N17513
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 |
| PHIL P. O'NEAL | Operator | on 1989-04-06 | Operator named in NTSB report |
Accident & incident history
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.
25 reports on file, 2001-04-07 – 2026-06-24.
Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 23,431 hrs · 20,986 cycles
FLIGHT VTE3340, KCNY - KDEN DEPARTED KCNY. DURING CLIMB AT FL250 THE CAPTAIN'S WINDSHIELD OUTER PANE CRACKED. AN EMERGENCY WAS NOT DECLARED AND THE FLIGHT CONTINUED TO ITS DESTINATION OF KDEN. THIS WINDSHIELD WAS REPLACED JUNE 1, 2026. IT WAS A REPAIRED WINDOW.
Earlier reports · 2001–2024 · 24 reports
2024
Part: BEARING — FAILED (NLG WHEEL)
THE LH NLG WHEEL ASSY DEPARTED THE AIRCRAFT ON TO OUT OF BWI WITH SERVICE TO MCN. COMPANY WAS NOTIFIED BY BWI AIRPORT OPERATIONS THAT THIS OCCURRED AS THE PIC WAS NOT AWARE. THE AIRCRAFT MADE A ROUTINE LANDING IN MCN. UPON INSPECTION, MAINTENANCE FOUND THAT THE LH AXLE HAD FAILED WHICH ALLOWED THE WHEEL ASSY TO SEPARATE FROM THE NLG ASSY. MAINTENANCE REMOVED AND REPLACED THE NLG ASSY. OPS CHECKED GOOD AND NO ADDITIONAL DAMAGE TO THE AIRCRAFT WAS IDENTIFIED.
2008
Part: BRACKET — WORN (RT AILERON) · airframe 16,706 hrs · 13,973 cycles
RIGHT AILERON PCA BRACKET BORE FOR THE BUSHING WORN. REMOVED AND REPLACED PCA BRACKET IAW EMB EC5750-01177, AIRCRAFT STILL IN C-CHECK.
Part: RMU — INOPERATIVE (COCKPIT) · airframe 14,996 hrs · 12,434 cycles
IAH - FLIGHT 2671, THE CREW REPORTED SMOKE FROM THE NUMBER TWO RADIO MANAGEMENT UNIT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO RADIO MANAGEMENT UNIT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
2007
Part: PROXIMITY SENSOR — DEFECTIVE (MLG DOOR) · airframe 15,526 hrs · 13,030 cycles
FLIGHT 2536 SHV - PILOTS REPORTED NOSE LANDING GEAR DOORS REMAIN OPEN WHEN NOSE GEAR IS UP. MAINTENANCE REMOVED & REPLACED NOSE LANDING GEAR SEQUENCE PROX SWITCH IAW EMB 135 AMM 32-63-03, OPS CHECK GOOD. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,390 hrs · 12,918 cycles
IAH - DURING MAINTENANCE INSPECTION, THE LEFT HAND FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFETCS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,772 hrs · 11,612 cycles
IAH - DURING MAINTENANCE INSPECTION, THE AISLE PATH LIGHTING BEHIND THE EMERGENCY EXITS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
2006
Part: ODOR — DETECTED (COCKPIT) · airframe 12,857 hrs · 10,881 cycles
IAH - DURING MAINTENANCE INSPECTION, A SMOKE SMELL WAS DETECTED IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT WITH NO DEFECTS BEING LOCATED.
Part: WINDSHIELD — SHORTED (COCKPIT) · airframe 11,800 hrs · 10,069 cycles
ELECTRICAL STRONG SMELL IN COCKPIT. INSPECTED COCKPIT AND FOUND F/O'S WINDSHIELD TERMINAL BLOCK SHORTED OUT. A/C RELEASED IAW MEL 30-42-02 CAT "C" 067598. REMOVED AND REPLACED F/O'S WINDSHIELD PER A/C MM 56-10-01. REPAIRED POWER CABLE LUG IAW EMB 135 STANDARD WIRING MANUAL 20-00-03. RELEASED AND RETURNED TO SERVICE.
2004
Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 9,060 hrs · 7,935 cycles
DURING SCHEDULED MAINTENANCE THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED THE EMERGENCY LIGHTING SYSTEM AND CLEARED THE DISCREPANCY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,812 hrs · 7,743 cycles
IAH- FLIGHT 2119, DURING PREFLIGHT INSPECTION, THE CREW REPORTED AN EMERGENCY LIGHT STRIP TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,519 hrs · 7,537 cycles
DURING A PREFLIGHT INSPECTION IT WAS FOUND THAT THE SECOND AND THIRD EMERGENCY LIGHT FLOOR STRIPS FROM THE FRONT OF THE AISLE WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 BATTERY CHARGER ASSEMBLY. THE EMERGENCY LIGHTS OPERATIONAL CHECKED GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,228 hrs · 6,455 cycles
TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND OMEGA BEAM AT FRAME 19. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB SRM 53-21-10, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.
