODED. (C-CHECK) REPLACED SECTION OF STRINGER 19.

Part: FLAP — CRACKED (LT WING) · airframe 36,593 hrs · 52,379 cycles

LEFT NACELLE FLAP CRACKED. (C-CHECK) LEFT NACELLE FLAP REPLACED.

Part: ROD END — CORRODED (AILERON TAB) · airframe 36,593 hrs · 52,379 cycles

LEFT AILERON TRIM TAB ROD ENDS CORRODED. (C-CHECK) REPLACED LEFT AILERON TRIM TAB ROD ENDS.

Part: SPAR CAP — CRACKED (LT WING) · airframe 36,593 hrs · 52,379 cycles

LEFT WING INBOARD INTERNAL AUX SPAR CAP CRACKED. (C-CHECK) REPAIRED SPAR CAP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,547 hrs · 49,433 cycles

WHITE FLOOR LEVEL EMERGENCY LIGHT AT ROW 9 INOP. (FLT 6653) REPLACED LIGHT ASSEMBLY.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 33,949 hrs · 48,544 cycles

FLT 6157 - EXIT ROW SIGN AT 6A BROKEN. REPLACED SIGN.

Part: SIGN — MISSING (CABIN) · airframe 33,624 hrs · 48,101 cycles

FLT 5734 - LIGHTED EXIT SIGN 6A MISSING, TAKEN BY PASSENGER. REPLACED MISSING COVER.

Part: ROD END — OUT OF ADJUST (RT MLG ACTUATOR) · airframe 33,433 hrs · 47,825 cycles

FLT 5739 - RIGHT MAIN GEAR WOULD NOT RETRACT. ADJUSTED RIGHT MAIN GEAR ACTUATOR ROD END.

Part: SIGNAL COND UNIT — MALFUNCTIONED (AUTOFEATHER SYS) · airframe 33,108 hrs · 47,387 cycles

FLT 5427 - ABORTED TAKEOFF DUE TO INADVERTENT AUTOFEATHER OF NR 1 ENGINE. REPLACED LEFT TORQUE PROBE AND TORQUE SIGNAL CONDITIONER PN ON 30005-0000-57, PN OFF 30005-0000-52, SN ON MM4720, SN OFF 4225.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 32,651 hrs · 46,795 cycles

AFTER TAKEOFF, OIL PRESSURE DROPPED TO 0 AND HAD SMOKE IN THE COCKPIT. SHUTDOWN ENGINE AND RETURNED TO FIELD. FLIGHT 5769. REPLACED LEFT ENGINE ASSEMBLY IAW EMB 120 MM 72-00-00. OPS CHECK GOOD. REPLACED OIL COOLER. NO LEAKS NOTED. S/N OFF: 115629, P/N 160282-6, S/N OFF 105-823.

Part: BRAKE SYS — MALFUNCTIONED (MLG) · airframe 32,228 hrs · 46,253 cycles

BRAKES FAILED TO STOP AIRCRAFT WHILE TAXIING. (FLT 5515) PERFORMED BRAKE VALVE PRESSURE TEST ON BOTH BRAKE SYSTEMS AND PERFORMED TAXI CHECK WITH ANTI-SKID ON AND OFF. OPS CHECK GOOD.

Part: ENGINE — SMOKE (LEFT) · airframe 31,992 hrs · 45,911 cycles

FLT 5571 - CABIN FILLED WITH SMOKE ON DESCENT. REPLACED LEFT ENGINE IAW EMB 120 MM 71-00-00. P/N PW118A S/N OFF 115676

Part: ACM — SMOKE (RIGHT) · airframe 31,873 hrs · 45,745 cycles

FLT 5712 - REPORTED SMOKE IN THE CABIN. REPLACED RIGHT PACK ACM PER MM 21-50-05, P/N 2204540-4, S/N OFF 987R.

Part: COVER — MISSING (EMERGENCY LIGHTS) · airframe 30,347 hrs · 43,598 cycles

EXIT LIGHT COVER IS MISSING AT ROW 9, FLIGHT NR 5595. REPLACED EMERGENCY EXIT SIGN COVER.

