# Service difficulty reports: N93875, cancelled Aug 16, 2013

A list on [N93875, cancelled Aug 16, 2013](https://openairdocs.org/deregistered/N93875-2013-08-16.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 · 96 reports

- [SDR CALA0000003](https://openairdocs.org/sdr/CALA0000003.md): Actuator · inoperative · Jan 8, 2000 · N93875 · Doug DC982 · Landing Gear Retraction/Extension System
  > THE LT AND RT MAIN GEAR RED UNSAFE LIGHTS REMAINED ILLUMINATED AFTER TAKEOFF FROM EWR. THE ABNORMAL CHECKLIST WAS FOLLOWED, BUT THE LIGHTS REMAINED ON. THE LIGHTS WENT OUT WHEN SLATS WERE EXTENDED ON RETURN TO EWR AND THE A/C LANDED WITHOUT INCIDENT. MAINTE
- [SDR CALA9901422](https://openairdocs.org/sdr/CALA9901422.md): Power Supply · inop · Oct 20, 1999 · N93875 · Doug DC982 · Emergency Lighting
  > INSPECTION FOUND CABIN OVERHEAD EMERGENCY LIGHTS FORWARD OF OVERWING EXITS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHTS POWER SUPPLY AND OPERATION CHECKED GOOD IAW MM 33-53-00.
- [SDR CALA9901337](https://openairdocs.org/sdr/CALA9901337.md): Actuator · inop · Oct 7, 1999 · N93875 · Doug DC982 · Landing Gear Door Actuator
  > THE LT MLG SHOWED RED UNSAFE LIGHT WITH DOOR LIGHT OUT AFTER GEAR RETRACTION. THE GEAR WAS RECYCLED IAW CHECKLIST AND GEAR INDICATED NORMAL. THE LT GEAR ACTUATING CYLINDER WAS REMOVED AND REPLACED IAW MM 32-32-02. THE LT MLG DOOR ACTUATING CYLINDER AND DOOR
- [SDR CALA9901234](https://openairdocs.org/sdr/CALA9901234.md): Spar Cap · cracked · Sep 15, 1999 · N93875 · Doug DC982 · Trailing Edge Flaps
  > INSPECTION FOUND A 3.5 INCH CRACK IN LT WING FLAP TRAILING EDGE CAP JUST O/B OF FLEX JOINT ASSEMBLY. REPAIRED IAW SRM 57-03, FIGURE 9 AND MM 51-00-00.
- [SDR CALA9901216](https://openairdocs.org/sdr/CALA9901216.md): Panel · cracked · Sep 14, 1999 · N93875 · Doug DC982 · Wing, Plate/Skin
  > INSPECTION FOUND A 3 INCH CRACK IN RT WING TRAILING EDGE PANEL NR 1610. THE PANEL WAS REPAIRED IAW SRM 51-30-2.
- [SDR CALA9901215](https://openairdocs.org/sdr/CALA9901215.md): Support · bent · Sep 14, 1999 · N93875 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT PIT FORWARD BULKHEAD CENTER VERTICAL SUPPORT BENT AT FS 1007, BL 0. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW 51-10-4, 51-10-2, 51-30-2, 51-30-5, AND 51-10-3.
- [SDR CALA9901214](https://openairdocs.org/sdr/CALA9901214.md): Doubler · cracked · Sep 14, 1999 · N93875 · Doug DC982 · Landing Gear Doors
  > INSPECTION FOUND A.75 INCH CRACK IN LT MLG DOOR LOWER LT CORNER DOUBLER. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 28.
- [SDR CALA9901213](https://openairdocs.org/sdr/CALA9901213.md): Slat · dented · Sep 14, 1999 · N93875 · Doug DC982 · Leading Edge Devices
  > INSPECTION FOUND RT WING 0 SLAT DENTED. REPAIRED SLAT IAW ECRA 5720-01170.
- [SDR CALA9901212](https://openairdocs.org/sdr/CALA9901212.md): Panel · cracked · Sep 14, 1999 · N93875 · Doug DC982 · Horizontal Stabilizer, Plate/Skin
  > INSPECTION FOUND A 1.5 CRACK IN RT HORIZONTAL STABILIZER PANEL NR 3804 L/E. THE CRACKED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-30-2, 55-01, 51-30-2, 55-01, FIGURE 4, AND 55-12.
- [SDR CALA9901211](https://openairdocs.org/sdr/CALA9901211.md): Tie Strap · corroded · Sep 14, 1999 · N93875 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND TIE STRAP CORRODED AT LEFT AFT SERVICE DOOR CUTOUT, FS 1136, LONGERON 27R. THE TIE STRAP WAS REMOVED AND A NEW TIE STRAP WAS INSTALLED IAW SRM 51-30-5 AND 51-10-4.
