N15509
Registered owner: CORPORATE FLIGHT MANAGEMENT INC, TN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| CORPORATE FLIGHT MANAGEMENT, INC. (FJTA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
Maintenance disclosures
DAY FLIGHT 2382 - THE CREW REPORTED 10 MINUTES INFLIGHT IN CLIMB MODE THE NR 2 ENGINE POWERED BACK TO FLIGHT IDLE UNCOMMANDED. THE AIRCRAFT DIVERTED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE FADEC 2A RESISTOR MODULE A0100 AND CONNECTOR J0584. OPERATIONAL CHECKS WERE GOOD.
DURING A ROUTINE MX INSPECTION, NR 1 EMERGENCY SIDE MARKER LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 4 INVERTER WITH OPERATIONAL CHECK GOOD. A/C APPROVED FOR RETURN TO SERVICE.
SDF - DISCREPANCY - 12A EMERGENCY LIGHT INOP. REMOVED AND REPLACED 12A EMERGENCY LIGHT IAW EMB 135 AMM 33-50-13. OPS CHECK GOOD.
DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT LIGHT WAS INOPERATIVE AT THE LEFT OVERWING EXIT DOOR. MAINTENANCE INSPECTED AND REPLACED THE NR 4 INVERTER. OPERATIONAL CHECKS OF THE EMERGENCY LIGHT SYSTEM WERE GOOD.
DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT WALL LIGHTED PLACARD WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LIGHTED PLACARD. OPERATIONAL CHECKS WERE GOOD.
CLE FLIGHT 2453 THE CREW REPORTED SMOKE VISIBLE FROM CAPTAIN'S LOWER WINDSHIELD. MAINTENANCE INSPECTED AND REPLACED THE CAPTAINS WINDSHIELD. OPERATIONAL CHECKS WERE GOOD.
CREW REPORTED MAIN CABIN DOOR HARD TO OPEN. MX INSP AND REPLACED ACTUATING CAM BELLCRANK AND BUSHING. OPS CHECK GOOD.
CLE FLIGHT 2944 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. MAINTENANCE INSPECTED AND ADJUSTED THE UPPER AND LOWER STABILIZER BARS OF THE MAIN CABIN DOOR. OPERATIONAL CHECKS WERE GOOD.
DURING ROUTINE MAINTENANCE, THE EXIT ROW EMERGENCY EXIT SIGN DID NOT ILLUMINATE DURING TESTING. MAINTENANCE REPLACED THE EXIT SIGN AND OPERATIONAL TESTS WERE GOOD.
SHV- DURING C-CHECK THE EMERGENCY LIGHT ON PANEL 233 BLC WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW EMB 135 AMM 33-50-15. THE LIGHT OPERATIONAL CHECKED GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
SHV- DURING C-CHECK THE EMERGENCY LIGHT ON PANEL 234ARC FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW EMB 135 AMM 33-50-14. THE LIGHT OPERATIONAL CHECKED GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
SHV- DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5320-01111. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
SHV- DURING C-CHECK THE NR 1 LOWER COWLING AFT EDGE STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
SHV- DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
SHV- DURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED AT FRAME 19 TO FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
SHV- DURING C-CHECK THE CROSSBEAM AT FRAME 22 BETWEEN THE RIGHT SILL AND THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
SHV- DURING C-CHECK THE FORWARD FLOORBEAM AT FRAME 16 TO FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DIGITAL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
SHV- DURING C-CHECK THE NR 1 ENGINE UPPER COWLING, AFT OUTBOARD RIB WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
SHV- DURING C-CHECK THE AFT FLOORBEAM AT FRAME 17 TO 19 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
SHV- DURING C-CHECK THE LEFT RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE AFFECTED ANGLE, FABRICATED AND INSTALLED A NEW RAMP ANGLE IAW EMB 135 SRM 51-30-01 AND EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE RIGHT HAND UPPER APU MOUNT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 135 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
SHV- DURING C-CHECK THE AFT FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
SHV- DURING C-CHECK THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
CLE FLIGHT 2152 THE CREW REPORTED THE FORWARD AISLE PATH EMERGENCY LIGHT WAS INTERMITTENT WHEN TESTED. MAINTENANCE INSPECTED AND RESECURED THE CONNECTION ON THE FORWARD EMERGENCY LIGHT STRIP. OPERATIONAL CHECK WAS GOOD.
CLE FLIGHT 2083, THE CREW REPORTED AISLE PATH EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD.
DURING ROUTINE MAINTENANCE THE FIRST ALL WHITE EMERGENCY AISLE PATH LIGHTING STRIP WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE AISLE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD.
CLE FLIGHT 2116 THE CREW REPORTED A ENGINE NR 2 FIRE DETECT FAIL MESSAGE INTERMITTENTLY IN FLIGHT. MAINTENANCE REPLACED THE NR 2 ENGINE PYLON FIRE DETECTOR ASSEMBLY. ALSO REPLACED THE NR 2 ENGINE FIRE CONTROL MODULE. OPERATIONAL CHECKS WERE GOOD.
CLE FLIGHT#2083 THE CREW REPORTED A ENGINE #2 FIRE DETECTOR FAIL MESSAGE INTERMITTENTLY ON THE DESCENT.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE #2 ENGINE FIRE DETECTOR LOOP ASSEMBLY.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.
