N546JB
Registered owner: JENNIFER BUTLER LLC, CA (owner ≠ operator)
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, 2003-10-27 – 2008-05-11.
Part: VALVE — LEAKING (BLEED AIR) · airframe 24,090 hrs · 8,605 cycles
FLT NR 303, IAD-FLL, AIR ENG 1 BLEED ABNORMAL PRESSURE (SUBSEQUENT PACK 1/PACK 2-FAULT). FOUND AIR LEAK ON PRESSURE REG VALVE CLAMP JOINT. CLAMP WAS REMOVED AND JOINT RE-ALIGNED WITH VALVE. NO FURTHER AIR LEAK NOTED FAN AIR VALVE THERMOSTAT SEAL WAS REPLACED TO CORRECT AIR LEAKAGE AS PER AMM REF 36-11-43. NO FURTHER LEAKS NOTED. POWER ASSURANCE TEST ACCOMPLISHED AT 1.25 EPR. ENG NR 1 & 2 BLEED AND NACELLE TEMP PARAMETERS EXAMINED. NO DEFECTS NOTED. PARAMETERS WITHIN LIMITS. BLEED SYS 1 & 2 CHECKED BY ALTERNATE SYSTEMS. BLEED NR 1 NR 2 SYSTEMS OPERATE AS DESIGNED PER AMM REF 71-00-00-710-013A & REF 36-11-00-710-001.
Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 21,581 hrs · 7,725 cycles
ECAM VENT SKIN VALVE FAULT SHORTLY AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE. CYCLED TO BURN FUEL AND AIRCRAFT LANDED AT 141,000 LBS. PERFORMED BITE TEST OF AEVC. PFR & BITE SHOWED SKIN AIR OUTLET VALVE FAULT. REMOVED AND REPLACED SKIN AIR VALVE (OUTLET) PER AMM 21-26-53-04, NO FURTHER FAULTS, OPS CHECK NORMAL.
Part: VIDEO DISPLAY — ODOR (SEAT 23D) · airframe 15,400 hrs · 5,536 cycles
SEAT 23D VDU WAS VERY HOT AND HAD A PLASTIC BURNING ODOR. THE MASTER SWITCH FOR LIVE TV WAS TURNED OFF. PERFORMED TASK 23-39-00-810-801. REMOVED AND REPLACED VDU IAW LTV AMM 23-39-00. ALL OPS CHECK OK.
Part: BLEED VALVE — FAILED (NR 1 ENGINE) · airframe 13,991 hrs · 5,026 cycles
AFTER TAKEOFF EN ROUTE TO LGB EXPERIENCED NR 1 ENGINE STALL WITH FULL RECOVERY. A/C AT 11,000 FEET AND 300 KTS. RETURNED TO JFK. PERFORMED TSM TASK 71-00-810-808. CHECKED 7A, 7B, 7C BLEED VALVE AND SOLENOID REF AMM 75-32-52. FOUND 7B VALVE FAILED. REPLACED BLEED VALVE 7B REF AMM 75-32-52. OPS CHECK OK. PERFORMED VSV LUBE REF AMM 75-32-42. CHECKED 2.5 BLEED ACT 4021KS LVDT AND TORQUE MOTOR AND CHAN A & B. REF TSM 75-30-00-810-856 CKS OK. BOROSCOPE PERFORMED NO FINDINGS. PERFORMED HIGH POWER ASSURANCE TEST AS PER AMM 71-00-00. OPS CHECK OK.
Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 4,705 hrs · 1,800 cycles
EPSU INT EMERGENCY RT FAULT ON EMERGENCY LIGHTS TEST. REMOVED AND REPLACED RT EPSU IAW AMM 33-51-38, OPS CHECK GOOD.