# Service difficulty reports: N59083, cancelled Aug 15, 2013

A list on [N59083, cancelled Aug 15, 2013](https://openairdocs.org/deregistered/N59083-2013-08-15.md).

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

- [SDR CNMA20060023](https://openairdocs.org/sdr/CNMA20060023.md): Seal · cut · Aug 23, 2006 · N59083 · Doug DC1030 · Hydraulic Pump (Electric/Engine), Main
  > ABOUT 1.5 HRS INTO FLIGHT NR3 ENG OIL PRESSURE WENT TO 10 PSI, NR3 ENG OIL QUANTITY WENT TO ZERO. PERFORMED PRECAUTIONARY ENG SHUTDOWN NR3 ENG. UPON INSPECTION OF ENGINE FOUND HYDRAULIC PUMP LOCKOUT KIT LEAKING. REF DMI NR 8739. REMOVED LOCKOUT KIT AND FOUND
- [SDR CNMA20060015](https://openairdocs.org/sdr/CNMA20060015.md): Oven · odor · Jun 24, 2006 · N59083 · Doug DC1030 · Buffet/Galleys
  > WHEN FORWARD OVENS 307 & 308 WHERE TURNED ON A STRONG ODOR CAME FROM THEM. WHEN TURNED OFF ODOR DISSIPATED. CLEANED TRAYS BOTH OVENS 307 & 308, OPS CHECK, NO ODOR NOTED, GOOD FOR SERVICE. OMNI AIR IS CURRENTLY ADDING AN INTERVAL FOR CLEANING OVENS AND OVEN
- [SDR CNMA20060007](https://openairdocs.org/sdr/CNMA20060007.md): Push-Pull Cable · broken · Apr 24, 2006 · N59083 · Doug DC1030 · Power Lever
  > DURING TAKEOFF ROLL NR 3 ENGINE WOULD NOT SPOOL UP. INDICATIONS DID NOT CHANGE NO MATTER THROTTLE POSITION. ENGINE REMAINED IN IDLE THRUST. ABORTED TAKEOFF AT 65KTS. FOUND THROTTLE PUSH-PULL CABLE BROKEN AT PYLON REMOVED AND REPLACED PUSH-PULL CABLE IAW MM
- [SDR CNMA200600002](https://openairdocs.org/sdr/CNMA200600002.md): Charger · malfunctioned · Feb 23, 2006 · N59083 · Doug DC1030 · Battery/Charger System
  > DURING CLIMBOUT BATTERY VOLTAGE READ 0 WITH NO CLOCKS. BATTERY CHARGER RELAY RESET 2 TIMES IN-FLIGHT WITH BATTERY VOLTAGE NORMAL AND CLOCKS RETURNED. CHARGER FAILED AGAIN, BATTERY VOLTAGE 0 FOR REMAINDER OF FLIGHT WITH NO CLOCKS. ALL OTHER INDICATIONS NORMA
- [SDR CNMA2006002](https://openairdocs.org/sdr/CNMA2006002.md): Charger · inoperative · Feb 23, 2006 · N59083 · Doug DC1030 · Battery/Charger System
  > DURING CLIMBOUT BATTERY VOLTAGE READ 0 WITH NO CLOCKS. BATTERY CHARGER RELAY RESET 2 TIMES IN-FLIGHT WITH BATTERY VOLTAGE NORMAL AND CLOCKS RETURNED. CHARGER FAILED AGAIN, BATTERY VOLTAGE 0 FOR REMAINDER OF FLIGHT WITH NO CLOCKS. ALL OTHER INDICATIONS NORMA
- [SDR CNMA200500015](https://openairdocs.org/sdr/CNMA200500015.md): Check Valve · leaking · Aug 31, 2005 · N59083 · Doug DC1030 · Fuel Storage
  > FUEL VENTING OUT OF THE LEFT WING VENT BOX AREA. RIGHT SIDE OK. NO TANK OVERFILLED LT ON. APPROX 1600 LBS VENTED. AFTER BLOCK IN FUEL LEAKING OUT OF LEFT FUEL VENT BOX DRAIN. REMOVED AND REPLACED CLIMB VENT FLOAT VALVE IAW DC10 M/M 28-12. ALSO REMOVED AN
- [SDR 2005000015](https://openairdocs.org/sdr/2005000015.md): Valve · malfunctioned · Aug 31, 2005 · N59083 · Doug DC1030 · Fuel Storage
  > FUEL VENTING OUT OF THE LEFT WING VENT BOX AREA. RIGHT SIDE OK. NO TANK OVERFILLED LIGHT ON. APPROX 1600 LBS VENTED. AFTER BLOCK IN FUEL LEAKING OUT OF LEFT FUEL VENT BOX DRAIN. REMOVED AND REPLACED CLIMB VENT FLOAT VLV IAW DC10 M/M 28-12. ALSO REMOVED AN
