# Service difficulty reports: N12061, cancelled Jun 7, 2017

A list on [N12061, cancelled Jun 7, 2017](https://openairdocs.org/deregistered/N12061-2017-06-07.md).

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

- [SDR HALA0100248](https://openairdocs.org/sdr/HALA0100248.md): Rccb · failed · Oct 10, 2001 · N12061 · Doug DC1030 · DC Power Distribution System
  > LAX - FLT 32 - AIR DIVERSION AT 3 HOURS INTO FLIGHT, LT EMERGENCY AC BUS OFF LIGHT ILLUMINATED, RESTORED SYSTEM. FOLLOWED CHECKLIST, 5 MINUTES LATER PROBLEM REOCCURRED. NR 1 GALLEY POWER OFF LIGHT ILLUMINATED. COULD NOT RESTORE POWER BY RESETTING, REMAINED
- [SDR CALA0100470](https://openairdocs.org/sdr/CALA0100470.md): Floor Support · cracked · May 17, 2001 · N12061 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 6 INCH CRACK IN CENTER CARGO FLOOR SUPPORT FLANGE AT STA 1601, X = 18R. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 53-30-1 AND GMM 10-900-01.
- [SDR CALA0100469](https://openairdocs.org/sdr/CALA0100469.md): Seat Track · corroded · May 17, 2001 · N12061 · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND SEAT TRACK CORRODED AT STA Y = 2000-2007, X = 90L. THE SEAT TRACK WAS REPAIRED IAW SRM 53-70-00, FIGURE 5 AND ECRA 5100-01844.
- [SDR CALA0100466](https://openairdocs.org/sdr/CALA0100466.md): Skin · cracked · May 16, 2001 · N12061 · Doug DC1030 · Wing, Plate/Skin
  > INSPECTION FOUND A CRACK IN RT WING LEADING EDGE SKIN AT SLAT NR 7 I/B TRACK, XORS 79.9. REPAIRED IAW SRM 57-10-00.
- [SDR CALA0100465](https://openairdocs.org/sdr/CALA0100465.md): Shear Tie · corroded · May 16, 2001 · N12061 · Doug DC1030 · Fuselage Main, Structure
  > INSPECTION FOUND SHEAR CLEAT IN CENTER CARGO BILGE CORRODED AT STA 1801 BETWEEN LONGERON 49L AND 49R. THE SHEAR CLEAT WAS REMOVED AND A NEW SHEAR CLEAT WAS INSTALLED IAW SRM 51-30-01 AND GMM 10-900-01.
- [SDR CALA0100464](https://openairdocs.org/sdr/CALA0100464.md): Shear Tie · corroded · May 16, 2001 · N12061 · Doug DC1030 · Fuselage Main, Structure
  > INSPECTION FOUND SHEAR CLEAT CORRODED AT STA 1841 BETWEEN LONGERON 48R AND 47R. THE SHEAR CLEAT WAS REMOVED AND A NEW SHEAR CLEAT WAS INSTALLED IAW SRM 51-30-01 AND GMM 10-900-01.
- [SDR CALA0100463](https://openairdocs.org/sdr/CALA0100463.md): Shear Tie · corroded · May 16, 2001 · N12061 · Doug DC1030 · Fuselage Main, Structure
  > INSPECTION FOUND SHEAR CLEAT CORRODED AT STA 1902 BETWEEN LONGERONS 51R AND 50R AND BETWEEN LONGERONS 48L AND 47L. THE SHEAR CLEATS WERE REMOVED AND NEW SHEAR CLEATS WERE INSTALLED IAW SRM 51-30-01 AND GMM 10-900-01.
- [SDR CALA0100462](https://openairdocs.org/sdr/CALA0100462.md): Floor Support · corroded · May 16, 2001 · N12061 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND J-SECTION FLOOR SUPPORT CORRODED AT STA Y = 824, X = 50 TO 74. THE FLOOR SUPPORT WAS REPLACED IAW SRM 53-14-01 AND GMM 10-900-01.
