N562SW

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,529 hrs · 47,746 cycles

FRONT SET OF EMERGENCY LIGHTS DO NOT ILLUMINATE. FLT 5659 RELAMPED.

Part: SCREW — LOOSE (EMERGENCY LIGHT) · airframe 33,188 hrs · 47,249 cycles

EMERGENCY LIGHT OVER SEAT 9BC INOPERATIVE. FLT#5331TIGHTENED GROUND TERMINAL SCREW BEHIND LIGHT ASSEMBLY.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 33,052 hrs · 47,064 cycles

SMOKE AURAL WARNING WITH NO OTHER ANNUNCIATORS OR INDICATION AT THE GATE WITH PACKS ON. FLT#6493 REPLACED AURAL WARNING UNIT. CARGO SMOKE/FIRE TEST NORMAL. PN 80-0557-11, SN ON 0206 & SN OFF UNK

Part: SKIN — DENTED (FUSELAGE) · airframe 32,455 hrs · 46,216 cycles

DENT IN SKIN ON RT UPPER SIDE OF NOSE JUST BELOW F/O'S WINDSCREEN. C-CHECK, INSTALLED DOUBLER AT RT UPPER FORWARD FUSELAGE SKIN JUST BELOW F/O'S WINDSCREEN IAW ETD AND SRM.

Part: FASTENER — LOOSE (FUSELAGE) · airframe 32,450 hrs · 46,209 cycles

PASSENGER ENTRY DOOR FWD ACTUATOR SUPPORT BRACKET HAS LOOSE FASTENERS AND IS CAUSING AN OIL CAN EFFECT ON FUSELAGE SKIN. (C-CHECK) REMOVED LOOSE HI-LOKS AT FWD PASSENGER DOOR ACTUATOR SUPPORT BRACKET AND INSTALLED NEXT AVAILABLE DIAMETER SIZE TO ELIMINATE ANY EXTRA FLEX IAW SRM.

Part: CLEAT — CRACKED (LT WING) · airframe 32,380 hrs · 46,110 cycles

LEFT WING NR 1 FUEL PANEL UPPER SKIN CLEATS CRACKED FWD OF PANEL. (C-CHECK) REPLACED LEFT WING NR 1 FUEL PANEL UPPER SKIN CLEATS IAW SRM.

Part: CLEAT — CRACKED (LT WING) · airframe 32,380 hrs · 46,110 cycles

LEFT WING NR 2 FUEL PANEL HAS A FWD UPPER SKIN CLEAT CRACKED. (C-CHECK) REPLACED LT WING NR 2 FUEL PANEL FWD UPPER SKIN CLEAT IAW SRM.

Part: SUPPORT — CRACKED (LT WING) · airframe 32,380 hrs · 46,110 cycles

LEFT WING NR 3 FUEL PANEL OTBD RIB AFT SKIN SUPPORT CRACKED. C-CHECK, REPLACED AFT RIB SUPPORT AT LT WING RIB 16 IAW SRM.

Part: CLEAT — CRACKED (LT WING) · airframe 32,380 hrs · 46,110 cycles

LEFT WING BETWEEN NR 1 AND NR 2 FUEL PANELS UPPER SKIN CLEAT CRACKED (SECOND FROM FORWARD SPAR). (C-CHECK) NEW SKIN CLEAT INSTALLED ON UPPER LT WING BETWEEN FUEL PANELS NR 1 AND NR 2 SECOND FROM SPAR IAW SRM.

Part: CLEAT — CRACKED (LT WING) · airframe 32,380 hrs · 46,110 cycles

LEFT WING BETWEEN NR 1 AND NR 2 FUEL UPPER SKIN CLEAT CRACKED. C-CHECK, NEW SKIN CLEAT INSTALLED ON LT WING BETWEEN NR 1 AND NR 2 FUEL PANELS UPPER FORWARD IAW SRM.

Part: CLEAT — CRACKED (LT WING) · airframe 32,380 hrs · 46,110 cycles

LT WING NR 5 FUEL PANEL UPPER INBD RIB, 2 SKIN CLEATS CRACKED. C-CHECK, 2 NEW SKIN CLEATS INSTALLED ON LT WING, NR 5 FUEL PANEL INBD UPPER RIB IAW SRM.

Part: COVER — BROKEN (CABIN) · airframe 32,327 hrs · 46,035 cycles

EMERGENCY GEAR DEPLOY COVER BROKEN. (SERVICE) REPLACED EMERGENCY GEAR DOOR COVER IAW SRM.

