N848VA
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.
33 reports on file, 2014-12-11 – 2024-07-16.
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 35,467 hrs · 11,791 cycles
MAIN CABIN FLOORBOARD 232DF DAMAGED BEYOND LIMITS. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOORBOARD 232DF AT FR20 TO FR35, STR23L TO STR23R P/N E5367191900000 IAW AMM 53-00-00-400-801-A.
Part: SKIN — GOUGED (ZONE 100) · airframe 35,467 hrs · 11,791 cycles
FUSELAGE SKIN GOUGED 10 IN LEFT OF LOWER CENTER LINE AT FR 31 GROUNDED - YES. ACCOMPLISHED FUSELAGE SKIN PANEL FR 31 STGR 42LH DOUBLER REPAIR PER ASA EA #A320-53EA-02245 REV 00
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 35,467 hrs · 11,794 cycles
MAIN CABIN FLOORBOARD 261DF DAMAGED. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOORBOARD 261DF P/N: E5367191300000 AT FR64 - FR70, STR 30L TO 30R BUTT LINE 60L TO BUTT LINE 60R IAW A320 AMM 53-00-00-00-801-A AND 53-00-00-400-801-A.
Part: HINGE ARM — WORN (RT ELEVATOR) · airframe 35,467 hrs · 11,791 cycles
R/H ELEVATOR HINGE ARM END FITTINGS 1 THROUGH 6 HAVE EXCESSIVE PLAY. GROUNDED - YES. REMOVED AND REPLACED R/H ELEVATOR HINGE ARM END FITTING 1 THROUGH 6 IAW AMI 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
Part: HINGE ARM — WORN (LT ELEVATOR) · airframe 35,467 hrs · 11,791 cycles
L/H ELEVATOR HINGE ARM END FITTINGS 1 THROUGH 6 HAVE EXCESSIVE PLAY. GROUNDED - YES. REMOVED AND REPLACED L/H ELEVATOR HINGE ARM END FITTINGS 1 THROUGH 6 P/N: D5598141100400 (5 EA) AND P/N: D5598141300400 (1 EA) IAW AMM 55-16-42-000-001-A AND 55-16-42-400-001-A.
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 35,467 hrs · 11,791 cycles
MAIN CABIN FLOORBOARD 251WF DAMAGED. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOORBOARD 251WF P/N: E5367191100000 BETWEEN FR47 AND FR64, STR 23L TO STR 23R IAW AMM 53-00-00-00-801-A AND 53-00-00-400-801-A.
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 35,467 hrs · 11,794 cycles
FLOORBOARD 251RF DAMAGED. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOORBOARD 251RF IAW A320 AMM 53-00-00-00-801-A AND 53-00-00-400-801-A.
Part: FLOORBOARD — DAMAGED (CABIN) · airframe 35,467 hrs · 11,791 cycles
AFTER CARPET REMOVAL FOUND FLOOR BOARD 261AG DAMAGED. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR BOARD 261AG IAW A320 AMM 53-00-00-400-801-A.
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 35,467 hrs · 11,794 cycles
MAIN CABIN FLOORBOARD 231QF DAMAGED. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOORBOARD 231QF IAW A320 AMM 53-00-00-00-801-A AND 53-00-00-400-801-A.
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 35,467 hrs · 11,791 cycles
MAIN CABIN FLOORBOARD 231KF DAMAGED. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOORBOARD 231KF P/N: E5367190500000 BETWEEN FR20 TO FR35, STR 23L TO STR 23R, BUTT LINE 71L TO 71R IAW AMM 53-00-00-00-801-A AND 53-00-00-400-801-A.
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 35,467 hrs · 11,794 cycles
MAIN CABIN FLOORBOARD 251LF IS DAMAGED. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOORBOARD 251LF P/N: E5367190500000 BETWEEN FR47 AND FR64, STR 23L TO STR 23R IAW A320 AMM 53-00-00-00-801-A AND 53-00-00-400-801-A.
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 35,467 hrs · 11,791 cycles
MAIN CABIN FLOORBOARD 231GF DAMAGED. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOORBOARD 231GF P/N: E5367190100000 BETWEEN FR20 TO FR35, STR 23L TO STR 35R, BUTT LINE 71 L TO 71 R IAW AMM 53-00-00-00-801-A AND 53-00-00-400-801-A.
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 35,467 hrs · 11,791 cycles
MAIN CABIN FLOORBOARD 241AF DAMAGED. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOORBOARD P/N: E5367190700000 241AF AT FR35 TO FR47, STR 23R TO STR23L, BUTT LINE 71R TO BUTT LINE 71L IAW AMM 53-00-00-00-801-A AND 53-00-00-00-400-801-A.
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 35,467 hrs · 11,794 cycles
MAIN CABIN FLOORBOARD 251AF DAMAGED. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOORBOARD 251AF IAW A320 AMM 53-00-00-00-801-A AND 53-00-00-400-801-A.
