N633VA
Registered owner: AJ AVIATION HOLDINGS LLC, FL (owner ≠ operator)
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.
39 reports on file, 2013-08-09 – 2022-04-21.
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 5" IINBOARD OF RIB 8 GROUNDED - YES. CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 5" IINBOARD OF RIB 8 REPAIRED PER EA A320-57EA-01458 REV 00 DATED 8/22/2022
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 12 INCHES I/B OF RIB 7 GROUNDED - YES. CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 12 INCHES I/B OF RIB 7 REPAIRED PER EA # A320-57EA-01458 REV 00, DATED 08/22/2022
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 12" O/B OF RIB 21 GROUNDED - YES. CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 12" O/B OF RIB 21 REPAIRED PER EA A320-57EA-01458 REV 00 DATED 8/22/2022
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 6" I/B OF RIB 14 GROUNDED - YES. CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 6" I/B OF RIB 14 REPAIRED PER EA A320-57EA-01458 REV 00 DATED 8/22/2022
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 3" I/B OF RIB 18 GROUNDED - YES. CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN UPPER SURFACE 3" I/B OF RIB 18 REPAIRED PER EA A320-57EA-01458 REV 00 DATED 8/22/2022
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN UPPER SURFACE 2" I/B OF RIB 13 GROUNDED - YES. CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN UPPER SURFACE 2" I/B OF RIB 13 REPAIRED PER EA A320-57EA-01458 REV 00 DATED 8/22/2022
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE UPPER R/W SKIN LOWER SURFACE LOCATED 3" O/B OF RIB 10 COMMON TO THE UPPER REAR SPAR GROUNDED - YES. CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE UPPER R/W SKIN LOWER SURFACE LOCATED 3" O/B OF RIB 10 COMMON TO THE UPPER REAR SPAR INSPECTED AND REPAIRED IAW EA A320-57EA-01458 REV 00 DATED 8/22/2022
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
CORROSION ON LEFT WING UPPER TRAILING EDGE SKIN UPPER SURFACE HAS 17 EA CORRODED FASTENERS AT FALSE SPAR RIB 9 GROUNDED - YES. CORROSION ON LEFT WING UPPER TRAILING EDGE SKIN UPPER SURFACE AT 17 EA FASTENERS AT FALSE SPAR RIB 9 REPAIRED PER EA # A320-57EA-01457 DATED 08/11/2022, REV 00
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
CORROSION ON LEFT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 3 INCHES I/B OF RIB 21 GROUNDED - YES. CORROSION ON LEFT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 3" I/B OF RIB 21 REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
CORROSION RIGHT WING UPPER SKIN AT RIB 19 T/E BETWEEN SPOILERS 4/5 HAS CORROSION AT FASTENERS GROUNDED - YES. CORROSION RIGHT WING UPPER SKIN AT RIB 19 T/E BETWEEN SPOILERS 4/5 HAS CORROSION AT FASTENERS INSP AND REPAIRED PER EA A320-57EA-01458 REV 00 DATED 8/22/2022
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
CORROSION ON LEFT WING UPPER TRAILING EDGE SKIN LOWER SURFACE AT FALSE RIB 8 GROUNDED - YES. CORROSION ON L/H WING UPPER TRAILING EDGE SKIN LOWER SURFACE AT FALSE REAR SPAR RIB 8 REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2L-C007 AT UPPER L/W SKIN LOWER SURFACE LOCATED 6" I/B OF RIB 7 COMMON TO THE UPPER REAR SPAR. GROUNDED - YES. CORROSION ON L/H WING UPPER SKIN LOWER SURFACE 6" I/B OF RIB 7 COMMON TO THE UPPER REAR SPAR REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
