N576SW
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
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.
101 reports on file, 1998-11-30 – 2014-11-21.
Part: AHRS — FAILED (COCKPIT) · airframe 32,421 hrs · 44,070 cycles
RETURNED TO FIELD DUE TO A NR 1 AHRS FAILURE. R & R THE NR 1 AHRS IAW AMM. OPS CHECKED GOOD.
Part: WIRE HARNESS — FAILED (UPLOCK SENSOR) · airframe 32,369 hrs · 44,002 cycles
LEFT MLG WOULD NOT RETRACT. REMOVED AND REPLACED PROXIMITY SENSOR B HARNESS; ADJUSTED THE LEFT GEAR UPLOCK SENSOR IAW AMM. CHECKED GOOD.
Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 32,250 hrs · 43,845 cycles
FLIGHT DECK FLASHLIGHT BATTERIES INOPERATIVE. R & R BATTERIES IN FLASHLIGHT. OPS CHECKED GOOD.
Part: SUPPORT BRACKET — CRACKED (FRAME 12) · airframe 32,161 hrs · 43,736 cycles
LT DV WINDOW SUPPORT BRACKET AT FRAME 12 IS CRACKED. C-CHECK, REPACED LT DV WINDOW SKIN SUPPORT BRACKET AT FRAME 12 IAW SRM.
Part: WIRE — CHAFED (SPEAKER) · airframe 32,161 hrs · 43,736 cycles
FOUND WIRE CHAFING UNDER CO-PILOT`S SEAT. C-CHECK, REPAIRED WIRE W201-0884-24 FOR RT AURAL WARNING SPEAKER. OPS CHECK GOOD AT THIS TIME.
Part: ATTACH FITTING — CRACKED (COCKPIT) · airframe 32,161 hrs · 43,736 cycles
UNDER CO-PILOTS SEAT CRACKED. C-CHECK, REPAIRED SEAT ATTACHED TO FRAME 13 IAW ETD.
Part: SUPPORT — CRACKED (RT NACELLE) · airframe 32,161 hrs · 43,736 cycles
RT NACELLE BLUE HYDRAULIC SYS HYDRAULIC PACK LOWER SUPPORT FRAME IS CRACKED. C-CHECK, REPLACED LOWER SUPPORT FRAME FOR RT NACELLE BLUE HYDRAULIC PACK.
Part: RIB — CRACKED (LT WING) · airframe 32,161 hrs · 43,736 cycles
LEFT INBD WING, INSIDE 1ST PANEL INBD OF NACELLE RIB NR 8 LOWER STRINGER TO RIB CLIP CRACKED. C-CHECK, REPLACED LOWER SKIN SUPPORT CLIP ON LT WING RIB NR 8 TO STRINGER NR 10 ATTACH IAW SRM.
Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 32,161 hrs · 43,736 cycles
LEFT WHEEL WELL AFT UPPER FIRE WALL CRACKED ON UPPER INBD SIDE. C-CHECK, REPAIRED IAW ETD.
Part: SEAT TRACK — CORRODED (FRAMES 16-19) · airframe 32,161 hrs · 43,736 cycles
LEFT FLOOR SEAT TRACK HAS CORROSION FWD AREA, FRAMES 16-19. C-CHECK, R & R SEAT TRACK.
Part: SEAT TRACK — CORRODED (FRAMES 35-38) · airframe 32,161 hrs · 43,736 cycles
LEFT FLOOR SEAT TRACK AFT AREA BETWEEN FRAMES 35-38 CORROSION FOUND. C-CHECK, R & R THE SEAT TRACK.
Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 32,161 hrs · 43,736 cycles
FLOOR SUPPORT CRACKED ON PILOTS SIDE. C-CHECK, REPAIRED THE FLOOR SUPPORT IAW ETD.
Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 32,161 hrs · 43,736 cycles
FLOOR SUPPORT ON CO PILOTS SIDE IS CRACKED. C-CHECK, REPAIRED THE FLOOR SUPPORT IAW ETD.
Part: MOUNT — CRACKED (LT ENGINE) · airframe 32,161 hrs · 43,736 cycles
LEFT ENGINE FRAME 1 CRACKED AT INBD AND OTBD TORSION MOUNT FITTINGS. C-CHECK, REPLACED LT ENGINE FRAME NR 1 IAW PART 2 OF S/B REPLACEMENT OF NACELLE FRAME NR 1, IN THE ENGINE MOUNTING SUPPORT AREA.