Part: PRESSURE PANEL — ERODED (LT MLG WW) · airframe 29,304 hrs · 42,097 cycles

LEFT WHEEL WELL FORWARD INBOARD WEB PANEL ERODED FROM INSPECTION PANELS, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT WHEEL WELL FORWARD INBOARD WEB IAW EMB 120 SRM 51-40-02.

Part: SKIN — CORRODED (FUSELAGE) · airframe 29,304 hrs · 42,097 cycles

FUSELAGE SKIN CORRODED AT FUSELAGE FRAME STATION 22 BETWEEN STRINGERS 21.5R TO 21.5L. (DISCOVERED DURING C-CHECK INSPECTION)NEW SKIN INSTALLED IAW SRM 51-10-02 PG. 3 SECT 3A AND RII CARD 53-800-1000.

Part: BRACE — CRACKED (RT NACELLE FLAP) · airframe 29,304 hrs · 42,097 cycles

RT NACELLE FLAP INTERNAL BRACING HAS A CRACK AT A STIFFENER. (DISCOVERED DURING C-CHECK INSPECTION) NEW STIFFENER INSTALLED IAW SRM 120 51-10-02 PG. 3 SEC. 3A.

Part: RIB — CRACKED (LT NACELLE) · airframe 29,304 hrs · 42,097 cycles

LT IB NACELLE RIB CRACKED BENEATH WING. (DISCOVERED DURING C-CHECK INSPECTION) DOUBLER INSTALLED IAW SRM 120 51-10-02 PG 2 SEC. 2B.

Part: WEB — CRACKED (PAX DOOR) · airframe 29,304 hrs · 42,097 cycles

FOUND CRACK CENTER FORWARD OF PAX DOOR ON UNDERSIDE OF WEBBING, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CRACKED FRAME IAW SRM 51-10-02 PG 3 SEC 3A AND RII 52-800-1000.

Part: CHAIN — CORRODED (RT AILERON TRIM) · airframe 29,304 hrs · 42,097 cycles

RIGHT AILERON TRIM CHAIN IS RUSTED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT AILERON TRIM TAB ACTUATOR ASSY IAW EMB 120 MM 27-12-01.

Part: WEB — CRACKED (PAX DOOR) · airframe 29,304 hrs · 42,097 cycles

FOUND CRACK CENTER AFT OF PAX DOOR ON UNDERSIDE OF WEBBING, DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CENTER AFT SUPPORT IAW SRM 52-10-02 AND RII 52-800-1000.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 29,304 hrs · 42,097 cycles

BRACKET BETWEEN FRAMES AFT OF DV WINDOW CAPTAIN'S SIDE COCKPIT CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED BRACKET BETWEEN FRAME IAW SRM 51-10-02 PG. 3 SEC 3A AND RII 53-500-1000.

Part: FRAME — CRACKED (LT NACELLE) · airframe 29,304 hrs · 42,097 cycles

LEFT NACELLE FRAME CRACKED AT AFT OUTBOARD DOOR AFT HINGE ATTACH POINT FORWARD BOSS, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT NACELLE FRAME AFT DOOR FORWARD HINGE ATTACH POINT IAW SRM 120 51-10-02 PG 2 SEC 2B.

Part: RACK — CRACKED (E/E BAY) · airframe 29,304 hrs · 42,097 cycles

AVIONICS EQUIPMENT RACK IN AVIONICS COMPARTMENT IS CRACKED IN (2) AREAS. (DISCOVERED DURING C-CHECK INSPECTION) (2) NEW BRACKETS INSTALLED IAW SRM 120 51-10-02 PG. 3 SEC. 3A.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 29,304 hrs · 42,097 cycles

FRAME SUPPORT CRACKED AFT OF FRAME 9 UNDER DV WINDOW BEAM. (DISCOVERED DURING C-CHECK INSPECTION) NEW SUPPORT INSTALLED IAW SRM 120 51-10-02 PG. 3 SEC. 3A ALSO IAW RII CARD 53-800-1000.

Part: PRESSURE PANEL — ERODED (LT MLG WW) · airframe 29,304 hrs · 42,097 cycles

LT WHEEL WELL FWD OB WEB PANEL ERODED FROM INSPECTION PANELS. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED LT WHEEL WELL OB WEBBING, SECURED IAW SRM 51-40-02.