L/H WING UPPER SKIN 3" I/B OF RIB 18 LOWER SURFACE HAS AREA OF CORROSION GROUNDED - YES. L/H WING UPPER SKIN 3" I/B OF RIB 18 LOWER SURFACE AREA OF CORROSION REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2L-C007 AT UPPER LEFT WING SKIN LOWER SURFACE LOCATED 3" O/B OF RIB 14 COMMON TO THE UPPER REAR SPAR. GROUNDED - YES. CORROSION ON L/H WING UPPER SKIN LOWER SURFACE 3" O/B OF RIB 14 COMMON TO THE UPPER REAR SPAR REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE UPPER R/W SKIN LOWER SURFACE LOCATED 5" O/B OF RIB 11 COMMON TO THE UPPER REAR SPAR GROUNDED - YES. CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE UPPER R/W SKIN LOWER SURFACE LOCATED 5" O/B OF RIB 11 COMMON TO THE UPPER REAR SPAR INSPECTED AND REPAIRED IAW EA A320-57EA-01458 REV 00 DATED 8/22/2022
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
L/H WING UPPER SKIN AT RIB 17 T/E JUST FWD OF #4 SPOILER I/B HINGE HAS CORROSION GROUNDED - YES. L/H WING UPPER SKIN AT RIB 17 T/E JUST FWD OF #4 SPOILER I/B HINGE CORROSION AT FASTENERS REPAIRED PER EA # A320-57EA-01457, DATED 08/11/2022, REV 00
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
LEFT WING UPPER TRAILING EDGE SKIN LOWER SURFACE AT RIB 16 HAS CORROSION GROUNDED - YES. CORROSION AT LEFT WING UPPER TRAILING EDGE SKIN LOWER SURFACE AT RIB 16 REPAIRED PER EA # A320-57EA-01457, DATED 08/11/2022, REV 00
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
CORROSION ON LEFT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 3" O/B OF RIB 10 GROUNDED - YES. CORROSION ON L/H WING UPPER TRAILING EDGE SKIN LOWER SURFACE 3" O/B OF RIB 10 REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
L/H WING UPPER SKIN 6" I/B OF RIB 19 LOWER SURFACE HAS AREA OF CORROSION GROUNDED - YES. L/H WING UPPER SKIN 6" I/B OF RIB 19 LOWER SURFACE AREA OF CORROSION REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE UPPER R/W SKIN LOWER SURFACE LOCATED 5" O/B OF RIB 19 COMMON TO THE UPPER REAR SPAR GROUNDED - YES. CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE UPPER R/W SKIN LOWER SURFACE LOCATED 5" O/B OF RIB 19 COMMON TO THE UPPER REAR SPAR INSPECTED AND REPAIRED IAW EA A320-57EA-01458 REV 00 DATED 8/22/2022
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
L/H WING UPPER SKIN AT RIB 5 T/E JUST FWD OF #1 SPOILER I/B HINGE HAS CORROSION AT FASTENERS GROUNDED - YES. L/H WING UPPER SKIN AT RIB 5 T/E JUST FWD OF #1 SPOILER I/B HINGE CORROSION AT FASTENERS REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
L/H WING UPPER SKIN AT RIB 13 T/E JUST FWD OF #2/3 SPOILERS HAS CORROSION GROUNDED - YES. CORROSION ON L/H WING UPPER SKIN AT RIB 13 T/E FASTENERS JUST FWD OF #2/3 SPOILERS REPAIRED IAW EA # A320-57EA-01457, DATED 08/11/2022 REV 00
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2L-C007 AT THE UPPER L/H WING SKIN LOWER SURFACE LOCATED 4" O/B OF RIB 11 COMMON TO THE UPPER REAR SPAR. GROUNDED - YES. CORROSION ON L/H WING UPPER SKIN LOWER SURFACE 4" O/B OF RIB 11 COMMON TO THE UPPER REAR SPAR REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2L-C007 AT UPPER LEFT WING SKIN LOWER SURFACE LOCATED 3" O/B OF RIB 15 COMMON TO THE UPPER REAR SPAR. GROUNDED - YES. CORROSION ON L/H WING UPPER SKIN LOWER SURFACE 3" O/B OF RIB 15 COMMON TO THE UPPER REAR SPAR REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
L/H WING UPPER SKIN AT RIB 19 T/E BETWEEN SPOILERS 4/5 HAS CORROSION AT FASTENERS GROUNDED - YES. L/H WING UPPER SKIN AT RIB 19 T/E BETWEEN SPOILERS 4 AND 5 CORROSION AT FASTENERS REPAIRED PER EA # A320-57EA-01457 REV 00, DATED 08/11/2022.
