# Service difficulty reports: N619AW, cancelled Mar 13, 2017

A list on [N619AW, cancelled Mar 13, 2017](https://openairdocs.org/deregistered/N619AW-2017-03-13.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 · 153 reports

- [SDR USAA2009031390594](https://openairdocs.org/sdr/USAA2009031390594.md): Cylinder · low pressure · Mar 13, 2009 · N619AW · Airbus A320232 · Passenger/Crew Doors
  > MIA - EES - FORWARD ENTRY DOOR OPEN ASSIST BOTTLE READS 800 PSI. SERVICED FORWARD ENTRY DOOR OPEN ASSIST BOTTLE IAW A320 AMM 52-10-00.
- [SDR USAA2009012690163](https://openairdocs.org/sdr/USAA2009012690163.md): Floorbeam · corroded · Jan 19, 2009 · N619AW · Airbus A320232 · Fuselage Main, Floor Beam
  > SAL - C3 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, -Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, -Y1292 IAW A320 SRM 51-72-11.
- [SDR USAA2009012690177](https://openairdocs.org/sdr/USAA2009012690177.md): Fitting · corroded · Jan 15, 2009 · N619AW · Airbus A320232 · Fuselage Miscellaneous Structure
  > SAL - C3 - MAJOR REPAIR - CORROSION ON FITTING AT FR59, S41R. REPLACED FITTING AT FR59, S41R IAW A320 SRM 51-72-11.
- [SDR USAA2009012690179](https://openairdocs.org/sdr/USAA2009012690179.md): Support · corroded · Jan 12, 2009 · N619AW · Airbus A320232 · Fuselage Main, Frame
  > SAL - C3 - MAJOR REPAIR - GALVANIC CORROSION ON FRAME SUPPORT BETWEEN FR69 TO FR70, S23R, -Y1300. REPLACED FRAME SUPPORT BETWEEN FR69 TO FR70, S23R, -Y1300 IAW A320 SRM 51-72-11.
- [SDR USAA2009012690180](https://openairdocs.org/sdr/USAA2009012690180.md): Floorbeam · corroded · Jan 11, 2009 · N619AW · Airbus A320232 · Fuselage Main, Floor Beam
  > SAL - C3 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR50 +10 INCHES, BL 0. REPLACED FLOORBEAM BETWEEN FR50 +10 INCHES, BL 0 IAW A320 SRM 51-42-11.
- [SDR USAA2009012690170](https://openairdocs.org/sdr/USAA2009012690170.md): Floorbeam · corroded · Jan 11, 2009 · N619AW · Airbus A320232 · Fuselage Main, Floor Beam
  > SAL - C3 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, Y1292 IAW A320 SRM 51-72-11.
- [SDR USAA2009012690165](https://openairdocs.org/sdr/USAA2009012690165.md): Floorbeam · corroded · Jan 11, 2009 · N619AW · Airbus A320232 · Fuselage Main, Floor Beam
  > SAL - C3 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, -Y1116. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, -Y1116 IAW A320 SRM 51-72-11.
- [SDR USAA2009012690181](https://openairdocs.org/sdr/USAA2009012690181.md): Shear Plate · corroded · Jan 11, 2009 · N619AW · Airbus A320232 · Fuselage Miscellaneous Structure
  > SAL - C3 - MAJOR REPAIR - CORROSION ON SHEAR PLATE BETWEEN FR62 TO FR63, S38L. REPLACED SHEAR PLATE BETWEEN FR62 TO FR63, S38L IAW A320 SRM 51-72-11.
- [SDR USAA2009012690176](https://openairdocs.org/sdr/USAA2009012690176.md): Plate · corroded · Jan 11, 2009 · N619AW · Airbus A320232 · Fuselage Miscellaneous Structure
  > SAL - C3 - MAJOR REPAIR - CORROSION ON FLUSH PLATE BETWEEN FR30 TO FR31, S41R. REPLACED FLUSH PLATE BETWEEN FR30 TO FR31, S41R IAW A320 SRM 51-72-11.
