# Service difficulty reports: N68042, cancelled Feb 13, 2013

A list on [N68042, cancelled Feb 13, 2013](https://openairdocs.org/deregistered/N68042-2013-02-13.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 · 51 reports

- [SDR RRXA011039](https://openairdocs.org/sdr/RRXA011039.md): Proximity Sensor · malfunctioned · Apr 24, 2001 · N68042 · Doug DC1010F · Landing Gear Position and Warning
  > LEFT LANDING GEAR RED LIGHT ON WITH GEAR HANDLE UP. REMOVED AND REPLACED PROXIMITY BOX IAW M/M 32-61-01. OPS CKS NORMAL.
- [SDR RRXA011036](https://openairdocs.org/sdr/RRXA011036.md): Skin · corroded · Apr 18, 2001 · N68042 · Doug DC1010F · Fuselage Main, Plate/Skin
  > ON WALKAROUND FOUND CORROSION ON UNDER SIDE OF FUSELAGE, LOCATED APPROX 18 INCHES LEFT OF CENTER ACCESSORY COMPARTMENT ACCESS DOOR. REPAIRED DAMAGED AREA PER EWA EO M0419011 & MO420011, NOTE: THIS REPAIR IS A CLASS III TEMPORARY TYPE WITH VISUAL INSP EVERY 1
- [SDR RRXA010007](https://openairdocs.org/sdr/RRXA010007.md): Mount · corroded · Feb 6, 2001 · N68042 · Doug DC1010F · Engine Mount Section
  > NR 1 ENG AFT PYLON AFT MOUNT SUPPORT CORRODED AND DOWL PINS ARE LOOSE. REMOVED AND REPLACED NR 1 ENGINE AFT MOUNT AS REQUIRED IAW DC-10 M/M 71-20-00, TORQUED ENGINE MOUNT IAW DC-10 M/M 20-50-02. OPS CHECK GOOD.
- [SDR RRXA001053](https://openairdocs.org/sdr/RRXA001053.md): Warning System · activated · Sep 1, 2000 · N68042 · Doug DC1010F · Leading Edge Slat Position Indicating System
  > WHEN EXTENDING FLAPS FOR LANDING, SLAT DISAGREE LIGHT ILLUMINATED. PERFORMED APPROPRIATE ABNORMAL CK LISTS, LANDED KDFW. OPERATED FLAPS/SLATS PER DC-10 MM 27-80-00 PG 538 THRU 542. ALL OPS CHECK NORMAL. VISUALLY CHECKED SLATS FOR DAMAGE AND OPS, NO DEFECTS
- [SDR RRXA11057](https://openairdocs.org/sdr/RRXA11057.md): Angle · corroded · Jul 29, 2000 · N68042 · Doug DC1010F · Fuselage Main, Bulkhead
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO CENTER PIT ANGLES AT STA 174, DAMAGE EXCEEDED LIMITATIONS IAW DC-10 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-21-01. FABRICATED PART AND INSTALLED IAW DC-10 SRM 51-35-01, 51-10-00.
- [SDR RRXA10692](https://openairdocs.org/sdr/RRXA10692.md): Skin · cracked · Jul 28, 2000 · N68042 · Doug DC1010F · Fuselage Main, Plate/Skin
  > DURING MAINTENANCE VISIT FOUND CRACK DAMAGE TO RT FUSELAGE SKIN AT STA 1154 - 1160. DAMAGE EXCEEDED LIMITATIONS IAW DC-10 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-10 SRM 51-21-01. FABRICATED REPAIR AND INSTALLED IAW DC-10 EA 10-5331-22-A07A1.