Part: LANDING GEAR — MALFUNCTIONED (RIGHT) · airframe 32,120 hrs · 43,674 cycles
DURING DEPARTURE WHEN SELECTING GEAR UP, RT MAIN APPEARED TO BE STUCK DOWN INDICATED BY RED A & B WITH WIND NOISE AND MISC GRINDING SOUND. PERFORMED SEVERAL GEAR SWINGS. NO DEFECTS NOTED. INSPECTED LT MLG EXTENSIVELY. NO DEFECTS NOTED. COULD NOT DUPLICATE. OPS CHECK GOOD.
Part: SEAL — OUT OF ADJUST (PAX DOOR) · airframe 31,781 hrs · 43,206 cycles
MAIN CABIN DOOR IS EXTREMELY HARD TO OPEN. ADJUSTED SEAL THICKNESS AT AFT UPPER FUSELAGE CORNER, LUBED RODS AND INSIDE MAIN CABIN DOOR.
Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 31,726 hrs · 43,135 cycles
MAIN CABIN DOOR IS DIFFICULT TO OPEN. LUBRICATED LOWER FORWARD AND AFT ROLLERS.
Part: ROD END — OUT OF ADJUST (RT MLG ACTUATOR) · airframe 31,612 hrs · 42,966 cycles
RIGHT MLG WOULD NOT RETRACT. FLT 5432 ADJUSTED THE RT MLG RETRACTION ACTUATOR ROD END & REPLACED RT MLG RETRACTION ACTUATOR ROD END BOLT IAW AMM. PERFORMED SEVERAL GEAR SWINGS AS REQUIRED WITH NO FAULTS NOTED. OPERATIONS CHECKED GOOD, PN O5CAS671501-101SW.
Part: SCREW — DEFECTIVE (LT WING) · airframe 31,330 hrs · 42,594 cycles
LT WING INBD FUEL ACCESS PANEL IS LEAKING FUEL. FLT 7446 REPLACED FUEL ACCESS PANEL 522DB INBD HALF SCREWS WITH PN NAS 1993-4T-SPLSL SELF-LOCKING SCREWS IAW AMM.
Earlier reports · 1998–2013 · 82 reports
2013
Part: UNKNOWN — ODOR (CABIN) · airframe 30,189 hrs · 41,240 cycles
LEFT PACK PRODUCES A STRONG BURNING SMELL ASSOCIATED WITH SMOKE IN THE CABIN DURING INITIAL DESCENT. ISOLATED THE LEFT PACK BY SELECTING OFF AND CONDITIONS DISSIPATED AFTER 2-5 MINUTES. NO FURTHER OCCURANCE WAS NOTED. (FLT 2825) GROUND RAN LEFT PACK WITH APU AND NR 1 ENGINE IN ALL CONFIGURATIONS AND LEFT PACK OPERATES NORMAL. SUSPECT NR 2 ENGINE IS CAUSING OIL BURNING SMELL IN BLEED SYSTEM.
Part: UNKNOWN — ODOR (COCKPIT) · airframe 30,123 hrs · 41,165 cycles
STRONG SMELL OF BURNING PACKS WITH BOTH SELECTED TO LOW. SMELL MOST NOTICABLE IN THE COCKPIT AND DISSIPATES WHEN LEFT PACK OFF. (FLT 7396) RAN LEFT AND RIGHT PACKS FROM ALL THREE BLEED SOURCES WITH NO CHANGE IN SMELL. OPERATED PACKS AT DIFFERENT TEMPERATURE SETTINGS WITH NO UNUSUAL SMELL. OPS CHECK GOOD.
Part: FAN — FAULTY (CABIN) · airframe 30,100 hrs · 41,136 cycles
RIGHT PACK PRODUCES BURNING SMELL AND SOME SMOKE AT HIGH AND LOW POWER SETTINGS. (FLT 7391) REPLACED RIGHT RECIRCULATION FAN AND RIGHT MIXING CHAMBER ASSEMBLY IAW AMM. OPS CHECK AND LEAK CHECK GOOD. P/N ON: AE1209AAB P/N OFF: EVAC523-C2 S/N ON: 514 S/N OFF: 467 / P/N: 120-37720-503
Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 30,028 hrs · 41,052 cycles
PACKS PRODUCED OVERHEATED SMELL. (FLT 5291) PERFORMED OPS CHECK OF BOTH COCKPIT AND CABIN PACKS AS REQUIRED AND COULD NOT DUPLICATE OVERHEAT SMELL. OPS CHECK GOOD AT THIS TIME.
