# Service difficulty reports: N424US, cancelled Feb 11, 2022

A list on [N424US, cancelled Feb 11, 2022](https://openairdocs.org/deregistered/N424US-2022-02-11.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 · 179 reports

- [SDR USAA2013041900005](https://openairdocs.org/sdr/USAA2013041900005.md): Battery Pack · discharged · Apr 18, 2013 · N424US · Boeing 737401 · Emergency Lighting
  > SHORT TERM STORAGE. EMERGENCY EXIT LIGHT OVER L-2 DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW B737 AMM REF 33-51-51. EMERGENCY EXIT LIGHT OVER L2 DOOR, OPS CHECK NORMAL.
- [SDR USAA2013041800006](https://openairdocs.org/sdr/USAA2013041800006.md): Battery Pack · discharged · Apr 17, 2013 · N424US · Boeing 737401 · Emergency Lighting
  > SHORT TERM STORAGE. AFT GALLEY EMERGENCY EXIT LIGHT INOP (CTR). REMOVED AND REPLACED BATTERY PACK M1197 FOR AFT GALLEY LIGHT (CTR) IAW B737 AMM 33-51-51. OPS CHECK NORMAL.
- [SDR USAA2013041800005](https://openairdocs.org/sdr/USAA2013041800005.md): Battery Pack · discharged · Apr 17, 2013 · N424US · Boeing 737401 · Emergency Lighting
  > SHORT TERM STORAGE. RIGHT AFT GALLEY DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK M1197 FOR RIGHT AFT GALLEY DOOR EMERGENCY EXIT LIGHT IAW B737 AMM 33-51-51, OPS CHECK NORMAL.
- [SDR USAA2013041800004](https://openairdocs.org/sdr/USAA2013041800004.md): Battery Pack · discharged · Apr 17, 2013 · N424US · Boeing 737401 · Emergency Lighting
  > SHORT TERM STORAGE. LEFT AFT GALLEY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK M1137 LEFT AFT GALLEY DOOR EMERGENCY LIGHT IAW B-737 AMM 33-51-5,1 OPS CHECK NORMAL.
- [SDR USAA2013012800029](https://openairdocs.org/sdr/USAA2013012800029.md): Support Fitting · cracked · Jan 23, 2013 · N424US · Boeing 737401 · Fuselage, Landing Gear Attach Fittings
  > C2 CHECK - CRACK ON RIGHT MAIN LANDING GEAR SUPPORT FITTING IN THE NR 2 HOLE AT WL 160. REPLACED RIGHT MAIN LANDING GEAR SUPPORT FITTING IAW EO 5702V054.
- [SDR USAA2012101200017](https://openairdocs.org/sdr/USAA2012101200017.md): Light · unsecure · Oct 12, 2012 · N424US · Boeing 737401 · Emergency Lighting
  > CREW REPORTED THE EMERGENCY LIGHT AT ROW 4ABC HANGING DOWN. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY AT ROW 4ABC. LIGHT OPS CHECK GOOD.
- [SDR USAA2012082800009](https://openairdocs.org/sdr/USAA2012082800009.md): Wire · broken · Aug 27, 2012 · N424US · Boeing 737401 · Light System Wiring
  > MAINTENANCE REPORTED SEAT 13C AND 24C EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND BROKEN WIRES AT SEAT 13C AND 24C. REPAIRED WITH SPLICE AND OPS CHECK OK.
- [SDR USAA2012072500005](https://openairdocs.org/sdr/USAA2012072500005.md): Cover · unsecure · Jul 24, 2012 · N424US · Boeing 737401 · Emergency Lighting
  > CREW REPORTED THE EMERGENCY EXIT LIGHT COVER ON SEAT 12C CAME OFF. MAINTENANCE RE-INSTALLED EMERGENCY EXIT LIGHT AT SEAT 12C. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.
