# Service difficulty reports: N35832, cancelled Apr 17, 2006

A list on [N35832, cancelled Apr 17, 2006](https://openairdocs.org/deregistered/N35832-2006-04-17.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 3 · 119 reports

- [SDR CALA0400143](https://openairdocs.org/sdr/CALA0400143.md): Longeron · corroded · Feb 20, 2004 · N35832 · Doug DC982 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND LONGERON 30 CORRODED FORWARD OF SPLICE IN FORWARD BAGGAGE BIN BETWEEN STA 484 AND 503. THE CORRODED SECTION OF LONGERON WAS REMOVED AND A SPLICE AND LONGERON SECTION WERE INSTALLED IAW SRM 53-02, FIGURE 18.
- [SDR CALA0400130](https://openairdocs.org/sdr/CALA0400130.md): Cable · out of rig · Feb 17, 2004 · N35832 · Doug DC982 · Emergency Exits
  > THE TAIL CONE WOULD NOT DEPLOY USING AFT ENTRY DOOR HANDLE. THE TAIL CONE CABLES WERE RIGGED IAW MM 53-53-00.
- [SDR CALA0300006](https://openairdocs.org/sdr/CALA0300006.md): Longeron · cracked · Jan 9, 2003 · N35832 · Doug DC982 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 1" CRACK IN LONGERON 2L AT AFT SIDE OF BELTFRAME, STA 1415. A LONGERON SPLICE WAS INSTALLED IAW SRM 53-02.
- [SDR CALA0100990](https://openairdocs.org/sdr/CALA0100990.md): Intercostal · corroded · Oct 30, 2001 · N35832 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND INTERCOSTAL CORRODED AT LOWER SECTION OF AFT BAGGAGE BIN DOOR CUTOUT, STA 1174. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 53-01, FIGURE 1 AND 51-30-2.
- [SDR CALA0100985](https://openairdocs.org/sdr/CALA0100985.md): Skin · cracked · Oct 29, 2001 · N35832 · Doug DC982 · Wing, Plate/Skin
  > INSPECTION FOUND A 1.5" CRACK IN R/H WING UPPER L/E SKIN BETWEEN #2 & #3 SLAT PANELS AT WS XOS 286. A SKIN DOUBLER REPAIR WAS INSTALLED IAW ECRA 5720-01731.
- [SDR CALA0001406](https://openairdocs.org/sdr/CALA0001406.md): Channel · corroded · Sep 8, 2000 · N35832 · Doug DC982 · Wing Miscellaneous Structure
  > INSPECTION FOUND DOME NUT GANG CHANNEL AND OUTER SHIM OF LT WING LOWER FUEL TANK OPENING (PANEL 1371C) CORRODED. THE RUB STRIP AND GANG CHANNEL WERE REMOVED AND REPLACED IAW SRM 51-22-2 AND ECRA 5100-02063.
- [SDR CALA0001405](https://openairdocs.org/sdr/CALA0001405.md): Access Panel · cracked · Sep 8, 2000 · N35832 · Doug DC982 · Horizontal Stabilizer, Plate/Skin
  > INSPECTION FOUND A.5 INCH CRACK AT LAST RIVET HOLE IN THE FIXED SECTION ON O/B SIDE OF RT HORIZONTAL STABILIZER ELEVATOR ACCESS TO ELEVATOR GEAR TAB MECHANISM 3616A. THE PUSH ROD AND CONDUIT WERE REMOVED TO GAIN ACCESS IAW SRM 51-30-2. THE CRACK WAS STOP D
- [SDR CALA0001404](https://openairdocs.org/sdr/CALA0001404.md): Skin · dented · Sep 8, 2000 · N35832 · Doug DC982 · Leading Edge Devices
  > INSPECTION FOUND THE LT NR 5 SLAT LEADING EDGE DENTED. THE SLAT WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-80-01, SRM 57-06, FIGURE 1, AND 51-30-2.
- [SDR CALA0001393](https://openairdocs.org/sdr/CALA0001393.md): Floor Panel · corroded · Sep 4, 2000 · N35832 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND R-1 ENTRYWAY FLOOR PANEL CORRODED AT FS 148 - 200. THE CORRODED FLOOR PANEL AREA WAS REPAIRED IAW SRM 53-24-0, FIGURE 3, 51-10-3, AND ECRA 5100-01844.
