# Service difficulty reports: N803AT, cancelled Aug 18, 2003

A list on [N803AT, cancelled Aug 18, 2003](https://openairdocs.org/deregistered/N803AT-2003-08-18.md).

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

- [SDR AT0100158](https://openairdocs.org/sdr/AT0100158.md): Threshold · corroded · Apr 21, 2001 · N803AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND AFT ENTRANCE THRESHOLD CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-10-02, 51-10-03, 51-10-04, 51-30, 51-30-02, 51-30-05, AND 51-30-08.
- [SDR AT0100157](https://openairdocs.org/sdr/AT0100157.md): Floorbeam · corroded · Apr 20, 2001 · N803AT · Doug DC932 · Fuselage Main, Floor Beam
  > FOUND AFT CARGO COMPARTMENT BS 965 RBL 12 FLOORBEAM ATTACH ANGLE TO HAVE EXFOLIATED CORROSION. REPLACED FLOORBEAM IAW REO L00433 REV A, DC9 SRM 53-04 FIG 12C, 53-05 FIG 79, 51-10-04, 51-10-03, 51-30-02, 51-30-05, 51-30-01, AND MM 20-18.
- [SDR AT0100156](https://openairdocs.org/sdr/AT0100156.md): Control Column · cracked · Apr 19, 2001 · N803AT · Doug DC932 · Control Column Section
  > FOUND CAPTAINS CONTROL COLUMN CRACKED BEYOND LIMITS. REPLACED CONTROL COLUMN IAW EO 12-2730-29-B1063.
- [SDR AT0100172](https://openairdocs.org/sdr/AT0100172.md): Frame · cracked · Apr 16, 2001 · N803AT · Doug DC932 · Fuselage Main, Frame
  > FOUND FRAME AT BS 598 LONGERON 11 CRACKED. FABRICATED AND INSTALLED REPAIR IAW REO-L00432.
- [SDR AT0100160](https://openairdocs.org/sdr/AT0100160.md): Longeron · cracked · Apr 16, 2001 · N803AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FOUND LONGERON 11 FRAME AT BS 598 CRACKED. INSTALLED REPAIR IAW REO L00432.
- [SDR AT0100159](https://openairdocs.org/sdr/AT0100159.md): Attach Angle · cracked · Apr 15, 2001 · N803AT · Doug DC932 · Fuselage, Stabilizer Attach Fittings
  > FOUND DORSAL FIN ATTACH ANGLES CRACKED BEYOND LIMITS. REPLACED ATTACH ANGLES IAW EO 09-5350-29-E1645.
- [SDR AT0100162](https://openairdocs.org/sdr/AT0100162.md): Door Frame · corroded · Apr 8, 2001 · N803AT · Doug DC932 · Fuselage Main, Structure
  > FOUND AFT STAIRWAY DOOR FRAME CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED ATTACH ANGLE REPAIR IAW DC9 SRM 53-01 FIG 1, 51-30, 51-10-03, 51-10-02, 51-10-04 AND 51-30-01.
- [SDR AT0000114](https://openairdocs.org/sdr/AT0000114.md): Fuse · failed · Mar 8, 2000 · N803AT · Doug DC932 · Emergency Lighting
  > FOUND CENTER SECTION OF EMERGENCY PATH LIGHTING INOPERATIVE.. REPLACED BLOWN FUSE AT AFT BATTERY CHARGER.
- [SDR AT0000080](https://openairdocs.org/sdr/AT0000080.md): Stringer · corroded · Feb 9, 2000 · N803AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FOUND LEFT HAND WING STRINGER 15 CORRODED. INSTALLED STRAP REPAIR IAW DC9 SRM 51-30-5, 51-10-4, 57-08 FIGURE 2 METHOD 2, 51-22-1 TO -3.
- [SDR AT0000079](https://openairdocs.org/sdr/AT0000079.md): Stringer · corroded · Feb 9, 2000 · N803AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FOUND LEFT HAND WING STRINGER 17 CORRODED. CUT AND SPLICED LEFT HAND WING STRINGER 17 IAW DC9 SRM 51-30-5, 51-10-4, 51-22-1, 51-10-3, 57-08 FIGURE 2.
- [SDR AT0000078](https://openairdocs.org/sdr/AT0000078.md): Stringer · corroded · Feb 9, 2000 · N803AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FOUND LEFT HAND WING STRINGER 20 CORRODED. CUT AND SPLICED LEFT HAND WING STRINGER 20 IAW DC9 SRM 51-30-5, 51-10-4, 51-22-1, 51-10-3, 57-08 FIGURE 2.
