# Service difficulty reports: N855VA, cancelled Jul 30, 2024

A list on [N855VA, cancelled Jul 30, 2024](https://openairdocs.org/deregistered/N855VA-2024-07-30.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR ASAA2024040450033](https://openairdocs.org/sdr/ASAA2024040450033.md): Skin · dented · Apr 4, 2024 · N855VA · Airbus A320214 · Trailing Edge Flaps
  > RIGHT WING, DENT ON I/B FLAP LOWER SKIN, 13 CM FROM UPPER EDGE,.812 MM DEEP, 17MM DIA 220 CM FROM INNER EDGE DOT: B386 GROUNDED - YES. ALL WORK ACCOMPLISHED ON CARD G1941548. PREFORED CATEGORY A PERMANENT REPAIR ON R/W I/B FLAP LOWER SURFACE IN ZONE 2. REPAIR
- [SDR ASAA2024040450032](https://openairdocs.org/sdr/ASAA2024040450032.md): Skin · dented · Apr 4, 2024 · N855VA · Airbus A320214 · Trailing Edge Flaps
  > LEFT WING, I/B FLAP HAS SEVERAL 3 DENTS ON LOWER SKIN ABOVE PYLON FAIRING 7CM LONG 2CM WIDE UNABLE TO MEASURE DEPTH DUE TO FAIRING GROUNDED - YES. REPAIRED LEFT WING I/B FLAP LOWER SKIN LOCATED 13 Ï¿½Ï¿½ FROM OUTBRD AND STOPS AT 10 Ï¿½Ï¿½ AND 8Ï¿½ FROM T/E. I
- [SDR ASAA2024040350523](https://openairdocs.org/sdr/ASAA2024040350523.md): Skin · gouged · Apr 3, 2024 · N855VA · Airbus A320214 · Fuselage Main, Plate/Skin
  > AFT LOWER EXTERNAL FUSELAGE, FRAME 58 TO 59 AT ANTENNA MOUNT, SKIN IS GOUGED GROUNDED - YES. REMOVED ANTENNA IAW AMM A320 34-42-11-000-001A REV 10. ORIGINAL MAT.118" IAW A320 SRM 53-41-11-42B REV 148. BLENDED DAMAGE, REMAINING MAT.115, LENGT 1.2", WIDTH.800
- [SDR ASAA2024040350522](https://openairdocs.org/sdr/ASAA2024040350522.md): Skin · gouged · Apr 3, 2024 · N855VA · Airbus A320214 · Fuselage Main, Plate/Skin
  > AFT LOWER EXTERNAL FUSELAGE, BELOW AFT CARGO DOOR, FRAME 55 TO 56 AT ANTENNA MOUNT, SKIN IS GOUGED GROUNDED - YES. REMOVED ANTENNA IAW A320 AMM 34-42-11-000-001-A REV 10. ORIGINAL MAT.118 IAW A320 SRM 53-41-11-42B REV 148. BLENDED DAMAGE, REMAINING MAT.110,
- [SDR ASAA2024040250001](https://openairdocs.org/sdr/ASAA2024040250001.md): Skin Panel · corroded · Apr 2, 2024 · N855VA · Airbus A320214 · Fuselage Main, Plate/Skin
  > FWD LOWER EXTERNAL FUSELAGE SKIN BETWEEN FRAME 33 AND 34 HAS CORROSION AT DRAIN/VENT PORT GROUNDED - YES. REMOVED FASTENERS TO FOM CORROSION REMOVAL IAW A320 SRM 51-42-11/001, PARA ZE, REV148. REMOVED CORROSION IAW A-320 SRM 51-74-00/001, PARA 5-A3, REV148 AND
- [SDR ASAA2024032950069](https://openairdocs.org/sdr/ASAA2024032950069.md): Door Frame · corroded · Mar 29, 2024 · N855VA · Airbus A320214 · Fuselage Main, Structure
  > AFT CARGO BAY FLOOR ON DOOR FRAME AT C53R CORRODED. GROUNDED - YES. REMOVED 2EA FASTENERS IAW A320 SRM 51-42-11/001/REV 148-01FEB2024. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW A320 SRM 53-41-49-283-004 REV 148- 01FEB2024. ACCOMPLISHED DVI AND HFEC INSPECT
- [SDR ASAA2024032950062](https://openairdocs.org/sdr/ASAA2024032950062.md): Door Frame · corroded · Mar 29, 2024 · N855VA · Airbus A320214 · Fuselage Main, Structure
  > AFT CARGO BAY FLOOR, AT DOOR FRAME FORWARD CORNER AT NET MOUNT PUCK, BETWEEN C52R AND C53R GROUNDED - YES. REMOVED 2EA FASTENERS IN CORRODED AREA IAW A320 SRM 51-42-11/001 REV 148-01FEB.2024. REMOVED CORROSION IN AREA WITH A REMAINING THICKNESS OF.087 AND FOU
