# Service difficulty reports: N842AS, cancelled Feb 25, 2019

A list on [N842AS, cancelled Feb 25, 2019](https://openairdocs.org/deregistered/N842AS-2019-02-25.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 5 · 201 reports

- [SDR ASOA2015060112960](https://openairdocs.org/sdr/ASOA2015060112960.md): Handle · lack of lube · May 28, 2015 · N842AS · Cndair CL6002B19 · Passenger/Crew Doors
  > "PAX DOOR STOW", CAUTION MESSAGE AND DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE AT GATE. TESTED MAIN PAX DOOR. LUBRICATED OUTER HANDLE, DOOR OPS CHECKS OK IAW AMM 52-11-01. ACFT OK FOR SERVICE.
- [SDR ASOA2015022712312](https://openairdocs.org/sdr/ASOA2015022712312.md): Door · none · Feb 26, 2015 · N842AS · Cndair CL6002B19 · Passenger/Crew Doors
  > MAIN AIRSTAIR DOOR WAS HARD TO OPEN ON. PERFORMED OPS CHECK OF MAIN PAX DOOR IAW AMM 52-10-00. NO DEFECTS FOUND. OUTER HANDLES FLUSH. INNER MARKINGS LINE UP.
- [SDR ASOA2015022512271](https://openairdocs.org/sdr/ASOA2015022512271.md): Door · none · Feb 21, 2015 · N842AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR WILL NOT OPEN, OPENED PAX DOOR ALL CHECKS GOOD IAW AMM 52-11-00.
- [SDR ASOA2014112611791](https://openairdocs.org/sdr/ASOA2014112611791.md): Skin · damaged · Nov 21, 2014 · N842AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT SKIN AT BS 640 - 755 STR 20L-20R, FOUND CRACKED, BUCKLED, DENTED AND DEFORMED.
- [SDR ASOA2014061810678](https://openairdocs.org/sdr/ASOA2014061810678.md): Light · damaged · Jun 14, 2014 · N842AS · Cndair CL6002B19 · Emergency Lighting
  > FLOOR LEVEL EMERGENCY FLOODLIGHT AT GALLEY DAMAGED. R & R FLOODLIGHT IAW AMM 33-51-19. SYSTEM OPS CHECKED GOOD.
- [SDR ASOA2014042910417](https://openairdocs.org/sdr/ASOA2014042910417.md): Isolator · cracked · Apr 18, 2014 · N842AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > LT LOWER SIDE OF AFT PRESSURE BULKHEAD HAS TWO BAD ISOLATORS CRACKED. INSTALLED NEW ISOLATORS IAW SRM 51-42-13.
- [SDR ASOA2014042910416](https://openairdocs.org/sdr/ASOA2014042910416.md): Wire · broken · Apr 18, 2014 · N842AS · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY LIGHT IS INOPERATIVE, AFT INBD. FOUND TWO WIRES ON LAMP ASSY BROKEN. REPAIRED WIRES IAW 0ESPM 20-16-00. PERFORMED OPS TEST OF EMERGENCY LIGHTING IAW 0AMM 33-51-00-710-801 OPS TEST GOOD AT THIS TIME.
- [SDR ASOA2014042910412](https://openairdocs.org/sdr/ASOA2014042910412.md): Access Panel · cracked · Apr 12, 2014 · N842AS · Cndair CL6002B19 · Wing, Plate/Skin
  > CRACK DISCOVERED ON ON RT WING LOWER PLANK, T/E AT WS 119.58 REMOVED UPPER & LOWER SKIN AND LOWER ACCESS PANELS IAW SRM 57-42-06 & 51-42-10. MAJOR REPAIR.
- [SDR ASOA2014042910411](https://openairdocs.org/sdr/ASOA2014042910411.md): Angle · cracked · Apr 9, 2014 · N842AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT ANGLE BRACKET AT AFT FUSELAGE S13AR, FS 261 HAS CRACK AT LOWER AFT RIVET HOLE, MARKED W/TAPE. R & R RT ANGLE BRACKET AT AFT FUSELAGE STR 15A, FS 261 IAW SRM 51-42-01.
