N635VA
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, 2013-07-25 – 2020-02-23.
Part: SPAR — CRACKED (LT PYLON) · airframe 43,135 hrs · 13,350 cycles
#1 ENGINE AFT FIXED FAIRING UPPER INBD SPAR HAS VISUAL CRACK INDICATION IN RADIUS @RIB 11 GROUNDED - YES. ACCOMP. HFEC OF SUPPECTED CRACK IAW A320 NTM 51-10-08, CRACK NOTED APPROX .25" IN LENGTH, REMOVED AND REINSTALLED PNLS 475BR, 475BL, AND 477AL TO F.O.M. IAW A320 AMM 54-53-11, REMOVED AND REINSTALLED AFT MOVABLE FAIRING IAW A320 AMM 54-55-00, REMOVED AND REINSTALLED AFT LOWER FAIRING PER A320 AMM 54-56-0, REMOVED AND REINSTALLED UPPER FWD. FITTING ON AFT FIXED FAIRING PER A320 AMM 20-21-11, REMOVED AND REINSTALLED AFT FIXED FAIRING IAW A320 AMM 54-54-00, REPAIRED AFT FIXED FAIRING UPPER I/B SPAR IAW A320 SRM 54-54-12-C1 REPAIR, REPAIR ANGLE P/N R5451205220400 P/O# 0, AFT MOVABLE FAIRING GAP CHECK GOOD.
Part: DOOR SILL — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 36,295 hrs · 11,275 cycles
MAIN CABIN, DOOR SILL CORRODED BETWEEN FR67 AND FR69 APPROX. -Y1250. MARKED GROUNDED - YES. REMOVED DOOR SILL TOP 3 PLATES, DOOR SILL, 4EA. DOOR SILL SPLICES AT FR.66, PLATE & SUPPORT AT FR.68-69, DRAIN LINES 2 EA AT FR.66 PER A320 SRM 51-42-11 AND A320 AMM 38-30-00. DRILLED, LOCATED NEW DOOR SILL PER A320 SRM 51-44-00 AND AIRBUS DWG #D53480505. INSTALLED DOOR SILL, DOOR SILL TOP PLATES (3EA), 4EA DOOR SILL SPLICES AT FR.66, PLATE AND SUPPORT AT FR.68-69 PER AIRBUS DWG #D53480505 AND RECONNECTED 2EA DRAIN LINES AT FR.66 PER A320 AMM 38-30-00-410-003-A.PART REPLACED DUE TO BEING OUT OF LIMITS P.O #964635.3
Part: FLOOR PANEL — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 43,136 hrs · 13,350 cycles
MAIN CABIN FLOOR PANEL HAS CORROSION: 262LG R2 FLOOR PNL: P/N: E5367180502500 GROUNDED - YES. REMOVED CORROSION DAMAGE AND REPAIRED IAW EA# A320-53EA-00355 REV 00. ORIGINAL THICKNESS OF UPPER SKIN .063" LENGTH OF DAMAGE IS 38.5" AND WIDTH OF DAMAGE IS 3" WITH NO REMAINING MATERIAL THICKNESS AND LOWER SKIN .024" LENGTH OF DAMAGE IS 18" AND WIDTH IS 3" WITH NO REMAINING MATERIAL THICKNESS. THE REPAIR ACCOMPLISHED PER MIG-70 EA A32053EA-00355 IS TEMPORARY FOR 24 MONTHS WITH ONE TIME INSPECTION REQUIRED AFTER 1 YEAR STARTING 19FEB2020. CAT C REPAIR
Part: SUPPORT — CORRODED (FRAMES 69-70) · corrosion level 2 · airframe 43,136 hrs · 13,350 cycles
MAIN CABIN FLOOR STRUCTURE, 304 FRAME SUPPORT CORRODED BETWEEN FR69 AND FR70 AND STRINGER 22RH AND 24RH. GROUNDED - YES. REMOVED SHEAR PLATE SUPPORT PER A320 SRM 51-42-11, INSTALLED NEW SHEARPLATE SUPPORT IAW A3200 SRM 51-42-11
Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · corrosion level 2 · airframe 43,136 hrs · 13,350 cycles
MAIN CABIN FLOOR STRUCTURE, LONGITUDINAL BEAM CORRODED AT FR68 APPROX. -Y780. MARKED GROUNDED - YES. LONGITUDINAL BEAM IS BEYOND MAX ALLOWABLE LIMITS OF .016 PER A320 SRM 53-41-14, REMOVED BEAM PER A320 SRM 51-42-11, LOCATED DRILLED AND DEBURRED NEW BEAM PART #D5347219320200 P.O. 964566.1 IAW A320 SRM 51-44-11 AND AIRBUS DWG D534727 80, INSTALLED ATTACH BRACKETS AND FITTINGS AND NEW BEAM IAW A320 SRM 51-42-11 AND DWG. D53472780
Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,135 hrs · 13,350 cycles
MAIN CABIN FLOOR STRUCTURE, SHEAR PLATE CORRODED BETWEEN FR69 AND FR70 AND STRINGER 22LH AND 24LH. GROUNDED - YES. DISPLACED VOR COAX CABLE AND REINSTALLED VOR COAX CABLE IAW A320 AMM 34-55-11 AND ESPM 20-33-11 REMOVED AND REPLACED SHEAR PLATE IAW A320 SRM 51-42-11 AND DWG. 53474180004. NO LIMITS AVAILABLE FOR SHEAR PLATE.