Part: WIRE — BROKEN (CABIN) · airframe 32,281 hrs · 45,983 cycles

FIRST ROW OF EMERGENCY TRACK FLOOR LIGHTING WILL NOT ILLUMINATE. (FLT 5529) REPAIRED BROKEN WIRE AT FORWARD CONNECTOR IAW AMM. OPS CHECK GOOD.

Part: PLUNGER — OUT OF ADJUST (RT MLG) · airframe 32,069 hrs · 45,691 cycles

SELECTED GEAR HANDLE UP OBSERVED RIGHT MAIN GEAR DISAGREEMENT LIGHT, BOTH A & B INDICATORS AND HEARD AIRFLOW SOUNDS SIGNALING NOSE GEAR DOORS WERE NOT FULLY CLOSED. AFTER 2 MINUTES RIGHT MAIN GEAR DISAGREEMENT LIGHT EXTINGUISHED. AIRCRAFT SOUNDED AND FLEW IN A MANNER INDICATING SUCCESSFUL GEAR RETRACTION. (FLT 5604) ADJUSTED RIGHT MLG UPLOCK HOOK LEVER PLUNGER. PERFORMED OPERATIONAL CHECK OF MLG EXTENSION AND RETRACTION SYSTEM, SEVERAL TIMES. OPS CHECK GOOD AT THIS TIME.

Part: FUSE — FAILED (EMERGENCY LIGHT) · airframe 31,698 hrs · 45,187 cycles

FIRST STRIP OF EMERGENCY FLOOR LIGHTING DOES NOT ILLUMINATE. (FLT 5440) REPLACED FUSE F0031.

Part: FUSE — BLOWN (CABIN) · airframe 31,652 hrs · 45,107 cycles

EMERGENCY LIGHTS OUT BY ROW 3A. (FLT 6489) REPLACED EMERGENCY LIGHT FUSE.

Part: UNKNOWN — SMOKE (LT ENGINE) · airframe 30,555 hrs · 43,613 cycles

SMOKE WAS COMING OUT OF INBOARD AFT VENT ON LEFT ENGINE COWLING. (FLT 6397) OPENED LEFT ENGINE AFT COWLING AND INSPECTED. FOUND NO SMOKE. CHECKS GOOD AT THIS TIME.

Part: WIRE — DAMAGED (CABIN) · airframe 29,947 hrs · 42,774 cycles

ONE FORWARD DOOR RED EMERGENCY FLOOR LIGHTING IS OUT. (FLT 6506) REPAIRED DAMAGED WIRING.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 29,652 hrs · 42,357 cycles

SMOKE IN REAR OF AIRCRAFT. RECEIVED A TRIPLE CHIME SMOKE ON MAP. (FLT 5621) REPLACED RIGHT ENGINE ASSEMBLY. PN: PW118B, SN OFF: AP0052.

Part: WIRE — BROKEN (CABIN) · airframe 28,609 hrs · 40,900 cycles

BOTH FORWARD RED FLOORING EMERGENCY LIGHTS ARE OUT. (SERVICE) REPAIRED WIRING FOR BOTH FORWARD CABIN RED FLOOR EMERGENCY LIGHTS.

Part: BOLT — OUT OF ADJUST (CABIN DOOR) · airframe 28,420 hrs · 40,631 cycles

MCD DIFFICULT TO OPEN. (FLT 5425) ADJUSTED MAIN CABIN DOOR ECCENTRIC BOLT AND BACKSTOPS.

Part: STRINGER — CRACKED (RT WING) · airframe 29,319 hrs · 41,872 cycles

RIGHT WING AT DEFUEL PANEL, STRINGER 10 CRACKED. (C-CHECK) INSTALLED STRINGER REPAIR REINFORCEMENT TO RIGHT WING STRINGER 10 AT DEFUEL PANEL PER SRM.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 28,187 hrs · 40,304 cycles

MAIN CABIN DOOR HARD TO OPEN. (FLT 6223) LUBED PAX DOOR ROLLERS ON DOOR FRAME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,420 hrs · 39,207 cycles

MCD OVERHEAD LIGHT IS OUT. (FLT 7038) RELAMPED OVERHEAD LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,063 hrs · 38,695 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 2 OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,903 hrs · 38,460 cycles

FLOOR EMERGENCY LIGHT BURNED OUT. (FLT 6411) RELAMPED EMERGENCY LIGHT.