- [SDR AT0000077](https://openairdocs.org/sdr/AT0000077.md): Stringer · corroded · Feb 9, 2000 · N803AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FOUND LEFT HAND STRINGER 23 CORRODED. REMOVED AND REPLACED LEFT HAND STRINGER 23 IAW DC9 SRM 51-30-5, 51-10-4, 51-22-1, 51-30-1, 57-08.
- [SDR AT0000072](https://openairdocs.org/sdr/AT0000072.md): Stringer · gouged · Feb 7, 2000 · N803AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FOUND AFT CARGO DOOR AT BS 937, LONGERON 23R - 25R WAS BENT AND GOUGED. FABRICATED, DRILLED AND INSTALLED REPAIR IAW TIMCO EO L00036.
- [SDR AT0000075](https://openairdocs.org/sdr/AT0000075.md): Door Pan · corroded · Feb 5, 2000 · N803AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND CORROSION AT LOWER DOOR STOP AT AFT CARGO DOOR FRAME AT BS 917. REMOVED AND REPLACED AFT CARGO DOOR JAMB PAN SECTION IAW DC9 SRM 53-10-01 FIGURE 1, 51-10-3, AND 53-05 FIGURE 44.
- [SDR AT0000074](https://openairdocs.org/sdr/AT0000074.md): Door Pan · corroded · Feb 3, 2000 · N803AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND C1 CARGO DOOR CUTOUT PAN HAD SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED CARGO DOOR PAN, FABRICATED AND INSTALLED PAN SPLICES IAW DC9 SRM 53-05 FIGURE 44, 51-30-2, 51-30-5, 51-10-4.
- [SDR AT0000076](https://openairdocs.org/sdr/AT0000076.md): Frame · corroded · Feb 2, 2000 · N803AT · Doug DC932 · Fuselage Main, Frame
  > FOUND CORROSION ON FORWARD SIDE FRAME AT BS 980, LONGERON 26R -24R. REMOVED CORROSION, BEYOND LIMITS. REMOVED FRAME SECTION AT BS 980, LONGERON 26R - 24R, INSTALLED NEW FRAME AND REPAIR SPLICES IAW DC9 SRM 53-03 FIGURE 2A.
- [SDR AT0000070](https://openairdocs.org/sdr/AT0000070.md): Skin · cracked · Feb 2, 2000 · N803AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND CRACK AT FORWARD ENTRY DOOR JAMB, FORWARD UPPER CORNER ON OUTER SKIN. CUT OUT CRACKED SKIN, FABRICATED DOUBLERS, AND INSTALLED IAW SRD 9530252.
- [SDR AT0000073](https://openairdocs.org/sdr/AT0000073.md): Bulkhead · corroded · Feb 1, 2000 · N803AT · Doug DC932 · Fuselage Main, Bulkhead
  > FOUND CANTED BULKHEAD AT BS 1143, LEFT HAND UNDER THE END OF LEFT HAND PYLON SKIN WAS CORRODED. REMOVED CORROSION, REPLACED SKIN AND DOUBLERS IAW DC9 SRM 53-01 FIGURE 4, 51-30-2, AND 51-30-3.
- [SDR AT0000069](https://openairdocs.org/sdr/AT0000069.md): Skin · cracked · Feb 1, 2000 · N803AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND CARGO COMPARTMENT DOOR JAMB FORWARD LOWER CORNER HAS A.375 CRACK ON OUTER SKIN. CUT OUT CRACK, FABRICATED 2 REPAIR DOUBLERS. TREATED PRIMED AND INSTALLED REPAIR DOUBLERS IAW DC9 SRM 51-10-03 AND EO 95310-29-E1410.
- [SDR AT0000062](https://openairdocs.org/sdr/AT0000062.md): Frame · cracked · Jan 28, 2000 · N803AT · Doug DC932 · Fuselage Main, Frame
  > FOUND FRAME CRACKED AT RIGHT HAND SIDE NEAR THE ACTUATOR LOWER MOUNT (AIRSTAIRS) AT BS 1143. CUT OUT CRACKED FRAME SECTION FABRICATED L & Z DOUBLERS, HEAT TREATED AND INSTALLED NEW FRAME SECTION AND L & Z DOUBLERS IAW DC9 SRM 51-30-2, 51-10-3 AND EO L00024.