Part: FRAME — CRACKED (FUSLEAGE) · airframe 29,304 hrs · 42,097 cycles

CROSS MEMBER OF FRAME (16) CRACKED. (DISCOVERED DURING C-CHECK INSPECTION NEW CROSS MEMBER INSTALLED IAW SRM 51-10-02 PG. 3 SEC. 3A P/N 120-06962-601.

Part: FRAME — CRACKED (LT NACELLE) · airframe 29,304 hrs · 42,097 cycles

LT NACELLE FRAME NR 1 CRACKED AT WEBBING. (DISCOVERED DURING C-CHECK INSPECTION) COMPLIED WITH SB 120-54-0036 REV. 02 09 JUN 99 TO LT ENGINE NACELLE FRAME NR 1.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 29,304 hrs · 42,097 cycles

CRACK ON CAPTAIN'S SIDE LOWER DV WINDOW BEAM AT VERTICLE WINDOW POST AREA. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED CAPTAIN'S SIDE DV WINDOW BEAM IAW SRM 51-10-02 PG SEC. 3A AND RII 53-800-1000.

Part: RACK — CRACKED (E/E BAY) · airframe 29,304 hrs · 42,097 cycles

AVIONICS BAY; RIGHT RADIO RACK CRACKED MIDWAY, DISCOVERED DURING C-CHECK INSPECTION. NEW RACK INSTALLED IAW SRM 120 51-10-02 PG 23 SEC 3A.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 28,993 hrs · 41,628 cycles

EMERGENCY LIGHT IN CABIN IS INOP. REPLACED LIGHT BULB. OPERATIONAL CHECKS GOOD.

Part: CLAMP — BROKEN (A/C PACK) · airframe 28,943 hrs · 41,553 cycles

RIGHT PACK LOW SQUEAL, ODOR IN CABIN AND LAV SMOKE DETECTOR ACTIVATED. REPLACED BROKEN CLAMP ON PACK. OPERATIONAL CHECKS GOOD.

Part: SMOKE — DETECTED (UNKNOWN) · airframe 26,593 hrs · 38,170 cycles

ON GROUND SEVERE SMOKE IN COCKPIT SMOKE FROM LEFT PACK BY WING, RIGHT SIDE "AIR COND" FAIL LIGHT ON OVERHEAD PANEL MAP LIGHT ELEC AND DOOR CONTINOUSLY. REPLACED RT WOW HARNESS WITH SERVICEABLE UNIT. TAXIED A/C, OPERATED LT AND RT PACKS. OPERATIONAL CHECK GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 26,484 hrs · 37,992 cycles

ROW 9 BC EXIT ROW LIGHT INOP. RESECURED BULB AT ROW 9BC. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 26,235 hrs · 37,631 cycles

ON FFOD CHECKS, MULTIPLE EMERGENCY LTS WILL NOT WORK ON FLOOR STRIP, AND AT EXITS. REPLACED BATTERY PACK AT ROW 5. OPERATIONAL CHECK GOOD.

Part: LIGHT — SMOKE (COCKPIT) · airframe 25,921 hrs · 37,129 cycles

SMOKE COMING FROM FO`S STORM LIGHT. REPLACED FO'S STORM LIGHT ASSY.

Part: TRIM SWITCH — INOPERATIVE (COCKPIT) · airframe 25,006 hrs · 35,757 cycles

ELECTRIC TRIM SWITCH INOPERATIVE ON CAPTAINS SIDE. REPLACED CAPTIANS TRIM SWITCH. OPERATIONAL CHECK GOOD IAW MM 22-10-00.

Part: SKIN — CRACKED (NACELLE FLAP) · airframe 24,333 hrs · 34,784 cycles

RIGHT NACELLE FLAP IS CRACKED ON BOTTOM SKIN. REPLACED RIGHT NACELLE FLAP, OPERATIONAL CHECK GOOD. WORK PERFORMED IAW MM 27-50-02.

