N451FL
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.
5 reports on file, 2012-09-25 – 2015-12-14.
Part: UNKNOWN — LEAKING (BLEED AIR SYS) · airframe 9,896 hrs · 8,167 cycles
CREW EXPERIENCED A SMOKEY SMELL ON CLIMB OUT WITH ANTI-ICE ON. THE SMELL DISSIPATED WHEN ANTI-ICE WAS TURNED OFF. MX FOUND THE SPIRAL WRAP FROM THE ANTI-ICE DUCTING. THE BLEED LEAK WAS ISOLATED & REPAIRED. THE SPIRAL WRAP WAS REPLACED & LEAK OPERATIONS CHECKS WERE GOOD. THE ACFT WAS RETURNED TO SERVICE.
Part: CLAMP — LOOSE (COALESCER SOCK) · airframe 8,012 hrs · 6,753 cycles
CREW REPORTED DURING CRUISE THAT THEY HEARD A LOUD POPPING NOISE FROM REAR OF ACFT. A RAPID DECOMPRESSION WAS FOLLOWED BY THE NOISE AND THE CREW DECLARED AN EMERGENCY PERFORMED AN EMERGENCY DECENT. DURING THE DECENT THE CABIN ALTITUDE. CONTINUED TO CLIMB TO A POINT WHERE THE O2 MASKS WERE DEPLOYED. THE ACFT LANDED SAFELY. MX INSPECTED THE ACFT AND FOUND THAT DUCT ON THE COALESCER SOCK WAS NOT SECURED.
Part: FLEX HOSE — CHAFED (ZONE 400)
DURING TAKE OFF, LT AND RT HYDRAULIC LEVEL LOW LIGHTS CAME ON CLIMBING THROUGH 5000 FT AND WITHIN TWO MINUTES LT AND RT HYD PRESSURE LOW LIGHTS CAME ON. HYD PRESS WENT TO 0 WITHIN 15 SEC RAN CHECKLISTS DECLARED AN EMERGENCY AND LANDING UNEVENTFULLY. LT ENGINE HYDRAULIC HOSE CHAFING. RECEIVED REPORTS OF AN IMPROPERLY CAMPED HYDRAULIC HOSE THAT CHAFE MAY LEAD TO HOSE DAMAGE AND HYDRAULIC LEAKS ON ENGINE NR 1.
Part: HOSE — MELTED (HYD SYSTEM) · airframe 7,853 hrs · 6,623 cycles
CREW REPORTED HYD LEVEL LOW ANNUNCIATOR ILLUMINANTED FOLLOWED BY LT PUMP PRESSURE LOW AND RT PUMP PRESSURE LOW ANNUNCIATOR. MX FOUND THE LT HYD PRESSURE HOSE IN CONTACT WITH THE BLEED AIR LINE, WHICH HAD MELTED THROUGH THE INSULATION OF THE HYD LINE. THE HYD PRESSURE HOSE LINE WAS REPLACED.
Part: BRAKE SYS — MALFUNCTIONED (MLG) · airframe 7,634 hrs · 6,443 cycles
CREW REPORTED DURING LANDING, NO BRAKING ACTION FOR APPROX 700FT AND THEN THEY OPERATED NORMAL. MX UNABLE TO DUPLICATE DISCREPANCY. BRAKING SYS WAS INSPECTED WITH A GROUND OPS CHECKED AND NO DEFECTS WERE FOUND. A MVF WAS PERFORMED AND PASSED.