- [SDR AT0000071](https://openairdocs.org/sdr/AT0000071.md): Skin · corroded · Jan 26, 2000 · N803AT · Doug DC932 · Fuselage Main, Plate/Skin
  > FOUND RIGHT HAND AFT VANITY CLOSE TO ANGLE SKIN WAS CORRODED OUT OF LIMITS. FABRICATED UPPER SKIN, FILLERS, HEAT TREATED AND INSTALLED IAW DC9 SRM 51-30-1, 51-10-3, 53-01 FIGURE 2, 51-7 0-1. DC9 MM 20-20-0, WEBER OVERHAUL MANUAL, 25-42-50, DPS 4901 AND DPS 1
- [SDR AT0000059](https://openairdocs.org/sdr/AT0000059.md): Longeron · corroded · Jan 26, 2000 · N803AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FOUND LONGERON 24R HAD CORROSION AT BS 935 FROM END CAP ALONG UPPER CHANNEL TO BS 945. REMOVED LONGERON 24R, END CLIP, END FITTING. INSTALLED NEW SKIN PATCH AT BS 945, LONGERON 24R, END CLIP AND END FITTING IAW DC9 SRM 53-04 FIGURE 38, 52-02 FIGURE 18.
- [SDR AT0000046](https://openairdocs.org/sdr/AT0000046.md): Frame · corroded · Jan 23, 2000 · N803AT · Doug DC932 · Fuselage Main, Frame
  > FOUND AFT PIT LONGERON CORRODED AT BS 832 ALONG FRAME. REMOVED CORROSION, TREATED, ALODINED AND PRIMED IAW DC9 SRM 53-01 FIGURE 1, TABLE 2, 51-10-3.
- [SDR AT0000044](https://openairdocs.org/sdr/AT0000044.md): Web · corroded · Jan 19, 2000 · N803AT · Doug DC932 · Fuselage Internal Mounting Structure
  > FOUND ELECTRICAL COMPARTMENT COCKPIT SUBFLOOR CORRODED AT BS 150-160. CUT OUT CORRODED AREA OF SUBFLOOR, FABRICATED FILLER/DOUBLER AND INSTALLED IAW DC9 SRM 51-30-2, 53-11-1, 53-01 FIGURE 4, 51-10-4, 51-10-3, 53-01.
- [SDR AT0000043](https://openairdocs.org/sdr/AT0000043.md): Floorbeam · corroded · Jan 19, 2000 · N803AT · Doug DC932 · Fuselage Main, Floor Beam
  > FOUND AFT PIT CABIN FLOORBEAM HAS EXFOLIATED CORROSION AT BS 996. REMOVED FLOORBEAM UPPER CAP, FABRICATED NEW CAP ANGLE, TREATED, PRIMED AND INSTALLED NEW CAP ANGLE IAW DC9 SRM 51-30-2, 51-30-5, 53-11-3 FIGURE 11, 51-10-4, 51-30-3.
- [SDR AT0000045](https://openairdocs.org/sdr/AT0000045.md): Fitting · corroded · Jan 18, 2000 · N803AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND DURING REMOVAL OF WEB, FITTING WAS EXFOLIATED WITH CORROSION AT BS 996. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-01 FIGURE 1, 51-10-4, 51-30-5.
- [SDR AT0000047](https://openairdocs.org/sdr/AT0000047.md): Doubler · corroded · Jan 17, 2000 · N803AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND CORROSION OUT OF LIMITS ON G-4 LEFT HAND GALLEY SIDEWALL. CUT OUT CORRODED AREA, FABRICATED FILLER/DOUBLER, AND INSTALLED IAW DC9 SRM 51-10-3, 51-10-4, 51-30-2.
- [SDR AT0000039](https://openairdocs.org/sdr/AT0000039.md): Angle · corroded · Jan 13, 2000 · N803AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND ELECTRICAL EQUIPMENT COMPARTMENT SUPPORT BETWEEN BS 110-120 IS CORRODED FROM LONGERON 25R TO 26R. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED CORROSION FROM COMPARTMENT, TREATED WITH ALODINE. FABRICATED REPAIR ANGLE FOR BRACKETS, PRIMED SUPPORT BRACK
- [SDR AT9900894](https://openairdocs.org/sdr/AT9900894.md): Light · inoperative · Dec 19, 1999 · N803AT · Doug DC932 · Emergency Lighting
  > DURING SERVICE CHECK, LEFT AFT OVERWING EMERGENCY EXIT IDENTIFIER LIGHT AT BS 669 WAS INOPERATIVE. TIGHTENED NUT ON GROUND TERMINAL OF LIGHT FIXTURE L2-245 AT BS 669 IAW DC9 MM 33-53.
