N853VA
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.
46 reports on file, 2016-07-21 – 2024-02-09.
Part: FITTING — CORRODED (NR 2 PYLON) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: PYLON #2 R/H FITTING BASEPLATE P.N. D5461020320100 HAS FRETTING GROUNDED - YES. ALL WORK ACCOMPLISHED ON NON ROUTINE 35903. AC FLIGHT HOURS 34712:52, AC CYCLES 11812, W.V. 015
Part: PLATE — CORRODED (NR 2 PYLON) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: PYLON #2 L/H FITTING BASEPLATE P.N. D5461020320000 HAS FRETTING GROUNDED - YES. ALL WORK ACCOMPLISHED ON NON ROUTINE 35903 AC FLIGHT HOURS 34712:52, AC CYCLES 11812, W.V. 015
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: FLOOR PANEL 231MF- A MINIMUM AREAS OF DELAMINATION GROUNDED - YES. FOUND DELAMINATIONS TO BE OUT OF LIMITS IAW A320 SRM 53-02-00-283-001 RECEIVED NEW PANEL P/N= E5367150100000,PO# 1078065.1.PANEL TO BE INSTALLED ON N/R#35077 AND 9900
Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 34,713 hrs · 11,812 cycles
PUNCTURE FOUND ON PAX FLOOR PANEL PN: E5367151200100 GROUNDED - YES. REPAIRED FLOOR PNL #242MF IAW ALASKA A320 SRM 51-77-13 REV 147 01 NOV 2023. DIAMATER OF THE DAMAGE IS < 0.65 IN
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM 316: FLOOR PANEL 222CF- MINIMUM 6 AREAS OF DELAMINATION. REPLACE GROUNDED - YES. FOUND PANEL TO BE OUT OF LIMITS IAW A320 SRM 53-02-00-283-001. RECEIVED NEW PANEL P/N= E5367192100000, PO# 10401169. PANEL TO BE INSTALLED ON OP# - 9900 AND N/R 35301
Part: SKIN — DAMAGED (FRM 5 S31-32R) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: DB#39, EVIDENCE OF LIGHTNING STRIKE FWD FUSE .6" AFT OF FR5, 13.5" ABOVE LWR SKIN SPLICE, PLEASE PROVIDE NOMINAL SKIN THICKNESS OF DAMAGE, PROVIDE CUTOUT MEASURES, P/N OF RIVETS USED IN DOUBLER,PROVIDE SRM DFPS,REPAIR LOCATION&MEASURES+SKETCH OR PHOTO OF LOCATION+NDT REPORT+MATERIALCERTS OF FILLER&DOUBLER MISSING.REASSESS OF AREA REQ GROUNDED - YES. UNABLE TO VERIFY INFORMATION ON EXISTING REPAIR REQUIRED BY LESSOR FOR PREVIOUS REPAIR INFO REFER TO LP-60306450 AND LP-60306482.REMOVED EXISTING REPAIR IAW A-320 SRM 51-42-11/001,PARA 2E,REV 147.PERFORMED HFEC AND BHEC OF SKIN AND FRAME HOLES COMMON TO REPAIR IAW NTM 51-10-08-250-803-A-01 AND NTM 51-10-01-250-301-A-01.(TOOL# T8257K,DUE 28SEP24)NO CRACK INDICATIONS FOUND.FABRICATED NEW REPAIR FILLER AND DOUBLER IAW A-320 SRM 53-11-11-300-041,FIG 3, REV 147/51-70-20/001 FIG 3,REV 147/51-44-11-001,TABLE 009 REV 147/51-70-20/001,FIG 3,REV 147 AND 51-42-11/001,PARA 2F,REV 147 CURRENT FC ARE 11812 AND FH ARE 34712
Part: SKIN — DENTED (FUSELAGE) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: DB#44, FWD FUSELAGE L/H DENTED BELOW L-2 COCKPIT WINDOW, WO-375836 NR-G176016. OIL #19. RE-EVALUATE REPAIR. REQUIRED ACTION1. PLEASE PROVIDE SRM DFP'S REF USED FOR EVAL. 2. PLEASE PROVIDE EXACT DAMAGE LOCATION. 3. PLEASE PROVIDE PHOTO OR SKETCH ORF DAMAGE. GROUNDED - YES. DENT LENGTH 2.276, HEIGHT 3.110 AND DEPTH .031. WITHIN TOLERANCE IAW A320 SRM 53-00-11-283-005 REV 146 - 01 AUG 2023 FIG 2 PG 6 CATEGORY B PERMANENT REPAIR. PERFORMED LFEC OF DENT IAW NTM 51-10-16-250-801-A - OR REV 142 - 01 NOV 2023. WORK PERFORMED ON CUSTOMER CARD NO. G1874752 THRESHOLD 5000 FC / 10000 FH PER A320 SRM 53-11-11-283-012 FIG 7 SHEET 9 ZONE/ AREA 1.