- [SDR ASOA2014042910410](https://openairdocs.org/sdr/ASOA2014042910410.md): Angle · cracked · Apr 9, 2014 · N842AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT ANGLE BRACKET AT AFT FUSELAGE S15L, FS 261 HAS CRACK AT LOWER AFT RIVET HOLE. REMOVED ANGLE BRACKET IAW SRM 51-42-06. INSTALLED ANGLE BRACKET IAW SRM 51-42-06.
- [SDR ASOA2014042910409](https://openairdocs.org/sdr/ASOA2014042910409.md): Seat Track · corroded · Apr 7, 2014 · N842AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LBL 9 SEAT TRACK BS 559 - 559+80. FOUND TO BE OUT OF LIMIT IAW SRM 51-21-00. REMOVED SEAT TRACK IAW SRM 51-41-02. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR ASOA2014042910408](https://openairdocs.org/sdr/ASOA2014042910408.md): Seat Track · corroded · Apr 7, 2014 · N842AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LBL 9, SEAT TRACK BS 394 - 409+128. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. R & R SEAT TRACK IAW AMM 53-01-1-000-802 AND 53-01-11-400-802.
- [SDR ASOA2014042910407](https://openairdocs.org/sdr/ASOA2014042910407.md): Seat Track · corroded · Apr 7, 2014 · N842AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RBL 9, SEAT TRACK BS 394 - 409+128. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT RAIL IAW AMM 53-01-11-400-802.
- [SDR ASOA2014042910406](https://openairdocs.org/sdr/ASOA2014042910406.md): Seat Track · corroded · Apr 7, 2014 · N842AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LBL 9, SEAT TRACK BS 364-409. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED CORRODED SEAT TRACK IAW SRM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR ASOA2014042910405](https://openairdocs.org/sdr/ASOA2014042910405.md): Floor Support · corroded · Apr 7, 2014 · N842AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON RT FLOOR SUPPORT BETWEEN BS 295 - 310. REPAIRED FLOOR SUPPORT BETWEEN BS 280 & 409+128 IAW REO 601R-53-00-530.
- [SDR ASOA2014042910404](https://openairdocs.org/sdr/ASOA2014042910404.md): Seat Track · corroded · Apr 7, 2014 · N842AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RBL 9 SEAT TRACK BS 364 - 394, R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR ASOA2014042910403](https://openairdocs.org/sdr/ASOA2014042910403.md): Structure · cracked · Apr 7, 2014 · N842AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR EDGE MEMBER CRACKED AT FWD LOCATION. COMPLIED WITH EC/TC REO 601R-52-11-279 IAW REO 601R-52-11-279.
- [SDR ASOA2014042910402](https://openairdocs.org/sdr/ASOA2014042910402.md): Frame · corroded · Apr 6, 2014 · N842AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME CRACKED AT BS 338 TOP OF DOOR. COMPLIED WITH REO 601R-52-11-402 FOR REPAIR. MAJOR REPAIR.
- [SDR ASOA2014042910401](https://openairdocs.org/sdr/ASOA2014042910401.md): Frame · cracked · Apr 6, 2014 · N842AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME CRACKED AT BS 320.10, TOP OF DOOR. COMPLIED WITH REO 601R-52-11-402 FOR REPAIR. MAJOR REPAIR.
- [SDR ASOA2014042910400](https://openairdocs.org/sdr/ASOA2014042910400.md): Isolator · broken · Apr 6, 2014 · N842AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BROKEN ISOLATER ON REAR PRESSURE BULKHEAD. R & R BROKEN ISOLATOR ON REAR PRESSURE BULKHEAD IAW SRM 51-42-13.