- [SDR CNMA200500014](https://openairdocs.org/sdr/CNMA200500014.md): Check Valve · leaking · Aug 29, 2005 · N59083 · Doug DC1030 · Fuel Storage
  > AFTER T/O, GOT THE TANK OVERFILLED LT ON. VISUAL CHECK CONFIRMED FUEL VENTING OUT OF THE LEFT WING VENT. FUEL VENTED FOR APPROX 20 MIN. FUEL LOSS CONFIRMED OUT OF NR 3 MAIN AT 2000 LBS. TRIED TAKING TANKS DOWN TO 3000 LBS BELOW FULL AND REFILLING THEM USIN
- [SDR CNMA2005014](https://openairdocs.org/sdr/CNMA2005014.md): Check Valve · malfunctioned · Aug 29, 2005 · N59083 · Doug DC1030 · Fuel Storage
  > AFTER T/O, GOT THE TANK OVERFILLED LEFT ON. VISUAL CHECK CONFIRMED FUEL VENTING OUT OF THE LEFT WING VENT. FUEL VENTED FOR APPROX 20 MIN. FUEL LOSS CONFIRMED OUT OF NR 3 MAIN AT 2000 LBS. TRIED TAKING TANKS DOWN TO 3000 LBS BELOW FULL AND REFILLING THEM US
- [SDR 2005000014](https://openairdocs.org/sdr/2005000014.md): Check Valve · malfunctioned · Aug 29, 2005 · N59083 · Doug DC1030 · Fuel Storage
  > AFTER T/O, RECEIVED TANK OVERFILLED LIGHT ON. VISUAL CHECK CONFIRMED FUEL VENTING OUT OF THE LEFT WING VENT. FUEL VENTED FOR APPROX 20 MIN. FUEL LOSS CONFIRMED OUT OF NR 3 MAIN AT 2000 LBS. TRIED TAKING TANKS DOWN TO 3000 LBS BELOW FULL AND REFILLING THEM
- [SDR 2004000015](https://openairdocs.org/sdr/2004000015.md): Cowling · departed · Nov 24, 2004 · N59083 · Doug DC1030 · Nacelle/Pylon, Main Frame
  > AT CLIMB-OUT, NR 3 ENG LOST ENGINE COWLING DUMPED FUEL RETURNED TO EDDF.
- [SDR 2004000007](https://openairdocs.org/sdr/2004000007.md): Engine · failed · Jun 13, 2004 · N59083 · Doug DC1030 · Engine (Turbine/Turboprop)
  > ON T/O ROLL, NR 1 ENGINE MADE LOUD BANG, ENGINE FAIL LIGHT ILLUMINATED AND EGT PEGGED. N1 WAS 130 PERCENT AND SPEED WAS 125 KIAS. T/O ABORTED. TOWER NOTED FIRE FROM INTAKE.
- [SDR 2004000001](https://openairdocs.org/sdr/2004000001.md): Seal · leaking · Mar 9, 2004 · N59083 · Doug DC1030 · Turbine Engine Oil System
  > NR 2 ENGINE OIL QUANITY STEADILY DECREASED DURING CRUISE. LOST 2.5 QTS IN 50 MINUTES. SHUTDOWN ENGINE TO PRESERVE OIL QTY. RESTARTED ENGINE AT ALT. FL 240, QTY HELD OK FOR APPROACH AND LANDING. FROM PREVIOUS ENGINE DRIVEN HYD PUMP REMOVAL AND BLOCKOUT FOUND S
- [SDR CNMA200300011](https://openairdocs.org/sdr/CNMA200300011.md): Rudder · stuck · Dec 17, 2003 · N59083 · Doug DC1030 · Rudder Control System
  > ON SHORT FINAL AND FLARE RUDDER PEDALS COULD NOT BE MOVED. RUDDER PEDALS COULD NOT BE MOVED ON TAXI IN. TILLER OPERATION NORMAL. CAPTAINS AND CO-PILOTS SAME. LIMITED TRAVEL AT GATE. TAXI CHECK OF RUDDER PEDALS NORMAL. F/O DID NOTICE ALOT OF RUDDER FORCE ON TAK
- [SDR CNMA200300008](https://openairdocs.org/sdr/CNMA200300008.md): Engine · overtemp · Dec 10, 2003 · N59083 · Doug DC1030 · Engine (Turbine/Turboprop)
  > ON INITIAL CLIMBOUT NR 1 ENGINE OIL TEMP CLIMBED TO AND EXCEEDED LIMITS. (PEGGED OUT) SHUT DOWN ENGINE.
