# Service difficulty reports: N70352, cancelled Nov 24, 2009

A list on [N70352, cancelled Nov 24, 2009](https://openairdocs.org/deregistered/N70352-2009-11-24.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 · 56 reports

- [SDR CALA0700325](https://openairdocs.org/sdr/CALA0700325.md): Stringer · cracked · Jun 26, 2007 · N70352 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A.25 INCH CRACK IN TAIL COMPARTMENT STRINGER 21R BETWEEN STA 1040 AND 1064. A REPAIR ANGLE AND SHIM WERE INSTALLED IAW SRM 53-00-00.
- [SDR CALA0700322](https://openairdocs.org/sdr/CALA0700322.md): Skin · cracked · Jun 26, 2007 · N70352 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1.5 INCH CRACK IN THE FUSELAGE SKIN AT AFT EDGE INSTRUMENT COOLING AIR DUCT OUTLET, STA 380, LBL 4, S28L TO S28R. THE CRACK WAS STOP DRILLED AND AN EXTERNAL DOUBLER AND INTERNAL DOUBLER WERE INSTALLED IAW ECRA 5330-02894.
- [SDR CALA0700320](https://openairdocs.org/sdr/CALA0700320.md): Frame · cracked · Jun 25, 2007 · N70352 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A.75 INCH CRACK IN FORWARD CARGO DOOR CUTOUT FORWARD FRAME AT LOWER STOP PAD, STA 440, S16R TO S27R. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700318](https://openairdocs.org/sdr/CALA0700318.md): Skin · cracked · Jun 24, 2007 · N70352 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 2.2 INCH CRACK IN THE FUSELAGE SKIN AT THE AFT LOWER CORNER OF THE R-1 DOOR. REPAIRED IAW SRM 53-10-01, REPAIR 2.
- [SDR CALA0700317](https://openairdocs.org/sdr/CALA0700317.md): Frame · cracked · Jun 24, 2007 · N70352 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A.5 INCH CRACK IN FORWARD CARGO DOOR CUTOUT AFT FRAME AT LOWER PAD FITTING, STA 480-500, S16R TO S27R. A NEW FRAME WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0700315](https://openairdocs.org/sdr/CALA0700315.md): Floorbeam · corroded · Jun 20, 2007 · N70352 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND AFT ENTRY FLOORBEAM UPPER CHORD CORRODED IN NUMEROUS AREAS THE ENTIRE LENGTH, STA 986.5, LBL 40 TO RBL 40. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03851.
- [SDR CALA0700312](https://openairdocs.org/sdr/CALA0700312.md): Floorbeam · corroded · Jun 19, 2007 · N70352 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND MAIN CABIN FLOORBEAM HAD CORROSION EXTENDING UNDER FLOOR MOUNT AT STA 946, LBL 13. THE UPPER FLANGE I-BEAM WAS REMOVED AND REPLACED FROM RBL 35 TO LBL 35 IAW SRM 53-00-51, FIGURE 201.
- [SDR CALA0700305](https://openairdocs.org/sdr/CALA0700305.md): Floorbeam · corroded · Jun 14, 2007 · N70352 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED AT STA 967, RBL 28. THE FLOORBEAM WAS REPAIRED IAW SRM 53-30-51, REPAIR 2.
- [SDR CALA0600418](https://openairdocs.org/sdr/CALA0600418.md): Spar · cracked · May 3, 2006 · N70352 · Boeing 7373T0 · Horizontal Stabilizer, Spar/Rib
  > LEFT REAR SPAR CRACKED 3 INCHES AT STA 297. REPAIRED IAW ECRA 5510-01835.
- [SDR CALA0500377](https://openairdocs.org/sdr/CALA0500377.md): Keelbeam · corroded · Oct 25, 2005 · N70352 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND RT LOWER CHORD OF KEELBEAM CORRODED AT STA 540, RT A/C BAY COMPARTMENT. THE CORROSION WAS REMOVED IAW ECRA 5310-04491.
