# Service difficulty reports: N620AW, cancelled Jun 18, 2015

A list on [N620AW, cancelled Jun 18, 2015](https://openairdocs.org/deregistered/N620AW-2015-06-18.md).

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

Page 1 of 4 · 195 reports

- [SDR USAA2014081500005](https://openairdocs.org/sdr/USAA2014081500005.md): Bottle · low pressure · Aug 14, 2014 · N620AW · Airbus A320231 · Passenger/Crew Doors
  > L2 DOOR ASSIST BOTTLE LOW. SERVICED L2 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001-A.
- [SDR USAA2014052700043](https://openairdocs.org/sdr/USAA2014052700043.md): Cylinder · low pressure · May 23, 2014 · N620AW · Airbus A320231 · Passenger/Crew Doors
  > L2 DOOR ASSIST BOTTLE PRESS LOW. SERVICED L2 DOOR ASSIST BOTTLE.
- [SDR USAA2014050200003](https://openairdocs.org/sdr/USAA2014050200003.md): Hinge Fitting · chafed · May 1, 2014 · N620AW · Airbus A320231 · Landing Gear Doors
  > C1 CHECK CHAFING DAMAGE ON LT MLG FWD DOOR HINGE FITTING APPROX 3 INCHES AFT OF LE AT DOOR ACTUATOR ATTACH POINT UPPER END. REPLACED LT MLG FWD DOOR HINGE FITTING IAW SRM 51-72-11.
- [SDR USAA2014042800018](https://openairdocs.org/sdr/USAA2014042800018.md): Shear Plate · cracked · Apr 27, 2014 · N620AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > C1 CHECK CRACK ON SHEAR PLATE TRAY BETWEEN FRAME 68 TO FRAME 69, Z-500, -Y 1292. REPLACED SHEAR PLATE TRAY BETWEEN FRAME 68 TO FRAME 69, Z-500, -Y 1292 IAW SRM 51-72-11 & DWG D53480020.
- [SDR USAA2014042500010](https://openairdocs.org/sdr/USAA2014042500010.md): Stringer · corroded · Apr 25, 2014 · N620AW · Airbus A320231 · Fuselage Main, Longeron/Stringer
  > C1 CHECK CORROSION ON FUSELAGE STRINGER 26R BETWEEN FRAME 65 TO FRAME 66. REPAIRED FUSELAGE STRINGER 26R BETWEEN FRAME 65 TO FRAME 66 IAW EA 207361.
- [SDR USAA2014042500006](https://openairdocs.org/sdr/USAA2014042500006.md): Floor Panel · delaminated · Apr 24, 2014 · N620AW · Airbus A320231 · Fuselage Floor Panel
  > C1 CHECK DELAMINATION ON FLOOR PANEL 231CF BETWEEN FRAME 20 TO FRAME 24, -Z500 & BETWEEN Y 254 TO Y 765. REPLACED FLOOR PANEL 231CF IAW 9701, REV G.
- [SDR USAA2014042500005](https://openairdocs.org/sdr/USAA2014042500005.md): Floor Panel · delaminated · Apr 24, 2014 · N620AW · Airbus A320231 · Fuselage Floor Panel
  > C1 CHECK DELAMINATION ON FLOOR PANEL 222EF BETWEEN FRAME 16 TO FRAME 20, -Z500 & BETWEEN -Y 345 TO -Y 1292. REPLACED FLOOR PANEL 222EF IAW 9701, REV G.
- [SDR USAA2014042400010](https://openairdocs.org/sdr/USAA2014042400010.md): Floor Support · corroded · Apr 23, 2014 · N620AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > C1 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BETWEEN FRAME 51 TO FRAME 52, STRINGER 38L, -Z 1970. REPLACED FLOOR SUPPORT BETWEEN FRAME 51 TO FRAME 52, STRINGER 38L, -Z1970 IAW SRM 51-42-11, 51-72-11 & 51-75-12 & DRAWING D53470321.
