N12569
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.
40 reports on file, 2003-08-21 – 2022-09-09.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 37,870 hrs · 30,726 cycles
LH FLOOR SILL AT FR. 60 NEXT TO SHROUD IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED LH FLOOR SILL (P/N: 145-25422-001) AT FR. 60 IAW EMB 145 SRM 51-40-02.
Earlier reports · 2003–2019 · 39 reports
2019
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,534 hrs · 29,613 cycles
IAH - FLIGHT 4291, DURING MAINTENANCE INSPECTION THE FLOOR PROXIMITY STRIP LIGHT FORWARD OF THE EMERGENCY EXIT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE #2 EMERGENCY LIGHT POWER SUPPLY BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
2018
Part: DISPLAY — SHORTED (NR 2) · airframe 34,960 hrs · 28,341 cycles
THE CREW REPORTED THAT THE NR 2 MFD CIRCUIT BREAKER TRIPPED, THE SCREEN BLANKED AND AN ELECTRICAL BURNING ODOR WAS NOTICED. MAINTENANCE REMOVED AND REPLACED THE NR 2 MFD, OPS TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
2017
Part: SKIN — CRACKED (FRAME 75) · airframe 33,597 hrs · 27,225 cycles
R/H REAR FUSELAGE SKIN AT FRAME 75 STRINGER 1R-3R CRACKED.CUT-OUT DAMAGE SECTION OF EXT FUSELAGE SKIN, FABRICATED REPAIR PARTS AND INSTALLED. AIRCRAFT STILL IN C CHECK.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,492 hrs · 27,139 cycles
AFT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED THE NR 4 BATTERY AND CHARGER ASSY. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.
2015
Part: BEAM — CORRODED (FRAMES 65-68) · corrosion level 2 · airframe 28,144 hrs · 22,842 cycles
DURING C-CHECK, THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
Part: A/C PACK — FAILED (NR 1) · airframe 27,970 hrs · 22,714 cycles
THE CREW REPORTED DUST OR SMOKE OBSERVED IN COCKPIT AND NOISE HEARD NEAR ROW 11 IN FLIGHT. PACK NR 1 OVERLOAD MESSAGE AFTER LANDING. MAINTENANCE INSPECTED AND REPLACED THE NR 1 PACK AIR CYCLE MACHINE. OPS CHECKS WERE GOOD.
2014
Part: FIRE LOOP — INOPERATIVE (NR 2 ENGINE) · airframe 24,834 hrs · 20,263 cycles
THE CREW REPORTED NR 2 ENGINE FIRE DETECTION FAIL MESSAGE DURING FLIGHT. ALL OTHER ENGINE DATA NORMAL. MAINTENANCE INSPECTED AND REPLACED NR 2 ENGINE FIRE LOOP. OPS CHECKED GOOD.
2013
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,912 hrs · 19,568 cycles
DURING ROUTINE MX THE FIRST 2 EMERGENCY AISLE PATH LIGHT STRIPS WERE FOUND INOPERATIVE. MX REPLACED THE NR 2 EMERGENCY LIGHT BATTERY AND OPS CHECKS WERE GOOD.
Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,827 hrs · 19,493 cycles
EMERGENCY LIGHTS INOPERATIVE. R & R INVERTER. OPS CHECKED GOOD, ACFT RELEASED AND RETURNED TO SERVICE.
Part: BULB — WRONG PART (EMERGENCY LIGHT) · airframe 22,316 hrs · 18,330 cycles
DURING MX INSPECTION, THE RT AFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MX TROUBLESHOT AND FOUND THE INCORRECT BULB INSTALLED. R & R BULB WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.
2011
Part: UNKNOWN — MALFUNCTIONED · airframe 18,777 hrs · 15,457 cycles
FLT 4322 EWR. CREW REPORTED UNCOMMANDED TO/RSV ON TAKEOFF ROLL WITH NO EXCEEDANCE NOTED. EWR MX PERFORMED TASK 76-12-01-700-801A AND WAS UNABLE TO DUPLICATE CONDITION. EWR MX ALSO PERFORMED ENGINE POWER RUNS WITH OPERATIONAL CHECKS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.
