# Service difficulty reports: N45793, cancelled Oct 25, 2003

A list on [N45793, cancelled Oct 25, 2003](https://openairdocs.org/deregistered/N45793-2003-10-25.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 2 · 94 reports

- [SDR CALA9901588](https://openairdocs.org/sdr/CALA9901588.md): Battery Pack · discharged · Dec 10, 1999 · N45793 · Boeing 727232 · Emergency Lighting
  > INSPECTION FOUND THE EMERGENCY LIGHT AT AFT AIRSTAIR INOPERATIVE. THE BATTERY PACK WAS REMOVED, RECHARGED, REINSTALLED, OPERATION CHECKED GOOD IAW MM 33-51-01, PAGE 6.
- [SDR CALA9901587](https://openairdocs.org/sdr/CALA9901587.md): Wire · broken · Dec 10, 1999 · N45793 · Boeing 727232 · Light System Wiring
  > INSPECTION FOUND THE EMERGENCY PATH LIGHTS IN SECTION 3 AND 4 INOPERATIVE. BROKEN WIRES AT SECTION 3 AND 4 WERE REPAIRED IAW MM 33-10-00 AND OPERATIONAL CHECK WAS GOOD.
- [SDR CALA9901586](https://openairdocs.org/sdr/CALA9901586.md): Battery Pack · discharged · Dec 10, 1999 · N45793 · Boeing 727232 · Emergency Lighting
  > THE RT OVERWING EMERGENCY EXIT LIGHTS IN THE MID AND AFT POSITIONS WERE FOUND INOPERATIVE. THE BATTERY PACK WAS REMOVED, RECHARGED, REINSTALLED AND OPERATION CHECKED GOOD IAW MM 33-51-01, PAGE 6.
- [SDR CALA9901585](https://openairdocs.org/sdr/CALA9901585.md): Battery · discharged · Dec 10, 1999 · N45793 · Boeing 727232 · Emergency Lighting
  > INSPECTION FOUND MID CABIN FIXED EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-51-00, PAGE 6.
- [SDR CALA9901584](https://openairdocs.org/sdr/CALA9901584.md): Wire · chafed · Dec 10, 1999 · N45793 · Boeing 727232 · Light System Wiring
  > INSPECTION FOUND THE LT OVERWING EMERGENCY LIGHTS IN MID AND AFT POSITIONS INOPERATIVE. MAINTENANCE FOUND A CHAFED WIRE BEHIND WHEEL WELL FAIRING PANEL AREA. THE WIRE WAS REPAIRED AND OPERATION CHECKED GOOD IAW MM 33-51-01, PAGE 6.
- [SDR CALA9901583](https://openairdocs.org/sdr/CALA9901583.md): Battery Pack · discharged · Dec 10, 1999 · N45793 · Boeing 727232 · Emergency Lighting
  > INSPECTION FOUND THE L-1 AND L-2 DOOR EXIT SIGNS INOPERATIVE. THE BATTERY PACK FOR EACH SIGN WAS REMOVED, RECHARGED, REINSTALLED AND OPERATION CHECKED GOOD IAW MM 33-51-01.
- [SDR CALA9901581](https://openairdocs.org/sdr/CALA9901581.md): Light · inoperative · Dec 9, 1999 · N45793 · Boeing 727232 · Emergency Lighting
  > INSPECTION FOUND THE EMERGENCY EXIT LIGHT AT AFT ENTRY INOPERATIVE. THE LIGHT ASSEMBLY WAS REPLACED AND OPERATION CHECKED IAW MM 33-50-01.
- [SDR CALA9901283](https://openairdocs.org/sdr/CALA9901283.md): Stringer · cracked · Sep 23, 1999 · N45793 · Boeing 727232 · Wing, Longeron/Stringer
  > INSPECTION FOUND A 5 INCH CRACK AT ATTACH POINT IN LT WING UPPER FORWARD STRINGER AT WING STA 629.0. THE CRACKED AREA WAS CUT OUT, REPAIR PARTS WERE INSTALLED IAW EA 5762-01050.
- [SDR CALA9901273](https://openairdocs.org/sdr/CALA9901273.md): Skin · delaminated · Sep 20, 1999 · N45793 · Boeing 727232 · Spoilers
  > INSPECTION FOUND O/B END UPPER SURFACE OF LT WING NR 7 SPOILER DELAMINATED. THE NR 7 SPOILER WAS REMOVED AND REPLACED IAW MM 27-62-1.