- [SDR RRXA11054](https://openairdocs.org/sdr/RRXA11054.md): Fitting · corroded · Jul 24, 2000 · N68042 · Doug DC1010F · Fuselage Floor Panel
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO CENTER PIT JAM AFT OMNI ROLER FITTING AT STA 1761 AND X=-70, DAMAGE EXCEEDED LIMITATIONS IAW DC-10 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-21-01. RECEIVED PART AND INSTA
- [SDR RRXA11053](https://openairdocs.org/sdr/RRXA11053.md): Web · corroded · Jul 24, 2000 · N68042 · Doug DC1010F · Fuselage Main, Bulkhead
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO CENTER PIT TOURQE BOX WEB AT STA 1721 AND X=-70, DAMAGE EXCEEDED LIMITATIONS IAW DC-10 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-21-01. FABRICATED PART AND INSTALLED IAW D
- [SDR RRXA11058](https://openairdocs.org/sdr/RRXA11058.md): Channel · corroded · Jul 22, 2000 · N68042 · Doug DC1010F · Fuselage Main, Bulkhead
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO CENTER PIT AFT LOAD RESTRAINT BLOCK CHANNEL AT STA 1781 AND X= -25, DAMAGE EXCEEDED LIMITATIONS IAW DC-10 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-21-01. FABRICATED PART
- [SDR RRXA11062](https://openairdocs.org/sdr/RRXA11062.md): Support · corroded · Jul 21, 2000 · N68042 · Doug DC1010F · Fuselage Main, Bulkhead
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO CENTER PIT FLOOR PANEL SUPPORT AT STA 1701 AND X= -21, DAMAGE EXCEEDED LIMITATIONS IAW DC-10 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-21-01. FABRICATED PART AND INSTALLED
- [SDR RRXA11059](https://openairdocs.org/sdr/RRXA11059.md): Plate · corroded · Jul 21, 2000 · N68042 · Doug DC1010F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO CENTER PIT ROLLER TRAY ATTACH PLATE AT STA 1701 AND BL=0, DAMAGE EXCEEDED LIMITATIONS IAW DC-10 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-21-01. FABRICATED PART AND INSTALLED IAW DC-10 SRM 51-31-4.
- [SDR RRXA11061](https://openairdocs.org/sdr/RRXA11061.md): Roller Tray · corroded · Jul 18, 2000 · N68042 · Doug DC1010F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO CENTER PIT CENTER LINE ROLLER TRAY AT STA 1601-1701 AND X=2 TO X= -2, DAMAGE EXCEEDED LIMITATIONS IAW DC-10 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-21-01. FABRICATED PART AND INSTALLED IAW DC-10 SR
- [SDR RRXA11060](https://openairdocs.org/sdr/RRXA11060.md): Structure · corroded · Jul 16, 2000 · N68042 · Doug DC1010F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FWD PIT SIDE RAIL AT STA760 AND X=60, DAMAGE EXCEEDED LIMITATIONS IAW DC-10 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-21-01.FABRICATED PART AND INSTALLED IAW DC-10 SRM 57-31-01.
- [SDR RRXA10691](https://openairdocs.org/sdr/RRXA10691.md): Structure · damaged · Jul 13, 2000 · N68042 · Doug DC1010F · Fuselage Miscellaneous Structure
  > DURING MAINTENANCE VISIT FOUND INTERIM DAMAGE TO STA 1156 AND L39L, DAMAGE EXCEEDED LIMITATIONS IAW DC-10 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-10 SRM 51-21-01. RECEIVED PART AND INSTALLED IAW DC-10 EO DM-5312-01-00.
