N567SW

Part: HMU — FAILED (LT PROPELLER) · airframe 36,843 hrs · 50,756 cycles

DURING INITIAL CLIMB, AT ABOUT 1,000 FEET AGL, LH PROPELLER INADVERTENTLY FEATHERED. WE PERFORMED MEMORY ITEMS, FOLLOWED BY QRH. ENGINE PARAMETERS RETURNED BACK TO NORMAL. CREW RETURNED BACK TO BQN. MAINTENANCE REMOVED AND REPLACED LEFT HAND HMU WITH OPS AND LEAK CHECKED GOOD ON GROUND.

Part: HMU — ERRATIC (LT ENGINE) · airframe 36,554 hrs · 50,571 cycles

THE FLIGHT CREW REPORTED THAT AT APPROXIMATELY 800-1000' AGL, THE LT PROPELLER INADVERTENTLY FEATHERED. THE FLIGHT CREW RAN THE "INADVERTENT PROPELLER FEATHER" QRH AND WAS ABLE TO UNFEATHER THE PROPELLER, PERFORMED A PRECAUTIONARY AIR RETURN WITH BOTH ENGINES OPERATING. UPON LANDING, THE LT EEC ALSO FAILED WHEN SELECTING REVERSE. MAINTENANCE FOUND THE LEFT ENGINE HYDRO MECHANICAL UNIT (HMU) BEHAVING ERRATICALLY CAUSING THE LEFT ENGINE TORQUE TO FLUCTUATE. THE FLUCTUATING TOQUE WAS THE CAUSE OF THE LEFT PROP FEATHERING AS THE AUTO FEATHER SYSTEM SENSED LOW TORQUE ON THE LEFT ENGINE. REPLACED LEFT ENGINE HMU WITH A SERVICEABLE UNIT. GROUND RUNS PERFORMED AND FOUND SATISFACTORY. AN OPERATIONAL CHECK FLIGHT OF THE AIRCRAFT WAS PERFORMED AND WAS SUCCESSFUL.

Part: TORQUE SENSOR — INTERMITTENT (RT ENGINE) · airframe 36,553 hrs · 50,570 cycles

THE FLIGHT CREW REPORTED THAT DURING INITIAL CLIMB OUT AT APPROXIMATELY 500 FEET, THERE WAS A PARTIAL LOSS OF POWER ON THE LEFT HAND ENGINE. THIS LOSS COULD BE BOTH FELT AND HEARD, AND WAS ACCOMPANIED BY A SLIGHT DROP IN TORQUE AND A SIGNIFICANT DROP IN PROP SPEED. THE CREW REQUESTED TO REMAIN IN CLOSED TRAFFIC, COMPLETED THE "ENGINE FAILURE IN FLIGHT CHECKLIST", THEN THE "PRECAUTIONARY ENGINE SHUTDOWN CHECKLIST," AND FINALLY THE "ONE ENGINE INOPERATIVE APPROACH AND LANDING CHECKLIST." THE CREW THEN REQUESTED FROM THE TOWER TO RETURN FOR LANDING AND ONCE CLEARED, PERFORMED A SINGLE-ENGINE LANDING AND RETURNED TO THE RAMP. MAINTENANCE FOUND THE RIGHT ENGINE TORQUE SIGNAL CONDITIONER WAS SENDING A FALSE SIGNAL TO THE LEFT ENGINE CAUSING THE LEFT PROPELLER TO GO TO FEATHER. REPLACED THE RIGHT ENGINE TORQUE SIGNAL CONDITIONER. PERFORMED GROUND RUNS, PROPELLER OPERATIONAL CHECK WAS NORMAL. TIME IN SERVICE ON THE TORQUE SIGNAL CONDITIONER IS UNKNOW. THIS IS AN ON CONDITION PART.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,136 hrs · 48,116 cycles

FLOOR LEVEL EMERGENCY LIGHTS BY 2A & 3A ARE INOPERATIVE. R & R THE BATTERY PACK IAW AMM. SYSTEM OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,947 hrs · 47,830 cycles

LEFT OVERWING EMERGENCY LIGHT WILL NOT ILLUMINATE. R & R BULB IAW AMM.

Part: RELAY — FAILED (APU) · airframe 33,902 hrs · 47,765 cycles

ELECTRICAL ODORIN THE COCKPIT. R & R APU FEEDER PROTECTION RELAY, APU FEEDER PROTECTION RELAY STAND AND APU START CONTACTOR. OPS CHECK GOOD AT THIS TIME.