- [SDR USAA2009012690175](https://openairdocs.org/sdr/USAA2009012690175.md): Fitting · corroded · Jan 11, 2009 · N619AW · Airbus A320232 · Fuselage Miscellaneous Structure
  > SAL - C3 - MAJOR REPAIR - CORROSION ON CLEAT AT FR28, BETWEEN S40R TO S41R. REPLACED CLEAT AT FR28, BETWEEN S40R TO S41R IAW A320 SRM 51-72-11.
- [SDR USAA2009012690174](https://openairdocs.org/sdr/USAA2009012690174.md): Floorbeam · corroded · Jan 11, 2009 · N619AW · Airbus A320232 · Fuselage Main, Floor Beam
  > SAL - C3 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM ASSEMBLY AT FR65 +22 INCHES, Y512. REPLACED FLOORBEAM ASSEMBLY AT FR65 +22 INCHES, Y512 IAW A320 SRM 51-72-11.
- [SDR USAA2009012690173](https://openairdocs.org/sdr/USAA2009012690173.md): Shear Plate · corroded · Jan 11, 2009 · N619AW · Airbus A320232 · Fuselage Miscellaneous Structure
  > SAL - C3 - MAJOR REPAIR - GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23L. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23L IAW A320 SRM 51-72-11.
- [SDR USAA2009012690172](https://openairdocs.org/sdr/USAA2009012690172.md): Floorbeam · corroded · Jan 11, 2009 · N619AW · Airbus A320232 · Fuselage Main, Floor Beam
  > SAL - C3 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, Y312. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, Y312 IAW A320 SRM 51-72-11.
- [SDR USAA2009012690171](https://openairdocs.org/sdr/USAA2009012690171.md): Floorbeam · corroded · Jan 11, 2009 · N619AW · Airbus A320232 · Fuselage Main, Floor Beam
  > SAL - C3 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, Y1292 IAW A320 SRM 51-72-11.
- [SDR USAA2009012690169](https://openairdocs.org/sdr/USAA2009012690169.md): Sill · corroded · Jan 11, 2009 · N619AW · Airbus A320232 · Fuselage Miscellaneous Structure
  > SAL - C3 - MAJOR REPAIR - GALVANIC CORROSION ON LOWER SILL AT L2 DOOR, FR66, Y1732. REPAIRED LOWER SILL AT L2 DOOR, FR66, Y1732 IAW A320 SRM 53-41-14.
- [SDR USAA2009012690168](https://openairdocs.org/sdr/USAA2009012690168.md): Floorbeam · corroded · Jan 11, 2009 · N619AW · Airbus A320232 · Fuselage Main, Floor Beam
  > SAL - C3 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM ASSEMBLY BETWEEN FR68 TO FR70, -Y160. REPLACED FLOORBEAM ASSEMBLY BETWEEN FR68 TO FR70, -Y160 IAW A320 SRM 51-72-11.
- [SDR USAA2009012690167](https://openairdocs.org/sdr/USAA2009012690167.md): Seat Track · corroded · Jan 11, 2009 · N619AW · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > SAL - C3 - MAJOR REPAIR - GALVANIC CORROSION ON SEAT BEAM BETWEEN FR64 TO FR65, -Y765. REPAIRED SEAT BEAM BETWEEN FR64 TO FR65, -Y765 IAW A320 SRM 51-72-11.
- [SDR USAA2009012690166](https://openairdocs.org/sdr/USAA2009012690166.md): Shear Plate · corroded · Jan 11, 2009 · N619AW · Airbus A320232 · Fuselage Miscellaneous Structure
  > SAL - C3 - MAJOR REPAIR - GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23R, -Y1300. REPAIRED SHEAR PLATE BETWEEN FR69 TO FR70, S23R, -Y1300 IAW A320 SRM 51-72-11.
- [SDR USAA2009012690164](https://openairdocs.org/sdr/USAA2009012690164.md): Floorbeam · corroded · Jan 11, 2009 · N619AW · Airbus A320232 · Fuselage Main, Floor Beam
  > SAL - C3 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, -Y1292. REPAIRED FLOORBEAM BETWEEN FR66 TO FR68, -Y1292 IAW A320 SRM 53-00-14.
