N568SW
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Tatonduk Outfitters, Ltd. (FXGA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
99 reports on file, 1998-09-09 – 2023-03-23.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 35,601 hrs · 49,117 cycles
PILOT REPORTED AFTER TAKEOFF FROM KPHX THE LT FIRE DETECTION LIGHT ILLUMINATED. PERFORMED AIR RETURN AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED FIRE LOOP AND FOUND NO DEFECTS. MAINTENANCE DISCONNECTED THE ELECTRICAL CONNECTOR FROM DETECTOR AND DISCOVERED DEBRIS WITHIN THE CONNECTOR AND WERE ABLE TO CLEAN IT THOROUGHLY. MAINTENANCE REINSTALLED CONNECTOR AND PERFORMED OPS CHECK. OPERATIONAL CHECKS WERE GOOD, AND AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED FOR THIS DISCREPANCY.
Earlier reports · 1998–2020 · 98 reports
2020
Part: CABIN PRESSURE — ERRATIC (ZONE 100) · airframe 34,714 hrs · 48,323 cycles
CABIN ALTITUDE WARNING CAME ON DURING DEPARTURE OUT OF KOGD TO KLRP. RETURNED TO DEPARTURE AIRPORT (KOGD). PERFORMED PRESSURIZATION SYSTEM OPERATIONS CHECK NORMAL, REFERENCE EMB 120 MM CH 21-30-01.
2014
Part: UNKNOWN — SMOKE (CABIN) · airframe 33,994 hrs · 47,437 cycles
SMOKE IN CABIN DURING FLIGHT. OPERATED BOTH PACKS FROM APU AND ENGINE BLEEDS FOR EXTENDED PERIOD AT VARIOUS POWER SETTINGS AND SWITCH POSITIONS. COULD NOT DUPLICATE ANY SMOKE OR ODOR FROM EITHER SYSTEM. OPS CHECKED GOOD.
Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,740 hrs · 47,108 cycles
LT AND RT EMERGENCY LIGHTS INOPERATIVE ON AFT FUSELAGE ABOVE WINGS. R & R AFT FUSE . OPS CHECKED GOOD.
Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 33,027 hrs · 46,096 cycles
WHITE FLOOR EMERGENCY LIGHT NEAR SEAT 5A WILL NOT ILLUMINATE. REPLACED LAMP.
Part: LEAD — LOOSE (WINDOW HEAT) · airframe 32,482 hrs · 45,352 cycles
DURING WINDOW HEAT OPERATION THERE IS AN ELECTRICAL BURNING SMELL. FLT 5379 FOUND POSITIVE TERMINAL LEAD ON FIRST OFFICER`S WINDSHIELD LOOSE. REMOVED, CLEANED & REINSTALLED POSITIVE LEAD ON FIRST OFFICER`S WINDSHIELD. OPERATED WINDSHIELD HEAT WITH NO DEFECTS NOTED, OPERATIONS CHECKED GOOD IAW AMM.
Part: TERMINAL — DAMAGED (ELECTRICAL SYS) · airframe 32,357 hrs · 45,173 cycles
MILD TO STRONG SMELL OF BURNT ELECTRICAL. FLT 5313 FOUND HEAT DAMAGED TERMINALS AT BOTH ENDS OF W240-0001-0 IN THE RT DC RELAY BOX. REPLACED BOTH HEAT DAMAGED TERMINALS OF W240-0001-0 IN THE RT DC RELAY BOX IAW WDM.
2013
Part: WIRE — UNSECURE (NR 2 BUSS) · airframe 32,344 hrs · 45,155 cycles
STRONG ELECTRICAL SMOKE SMELL THAT GOT PROGRESSIVELY WORSE. FLT 5459 RESECURED RT SIDE NR 2 BUS TIE CONTACTOR WIRE LOOP AT ATTACHING STUDS. RESECURED BOTH ENDS RAN ENGINES & FOUND NO HEAT IN THE WIRE, OPERATIONS CHECKED GOOD.
Part: FITTING — CRACKED (LT WING) · airframe 32,070 hrs · 44,758 cycles
LT INBD WING CORNER CLIP CRACKED AT RIB NR 5 & STRINGER NR 10. C-CHECK REPLACED LT INBD WING CORNER CLIP AT RIB NR 5 & STRINGER NR 10 IAW SRM.
Part: FITTING — CRACKED (LT WING) · airframe 32,070 hrs · 44,758 cycles
LT INBD WING LOWER SKIN CLIP AT RIB NR 8 CRACKED. C-CHECK REPLACED LT INBD WING LOWER SKIN CLIP AT RIB NR 8 IAW SRM.