Part: RCCB — FAILED (ELECTRICAL SYS) · airframe 29,967 hrs · 40,980 cycles
INFLIGHT RECEIVED ELECTRIC LIGHT ON THE MAP WITH AN EMERGENCY BUS OFF, ON ELECTRICAL PANEL. RAN QRH PROCEDURE EMERGENCY BUS OFF, DID NOT EXTINGUISH. DUE TO LOSS OF ELECTRICAL GEAR DID NOT DESCEND NORMALLY. EMERGENCY DECLARED. RAN QRH FOR LANDING GEAR EXTENSION BY FREE FALL. (FLT 7399) FOUND NR 2 AUX FEATHER PUMP RCCB STUCK CLOSED AND CB 0470 POPPED AND SIGNS OF ARCING ON C/B. REPLACED RCCB K0217, CB0470 AND FOUND WIRE W206.0481-8 IN LT DC RELAY PANEL OVERHEATED WITH BURNED INSULATION. SWUNG LANDING GEAR, NO DEFECTS NOTED.
Part: DOOR — LACK OF LUBE (CABIN) · airframe 29,913 hrs · 40,916 cycles
MAIN CABIN DOOR EXTREMELY DIFFICULT TO OPEN. (FLT 5636 ) LUBED MAIN CABIN DOOR, DOOR HANDLE, AND HANDLE TORQUE TUBE ASSEMBLY.
Part: CONTROL MODULE — FAILED (LANDING GEAR) · airframe 29,689 hrs · 40,615 cycles
ON DEPARTURE GEAR HANDLE WOULD NOT COME UP. PUSHED DOWNLOCK RELEASE TO RAISE GEAR/HANDLE. (FLT 5356) REPLACED LANDING GEAR INDICATION/CONTROL MODULE ASSEMBLY IN REFERENCE TO EMB120 AMM.
2012
Part: SIGN — MISINSTALLED (CABIN) · airframe 29,395 hrs · 40,263 cycles
EXIT ROW SIGN OVER ROW 5 SEAT B, C, IS POINTING FORWARD NOT AFT. (FLT 5409) REPLACED SIGN.
Part: ANTENNA — DEFECTIVE (WEATHER RADAR) · airframe 29,212 hrs · 40,032 cycles
A STRONG ELECTRICAL SMELL. THE RADAR WAS NOT WORKING, CIRCUIT BREAKER NEVER POPPED AND THEN THE "115 VAC BUS OFF" ON THE EMERGENCY INVERTER 2 TRIPPED. (FLT 7799) REPLACED WEATHER RADAR ANTENNA AND REPLACED FLIGHT MAX DISPLAY UNIT IN REFERENCE TO AMM. P/N: 622-2504-001 S/N OFF: 2166; P/N: D98-00001-58-G S/N OFF: 1571.
Part: PLUNGER — OUT OF ADJUST (SEQUENCE VALVE) · airframe 28,795 hrs · 39,498 cycles
LEFT MAIN GEAR WOULD NOT RETRACT. (FLT 5449) ADJUSTED LEFT INBOARD FORWARD DOOR SEQUENCE VALVE PLUNGER.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,795 hrs · 39,498 cycles
FLOOR EMERGENCY LIGHTS AFT OF ROW 9 ARE INOPERATIVE. (FLT 5549) RELAMPED EMERGENCY LIGHTS.
Part: STRINGER — CRACKED (RT WING) · airframe 28,842 hrs · 39,555 cycles
RIGHT WING NR 8 STRINGER CRACKED AT RIB NR 9. (C-CHECK) REPAIRED RIGHT WING STRINGER NR 8 AT RIB NR 9 IN REFERENCE TO SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,782 hrs · 39,476 cycles
LEFT CABIN FLOORBEAM AT FRAME 16 AREA HAS CORROSION. (SERVICE) REPLACED LEFT CABIN FLOORBEAM AT FRAME 16 PER EMB SRM 51-40-02.