- [SDR CALA0500314](https://openairdocs.org/sdr/CALA0500314.md): Skin · cracked · Sep 12, 2005 · N70352 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > MAINTENANCE FOUND A 2 INCH CRACK IN RT FUSELAGE SKIN AT STA 727D AND S23R. A REPAIR WAS INSTALLED IAW ECRA 5330-03482. A DIP WAS ISSUED TO REINSPECT THE AREA WITHIN 60,000 FLIGHT CYCLES AND TO ACCOMPLISH SUBSEQUENT REPEAT INSPECTIONS EVERY 25,000 FLIGHT CYCL
- [SDR CALA0400679](https://openairdocs.org/sdr/CALA0400679.md): Skin · cracked · Oct 15, 2004 · N70352 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > A WALKAROUND INSPECTION FOUND A 3 INCH CRACK IN FUSELAGE SKIN AT STA 727D TO STA 727E, S22L TO S24L. THE SKIN WAS REPAIRED IAW ECRA 5330-03376.
- [SDR CALA0400586](https://openairdocs.org/sdr/CALA0400586.md): Drive Shaft · sheared · Jul 24, 2004 · N70352 · Boeing 7373T0 · Accessory Gearboxes
  > THE NR 2 ENGINE STOPPED RUNNING AT TOP OF CLIMB AT FL 270 AFTER DEPARTING DFW BOUND FOR IAH. THE ENGINE FAILURE CHECKLIST WAS PERFORMED. A RESTART WAS NOT ATTEMPTED BECAUSE NO OIL PRESSURE AND NO N2 WAS PRESENT. THE FLIGHT CONTINUED TO IAH WHERE IT LANDED W
- [SDR CALA0400564](https://openairdocs.org/sdr/CALA0400564.md): Battery Pack · inoperative · Jul 3, 2004 · N70352 · Boeing 7373T0 · Emergency Lighting
  > INSPECTION FOUND THE EMERGENCY LIGHTS INOPERATIVE NEAR L-1 DOOR. THE OVERHEAD BATTERY PACK IN FORWARD GALLEY WAS REMOVED AND REPLACED.
- [SDR CALA0400289](https://openairdocs.org/sdr/CALA0400289.md): Megaphone · inoperative · Mar 28, 2004 · N70352 · Boeing 7373T0 · Emergency Equipment
  > THE MEGAPHONE IN FIRST CLASS CABIN WAS FOUND INOPERATIVE. THE MEGAPHONE WAS REPLACED.
- [SDR CALA0300327](https://openairdocs.org/sdr/CALA0300327.md): Skin · cracked · Jun 21, 2003 · N70352 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 2 INCH CRACK IN INTERIOR SKIN OF FORWARD CARGO DOOR LOCATED OVER HANDLE AREA. A DOUBLER WAS INSTALLED IAW ECRA 5232-01031.
- [SDR CALA0300325](https://openairdocs.org/sdr/CALA0300325.md): Angle · corroded · Jun 17, 2003 · N70352 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SUPPORT ANGLE CORRODED AT STA 1016, BL 0. THE ANGLE WAS REPLACED IAW SRM 51-10-02 AND ECRA 5311-01152.
- [SDR CALA0300316](https://openairdocs.org/sdr/CALA0300316.md): Skin · gouged · Jun 16, 2003 · N70352 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A GOUGE IN CENTER OF AFT BAGGAGE BIN DOOR EXTERIOR SKIN ABOUT 12 INCHES ABOVE HANDLE. THE SKIN WAS REPAIRED IAW SRM 52-00-01, PAGE 203.
- [SDR CALA0300314](https://openairdocs.org/sdr/CALA0300314.md): Skin · cracked · Jun 14, 2003 · N70352 · Boeing 7373T0 · Wing, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN NR 4 SLAT ACTUATOR CUTOUT ON RT FIXED LEADING EDGE SKIN AT WBL 325. A DOUBLER WAS INSTALLED IAW SRM 57-41-01.