Part: FITTING — CRACKED (LT WING) · airframe 32,070 hrs · 44,758 cycles
LT OTBD WING UPPER SKIN CLIP CRACKED AT RIB NR 19. C-CHECK REPLACED LT UPPER WING SKIN AFT MOST SKIN SUPPORT CLIP ON RIB 19 IAW SRM.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 32,070 hrs · 44,758 cycles
FLOOR PROP AT FRAME 13 CAPTAINS SIDE CRACKED. C-CHECK CUT OUT DAMAGED SECTION, INSTALLED A NEW SECTION WITH INTERNAL DOUBLER IN COCKPIT LT FLOOR PROP AT FRAME 13 IAW ETD.
Part: FITTING — CRACKED (LT WING) · airframe 32,070 hrs · 44,758 cycles
LT OTBD WING LOWER SKIN CLIP AT RIB NR 16 CRACKED. C-CHECK R & R LOWER SKIN CLIP ON LT OTBD LOWER WING AT RIB 1.
Part: FRAME — CRACKED (LT NACELLE) · airframe 32,070 hrs · 44,758 cycles
LT NACELLE FRAME NR 1 CRACKED AT TORSION MOUNTS. C-CHECK REPLACED LT NACELLE FRAME NR 1 IAW SB.
Part: SUPPORT BRACKET — CRACKED (CABIN DOOR) · airframe 32,070 hrs · 44,758 cycles
MAIN CABIN DOOR 3RD STEP FROM BOTTOM FWD STEP POST IS CRACKED. C-CHECK REMOVED SUPPORT BRACKET PROFILE & INSTALLED SERVICEABLE IAW SRM.
Part: FRAME — CRACKED (RT NACELLE) · airframe 32,070 hrs · 44,758 cycles
RT NACELLE FRAME NR 1 CRACKED AT TORSION MOUNTS. C-CHECK REPLACED RT NACELLE FRAME NR 1 IAW SB.
Part: OIL COOLER — CRACKED (LT ENGINE) · airframe 32,070 hrs · 44,758 cycles
LT ENGINE OIL COOLER AIR OUTLET CRACKED ON INBD SIDE. C-CHECK PERFORMED REPAIR TO LT ENGINE OIL COOLER OUTLET INBD SKIN IAW ETD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,034 hrs · 44,706 cycles
EMERGENCY EXIT LIGHT AT ROW 6A IS BURNED OUT. FLT#6232 RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,757 hrs · 44,318 cycles
WHITE FLOOR EMERGENCY LIGHT 11A BURNED OUT. SERVICE RELAMPED.
Part: WIRE — DAMAGED (CABIN) · airframe 31,757 hrs · 44,318 cycles
RED FLOOR EMERGENCY LIGHT NEAR SEAT 2A IS BURNED OUT. FLT#5625 SPLICED WIRES IAW SPM 20-00-00.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,657 hrs · 44,189 cycles
FLOOR LEVEL EMERGENCY LIGHT BY SEAT 9A IS BURNED OUT. FLT#5360 RELAMPED.
Part: COVER — LOOSE (CABIN) · airframe 31,617 hrs · 44,142 cycles
EMERGENCY LIGHTING FLOOR COVER IS LOOSE. FLT#6307 RESECURED EMERGENCY LIGHT COVER.
Part: WIRE — LOOSE (CABIN) · airframe 30,762 hrs · 42,902 cycles
FORWARD FLOOR EMERGENCY LIGHT LOOSE WIRES NEAR CABIN DOOR. (FLT 1358) REPLACED THE FORWARD EMERGENCY FLOOR LIGHT.
Part: WIRE — DISCONNECTED (CABIN) · airframe 30,724 hrs · 42,845 cycles
1 RED PASSENGER DOOR EMERGENCY FLOOR LIGHT DOES NOT ILLUMINATE. (SERVICE) RE-SECURED POWER WIRE TO ONE RED FORWARD EMERGENCY FLOOR LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,724 hrs · 42,845 cycles
EMERGENCY LIGHT ADJACENT SEAT 6C BURNED OUT. (FLT 5466) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,569 hrs · 42,641 cycles
FORWARD FLOOR RED EMERGENCY LIGHT DOES NOT ILLUMINATE. (FLT 5428) RELAMPED EMERGENCY LIGHT.
