# Service difficulty reports: N68047, cancelled Jul 23, 2013

A list on [N68047, cancelled Jul 23, 2013](https://openairdocs.org/deregistered/N68047-2013-07-23.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 · 59 reports

- [SDR ARWA20060301](https://openairdocs.org/sdr/ARWA20060301.md): Pump · failed · Mar 8, 2006 · N68047 · Doug DC1010 · Turbine Engine Oil System
  > DURING CLIMB FIRST OFFICER NOTICE OIL QUANTITY AND OIL PRESSURE DROP TO ZERO; FOLLOWED BY OIL PRESSURE LIGHT. SHUTDOWN ENGINE NR 2 IN ACCORDANCE WITH ABNORMAL PROCEDURES AND DUMPED 6 MINUTES OF FUEL, DECLARED EMERGENCY LANDING AND LANDED IN MHLM WITH OTHER AB
- [SDR ARWA20060204](https://openairdocs.org/sdr/ARWA20060204.md): Engine · leaking · Feb 22, 2006 · N68047 · Doug DC1010 · Turbine Engine Oil System
  > CLIMBING TO FL 360 AT FL 240, OIL QUANTITY AT ENGINE NR 2 DROPPED TO 1.5 QUARTS AND OIL PRESSURE STARTED TO FLUCTUATE; FOLLOW BY ENGINE NR 2 OIL PRESSURE LO LIGHT; PROCEEDED WITH ABNORMAL ENGINE SHUTDOWN CHECK LIST (OIL TEMPERATURE 115 CELSIUS) AND RETURN TO M
- [SDR ARWA20060201](https://openairdocs.org/sdr/ARWA20060201.md): Drive Assy · malfunctioned · Feb 2, 2006 · N68047 · Doug DC1010 · Engine Thrust Reverser
  > ENGINE NR 2 REVERSER UNLOCK LIGHT ON; ITEM TRANSFERRED TO DMI 19850 AS PER MEL 78-1 CAT-C; DEACTIVATED AND SECURE REVERSER NR 2 STOW POSITION IN ACCORDANCE WITH M/M 78-00-01 PAGE 201. REMOVED AND REPLACED REVERSER DRIVE MOTOR IN ACCORDANCE WITH MAINTENANCE MA
- [SDR ARWA20051201](https://openairdocs.org/sdr/ARWA20051201.md): Cabin Pressure · unknown · Dec 8, 2005 · N68047 · Doug DC1010 · Cabin Pressure Control System
  > AFTER TAKEOFF, UNABLE TO PRESSURIZE; RUN CHECK LIST TWICE, NO RESULT. RETURN TO MPTO. SYSTEM WAS VISUALLY INSPECTED AND PRESSURIZATION CONTROL SYSTEM TEST PERFORMED UNTIL 4 PSI OF DIFFERENTIAL PRESSURE FOUND OK AT THIS TIME IN ACCORDANCE WITH M/M 21-00-00 PA
- [SDR RRXA010032](https://openairdocs.org/sdr/RRXA010032.md): Buss · contaminated · Apr 11, 2001 · N68047 · Doug DC1010F · AC Power Distribution System
  > GEN-B OFF LIGHT CAME ON, AC LOAD ZERO ALT WITH AC BUS TIE 3 ISON LIGHT AND RT EMER PWR. NO CODE TO COVER PROBLEM. FOUND MOISTURE ON DC POWER CENTER IN CACC. REMOVED MOISTURE AND RAN ALL 3 ENGINES IAW DC-10 ENGINE RUN HANDBOOK. NO FAULTS NOTED ON ELECTRICAL
- [SDR CALA9901545](https://openairdocs.org/sdr/CALA9901545.md): Spar · cracked · Dec 1, 1999 · N68047 · Doug DC1010 · Horizontal Stabilizer, Spar/Rib
  > INSPECTION FOUND RT HORIZONTAL STABILIZER UPPER SPAR CRACKED AT UPPER 11B MOUNTING HOLE FOR I/B L/E SECTION. THE AREA WAS REPAIRED IAW ECRA 5510-01473 AND EA 10-5510-2-A0514.
- [SDR CALA9901379](https://openairdocs.org/sdr/CALA9901379.md): Former · cracked · Oct 14, 1999 · N68047 · Doug DC1010 · Wing Miscellaneous Structure
  > LEFT WING TIP CRACKED IN THREE PLACES (3) INSIDE PANEL. REMOVED FORMER. FABRICATED AND INSTALLED NEW FORMER PER SRM 51-31-01, 57-23-01 AND 51-10-04.