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 35,467 hrs · 11,791 cycles
AFTER CARPET REMOVAL FOUND FLOORBOARD 251FF DAMAGED GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOORBOARD 251FF P/N E5367191000000 BETWEEN FR 47 AND FR 64 STGR 23L TO STGR 23R IAW A320 AMM 53-00-00-801-A AND AMM 53-00-00-400-801-A.
Part: FLOORBOARD — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,467 hrs · 11,791 cycles
MAIN CABIN FLOORBOARD 262LG HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOORBOARD 262LG AT FR66 TO FR68, STGR 23R TO STGR 23L IAW SRM 53-02-00-283-801.
Part: WEB — CORRODED (FRS 69-70) · corrosion level 2 · airframe 35,467 hrs · 11,791 cycles
L2 DOOR AFT OF FR C69 AT FLOOR LEVEL A TRIANGLE WEB HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED TRIANGLE WEB (SHEAR PLATE) P/N: D534742420200 AT L2 DOOR AFT OF C69 FRAME AT FLOOR LEVEL IAW SRM 51-72-911-001 REV. 149 AND SRM 51-42-11/001 REV. 149.
Part: WEB — CORRODED (FRS 69-70) · corrosion level 2 · airframe 35,467 hrs · 11,791 cycles
R2 DOOR BETWEEN FR C69-C70 AT FLOOR LEVEL. A TRIANGLE WEB HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED TRIANGLE WEB (SHEAR PLATE) P/N: 53-47112420300 AT R2 DOOR BETWEEN FR C69-C79 AT FLOOR LEVEL IAW SRM 51-72-11-911-001 REV. 149 AND SRM 51-42-11/001 REV. 149
Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,467 hrs · 11,791 cycles
R2 DOOR GIRT BAR FITTING HAS SIGNS OF CORROSION ON FWD AND AFT GIRT BAR FITTINGS. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MAJOR REPAIR TO R2 DOOR LOWER SILL BEAM PN: D5348004320700 PER EA A320-53EA-02219 REV 00
Part: FLOOR SUPPORT — CORRODED (FRS 67-69) · corrosion level 2 · airframe 35,467 hrs · 11,791 cycles
R2 DOOR UNDER FLOOR PANEL 262LG HAS CORROSION ON FLOOR STRUCTURE. GROUNDED - YES. REMOVED AND REPLACED LONGITUDINAL BEAM AT R2 DOOR FR67 TO FR69, Y=-765 IAW SRM 51-72-11-911-001 AND SRM 51-42-11/001 REV. 149
Part: FLOORBOARD — DAMAGED (CABIN) · airframe 35,467 hrs · 11,791 cycles
MAIN CABIN FLOORBOARD 231VF DAMAGED. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOORBOARD P/N E5367190600000 AT FR 36 TO FR 42. STGR 23L TO STRGR 23R BUTT LINE 10L TO BUTT LINE 10R IAW A320 AMM 53-00-00-00-801-A AND AMM 53-00-00-400-801-A.
Part: WEB — CORRODED (AFT CABIN) · corrosion level 2 · airframe 35,467 hrs · 11,791 cycles
R1 DOOR AFT FLOOR STRUCTURE HAS CORROSION AT FR20. GROUNDED - YES. REMOVED AND REPLACED R1 DOOR AFT FLOOR STRUCTURE P/N: D5311816020000 AT FR C20R-FR C23R IAW SRM 51-72-911-00 REV 149 AND SRM 51-23-12 REV. 149.
Part: FLOOR SUPPORT — CORRODED (FRMS 67-70) · corrosion level 2 · airframe 35,467 hrs · 11,791 cycles
L2 DOOR FLOOR SUPPORT UNDER PANEL 261 LG HAS CORROSION GROUNDED - YES. REMOVED AND REPLACED FLOOR BEAM P/N: D5347219220200 AT L2 DOOR BETWEEN FR67 TO FR70 AND Y=765 IAW SRM 51-72-11-911-001 AND SRM 51-42-11/001 PARA 2F REV 149.
Part: LINK — CORRODED (LT ELEVATOR) · corrosion level 2 · airframe 35,467 hrs · 11,791 cycles
L/H HORIZ. STAB TO OUTBD ELEVATOR SUPPORT LINK THE CLEVIS LINK HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED LH HORIZ. STAB OUTBD ELEVATOR STRUT SUPPORT LINK IAW AMM 55-16-48-000-001-A AND 55-16-48-400-001-A. P/N: D5598181320200
Part: WEB — CORRODED (AFT CARGO) · corrosion level 2 · airframe 35,467 hrs · 11,791 cycles
AFT CARGO SIGNS OF CORROSION ON WEB AT SEVERAL LOCATIONS. GROUNDED - YES. REMOVE AND REPLACED WEB/SHEET P/N: D5347556522600 IN AFT CARGO ENTRYWAY FR C52A-FR C56, Y= -336.55R TO Y= -609.6 IAW SRM 51-72-11-911-001 REV. 149.