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
CORROSION RIGHT WING UPPER SKIN AT RIB 8 TO 10" HAS CORROSION AT FASTENERS GROUNDED - YES. CORROSION RIGHT WING UPPER SKIN AT RIB 8 TO 10" HAS CORROSION AT FASTENERS INSPECTED AND REPAIRED PER EA A320-57EA-01458 REV 00 DATED 8/22/2022
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE UPPER R/W SKIN LOWER SURFACE LOCATED 5" O/B OF RIB 14 COMMON TO THE UPPER REAR SPAR GROUNDED - YES. CORROSION NOTED DURING NDI INSPECTION CUSTOMER CARD 572127-01-1A-2R-C007 AT THE UPPER R/W SKIN LOWER SURFACE LOCATED 5" O/B OF RIB 14 COMMON TO THE UPPER REAR SPAR INSPECTED AND REPAIRED IAW EA A320-57EA-01458 REV 00 DATED 8/22/2022
Part: SKIN — CORRODED · corrosion level 2 · airframe 44,509 hrs · 14,007 cycles
CORROSION RH WING UPPER SKIN AT RIB 5 T/E JUST FWD OF #1 SPOILER I/B HINGE HAS CORROSION AT FASTENERS GROUNDED - YES. CORROSION RH WING UPPER SKIN AT RIB 5 T/E JUST FWD OF #1 SPOILER I/B HINGE HAS CORROSION AT FASTENERS INSP AND REPAIRED PER EA A320-57EA-01458 REV 00 DATED 8/22/2022
Earlier reports · 2013–2019 · 11 reports
2019
Part: SEAT TRACK — CORRODED (FRAMES 67-70) · airframe 42,787 hrs · 13,222 cycles
AFT WET AREA FLOOR STRUCTURE BEAM ASSY AT FR68: Y-765 HAS CORROSION GROUNDED - YES. REMOVED AND REPLACED BEAM ASSY IAW A320 SRM 51-72-11 CAT A REPAIR, NO REINSPECT REQUIRED. CORRODED AROUND HARD PAINT. NO DAMAGE ALLOWED IAW A320 SRM 53-41-14
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,787 hrs · 13,222 cycles
SEAT TRACK CORRODED AT FRAME 18 -Y1292 GROUNDED - YES. REMOVED AND REPLACED FLOORBEAM PER SRM 51-42-11 AND DWG # D53112814. CAT A REPAIR NO REINSPECT REQUIRED DAMAGE FOUND TO BEW OUT OF LIMITS PER SRM 53-11-15-287-005.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,787 hrs · 13,222 cycles
CORROSION 3 PLACES AT R2 DOOR UNDER CABIN FLOOR BOARD 262LG. GROUNDED - YES. REMOVED CORROSION, CORRODED AREA EXTENDS COMPLETELY THREW FLOOR SUPPORT - EXFOLIATED- AREA OUT OF LIMITS IAW SRM 53-41-14-283-002, FABRICATED REPAIR IAW SRM 53-41-14-300-001 FIG 001 HFEC CUTOUT AREAS USING T8257A IAW NTM TASK 51-10-08 NO CRACKS NOTED. ALODINED REPAIR & AREAS IAW SRM 51-21-11, PRIMED IAW SRM 51-21-11 AND TOPCOATED AREAS IAW SRM 51-21-11 AND INSTALLED REPAIR IAW SRM 53-41-14-300-001 FIG 001. CAT A REPAIR, NO REINSPECT REQUIRED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,787 hrs · 13,222 cycles
CORROSION CABIN FLOOR SUPPORT, AT FR15 UNDER FLOOR PANEL 221EF GROUNDED - YES. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-72-11. DAMAGE REMOVED. ORIG THICKNESS .087, REMOVED .055, REMAINING .032, FOUND TO BE OUT OF LIMITS IAW SRM 53-11-15-283-005. CAT A REPAIR, NO REINSPECTS REQUIRED
2017
Part: SUMP — LEAKING (CENTER TANK)
ON ARRIVAL AT ACFT FOR FIRST FLIGHT, CREW DETECTED A STRONG FUEL ODOR IN THE COCKPIT AND THROUGHOUT CABIN. ODOR DISSIPATED WITH APU BLEED ON. DURING INSPECTION, IAW TSM 055000810831A, FOUND RT CENTER TANK FUEL SUMP LEAKING. RESEATED SUMP DRAIN AND CLEANED AREA, NO LEAKS NOTED, ACFT OK TO CONTINUE. ON ARRIVAL, NO DEFECTS WERE NOTED.