- [SDR CALA9802185](https://openairdocs.org/sdr/CALA9802185.md): Skin · corroded · Dec 18, 1998 · N68047 · Doug DC1010 · Wing, Plate/Skin
  > INSPECTION FOUND CORROSION AROUND FASTENERS ON RT WING LOWER SKIN PANEL AT XORS 230. THE CORRODED AREA WAS TRIMMED OUT. FILLER AND DOUBLER WERE INSTALLED IAW ECRA 5730-01616.
- [SDR CALA9802184](https://openairdocs.org/sdr/CALA9802184.md): Strap · corroded · Dec 18, 1998 · N68047 · Doug DC1010 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CORROSION ON FORWARD CARGO COMPARTMENT REINFORCEMENT STRAP AT STA 999, LONGERON 43L. THE CORRODED AREA OF STRAP AND WEB WERE TRIMMED OUT AND A REPAIR WAS PERFORMED IAW SRM 53-50-00, FIGURE 1.
- [SDR CALA9802183](https://openairdocs.org/sdr/CALA9802183.md): Skin · corroded · Dec 18, 1998 · N68047 · Doug DC1010 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND CORROSION AT LOWER SIDE OF CENTER CARGO DOOR COMPARTMENT CUTOUT. THE AREA WAS REPAIRED IAW ECRA 5315-01027 AND SRM 53-50-00, FIGURE 22.
- [SDR CALA9802176](https://openairdocs.org/sdr/CALA9802176.md): Rib · cracked · Dec 14, 1998 · N68047 · Doug DC1010 · Leading Edge Devices
  > INSPECTION FOUND A 4 INCH CRACK IN NR 2 SLAT RIB. THE RIB WAS REPLACED IAW MM 27-80-01, PAGE 402B AND 601 AND SRM 51-31-01.
- [SDR CALA9802160](https://openairdocs.org/sdr/CALA9802160.md): Support · corroded · Dec 9, 1998 · N68047 · Doug DC1010 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1902 TO 1921, RBL 26. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-31-01.
- [SDR CALA9802159](https://openairdocs.org/sdr/CALA9802159.md): Frame · corroded · Dec 9, 1998 · N68047 · Doug DC1010 · Fuselage Main, Frame
  > INSPECTION FOUND FRAME CORRODED IN LOWER LOBE CENTER CARGO BILGE AREA AT STA 1701 BETWEEN STRINGER 48R AND 48L. THE FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW SRM 51-31-01 AND 51-31-01.
- [SDR CALA9802141](https://openairdocs.org/sdr/CALA9802141.md): Support · corroded · Dec 6, 1998 · N68047 · Doug DC1010 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND GALLEY FLOOR SUPPORT CORRODED AT STA 791, RBL 50 TO 70. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-31-01.
- [SDR CALA9802140](https://openairdocs.org/sdr/CALA9802140.md): Frame · cracked · Dec 6, 1998 · N68047 · Doug DC1010 · Aerodynamic Fairings
  > INSPECTION FOUND A 2 INCH CRACK IN TAIL CONE FRAME UNDER ACTUATOR LINK AREA. THE CRACKED AREA WAS TRIMMED OUT. THE AREA WAS REINFORCED WITH FRAME AND SPLICE IAW SRM 53-30-00, FIGURE 3, 51-31-01 AND 51-21-01.
- [SDR CALA9802139](https://openairdocs.org/sdr/CALA9802139.md): Rib · cracked · Dec 6, 1998 · N68047 · Doug DC1010 · Wing, Rib/Bulkhead
  > INSPECTION FOUND A 1 INCH CRACK ON RIB OF RT WING FIXED LEADING EDGE JUST IN FRONT OF L/E DEVICE NR 5. THE CRACKED AREA OF RIB WAS TRIMMED OUT. THE AREA WAS REINFORCED WITH A DOUBLER IAW SRM 57-00-01, FIGURE 4, 51-21-01, AND 51-33-01.