- [SDR CALA0100456](https://openairdocs.org/sdr/CALA0100456.md): Floor Support · corroded · May 13, 2001 · N12061 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LAV J O/B FLOOR SUPPORT BEAM CORRODED IN AREAS OF TIE DOWN BOLTS AT STAY = 1887-2007 AT X = 58R. THE FLOOR SUPPORT BEAM WAS REMOVED AND A NEW FLOOR SUPPORT BEAM WAS INSTALLED IAW SRM 53-16-01.
- [SDR CALA0100450](https://openairdocs.org/sdr/CALA0100450.md): Beam · corroded · May 8, 2001 · N12061 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND REAR PRESSURE BULKHEAD T-SECTION LATERAL BEAM CORRODED AT ATTACHMENT POINTS AT STA Y = 2007 AND X = 58R, 58L, 27R, AND 27L. A NEW BEAM WAS INSTALLED IAW ECRA 5100-01844 AND SRM 53-16-01.
- [SDR HALA0000237](https://openairdocs.org/sdr/HALA0000237.md): Fuse · failed · Jul 22, 2000 · N12061 · Doug DC1030 · AC Power Distribution System
  > FLT 006 - OGG - AFTER ENGINE START AC BUS TIE WAS NOT POWERED BY ANY GENERATOR. PERFORMED AC BUS TIE. ISOL LIGHTS ILLUMINATED. NO CHANGE. TROUBLESHOT AND FOUND BCU INPUT FUSE LIGHT ON. REPLACED FUSE. RAN ALL 3 ENGINES. AC BUS TIE ISOLATION OFF. BUSSES
- [SDR HALA0000236](https://openairdocs.org/sdr/HALA0000236.md): Pump · failed · Jul 22, 2000 · N12061 · Doug DC1030 · Hydraulic Pump (Electric/Engine), Main
  > FLT 006 - OGG - NR 2 ENGINE DRIVEN HYDRAULIC PUMP WOULD NOT DEPRESSURIZE WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYD PUMP, LEFT PUMP. OPERATIONAL AND LEAK CHECK GOOD. ALL HYDRAULIC QUANTITIES ARE AT NORMAL FULL LEVEL. WORK DONE
- [SDR CALA0000395](https://openairdocs.org/sdr/CALA0000395.md): Hinge · cracked · Apr 4, 2000 · N12061 · Doug DC1030 · Wing Miscellaneous Structure
  > INSPECTION FOUND A 0.2 INCH CRACK IN RT WING TRAILING EDGE HINGE AT STA XORS 714. THE HINGE WAS REPLACED IAW SRM 57-31-01.
- [SDR CALA9900664](https://openairdocs.org/sdr/CALA9900664.md): Fuse · blown · Jun 10, 1999 · N12061 · Doug DC1030 · Emergency Lighting
  > THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE FROM ROWS 35-45 A/B. MAINTENANCE FOUND A FUSE BLOWN FOR THAT SECTION. THE FUSE WAS REPLACED. OPERATION OF THE LIGHTS CHECKED GOOD.
- [SDR CALA9900333](https://openairdocs.org/sdr/CALA9900333.md): Skin · corroded · Mar 27, 1999 · N12061 · Doug DC1030 · Ailerons
  > INSPECTION FOUND RT WING O/B AILERON LOWER SKIN CORRODED. THE AILERON WAS REMOVED AND REPLACED IAW MM 27-10-02.
- [SDR CALA9900331](https://openairdocs.org/sdr/CALA9900331.md): Panel · cracked · Mar 26, 1999 · N12061 · Doug DC1030 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND A 3 INCH CRACK ON NR 3 PYLON PANEL NR 487ER. THE PANEL WAS REPLACED IAW SRM 51-30-00.