Part: SMOKE DETECTOR — FAULTY (CABIN) · airframe 18,573 hrs · 15,315 cycles
DURING ROUTINE MAINTENANCE THE LAV SMOKE DETECTOR WOULD NOT TEST. MAINTENANCE REPLACED THE LAV SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD.
Part: RESOLVER — FAULTY (COCKPIT) · airframe 18,557 hrs · 15,302 cycles
CLE FLT 4597 THE CREW REPORTED ACTUAL N1 DID NOT ACHIEVE TARGET N1 ON THE NR 1 ENGINE AT FULL THRUST/TAKEOFF. MAINTENANCE REPLACED THE NR 1 THRUST LEVER RESOLVER. OPERATIONAL CHECKS WERE GOOD.
Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 18,550 hrs · 15,297 cycles
SHV - DURING C-CHECK FRAME 75 VERTICAL STAB ATTACH FITTING LT BOLT SHOWS SIGNS OF FRETTING. MAINTENANCE PERFORMED REPAIR ON FRAME 75 VERTICAL STAB ATTACH FITTING IAW EC5310-01317 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
Part: INVERTER — DEFECTIVE (CABIN) · airframe 18,267 hrs · 15,094 cycles
TYS - A/C WAS IN FOR AA SERVICE CHECK WHEN MAINTENANCE FOUND THE EXIT SIGN AT SEAT 3BC INOP. MAINTENACE REMOVED AND REPLACED THE NR 3 INVERTER IAW 145 AMM 33-50-11. OPS CHECK GOOD AND WAS RELEASED.
Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 17,678 hrs · 14,583 cycles
CMH - FLIGHT 3135, THE CREW REPORTED A BAGGAGE SMOKE INDICATION DURING DESCENT. THE AIRCRAFT LANDED AT CMH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, AND PLACED THE BAGGAGE SMOKE INDICATION ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT SUBSEQUENTLY RETURNED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE AFT CARGO COMPARTMENT SMOKE DETECTOR, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
2010
Part: SMOKE DETECTOR — NO TEST (LAVATORY) · airframe 16,762 hrs · 13,860 cycles
GRB FLT 5958 THE CREW REPORTED THE LAV SMOKE DETECTOR WOULD NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD.
Part: DISPLAY — FAULTY (COCKPIT) · airframe 16,460 hrs · 13,582 cycles
ORD - FLT 5882 THE CREW REPORTED THE CAPTAINS PVD WENT BLANK AND HAD A BURNING SMELL. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE CAPTAINS PFD AND OPERATIONAL CHECKS WERE GOOD.
Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 14,863 hrs · 12,107 cycles
PIT FLT 157 THE CREW REPORTED THE LAV SMOKE DETECTOR WAS INOPERATIVE. MAINTENANCE REPLACED THE LAV SMOKE DETECTOR AND OPERATIONAL CHECKS WERE GOOD.
