# Service difficulty reports: N19357, cancelled Mar 21, 2013

A list on [N19357, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N19357-2013-03-21.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 · 88 reports

- [SDR CALA0700194](https://openairdocs.org/sdr/CALA0700194.md): Skin · corroded · Apr 21, 2007 · N19357 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN INSIDE AIR DISTRIBUTION BAY FWD SIDE OF STA 540 STR 28RT KEEL BEAM CORRODED. REPAIRED IAW ECRA 5331-01301.
- [SDR CALA0700193](https://openairdocs.org/sdr/CALA0700193.md): Frame · cracked · Apr 21, 2007 · N19357 · Boeing 7373T0 · Fuselage Main, Frame
  > FUSELAGE FRAME AND WEB CRACKED AT STA 639 AT STRINGER 17L. REPAIRED IAW ECRA 5311-01311.
- [SDR CALA0700192](https://openairdocs.org/sdr/CALA0700192.md): Frame · cracked · Apr 21, 2007 · N19357 · Boeing 7373T0 · Fuselage Main, Frame
  > LEFT FRAME CRACKED AT STA 639 ON O/B CHORD. REPAIRED IAW ECRA 5311-01312.
- [SDR CALA0700191](https://openairdocs.org/sdr/CALA0700191.md): Frame · cracked · Apr 21, 2007 · N19357 · Boeing 7373T0 · Fuselage Main, Frame
  > LEFT FRAME CRACKED AT STA 639 ON OUTBOARD CHORD. REPAIRED IAW ECRA 5311-01312.
- [SDR CALA0700190](https://openairdocs.org/sdr/CALA0700190.md): Plate · cracked · Apr 21, 2007 · N19357 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > NR 1 ENGINE PYLON PANEL OPENING FOR PANEL 5724 CRACKED. REPAIRED IAW ECRA 5431-01034.
- [SDR CALA0700189](https://openairdocs.org/sdr/CALA0700189.md): Keelbeam · damaged · Apr 21, 2007 · N19357 · Boeing 7373T0 · Fuselage Main, Keel
  > LWR FUSELAGE SKIN BULGING AT STA 540, RBL 4. REPAIRED IAW SRM 51-40-02, AND 53-60-12.
- [SDR CALA0700188](https://openairdocs.org/sdr/CALA0700188.md): Shear Tie · cracked · Apr 21, 2007 · N19357 · Boeing 7373T0 · Fuselage Internal Mounting Structure
  > FWD BAG BIN STA 500D, BL 0, CRACKED SHEAR TIE. REPAIRED IAW SRM 51-40-02, AND DRWG 69-73057-11.
- [SDR CALA0700187](https://openairdocs.org/sdr/CALA0700187.md): Frame · corroded · Apr 20, 2007 · N19357 · Boeing 7373T0 · Fuselage Main, Frame
  > CORROSION INSIDE LWR NOSE COMPARTMENT AFT SIDE OF CUTOUT, STA 227. REPAIRED IAW ECRA 5311-01308.
- [SDR CALA0700178](https://openairdocs.org/sdr/CALA0700178.md): Angle · cracked · Apr 16, 2007 · N19357 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE FOR INTERCOSTAL STRINGER 16L AT STA 344. REPAIRED IAW SRM 53-10-04.
- [SDR CALA0700176](https://openairdocs.org/sdr/CALA0700176.md): Door Frame · cracked · Apr 12, 2007 · N19357 · Boeing 7373T0 · Fuselage Main, Structure
  > CRACK AROUND LWR STOP PAD FITTING AT THE FWD CARGO DOOR AFT FRAME. REPAIRED IAW SRM 51-40-02.
- [SDR CALA0700172](https://openairdocs.org/sdr/CALA0700172.md): Door Frame · cracked · Apr 10, 2007 · N19357 · Boeing 7373T0 · Fuselage Main, Structure
  > FWD CARGO DOOR CUTOUT, FWD FRAME CRACKED AROUND THE LOWER STOP PAD FITTING. REPLACED FRAME IAW SRM 51-40-02, AND DRAWING 65-20722.
