N16511
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
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.
19 reports on file, 2000-07-26 – 2024-07-24.
Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 20,392 hrs · 22,230 cycles
7/24/2024 - FLT VTE3348 - CREW REPORTED THAT CAPT WINDSHIELD BROKE UPON LEVELING AT FL290. RETURNED TO KPHX. MAITNENANCE REMOVED AND REPLACED THE WINDSHIELD IAW EMB135 AMM PROCEDURES. OPS CHECKED GOOD.
Earlier reports · 2000–2008 · 18 reports
2008
Part: LIGHT — DEFECTIVE (CABIN) · airframe 15,093 hrs · 15,474 cycles
FLIGHT 2513 -EWR- FLIGHT CREW REPORTED ELECTRICAL BURNING ODOR IN FORWARD CABIN. EWR MX REMOVED AND REPLACED PASSENGER CABIN LIGHT AT ROW 1A AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)
2006
Part: ROLLER — OUT OF ADJUST (PAX DOOR) · airframe 11,859 hrs · 12,194 cycles
FLIGHT NR 3176 THE CREW REPORTED THE MAIN CABIN DOOR WAS VERY DIFFICULT TO CLOSE. MAINTENANCE INSPECTED AND ADJUSTED THE MAIN CABIN DOOR TOP AFT FRAME ROLLER. OPERATIONAL CHECKS WERE GOOD.
Part: FUEL CONTROL — LEAKING (APU) · airframe 10,608 hrs · 10,805 cycles
CLE FLIGHT NR 2592, THE CREW REPORTED A STRONG FUEL SMELL WHEN STARTING THE APU. MAINTENANCE INSPECTED AND PLACED THE APU ON MEL IAW 49-00-00. CLE FLIGHT NR 3235 MAINTENANCE ENTRY FOR CLEARING MEL. MAINTENANCE REMOVED AND REPLACED THE APU FUEL CONTROL UNIT. ALL OPS CHECKS WERE REPORTED GOOD ENTRY DATED 27 MAR 06.
Part: SPLICE — LOOSE (EMERGENCY LIGHT) · airframe 10,329 hrs · 10,507 cycles
DURING ROUTINE MAINTENANCE THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE SPLICE SP9043 AT THE EXIT IDENTIFIER SIGN AT THE SERVICE DOOR. OPERATIONAL CHECKS WERE GOOD.
2005
Part: ENGINE — LEAKING (NR 1)
CLE FLIGHT NR 2153, AFTER TAKEOFF, THE CREW SAW AND SMELLED SMOKE AND THE LAV SMOKE ALARM SOUNDED. THE AIRCRAFT RETURNED TO CLE WITHOUT INCIDENT. MAINTEANCE FOUND THE NR 1 ENGINE BLOWING SMOKE INTO THE AIRCRAFT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. THE AIRCRAFT RETURNED TO SERVICE.
2004
Part: BRACKET — GOUGED (RT AILERON) · airframe 7,276 hrs · 7,346 cycles
TYS - DURING A SCHEDULED 2C INSPECTION THE RT AILERON PCA ATTACH BRACKET WAS FOUND GOUGED. MAINT REMOVED AND REPLACED THE AILERON PCA BRACKET PRIMED AND PAINTED IAW SRM 51-20-03 AND EA 2710-01017. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.
Part: BRACKET — WORN (RT AILERON) · airframe 7,276 hrs · 7,346 cycles
TYS - DURING A SCHEDULED 2C INSPECTION THE RIGHT PCS AILERON O/B BRACKET BUSHING WAS FOUND MIGRATING. MAINT REMOVED AND REPLACED THE RIGHT AILERON PCA ATTACH BRACKET IAW EA-2710-01017 AND 51-20-03; 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.
2001
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 3,523 hrs · 3,161 cycles
TYS DURING A SCHEDULED INSPECTION THE CENTER FLOORBEAM TOP CAP WAS FOUND CORRODED BETWEEN FRAMES 19 AND 22. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB135 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.
Part: STRINGER — CHAFED (FUSELAGE) · airframe 3,523 hrs · 3,161 cycles
TYS DURING A SCHEDULED INSPECTION THE EXTERNAL STRINGER 19L WAS FOUND CHAFED JUST AFT OF HYDRAULIC PUMP. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR OF STRINGER 19L IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION 5310-01207, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.
