N703AV
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Avianca | Operator | on 2020-01-23 | 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.
2 reports on file, 2020-01-23 – 2020-02-26.
Part: SWITCH — MALFUNCTIONED (HYD SYSTEM) · airframe 22,006 hrs · 8,937 cycles
AFTER TAKE OFF FROM SAL TO TGU THE AIRCRAFT RETURNED TO SAL DUE TO THE ECAM SHOWED HYDRAULIC YELLOW RESERVOIR LOW LEVEL FOLLOWED BY HYDRAULIC YELLOW ENGINE 2 PUMP LOW PRESSURE THE ENGINE 2 DRIVEN PUMP WAS SHUTDOWN AFTER 1 MINUTE OF OPERATION. NO OVERWEIGHT LANDING ACTUAL LANDING WEIGHT 59600 KG. FOLLOWING TSM 29-13-00-810-801-A WAS REMOVED AND REPLACED LOW LEVEL SWITCH AS PER AMM 29-13-41-000-004 AND AMM 29-13-41-400-004 AND QUANTITY INDICATOR AS PER AMM 29-13-41-000-003 AND AMM 29-13-41-400-003 PERFORMED OPERATIONAL TEST OF THE FLUID LOW LEVEL WARNING SYSTEM IAW AMM 29-31-00-710-001. SYSTEM OK NORMAL FOLLOWING TSM 05-50-00-810-802 AND AMM 05-51-11-200-004 WAS PERFORMED FDR READOUT AND NO HARDOVERWEIGHT LANDING CONDITION WERE FOUND. ALSO WAS REPLACED PCMCIA AS PER AMM 31-36-00-000-001-A AND AMM 31-36-00-400-001-A THE AIRCRAFT RETURNED TO NORMAL OPERATION.
Part: FLT CONTROLS — MALFUNCTIONED · airframe 21,864 hrs · 8,879 cycles
DURING FLIGHT FROM SJO TO BOG THE AIRCRAFT DIVERTED TO PTY DUE TO ECAM WARNING LOST OF FLIGHT CONTROLS AT FL 370 DUE TO AIRBUS REFERENCE : 80742128/008 ACTION: PERFORMED AFS TEST IN ACCORDANCE WITH AMM TASK 22-96-00-710-001-A, TEST OK. DUE TO PFR AUTO FLT A/THR OFF. ACTION: AS PER TSM 22-31-00-810-816-A, PERFORMED CHECK IN ACCORDANCE WITH TSM SUBTASK 22-31-00-710-079-A, IT IS NOT RELATED WITH ANY FAILURE MESSAGE OR WARNING, CHECK OK. NO MAINTENANCE ACTION IS NECESSARY. DUE TO AUTO FLT AP OFF. ACTION: AS PER TSM 31-53-00-810-974-A, PERFORMED TEST IN ACCORDANCE WITH TSM SUBTASK 31-53-00-700-058-A, TEST OK. NO FAULTS PRESENT. DUE TO HYD B RSVR LO LVL. ACTION: AS PER TSM 29-12-00-810-803-A, PERFORMED CHECK IN ACCORDANCE WITH TSM SUBTASK 29-12-00-860-052-A, CHECK OK. NO FAULTS PRESENT.DUE TO HYD G RSVR LO LVL AND DUE TO HYD Y RSVR LO LVL.ACTION: AS PER TSM 29-11-00-810-803-A, PERFORMED CHECK IN ACCORDANCE WITH TSM SUBTASK 29-11-00-860-050-A, CHECK OK. NO FAULTS PRESENT. DUE TO AIRBUS REFERENCE : 80742128/010 ACTION: PERFORMED INSPECTION AFTER IN-FLIGHT EXCESSIVE LOAD FACTOR DUE TO TURBULENCE OR MANEUVER IN ACCORDANCE WITH AMM TASK 05-51-17-200-001-A, PHASE 1 COMPLETED AND NO DISCREPANCIES FOUND. CHECK OK. DUE TO AIRBUS REFERENCE : 80742128/015 ACTION: PERFORMED INSPECTION CHECK FOR FLUID LEVEL QUANTITY IN ACCORDANCE WITH AMM 29-10-00-200-001-A, CHECK OK. AND CHECK FOR AIR AS PER AMM 29-00-00-210-001-A, CHECK OK. NO DISCREPANCIES FOUND. DUE TO AIRBUS REFERENCE : 80742128/020 ACTION: PERFORMED INSPECTION AFTER AIRCRAFT OPERATION WITH HIGH LATERAL ACCELERATION IN ACCORDANCE WITH AMM 05-51-44-200-001-A. PHASE 1 COMPLETED AND NO DISCREPANCIES FOUND. CHECK OK. AND BETWEEN FR70 AND FR74 ABOVE STRINGERS 19LH AND 19RH IN ACCORDANCE WITH AMM TASK 53-51-00-210-020, NO DISCREPANCIES FOUND. CHECK OK.DUE TO ENGINEERING REQUEST MESSAGE ACTION: PERFORMED TSM 79-33-00-810-830-A âOIL PRESSURE LESS THAN 80 PSI ON ENGINE 1â. PERFORMED INSPECTION OF THE MAGNETIC CHIP DETECTORS IN ACORANCE WITH AMM 79-00-00-200-011, CHECK OK. AND INSPECTION OF THE FINE SCAVENGE AND PRESSURE FILTERS IN ACCORDANCE WITH AMM 79-00-00-200-012. CHECK OK. DUE TO ENGINEERING REQUEST MESSAGE ACTION: PERFORMED TSM 79-33-00-810-820-A âOIL LOW PRESSURE WARNING WITH OIL PRESSURE INDICATION LESS THAN 60 PSI ON ENGINE 1â PERFORMED CHECK IN ACCORDANCE WITH TSM SUBTASK 79-33-00-810-072-A, CHECK OK. NO LEAKS FOUND. NO DEBRIS FOUND. DUE TO ENGINEERING MESSAGE OF A320 ENGINE MECH ADV REPORT <07> ENG 1 OIL PRESSURE LOW ACTION: PERFORMED R/R OF THE ENG 1 OIL PRESSURE PUMP IN ACCORDANCE WITH AMM 79-21-41-000-010 AND REF. AMM 79-21-41-400-010. PERFORMED IDLE LEAK CHECK IN ACCORDANCE WITH AMM TASK 71-00-00-710-012, CHECK OK. IAW AIBUS REFERENCE 80742128035 INFORMED THAT THE FINAL LOADS ANALYSIS HAS BEEN SUCCESSFULLY PERFORMED BY OUR SPECIALISTS.ACCORDING TO THE RESULTS, NO LOADS EXCEEDANCE ABOVE THE LIMIT LOADS HAS BEEN EXPERIENCED BY ANY OF THE AIRFRAME COMPONENTS. CONSEQUENTLY, CONSIDERING THAT ALL PRELIMINARY INSPECTIONS WERE PERFORMED WITH NIL FINDINGS AS PER REPORT REF. 80742128/028, NO ADDITIONAL INSPECTION IS REQUESTED. AS PER ABOVE STATEMENT, WE THEREFORE CONFIRM THAT THE AIRCRAFT CAN BE RELEASED TO SERVICE ON A PERMANENT BASIS WITH NO FURTHER ACTIONâ. THE AIRCRAFT RETURN TO SERVICE NORMAL.