# Service difficulty reports: N92874, cancelled Mar 21, 2013

A list on [N92874, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N92874-2013-03-21.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 · 100 reports

- [SDR CALA0300589](https://openairdocs.org/sdr/CALA0300589.md): Doubler · corroded · Oct 12, 2003 · N92874 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND INTERNAL DOUBLER FOR OUTFLOW VALVE CORRODED AT STA 1325 BETWEEN L21L AND L22L. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-02.
- [SDR CALA0300333](https://openairdocs.org/sdr/CALA0300333.md): Battery Pack · inoperative · Jun 23, 2003 · N92874 · Doug DC982 · Emergency Lighting
  > INSPECTION FOUND THE OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. THE BATTERY PACK WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD IAW MM 33-53-00, PAGE 407.
- [SDR CALA0300270](https://openairdocs.org/sdr/CALA0300270.md): Slide · discharged · May 28, 2003 · N92874 · Doug DC982 · Escape Slide
  > INSPECTION FOUND THE R-1 DOOR SLIDE PRESSURE LOW. THE EMERGENCY DOOR SLIDE WAS REMOVED AND REPLACED IAW MM 25-62-00.
- [SDR CALA0200430](https://openairdocs.org/sdr/CALA0200430.md): Skin · cracked · Jul 25, 2002 · N92874 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND A 1/4" CRACK AT RIVET IN L-1 DOOR SKIN AND THE CORNER WAS BENT. THE CRACK WAS LOCATED AT THE UPPER AFT CORNER OF DOOR. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 32 AND 51-10-3B.
- [SDR CALA0200421](https://openairdocs.org/sdr/CALA0200421.md): Seat Track · corroded · Jul 19, 2002 · N92874 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND R/H I/B SEAT TRACK CORRODED AT STA 200-228. THE SEAT TRACK SECTION WAS REPLACED IAW SRM 53-05, FIGURE 4F, SHEET 1.
- [SDR CALA0200405](https://openairdocs.org/sdr/CALA0200405.md): Seat Track · corroded · Jul 17, 2002 · N92874 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND L/H CENTER SEAT TRACK CORRODED AROUND FLOOR PANEL MOUNT HOLES BETWEEN STA 1136 AND 1174. A NEW SEAT TRACK SECTION WAS INSTALLED IAW SRM 53-05.
- [SDR CALA0200401](https://openairdocs.org/sdr/CALA0200401.md): Seat Track · corroded · Jul 15, 2002 · N92874 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND R/H I/B SEAT TRACK CORRODED AT STA 200-228. THE CORRODED SECTION OF SEAT TRACK WAS REPLACED IAW SRM 53-05, FIGURE 4F, SHEET 1.
- [SDR CALA0200141](https://openairdocs.org/sdr/CALA0200141.md): Fan · overheated · Mar 19, 2002 · N92874 · Doug DC982 · Air Distribution Fan
  > THE FLIGHT ATTENDANT REPORTED AN ELECTRICAL SMOKE ODOR APPARENTLY COMING FROM THE RIGHT AFT LAV AREA AFTER TAKEOFF FROM MIA. THE AIRCRAFT WAS RETURNED TO MIA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE CABIN AIR RECIRCULATION FAN HAD OVERHEA
- [SDR CALA0100655](https://openairdocs.org/sdr/CALA0100655.md): Charger · inoperative · Jul 14, 2001 · N92874 · Doug DC982 · Emergency Lighting
  > INSPECTION FOUND EMERGENCY AISLE PATH LIGHTING IN CENTER OF AIRCRAFT INOPERATIVE. THE EMERGENCY BATTERY CHARGER NEAR TOP BEACON WAS REMOVED AND REPLACED AND OPERATION OF AISLE PATH LIGHTING CHECKED GOOD.