- [SDR ASOA2014042910399](https://openairdocs.org/sdr/ASOA2014042910399.md): Seat Track · corroded · Apr 5, 2014 · N842AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SEAT TRACK SEGMENT CORRODED IN TWO SPOTS, BS 552 -559+24. FOUND OUT OF LIMITS IAW SRM 53-41-49. R & R SIDE SEAT TRACK IAW AMM 53-01-011-000/400-802 AND EC/TC REO 601R-53-00-055. COMPLIED WITH EC/TC REO 601R-53-00-055 AND REO 601R-53-00-055 REV A.
- [SDR ASOA2014042910398](https://openairdocs.org/sdr/ASOA2014042910398.md): Seat Track · corroded · Apr 5, 2014 · N842AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDE SEAT TRACK SEGMENT AT FS 409.20. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-31-49, PAGE 101. COMPLETED FABRICATION OF REPAIR SECTION INSTALLED REPAIR IAW EC/TC REO 601R-53-00-055. COMPLIED WITH EC/TC REO 601R-53-00-055 AND REO 601R-53-00-55, REV A.
- [SDR ASOA2014042910397](https://openairdocs.org/sdr/ASOA2014042910397.md): Seat Track · corroded · Apr 5, 2014 · N842AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SEAT TRACK SEGMENT IS CORRODED AT BS 400. REMOVED DAMAGED SEAT TRACK IAW AMM 53-01-11-0000-802 FROM BS 364 - 409+16. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR ASOA2014042910396](https://openairdocs.org/sdr/ASOA2014042910396.md): Light · inoperative · Apr 4, 2014 · N842AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT ON RT SIDE FROM 1-6 SEATS IS INOPERATIVE. REPLACED EMERGENCY LIGHT IAW CMM 33-60-13.
- [SDR ASOA2014042910395](https://openairdocs.org/sdr/ASOA2014042910395.md): Wire · broken · Apr 4, 2014 · N842AS · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY LIGHT ON FWD WARDROBE HAS A BROKEN WIRE. REPAIRED BROKEN WIRE IAW ESPM 20-17-10. PERFORMED OPS TEST OF THE EMERGENCY LIGHTING IAW AMM 33-1-00-710-801, OPS TESTED GOOD.
- [SDR ASOA2014022810042](https://openairdocs.org/sdr/ASOA2014022810042.md): Lamp · burned out · Feb 27, 2014 · N842AS · Cndair CL6002B19 · Emergency Lighting
  > CABIN CEILING NR 3 EMERGENCY LIGHT INOPERATIVE. REPLACED LAMPS IAW AMM 33-51-16. OPS CHECKED GOOD.
- [SDR ASOA2013042603450](https://openairdocs.org/sdr/ASOA2013042603450.md): Battery Pack · discharged · Apr 22, 2013 · N842AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE. CHARGED BATTERY PACKS. OPS CHECKED OK IAW AMM 33-51-00.
- [SDR ASOA201201275](https://openairdocs.org/sdr/ASOA201201275.md): Rib · cracked · Apr 6, 2012 · N842AS · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > LEFT HORIZONTAL STAB ANGLE AND STRAP UNDER UPPER SURFACE OF STAB TIP FAIRING HAS LIGHTNING STRIKE DAMAGE. ON INSTALLATION OF UPPER ANGLE, FOUND A CRACKED NR 9 RIB AT UPPER FLANGE. REMOVED CRACKED RIB. REMOVED LOWER ANGLE AND CLIPS ATTACHED TO DAMAGED PART I
- [SDR ASOA201201261](https://openairdocs.org/sdr/ASOA201201261.md): Floor Support · corroded · Apr 3, 2012 · N842AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR THRESHOLD FLOOR SUPPORT HAS MINOR CORROSION. REMOVED AND REPLACED IAW SRM 51-42-06, 51-42-13 AND 51-42-21.
- [SDR ASOA201201141](https://openairdocs.org/sdr/ASOA201201141.md): Floorbeam · corroded · Apr 3, 2012 · N842AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM AT LBL 35 ON FS 349. TREATED AND REFINISHED BLEND AREAS IAW SRM 51-21-06, STEP 3D.
