N224SW

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 42,198 hrs · 54,818 cycles

FWD GALLEY FLASHLIGHT INOPERATIVE. R & R FWD GALLEY FLASHLIGHT BATTERIES WITH SERVICEABLE UNITS. OPS CHECKED GOOD.

Part: SKIN — CRACKED (RT NACELLE) · airframe 41,801 hrs · 54,302 cycles

RIGHT ENGINE TOP COWL, WHERE THE FORWARD INBD DOOR HOLD OPEN ROD ATTACHES HAS A CRACK APPROXIMATELY 1.5" LONG. REPAIRED 1.5" LONG CRACK ON HALF FRAME. LOCATED ON RT ENGINE TOP COWL BY FWD INBD DOOR HOLD OPEN ROD ATTACHES IAW ETD.

Part: MOUNT — CHAFED (LT ENGINE) · airframe 41,801 hrs · 54,302 cycles

LEFT ENGINE INBD FRONT MOUNT CHAFED AFT OF MOUNTING BOLT. REPLACED LT ENG FWD INBD UPPER MOUNT IAW SRM AND AMM.

Part: AHRS — FAILED (NR 2) · airframe 41,477 hrs · 53,892 cycles

WITH AUTOPILOT OFF, FIRST OFFICER'S HEADING INDICATOR STARTED PROCESSING & THE A/C DID AN UNCOMMANDED TURN TO THE RIGHT. FLT 5303 REPLACED NR 2 AHARS COMPUTER, PN 622-6190-204, SN ON 2667 & SN OFF 1589.

Part: MODULE — FAULTY (COCKPIT) · airframe 41,272 hrs · 53,602 cycles

AFTER SELECTING THE GEAR DOWN ON, RECEIVED THE AURAL LANDING GEAR RED GEAR WARNINGS. AFTER ATC VERIFIED THAT THE GEAR WAS DOWN, COMPLIED WITH THE QRH & LANDED. FLT6300 R & R LANDING GEAR HANDLE MODULAR ASSEMBLY IAW AMM. INSPECTED LANDING GEAR INDICATION HARNESSES, NO DEFECTS NOTED. SWUNG GEAR SEVERAL TIMES & OPERATIONS CHECKED GOOD. PN 120-38594-401 SN ON 120346 SN OFF 120344

Part: UNKNOWN — SMOKE (CABIN & COCKPIT) · airframe 41,265 hrs · 53,591 cycles

SMOKE IN CABIN & COCKPIT. FLT5373 INSPECTED BOTH PACKS & ALL ENG BLEED VLVS. OPERATED ALL THE AIRCRAFT SYSTEMS, NO SMOKE OR BURNED SMELL WAS FOUND.

Part: RELAY — MALFUNCTIONED (LANDING GEAR) · airframe 41,265 hrs · 53,591 cycles

BURNING ELECTRICAL SMELL IN FLIGHT DECK. CIRCUIT BREAKER HYD GREEN QTY POPPED, CIRCUIT BREAKER UP DOWN ON GEAR POPPED, SMELL WENT AWAY. RAN QRH, RESET CIRCUIT BREAKER FOR GEAR OPERATION CIRCUIT BREAKER POPPED ALMOST IMMEDIATELY. HAD TO FREEFALL GEAR, NORMAL LANDING. FLT 5521 REPLACED LANDING GEAR RELAY BOX ASSEMBLY IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 41,181 hrs · 53,476 cycles

ROW 9 LOWER EMERGENCY EXIT SIGN IS BROKEN. FLT 6452 REPLACED EMERGENCY LIGHT SIGN AT ROW 9 IAW WDM, PN 10-1262-1.

Part: DUCT — FAILED (BLEED AIR SYS) · airframe 40,896 hrs · 53,067 cycles

DURING CLIMB HEARD A LOUD POPPING SOUND FROM THE LT SIDE OF THE AIRCRAFT FOLLOWED BY A LT BLEED OVERHEAT CAUTION MESSAGE. FLT#5446 REPLACED WING ROOT ENGINE BLEED AIR DUCT IAW AMM.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 40,843 hrs · 52,978 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. FLT#5373 LUBED & OPERATED MAIN CABIN DOOR.

Part: HANDLE — LACK OF LUBE (CABIN DOOR) · airframe 40,800 hrs · 52,917 cycles

MAIN CABIN DOOR DIFFICULT TO LATCH CLOSED. FLT#5369 LUBED MAIN CABIN DOOR HANDLE.

Part: LINKAGE — LACK OF LUBE (PAX DOOR) · airframe 40,679 hrs · 52,748 cycles

PAX DOOR DIFFICULT TO OPEN & CLOSE. FLT#6453 LUBRICATED PAX DOOR LATCHING & ACTUATING LINKAGE & ROLLER ON PAX DOOR CUT OUT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,668 hrs · 52,732 cycles

EMERGENCY LIGHT ON CEILING NEAR ROW 7 IS BURNED OUT. FLT#6268 RELAMPED.

Part: HANDLE — DIRTY (CABIN DOOR) · airframe 40,653 hrs · 52,709 cycles

MAIN CABIN DOOR IS DIFFICULT TO OPEN & CLOSE. FLT#5343 CLEANED & LUBED MAIN DOOR HANDLE & ROLLERS, ADJUSTED MAIN CABIN DOOR LOCK CAM ACTUATING RODS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,506 hrs · 52,498 cycles

COCKPIT FRAME BELOW LT DIRECT VISION WINDOW IS CRACKED. C-CHECK REPLACED COCKPIT FRAME BELOW LT DIRECT VISION WINDOW IAW AMM.