- [SDR CNMA200300001](https://openairdocs.org/sdr/CNMA200300001.md): Slide · dislodged · Jan 17, 2003 · N59083 · Doug DC1030 · Escape Slide
  > WHILE AT GATE FLIGHT ATTENDANT OPENED R-1 DOOR WITHOUT DISARMING DOOR. SLIDE CAME OUT OF ITS CONTAINER AND LANDED ON TOP OF CATERING TRUCK AWAITING TO DELIVER. APPARENTLY SLIDE DID NOT FALL FAR ENOUGH TO ACTIVATE DEPLOYMENT MECHANISM. SLIDE WAS REMOVED AND
- [SDR CNMA200200007](https://openairdocs.org/sdr/CNMA200200007.md): Electrical Box · Dec 20, 2002 · N59083 · Doug DC1030 · Landing Gear Position and Warning
  > Overspeed warning sounded at 270 knots - slats confirmed retracted. Removed and replaced Proximity Electronic Unit. Bite test normal.
- [SDR CALA0100762](https://openairdocs.org/sdr/CALA0100762.md): Spar · cracked · Aug 15, 2001 · N59083 · Doug DC1030 · Nacelle/Pylon, Frame/Spar/Rib
  > INSPECTION FOUND A 2 INCH CRACK IN NR 3 PYLON LOWER SPAR WEB AT FAN DUCT CUTOUT. A REPAIR ANGLE AND STIFFENER WERE INSTALLED IAW SRM 54-20-00, FIGURE 19A.
- [SDR 20000810SH021](https://openairdocs.org/sdr/20000810SH021.md): Harness · chafed · Aug 10, 2000 · N59083 · Doug DC1030 · Fuel Quantity Indicator
  > D-CHECK, FQI SYSTEM WIRING CHAFING AND ARCING INSIDE FUEL TANK NR 3, PROBE NR 6, HARNESS FOUND CHAFING ON MOUNT BRACKET OF THE FILL ALOT VALVE IN BAY R07 (XORS- -298-500). WIRES 3E900E22GR X 3E901E22WH DAMAGED THROUGH OUTER SLEEVE INSULATION CAUSING ARCING ON
- [SDR 20000829SH007](https://openairdocs.org/sdr/20000829SH007.md): Harness · chafed · Jul 28, 2000 · N59083 · Doug DC1030 · Fuel Quantity Indicator
  > D-CHECK, FQI SYSTEM WIRING CHAFING AND ARCING INSIDE FUEL TANK NR 3, PROBE NR 6. HARNESS FOUND CHAFING ON MOUNT BRACKET OF THE FILL PILOT VALVE IN BAY R07 (XORS: -298-500). WIRES 3E900E22GR X 3E901E22WH DAMAGED THROUGH OUTER SLEEVE INSULATION CAUSING ARCING
- [SDR CALA0001384](https://openairdocs.org/sdr/CALA0001384.md): Harness · frayed · Jul 26, 2000 · N59083 · Doug DC1030 · Fuel Indicating System
  > INSPECTION FOUND RT WING FUEL TANK WIRING OUTER AND INNER INSULATION CHAFING AND ARCING DAMAGE ON FLOAT SWITCH BRACKET ZONE R07-11, LOCATION T2-104, PROBE XORS = 298.500. ALSO FOUND RT WING FUEL TANK WIRING FRAYED AND INNER FERRULE AT TANK PROBE T2-105, ZONE
- [SDR CALA9901355](https://openairdocs.org/sdr/CALA9901355.md): Floorbeam · corroded · Oct 10, 1999 · N59083 · Doug DC1030 · Fuselage Main, Floor Beam
  > FLOORBEAM J SECTION AT STN 1887 AT 27R - 33R CORRODED. REMOVED CORRODED AREA. FABRICATED AND INSTALLED NEW SECTION PER SRM 51-21-00 AND GMM 10-900-01.