- [SDR CALA0100566](https://openairdocs.org/sdr/CALA0100566.md): Intercostal · corroded · Jun 21, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FIVE INTERCOSTALS CORRODED INSIDE TORQUE BOX AT AFT CARGO PIT AREA, FS 1165 - 1203. THE INTERCOSTALS WERE REMOVED AND NEW INTERCOSTALS WERE INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-1, AND 51-30-5.
- [SDR CALA0100565](https://openairdocs.org/sdr/CALA0100565.md): Skin · gouged · Jun 21, 2001 · N92874 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERNAL FUSELAGE SKIN GOUGED AFT OF R-1 DOOR GUST LOCK. THE GOUGED AREA WAS REMOVED. SKIN FILLER AND REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-34-0, 51-10-4, 51-10-3, AND 53-04, FIGURE 24.
- [SDR CALA0100540](https://openairdocs.org/sdr/CALA0100540.md): Skin · dented · Jun 12, 2001 · N92874 · Doug DC982 · Trailing Edge Flaps
  > INSPECTION FOUND LEFT I/B FLAP LOWER SKIN SURFACE DENTED. THE LEFT I/B FLAP PANEL WAS REMOVED AND NEW SKIN WAS INSTALLED IAW SRM 51-50-14, 51-10-3, 51-50-20, AND 57-52-14. THE PANEL WAS INSTALLED IAW SRM 51-30-1.
- [SDR CALA0100539](https://openairdocs.org/sdr/CALA0100539.md): Intercostal · corroded · Jun 12, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND MID CARGO INTERCOSTAL CORRODED AT FS 769-788 BETWEEN LONGERONS 27R AND 28R. PANEL 2214C WAS REMOVED IAW SRM 51-30-01. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-05. PANEL 2214C WAS REINSTALLED IAW SRM 51-30-01.
- [SDR CALA0100537](https://openairdocs.org/sdr/CALA0100537.md): Web · corroded · Jun 10, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO PIT TORQUE BOX WEB CORRODED. THE TORQUE BOX WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-5.
- [SDR CALA0100536](https://openairdocs.org/sdr/CALA0100536.md): Door Frame · corroded · Jun 7, 2001 · N92874 · Doug DC982 · Fuselage Main, Structure
  > INSPECTION FOUND FORWARD CARGO DOOR FORWARD JAMB UPPER WEB CORRODED. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-30-5.
- [SDR CALA0100534](https://openairdocs.org/sdr/CALA0100534.md): Angle · corroded · Jun 6, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CUSP ANGLE CORRODED AT FS 200, RBL 54. THE R-1 DOOR, FRAME FITTING, AND CUSP ANGLE WERE REMOVED IAW MM 52-41-00, SRM 51-30-05, AND 53-05, FIGURE 55. A NEW ANGLE AND REPAIR SPLICE ANGLES WERE INSTALLED IAW SRM 51-30-01. THE R-1 DOOR WAS REIN
- [SDR CALA0100533](https://openairdocs.org/sdr/CALA0100533.md): Frame · corroded · Jun 3, 2001 · N92874 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND TAIL COMPARTMENT LT SIDE CANTED FRAME GOUGED AT FS 1463. THE CORROSION WAS REMOVED AND REPAIR ANGLES WERE INSTALLED IAW SRM 51-30-5, 53-01, FIGURE 1, 51-10-3, AND EA 9-5311-2-A0888, FIGURE 2.
- [SDR CALA0100532](https://openairdocs.org/sdr/CALA0100532.md): Web · cracked · Jun 3, 2001 · N92874 · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND A 1 INCH CRACK IN L1 DOOR TORQUE BOX WEB AFT OF TANG AT LONGERON 15L. THE FASTENERS WERE REMOVED, TANGS TRIMMED, AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 51-30-2, 51-10-4, AND EA 9-5314-2-A0884.