Part: HYDRAULIC LINE — LEAKING (RT MLG) · airframe 33,206 hrs · 46,778 cycles

LOST ALL FLUID IN THE GREEN HYD RESERVOIR. FOUND RT MLG FWD OTBD GEAR DOOR ACTUATOR HOSE LEAKING. FLT 5325 REPLACED HYD HOSE FOR THE RT MLG FWD OTBD GEAR DOOR ACTUATOR. OPERATED DOORS WITH NO LEAKS NOTED.

Part: CHANNEL — CRACKED (PAX DOOR) · airframe 33,089 hrs · 46,604 cycles

PAX DOOR LOWER INNER CHANNEL CRACKED. C-CHECK R & R PAX DOOR LOWER INNER CHANNEL IAW SRM, PN 120-26563-001.

Part: RIB — CRACKED (RT WING) · airframe 33,089 hrs · 46,604 cycles

RT WING INBD LE INBD FALSE RIB CRACKED. C-CHECK STOP DRILLED CRACK & INSTALLED REINFORCED DOUBLER 2024-T3 0.032" ON RT WING INBD LE INBD FALSE RIB IAW SRM.

Part: FRAME — CRACKED (LT NACELLE) · airframe 33,089 hrs · 46,604 cycles

CRACK ON LT OTBD NACELLE OTBD OF FWD UPPER LATERAL FWD ATTACH POINT. C-CHECK REPLACED LT OTBD NACELLE FWD UPPER LATERAL FWD ATTACH POINT FRAME IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 33,089 hrs · 46,604 cycles

CRACK ON LOWER LT ANGLED FRAME UNDER OBSERVERS SEAT. C-CHECK INSTALLED INSERTION DOUBLER TO LT BRACKET AT LT COCKPIT ENTRY STEP IAW SRM.

Part: RECEPTACLE — CRACKED (LT NACELLE) · airframe 33,089 hrs · 46,604 cycles

CRACK ON LT INBD NACELLE AT LOWER SHOOT BOLT RECEPTACLE. C-CHECK REPLACED LT INBD NACELLE LOWER SHOOT BOLT RECEPTACLE IAW SRM.

Part: DRAIN MAST — CRACKED (RT NACELLE) · airframe 33,089 hrs · 46,604 cycles

RT NACELLE DRAIN MAST SHEET METAL PORTION CRACKED ON NACELLE. C-CHECK REPLACED RT NACELLE DRAIN MAST IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 33,089 hrs · 46,604 cycles

CABIN PAX ENTRANCE LOWER THRESHOLD ANGLE IS CORRODED. C-CHECK REPLACED PAX DOOR ENTRYWAY LOWER & AFT LOWER THRESHOLD ANGLES IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 33,089 hrs · 46,604 cycles

CRACK ON LOWER RT ANGLED FRAME UNDER OBSERVERS SEAT. C-CHECK INSTALLED INSERTION DOUBLER TO L BRACKET AT RT COCKPIT ENTRY STEP IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 33,089 hrs · 46,604 cycles

CARGO COMPARTMENT AFT TRACK UPPER SUPPORT BOX IS CRACKED. C-CHECK REPLACED CARGO COMPARTMENT AFT TRACK UPPER SUPPORT IAW SRM, PN 120-48716-001.

Part: FRAME — CRACKED (PAX DOOR) · airframe 33,089 hrs · 46,604 cycles

PAX DOOR AFT STEP FRAME CRACKED AT LOWER RADIUS. C-CHECK REPLACED PAX DOOR AFT STEP FRAME IAW SRM, PN 120-19619-001.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 33,089 hrs · 46,604 cycles

PAX DOOR FRAME 15 UNDERSIDE CRACKED. C-CHECK REPLACED PAX DOOR CHANNEL FRAME ASSEMBLY IAW SRM, PN 120-21058-003.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 33,089 hrs · 46,604 cycles

CORROSION ON FLOOR TO WALL STRINGER UNDER LAVATORY. C-CHECK REPLACED CARGO SILL ASSEMBLY FLOOR SUPPORT IAW SRM, PN 120-06159-501.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 33,089 hrs · 46,604 cycles

CORROSION ON LT BUTT STRAP JUST FWD OF CARGO DOOR. C-CHECK NEW BUTT STRAP INSTALLED ON LT JUST FWD OF CARGO DOOR IAW SRM, PN 120-46163-001.