- [SDR USAA2012072500004](https://openairdocs.org/sdr/USAA2012072500004.md): Sign · unsecure · Jul 24, 2012 · N424US · Boeing 737401 · Emergency Lighting
  > CREW REPORTED THE EXIT SIGN OVER SEAT 12ABC NEEDS RE-ATTATCHED. MAINTENANCE RE-INSTALLED EMERGENCY EXIT SIGN AS REQUIRED. AIRCRAFT OK FOR SERVICE.
- [SDR USAA2012070200033](https://openairdocs.org/sdr/USAA2012070200033.md): Door Frame · cracked · Jul 1, 2012 · N424US · Boeing 737401 · Service Doors
  > Q4 CHECK - FORWARD SERVICE DOOR FRAME CRACKED FROM LOWER HOLE AT BS 328. REMOVED AND REPLACED DOOR.
- [SDR USAA2012070200032](https://openairdocs.org/sdr/USAA2012070200032.md): Skin · delaminated · Jun 30, 2012 · N424US · Boeing 737401 · Leading Edge Devices
  > Q4 CHECK - NR 2 SLAT TRAILING EDGE WEDGE UPPER SKIN DELAMINATED AT INBOARD END (7 IN X 5 IN AREA). REPAIRED SKIN IAW B737 SRM 51-70-10.
- [SDR USAA2012070200031](https://openairdocs.org/sdr/USAA2012070200031.md): Skin · delaminated · Jun 30, 2012 · N424US · Boeing 737401 · Leading Edge Devices
  > Q4 CHECK - NR 3 SLAT TRAILING EDGE UPPER SKIN DELAMINATED AT INBOARD END (3 IN X 3 IN AREA). REPAIRED SKIN IAW B737 SRM 51-70-10.
- [SDR USAA2012070200030](https://openairdocs.org/sdr/USAA2012070200030.md): Frame · corroded · Jun 30, 2012 · N424US · Boeing 737401 · Rudder, Spar/Rib
  > Q4 CHECK - RUDDER RIGHT SIDE CONDUCTIVE FRAME CORRODED AT RUDDER STA 234.89. REMOVED FRAME, FABRICATED AND INSTALLED NEW FRAME IAW BOEING DRAWING 65C31496 AND EA 104047.
- [SDR USAA2012070200029](https://openairdocs.org/sdr/USAA2012070200029.md): Stringer Clip · cracked · Jun 30, 2012 · N424US · Boeing 737401 · Fuselage Main, Attach Fittings
  > Q4 CHECK - STRINGER TIE CLIP CRACKED AT BS F294, S23L. REMOVED CLIP, FABRICATED AND INSTALLED NEW CLIP IAW BOEING 737 SRM 51-20-01 AND BOEING DRAWING BAC 69-37271.
- [SDR USAA2012061900010](https://openairdocs.org/sdr/USAA2012061900010.md): Angle · corroded · Jun 17, 2012 · N424US · Boeing 737401 · Fuselage Miscellaneous Structure
  > Q4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON LEFT AFT CARGO FLOOR TRACK TRANSITION ANGLE BETWEEN BS 797 TO BS 840, LBL 21.8. REPLACED TRANSITION ANGLE BETWEEN BS 797 TO BS 840, LBL 21.8 IAW B737-400 SRM 053-60-532R.
- [SDR USAA2012061900011](https://openairdocs.org/sdr/USAA2012061900011.md): Angle · corroded · Jun 17, 2012 · N424US · Boeing 737401 · Fuselage Miscellaneous Structure
  > Q4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON LEFT AFT CARGO TRANSITION ANGLE AT BS 727D+10 INCHES, LBL 21. REPLACED LEFT AFT CARGO TRANSITION ANGLE AT BS 727D+10 INCHES, LBL 21 IAW B737-400 SRM 53-60-53-2R.
- [SDR USAA2012070200028](https://openairdocs.org/sdr/USAA2012070200028.md): Support Beam · cracked · Jun 16, 2012 · N424US · Boeing 737401 · Fuselage Miscellaneous Structure
  > Q4 CHECK - NOSE LANDING GEAR WHEEL WELL SUPPORT BEAM WEB CRACKED AT BS 237, BL 0, WL 188. REPAIRED WEB IAW B737 SRM 51-70-13 AND EA 104046.