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 43,136 hrs · 13,350 cycles
MAIN CABIN FLOOR PANEL DELAMINATED: 231MF GROUNDED - YES. REPAIRED DELAMINATED MAIN CABIN FLOOR PANEL 231MF OIAW A320 SRM 53-02-00-300-013, A320 SRM 51-77-11 & AIPC 53-22-02-01G, AND EA A320-53EA-00320
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 43,136 hrs · 13,350 cycles
MAIN CABIN FLOOR PANEL DELAMINATED: 231SF GROUNDED - YES. REPAIRED DELAMINATED MAIN CABIN FLOOR PANEL 231SF IAW A320 SRM 53-02-00-300-013, A320 SRM 51-77-11 & AIPC 53-22-02-01G AND EA A320-53EA-00319.
Part: FLOOR SUPPORT — CORRODED (FRAMES 67-70) · corrosion level 2 · airframe 43,136 hrs · 13,350 cycles
MAIN CABIN FLOOR STRUCTURE, LONGITUDINAL BEAM CORRODED BETWEEN FR69 AND FR70 APPROX. +Y180. MARKED GROUNDED - YES. REMOVED FLOOR BEAM PER A320 SRM 51-42-11, LOCATED AND DRILLED NEW FLOOR BEAM PER A320 SRM 51-44-11, INSTALLED FLOOR BEAM BETWEEN FR. 69-70 IAW A320 SRM 51-42-11 AND AIRBUS DWG. #E53474250
Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,135 hrs · 13,350 cycles
MAIN CABIN FLOOR STRUCTURE , SHEAR PLATE CORRODED BETWEEN FR69 AND FR70 AND STRINGER 22RH AND 24RH GROUNDED - YES. DISPLACED VACUUM BEN WIRES BETWEEN FRAME 69-70 RH AND REINSTALLED VAC. GENE WIRES IAW A320 AMM 38-31-64, OPS CHECK VACUUM GEN. WIRES IS GOOD IAW A320 AMM 38-31-64 AND A320 AMM 38-31-00-790-003 REMVOED AND REPLACED SHEAR PLATE IAW A320 51-42-11 AND DWG D5347418004, PART # D5347112420300 PO# 952453 SRM HAS NO ALLOWABLE LIMITS FOR SHEAR PLATE
Part: FLOORBOARD — PUNCTURED (FRAMES 31-34) · airframe 43,135 hrs · 13,350 cycles
(PARTS RACK) FWD PIT PANEL 131HF IS PUNCTURED. GROUNDED-YES. REPAR PANEL 131HF PUNCTURED IAW A320 SRM 53-02-00-283-001 AND 53-02-00-300-002
Part: PANEL — DELAMINATED (AFT CARGO) · airframe 43,135 hrs · 13,350 cycles
AFT PIT PANEL 152NF IS DAMAGED. GROUNDED - YES. REPAIRED PANEL 152NF IAW A320 SRM 53-02-00-283-001, 53-02-00-300-004, 51-77-11-91-031
Earlier reports · 2013–2019 · 7 reports
2019
Part: FAN — MALFUNCTIONED (E&E BAY) · airframe 41,144 hrs · 12,542 cycles
FA(S) REPORTED INTENSE BURNT PLASTIC SMELL ROWS 29-32 GASPER VENTS.ALSO INTENSE BURNT PLASTIC SMELL AFT GALLEY A/C WAS CHECKED FOR ANY MALFUCTIONING ELECTRONIC DEVICES, NONE FOUND. B/C FLIGHT ATTENDANT REPORTED ILL FEELING FROM FUMES. FAINT SMELL DETECTABLE FROM FLIGHT DECK. UNKNOWN IF INTENSIFIED AS PILOTS WERE ON O2 MASKS. NR 1 PACK AND NR 1 ENG BLEED FAULTED SHORTLY AFTER LANDING UNKNOWN IF ASSOCIATED SMELL DISSIPATED AFTER ALL PACKS AND ENG BLEEDS WERE SELECTED OFF. GROUNDED - YES. REF RMA 2962 AND ALL T/S FOR CORRECTIVE ACTIONS + LP 1231156 ITEM 1 & 2 R & R AVIONICS FILTER AND OPS CHK GOOD PER AMM 21-25-43. ACCOMPLISHED VISUAL INSPECTION OF APU INLET PLENUM AND APU AIR INTAKE, NO CONTAMINATION FOUND. INSPECTED BALLAST 29-32 NO DEFECTS NOTED, INSPECTED IFE SYS CLUSTER FANS OPS CHECK GOOD INSPECTED PSU FOR AFFECTED ROWS OPS CK GOOD. REPLACED RECIRCULATION FILTER. R&R'D BLOWER FIN20 HQ PER AMM 21-26-51 PERFORMED OPERATIONAL TEST OF THE VENTILATION SYS OF AVIONIC EQUIP
