N842VA
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.
9 reports on file, 2013-06-28 – 2023-06-22.
Part: FLAP — DENTED (UNKNOWN) · airframe 36,068 hrs · 11,877 cycles
LESSOR ITEM 383: DENT DISCOVERED ON RIGHT HAND INBOARD FLAP TOP (UPPER SURFACE) GROUNDED - YES. CLEANED SANDED AND REPAIRED LESSOR ITEM 383, DENT ON RIGHT HAND INBOARD FLAP UPPER SURFACE 49" FROM INBD EDGE , 9" FROM T/E DIA 1" DEPTH .027, CATEGORY A POTTING PERMANENT REPAIR IAW A320-200 SRM 57-52-00-283-106, FC: 11877, FH 36068.57, WV=015
Part: FLOORBEAM — CORRODED (UNKNOWN) · airframe 36,068 hrs · 11,877 cycles
AFT WET AREA FLOOR BEAM CORRODION AT FR 67-68 Y-969 GROUNDED - YES. REMOVED AND REPLACED AFT WET AREA FLOOR BEAM AT FR 67-68 Y-969 IAW ASA A320 SRM 51-72-11 PER DWG D53472458 PO 1061646.1
Part: FLOORBEAM — CORRODED (UNKNOWN) · airframe 36,068 hrs · 11,877 cycles
AFT WET AREA FLOOR BEAM CORRODED AT FR68 Y-464.8 GROUNDED - YES. REPLACED NEW AFT WET AREA FLOOR BEAM AT FR68-Y-468.8 IAW A320 SRM 51-72-11 A SRM 51-42-11 AIRBUS DWG D53472780 REV -D P/N D5347219520600 PO: 1061646.1
Part: DOOR SILL — CORRODED (UNKNOWN) · corrosion level 2 · airframe 36,068 hrs · 11,877 cycles
R2 DOOR SILL CORRODED IN MULTIPLE PLACES GROUNDED - YES. REPAIRED R2 DOOR SILL IAW A320 SRM 53-41-14-300--001 REPAIR PRINCIPLE 5 AND 11. CATEGORY "A" REPAIR
Part: FLOORBEAM — CORRODED (UNKNOWN) · airframe 36,068 hrs · 11,877 cycles
AFT WET AREA FLOOR BEAM CORRODED AT FR 67-68 Y765 GROUNDED - YES. REMOVED AND REPLACED AFT WET AREA FLOOR BEAM AT FR 67-68 RECEIVED NEW PART 5347219220200 PO 10388742.1 LOCATED AND DRILLED PART IAW A320 SRM 51-44-11. INSTALLED PART IAW AIRBUS DWG 18D53472837 REV B.
Part: LIGHT — INOPERATIVE (O/W EXIT DOOR) · airframe 36,069 hrs · 11,877 cycles
LESSOR ITEM 19 - R/H FWD OVERWING EMERGENCY EXIT DOOR EXIT SIGN HAS ONE BULB BLOWN. HAECO DOT ATTACHED GROUNDED - YES. REMOVED AND REPLACED R/H FWD O/W EMERGENCY EXIT DOOR EXIT SIGN IAW A320 AMM 33-51-16-400-001-A, OPS CHECK GOOD, REMOVED HAECO DOT AND AMM 33-51-16-000-001-A PO:1061461.2
Part: SKIN — CORRODED (FRAMES 69-70) · corrosion level 2 · airframe 31,567 hrs · 9,831 cycles
SKIN CORRODED JUST FWD OF LAV WASTE VENT AT FUSELAGE R/H SIDE GROUNDED - YES. SKIN REPAIRED PER EA # A320-53EA-00851
Part: LINE — DETACHED (EVAC SLIDE) · airframe 21,353 hrs · 6,354 cycles
PROBLEM DURING REMOVAL OF THE L1 SLIDE S/N A12397. FOUND MOORING LINE DETACHED AND STUCK BETWEEN THE GIRT BAR AND THE DOOR DURING THE REMOVAL OF THE PACK ASSEMBLY, STEP 7 PAGE 10 AMM 25-66-44 PB 401, DOOR WILL NOT OPEN AFTER REMOVING THE GIRT BAR FROM L1 DOOR. FOUND ALSO CYLINDER DOOR DAMPER WITH LOW PRESSURE LESS THAN 400 PSI. GROUNDED - YES. WITH THE STRIKER LEVER DISCONNECTED AND SECURED A FINAL PUNCTURED OF THE DIAPHRAGM-SEALING OCCURS WHEN WE TRYING TO REMOVE THE JAM OF THE GIRT BAR AND THE MOORING LINE. NO DEPLOYMENT OF THE SLIDE OCCURS. THE NEW L1 SLIDE WAS INSTALLED AND TESTED.
Part: WIRE — CROSSED (EMERGENCY LIGHT)
WHILE PERFORMING A SCHEDULED TEST OF EMERGENCY GENERATOR SYS, NOTED THE EMERGENCY SIGN OVER AISLE AT ROW 17 DID NOT ILLUMINATE. TROUBLESHOOTING REVEALED THE LED LIGHT HAD BEEN CROSS-CONNECTED. WIRES PROPERLY POSITIONED IAW AMM 33-51-11-04 AND OPS CHECKED GOOD. T