Part: SCUFF PLATE — CORRODED (FRS 16-20 S23L) · corrosion level 2 · airframe 35,467 hrs · 11,791 cycles
CENTER FITTING UNDER SCUFF PLATE AT L1 DOOR HAS MULTIPLE AREAS OF CORROSION AT STR 23 BETWEEN LH FR 16-FR20. GROUNDED - YES. REMOVED AND REPLACED FITTING AT L1 DOOR STR 23L BETWEEN FR16 TO FR20 IAW SRM 51-72-11-911-001 REV. 149 AND SRM 51-42-11/001 REV. 149
Part: FITTING — CORRODED (FWD CABIN) · corrosion level 2 · airframe 35,467 hrs · 11,791 cycles
CENTER FITTING P/N: D5311219820106 UNDER R1 DOOR SCUFF PLATE HAS MULTIPLE AREAS OF CORROSION. GROUNDED - YES. REMOVED AND REPLACED CENTER FITTING P/N: D5311219820106 UNDER R1 DOOR SCUFF PLATE AT STR 23 BETWEEN RH FR16 - FR20 IAW A320 SRM 51-72-11-911-001 REV 149 AND SRM 51-42-11/001.
Part: SKIN — DENTED (ZONE 100) · airframe 35,467 hrs · 11,794 cycles
RAMP REPORTS SMALL DENT FWD OF POTABLE WATER SERVICE DOOR GROUNDED - YES. ACCOMPLISHED MAJOR REPAIR IAW AIRBUS TD/81405756/032/2024#A AND ALASKA AIRLINES EA A320-53EA-02190 REV 00. PER AIRBUS RDAF 81405756/003/2024#A DATED 09/07/2024, THE PERFORMED REPAIR IS CONSIDERED ACCEPTABLE AS PERMANENT PS2 FROM THE FATIGUE AND DAMAGE TOLERANCE VIEWPOINT WITH THE FOLLOWING INSPECTION PROGRAM: FOR DENT DAMAGE - TH=59500 FC (FH NOT RELEVANT) (FROM 1ST A/C FC), II=13000 FC (FH NOT RELEVANT), MET=GVI AS PER NTM 51-90-00. FOR DOUBLER REPAIR - TH=103900 FC (FH NOT RELEVANT) (FROM 1ST A/C FC), II=TBD, MET=TBD.
Earlier reports · 2014–2020 · 5 reports
2020
Part: ADIRU — FAILED (FLIGHT DECK) · airframe 31,071 hrs · 9,792 cycles
INFLIGHT ECAM ANTI-ICE F/O PITOT F/O AOA, F/O L/R STATIC PORT FAULT DIVERTED A/C IN VFR CONDITIONS. GROUNDED-YES. PERFORMED OPS TEST ON PHC, IN REF TO A320 AMM 30-31-00, WITH NO DEFECTS NOTED AT THIS TIME. REMOVED AND REPLACED NR 2 ADIRU IN REF TO AMM 34-12-34, NO DEFECTS NOTED AT THIS TIME. A/C GOOD FOR SERVICE.
2018
Part: PRESSURE SWITCH — FAILED (HYDRAULIC SYS) · airframe 25,873 hrs · 7,735 cycles
YELLOW HYDRAULIC SYSTEM LOW PRESSURE INDICATED IN FLIGHT NOSE WHEEL STEERING INOP. GROUNDED - YES. REMOVED & REPLACED PRESSURE SWITCH (3151GN) PER AMM 29-32-12-000-001-A. OPS & LEAK CK NO LEAKS FOUND OPS CK NORMAL.
Part: COMPUTER — FAILED (AVIONICS BAY) · airframe 24,516 hrs · 7,272 cycles
VENT AVIONICS SYSTEM FAULT. ACFT GROUNDED. CONNECTED THE ISOLATION VALVE 24HQ, R & R AEVC COMP, 10HQ IAW AMM 21-26-34. OPS CHECKED GOOD.
2015
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)
EMERGENCY EXIT LIGHTS STAYED ON AFTER GEAR RETRACTION. OVERWING AND AFT GALLEY STAYED ON, FWD GALLEY SHUT OFF. R & R 8WL CENTRAL POWER SUPPLY IAW ESPM 20-46-50. PERFORM OPS CHECK IAW AMM 33-51-38, CHECKED ON SUBSEQUENT FLIGHT, NO DEFECTS NOTED.
2014
Part: PIN — MISSING (NLG)
CLEARING RUNWAY, NOSE WHEEL BEGAN VIOLENT VIBRATION, LIMITED NOSE WHEEL STEERING CONTROL. AIRCRAFT TOWED TO THE GATE. ON ARRIVAL AT GATE, IT WAS NOTED APEX PIN AND NUT WERE MISSING. ACCOMPLISHED OVERLOAD INSPECTION IAW AMM 05-51-22-601. REPLACED UPPER AND LOWER TORQUE LINKS IAW AMM 32-21-27-401. INSTALLED APEX PIN AND NUT IAW AMM 32-21-27-400-002, PERFORMED FUNCTION TEST OF NOSE WHEEL STEERING IAW AMM 32-51-00-720-001. PERFORMED FULL FUNCTIONAL TEST OF NLG EXTENSION/RETRACTION. OPS CHECK GOOD.