TYS DURING A SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE FORWARD DIGITAL BETWEEN FRAMES 15 AND 16 AT CENTER AND LEFT SIDE. MAINTENANCE REMOVED THE DAMAGED SECTION, FABRICATED NEW ANGLE, SHIM, FILLER AND PLATE. INSTALLED REPAIRED PARTS IAW-EMB-135/145-SRM-51-20-03 & 51-40-02, CPM-51-21-04, 05, AND EC5320-01059. REPAIR PROCEDURES WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE.
TYS DURING A SCHEDULED 1-C INSPECTION THE LEFT FUSELAGE TO SPAR 3 ROD END ASSEMBLY HAD CORRODED ON THE LOWER ROD END. MAINTENANCE REMOVED AND REPLACED THE LEFT ROD ASSEMBLY IAW GST-3655A-01 WHICH WAS ACCOMPLISHED. THE AIRCRAFT WILL BE RELEASED TO SERVICE UPON COMPLETION OF INSPECTION.
TYS During a scheduled inspection the lower TCAS antenna was found corroded. Maintenance removed and replaced the TCAS antenna I.A.W.-EMB-135-AMM-34-43-03, operational checks were satisfactory. Aircraft released for service.
TYS DURING A SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE LEFT OMEGA BEAM AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED SECTION, FABRICATED NEW ANGLE, SHIM, FILLER AND PLATE. INSTALLED REPAIRED PARTS AND FLOORBEAM IAW EMB-135/145-SRM-53-21-10 & 53-40-02, CPM-51-21-04, 05, 06 AND EC5320-01010 (6.1.3). REPAIR PROCEDURES WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE.
TYS DURING A 1-C INSPECTION THE RIGHT FUSELAGE TO SPAR 3 ROD ASSEMBLY HAD CORROSION ON THE LOWER ROD ENDS. MAINTENANCE REMOVED AND REPLACED RIGHT ROD ASSEMBLIES IAW EMB GST-3655A/01 WHICH WAS ACCOMPLISHED. THE AIRCRAFT WILL BE RELEASED TO SERVICE UPON COMPLETION OF INSPECTION.
TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE AFT GUSSET AT FRAME 18. MAINTENANCE REMOVED AND REPLACED AFT GUSSET AT FRAME 18 IAW EMB-135 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.
TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM RAMP ANGLE AT FRAME 17. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB-135 SRM 51-20-03, 51-40-02 AND 51-20-01. THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.
CLE FLIGHT NR 3899 CREW REPORTED THAT THE NUMBER 1 TRANSPONDER NO MODE "C". NUMBER 2 TRANSPONDER ALREADY ON MEL. RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, AND REMOVED AND REPLACED THE NUMBER 1 TRANSPONDER. SYSTEM OPERATIONAL CHECKS GOOD. AIRCRAFT WAS RELEASED TO SERVICE.
YYZ FLIGHT 3991 THE CREW REPORTED A AIR/GROUND MESSAGE WHILE POWERING UP THE AIRCRAFT AT THE GATE. REPORTED THE SENSORS APPEAR TO INDICATE THE AIRCRAFT WAS IN FLIGHT. MAINTENANCE REPLACED THE RIGHT MAIN GEAR AFT WOW PROXIMITY SENSOR. OPERATIONAL CHECKS WERE GOOD.
EWR - FLT 3619 - THE CREW REPORTED SMOKE IN THE COCKPIT WHILE TAXI. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PITOT 2 CURRENT SENSOR AND RELAY. OPS CHECK WERE GOOD IAW 30-53-00 AND 30-31-00. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)
TYS - FLIGHT 3809, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH EMERGENCY EXIT LIGHTS DID NOT STAY ILLUMINATED. MAINTENANCE CLEANED AND RESECURED THE CONNECTORS ON THE AFFECTED LIGHT STRIPS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
CLE - FLIGHT 3667, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH LIGHTING STRIP AT ROWS 8 AND 9 WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP IN ACCORDANCE WITH EMB145 M/M 33-50-12, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
CLE - FLT 4194 - THE CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED A LAVATORY SMOKE WARNING. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND NO EVIDENCE OF SMOKE OR FIRE AND REPLACED THE LAVATORY SMOKE DETECTOR IAW EMB MM 26-14-01. OPS CHECKS WERE GOOD IAW 26-14-00. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)
CLE - FLT 4046 - THE CREW REPORTED WHEN THE ANTI-ICE WAS TURNED ON IN FLIGHT THERE WERE EXHAUST FUMES EVIDENT IN THE CABIN. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FUEL NOZZLES IAW ROLLS ROYCE MM 73-11-00. OPERATIONAL CHECKS WERE GOOD IAW 72-00-00. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)
CLE - FLT 3815 - THE CREW REPORTED AFTER TAKEOFF, RECEIVED A LAVATORY SMOKE WARNING. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND RESIDUAL COMPRESSOR WASH FLUID FROM PREVIOUS OVERNIGHT MAINTENANCE. PERFORMED ENGINE GROUND RUNS IAW EMB 135 MM 71-00-01 AND 26-23-00, NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)