- [SDR CALA0300307](https://openairdocs.org/sdr/CALA0300307.md): Skin · cracked · Jun 11, 2003 · N70352 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND A 2 INCH CRACK IN NR 6 SLAT PANEL SKIN AT LOWER RIVET LOCATED JUST O/B OF I/B AUX TRACK, RIGHT SLAT STA 300. A REPAIR WAS INSTALLED IAW SRM 57-43-01.
- [SDR CALA0300302](https://openairdocs.org/sdr/CALA0300302.md): Skin · cracked · Jun 10, 2003 · N70352 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.5 INCH CRACK IN LT WINDSHIELD POST SKIN. THE CRACK WAS ROUTED OUT AND DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-10-01, FIGURE 210.
- [SDR CALA0300301](https://openairdocs.org/sdr/CALA0300301.md): Fitting · cracked · Jun 9, 2003 · N70352 · Boeing 7373T0 · Horizontal Stabilizer Structure
  > INSPECTION FOUND A 4 INCH CRACK IN HORIZONTAL STABILIZER CENTER SECTION UPPER CROSS BEAM FITTING AT STA 1121, LBL 10. THE FITTING WAS REMOVED AND REPLACED IAW BOEING DRAWING 65-47598 AND SRM 51-40-2.
- [SDR CALA0300300](https://openairdocs.org/sdr/CALA0300300.md): Floor Support · corroded · Jun 9, 2003 · N70352 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED FROM STA 787 TO 850 AT STRINGER 25R. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-02.
- [SDR CALA0300298](https://openairdocs.org/sdr/CALA0300298.md): Fitting · cracked · Jun 8, 2003 · N70352 · Boeing 7373T0 · Horizontal Stabilizer Structure
  > INSPECTION FOUND A 1 INCH CRACK IN HORIZONTAL STABILIZER CENTER SECTION UPPER CROSS BEAM FITTING AT STA 1121, RBL 10. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02, FIGURE 12, SHEET 2.
- [SDR CALA0300296](https://openairdocs.org/sdr/CALA0300296.md): Skin · cracked · Jun 7, 2003 · N70352 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND A 1 INCH CRACK IN NR 5 SLAT PANEL AT I/B AUX TRACK. REPAIRED SLAT SKIN IAW SRM 57-43-01, FIGURE 206, SHEETS 1-4.
- [SDR CALA0300295](https://openairdocs.org/sdr/CALA0300295.md): Skin · cracked · Jun 7, 2003 · N70352 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN EXTERIOR FUSELAGE SKIN AT R-2 DOOR UPPER HINGE ARM CUTOUT. THE SKIN WAS REPAIRED IAW SRM 53-60-01.
- [SDR CALA0300294](https://openairdocs.org/sdr/CALA0300294.md): Cargo Track · corroded · Jun 7, 2003 · N70352 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RIGHT CARGO TRACK CORRODED AT STA 944. THE CORRODED SECTION OF TRACK WAS REMOVED AND A NEW TRACK AND SPLICE WERE INSTALLED IAW SRM 53-00-53.
- [SDR CALA0300293](https://openairdocs.org/sdr/CALA0300293.md): Intercostal · cracked · Jun 7, 2003 · N70352 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK AT SCREW HOLE OF INTERCOSTAL AT BS 500D-520, MAIN CABIN FLOOR CENTERLINE. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0300304](https://openairdocs.org/sdr/CALA0300304.md): Angle · cracked · Jun 6, 2003 · N70352 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN VERTICAL ANGLE ON BOTTOM END AT BS 616, LBL 65 OF MAIN CABIN, TOP OF WING CENTER SECTION. THE ANGLE FORMS I/B SECTION OF BS 616 FORGING AT EXIT HATCH. REPAIRED IAW ECRA 5311-01150.