Part: MODULE — FAILED (COCKPIT) · airframe 33,088 hrs · 46,603 cycles

AFTER TAKEOFF, HAD TO USE THE DOWN LOCK RELEASE TO RAISE THE GEAR HANDLE, COMPLIED WITH THE QRH. DURING THE CLIMB, RECEIVED THE "FLAPS, TRIM, AUTOFEATHER" CONFIG WARNINGS UNTIL AIRCRAFT LEVELED OFF & CREW PULLED THE POWER BACK. FLT 5541 REPLACED LG LEVER MODULE ASSEMBLY IAW EMB 120 MM. PN ON 120-38594-501, SN ON 120191-310, PN OFF 120-38594-001 & SN OFF 120284.

Part: UNKNOWN — ODOR (CABIN) · airframe 33,088 hrs · 46,603 cycles

UPON STARTING THE APU & OPENING THE BLEEDS, THE AIRCRAFT WAS FILLED WITH A VERY STRONG SMELL OF FUEL. FLT 5532 INSPECTED APU FOR FUEL LEAKS, NO LEAKS FOUND. SHUT APU DOWN, STARTED APU UP, NO SMELL OF FUEL DETECTED.

Part: LIGHT — OBSTRUCTED (CABIN) · airframe 32,709 hrs · 46,057 cycles

EMERGENCY FLOOR LIGHTING AT ROW 9 OBSTRUCTED. FLT 5438 REPOSITIONED FLOOR STRIP TO EXPOSE 2ND RED LIGHT.

Part: COVER — MISSING (CABIN) · airframe 32,680 hrs · 46,013 cycles

EMERGENCY EXIT LIGHT COVER IS MISSING. FLT 5404 REPLACED EMERGENCY EXIT LIGHT ASSEMBLY BY FLIGHT ATTENDANT'S JUMP SEAT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,895 hrs · 44,896 cycles

REAR RED FLOOR EMERGENCY LIGHT DOES NOT ILLUMINATE. RELAMPED.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 31,625 hrs · 44,493 cycles

FIVE FLOOR LEVEL EMERGENCY LIGHTS DO NOT ILLUMINATE. (FLT 5307) RECONNECTED LOOSE CONNECTOR ON FIRST ROW FLOOR EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,829 hrs · 43,334 cycles

EMERGENCY FLOOR LIGHT ADJACENT TO SEAT 11A BURNED OUT. (FLT 5442) RELAMPED EMERGENCY LIGHT.

Part: UNKNOWN — MALFUNCTIONED (FLIGHT CONTROL) · airframe 30,633 hrs · 43,083 cycles

RETURN TO FIELD DUE TO EXCESSIVE AND UNUSUAL CONTROL FORCES AND INPUTS TO MAINTAIN LEVEL FLIGHT. RUDDER & AILERON INPUT MUCH GREATER THAN NORMAL. (FLT 1352) COMPLIED WITH INSPECTION OF LEFT AND RIGHT AILERON BELLCRANKS, PRIMARY AILERON SERVO, PRIMARY RUDDER SERVO, FLAP SYSTEM COMPONENTS, WITH NO DEFECTS FOUND. PASSED FUNCTIONAL FLIGHT.

Part: COMPUTER — FAILED (NR 1) · airframe 30,498 hrs · 42,878 cycles

UNCOMMANDED PITCH DOWN, CAPTAIN'S COMMAND BARS DISAPPEARED AND RECEIVED "FD" FLAG ON EADI, AND "EGPWS INOP" AND "TERRAIN INOP" ON MAP. (FLT 6246) REPLACED NR 1 AHC-85 IN REFERENCE TO AMM. P/N: 622-6190-204 S/N OFF: 1513

Part: DUCT — BLOWN (BLEED AIR SYS) · airframe 30,297 hrs · 42,584 cycles

ON ROTATION DUCT LEAKAGE LIGHT ON LEFT SIDE CAME ON. (FLT 5367) FOUND BLOWN LEFT WRAP AROUND BLEED DUCT. REPLACED LEFT ENGINE WRAP AROUND BLEED DUCT IN REFERENCE TO AMM.

Part: RIB — DAMAGED (LT WING) · airframe 29,407 hrs · 41,315 cycles

DAMAGED RIB 27 WING TIP EDGE. (SERVICE) REPAIRED LEFT WING RIB 27 TRAILING EDGE.

Part: SIGN — BROKEN (CABIN) · airframe 29,407 hrs · 41,315 cycles

EXIT ROW SIGN AT 6A BROKEN. (FLT 5506) REPLACED EXIT ROW'S SEAT 6A EMERGENCY LIGHT ASSEMBLY PER AMM.

