# Service difficulty reports: N68051, cancelled Feb 1, 2024

A list on [N68051, cancelled Feb 1, 2024](https://openairdocs.org/deregistered/N68051-2024-02-01.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 4 · 174 reports

- [SDR FDEA201506071715](https://openairdocs.org/sdr/FDEA201506071715.md): Tire · vibration · Jun 7, 2015 · N68051 · Doug MD1010F · Tire
  > SEVERE NOSE WHEEL VIBRATION AT ROTATION THAT CARRIED INTO THE WW AFTER GEAR RETRACTION. EMERGENCY DECLARED, NORMAL GEAR EXTENSION & TOUCHDOWN. NO ABNORMAL INDICATIONS WITH LANDING ROLLOUT. ACCOMPLISHED DVI FOR FLAT SPOTS ON TIRES, TORQUE LINKS, STEERING CO
- [SDR FDEA201502050457](https://openairdocs.org/sdr/FDEA201502050457.md): Control Latch · dirty · Feb 5, 2015 · N68051 · Doug MD1010F · Landing Gear Selector
  > ON FINAL APPROACH WITH GEAR HANDLE DOWN, HAD GEAR UNSAFE INDICATION ON GEAR LIGHTS & SYNOPTIC. DID NOT TURN GREEN TILL ON GO AROUND. FOUND LG CONTROL LEVER STICKING. CLEANED & LUBRICATED CONTROL LEVER. CONTROL LEVER MOVES FREELY & ALL GEAR INDICATIONS INDI
- [SDR FDEA201501030015](https://openairdocs.org/sdr/FDEA201501030015.md): Indicator · faulty · Jan 3, 2015 · N68051 · Doug MD1010F · Emergency Equipment
  > L1 DOOR SLIDE LIGHT WILL NOT TEST. REPLACED BATTERIES & BULBS, NO HELP. SUSPECT LIGHT ASSEMBLY. R & R REMOTE SLIDE PACK PRESS INDICATOR AS REQUIRED. GND CHECKED NORMAL IAW AMM 25-61-03.
- [SDR FDEA201403080460](https://openairdocs.org/sdr/FDEA201403080460.md): Target · sheared · Mar 8, 2014 · N68051 · Doug MD1010F · Landing Gear Position and Warning
  > AFTER GEAR WAS EXTENDED THE RT GEAR INDICATED UNSAFE ON BOTH PRIMARY NS SECONDARY SYSTEMS. ON LOW APPROACH TOWER OBSERVED GEAR APPEARED DOWN. COMPLIED WITH THE QRH & LANDED WITHOUT INCIDENT. UPON INSPECTION OF RT GEAR, FOUND TARGET SENSOR PLATE SHEARED FROM
- [SDR FDEA201311022668](https://openairdocs.org/sdr/FDEA201311022668.md): Light · inoperative · Nov 2, 2013 · N68051 · Doug MD1010F · Emergency Equipment
  > R1 DOOR DISARM LIGHT INOPERATIVE. REMOVED AND REPLACED R1 DISARMED INDICATOR LIGHT ASSY IAW AMM 20-30-08-2 AND SMP. OPS CHECKED NORMAL.
- [SDR FDEA201307111545](https://openairdocs.org/sdr/FDEA201307111545.md): Spar · cracked · Jul 11, 2013 · N68051 · Doug MD1010F · Wing Spar
  > RIGHT WING REAR LOWER SPAR HAS A CRACK AT XORS 402-452. REPAIRED IAW EA 8-5710-T03001500.
- [SDR FDEA201307111544](https://openairdocs.org/sdr/FDEA201307111544.md): Skin · cracked · Jul 11, 2013 · N68051 · Doug MD1010F · Wing, Plate/Skin
  > RIGHT WING SKIN CRACKED, MIGRATING AT XORS 348 FWD OF INBD AILERON. REPAIRED IAW EA 8-5710-T0301500.