- [SDR CALA0300292](https://openairdocs.org/sdr/CALA0300292.md): Fitting · corroded · Jun 6, 2003 · N70352 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND LEFT O/B SUPPORT FITTING CORRODED BETWEEN STA 1006 AND 1016, LBL 36. THE SUPPORT FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0300290](https://openairdocs.org/sdr/CALA0300290.md): Fitting · corroded · Jun 6, 2003 · N70352 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND FITTING O/B OF STRINGER 18R AT STA 1016 CORRODED. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0300285](https://openairdocs.org/sdr/CALA0300285.md): Angle · corroded · Jun 6, 2003 · N70352 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT STA 940-992. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 53-60-15.
- [SDR CALA0300284](https://openairdocs.org/sdr/CALA0300284.md): Stiffener · corroded · Jun 5, 2003 · N70352 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND STIFFENERS ON FORWARD SIDE OF AFT PRESSURE BULKHEAD CORRODED AT STA 1016 BETWEEN S28L AND S28R. THE STIFFENERS WERE REPAIRED IAW BOEING DRAWING 65C28106 AND SRM 51-10-02.
- [SDR CALA0300330](https://openairdocs.org/sdr/CALA0300330.md): Frame · cracked · Jun 2, 2003 · N70352 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN THE INNER CHORD OF THE LT FRAME AT STA 616. REPAIRED IAW ECRA 5311-01150.
- [SDR CALA0300281](https://openairdocs.org/sdr/CALA0300281.md): Stringer · cracked · Jun 2, 2003 · N70352 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A.5 INCH CRACK IN STRINGER 16L AT BS 500C + 4, JUST FORWARD OF LEFT ICE LIGHT HOUSING. THE STRINGER WAS REPAIRED IAW SRM 53-00-03, FIGURE 201.
- [SDR CALA0300277](https://openairdocs.org/sdr/CALA0300277.md): Floor Support · corroded · Jun 1, 2003 · N70352 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LEFT O/B FLOOR SUPPORT CORRODED BETWEEN STA 1006-1016, LBL 36. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0200482](https://openairdocs.org/sdr/CALA0200482.md): Skin · cracked · Oct 2, 2002 · N70352 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > A WALKAROUND INSPECTION FOUND A 3" CRACK IN L/H FUSELAGE SKIN AT STA 727C, STRINGER 25L AND 26L. THE CRACKED AREA OF SKIN WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-00-00, FIGURE 201.
- [SDR CALA0100954](https://openairdocs.org/sdr/CALA0100954.md): Flange · corroded · Oct 16, 2001 · N70352 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > AFT CARGO COMPARTMENT UNDER LAV FLOOR BEAMS AT STATION 986.5 NUT CLIPS CORRODED ON UPPER BEAM. REMOVED DAMAGED UPPER BEAM AND CLIPS. INSTALLED REPAIR DOUBLER PER SRM 51-40-2.
- [SDR CALA0100953](https://openairdocs.org/sdr/CALA0100953.md): Flange · corroded · Oct 16, 2001 · N70352 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > AFT CARGO COMPARTMENT UNDER RIGHT LAV FLOOR BEAM STATION 986.5 HAS CORROSION ON THE OUTBOARD. REMOVED CORRODED PREVIOUS REPAIR AND INSTALLED NEW UPPER FLANGE DOUBLER PER SRM 5310-03139 AND SRM 51-40-2.
- [SDR CALA0100952](https://openairdocs.org/sdr/CALA0100952.md): Flange · corroded · Oct 16, 2001 · N70352 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > AFT CARGO COMPARTMENT UNDER LEFT LAV FLOOR BEAM STATION STATION 986.5 CORRODED. REMOVED CORRODED REPAIR AND REINSTALLED NEW UPPER FLANGE DOUBLER PER SRM 5310-03139 ADN SRM 51-40-2.
- [SDR CALA0100951](https://openairdocs.org/sdr/CALA0100951.md): Cargo Track · cracked · Oct 15, 2001 · N70352 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD BAG BIN CRACKED (10 INCHES) ON RIGHT TIE DOWN RAIL FROM STATION 480 - 500. INSTALLED NUT PLATES ON UPPER FLANGE OF TIE DOWN RAIL PER SRM 51-10-2.