Part: SUPPORT FITTING — GOUGED (NR 2 PYLON) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: PYLON #2 - FWD SUPPORT - GOUGES AND FRETTING FOUND, IT HAS TO BE INSPECTED PRIOR TO ENGINE INSTALLATION. GROUNDED - YES. BLENDED OUT DAMAGE IAW A-320 SRM 51-73-00-001 AND FOUND BLEND OUTS TO BE WITHIN ALLOWABLE LIMITS IAW A-320 SRM 54-51-18-283-001 FIG 3 AND FIG 5. TOOL#'S T8919A,DUE 23OCT24 AND T8493E, DUE 02JAN25.SEE ATTACHED SKETCH (2EA) FOR DETAILED LOCATION AND DIMENSIONS. VERIFIED REPAIR CLASSIFICATION AS CATEGORY A,PERMANENT REPAIR WITH NO SUPPLEMENTAL INSPECTIONS REQUIRED IAW A-320 SRM 54-51-18-283-001 AND 51-11-14/001.A-320 SRM REV.147-01NOV2023.PYLON IS PRE MOD 155374K17141.
Part: SPIGOT — GOUGED (NR 1 NACELLE) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: PYLON #1 - FWD SUPPORT - GOUGES FOUND, IT HAS TO BE INSPECTED PRIOR TO ENGINE INSTALLATION.853 GROUNDED - YES. BLENDED OUT DAMAGE IAW A-320 SRM 51-73-00-001 AND FOUND BLEND OUTS TO BE WITHIN ALLOWABLE LIMITS IAW A-320 SRM 54-51-18-283-001 FIG 3 AND FIG 5. TOOL#'S T8919A,DUE 23OCT24 AND T8493E, DUE 02JAN25.SEE ATTACHED SKETCH (2EA) FOR DETAILED LOCATION AND DIMENSIONS. VERIFIED REPAIR CLASSIFICATION AS CATEGORY A,PERMANENT REPAIR WITH NO SUPPLEMENTAL INSPECTIONS REQUIRED IAW A-320 SRM 54-51-18-283-001 AND 51-11-14/001.A-320 SRM REV.147-01NOV2023.PYLON IS PRE MOD 155374K17141
Earlier reports · 2016–2023 · 37 reports
2023
Part: SKIN — DENTED (FRM 9) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: DENT LOCATED LH SKIN PANEL 1" FWD OF FRAME 9, 14" BELOW CAPT FIXED WINDOW CUT OUT. NEED PERMENANT REPAIR ACCOMPLISHED. ALSO, REFERENCE DB CHART ITEM 10 GROUNDED - YES. STRIPPED AREA IAW SRM 51-75-11/001, REV 146-01AUG2023 DENT DEPTH .031, LENGTH 2.270, HEIGHT 3.110 WITHIN TOLERANCE IAW A320 SRM 53-00-11-283-005. REV 146-01 AUG 2023 ALODINED AREA IAW A320 SRM 51-21-11-001 REV 147- 01 NOV 2023 PRIMED AND PAINTED IAW A320 51-75-12-911-003 REV 147-01 NOV 2023. CATEGORY B PERMANENT REPAIR IAW A320 SRM 53-00-11-283-005 REV 146-01 AUG 2023 FIG2 PG6. PERFORMED LFEC OF DENT IAW NTM 51-10-16-250-801-A-01 REV 142 -01NOV 2023 THRESOLD 5000FC/10000FH PER A320 SRM 53-11-283-012 FIG 7 SHEET 9 ZONE 1 AREA 1.