- [SDR USAA2014042400009](https://openairdocs.org/sdr/USAA2014042400009.md): Floor Support · corroded · Apr 23, 2014 · N620AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > C1 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BETWEEN FRAME 49 TO FRAME 50, STRINGER 38L, -Z 1970. REPLACED FLOOR SUPPORT BETWEEN FRAME 49 TO FRAME 50, STRINGER 38L, -Z 1970 IAW SRM 51-42-11, 51-72-11 & 51-1-75-12 & DWG D53470321.
- [SDR USAA2014050700001](https://openairdocs.org/sdr/USAA2014050700001.md): Shear Web · cracked · Apr 22, 2014 · N620AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > BC1 CHECK SHEAR WEB CRACKED BETWEEN FRAME 68 & FRAME 69 AT Y 1732 & Z -500. FABRICATED & INSTALLED NEW SHEAR WEB IAW SRM 51-72-00 & DWG D53480020.
- [SDR USAA2014042100030](https://openairdocs.org/sdr/USAA2014042100030.md): Panel · corroded · Apr 20, 2014 · N620AW · Airbus A320231 · Wing, Plate/Skin
  > C1 CHECK LEVEL 2 GALVANIC CORROSION ON RT WING LOWER FUEL PANEL 640HB BETWEEN WING RIB 13 TO WING RIB 14 & BETWEEN STRINGER 8R TO STRINGER 11R. REPLACED RT WING LOWER FUEL PANEL 640HB BETWEEN WING RIB 13 TO WING RIB 14 & BETWEEN STRINGER 8R TO STRINGER 11R IA
- [SDR USAA2014042100026](https://openairdocs.org/sdr/USAA2014042100026.md): Stringer · corroded · Apr 19, 2014 · N620AW · Airbus A320231 · Fuselage Main, Longeron/Stringer
  > C1 CHECK LEVEL 2 EXFOLIATION CORROSION ON STRINGER BETWEEN FRAME 65 TO FRAME 66, STRINGER 25R, Z-575. REPLACED STRINGER SECTION BETWEEN FRAME 65 TO FRAME 66, STRINGER 25R, Z-575 IAW SRM 51-72-11 & 51-74-00.
- [SDR USAA2014042800017](https://openairdocs.org/sdr/USAA2014042800017.md): Floorbeam · corroded · Apr 18, 2014 · N620AW · Airbus A320231 · Fuselage Main, Floor Beam
  > C1 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FRAME 67, Z-500, -Y 1162.5. REPLACED FLOORBEAM AT FRAME 67, Z-500, -Y 1162.5 IAW SRM 51-72-11 & DWG 17D53472000 & 18D5347208.
- [SDR USAA2014042400014](https://openairdocs.org/sdr/USAA2014042400014.md): Floorbeam · corroded · Apr 18, 2014 · N620AW · Airbus A320231 · Fuselage Main, Floor Beam
  > C1 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FRAME 66, Z-500, Y 1292. REPLACED FLOORBEAM AT FRAME 66, Z-500, Y 1292 IAW SRM 53-41-14, 53-00-14, 51-20-00 & DWG D53472000.
- [SDR USAA2014042400012](https://openairdocs.org/sdr/USAA2014042400012.md): Floorbeam · corroded · Apr 18, 2014 · N620AW · Airbus A320231 · Fuselage Main, Floor Beam
  > C1 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FRAME 68, Z-500, Y 1162.5. REPLACED FLOORBEAM AT FRAME 68, Z-500, Y 1162.5 IAW SRM 53-00-14, 53-41-14 & DWG D53472000.
- [SDR USAA2014042400011](https://openairdocs.org/sdr/USAA2014042400011.md): Floorbeam · corroded · Apr 18, 2014 · N620AW · Airbus A320231 · Fuselage Main, Floor Beam
  > C1 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FRAME 66 TO FRAME 68, Z-500 & -Y 1162.5. REPLACED FLOORBEAM BETWEEN FRAME 66 TO FRAME 68, Z -500, -Y 1162.5 IAW A320 SRM 53-00-14, 53-41-14 & DWG D53472000.