Part: SEQUENCE VALVE — FAILED (RT MLG) · airframe 30,436 hrs · 42,461 cycles
WHEN RETRACTING LANDING GEAR ON DEPARTURE, RIGHT MAIN LANDING GEAR WOULD NOT RETRACT. (FLT 5474) REPLACED RIGHT OUTBOARD MLG SEQUENCING VALVE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,426 hrs · 42,445 cycles
FORWARD FLOOR STRIP EMERGENCY RED LIGHT AT MAIN CABIN DOOR DOES NOT ILLUMINATE. (SERVICE) REPLACED FORWARD INTERIOR RED EMERGENCY FLOOR LIGHT ASSEMBLY.
2012
Part: LENS — MISSING (CABIN) · airframe 30,393 hrs · 42,393 cycles
FORWARD CABIN RED ESCAPE PATH LIGHT DOES NOT ILLUMINATE MISSING RED LENS. (FLT 6506) REPLACED THE MISSING RED EMERGENCY TRACK LIGHT LENS AND TRACK COVER.
Part: WIRE — CUT (CABIN) · airframe 30,393 hrs · 42,393 cycles
NO RED EMERGENCY LIGHTS ON GROUND TRACK NEXT TO MAIN CABIN DOOR AND CUT WIRES. (FLT 6506) REPLACED EMERGENCY LIGHT ON FLOOR BY MAIN CABIN DOOR.
Part: LIGHT — INOPERATIVE (CSABIN) · airframe 30,345 hrs · 42,319 cycles
ONE RED FORWARD FLOOR LIGHT INOPERATIVE. (FLT 5473) REPLACED RED FLOOR EMERGENCY LIGHT AT FORWARD END NEAR MAIN CABIN DOOR.
Part: ACTUATOR — FAILED (RT MLG) · airframe 30,330 hrs · 42,297 cycles
RIGHT MAIN LANDING GEAR WOULD NOT RETRACT, RED AND GREEN LANDING GEAR INDICATING LIGHTS CONTINUOUSLY ILLUMINATED, ACCOMPANIED BY LOUD GRINDING NOISE. (FLT 6293) REPLACED RIGHT MLG ACTUATING CYLINDER IAW AMM. PN: 19595-000-07 SN ON: B130 SN OFF: B132.
Part: WARNING SYSTEM — FALSE INDICATION (COCKPIT) · airframe 30,263 hrs · 42,214 cycles
ON DEPARTURE AFTER GEAR RETRACTION THE RIGHT MAIN GEAR INDICATED STILL EXTENDED. RECYCLED THE GEAR HANDLE DOWN AND UP, RECEIVED RED "A & B" LIGHTS AND TWO GREEN "A & B" LIGHTS. AFTER 5 MINUTES ALL LIGHTS EXTINGUISHED AND ALL INDICATIONS SHOWED THE GEAR WAS UP AND LOCKED. (FLT 5308) INSPECTED RIGHT MAIN LANDING GEAR CARRIED OUT APPROXIMATELY 20 GEAR SWINGS WHILE MOVING HARNESSES AND ADDING RESISTANCE TO GEAR ON UPSWING, CLEANED AND INSPECTED ALL PROX & SENSOR HARNESSES AND REINSTALLED, CARRIED OUT FINAL GEAR SWINGS, COULD NOT DUPLICATE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,625 hrs · 41,342 cycles
RED FLOOR EMERGENCY LIGHT AT THE FORWARD DOOR IS OUT. (FL T5574) RELAMPED EMERGENCY LIGHT.
Part: VALVE — MALFUNCTIONED (AC BAY) · airframe 29,223 hrs · 40,778 cycles
SMOKE APPEARS TO BE COMING FROM LEFT PACK. (FLT 5645) REPLACED LEFT PACK INLET VALVE, TEMP CONTROL VALVE, AND BUTTERFLY VALVE IN REFERENCE TO EMB120 MM. P/N 3290054-1, S/N OFF 1887, P/N 979990-1, /N OFF 528, PN 979990-1, SN OFF 2279.
Part: COOLING FAN — MALFUNCTIONED (AC BAY) · airframe 29,180 hrs · 40,720 cycles
LEFT PACK GROUND COOLING FAN INTERMITTENT AND SMOKE SMELL IN COCKPIT. (FLT 5487) REPLACED LEFT GROUND COOLING FAN. P/N AE1711AA0, S/N OFF 193.
Part: ACM — DEFECTIVE (AC BAY) · airframe 28,816 hrs · 40,214 cycles
LEFT PACK BLOWS SMOKE IN THE COCKPIT. (SERVICE) REPLACED LEFT ACM. PN OFF 2204540-2, SN OFF 124-107
Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,434 hrs · 39,706 cycles
OVERHEAD EMERGENCY LIGHT AT ROW 6A IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: COOLING FAN — MALFUNCTIONED (NR 2) · airframe 28,306 hrs · 39,527 cycles
RECEIVED TRIPLE CHIME SMOKE ON MAP DURING GROUND OPERATIONS. CABIN WAS FILLING WITH SMOKE. (FLT 6233) REPLACED NR 2 GROUND COOLING FAN.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,306 hrs · 39,527 cycles
FLOOR EMERGENCY LIGHT AT ROW 9 IS OUT. (FLT 5632) RELAMPED EMERGENCY LIGHT.