Part: SERVO — INOPERATIVE (STICK SHAK) · airframe 24,295 hrs · 34,729 cycles

CAPTAIN'S STICK SHAKER INOPERATIVE. REMOVED AND REPLACED CAPTAIN'S STICK SHAKER. OPERATIONAL CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,093 hrs · 34,416 cycles

RED EMERGENCY LAMP BELOW FLIGHT ATTENDANT JUMPSEAT IS INOPERATIVE. ADJUSTED RED LIGHT AT FA STATION. OPERATIONAL CHECK GOOD.

Part: SIGNAL COND UNIT — MALFUNCTIONED (ENG TORQUE) · airframe 22,864 hrs · 32,479 cycles

ON APPROACH, LEFT ENGINE HAD UNCOMMANDED AUTOFEATHER. TORQUE REACHED 115 PERCENT. REPLACED TORQUE SENSOR, SIGNAL CONDITIONER AND EEC HARNESS WITH SERVICEABLE UNIT IAW EMB-120 MM 73-22-00. OPS CHECKS GOOD. TORQUE SENSOR P/N OFF: 3105076-01.

Part: SERVO — INOPERATIVE (STALL WARNING) · airframe 22,819 hrs · 32,410 cycles

NR 1 STALL WARNING SYSTEM INOP. MEL 27-36-2. REPLACED STICK SHAKER ON CAPTAIN'S SIDE. OPS CHECKS GOOD IAW MM 27-34-04.

Part: PCU — MALFUNCTIONED (LT ENGINE) · airframe 22,812 hrs · 32,398 cycles

ON FINAL APPROACH APPROX 1000 FT LEFT ENGINE AUTOFEATHERED. CONTINUED APPROACH LEFT ENGINE SEEMED TO CYCLE OUT OF FEATHER AND THEN BACK INTO FEATHER. UPON LANDING, ALL PARAMETERS APPEARED NORMAL. REPLACED LEFT ENGINE PCU AND RELAY K0162 PER MM 61-21-00. OPS CHECKED GOOD IAW 61-00-00 TABLE 202.

Part: SERVO — MALFUNCTIONED (AUTOPILOT) · airframe 22,770 hrs · 32,338 cycles

AUTOPILOT FAILS INTERMITTENTLY ON CAPTAIN'S SIDE. WHEN THE AUTOPILOT ENGAGES, THE AIRCRAFT IS OUT OF PITCH TRIM. ADJUSTED ELEVATOR SERVO MOUNT BREAK AWAY TORQUE AND REPLACED ELEVATOR SERVO WITH A SERVICEABLE UNIT. OPS CHECK GOOD IAW MM 22-10-00.

Part: SKIN — CORRODED (FUSELAGE) · airframe 22,728 hrs · 32,271 cycles

FUSELAGE SKIN CORRODED BY FRAME 23 BY 21L STRINGER. DISCOVERED DURING C-CHECK INSPECTION.

Part: FRAME — CRACKED (HYD BAY) · airframe 22,775 hrs · 32,350 cycles

LEFT HYDRAULIC BAY CUTOUT AFT FRAME CRACKED OUT OF OUTBOARD CORNER. DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT HYD BAY DOOR CUTOUT AFT FRAME WITH SERVICEABLE UNIT IAW SRM 54-20-09.

Part: CLIP — CRACKED (LT WING) · airframe 22,775 hrs · 32,350 cycles

LEFT WING 1ST FUEL PANEL OUTBOARD OF NACELLE OUTBOARD CLIP IS CRACKED AT AFT END, RIB 16. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SERVICEABLE CLIP TO LEFT WING 1ST FUEL PANEL OUTBOARD OF NACELLE, OUTBOARD CLIP IAW EMB SRM 51-40-00.

Part: COMPUTER — FAULTY (AUTOPILOT SYS) · airframe 22,520 hrs · 31,962 cycles

WHEN AP ON CAPT'S SIDE, TRIM FAIL AND RED AUTO PILOT FAIL ON MAP AND COMPUTER FLAG ON CA ATTITUDE. FGS 1 DC CIRCUIT BREAKER POPPED. REMOVED AND REPLACED NR 1 APC-65 IAW MM 22-10-02. OPS CHECK GOOD. 622-8318-402, S/N ON: 1641, S/N OFF: 3788.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 22,444 hrs · 31,861 cycles