- [SDR FDEA201307111542](https://openairdocs.org/sdr/FDEA201307111542.md): Bulkhead · cracked · Jul 11, 2013 · N68051 · Doug MD1010F · Fuselage Main, Bulkhead
  > CAC AFT PRESSURE BULKHEAD ABOVE SYSTEM NR 2 DUCT HAS A APPROX 15 INCH CRACK. REPAIRED IAW EA 8-5310-T-0301508.
- [SDR FDEA201211254154](https://openairdocs.org/sdr/FDEA201211254154.md): Charger · inoperative · Nov 25, 2012 · N68051 · Doug MD1010F · Battery/Charger System
  > BATTERY CHARGER INOPERATIVE MESSAGE DISPLAYED, EMERGENCY POWER TEST FAILED AS WELL. TROUBLESHOT IAW MM 24-30-00-0-2. BATTERY CHARGER FAILED. R & R BATTERY CHARGER UNIT IAW MM 24-30-00-0-2 & PERFORMED SATISFACTORY OPS CHECK. EMERGENCY POWER TEST SATISFACTO
- [SDR FDEA201207232882](https://openairdocs.org/sdr/FDEA201207232882.md): Structure · cracked · Jul 23, 2012 · N68051 · Doug MD1010F · Fuselage Miscellaneous Structure
  > CRACK ON INBD SIDEWALL 30 INCHES FWD OF BS 1521 AND 20 INCHES DOWN FROM UPPER BULKHEAD. REPAIRED IAW EA 8-5310-157357.
- [SDR FDEA201207232881](https://openairdocs.org/sdr/FDEA201207232881.md): Bulkhead · cracked · Jul 23, 2012 · N68051 · Doug MD1010F · Fuselage Main, Bulkhead
  > LT MLG WW SIDEWALL CRACKED 20 INCHES AFT OF BS 1381 AND 7 INCHES DOWN AND A CRACK 17 INCHES AFT OF 1381 5.5 INCHES DOWN. REPAIRED CRACK REF EA 8-5310-157358, REV B.
- [SDR FDEA201207232880](https://openairdocs.org/sdr/FDEA201207232880.md): Skin · cracked · Jul 23, 2012 · N68051 · Doug MD1010F · Fuselage Main, Plate/Skin
  > AFT UPPER CORNER OF NR 2 ACM EXHAUST CRACKED. REPAIRED CORNER ACM EXHAUST AS REQUIRED IAW SRM 53-20-00, FIG 2.
- [SDR FDEA201207232879](https://openairdocs.org/sdr/FDEA201207232879.md): Skin · cracked · Jul 23, 2012 · N68051 · Doug MD1010F · Fuselage Main, Plate/Skin
  > AFT UPPER CORNER OF NR 1 ACM EXHAUST CRACKED. INSTALLED DOUBLER AND TRIPLER ON AFT UPPER COUNER OF NR 1 ACM EXHAUST USING SRM 53-20-00 AS A REF.
- [SDR FDEA201207232878](https://openairdocs.org/sdr/FDEA201207232878.md): Bulkhead · cracked · Jul 23, 2012 · N68051 · Doug MD1010F · Fuselage Main, Bulkhead
  > LEFT FWD CORNER OF NOSE WW CRACKED. REPAIRED CRACK AND INSTALLED DOUBLERS IAW SRM VOL I 53-50-00, FIG 25.
- [SDR FDEA201108123248](https://openairdocs.org/sdr/FDEA201108123248.md): Spar · damaged · Aug 12, 2011 · N68051 · Doug MD1010F · Wing Spar
  > WHILE ACCOMPLISHING EO 8-5710-7-5007, PT 2 MISDRILLED HOLE WHILE REMOVING FASTENERS. REPAIRED MISDRILLED HOLES BY REWORKING IAW EA 8-5710 -150976. MAJOR REPAIR.