2011
Part: STRINGER — CORRODED (FUSELAGE) · airframe 28,256 hrs · 39,465 cycles
CORROSION ON FUSELAGE STRINGER 19 NEAR FRAME 13 BELOW FLOORBOARDS. (C-CHECK) REPLACED FORWARD SECTION OF STRINGER 19.
Part: WIRE — BROKEN (CABIN) · airframe 27,296 hrs · 38,174 cycles
EMERGENCY LIGHT AT ROW 9 DOES NOT ILLUMINATE. (FLT 5442) REPAIRED BROKEN WIRE AT ROW 9 EXIT SIGN.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,232 hrs · 36,695 cycles
FORWARD EMERGENCY LIGHTS DO NOT ILLUMINATE. (FLT 6747) REPLACED FORWARD EMERGENCY LIGHT BATTERY PACK.
Part: WIRE — BROKEN (CABIN) · airframe 26,232 hrs · 36,695 cycles
FORWARD FLOOR EMERGENCY LIGHTS INOPERATIVE. (FLT 6720) REPAIRED BROKEN WIRE AT FLOOR EMERGENCY LIGHT CONNECTOR.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,232 hrs · 36,695 cycles
FORWARD HALF OF CABIN EMERGENCY LIGHTS INOPERATIVE. (FLT 6711) REPLACED NR 1 ELBP.
2010
Part: STRINGER — CRACKED (RT WING) · airframe 26,018 hrs · 36,404 cycles
RIGHT WING STRINGER 8 IS CRACKED AT NR 2 INBOARD FUEL PANEL. (C-CHECK) REPAIRED RIGHT WING NR 2 INBOARD FUEL PANEL STRINGER 8 PER SRM.
Part: FRAME — CORRODED (FUSELAGE) · airframe 25,539 hrs · 35,725 cycles
CORROSION FOUND AT RIGHT INTERIOR FUSELAGE FRAME 40. (C-CHECK) REMOVED AND REPLACED RIGHT FLOORBEAM AT FRAME 40 PER SRM.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 25,539 hrs · 35,725 cycles
FORWARD END OF STRINGER 18 UNDER PAX DOOR CORRODED. (C-CHECK) REMOVED AND REPLACED FORWARD SECTION OF STRINGER 18 PER SRM.
Part: TORQUE TUBE — DEFECTIVE (CABIN DOOR) · airframe 24,844 hrs · 34,760 cycles
MAIN DOOR INSIDE DOOR HANDLE DIFFICULT TO OPEN AND CLOSE. (FLT 6247) REPLACED INTERCONNECT TORQUE TUBE ASSY AND BOTH BUSHINGS.
Part: BOLT — OUT OF ADJUST (CABIN DOOR) · airframe 24,773 hrs · 34,653 cycles
MAIN CABIN DOOR VERY DIFFICULT TO OPEN AND CLOSE. (FLT 6174) ADJUSTED CONCENTRIC BOLT AT FORWARD HINGE ARM.
Part: MECHANISM — LACK OF LUBE (PAX DOOR) · airframe 24,155 hrs · 33,709 cycles
FLT 6030 - MAIN DOOR HARD TO CLOSE. LUBED DOOR MECHANISM.
2009
Part: SMOKE DETECTOR — MALFUNCTIONED · airframe 23,199 hrs · 32,338 cycles
ON TAKEOFF ROLL "SMOKE" ILLUMINATED ON MAP PANEL. (FLT 6605) RESET SMOKE DETECTOR.
Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 22,455 hrs · 31,320 cycles
FLT 7779 - EMERGENCY EXIT ROW "9 C" SIGN BROKEN. REPLACED.
2008
Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 22,047 hrs · 30,798 cycles
FLT 5538 - DURING ENGINE START RECEIVED SMOKE WARNING. INSPECTED LAVATORY AREA, RESET SMOKE ALARM.
Part: LIGHT — SHORTED (CABIN) · airframe 21,715 hrs · 30,368 cycles
FA REPORTS BURNING ELECTRICAL SMELL NEAR FRONT OF CABIN. (FLT 5729)RELAMPED CEILING LIGHT AT 4A.
Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 21,458 hrs · 30,039 cycles
FORWARD SECTION OF EMERGENCY LIGHTS ARE NOT WORKING. FLIGHT 3599. REPLACED NR 1 ELBP IAW MM 33-51-04. OPS CHECK GOOD. P/N D366-04-001, S/N OFF 1329.
Part: UNKNOWN — UNKNOWN · airframe 21,415 hrs · 29,991 cycles
FLT 3619, AIRPLANE WOULD NOT GO INTO REVERSE PITCH AND BRAKES FAILED AS THE AIRPLANE SLOWED BELOW 40 KTS. INSPECTED BRAKE SYSTEM IAW MM 32-45-00. INSPECTED ANTISKID SYSTEM IAW MM 32-41-00, PART A, B, C AND D. ALL SYSTEMS CHECKED GOOD. COMPLIED WITH MAX REVERSE TEST IAW MM 71-00-00. NO DEFECTS FOUND.
Part: WIRE — LOOSE (EMERGENCY BUSS) · airframe 20,470 hrs · 28,811 cycles
FLT 3687 - EMERGENCY BUSS OFF LIGHT ILLUMINATED ON APPROACH. RESET SYSTEM CIRCUIT BREAKER AND SECURED WIRING TERMINAL HARDWARE. NO FAULTS NOTED.
Part: ACTUATOR — MALFUNCTIONED (RUDDER) · airframe 20,322 hrs · 28,625 cycles
FLT 3677 - AFTER DEPARTURE, THE RUDDER PEDALS FELT STIFF. REPLACED BLUE SYSTEM RUDDER ACTUATOR. OPS CHECKS GOOD IAW 27-22-00, PN 388140-1003, SN/OFF 4995.
2007
Part: ALTIMETER — FAILED (COCKPIT) · airframe 18,880 hrs · 26,648 cycles
ON CLIMB-OUT, CAPTAINS ALTIMETER FAILED ALONG WITH ALTITUDE ALERTER. BOTH DISPLAYS SHOW HEADING FLAGS. ATC ADVISED WE WERE OFF COURSE AND ALTITUDE WAS NOT REPORTING. RETURNED TO FIELD. REPLACED CAPTAINS ALTIMETER WITH SERVICEABLE UNIT. PERFORMED PITOT STATIC LEAK CHECK IAW MM 34-22-00.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 18,916 hrs · 26,687 cycles
FIRST OFFICERS WINDSHIELD IS CRACKED ON OUTER LAYER. REPLACED WINDSHIELD IAW MM 56-10-01.
Part: RIB — CRACKED (PAX DOOR) · airframe 18,929 hrs · 26,703 cycles
PAX DOOR RIB MIDWAY UP THE AFT SIDE OF DOOR IS CRACKED. REPLACED RIB IAW SRM 51-10-02 PG 3 SEC 3A.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,929 hrs · 26,703 cycles
FORWARD SEAT TRACK ON LEFT SIDE OF FLOOR IS CORRODED IN MULTIPLE AREAS.REPLACED LEFT FLOOR SEAT TRACK FORWARD SECTION IAW EMB120 MM 53-01-05.
2006
Part: OUTFLOW VALVE — SMOKE (CABIN PRESSURE) · airframe 17,537 hrs · 24,822 cycles
ON TAXI TO HANGAR, AIRCRAFT FILLED WITH SMOKE. PACKS WERE NOT SELECTED ON. INSTALLED SERVICEABLE PRESS REGULATING VALVE IN LEFT POSITION IAW 21-50-00. OPERATIONAL CHECKS GOOD.
Part: APU — MALFUNCTIONED (APU BAY) · airframe 17,534 hrs · 24,819 cycles
STARTED APU WITH GENERATOR ON AND BLEED ON AND COCKPIT FILLED WITH SMOKE. BOTH PACKS WERE OFF. REPLACED APU IAW MM 49-00-02 AND RII 49-300-1000. OPERATIONAL CHECKS GOOD.
Part: TRANSMITTER — ODOR (FUEL FLOW) · airframe 17,480 hrs · 24,760 cycles
UPON LANDING, SMELLED STRONG FUEL ODOR. REPLACED LEFT FUEL FLOW TRANSMITTER AND ASSOCIATED O-RINGS IAW 28-41-00. OPERATIONAL AND LEAK CHECKS GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,362 hrs · 23,301 cycles
2 WHITE EMERGENCY FLOOR TRACK LIGHTS ARE INOP AT SEATS 7, 8A. REPLACED THE TWO WHITE LIGHTS. OPERATIONAL CHECK GOOD.
Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 16,166 hrs · 23,038 cycles
FO SIDE STALL TEST, STALL WARNINGS INOP. REPLACED RIGHT STALL WARNING COMPUTER. OPERATIONAL CHECK GOOD.