- [SDR CALA0100531](https://openairdocs.org/sdr/CALA0100531.md): Floorbeam · corroded · Jun 3, 2001 · N92874 · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND AFT CARGO FLOORBEAM AND NUT PLATES CORRODED AT FS 1338. THE UPPER L-ANGLE ON FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-05, 51-30-01, 51-30-02, 51-30-05, AND 51-10-4.
- [SDR CALA0100530](https://openairdocs.org/sdr/CALA0100530.md): Skin · dented · Jun 3, 2001 · N92874 · Doug DC982 · Leading Edge Devices
  > INSPECTION FOUND RT WING EXTERNAL SURFACE OF ZERO SLAT SKIN DENTED I/B OF THE DRIVE TRACK. THE SLAT WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-80-01, EA 9-5740-2-A0890, AND ECRA 5740-01040.
- [SDR CALA0100529](https://openairdocs.org/sdr/CALA0100529.md): Strap · corroded · Jun 2, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO DOOR JAMB TORQUE BOX FWD STRAP CORRODED. THE FORWARD STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 53-01, FIGURE 1, 51-10-4, 51-10-3, AND 51-30-5.
- [SDR CALA0100528](https://openairdocs.org/sdr/CALA0100528.md): Floorbeam · corroded · Jun 2, 2001 · N92874 · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND AFT CARGO CABIN FLOORBEAM AND NUT PLATES CORRODED AT FS 1322. THE FLOORBEAM WAS REPAIRED IAW SRM 53-05 AND 53-05, FIGURE 20A.
- [SDR CALA0100527](https://openairdocs.org/sdr/CALA0100527.md): Beam · corroded · Jun 2, 2001 · N92874 · Doug DC982 · Fuselage Main, Structure
  > INSPECTION FOUND AFT CARGO DOOR JAMB BEAM CORRODED. THE LOWER DOOR JAMB BEAM WAS REMOVED AND A NEW LOWER DOOR JAMB BEAM WAS INSTALLED USING A DOUBLER AND SPACER IAW SRM 51-30-5 AND 51-30-2.
- [SDR CALA0100524](https://openairdocs.org/sdr/CALA0100524.md): Frame · corroded · May 31, 2001 · N92874 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND MID CARGO FRAME CORRODED AT FS 541 BETWEEN LONGERONS 26R AND 26L. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 2A, 51-10-4, 51-10-3, 53-05, FIGURE 2A, AND 51-30-5.
- [SDR CALA0100523](https://openairdocs.org/sdr/CALA0100523.md): Frame · corroded · May 30, 2001 · N92874 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND MID CARGO FRAME CORRODED AT FS 560 BETWEEN LONGERONS 26R AND 26L. THE CORRODED SECTION OF FRAME WAS REMOVED AND A Z-FRAME REPAIR SPLICE WAS INSTALLED IAW SRM 53-03, FIGURE 2A AND 51-10-3.
- [SDR CALA0100522](https://openairdocs.org/sdr/CALA0100522.md): Support · cracked · May 30, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO FALSE BULKHEAD LOWER SUPPORTS CORRODED AND CRACKED AT FS 1007, LONGERON 28L AND 28R. BOTH SUPPORTS WERE REMOVED AND NEW SUPPORTS WERE INSTALLED IAW SRM 51-10-5, 51-10-4, AND 51-10-3.
- [SDR CALA0100521](https://openairdocs.org/sdr/CALA0100521.md): Skin · damaged · May 30, 2001 · N92874 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERNAL FUSELAGE SKIN CREASED AT FS 230 BETWEEN LONGERON 17L AND 18L. THE SKIN WAS REPAIRED IAW ECRA 5330-02445.
- [SDR CALA0100520](https://openairdocs.org/sdr/CALA0100520.md): Floorbeam · corroded · May 29, 2001 · N92874 · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND AFT CARGO OVERHEAD FLOORBEAM CORRODED ON NUT PLATES AND EXFOLIATION CORROSION ON RT SIDE AT FS 1309. THE FLOORBEAM WAS REMOVED AND A NEW FLOORBEAM WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4.