Part: UNKNOWN — MALFUNCTIONED (BRAKE SYSTEM) · airframe 26,265 hrs · 37,535 cycles

AIRCRAFT HAS POOR BRAKING, AIRCRAFT BRAKES MAKE A GRINDING NOISE AND SHIMMY. (FLT 6247) PERFORMED TAXI CHECK, BRAKE PRESS CHECK, AND INSPECTED WHEEL SPEED TRANSDUCERS, NO FAULTS FOUND. OPERATIONAL CHECKS NORMAL.

Part: SCREW — DISTORTED (CABIN DOOR) · airframe 26,097 hrs · 37,307 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6066) REPLACED SCREWS FOR UPPER AFT BACK STOP SHIMS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,275 hrs · 36,117 cycles

NR 1 CEILING EMERGENCY LIGHT INOP. (FLT 6196) RELAMPED EMERGENCY LIGHT.

Part: FRAME — CRACKED (RT NACELLE) · airframe 25,190 hrs · 35,989 cycles

RIGHT ENGINE FRAME 1 CRACKED. (C CHECK) REPLACED FRAME PER SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,190 hrs · 35,989 cycles

RIGHT SIDE FORWARD FLOOR SEAT TRACK CORRODED. (C CHECK) REPLACED TRACK PER AMM.

Part: FRAME — CRACKED (LT NACELLE) · airframe 25,201 hrs · 36,008 cycles

LEFT ENGINE FRAME 1 CRACKED AT INBOARD CORNER. (C CHECK) REPLACED FRAME PER SB120-54-0036.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 25,190 hrs · 35,989 cycles

FLOORBEAM BUTTSTRAP ON LEFT SIDE CORRODED. (C CHECK) REPLACED BUTTSTRAP PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 25,201 hrs · 36,008 cycles

PASSENGER ENTRANCE LOWER THRESHOLD ANGLE CORRODED. (C CHECK) REPLACED ANGLE PER SRM.

Part: SUPPORT — CRACKED (FLAP) · airframe 25,190 hrs · 35,989 cycles

LEFT ENGINE NACELLE FLAP OUTBOARD SUPPORT CRACKED. (C CHECK) REPLACED PER SRM.

Part: HINGE — OUT OF ADJUST (MAIN DOOR) · airframe 25,158 hrs · 35,941 cycles

MAIN DOOR VERY HARD TO OPEN FROM OUTSIDE. (FLT 5763) ADJUSTED LOWER DOOR HINGE CONCENTRIC.

Part: CAM — LACK OF LUBE (CABIN DOOR) · airframe 25,158 hrs · 35,941 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6818) LUBED FORWARD OVER CENTERING CAM AND CHECKED DOOR TENSION.

Part: SERVO — FAULTY (AUTOPILOT SYS) · airframe 24,695 hrs · 35,295 cycles

AFTER T/O, TURNING AC TO THE LEFT WAS EXTREMELY DIFFICULT. AC TURNS TO THE RIGHT FINE. (FLT 6379) REPLACED ROLL SERVO IAW EMB 120 MM 22-10-05.

Part: SERVO — FAULTY (AILERON) · airframe 24,228 hrs · 34,638 cycles

AILERONS BINDING. (FLT 5766) REPLACED AILERON SERVO.

Part: WINDOW — LACK OF LUBE (COCKPIT) · airframe 24,061 hrs · 34,400 cycles

CAPTAINS SIDE DV WINDOW DIFFICULT TO OPEN. (FLT 6311) LUBED CAPTAINS DV WINDOW.

Part: LAMP — LOOSE (EMERGENCY LIGHT) · airframe 23,374 hrs · 33,517 cycles

FLT 5571 - 3RD AFT (FLOOR LEVEL) EMERGENCY LIGHT INOP. RELAMPED.

Part: LIGHT — BROKEN (CABIN) · airframe 23,056 hrs · 33,096 cycles

EMERGENCY EXIT SIGN AND LIGHT BROKEN AT ROW 6BC. REPLACED SIGN.