CAPTAIN'S AUTOPILOT DISCONNECTS INFLIGHT, FOLLOWED BY RED COMPUTER FLAG. INSTALLED SERVICEABLE APC-65B IN NR 1 POSITION. OPS CHECK GOOD. PN ON 622-8315-402, S/N ON 3788 OFF 1534.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 22,444 hrs · 31,861 cycles

CAPTAIN'S FLIGHT DIRECTOR COMMAND BARS ERRATIC IN ROLL DURING TURNS. BARS JERK +/- 3 DEGREES IN ROLL DURING TURNS. COMMAND BARS ARE STABLE IN STRAIGHT FLIGHT. REPLACED CAPT'S AUTOPILOT COMPUTER APC-65B. OPS CHECK GOOD IAW MM 22-10-00.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 21,957 hrs · 31,078 cycles

RIGHT NP FLUCTUATING +/- 3 PERCENT. LOSS OF RT TORQUE GAUGE, LOSS OF RT OIL PRESSURE. PERFORMED PRECAUTIONARY ENGINE SHUT DOWN. REMOVED AND REPLACED RT ENGINE WITH A SERVICEABLE ASSY. OPS AND LEAKS CHECKS GOOD.

Part: APU — SMOKE · airframe 21,075 hrs · 29,757 cycles

APU BLEED CAUSES LAVATORY SMOKE DETECTOR TO GO OFF. REMOVED AND REPLACED APU IAW EMB 120 MM 49-00-02. S/N OFF P-456.

Part: RELAY — MALFUNCTIONED (RT ENGINE) · airframe 20,524 hrs · 28,896 cycles

ON TAKEOFF ROLL WE RECEIVED A RIGHT ENGINE EEC, ENGINE CONTROL WARNING. ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AND REPLACED RIGHT ENGINE REVERSION RELAY. RAN ENGINE. OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 20,510 hrs · 28,879 cycles

DURING LEVEL FLIGHT AT FL230 AND -12 DEGREES CELSIUS WITH THE A/P SELECTED ON, THE CAPTAIN'S FLIGHT DIRECTOR COMMANDED AN ABRUPT ROLL TO THE LEFT, FOLLOWED BY A PITCH DOWN TO 5 DEGREES. PREVIOUS CREW REPORTED SIMILAR OCCURRENCE AT FL240. REPLACED CAPTAIN'S AUTOPILOT COMPUTER APC-65B IAW MM 22-10-00. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 20,409 hrs · 28,692 cycles

4 WHITE & 1 RED LIGHTS ON FLOOR LEVEL EMERGENCY LIGHTING SYSTEM INOP. REMOVED AND REPLACED MID CABIN EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 19,085 hrs · 26,696 cycles

FUSELAGE FRAME CRACKED BEHIND CAPTAIN'S DV WINDOW. REPLACED AFFECTED BRACKET IAW EMB120 SRM 51-10-02.

Part: CONTROL BOX — MALFUNCTIONED (E/E BAY) · airframe 18,760 hrs · 26,252 cycles

RIGHT MAIN A LIGHT ON LANDING GEAR REMAINED ILLUMINATED AFTER T/O WITH CORRESPONDING VIBRATION SIMILAR TO GEAR BEING DOWN. RETURNED TO FIELD. INSPECTED AND ADJUSTED RT MLG UPLOCK PROXIMITY TARGET. ALSO REPLACED LDG RELAY BOX AND LDG SELECTOR BOX. PERFORMED NUMEROUS GEAR SWINGS. GROUND CHECK NORMAL. RELAY BOX P/N: 120-43270-501, S/N ON: 120154, S/N OFF: 120290. SELECTOR BOX P/N ON: 120-25226-501, S/N ON: 120039, P/N OFF: 120-38594-301, S/N OFF: 137101-304.

Part: SEAL — LEAKING (EMERGENCY EXIT) · airframe 17,938 hrs · 25,056 cycles

DOOR SQUEAL AT EMERGENCY EXIT 9BC. UPDATE 7/26/2001 - LOUD SQUEAL AT EXIT DOOR 9BC, SQUEALS AT ALTITUDE.RESEALED DOOR GASKET AT EMERGENCY EXIT 9BC. PRESSURIZED TO 6 PSI, NO SQUEAL. UPDATE 7/26/2001 - CLEANED SEAL AND REPLACED EXIT TAPE ON LOWER PART OF DOOR. REMOVED EXCESS SILICON FROM AROUND EXIT DOOR SEAL CUTOUT. REMOVED INSULATION TAPE FROM AROUND LOWER HANDLE SEAL. AIRCRAFT PRESSURIZED ON GROUND, NO LEAKS NOTED.