Part: STOP FITTING — OUT OF ADJUST (CABIN DOOR) · airframe 28,648 hrs · 39,316 cycles
MAIN CABIN DOOR HARD TO OPEN UP. (FLT 5460) RE-SECURED LOWER PAX DOOR STOP IN REFERENCE TO MM.
Part: WIRE — BROKEN (CABIN) · airframe 28,648 hrs · 39,316 cycles
ONE RED EMERGENCY LIGHT ON FLOOR IS OUT. (SERVICE) REPAIRED WIRE TO LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,648 hrs · 39,316 cycles
RED EMERGENCY EXIT LIGHT NEAR MAIN CABIN DOOR IS OUT. (FLT 7800) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,540 hrs · 39,181 cycles
FOWARD EMERGENCY EXIT LIGHT IS OUT. (FLT 7778) RELAMPED EMERGENCY LIGHT.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,466 hrs · 39,104 cycles
SEVERAL EMERGENCY LIGHTS ON SIDE WALL AND CEILING ARE OUT. (FLT 7757) REPLACED NR 3 ELBP. PN D366-04-001 SN OFF 176
2011
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,034 hrs · 37,307 cycles
CABIN EMERGENCY FLOOR LIGHTING FROM ROW 6 AND BACK IS OUT. (FLT 5312) REPLACED AFT ELPB. P/N D366-04-001, S/N OFF 1260.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,602 hrs · 36,732 cycles
EMERGENCY LIGHT AT PAX DOOR IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — UNSECURE (CABIN) · airframe 26,602 hrs · 36,732 cycles
FORWARD RED FLOOR EMERGENGY LIGHT IS OUT. (FLT 6821) REPOSITIONED BULB INTO RED LENS.
Part: LENS — OUT OF POSITION (CABIN) · airframe 26,345 hrs · 36,391 cycles
ONE RED LIGHT ON FLOOR LEVEL EMERGENCY LIGHTS IS OUT. (FLT 7794) FOUND RED LENSE COVER SHIFTED AWAY FROM LIGHT AND ADJUSTED AS NEEDED.
Part: MECHANISM — LACK OF LUBE (PAX DOOR) · airframe 26,194 hrs · 36,187 cycles
PAX DOOR HARD TO OPEN. (SERVICE) LUBED PAX DOOR HANDLE MECHANISM.
2010
Part: STRINGER — CRACKED (RT WING) · airframe 25,291 hrs · 35,077 cycles
RIGHT WING LOWER NR 10 STRINGER CRACKED INSIDE THE NR 2 FUEL CELL. (C-CHECK) REPAIRED PER SRM.
Part: SPAR CAP — CRACKED (RT WING) · airframe 25,291 hrs · 35,077 cycles
RIGHT WING INBOARD OF NACELLE UPPER SPAR CAP CRACKED AT HI-LOC ON OUTBOARD SIDE. (C-CHECK) REPAIRED PER EMBRAER APPROVAL ETD2010-120/07092.
Part: WINDOW — CRACKED (COCKPIT) · airframe 25,291 hrs · 35,077 cycles
COCKPIT LEFT DIRECT VISION WINDOW IS CRACKED AT LOWER END. (C-CHECK) REPLACED LEFT COCKPIT DIRECT VISION WINDOW PER AMM.
Part: CONNECTOR — OVERHEATED (ELECTRICAL SYS) · airframe 24,978 hrs · 34,685 cycles
WIRE W206-0051-10 TERMINAL CONNECTOR AT CB0207 IN RT DC BOX IS SHOWING SIGNS OF OVERHEAT. (C CHECK) REPLACED TERMINAL CONNECTOR.
Part: ROLLER — DIRTY (CABIN DOOR) · airframe 24,716 hrs · 34,323 cycles
CABIN DOOR DIFFICULT TO OPEN FROM INSIDE. (FLT 6814)CLEANED ROLLERS FOR CABIN DOOR.
Part: RELAY — MALFUNCTIONED (APU) · airframe 24,716 hrs · 34,323 cycles
APU GENERATOR TRIPPED WITH ASSOCIATED SMOKE SMELL. (FLT 6571)REPLACED APU FEEDER PROTECTION RELAY.