- [SDR USAA2014042200006](https://openairdocs.org/sdr/USAA2014042200006.md): Shear Plate · cracked · Apr 18, 2014 · N620AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > C1 CHECK CRACK IN RT LATERAL SHEAR PLATE BETWEEN FRAME 69 TO FRAME 70, Z-500 & -Y1292. REPLACED RT LATERAL SHEAR PLATE BETWEEN FRAME 69 TO FRAME 70, Z-500 & -Y1292 IAW SRM 51-72-11.
- [SDR USAA2014042100028](https://openairdocs.org/sdr/USAA2014042100028.md): Shear Plate · cracked · Apr 18, 2014 · N620AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > C1 CHECK CRACK ON LT LATERAL SHEAR PLATE BETWEEN FRAME 69 TO FRAME 70, Z-500, Y 1162.5. REPLACED LT LATERAL SHEAR PLATE BETWEEN FRAME 69 TO FRAME 70, Z-500, Y 1162.5 IAW SRM 51-72-11 & DWG D53474180.
- [SDR USAA2014042800016](https://openairdocs.org/sdr/USAA2014042800016.md): Sill · corroded · Apr 16, 2014 · N620AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > C1CHECK, LEVEL 2 EXFOLIATION CORROSION ON SILL PLATE BETWEEN FRAME 66 TO FRAME 68, Z-500, -Y 1162.5. REPLACED SILL PLATE BETWEEN FRAME 66 TO FRAME 68, Z-500, -Y 1162.5 IAW SRM 51-72-11.
- [SDR USAA2014042400013](https://openairdocs.org/sdr/USAA2014042400013.md): Floorbeam · corroded · Apr 16, 2014 · N620AW · Airbus A320231 · Fuselage Main, Floor Beam
  > C1 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FRAME 66, Z-500, -Y 464.8. REPLACED FLOORBEAM AT FRAME 66, Z-500, -Y 464.8 IAW SRM 51-72-11.
- [SDR USAA2014042100029](https://openairdocs.org/sdr/USAA2014042100029.md): Seat Track · corroded · Apr 16, 2014 · N620AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > C1 CHECK LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BEAM BETWEEN FRAME 64 TO FRAME 66+8 INCHES, Z-500 & -Y 765. REPLACED SEAT TRACK BEAM BETWEEN FRAME 64 TO FRAME 66+8 INCHES, Z-500 & -Y 765 IAW SRM 51-72-11.
- [SDR USAA2014042100027](https://openairdocs.org/sdr/USAA2014042100027.md): Sill · corroded · Apr 16, 2014 · N620AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > C1 CHECK LEVEL 2 SURFACE CORROSION ON AFT LOWER CORNER SHAPE SILL ON LT PAX & CREW DOOR CUT OUT BETWEEN FRAME 66 TO FRAME 68, Z-500, Y 1584. REPLACED AFT LOWER CORNER SHAPE SILL BETWEEN FRAME 66 TO FRAME 68, Z-500, Y 1584 IAW SRM 51-72-11.
- [SDR USAA2014031700020](https://openairdocs.org/sdr/USAA2014031700020.md): Splice · defective · Mar 16, 2014 · N620AW · Airbus A320231 · Light System Wiring
  > FOUND EMERGENCY EXIT LIGHTS AT ROW 7 NOT WORKING. REPLACED PIN SPLICE FOR EMERGENCY EXIT LIGHTS AT ROW 7 IAW A320N ESPM 20-48-25, OPERATIONS CHECKED GOOD.
- [SDR USAA2014031300007](https://openairdocs.org/sdr/USAA2014031300007.md): Power Supply · faulty · Mar 12, 2014 · N620AW · Airbus A320231 · Emergency Lighting
  > AFT EMERGENCY POWER SUPPLY SHOWS INTERNAL FAULT. REPLACED AFT EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-38.
- [SDR USAA2014030300003](https://openairdocs.org/sdr/USAA2014030300003.md): Lens · missing · Mar 1, 2014 · N620AW · Airbus A320231 · Emergency Lighting
  > FORWARD LT FIRST CLASS WINDSCREEN MISSING RED EMERGENCY LIGHT LENS. REPLACED FWD LT FIRST CLASS WINDSCREEN RED EMERGENCY LIGHT LENS.