- [SDR FDEA201108083140](https://openairdocs.org/sdr/FDEA201108083140.md): Floor Support · corroded · Aug 8, 2011 · N68051 · Doug MD1010F · Fuselage Miscellaneous Structure
  > CTR CARGO FLOOR SUPPORT AT STA 1521 Y "0" HAS CORROSION. REMOVED ROLLER TRAY FOR ACCESS. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 1B. FABRICATED REPAIR ANGLES AND FILLER. INSTALLED REPAIR PARTS IAW SRM 53-00-1 FIG 7, SHEET 3, INSTA
- [SDR FDEA201108023078](https://openairdocs.org/sdr/FDEA201108023078.md): Intercostal · cracked · Aug 2, 2011 · N68051 · Doug MD1010F · Fuselage Miscellaneous Structure
  > AFT CARGO BILGE AREA BETWEEN STA 1964 AND STA 1975 AND FROM LONGERON 48 - 47R INTERCOASTAL WEB HAS A CRACK. R & R INTERCOSTAL IAW SRM 51-31-01 AND REPAIRED PARTS. FABRICATED IAW SRM 53-16-01, REPAIR IS CLASSIFIED AS MAJOR.
- [SDR FDEA201108013056](https://openairdocs.org/sdr/FDEA201108013056.md): Seat Track · corroded · Aug 1, 2011 · N68051 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CARGO SEAT TRACK 8R, F.S 879 TO 940, TRACK CORRODED BELOW LOBES BLENDED OUT CORROSION IAW SRM 53-70-00, FIG 5, MAT LOSS.023. OUT OF LIMITS. CUT OUT AND REPLACED DISCREPANT SECTION OF SEAT TRACK IAW SRM 53-70-01, FIG 1, SRM 51-31-01.
- [SDR FDEA201108013055](https://openairdocs.org/sdr/FDEA201108013055.md): Skin · dented · Aug 1, 2011 · N68051 · Doug MD1010F · Trailing Edge Flaps
  > LT INBD FLAP LOWER SURFACE HAS MULTIPLE DENTS FROM INBD END TO OTBD END. DENT LOCATED 28" FROM L/E AND 82" FROM INBD EDGE, D= O.150", DIA= 10.0" FOUND OUT OF LIMITS IAW SRM 57-10-00, FIG. 48, REPAIRED AREA IAW SRM 57-10-00, FIG 4, REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201107242928](https://openairdocs.org/sdr/FDEA201107242928.md): Floorbeam · corroded · Jul 24, 2011 · N68051 · Doug MD1010F · Fuselage Main, Floor Beam
  > AFT CARGO FLOORBEAM AT STA 1901, RBL 13 UPPER FLANGE HAS CORROSION. REMOVED AND REPLACED SUPPORT ANGLE, REPAIR SPLICE AND REINSTALLED EXISTING STIFFNER IAW SRM 51-31-01, PARTS FABRICATED PER SRM 53-00-01, REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201107242927](https://openairdocs.org/sdr/FDEA201107242927.md): Floorbeam · corroded · Jul 24, 2011 · N68051 · Doug MD1010F · Fuselage Main, Floor Beam
  > AFT CARGO FLOORBEAM AT STA 1901, LBL 40 TOP AND BOTTOM SURFACE HAS CORROSION. REMOVED CORROSION. ORIG MAT.063. MAT LOSS IS.031. FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 1B. FABRICATED FILLER AND REPAIR ANGLE. REPAIRED AFT CARGO FLOORBEAM IAW SRM 53-00-010 F
- [SDR FDEA201107232917](https://openairdocs.org/sdr/FDEA201107232917.md): Skin · corroded · Jul 23, 2011 · N68051 · Doug MD1010F · Wing, Plate/Skin
  > CENTER WING LOWER SKIN BS 1368 (REAR SPAR AREA) CORRODED AT 2EA. LOCATIONS, 12" AND 36" OTBD OF LT KEELBEAM. REMOVED CORROSION ON CENTER WING LWR SKIN IAW EA 8-5710-152431.