- [SDR RRXA10690](https://openairdocs.org/sdr/RRXA10690.md): Mount · corroded · Jul 10, 2000 · N68042 · Doug DC1010F · Nacelle/Pylon, Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMANGE TO NR 3 ENGINE PYLON AFT MOUNT, DAMAGE EXCEEDED LIMITATIONS IAW DC-10 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-10 SRM 51-21-01. RECEIVED PART AND INSTALLED IAW DC-10 SRM 20-50-02. (CORROSION DAMAGE RECORDED
- [SDR RRXA11052](https://openairdocs.org/sdr/RRXA11052.md): Door · corroded · Jul 7, 2000 · N68042 · Doug DC1010F · Wing, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SKIN ON PANEL #518CB AT XORS372 AND X=-400, DAMAGE EXCEEDED LIMITATIONS IAW DC-10 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-10 SRM 51-21-01. FABRICATED PART AND INSTALLED IAW DC-10
- [SDR RRXA11063](https://openairdocs.org/sdr/RRXA11063.md): Fastener · corroded · Jul 6, 2000 · N68042 · Doug DC1010F · Nacelle/Pylon, Main Frame
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO NR 2 ENGINE LEFT CORE COWL, FWD HINGE MOUNT 4EA FASTNERS, DAMAGE EXCEEDED LIMITATIONS IAW DC-10 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-21-01. RECEIVED PART AND INSTALLED 4EA FASTNERS IAW DC-10 SRM
- [SDR RRXA10689](https://openairdocs.org/sdr/RRXA10689.md): Sill · corroded · Jul 6, 2000 · N68042 · Doug DC1010F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FWD CARGO COMPARTMENT LOWER DOOR SILL TRAY AT STA 939 AND L43R, DAMAGE EXCEEDED LIMITATIONS IAW DC-10 SRM. TREATED AREA IAW DC-10 SRM 51-21-01. RECEIVED PART AND INSTALLED IAW DC-10 SRM 51-31-01. (CORROSI
- [SDR RRXA10688](https://openairdocs.org/sdr/RRXA10688.md): Spar · corroded · Jul 6, 2000 · N68042 · Doug DC1010F · Wing Spar
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON THE LEFT HAND WHEEL WELL BETWEEN TRAPEZOID AND REAR SPAR OF CENTER WING ON INBOARD AND OUTBOARD LEGS AT STA 1392 AND LBL 118.2, DAMAGE EXCEEDED LIMITATIONS IAW DC-10 SRM. REMOVED DAMAGE, TREATED AREA IAW DC
- [SDR RRXA11056](https://openairdocs.org/sdr/RRXA11056.md): Bushing · corroded · Jul 5, 2000 · N68042 · Doug DC1010F · Fuselage Main, Bulkhead
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO #3 A/C DOOR HANDLE TOURQE TUBE BUSHINGS AT STA 500, DAMAGE EXCEEDED LIMITATIONS IAW DC-10 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-21-01.RECEIVED PART AND INSTALLED IAW D
- [SDR RRXA11051](https://openairdocs.org/sdr/RRXA11051.md): Skin · corroded · Jul 5, 2000 · N68042 · Doug DC1010F · Trailing Edge Flaps
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RT WING NR 1 SLAT TRACK ATTACH FITTING AT STA XIS285, DAMAGE EXCEEDED LIMITATIONS IAW DC-10 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-10. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-10-00 FIG 31.
- [SDR RRXA11055](https://openairdocs.org/sdr/RRXA11055.md): Angle · corroded · Jul 4, 2000 · N68042 · Doug DC1010F · Fuselage Main, Bulkhead
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FWD CARGO FLOOR SUPPORT ANGLE AT STA 905-910 AND X=48, DAMAGE EXCEEDED LIMITATIONS IAW DC-10 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-21-01. FABRICATED REPAIR AND INSTALL
- [SDR RRXA001004](https://openairdocs.org/sdr/RRXA001004.md): Coalescer Bag · dirty · Jun 22, 2000 · N68042 · Doug DC1010F · Humidity Control System
  > AFTER TAKEOFF, WHEN NR 1 PACK IS TURNED ON WITH NR 1 ENG PANEL SUPPLING AIR, EXPERIENCED BURNING SMELL. TURNED PACK OFF FOR REMAINDER OF FLT. OPERATED WITH NR 2 & 3 PACK. OCCURRED WITH PACK NR 1 IN AUTO + MIX IN FULL HOT ON GROUND WITH PACK NR 1 IN MAN FULL
- [SDR CALA9701709](https://openairdocs.org/sdr/CALA9701709.md): Prox Unit · inoperative · Dec 3, 1997 · N68042 · Doug DC1010 · Landing Gear Position and Warning
  > THE AIRCRAFT RETURNED TO NGO A SECOND TIME FOR THE SAME PROBLEM. THE RED MLG LIGHTS ILLUMINATED WITH TAKEOFF WARNING HORN ACTIVATING AFTER GEAR RETRACTION ON TAKEOFF. THE GEAR WAS CYCLED, BUT THE WARNINGS REPEATED. MAINTENANCE CHECKED RESISTANCE OF PROXIMIT
- [SDR CALA9700726](https://openairdocs.org/sdr/CALA9700726.md): Intercostal · corroded · May 9, 1997 · N68042 · Doug DC1010 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CORROSION ON AFT WASTE TANK INTERCOSTAL AT STA 1964 TO 1975, STRINGER 47L TO 48L. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-00-01.