- [SDR CALA9901272](https://openairdocs.org/sdr/CALA9901272.md): Seat Track · corroded · Sep 20, 1999 · N45793 · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND G-1 GALLEY SEAT TRACK CORRODED AT STA 344-380. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-30-1, 51-10-06, 53-10-5, AND ECRA 5100-01844.
- [SDR CALA9901271](https://openairdocs.org/sdr/CALA9901271.md): Support · corroded · Sep 20, 1999 · N45793 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT CENTERLINE FLOORBEAM, STA 1035. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-2 AND 51-30-2.
- [SDR CALA9901251](https://openairdocs.org/sdr/CALA9901251.md): Wire · disconnected · Sep 17, 1999 · N45793 · Boeing 727232 · Light System Wiring
  > THE EMERGENCY EXIT LIGHT WIRING WAS FOUND PULLED OUT OF CONDUIT AND DISCONNECTED AT ROW 11. THE WIRING WAS RECONNECTED AND PLACED BACK INTO CONDUIT IAW MM 20-00-00.
- [SDR CALA9901250](https://openairdocs.org/sdr/CALA9901250.md): Intercostal · cracked · Sep 17, 1999 · N45793 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AT STA 990, STRINGER 23L. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2 AND 51-10-1.
- [SDR CALA9901232](https://openairdocs.org/sdr/CALA9901232.md): Frame · corroded · Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Main, Frame
  > INSPECTION FOUND FRAME CORRODED AT STA 580, STRINGER 26R-27R. THE CORRODED AREA WAS REMOVED IAW SRM 53-10-4 AND A REPAIR WAS INSTALLED IAW SRM 51-10-1 AND 53-10-4.
- [SDR CALA9901231](https://openairdocs.org/sdr/CALA9901231.md): Frame · corroded · Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Main, Frame
  > INSPECTION FOUND FRAME AND WEB CORRODED AT STA 1148 FROM STRINGER 27L-27R. THE WEB WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 51-10-6, 53-10-4, FIGURE 45, AND 51-30-2. THE FRAME WAS REPAIRED IAW SRM 53-10-4, FIGURE 15.
- [SDR CALA9901230](https://openairdocs.org/sdr/CALA9901230.md): Stringer · corroded · Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 29R CORRODED AT STA 344. THE SKIN WAS CUT AND CORRODED STRINGER WAS REMOVED. A FILLER, DOUBLER, AND STRINGER REPAIR WERE INSTALLED IAW SRM 53-30-3.
- [SDR CALA9901229](https://openairdocs.org/sdr/CALA9901229.md): Web · corroded · Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND WEB SKIN CORRODED AT STA 1142-1148, STRINGER 26R TO 20R. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2 AND 51-40-2.
- [SDR CALA9901228](https://openairdocs.org/sdr/CALA9901228.md): Floorbeam · corroded · Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 380, RBL 15. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-8 AND 51-30-2.
- [SDR CALA9901227](https://openairdocs.org/sdr/CALA9901227.md): Shear Tie · corroded · Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FRAME SHEAR TIES CORRODED AT STA 720B, STRINGER 28L-28R, STA 720C, S28L-28R, AND STA 720F, S25R-27R. THE SHEAR TIES WERE REMOVED AND REPLACED IAW SRM 51-10-1, 51-10-6, 53-10-4, 51-30-2.
- [SDR CALA9901226](https://openairdocs.org/sdr/CALA9901226.md): Shear Tie · corroded · Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SHEAR TIE CORRODED AT STA 1148, STRINGER 24R TO 27R. REPAIRED SHEAR TIE IAW SRM 53-10-4.
- [SDR CALA9901225](https://openairdocs.org/sdr/CALA9901225.md): Angle · corroded · Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND THREE ANGLES CORRODED IN KEEL BEAM AREA FROM STA 759-824. THE ANGLES WERE REMOVED AND REPLACED IAW SRM 51-40-4, 51-30-2, AND 51-10-1.