- [SDR CALA0001391](https://openairdocs.org/sdr/CALA0001391.md): Access Panel · corroded · Sep 3, 2000 · N35832 · Doug DC982 · Wing, Plate/Skin
  > INSPECTION FOUND LT WING FUEL ACCESS PANELS 1303C, 1355C, AND 1363C CORRODED AND GOUGED. THE FUEL PANELS WERE REMOVED AND REPLACED IAW ECRA 5730-01688.
- [SDR CALA0001390](https://openairdocs.org/sdr/CALA0001390.md): Access Panel · corroded · Sep 3, 2000 · N35832 · Doug DC982 · Wing, Plate/Skin
  > INSPECTION FOUND RT WING FUEL ACCESS PANELS 1410C, 1409C, AND 1436C CORRODED AND GOUGED. THE FUEL PANELS WERE REMOVED AND REPLACED IAW ECRA 5730-01688.
- [SDR CALA0001368](https://openairdocs.org/sdr/CALA0001368.md): Slat Track · gouged · Sep 2, 2000 · N35832 · Doug DC982 · Leading Edge Devices
  > INSPECTION FOUND RT WING NR 5 SLAT TRACK GOUGED. THE SLAT TRACK WAS REMOVED AND REPLACED IAW MM 27-80-01.
- [SDR CALA0001362](https://openairdocs.org/sdr/CALA0001362.md): Panel · gouged · Sep 1, 2000 · N35832 · Doug DC982 · Wing, Plate/Skin
  > INSPECTION FOUND LT WING LOWER SURFACE FUEL ACCESS PANEL NR 2 GOUGED. THE PANEL WAS REPAIRED IAW SRM 5730-01688 AND SRM 51-30-2.
- [SDR CALA0001358](https://openairdocs.org/sdr/CALA0001358.md): Fitting · corroded · Sep 1, 2000 · N35832 · Doug DC982 · Spoilers
  > INSPECTION FOUND LEFT O/B FLIGHT SPOILER CENTER FITTING CORRODED. THE SPOILER WAS REMOVED IAW MM 27-62-01. THE HINGE FITTING WAS REMOVED AND REPLACED IAW OHM 27-61-10 AND THE SPOILER WAS REINSTALLED IAW MM 27-61-01.
- [SDR CALA0001357](https://openairdocs.org/sdr/CALA0001357.md): Access Panel · gouged · Sep 1, 2000 · N35832 · Doug DC982 · Wing, Plate/Skin
  > INSPECTION FOUND FUEL ACCESS PANELS NR 1, 6 AND 7 GOUGED AND CORRODED ON RT WING LOWER SURFACE. THE PANELS WERE REPAIRED IAW ECRA 5730-01688 AND SRM 51-30-2.
- [SDR CALA0001356](https://openairdocs.org/sdr/CALA0001356.md): Fitting · cracked · Sep 1, 2000 · N35832 · Doug DC982 · Leading Edge Devices
  > INSPECTION FOUND TWO 1 INCH CRACKS AT FASTENER HOLE OF RT WING NR 5 SLAT END FITTING. THE SEAL AND RETAINER ON END FITTING WERE REMOVED IAW SRM 51-30-3. THE CRACKS WERE WELDED IAW DPS 10.225. THE SEAL AND RETAINER WERE REINSTALLED IAW SRM 51-30-2.
- [SDR CALA0001355](https://openairdocs.org/sdr/CALA0001355.md): Floor Panel · corroded · Sep 1, 2000 · N35832 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND AFT CARGO FLOOR PANEL CORRODED AND DENTED AT STA 1211 - 1231. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 53-24-0, FIGURE 1A, 51-10-2, AND 51-60-0, PAGE 5.
- [SDR CALA0001350](https://openairdocs.org/sdr/CALA0001350.md): Floor Panel · corroded · Aug 30, 2000 · N35832 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND AFT CARGO FLOOR PANEL CORRODED AT FS 1211 - 1231. THE FLOOR PANEL WAS REPLACED IAW SRM 53-24-0, FIGURE 11A, 51-10-2, AND 51-60-0, PAGE 5.
- [SDR CALA0001349](https://openairdocs.org/sdr/CALA0001349.md): Fitting · corroded · Aug 30, 2000 · N35832 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND NR 4 GALLEY ATTACH MOUNT FITTINGS (2) CORRODED. THE FITTINGS WERE REMOVED AND REPLACED IAW ECRA 2530-01257.