- [SDR CALA9700725](https://openairdocs.org/sdr/CALA9700725.md): Support · corroded · May 9, 1997 · N68042 · Doug DC1010 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SUPPORT CORRODED IN AFT CARGO COMPARTMENT AT STA 1785, LBL 30 TO LBL 40. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-00-01.
- [SDR CALA9700724](https://openairdocs.org/sdr/CALA9700724.md): Support · corroded · May 9, 1997 · N68042 · Doug DC1010 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SUPPORT CORRODED IN AFT CARGO COMPARTMENT AT STA 1780, RBL 20 TO RBL 30. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-00-01.
- [SDR CALA9700723](https://openairdocs.org/sdr/CALA9700723.md): Angle · corroded · May 9, 1997 · N68042 · Doug DC1010 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CORROSION ON ANGLE IN CENTER CARGO COMPARTMENT AT STA 1701, LBL 40 TO LBL 55. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-15-01.
- [SDR CALA9700722](https://openairdocs.org/sdr/CALA9700722.md): Floorbeam · corroded · May 9, 1997 · N68042 · Doug DC1010 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED IN CENTER CARGO COMPARTMENT AT STA 1701. REPAIRED IAW SRM 53-60-01, FIGURE 2.
- [SDR CALA9700721](https://openairdocs.org/sdr/CALA9700721.md): Support · corroded · May 9, 1997 · N68042 · Doug DC1010 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED IN CENTER CARGO COMPARTMENT AT STA 1781, RBL 45 TO LBL 20. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-15-01, FIGURE 14A, ITEM 22.
- [SDR CALA9700729](https://openairdocs.org/sdr/CALA9700729.md): Flange · corroded · Apr 16, 1997 · N68042 · Doug DC1010 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CORROSION ON LOWER FLANGE IN AFT CARGO COMPARTMENT AT STA 1785, STRINGER 49-48L. A NEW LOWER FLANGE WAS FABRICATED AND INSTALLED IAW SRM 53-00-01 AND 51-35-01.
- [SDR CALA9700728](https://openairdocs.org/sdr/CALA9700728.md): Intercostal · corroded · Apr 16, 1997 · N68042 · Doug DC1010 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND INTERCOSTAL CORRODED IN AFT CARGO COMPARTMENT AT STA 1780 TO 1785, STRINGER 44L. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-00-01 AND 51-33-01.
- [SDR CALA9700741](https://openairdocs.org/sdr/CALA9700741.md): Web · cracked · Apr 14, 1997 · N68042 · Doug DC1010 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 7.5 INCH CRACK IN NLG WHEEL WELL LT WALL WEB AT STA 580, 15 INCHES FROM AFT BULKHEAD AND 7 INCHES FROM LOWER HORIZONTAL PRESSURE PANEL. A 4.75 INCH CRACK WAS FOUND IN NLG WHEEL WELL RT WALL WEB AT STA 580, 15 INCHES FROM AFT BULKHEAD AND 3.
- [SDR CALA9700727](https://openairdocs.org/sdr/CALA9700727.md): Skin · corroded · Apr 13, 1997 · N68042 · Doug DC1010 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN CORRODED BETWEEN STA 715 AND 725 AT STRINGER 13L. THE CORRODED AREA WAS REMOVED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-00-01 AND 51-33-01.