- [SDR CALA9802138](https://openairdocs.org/sdr/CALA9802138.md): Rib · cracked · Dec 6, 1998 · N68047 · Doug DC1010 · Wing, Rib/Bulkhead
  > INSPECTION FOUND A 1 INCH CRACK ON RIB OF FIXED LEADING EDGE RT WING BETWEEN STA XORS 455 AND 506. THE CRACKED AREA OF RIB WAS TRIMMED. THE AREA WAS REINFORCED WITH A DOUBLER IAW SRM 57-00-01, FIGURE 4 AND 51-31-01.
- [SDR CALA9802137](https://openairdocs.org/sdr/CALA9802137.md): Floorbeam · cracked · Dec 6, 1998 · N68047 · Doug DC1010 · Fuselage Main, Floor Beam
  > INSPECTION FOUND A 2 INCH CRACK ON FLOORBEAM STA 1289, AT NR 3 DOOR LOWER JAMB. THE CRACKED AREA OF FLOORBEAM WAS TRIMMED OUT, A REPAIR WAS PERFORMED IAW ENGINEERING ORDER D10-53-86781 AND ECRA 5314-01003.
- [SDR CALA9800922](https://openairdocs.org/sdr/CALA9800922.md): Batt Charger · inoperative · May 29, 1998 · N68047 · Doug DC1010 · Emergency Lighting
  > INSPECTION FOUND EMERGENCY PATH LIGHTING AT SEATS 28 TO 35AB (STA 825) INOPERATIVE. THE EMERGENCY AISLE LIGHT BATTERY CHARGER WAS REMOVED AND REPLACED IAW MM 33-55-00, PAGE 1.
- [SDR CALA9800786](https://openairdocs.org/sdr/CALA9800786.md): Wire · shorted · May 5, 1998 · N68047 · Doug DC1010 · Light System Wiring
  > EMERGENCY FLOOR ILLUMINATION LIGHTS INOP ROWS 29 TO 35 LEFT AND RIGHT AISLES. FOUND WIRES UNDER SEAT 30B SHORTED. REPAIRED WIRING AND REPLACED BATTERY FUSE.
- [SDR CALA9800607](https://openairdocs.org/sdr/CALA9800607.md): Skin · punctured · Mar 31, 1998 · N68047 · Doug DC1010 · Leading Edge Devices
  > INSPECTION FOUND A 1 INCH DIAMETER HOLE IN NR 4 LEADING EDGE SLAT JUST OUTBOARD OF CENTER TRACK. THE DAMAGED AREA WAS CUT OUT, FILLER, DOUBLER, BAFFLE AND SPLICE PLATE WERE FABRICATED AND INSTALLED IAW SRM 57-10-00, PAGE 27 AND ECRA 5752-01022.
- [SDR CALA9701671](https://openairdocs.org/sdr/CALA9701671.md): Skin · cracked · Nov 20, 1997 · N68047 · Doug DC1010 · Air Conditioning Doors
  > INSPECTION FOUND A 2 AND 19.5 INCH CRACK IN LT FORWARD AC PACK ACCESS DOOR UPPER SKIN DOUBLER AT BS 501 TO 526. THE DOOR SKIN WAS REPAIRED IAW ECRA 5240-01214.
- [SDR CALA9701670](https://openairdocs.org/sdr/CALA9701670.md): Skin · corroded · Nov 20, 1997 · N68047 · Doug DC1010 · Wing, Plate/Skin
  > INSPECTION FOUND CORROSION ON RT WING SKIN LOWER SURFACE, 2.5 FEET INBOARD AND 3 FEET OUTBOARD OF NR 3 PYLON TRAILING EDGE FROM REAR SPAR TO TWO FEET FORWARD (XORS 370-433). THE CORROSION WAS REMOVED IAW SRM 51-21-00. THE FASTENERS WERE REINSTALLED IAW SRM 5
- [SDR CALA9701669](https://openairdocs.org/sdr/CALA9701669.md): Doubler · cracked · Nov 20, 1997 · N68047 · Doug DC1010 · Horizontal Stabilizer Structure
  > INSPECTION FOUND RT HORIZONTAL STABILIZER LEADING EDGE CENTER SECTION (BEAD DOUBLER) CRACKED IN TWO PLACES AT WAFFLES FORE AND AFT OF NR 4 RIB, XFS 343 AND XFS 349. THE CRACKED MEASURED 1 AND 3 INCH LONG. THE CRACKED AREA WAS CUT OUT, FILLER AND DOUBLER WERE
- [SDR CALA9701668](https://openairdocs.org/sdr/CALA9701668.md): Longeron · corroded · Nov 20, 1997 · N68047 · Doug DC1010 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND LONGERON 46R CORRODED AT STA 1046. THE LONGERON, FINGER TIP, AND OLD DOUBLER WERE REMOVED. A NEW DOUBLER, LONGERON, AND FINGER TIP WERE FABRICATED AND INSTALLED IAW SRM 53-20-0 AND ECRA 5310-03621.