- [SDR CALA0100948](https://openairdocs.org/sdr/CALA0100948.md): Floor Support · cracked · Oct 15, 2001 · N70352 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > FBB 3 INCH CRACK ON FLOOR SUPPORT STRUCTURE BETWEEN STA 500 AND 500A AND ABOUT 2 INCHES TO RT SIDE FROM CENTER LINE MARKED. REMOVED AND REPLACED SUPPORT PER SRM 51-10-02.
- [SDR CALA0100941](https://openairdocs.org/sdr/CALA0100941.md): Web · cracked · Oct 11, 2001 · N70352 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN CABIN FLOOR WEB ON FORWARD SIDE OF FLOORBEAM AT BS 328. AN INTERCOSTAL WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0100940](https://openairdocs.org/sdr/CALA0100940.md): Web · cracked · Oct 11, 2001 · N70352 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN CABIN FLOOR WEB ON AFT SIDE OF FLOORBEAM AT BS 328. AN INTERCOSTAL WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0100827](https://openairdocs.org/sdr/CALA0100827.md): Control Cable · out of rig · Sep 3, 2001 · N70352 · Boeing 7373T0 · Landing Gear Retraction/Extension System
  > THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM DTW. THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDED WITHOUT INCIDENT. TROUBLESHOOTING FOUND THE RT MLG TELEFLEX CABLE OUT OF RIG. THE TELEFLEX CABLE WAS RIGGED AND AN ADJUSTMENT/TEST WAS PERFORMED IAW
- [SDR CALA0100012](https://openairdocs.org/sdr/CALA0100012.md): Socket · inoperative · Jan 11, 2001 · N70352 · Boeing 7373T0 · Emergency Lighting
  > INSPECTION FOUND THE AFT EXTERIOR OVERWING EXIT EMERGENCY LIGHT INOPERATIVE AT STA 773. THE SOCKET ASSEMBLY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD.
- [SDR CALA0001946](https://openairdocs.org/sdr/CALA0001946.md): Strut · flat · Dec 15, 2000 · N70352 · Boeing 7373T0 · Nose/Tail Landing Gear Strut/Axle
  > THE NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM IAH. QRH PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE STRUT FLAT. THE NOSE STRUT WAS REPLACED AND SERVICED IAW MM 32-2
- [SDR CALA0000002](https://openairdocs.org/sdr/CALA0000002.md): Fire Detector · malfunctioned · Jan 6, 2000 · N70352 · Boeing 7373T0 · Fire Detection
  > THE APU FIRE WARNING LIGHT ILLUMINATED WHILETHE APU WAS NOT RUNNING, AFTER TAKEOFF FROM JAX. THE FIRE BOTTLE WAS DISCHARGED, BUT THE LIGHT DID NOT EXTINGUISH. THE AIRCRAFT WAS RETURNED TO JAX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE O
- [SDR CALA9901541](https://openairdocs.org/sdr/CALA9901541.md): Fan · failed · Nov 29, 1999 · N70352 · Boeing 7373T0 · Cabin Cooling System
  > A BURNING ODOR ENTERED THE COCKPIT AND CABIN ON CLIMBOUT FROM ABQ. THE AIRCRAFT WAS RETURNED TO ABQ WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AVIONICS COOLING FAN INOPERATIVE. THE AVIONICS COOLING FAN WAS REMOVED AND REPLACED. OPERATIONAL CHE
- [SDR CALA9900871](https://openairdocs.org/sdr/CALA9900871.md): Skin · cracked · Jul 27, 1999 · N70352 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND A 1 CRACK IN NR 1 ENGINE PYLON SKIN AT PANEL CUTOUT 5727L (NAC STA 213). THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5430-01230.

Next page: https://openairdocs.org/deregistered/N70352-2009-11-24/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 = 'N70352' AND deregistration_id = 'N70352-2009-11-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N70352-2009-11-24/reports

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