Part: DOOR — BINDING (MAIN PAX) · airframe 22,172 hrs · 31,936 cycles

CABIN DOOR IS OCCASIONALLY DIFFICULT TO OPEN. (FLT 5441) INSPECTED, CLEANED AND PERFORMED OPS CHECK ON MAIN CABIN DOOR SEVERAL TIMES. NO DISCREPANCIES NOTED.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 22,696 hrs · 32,635 cycles

PILOT'S SIDE AFT OF DV WINDOW AREA FRAME 12 EAR SUPPORT CLIP, AFT, IS CRACKED. INSTALLED DOUBLER IN PLACE WITH RIVETS PER SRM 51-30-01 AND 51-40-02.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,856 hrs · 31,490 cycles

FLT 5477 - FLOOR LEVEL EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED MIDDLE ELBP IAW AMM 33-59-02. OPS CHECK GOOD, PN D366-04-001, SN OFF 975/05-91.

Part: SENSOR — FAULTY · airframe 20,548 hrs · 29,727 cycles

FLT 5768 - AFTER ROTATION RIGHT NP FLUCTUATED ON BOTH ANALOG AND DIGITAL INDICATIONS. REPLACED NP SENSOR IAW MM 27-12-00. OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 19,637 hrs · 28,565 cycles

AUTOPILOT PITCHES AIRCRAFT UP AND DOWN. REPLACED NR 1 AUTOPILOT COMPUTER IAW MM 22-00-00, P/N - 622-8315-102 S/N OFF - 1303.

Part: COMPUTER — MALFUNCTIONED (AUTO PILOT SYS) · airframe 19,619 hrs · 28,539 cycles

WITH AUTOPILOT ENGAGED, AIRCRAFT PITCHED NOSE UP THEN NOSE DOWN. REPLACED NR 2 AUTOPILOT COMPUTER.

Part: CAP — LOOSE (LT ENGINE) · airframe 18,424 hrs · 26,817 cycles

CLIMBING OUT OF DEN STARTED LOSING OIL PRESSURE ON LEFT ENGINE AND RECEIVED OIL PRESSURE WARNINGS. IMMEDIATELY SHUT DOWN NR 1 ENGINE AND RETURNED TO FIELD. SERVICED ENGINE WITH OIL TO PROPER LIMITS AND REINSTALLED OIL CAP PROPERLY.

Part: FRAME — CORRODED (PAX DOOR) · airframe 18,344 hrs · 26,726 cycles

PAX DOOR BOTTOM END STEP FRAME CORRODED, DISCOVERED DURING C-CHECK INSPECTION. NEW FRAME INSTALLED IAW SRM 120 51-10-02 PG 3 SEC 3A AND RII CARD 52-800-1000.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 18,344 hrs · 26,726 cycles

CRACK ON PAX DOOR FORWARD CENTER FRAME, DISCOVERED DURING C-CHECK INSPECTION. REPLACED PAX DOOR FORWARD CENTER FRAME SECURED IAW EMB 120 SRM 51-40-02, PN OFF: 120-21058-003.

Part: RAIL — CORRODED (PAX DOOR) · airframe 18,344 hrs · 26,726 cycles

PAX DOOR FORWARD STEP RAIL CORRODED, DISCOVERED DURING C-CHECK INSPECTION. NEW FORWARD STEP RAIL INSTALLED IAW SRM 120 51-10-02 PG 3 SEC 3A AND IAW RII CARD 52-800-1000.

Part: FRAME — CRACKED (PAX DOOR) · airframe 18,344 hrs · 26,726 cycles

PAX DOOR BOTTOM STEP FORWARD SIDE FRAME CRACKED, DISCOVERED DURING C-CHECK INSPECTION. NEW FRAME INSTALLED IAW SRM 120 51-10-02 PG 3 SEC 3A AND RII CARD 52-800-1000.

Part: BELLCRANK — CORRODED (PAX DOOR) · airframe 18,344 hrs · 26,726 cycles

PAX DOOR 3RD STEP AFT BELLCRANK CORRODED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED PAX DOOR 3RD STEP AFT BELLCRANK, PN OFF: 120-20935-001.

Part: RIB — CRACKED (RT WING) · airframe 18,344 hrs · 26,726 cycles

RIGHT INBOARD LEADING EDGE RIB IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT INBOARD LEADING EDGE RIB IAW EMB 120 SRM 51-40-02.