2017
Part: INDICATOR — MISSING (L2 GIRT BAR)
DURING PREFLIGHT, DOOR SLIDE IS BULGING ON L2 DOOR, CANNOT SECURE DOOR SLIDE COVER BECAUSE OF IT, PER INFLIGHT CREW REPORTING AND VISUAL INDICATOR ON FWD SIDE OF GIRT BAR MISSING. DOOR SLIDE REMOVED IAW AMM 25-62-44 PB 401. INSTALLATION ON ITEM 3 OF LOG PAGE 1104387. REPLACED GIRT BAR WITH VISUAL INDICATOR INSTALLED TOGETHER AS ASSEMBLY WITH ESCAPE SLIDE REF TO ITEM 3 LOG PAGE 1104387. L2 DOOR ESCAPE SLIDE INSTALLED IAW 25-62-44 PB 401. OPS CHECK COMPLIED WITH. OK FOR SERVICE.
Part: VALVE — LEAKING (SUMP DRAIN)
A DIESEL ODOR WAS IN THE CABIN SHORTLY AFTER TAKEOFF AND THE ACFT RETURNED TO FIELD. MX PERFORMED TSM 05-50-00-810-831-A AND FOUND FUEL LEAKING FROM THE RT CENTER FUEL TANK DRAIN VALVE. CLEANED RESIDUAL FUEL FROM FUSELAGE AREA AND APU INTAKE AREA. RAN APU AND BOTH PACKS NO ODORS NOTED. REPLACED THE SUMP DRAIN VALVE.
2016
Part: UNKNOWN — ODOR (CABIN) · airframe 29,984 hrs · 8,845 cycles
ON ARRIVAL, FUMES, ODOR OF BURNED RUBBER FROM AFT CABIN AT 20000 FT. THEN AGAIN AT TOP OF DESCENT. PERFORMED CABIN ODOR FAULT CONFIRMATION TASK IAW TSM05-50-810-831-A. UNABLE TO CONFIRM FAULT FLIGHT CREW PACK ISOLATED LT AND RT ENGINE IDLE RUN AND AMM 71-00-00-710-006B & AMM 49-00-00-710-010. OK FOR SERVICE AT THIS TIME.
2014
Part: PUMP — OVERHEATED (YELLOW HYD SYS)
ACFT WAS ON THE DEPARTURE PHASE OV VDR26, CREW REPORTED A "YELLOW HYDRAULIC RESERVOIR OVERHEAT", PERFORMED AIR TURNBACK, SAFELY LANDING WITHOUT INCIDENT. CREW DEFECT ENTERED ON LP 688766-1, YELLOW HYDRAULIC RESERVOIR OVERHEAT ON DEPARTURE. MAINTENANCE PERFORMED TROUBLESHOOTING AND R & R CHECKVALVE "Y", 3038GM, IAW TSM 29-24-00-810-804A AND AMM 29-24-51 PB401, OPS CHECK GOOD.
2013
Part: MONITOR — MALFUNCTIONED (BRAKE TEMP)
DURING ROTATION, NR 4 BRAKE TEMP CLIMBED TO 800 DEGREES C WITH AN ASSOCIATED ECAM FOR HOT BRAKES. SELECTED GEAR DOWN AND BRAKE COOLED TO BELOW 500 DEGREES C ON ECAM AND RETURNED TO DEPARTURE AS A PRECAUTION. A NORMAL CONFIGURATION, OVERWEIGHT LANDING PERFORMED. MX NOTED THAT NR 4 BRAKE WAS COLD TO THE TOUCH. RELEASED FOR SERVICE. THE ACFT FLEW ITS NEST 2 LEGS WITHOUT INCIDENT. DURING TROUBLESHOOTING, REVEALED A FAULTY BTMU. REPLACED.
Part: WIRE — BROKEN (EMERGENCY LIGHT)
DURING PREFLIGHT, NOTED EMERGENCY EXIT LIGHT AT SEAT 23L INOPERATIVE. TROUBLESHOOTING REVEALED A BROKEN IN SEAT WIRE. WIRE REPAIRED ESPM 20-43-10 AND OPS CHECKED GOOD IAW AMM 33-51-19. RELEASED FOR SERVICE.