2005
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 15,578 hrs · 22,224 cycles
AFT EMERGENCY LIGHTS DO NOT ILLUMINATE. REPLACED AFT EMERGENCY BATTERY PACK, OPERATIONAL CHECK GOOD.
Part: VALVE — SMOKE (RT A/C PACK) · airframe 15,219 hrs · 21,700 cycles
STRONG SMELL OF SMOKE IN CABIN. RECEIVED A PACK FAIL LIGHT. REPLACED RIGHT PACK PRESSURE REGULATOR SHUT OFF VALVE. OPERATIONAL CHECK GOOD.
Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 14,523 hrs · 20,744 cycles
FLOOR LEVEL E-LIGHTS AT ROWS 7A AND 8A ARE INOPERATIVE. REPAIRED SPLICE AT ROW 7A. OPERATIONAL CHECK GOOD.
2004
Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 13,356 hrs · 19,190 cycles
ON TAXI, STALL WARNING LIGHT ON MAP ILLUMINATED. REMOVED AND REPLACED STALL PROTECTOR COMPUTER IAW MM 27-34-02. ALSO REMOVED AND REPLACED STALL WARNING TEST PANEL IAW MM 27-34-00. OPERATIONAL CHECK GOOD.
Part: A/C PACK — SMOKE (LEFT) · airframe 13,212 hrs · 19,023 cycles
LEFT PACK BLOWING SMOKE INTO THE AIR CONDITIONING SYSTEM. PERFORMED AIR CONDITIONING SYSTEM OPERATIONAL CHECK PER MM 21-50-00. SYSTEM OPERATIONAL CHECK GOOD.
Part: PROXIMITY SENSOR — MALFUNCTIONED (RT ELEVATOR TRIM) · airframe 12,986 hrs · 18,728 cycles
TAKEOFF TRIM AURAL WARNINGS CAME ON WITH TRIM IN GREEN BAND. REMOVED AND REPLACED LEFT AND RIGHT ELEVATOR TRIM PROXIMITY SENSORS IAW EMB MM 27-32-05. OPERATIONAL CHECK GOOD.
2003
Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,751 hrs · 17,239 cycles
EXIT SIGN ON FRONT OF SEAT 1B AND C DOES NOT ILLUMINATE WITH THE EMERGENCY LIGHTS. REPLACED FORWARD EXIT SIGN WITH SERVICEABLE UNIT. OPS CHECK GOOD.
Part: BULKHEAD — CRACKED (RT NACELLE) · airframe 11,823 hrs · 17,338 cycles
RIGHT ENGINE AFT OUTBOARD SIDE LOWER NACELLE BULKHEAD CRACKED AT HYDRAULIC LINE CONNECTIONS. LOCATION REF: S/B 120-29-0049 PAGE 15, FIG 2, DET D. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED OUTBOARD LOWER RIGHT NACELLE FIREWALL IAW EMBRAER INSTRUCTIONS PER EACS REF 1C2003-120/3922.
Part: STRUCTURE — CRACKED (RT NACELLE) · airframe 11,823 hrs · 17,338 cycles
RIGHT ENGINE INBOARD SIDE NACELLE DECK CHAFED AND CRACKED AT HYDRAULIC PRESSURE HOSE NIPPLE CONNECTION (REF: S/B 120-29-0049 PAGE 2, FIG 1, DET B). DISCOVERED DURING C-CHECK INSPECTION. DOUBLER ADDED TO AREA, INBOARD NACELLE DECK IAW SRM120 51-10-02 PG 2 SEC 2B.
Part: PIN — FROZEN (RUDDER ROD) · airframe 11,823 hrs · 17,338 cycles
FORWARD FEEDBACK ROD (RUDDER) CONCENTRIC PIN FROZEN WITHIN BOLT. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED FORWARD FEEBACK ROD (RUDDER) CONCENTRIC PIN AND BOLT WITH SERVICEABLE UNIT IAW EMB120 MM 27-21-00.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,823 hrs · 17,338 cycles
LEFT SIDE AFT SECTION OF SEAT TRACK NEEDS TO BE REPLACED DUE TO CORROSION ABOVE SCREW HOLES. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED LT SIDE AFT SECTION OF SEAT TRACK AS REQUIRED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,032 hrs · 16,311 cycles
FLOOR TRACK LIGHTING AT SEAT 7A INOPERATIVE. REPLACED DEFECTIVE FLOOR TRACK LIGHT AT 7A IAW MM 33-50-00. OPS CHECK GOOD.
Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 10,928 hrs · 16,188 cycles
EMERGENCY LIGHTS ROW 9B/C INOPERATIVE. REMOVED AND REPLACED ELBP (AFT) IAW MM 33-50-02. OPS CHECK GOOD.
Part: LIGHT — BROKEN (ROW 6A) · airframe 10,778 hrs · 16,012 cycles
EXIT LIGHT AT ROW 6A IS BROKEN. INSTALLED NEW EXIT LIGHT ASSEMBLY AT ROW 6A. OPS CHECK GOOD.
2002
Part: TAB — CRACKED (LT AILERON) · airframe 9,677 hrs · 14,323 cycles
LT AILERON TRIM TAB CRACKED ON LOWER INBOARD SIDE.REMOVED AND REPLACED LEFT AILERON TRIM TAB ASSEMBLY WITH SERVICEABLE UNIT IAW MM 27-12-02.
Part: INDICATOR — ERRATIC (COCKPIT) · airframe 9,008 hrs · 13,241 cycles
LEFT ENGINE HAD ERRATIC T6 ANALOG NEEDLE READINGS AND HIGH DIGITAL INDICATION (1200 DEGREES C) WITH ASSOCIATED T6 WARNING. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT ENGINE T6 GAUGE. RAN LEFT ENGINE. OPS CHECKS GOOD.
2001
Part: TERMINAL — BROKEN (CABIN) · airframe 8,109 hrs · 11,853 cycles
FORWARD EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. REPAIRED BROKEN TERMINAL END AT EMERGENCY EXIT LIGHT FIXTURE AT FWD CLOSET. OPS CHECK GOOD.
Part: STRIKER — OUT OF ADJ (CARGO DOOR) · airframe 7,617 hrs · 11,184 cycles
CARGO DOOR LIGHT ILLUMINATED ON TAKEOFF ROLL. READJUSTED MICRO SWITCHES STRIKER PLATES IAW EMB 120 MM 52-70-02. OPS CHECK GOOD.
Part: PRESSURE SWITCH — FAULTY (HYD SYSTEM) · airframe 6,779 hrs · 9,901 cycles
RUDDER OVERBOOST LIGHT ILLUMINATED ON DESCENT. FOLLOWED QRH. REPLACED RELAYS K0331, K0319, K0323, K0317, DID NOT SOLVE PROBLEM. REPLACED NR 1 AND 2 AIRSPEED INDICATORS WITH SERVICEABLE UNIT. DID NOT FIX PROBLEM. REINSTALLED NR 1 AND 2 AIRSPEED INDICATORS TO ORIGINAL POSITIONS. BOTH AIRSPEED INDICATORS OPS CHECK GOOD MM 34-12-00. PERFORMED OVERBOOST FAULT ISOLATION MM CHECKS, STEPS 1 THRU 2, 3, AND 4. REMOVED AND REPLACED GREEN SYSTEM PRESSURE SWITCH. PROBLEM STILL EXISTS. REMOVED AND REPLACED RUDDER CONTROL SWITCH S0449 (GREEN SYSTEM SWITCH). OPS CHECKED SYSTEM AND FOUND NORMAL. OVERBOOST LIGHT DID NOT ILLUMINATE. NO LEAKS NOTED AT THIS TIME.GREEN PRESSURE SWITCH P/N 1206P0114-01.
Part: SENSOR — FAILED (RT ELEVATOR) · airframe 6,146 hrs · 9,007 cycles
TRIM AURAL WARNING ACTIVATED ON TAKEOFF ROLL WHEN TRIM WAS SET CORRECTLY. ABORTED TAKEOFF. FOUND RIGHT ELEVATOR TRIM PROXIMITY SENSOR BAD. REMOVED AND REPLACED SENOR, OPS CHECKED GOOD.
Part: RELAY — BURNED (LT DC RELAY BOX) · airframe 6,055 hrs · 8,880 cycles
BURNING SMELL IN COCKPIT INFLIGHT REPORTED BY FLIGHT CREW. ISOLATED SMELL AND EVIDENCE OF SMOKE TO K0543 FEEDER PROTECTION RELAY IN LEFT DC RELAY BOX. REMOVED AND REPLACED K0543 IAW MM 54-52-00 AND MM 24-52-00. RAN ENGINES, SYSTEMS OPS CHECKS GOOD. NO FURTHER ODORS NOTED.