- [SDR CALA0600498](https://openairdocs.org/sdr/CALA0600498.md): Charger · inoperative · Nov 25, 2006 · N19357 · Boeing 7373T0 · Emergency Lighting
  > THE AFT CENTER EMERGENCY LIGHT BATTERY PACK AND CHARGER WERE FOUND INOPERATIVE. THE BATTERY AND CHARGER WERE REPLACED IAW MM 33-51-51-201.
- [SDR CALA0600368](https://openairdocs.org/sdr/CALA0600368.md): Skin · cracked · Sep 12, 2006 · N19357 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 2.5 INCH CRACK IN FUSELAGE SKIN AT STA 727D + 9.9, S22L. THE SKIN WAS REPAIRED IAW ECRA 5330-03580 AND A DIP WAS ISSUED TO REINSPECT THE AREA EVERY 9000 FLIGHT CYCLES PER PART 2 OF THE ECRA.
- [SDR CALA0600268](https://openairdocs.org/sdr/CALA0600268.md): Skin · corroded · Jul 12, 2006 · N19357 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND INSIDE SURFACE OF FUSELAGE SKIN PANEL CORRODED AT STA 967 BETWEEN S27L AND S27R. THE PANEL WAS REPAIRED IAW ECRA 5331-01246.
- [SDR CALA0400741](https://openairdocs.org/sdr/CALA0400741.md): Skin · cracked · Dec 9, 2004 · N19357 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A.5 INCH CRACK AT LIGHTENING HOLE (3RD FROM TOP AND 1 FROM AFT EDGE OF DOOR) IN AFT CARGO DOOR INNER SKIN. A DOUBLER WAS INSTALLED IAW ECRA 5230-01740.
- [SDR CALA0400740](https://openairdocs.org/sdr/CALA0400740.md): Skin · cracked · Dec 9, 2004 · N19357 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A.5 INCH CRACK AT LIGHTENING HOLE (2ND ROW FROM TOP) IN C-1 DOOR INNER SKIN. A DOUBLER WAS INSTALLED IAW ECRA 5232-01053.
- [SDR CALA0400724](https://openairdocs.org/sdr/CALA0400724.md): Seat Track · corroded · Nov 21, 2004 · N19357 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 328-360. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52.
- [SDR CALA0400723](https://openairdocs.org/sdr/CALA0400723.md): Floorbeam · corroded · Nov 21, 2004 · N19357 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 328, LBL 29 TO RBL 58. THE FLOORBEAM UPPER CHORD WAS REPLACED IAW SRM 53-10-51.
- [SDR CALA0400722](https://openairdocs.org/sdr/CALA0400722.md): Angle · corroded · Nov 20, 2004 · N19357 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND R-2 DOOR ZEE ANGLE CORRODED AT STA 907-1006, RBL 0 TO RBL 45. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400725](https://openairdocs.org/sdr/CALA0400725.md): Stringer · cracked · Nov 19, 2004 · N19357 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND MULTIPLE CRACKS IN STRINGER 16L AND 16R AT STA 540. THE CRACKS WERE 0.025 INCH LONG. CHANNELS WERE INSTALLED IAW ECRA 5310-03418.
- [SDR CALA0400720](https://openairdocs.org/sdr/CALA0400720.md): Fitting · corroded · Nov 19, 2004 · N19357 · Boeing 7373T0 · Fuselage, Landing Gear Attach Fittings
  > INSPECTION FOUND LT MLG UPLOCK FORWARD SUPPORT FRAME FITTINGS (2 EACH) CORRODED WITH BUSHINGS WORN AT STA 685, S17L. THE LUG FITTING WAS REWORKED TO REMOVE THE CORROSION AND SLEEVE AND BUSHINGS WERE INSTALLED IAW SRM 53-60-14.
