# Service difficulty reports: N13066, cancelled Jan 11, 2018

A list on [N13066, cancelled Jan 11, 2018](https://openairdocs.org/deregistered/N13066-2018-01-11.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR CALA0100085](https://openairdocs.org/sdr/CALA0100085.md): Charger · inoperative · Jan 31, 2001 · N13066 · Doug DC1030 · Emergency Lighting
  > INSPECTION FOUND EMERGENCY SEAT LIGHTS INOPERATIVE AT ROWS 29 - 45 A, B. THE BATTERY CHARGER WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-55-00.
- [SDR CALA0000913](https://openairdocs.org/sdr/CALA0000913.md): Skin · delaminated · Jun 17, 2000 · N13066 · Doug DC1030 · Engine Cowling System
  > INSPECTION FOUND INTERNAL SURFACE OF NR 2 ENGINE LT TRANSLATING COWL DELAMINATED. THE LT TRANSLATING COWL WAS REMOVED AND REPLACED IAW MM 78-32-17.
- [SDR CALA0000910](https://openairdocs.org/sdr/CALA0000910.md): Bracket · cracked · Jun 15, 2000 · N13066 · Doug DC1030 · Trailing Edge Flaps
  > INSPECTION FOUND A.5 INCH CRACK IN LT WING O/B FLAP INTERNAL AFT ANGULAR BRACKET. THE BRACKET WAS REPLACED IAW SRM 51-31-01.
- [SDR CALA0000907](https://openairdocs.org/sdr/CALA0000907.md): Structure · cracked · Jun 15, 2000 · N13066 · Doug DC1030 · Landing Gear Doors
  > INSPECTION FOUND A 1 INCH CRACK AT CORNER OF LT MLG DOOR. THE DOOR CORNER WAS REPAIRED IAW SRM 51-31-01.
- [SDR CALA9900649](https://openairdocs.org/sdr/CALA9900649.md): Skin · corroded · Jun 1, 1999 · N13066 · Doug DC1030 · Ailerons
  > INSPECTION FOUND RT WING OUTBOARD AILERON LOWER SKIN INTERNALLY CORRODED. THE AILERON SKIN WAS REPLACED IAW SRM 51-31-01 AND 51-33-01.
- [SDR CALA9900648](https://openairdocs.org/sdr/CALA9900648.md): Panel · cracked · Jun 1, 1999 · N13066 · Doug DC1030 · Wing, Plate/Skin
  > INSPECTION FOUND A FOUR INCH CRACK IN RT WING PANEL NR 617CT. REPAIRED IAW SRM 57-10-00, PAGE 25.
- [SDR CALA9900647](https://openairdocs.org/sdr/CALA9900647.md): Spar · cracked · Jun 1, 1999 · N13066 · Doug DC1030 · Wing Spar
  > INSPECTION FOUND A 1.5 INCH CRACK IN RT WING DROOPED LEADING EDGE ON INTERNAL SPAR AT STA XORS 317. A REPAIR WAS PERFORMED IAW ECRA 5720-01738.
- [SDR CALA9900646](https://openairdocs.org/sdr/CALA9900646.md): Spar · cracked · Jun 1, 1999 · N13066 · Doug DC1030 · Wing Spar
  > INSPECTION FOUND A 0.8 INCH CRACK IN RT WING DROOPED LEADING EDGE ON LATERAL SPAR AT STA XORS 317. A REPAIR WAS PERFORMED IAW ECRA 5720-01738.
- [SDR CALA9900645](https://openairdocs.org/sdr/CALA9900645.md): Skin · cracked · Jun 1, 1999 · N13066 · Doug DC1030 · Wing, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE OUTBOARD LOWER SKIN AT STA XORS 402. A REPAIR WAS PERFORMED IAW SRM 57-10-00, PAGE 216.
- [SDR CALA9900644](https://openairdocs.org/sdr/CALA9900644.md): Skin · delaminated · May 29, 1999 · N13066 · Doug DC1030 · Wing, Plate/Skin
  > INSPECTION FOUND LT WING LOWER SKIN PANEL OF LANDING GEAR VANE DELAMINATED ON THE UPPER AND LOWER SURFACE. THE UPPER AND LOWER SKIN WAS REPAIRED IAW SRM 51-71-00, PARAGRAPH 18B.
- [SDR CALA9900643](https://openairdocs.org/sdr/CALA9900643.md): Beam · cracked · May 28, 1999 · N13066 · Doug DC1030 · Wing Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN RT WING TRAILING EDGE PANEL FITTING BEAM AT STA XORS 299. A REPAIR WAS PERFORMED IAW SRM 57-00-01.
- [SDR CALA9900642](https://openairdocs.org/sdr/CALA9900642.md): Skin · cracked · May 28, 1999 · N13066 · Doug DC1030 · Elevator, Plate/Skin
  > INSPECTION FOUND A.75 INCH CRACK IN LT OUTBOARD ELEVATOR TRAILING EDGE. THE TRACK SECTION TRAILING EDGE WAS REPLACED IAW SRM 55-30-00.