Part: STRINGER — CRACKED (RT WING) · airframe 40,506 hrs · 52,498 cycles

LOWER WING STRINGER NR 8 CRACKED AT RT DRY BAY. C-CHECK REPLACED INBD SECTION OF RT WING LOWER STRINGER NR 8 & SPLICED SECTIONS AT RIB 5 & 6 IAW AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,506 hrs · 52,498 cycles

INTERNAL CORROSION ON FRAME 23 BETWEEN STRINGER 21R & STRINGER 20R. C-CHECK INSTALLED PERMANENT REPAIR IAW ETD.

Part: CLEAT — CRACKED (LT WING) · airframe 40,506 hrs · 52,498 cycles

CRACKED SKIN CLEAT IN LT WING NR 4 FUEL CELL OTBD UPPER FORWARD. C-CHECK NEW SKIN CLEAT INSTALLED ON LT WING OTBD UPPER FORWARD NR 4 FUEL PANEL IAW SRM.

Part: CLEAT — CRACKED (LT WING) · airframe 40,506 hrs · 52,498 cycles

CRACKED SKIN CLEAT IN LT WING NR 5 FUEL CELL UPPER INBD. C-CHECK NEW SKIN CLEAT INSTALLED ON LT WING AT NR 5 FUEL CELL UPPER INBD IAW SRM.

Part: CLEAT — CRACKED (RT WING) · airframe 40,506 hrs · 52,498 cycles

RT WING NR 4 FUEL PANEL UPPER OTBD SKIN CLEAT CRACKED. C-CHECK NEW UPPER OTBD CLEAT INSTALLED ON RT WING AT NR 4 FUEL PANEL IAW SRM.

Part: CLEAT — CRACKED (RT WING) · airframe 40,506 hrs · 52,498 cycles

RT WING NR 5 FUEL PANEL UPPER OTBD SKIN CLEAT CRACKED. C-CHECK NEW UPPER OTBD SKIN CLEAT ON RT WING AT NR 5 FUEL PANEL IAW SRM.

Part: CLEAT — CRACKED (LT WING) · airframe 40,506 hrs · 52,498 cycles

TWO CRACKED SKIN CLEATS IN LT WING BETWEEN NR 4 & NR 5 FUEL CELLS UPPER. C-CHECK TWO NEW SKIN CLEATS INSTALLED ON LT WING BETWEEN FUEL PANELS NR 4 & NR 5 IAW AMM.

Part: CLEAT — CRACKED (LT WING) · airframe 40,506 hrs · 52,498 cycles

CRACKED SKIN CLEAT LT WING NR 3 FUEL CELL OTBD LOWER. C-CHECK NEW SKIN CLEAT INSTALLED ON LT WING NR 3 FUEL CELL OTBD LOWER IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,524 hrs · 51,179 cycles

EMERGENCY LIGHT NEAR MCD IS BURNED OUT. (FLT 7780) RELAMPED EMERGENCY LIGHT.

Part: BLADE — CRACKED (LT PROPELLER) · airframe 39,497 hrs · 51,147 cycles

LEFT PROP NR 2 BLADE LEADING EDGE IS CRACKED. (SERVICE) REPLACED LEFT PROP NR 2 BLADE IN REFERENCE TO CMM.

Part: LIGHT — NOT SEATED (CABIN) · airframe 38,870 hrs · 50,307 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6283) RE-SEATED OVERHEAD EMERGENCY LIGHT BULB.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,870 hrs · 50,307 cycles

FORWARD OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6376) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,759 hrs · 50,141 cycles

MOST FORWARD OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 6376) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,616 hrs · 49,939 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7802) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,327 hrs · 49,630 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6489) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,867 hrs · 49,076 cycles

EMERGENCY LIGHT AT CABIN DOOR ENTRANCE IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,728 hrs · 48,888 cycles

EMERGENCY LIGHTS OVER THE EXIT ROW ARE OUT. (FLT 7797) REPLACED NR 2 ELBP.

Part: FUSE — BLOWN (CABIN) · airframe 37,252 hrs · 48,316 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7777) REPLACED THE FUSE.

Part: FUSE — FAILED (CABIN) · airframe 37,237 hrs · 48,298 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7767) REPLACED THE NR 1 EMERGENCY LIGHT FUSE.

Part: LIGHT — NOT SEATED (CABIN) · airframe 36,373 hrs · 47,256 cycles

FORWARD OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6312) RE-SEATED LIGHT BULB.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,873 hrs · 46,600 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — LOOSE (ELBP) · airframe 35,809 hrs · 46,528 cycles

EMERGENCY LIGHTS AT ROW 6 INTERMITTENT. (FLT 6232) RE-SECURED ELBP CONNECTOR.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,778 hrs · 46,478 cycles

ALL OF THE FORWARD EMERGENCY LIGHTS ARE INOPERATIVE. (FLT 6312) REPLACED FORWARD ELBP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,675 hrs · 46,339 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. (FLT 7791) RELAMPED EMERGENCY LIGHT.

Part: SIGN — BROKEN (CABIN) · airframe 35,276 hrs · 45,858 cycles

EXIT SIGN NEAR FLOOR AT MAIN CABIN DOOR FELL OFF. (FLT 7767) REMOVED AND REPLACED EXIT LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,602 hrs · 43,856 cycles

FORWARD MOST CABIN OVERHEAD EMERGENCY FLOODLIGHT INOP. (FLT 6237) RELAMPED EMERGENCY LIGHT.

Part: FRAME — CRACKED (RT NACELLE) · airframe 33,575 hrs · 43,820 cycles

RIGHT NACELLE FRAMES CRACKED. (C CHECK) REPLACED FRAMES PER SRM.

