N700LE
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.
30 reports on file, 2000-04-01 – 2006-12-20.
Part: SWITCH — FAILED (PITCH TRIM) · airframe 16,076 hrs · 14,573 cycles
FIRST OFFICER'S PITCH TRIM MAIN INOP MESSAGE ILLUMINATED ON CLIMB-OUT. AIRCRAFT DECLARED EMERGENCY. REMOVED AND REPLACED FIRST OFFICERS YOKE TRIM SWITCH IAW EMB AMM 27-40-03. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICED.
Part: WIRE HARNESS — DAMAGED (CABIN LIGHTS) · airframe 15,926 hrs · 14,451 cycles
BURNING SMELL NOTED COMING FROM MIDDLE ROW SEATS. REMOVED AND REPLACED HARNESS ASSEMBLY AT ROW 7A IAW EMB AMM 33-21-06. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.
Part: WARNING MESSAGE — FALSE ACTIVATION (BRAKES)
ON INITIAL POWER UP FOR TAKEOFF RECEIVED BRAKE DEGRADE EICAS MESSAGE. UPON ABORT OF TAKEOFF MESSAGE WENT AWAY UNTIL RESET FOR TAKEOFF. ONCE POWER WAS ADDED ABOVE IDLE POSITION, MESSAGE CAME BACK. PERFORMED INSPECTION OF ALL BRAKES, NO DEFECTS NOTED. NO BRAKE DEGRADE MSG ON CMC. PERFORMED HIGH POWER ENGINE RUN AND TAXI, IAW AMM 71-00-01. NO FAULTS NOTED, NO BRAKE DEGRADED MESSAGES ON EICAS. COULD NOT DUPLICATE FAULTS, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Earlier reports · 2000–2005 · 27 reports
2005
Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)
CLT - FLT 4892 - DURING PREFLIGHT, EMERGENCY LIGHT FROM ROW 7 FORWARD FAILED TO ILLUMINATE. REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY IAW EMB AMM 33-50-04. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SILL — CORRODED (FUSELAGE)
ABI - DURING INSPECTION OF AIRCRAFT, THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED AFT SILL. INSTALLED NEW SILL IAW EMB SRM, SRM 145/1142 REV 28, CHAPTERS 51-20-03 AND 51-40-02. (M)
Part: SILL — CORRODED (FUSELAGE)
ABI - DURING INSPECTION OF AIRCRAFT, THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED FORWARD SILL. INSTALLED SERVICEABLE SILL IAW EMB 145 (SRM-145/1142 REV 28, CHAPTERS 51-20-03, 51-40-06 AND 51-40-02. (M)
Part: SILL — CORRODED (FUSELAGE)
ABI - DURING INSPECTION OF AIRCRAFT, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMIOVED
Part: FLOOR SUPPORT — CORRODED (FRAME 20)
THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORRODED SECTION. FABRICATED A FILLER, EXTERNAL ANGLE, SHIM AND PLATE. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 28, CHAPTER 53-21-10. (M)
2002
Part: SILL — CORRODED (GALLEY)
ABI - DURING AN IMBV INSPECTION, THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED DAMAGED CENTER SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM (SRM 145/1142 REV 20) CHAPTER 51-40-02, 51-20-03, AND EMB 145 CPM 51-21-04 THROUGH 51-21-06. (M)
Part: FLOORBEAM — CORRODED (GALLEY)
ABI - THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION, GALLEY AREA CENTER BEAM HAS CORROSION AT FRAME 20. REMOVED AND INSTALLED SERVICEABLE BEAM IAW EMB 135 SRM 53-21-40. (M)
Part: SUPPORT — CORRODED (GALLEY)
ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTION GALLEY AREA RAMP SUPPORT HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE SUPPORT IAW EMB 135 SRM 51-40-02. (M)
Part: FLOORBEAM — CORRODED (GALLEY)
ABI - DURING AN IMBV INSPECTION, THE CENTER SECTION OF THE FORWARD DIGITAL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED 15.5 INCHES BY 21.25 INCH SECTION OF THE FORWARD DIGITAL BY CUTOUT. FABRICATED A REPAIR DOUBLER FOR FLANGE TO BE INSTALLED IN CONJUNCTION WITH DIGITAL REPAIR. FABRICATED A REPLACEMENT FORWARD DIGITAL CENTER SECTION, DOUBLERS AND SHIMS. REPAIR DONE IAW EMB145 (SRM 145/1142, REV 20) 53-21-10 PARA 4 FIG 203, EMB GST-3718/02 AND STANDARD SRM PRACTICES. (M)
Part: FITTING — GOUGED (VERTICAL STAB)
ABI - DURING AN IMBV INSPECTION, VERTICAL STABILIZER FITTINGS THAT ATTACH TO THE HORIZONTAL STABILIZER WERE FOUND TO BE GOUGED. REMOVED GOUGES BY REAMING LEFT AND RIGHT FITTINGS TO 2.2834 INCH. REPAIR DONE IAW EMB GST-3689/02. (M)
Part: BEAM — CORRODED (GALLEY)
