N530VA
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.
19 reports on file, 2011-09-08 – 2020-02-18.
Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,013 hrs · 13,998 cycles
AT THE R-2 DOOR, FR. 68 RBL 50, JUST I/B OF THE GIRT BAR FITTING, THE FRAME HAS CORROSION ON THE UPPER SURFACE. GROUNDED - YES. REMOVED CORR ON EXISTING REPAIR, REMOVED REPAIR PARTS IAW A319 SRM 51-42-11FABBED IAW A319 SRM 51-74-00, LOCATED, DRILLED AND INSTALLED REPAIR PARTS IAW A319 SRM 53-41-14-300-001, REPAIR PRINCIPLE 5, ALODINED IAW A319 SRM 51-21-11 PRIMED IAW A319 51-21-11, PRIMED IAW A319 SRM 51-23-00, TOPCOAT IAW A319 51-75-12
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,421 hrs · 12,539 cycles
FRAME 66, RBL 50, JUST FWD OF THE GIRT BAR FITTING THE FRAME HAS CORROSION GROUNDED - YES. REMOVED CORROSION ORIG .150 REMAIN .050 LOSS OF .100. FOUND OUT OF LIMITS IAW A319 53-41-14. FABBED, LOCATED, DRILLED AND INSTALLED REPAIR PARTS IAW A319 SRM 53-41-14-300-001 REPAIR PRINCIPLE 9. HFEC INSP ACCOMPLISHED IAW AIRBUS NTM 51-10-08. DEFECTS FOUND. CLEAN AREA IAW A319 SRM 51-78-00 AND REINSPECTED AREA IAW NTM 51-10-08. NO DEFECTS FOUND. REMOVED AND REINSTALLED MOPSILL IAW A319 SRM 51-42-11. ALODINED IAW A319 SRM 51-21-11. PRIMED IAW A319 SRM 51-23-00 TOP COAT APPLIED IAW A319 SRM 51-23-00
Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,502 hrs · 12,526 cycles
AFT CABIN UNDERFLOOR COMPARTMENT BETWEEN STA. 68 AND 69 LONGITUDINAL BEAM -Y765 HAS CORROSION GROUNDED - YES. REMOVED CORROSION ORG. .150 REMAIN .115 LOSS OF .035. FOUND OUT OF LIMITS IAW A319 SRM 53-41-41. REMOVED AND REPLACE BEAM IAW AIRBUS DWG 53472093
Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,013 hrs · 13,998 cycles
AFT CABIN UNDERFLOOR COMPARTMENT WET AREA AT C66 LONGETUDINAL BEAM Y765 CORROSION GROUNDED - YES. REMOVED CORROSION ORIG. .150 REMAIN .115 LOSS OF .035 FOUND OUT OF LIMITS IAW A319 SRM 53-41-14. REMOVED AND REPLACED BEAM IAW A319 SRM 51-43-11 AND AIRBUS DWG D53472209
Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,013 hrs · 13,998 cycles
AFT CABIN UNDERFLOOR COMPARTMENT, IN WET AREA JUST AFT OF STATION 68 FRAME HAS SURFACE CORROSION GROUNDED - YES. REMOVED AND REPLACED BEAM # D53472197200 AT FRAME STA 68-70 Y765 IAW A319 SRM 51-42-11, 53-41-03-A, DWG 18-D5374-72040 & 51-22-00. REMOVED CORR ORG .150 REMAIN .100 LOSS OF .050. FOUND OUT OF LIMITS IAW A319 SRM 53-41-41.
Part: SKIN — DENTED (TE FLAP) · airframe 34,496 hrs · 12,522 cycles
L/H I/B FLAP IS DENTED ON LOWER SURFACE AT #2 FLAP TRACK. GROUNDED - YES. REPAIRED L/H I/B FLAP DENT ON LOWER SURFACE AT #2 FLAP TRACK IAW A319 SRM 57-52-00-300-015, 51-25-00 & EA #CMPT-57EA-00420 REV:00 REV DATE: 03/20/2020
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,809 hrs · 12,724 cycles
MAIN CABIN AFT R/H LAV FLOOR PAN DELAMINATED AFT EDGE. GROUNDED - YES. REPAIRED MAIN CABIN AFT R/H LAV FLOOR PANEL WITH DELAMINATION AT AFT EDGE IAW A319 SRM 53-02-00 TSK 53-02-00-300-01. REMVOED AND REINSTALLED AFT R/H LAV FLOOR PAN (LAV G) IAW DIEHL CMM 25-43-48. REMOVED AND REINSTALLED LAV G TOILET ASSY IAW A319 AMM 38-31-41. OPS CHECK GOOD.
Earlier reports · 2011–2018 · 12 reports
2018
Part: SWITCH — DEFECTIVE · airframe 34,115 hrs · 12,325 cycles
EMERGENCY LIGHTS ILLUMINATED IN ARM POSITION GROUNDED - YES. REMOVED + REPLACED EMERGENCY LIGHT TOGGLE SWITCH IAW ESPM 20-45-21. OPS CHECK GOOD IAW AMM 33-51-00
2017
Part: SWITCH — FAILED (EMERGENCY LIGHTS)
EMERGENCY LIGHTS ON WITH SWITCH OFF. REMOVED AND REPLACED THE SWITCH. OPS CHECKED GOOD IAW ESPM 20-45-21 AND AMM33-50-00.