- [SDR CALA0001342](https://openairdocs.org/sdr/CALA0001342.md): Floor Support · cracked · Aug 28, 2000 · N35832 · Doug DC982 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND A 6 INCH CRACK IN MID CARGO BAY FIBERGLASS FLOOR SUPPORT ANGLE AT STA 617, LONGERON 26R TO 27R. THE FLOOR SUPPORT ANGLE WAS REMOVED, REPAIRED WITH FIBERGLASS OVERLAY, AND REINSTALLED IAW SRM 51-70-1, FIGURE 4 AND 51-30-5.
- [SDR CALA0001341](https://openairdocs.org/sdr/CALA0001341.md): Web · cracked · Aug 28, 2000 · N35832 · Doug DC982 · Entrance Stairs
  > INSPECTION FOUND A 4.5 INCH CRACK IN AFT AIRSTAIR LT SIDE WEB. THE CRACKED AREA WAS CUT OUT IAW SRM 52-01, FIGURE 2. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 52-01, FIGURE 2, 51-30-2, AND 51-10-3.
- [SDR CALA0001334](https://openairdocs.org/sdr/CALA0001334.md): Fairing · gouged · Aug 27, 2000 · N35832 · Doug DC982 · Trailing Edge Flaps
  > INSPECTION FOUND RT WING NR 3 AFT LOWER FLAP HINGE FAIRING GOUGED. A SPLICE REPAIR WAS INSTALLED IAW SRM 51-30-2 AND 57-50-14, FIGURE 4.
- [SDR CALA0001333](https://openairdocs.org/sdr/CALA0001333.md): Fairing · cracked · Aug 27, 2000 · N35832 · Doug DC982 · Trailing Edge Flaps
  > INSPECTION FOUND A 4 INCH CRACK IN RT WING O/B FLAP HINGE FAIRING LOWER HALF. A DOUBLER REPAIR WAS INSTALLED IAW SRM 57-50-14 AND 51-30-2.
- [SDR CALA0001327](https://openairdocs.org/sdr/CALA0001327.md): Cargo Track · corroded · Aug 25, 2000 · N35832 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND AFT CARGO TRACK CORRODED AT NUT CLIP HOLES. THE CARGO TRACK WAS REMOVED AND A NEW CARGO TRACK WAS INSTALLED IAW SRM 51-30-1 AND 53-24-0, FIGURE 11.
- [SDR CALA0001326](https://openairdocs.org/sdr/CALA0001326.md): Frame · cracked · Aug 25, 2000 · N35832 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN FORWARD END OF FRAME OF THE FORWARD LAV TOILET SERVICING UNIT AT STA 240, LT SIDE. A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 53-34-0, FIGURE 2, AND 51-30-1.
- [SDR CALA0001325](https://openairdocs.org/sdr/CALA0001325.md): Flap Track · corroded · Aug 25, 2000 · N35832 · Doug DC982 · Trailing Edge Flaps
  > INSPECTION FOUND RIGHT I/B FLAP TRACK UPPER ROLLER SURFACE CORRODED. THE RIGHT I/B FLAP TRACK WAS REMOVED AND REPLACED IAW MM 27-51-01.
- [SDR CALA0001324](https://openairdocs.org/sdr/CALA0001324.md): Vane · gouged · Aug 25, 2000 · N35832 · Doug DC982 · Trailing Edge Flaps
  > INSPECTION FOUND RIGHT I/B FLAP MOVEABLE VANE GOUGED. THE GOUGED AREA OF SKIN WAS REMOVED AND REPAIR PARTS WERE INSTALLED IAW SRM 51-70-2, FIGURE 72 AND PARAGRAPH 22C.
- [SDR CALA0001323](https://openairdocs.org/sdr/CALA0001323.md): Angle · cracked · Aug 25, 2000 · N35832 · Doug DC982 · Nacelle/Pylon, Attach Fittings
  > INSPECTION FOUND FOUR INCH CRACKS IN TWO ANGLES ON I/B FAIRING OF NR 2 ENGINE UPPER T/R BUCKET. THE ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-10-2.
- [SDR CALA0001322](https://openairdocs.org/sdr/CALA0001322.md): Flap Track · corroded · Aug 25, 2000 · N35832 · Doug DC982 · Trailing Edge Flaps
  > INSPECTION FOUND LEFT I/B FLAP TRACK UPPER ROLLER SURFACE CORRODED. THE LEFT I/B FLAP TRACK WAS REMOVED AND REPLACED IAW MM 27-51-01.