- [SDR CALA9900641](https://openairdocs.org/sdr/CALA9900641.md): Skin · cracked · May 28, 1999 · N13066 · Doug DC1030 · Wing, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN LT WING LEADING EDGE INTERNAL SKIN AT OUTBOARD LOWER CORNER. A REPAIR WAS PERFORMED IAW SRM 57-00-01.
- [SDR CALA9900640](https://openairdocs.org/sdr/CALA9900640.md): Angle · cracked · May 28, 1999 · N13066 · Doug DC1030 · Wing Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN RT WING INBOARD FLAP OUTBOARD AFT FITTING ANGLE. THE ANGLE WAS REPLACED IAW SRM 51-30-00.
- [SDR CALA9900627](https://openairdocs.org/sdr/CALA9900627.md): Floorbeam · corroded · May 28, 1999 · N13066 · Doug DC1030 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM CORRODED BETWEEN STA 1887 AND 2007 ON LT SIDE. THE FLOORBEAM WAS REPLACED IAW SRM 51-31-01.
- [SDR CALA9900626](https://openairdocs.org/sdr/CALA9900626.md): Floor · corroded · May 28, 1999 · N13066 · Doug DC1030 · Fuselage Floor Panel
  > INSPECTION FOUND FORWARD CARGO RT SUPPORT FLOOR PANEL CORRODED AT STA 1099. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-30-00.
- [SDR CALA9900625](https://openairdocs.org/sdr/CALA9900625.md): Floorbeam · corroded · May 28, 1999 · N13066 · Doug DC1030 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM CORRODED BETWEEN STA 427.668 AND 450.162 ON LT SIDE. THE BEAM WAS REPLACED IAW SRM 51-30-00.
- [SDR CALA9900624](https://openairdocs.org/sdr/CALA9900624.md): Floorbeam · corroded · May 28, 1999 · N13066 · Doug DC1030 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 450.162 IN CENTER AND ON RT SIDE. THE FLOORBEAM SECTIONS WERE REPLACED IAW SRM 51-30-00.
- [SDR CALA9900623](https://openairdocs.org/sdr/CALA9900623.md): Floorbeam · corroded · May 28, 1999 · N13066 · Doug DC1030 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 450.162 AND 515, LT SIDE. A NEW FLOORBEAM WAS INSTALLED IAW SRM 51-30-00.
- [SDR CALA9900620](https://openairdocs.org/sdr/CALA9900620.md): Floorbeam · corroded · May 28, 1999 · N13066 · Doug DC1030 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 449.250 ON RT SIDE. THE FLOORBEAM WAS REPLACED IAW SRM 51-30-00.
- [SDR CALA9900639](https://openairdocs.org/sdr/CALA9900639.md): Seat Track · corroded · May 27, 1999 · N13066 · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND SEAT TRACKS CORRODED AT STA 824, LT AND RT SIDES. THE SEAT TRACKS WERE REPLACED IAW MM 53-20-00.
- [SDR CALA9900619](https://openairdocs.org/sdr/CALA9900619.md): Floorbeam · corroded · May 25, 1999 · N13066 · Doug DC1030 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM CORRODED BETWEEN STA 1902 AND 2007, RT SIDE. THE FLOORBEAM WAS REPLACED IAW SRM 51-31-01.
- [SDR CALA9900618](https://openairdocs.org/sdr/CALA9900618.md): Floorbeam · corroded · May 25, 1999 · N13066 · Doug DC1030 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CENTRAL FLOORBEAM (NR 2) CORRODED BETWEEN STA 1841 AND 1887. THE FLOORBEAM WAS REPLACED IAW SRM 51-31-01.
- [SDR CALA9900617](https://openairdocs.org/sdr/CALA9900617.md): Floorbeam · corroded · May 24, 1999 · N13066 · Doug DC1030 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM CORRODED AT RT SIDE BETWEEN STA 1905 AND 2007. THE FLOORBEAM WAS REPLACED IAW SRM 51-31-01.
- [SDR CALA9900616](https://openairdocs.org/sdr/CALA9900616.md): Floorbeam · corroded · May 24, 1999 · N13066 · Doug DC1030 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM CORRODED ON LT AND RT SIDES AT STA 1821-1887. THE FLOORBEAM SECTIONS WERE REPLACED IAW SRM 51-30-00.
- [SDR CALA9900615](https://openairdocs.org/sdr/CALA9900615.md): Floorbeam · corroded · May 20, 1999 · N13066 · Doug DC1030 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED BETWEEN STA 859 AND 879, RT SIDE. THE BEAM WAS REPLACED IAW SRM 51-30-00.