Part: CONTROL CABLE — CORRODED (POWER LEVER) · airframe 33,575 hrs · 43,820 cycles

POWER LEVER CONTROL CABLES CORRODED. (C-CHECK) REPLACED PER AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,575 hrs · 43,820 cycles

COCKPIT OVERHEAD FRAME CRACKED. (C-CHECK) REPAIRED PER SRM.

Part: CONTROL CABLE — CORRODED (ELEVATOR) · airframe 33,575 hrs · 43,820 cycles

ELEVATOR CONTROL CABLES CORRODED. (C-CHECK) REPLACED PER AMM.

Part: CONTROL CABLE — CORRODED (RUDDER) · airframe 33,575 hrs · 43,820 cycles

RUDDER CONTROL CABLE CORRODED. (C-CHECK) REPLACED PER AMM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 33,575 hrs · 43,820 cycles

STRINGERS 19R & 18R CORRODED. (C-CHECK) REPAIRED PER SRM.

Part: SPLICE — DAMAGED (EMERGENCY LIGHT) · airframe 33,575 hrs · 43,820 cycles

SECOND EMERGENCY RED LIGHT INOP. (FLT 6546) REPAIRED ENVIRONMENTAL SPLICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,372 hrs · 43,554 cycles

CRACKED AND CORRODED FUSELAGE SKIN, ZONE142. (C-CHECK) REPAIR IN PROGRESS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,363 hrs · 43,544 cycles

SKIN PLATE FORWARD OF LOWER BEACON CRACKED. (SVC CHECK) REPAIRED PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,363 hrs · 43,544 cycles

CENTER EMERGENCY LIGHTS DIM. (FLT 6345) REPLACED BATTERY PACK.

Part: SIGN — BROKEN (CABIN) · airframe 33,356 hrs · 43,537 cycles

EMERGENCY EXIT LIGHT SIGN BROKEN. (FLT 7790) REPLACED LIGHT ASSEMBLY.

Part: RELAY — ODOR · airframe 32,316 hrs · 42,127 cycles

FLT 5793 - STRONG ELECTRICAL SMELL DEVELOPED IN COCKPIT. REPLACED FEEDER PROTECTION RELAY.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 31,637 hrs · 41,203 cycles

FORWARD EMERGENCY DOME LIGHT INOP (FLT 5457). RELAMPED EMERGENCY LIGHT.

Part: FITTING — DIRTY (PAX DOOR) · airframe 31,224 hrs · 40,657 cycles

MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN. (FLIGHT NR 3614) INSPECTED AND CLEANED MAIN CABIN DOOR FITTINGS AND OPERATED DOOR MULTIPLE TIMES. OPS CHECK GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (ROW 5) · airframe 31,177 hrs · 40,591 cycles

ROW 5 OXYGEN MASKS DEPLOYED. (FLIGHT NR 5474) RESTOWED O2 MASKS AS REQUIRED.

Part: LIGHT — BROKEN (GALLEY) · airframe 31,053 hrs · 40,427 cycles

EMERGENCY LIGHT STRIP IS INOP NEAR THE GALLEY. REPLACED EMERGENCY LIGHT STRIP AS REQUIRED.

Part: ROLLER — OUT OF ADJUST (PAX DOOR) · airframe 31,053 hrs · 40,427 cycles

MAIN CABIN DOOR IS DIFFICULT TO OPEN. INSPECTED AND ADJUSTED FORWARD, UPPER ROLLER IAW AMM 52-11-00. OPS CHECK NORMAL.

Part: HANDLE — WORN (PAX DOOR) · airframe 31,053 hrs · 40,427 cycles

FLT 3632 - MAIN CABIN DOOR DOES NOT OPEN PROPERLY FROM INSIDE THE CABIN. REPLACED INNER PAX DOOR HANDLE IAW AMM 52-11-01. OPS CHECK GOOD.

Part: HANDLE — BINDING (PAX DOOR) · airframe 30,856 hrs · 40,178 cycles

MAIN CABIN DOOR HANDLE IS DIFFICULT TO CLOSE AND OPEN, FLIGHT NR 3614. INSPECTED, CLEANED AND OPERATED CABIN DOOR FROM INSIDE AND OUTSIDE WITH NO DISCREPANCIES NOTED.

Part: DOOR — OUT OF ADJUST (PAX DOOR) · airframe 30,586 hrs · 39,856 cycles

FLT 5442 - PAX DOOR IS DIFFICULT TO OPEN AND CLOSE. ADJUSTED AND LUBED CABIN DOOR. OPS CHECK GOOD AT THIS TIME.

Part: LINKAGE — BINDING (PAX DOOR) · airframe 30,183 hrs · 39,359 cycles

FLT 5714 - FLIGHT ATTENDANT REPORTS CABIN DOOR IS DIFFICULT TO OPERATE. LUBRICATED CABIN DOOR LINKAGE AND ROLLERS. OPS CHECKS GOOD.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 30,145 hrs · 39,306 cycles

FLT 5672 - EXIT SIGN BELOW WINDOW IN 6A IS BROKEN. REPLACED EMERGENCY EXIT SIGN AT 6A. OPS CHECK GOOD.

Part: GALLEY TRACK — CORRODED (FUSELAGE) · airframe 30,272 hrs · 39,478 cycles

CORROSION ON FLOOR BUTTSTRAP UNDER FORWARD GALLEY ATTACH TRACK, FOUND AT C-CHECK. REPLACED BUTTSTRAP UNDER FORWARD GALLEY ATTACH POINT IAW EMB 120 SRM 51-40-02 PG 3 SECTION 3A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,272 hrs · 39,478 cycles

LEFT FORWARD FLOOR SEAT TRACK IS CORRODED IN SEVERAL SPOTS, FOUND AT C-CHECK. REPLACED SEAT TRACK IAW EMB 120 MM 53-01-05.