Part: DOOR SILL — CORRODED (R1 DOOR AREA) · corrosion level 2 · airframe 34,713 hrs · 11,812 cycles
R1 DOOR CUT-OUT SURFACE CORROSION ON DOOR SILL AT FWD GIRT BAR ATTACH POINT GROUNDED - YES. REMOVED AREA IAW A320 SRM 53-11-14-283-005 STEP 2. ORIGINAL THICKNESS .1968 IAW DWG# D534215. REMOVED .0098" LEAVING .187" THICKNESS (TOOL# T8224T). SPOT FACED AREA IAW A320 SRM 53-11-14-283-005 STEP 7B AND 51-46-12/001. AFTER SPOT FACE REMAINING THICKNESS IS .177 (TOOL# T8224T) REAMED HOLE TO .3287" IAW A320 SRM 53-11-14-283-005 STEP 7D(B)/ SEE ATTACHED JPD'S AND PHOTO'S FOR DETAILED WORK AND DIMENSIONS. THIS REPAIR IS A CATEGORY B. INSPECTION THESHOLD 60,000 FC. FH NO RELEVANT. FH AT TIME OF REPAIR COMPLETION 34712:52, FC 11812. NO OHTER MODS ACCOMPLISHED DURING THIS VISIT AT TIME OF REPAIR, REF SRI 53-11-14-205/001. DRAIN PAN, PLATE ASSY, AND GIRT BAR FITTINGS TO BE INSTALLED ON OPS 551
Part: FLOOR PANEL — PUNCTURED (UNKNOWN) · airframe 34,713 hrs · 11,812 cycles
MAIN CABIN AFT WET AREA FLOORBOARD 261DF HAS A PUNCTURE GROUNDED - YES. RECEIVED NEW PANEL 261DF P/N= E5367191300000. PO# 1076855.1. IAW A320 IPC 53-42-04-47C AND SRM 53-02-00-283-001. INSTALLED ON CUSTOMER CARD NUMBER PANEL BOOK (9900)
Part: DOOR SILL — CORRODED (R2) · corrosion level 2 · airframe 34,713 hrs · 11,812 cycles
R2 DOOR CUTOUT AFT LOWER CORNER AREA, LOWER SILL OF THE DOOR CUTOUT CORRODED BETWEEN FR67 AND FR68 GROUNDED - YES. REMOVED CORROSION IAW A320 SRM 51-71-00-001, FOUND TO BE OUT OF LIMITS WITH MORE THAN 50% MATERIAL LOSS. REPAIRED AREA IAW A320 SRM 53-41-14-300-001
Part: FLOORBEAM — CORRODED (UNKNOWN) · corrosion level 2 · airframe 34,713 hrs · 11,812 cycles
AFT WET AREA: CORROSION ON FLOOR BEAM @ APPROX STA 31577, FRAME 66 GROUNDED - YES. REMOVED AND REPLACED CORRODED BEAM IAW AIRBUS DRAWING # D53472816 AND A320 SRM 51-42-11-001
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEMÿ½ FLOOR PANEL 231LF- 4 MINIMUM AREAS OF DELAMINATION GROUNDED - YES. RECEIVED NEW PANEL 231LF P/N# E5367192300000. PO# 1077187.1 IAW A320 IPC 53-22-02 AND SRM 53-02-00-283-001. INSTALLED ON CUSTOMER CARD NUMBER PANEL BOOK (9900)
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: CABIN FLOOR PANEL 261AG-MINIMUM 4 AREAS OF DELAMINATION GROUNDED - YES. FOUND DELAMINATION TO BE OUT OF LIMITS IAW A320 SRM 53-02-00-283-001.PANEL TO BE REINSTALLED ON OPS 9900 AND 1541 RECEIVED NEW PANEL 261AG P/N= E5367191202800, PO# 1077241.1
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: FLOOR PANEL 232MF -MINIMUM 4 AREAS OF DELAMINATION GROUNDED - YES. RECEIVED NEW PANEL 232MF P/N# E5367150100000. PO# 1077173.1 IAW A320 IPC 53-22-02-01R AND SRM 53-02-00-283-001. INSTALLED ON N/R 35077 CUSTOMER CARD NUMBER #G1874077
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: FLOOR PANEL 231BF -MINIMUM 4 AREAS OF DELAMINATION GROUNDED - YES. FOUND DELAMINATION TO BE OUT OF LIMITS IAW A320 SRM 53-02-00-283-001. RECEIVED NEW PANEL ALT P/N # E5367190100000 OF P/N # E5367147700000 P/O # 967910.1 IAW A320 ASA 53-12-01-32V. PANEL TO BE INSTALLED ON N/R # 35077