- [SDR CALA0100519](https://openairdocs.org/sdr/CALA0100519.md): Support · corroded · May 29, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND MID CARGO SUPPORT CORRODED AT FS 750 BETWEEN LONGERONS 29L AND 29R. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW 51-30-5, 51-10-4, AND 51-30-2.
- [SDR CALA0100518](https://openairdocs.org/sdr/CALA0100518.md): Frame · corroded · May 29, 2001 · N92874 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND AFT CARGO FRAME CORRODED AT FS 1117, LONGERON 30. THE CORRODED SECTION OF FRAME WAS REMOVED AND A NEW FRAME SECTION WAS INSTALLED IAW SRM 51-30-5, 51-10-4, AND 51-10-3.
- [SDR CALA0100517](https://openairdocs.org/sdr/CALA0100517.md): Cargo Track · corroded · May 29, 2001 · N92874 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND MID CARGO RT TIE DOWN TRACK CORRODED BETWEEN FS 693 AND 788. THE CARGO TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-01, 51-10-4, AND 51-10-3.
- [SDR CALA0100516](https://openairdocs.org/sdr/CALA0100516.md): Door Frame · corroded · May 29, 2001 · N92874 · Doug DC982 · Fuselage Main, Structure
  > INSPECTION FOUND MID CARGO DOOR LOWER JAMB BEAM CORRODED AROUND RIVNUTS. THE DOOR JAMB WAS REPAIRED IAW ECRA 5310-03027.
- [SDR CALA0100512](https://openairdocs.org/sdr/CALA0100512.md): Web · corroded · May 26, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CUSP WEB CORRODED AT FS 200 - 207, RBL 56. THE CUSP WEB WAS REMOVED AND A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, FIGURE 1, 51-30-02, 51-30-08, AND 51-10-3.
- [SDR CALA0100511](https://openairdocs.org/sdr/CALA0100511.md): Web · cracked · May 26, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND MAIN CABIN CUSP WEB CRACKED IN SEVERAL PLACES AT FS 1280, RBL 54. THE CRACKS WERE APPROXIMATELY 1 INCH LONG. FLOOR PANELS WERE REMOVED TO GAIN ACCESS. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-05, FIGURE 96, 51-10-3, AND 51-30-2. THE FLOOR
- [SDR CALA0100510](https://openairdocs.org/sdr/CALA0100510.md): Web · corroded · May 26, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND MAIN CABIN CUSP WEB CORRODED AT FS 160 - 200, RBL 56. THE CORRODED AREA WAS CUT OUT IAW SRM 53-01, FIGURE 3. A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-14-1, FIGURE 11, 51-30-02, 51-10-3, AND 53-01, FIGURE 3.
- [SDR CALA0100509](https://openairdocs.org/sdr/CALA0100509.md): Floor Support · corroded · May 26, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED ON UPPER AND LOWER SURFACE IN MID CARGO AREA AT FS 636, LONGERON 28R-29R. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-1.
- [SDR CALA0100508](https://openairdocs.org/sdr/CALA0100508.md): Support · corroded · May 26, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SUPPORT CORRODED AT AFT LT SIDE OF WEB AT CUSP AREA, STA 1309. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4.
- [SDR CALA0100506](https://openairdocs.org/sdr/CALA0100506.md): Skin · dented · May 25, 2001 · N92874 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LT EXTERNAL FUSELAGE SKIN DENTED AT FS 195, LONGERON 23L. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.
- [SDR CALA0100505](https://openairdocs.org/sdr/CALA0100505.md): Floor Support · corroded · May 25, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND MAIN CABIN FLOOR SUPPORT CORRODED AT FS 160-200, RBL 56. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-4, 51-30-3, 51-30-4, AND 51-30-2.