- [SDR USAA2014021900008](https://openairdocs.org/sdr/USAA2014021900008.md): Floor Panel · damaged · Feb 16, 2014 · N620AW · Airbus A320231 · Fuselage Floor Panel
  > REGULAR OVERNIGHT VISIT, CARGO FLOOR PANEL AT BS 2616 BETWEEN STRINGER 38L & STRINGER 38R HAS A 1 INCH X 1 INCH PIECE OF MISSING HONEYCOMB CORE AT Y +763. R & R FLOOR PANEL IAW A320 AMM 53-42-14-400-001-A.
- [SDR USAA2014021800004](https://openairdocs.org/sdr/USAA2014021800004.md): Floor Panel · delaminated · Feb 14, 2014 · N620AW · Airbus A320231 · Fuselage Floor Panel
  > REGULAR OVERNIGHT VISIT DELAMINATION ON THE CORNER OF AFT CARGO FLOOR PANEL AT BS 2616, STRINGER 38R & -Y 765. REPLACED AFT CARGO FLOOR PANEL AT BS 2616, STRINGER 38R &, -Y 765 IAW A320 AMM 53-42-14-400-001-A.
- [SDR USAA2014021700024](https://openairdocs.org/sdr/USAA2014021700024.md): Floor Support · missing · Feb 14, 2014 · N620AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > REGULAR OVERNIGHT VISIT, AFT CARGO COMPARTMENT FLOOR PANEL CROSS BEAM SUPPORT HAS PIECE OF MATERIAL MISSING AT FRAME 56, STRINGER 38R & -Y9.5. REPLACED AFT CARGO COMPARTMENT FLOOR PANEL CROSS BEAM SUPPORT AT FRAME 56, STRINGER 38R & -Y9.5 IAW A320 SRM 51-42-1
- [SDR USAA2014020600004](https://openairdocs.org/sdr/USAA2014020600004.md): Battery · discharged · Feb 5, 2014 · N620AW · Airbus A320231 · Emergency Equipment
  > FORWARD FLIGHT ATTENDANT FLASHLIGHT BATTERY LOW. REPLACED FWD FLIGHT ATTENDANT FLASHLIGHT BATTERY.
- [SDR USAA2014020300004](https://openairdocs.org/sdr/USAA2014020300004.md): Floor Panel · delaminated · Feb 1, 2014 · N620AW · Airbus A320231 · Fuselage Floor Panel
  > RON VISIT DELAMINATION ON FLOOR PANEL 232FF & CORROSION ON INSERTS BETWEEN FRAME 20 TO FRAME 24, STRINGER 23R - Y 1292. REPLACED FLOOR PANEL 232FF IAW AMM 53-12-12-400-001.
- [SDR USAA2014020300006](https://openairdocs.org/sdr/USAA2014020300006.md): Floor Support · corroded · Jan 30, 2014 · N620AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > RON VISIT CORROSION ON FLOOR SUPPORT AT FRAME 20, STRINGER 23R, - Y 1030. REPLACED FLOOR SUPPORT AT FRAME 20, STRINGER 23R - Y 1030 IAW SRM 51-42-11 & DWG D53112669.
- [SDR USAA2014013100007](https://openairdocs.org/sdr/USAA2014013100007.md): Gust Lock · cracked · Jan 30, 2014 · N620AW · Airbus A320231 · Passenger/Crew Doors
  > L1 DOOR GUST LOCK BUTTON CRACKED FOUND WHEN ATTEMPTING TO ROB FOR ACFT. REPLACED L1 DOOR GUST LOCK BUTTON IAW AMM 52-11-12-000-802A STEP 4 A1-3 & INSTALLED IAW AMM 52-11-12-400-802A STEP 4 A 4-7. OPERATIONS CHECKED GOOD.