Part: SWITCH — MALFUNCTIONED (AC BAY) · airframe 24,497 hrs · 34,041 cycles
BURNING SMELL FROM LEFT PACK ON GROUND. (FLT 6645) REPLACED PACK SWITCH AND REPAIRED WIRES.
Part: OIL COOLER — LEAKING (RT ENGINE) · airframe 24,346 hrs · 33,869 cycles
GRADUAL LOSS OF OIL PRESSURE, RIGHT ENGINE SHUT DOWN PRECAUTIONARY. (FLT 6237) REPLACED OIL COOLER.
Part: FRAME — CORRODED (FUSELAGE) · airframe 24,338 hrs · 33,860 cycles
FLT 7769-2--MAIN CABIN DOOR FRAMES AND STRINGERS CORRODED. REPAIRED PER SRM.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 24,346 hrs · 33,869 cycles
STRINGERS AND FITTINGS IN AREA OF MAIN CABIN DOOR CORRODED. (FLT 7769) REPAIRED PER SRM.
Part: WIRE — LOOSE (CABIN) · airframe 24,287 hrs · 33,805 cycles
OVERHEAD EMERGENCY EXIT LIGHT ABOVE SEAT 9BC INOP. (FLT 7756) SECURED LOOSE WIRE.
Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 24,171 hrs · 33,660 cycles
FLT 5942 - MAIN CABIN DOOR HARD TO OPEN. LUBED HANDLE MECHANISM.
2009
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,105 hrs · 33,558 cycles
EMERGENCY LIGHTS AT MID FLOOR AND OVERWING EXITS INOP. (FLT 7771) REPLACED EMERGENCY LIGHTS BATTERY PACK.
Part: SOCKET — DIRTY (CABIN) · airframe 24,051 hrs · 33,501 cycles
EMERGENCY LIGHT UNDER FORWARD RIGHT EMERGENCY EXIT INOP. (SVC CK) CLEANED SOCKET.
Part: CAP — LOOSE (EMERGENCY LIGHT) · airframe 23,934 hrs · 33,368 cycles
MULTIPLE EMERGENCY LIGHTS INOP. (FLT 6202)RESECURED LOOSE FUSE CAP.
Part: STRUCTURE — CRACKED (LT NACELLE) · airframe 23,880 hrs · 33,301 cycles
LEFT ENGINE NACELLE CRACKED. (C-CHECK) REPAIRED PER SRM.
Part: BOLT — OUT OF ADJUST (CABIN DOOR) · airframe 23,736 hrs · 33,122 cycles
MAIN CABIN DOOR DIFFICULT TO CLOSE. (FLT 6574) ADJUSTED MAIN CABIN DOOR HINGE ECCENTRIC BOLTS.
Part: SIGN — CRACKED (EMERGENCY LIGHTS) · airframe 22,587 hrs · 31,546 cycles
FLT 6817 - EMERGENCY EXIT SIGN AT 9C CRACKED. REPLACED LIGHT ASSEMBLY.
Part: LIGHT — BURNED (CABIN) · airframe 22,177 hrs · 30,992 cycles
FLT 5785 - ELECTRICAL BURNING ODOR IN MID CABIN. REPLACED BURNED LIGHT ASSEMBLY AT ROW 5.
2008
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,061 hrs · 30,831 cycles
FLT 7796 - ENTRY EMERGENCY LIGHT INOP. RELAMPED.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 22,300 hrs · 31,154 cycles
C-CHECK, FLOOR SUPPORT WEB AT STATIONS 4410.5 - 6653 CORRODED BEYOND LIMITS. REPLACED WEB PER SRM.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 22,300 hrs · 31,154 cycles
C-CHECK, FLOOR SUPPORT WEB CORROSION REMOVAL BEYOND LIMITS PER SRM. REPLACED FLOOR SUPPORT WEB LEFT SIDE AT FS13056 -1573 PER SRM.
Part: ATTACH FITTING — CRACKED (RT WING RIB) · airframe 22,300 hrs · 31,154 cycles
C-CHECK, RIGHT WING RIB NR 16 LOWER CLIP CRACKED. REPLACED PER SRM.
Part: CONNECTOR — CORRODED (NR 2 DPU) · airframe 22,300 hrs · 31,154 cycles
C-CHECK, J1 CONNECTOR OF NR 2 DPU CONNECTOR CORRODED. REPLACED CONNECTOR.