Part: RAIL — CORRODED (PAX DOOR) · airframe 18,344 hrs · 26,726 cycles

PAX DOOR AFT STEP RAIL CORRODED, DISCOVERED DURING C-CHECK INSPECTION. NEW FWD STEP RAIL INSTALLED IAW SRM 120 51-10-02 PG 3 SEC 3A AND IAW RII CARD 52-800-1000.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 18,344 hrs · 26,726 cycles

CRACK ON PAX DOOR AFT CENTER FRAME. NEW FRAME INSTALLED IAW SRM 120 51-10-02 PG 3 SEC 3A AND IAW RII CARD 52-800-1000, PN OFF: 120-21059-001.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 18,254 hrs · 26,606 cycles

BACK HALF OF EMERGENCY LIGHTS TURN OFF AFTER 2 SECONDS OF PERFORMING TEST. REPLACED MIDDLE AND AFT ELBP'S. OPERATIONAL CHECKS GOOD. NR 2 SN OFF 1336.

Part: A/C PACK — LEAKING (RIGHT) · airframe 18,203 hrs · 26,533 cycles

RT PACK FAIL AND ASSOCIATED DUCT LEAK CAUSED SMOKE IN CABIN AND COCKPIT. OPERATED PACKS FROM ENGINE BLEED WITH NO SMOKE OR OTHER DEFECTS. OPERATIONAL CHECKS GOOD.

Part: BRAKE — CONTAMINATED (LT MLG) · airframe 18,104 hrs · 26,413 cycles

SMOKE FROM LEFT MAIN TIRE/BRAKE ASSEMBLY AFTER PARKING. CLEANED RESIDUAL OIL OFF OF GEAR ASSEMBLY. OPERATIONAL CHECKS GOOD.

Part: RELAY — MALFUNCTIONED (COCKPIT) · airframe 17,962 hrs · 26,200 cycles

CHEMICAL ODOR IN THE FLIGHT DECK MOSTLY FROM RIGHT SIDE. REPLACED OVERHEATED APU FEEDER PROTECTION RELAY IAW MM 24-37-00. OPERATIONAL CHECKS GOOD, P/N - 44B258051-002.

Part: CONTROL UNIT — MALFUNCTIONED (HYDRAULIC SYS) · airframe 17,506 hrs · 25,592 cycles

RUDDER FEELS STIFF. REPLACED RUDDER PCU. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (RUDDER) · airframe 17,198 hrs · 25,182 cycles

RUDDER IS EXTREMELY STIFF AND DIFFICULT TO MOVE, BOTH INFLIGHT AND ON THE GROUND. REPLACED THE BLUE HYD RUDDER PCU ACTUATOR IAW MM 27-22-02.

Part: WIRE — LOOSE (TERMINAL BLOCK) · airframe 16,124 hrs · 23,741 cycles

TURNED ON WINDSHIELD CLIMBING THROUGH FL180. BEGAN TO SMELL ELECTRICAL BURNING. SHORTLY THEREAFTER, SAW SMOKE COMING FROM UNDER FORWARD GLARESHIELD. TIGHTENED LOOSE GROUND WIRE ON TERMINAL BLOCK. OPERATIONAL CHECK GOOD.

Part: SERVO — MALFUNCTIONED (RUDDER) · airframe 15,362 hrs · 22,788 cycles

RUDDER PEDALS BINDING ON FIRST FLIGHT TEST. REPLACED RUDDER SERVO IAW EMB MM 22-10-05. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,061 hrs · 22,399 cycles

EMERGENCY LIGHTS WILL NOT ILLUMINATE. CHANGED EMERGENCY LIGHTS, OPERATIONAL CHECK OK.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 14,749 hrs · 22,031 cycles

FLOOR EMERGENCY LIGHTING INOPERATIVE AT GALLEY. REPAIRED WIRES AS REQUIRED.

Part: BUSHING — SEIZED (CARGO DOOR) · airframe 14,701 hrs · 21,976 cycles

MCD IS VERY HARD TO OPEN/CLOSE. REMOVED AND REPLACED FORWARD INTERMEDIATE TORQUE TUBE BUSHING PER EMB 120 MM 52-11-00. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 14,564 hrs · 21,814 cycles

THE FIRST EMERGENCY EXIT LIGHT ABOVE CENTER AISLE IN PASSENGER CABIN WILL NOT ILLUMINATE. REPLACED EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 14,980 hrs · 22,304 cycles

CRACKED SUPPORT ANGLE, FORWARD OF PAX DOOR AFT HINGE ARM, UNDER FLOOR (MARKED). ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW SUPPORT ANGLE ON FORWARD OF PAX DOOR AFT HINGE ARM UNDER FLOOR.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 13,978 hrs · 21,121 cycles

FO'S AUTOPILOT KICKED OFF AT LEVEL OFF , 25,000 FT. REMOVED AND REPLACED AUTOPILOT COMPUTER IAW MM 22-10-02, OPERATIONAL CHECKED GOOD.