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: FLOOR PANEL 251AF -MINIMUM 12 AREAS OF DELAMINATION GROUNDED - YES. RECEIVED NEW PANEL 251AF P/N# E5367190500000. PO# 1077176.2 IAW A320 IPC 53-42-04-01F AND SRM 53-02-00-283-001. INSTALLED ON N/R 35077 CUSTOMER CARD NUMBER #G1874077
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,713 hrs · 11,812 cycles
CABIN FLOOR PANEL 241AF- MINIMUM 2 AREAS OF DELAMINATION GROUNDED - YES. FOUND DAMAGE TO BE OUT OF LIMITS IAW A320 SRM 53-02-00-283-001, RECIEVED NEW PANEL P/N= ES36719000000, PO# 1077261.1 PANEL TO BE REINSTALLED ON N/R# 35077.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: CABIN FLOOR PANEL 242CF- MINIMUM 3 AREAS OF DELAMINATION GROUNDED - YES. FOUND DELAMINATIONS TO BE OUT OF LIMITS IAW A320 SRM 53-02-00-283-001. RECEIVED NEW PANEL P/N= E536150900000, PO# 1077284.1 PANEL TO BE INSTALLED ON N/R= 35077
Part: FLOOR PANEL — UNKNOWN (UNKNOWN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEMÿ½ FLOOR PANEL 241LF - CORE OF PANEL ROTTED AT DOT LOCATION GROUNDED - YES. RECEIVED NEW PANEL 241LF P/N# E5367151300000. PO# 1077249.2 IAW A320 IPC 53-32-04-08 AND SRM 53-02-00-283-001. INSTALLED ON CUSTOMER CARD NUMBER PANEL BOOK (9900)
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: FLOOR PANEL 231QF -MINIMUM 7 AREAS OF DELAMINATION GROUNDED - YES. RECEIVED NEW PANEL 231QF P/N# E5367190500000. PO# 1077181.1 IAW A320 IPC 53-22-02-02J AND SRM 53-02-00-283-001. INSTALLED ON N/R 35077 CUSTOMER CARD NUMBER #G1874077
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: FLOOR PANEL 231XF - MINIMUM 2 AREAS OF DELAMINATION GROUNDED - YES. FOUND DELAMINATION TO BE OUT OF LIMITS IAW A320 SRM 53-02-00-283-001. RECEIVED NEW PANEL ALT P/N # E5367150500000 IAW A320 ASA 53-12-01-32V PO # 1077189.1. NEW PANEL TO BE INSTALLED ON N/R # 35077
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: FLOOR PANEL 231EF-MINIMUM 3 AREAS OF DELAMINATION GROUNDED - YES. FOUND DELAMINATION TO BE OUT OF LIMITS IAW A320 SRM 53-02-00-283-001. RECEIVED NEW PANEL ALT P/N # E5367191000000 OF P/N # E5367162400000 IAW A320 ASA 53-12-01-32V PO # 1077190.1. NEW PANEL TO BE INSTALLED ON N/R # 35077
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: CABIN FLOOR PANL 241EF-MINIMUM 11 AREAS OF DELAMINATION GROUNDED - YES. FLOOR PANEL 241EF FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-02-00-283-001. ORDERED AND RECEIVED NEW FLOOR PANEL 241EF P.N. E5367190800000 P.O.1077261.53 PANEL TO BE INSTALLED ON ALASKA OPS 9900
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: CABIN FLOOR PANL 241EF-MINIMUM 11 AREAS OF DELAMINATION GROUNDED - YES. FLOOR PANEL 232EF FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-02-00-281-001. ORDERED AND RECEIVED NEW FLOOR PANEL 232EF P.N. E5367191600100 P.O.# 1077191.1. PANEL TO BE INSTALLED ON ALASK N/R 35077
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: FLOOR PANEL 231SF -MINIMUM 1 AREA OF DELAMINATION GROUNDED - YES. RECEIVED NEW PANEL 231SF P/N# E5367150100000. PO# 1077171.1 IAW A320 IPC 53-22-02-02J AND SRM 53-02-00-283-001. INSTALLED ON N/R 35077 CUSTOMER CARD NUMBER #G1874077