- [SDR CALA9900330](https://openairdocs.org/sdr/CALA9900330.md): Panel · cracked · Mar 26, 1999 · N12061 · Doug DC1030 · Wing, Plate/Skin
  > INSPECTION FOUND A 3 INCH CRACK IN RT WING LEADING EDGE ACCESS PANEL NR 617CT. THE PANEL WAS REPLACED IAW SRM 51-31-01.
- [SDR CALA9900325](https://openairdocs.org/sdr/CALA9900325.md): Skin · cracked · Mar 25, 1999 · N12061 · Doug DC1030 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND A 1 CRACK IN NR 3 PYLON SKIN. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5450-01212. A DIP WAS ISSUED TO CHECK BLIND FASTENERS FOR SECURITY EVERY 1000 CYCLES UNTIL A PERMANENT REPAIR IS INSTALLED WITHIN 400 DAYS.
- [SDR CALA9900324](https://openairdocs.org/sdr/CALA9900324.md): Battery · discharged · Mar 25, 1999 · N12061 · Doug DC1030 · Emergency Lighting
  > INSPECTION FOUND FLASHLIGHTS INOPERATIVE AT FLIGHT ATTENDANT SEATS 1L-4L AFT. THE FLASHLIGHT BATTERIES WERE REPLACED IAW MM 25-60-00.
- [SDR CALA9900321](https://openairdocs.org/sdr/CALA9900321.md): Skin · cracked · Mar 24, 1999 · N12061 · Doug DC1030 · Trailing Edge Flaps
  > INSPECTION FOUND A 1 CRACK IN RT WING OUTBOARD FLAP SKIN. THE SKIN WAS REPLACED IAW DOUGLAS DRAWING ARC1653.
- [SDR CALA9900320](https://openairdocs.org/sdr/CALA9900320.md): Inlet · cracked · Mar 24, 1999 · N12061 · Doug DC1030 · Engine Cowling System
  > INSPECTION FOUND TWO INCH CRACKS IN THE NR 3 ENGINE FAN INLET. REPAIRED IAW SRM 54-11-00, PAGE 23.
- [SDR CALA9900319](https://openairdocs.org/sdr/CALA9900319.md): Skin · cracked · Mar 24, 1999 · N12061 · Doug DC1030 · Air Conditioning Doors
  > INSPECTION FOUND A 1.5 CRACK IN SKIN OF PACK DOOR NR 3. THE AREA WAS REPAIRED IAW SRM 53-50-00, FIGURE 3.
- [SDR CALA9900302](https://openairdocs.org/sdr/CALA9900302.md): Skin · cracked · Mar 20, 1999 · N12061 · Doug DC1030 · Landing Gear Doors
  > INSPECTION FOUND A.75 INCH CRACK IN LT MLG DOOR SKIN. REPAIRED IAW SRM 53-00-01.
- [SDR CALA9900242](https://openairdocs.org/sdr/CALA9900242.md): Skin · cracked · Mar 10, 1999 · N12061 · Doug DC1030 · Wing, Plate/Skin
  > INSPECTION FOUND A.25 INCH CRACK NEAR WING SKIN PANEL 515AB HOLE. A REPAIR WAS PERFORMED IAW SRM 57-00-01, FIGURE 4.