- [SDR USAA2014020300008](https://openairdocs.org/sdr/USAA2014020300008.md): Floor Support · corroded · Jan 28, 2014 · N620AW · Airbus A320231 · Fuselage Miscellaneous Structure
  > RON VISIT CORROSION ON FLOOR SUPPORT AT FRAME 20, STRINGER 23R - Y 1292. REPLACED FLOOR SUPPORT AT FRAME 20, STRINGER 23R - Y 1292 IAW SRM 51-42-11.
- [SDR USAA2014020300007](https://openairdocs.org/sdr/USAA2014020300007.md): Seat Track · corroded · Jan 28, 2014 · N620AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > RON VISIT CORROSION ON SEAT TRACK AT FRAME 20, STRINGER 23R - Y 1292. REPLACED SEAT TRACK AT FRAME 20, STRINGER 23R - Y 1292 IAW SRM 51-42-11.
- [SDR USAA2014020300005](https://openairdocs.org/sdr/USAA2014020300005.md): Seat Track · corroded · Jan 28, 2014 · N620AW · Airbus A320231 · Fuselage, Seat/Cargo Attach Fittings
  > RON VISIT CORROSION ON SEAT TRACK AT FRAME 20, STRINGER 23R - Y 765. REPLACED SEAT TRACK AT FRAME20, STRINGER 23R - Y 765 IAW SRM 51-42-11.
- [SDR USAA2013120900008](https://openairdocs.org/sdr/USAA2013120900008.md): Lens · missing · Dec 7, 2013 · N620AW · Airbus A320231 · Emergency Lighting
  > ROW 22L EMERGENCY LIGHT LENS MISSING. INSTALLED NEW ROW 22L EMERGENCY LIGHT LENS.
- [SDR USAA2013111300028](https://openairdocs.org/sdr/USAA2013111300028.md): Floor Panel · damaged · Nov 9, 2013 · N620AW · Airbus A320231 · Fuselage Floor Panel
  > FORWARD CARGO BAY FORWARD EDGE CENTER FLOOR PANEL 131EF UPPER SKIN DAMAGED. REPLACED FLOOR PANEL IAW AMM 53-22-14.
- [SDR USAA2013111200005](https://openairdocs.org/sdr/USAA2013111200005.md): Floor Panel · delaminated · Nov 9, 2013 · N620AW · Airbus A320231 · Fuselage Floor Panel
  > CARGO FLOOR PANEL 132FF DELAMINATED. R & R FLOOR PANEL IAW AMM 53-22-14.
- [SDR USAA2013092400007](https://openairdocs.org/sdr/USAA2013092400007.md): Lens · missing · Sep 23, 2013 · N620AW · Airbus A320231 · Emergency Lighting
  > COVER FOR EMERGENCY EXIT LIGHT ACFT RT REAR DOOR MISSING. REPLACED MISSING EMERGENCY LIGHT COVER AT DOOR L-2.
- [SDR USAA2013091600003](https://openairdocs.org/sdr/USAA2013091600003.md): Lens · missing · Sep 15, 2013 · N620AW · Airbus A320231 · Emergency Lighting
  > EMERGENCY LIGHT LENS AT SEAT ROW 19L IS MISSING. INSTALLED AISLE EMERGENCY LIGHT LENS AT SEAT ROW 19L.
- [SDR USAA2013081900004](https://openairdocs.org/sdr/USAA2013081900004.md): Lens · missing · Aug 17, 2013 · N620AW · Airbus A320231 · Emergency Lighting
  > EMERGENCY EXIT LIGHT LENS MISSING ON SEAT ROW 5. REPLACED LENS SEAT ROW 5.
- [SDR USAA2013081300008](https://openairdocs.org/sdr/USAA2013081300008.md): Lens · missing · Aug 12, 2013 · N620AW · Airbus A320231 · Emergency Lighting
  > RED LENS ON L2 DOOR EMERGENCY LIGHT MISSING. REPLACED LENS.