- [SDR USAA2012061900013](https://openairdocs.org/sdr/USAA2012061900013.md): Skin · delaminated · Jun 15, 2012 · N424US · Boeing 737401 · Leading Edge Devices
  > Q4 CHECK - DELAMINATION ON UPPER SURFACE NR 4 SLAT TRAILING EDGE WEDGE 2 INCHES OUTBOARD OF INBOARD END. REPAIRED NR 4 SLAT TRAILING EDGE WEDGE IAW B737-400 SRM 51-70-10.
- [SDR USAA2012061900012](https://openairdocs.org/sdr/USAA2012061900012.md): Skin · corroded · Jun 15, 2012 · N424US · Boeing 737401 · Leading Edge Devices
  > Q4 CHECK - DELAMINATION ON UPPER AND LOWER TRAILING EDGE SURFACES, OUTBOUND AFT CORNER OF NR 2 SLAT TRAILING EDGE WEDGE. REPAIRED NR 2 SLAT TRAILING EDGE WEDGE IAW B737-400 SRM 51-70-10.
- [SDR USAA2012061500005](https://openairdocs.org/sdr/USAA2012061500005.md): Web · cracked · Jun 14, 2012 · N424US · Boeing 737401 · Fuselage Miscellaneous Structure
  > Q4 CHECK - CRACKED FLOOR WEB AT BS 297, RBL 58. REPAIRED FLOOR WEB AT BS 297, RBL 58 IAW EA 104000.
- [SDR USAA2012061500008](https://openairdocs.org/sdr/USAA2012061500008.md): Strap · corroded · Jun 13, 2012 · N424US · Boeing 737401 · Fuselage Miscellaneous Structure
  > Q4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR STRAP AT BS 727F + 6 INCHES, BETWEEN LBL 20 TO RBL 20. REPAIRED FLOOR STRAP AT BS 727F + 6 INCHES, BETWEEN LBL 20 TO RBL 20 IAW B737-400 SRM 51-10-02.
- [SDR USAA2012061400010](https://openairdocs.org/sdr/USAA2012061400010.md): Attach Angle · corroded · Jun 13, 2012 · N424US · Boeing 737401 · Fuselage Miscellaneous Structure
  > Q4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON TRANSITION ANGLE BETWEEN BS 727E + 6 INCHES TO BS 767, RBL 21. REPLACED TRANSITION ANGLE BETWEEN BS 727E + 6 INCHES TO BS 767, RBL 21 IAW B737-400 SRM 53-60-53.
- [SDR USAA2012061400009](https://openairdocs.org/sdr/USAA2012061400009.md): Tee Fitting · corroded · Jun 6, 2012 · N424US · Boeing 737401 · Fuselage Miscellaneous Structure
  > Q4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON TEE CHORD AT BS 203.8, BL 0. REPAIRED TEE CHORD AT BS 203.8, BL 0 IAW EA 10411.
- [SDR USAA2012061100007](https://openairdocs.org/sdr/USAA2012061100007.md): Tie Clip · cracked · Jun 6, 2012 · N424US · Boeing 737401 · Fuselage Miscellaneous Structure
  > Q4 CHECK - CRACK ON TIE CLIP AT BS 277, S15R. REPAIRED TIE CLIP AT BS 277, S15R IAW B737-400 SRM 51-40-02.
- [SDR USAA2012062500010](https://openairdocs.org/sdr/USAA2012062500010.md): Floorbeam · corroded · Jun 3, 2012 · N424US · Boeing 737401 · Fuselage Main, Floor Beam
  > Q4 CHECK - FLOORBEAM WEB HAS MULTIPLE SCREW HOLES WITH CORROSION AROUND THEM (7" X 0.75" X.020" AREA) AT BS 630, LBL 40.875. REPAIRED IAW EA 103997.
