N411AV
Registered owner: AIRCOL 9, DE (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Avianca | Operator | on 2024-11-16 | 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.
5 reports on file, 2011-10-14 – 2025-08-11.
Part: FILTER — CLOGGED (FUEL SYS) · airframe 37,537 hrs · 35,392 cycles
ENG 2 FUEL FILTER CLOG AFTER T/O ON ECAM. FROM TSM 73-00-00-810-976-A STEP 4.A (A) (B) THE FUEL FILTER ELEMENT WAS REMOVED AND REPLACED IAW AMM 73-11-10-000-004-A/400-004-A. AND IDLE CHECK WAS PERFORMED WITHOUT LEAKS IAW AMM 71-00-00-710-006.
Part: COMPUTER — MALFUNCTIONED (ELAC) · airframe 21,341 hrs · 20,415 cycles
HIGH VIBRATION ON INITIAL CLIMB, LT & RT AILERON FAULTS ON ECAM. DURING TAKEOFF ROLL THE VIBRATION WAS FELT ON THE NOSE GEAR. LT AND RT NWA WERE REPLACED IAW AMM 27-93-34, PB 401, ELAC 2CE1 WAS REPLACED IAW AMM 27-93-00-710A. OPS TESTED SATISFACTORY.
Part: FAN — MALFUNCTIONED (E&E BAY) · airframe 1,527,542 hrs · 14,179 cycles
ELECTRICAL SHORT CIRCUIT SMELL WAS FELT BEFORE TAKEOFF AT GND, RETURN WAS DONE. IAW AMM 21-26-51 PB 401 THE BLOWER FAN WAS REPLACED IAW ESPM 20-46-10 THE CB 1HQ AVNCS VENT BLOWER FAN WAS REPLACED & IAW ESPM 20-44-11 THE CONNECTOR 20 HQA WAS REPLACED. IAW AMM 24-51-55 P 401 THE CONTACTOR 8HQ BLOWER FAN CTL AVCNS VENT WAS R & R IAW AMM 21-26-00-710-001-A. OPERATIONAL CHECK OF THE AVIONICS EQUIP VENTILATION SYS VIA MCDU WAS PERFORMED WITH SATISFACTORY RESULTS. PN EVT3454HC SN OFF 164900864 SN ON 164903466.
Part: CONTROL UNIT — MALFUNCTIONED (ZONE 700) · airframe 1,072,651 hrs · 9,427 cycles
WHEN SELECTING THE L/G DOWN AND FLAPS 3, ECAM WARNING BRAKES NORMAL BRAKE SYS FAULT CAME ON AFTER APPLYING THE LANDING DISTANCE PROCEDURE, WE DECIDED TO COME BACK TO DEPARTURE. THE ANTI-SKID N/W STRG SW WAS RESET SUCCESSFULLY IAW AMM 32-43-34-000-001A AND 32-43-34-400 001A THE ABCU WAS R & R IAW AMM 32-43-00-710-002A OPS CHECK TO START FUNCTIONAL TEST OF ALTERNATE BRAKING WAS ACCOMPLISHED.
Part: UNKNOWN — MALFUNCTIONED (RT ENGINE) · airframe 5,815 hrs · 5,024 cycles
AFTER T/O THRUST WAS APPLIED AT 50 PERCENT POWER SET, POWER DROP TO 21.1 PERCENT ON RIGHT ENGINE, AIRCRAFT TURN TO THE RIGHT, REJECTED T/O WAS EXCECUTED. IAW TSM 77-00-00-810-852, OPERATIONAL TEST OF THE FADEC ON GROUND WITH ENGINE NON-MOTORING PERFORMED, IAW AMM 73-21-50-210-002, VISUALLY CHECK OF J9/J10 HARNESS CONNECTORS WERE PERFORMED SATISFACTORY, AND IAW AMM 71-00-00-710-025 ACELERATION CHECK OF ENGINE 2 PERFORMED SATISFACTORY.