Part: TRACK — CORRODED (GALLEY DOOR) · airframe 30,272 hrs · 39,478 cycles

FORWARD DOOR GALLEY ATTACH TRACK IS CORRODED, FOUND AT C-CHECK. REPLACED FORWARD GALLEY FLOOR ATTACH TRACK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,272 hrs · 39,478 cycles

RIGHT FORWARD SEAT TRACK HAS SURFACE CORROSION IN VERIOUS LOCATIONS, FOUND AT C-CHECK. REPLACED WITH NEW SEAT TRACK IAW EMB 120 MM 53-01-05.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,272 hrs · 39,478 cycles

CORROSION ON FLOOR CENTER FLOORBEAM BUTT STRAP NEAR PAX ENTRANCE, FOUND AT C-CHECK. REPLACED BUTT STRAP IAW EMB 120 SRM 51-40-02 PG 3 SECTION 3A.

Part: STIFFENER — CRACKED (LT NACELLE FLAP) · airframe 29,903 hrs · 38,999 cycles

THE LEFT NACELLE FLAP INTERNAL STIFFENER IS CRACKED. REPLACED THE LEFT NACELLE FLAP ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,170 hrs · 36,652 cycles

FORWARD FLOOR RED EMERGENCY LIGHTS INOP. REPAIRED RED EMERGENCY FLOOR LIGHT BY MCD. OPERATIONAL CHECKS GOOD.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 28,146 hrs · 36,617 cycles

FORWARD CEILING EMERGENCY LIGHT INOP. REPLACED FUSE AND FORWARD CEILING EMERGENCY LIGHT HOUSING. OPERATIONAL CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,062 hrs · 36,501 cycles

EMERGENCY LIGHTS ROW 9 DON'T ILLUMINATE. REPLACED EMERGENCY LIGHT BATTERY PACK PER EMB 120 AMM 33-50-02. OPERATIONAL CHECKS GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 28,062 hrs · 36,501 cycles

FORWARD CABIN EMERGENCY EXIT SIGN INOP. REPAIRED BROKEN WIRE FOR EXIT SIGN. OPERATIONAL CHECKS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,995 hrs · 36,424 cycles

AFT EMERGENCY LIGHTS INOP. REPLACED AFT EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS GOOD.

Part: PROXIMITY SENSOR — SMOKE (COCKPIT) · airframe 27,956 hrs · 36,380 cycles

WHILE ON THE GROUND, THERE WAS SMOKE IN THE COCKPIT. REPLACED LEFT MLG SHOCK ABSORBER PROX SENSOR IAW 120 MM 32-01-01. OPERATIONAL CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,765 hrs · 34,787 cycles

EMERGENCY LIGHTS AT ROW 6 "EXIT" AND FLOOR LIGHTS NEAR ROW 6 ARE NOT WORKING. REPLACED MID BATTERY PACK ELBP. OPERATIONAL CHECK GOOD.

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 26,472 hrs · 34,367 cycles

TAKEOFF AURAL WARNING FOR "FLAPS AND AUTOFEATHER" CAME ON AFTER FLAP RETRACTION AT 1000' AGL. INSTALLED A SERVICEABLE FLAP SELECTOR AND FLAP FCU. INSTALLED NEW NOSE SHOCK RELAY K0122; REPLACED NLG WOW SENSOR. RESERVICED STRUT DUE. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (RUDDER) · airframe 26,462 hrs · 34,344 cycles

COULD NOT DEPRESS RIGHT RUDDER AFTER TAKEOFF. REPLACED GREEN SYSTEM ACTUATOR IAW MM 27-22-00. OPERATIONAL CHECK GOOD.

Part: SERVO — MALFUNCTIONED (AUTOPILOT) · airframe 25,383 hrs · 32,861 cycles

GRINDING NOISE HEARD WITH YAW ENGAGED INFLIGHT, VIBRATION FELT THOUGHT PEDALS. REPLACED RUDDER AUTOPILOT SERVO IAW MM 22-10-05. OPERATIONAL CHECK GOOD IAW MM 22-10-00.

Part: SERVO — WEAK (STICK SHAKER) · airframe 25,288 hrs · 32,745 cycles

FO'S STICK SHAKER VERY WEAK. REPLACED FO'S STICK SHAKER SERVO IAW EMB 120 AMM 27-34-04. OPERATIONAL CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 25,045 hrs · 32,449 cycles

ONE WHITE FLOOR EMERG LIGHT INOP. REPLACED LIGHT BULB TO WHITE EMERG ROW LIGHT STRIPE BY ROW 7. OPERATIONAL CHECK GOOD.

Part: CIRCUIT BOARD — MALFUNCTIONED (INSTR LIGHTING) · airframe 24,761 hrs · 32,102 cycles

SMOKE AND BURNING ODOR COMING FROM BACKUP BATTERY BACKLIGHTING PANEL. REPLACED BACK-UP BATTERY CIRCUIT BOARD AND PANEL. OPS CHECK GOOD.

Part: FIXTURE — BROKEN (EMERGENCY LIGHT) · airframe 23,857 hrs · 30,979 cycles

LEFT OVERWING EMERGENCY EXIT LOWER RIGHT FIXTURE BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LOWER LIGHT FIXTURE IAW MM 33-51-00, OPERATIONAL CHECK GOOD.