Part: FRAME — CRACKED (FUSELAGE) · airframe 22,300 hrs · 31,154 cycles
C-CHECK, FUSELAGE FRAME 10 CRACKED JUST BELOW LEFT DV WINDOW. REPAIRED PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 22,300 hrs · 31,154 cycles
C-CHECK, LEFT INBOARD FRAME 10 WEB CRACKED, LEFT WHEEL WELL. REPAIRED PER SRM.
Part: CONTROL CABLE — STIFF (AILERON) · airframe 21,331 hrs · 29,884 cycles
AILERON CONTROLS FEEL STIFF IN FLIGHT. (FLIGHT NR 5536) ADJUSTED LT AND RT AILERON TENSIONS IAW MM 27-00-00. OPS CHECK GOOD.
Part: BEAM — DAMAGED (NACELLE) · airframe 20,993 hrs · 29,471 cycles
FLT 3613 - DAMAGE TO KEELSON BEAM FOUND NEAR INBOARD SIDE OF GEAR AT NACELLE. REPLACED DAMAGED SECTION OF KEELSON BEAM IAW EMB SRM 51-40-02.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 20,814 hrs · 29,239 cycles
SKIN DAMAGE ON KEELBEAM AND NACELLE, COMPLIED WITH REPAIRS OF SKIN ON KEELBEAM AND NACELLE AS REQUIRED.
Part: SKIN — DELAMINATED (NR 1 PROP BLADE) · airframe 20,403 hrs · 28,738 cycles
FLT 5543 - RIGHT PROPELLER TIP APPEARS TO BE DELAMINATED. REPLACED NR 1 BLADE ON RIGHT PROP WITH A SERVICEABLE UNIT IAW MM 61-11-01, P/N: RFC11M1-6A S/N OFF: 2172.
Part: MECHANISM — BINDING (PAX DOOR HANDLE) · airframe 20,367 hrs · 28,685 cycles
PAX DOOR HANDLE WILL NOT LOCK AND STOW. LUBED HANDLE LOCKING MECHANISM, OPS CHECK GOOD.
2007
Part: TORQUE TUBE — CORRODED (PAX DOOR) · airframe 20,098 hrs · 28,358 cycles
FLT 3724 - CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE. REPLACED CORRODED CABIN DOOR LOCKING TORQUE TUBE AND BUSHINGS IAW MM 52-1105. DOOR OPS CHECKS GOOD.
Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 19,932 hrs · 28,135 cycles
FLT 5441 - OXYGEN MASKS DEPLOYED IN THE CABIN. RESTOWED ALL O2 MASKS.
Part: HANDLE — BINDING (PAX DOOR) · airframe 19,405 hrs · 27,395 cycles
MAIN CABIN DOOR IS DIFFICULT TO OPEN, FLIGHT NR 5469. CLEANED AND LUBED DOOR HANDLE MECHANISM AND LINKAGE IAW EMB 120 MM 52-11-00.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 19,405 hrs · 27,395 cycles
FORWARD CABIN EMERGENCY LIGHTS DO NOT STAY ON, FLIGHT NR 5706. REPLACED FORWARD EMERGENCY BATTERY PACK IAW 33-50-02 EMB 120 MM.
Part: SKIN — DENTED (FUSELAGE) · airframe 19,204 hrs · 27,117 cycles
FUSELAGE LOWER SECTION HAS A DENT AT STATION 18B AREA. APPLIED STRINGER REPAIR AT STRINGER 20L JUST FORWARD OF FRAME 19 PER SRM 53-00-03.
Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 18,927 hrs · 26,700 cycles
EMERGENCY EXIT SIGN OVER 6A IS INOPERATIVE. REPAIRED BROKEN WIRE BEHIND EMERGENCY LIGHT. OPS CHECKS GOOD.
Part: ACTUATOR — MALFUNCTIONED (NLG) · airframe 18,455 hrs · 26,014 cycles
AFTER TAKEOFF, NOSE GEAR WOULDN'T RETRACT. RETURNED TO FIELD. REPLACED NOSE GEAR ACTUATOR WITH SERVICEABLE IAW EMB 120 MM CH 37-32-11. OPERATIONAL CHECKS GOOD, PN 20605-000-05, SN/ON B51, SN/OFF 4S.