- [SDR AT9900606](https://openairdocs.org/sdr/AT9900606.md): Floor · weak · Aug 14, 1999 · N803AT · Doug DC932 · Fuselage Floor Panel
  > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, UPON INSTALLATION FOUND CABIN FLOORBOARD NR 97 WEAK. FABRICATED A REPLACEMENT FLOORBOARD PANEL IAW DC9 SRM 53-21-0, DOUGLASS DRAWING NR 9915532 AND TIMCO RES NR 07642.
- [SDR AT9900604](https://openairdocs.org/sdr/AT9900604.md): Bracket · corroded · Aug 9, 1999 · N803AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND CORROSION ON TOP OF CONTROL CABLE AILERON PULLEY TOWER IN FORWARD OUTBOARD OF LEFT WHEEL WELL. REMOVED AND REPLACED PULLEY BRACKET AND HARDWARE IAW DC9 MM 20-16-0, 27-61-10, AND TIMCO EO NR 99-1207.
- [SDR AT9900775](https://openairdocs.org/sdr/AT9900775.md): Web · corroded · Aug 6, 1999 · N803AT · Doug DC932 · Fuselage Floor Panel
  > FOUND 4 CRACK AT BS 955-960, LBL 48-52 IN CUSP WEB AND CORROSION OUT OF LIMITS. FABRICATED REPAIR IAW DC9 SRM 53-05 FIGURE 97, 51-10-3, 51-30-1, 51-30-2, AND DC9 MM 53-20-1.
- [SDR AT9900605](https://openairdocs.org/sdr/AT9900605.md): Skin · chafed · Aug 4, 1999 · N803AT · Doug DC932 · Vertical Stabilizer
  > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE LEFT LOWER AFT BANANA FAIRING ON THE VERTICAL STABILIZER AND SKIN CHAFFED AT YV 227-247. BLEND CHAFFED AREA ON THE BANANA FAIRING AND FABRICATED NEW SKIN PANEL FOR THE VERTICAL STABILIZER. HEAT TREATED,
- [SDR AT9900776](https://openairdocs.org/sdr/AT9900776.md): Web · corroded · Jul 29, 1999 · N803AT · Doug DC932 · Fuselage Miscellaneous Structure
  > FOUND CUSP WEB AT BS 945-965 WITH EXFOLIATED CORROSION. FABRICATED REPAIR WEB IAW DC9 SRM 53-05 FIGURE 97, 51-10-3, 51-30-1, 51-30-2, AND DC9 MM 53-20-1.
- [SDR AT9900603](https://openairdocs.org/sdr/AT9900603.md): Skin · cracked · Jul 29, 1999 · N803AT · Doug DC932 · Cargo/Baggage Doors
  > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE AFT CARGO DOOR OUTER SKIN CRACK AT FASTENERS ON THE LOWER SIDE. REMOVED LOWER HALF OF PRESSURE SEAL FOR ACCESS. CUT OUT CRACKED AREA, NDT VERIFIED CRACK TERMINATION. DRILLED DOUBLER, TRIMMED, DEBURRED, P
- [SDR AT9900805](https://openairdocs.org/sdr/AT9900805.md): Longeron · corroded · Jul 25, 1999 · N803AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FOUND AFT PIT LONGERON AT BS 870-965 CORRODED. INSTALLED LONGERON REPAIR BETWEEN BS 870-955 IAW DC9 SRM 53-03 FIGURE 2A, 51-10-2, 51-10-4, 51-30-2, 51-70-2, 53-02 FIGURE 14.
- [SDR AT9900777](https://openairdocs.org/sdr/AT9900777.md): Skin&Longeron · corroded · Jul 24, 1999 · N803AT · Doug DC932 · Fuselage Main, Plate/Skin
  > LOWER KEEL BEAM SKIN AT BS 658-756 HAS A BULDGING AREA OF CORROSION THAT HAS PUSHED OUT AND CRACKED THE SKIN. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPLACED SKIN AT BS 658-756 AND LONGERON AT 29L AND 29R IAW DC9 SRM 53-04 FIGURE 42, 52-05 FIGURE 4
- [SDR AT9900615](https://openairdocs.org/sdr/AT9900615.md): Cusp Web · corroded · Jul 22, 1999 · N803AT · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FLORIDA, FOUND RT CUSP WEB CORRODED AT BS 945-965. REMOVED CUSP WEB. FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR SECTIONS OF WEB IAW DC9 SRM 53-05 FIG 97 AND MM 53-20-1.