Part: SPLICE — DIRTY (PAX DOOR) · airframe 23,605 hrs · 30,670 cycles

MAIN CABIN DOOR HANDLE WILL NOT ACTUATE DOOR LOCKS. INSTALLED NEW BOLT ON MAIN CABIN DOOR INSIDE LOCKING HANDLE AND CLEANED OUT SPLICES ON HANDLE AND DOOR HANDLE SHAFT IAW MM 52-11-00. OPERATIONAL CHECK GOOD.

Part: CONTROL PANEL — FAILED (AUTO PILOT) · airframe 22,831 hrs · 29,682 cycles

AUTOPILOT ELEVATOR SERVO FAILURE ON FINAL APPROACH. REPLACED AUTOPILOT ENGAGE PANEL ASSY WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD.

Part: SERVO — MALFUNCTIONED (RUDDER YAW) · airframe 22,765 hrs · 29,587 cycles

WITH THE RUDDER YAW ENGAGED DURING APPROACH, THERE WERE SEVERAL MODERATE VIBRATIONS FELT ON THE RUDDER PEDALS (BOTH SIDES). REMOVED AND REPLACED RUDDER SERVO. OPERATIONAL CHECK GOOD IAW MM 22-10-00.

Part: CONTROL PANEL — MALFUNCTIONED (STALL WARNING) · airframe 22,701 hrs · 29,471 cycles

RIGHT STALL WARNING SYSTEM DOES NOT TEST. REMOVED AND REPLACED STALL WARNING PANEL, OPERATIONAL CHECK GOOD IAW EMB MM 27-36-00.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 22,056 hrs · 28,676 cycles

WHEN A/P ON CAPTAIN'S SIDE, OCCASIONALLY THE A/P WOULD INITIATE A CLIMB, THEN DESCENT ON ITS OWN. A/P AURAL DID NOT COME ON, SEEMED LIKE AN ELEVATOR FLUCTUATION. REPLACED NR 1 APC-65B IAW MM 22-10-02. OPS CHECK GOOD IAW MM 22-10-00. P/N: 622-8315-402, S/N ON: 2966, S/N OFF: 2947.

Part: HUB — CORRODED (PROPELLER) · airframe 22,031 hrs · 28,647 cycles

RIGHT PROP HUB ASSEMBLY HAS CORROSION DAMAGE. DISCOVERED DURING E001 INSPECTION. REPLACED RIGHT PROP HUB ASSEMBLY WITH SERVICEABLE UNIT IAW MM 61-10-00. S/N OFF 1823.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,560 hrs · 28,072 cycles

EMERGENCY LIGHT NEAR MAIN CABIN DOOR INOP. REMOVED AND REPLACED FORWARD EMERGENCY LIGHT POWER SUPPLY IAW MM 33-50-02. OPS CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (RUDDER) · airframe 20,994 hrs · 27,374 cycles

ON CLIMBOUT RIGHT RUDDER PEDDLE FROZE. RAN QRH, TURNED OFF BLUE SYSTEM AND REGAINED CONTROL. REPLACED UPPER RUDDER ACTUATOR IAW 27-22-02. LEAK AND OPS CHECK GOOD.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 20,982 hrs · 27,360 cycles

EMERGENCY LIGHTING INOPERATIVE, ROW 9 AND AFT. REMOVED AND REPLACED AFT ELBP IAW EMB120 MM 33-50-02. OPS CHECK GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (AUTOPILOT SYS) · airframe 20,854 hrs · 27,206 cycles

THE AUTOPILOT FAILURE WITH AP LIGHT ON FCP AND AUTOPILOT PANEL. THE CAPTAIN'S AP WAS SELECTED. REMOVED AND REPLACED AUTOPILOT CONTROL PANEL APPG5A WITH SERVICEABLE UNIT. AUTOPILOT OPS CHECK GOOD IAW 22-10-00. PN: 622-6284-006.

Part: ENGINE — OVERSERVICED (LT & RT) · airframe 20,576 hrs · 26,823 cycles

AFTER SWITCHING FROM APU TO ENGINE BLEED, SMOKE FILLED THE AFT CABIN . SMOKE AND ODOR DISSIPATED GRADUALLY PRIOR TO LANDING. FOUND LEFT AND RIGHT ENGINES TO BE OVER-SERVICED. REMOVED 1 QT OF OIL FROM EACH ENGINE. RAN ENGINES AND AIRCONDITIONING PACKS IAW 21-00-00. NO SMOKE NOTED AT THIS TIME.

Part: FUSE — LOOSE (INDICATOR) · airframe 20,335 hrs · 26,536 cycles

TEN MINUTES AFTER TAKEOFF F/O'S ADI & EHSI WENT INOP WITH ALL FLAGS, ATT DISPLAY CAUTION LIGHT ILLUMINATED. AP WOULD NOT ENGAGE, AND TCAS WAS INOP. RETURNED TO FIELD. FOUND FUSE F0029 NOT SECURE IN FUSE HOLDER. VERIFIED FUSE GOOD AND REINSTALLED INTO FUSE HOLDER AND REPLACED AUX GEN 2 BUS 2 CONTROL RELAY K0396. F/O'S ADI, EHSI, AUTOPILOT AND TCAS, OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 20,201 hrs · 26,379 cycles

EMERGENCY FLOOR LIGHT AT 6A BURNED OUT. REMOVED AND REPLACED LAMP. OPS CHECK GOOD. P/N OL-3071 BPE.