- [SDR USAA2009012690162](https://openairdocs.org/sdr/USAA2009012690162.md): Shear Plate · corroded · Jan 11, 2009 · N619AW · Airbus A320232 · Fuselage Miscellaneous Structure
  > SAL - C3 - MAJOR REPAIR - CORROSION ON SHEAR PLATE BETWEEN FR50 TO FR51, -Y690. REPLACED SHEAR PLATE BETWEEN FR50 TO FR51, -Y690 IAW A320 SRM 51-72-11.
- [SDR USAA2009012690178](https://openairdocs.org/sdr/USAA2009012690178.md): Fitting · corroded · Jan 10, 2009 · N619AW · Airbus A320232 · Fuselage Miscellaneous Structure
  > SAL - C3 - MAJOR REPAIR - GALVANIC CORROSION ON CLEAT AT FR32, BETWEEN S40R TO S41R. REPLACED CLEAT AT FR32, BETWEEN S40R TO S41R IAW A320 SRM 51-72-11.
- [SDR USAA2009012690161](https://openairdocs.org/sdr/USAA2009012690161.md): Seat Track · corroded · Jan 10, 2009 · N619AW · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > SAL - C3 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR41 TO FR47, -Y765. REPLACED SEAT TRACK BETWEEN FR41 TO FR47, -Y765 IAW A320 SRM 51-42-11 & AIRBUS DRAWING D53371110.
- [SDR USAA2009012690160](https://openairdocs.org/sdr/USAA2009012690160.md): Door Frame · cracked · Jan 10, 2009 · N619AW · Airbus A320232 · Fuselage Main, Structure
  > SAL - C3 - MAJOR REPAIR - CRACK ON WEB AT PASSENGER/CREW DOOR CUTOUT AT FR68 TO FR69, S23L. REPLACED WEB AT PASSENGER/CREW DOOR CUTOUT AT FR68 TO FR69, S23L IAW A320 SRM 51-72-11.
- [SDR USAA2009012690159](https://openairdocs.org/sdr/USAA2009012690159.md): Web · cracked · Jan 10, 2009 · N619AW · Airbus A320232 · Fuselage Miscellaneous Structure
  > SAL - C3 - MAJOR REPAIR - CRACK ON WEB AT PASSENGER/CREW DOOR CUTOUT AT FR68 + 12 INCHES, S23R. REPLACED WEB AT PASSENGER/CREW DOOR CUTOUT AT FR68 + 12 INCHES, S23R IAW A320 SRM 51-72-11.
- [SDR USAA2008120192158](https://openairdocs.org/sdr/USAA2008120192158.md): Wire · broken · Nov 28, 2008 · N619AW · Airbus A320232 · Light System Wiring
  > FLT 460 PHX-IND - EEL - EMERGENCY EXIT LIGHT SEAT 19 LT INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT EMERGENCY EXIT LIGHT SEAT 19 LT. OPERATIONAL CHECK GOOD.
- [SDR USAA920081753](https://openairdocs.org/sdr/USAA920081753.md): Battery · discharged · Sep 28, 2008 · N619AW · Airbus A320232 · Emergency Equipment
  > FLT NR 343 - PHX - FWD FLT ATTENDANT FLASHLIGHT STOPPED CHARGING. MX REMOVED AND REPLACED THE FWD FLT ATTENDANT FLASHLIGHT BATTERY. OPS CHECK GOOD.
- [SDR USAA920080513](https://openairdocs.org/sdr/USAA920080513.md): Control Arm · out of adjust · Feb 24, 2008 · N619AW · Airbus A320232 · Escape Slide
  > FLT NR 310, EMERGENCY EQUIP SLIDE AT R2 IS DISARMING WHILE IN FLIGHT. MAINTENANCE REPLACED THE R2 GIRT BAR. AFTER EXTENSIVE TROUBLESHOOTING, MAINTENANCE ADJUSTED THE VERTICAL CONTROL ROD OF ARMING LEVER, 3/4 TURN COMPLIED WITH TO TIGHTEN ARMING LEVER DOWN.