- [SDR AT9900614](https://openairdocs.org/sdr/AT9900614.md): Floor · cracked · Jul 22, 1999 · N803AT · Doug DC932 · Fuselage Floor Panel
  > DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FLORIDA, FOUND CUSP WEB CRACKED AT BS 955-960 LBL 48-52. REMOVED CUSP FOUND CORROSION. FORMED, DRILLED AND DEBURRED ONE CUSP SECTION AND FOUR REPAIR STRAPS. TREATED, PRIMED AND INSTALLED IAW DC9 SRM 53-05 FIG 9
- [SDR AT9900610](https://openairdocs.org/sdr/AT9900610.md): Seat Track · corroded · Jul 19, 1999 · N803AT · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE LEFT OUTBOARD SEAT TRACK AT BS 570 - 590 WITH NICKS, SCRATCHES AND CORROSION. CUT OUT SECTION OF SEAT TRACK, FABRICATED, DRILLED, DEBURRED, COUNTERSUNK, AND INSTALLED IAW DC9 SRM 51-10-3, 53-05-0, 51-30-
- [SDR AT9900804](https://openairdocs.org/sdr/AT9900804.md): Seat Track · corroded · Jul 18, 1999 · N803AT · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND RIGHT INBOARD SEAT TRACK AT BS 218-965 WITH NICKS, SCRATCHES AND CORROSION. REPLACED SEAT TRACK IAW DC9 SRM 53-05 FIGURE 4, 51-30-2, 51-10-3.
- [SDR AT9900618](https://openairdocs.org/sdr/AT9900618.md): Longeron · corroded · Jul 14, 1999 · N803AT · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FLORIDA, FOUND AFT PIT LONGERON 30 CORRODED AT BS 870-965. CUT LONGERON FROM BS 870-955. REMOVED SHEAR TIES, FLOOR SUPPORT AND CUT FRAME AT BS 917. REMOVED LONGERON, DRILLED, DEBURRED, TREATED, PRIMED AND INSTA
- [SDR AT9900619](https://openairdocs.org/sdr/AT9900619.md): Adf Panel · corroded · Jul 8, 1999 · N803AT · Doug DC932 · Automatic Direction Finder (ADF) System
  > DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FLORIDA, FOUND FLAKING PAINT AND FLARE SPRAY ON LEFT FORWARD ADF PANEL. REMOVED CORROSION AND PEELING FLARE SPRAY FROM ADF PANEL. CLEANED, PREPARED AREA AND APPLIED ASTRO STRIKE. REMOVED AND REPLACED ANTENNA FEE
- [SDR AT9900617](https://openairdocs.org/sdr/AT9900617.md): Seat Track · corroded · Jul 8, 1999 · N803AT · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FLORIDA, FOUND RT INBOARD SEAT TRACK SCRATCHED AND CORRODED AT BS 218 TO 965. REMOVED SECTION OF SEAT TRACK FROM BS 218-235 AT EXISTING SPLICE. FABRICATED REPAIR SECTION, ALODINED, PRIMED AND INSTALLED SECTION A
- [SDR AT9900616](https://openairdocs.org/sdr/AT9900616.md): Skin · corroded · Jul 6, 1999 · N803AT · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FLORIDA, FOUND LOWER KEEL BEAM SKIN AT BS 770 HAS AN AREA OF BULGING CORROSION THAT HAS PUSHED OUT AND CRACKED THE SKIN. REMOVED SKIN PANEL AND LONGERONS 29L AND 29R FROM BS 658-756. DRILLED, DEBURRED, COUNTERSU
- [SDR AT9900620](https://openairdocs.org/sdr/AT9900620.md): Skin · misrepaired · Jun 27, 1999 · N803AT · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FLORIDA, FOUND CLASS III TEMPORARY REPAIR ON FUSELAGE FORWARD OF RIGHT WING ROOT PER DC9 SRM 53-40 FIG 12B SHT 15 PAGE 60A. REMOVED BLIND RIVETS AND REPLACED WITH SOLID FASTENERS. CHANGED CLASS III REPAIR TO CLA

## 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 = 'N803AT' AND deregistration_id = 'N803AT-2003-08-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N803AT-2003-08-18/reports

---
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