Part: PLUNGER — OUT OF ADJUST (MLG) · airframe 20,178 hrs · 26,349 cycles

DURING TAKEOFF RIGHT MAIN LANDING GEAR WOULD NOT RETRACT. CYCLED GEAR DOWN AND RECEIVED ALL GEAR DOWN INDICATIONS. RETURNED TO LAX. ADJUSTED RIGHT GEAR DOOR PLUNGER. SWUNG GEAR NUMEROUS TIMES. OPS CHECKS GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 20,148 hrs · 26,304 cycles

RED EMERGENCY LIGHTS ON FLOOR (BOTH) AT MAIN CABIN DOOR ARE INOP. REWIRED BROKEN WIRES ON FORWARD EMERGENCY RED LIGHTS ON THE FLOOR. OPS CHECKS GOOD.

Part: ACTUATOR — MALFUNCTIONED (RT MLG) · airframe 19,997 hrs · 26,114 cycles

ON DEPARTURE, RT MAIN GEAR DISAGREEMENT. A & B LIGHTS REMAIN ON AND RIGHT MAIN GEAR WOULD NOT RETRACT AS OBSERVED BY TOWER. RECYCLED THE GEAR 3 TIMES BEFORE RIGHT MAIN GEAR WOULD RETRACT. A & B DISAGREEMENT LIGHTS THEN EXTINGUISHED. RETURNED TO SLC. REPLACED MAIN LANDING GEAR ACTUATOR ON RIGHT SIDE PER MM 32-32-10. OPS CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (LT MLG) · airframe 19,753 hrs · 25,818 cycles

DURING GEAR RETRACTION ON TAKEOFF, THE LEFT MAIN GEAR RED A AND B LIGHTS REMAINED ILLUMINATED AND A NOTICEABLE DRAG CAME FROM THE LEFT SIDE. RETURNED TO DEN. REMOVED AND REPLACED LEFT MAIN GEAR ACTUATOR IAW MM 32-11-00. S/N OFF 237.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 19,236 hrs · 25,180 cycles

EMERGENCY FLOOR LIGHTING AT ROW 5 AND 6 INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY. OPS CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 18,844 hrs · 24,698 cycles

A 767 POWERED UP ACROSS A RUNWAY IN FRONT OF AIRCRAFT, BLOWING ROCKS AND CRACKING THE LEFT WINDSHIELD. INSTALLED SERVICEABLE WINDSHIELD ON LT SIDE IAW 56-10-01.

Part: ACTUATOR — LEAKING (T/E FLAP) · airframe 18,837 hrs · 24,689 cycles

ON SHORT FINAL, LOST GREEN HYD FLUID & PSI AFTER EXTENDING THE FLAPS TO 25 DEGREES. REMOVED THE RT FLAP ACTUATOR AND INSTALLED A SERVICEABLE ACTUATOR. SERVICED THE HYD SYSTEM AS NEEDED. OPS CHECK GOOD, LEAK CHECK GOOD.

Part: COOLING FAN — MALFUNCTIONED (CABIN) · airframe 18,800 hrs · 24,644 cycles

ON TAXI OUT, STRONG ELECTRICAL ODOR IN FLIGHT DECK, THEN F/A REPORTS A VERY LOUD WHIPPING & CRACKING NOISE IN THE BACK OF CABIN. RETURNED TO GATE. REPLACED LEFT PACK GROUND COOLING FAN. RAN BOTH PACKS & BOTH ENGINES. ALL CHECKS NORMAL.

Part: BOOT — DAMAGED (RT WING) · airframe 18,245 hrs · 23,958 cycles

FOUND RIGHT INBOARD DEICE BOOT RIPPED. REMOVED & REPLACED DEICE BOOT IAW 30-10-00..

Part: FCU — MALFUNCTIONED (T/E FLAP) · airframe 17,906 hrs · 23,559 cycles

FLAP CONTROL FAULT, INBOARD FLAPS STUCK. REPLACED FCU WITH SERVICEABLE UNIT. OPS CHECK GOOD.

Part: WIRE HARNESS — MALFUNCTIONED (LT ENGINE) · airframe 17,541 hrs · 23,131 cycles

CLIMBING OUT OF GJT THROUGH 16,000 EXPERIENCED A TORQUE DROP FLUCTUATION ON LEFT ENGINE TO 30 PERCENT. EXPERIENCED CONTINUED TORQUE FLUCTUATIONS IN CLIMB THROUGH 19,000. RESET LEFT ENGINE EEC WITH NO CHANGE. RETURNED FOR PRECAUTIONARY LANDING WITH CONTINUED TORQUE DROPS ON LEFT ENGINE. REPLACED LEFT ENGINE WIRING HARNESS. PERFORMED EXTENSIVE ENGINE RUNS IAW MM 71-00-00. OPS CHECK GOOD. NO DEFECTS NOTED.

Part: LOCK — FROZEN (PAX DOOR) · airframe 17,453 hrs · 23,026 cycles

MAIN CABIN DOOR WILL NOT OPEN SMOOTHLY. FOUND UPPER DOOR CENTERING PLATES TOO TIGHT. ADJUSTED AND FOUND AFT OVER CENTER LOCK FROZEN. REMOVED AFT SHAFT, CLEANED AND LUBED, REINSTALLED SHAFT. OPS CHECK GOOD IAW 52-11-00.

Part: FLUX DETECTOR — FAULTY (LT & RT) · airframe 17,133 hrs · 22,653 cycles

FIRST OFFICER'S HDG AND GYRO FLAGS ON EHSI & ADI. REMOVED AND REPLACED LEFT AND RIGHT FLUX DETECTORS PER 34-21-03. OPS CHECK GOOD.