- [SDR CALA9901210](https://openairdocs.org/sdr/CALA9901210.md): Skin · dented · Sep 14, 1999 · N93875 · Doug DC982 · Leading Edge Devices
  > INPECTION FOUND LEFT WING 0 SLAT DENTED. THE SLAT WAS REPAIRED IAW ECRA 5720-01120.
- [SDR CALA9901209](https://openairdocs.org/sdr/CALA9901209.md): Pan · gouged · Sep 14, 1999 · N93875 · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT CARGO DOOR GOUGED ON PAN AROUND DOOR STOPS. REPAIR DOUBLERS WERE INSTALLED IAW SRM 52-03, 51-10-4, 52-03, FIGURE 8 AND EA 5233-2-A0495.
- [SDR CALA9901204](https://openairdocs.org/sdr/CALA9901204.md): Skin · dented · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 140, LONGERON 19R. REPAIRED IAW SRM 53-04, FIGURE 38, SHEET 22, VIEW I.
- [SDR CALA9901203](https://openairdocs.org/sdr/CALA9901203.md): Doubler · corroded · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LOWER FUSELAGE EXTERNAL CUTOUT FOR NR 2 AD ANTENNA CORRODED BETWEEN SKIN AND INTERNAL DOUBLER AND MATING SURFACE AT FS 484-503, LONGERON 29L AND 30. THE INTERNAL DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.
- [SDR CALA9901202](https://openairdocs.org/sdr/CALA9901202.md): Panel · corroded · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND KEEL ACCESS PANEL BETWEEN BOTH MLG DOORS CORRODED ON ONE END AT FS 864-870. A NEW PANEL WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-00-60.
- [SDR CALA9901201](https://openairdocs.org/sdr/CALA9901201.md): Angle · cracked · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND 3 CRACKS IN CENTER WING TO BODY FAIRING SUPPORT ANGLES(3) AT STA 875, BL 0. THE ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-10-4, 51-30-4, AND 51-30-5.
- [SDR CALA9901200](https://openairdocs.org/sdr/CALA9901200.md): Panel · cracked · Sep 12, 1999 · N93875 · Doug DC982 · Vertical Stabilizer, Plate/Skin
  > INSPECTION FOUND CRACKS IN VERTICAL STABILIZER PANEL NR 6404. THE CRACKS WERE 1-2 INCHES LONG. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA9901198](https://openairdocs.org/sdr/CALA9901198.md): Tab · disbonded · Sep 12, 1999 · N93875 · Doug DC982 · Rudder, Tab Structure
  > INSPECTION FOUND RUDDER TRIM TAB METAL TAB DISBONDED ON RT SIDE OF TAB. THE RUDDER TAB WAS REMOVED AND THE METAL TAB WAS REMOVED AND REPLACED. THE RUDDER TAB WAS REINSTALLED AND RIGGED IAW MM 27-20-02.
- [SDR CALA9901197](https://openairdocs.org/sdr/CALA9901197.md): Fitting · cracked · Sep 12, 1999 · N93875 · Doug DC982 · Leading Edge Devices
  > INSPECTION FOUND A.25 INCH CRACK IN RT WING NR 5 SLAT O/B FITTING. THE FITTING WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-30-2, 51-30-8, AND ECRA 5750-03276.
- [SDR CALA9901196](https://openairdocs.org/sdr/CALA9901196.md): Skin · cracked · Sep 12, 1999 · N93875 · Doug DC982 · Spoilers
  > INSPECTION FOUND A 2.2 INCH CRACK IN RT I/B SPOILER FIXED SUPPORT PANEL. THE CRACKED AREA OF SKIN WAS REMOVED AND A NEW PLATE WAS INSTALLED IAW SRM 51-30-1 AND 51-10-4.
- [SDR CALA9901195](https://openairdocs.org/sdr/CALA9901195.md): Web · punctured · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A SMALL HOLE PUNCTURED IN CUSP WEB AT FS 1050, RBL 59. THE PUNCTURED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-30-5, 51-10-2, AND ECRA 5310-03907.
- [SDR CALA9901194](https://openairdocs.org/sdr/CALA9901194.md): Angle · corroded · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FALSE BULKHEAD LOWER ATTACH ANGLE CORRODED AT FS 1333, LONGERON 28L-28R. THE ATTACH ANGLE WAS REMOVED AND A NEW ANGLE AND DOUBLER WERE INSTALLED IAW SRM 51-10-4 AND 53-01, FIGURE 2, SHEET 4.
- [SDR CALA9901193](https://openairdocs.org/sdr/CALA9901193.md): Frame · corroded · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND FRAME LOWER LOBE AND WEB CORRODED AT FS 1269, LONGERON 28L-28R. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 51-10-2, 51-10-3, 51-10-4, AND 53-05, FIGURE 4A.