2016
Part: UNKNOWN — SMOKE (AFT CABIN)
SMOKE ODOR IN BOTH REAR LAVS. ACCOMPLISH BITE TEST FOR BOTH LAV SMOKE DETECTOR TEST. TEST PASS, NO FAULT NOTED. ACCOMPLISHED OPS TEST OF LAV FLUSH SYSTEM NO ABNORMAL NOISE NOTED, ACCOMPLISHED WALK AROUND ACFT NO SIGN OF ANY KIND OF LEAK OK FOR SERVICE.
2014
Part: DOOR SILL — CORRODED (FRAMES 66-68)
RIGHT AFT PASSENGER DOOR SILL BETWEEN FRAMES 66-68 HAS AN AREA OF CORROSION BEYOND LIMITS. DOOR SILL REPAIRED IAW SRM 53-41-14, FIG 201 VIEW K, PRINCIPLE 5.
Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70)
CABIN FLOOR SUPPORT BETWEEN FRAME 66-70 AT Y65 HAS CORROSION BEYOND LIMITS. FLOORB SUPPORT REPLACED IAW SRM 51-42-11.
Part: SHEAR PLATE — CORRODED (FRAMES 69-70)
RIGHT AFT SHEAR PLATE BETWEEN FRAMES 69-70, S23-24R, HAS CORROSION BEYOND LIMITS. SHEAR PLATE WAS R & R IAW SRM 51-42-11.
Part: SEAT TRACK — CORRODED (FRAMES 64-66)
CABIN SEAT TRACK BETWEEN FRAMES 64-66 AT Y765 HAS CORROSION BEYOND LIMITS. SEAT TRACK WAS REPLACED IAW SRM 51-42-11.
Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66)
CABIN FLOOR SUPPORT BETWEEN FRAMES 64-66 AT Y1292 HAS CORROSION BEYOND LIMITS. FLOOR SUPPORT WAS REPLACED IAW SRM 51-42-11.
Part: SEAT TRACK — CORRODED (FRAMES 64-66)
CABIN SEAT TRACK BETWEEN FRAMES 64-66 AT Y1292 HAS CORROSION BEYOND LIMITS. SEAT TRACK REPLACED IAW SRM 51-42-11.
2013
Part: SWIVEL — BROKEN (HYD LINE) · airframe 19,400 hrs · 21,700 cycles
DURING CLIMBOUT AND GEAR RETRACTION, ACFT LOST GREEN SYS FLUID. LANDING GEAR WAS EXTENDED BY THE NORMAL SYS BUT GEAR DOORS REMAINED OPEN. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED AND TAXIED BACK TO THE GATE WITHOUT INCIDENT. DURING INSPECTION, THE RT MAIN GEAR SIDE STAY ACTUATOR SUPPLY LINE SWIVEL WAS FOUND BROKEN. THE LINE WAS REPALCED, THE GREEN HYD SYS WAS SERVICE AND ALL REQUIRED INSPECTIONS WERE ACCOMPLISHED. THE ACFT DEPARTED WITHOUT FURTHER INCIDENT.
Part: PROXIMITY SENSOR — FAULTED (CARGO DOOR) · airframe 19,185 hrs · 6,144 cycles
DURING CLIMB, AFT CARGO DOOR OPEN WARNING WAS DISPLAYED ON ECAM NO CABIN PRESSURE ABNORMALITIES WERE NOTED AND ACFT DEPARTED. ON ARRIVAL, AIRCRAFT WAS INSPECTED AND IT WAS DETERMINED THAT THE AFT CARGO DOOR SENSOR 32WV WAS AT FAULT. FAULTY SENSOR REPLACED, NO FURTHER ISSUES NOTED.
2011
Part: ENGINE — FAILED (NR 2)
APPROX 1 HR INTO FLIGHT, CLIMBING FROM FL 350 TO 370, CREW NOTED A LOSS OF N1 AND N2 WITH ASSOCIATED ECAM ENG 2 FAIL, STALL AND SENSOR FAULT WARNINGS. RECEIVED AN ENG 2 SHUTDOWN WARNING. ACARS TRANSMISSION TO THE DISPATCHER WAS SENT STATING ENG FAILURE - PLANNING GJT LANDING. MADE AN UNEVENTFUL LANDING AFTER DECLARING AN EMERGENCY. CREW DID A WALK AROUND AFTER LANDING AND CONFIRMED ENGINE FAILURE BY NOTING TURBINE SECTION DEBRIS IN THE TAIL PIPE. MC COORDINATED AN ENG CHANGE WITH THE LINE MX MANAGERS PROVIDING PERSONNEL. THE ENGINE CHANGE WAS COMPLETE AT 1500Z ON 9/12/2011. FOLLOW UP INFO FROM THE ENGINE O/H SHOP FINDINGS WILL BE FORTHCOMING WHEN THE INFO COMES AVAILABLE AS A SUPPLEMENT TO THIS SDR.