# Service difficulty reports: N41068, cancelled Sep 24, 2002

A list on [N41068, cancelled Sep 24, 2002](https://openairdocs.org/deregistered/N41068-2002-09-24.md).

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

- [SDR CALA0000190](https://openairdocs.org/sdr/CALA0000190.md): Skin · cracked · Feb 23, 2000 · N41068 · Doug DC1030 · Leading Edge Devices
  > INSPECTION FOUND THE LEFT NR 1 SLAT I/B SKIN CRACKED. THE SLAT WAS REPLACED IAW MM 27-80-01.
- [SDR CALA9900251](https://openairdocs.org/sdr/CALA9900251.md): Frame · corroded · Mar 14, 1999 · N41068 · Doug DC1030 · Fuselage Main, Frame
  > INSPECTION FOUND CENTER CARGO DOOR APERTURE AFT FRAME AND FORWARD FRAME CORRODED AT STA 1781 AND 1701. THE FRAME AREAS WERE REPAIRED IAW SRM 53-50-00.
- [SDR CALA9900247](https://openairdocs.org/sdr/CALA9900247.md): Support · corroded · Mar 12, 1999 · N41068 · Doug DC1030 · Wing Miscellaneous Structure
  > INSPECTION FOUND LT AND RT MLG CYLINDER SUPPORT FRAME CORRODED IN ATTACHMENT BOLT HOLES. THE BOLT HOLES WERE REPAIRED IAW ECRA 5743-01015.
- [SDR CALA9900211](https://openairdocs.org/sdr/CALA9900211.md): Floorboard · corroded · Mar 3, 1999 · N41068 · Doug DC1030 · Fuselage Floor Panel
  > INSPECTION FOUND FLIGHT DECK FLOORBOARD NR 216AF DELAMINATED AND CORRODED. A NEW FLOORBOARD WAS INSTALLED AND SEALED IAW ECRA 5100-01844.
- [SDR CALA9801131](https://openairdocs.org/sdr/CALA9801131.md): Switch · inoperative · Jun 17, 1998 · N41068 · Doug DC1030 · Landing Gear Position and Warning
  > WHEN GEAR WAS RETRACTED AFTER TAKEOFF, ALL GEAR RED LIGHTS REMAINED ILLUMINATED. THE AIRCRAFT WAS RETURNED TO GIG WHERE IT LANDED WITHOUT INCIDENT. THE LANDING GEAR WAS SWUNG SEVERAL TIMES AND THE FAILURE COULD NOT BE DUPLICATED. THE AIRCRAFT HAD A BRIEF HI
- [SDR CALA9800608](https://openairdocs.org/sdr/CALA9800608.md): Fitting · corroded · Apr 1, 1998 · N41068 · Doug DC1030 · Wing, Landing Gear Attach Fittings
  > INSPECTION FOUND LT MLG FITTING ATTACHMENT TO LOWER SUPPORT DOUBLER CORRODED AROUND FASTENER HOLE AT INNER SURFACE. THE CORROSION WAS REMOVED IAW SRM 51-21-01. THE AREA WAS REPAIRED IAW ECRA 5740-01831.
- [SDR CALA9800593](https://openairdocs.org/sdr/CALA9800593.md): Longeron · corroded · Mar 26, 1998 · N41068 · Doug DC1030 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND LONGERON 48L IN CENTER CARGO BAY CORRODED AT STA 1571 TO 1711. A NEW END CAP WAS FITTED TO LONGERON AND A NEW SECTION OF LONGERON WAS SPLICED IN IAW GMM 10-900-01.
- [SDR CALA9800592](https://openairdocs.org/sdr/CALA9800592.md): Frame · cracked · Mar 26, 1998 · N41068 · Doug DC1030 · Fuselage Main, Frame
  > INSPECTION FOUND A 2 INCH CRACK IN FRAME AT STRINGER 2 STA 2140Y. A REPAIR WAS PERFORMED IAW SRM 53-30-00.
- [SDR CALA9800591](https://openairdocs.org/sdr/CALA9800591.md): Longeron · cracked · Mar 26, 1998 · N41068 · Doug DC1030 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 2 INCH CRACK IN LONGERON 36L AT FUSELAGE SKIN JOINT STA 1129. THE CRACKED SECTION OF LONGERON WAS REMOVED AND A NEW SECTION WAS FITTED IAW SRM 53-10-00.
- [SDR CALA9800590](https://openairdocs.org/sdr/CALA9800590.md): Longeron · corroded · Mar 26, 1998 · N41068 · Doug DC1030 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND LONGERON 46L CORRODED AROUND FASTENER HOLE ON END CAP AT SPLICE JOINT IN CENTER CARGO BAY AT STA 1521 TO 1571. A NEW END CAP WAS FITTED TO THE LONGERON IAW GMM 10-900-01.
- [SDR CALA9800579](https://openairdocs.org/sdr/CALA9800579.md): Longeron · corroded · Mar 23, 1998 · N41068 · Doug DC1030 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND CORROSION ON LONGERON 30L BETWEEN STA 1421 TO 1441. THE CORRODED SECTION OF LONGERON WAS REMOVED AND REPLACEMENT LONGERON AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-00, FIGURE 2.
- [SDR CALA9800414](https://openairdocs.org/sdr/CALA9800414.md): Bolts · loose · Mar 12, 1998 · N41068 · Doug DC1030 · Engine Mount Section
  > INSPECTION FOUND NR 3 ENGINE FORWARD ENGINE MOUNT TRUSS BOLTS LOOSE AT TRUSS TO PYLON BOX INTERSECTION LOWER SURFACE. THE BOLTS WERE RETORQUED IAW SERVICE BULLETIN A54-99.
- [SDR CALA9800408](https://openairdocs.org/sdr/CALA9800408.md): Support · corroded · Mar 8, 1998 · N41068 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LAV B INBOARD SUPPORT BEAM FORWARD END CORRODED. THE SUPPORT BEAM WAS REPLACED IAW GMM 10-900-01, PAGE 1.