- [SDR USAA2013042500004](https://openairdocs.org/sdr/USAA2013042500004.md): Overwing Exit · not seated · Apr 24, 2013 · N620AW · Airbus A320231 · Emergency Exits
  > SLIDE ARMED LIGHT OVERWING EXIT DOORS DOES NOT SHOW ARMED ON ECAM. REMOVED AND RE-INSTALLED RIGHT AFT OVERWING EXIT DOOR, OPERATIONAL CHECK GOOD REFERENCE AIRBUS MAINTENANCE MANUAL 52-21-11.
- [SDR USAA2012112600007](https://openairdocs.org/sdr/USAA2012112600007.md): Lens · missing · Nov 24, 2012 · N620AW · Airbus A320231 · Emergency Lighting
  > DOOR 1L FIRST CLASS PARTITION LIGHT COVER MISSING. REPLACED EMERGENCY EXIT LIGHT LENS.
- [SDR USAA2012111900017](https://openairdocs.org/sdr/USAA2012111900017.md): Bottle · low pressure · Nov 18, 2012 · N620AW · Airbus A320231 · Passenger/Crew Doors
  > L1 DOOR ASSIST BOTTLE LOW PRESSURE. SERVICED L1 DOOR ASSIST BOTTLE TO PROPER PRESSURE.
- [SDR USAA2012101100009](https://openairdocs.org/sdr/USAA2012101100009.md): Unknown · malfunctioned · Oct 10, 2012 · N620AW · Airbus A320231 · Interphone/Passenger Announcement (PA) System
  > C2 CHECK - EVACUATION SIGNALING SYSTEM FAILS OPERATIONAL TEST. NO RESPONSE TO COMMAND SWITCH. REPROGRAMMED CABIN LAYOUT SELECTION PERCENTAGE, PERFORMED OPERATIONAL TEST OF THE EMERGENCY EVACUATION SIGNALING SYSTEM (EVAC) IAW A320 AMM 23-73-00 & 23-73-00-860-
- [SDR USAA2012101600014](https://openairdocs.org/sdr/USAA2012101600014.md): Damper · low pressure · Oct 8, 2012 · N620AW · Airbus A320231 · Service Doors
  > BC2 CHECK - R2 DOOR OPEN ASSIST CYLINDER READ 0 PSI, UPON AIRCRAFT ARRIVAL. SERVICED R2 DOOR DAMPER & EMERGENCY OPERATIONS CYLINDER IAW A320 AMM 52-10-00.
- [SDR USAA2012100900028](https://openairdocs.org/sdr/USAA2012100900028.md): Housing · broken · Oct 8, 2012 · N620AW · Airbus A320231 · Emergency Lighting
  > BC2 CHECK - PAX SEAT 22ABC EMERGENCY LIGHT HOUSING BROKEN. REPLACED EMERGENCY LIGHT HOUSING AT PAX SEAT 22ABC IAW A320 SRM 51-42-11.
- [SDR USAA2012100900027](https://openairdocs.org/sdr/USAA2012100900027.md): Housing · broken · Oct 8, 2012 · N620AW · Airbus A320231 · Emergency Lighting
  > BC2 CHECK - PAX SEAT 7ABC EMERGENCY LIGHT HOUSING BROKEN. REPLACED EMERGENCY LIGHT HOUSING AT PAX SEAT 7ABC IAW A320 SRM 51-42-11.
- [SDR USAA2012100500007](https://openairdocs.org/sdr/USAA2012100500007.md): Diaphragm · unserviceable · Oct 4, 2012 · N620AW · Airbus A320231 · Passenger/Crew Doors
  > BC2 CHECK - L2 DOOR OPEN ASSIST CYLINDER READS ZERO PSI. REMOVED DIAPHRAGM ON THE L2 DOOR OPEN ASSIST CYLINDER FOUND TO BE UNSERVICABLE. INSTALLED NEW DIAPHRAGM IAW A320 AMM 52-10-00-610-001-14 SERVICED IAW A320 AMM 52-10-00-614-001-A, NO LEAKS NOTED.

Next page: https://openairdocs.org/deregistered/N620AW-2015-06-18/reports.md?page=2

## 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 = 'N620AW' AND deregistration_id = 'N620AW-2015-06-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N620AW-2015-06-18/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.