- [SDR ASAA2024032950031](https://openairdocs.org/sdr/ASAA2024032950031.md): Web · corroded · Mar 29, 2024 · N855VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FLOOR CORRODED AT STATION C53R FROM 16 TO 20 INCHES RIGHT OF CENTERLINE. GROUNDED - YES. REMOVED 6EA FASTENERS IAW A320 SRM 51-42-11/001/REV 148-01FEB2024. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW A320 SRM 53-41-49-283-004 REV 148- 01FEB202
- [SDR ASAA2024032950030](https://openairdocs.org/sdr/ASAA2024032950030.md): Door Frame · corroded · Mar 29, 2024 · N855VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FLOOR DOOR FRAME FORWARD C53R. GROUNDED - YES. REMOVED 4EA FASTENERS IAW A320 SRM 51-42-11/001/REV 148-01FEB2024. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW A320 SRM 53-41-49-283-004 REV 148- 01FEB2024. ACCOMPLISHED DVI AND HFEC INSPECTION IA
- [SDR ASAA2024032950029](https://openairdocs.org/sdr/ASAA2024032950029.md): Web · corroded · Mar 29, 2024 · N855VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FLOOR ON DOOR FRAME CORRODED JUST AFT OF C54R 2 PLACES 24 INCHES RIGHT OF CENTER. GROUNDED - YES. REMOVED 2EA FASTENER IAW A320 SRM 51-42-11/001/REV 148-01FEB2024. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW A320 SRM 53-41-49-283-004 REV 148-
- [SDR ASAA2024032950005](https://openairdocs.org/sdr/ASAA2024032950005.md): Web · corroded · Mar 29, 2024 · N855VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FLOOR DOOR FRAME CORRODED FORWARD OF C54R 2 PLACES 24 INCHES RIGHT OF CENTER GROUNDED - YES. REMOVED 1EA FASTENER IAW A320 SRM 51-42-11/001/REV 148-01FEB2024. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW A320 SRM 53-41-49-283-004 REV 148- 01FEB2
- [SDR ASAA2024032950004](https://openairdocs.org/sdr/ASAA2024032950004.md): Web · corroded · Mar 29, 2024 · N855VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FLOOR JUST INSIDE DOOR NEAR AFT DOOR FRAME CORRODED AT AND AROUND NET MOUNT PUCK AT STATION 56R 20 INCHES RIGHT OF CENTER. GROUNDED - YES. REMOVED 1EA FASTENER IAW A320 SRM 51-42-11/001/REV 148-01FEB2024. REMOVED CORROSION AND FOUND WITHIN LIMITS
- [SDR ASAA2024032950003](https://openairdocs.org/sdr/ASAA2024032950003.md): Door Frame · corroded · Mar 29, 2024 · N855VA · Airbus A320214 · Fuselage Main, Structure
  > AFT CARGO BAY FLOOR ON DOOR FRAME CORRODED AT STATION C55R GROUNDED - YES. REMOVED 1EA FASTENER IAW A320 SRM 51-42-11/001/REV 148-01FEB2024. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW A320 SRM 53-41-49-283-004 REV 148- 01FEB2024. ACCOMPLISHED DVI AND HFEC I
- [SDR ASAA2024032950002](https://openairdocs.org/sdr/ASAA2024032950002.md): Torque Box · corroded · Mar 29, 2024 · N855VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FLOOR JUST INSIDE DOOR NEAR AFT DOOR FRAME CORRODED AT LOCK FASTENER, JUST FORWARD OF STATION C5624 INCHES RIGHT OF CENTERLINE GROUNDED - YES. REMOVED 3EA FASTENERS IAW A320 SRM 51-42-11/001/REV 148-01. REMOVED CORROSION AND FOUND WITHIN LIMITS I