- [SDR CALA9800407](https://openairdocs.org/sdr/CALA9800407.md): Support · corroded · Mar 8, 1998 · N41068 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LAV A INBOARD SUPPORT BEAM CORRODED. THE CORRODED BEAM WAS REMOVED, A NEW SECTION WAS FABRICATED AND INSTALLED IAW GMM 10-900-01, PAGE 1.
- [SDR CALA9800406](https://openairdocs.org/sdr/CALA9800406.md): Support · corroded · Mar 8, 1998 · N41068 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT BEAM CORRODED AT STA 420 TO 440. THE CORRODED SECTION OF FLOOR SUPPORT BEAM WAS REPLACED IAW GMM 10-900-01, PAGE 1.
- [SDR CALA9800405](https://openairdocs.org/sdr/CALA9800405.md): Support · corroded · Mar 8, 1998 · N41068 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LT FLOOR SUPPORT CHANNEL CORRODED AT STA 1887. THE FLOOR SUPPORT CHANNEL WAS REPLACED IAW GMM 10-900-01.
- [SDR CALA9800369](https://openairdocs.org/sdr/CALA9800369.md): Floorbeam · corroded · Feb 28, 1998 · N41068 · Doug DC1030 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOOR SUPPORT BEAM CORRODED AT L-1 DOOR, STA 442. THE CORRODED SECTION OF BEAM WAS REPLACED IAW GMM 10-900-01, PAGE 1.
- [SDR CALA9800368](https://openairdocs.org/sdr/CALA9800368.md): Floorbeam · corroded · Feb 28, 1998 · N41068 · Doug DC1030 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 450 FROM CENTERLINE TO 24 RIGHT OF CENTERLINE. THE CORRODED SECTION OF FLOORBEAM WAS REPLACED IAW GMM 10-900-01, PAGE 1.
- [SDR CALA9800348](https://openairdocs.org/sdr/CALA9800348.md): Doubler · cracked · Feb 27, 1998 · N41068 · Doug DC1030 · Wing Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN LT LOWER LEADING EDGE STRINGER DOUBLER AT STA XORS 827. REPAIRED IAW SRM 57-10-00, FIGURE 49.
- [SDR CALA9700972](https://openairdocs.org/sdr/CALA9700972.md): Hyd Pump · leaking · Jun 26, 1997 · N41068 · Doug DC1030 · Hydraulic Pump (Electric/Engine), Main
  > THE NR 1 HYDRAULIC SYSTEM FLUID QUANTITY DROPPED STEADILY DURING FLIGHT TO EWR. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 LT ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE HYDRAULIC PUMP WAS REMOVED AND REPLACED. THE HYDRAULIC SYST
- [SDR CAL960071](https://openairdocs.org/sdr/CAL960071.md): Hpc Blade · damage · Jan 29, 1996 · N41068 · Doug DC1030 · Turbine Engine Compressor Section
  > FLT NR 56 - EWR - THE NR 2 ENGINE FAILED ON TAKEOFF FROM EWR. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WAS REMOVED AND REPLACED. INVESTIGATION REVEALED THAT THE PRIMARY CAUSE OF ENGINE FAILURE WA
- [SDR CAL960220](https://openairdocs.org/sdr/CAL960220.md): Stringer · corroded · Dec 12, 1995 · N41068 · Doug DC1030 · Fuselage Main, Longeron/Stringer
  > KUL - INSPECTION FOUND CORROSION ON STRINGER 30R AT STATION 1501. THE STRINGER WAS REPAIRED IAW SRM 53-10-00. (M)
- [SDR CAL960222](https://openairdocs.org/sdr/CAL960222.md): Support · corroded · Nov 8, 1995 · N41068 · Doug DC1030 · Fuselage Miscellaneous Structure
  > KUL - INSPECTION FOUND THE FLOOR BOARD SUPPORT CHANNEL CORRODED AT AFT SIDE BETWEEN G6 AND G7 AISLE. THE SUPPORT WAS REPLACED IAW SRM 53-16-01, FIGURE 10, SHEET 2, ITEM 6. (M)
- [SDR CAL960221](https://openairdocs.org/sdr/CAL960221.md): Skin · warped · Nov 1, 1995 · N41068 · Doug DC1030 · Horizontal Stabilizer, Plate/Skin
  > KUL - INSPECTION FOUND THE RIGHT OUTBOARD ELEVATOR UPPER SKIN WARPED. THE SKIN WAS REPAIRED IAW SRM 55-10-00, PAGE 15, FIGURE 8. (M)
- [SDR CAL960223](https://openairdocs.org/sdr/CAL960223.md): Support · corroded · Oct 28, 1995 · N41068 · Doug DC1030 · Fuselage Miscellaneous Structure
  > KUL - INSPECTION FOUND FLOOR BOARD SUPPORT CORRODED AT STATION 1887. THE SUPPORT WAS REPLACED IAW SRM 53-16-01, FIGURE 10, ITEM 6. (M)
- [SDR CAL960224](https://openairdocs.org/sdr/CAL960224.md): Attachment · cracked · Oct 14, 1995 · N41068 · Doug DC1030 · Fuselage Miscellaneous Structure
  > KUL - INSPECTION FOUND A 2 INCH CRACK IN STATION 1967 FRAME ATTACHMENT TO STRINGER 51R. A REPAIR WAS CARRIED OUT IAW SRM 53-16-01, FIGURE 17, ITEM 42G. (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 = 'N41068' AND deregistration_id = 'N41068-2002-09-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N41068-2002-09-24/reports

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