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 34,712 hrs · 11,812 cycles
LESSOR ITEM: FLOOR PANEL 241JF -MINIMUM 8 AREAS OF DELAMINATION GROUNDED - YES. RECEIVED PANEL 242JF P/N# E5367161700000. PO# 1077260.1 IAW A320 IPC 53-32-04-08 AND SRM 53-02-00-283-001. INSTALLED ON CUSTOMER CARD NUMBER PANEL BOOK (9900)
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: FLOOR PANEL 232DF -MINIMUM 5 AREAS OF DELAMINATION GROUNDED - YES. PANEL FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-02-00-283-001. PANEL RECEIVED- P/N= E5367191900000. PO # 1077204.1. PANEL WILL BE INSTALLED ON N/R # 35077
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: CABIN FLOOR PANEL 251RF- MINIMUM 6 AREAS OF DELAMINATION GROUNDED - YES. FLOOR PANEL 251RF DAMAGED OUT OF LIMITS IAW A320 SRM 53-02-00-283-001. ORDERED AND RECEIVED NEW FLOOR PANEL 251RF P.N E5367190500000 P.O# 1077278.1 PANEL TO BE INSTALLED ON ALASKA N/R 35077 CUST CARD# G1874077
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: FLOOR PANEL 252TF -MINIMUM 2 AREAS OF DELAMINATION GROUNDED - YES. RECEIVED NEW PANEL 252TF P/N# E5367150100000. PO# 1077171.2 IAW A320 IPC 53-42-04-04G AND SRM 53-02-00-283-001. INSTALLED ON N/R 35077 CUSTOMER CARD NUMBER #G1874077
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: FLOOR PANEL 252KF -MINIMUM 2 AREAS OF DELAMINATION GROUNDED - YES. RECEIVED NEW PANEL 252KF P/N# E5367151700000. PO# 1077206.1 IAW A320 IPC 53-42-04-02G AND SRM 53-02-00-283-001. INSTALLED ON N/R 35077 CUSTOMER CARD NUMBER #G1874077
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: CABIN FLOOR PANEL 242GF- MINIMUM 3 AREAS OF DELAMINATION GROUNDED - YES. FOUND DAMAGE TO BE OUT OF LIMITS IAW A320 SRM 53-02-00-283-001, RECEIVED NEW PANEL P/N = ES367151100000, PO# 1077284.1 PANEL TO BE INSTALLED ON N/R # 35077 CUST CARD# G1874077
Part: FLOOR PANEL — CORRODED (UNKNOWN) · corrosion level 2 · airframe 34,713 hrs · 11,812 cycles
MAIN CABIN AFT WET AREA FLOORBOARD 262LG HAS CORROSION GROUNDED - YES. PANEL FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-02-00-283-001. PANEL RECEIVED- P/N= D5367680500300. PO # 1076854.7. PANEL WILL BE INSTALLED ON N/R # 35077
Part: FLOOR PANEL — DENTED (CABIN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM:FLOOR PANEL 231KF- MINIMUM 13 AREAS OF DELAMINATION GROUNDED - YES. FOUND DAMAGE TO BE OUT OF LIMIT IAW A320 SRM 53-02-00-283-001. RECEIVED NEW PNL P/N E5367190500000 PO# 1078089.1 PNL TO BE INSTALLED ON N/R 35077
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: FLOOR PANEL 251LF -MINIMUM 8 AREAS OF DELAMINATION GROUNDED - YES. RECEIVED NEW PANEL 251LF P/N# E5367190500000. PO# 1077176.1 IAW A320 IPC 53-42-04-03G AND SRM 53-02-00-283-001. INSTALLED ON N/R 35077 CUSTOMER CARD NUMBER #G1874077
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: FLOOR PANEL 232PF -MINIMUM 6 AREAS OF DELAMINATION GROUNDED - YES. RECEIVED NEW PANEL 232PF P/N# E5367150200000. PO# 1077186.1 IAW A320 IPC 53-22-02-01R AND SRM 53-02-00-283-001. INSTALLED ON N/R 35007 CUSTOMER CARD NUMBER #G1874077