- [SDR CALA0001319](https://openairdocs.org/sdr/CALA0001319.md): Panel · corroded · Aug 25, 2000 · N35832 · Doug DC982 · Wing, Plate/Skin
  > INSPECTION FOUND RT WING FUEL PANEL 1414C CORRODED. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA0001318](https://openairdocs.org/sdr/CALA0001318.md): Galley Track · corroded · Aug 25, 2000 · N35832 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND FORWARD GALLEY I/B LOWER MOUNT FITTING CORRODED. A REPLACEMENT MOUNT FITTING WAS INSTALLED IAW ECRA 2530-01257.
- [SDR CALA0001317](https://openairdocs.org/sdr/CALA0001317.md): Angle · cracked · Aug 25, 2000 · N35832 · Doug DC982 · Nacelle/Pylon, Attach Fittings
  > INSPECTION FOUND CRACKS IN FIRST AND THIRD ANGLES ON INBOARD T/R FAIRING ON UPPER BUCKET OF NR 1 ENGINE. THE CRACKS WERE APPROXIMATELY 3 INCHES LONG. THE ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-10-2.
- [SDR CALA0001316](https://openairdocs.org/sdr/CALA0001316.md): Fitting · corroded · Aug 25, 2000 · N35832 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT FITTING CORRODED AT STA 160 - 196, LBL 55. THE FLOOR SUPPORT FITTING WAS REMOVED AND A NEW SUPPORT FITTING WAS INSTALLED IAW SRM 53-01, FIGURE 1, 53-15-1, AND 51-30-5.
- [SDR CALA0001315](https://openairdocs.org/sdr/CALA0001315.md): Attach Angle · cracked · Aug 25, 2000 · N35832 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 3 INCH CRACK IN MID CARGO LT SIDEWALL FORWARD ATTACH ANGLE AT STA 524. THE ATTACH ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 53-24-0, FIGURE 9.
- [SDR CALA0001314](https://openairdocs.org/sdr/CALA0001314.md): Skin · dented · Aug 25, 2000 · N35832 · Doug DC982 · Leading Edge Devices
  > INSPECTION FOUND THREE DENTS IN NR 1 SLAT T/E BETWEEN XOS 166 AND XOS 147. THE DENTED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5750-03426.
- [SDR CALA0001312](https://openairdocs.org/sdr/CALA0001312.md): Web · cracked · Aug 25, 2000 · N35832 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 6 INCH CRACK IN SUBFLOOR WEB AT STA 1170, LBL 56. THE CRACKED AREA OF WEB WAS REMOVED AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-01, FIGURE 4, 53-14-3, FIGURE 12, AND 51-30-2.
- [SDR CALA0001311](https://openairdocs.org/sdr/CALA0001311.md): Panel · corroded · Aug 25, 2000 · N35832 · Doug DC982 · Wing, Plate/Skin
  > INSPECTION FOUND LT WING FUEL PANELS 1311C AND 1307C CORRODED. THE FUEL PANELS WERE REMOVED AND REPLACED IAW ECRA 5730-01688.
- [SDR CALA0001310](https://openairdocs.org/sdr/CALA0001310.md): Panel · gouged · Aug 25, 2000 · N35832 · Doug DC982 · Wing, Plate/Skin
  > INSPECTION FOUND RT WING FUEL PANEL 1472C GOUGED. THE FUEL PANEL WAS REMOVED AND REPLACED IAW ECRA 5730-01688.
- [SDR CALA0001291](https://openairdocs.org/sdr/CALA0001291.md): Shim · corroded · Aug 21, 2000 · N35832 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND SHIMS UNDER STRAPS OF DOOR STOP NUMBER 11 & 12 OF AFT CARGO DOOR CORRODED. THE SHIMS WERE REMOVED AND REPLACEMENT SHIMS WERE INSTALLED. THE STRAPS WERE REINSTALLED. WORK WAS PERFORMED IAW SRM 51-30-1, 51-30-2, AND 51-30-5.