2006
Part: DOOR — BINDING (CARGO BAY) · airframe 16,398 hrs · 23,399 cycles
MAIN CARGO DOOR HARD TO OPEN FROM INSIDE. ADJUSTED THE MAIN CABIN DOOR. OPERATIONAL CHECK GOOD.
2005
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,756 hrs · 22,579 cycles
EMERGENCY LIGHTS REAR OF ROW 9 INOP. REPLACED AFT ELBP. OPERATIONAL CHECK GOOD IAW 24-10-05.
Part: PUMP — LEAKING (HYD SYSTEM) · airframe 15,369 hrs · 22,046 cycles
ON DESCENT, GREEN SYSTEM MAIN PUMP LOW PRESSURE LIGHT ILLUMINATED AND ELECTRIC PUMP CYCLED ON AND OFF. HYDRAULIC QUANTITY WENT TO -0- AND FREE FALL ACCOMPLISHED. REPAIRED LEFT ENGINE HYD PUMP PRESSURE LINE, LEAK CHECK GOOD.
Part: WIRE — BROKEN (EXIT SIGN) · airframe 15,129 hrs · 21,693 cycles
EXIT SIGN ABOVE SEAT 6A INOP. REPAIRED WIRE IAW WAM STANDARD PRACTICES 20-00-00. OPERATIONAL CHECK GOOD IAW AMM 23-50-00.
Part: FLAP — CRACKED · airframe 14,985 hrs · 21,452 cycles
LEFT NACELLE FLAP IS IN THE DOWN POSITION ROUGHLY 10 DEGREES IN THE FLAPS 0 DEGREE SETTING. REPLACED LT NACELLE FLAP ASSY IAW MM 27-50-02.
Part: TERMINAL — LOOSE · airframe 14,985 hrs · 21,452 cycles
ROW 6A EMERGENCY EXIT ROW LIGHT DOES NOT ILLUMINATE. CONNECTED RING TERMINALS TO SIGN. OPERATIONAL CHECK GOOD.
Part: FRAME — CRACKED · airframe 15,008 hrs · 21,478 cycles
RIGHT FRAME 1 OUTBOARD SIDE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED RIGHT FRAME NR 1 IAW SB 120-54-0036 "REV 02".
2004
Part: WIRE — BROKEN (ELEVATOR) · airframe 12,759 hrs · 18,473 cycles
NO LIGHTS OR ALARMS SOUNDED DURING AILERON/ELEVATOR DISCONNECT OPERATION. REPAIRED TWO BROKEN WIRES WERE NEAR THE CONNECTOR AT THE ELEVATOR DISCONNECT. OPERATIONAL CHECK GOOD REFERENCING MM 27-13-01.
Part: RIB — CRACKED (RT WING LE) · airframe 11,915 hrs · 17,390 cycles
RT INBOARD LEADING EDGE I/B RIB IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED AFFECTED CRACKED RIB AND INSTALLED NEW-LIKE UNIT IAW EMB120 SRM 51-10-02 PG 3 SEC 3A.
Part: FRAME — CRACKED (LT NACELLE) · airframe 11,937 hrs · 17,412 cycles
LEFT NACELLE INBOARD HALF FRAME UNDER TAILPIPE AFT MOUNT FRAME CRACK. DISCOVERED DURING C-CHECK INSPECTION. REPLACED NACELLE HALF FRAME IAW 120 SRM 51-10-02.
Part: CHANNEL — CRACKED (PAX DOOR) · airframe 11,937 hrs · 17,412 cycles
PAX DOOR MID SECTION OF DOOR AFT CHANNEL CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CHANNEL TO PAX DOOR MID SECTION AFT AREA OF DOOR IAW SRM 120 51-10-02 PG 3 SEC 3A.
Part: CHANNEL — CRACKED (PAX DOOR) · airframe 11,915 hrs · 17,390 cycles
PAX DOOR MID SECTION OF DOOR FWD CHANNEL CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CHANNEL TO PAX DOOR MID SECTION FORWARD AREA OF DOOR IAW SRM 120 51-10-02 PG 3 SEC 3A.
2003
Part: ACTUATOR — MALFUNCTIONED (RUDDER) · airframe 11,025 hrs · 16,304 cycles
ON CLIMBOUT NO RUDDER TRAVEL. RAN QRH, TURNED OFF BLUE SYSTEM, PROBLEM CEASED. REPLACED BLUE SYSTEM RUDDER ACTUATOR IAW EMB MM 27-21-00. OPS CHECKS AND LEAK CHECKS GOOD.
