N557AV
Registered owner: UMB BANK NA TRUSTEE, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Aerovías del Continente Americano AVIANCA | Operator | on 2020-12-31 | 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, 2016-01-23 – 2026-01-26.
Part: ENGINE — VIBRATION (NR 1) · airframe 39,011 hrs · 21,815 cycles
NR 1 ENGINE HIGH VIBRATION DURING TAKEOFF BEFORE 80 KTS. SECOND TIME IAW TSM 77-00-00-810-864-A, CHECKED WIRING, CONNECTORS, & RECEPTACLES BTWN THE NR 1 VIBRATION SENSOR (4002EV) TO EVMU (2EV) THE TRF VIBRATION SENSOR (4003EV) TO THE EVMU (2EV) IAW ASM 77-32-02, CHECK FOR DAMAGED PINS OR CONNECTOR OXIDATION PERFORMED. NO DAMAGE FOUND IAW 77-32-34-710-040-B OPS CHK OF EVMU THROUGH CFDS FOR ADVISORY INDICATION ON ECAM PERFORMED, TESTED OK IAW 72-21-00-210-009-A. INSPECTION OF FAN ROTOR BLADES, NO DAMAGE FOUND. Â IAW 79-00-00-281-002-A CHKD THE ELECT MASTER CHIP DETECTOR (EMCD) FOR PARTICLES PERFORMED, NO PARTICLES FOUND. IAW 72-21-00-290-003-A BORESCOPE INSP OF BOOSTER ROTOR BLADES, STAGES 2, 3, 4, & 5 THROUGH THE BOOSTER INLET & BORESCOPE PORTS SO3 & SO5 PERFORMED, NO DAMAGE FOUND. IAW 72-54-00-290-006-A INSP OF LPT STAGE 4 BLADES PERFORMED, NO DAMAGE FOUND. IAW AMM Â 31-36-00-710-016-A, DOWNLOADED PROCEDURE OF THE FDIMU/DMU DATA ON A PCMCIA CARD PERFORMED. FOLLOWING TSM 77-00-00-810-864-A, STEP 4. A. (1) (D), NR 1 ENG ACCELEROMETER SWITCH MODE TO TRF CONFIG PERFORMED. IAW AMM 71-00-00-710-003-B, ENGINE AUTOMATIC START PERFORMED & N1 INDICATION VIBRATION CHECKED FROM IDLE TO TO/GA THE VIBRATION VALUES FOUND WITHIN LIMITS.
Part: ECU — FAULTED (ENGINE) · airframe 34,864 hrs · 18,563 cycles
DURING TAKE OFF ABOVE 100 KNOTS DUE TO MASTER CAUTION ALERT THR LEVERS FAULT. IAW AMM 73-29-00-710-040-B02 REV. 65 DATE: 01.AUG.2023 OPERATIONAL TEST OF THE FADEC 1 AND 2 CHANELS A/B ON THE GROUND WITH ENGS NON MOTORING WAS PERFORMED SATISFACTORY. NO FAULTS RECORDED. IAW AMM 32-46-00740.001-A REV.65 DATE: 01.AUG.2023 BITE TEST OF THE BSCU 1 AND 2 WAS PERFORMED SATISFACTORY. NO FAULTS DETECTED. IAW TSM 05-50-00-810-825-A REV. DATE: 01.AUG.2023 VISUAL INSPECTION OF THE BRAKES BY BRAKE EMERGENCY APPLICATION AND OVERHEAT WAS PERFORMED SATISFACTORY. BRAKES AND WHEELS WERE FOUND OK
Part: UNKNOWN — ODOR (CARGO BAY) · airframe 21,748 hrs · 11,661 cycles
FISH SMELL IN AFT CARGO COMPARTMENT.
Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 15,091 hrs · 7,501 cycles
AFTER TAKEOFF VENT SKIN VLV FAULT, MAN V/S CTL USED UNSATISFACTORY. IAW AMM 21-26-53-00-002A 400-003-A THE SKIN OUTLET VLV WAS R & R. OPERATIONAL TESTED SATISFACTORY, PN BFT300B00
Part: STARTER — MALFUNCTIONED (NR 1 ENGINE) · airframe 1,415,802 hrs · 7,022 cycles
ENGINE 1 FAULT DURING THE START SEQUENCE. IAW AMM 80-11-10 PB 401 THE STARTER MOTOR IN ENG NR 1 WAS R & R. ENG AUTOMATIC START WAS PERFORMED & TESTED SATISFACTORY. PN 3505582-2, SN OFF SYG440526-B & SN ON SAV-1-012.