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: FLOOR PANEL 242LF -MINIMUM 1 AREA OF DELAMINATION GROUNDED - YES. RECEIVED PANEL 242LF P/N# E5367151300000. PO# 1077249.1 IAW A320 IPC 53-32-04-08 AND SRM 53-02-00-283-001. INSTALLED ON CUSTOMER CARD NUMBER PANEL BOOK (9900)
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: FLOOR PANEL 231NF- MINIMUM 1 AREA OF DELAMINATION GROUNDED - YES. PANEL DELAMINATION FOUND TO BE OUT OF LIMITS IAW A320 SRM 50-02-00-283-001. PANEL ORDERED ON THIS OPS CARD. PANEL INSTALLATION ON OPS# 35077. RECEIVED PANEL P/N=E5367150000000 PO# 1077312.4
Part: FLOOR PANEL — CORRODED (UNKNOWN) · corrosion level 2 · airframe 34,713 hrs · 11,812 cycles
AFT WET AREA: CORROSION ON L/H AFT ENTRY DOOR SCUFF PLATE PANEL DOT ATTACHED GROUNDED - YES. PANEL FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-02-00-283-001. PANEL RECEIVED- P/N= E5367680500000. PO# 1076865.1. PANEL WILL BE INSTALLED ON N/R # 35077
Part: FLOOR PANEL — DELAMINATED (UNKNOWN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: FLOOR PANEL 23CBF - MINIMUM 4 AREAS OF DELAMINATION GROUNDED - YES. PANEL FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-02-00-283-001. PANEL RECEIVED- P/N= E5367191800000. PO# 1077193.1. PANEL WILL BE INSTALLED ON N/R # 35077
Part: FLOOR PANEL — PUNCTURED (UNKNOWN) · airframe 34,713 hrs · 11,812 cycles
LESSOR ITEM: FLOOR PANEL 251TF - PUNCTURE LOCATED AT DOT GROUNDED - YES. RECEIVED NEW PANEL 25TJF P/N# E5367150100000. PO# 1077173.2 IAW A320 IPC 53-32-04-08 AND SRM 53-02-00-283-001. INSTALLED ON N/R 35007 CUSTOMER CARD NUMBER #G1874077
2021
Part: LGCIU — FAULTED (MLG) · airframe 30,850 hrs · 10,040 cycles
LANDING GEAR LGCIU 1 FAULT MESSAGE. GROUNDED - YES. CONFIRMED LGCIU 1 FAULT, BITE TEST FAILED. PER TSM 32-31-00-810-802-A REPLACED LGCIU 1, TEST OK. C/W OPS CHECK OF #1 ENGINE THRUST REVERSER PER AMM 78-31-00-710-042-A.TEST OK. NO FAULTS OR DEFECTS NOTED. A/C OK FOR SERVICE.
2016
Part: BLOWER — FAILED (E&E BAY)
ACFT EXPERIENCED AN ACRID ELECTRICAL SMELL IN THE FLIGHT DECK ON FINAL. UPON ARRIVAL IN ORD MX TECHNICIANS ACCOMPLISHED TSM TASK 055000810831A AND FOUND THE SOURCE OF THE SMELL TO BE COMING FROM THE AVIONICS BLOWER FAN. DUE TO NO PARTS IN ORD BLOWER FAN WAS PLACED ON MEL 21260101, BLOWER FAN WAS DEACTIVATED. SFO TECHNICIANS R&R THE BLOWER FAN IAW AMM212651.
Part: UNKNOWN — ODOR (CABIN)
EXPERIENCED A BURNING PLASTIC ODOR IN THE CABIN. THE IFE SYSTEM WAS SHUTDOWN AND THE ODOR DISSIPATED, UPON ARRIVAL AT DESTINATION, THE ACFT WAS REMOVED FROM SERVICE AND MAINTENANCE TECH ACCOMPLISHED TSM TASK 05-50-00-810-831-A AND 24-00-00-810-823-A. NO DEFINITIVE FAILURES WERE FOUND HOWEVER 1 ISPS WAS FOUND FAULTY AND REPLACED. ODOR WAS AGAIN REPORTED ON SUBSEQUENT FLIGHT VX 162, THE IFE WAS SHUTDOWN AND THE ODOR DISSIPATED. TSM TASK 05-50-00-810-831-A & 24-00-00-810-823-A WAS ACCOMPLISHED WITH NO FINDINGS AND THE IFE WAS PLACED ON DEFERRAL.