Part: SIGN — BROKEN (CABIN) · airframe 13,166 hrs · 19,931 cycles

FORWARD BULKHEAD EXIT SIGN IS BROKEN. REMOVED AND REPLACED BROKEN EXIT SIGN, OPS CHECK OK. P/N: 10-1301-15.

Part: RELAY — OVERHEATED (ELECTRICAL SYS) · airframe 12,042 hrs · 18,210 cycles

JUST PRIOR TO ENGINE START, FLIGHT DECK BEGAN TO SMELL OF SOMETHING ELECTRICAL OVERHEATING. ISOLATED TO APU PANEL RT SIDE CONSOLE. FOUND APU FEEDER PROTECTION RELAY SHOWING SIGNS OF EXCESSIVE HEAT. REMOVED AND REPLACED FEEDER PROTECTION RELAY IAW W/M 20-10-00. OPS CHECK OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,443 hrs · 17,207 cycles

SECOND FROM FRONT RED EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED RED EMERGENCY EXIT LIGHT. OPS CHECK GOOD.

Part: INDICATOR — MALFUNCTIONED (AIR SPEED) · airframe 10,825 hrs · 16,244 cycles

ABORTED TAKEOFF AT 50-60 KNOTS DUE TO TRIPLE CHIME, RED MASTER WARNING LIGHT AND HIGH SPEED AURAL ANNUNCIATION. REPLACED BOTH LT AND RT AIRSPEED INDICATORS. GROUND TESTED OPS CHECK GOOD. LEFT S/N OFF AJ102.

Part: WIRE — BURNED (WINDSHIELD HEAT) · airframe 10,853 hrs · 16,286 cycles

FOUND BURNED WIRE IN LEFT RELAY BOX ON CAPTAIN'S SIDE. WIRE IS FOR LEFT WINDSHIELD HEAT. FOUND DURING C-CHECK INSPECTION. REMOVED AND REPLACED WIRE AS NEEDED PE-88022-116.

Part: FRAME — CRACKED (FUSELAGE) · airframe 10,853 hrs · 16,286 cycles

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

Part: ACM — MALFUNCTIONED (A/C BAY) · airframe 10,282 hrs · 15,363 cycles

VENTILATION SYSTEM BLOWING SMOKE INTO CABIN. REMOVED & REPLACED LEFT AND RIGHT ACM, OPS CHECK GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 9,584 hrs · 14,262 cycles

ABORTED TAKEOFF IN SFO DUE TO RED FLASHING WARNING LIGHT AND TRIM FAIL ON MAP. RETURNED TO GATE. INSPECTED AND TESTED ELECTRIC TRIM SYSTEM. OPS CHECK GOOD.

Part: DOOR SEAL — LOOSE (CARGO DOOR) · airframe 9,393 hrs · 13,950 cycles

ON CLIMBOUT LOST CABIN PRESSURIZATION FOR ABOUT 1 MINUTE, THEN THE SYSTEM BEGAN WORKING NORMALLY AGAIN IN MANUAL AND AUTO MODE. RETURNED TO LAX. SECURED CARGO DOOR SEAL. PRESSURIZED AIRCRAFT TO 7 PSID. OPS CHECK GOOD. NO DISCREPANCIES NOTED.

Part: INDICATOR — DEFECTIVE (COCKPIT) · airframe 8,955 hrs · 13,250 cycles

HIGH SPEED VOICE WARNING DURING TAKEOFF ROLL. ABORTED TAKEOFF. REPLACED NR 2 AIRSPEED INDICATOR. PERFORMED OPS CHECK. OPS CHECK GOOD.

Part: PROXIMITY SWITCH — FAULTY (ELEVATOR) · airframe 3,957 hrs · 5,641 cycles

UPON APPLICATION OF TAKEOFF POWER RECEIVED TRIM AURAL WARNING. REPLACED ELEVATOR RIGHT TRIM PROXIMITY SENSOR WITH SERVICEABLE UNIT IAW MM 27-32-05. ADJUSTED PROXIMITY SWITCH IAW MM 27-32-00. OPS CHECK GOOD AT THIS TIME.