Part: WIRE — BROKEN (CABIN) · airframe 29,235 hrs · 41,060 cycles

THE CABIN FLOOR EMERGENCY LIGHTS BETWEEN ROW 3 AND 6 DO NOT ILLUMINATE. (FLT 5478) REPAIRED BROKEN WIRE BELOW FLOOR AT ROW 5.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,201 hrs · 41,016 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 9 IS OUT. (C-CHECK) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,452 hrs · 39,944 cycles

FLOOR EMERGENCY EXIT LIGHT NEAR MCD IS OUT. (FLT 5347) RELAMPED EMERGENCY LIGHT.

Part: WIRE — BROKEN (CABIN) · airframe 28,267 hrs · 39,702 cycles

EMERGENCY LIGHTS ON FLOOR BY ROWS 1 AND 2 ARE INOPERATIVE. (FLT 5322) REPAIRED BROKEN WIRE ON TRACK LIGHTING AT FORWARD CONNECTOR TO RED LIGHTS.

Part: SEQUENCE VALVE — FAILED (LT MLG) · airframe 27,890 hrs · 39,176 cycles

LEFT MAIN GEAR DID NOT RETRACT FOR 2 MINS AFTER RAISING GEAR LEVER. (FLT 6323) REPLACED LEFT INBOARD SEQUENCE VALVE ASSEMBLY AND LEFT GEAR DOWN UNLOCKING ACTUATOR. P/N 120-32943-001, S/N OFF UNREADABLE / P/N 19535-000-01, S/N OFF 11.

Part: SOCKET — FAULTY (CABIN) · airframe 26,917 hrs · 37,851 cycles

OVERHEAD EMERGENCY LIGHT ABOVE ROW 6 FLICKERS. (FLT 6423)REPLACED LIGHT SOCKET FOR EMERGENCY LIGHT ABOVE ROW 6.

Part: SENSOR — FAULTY (LANDING GEAR) · airframe 26,163 hrs · 36,779 cycles

RECEIVED INTERMITTENT "ELEC" LIGHT ON MAP. NUMEROUS RELAYS SWITCHING AND ELECTRICAL BURNING SMELL. (FLT 6571) REPLACED LT WOW SENSOR AND LANDING GEAR RELAY BOX.

Part: SERVO — MALFUNCTIONED (RUDDER) · airframe 25,913 hrs · 36,415 cycles

AFTER ENGAGING F/O'S AUTOPILOT, RUDDER KICKED HARD TAIL RIGHT. (FLT 6810) TROUBLESHOOTING AUTOPILOT SYSTEMS. REPLACED RUDDER PRIMARY SERVO AND SERVO SUPPORT PER AMM.

Part: STRINGER — CRACKED (RT WING) · airframe 25,931 hrs · 36,441 cycles

RIGHT INBOARD WING STRINGER 10 CRACKED BETWEEN RIBS 8 AND 9 AT ACCESS PANEL AREA. (C-CHECK) REPAIRED PER SRM.

Part: STRINGER — CRACKED (LT WING) · airframe 25,931 hrs · 36,441 cycles

LEFT INBOARD WING FUEL TANK LOWER STRINGER 10 IS CRACKED BETWEEN STATION 8-9. (C-CHECK) REPAIRED PER SRM.

Part: ROLLER — OUT OF ADJUST (CABIN DOOR) · airframe 24,754 hrs · 34,745 cycles

MAIN CABIN DOOR DIFFICULT TO CLOSE. (FLT 6263) LUBED DOOR AND ADJUSTED MAIN CABIN DOOR FORWARD LOCK CAM ACTUATING ROD AND UPPER ROLLER.

Part: CUSHION — OUT OF POSITION (F/A SEAT) · airframe 24,742 hrs · 34,728 cycles

MAIN CABIN DOOR HARD TO CLOSE. (FLT 5815) REPOSITIONED FLIGHT ATTENDANT SEAT CUSHION.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 24,683 hrs · 34,646 cycles

MAIN CABIN DOOR WILL NOT SHUT. (FLT 6175) LUBED ROLLERS AND ATTACH POINTS.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 24,641 hrs · 34,586 cycles

FLT 5763 - BAGGAGE SMOKE/FIRE WARNING LIGHT REMAINS ON. REPLACED AFT SMOKE DETECTOR.