- [SDR CALA9901224](https://openairdocs.org/sdr/CALA9901224.md): Intercostal · cracked · Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN INTERCOSTAL BETWEEN STA 990 AND 1010 AT S24L. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-1, 51-40-3, AND 51-30-2.
- [SDR CALA9901223](https://openairdocs.org/sdr/CALA9901223.md): Angle · corroded · Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND KEEL BEAM ANGLES AT STA 750, RT SIDE AND STA 850, RBL 5 TO LBL 5 CORRODED. THE ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-30-2.
- [SDR CALA9901222](https://openairdocs.org/sdr/CALA9901222.md): Stringer · corroded · Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER S28R AND S27L CORRODED AT STA 660-680. THE CORRODED SECTION OF STRINGERS WERE REMOVED AND NEW SECTIONS WERE INSTALLED IAW 51-30-2, 53-10-3, 51-30-1, 51-10-2, AND 51-10-6.
- [SDR CALA9901221](https://openairdocs.org/sdr/CALA9901221.md): Frame · cracked · Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Main, Frame
  > INSPECTION FOUND A 4 INCH CRACK IN FRAME AT STA 500, STRINGER 21L. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER WAS INSTALLED IAW SRM 51-40-3.
- [SDR CALA9901220](https://openairdocs.org/sdr/CALA9901220.md): Shear Tie · corroded · Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Internal Mounting Structure
  > INSPECTION FOUND SHEAR TIES CORRODED AT STA 990, S29R AND STA 1090, S29R. NEW SHEAR TIES WERE INSTALLED IAW SRM 53-10-4, 51-30-2, AND 51-10-2.
- [SDR CALA9901219](https://openairdocs.org/sdr/CALA9901219.md): Keel Beam · corroded · Sep 15, 1999 · N45793 · Boeing 727232 · Fuselage Main, Keel
  > INSPECTION FOUND KEEL BEAM WEB CORRODED AT STA 801, LT SIDE. THE CORRODED WEB AREA WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-1.
- [SDR CALA9901169](https://openairdocs.org/sdr/CALA9901169.md): Stringer · corroded · Sep 9, 1999 · N45793 · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND FORWARD CARGO STRINGER 27L CORRODED AT FS 660-640, FS 720C-720B, AND 720B-720A. THE CORRODED AREAS WERE CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-10-3 AND 51-20-0.
- [SDR CALA9900021](https://openairdocs.org/sdr/CALA9900021.md): Wire · shorted · Jan 14, 1999 · N45793 · Boeing 727232 · Light System Wiring
  > EMERGENCY EXIT LIGHT RIGHT HAND CONTROL CIRCUIT BREAKER POPPED AND WOULD NOT RESET. FOUND WIRE SHORTED IN AFT LEFT TAIL COMPARTMENT. SECURED WIRES AND PROTECTED PER STANDARD PRACTICES. LIGHTS OPS CHECK NORMAL.
- [SDR CALA9802132](https://openairdocs.org/sdr/CALA9802132.md): Floor · corroded · Dec 2, 1998 · N45793 · Boeing 727232 · Fuselage Floor Panel
  > INSPECTION FOUND CABIN FLOOR PAN CORRODED AT AFT ENTRY STA 1177 TO 1171, BL 0 TO LBL 18. THE FLOOR PAN WAS REMOVED AND A NEW FLOOR PAN WAS INSTALLED IAW SRM 53-10-2.
- [SDR CALA9802125](https://openairdocs.org/sdr/CALA9802125.md): Floor · corroded · Nov 30, 1998 · N45793 · Boeing 727232 · Fuselage Floor Panel
  > INSPECTION FOUND CORROSION ON RT AFT LAV FLOOR PAN AT BS 1111 TO 1183. THE FLOOR PAN WAS REMOVED AND A NEW PAN WAS INSTALLED IAW SRM 51-30-2, 51-40-2 FIGURE 1, 51-10-2 AND MM 51-20-11.
- [SDR CALA9802038](https://openairdocs.org/sdr/CALA9802038.md): Skin · delaminated · Nov 4, 1998 · N45793 · Boeing 727232 · Trailing Edge Flaps
  > INSPECTION FOUND RT WING O/B TE AFT FLAP O/B END UPPER SURFACE DELAMINATED AT SPAR. THE AFT FLAP WAS REMOVED AND REPLACED IAW MM 27-51-11.