- [SDR USAA920080416](https://openairdocs.org/sdr/USAA920080416.md): Power Supply · discharged · Feb 12, 2008 · N619AW · Airbus A320232 · Emergency Lighting
  > FLT 274 - PHX-IAH - EEL - EMERGENCY LIGHT TEST FAILS - EMERGENCY POWER SUPPLY UNIT ARMED/ON LEFT AFT. MAINTENANCE REMOVED AND REPLACED THE LT AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONAL CHECK WAS GOOD.
- [SDR USAA920080415](https://openairdocs.org/sdr/USAA920080415.md): Slide Raft · defective · Feb 10, 2008 · N619AW · Airbus A320232 · Escape Slide
  > FLT 560 - PDX-LAS - EMERG EQUIP - R2 DOOR SLIDE ARMING LEVER POPPED OUT AFTER TAKEOFF. DOOR SHOWS DISARMED IN FLIGHT. ARMING LEVER STAYS OUT. MAINTENANCE REMOVED AND REPLACED THE AFT SLIDE RAFT ASSEMBLY IAW TASK CARD R1C25304.
- [SDR USAA920071343](https://openairdocs.org/sdr/USAA920071343.md): Actuator · faulty · Dec 13, 2007 · N619AW · Airbus A320232 · Leading Edge Slat Actuator
  > FLT 598 - PHL - LAS - EL - FLIGHT CONTROL SLATS FAULT/LOCKED ON APPROACH. FLAP LEVER RECYCLE PER ECAM UNSUCCESSFUL. CREW DECLARED AN EMERGENCY. PASSENGERS DID NOT BRACE. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED SLAT ACTUATOR ASSY P
- [SDR USAA920070870](https://openairdocs.org/sdr/USAA920070870.md): Pump · leaking · Sep 27, 2007 · N619AW · Airbus A320232 · Hydraulic Pump (Electric/Engine), Main
  > CREW REPORTED GREEN HYDRAULIC SYSTEM DRAINED DOWN CAUSING AN AMBER INDICATION WHEN GEAR WAS EXTENDED. CREW DECLARED AN EMERGENCY. THE LANDING WAS UNEVENTFUL. MX REPLACED THE NR 1 ENGINE HYDRAULIC PUMP. OPERATIONAL / LEAK CHECK WAS GOOD. OPEN
- [SDR AWXA200700570](https://openairdocs.org/sdr/AWXA200700570.md): Battery · failed · May 7, 2007 · N619AW · Airbus A320232 · Emergency Lighting
  > PHX - EEL - LEFT EMERGENCY EXIT LIGHT FAILS TEST. REPLACED AND OPERATIONAL CHECKED THE LEFT EMERGENCY LIGHT POWER SUPPLY BATTERY IAW AWA TASK CARD A1C33302.
- [SDR AWXA200700124](https://openairdocs.org/sdr/AWXA200700124.md): Door · malfunctioned · Jan 25, 2007 · N619AW · Airbus A320232 · Landing Gear Door Retract Section
  > MSP - ATB - DURING CLIMB-OUT, THE NOSE LANDING GEAR DOORS WOULD NOT CLOSE. THE CREW RETURNED TO MSP WITH OUT INCIDENT. A/C IS AOS IN MSP.
- [SDR AWXA200700123](https://openairdocs.org/sdr/AWXA200700123.md): Door · failed · Jan 25, 2007 · N619AW · Airbus A320232 · Landing Gear Door Retract Section
  > MSP - ATB - DURING CLIMB-OUT, THE NOSE LANDING GEAR DOORS WOULD NOT CLOSE. THE CREW RETURNED TO MSP WITHOUT INCIDENTA/C IS AOS IN MSP.
- [SDR AWXA200700032](https://openairdocs.org/sdr/AWXA200700032.md): Power Supply · inoperative · Jan 1, 2007 · N619AW · Airbus A320232 · Emergency Lighting
  > LAS - EEL - MX DISCOVERED EMERGENCY EXIT LIGHTS INOP LEFT OVERWING WALL AND CEILING. MX REPLACED THE EMERGENCY LIGHT POWER SUPPLY. OPS CHECK WAS GOOD.