- [SDR USAA2012061900015](https://openairdocs.org/sdr/USAA2012061900015.md): Stiffener · corroded · Jun 3, 2012 · N424US · Boeing 737401 · Fuselage Miscellaneous Structure
  > Q4 CHECK - CORROSION ON STIFFENER AT BS 1120, S15R. REPLACED STIFFENER AT BS 1120, S15R IAW B737-400 DRAWING 65-46579.
- [SDR USAA2012061900014](https://openairdocs.org/sdr/USAA2012061900014.md): Stringer · corroded · Jun 3, 2012 · N424US · Boeing 737401 · Fuselage Main, Longeron/Stringer
  > Q4 CHECK - CORROSION ON STRINGER AT BS 1120, S14R. REPLACED STRINGER AT BS 1120, S14R IAW B737-400 DRAWING 65-46579.
- [SDR USAA2012061500007](https://openairdocs.org/sdr/USAA2012061500007.md): Beam · corroded · Jun 3, 2012 · N424US · Boeing 737401 · Fuselage Miscellaneous Structure
  > Q4 CHECK - LEVEL 2 EXFOLIATION ON LOWER BEAM WEB AT BS 630, LBL 40.875. REPAIRED LOWER BEAM WEB AT BS 630, LBL 40.875 IAW EA 103995.
- [SDR USAA2012061500003](https://openairdocs.org/sdr/USAA2012061500003.md): Tie Clip · cracked · Jun 2, 2012 · N424US · Boeing 737401 · Fuselage Miscellaneous Structure
  > Q4 CHECK - CRACK ON STRINGER TIE CLIP AT BS 380, S22L. REPAIRED STRINGER TIE CLIP AT BS 380, S22L IAW B737-400 SRM 51-10-02.
- [SDR USAA2012061100010](https://openairdocs.org/sdr/USAA2012061100010.md): Beam · cracked · Jun 2, 2012 · N424US · Boeing 737401 · Fuselage Miscellaneous Structure
  > Q4 CHECK - CRACK ON STUB BEAM AT BS 578, LBL 64. REPAIRED STUB BEAM AT BS 578, LBL 64 IAW B737-400 SRM 51-40-02, AND DRAWING 65C52755.
- [SDR USAA2012061100009](https://openairdocs.org/sdr/USAA2012061100009.md): Wedge · delaminated · Jun 2, 2012 · N424US · Boeing 737401 · Trailing Edge Flaps
  > Q4 CHECK - DELAMINATION ON LEFT WING INBOARD AFT FLAP TRAILING EDGE WEDGE 29 INCHES FROM OUTBOARD END ON THE UPPER SURFACE. REPAIRED AFT FLAP TRAILING EDGE WEDGE IAW B737-400 SRM 51-70-10.
- [SDR USAA2012061400011](https://openairdocs.org/sdr/USAA2012061400011.md): Frame · corroded · Jun 1, 2012 · N424US · Boeing 737401 · Fuselage Main, Frame
  > Q4 CHECK - LEVEL 2 CORROSION ON APU INLET OPENING FRAME AT BS 1112, BETWEEN S5R TO S12R. REPAIRED APU INLET OPENING FRAME AT BS 1112, BETWEEN S5R TO S12R IAW EA 103980.
- [SDR USAA2012070200027](https://openairdocs.org/sdr/USAA2012070200027.md): Skin · corroded · May 31, 2012 · N424US · Boeing 737401 · Trailing Edge Flaps
  > Q4 CHECK - RIGHT OUTBOARD TRAILING EDGE MID-FLAP HAS MULTIPLE (3) AREAS OF CORROSION; 1"X1"X.002"; 1.5"X1"X.005"; 1.5"X1.5"X.006" ON UPPER LEADING EDGE SURFACE FROM WBL 262 TO WBL 400. REMOVED AND REPLACED MID-FLAP ASSEMBLY.
- [SDR USAA2012061500004](https://openairdocs.org/sdr/USAA2012061500004.md): Stiffener · corroded · May 31, 2012 · N424US · Boeing 737401 · Fuselage Miscellaneous Structure
  > 2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON STIFFENER AT BS 1126, BETWEEN S5R TO S12R. REPAIRED STIFFENER AT BS 1126, BETWEEN S5R TO S12R IAW BOEING DRAWING 65-46579.