- [SDR CALA9701667](https://openairdocs.org/sdr/CALA9701667.md): Shear Tie · corroded · Nov 20, 1997 · N68047 · Doug DC1010 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SHEAR TIE CORRODED IN CAC COMPARTMENT FORWARD OF THE DOOR CUTOUT FRAME AT FS 1104.5, LONGERON 48R. THE CAC DOOR AND RIVETS WERE REMOVED TO GAIN ACCESS IAW SRM 51-31-01. THE CORRODED SHEAR TIE WAS CUT OUT IAW SRM 51-31-1. A NEW SHEAR TIE WAS
- [SDR CALA9701666](https://openairdocs.org/sdr/CALA9701666.md): Skin · cracked · Nov 20, 1997 · N68047 · Doug DC1010 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN CRACKED AROUND CUTOUT FOR EXHAUST DOOR OF NR 2 PACK AT FS 561 AND 587. THE CRACKS MEASURED.5 TO 3 INCH LONG. THE FASTENERS WERE REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5330-02605.
- [SDR CALA9701631](https://openairdocs.org/sdr/CALA9701631.md): Skin · corroded · Nov 13, 1997 · N68047 · Doug DC1010 · Wing, Plate/Skin
  > INSPECTION FOUND RT WING LEADING EDGE UPPER AFT SKIN CORRODED WITH SEVERAL.125 INCH CRACKS AT FASTENERS. THE LEADING EDGE WAS REMOVED, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 57-10-0. INSTALLED FLEX PANEL IAW MM 27-80-02 AND OPERATIONAL CHECK WAS
- [SDR CALA9701630](https://openairdocs.org/sdr/CALA9701630.md): Spar Cap · corroded · Nov 13, 1997 · N68047 · Doug DC1010 · Wing Spar
  > INSPECTION FOUND CORROSION ON REAR SPAR CAP OF LT WING AT XORS 538 (NR 2 SPOILER ACTUATOR MOUNT CASTING). THE CORROSION WAS REMOVED IAW SRM 51-10-03. THE AREA WAS REPAIRED IAW ECRA 5710-01848.
- [SDR CALA9701629](https://openairdocs.org/sdr/CALA9701629.md): Spar Cap · corroded · Nov 13, 1997 · N68047 · Doug DC1010 · Wing Spar
  > INSPECTION FOUND CORROSION ON LOWER SIDE OF UPPER SPAR CAP OF LT WING AT XORS 544 (AFT SPAR 12 OUTBOARD OF NR 2 SPOILER ACTUATOR MOUNT CASTING). THE CORROSION WAS REMOVED IAW SRM 51-10-3. THE AREA WAS REPAIRED IAW ECRA 5710-01848.
- [SDR CALA9701628](https://openairdocs.org/sdr/CALA9701628.md): Spar · corroded · Nov 13, 1997 · N68047 · Doug DC1010 · Wing Spar
  > INSPECTION FOUND CORROSION ON LT WING REAR SPAR AT XORS 588 (NR 3 SPOILER AREA 10 OUTBOARD OF SPOILER INBOARD MOUNT FITTING). THE AREA WAS REPAIRED IAW ECRA 5710-01848.
- [SDR CALA9701617](https://openairdocs.org/sdr/CALA9701617.md): Vane · disbonded · Nov 12, 1997 · N68047 · Doug DC1010 · Trailing Edge Flaps
  > INSPECTION FOUND RT INBOARD FLAP VANE DISBONDED ON UPPER TRAILING EDGE. THE FLAP VANE WAS REMOVED AND REPLACED IAW MM 27-50-03.
- [SDR CALA9701616](https://openairdocs.org/sdr/CALA9701616.md): Bracket · cracked · Nov 12, 1997 · N68047 · Doug DC1010 · Wing Miscellaneous Structure
  > INSPECTION FOUND A.75 INCH CRACK IN UPPER RIB TO STRINGER CLIP/BRACKET JUST AFT OF TANK ACCESS 634 AT INBOARD RIB, STA XORS 402. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-31-1.