2009
Part: WIRE — BROKEN (CABIN) · airframe 14,850 hrs · 12,096 cycles
SHV - RIGHT EMERGENCY LIGHT HAS BROKEN WIRE. REPAIRED BROKEN WIRE IAW EMB 145 SWPM 20-21-00. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
2008
Part: ATTACH FITTING — WORN (RT AILERON) · airframe 13,626 hrs · 11,156 cycles
SHV - DURING C-CHECK THE RIGHT HAND AILERON TO PCA ATTACH FITTING WAS FOUND TO HAVE MIGRATED HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW CONTINENTAL EXPRESS EC5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
Part: ATTACH FITTING — GOUGED (LT AILERON) · airframe 13,626 hrs · 11,156 cycles
SHV - DURING C-CHECK THE LEFT HAND OUTBOARD AILERON TO PCA ATTACH FITTING WAS FOUND TO BE GOUGED AND ALSO HAD MIGRATED HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW CONTINENTAL EXPRESS EC5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
Part: WARNING SYSTEM — MALFUNCTIONED (SMOKE DETECTION) · airframe 13,516 hrs · 11,067 cycles
FLT 7822 - SMF - THIS FLIGHT DIVERTED TO SMF ON A ROUTE FROM LAX TO BOI, DUE TO A BAGGAGE SMOKE LIGHT ILLUMINATED INFLIGHT. NO EMERGENCY WAS DECLARED AND AIRCRAFT LANDED SAFELY. FLIGHT CREW REPORTED CLIMBING OUT OF LAX WENT THROUGH MOD TURB SET OFF BAGGAGE LIGHT, NO MASTER WARNING. JUST LIGHT; DIVERTED TO SMF. MX INSPECTED CARGO DETECTORS, NO DEFECTS NOTED AT THE TIME. AIRCRAFT PWR RESET NORMAL. FIRE AND SMOKE TEST OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE.
Part: OIL FILTER — CLOGGED (NR 2 ENGINE) · airframe 13,516 hrs · 11,067 cycles
FLT 7823 - GEG - FLIGHT CREW REPORTED E2 OIL IMPENDING BYPASS MSG ON TAKEOFF ROLL. FLIGHT CREW DID NOT DECLARED EMERGENCY AND AIRCRAFT LANDED SAFELY. CONTRACT MX REMOVED AND REPLACED OIL FILTER AND CREW OPERATIONALLY AND LEAK CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,276 hrs · 10,876 cycles
FLT 7782 - SJC TO LAX - WHILE PERFORMING SERVICE CHECK MX PERSONNEL FOUND LT OVERWING EMERGENCY LIGHT INOP. MX PERSONNEL REMOVED AND REPLACED LT OVERWING EMERGENCY LIGHT BULBS OPERATIONALLY CHECK SATISFACTORY. A/C WAS RELEASED TO RETURN FOR SERVICE.
2007
Part: SELECTOR VALVE — NOISY (LANDING GEAR) · airframe 12,931 hrs · 10,602 cycles
FLT 7803 - LAX TO LAX - FLIGHT CREW REPORTED KNOCKING SOUND WHEN GEAR RETRACTED - FERRY TO ONT, CHANGED SEVERAL COMPONENTS E.I BCU, RELAY K0273 AND FINALLY REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE. OPERATIONALLY, TEST FLEW CHECKED SATISFACTORY AND AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE.
Part: BATTERY — OVERHEATED (ZONE 100) · airframe 12,006 hrs · 9,655 cycles
FLIGHT 7770 - OAK TO LAX - FLIGHT CREW DECLARED EMERGENCY IN FLIGHT DUE TO BATTERY NR 2 OVERHEAT TO 80 DEGREES F. CREW LANDED IN LAX WITHOUT INCIDENT. MX PERSONNEL REMOVED AND REPLACED NR 2 MAIN BATTERY OPERATIONALLY CHECKED WITH NO DEFECTS AND A/C WAS APPROVED TO RETURN FOR SERVICE.
Part: SIGN — MALFUNCTIONED (CABIN) · airframe 11,848 hrs · 9,485 cycles
FLT MX - ONT MX HANGAR - WHILE PERFORMING A TEST ON EMERGENCY LIGHTS, MX PERSONNEL FOUND EMERGENCY EXIT SIGN AT AFT GALLEY FACING PASSENGER CABIN THAT DOES NOT ILLUMINATE. MX PERSONNEL RESET EMERGENCY LIGHT SYSTEM AND FOUND THE EMERGENCY EXIT SIGN AT AFT GALLEY FACING PASSENGER CABIN TO ILLUMINATE. OPERATIONALLY CHECK GOOD AND AIRCRAFT WAS RELEASE TO RETURN FOR SERVICE IN AIRWORTHY CONDITIONS.