- [SDR USAA2012061100006](https://openairdocs.org/sdr/USAA2012061100006.md): Wedge · delaminated · May 30, 2012 · N424US · Boeing 737401 · Leading Edge Devices
  > Q4 CHECK - DELAMINATION ON RIGHT WING NR 4 SLAT TRAILING EDGE WEDGE. REPAIRED RIGHT WING NR 4 SLAT TRAILING EDGE WEDGE IAW B737-400 SRM51-70-10 REPAIR 4 AND TYPICAL REPAIR 737-5130-11-0347.
- [SDR USAA2012061100008](https://openairdocs.org/sdr/USAA2012061100008.md): Floorbeam · corroded · May 29, 2012 · N424US · Boeing 737401 · Fuselage Main, Floor Beam
  > Q4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM T-CAP AT BS 328, BETWEEN LBL 30 TO RBL 64. REPAIRED FLOORBEAM T-CAP AT BS 328, BETWEEN LBL 30 TO RBL 64 IAW B737-400 SRM 53-10-51-2R.
- [SDR USAA2012061100004](https://openairdocs.org/sdr/USAA2012061100004.md): Angle · corroded · May 29, 2012 · N424US · Boeing 737401 · Fuselage Miscellaneous Structure
  > Q4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON Z-ANGLE BETWEEN BS 947 TO BS 986.5, LBL 50. REPLACED Z-ANGLE IAW B737-400 SRM 51-40-02 AND DRAWING 65-52878.
- [SDR USAA2012052500012](https://openairdocs.org/sdr/USAA2012052500012.md): Frame · cracked · May 22, 2012 · N424US · Boeing 737401 · Fuselage Main, Frame
  > Q4 CHECK - CRACK ON FUSELAGE FRAME AT BS 787, S9R. REPAIRED FUSELAGE FRAME AT BS 787, S9R IAW TYPICAL REPAIR TR737-5310-10-287.
- [SDR USAA2012042300012](https://openairdocs.org/sdr/USAA2012042300012.md): Placard · missing · Apr 22, 2012 · N424US · Boeing 737401 · Placards and Markings
  > MAINTENANCE REPORTED ROW 12 EXIT PLACARD MISSING. MAINTENANCE INSTALLED PLACARD. OK FOR SERVICE.
- [SDR USAA2012022100002](https://openairdocs.org/sdr/USAA2012022100002.md): Skin · cracked · Feb 21, 2012 · N424US · Boeing 737401 · Fuselage Main, Plate/Skin
  > RON CHECK, CRACK IN FUSELAGE SKIN AT BS 947, S25R. REPAIRED SKIN IAW SRM 53-00-01-2R-31 DETAIL XIX.
- [SDR USAA2012020600027](https://openairdocs.org/sdr/USAA2012020600027.md): Control Module · faulty · Feb 3, 2012 · N424US · Boeing 737401 · Aileron Control System
  > AT CRUISE, ON AUTO PILOT, CREW REPORTED THE LEFT FLIGHT CONTROL SURFACE DEPLOYED. AIRCRAFT WAS DIFFICULT TO CONTROL, CREW DECLARED AN EMERGENCY AND DIVERTED TO GSO. FLIGHT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLA
- [SDR USAA2011120200010](https://openairdocs.org/sdr/USAA2011120200010.md): Sign · detached · Dec 1, 2011 · N424US · Boeing 737401 · Placards and Markings
  > EMERGENCY SIGN OVER LEFT WING EXITS FELL OFF. RE-SECURED SIGN.
- [SDR USAA2011082600011](https://openairdocs.org/sdr/USAA2011082600011.md): Skin · cracked · Aug 24, 2011 · N424US · Boeing 737401 · Fuselage Main, Plate/Skin
  > UFRSI CHECK - CRACK IN FUSELAGE SKIN AT L1 DOOR LOWER HINGE CUTOUT AT BS 303, S15L. REPAIRED FUSELAGE SKIN AT L1 DOOR LOWER HINGE CUTOUT IAW B737 SRM 53-10-01 FIG 201 & EA 130664.