- [SDR CALA9801806](https://openairdocs.org/sdr/CALA9801806.md): Fuse · reqd bleeding · Sep 20, 1998 · N12061 · Doug DC1030 · Landing Gear Retraction/Extension System
  > THE LANDING GEAR HANDLE WOULD NOT MOVE TO UP POSITION AFTER TAKEOFF. THE APPROPRIATE CHECKLIST WAS COMPLETED WITH NO HELP. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE TRIM CYLINDER INTERLOCK FUSE IN THE RT WHEEL
- [SDR CALA9800267](https://openairdocs.org/sdr/CALA9800267.md): Jamb · cracked · Feb 16, 1998 · N12061 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND TWO, 2 INCH CRACKS AT UPPER SIDE OF FORWARD VERTICAL DOOR JAMB OF LT FORWARD AIR CONDITIONING COMPARTMENT. ONE AREA WAS TRIMMED AND BLENDED OUT. THE OTHER AREA WAS REWORKED AND REINFORCED WITH A DOUBLER IAW SRM 53-30-00, FIGURE 4. NEW RIVET
- [SDR CALA9601511](https://openairdocs.org/sdr/CALA9601511.md): Connector · pulled wire · Oct 25, 1996 · N12061 · Doug DC1030 · Landing Gear Position and Warning
  > THE RT MLG RED UNSAFE LIGHT ILLUMINATED DURING APPROACH FOR LANDING AT LGW. THE APPROACH WAS ABORTED AND ALTERNATE GEAR EXTENSION WAS USED. GEAR DOWN INDICATIONS WERE NORMAL AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT MLG PROXIMITY DO
- [SDR CALA9601319](https://openairdocs.org/sdr/CALA9601319.md): Hyd Line · leaking · Sep 18, 1996 · N12061 · Doug DC1030 · Hydraulic System, Main
  > THE AIRCRAFT LOST THE NR 1 HYDRAULIC SYSTEM WHILE IN FLIGHT. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE LT HYDRAULIC PUMP SUPPLY LINE LEAKING. THE HYDRAULIC SUPPLY LINE WAS REMOVED AND REPLACED. THE
- [SDR CAL950500](https://openairdocs.org/sdr/CAL950500.md): Hyd Line · leaking · Jun 18, 1995 · N12061 · Doug DC1030 · Hydraulic System, Main
  > EWR - FLT 0010 - THE NR 1 HYDRAULIC SYSTEM QUANTITY WAS LOST WHILE ENROUTE FROM IAH TO ORY. THE AIRCRAFT WAS DIVERTED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC PRESSURE LINE FROM THE LEFT ENGINE DRIVEN PUMP TO THE PRESSURE MODU
- [SDR CAL950406](https://openairdocs.org/sdr/CAL950406.md): Harness · burned · May 19, 1995 · N12061 · Doug DC1030 · Electrical Power System Wiring
  > FLT 57 - LGW - SEVERAL C/B'S POPPED AND BOTH THE NR 1 AND NR 2 GEN'S HAD NO VOLTS AND NO FREQUENCY WHILE EN ROUTE FROM ORY TO EWR. THE CREW WAS UNABLE TO RESTORE EITHER GEN AND THE A/C WAS DIVERTED TO LGW WHERE IT LANDED W/O INCIDENT. ALL TRIPPED C/B'S WERE
- [SDR CAL950343](https://openairdocs.org/sdr/CAL950343.md): Fire Loop · damaged · Apr 24, 1995 · N12061 · Doug DC1030 · Fire Detection
  > EWR - FLT 56 - AFTER TAKEOFF. NR 3 ENGINE 'A' FIRE LIGHT AND BELL CAME ON. DUMPED FUEL AND RETURNED TO EWR. FOUND FWD PYLON DETECTION ASSY DAMAGED. REF MM 26-15-01 ITEM 117, REPLACED PART AUL7122-1 OPS. CHECK SYSTEM, ALL NORMAL. (Z)
- [SDR CAL950319](https://openairdocs.org/sdr/CAL950319.md): Loop · damaged · Apr 24, 1995 · N12061 · Doug DC1030 · Fire Detection
  > FLT NR 56 - EWR - ON TAKEOFF WARNING BELL CAME ON AIRCRAFT RETURNED TO EWR 'NO EMERGENCY DECLARED'. MAINTENANCE FOUND DAMAGE TO FIRE LOOP FWD HALF. REPAIRED AND REPLACED DAMAGED AREA AND PARTS. OPS CHECKED, SYSTEMS ALL NORMAL. AIRCRAFT DEPARTED NO FURTHER

## 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 = 'N12061' AND deregistration_id = 'N12061-2017-06-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N12061-2017-06-07/reports

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