Part: FIRE LOOP — CHAFED (LT ENGINE) · airframe 3,523 hrs · 3,161 cycles
TYS DURING A SCHEDULE INSPECTION THE LEFT HAND ENGINE FIRE DETECTION LOOP WAS FOUND TO BE CHAFED BEYOND MANUFACTURES LIMITS. MAINTENANCE REMOVED AND REPLACED THE FIRE DETECTION LOOP IAW EMB135 MM 26-11-01, OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 3,523 hrs · 3,161 cycles
TYS DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL PLATE LOCATED JUST AFT OF THE COCKPIT ENTRANCE DOOR WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE FORWARD DIGITAL PLATE IAW EMB 135 SRM 51-40-02 AND EC 35320-01059, THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.
Part: CONNECTOR — BROKEN (CABIN) · airframe 3,523 hrs · 3,161 cycles
TYS DURING A SCHEDULED 1-C INSPECTION, PANEL 251 HF EMERGENCY LIGHT STRIP, WAS INOPERATIVE, DUE TO A BROKEN CONNECTOR. MAINTENANCE INSTALLED A NEW CONNECTOR ON PANEL 251 HF IAW EMB 135/145 AMM AND PERFORM A OPS CHECK, EVERYTHING WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF ALL MAINTENANCE.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 3,523 hrs · 3,161 cycles
TYS DURING A SCHEDULED 1C INSPECTION THE FLOORBEAM SPLICE CAP OVER FRAME 20 ON RIGHT SIDE WAS FOUND CORRODED AROUND THE RIVETS. MAINTENANCE REMOVED AND REPLACED THE RIVETS, CLEAN THE CORROSION, REWORKED THE AREA IAW EMB 135/145 SRM 51-40-02 AND CPM 51-17-00--51-21-07. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF ALL MAINTENANCE.
Part: SILL — CORRODED (FUSELAGE) · airframe 3,523 hrs · 3,161 cycles
TYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS FOUND UNDER THE SERVICE DOOR SILL AND SCREW HOLES. MAINTENANCE REMOVED AND REPLACED ONE NUT PLATE, CLEAN THE CORROSION, REFINISH THE AREA IAW EMB 135/145 SRM 51-40-02 AND CPM 51-17-04--51-21-07, ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF ALL MAINTENANCE.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 3,523 hrs · 3,161 cycles
TYS DURING A SCHEDULED 1-C INSPECTION THE LEFT FLOOR SUPPORT PLATE FWD OF SERVICE DOOR WAS FOUND CORRODED AROUND SCREW HOLES. MAINTENANCE REMOVED AND REPLACED THE NUT PLATE, CLEAN THE CORROSION, REFINISH THE AREA IAW EMB 135/145 SRM 51-40-02, CPM 51-21-17-00 AND 51-21-04, 05 AND 06. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF ALL MAINTENANCE.
Part: OIL CAP — OUT OF POSITION (APU)
CLE FLIGHT 3864 THE CREW REPORTED A LAV SMOKE WARNING INDICATION ON TAXI OUT WITH A SMELL OF SMOKE IN LAV. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE APU OIL SERVICE CAP WAS OFF AND OIL LEAKING OUT OF RESERVOIR. THE APU WAS SERVICED TO PROPER LEVEL AND THE CAP WAS INSTALLED. THE SPILLED OIL WAS CLEANED UP. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE.
2000
Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)
LGA - FLT 3698 - CREW REPORTED AFTER TAKEOFF, RECEIVED A ''LAV SMOKE'' EICAS MESSAGE AND SMELLED SMOKE IN THE COCKPIT. MAINTENANCE INSPECTED LAV SMOKE DETECTION SYSTEM IAW EMB MM 26-14-00. NO FAULT OR DEFECTS NOTED. REMOVED FROM MEL AND THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)
Part: SMOKE — DETECTED (COCKPIT)
LGA - FLT 3698 - THE CREW REPORTED AFTER TAKEOFF, RECEIVED A LAV SMOKE EICAS MESSAGE AND SMELLED SMOKE IN THE COCKPIT. THE AIRCRAFT RETURNED TO LAGUARDIA WITH NO INCIDENT. MAINTENANCE INSPECTED ENGINES AND APU FOR ANY OIL FUEL LEAKS. PERFORMED GROUND RUN OF BOTH ENGINES. RAN APU ADN LEFT AND RIGHT PACKS. NO DEFECTS WERE FOUND. PLACED LAV SMOKE DETECTOR ON MEL AND RELEASED AIRCRAFT BACK TO SERVICE. (M)