Part: BOOT — FAILED (LT WING) · airframe 16,946 hrs · 22,421 cycles

LEFT WING MIDDLE AND RIGHT WING MIDDLE DEICE BOOT FAILED IN FLIGHT BOTH TIMES. RETURNED TO SLC. REMOVED AND REPLACED LEFT MIDDLE DEICE BOOT WITH NEW IAW EMB 120 MM 30 AND GOODRICH FAST BOOT INSTALLATION INSTRUCTIONS. OPS CHECK GOOD. P/N P29S-7D5135-27, S/N ON MT25530, S/N OFF MK84510.

Part: CONTACTOR — DIRTY (CARGO DOOR) · airframe 16,921 hrs · 22,390 cycles

DOORS AURAL WARNING AND CARGO DOOR LIGHT ILLUMINATED DURING FLIGHT. CLEANED CONTACTORS. OPS CHECK GOOD AT THIS TIME.

Part: FLAP TRACK — DIRTY (TE FLAPS) · airframe 16,624 hrs · 22,039 cycles

WHEN SELECTING FLAPS 25 DEGREES THE COMMAND BARS WENT TO 25 DEGREES, BUT ALL THREE PAIRS OF FLAPS STAYED AT 15 DEGREES. WE GOT A CONTROL FAULT WHICH RESET AFTER RUNNING THE QRH.CLEANED FLAP TRACKS. PERFORMED OPS CHECK OF FLAP SYSTEM. OPS CHECK GOOD.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 15,995 hrs · 21,318 cycles

ABORTED TAKEOFF DUE TO ''HIGH SPEED WARNING''. REMOVE AND REPLACE CAPTAIN'S AIRSPEED INDICATOR. OPS CHECK GOOD. DONE IAW MM 34-12-01. SN ON AH485 SN OFF AH790

Part: ACTUATOR — OUT OF ADJ (LT MLG) · airframe 15,233 hrs · 20,340 cycles

LEFT MAIN LANDING GEAR WOULD NOT FULLY RETRACT AFTER TAKEOFF, (BOTH A AND B RED DISAGREEMENT LIGHTS ILLUMINATED). RETURNED TO RDM. TROUBLESHOT SYSTEM. FOUND LEFT MAIN GEAR ACTUATOR OUT OF ADJUSTMENT. ADJUSTED AS PER EMB MM 32-32-11. OPS CHECKS GOOD.

Part: CONTROLLER — MALFUNCTIONED (CABIN) · airframe 15,199 hrs · 20,292 cycles

AUTO PRESSURIZATION BECAME VERY ERRATIC DURING CLIMBOUT. RETURNED TO SFO. DEF AUTO PRESSURIZATION AS PER MEL 21-31-1A CW MX PROCEDURE PER MEL APPX A. VALVE SAFTIED CLOSE. REPLACED ELECTRONIC CONTROLLER IAW EMB 120 MM 21-30-01. OPS CHECK GOOD. (P/N ON 22201T011400) (S/N ON 164) (S/N OFF 518).

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 14,906 hrs · 19,949 cycles

FLAP DISAGREEMENT AFTER LANDING WHILE BRINGING FLAPS UP. INSTALLED SERVICABLE NACELLE FLAP ACTUATOR TO LEFT SIDE IAW MM 27-50-00 AND RII 27-307. OPS CHECK GOOD, LEAK CHECK GOOD. PN ON 343100-1001 SN ON 1259 SN OFF 0014

Part: BOOT — FAILED (VERTICAL STAB) · airframe 14,551 hrs · 19,528 cycles

TIMER ONE LIGHT VERTICAL STABILIZER BOOT FAILED. RESET TO TIMER TWO, VERTICAL BOOT FAILED FOR SECOND TIME. FOLLOWED QRH PROCEDURE AND ALL BOOTS FAILED. REPEATED THREE MORE TIMES, EACH TIME ALL BOOT SECTIONS FAILED. DIVERTED TO IDA. RAN AIRCRAFT AND PERFORMED LEAK CHECK OF ALL DEICE EQUIPMENT. LEAK CHECK BRAIDED ENGINE BLEED LINES, NO LEAKS DETECTED. REMOVED AND REPLACED LEFT FORWARD EJECTOR VALVE IAW MM 30-20-04, RAN AIRCRAFT DEICE SYSTEM. OPS CHECKS GOOD AT THIS TIME.

Part: PRESSURE SWITCH — LEAKING (RUDDER) · airframe 14,235 hrs · 19,169 cycles

APPROX 5 MINUTES AFTER DEPARTURE RIGHT SIDE HYDRAULIC RESERVOIR LOW PRESSURE LIGHT ILLUMINATED FOLLOWED BY TOTAL LOSS OF THE BLUE HYDRAULIC FLUID ACTUATING THE LOW LEVEL LIGHT. RETURNED TO SLC PER QRH. FOUND BLUE RUDDER SYSTEM PRESSURE SWITCH TO BE LEAKING. REMOVED AND REPLACED SWITCH. LEAK CHECKS OK. (S/N 1359) 0N, (S/N 0739) OFF.

Part: SOCKET — LOOSE (AHRS) · airframe 14,186 hrs · 19,117 cycles

AT CRUISE ALT RIGHT AHRS FAILED. RETURNED TO SLC. RESET ON GROUND AFTER LANDING. FOUND FUSE SOCKET LOOSE. REINSERTED ONE 107 FUSE AND SECURED. OPS CHECKS GOOD.

Part: DISPLAY — FAILED (AHRS) · airframe 14,123 hrs · 19,041 cycles

ALT DISP ON MAP. REMOVED NR 2 AHRS AND INSTALLED SERVICEABLE UNIT IAW MM 34-21-01 AND RE-INITIALIZED. OPS CK GOOD.