- [SDR CALA0400718](https://openairdocs.org/sdr/CALA0400718.md): Splice · cracked · Nov 18, 2004 · N19357 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 0.65 INCH CRACK IN STRINGER 4R SPLICE AT STA 907. THE STRINGER SPLICE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400717](https://openairdocs.org/sdr/CALA0400717.md): Splice · cracked · Nov 18, 2004 · N19357 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN STRINGER 4L SPLICE AT STA 907. THE STRINGER SPLICE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400716](https://openairdocs.org/sdr/CALA0400716.md): Seat Track · corroded · Nov 17, 2004 · N19357 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND G-1 GALLEY HOLD DOWN SEAT TRACK CORRODED AT STA 277-294.5 FROM BL 0 TO RBL 43. THE CORRODED SECTION OF TRACK WAS REMOVED AND A NEW SECTION OF TRACK WAS INSTALLED IAW SRM 53-00-52, FIGURE 202, REPAIR 1.
- [SDR CALA0400714](https://openairdocs.org/sdr/CALA0400714.md): Connector · shorted · Nov 11, 2004 · N19357 · Boeing 7373T0 · Fire Protection System Wiring
  > THE APU DET INOP LIGHT CAME ON WHILE CLIMBING THROUGH FL 180. THE APU FIRE WARNING LIGHT WITH FIRE BELL ACTIVATED WHILE CLIMBING THROUGH FL 330. THE APU FIRE BOTTLE WAS DISCHARGED AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTE
- [SDR CALA0400592](https://openairdocs.org/sdr/CALA0400592.md): Skin · cracked · Jul 29, 2004 · N19357 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > MAINTENANCE FOUND THE FUSELAGE SKIN DENTED AND CRACKED BETWEEN STA 500D + 10 AND 520, S12L. THE CRACK WAS 1.4 INCHES LONG. AN INTERIM REPAIR WAS INSTALLED IAW ECRA 5330-03361. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR WITHIN 12 MONTHS.
- [SDR CALA0300539](https://openairdocs.org/sdr/CALA0300539.md): Skin · cracked · Sep 19, 2003 · N19357 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND A.5 INCH CRACK IN NR 1 ENGINE PYLON ACCESS PANEL NR 5727L CUTOUT. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01230.
- [SDR CALA0300535](https://openairdocs.org/sdr/CALA0300535.md): Cargo Track · damaged · Sep 18, 2003 · N19357 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND IMPACT DAMAGE TO AFT BAGGAGE BIN LT TIE DOWN RAIL AT BS 787. REPLACED TIE DOWN RAIL IAW SRM 53-00-53.
- [SDR CALA0300534](https://openairdocs.org/sdr/CALA0300534.md): Attach Fitting · corroded · Sep 17, 2003 · N19357 · Boeing 7373T0 · Horizontal Stabilizer, Attach Fittings
  > INSPECTION FOUND THE RT HORIZONTAL STABILIZER CENTER SECTION FORWARD UPPER LUG CORRODED AT AFT SIDE AROUND BUSHING. AN OVERSIZED BUSHING WAS INSTALLED IAW CMM 55-10-06 AND SRM 55-10-10.
- [SDR CALA0100381](https://openairdocs.org/sdr/CALA0100381.md): Fitting · gouged · Apr 16, 2001 · N19357 · Boeing 7373T0 · Spoilers
  > INSPECTION FOUND RT WING AFT SPAR SPOILER FITTING GOUGED AT WS 133. THE SPOILER FITTING WAS REPLACED IAW ECRA 5750-03517 AND AMS EA 04-5750-0842.
- [SDR CALA0100380](https://openairdocs.org/sdr/CALA0100380.md): Stiffener · cracked · Apr 16, 2001 · N19357 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN VERTICAL STIFFENER 18 INCHES ABOVE RT KEEL BEAM AT MAIN WHEEL WELL FORWARD BULKHEAD, STA 663, RBL 6. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 57-10-60 AND 51-10-01.