- [SDR ASOA201201139](https://openairdocs.org/sdr/ASOA201201139.md): Web · corroded · Apr 3, 2012 · N842AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT PRESSURE FLOOR SILL PANEL AND SILL ANGLES HAVE NUMEROUS AREAS OF CORROSION BETWEEN FS 409+128 AND 559. BLENDED CORROSION IAW REO 601R-53-41-666. FOUND OUT OF LIMITS IAW REO 601R-53-41-666, STEP 1. REPAIRED.
- [SDR ASOA201201137](https://openairdocs.org/sdr/ASOA201201137.md): Web · corroded · Apr 3, 2012 · N842AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT PRESSURE FLOOR SILL PANEL AND SILL ANGLES HAVE NUMEROUS AREAS OF CORROSION BETWEEN FS 409+128 AND 559. BLENDED OUT AREAS OF CORROSION IAW REO 601R-53-41-666. PERFORMED NDT IAW REO 601R-53-41-666 STEPS 5 & 12 AND CNDTM PT 1 51-20-06. NO INDICATIONS NOTE
- [SDR ASOA201201135](https://openairdocs.org/sdr/ASOA201201135.md): Floor Support · corroded · Apr 3, 2012 · N842AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT LOWER FLOOR SUPPORT ANGLE IS CORRODED. R & R AFT LOWER FLOOR SUPPORT ANGLE IAW SRM 51-42-21. REPAIR CLASSIFIED AS MINOR.
- [SDR ASOA201201133](https://openairdocs.org/sdr/ASOA201201133.md): Floorbeam · corroded · Apr 3, 2012 · N842AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM AT LBL 35 ON FS 349. REMOVED CORROSION IAW SRM 51-21-06, STEP 3D. FOUND OUT OF LIMITS IAW SRM 53-00-00, FIG 102. REPLACED IAW SRM 51-40-11 AND 51-42-06.
- [SDR ASOA201201115](https://openairdocs.org/sdr/ASOA201201115.md): Floor Support · cracked · Apr 2, 2012 · N842AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT AND RIGHT FWD EQUIPMENT BAY FLOOR SUPPORT AT FS 193.00 IS CRACKED APPROX.5L. REPAIRED IAW REO 601R-53-11-245, REV B.
- [SDR ASOA201201097](https://openairdocs.org/sdr/ASOA201201097.md): Glowstrip · missing · Mar 29, 2012 · N842AS · Cndair CL6002B19 · Emergency Equipment
  > 232EZ AFT PHOTOLUMINESCENT STRIP MISSING. INSTALLED NEW PHOTOLUMINESCENT STRIP IAW AMM 11-30-00-400-801.
- [SDR ASOA201201088](https://openairdocs.org/sdr/ASOA201201088.md): Isolator · cracked · Mar 29, 2012 · N842AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > THREE ISOLATORS ON BS 621 BULKHEAD ARE CRACKED. R & R ISOLATORS IAW SRM 51-42-13.
- [SDR ASOA201201086](https://openairdocs.org/sdr/ASOA201201086.md): Support · cracked · Mar 29, 2012 · N842AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 484.00, LBL 27.00 VERTICAL SUPPORT CRACKED. R & R VERTICAL SUPPORT CLIP IAW SRM 51-42-21.
- [SDR ASOA201201084](https://openairdocs.org/sdr/ASOA201201084.md): Floorbeam · cracked · Mar 29, 2012 · N842AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 484.00, RBL 27 AND RBL 36 FLOORBEAM CRACKED. R & R IAW SRM 51-42-21.
- [SDR ASOA201201082](https://openairdocs.org/sdr/ASOA201201082.md): Support Bracket · cracked · Mar 29, 2012 · N842AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PILOT WINDSHIELD SIDE POST AFT LOWER SUPPORT BRACKET CRACKED. REMOVED CRACKED PILOT WINDSHIELD AFT LOWER POST BRACKET. FIT, DRILLED AND INSTALLED NEW BRACKET IAW SRM 51-42-21.