Part: CONTROL PANEL — MALFUNCTIONED (AUTO PILOT) · airframe 5,975 hrs · 8,769 cycles
AFTER TAKEOFF, AUTO PILOT TURNED ON BY ITS SELF. RETURNED TO FIELD. WHILE ON THE GROUND THE AUTO PILOT TURNED ON BY ITS SELF. RAN THE TRIM WHEEL FULL NOSE DOWN AFTER DISCONNECTING AND TRANSFERRING TO FIRST OFFICERS SIDE IT AGAIN TURNED ITSELF ON. REPLACED AUTO PILOT PANEL. OPS CHECKS GOOD. S/N ON: 1689, S/N OFF: 2176.
2000
Part: ROD — CONTAMINATED (RUDDER PEDAL) · airframe 5,869 hrs · 8,607 cycles
CAPTAINS RUDDER PEDALS SLID FORWARD DURING TAKEOFF ROLL. ABORTED TAKEOFF. CLEANED GREASE FROM PEDAL ADJUSTER ROD. CHECKS OK.
Part: LATCH — WORN (MLG DOOR) · airframe 5,821 hrs · 8,528 cycles
LEFT FORWARD LANDING GEAR DOOR REMAINS OPEN ON LEFT SIDE. (DURING FLIGHT) REPLACED WORN OUT DOOR LATCH. FERRY AIRCRAFT TO FAT FOR REPAIR OF LEFT OUTBOARD NACELLE STRINGER AND SKIN DAMAGE DUE TO DOOR COMING OPEN IN FLIGHT. REPAIRS ACCOMPLISHED AND OPS CHECKS GOOD.
Part: LOCK — LOOSE (FUEL DOOR) · airframe 5,753 hrs · 8,430 cycles
AT APPROXIMATELY 100 KIAS, ''DOORS'' LIGHT ILLUMINATED ON MAP AND ''SERVICE'' LIGHT ON OVERHEAD ILLUMINATED. NO AURAL TRIPLE CHIME SOUNDED. ABORTED TAKEOFF. LIGHTS EXTINGUISHED AS WE CLEARED THE RUNWAY. FOUND INBOARD FUEL DOOR FOWARD CAMLOCK POPPED. RESECURED CAMLOCK. SERVICE LIGHT OUT
Part: LOCK — UNSECURE (FUEL DOOR) · airframe 5,582 hrs · 8,167 cycles
SERVICE DOOR LIGHT AND DOORS LIGHT ON MAP ILLUMINATED ON TAKEOFF ROLL. INBOARD FUEL DOOR CAMLOCK NOT COMPLETELY SECURED. LOCKED CAMLOCKS, OPS CHECK GOOD.
1999
Part: ACTUATOR — FAILED (ELEVATOR TRIM)
ON DESCENT WHEN AUTO PILOT WAS DISCONNECTED, FOUND THAT TRIM WHEEL WAS FROZEN IN POSITION. AS DESCENDED BELOW FREEZING LEVEL TRIM SLOWLY BECAME FREE. NORMAL APPROACH AND LANDING. REMOVED BOTH LEFT AND RIGHT ELEVATOR TRIM ACTUATORS AND REPLACED TRIM WITH A SERVICEABLE ONE, OPS IAW MM 27-31-00. ALSO, REMOVED ELEVATOR TRIM SERVO FOR TROUBLESHOOTING. OPS CHECKS GOOD ON GROUND. CLEARED TEST FLIGHT.
1998
Part: REGULATOR — FAILED (WING DEICE)
WING DEICE BOOT OUTBOARD, INBOARD AND MIDDLE FAILED IN FLIGHT IN ICING CONDITIONS. RETURNED TO FAT. REMOVED AND REPLACED 18 PSI REGULATOR. OPS CHECKS GOOD.
Part: PRESS REGULATOR — INOPERATIVE (RT ENGINE)
LEFT AND RIGHT ENGINES DUCT LEAK LIGHT ILLUMINATE AFTER TAKEOFF. LEFT ILLUMINATED AND EXTINGUISHED BUT THE RIGHT ENGINE DID NOT. CHECKED, INSPECTED AND REINSTALLED RIGHT PRESSURE REGULATOR. OPS AND LEAKS CHECKS GOOD ON GROUND.
Part: PRESS REGULATOR — LOOSE (RT ENGINE)
RIGHT ENGINE DUCT LEAK LIGHT ILLUMINATED AFTER TAKEOFF. RETURNED TO FAT. SECURED COLLECTOR CAN ON RIGHT PRESSURE REGULATOR. OPS AND LEAKS GOOD ON GROUND.
Part: DUCT — LOOSE (NR 2 ENGINE)
AT 8.500 FT, NR 2 ENGINE DUCT LEAK LIGHT ILLUMINATED. PER QRH PROCEDURE WITH PRECAUTIONARY ENGINE SHUT DOWN. REINSTALLED DUCT AT DE-ICE PRESSURE REGULATOR.