Part: BONDING STRAP — OUT OF POSITION (OUTFLOW VALVE) · airframe 24,257 hrs · 34,023 cycles

AT CRUISE CABIN LOST PRESSURIZATION. (FLT 6843) REMOVED BONDING STRAP FROM OUTFLOW VALVE. ALL CABIN O2 MASKS DEPLOYED DUE TO LOSS OF PRESSURIZATION. INSPECTED, FOUND SAFETY WIRE IN MANUAL VALVE BROKEN, NO LONGER SECURED CLOSED. RE-SECURED MANUAL VALVE PER MEL MX ACTION. REMOVED BONDING STRAP FROM ELECTRO-OUTFLOW VALVE ASSEMBLY DUE TO BEING CAUGHT INSIDE OF VALVE BODY. AUTO PRESSURIZATION OPERATES NORMALLY. NO DEFECTS NOTED. MANUAL MODE STILL DEFERRED. PANELS SECURED.

Part: LIGHT — BROKEN (EXTERIOR) · airframe 23,032 hrs · 32,343 cycles

FLT 7756 - EMERGENCY LIGHT ON OUTSIDE OF FUSELAGE RIGHT AFT SIDE INOP. REPLACED LIGHT HOUSING.

Part: LIGHT — DETACHED (CABIN) · airframe 22,998 hrs · 32,303 cycles

FLT 7791 - EMERGENCY EXIT LIGHT AT ROW 9 DISLODGED FROM WALL. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY.

Part: RELAY — MALFUNCTIONED (LANDING GEAR) · airframe 22,620 hrs · 31,822 cycles

FLT 5788 - GEAR WILL NOT RETRACT. REPLACED THE LANDING GEAR RELAY BOX, PN 120-61110-001, SN ON 236905-314, SN OFF 333570.

Part: FLOORBEAM — CORRODED (CORRODED) · airframe 22,715 hrs · 31,964 cycles

DURING C-CHECK, LEFT SIDE FLOOR CROSS MEMBER AT FRAME 39 CORRODED. REPLACED PER SRM.

Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 22,715 hrs · 31,964 cycles

C-CHECK, RIGHT SIDE BELOW COCKPIT FLOOR, SUPPORT ANGLE CRACKED. REPLACED PER SRM.

Part: STRINGER — CRACKED · airframe 22,715 hrs · 31,964 cycles

C-CHECK, STRINGER NEAR NR 2 FUEL ACCESS PANEL CRACKED. REPLACED PER SRM.

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 22,336 hrs · 31,449 cycles

FLT 5446 - BURNING ELECTRICAL ODOR ON FLIGHT DECK. FOUND GALLEY HOT JUGS ARCING. REPLACED.

Part: CONTROL UNIT — OVERSPEED (PROPELLER) · airframe 22,281 hrs · 31,376 cycles

FLT 5549 - RIGHT PROPELLER NP CONTINUALLY SURGED FROM 103 PERCENT TO 95 PERCENT ON CLIMB. REPLACED RIGHT ENGINE PCU, P/N 782490-46, S/N ON, 931245 S/N OFF, 980912.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,214 hrs · 31,281 cycles

OVERHEAD EMERGENCY LIGHT AT MAIN CABIN DOOR INOP (FLT 5459). RELAMPED EMERGENCY LIGHT.

Part: UNKNOWN — SMOKE (GALLEY) · airframe 22,186 hrs · 31,243 cycles

F/A SMELLED SMOKE IN GALLEY AND PILOT SMELLED FAINT ELECTRICAL SMOKE IN COCKPIT (FLT 5138). INSPECTED GALLEY AREA FOR SMOKE, NONE FOUND. ALL SYSTEMS OPERATING NORMAL IN GALLEY.

Part: SEAL — DAMAGED (CARGO DOOR) · airframe 21,368 hrs · 30,160 cycles

FLT 3597 - CABIN ALTITUDE CLIMBED ON DESCENT AND O2 MASKS DEPLOYED. INSPECTED SYSTEM AND REPLACED DAMAGED CARGO DOOR SEAL IAW MM 52-30-01.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 21,368 hrs · 30,160 cycles

FOUND ALL CABIN OXYGEN MASKS DROPPED. INSPECTED AND RESTOWED ALL OXYGEN MASKS AS REQUIRED.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 20,583 hrs · 29,098 cycles

FLT 3676 - FLIGHT ATTENDANT REPORTS DOOR IS HARD TO OPEN AND CLOSE. INSPECTED, CLEANED AND LUBRICATED THE DOOR. NO DEFECTS NOTED.