- [SDR ASOA201201080](https://openairdocs.org/sdr/ASOA201201080.md): Support Bracket · cracked · Mar 29, 2012 · N842AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CO-PILOT WINDSHIELD SIDE POST AFT LOWER SUPPORT BRACKET CRACKED. R & R LOWER AFT WINDSHIELD POST BRACKET IAW SRM 51-42-20.
- [SDR ASOA201201074](https://openairdocs.org/sdr/ASOA201201074.md): Skin · corroded · Mar 28, 2012 · N842AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CORRODED BETWEEN FS 559+80 TO FS 559+112 AT STR 23R. REMOVED LIGHT CORROSION IAW SRM 51-21-06.
- [SDR ASOA201201072](https://openairdocs.org/sdr/ASOA201201072.md): Skin · corroded · Mar 28, 2012 · N842AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS AREA OF CORROSION AT FS 559 +112 AT STR 24R. REMOVED LIGHT CORROSION IAW SRM 51-21-06.
- [SDR ASOA201201070](https://openairdocs.org/sdr/ASOA201201070.md): Skin · corroded · Mar 28, 2012 · N842AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN HAS AREA OF CORROSION AT STR 24R AT BS 559.00 +112. REMOVED LIGHT CORROSION IAW SRM 51-21-06.
- [SDR ASOA201201068](https://openairdocs.org/sdr/ASOA201201068.md): Post · cracked · Mar 28, 2012 · N842AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128 VERTICAL POST BL 0 FAILS NDT WITH A CRACK INDICATION IN LT AFT RADIUS OF POST WITH AN INDICATION GREATER THAN 50 PERCENT SCREEN HEIGHT APPROX.2 LONG. REMOVED POST IAW SRM 51-42-06 & 51-42-21. LOCATED, DRILLED & SUBASSEMBLED NEW SERVICEABLE POST I
- [SDR ASOA201201259](https://openairdocs.org/sdr/ASOA201201259.md): Floor Support · corroded · Mar 27, 2012 · N842AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR THRESHOLD VERTICAL FLOOR SUPPORT HAS MINOR CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-06 AND 51-42-13.
- [SDR ASOA201201093](https://openairdocs.org/sdr/ASOA201201093.md): Floor Support · corroded · Mar 27, 2012 · N842AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LOWER FLOOR SUPPORT ANGLE CORRODED. REMOVED LWR FLOOR SUPPORT ANGLE IAW SRM 51-42-21, 51-42-10, 51-42-06 AND 51-42-34. LOCATED & DRILLED NEW FLOOR SUPPORT & INSTALLED IAW SRM 51-42-21, 51-42-10, 51-42-06 AND 51-42-34.
- [SDR ASOA201201058](https://openairdocs.org/sdr/ASOA201201058.md): Floor Panel · cracked · Mar 27, 2012 · N842AS · Cndair CL6002B19 · Fuselage Floor Panel
  > LEFT & RIGHT FWD EQUIPMENT COMPARTMENT FLOOR STRUCTURE AT FS 193.00 IS CRACKED APPROX.5L. TRIMMED CRACKED SECTION OF FLOOR WEB IAW REO 601R-53-11-245. PERFORMED EDDY CURRENT IAW STEP 4 OF REO 601R-53-11-245. NO INDICATIONS NOTED. FABRICATED REPAIR AND IN
- [SDR ASOA201201056](https://openairdocs.org/sdr/ASOA201201056.md): Seat Track · corroded · Mar 27, 2012 · N842AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED AT LBL 9.0 FROM 409+128 TO 559. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SERVICEABLE SEAT TRACK IAW SRM 51-41-02 AND AMM 53-01-11-400-802.
- [SDR ASOA201201054](https://openairdocs.org/sdr/ASOA201201054.md): Seat Track · corroded · Mar 27, 2012 · N842AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED AT RBL 9.0 FROM FS 409+128 TO 559.00. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW MM TASK 53-01-11-400-802.

Next page: https://openairdocs.org/deregistered/N842AS-2019-02-25/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 = 'N842AS' AND deregistration_id = 'N842AS-2019-02-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N842AS-2019-02-25/reports

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