Part: SIGN — MALFUNCTIONED (CABIN) · airframe 11,848 hrs · 9,485 cycles
FLT MX - ONT MX HANGAR - WHILE PERFORMING A TEST ON EMERGENCY LIGHTS, MX PERSONNEL FOUND EMERGENCY EXIT SIGN AT AFT GALLEY FACING PASSENGER CABIN THAT DOES NOT ILLUMINATE. MX PERSONNEL RESET EMERGENCY LIGHT SYSTEM AND FOUND THE EMERGENCY EXIT SIGN AT AFT GALLEY FACING PASSENGER CABIN TO ILLUMINATE. OPERATIONALLY CHECK GOOD AND AIRCRAFT WAS RELEASE TO RETURN FOR SERVICE IN AIRWORTHY CONDITIONS.
2006
Part: FIREWALL — CHAFED (APU BAY) · airframe 8,659 hrs · 6,932 cycles
SHV - DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CHAFED AT THE SIX O`CLOCK POSITION. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5310-01359. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
Part: SKIN — CORRODED (CARGO DOOR) · airframe 8,659 hrs · 6,932 cycles
SHV - DURING C-CHECK THE CARGO DOOR LOWER INTERNAL SKIN WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5230-01132. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
2005
Part: CARBON SEAL — FAILED (NR 1 ENGINE) · airframe 7,489 hrs · 6,011 cycles
CLE FLIGHT 2201 - THE CREW REPORTED DURING CLIMB AND DESCENT THERE WAS A OIL ODOR IN THE COCKPIT AND CABIN. MAINTENANCE REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD. SUPPLEMENT THE NR 4 CARBON SEAL WAS FOUND TO BE THE CAUSE OF OIL ODOR.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 6,570 hrs · 5,269 cycles
MCI - DURING MAINTENANCE INSPECTION, THE MAINTENANCE DISCOVERED THAT THE EMEGENCY EXIT SIGN ON THE AFT WALL OF THE GALLEY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (THIS PART IS NOT TRACKED BY SERIAL NUMBER AND NO TIMES ARE AVAILABLE)
2004
Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 5,342 hrs · 4,286 cycles
BNA - CREW REPORTED, DURING PREFLIGHT FOUND EXIT ROW 12 OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXIT ROW EMERGENCY LIGHT IAW EMB 145 AMM 33-50-00. OPS CHECKED SYSTEM GOOD.
Part: FIREWALL — CRACKED (APU BAY) · airframe 4,106 hrs · 3,341 cycles
TYS, DURING A SCHEDULED INSPECTION THE APU FIREWALL WAS FOUND CRACKED AT THE UPPER LEFT ENGINE MOUNT. MAINTENANCE STOP DRILLED THE CRACK, FABRICATED A DOUBLER AND INSTALLED IAW EMB-145/135 SRM-53-32-13.
Part: FIREWALL — CRACKED (APU BAY) · airframe 4,106 hrs · 3,341 cycles
TYS, DURING A SCHEDULED INSPECTION THE APU FIREWALL WAS FOUND CRACKED AT THE UPPER RIGHT ENGINE MOUNT. MAINTENANCE FABRICATED A FILLER AND DOUBLER, AND INSTALLED IAW EC5330-01267.
2003
Part: ODOR — DETECTED (COCKPIT)
FLIGHT 2082 - THE FLIGHT CREW REPORTED THAT A STRONG BURNING SMELL WAS EMITTED FROM THE ENVIRONMENTAL SYSTEM. THE SMELL WENT AWAY WHEN THE POWER LEVERS WERE PUSHED FORWARD. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE ENVIRONMENTAL SYSTEM. THE DISCREPANCY COULD NOT BE DUPLICATED AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: LIGHT — INOPERATIVE (LT OVERWING)
DURING ROUTINE MAINTENANCE THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.
Part: LIGHT — INOPERATIVE (CABIN)
IAH - DURING SCHEDULED MAINTENANCE THE RIGHT CENTER FAIRING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP ON THE EMERGENCY LIGHT ASSEMBLY AND OPERATIONALLY CHECKED THE LIGHT.