- [SDR FDEA201003311037](https://openairdocs.org/sdr/FDEA201003311037.md): Bungee · failed · Mar 31, 2010 · N68051 · Doug MD1010F · Drag Control System
  > DURING T/O FELT LT TURNING TENDENCY THAT INCREASED WITH SPEED. (AFTER CLEAN UP). AP WOULD NOT HOLD LEVEL FLIGHT AND HAD APP 5 DEGREES (UNITS OF AILERON RUDDER TO HAVE CONTROL OF AC. RETURN TO DEPARTURE DUE TO MALFUNCTION. FOUND LT SPOILER MIXER 2-3 BUNGEE B
- [SDR FDEA201001160161](https://openairdocs.org/sdr/FDEA201001160161.md): Spring · damaged · Jan 16, 2010 · N68051 · Doug MD1010F · Drag Control System
  > AT FL 340 APPROX 50 MIN INT FLT W/ PNEU SYS 2 MEL(ED) INOP (SYS CONFIGURED W/ 1-2 ISOL ON & NR 2 PACK & BLEED OFF) GOT AIR SYS 2 OFF FOLLOWED BY LVL 3 AIR MANF 2 FAIL. AIR MANF 2 FAIL SOON CLEARED BUT PNEU SYS 2 SCHEMATIC & OVERHEAD MANF LIGHT REMAINED RED E
- [SDR FDEA200910303742](https://openairdocs.org/sdr/FDEA200910303742.md): Flap System · malfunctioned · Oct 30, 2009 · N68051 · Doug MD1010F · Trailing Edge Flap Control System
  > FLAPS SETTINGS WERE 8,8/6,8. ROLL TENDENCY BEGAN AT APPROX 80 KTS AND ENDED AT LIFTOFF. INSPECTED DRIVE MECHANISM CABLES AND PULLIES IN CTR ACCY COMPARTMENT. PERFORMED A VISUAL INSP OF THE ALL SLAT CABLES, PULLIES, BRACKETS FOR BEING LOOSE OR DAMAGED. NO
- [SDR 07FDEA03364](https://openairdocs.org/sdr/07FDEA03364.md): Doubler · unknown · Sep 5, 2007 · N68051 · Doug DC1010F · Fuselage Main, Plate/Skin
  > EXISTING DOUBLER ON EXTERNAL FUSELAGE. REPAIRED AREA IAW SRM 53-20-00 FIG 6 VOL I.
- [SDR 07FDEA03363](https://openairdocs.org/sdr/07FDEA03363.md): Door Frame · corroded · Sep 5, 2007 · N68051 · Doug DC1010F · Fuselage Main, Structure
  > UPPER MAIN CARGO DOOR FOUND DEEP INTERGRANULAR CORROSION ON TOP OF LOWER DOOR JAMB, UNDER SPOOL FITTING NR 6. ACCOMPLISHED EA NR 8-5310-111456.
- [SDR 07FDEA03362](https://openairdocs.org/sdr/07FDEA03362.md): Doubler · unknown · Sep 5, 2007 · N68051 · Doug DC1010F · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE EXISTING EXTERNAL DOUBLER. REPAIRED AREA IAW SRM 53-20-00 FIG 6 VOL I.
- [SDR 07FDEA02666](https://openairdocs.org/sdr/07FDEA02666.md): Longeron · cracked · Jul 30, 2007 · N68051 · Doug DC1010F · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPT BILGE ON LONGERON LT SIDE FOUND CRACKS. REPAIRED LONGERON IAW SRM 53-10-00 VOL 1 FIG 5 SHT 1.
- [SDR 07FDEA02468](https://openairdocs.org/sdr/07FDEA02468.md): Shear Tie · cracked · Jul 13, 2007 · N68051 · Doug DC1010F · Fuselage Internal Mounting Structure
  > CTR CARGO COMPT TUNNEL ON SHEAR CLIP FOUND CRACK 0.75" LONG. REPAIRED SHEAR CLIP IAW SRM 53-30-00 FIG 10 VOL 1.
- [SDR 07FDEA02466](https://openairdocs.org/sdr/07FDEA02466.md): Bulkhead · cracked · Jul 13, 2007 · N68051 · Doug DC1010F · Fuselage Main, Bulkhead
  > CLG WHEEL WELL AREA CRACK ON VERTICAL BULKHEAD. REPAIRED AREA IAW SRM 53-00-01 FIG 10 VOL 1.