Part: SIGN — UNSECURE (CABIN) · airframe 20,410 hrs · 28,894 cycles

FLT 3720 - EXIT SIGN AT ROW 6 IS UNSECURE. REPLACED LIGHT ASSEMBLY. OPS CHECK GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 19,503 hrs · 27,655 cycles

EMERGENCY EXIT SIGN AT ROW 9 IS NOT LIGHTING UP. REPAIRED BAD SPLICE CONNECTORS. OPS CHECK GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 19,390 hrs · 27,488 cycles

FOUND EMERGENCY EXIT SIGN OVER ROW 9 IS INOP. REPLACED SPLICE FOR EXIT SIGN AT ROW 9. OPS CHECK GOOD.

Part: A/C PACK — SMOKE · airframe 19,328 hrs · 27,383 cycles

ON TAXI OUT, THE CABIN AND FLIGHT DECK BEGAN TO FILL WITH SMOKE. ASSOCIATED WITH AIR CONDITIONING PACKS. OPERATED BOTH PACKS ON GROUND WITH ENGINE AND APU BLEEDS. FOUND WHEN PACKS SET TO COLD SETTING BOTH PACKS WOULD EMIT SMOKE. TURNED TEMPERATURE SETTING UP AND SMOKE CEASED.

Part: UNKNOWN — ODOR (CABIN) · airframe 18,322 hrs · 25,974 cycles

AFTER LANDING SMELLED ODOR FROM PACKS. REPLACED LEFT WOW PROX SWITCH AND HARNESS. OPERATIONAL CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,870 hrs · 25,386 cycles

AFT LEFT EMERGENCY LIGHT INOP. RELAMPED LEFT AFT EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD.

Part: HINGE — CRACKED (RT MLG DOOR) · airframe 17,812 hrs · 25,319 cycles

UPON POST FLIGHT A CRACK WAS FOUND IN LINKAGE ON RIGHT SIDE INNER AFT LANDING GEAR DOOR. REPLACED RIGHT MLG INBOARD/AFT DOOR AFT HINGE IN REF SRM 51-00-00 . OPERATIONAL CHECKS GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 17,518 hrs · 24,933 cycles

RIGHT PACK PRODUCES SMOKEY SMELL. OPERATIONAL CHECKS GOOD IAW MM 21-00-00. UNABLE TO DUPLICATE DISCREPANCY.

Part: SELECTOR — MALFUNCTIONED (TE FLAPS) · airframe 16,428 hrs · 23,536 cycles

ICE COND LOW SPEED ALARM SYSTEM DOES NOT COME ON WITH REQ PARAMETERS INFLIGHT (SPEED 155 KTS, BOOTS ON FLAPS UP). REPLACED FLAP SELECTOR HANDLE REF EMB 120 MM 27-50-01. OPERATIONAL CHECKS GOOD IAW MM 30-90-00 AND MM 27-50-00, PN 120-64207-615, SN OFF 120-152.

Part: SERVO — MALFUNCTIONED (AUTOPILOT) · airframe 16,378 hrs · 23,480 cycles

BOTH CA AND FO AUTOPILOT WILL NOT TRACK LOCALIZER. REPLACED AILERON SERVO "AUTOPILOT" REF AMM 27-00-03. OPERATIONAL CHECK GOOD.

Part: WARN PANEL — FAULTY (COCKPIT) · airframe 16,206 hrs · 23,274 cycles

DURING CRUISE FLIGHT RECEIVED SEVERAL SPARADIC (STALL WARNING) AURAL WARNINGS. REPLACED STALL WARNING PANEL IAW MM 27-34-08. OPERATIONAL CHECK GOOD.

Part: SIGN — BROKEN (EMERGENCY EXIT) · airframe 15,994 hrs · 22,944 cycles

6A LOWER EMERG EXIT SIGN BROKEN. REPLACED 6A EXIT SIGN ASSY. OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 15,852 hrs · 22,763 cycles

EXIT SIGN OVER ROW 9 ON OVERHEAD BIN INOP. REPAIRED BROKEN WIRE FOR "EXIT" LIGHT ON ROW 9 OVERHEAD BIN. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 15,496 hrs · 22,277 cycles

AFT SECTION OF EMERGENCY LIGHTS INOP. REPLACED AFT ELBP PER MM 33-50-02. OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 15,450 hrs · 22,207 cycles

"EXIT" LIGHT AT ROW 9BC INOP. REPAIRED BROKEN WIRE. OPERATIONAL CHECK GOOD.