Part: FLUX DETECTOR — MALFUNCTIONED (WING) · airframe 7,582 hrs · 11,208 cycles

YELLOW HEADING FLAG BOTH SIDES, RED HEADING FLAG FIRST OFFICER''S SIDE. BOTH DG''S OFF OF MAG COMPASS 35 DEGREES. RED FLAGS BOTH RMIS. GYRO SLAVING ON CAPTAINS SIDE PEGGED NEG (-), GYRO SLAVING ON F/O SIDE PEGGED POS (+). DIVERTED TO FAT. FOUND AIRCRAFT HAD NUMEROUS LIGHTNING STRIKES. COMPLIED WITH LIGHTNING STRIKE INSPECTION. REPLACED NR 2 FLUX DETECTOR, P/N 622-5812-004, S/N ON 25412, OFF 20021. REPLACED NR 1 AHRS P/N 622-6190-204, S/N ON 2926, OFF 1894. PERFORMED COMPASS SWING. BOTH AHRS SYSTEMS OP CHECKED GOOD IAW AMM 34-21-00 PG 501.

Part: FLUX DETECTOR — DEFECTIVE (RT WING) · airframe 7,568 hrs · 11,185 cycles

UPON TAKEOFF OUT OF IYK, GOT THE HDG FLAG. SHORTLY THEREAFTER, GOT THE PIT AND ROL FLAGS. ATTEMPTED QRH RESET, NO RESULTS. THE FIRST OFFICERS ATTITUDE INDICATOR SHOWED PITCH DOWN 10 PERCENT THE WHOLE FLIGHT. THE CAPTAINS ADI AND HEADING INDICATOR SHOWED FLAGS, BUT SEEMED TO OPERATE FINE. DIVERTED DUE TO WEATHER. REPLACED FDU-70 FLUX DETECTOR ON RIGHT WING TIP FIRST OFFICERS SIDE IAW MM 34-21-03. OPS CHECK GOOD. P/N ON 622-5812-004, S/N ON 20021, S/N OFF 16722.

Part: GENERATOR — VIBRATION (LT ENGINE) · airframe 7,465 hrs · 11,025 cycles

VIBRATION FELT FROM LEFT ENGINE DURING OPERATION. REMOVED AND REPLACED LEFT ENGINE HYD PUMP. (NO FIX). PUMP OPS CHECKS GOOD IAW 29-13-00. REMOVED AND REPLACED LEFT AUX GEN. VIBRATION FIXED, NO DEFECTS. OPS CHECKS GOOD. PUMP - P/N ON PV3-022-2A, S/N ON MX503650, OFF MX375399. AUX GEN P/N ON 30091-010, S/N ON 90007, OFF 677.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 7,414 hrs · 10,957 cycles

DURING FLIGHT, LOSS OF FLUID QUANTITY WAS NOTED ON GREEN HYDRAULIC SYSTEM. ON DEPARTURE, QUANTITY WAS APPROXIMATELY 7/8 ON GAUGE. APPROX 30-35 MINUTES INTO FLIGHT, RESERVOIR LOW LEVEL LIGHT ILLUMINATED; QTY WAS IN YELLOW ARC. CONSTANT DECREASE IN QUANTITY WAS NOTED FOR THE DURATION OF THE FLIGHT. UPON LANDING, FLUID QUANTITY WAS IN YELLOW ARC; FLUID PRESSURE REMAINED IN GREEN ARC DURING ALL PHASED/NO CAUTION SIGNS OBSERVED. MANUAL GEAR EXTENSION PERFORMED OUT OF CONCERN FOR PARTIAL GEAR EXTENSION (FREE FALL). AN EMERGENCY WAS DECLARED AS A PRECAUTION. INSTALLED NEW LEFT ENGINE DRIVEN PUMP MAIN PRESSURE LINE (120-35694-025) PER EMB 120 MM 20-10-04. REPLENISHED RESERVOIR, LEAK CHECK GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (TRIM SYSTEM) · airframe 6,752 hrs · 10,024 cycles

TAKEOFF TRIM AURAL WARNING ON TAKEOFF. ABORTED TAKEOFF. TRIM IN GREEN BAND. POWERED DOWN AIRCRAFT. POWERED UP AIRCRAFT. PERFORMED OPERATIONAL CHECK OF AURAL TRIM WARNING SEVERAL TIMES. TRIM AURAL WARNING OPERATES NORMAL. OPS CHECKS GOOD. COULD NOT DUPLICATE DISCREPANCY.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 6,666 hrs · 9,890 cycles