- [SDR CALA9700490](https://openairdocs.org/sdr/CALA9700490.md): Smoke Detector · inoperative · Apr 6, 1997 · N68042 · Doug DC1010 · Smoke Detection
  > THE NR 4 SMOKE DETECTOR LIGHT AND CARGO FIRE LIGHT ILLUMINATED WHILE ON APPROACH TO OSA. THE NR 1 CARGO FIRE EXTINGUISHER WAS DISCHARGED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE NR 4 SMOKE DETECTOR WAS REMOVED AN
- [SDR CALA9700189](https://openairdocs.org/sdr/CALA9700189.md): Connector · dirty · Feb 18, 1997 · N68042 · Doug DC1010 · Fire Detection
  > THE NR 1 ENGINE B-FIRELOOP LIGHT FLICKERED DURING CLIMBOUT AND THEN STOPPED. FIRE TEST WAS GOOD. THE NR 2 ENGINE A-FIRELOOP DID NOT TEST. THE NR 2 ENGINE B-LOOP WAS ON PLACARD. THE NR 1 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS DIVERTED TO OSA WHERE IT LAND
- [SDR CALA9700129](https://openairdocs.org/sdr/CALA9700129.md): Manifold · cracked · Feb 2, 1997 · N68042 · Doug DC1010 · Engine Cooling System
  > THE NR 1 START LEVER LIGHT AND MASTER WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL. TAKEOFF WAS ABORTED AT 25 TO 30 KNOTS AND THE AIRCRAFT WAS RETURNED TO GATE. MAINTENANCE FOUND THE NR 1 ENGINE LOW PRESSURE TURBINE COOLING AIR MANIFOLD CRACKED. THE MANIFO
- [SDR CALA9601315](https://openairdocs.org/sdr/CALA9601315.md): Prox Control · inoperative · Sep 15, 1996 · N68042 · Doug DC1010 · Landing Gear Position and Warning
  > THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION ON APPROACH. ALTERNATE GEAR EXTENSION WAS USED AND GEAR WAS DOWN AND LOCKED. THE AIRCRAFT LANDED AT KIX WITHOUT INCIDENT. MAINTENANCE RESEATED THE PROXIMITY CONTROL UNIT, GEAR INDICATIONS CHE
- [SDR CALA9601254](https://openairdocs.org/sdr/CALA9601254.md): Spring · broken · Sep 2, 1996 · N68042 · Doug DC1010 · Landing Gear Door Retract Section
  > THE LT MLG RED LIGHT CAME ILLUMINATED DURING CRUISE AFTER ACCELERATING TO 300 KNOTS. THE LIGHT EXTINGUISHED BELOW 240 KNOTS WHILE ON DESCENT DURING RETURN TO GUM. MAINTENANCE FOUND THE LEFT GEAR DOOR EXTENSION SPRING ON LEVER BROKEN. THE SPRING WAS REPLACED
- [SDR CALA9600657](https://openairdocs.org/sdr/CALA9600657.md): Charger · inoperative · May 11, 1996 · N68042 · Doug DC1010 · Emergency Lighting
  > THE EMERGENCY LIGHT TEST IN COCKPIT FAILED TO TEST DURING C-CHECK. THE FAULT ISOLATION PANEL INDICATED MID-POWER PACK FAILURE. THE EMERGENCY LIGHT CHARGER WAS REMOVED AND REPLACED AND EMERGENCY LIGHT TEST CHECKED GOOD.
- [SDR CALA9600669](https://openairdocs.org/sdr/CALA9600669.md): Frame · corroded · Apr 24, 1996 · N68042 · Doug DC1010 · Fuselage Main, Frame
  > INSPECTION FOUND FORWARD CARGO FRAME CORRODED IN CHANNEL AT BASE OF FRAME, STA 879. THE FRAME WAS REPAIRED IAW ECRA 5310-03264.
- [SDR CALA9600668](https://openairdocs.org/sdr/CALA9600668.md): Support · corroded · Apr 24, 1996 · N68042 · Doug DC1010 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOORBOARD SUPPORT CORRODED THROUGH AT STA 1911, LAV H AND J. THE FLOORBOARD SUPPORTS WERE REMOVED AND REPLACED IAW SRM 53-16-01, FIGURE 5F.