Part: COOLING FAN — FAILED (COCKPIT) · airframe 15,223 hrs · 21,872 cycles

BURNING ODOR FROM COCKPIT VENTS. REPLACED LT GROUND COOLING FAN. OPS CHECK GOOD MM 21-51-03.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 14,518 hrs · 20,924 cycles

TOP EMERGENCY LIGHT ON PAX DOOR IS INOPERATIVE. REPLACED LIGHT BULB. OPERATIONAL CHECK GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 13,831 hrs · 19,979 cycles

ONE FORWARD EMERGENCY EXIT RED LIGHT, FLOOR LEVEL, IS MISSING. INSTALLED SERVICEABLE FORWARD RED EMERGENCY LIGHT ON FLOOR AS REQUIRED, OPERATIONAL CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 12,386 hrs · 18,197 cycles

CREW REPORTS NR 1 AUTOPILOT WON'T CAPTURE HDG. REMOVED AND REPLACED NR 1 AUTOPILOT COMPUTER IAW MM 22-10-02. OPS CHECK GOOD IAW MM 22-10-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 12,030 hrs · 17,754 cycles

LEFT FRAME 9 SKIN SUPPORT CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REWORKED LEFT SIDE FRAME 9 PER SERVICE BULLETIN NR 120-53-0073 REV 00 DATED 21 JUL 99.

Part: FRAME — CRACKED (FUSELAGE) · airframe 12,030 hrs · 17,754 cycles

RT FRAME 9 SKIN SUPPORT CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REWORKED RIGHT SIDE FRAME 9 PER SB NR 120-53-0073 REV 00 DATED 21 JUL 99.

Part: FRAME — CRACKED (FUSELAGE) · airframe 12,030 hrs · 17,754 cycles

SKIN SUPPORT BRACKET AT FRAME 12 BEHIND LEFT DV WINDOW CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT BRACKET AT FRAME 12 BEHIND LEFT DV WINDOW IAW EMB SRM 51-10-02, 51-40-00. P/N: 120-12545-001.

Part: ENGINE — LACK OF LUBE (NR 1) · airframe 11,982 hrs · 17,676 cycles

SHUT DOWN NR 1 ENG ON TAXI DUE TO LOSS OF OIL PRESSURE. SERVICED ENGINE WITH OIL AND TIGHTENED OIL FILL CAP. OPS CHECKS GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (STALL WARNING) · airframe 11,817 hrs · 17,477 cycles

NUMBER ONE STALL WARNING SYSTEM TEST DOES NOT CLEAR THE STALL WARNING ANNUNCIATION FROM THE MAP. REMOVED AND REPLACED STALL WARNING TEST PANEL. OPS CHECK GOOD IAW 27-00-00.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 11,817 hrs · 17,477 cycles

FORWARD EMERGENCY LIGHTS INOP. REMOVED AND REPLACED FORWARD EMERGENCY BATTERY PACK IAW EMB MM 33-50-02. OPS CHECK GOOD.

Part: STRUCTURE — DAMAGED (RT TE FLAPS) · airframe 10,931 hrs · 16,301 cycles

SEVERAL LOOSE RIVETS FOUND ON UNDERSIDE OF RT NACELLE FLAP TRAILING EDGE. ALSO UNUSUAL LARGE DRAIN HOLE IN UNDERSIDE AT UPPER CORNER. FOUND DURING LINE INSPECTION. REMOVED AND REPLACED RIGHT NACELLE FLAP IAW MM 27-50-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,931 hrs · 16,301 cycles

WIRES PULLED OUT OF EMERGENCY EXIT LIGHTS ON LEFT ROW. REPLACED AFT MOST EMERGENCY FLOOR LIGHT ASSEMBLY. OPS CHECK GOOD.

Part: WARNING SYSTEM — ACTIVATED (NR 2 ENGINE) · airframe 10,052 hrs · 14,969 cycles

TRIPLE CHIME ''OIL'' WARNING ON ROTATION. FLUCTUATION 45 TO 55 PSID ON NR 2 ENGINE. RETURNED TO SBA. ADDED 1-1/2 QUARTS OF OIL TO NR 2 ENGINE. RAN NR 2 ENGINE EXTENSIVELY. COULD NOT DUPLICATE LOW OIL PRESS OR FLUCTUATION. COMPLIED WITH ST72-344.

