N836VA
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.
18 reports on file, 2013-07-06 – 2023-04-05.
Part: DOOR SILL — CORRODED · corrosion level 2 · airframe 38,647 hrs · 12,689 cycles
SHAPE SILL CORRODED BEYOND LIMITS AT R2 DOOR. (REF G1724557 HAECO CARD 28057) GROUNDED - YES. NEW SHAPE SILL RECEIVED IAW A320 IPC 53-41-69-02-A, EA A320-53EA-01730. REPLACEMENT ACCOMPLISHED ON CUSTOMER CARD G1724552 (HAECO OPS 28052).
Part: FRAME — CORRODED · airframe 38,643 hrs · 12,686 cycles
FOUND CORROSION ON FR68 AT R2 DOOR GROUNDED - YES. ACCOMPLISHED ASA EA A320-53EA-01729 REV OO
Part: STRUCTURE — CORRODED · corrosion level 2 · airframe 38,643 hrs · 12,686 cycles
FOUND SHAPE SILL AND CORNER SILL CORRODED BEYOND LIMITS AT R2 DOOR GROUNDED - YES. RECEIVED NEW SHAPE SILL AND CORNER SILL IAW A320 IPC 53-41-69-02-1, EA A320-53EA-01730. REPLACEMENT ACCOMPLISHED ON CUSTOMER CARD G1724552 (HAECO OPS 28052) STEPS 013 & 015, 017
Part: UNKNOWN — CORRODED · airframe 38,643 hrs · 12,686 cycles
R2 DOOR SILL IS CORRODED AT AFT GIRT BAR FITTING GROUNDED - YES. REMOVED, LOCATED, DRILLED, INSTALLED NEW SILL, AND RESTORED COATINGS REF A320 SRM 51-43-11, 51-75-11, AND AIRBUS DWG D53480505
Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 38,643 hrs · 12,686 cycles
FLOOR BOARD SUPPORT STRUCTURE BEAM JUST AFT OF C66 @LBL35- UPPER SURFACE HAS CORROSION AROUND FIXTURE ATTACHMENT HOLE GROUNDED - YES. REMOVED AND REPLACED BEAM ASSY BTW C65-C67 Y919 IAW AIRBUS DWG # D53472812 REV A , A320 SRM 51-42-11, 51-72-11-911-001. T# 38349WW CAL DUE 19APR23
Part: WEB — CORRODED · corrosion level 2 · airframe 38,643 hrs · 12,686 cycles
SHEAR WEB BETWEEN FLOOR BEAM STA.C69LH - C70LH@LBL40. TOP SURFACE HAS CORROSION AROUND NUTCLIP HOLES GROUNDED - YES. REMOVED, LOCATED DRILLED, AND INSTALLED NEW SHEAR PLATE REF A320 SRM 51-42-11 AND AIRBUS DWG D53474180 REV V
Part: BEAM — GOUGED · airframe 38,643 hrs · 12,686 cycles
MAIN CABIN, LEFT AFT EMERGENCY EXIT DOOR, FRAME ABOVE WINDOW AND BELOW HANDLE HAS 2 EA NICKS ON LOWER SURFACE. ( STREAMER ATTACHED) GROUNDED - YES. REMOVED AND REINSTALLED HANDLE ASSY, ESCAPE SLIDE ASSY AND LOCKING MECHANISM IAW AIRBUS CMM 52-21-11 REMOVED AND REINSTALLED UPPER STRUCTURE IAW AIRBUS SRM 51-42-11 AND DWG D52279001 ISSUE AJ. AND DWG 15D52279037. LOCATED , DRILLED, DEBURRED, AND INSTALLED NEW FRAME IAW AIRBUS SRM 51-42-11. ALODINED PRIMED AND TOP COATED REPAIR AREA IAW AIRBUS SRM 51-21-11 AND 51-75-12 FLIGHT HOURS 38643 FLIGHT CYCLES 12686 WIEGHT VAR 010
Part: BEAM — GOUGED · airframe 38,643 hrs · 12,686 cycles
MAIN CABIN, LEFT FORWARD EMERGENCY EXIT DOOR, FRAME ABOVE WINDOW AND BELOW HANDLE HAS 2 EA NICKS ON LOWER SURFACE, (STREAMER ATTACHED) GROUNDED - YES. REMOVED AND REINSTALLED HANDLE ASSY, ESCAPE SLIDE ASSY AND LOCKING MECHANISM IAW AIRBUS CMM 52-21-11. REMOVED AND REINSTALLED UPPER STRUCTURE IAW AIRBUS SRM 51-42-11 AND DWG 15D52279037 AND DWG D52279001 ISSUE AJ. LOCATED, DRILLED, DEBURRED, AND INSTALLED NEW FRAME IAW AIRBUS SRM 52-42-11. ALODINED, PRIMED, AND TOP COATED REPAIR AREA IAW AIRBUS SRM 51-21-11 AND 51-75-12 SLIGHT HOURS 38643 FLIGHT CYCLES 12686 WEIGHT VAR 010.