- [SDR CALA9901192](https://openairdocs.org/sdr/CALA9901192.md): Web · cracked · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN SUBFLOOR CUSP WEB AT STA 195, RBL 9. THE SUBFLOOR CUSP WEB WAS REPAIRED IAW SRM 53-01, FIGURE 4, SHEET 3.
- [SDR CALA9901191](https://openairdocs.org/sdr/CALA9901191.md): Longeron · cracked · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 2 INCH CRACK IN LONGERON 27L AT FS 256. THE CRACKED SECTION OF LONGERON WAS REMOVED AND A NEW SPLICE AND LONGERON WERE INSTALLED IAW SRM 53-14-02, FIGURE 3, 53-02, FIGURE 18, 51-30-02, AND 51-30-05.
- [SDR CALA9901190](https://openairdocs.org/sdr/CALA9901190.md): Support · corroded · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LT FLOOR SUPPORT CORRODED AT FS 1155, JUST O/B OF I/B SEAT TRACK. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5.
- [SDR CALA9901189](https://openairdocs.org/sdr/CALA9901189.md): Floorbeam · corroded · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM WEB CORRODED AT STA 1338, RBL 54.5 AND RBL 35-45. THE CORRODED AREAS WERE CUT OUT AND REPAIRS WERE INSTALLED IAW SRM 53-01, FIGURE 4, 51-10-3, 51-30-2, 51-30-5 AND ECRA 5310-03899.
- [SDR CALA9901188](https://openairdocs.org/sdr/CALA9901188.md): Floor · corroded · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN LT FLOOR SKIN CORRODED AT FS 1138, LBL 42. INSTALLED NEW SKIN AND SUPPORTS IAW SRM 51-30-2, 51-30-3, AND 51-30-5.
- [SDR CALA9901187](https://openairdocs.org/sdr/CALA9901187.md): Floor · corroded · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND CABIN LT FLOOR SKIN CORRODED AT FS 1183, LBL 42. REMOVED FORWARD AND AFT FRAME FITTINGS TORQUE BOX DOUBLER AND VERTICAL STIFFENER IAW SRM 51-30-1 AND 51-30-5. A REPAIR WEB WAS INSTALLED IAW SRM 51-10-3, 51-10-4, 51-30-2, AND 51-30-5. THE FI
- [SDR CALA9901186](https://openairdocs.org/sdr/CALA9901186.md): Support · corroded · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT LT SERVICE DOOR LOWER CUTOUT FLOOR LEVEL SUPPORT CORRODED AT FS 1330-1338, LBL 14. A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2.
- [SDR CALA9901185](https://openairdocs.org/sdr/CALA9901185.md): Floor · corroded · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage Floor Panel
  > INSPECTION FOUND COCKPIT RT FLOOR SKIN CORRODED AT FS 148, RBL 6. THE CORRODED AREA WAS CUT OUT, FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-01, FIGURE 4, 51-10-3 AND 51-30-2.
- [SDR CALA9901183](https://openairdocs.org/sdr/CALA9901183.md): Angle · corroded · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND L-ANGLE ABOVE LONGERON 18R AT STA 148-160 CORRODED. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10-3.
- [SDR CALA9901182](https://openairdocs.org/sdr/CALA9901182.md): Subfloor · corroded · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage Main, Structure
  > INSPECTION FOUND SUBFLOOR CORRODED AT STA 218, LBL 42-44. THE SUBFLOOR WEB AND STIFFENERS WERE REMOVED AND A NEW WEB AND STIFFENERS WERE INSTALLED IAW SRM 53-10-4, 51-30-2, 51-30-4, AND 51-30-8.
- [SDR CALA9901181](https://openairdocs.org/sdr/CALA9901181.md): Subfloor · corroded · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage Main, Structure
  > INSPECTION FOUND SUBFLOOR CORRODED AT STA 200, LBL 40 AND LBL 18 TO RBL 30. THE SUBFLOOR AREAS WERE REPAIRED IAW SRM 51-30-2, 53-05, FIGURE 25, 51-30-5, AND 53-01, FIGURE 4.
- [SDR CALA9901180](https://openairdocs.org/sdr/CALA9901180.md): Support · corroded · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 200, BL 0 TO LBL 12 AND LBL 40. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 53-14-1, 51-10-3, 51-30-4, AND 51-30-5.
- [SDR CALA9901179](https://openairdocs.org/sdr/CALA9901179.md): Support · corroded · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 157-200, BL 0 AND STA 200, BL 0 TO RBL 40. THE SUPPORTS WERE REMOVED AND REPLACED IAW SRM 53-14-1, FIGURE 11, 51-10-4, 51-10-3, 51-30-1, 51-30-2, AND 51-30-5.
- [SDR CALA9901178](https://openairdocs.org/sdr/CALA9901178.md): Support · corroded · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 157-180, RBL 40. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, AND 51-10-3.