2002
Part: WIRE — CHAFED (LT ENGINE) · airframe 7,817 hrs · 11,438 cycles
FLIGHT IDLE UNLOCK LIGHT ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. INSPECTED FLIGHT IDLE STOP WIRING AT LEFT ENGINE DECK. FOUND WIRE RUBBING ON ENGINE DECK. WIRE STILL SERVICEABLE AT THIS TIME. APPLIED ANTI-CHAFE AT RUBBING POINT. OPS CHECK GOOD.
2001
Part: LATCH — FAILED (RT MLG DOOR) · airframe 6,251 hrs · 9,195 cycles
RIGHT SIDE FORWARD, OUTBOARD, GEAR DOOR WON''T RETRACT. RETURNED TO PDX. REPLACED LATCH ASSEMBLY ON RIGHT FORWARD OUTBOARD GEAR DOOR PER MM 32-32-00 AND MM 52-81-01. OPS CHECK GOOD.
Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT) · airframe 5,913 hrs · 8,702 cycles
BOTH CAPTAINS AND FIRST OFFICER''S YAW DAMPER FAILED TO ENGAGE. TRIM FAIL LIGHT ILLUMINATED (RED TRIM FAIL LIGHT ON MAP). BURNING SMELL IN COCKPIT. EN ROUTE FRESNO, DIVERTED TO BURBANK AIRPORT. DETERMINED AUTOPILOT CONTROL PANEL SOURCE OF BURNING SMELL. REPLACED APP65A CONTROL PANEL. OPERATED SYSTEMS FOR EXTENDED PERIOD OF TIME WITH NO FURTHER FAILURES. OPS CHECK GOOD. S/N ON: 713, S/N OFF: 7129.
Part: INDICATOR — FAILED (COCKPIT) · airframe 5,660 hrs · 8,345 cycles
ON TAKEOFF AT 80 KTS, HIGH SPEED AURAL SOUNDED. ABORTED TAKEOFF. REMOVED AND REPLACED FIRST OFFICERS HIGH SPEED INDICATOR WITH SERVICEABLE. PERFORMED OPS CHECK WITH PITOT STATIC BOX. OPS CHECK GOOD. LEAK CHECK GOOD IAW MM 34-12-01. (S/N ON: 1795) (S/N OFF: AH732).
2000
Part: STRUCTURE — DAMAGED (TE FLAP) · airframe 4,183 hrs · 6,199 cycles
ON CLIMBOUT THE FLAPS CONTROL FAULT CAME ON INBOARD PAIR, WOULD NOT RESET. INSPECTED FLAP ASSEMBLY, FOUND RIGHT INBOARD BOND SHOE MANGLED AND APPEARED TO HAVE BEEN STUCK IN TRACK. REPLACED BOND SHOE ASSEMBLY IAW 201321 AND 275000. CYCLED FLAPS, OPS CHECK GOOD.
1999
Part: SWITCH — OUT OF ADJUST (CARGO DOOR)
THE CARGO DOOR LIGHT CAME ON DURING FLIGHT. RETURNED TO LAX. ADJUSTED CARGO DOOR MICROSWITCH ROCKER ARM TONGUE IAW 52-72-02. OPS CHECKS GOOD. RESET CARGO DOOR WARNING CB.
1998
Part: WARNING — ACTIVATED (RIGHT)
RIGHT DUCT LEAK WARNING OCCURRED DURING TAKEOFF. RETURNED TO AIRPORT MEL 75-32-2. OPS CHECKS GOOD WITH NO DEFECTS NOTED.
Part: VALVE — FAILED (RT PRESS REG)
SIX SECONDS AFTER TURNING ON THE DEICE BOOTS THE LEFT AND RIGHT MIDDLE LEADING EDGE BOOTS FAILED. THE RIGHT OUTBOARD LEADING EDGE AND VERTICAL FIN AND LEFT INTAKE BOOTS ALL FAILED IN FLIGHT. RETURNED TO SEA. REMOVED AND REPLACED RIGHT PRESSURE REGULATOR VALVE IAW MM 30-10-06, OPS CKS GOOD.