- [SDR 07FDEA02464](https://openairdocs.org/sdr/07FDEA02464.md): Beam · cracked · Jul 13, 2007 · N68051 · Doug DC1010F · Fuselage Main, Structure
  > FWD CARGO COMPT ON BEAM FOUND CRACK. REPAIRED BEAM IAW SRM 53-00-01 VOL 1 FIG 9 SHT 7.
- [SDR 07FDEA02463](https://openairdocs.org/sdr/07FDEA02463.md): Panel · cracked · Jul 13, 2007 · N68051 · Doug DC1010F · Horizontal Stabilizer, Plate/Skin
  > DURING INSPECTION OF UPPER INTERIOR SKIN PANELS OF STB HORIZONTAL SECTION FOUND 1 PANEL P/N 7207-1 WITH CRACK. ACCOMPLISHED EA NR 8-5510-96123.
- [SDR 07FDEA02462](https://openairdocs.org/sdr/07FDEA02462.md): Skin · unknown · Jul 13, 2007 · N68051 · Doug DC1010F · Wing, Plate/Skin
  > EXISTING REPAIR LT WING I/B FLAP LOWER SKIN. REPAIRED IAW SRM 57-00-01 VOL 1 FIG 1A SHT 2.
- [SDR 07FDEA02461](https://openairdocs.org/sdr/07FDEA02461.md): Seat Track · unknown · Jul 13, 2007 · N68051 · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING SEAT TRACK SPLICE REPAIR MAIN CABIN. REPAIRED AREA IAW SRM 53-70-00 FIG 1 VOL 1 AND SRM 51-31-00 VOL 2 PAR 6.
- [SDR 07FDEA02460](https://openairdocs.org/sdr/07FDEA02460.md): Skin · unknown · Jul 13, 2007 · N68051 · Doug DC1010F · Fuselage Main, Plate/Skin
  > EXISTING DOUBLER EXTERNAL SKIN. REPAIRED AREA IAW SRM 53-20-00 FIG 6 VOL 1, SRM 51-00-01 VOL 1 AND DWG NCA6012.
- [SDR 07FDEA02459](https://openairdocs.org/sdr/07FDEA02459.md): Shear Tie · cracked · Jul 13, 2007 · N68051 · Doug DC1010 · Fuselage Internal Mounting Structure
  > CTR CARGO COMPT TUNNEL ON SHEAR CLIP FOUND CRACK. REPAIRED SHEAR CLIP IAW SRM 53-30-00 VOL1 FIG 10.
- [SDR 07FDEA02458](https://openairdocs.org/sdr/07FDEA02458.md): Shear Tie · cracked · Jul 13, 2007 · N68051 · Doug DC1010F · Fuselage Internal Mounting Structure
  > CTR CARGO COMPT TUNNEL ON SHEAR CLIP NR 2 CRACKS. REPAIRED SHEAR CLIP IAW SRM 53-30-00 FIG 10 VOL 1.
- [SDR 07FDEA02457](https://openairdocs.org/sdr/07FDEA02457.md): Shear Tie · cracked · Jul 13, 2007 · N68051 · Doug DC1010F · Fuselage Internal Mounting Structure
  > CTR CARGO COMPT TUNNEL ON SHEAR CLIP FOUND CRACK 0.50" LONG. REPAIRED SHEAR CLIP IAW SRM 53-30-00 VOL 1 FIG 10.
- [SDR 07FDEA02335](https://openairdocs.org/sdr/07FDEA02335.md): Seat Track · corroded · Jun 29, 2007 · N68051 · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEVERE CORROSION WITH EXFOLIATION ON SEAT TRACK. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1.
- [SDR 07FDEA02334](https://openairdocs.org/sdr/07FDEA02334.md): Skin · unknown · Jun 29, 2007 · N68051 · Doug DC1010F · Standard Practices/Structures
  > EXISTING DOUBLER EXTERNAL SKIN. REPAIRED IAW SRM 53-20-00 FIG 6 VOL 1.