- [SDR CALA9802037](https://openairdocs.org/sdr/CALA9802037.md): Fuse · blown · Nov 4, 1998 · N45793 · Boeing 727232 · Emergency Lighting
  > INSPECTION FOUND LT AFT EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BLOWN FUSE AND OPERATION CHECKED GOOD IAW MM 33-51-00.
- [SDR CALA9802036](https://openairdocs.org/sdr/CALA9802036.md): Skin · delaminated · Nov 4, 1998 · N45793 · Boeing 727232 · Spoilers
  > INSPECTION FOUND TOP SURFACE OF NR 8 SPOILER DELAMINATED. THE NR 8 SPOILER WAS REMOVED AND REPLACED IAW MM 27-62-81.
- [SDR CALA9802019](https://openairdocs.org/sdr/CALA9802019.md): Stiffener · corroded · Nov 3, 1998 · N45793 · Boeing 727232 · Wing Miscellaneous Structure
  > INSPECTION FOUND RT WING FRONT SPAR VERTICAL STIFFENER CORRODED AT STA 244. THE STIFFENER WAS REPLACED IAW SRM 51-10-1 PAGE 4 AND 6A, SRM 51-10-2 AND 51-30-2.
- [SDR CALA9802018](https://openairdocs.org/sdr/CALA9802018.md): Spar · cracked · Nov 2, 1998 · N45793 · Boeing 727232 · Elevator, Spar/Rib
  > INSPECTION FOUND A.5 INCH CRACK IN LT ELEVATOR REAR SPAR. THE LT ELEVATOR WAS REMOVED AND REPLACED IAW MM 27-30-1, PAGE 401 AND 402. RIG AND OPERATIONAL CHECK WAS ACCOMPLISHED IAW MM 27-30-81 PAGE 507.
- [SDR CALA9802017](https://openairdocs.org/sdr/CALA9802017.md): Frame · cracked · Nov 2, 1998 · N45793 · Boeing 727232 · Fuselage Main, Frame
  > INSPECTION FOUND A.5 INCH CRACK IN FLOOR LEVEL RIB AT RT SIDE OF STA 344. A STRAP WAS INSTALLED IAW SRM 51-10-2 AND 53-10-8 FIGURE 6.
- [SDR CALA9802016](https://openairdocs.org/sdr/CALA9802016.md): Angle · cracked · Nov 2, 1998 · N45793 · Boeing 727232 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1 INCH CRACK IN C-3 DOOR T-ANGLE AT LOWER AFT DOOR STOP AREA. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-101.
- [SDR CALA9802015](https://openairdocs.org/sdr/CALA9802015.md): Chord · cracked · Nov 2, 1998 · N45793 · Boeing 727232 · Wing Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN LT WING AFT FALSE SPAR LOWER CHORD AT WBL 135.2. THE CRACKED AREA WAS CUT OUT AND SPLICE ANGLE AND STRAPS WERE INSTALLED IAW SRM 51-30-2, 51-10-2, ECRA 5740-01866.
- [SDR CALA9802011](https://openairdocs.org/sdr/CALA9802011.md): Bracket · cracked · Nov 2, 1998 · N45793 · Boeing 727232 · Leading Edge Slat Actuator
  > INSPECTION FOUND A.5 INCH CRACK IN INBOARD SUPPORT BRACKET AT LOWER END WHERE LT WING NR 1 L/E FLAP ACTUATOR IS MOUNTED. A NEW SUPPORT BRACKET WAS INSTALLED IAW SRM 51-30-2, PAGE 3.
- [SDR CALA9802010](https://openairdocs.org/sdr/CALA9802010.md): Skin · punctured · Nov 2, 1998 · N45793 · Boeing 727232 · Elevator, Plate/Skin
  > INSPECTION FOUND TWO.25 INCH DIAMETER HOLES IN RT ELEVATOR UPPER SKIN JUST AFT OF NR 3 ATTACH HINGE. A DOUBLER REPAIR WAS INSTALLED IAW SRM 55-20-3, PAGE 9.
- [SDR CALA9801992](https://openairdocs.org/sdr/CALA9801992.md): Terminal · inop · Oct 27, 1998 · N45793 · Boeing 727232 · Emergency Lighting
  > INSPECTION FOUND L-1 OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPAIRED TERMINAL AT LIGHT SOCKET ASSEMBLY AND OPERATIONAL CHECKS WERE GOOD AT MM 33-60-00, PAGE 201.