- [SDR CALA9800722](https://openairdocs.org/sdr/CALA9800722.md): Actuator · failed · Apr 29, 1998 · N13066 · Doug DC1030 · Landing Gear Actuator
  > THE LT MLG WOULD NOT RETRACT AFTER TAKEOFF. CYCLING THE GEAR DID NOT HELP. FUEL WAS DUMPED AND THE GEAR WAS VISUALLY CONFIRMED DOWN BY TOWER. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE SWUNG THE LANDING GEAR SEVERAL TIME
- [SDR CALA9800688](https://openairdocs.org/sdr/CALA9800688.md): Skin · corroded · Apr 23, 1998 · N13066 · Doug DC1030 · Trailing Edge Flaps
  > INSPECTION FOUND LT WING INBOARD FLAP SKIN TORN AND CORRODED AT OUTBOARD EDGE CLOSURE RIB. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-21-01, 51-31-01, AND ECRA 5752-01023.
- [SDR CALA9800683](https://openairdocs.org/sdr/CALA9800683.md): Fitting · cracked · Apr 18, 1998 · N13066 · Doug DC1030 · Passenger/Crew Doors
  > INSPECTION FOUND A 2 INCH CRACK IN R-3 DOOR LOWER FITTING. THE LOWER FITTING WAS REMOVED, A NEW BEAM AND FASTENERS WERE INSTALLED IAW SRM 51-31-01.
- [SDR CALA9800682](https://openairdocs.org/sdr/CALA9800682.md): Stiffener · cracked · Apr 18, 1998 · N13066 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK ON LT MLG WHEEL WELL AFT WEB VERTICAL STIFFENER. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 53-53-01, 51-21-01, AND 51-31-01.
- [SDR CALA9800483](https://openairdocs.org/sdr/CALA9800483.md): Hyd Hose · punctured · Mar 18, 1998 · N13066 · Doug DC1030 · Hydraulic System, Main
  > THE NR 2 HYDRAULIC SYSTEM QUANTITY WAS LOST WHILE EN ROUTE FROM IAH TO LGW. THE AIRCRAFT LANDED AT LGW WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC LINE FROM 2-3 REVERSIBLE MOTOR PUMP PUNCTURED AND THE FORWARD SHUTOFF VALVE OF 2-3 REVERSIBLE MOTOR PUMP WAS
- [SDR CALA9601256](https://openairdocs.org/sdr/CALA9601256.md): Batt Charger · inoperative · Sep 2, 1996 · N13066 · Doug DC1030 · Emergency Lighting
  > THE CREW REPORTED EMERGENCY LIGHT TEST IN COCKPIT DID NOT GIVE GREEN LIGHT. MAINTENANCE FOUND MID CABIN OVERWING BATTERY CHARGER SUPPLY AT FAULT. THE BATTERY CHARGER WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD.
- [SDR CAL960226](https://openairdocs.org/sdr/CAL960226.md): Intercostal · corroded · Jan 31, 1996 · N13066 · Doug DC1030 · Fuselage Miscellaneous Structure
  > KUL - INSPECTION FOUND INTERCOSTAL CORRODED ON LEFT SIDE OF AVIONICS COMPARTMENT AT STATION 470, STRINGER 48L. THE INTERCOSTAL WAS REPLACED IAW SRM 53-11-01, FIGURE 5. (M)
- [SDR CAL960225](https://openairdocs.org/sdr/CAL960225.md): Intercostal · corroded · Jan 31, 1996 · N13066 · Doug DC1030 · Fuselage Miscellaneous Structure
  > KUL - INSPECTION FOUND INTERCOSTAL CORRODED AT LOWER FUSELAGE FORWARD SECTION STATION 464R. THE INTERCOSTAL WAS REPLACED IAW SRM 53-11-01, FIGURE 5. (M)
- [SDR CAL960228](https://openairdocs.org/sdr/CAL960228.md): Support · corroded · Jan 30, 1996 · N13066 · Doug DC1030 · Fuselage Miscellaneous Structure
  > KUL - INSPECTION FOUND A GALLEY 'G' SUPPORT CORRODED. THE SUPPORT WAS REPLACED IAW SRM 53-70-00, FIGURE 13. (M)
- [SDR CAL960229](https://openairdocs.org/sdr/CAL960229.md): Support · corroded · Jan 18, 1996 · N13066 · Doug DC1030 · Fuselage Miscellaneous Structure
  > KUL - INSPECTION FOUND GALLEY 7 INBOARD SUPPORT CORRODED. THE SUPPORT WAS REPAIRED IAW SRM 53-70-00, FIGURE 13. (M)
- [SDR CAL960227](https://openairdocs.org/sdr/CAL960227.md): Support · corroded · Jan 17, 1996 · N13066 · Doug DC1030 · Fuselage Miscellaneous Structure
  > KUL - INSPECTION FOUND LAV 'E' OUTBOARD SUPPORT CORRODED AT STATION 1871. THE SUPPORT WAS REPAIRED IAW SRM 53-70-00, FIGURE 13. (M)

## 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 = 'N13066' AND deregistration_id = 'N13066-2018-01-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N13066-2018-01-11/reports

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