Part: INVERTER — FAILED (AHRS) · airframe 14,123 hrs · 19,041 cycles

ATTITUDE DISPLAY MAP REOCCURRED ON 2ND ATTEMPT FOR SUN, CLIMBING THROUGH 18,000. RETURNED TO SLC. REMOVED AND REPLACED NR 2 INVERTER IAW 24-20-01, OPS CHECKS GOOD. P/N ON: PC251-1C, S/N: 7193, S/N OFF: 8893.

Part: GASKET — MISINSTALLED (RT PRESS REG)

RIGHT DUCT LEAK LIGHT CAME ON CLIMBING OUT OF GJT. SHUT DOWN ENGINE AFTER THREE MINUTES. FOUND GASKET ON RIGHT PRESSURE REGULATOR CANISTER TO HAVE BEEN INCORRECTLY INSTALLED. REINSTALLED GASKET IN PRESSURE REGULATOR CANISTER IAW MM 30-10-00. RAN AIRCRAFT AND OPS CHECKS GOOD AT THIS TIME.

Part: PRESS REG — FAILED (RT DEICE SYS)

ON CLIMBOUT FROM SLC RIGHT DUCT LEAK CAME ON. RETURNED TO SLC. REPLACED RIGHT DEICE PRESSURE REGULATOR. OPS CHECKS GOOD WITH NO LEAKS FOUND.

Part: HANDLE — FAILED (LANDING GEAR)

LEFT B-SYSTEM GREEN LIGHT ILLUMINATED IN FLIGHT. RETURNED TO FIELD. REPLACED LANDING GEAR SELECTOR HANDLE. LANDING GEAR INDICATION OPERATES NORMALLY IAW MM 32-60-00.

Part: ACTUATOR — FAILED (RT TE FLAP)

LOSS OF BLUE SYSTEM DUE TO LOSS OF ALL FLUID. SERVICED BLUE SYSTEM AS NECESSARY AND REPLACED RIGHT NACELLE FLAP ACTUATOR IAW MM 27-50-00.

Part: INLET BOOT — FAILED (RT ENGINE)

RIGHT ENGINE INLET DE-ICE BOOT FAILED IN FLIGHT. RETURNED TO FIELD. REPLACED INLET DUCT ASSEMBLY WITH SERVICEABLE DUCT AND DE-ICE BOOT. OPS CHECKS GOOD.

Part: WARNING LIGHT — ILLUMINATED (RT MLG)

RIGHT MAIN GEAR RED LIGHT ON AFTER TAKEOFF AND GEAR RETRACTION. RETURNED TO LAX. RETRACTED GEAR DOORS AND PERFORMED GEAR CHECK. ALL OPS CHECKS GOOD.

Part: SEAT TRACK — CORRODED (CABIN)

SEAT TRACK SECTION FOR FORWARD INBOARD CORNER OF GALLEY CORRODED. REPLACED FORWARD INBOARD SEAT TRACK FOR GALLEY IAW MM 53.

Part: STRAP — CORRODED (BS 4992-6249)

CENTER FLOOR BUTT STRAP JUST AFT OF CABIN ENTRANCE AREA HAS AREAS OF CORROSION AND NEEDS TO BE REPLACED. REPLACED CENTER BUTT STRAP ON FLOORBEAM FROM FS 4992.0 TO FS 6249.2 IAW SRM 51-40-02.

Part: DOOR LATCH — INOPERATIVE (LT MLG)

LEFT MAIN LANDING GEAR WOULD NOT RETRACT. RETURNED TO FIELD REPLACED INBOARD GEAR DOOR LATCH ASSEMBLY ON LEFT MAIN GEAR. OPERATED GEAR DOORS SEVERAL TIMES, OPS CHECKS GOOD. SWUNG GEAR SEVERAL TIMES AND FOUND LANDING GEAR CONTROL BOX WOULD NOT LET GEAR RETRACT. REPLACED LANDING GEAR CONTROL AND SWUNG GEAR SEVERAL TIMES, OPS CHECKS GOOD.

Part: CONTROL CABLE — WORN (RUDDER CONTL)

RT RUDDER OUTBOARD AFT SECTION OF CABLE WORN. REPLACED RT RUDDER OUTBOARD AFT CABLE PER MM 27-00-01.

Part: CONTROL CABLE — WORN (LT AILERON)

LT AILERON CABLE OUTBOARD OF NACELLE IS WORN. REPLACED BOTH AILERON CABLES FOR LT AILERON.

Part: FUEL CONTROL — FAILED (LT ENGINE)

LT ENGINE FAILURE AT 2,500 FEET WITH CLIMB POWER. RETURNED TO LAX. TORQUE FLUXUATED 65 TO 84 THEN TO 101. REPLACED HMU FUEL CONTROL, IAW MM 73-21-00, OPS CKS GOOD, NO LEAKS NOTED.

Part: FUEL CONTROL — FAILED (RT ENGINE)

RT TORQUE UNCOMMANDED INCREASE AND DECREASE WITH LITTLE OR NO POWER LEVER INPUT. INSTALLED SERVICEABLE HMU AND T1.8 SENSOR.

Part: FUEL NOZZLE — FAILED (LT ENGINE)

LT ENGINE FAILURE AT ROTATION RETURNED FOR LANDING. FOUND O-RINGS FOR NR 10 FUEL NOZZLE SPLIT. INSTALLED NEW O-RINGS RAN ENGINE, FLAMED OUT, INSTALLED, SERVICED NR 10 NOZZLE AND NEW TUBE. RAN ENGINE AT 100 PECENT TORQUE FOR 5 MINUTES. OPS CKS GOOD, NO LEAKS FOUND.