- [SDR CALA9901177](https://openairdocs.org/sdr/CALA9901177.md): Seat Track · corroded · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND AFT RIGHT O/B SEAT TRACK CORRODED AT STA 1022-1041, RBL 54.5 AND STA 1092-1243, RBL 54.5. THE CORRODED SECTIONS OF SEAT TRACK WERE REMOVED AND NEW SECTIONS WERE INSTALLED IAW SRM 51-30-1, 51-10-4, AND 53-05, FIGURE 4.
- [SDR CALA9901176](https://openairdocs.org/sdr/CALA9901176.md): Seat Track · cracked · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND A 3 INCH CRACK IN LT CENTER SEAT TRACK AT FS 1309, LBL 22. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1, 51-30-5, 51-10-3, AND 53-05, FIGURE 4A.
- [SDR CALA9901175](https://openairdocs.org/sdr/CALA9901175.md): Doubler · cracked · Sep 12, 1999 · N93875 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN RT COCKPIT SLIDING WINDOW CUTOUT UPPER AFT CORNER INSIDE DOUBLER. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-30-2, AND 51-30-1.
- [SDR CALA9901199](https://openairdocs.org/sdr/CALA9901199.md): Skin · punctured · Sep 10, 1999 · N93875 · Doug DC982 · Vertical Stabilizer, Plate/Skin
  > INSPECTION FOUND A HOLE THROUGH SKIN AND RIB OF VERTICAL STABILIZER AFT UPPER STRINGER TIP FAIRING. THE RIB AND SKIN WERE REPAIRED IAW SRM 55-01, FIGURES 2 & 4.
- [SDR CALA9901170](https://openairdocs.org/sdr/CALA9901170.md): Power Supply · inop · Sep 10, 1999 · N93875 · Doug DC982 · Emergency Lighting
  > INSPECTION FOUND EMERGENCY OVERWING AFT LIGHT INOPERATIVE. THE BATTERY POWER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-50-22.
- [SDR CALA9901206](https://openairdocs.org/sdr/CALA9901206.md): Floorbeam · corroded · Sep 9, 1999 · N93875 · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 294, BL 0 TO RBL 50 AND STA 328, BL 0 TO RBL 50. NEW FLOORBEAM SECTIONS WERE INSTALLED IAW SRM 53-10-51.
- [SDR CALA9901167](https://openairdocs.org/sdr/CALA9901167.md): Floorbeam · corroded · Sep 8, 1999 · N93875 · Doug DC982 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 1332, LBL 34 TO 42.5. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-10-3 AND 53-05, FIGURE 20A.
- [SDR CALA9901166](https://openairdocs.org/sdr/CALA9901166.md): Support · corroded · Sep 8, 1999 · N93875 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1155, LONGERON 28R-29R. A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-2, 51-10-4, 51-10-3, AND 51-30-5.
- [SDR CALA9901165](https://openairdocs.org/sdr/CALA9901165.md): Fitting · cracked · Sep 8, 1999 · N93875 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1.5 INCH CRACK IN FLOORBEAM TO FRAME SUPPORT FITTING AT STA 1338, RBL 54.5. THE FITTING WAS REPLACED IAW SRM 51-10-4, 51-10-3, AND 51-30-5.
- [SDR CALA9901164](https://openairdocs.org/sdr/CALA9901164.md): Support · cracked · Sep 8, 1999 · N93875 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM TO FRAME SUPPORT AT FS 446, LONGERON 23L. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-5, AND 51-30-2.
- [SDR CALA9901163](https://openairdocs.org/sdr/CALA9901163.md): Seat Track · corroded · Sep 8, 1999 · N93875 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT CENTER SEAT TRACK CORRODED AROUND CLIP NUTS AT STA 1009-1079. THE SEAT TRACK WAS REPLACED IAW ECRA 5310-03904.
- [SDR CALA9901162](https://openairdocs.org/sdr/CALA9901162.md): Support · corroded · Sep 8, 1999 · N93875 · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 218, LBL 6. A NEW SUPPORT WAS INSTALLED IAW SRM 53-14-1, FIGURE 11, 51-10-4, 51-10-3, AND 51-30-2.
- [SDR CALA9901161](https://openairdocs.org/sdr/CALA9901161.md): Skin · corroded · Sep 8, 1999 · N93875 · Doug DC982 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FORWARD ENTRANCE DOOR CUTOUT CORRODED ON LOWER FORWARD CORNER AT FS 200, LONGERON 18L. A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW ECRA 5310-03900 AND EA 9-5314-2-A0486.

Next page: https://openairdocs.org/deregistered/N93875-2013-08-16/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 = 'N93875' AND deregistration_id = 'N93875-2013-08-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N93875-2013-08-16/reports

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