ABI - DURING AN IMBV INSPECTION, THE GALLEY CENTER BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. PERFORMED TWO CUT OT OF DAMAGED AREAS. BOTH CUTOUT AREAS FALL WITHIN THE TOTAL LENGTH OF CUTOUT ALLOWED. FABRICATED A U-SHAPE EXTERNAL DOUBLER. REPAIR DONE IAW EMB 135 SRM (145/1142 REV 20) 53-21-10 PARA 5 FIG 204 SHEET 2. (M)
Part: FLOORBEAM — CORRODED (GALLEY)
ABI - THIS IS A LEVEL 2 FINDING DURING AN IMBV INSPECTION, GALLEY AREA AFT DIGITAL HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE DIGITAL IAW EMB 145 SRM 51-40-02. (M)
Part: SILL — CORRODED (GALLEY)
ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTION SERVICE DOOR AFT SILL HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 135 SRM 51-40-02. (M)
Part: BEAM — CORRODED (GALLEY)
ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTION, LEFT OMEGA BEAM DOUBLER BETWEEN FRAME 65 AND 68 CORRODED. REMOVED AND INSTALLED SERVICEABLE BEAM IAW EMB 135 SRM 51-40-02. (M)
Part: SILL — CORRODED (GALLEY)
ABI - THIS IS A LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTION GALLEY AREA LEFT SILL HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 135 SRM 51-40-02. (M)
Part: SILL — CORRODED (GALLEY)
ABI - THIS IS LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTION SERVICE DOOR FORWARD SILL HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 135 SRM 51-14-02. (M)
Part: PROXIMITY SWITCH — FAILED (MLG)
RDU - FLT 4879 - RIGHT MAIN GEAR UNSAFE INDICATION ON APPROACH INTO RDU. CREW PERFORMED CHECKLIST. GEAR STILL SHOWING UNSAFE. LANDED WITHOUT INCIDENT HAD GEARS PINNED BEFORE EXITING RUNWAY. RAI CHANNEL A PROX SWITCHES ON RIGHT AND LEFT MLG IAW AMM 32-61-02. EXTENSION/RETRACTION CHECK GOOD PER 32-32-00, S/N RT A11243/ LT A11215. (M)
2001
Part: SWITCH — FAILED (NR 1)
DFW - FLT 3423 - NR 1 THRUST REVERSER DISAGREE DURING TAKEOFF. ABORTED TAKEOFF. REMOVED AND REPLACED LOWER INBOARD UPPER OUTBOARD STOW SWITCH IAW EMB AMM 78-34-01-000. OPS CHECK GOOD. (M)
Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT)
SAV - FLT 3478 - ABORTED TAKEOFF. THRUST REVERSE DISAGREE ICAS MESSAGE. PERFORMED OPS CHECKS AND HIGH SPEED RUNS IAW AMM. OPS CHECK GOOD. COULD NOT DUPLICATE. (M)
Part: WARNING SYSTEM — FALSE INDICATION (COCKPIT)
MKE - FLT 3276 - THRUST REVERSER DISAGREE ON TAKEOFF ROLL ALONG WITH NO TAKEOFF CONFIG ON EICAS. COMPLETED HIGH SPEED TAXI AND THRUST REVERSER OPS CHECK IAW AMM 78-31-01. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
ABI - MAINTENANCE FOUND THE LEFT OMEGA BEAM TO BE CORRODED BEYOND SRM LIMITS AT FRAME 20. MAINTENANCE REPAIRED FRAME IAW EMB SRM 53-21-10. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
ABI - MAINTENANCE REPORTED THE LEFT OMEGA BEAM TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAMES 23 AND 25. MAINTENANCE REPAIRED DAMAGE IAW EMB SRM AND REPAIR STATEMENT GST 1298/01. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)
ORD - FLT 4433 - CREW REPORTED THAT AFTER TAKEOFF LAV SMOKE WARNING CAME ON EICAS. CREW FOLLOWED AOM PROCEDURE AND RETURNED TO ORD. LAV SMOKE WARNING LIGHT WENT OUT DURING APPROACH, BUT NOTED NO BURNING SMELL IN LAV AREA. REMOVED AND REPLACED LAV SMOKE DETECTOR IAW AMM. OPS CHECK GOOD. (M)
Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)
ORD - FLT 4127 - LAVATORY SMOKE INDICATION CAME ON DURING CLIMB-OUT. REMOVED AND REPLACED LAV SMOKE DETECTOR IAW AMM. OPS CHECK GOOD. (M)
2000
Part: UNKNOWN — ODOR (COCKPIT)
CMH - FLT 5169 - CREW DETECTED AN OIL ODOR IN THE COCKPIT. OIL PRESSURE SENSOR REPLACED AND AIRCRAFT RETURNED TO SERVICE. (X)
Part: UNKNOWN — ODOR (CABIN)
MSN - FLT 4116 - UPON LANDING, CREW NOTED FOG/SMOKE IN CABIN AREA WITH OILY SMELL AND LAV SMOKE INDICATION. CREW TAXIED TO GATE, NO FIRE BOTTLES WERE USED. NO FURTHER INCIDENTS WERE REPORTED. APU PUT ON MEL AT THIS TIME. (M)
Part: LIGHT — INOPERATIVE (CABIN) · airframe 1,188 hrs
CMH - FLT 4980 - EMERGENCY FLOOR LIGHTING INOPERATIVE ON CENTER SECTION. REMOVED AND REPLACE DLIGHT STRIP. OPS CHECK GOOD. (M)