- [SDR CALA0100367](https://openairdocs.org/sdr/CALA0100367.md): Floorbeam · corroded · Apr 15, 2001 · N19357 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED ON UPPER SURFACE AROUND SCREW HOLES AT STA 967, RBL 27, LBL 6, AND LBL 27. REPAIR STRAPS AND SHIMS WERE INSTALLED IAW SRM 53-00-51, FIGURE 203, 51-20-01, AND 51-30-01.
- [SDR CALA0100360](https://openairdocs.org/sdr/CALA0100360.md): Attach Angle · corroded · Apr 13, 2001 · N19357 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FORWARD CARGO COMPARTMENT AFT PRESSURE BULKHEAD RT PANEL LOWER ATTACH ANGLE CORRODED AT STA 500D, S26R. THE ATTACH ANGLE WAS REMOVED AND TWO REPAIR ANGLES WERE INSTALLED IAW SRM 51-70-12 AND 51-40-02.
- [SDR CALA0100359](https://openairdocs.org/sdr/CALA0100359.md): Door Frame · cracked · Apr 13, 2001 · N19357 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 2.5 INCH CRACK IN AFT CARGO DOOR FORWARD FRAME SPLICE, THROUGH HOLE FOR TENSION PULLEY FOR COUNTER BALANCE MECHANISM, APPROXIMATELY 3.5 INCH FROM CENTERLINE OF DOOR. THE AFT CARGO DOOR WAS REMOVED AND THE FORWARD UPPER AND LOWER FRAME SECTI
- [SDR CALA0100358](https://openairdocs.org/sdr/CALA0100358.md): Intercostal · bent · Apr 13, 2001 · N19357 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND INTERCOSTAL IN FORWARD CARGO COMPARTMENT BENT ON UPPER SURFACE AT STA 440-460, S28R. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0100357](https://openairdocs.org/sdr/CALA0100357.md): Angle · cracked · Apr 13, 2001 · N19357 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT INTERCOSTAL ANGLE AT STA 927-947, BL 0. REMOVED CRACKED ANGLE ON INTERCOSTAL AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA0100356](https://openairdocs.org/sdr/CALA0100356.md): Floor Support · corroded · Apr 13, 2001 · N19357 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 967-986.5, LBL 18 AND RBL 18. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0100350](https://openairdocs.org/sdr/CALA0100350.md): Web · corroded · Apr 12, 2001 · N19357 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FORWARD CARGO COMPARTMENT DOOR OPENING LOWER SUPPORT PANEL (SILL WEB) CORRODED AT STA 440-490, S25R. THE SILL WEB WAS REMOVED AND A NEW SILL WEB WAS INSTALLED IAW SRM 51-40-5, 51-40-6, AND 51-40-8.
- [SDR CALA0100349](https://openairdocs.org/sdr/CALA0100349.md): Pan · corroded · Apr 12, 2001 · N19357 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR PAN AT STA 1016 TO AFT PRESSURE BULKHEAD CORRODED AT BL 0 TO LBL 48. THE FLOOR PAN WAS REMOVED AND A NEW FLOOR PAN WAS INSTALLED IAW SRM 51-10-02, DRAWING 65-52878 AND DRAWING 65C32677.
- [SDR CALA0100348](https://openairdocs.org/sdr/CALA0100348.md): Web · corroded · Apr 12, 2001 · N19357 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FORWARD END OF FLOOR PAN CORRODED AT STA 986.5-1016, RBL 36-48. THE CORRODED FLOOR PAN WEB WAS REMOVED AND A NEW FLOOR PAN WEB WAS INSTALLED IAW SRM 51-10-2, 51-40-01, AND DRAWING 65C32677.
- [SDR CALA0100346](https://openairdocs.org/sdr/CALA0100346.md): Seat Track · corroded · Apr 12, 2001 · N19357 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RIGHT O/B MAIN CABIN SEAT TRACK CORRODED AT STA 540-727. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52.