- [SDR 07FDEA02333](https://openairdocs.org/sdr/07FDEA02333.md): Seat Track · cracked · Jun 29, 2007 · N68051 · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN CRACK 1' LONG ON SEAT TRACK. REPAIRED IAW SRM 53-70-00 FIG 1 VOL 1.
- [SDR 07FDEA02332](https://openairdocs.org/sdr/07FDEA02332.md): Beam · corroded · Jun 29, 2007 · N68051 · Doug DC1010F · Fuselage Main, Structure
  > FWD CARGO COMPT DOOR SILL ON BEAM FOUND SEVERE CORROSION WITH EXFOLIATION. REPAIRED BEAM IAW SRM 53-00-01 VOL 1 FIG 9 SHT 7.
- [SDR 07FDEA02331](https://openairdocs.org/sdr/07FDEA02331.md): Channel · corroded · Jun 29, 2007 · N68051 · Doug DC1010F · Fuselage Miscellaneous Structure
  > CTR CARGO COMPT ON CHANNEL FOUND CORROSION. REPAIRED CHANNEL IAW SRM 53-70-00 VOL 1 FIG 7 SHT 5.
- [SDR 07FDEA02330](https://openairdocs.org/sdr/07FDEA02330.md): Channel · cracked · Jun 29, 2007 · N68051 · Doug DC1010F · Fuselage Miscellaneous Structure
  > CTR CARGO COMPT BILGE ON "T" CAP ANGLE UNDER CHANNEL ON BLKHD FOUND CRACK 1" LONG. REPAIRED TEE IAW SRM 53-00-01 VOL 1 FIG 9 SHT 3.
- [SDR 07FDEA02329](https://openairdocs.org/sdr/07FDEA02329.md): Bulkhead · cracked · Jun 29, 2007 · N68051 · Doug DC1010 · Fuselage Main, Bulkhead
  > AFT FUSE COMPT FOUND 1 CRACK 1" LONG ON "T" VERTICAL ANGLE AFT VERTICAL BULKHEAD. REPAIRED IAW SRM 53-00-01 FIG 9 VOL 1.
- [SDR 07FDEA02328](https://openairdocs.org/sdr/07FDEA02328.md): Beam · corroded · Jun 29, 2007 · N68051 · Doug DC1010F · Fuselage Main, Structure
  > FWD CARGO COMPT DOOR SILL ON BEAM FOUND SEVERE CORROSION WITH EXFOLIATION. REPAIRED IAW SRM 53-00-01 VOL 1 FIG 9 SHT 7.
- [SDR 07FDEA02327](https://openairdocs.org/sdr/07FDEA02327.md): Skin · unknown · Jun 29, 2007 · N68051 · Doug DC1010F · Standard Practices/Structures
  > EXISTING REPAIR RT WING O/B FLAP LOWER SKIN. REPAIRED AREA IAW SRM 57-10-00 FIG 7 VOL 1.
- [SDR 07FDEA02326](https://openairdocs.org/sdr/07FDEA02326.md): Bulkhead · cracked · Jun 29, 2007 · N68051 · Doug DC1010F · Fuselage Main, Bulkhead
  > CLG WHEEL WELL AREA CRACK 8.5" LONG ON VERTICAL BULKHEAD WEB. REPAIRED CRACK IAW SRM 53-00-01 FIG 10 VOL 1.
- [SDR 07FDEA01976](https://openairdocs.org/sdr/07FDEA01976.md): Bulkhead · cracked · May 25, 2007 · N68051 · Doug DC1010 · Fuselage Main, Bulkhead
  > CLG WHEEL WEEL AREA CRACK ON VERTICAL BULKHEAD. REPAIRED AREA IAW SRM 53-00-01 FIG 10 SHT 3 VOL 1.

Next page: https://openairdocs.org/deregistered/N68051-2024-02-01/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 = 'N68051' AND deregistration_id = 'N68051-2024-02-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N68051-2024-02-01/reports

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