Part: BALLAST — SHORTED (LAVATORY) · airframe 9,213 hrs · 13,706 cycles

ELECTRICAL FUMES/BURNING SMELL IN AIRCRAFT. FOUND LIGHT BALLAST SHORTED. COULD NOT DUPLICATE BURNING SMELL. INSPECTED GALLEY BALLAST FOR EVIDENCE OF BURNING. NO BURN DETECTED. REMOVED AND REPLACED LAV LIGHT BALLAST FOR POSSIBLE CAUSE OF BEING BAD IAW MM 33-22-00. OPS CHECK GOOD. NO DEFECTS NOTED.

Part: WIRE — BROKEN (CABIN) · airframe 8,926 hrs · 13,264 cycles

EMERGENCY LIGHTS OUT ON ROW 9. REPAIRED BROKEN WIRE IN OVERHEAD BIN AT ROW 9. OPS CHECK GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 8,408 hrs · 12,431 cycles

ROW 5 RIGHT SIDE EXIT SIGN NOT ILLUMINATED. REMOVED AND REPLACED ROW 5 RIGHT SIDE EXIT SIGN FIXTURE. OPS CHECK GOOD.

Part: COMPUTER — FAULTY (E/E BAY) · airframe 8,316 hrs · 12,272 cycles

CAPTAIN SIDE FLIGHT DIRECTOR FLAGGED AND F/O'S FLT DIRECTOR PITCHES +/- 10 DEGREES. REMOVED AND REPLACED CAPTAIN'S AHARS COMPUTER. S/N OFF: 422.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 8,203 hrs · 12,117 cycles

FLOOR CROSS BRACE ON RIGHT SIDE PITTED BEYOND LIMITS AT STATION 38.5. REPLACED FLOOR CROSS BRACE ON RIGHT SIDE AT STATION 38.5 IAW SRM 53-20-10 WITH SERVICEABLE PART.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 8,203 hrs · 12,117 cycles

FLOORBOARD BRACE ON LEFT SIDE AT STATION 38 CORRODED. REPLACED FLOORBOARD CROSS BRACE WITH SERVICEABLE PART IAW SRM 53-20-10.

Part: FLOOR SUPPORT — CORRODED (FUSLEAGE) · airframe 8,203 hrs · 12,117 cycles

REINFORCEMENT ANGLE FOR RIGHT FLOOR PROP AT FRAME 13 CRACKED. REMOVED AND REPLACED BRACKET AT FRAME 13 RIGHT FLOOR PROP WITH A NEW PART. P/N: 120-08000-001.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 7,773 hrs · 11,497 cycles

MIDDLE EMERGENCY LIGHT STRIP INOP.REPLACED BATTERY. OPS CHECK GOOD.

Part: RELAY — FAILED (ELECTRICAL PWR) · airframe 7,038 hrs · 10,391 cycles

LOST NR 1 INVERTER ON CLIMBOUT, 115 VAC. REMOVED AND REPLACED 115 VAC SENSE RELAY K0005. OPS CHECK GOOD.

Part: LATCH — LOOSE (FUEL DOOR) · airframe 5,817 hrs · 8,561 cycles

ABORTED TAKEOFF FOR DOOR LIGHT ON MAP. FOUND FUEL DOOR LATCH LOOSE, SECURED LATCH, LIGHT OUT ON DECK. OPS CHECKS GOOD.

Part: LOCK — UNSECURE (FUEL DOOR) · airframe 5,705 hrs · 8,374 cycles

SERVICE DOOR LIGHT ILLUMINATED DURING TAKEOFF ROLL. ABORTED TAKEOFF. FOUND ONE CAMLOCK UNSECURE ON INBOARD FUEL DOOR. RELATCHED DOOR, OPS CHECKS GOOD.

Part: ACTUATOR — FAILED (ELEVATOR TRIM)

ELEVATOR TRIM FREEZES INFLIGHT WITH AND WITHOUT AUTO PILOT. REMOVED AND REPLACED BOTH TRIM TAB ACTUATORS AS PER MM 27-00-01.

Part: SENSOR — FAILED (LT MLG)

LEFT A GREEN LIGHT REMAINS ON AT ALL TIMES WHEN CYCLING LANDING GEAR, LEFT RED A DISAGREEMENT LIGHT STAYS OUT. RETURNED TO FIELD. REPLACED LEFT STRUT GREEN A LIGHT PROX SENSOR. SWUNG GEAR SEVERAL TIMES, OPS CHECKS GOOD.