- [SDR USAA2011082600010](https://openairdocs.org/sdr/USAA2011082600010.md): Skin · cracked · Aug 24, 2011 · N424US · Boeing 737401 · Fuselage Main, Plate/Skin
  > UFRSI CHECK - CRACK IN FUSELAGE SKIN AT L1 DOOR UPPER HINGE CUTOUT AT BS 303, S10L. REPAIRED FUSELAGE SKIN AT L1 DOOR UPPER HINGE CUTOUT IAW EA 130664.
- [SDR USAA2011082600016](https://openairdocs.org/sdr/USAA2011082600016.md): Tie Clip · cracked · Aug 21, 2011 · N424US · Boeing 737401 · Fuselage Miscellaneous Structure
  > UFRSI CHECK - CRACK IN TIE CLIP AT BS 294.5, S11L. REPLACED TIE CLIP AT BS 294.5, S11L IAW B737 SRM 51-40-02.
- [SDR USAA2011082600014](https://openairdocs.org/sdr/USAA2011082600014.md): Intercostal · cracked · Aug 20, 2011 · N424US · Boeing 737401 · Fuselage Miscellaneous Structure
  > UFRSI CHECK - CRACK IN AUXILIARY INTERCOSTAL (ATTACH ANGLE) AT BS 301.5, S10L. REPLACED AUXILIARY INTERCOSTAL AT AT BS 301.5, S10L IAW B737 SRM 51-40-02.
- [SDR USAA2011082600015](https://openairdocs.org/sdr/USAA2011082600015.md): Intercostal · cracked · Aug 13, 2011 · N424US · Boeing 737401 · Fuselage Miscellaneous Structure
  > UFRSI CHECK - CRACK IN INTERCOSTAL BETWEEN BS 294.5 TO BS 303.9, S8L. REPLACED INTERCOSTAL BETWEEN BS 294.5 TO BS 303.9, S8L IAW B737 SRM 51-40-02.
- [SDR USAA2011082600013](https://openairdocs.org/sdr/USAA2011082600013.md): Frame · cracked · Aug 10, 2011 · N424US · Boeing 737401 · Fuselage Main, Frame
  > UFRSI CHECK - CRACK IN FUSELAGE FRAME AT BS 500G BETWEEN S13L TO S14L. REPAIRED FUSELAGE FRAME AT BS 500G BETWEEN S13L TO S14L IAW TYPICAL REPAIR TR737-5310-10-0327.
- [SDR USAA2011082600012](https://openairdocs.org/sdr/USAA2011082600012.md): Frame · cracked · Aug 10, 2011 · N424US · Boeing 737401 · Fuselage Main, Frame
  > UFRSI CHECK - CRACK IN FUSELAGE FRAME AT BS 500E BETWEEN S20L TO S21L. REPAIRED FUSELAGE FRAME AT BS 500E BETWEEN S20L TO S21L IAW B737 SRM 53-00-07 REPAIR 13.
- [SDR USAA2011082600009](https://openairdocs.org/sdr/USAA2011082600009.md): Skin · cracked · Aug 10, 2011 · N424US · Boeing 737401 · Fuselage Main, Plate/Skin
  > UFRSI CHECK - 2 CRACKS IN FUSELAGE SKIN AT BS 727E+8 APPROX 1.5 INCHES & AT BS 727D+18 INCHES APPROX 2 INCHES IN LENGTH AT S24R. REPAIRED FUSELAGE SKIN AT BS 727E+8 & BS 727D+18 INCHES, S24R IAW B737 SRM 53-00-01 FIG 201 REPAIR 31.

Next page: https://openairdocs.org/deregistered/N424US-2022-02-11/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 = 'N424US' AND deregistration_id = 'N424US-2022-02-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N424US-2022-02-11/reports

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