- [SDR CALA9600656](https://openairdocs.org/sdr/CALA9600656.md): Frame · corroded · Apr 24, 1996 · N68042 · Doug DC1010 · Fuselage Main, Frame
  > INSPECTION FOUND THE FORWARD INTERMEDIATE FUSELAGE FRAME CAP CORRODED AT STA 899, LONGERON 51L AND 50R; STA 959, LONGERON S50L AND 50R; AND STA 1019, LONGERON 49L AND 51L. REPAIRS WERE PERFORMED IAW ECRA 5310-03264.
- [SDR CALA9600655](https://openairdocs.org/sdr/CALA9600655.md): Doubler · corroded · Apr 23, 1996 · N68042 · Doug DC1010 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND THE FORWARD SKIN DOUBLER AT STA 959 TO 979, LONGERONS 47R AND 46R CORRODED. THE SKIN DOUBLER WAS REPAIRED IAW ECRA 5330-02397.
- [SDR CALA9600654](https://openairdocs.org/sdr/CALA9600654.md): Beam · corroded · Apr 23, 1996 · N68042 · Doug DC1010 · Wing Miscellaneous Structure
  > INSPECTION FOUND THE LT WING UPPER CAP TRAILING EDGE BEAM CORRODED. THE BEAM WAS REPAIRED IAW ECRA 5720-01518.
- [SDR CALA9600653](https://openairdocs.org/sdr/CALA9600653.md): Frame Cap · corroded · Apr 23, 1996 · N68042 · Doug DC1010 · Fuselage Main, Frame
  > INSPECTION FOUND THE AFT INTERMEDIATE FUSELAGE FRAME CAP CORRODED AT STA 1701. THE AREA WAS REPAIRED IAW ECRA 5310-03265.
- [SDR CALA9600652](https://openairdocs.org/sdr/CALA9600652.md): Shear Clip · corroded · Apr 23, 1996 · N68042 · Doug DC1010 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SHEAR CLIPS CORRODED AT STA 1099, LONGERON 47L TO 49L AND LONGERON 51L TO 52L. REPAIR WAS PERFORMED IAW ECRA 5310-03268.
- [SDR CALA9600670](https://openairdocs.org/sdr/CALA9600670.md): Support · corroded · Apr 22, 1996 · N68042 · Doug DC1010 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT BEAM CORRODED AT FORWARD CARGO DOOR FORWARD JAMB. THE FLOOR SUPPORT BEAM WAS REPLACED IAW SRM 53-13-01 FIGURE 7 ITEM 6.
- [SDR CAL960275](https://openairdocs.org/sdr/CAL960275.md): Relief Valve · sticking · Mar 4, 1996 · N68042 · Doug DC1010 · Hydraulic Pressure Relief Valve, Main
  > FLT NR 973 - NGO - THE A/C PITCHED DOWN SLIGHTLY DURING APPROACH TO NGO. THE OUT OF TRIM LIGHT FLASHED AND THEN THE HYDRAULIC SYSTEM 3 ELEVATOR OFF LIGHT ILLUMINATED. THE SYSTEM NR 3 HYDRAULIC QUANTITY GAUGE READ DOWN.5 GALLON. THE AIRCRAFT LANDED WITHOUT
- [SDR CAL960058](https://openairdocs.org/sdr/CAL960058.md): Clamp · worn · Jan 23, 1996 · N68042 · Doug DC1010 · Pneumatic Distribution System
  > GUM - FLT 0977 - NR 2 ENGINE A-FIRE LOOP LIGHT ILLUMINATED DURING CLIMB OUT OF GUM WITH B-LOOP ON PLACARD. THE B-LOOP HAD BEEN PLACARDED PREVIOUSLY FOR BEING INTERMITTENLY INOPERABLE. LATER, BOTH LOOP LIGHTS AND FIRE LIGHT WERE ON. ENGINE POWER REDUCED AND

Next page: https://openairdocs.org/deregistered/N68042-2013-02-13/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 = 'N68042' AND deregistration_id = 'N68042-2013-02-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N68042-2013-02-13/reports

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