2015
Part: OVEN — ODOR (GALLEY) · airframe 29,759 hrs · 8,923 cycles
FLIGHT CREW REPORTED A BURNING ODOR IN THE FORWARD GALLEY DURING CLIMBOUT. THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. UPON ARRIVAL, TECH OPS ACCOMPLISHED TROUBLESHOOTING IAW AMM 05-50-00-810-831-A. NO ODORS OR ABNORMAL OIL CONSUMPTION NOTED DURING ENGINE AND APU RUNS. UPON FURTHER EVALUATION IT WAS DETERMINED THA THE ODOR WAS EMANATING FROM THE FORWARD GALLEY OVEN, THE OVEN WAS R & R IAW AMM 25-35-19. NO FURTHER ISSUES NOTED ON SUBSEQUENT FLIGHTS.
2014
Part: CONNECTOR — BURNED (LAVATORY)
ODOR OF MELTED PLASTIC IN LAVATORY F. COMPLIED WITH AMM 05-5000-810-831, CAUSE OF ODOR, FOUND RAZOR SOCKET ON AFT LAVATORY F BROKEN AND ODOR OF ELECTRICAL BURN ON THE SOCKET. R & R AFT LAV RAZOR SOCKET LAV "F", OPS CHECK SATISFACTORY. REF 25-44-41. THIS RESULTED IN A 1:13 MIN DELAY ON OUTBOUND FLIGHT. RAZOR OUTLET SOCKET WAS FOUND TO BE DAMAGED BY TAMPERING AND DID NOT FAIL DUE TO NORMAL WEAR AND TEAR.
2013
Part: SUPPORT — CORRODED (FUSELAGE)
LEFT AFT SHEAR PLATE SUPPORT FRAMES 69-70, S23-24L HAS CORROSION BEYOND LIMITS. EXTENT OF DAMAGE 1" LENGTH X 1" WIDTH X .030" DEPTH. SUPPORT BELOW SHEAR PLATE WAS R & R IAW SRM 51-40-00 AND 51-42-11.
Part: SUPPORT — CORRODED (FUSELAGE)
RIGHT AFT SHEAR PLATE SUPPORT FR 69-70, S23-24R HAS CORROSION BEYOND LIMITS. EXTENT OF DAMAGE 1" LENGTH X 1" WIDTH X .025" DEPTH. SUPPORT BELOW SHEAR PLATE WAS R & R IAW SRM 51-40-00 AND 51-42-11.
Part: SHEAR PLATE — CORRODED (FUSELAGE)
LEFT AFT SHEAR PLATE FRAMES 69-70, S23-24L HAS CORROSION BEYOND LIMITS. EXTENT OF DAMAGE 2" LENGTH X 2" WIDTH X .032" DEPTH. SHEAR PLATE WAS R & R IAW SRM 51-40-00 AND 51-42-11.
Part: SHEAR PLATE — CORRODED (FUSELAGE)
RIGHT AFT SHEAR PLATE FR 69-70, ST23R-24R HAS CORROSION BEYOND LIMITS. EXTENT OF DAMAGE 2" LENGTH X 2" WIDTH X .030" DEPTH. SHEAR PLATE WAS R & R IAW SRM 51-40-00 AND 51-42-11.