Part: RADAR — INOPERATIVE (FUSELAGE) · airframe 16,950 hrs · 23,634 cycles

WEATHER RADAR INOP, PAINTS ONLY SPOKES OF GREEN. DIVERTED FROM BFL TO SFO. REPLACED WXT 250B RADAR TRANSCEIVER. OPS CHECK GOOD. P/N: 622-7337-001, S/N ON: 624, S/N OFF: 4550.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 16,811 hrs · 23,449 cycles

HYDRAULIC MASTER CAUTION AND GREEN HYDRAULIC SYSTEM LOW LEVEL LIGHT ON TAKEOFF ROLL. FLUID QUANTITY GAUGE SHOWED IN GREEN. ABORTED TAKEOFF. DEFERRED PER MEL 29-31-4.

Part: FLIGHT DIR — FAILED (COCKPIT) · airframe 16,783 hrs · 23,409 cycles

CAPTAINS COURSE SELECTOR NEEDLE TURNS ON ITS OWN INFLIGHT. UNABLE TO SELECT AND RETAIN A COURSE. RETURNED TO FAT. REPLACED CAPTAINS HCP AND CAPTAINS COURSE SELECTOR. OPS CHECKS GOOD IAW MM 34-21-00.

Part: BOLT — BROKEN (PROPELLER HUB)

FRACTURE INITIATED TWO THREADS ABOVE SHANK AND AS BOLT WAS BROUGHT UP TO APPROXIMATELY 100 FEET\POUNDS, IT BROKE INTO TWO PIECES. FRACTURE AREA APPEARED CRYSTALIZED AND DARK GREY IN COLOR. HAMILTON STANDARD AND BOSTON ACO WERE NOTIFIED.

Part: ANNUNCIATOR — MALFUNCTIONED (TE FLAP)

AFTER TAKEOFF, REPLACED FLAP ANNUNCIATOR PANEL WITH SERVICEABLE UNIT. RAN SYSTEM AND OPS CHECKS GOOD. (S/N 0178) ON, (S/N 0145) OFF.

Part: PROX SENSOR — MALFUNCTIONED (MLG)

APPROXIMATELY EIGHT MINUTES AFTER DEPARTURE, RIGHT MAIN GREEN A SYSTEM LIGHT ILLUMINATED. CYCLED LANDING GEAR, LANDING INDICATION ALL RED EXCEPT A SYSTEM. GREEN REMAINED ILLUMINATED A RED EXTINGUISHED. LANDING GEAR REQUIRED ELECTRICAL OVERRIDE. REPLACED RIGHT MAIN A DOWNLOCK PROX SWITCH WITH SERVICEABLE UNIT. SWUNG GEAR AND ALL CHECKS GOOD ON GROUND. (S/N 97675).

Part: SELECTOR — MALFUNCTIONED (MLG)

AFTER TAKEOFF WITH GEAR HANDLE SELECTED UP, RIGHT MAIN GREEN A LIGHT REMAINED ILLUMINATED. ATTEMPTED TO CYCLE LANDING GEAR WITH GEAR HANDLE SELECTED TO DOWN AND ALL LANDING GEAR RED INDICATIONS ILLUMINATED EXCEPT FOR RIGHT MAIN A RED REMAINED EXTINGUISHED AND LANDING GEAR WOULD NOT EXTEND. SELECTED ELECTRICAL OVERRIDE. GEAR EXTENDED AND ALL GREEN LIGHTS ILLUMINATED. REPLACED LANDING GEAR CONTROL BOX WITH SERVICEABLE UNIT. CYCLED LANDING GEAR NUMEROUS TIMES, ALL CHECKS GOOD. (S/N 15710304) ON, (S/N 322306) OFF.