- [SDR AWXA200602103](https://openairdocs.org/sdr/AWXA200602103.md): Fan · burned out · Dec 21, 2006 · N619AW · Airbus A320232 · Air Distribution Fan
  > PHX - THE CREW WAS DESCENDING THRU FL220 AND NOTICED A LOW FREQ VIBRATION (AVIONICS BAY) FOLLOWED BY TOXIC FUMES. THE CREW DONNED O2 MASKS. THE CREW RECEIVED AN EXTRACT FAN "FAULT" LIGHT. THE CREW DECLARED AN EMERGENCY. THE LANDING WAS UNEVENTFUL. MX REPL
- [SDR AWXA200601975](https://openairdocs.org/sdr/AWXA200601975.md): Unknown · odor · Nov 26, 2006 · N619AW · Airbus A320232 · Air Distribution System
  > PHX - BURNING SMELL, A STRONG ELECTRICAL SMELL REPORTED AND VERIFIED BY F/O. F/A'S REPORT A BURNING SENSATION IN EYES. SMELL DID NOT GO AWAY WITH GALLEY POWER OFF. NO SMOKE. MX INSPECTED AFT GALLEY APPLIANCES, LIGHTS, BALLASTS WIRING AND C/B'S. INSPECTED
- [SDR AWXA200601470](https://openairdocs.org/sdr/AWXA200601470.md): Wire · broken · Jul 26, 2006 · N619AW · Airbus A320232 · Light System Wiring
  > SAL - INOP EMERGENCY LIGHTS IN THE FOLLOWING POSITIONS SEAT ROWS 13, 17, 19, 22, AND 24. REPAIRED WIRING ON EMERGENCY LIGHTS IN THE FOLLOWING POSITIONS SEAT ROWS 13, 17, 19, 22, AND 24. THEN PERFORMED TEST OK AMM 33-51-00.
- [SDR AWXA200601437](https://openairdocs.org/sdr/AWXA200601437.md): Angle · cracked · Jul 26, 2006 · N619AW · Airbus A320232 · Fuselage Miscellaneous Structure
  > SAL - KEEL BEAM LT ATTACH ANGLE CRACKED JUST AFT OF MLG ANGLE LOC ON KEEL BEAM LT, JUST AFT OF MLG DOOR REPAIRED IAW A320 SRM 53-35-11 FIG 229 AND ER NR 26-5335-06205-HF4.
- [SDR AWXA200601430](https://openairdocs.org/sdr/AWXA200601430.md): Tube · damaged · Jul 25, 2006 · N619AW · Airbus A320232 · Landing Gear Doors
  > SAL - FOUND IMPACT DAMAGE ON OUTER CYLINDER LOWER EDGE OF NLG AT FWD AREA. REMOVED AND REPLACED BUSHED TURNING TUBE ASSY IAW WESSIER DOWTY CMM 32-27-18.
- [SDR AWXA200601438](https://openairdocs.org/sdr/AWXA200601438.md): Angle · cracked · Jul 24, 2006 · N619AW · Airbus A320232 · Fuselage Miscellaneous Structure
  > SAL - FOUND KEEL BEAM RT ATTACH ANGLE CRACKED JUST AFT OF MLG KEEL BEAM RT ATTACH ANGLE JUST AFT OF MLG DOOR WAS REPAIRED IAW SRM A320 53-35-11 PAGE 351/352 FIG 229 SHEET 1.
- [SDR AWXA200601435](https://openairdocs.org/sdr/AWXA200601435.md): Floor Panel · cracked · Jul 24, 2006 · N619AW · Airbus A320232 · Fuselage Floor Panel
  > SAL - THE FLOOR PANEL NR 151 FF IN AFT CARGO COMPARTMENT WAS FOUND WITH CRACKS. THE FLOOR PANEL NR 151 FF IN AFT CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-02-00 PAR 8C.