- [SDR CALA9801991](https://openairdocs.org/sdr/CALA9801991.md): Wire · loose · Oct 27, 1998 · N45793 · Boeing 727232 · Light System Wiring
  > INSPECTION FOUND THE L-2 OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE FOUND A LOOSE WIRE IN HARNESS. THE WIRE WAS REPQIRED AND OPERATIONAL CHECKS WERE GOOD IAAW MM 33-60-01, PAGE 201.
- [SDR CALA9800842](https://openairdocs.org/sdr/CALA9800842.md): Nut · leaking · May 9, 1998 · N45793 · Boeing 727232 · Hydraulic System, Main
  > ON TAKEOFF DURING GEAR RETRACTION, A-SYSTEM HYDRAULICS FAILED. FOUND LEAK AT A-SYSTEM RETURN LINE T-FITTING AT FWD KEEL BEAM RT WHEEL WELL. TIGHTENED B-NUT AND SERVICED SYSTEM.
- [SDR CALA9800002](https://openairdocs.org/sdr/CALA9800002.md): Hyd Line · ruptured · Jan 4, 1998 · N45793 · Boeing 727232 · Hydraulic System, Main
  > THE AIRCRAFT LOST A-SYSTEM HYDRAULIC QUANTITY DURING GEAR EXTENSION WHILE ON APPROACH TO IAH. ABNORMAL AND EMERGENCY PROCEDURES WERE FOLLOWED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT GEAR DOOR HYDRAULIC LINE RUPTURED. THE HYDRAULIC
- [SDR CALA9701752](https://openairdocs.org/sdr/CALA9701752.md): Relay · inoperative · Dec 12, 1997 · N45793 · Boeing 727232 · Fire Detection
  > THE NR 1 ENGINE FIRE DETECTION FAULT LIGHT AT B POSITION ILLUMINATED INTERMITTENTLY WHILE IN FLIGHT. TROUBLESHOOTING THE NR 1 ENGINE FIRE DETECTION SYSTEM FOUND R147 TEAT RELAY FAULTY. THE R147 RELAY WAS REMOVED AND REPLACED. THE NR 1 ENGINE B FIRE DETECTION
- [SDR CALA9701502](https://openairdocs.org/sdr/CALA9701502.md): Power Supply · inoperative · Oct 24, 1997 · N45793 · Boeing 727232 · Emergency Lighting
  > INSPECTION FOUND LEFT OVERWING EXIT AFT LIGHT INOPERATIVE. THE LEFT OVERWING EXIT LIGHT POWER SUPPLY WAS REMOVED AND REPLACED. OPERATION OF THE LIGHT CHECKED GOOD.
- [SDR CALA9701397](https://openairdocs.org/sdr/CALA9701397.md): Battery Pack · discharged · Sep 29, 1997 · N45793 · Boeing 727232 · Emergency Lighting
  > INSPECTION FOUND OVERHEAD EMERGENCY LIGHTS AT ROW 17 INOPERATIVE. THE BATTERY PACK WAS REPLACED.
- [SDR CALA9701186](https://openairdocs.org/sdr/CALA9701186.md): Stringer · cracked · Jul 28, 1997 · N45793 · Boeing 727232 · Wing, Longeron/Stringer
  > INSPECTION FOUND A 1 INCH CRACK IN UPPER AREA OF RT WING STRINGER, SECOND FROM AFT AT STA 686.5. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW EA 5762-01050 AND SRM 51-30-2.
- [SDR CALA9701183](https://openairdocs.org/sdr/CALA9701183.md): Rib · cracked · Jul 28, 1997 · N45793 · Boeing 727232 · Wing, Rib/Bulkhead
  > INSPECTION FOUND A 2 INCH CRACK IN RT WING FUEL TANK RIB AT WS 760. THE CRACK WAS STOP DRILLED, A REPAIR WAS INSTALLED IAW SRM 57-10-5.

Next page: https://openairdocs.org/deregistered/N45793-2003-10-25/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 = 'N45793' AND deregistration_id = 'N45793-2003-10-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N45793-2003-10-25/reports

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