AURAL WARNING TRIM ALERTER WENT OFF ON TAKE OFF, TRIM SET AT 27. ABORTED TAKEOFF. POWERED DOWN AIRCRAFT THEN BACK UP, ALL CHECKS GOOD AT THIS TIME.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 5,982 hrs · 8,917 cycles

ANTI-SKID OUTBOARD INOP LIGHT ILLUMINATED DURING APPROACH, LIGHT EXTINGUISHED DURING GO-AROUND. RETURNED TO LAX. CHECKED OUTBOARD WHEEL SPEED TRANSDUCER FOR SECURITY. JACKED AIRCRAFT AND CYCLED GEAR 10 TIMES. UNABLE TO DUPLICATE PROBLEM. OPS CHECK GOOD.

Part: FUEL DOOR — OPEN (EXTERIOR) · airframe 5,732 hrs · 8,552 cycles

SERVICE DOOR WARNING LIGHT CAME ON EARLY IN TAKEOFF ROLL. ABORTED TAKEOFF. FOUND CAMLOCK ON OUTBOARD FUEL DOOR CAME LOOSE. RESECURED DOOR CLOSED. OPS CHECKS GOOD.

Part: SWITCH — FAILED (LT ENGINE)

LEFT ENGINE INLET DEICING BOOT FAILED IN FLIGHT. NUMEROUS ATTEMPTS TO RESET ALSO FAILED. DIVERTED TO SBA. REPLACED LEFT INLET PRESSURE SWITCH WITH SERVICEABLE UNIT, OPS CHECK GOOD. (S/N 2230) ON, (S/N 0141) OFF.

Part: EJECTOR VALVE — FAILED (RT ENGINE)

RIGHT ENGINE AIR INLET DE-ICE FAILED. RETURNED TO THE FIELD. REPLACED RIGHT ENGINE INLET EJECTOR VALVE IAW 300000. OPS CHECKS GOOD ON GROUND. PN ON 3D237606, SN: N677SN OFF: N3479.

Part: BOOT — FAILED (HORIZ STAB)

RIGHT INBOARD STAB BOOT FAILED ABOVE 10,000, RESET ON DESCENT BELOW 10,000. RETURNED TO SEA. PERFORMED FUNCTIONAL TEST OF EMPENNAGE LEADING EDGE DE-ICERS USING ENGINE PNEUMATIC POWER PER MM 301000. SYSTEM OPERATED PER FUNCTIONAL TEST REQUIREMENTS, UNABLE TO DUPLICATE DISCREPANCY.

Part: WIRE — BROKEN (LT PACK DUCT)

LEFT DUCT LEAK LIGHT ILLUMINATED AFTER TAKEOFF. APU BLEED ON, ENGINE BLEEDS OFF. STARTED QUICK REFERENCE HANDBOOK PROCEDURE, LIGHT WENT OUT. RETURNED TO AIRPORT. FOUND BROKEN SOLDER JOINT ON LEFT PACK DUCT LEAK SENSOR NEAR BLEED AIR CONTROL VALVE. RESOLDERED WIRE. LEFT PACK OPS CHECKED GOOD.

Part: BOOT — DAMAGED (RT ENGINE DEICE)

RIGHT ENGINE INLET DEICE FAILED AGAIN IN FLIGHT. COULD NOT ESCAPE ICING CONDITIONS ALONG ROUTE AND DIVERTED BACK TO SFO. INSTALLED SERVICEABLE EJECTOR VALVE AND INSTALLED SERVICEABLE PRESSURE SWITCH AND PATCHED SMALL HOLE IN THROAT BOOT SYSTEM. OPS CHECKS GOOD.

Part: SOLENOID VALVE — FAILED (LANDING GEAR)

LANDING GEAR CYCLED UP AND DOWN UPON EXTENSION, GEAR LIGHTS ON PANEL. REMOVED AND REPLACED LANDING GEAR SOLENOID VALVE. CYCLED LANDING GEAR NUMEROUS TIMES, OPS CHECKS GOOD.

Part: PROX SENSOR — MALFUNCTIONED (NLG)

AFTER TAKEOFF, UPON GEAR RETRACTION, NOSE GEAR INDICATED 1 GREEN LIGHT B AND ONE RED LIGHT A. RETURNED TO PSP. REPLACED NOSE B GEAR DOWN LOWER PROXIMITY SENSOR AND HARNESS. SET GAP, SAFTIED AND PERFORMED NUMEROUS GEAR SWINGS. OPS CHECKS GOOD.