- [SDR CALA9901354](https://openairdocs.org/sdr/CALA9901354.md): Floorbeam · corroded · Oct 10, 1999 · N59083 · Doug DC1030 · Fuselage Main, Floor Beam
  > FLOORBEAM J SECTION AT STA 1887 AT 60L - 90L CORRODED. REMOVED CORRODED AREA. FABRICATED AND INSTALLED NEW SECTION PER SRM 51-21-00 AND GMM 10-900-01.
- [SDR CALA9901353](https://openairdocs.org/sdr/CALA9901353.md): Floorbeam · corroded · Oct 10, 1999 · N59083 · Doug DC1030 · Fuselage Main, Floor Beam
  > FLOORBEAM J SECTION CORRODED AT ST 1887 AT 60R - 90R. REMOVED CORROSION. FABRICATED AND INSTALLED NEW SECTION PER SRM 51-21-00 AND GMM 10-900-01.
- [SDR CALA9901352](https://openairdocs.org/sdr/CALA9901352.md): Floorbeam · corroded · Oct 10, 1999 · N59083 · Doug DC1030 · Fuselage Main, Floor Beam
  > FLOOR BEAM J SECTION CORRODED AT ST 1887 AT 39L TO 58 L. REMOVED CORROSION AND INSTALLED NEW SECTION PER SRM 51-21-00 AND GMM 10-900-01.
- [SDR CALA9900878](https://openairdocs.org/sdr/CALA9900878.md): Decoder · shorted · Jul 28, 1999 · N59083 · Doug DC1030 · Interphone/Passenger Announcement (PA) System
  > SMOKE APPEARED IN THE AIRCRAFT CABIN NEAR THE VICINITY OF SEATS 37 AND 38KL WHILE ON FINAL APPROACH TO DUS. THE FLIGHT ATTENDANT'S PULLED OVERHEAD PANEL IN THE AREA AND USED HALON TO COOL THE AREA. NO FIRE WAS OBSERVED. THE AIRCRAFT LANDED AT DUS WITHOUT IN
- [SDR CALA9801129](https://openairdocs.org/sdr/CALA9801129.md): Battery Charger · inoperative · Jun 18, 1998 · N59083 · Doug DC1030 · Emergency Lighting
  > INSPECTION FOUND THE EMERGENCY AISLE LIGHTING INOPERATIVE AT ROWS 9 AND 10 (LEFT AND RIGHT). THE BATTERY CHARGER AT DOOR 2R AND 2L GALLEY OVERHEAD PANEL WAS REPLACED AND THE EMERGENCY LIGHT BATTERY PACK WAS CHARGED. OPERATIONAL CHECKS WERE GOOD IAW MM 33-50-
- [SDR CALA9800537](https://openairdocs.org/sdr/CALA9800537.md): Slide · inoperative · Mar 23, 1998 · N59083 · Doug DC1030 · Escape Slide
  > INSPECTION FOUND THE R-3 DOOR SLIDE BOTTLE PRESSURE LIGHT ILLUMINATED. THE R-3 DOOR SLIDE WAS REMOVED AND REPLACED AND THE LIGHT TESTED NORMAL.
- [SDR CALA9800206](https://openairdocs.org/sdr/CALA9800206.md): Fire Detector · chafed · Feb 10, 1998 · N59083 · Doug DC1030 · Fire Detection
  > THE NR 2 ENGINE A FIRE LOOP DETECTOR LIGHT BEGAN TO FLICKER WHILE IN CRUISE FLIGHT FROM LGW TO EWR. WHEN THE NR 2 ENGINE THRUST WAS REDUCED THE FLICKERING STOPPED. WHEN THRUST WAS ADDED THE FLICKERING RESUMED. THE NR 2 ENGINE WAS OPERATED WITH PARTIAL THRUS

## 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 = 'N59083' AND deregistration_id = 'N59083-2013-08-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N59083-2013-08-15/reports

---
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