- [SDR CALA9701611](https://openairdocs.org/sdr/CALA9701611.md): Skin · corroded · Nov 12, 1997 · N68047 · Doug DC1010 · Landing Gear Doors
  > INSPECTION FOUND THE LEADING EDGE INNER SKIN OF BOTH THE LEFT AND RIGHT FORWARD NOSE GEAR DOORS CORRODED. THE CORRODED AREAS WERE REMOVED. REPAIRS WERE FABRICATED AND INSTALLED IAW ECRA 5280-01166.
- [SDR CALA9701610](https://openairdocs.org/sdr/CALA9701610.md): Longeron · corroded · Nov 12, 1997 · N68047 · Doug DC1010 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND CIRCUMFERENTIAL FRAME AND LONGERON 48L CORRODED AT STA 1820 IN AFT CARGO COMPARTMENT. THE ANGLE SUPPORT WAS REMOVED AND THE CORRODED AREA WAS CUT OUT IAW SRM 53-10-0. A NEW ANGLE SUPPORT WAS FABRICATED IAW SRM 51-10-1. THE CORROSION ON FING
- [SDR CALA9701609](https://openairdocs.org/sdr/CALA9701609.md): Longeron · corroded · Nov 12, 1997 · N68047 · Doug DC1010 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND LONGERON 45L CORRODED AT STA 1954. A NEW SECTION OF LONGERON WAS FABRICATED AND INSTALLED IAW SRM 51-31-01.
- [SDR CALA9701608](https://openairdocs.org/sdr/CALA9701608.md): Skin · dented · Nov 12, 1997 · N68047 · Doug DC1010 · Horizontal Stabilizer, Plate/Skin
  > INSPECTION FOUND RT HORIZONTAL STABILIZER DENTED ON LOWER LEADING EDGE AT XE 332. THE ACCESS PANEL WAS REMOVED AND THE DENTED AREA WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-10-00.
- [SDR CALA9701561](https://openairdocs.org/sdr/CALA9701561.md): Shear Tie · cracked · Oct 15, 1997 · N68047 · Doug DC1010 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SHEAR TIE IN CAC COMPARTMENT FORWARD OF THE DOOR CUTOUT CRACKED AT LONGERON 48 AND 49. THE SHEAR TIE WAS REMOVED AND A REPLACEMENT WAS FABRICATED AND INSTALLED IAW SRM 51-31-01, 51-10-00, 51-21-01, AND 53-30-0.
- [SDR CALA9701560](https://openairdocs.org/sdr/CALA9701560.md): Structure · corroded · Oct 13, 1997 · N68047 · Doug DC1010 · Fuselage Main, Structure
  > INSPECTION FOUND NR 1 AND NR 2 PACK COMPARTMENT FRAMES AND SKIN CORRODED. THE CORROSION WAS REMOVED AND AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-50-2 AND 51-31-01.
- [SDR CALA9701568](https://openairdocs.org/sdr/CALA9701568.md): Skin · punctured · Oct 12, 1997 · N68047 · Doug DC1010 · Horizontal Stabilizer, Plate/Skin
  > INSPECTION FOUND A HOLE IN LEADING EDGE OF LEFT HORIZONTAL STABILIZER AT XFS 154.311. FILLER AND DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-35-01.
- [SDR CALA9701569](https://openairdocs.org/sdr/CALA9701569.md): Structure · corroded · Oct 8, 1997 · N68047 · Doug DC1010 · Fuselage Main, Structure
  > INSPECTION FOUND CORROSION ON FRAME AND LONGERON IN AFT CARGO COMPARTMENT AT STA 1781, LONGERON 45L AND 46L. THE CORROSION WAS REMOVED, A SHEAR TIE WAS FABRICATED AND INSTALLED IAW SRM 51-90-0.
- [SDR CALA9701563](https://openairdocs.org/sdr/CALA9701563.md): Spar Chord · corroded · Oct 6, 1997 · N68047 · Doug DC1010 · Wing Spar
  > INSPECTION FOUND RT WING REAR SPAR LOWER CHORD CORRODED ON BOTH SIDES OF NR 2 SPOILER ACTUATOR INBOARD SUPPORT LEG. THE FASTENERS WERE REMOVED, THE CORROSION WAS REMOVED AND THE FASTENERS WERE REINSTALLED IAW ECRA 5710-01849.