Part: FLOORBEAM — CORRODED (GALLEY FLOOR SUP) · airframe 7,228 hrs · 6,455 cycles
DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FORWARD DIGITAL AT FRAME 23. MAINTENANCE REMOVED AND REPLACED THE DIGITAL IAW EMB SRM 51-40-02 AND CPM 51-21-04, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.
2002
Part: OUTFLOW VALVE — FAULTY (AFT FUSELAGE)
CRW FLIGHT#3064 THE CREW REPORTED RAPID DECOMPRESSION IN FLIGHT.THE PRESSURIZATION WAS INOPERATIVE IN AUTO AND MANUAL MODES.MAINTENANCE REPLACED THE ELECTROPNEUMATIC OUTFLOW VALVE.OPERATIONAL CHECKS WERE GOOD.
Part: COFFEEMAKER — ODOR (GALLEY)
CLE FLIGHT NR 3180 THE CREW REPORTED THE LT COFFEE POT WAS SMOKING AND HAD A ELECTRICAL SMELL.MAINTENANCE INSPECTED AND PLACED ON MEL 25-60-02/3.SUPPLEMENT TO FOLLOW.
Part: ACM — INOPERATIVE (CABIN)
IAH FLIGHT # 3958 CREW REPORTED SMOKE IN CABIN WITH #1 PACK RUNNING. MAINTENANCE REPLACED #1 PACK ACM OPERATIONAL CHECK GOOD.
Part: RECEPTACLE — BURNED (GALLEY)
CLE FLIGHT 2955 THE FLIGHT ATTENDANT REPORTED A SMOKE SMELL IN THE GALLEY IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT COFFEE WARMER AND THE CONNECTOR RECEPTACLE. OPERATIONAL CHECKS WERE GOOD. COFFEE WARMER (P/N 1095A).
Part: LEVER — FAULTY (COCKPIT)
CLE FLIGHT NR 3052 THE CREW REPORTED UPON GEAR RETRACTION RECEIVED A LANDING GEAR WARNING AND THE WARNING WOULD NOT CANCEL UNTIL THE GEAR WAS EXTENDED. MAINTENANCE INSPECTED AND REPLACED THE FLAP SELECTOR LEVER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.
Part: WARNING SYSTEM — FAULTY (COCKPIT)
CLE FLIGHT 3078 THE CREW REPORTED A LANDING GEAR WARNING AFTER TAKEOFF. THE WARNING WOULD NOT CANCEL. MAINTENANCE INSPECTED AND REPLACED THE AURAL WARNING UNIT. OPERATIONAL CHECKS WERE GOOD. MAINTENANCE ALSO PERFORMED CONTINUITY CHECK OF WIRES W001-0843-24 AND W001-0845-24. OPERATIONAL CHECKS OF LANDING GEAR ELECTRONIC UNIT. THE AIRCRAFT WAS RELEASED FOR SERVICE.
Part: SKIN — CRACKED (RUDDER II)
DURING ROUTINE MAINTENANCE THE RUDDER II SKIN WAS FOUND CRACKED.THE CRACK WAS APROX.7 1/2 INCHES LONG AND APROX. 4 INCHES FROM THE BOTTOM.THE CRACK WAS PERPENDICULAR TO THE TRAILING EDGE.MAINTENANCE REPAIRED THE RUDDER II SKIN I/A/W CONTINENTAL EXPRESS EC5540-01015.THE AIRCRAFT WAS RELEASED FOR SERVICE.
Part: OUTFLOW VALVE — FAILED (AFT FUSELAGE)
CLE FLIGHT#3146 THE CREW REPORTED A TOTAL LOSS OF PRESSURIZATION IN FLIGHT.THE AIRCRAFT DESENDED TO 10000 FT.AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE ELECTOPNEUMATIC OUTFLOW VALVE.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,242 hrs · 2,821 cycles
TYS DURING A SCHEDULED INSPECTION THE NR 3 AISLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 AISLE EMERGENCY LIGHT ASSEMBLE LIGHT BULB IAW EMB-135 MM 33-50-08, THE OPERATIONAL CHECK WERE SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE.
2001
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 3,090 hrs · 2,670 cycles
TYS DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL PLATE LOCATED BENEATH THE FLOOR AND JUST AFT OF THE COCKPIT ENTRANCE DOOR WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED THE DAMAGED AREA AND ACCOMPLISHED A FILLER/DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5320-01059, EMB SRM 51-20-03, 51-40-02 AND CPM 51-21-04, 05 AND 06. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.
Part: RELAY — BURNED (COCKPIT)
CLE-FLT 3800 THE CREW REPORTED TAT NR 2 HEAT INOPERTATIVE MESSAGE ON SHORT FINAL. ACCOMPANIED BY A STRONG BURNING SMELL IN COCKPIT AND CABIN. MAINTENANCE REPLACED RELAY KO494 AND CONNECTORS XK0494 AND XK0054. PERFORMED OPERATIONAL CHECKS AND AIRCRAFT WAS RETURNED TO SERVICE.