Part: SWITCH — MALFUNCTIONED (RT WING DEICE)

RIGHT INBOARD WING LEADING EDGE BOOT WENT INOP 15 MINUTES AFTER DEPARTURE FROM SFO. RETURNED TO SFO. REPLACED RIGHT INBOARD WING DEICE BOOT PRESSURE SWITCH, OPS CHECK GOOD.

Part: REGULATOR — FAILED (RT ENGINE)

RIGHT ENGINE DUCT LEAK IN FLIGHT. DID NOT EXTINGUISH AFTER 3 MINUTES, SHUTDOWN ENGINE. AFTER ENGINE SHUT DOWN, LIGHT EXTINGUISHED. RETURNED TO LAX. REPLACED RIGHT ENGINE 18 PSI REGULATOR, CHECKS GOOD.

Part: BOLT — MISSING (LT MLG DOOR ACT)

WHEN GEAR WAS RETRACTED, LEFT SIDE SHOWED INTRANSIT LIGHT. CYCLED GEAR, SAME. RETURNED TO LAX. FOUND BOLTS MISSING FORM LEFT INBOARD FOWARD GEAR DOOR ACTUATOR. INSTALLED PROPER HARDWARE, OPS CHECKS GOOD.

Part: REGULATOR — FAILED (EMPENNAGE DEICE)

VERTICAL STABALIZER, LEFT AND RIGHT HORIZONTAL STABALIZER FAILED IN FLIGHT. RETURNED TO FAT. REPLACED LEFT AND RIGHT PRESSURE REGULATORS. OPS CHECKS GOOD.

Part: ENGINE — FAILED (RIGHT)

RIGHT ENGINE FAILED IN FLIGHT. RETURNED TO LAX. REMOVED AND REPLACED RIGHT ENGINE ASSEMBLY WITH A SERVICEABLE UNIT PER MM 71-00-00.

Part: CONTROL BOX — MALFUNCTIONED (LT MLG)

AFTER TAKEOFF, LEFT MAIN LANDING GEAR DID NOT RETRACT. MADE A STRANGE NOISE (SURGING HYDRAULIC AND/OR WIND NOISE). LOWERED GEAR AND LANDED NORMALLY AFTER RETURNING TO LA. REPLACED LANDING CONTROL BOX.

Part: AHARS — FAILED (LT/RT)

BOTH AHRS FAILED IN FLIGHT. RETURNED TO FIELD AS HEADINGS GAVE ERRONEOUS READINGS. REINITIALIZED BOTH AHRS COMPUTORS. OPS CHECKS GOOD ON GROUND.

Part: UNSAFE LIGHT — ILLUMINATED (RT MLG)

RIGHT LANDING GEAR SHOW RED GEAR UNSAFE WHEN RETRACTED. RETURNED TO FIELD, SWUNG LANDING GEAR SEVERAL TIMES, INSPECTED AND CHECKED CLEARANCE ON UPLOCK HOOKS AND PROXIMITY SENSOR. ALL ITEMS CHECK GOOD AND COULD NOT GET LANDING GEAR TO FAIL.

Part: ACTUATOR — OUT OF ADJUST (RT MLG)

RIGHT MAIN GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED FOR LANDING. ADJUSTED RIGHT MAIN ACTUATOR OUT 1 TURN IAW MM 32-00-00. SWUNG GEAR 12 TIMES, OPS CHECKS GOOD ON GROUND.

Part: TORQUE IND — FAILED (RT ENGINE)

DIGITAL READ-OUT ON RIGHT TORQUE GAUGE DOES NOT FUNCTION. ANALOG FUNCTIONS NORMAL. ABORTED TAKEOFF AND TAXIED BACK TO THE GATE. REPLACED RIGHT TORQUE INDICATOR. OPS CHECKS GOOD ON GROUND.

Part: NP INDICATION — FLUCTUATES (RT PROP)

RT NP INDICATION FLUCTUATES INTERMITTENTLY. RAN A/C AND FOUND RT PROP FLUCTUATES .2 TO .5 PERCENT. FOUND WITHIN MM LIMITS AND OPS CHECK GOOD.

Part: HARNESS — FAILED (LANDING GEAR)

LANDING GEAR WILL NOT COME UP. REMOVED AND REPLACED NOSE GEAR A SYSTEM UP HARNESS. CYCLED GEAR. OPS CHECKS GOOD.