- [SDR ASAA2024031550036](https://openairdocs.org/sdr/ASAA2024031550036.md): Skin · dented · Mar 15, 2024 · N855VA · Airbus A320214 · Trailing Edge Flaps
  > LESSOR ITEM: MULTIPLE LOWER FLAP DENTS BEHIND RIGHT MAIN WHEEL, MAP AND MEASURE ALL. GROUNDED - YES. PERFORMED CATEGORY A PERMANENT REPAIR IN 2EA AREAS ON R/W I/B FLAP LOWER SURFACE IN ZONE 2. AREA 1 REPAIR MEASURES 55" FROM I/B EDGE, 6" FROM T/E REPAIR DOUBLE
- [SDR ASAA2024031550035](https://openairdocs.org/sdr/ASAA2024031550035.md): Skin · dented · Mar 15, 2024 · N855VA · Airbus A320214 · Trailing Edge Flaps
  > LESSOR ITEM: MULTIPLE LOWER FLAP DENTS BEHIND LEFT MAIN WHEEL, MAP AND MEASURE ALL GROUNDED - YES. REPAIRED CLUSTER 1 DENTS ON L/W LOWER FLAP, FINAL MEASUREMENT OF REPAIR IS 14.4" X 11.4" LOCATED 45.25" FROM INBOARD AND STOPS 59.65". CLUSTER 2 IS BEING TRACK
- [SDR ASAA2022110140679](https://openairdocs.org/sdr/ASAA2022110140679.md): Skin · gouged · Nov 1, 2022 · N855VA · Airbus A320214 · Cargo/Baggage Doors
  > FWD CARGO DOOR, OUTER SKIN FWD EDGE BENT/DENT WITH A GOUGE IN THE MIDDLE AT 29" FROM LOWER EDGE. GROUNDED - YES. ACCOMPLISHED A CATEGORY "B" REPAIR ON THE FORWARD CARGO COMPARTMENT DOOR, PART # D5237175000800, SERIAL # UH15179 IAW ASA EA # CMPT-52EA-01622 REV
- [SDR VQIA2018F00018](https://openairdocs.org/sdr/VQIA2018F00018.md): Unknown · odor · Jan 8, 2018 · N855VA · Airbus A320214 · Air Distribution System
  > STRONG CHEMICAL ODOR LIKE BURNED HYDRAULIC FLUID OR OIL COMBINATION DURING TAKEOFF AND DESCENT. PERFORMED TSM 055000810831A, NO DEFECTS NOTED.
- [SDR VQIA2017F00060](https://openairdocs.org/sdr/VQIA2017F00060.md): Control Lever · failed · Oct 22, 2017 · N855VA · Airbus A320214 · Landing Gear Selector
  > ON 10/20/17 A/C N855VA OPERATING VX1067 AN AIRBUS A320-314 WITH 19772 FLT HOURS AND 5977 CYCLES HAD THE FOLLOWING DEFECT ON APPROACH TO SFO: LANDING GEAR WOULD NOT EXTEND WHEN HANDLE PLACED DOWN. PERFORMED MANUAL GEAR EXTENSION. CREW LANDED SAFELY AND DID N
- [SDR VQIA2017080900033](https://openairdocs.org/sdr/VQIA2017080900033.md): Fmc · failed · Mar 3, 2017 · N855VA · Airbus A320214 · Auto Flight System
  > ON SELECTING FLAPS 0 AFTER TAKEOFF, LOST FMA INFORMATION AND ENGS TRIED TO SLOW TO IDLE. RESET A/P & A/T, SYSTEMS NORMAL AFTER THAT, NO ECAM. PERFORMED OPS TEST OF AFS IAW AMM 22-96-00-71-00-01A, BITE TEST OF EFCS IAW AMM 27-96-00-74-00-01A. PERFORMED OPS
- [SDR VQI20140822000019](https://openairdocs.org/sdr/VQI20140822000019.md): Fan · failed · Aug 15, 2014 · N855VA · Airbus A320214 · Air Distribution Fan
  > ACFT ENCOUNTERED A VENT BLOWER FAULT IN FLIGHT, COMPLIED WITH ECAM. ELECTRICAL SMOKE FUMES WERE PERCEIVED FOR APPROXIMATELY 5 MINUTES. ON ARRIVAL, MAINTENANCE ACCOMPLISHED INSPECTION FOR ELECTRICAL SMOKE ODOR IAW TSM 05-50-00-810-831-A. VERIFIED INOPERATI

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N855VA' AND deregistration_id = 'N855VA-2024-07-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N855VA-2024-07-30/reports

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