- [SDR CALA0100343](https://openairdocs.org/sdr/CALA0100343.md): Channel · corroded · Apr 12, 2001 · N19357 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CHANNEL CORRODED AT L-1 DOOR THRESHOLD CUSP WEB, L18L. THE CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0100342](https://openairdocs.org/sdr/CALA0100342.md): Angle · cracked · Apr 12, 2001 · N19357 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN FORWARD ENTRYWAY L-ANGLE AT FLOORBEAM AFT FLANGE ATTACH POINT, STA 344, LBL 10. THE L-ANGLE ON TOP OF INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-0.
- [SDR CALA0100341](https://openairdocs.org/sdr/CALA0100341.md): Floor Support · cracked · Apr 12, 2001 · N19357 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 3 INCH CRACK IN FORWARD CARGO COMPARTMENT FLOOR SUPPORT AT STA 500 ABOVE S27R. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-40-02 AND 51-40-03.
- [SDR CALA0100340](https://openairdocs.org/sdr/CALA0100340.md): Rib · worn · Apr 12, 2001 · N19357 · Boeing 7373T0 · Horizontal Stabilizer, Spar/Rib
  > INSPECTION FOUND RT ELEVATOR CENTER BALANCE HAD WEAR MARKS ON I/B WALL (HOR STAB RIB) AT STA 66.54. THE WORN AREA WAS REMOVED IAW SRM 57-70-10, PARA 4B. FILLER AND DOUBLER WERE INSTALLED IAW SRM 51-70-10, PARA 5 & 9. REINSTALLED SEALS REMOVED FOR REPAIR IAW
- [SDR CALA0100338](https://openairdocs.org/sdr/CALA0100338.md): Bearing · frozen · Apr 12, 2001 · N19357 · Boeing 7373T0 · Wing, Landing Gear Attach Fittings
  > INSPECTION FOUND RT MLG SUPPORT BEAM HAD LOOSE BEARING HOUSING AND FROZEN BEARING AT MOUNT FITTING. REMOVED NR 5 FLAP TRACK WITH TRANSMISSION, REMOVED FITTING AND INSTALLED NEW BEARING. REINSTALLED NR 5 FLAP TRACK WITH TRANSMISSION. MAINTENANCE WAS PERFORME
- [SDR CALA0100337](https://openairdocs.org/sdr/CALA0100337.md): Angle · corroded · Apr 11, 2001 · N19357 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND R-1 DOOR I/B CHORD O/B L-ANGLE CORRODED ON TOP AND BOTTOM SURFACES AT STA 312, S18R. THE L-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND 51-10-02.
- [SDR CALA0100336](https://openairdocs.org/sdr/CALA0100336.md): Intercostal · cracked · Apr 11, 2001 · N19357 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN FORWARD ENTRYWAY INTERCOSTAL AT FLOORBEAM ATTACH AREA, STA 312, BL 0. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0100335](https://openairdocs.org/sdr/CALA0100335.md): Floorbeam · corroded · Apr 11, 2001 · N19357 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT STA 986.5. THE CORRODED SECTION OF FLOORBEAM T-CAP WAS REMOVED AND A NEW SECTION WAS INSTALLED USING REPAIR STRAP AND ANGLES IAW SRM 51-40-00 AND ECRA 5310-03851.
- [SDR CALA0100334](https://openairdocs.org/sdr/CALA0100334.md): Frame · worn · Apr 11, 2001 · N19357 · Boeing 7373T0 · Nacelle/Pylon, Frame/Spar/Rib
  > INSPECTION FOUND RT ENGINE PYLON FORWARD O/B UPPER CHORD WORN. THE CHORD WAS REPAIRED IAW ECRA 5440-01221 AND EA 04-5440-0836.

Next page: https://openairdocs.org/deregistered/N19357-2013-03-21/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 = 'N19357' AND deregistration_id = 'N19357-2013-03-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N19357-2013-03-21/reports

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