- [SDR CALA0100504](https://openairdocs.org/sdr/CALA0100504.md): Skin · gouged · May 25, 2001 · N92874 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND RT INTERNAL FUSELAGE SKIN GOUGED AT FS 1429. THE AREA WAS BLENDED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, 51-10-3, 51-10-4, AND 51-30-2.
- [SDR CALA0100503](https://openairdocs.org/sdr/CALA0100503.md): Skin · dented · May 24, 2001 · N92874 · Doug DC982 · Landing Gear Doors
  > INSPECTION FOUND RT MLG DOOR EXTERNAL SKIN DENTED IN TWO PLACES 7 INCHES APART I/B OF DOOR SKID. A REPAIR PATCH WAS INSTALLED IAW SRM 52-01, FIGURE 2 AND 51-30-3.
- [SDR CALA0100502](https://openairdocs.org/sdr/CALA0100502.md): Skin · dented · May 24, 2001 · N92874 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND RT EXTERNAL FUSELAGE SKIN DENTED BETWEEN FS 313 - 332, LONGERON 20-21R. THE EXISTING DOUBLER WAS REMOVED IAW SRM 51-30-05 AND 51-30-02. THE DENTED SKIN WAS REMOVED IAW SRM 53-04, FIGURE 12 & 13. REPAIR DOUBLERS AND FINGER DOUBLERS WERE INST
- [SDR CALA0100501](https://openairdocs.org/sdr/CALA0100501.md): Skin · dented · May 24, 2001 · N92874 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LT EXTERNAL FUSELAGE SKIN DENTED AT FS 233, LONGERON 23L. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-4 AND 51-30-2.
- [SDR CALA0100493](https://openairdocs.org/sdr/CALA0100493.md): Skin · dented · May 22, 2001 · N92874 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AND CREASED AT FS 322, LONGERON 25R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, 51-10-4, AND 51-10-3.
- [SDR CALA0100492](https://openairdocs.org/sdr/CALA0100492.md): Skin · dented · May 22, 2001 · N92874 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND THE EXTERNAL FUSELAGE SKIN DENTED AT FS 340, LONGERON 24L. THE DENTED AREA WAS REFORMED AND A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.
- [SDR CALA0100491](https://openairdocs.org/sdr/CALA0100491.md): Skin · damaged · May 22, 2001 · N92874 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND EXTERNAL FUSELAGE SKIN CREASED AT FS 312, LONGERON 24L. THE SKIN WAS COLD WORKED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-2, 53-04, FIGURE 38, 51-10-3, AND 51-30-2.
- [SDR CALA0100489](https://openairdocs.org/sdr/CALA0100489.md): Floor Panel · delaminated · May 21, 2001 · N92874 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND CABIN CENTER FLOOR PANEL DELAMINATED AT FS 905 - 946. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW ECRA 5100-01844.
- [SDR CALA0100486](https://openairdocs.org/sdr/CALA0100486.md): Floor Panel · cracked · May 21, 2001 · N92874 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND CABIN CENTER FLOOR PANEL CRACKED AT FS 905-946. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-2 AND 51-30-8.
- [SDR CALA0100484](https://openairdocs.org/sdr/CALA0100484.md): Web · cracked · May 20, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN CUSP WEB AT FS 237, RBL 56. THE CUSP WEB WAS REMOVED AND THE CRACK WAS STOP DRILLED IAW SRM 51-30-2 AND 53-01, FIGURE 2. A REPAIR DOUBLER AND THE CUSP WEB WERE INSTALLED IAW SRM 53-01, FIGURE 4, 51-30-2, AND 51-30-1.
- [SDR CALA0100482](https://openairdocs.org/sdr/CALA0100482.md): Floor Support · cracked · May 20, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN RT I/B FLOOR SUPPORT CORRODED WITH A 1.5 INCH EDGE CRACK AT FS 210. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-10-3.

Next page: https://openairdocs.org/deregistered/N92874-2013-03-21/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 = 'N92874' AND deregistration_id = 'N92874-2013-03-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N92874-2013-03-21/reports

---
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