Part: SKIN — DENTED · airframe 38,597 hrs · 12,666 cycles
LESSOR ITEM 2:FUSELAGE-TAIL CONE, MIDDLE, HAS 2 DENTS TO BE EVALUATED. GROUNDED - YES. MEASURED DENT 1 Y=.900, X=.900 DEPTH=.020 DENT LOCATION BETWEEN FR 83 TO FR 84, STR1 RH AND STR2 RH FOUND TO BE WITHIN LIMITS REF A320 SRM 53-51-11-283-024/53-00-11-283-005 THIS IS A CAT B DENT REINSPECT THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 60,000FC 120,000 FLT DVI DENT 2 FOUND TO BE OUT OF LIMITS DUE TO GOUGE IN DENT, REMOVED DAMAGE, FABRICATED, LOCATED, DRILLED, INSTALLED REPAIR AND RESTORED COATINGS REF A320 SRM 53-51-11-300-002 THIS IS A CAT A REPAIR NO FURTHER ACTION REQUIRED ON DENT 2 LOCATION BETWEEN FR 82 TO FR 83 STR1 LH STR 2 LH APPLIED YELLOW DENT DOT
Part: SKIN PANEL — DENTED · airframe 38,643 hrs · 12,686 cycles
LESSOR ITEM: RIGHT HAND AFT FUSELAGE ABOVE CABIN WINDOWS, DENT TO BE EVALUATED GROUNDED - YES. MEASURED DENT , FOUND TO BE OUT OF LIMITS DUE TO GOUGE IN DENT, REMOVED DAMAGE, FABRICATED, LOCATED, DRILLED, INSTALLED REPAIR AND RESTORED COATINGS REF A320 SRM 53-00-11-300-029 THIS IS A CAT B REPAIR REINSPECT THRESHOLD FROM TIME OF ADL / REPAIR EMBODIMENT 60,000 FC 120,000 FH REF A320 SRI 53-00-11-205-017 REPAIR LOCATION BETWEEN FR 54 TO FR55 AND STR 7R/H TO STR 8 R/H
Part: SKIN PANEL — DENTED · airframe 38,643 hrs · 12,686 cycles
LESSOR ITEM: L/H AFT FUSELAGE AT FWD VERTICAL FIN JUNCTION, DENT TO BE MEASURED GROUNDED - YES. ACCOMPLISHED DVI OF DENT, FOUND TO BE OUT OF LIMITS DUE TO GOUGE IN DENT. REMOVED DAMAGE, FABRICATED , LOCATED, DRILLED , INSTALLED REPAIR ANDRESTORED COATINGS REF A320 SRM 53-51-11-300-002 THIS IS A CAT A REPAIR NO FURTHER ACTION REQUIRED. REPAIR LOCATION BETWEEN STR 78 TO FR79 AND BETWEEN STR1 L/H TO STR 2 L/H
Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 38,647 hrs · 12,689 cycles
AFT WET AREA FLOOR BEAM CORRODED AT FR67 Y765 GROUNDED - YES. REMOVED AND REPLACED LONGITUDINAL BEAM ASSY BTW C66-C70 Y765, REMOVED AND REINSTALLED SPLICES (4EA) AND BRACKETS (2EA) IAW AIRBUS DWG #D53472780 REV. J A320 SRM 51-42-11, 51-72-11-911-001 T#T8349WW CAL DUE 19APR23
Part: SKIN PANEL — UNKNOWN · airframe 38,643 hrs · 12,686 cycles
WATER INDICATION WAS NOTED AT LH SIDE OF RUDDER AROUND HOISTING POINT #2. MARKED IN RED GROUNDED - YES. REMOVED WATER AND WATER DAMAGE TO RUTTER SKIN AND CORE AROUND #2 HOIST POINT.ON RUDDER LEFT HAND SIDE IAW A320-200 SRM 55-41-13-300-030-REV 143- 11/01/2022. A/C FLIGHT CYCLES: 12,866, A/C FLIGHT HOURS:38, 643;15, A/C WEIGHT VARIANT: WV010, A/C TYPE: A320-214, A/C S/N: 4480.
Part: WEB — CORRODED · airframe 38,643 hrs · 12,686 cycles
AFT WET AREA RIGHT HAND SHEAR PLATE CORRODED GROUNDED - YES. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SHEAR PLATE REF A320 SRM 51-42-11 AND DWG D53474180 ISSUE U
Part: SKIN PANEL — DENTED · airframe 38,643 hrs · 12,686 cycles
FOUND SCRATCH ON CROWN SKIN BETWEEN FR49 AND FR50 AND S3R TO S4R GROUNDED - YES. REMOVED DAMAGE, FABRICATED, LOCATED, DRILLED INSTALLED AND RESTORED COATINGS REF ASA EA A320-53EA-01726 REV 00
Earlier reports · 2013–2016 · 3 reports
2016
Part: DEU — FAILED · airframe 22,364 hrs · 6,674 cycles
SMOKE DETECTOR IN LAVATORY ACTIVATED WITH ERRATIC FAULT. AT FLIGHT ATTENDANT REPORTED A SMOKE ODOR. R & R THE DEU-B IAW AMM 23-73-473. TESTED OK IAW AMM 23-73-710-050-C.
Part: FAN — FAILED (CABIN) · airframe 19,367 hrs · 5,757 cycles
FLIGHT EXPERIENCED A VENT EXTRACT FAULT MESSAGE ON ECAM AND ELECTRICAL BURNING ODOR, THE FLIGHT CREW LANDED SAFELY. TSM 24-00-00-810-823-A AND 21-26-00-810-809A WERE FOLLOWED BY MAINTENANCE, EXTRACT FAN WAS FOUND FAILED AND DEFERRED IAW MEL 21-26-02-03. IT WAS REPLACED IAW AMM 21-26-51-401 ON THE OVERNIGHT VISIT.
2013
Part: STRUCTURE — DELAMINATED (HORIZONTAL STAB)
DURING THE WALK AROUND, DAMAGED SECTION OF L/E ON RT HORIZONTAL STABILIZER WAS DISCOVERED. OUT OF REPAIRABLE LIMITS. L/E PROTECTIVE COVERING WAS FOUND DELAMINATED DOWN ENTIRE LENGTH OF THE UPPER SURFACE. APPROX A 6 FT X 2 INCH SECTION MISSING. ACFT REMOVED FROM SERVICE AND THE L/E ASSY WAS REPLACED IAW AMM 55-12-11-04.