- [SDR CALA0001290](https://openairdocs.org/sdr/CALA0001290.md): Cargo Track · corroded · Aug 21, 2000 · N35832 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND THE UPPER FLANGE OF THE RIGHT CARGO TIE DOWN TRACK IN THE MID CARGO PIT CORRODED AROUND FASTENER HOLES ON UPPER AND LOWER SURFACES AT STA 579 - 598. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-30-1, 53-05, FIGURE 4C, 51-30-
- [SDR CALA0001289](https://openairdocs.org/sdr/CALA0001289.md): Vane · dented · Aug 21, 2000 · N35832 · Doug DC982 · Trailing Edge Flaps
  > INSPECTION FOUND LT WING O/B FLAP O/B NR 2 FIXED VANE DENTED ON LEADING EDGE. THE DENTED AREA WAS REMOVED AND REPAIR DOUBLERS WERE INSTALLED IAW SRM 57-50-14 AND 51-70-2.
- [SDR CALA0001288](https://openairdocs.org/sdr/CALA0001288.md): Floor Panel · corroded · Aug 21, 2000 · N35832 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND FORWARD ENTRY FLOOR CORRODED AT STA 170 - 184, LBL 55. THE CORRODED AREA WAS CUT OUT IAW SRM 53-01. DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-30-2.
- [SDR CALA0001287](https://openairdocs.org/sdr/CALA0001287.md): Skin · bulged · Aug 21, 2000 · N35832 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LOWER FUSELAGE SKIN BULGED AT STA 389, LONGERON 16L-17L. THE EXISTING REPAIR WAS REMOVED IAW SRM 51-30-2. AN EXTERNAL AND INTERNAL DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-04, FIGURE 38, 51-30-2, 51-30-5, AND ECRA 5330-02944.
- [SDR CALA0001281](https://openairdocs.org/sdr/CALA0001281.md): Panel · gouged · Aug 20, 2000 · N35832 · Doug DC982 · Wing, Plate/Skin
  > INSPECTION FOUND RT WING LOWER PANEL NR 1222C GOUGED. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 57-30-3, FIGURE 3 AND 51-10-3.
- [SDR CALA0001280](https://openairdocs.org/sdr/CALA0001280.md): Fitting · bent · Aug 20, 2000 · N35832 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND MID CARGO DOOR FRAME LOWER BEAM TEE FITTING BENT. THE TEE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-10-1, 51-30-5, AND 51-10-3.
- [SDR CALA0001279](https://openairdocs.org/sdr/CALA0001279.md): Panel · gouged · Aug 20, 2000 · N35832 · Doug DC982 · Wing, Plate/Skin
  > INSPECTION FOUND RT WING LOWER FUEL PANEL NR 1244C GOUGED. A DOUBLER WAS INSTALLED IAW SRM 57-01, FIGURE 3, SHEET 2, 51-10-3, 51-30-2, AND DRAWING 9937483.
- [SDR CALA0001278](https://openairdocs.org/sdr/CALA0001278.md): Door Frame · corroded · Aug 19, 2000 · N35832 · Doug DC982 · Fuselage Main, Structure
  > INSPECTION FOUND AFT CARGO DOOR JAMB CENTER LOWER SECTION CORRODED. THE DOOR JAMB CENTER LOWER SECTION WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 51-30-5, 53-05, FIGURE 63, 51-10-3, AND 51-30-4.
- [SDR CALA0001277](https://openairdocs.org/sdr/CALA0001277.md): Floor Support · corroded · Aug 19, 2000 · N35832 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO DOOR JAMB FLOOR SUPPORT CORRODED AT STA 1155 - 1211, RBL 24. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-1 AND 51-30-2.
- [SDR CALA0001276](https://openairdocs.org/sdr/CALA0001276.md): Web · corroded · Aug 19, 2000 · N35832 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND FORWARD CARGO PIT FORWARD DOOR FRAME TORQUE BOX WEB CORRODED. A DOUBLER AND CONICAL WASHERS WERE INSTALLED IAW SRM 53-01, FIGURE 2, 51-30-1, 51-30-8, AND 51-30-2.
- [SDR CALA0001275](https://openairdocs.org/sdr/CALA0001275.md): Floor Support · cracked · Aug 19, 2000 · N35832 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SUPPORT SPLICE UNDER CABIN FLOOR HAD 7 CRACKS AT STA 826 - 886. THE CRACKS WERE 4 - 6 INCHES LONG. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-3 AND 51-30-1.

Next page: https://openairdocs.org/deregistered/N35832-2006-04-17/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 = 'N35832' AND deregistration_id = 'N35832-2006-04-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N35832-2006-04-17/reports

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