- [SDR AWXA200601434](https://openairdocs.org/sdr/AWXA200601434.md): Floorboard · delaminated · Jul 24, 2006 · N619AW · Airbus A320232 · Fuselage Floor Panel
  > SAL - FOUND DAMAGE FLOORBOARD 231 WF AT PASSENGER CABIN. FLOORBOARD 231 WF WAS REPLACED IAW SRM 53-02-00 TABLE 103 ZONE "A" PAR 8G, 8H AND IRM 9701 REV F.
- [SDR AWXA200601433](https://openairdocs.org/sdr/AWXA200601433.md): Floorboard · delaminated · Jul 24, 2006 · N619AW · Airbus A320232 · Fuselage Floor Panel
  > SAL - FOUND DAMAGE FLOORBOARD 252 MF AT PASSENGER CABIN. FLOORBOARD 252 MF WAS REPLACED IAW SRM 53-02-00 TABLE 103 ZONE "A" PAR 8G, 8H AND IRM 9701 REV F.
- [SDR AWXA200601432](https://openairdocs.org/sdr/AWXA200601432.md): Floorboard · delaminated · Jul 24, 2006 · N619AW · Airbus A320232 · Fuselage Floor Panel
  > SAL - FOUND DAMAGE FLOORBOARD NR 242 DF AT PASSENGER CABIN. FLOORBOARD NR 242 DF WAS REPLACED IAW SRM 53-02-00 TABLE 103 ZONE "A" PAR 8G, 8H, AND IRM 9701 REV I.
- [SDR AWXA200601429](https://openairdocs.org/sdr/AWXA200601429.md): Floorboard · delaminated · Jul 24, 2006 · N619AW · Airbus A320232 · Fuselage Floor Panel
  > SAL - FOUND DAMAGED FLOORBOARD NR 251 GF AT PASSENGER CABIN. FLOORBOARD NR 251 GF WAS REPLACED IAW SRM 53-02-00 TABLE 103 ZONE "A" PAR 8G, 8H AND IRM 9701 REV F.
- [SDR AWXA200601428](https://openairdocs.org/sdr/AWXA200601428.md): Floorboard · delaminated · Jul 24, 2006 · N619AW · Airbus A320232 · Fuselage Floor Panel
  > SAL - FOUND DAMAGE FLOOR BOARD NR 231 VF AT PASSENGER CABIN. FLOORBOARD NR 231 VF WAS REPLACED IAW SRM 53-02-00 ZONE "A" PAR 8G 8H AND IRM 9701 REV. F.
- [SDR AWXA200601427](https://openairdocs.org/sdr/AWXA200601427.md): Floorboard · delaminated · Jul 24, 2006 · N619AW · Airbus A320232 · Fuselage Floor Panel
  > SAL - FOUND DAMAGE FLOORBOARD NR 242 BF AT PASSENGER CABIN. FLOORBOARD NR 242 BF WAS REPLACED IAW SRM 53-02-00 TABLE 103 ZONE "A" PAR 8G, 8H AND IRM 9701 REV. F.
- [SDR AWXA200601425](https://openairdocs.org/sdr/AWXA200601425.md): Floorboard · delaminated · Jul 24, 2006 · N619AW · Airbus A320232 · Fuselage Floor Panel
  > SAL - DAMAGE FLOORBOARD NR 242 LF AT PASSENGER CABIN. FLOORBOARD NR 242 LF WAS REPLACED IAW SRM 53-02-00 TABLE 103 ZONE "A" PAR 8G, 8H AND IRM 9701 REV I.
- [SDR AWXA200601424](https://openairdocs.org/sdr/AWXA200601424.md): Floorboard · delaminated · Jul 24, 2006 · N619AW · Airbus A320232 · Fuselage Floor Panel
  > SAL - FOUND DAMAGE FLOORBOARD NR 251 LF AT PASSENGER CABIN. FLOORBOARD NR 251 LF WAS REPLACED IAW SRM 53-02-00 TABLE 103 ZONE "A" PAR 8G 8H AND IRM 9701 REV. I.

Next page: https://openairdocs.org/deregistered/N619AW-2017-03-13/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 = 'N619AW' AND deregistration_id = 'N619AW-2017-03-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N619AW-2017-03-13/reports

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