- [SDR CALA9701562](https://openairdocs.org/sdr/CALA9701562.md): Spar · corroded · Oct 6, 1997 · N68047 · Doug DC1010 · Wing Spar
  > INSPECTION FOUND CORROSION ON LT WING REAR SPAR IN NR 3 SPOILER AREA TEN INCHES OUTBOARD OF SPOILER INBOARD MOUNT FITTING. THE FASTENERS WERE REMOVED, THE CORROSION WAS REMOVED, AND THE FASTENERS WERE REINSTALLED IAW SRM 51-21-01.
- [SDR CALA9701567](https://openairdocs.org/sdr/CALA9701567.md): Skin · dented · Oct 4, 1997 · N68047 · Doug DC1010 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT FS 1927 BETWEEN LONGERON 27R AND 29R. THE DENTED AREA WAS CUT OUT, FILLER AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-20-0, FIGURE 6.
- [SDR CALA9701566](https://openairdocs.org/sdr/CALA9701566.md): Skin · corroded · Oct 3, 1997 · N68047 · Doug DC1010 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND CORROSION IN SKIN AROUND FASTENERS OF AFT LOWER BELLY AT FS 1816, LONGERON 43R. THE CORRODED AREA WAS CUT OUT, FILLER, FINGER DOUBLER AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-20-0, FIGURE 6.
- [SDR CALA9701565](https://openairdocs.org/sdr/CALA9701565.md): Casting · corroded · Oct 3, 1997 · N68047 · Doug DC1010 · Drag Control Actuator
  > INSPECTION FOUND CORROSION IN LT WING NR 2 SPOILER ACTUATOR MOUNT CASTING (UPPER OUTBOARD MOUNT AT AFT SPAR). THE CORROSION WAS REMOVED IAW SRM 51-30-02 AND 51-10-03.
- [SDR CALA9701564](https://openairdocs.org/sdr/CALA9701564.md): Spar Cap · corroded · Oct 3, 1997 · N68047 · Doug DC1010 · Wing Spar
  > INSPECTION FOUND CORROSION ON LOWER SIDE OF LT WING UPPER SPAR CAP, AFT SPAR TWELVE INCHES OUTBOARD OF NR 2 SPOILER ACTUATOR MOUNT CASTING. THE UPPER WING PANEL WAS REMOVED, THE CORROSION WAS REMOVED AND THE PANEL WAS REINSTALLED IAW SRM 51-30-02 AND 51-10-03
- [SDR CALA9701248](https://openairdocs.org/sdr/CALA9701248.md): Slide · low pressure · Aug 27, 1997 · N68047 · Doug DC1010 · Escape Slide
  > THE CREW FOUND THE L-3 DOOR SLIDE LOW PRESSURE LIGHT ILLUMINATED. THE L-3 DOOR SLIDE WAS REMOVED AND REPLACED IAW MM 25-61-02.
- [SDR CALA9700173](https://openairdocs.org/sdr/CALA9700173.md): Balance Valve · leaking · Feb 13, 1997 · N68047 · Doug DC1010 · Hydraulic System, Main
  > THE NR 2 HYDRAULIC SYSTEM WAS OBSERVED TO BE AT ONE GALLON DURING DESCENT. THE EMERGENCY CHECKLIST WAS ACCOMPLISHED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 HYDRAULIC SYSTEM BALANCE VALVE LEAKING. THE BALANCE VALVE WAS REMOVED AN
- [SDR CALA9700068](https://openairdocs.org/sdr/CALA9700068.md): Actuator · inoperative · Jan 17, 1997 · N68047 · Doug DC1010 · Rudder Actuator
  > THE AIRCRAFT EXPERIENCED A HARD RIGHT AND VERY ABRUPT RUDDER UNCOMMANDED YAW AT ROTATION ON TAKEOFF. MAINTENANCE FOUND THE LOWER RUDDER ACTUATOR AT FAULT. THE LOWER RUDDER ACTUATOR WAS REMOVED AND REPLACED IAW MM 27-23-01. LEAK AND OPERATIONAL CHECKS WERE G

Next page: https://openairdocs.org/deregistered/N68047-2013-07-23/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 = 'N68047' AND deregistration_id = 'N68047-2013-07-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N68047-2013-07-23/reports

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