# Service difficulty reports: N68052, cancelled Jan 29, 2024

A list on [N68052, cancelled Jan 29, 2024](https://openairdocs.org/deregistered/N68052-2024-01-29.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 · 89 reports

- [SDR FDEA201503261089](https://openairdocs.org/sdr/FDEA201503261089.md): Unknown · malfunctioned · Mar 26, 2015 · N68052 · Doug MD1010F · Fire Detection
  > ON PREFLIGHT, AFTER CARGO FIRE TEST INITIATED, AFT 1 DISCHARGE SWITCH WAS FLASHING & CONTINUED TO FLASH. THIS WAS AUTO TEST WHEN IRU'S SELECTED ON AMM, SMP. RESET BOTH MSC CB'S IAW MM 31-42-01-5, RTS PASSED, PERFORMED CARGO FIRE TEST & ALL CHECKS NORMAL. N
- [SDR FDEA201412204154](https://openairdocs.org/sdr/FDEA201412204154.md): Battery Pack · discharged · Dec 20, 2014 · N68052 · Doug MD1010F · Emergency Lighting
  > EMER LIGHT BATTERY 1 LOW ALERT ON POST FLIGHT INSPECTION. R & R EMER BATTERY PACK. OPERATIONS CHECKED NORMAL.
- [SDR FDEA201410183314](https://openairdocs.org/sdr/FDEA201410183314.md): Actuator · malfunctioned · Oct 18, 2014 · N68052 · Doug MD1010F · Aileron Control System
  > AIRCRAFT TAKES AT LEAST 3.5 DEGREES OF LT DOWN AILERON TRIM FOR LEVEL FLIGHT. REMOVED AND REPLACED LT IBD AILERON ACTUATOR IAW MM.
- [SDR FDEA201409172641](https://openairdocs.org/sdr/FDEA201409172641.md): Sensor · failed · Sep 17, 2014 · N68052 · Doug MD1010F · Engine Oil Indicating System
  > NR 1 ENGINE OIL TEMP HIGH, 194 DEGREES AT CRUISE. COMPLIED WITH QRH & EVENTUALLY SHUTDOWN NR 1 ENG. R & R NR 1 ENGINE OIL TEMP SENSOR IAW MM 79-32-01-2, FOUND OIL IN CONNECTOR SUSPECT OIL TEMP BULB LEAKING. CLEANED CONNECTOR. RUN CHECK IAW JRH CH 5, OIL T
- [SDR FDEA201405141019](https://openairdocs.org/sdr/FDEA201405141019.md): Motor · cracked · May 14, 2014 · N68052 · Doug MD1010F · Stabilizer Actuator
  > PASSING FL190 DURING CLIMB GOT A LEVEL 2 HYD 3 FAIL ALERT, QTY WENT TO ZERO. ALTERNATE GEAR EXTENSION WAS USED IAW QRH. LEAK APPARENTLY COMING FROM REAR STAB COMPARTMENT ACCESS PANEL AREA. TROUBLESHOOTING IN PROGRESS. FOUND LEAK TO BE COMING FROM RT STAB T
- [SDR FDEA201311192829](https://openairdocs.org/sdr/FDEA201311192829.md): Towershaft · failed · Nov 19, 2013 · N68052 · Doug MD1010F · Turbine Engine Accessory Drive
  > FL 350 CRUISE FLIGHT ENG 3 FLAMED OUT DUE TO HIGH OIL PRESS & 0 ZERO N2 COMPLIED WITH QRH DIVERTED TO KMIA. NR 3 ENG R & R DUE TO TOWER SHAFT FAILURE, OPERATIONS CHECKED GOOD.
- [SDR FDEA201308081813](https://openairdocs.org/sdr/FDEA201308081813.md): Angle · corroded · Aug 8, 2013 · N68052 · Doug MD1010F · Fuselage Miscellaneous Structure
  > RT SLANT PANEL LOWER HORIZONTAL TEE ANGLE CORRODED. REMOVED CORRODED TEE ANGLE. LOCATED AND DRILLED UP HOLES IN NEW TEE ANGLE. INSTALLED NEW TEE ANGLE IAW DWG.
- [SDR FDEA201308081812](https://openairdocs.org/sdr/FDEA201308081812.md): Structure · corroded · Aug 8, 2013 · N68052 · Doug MD1010F · Fuselage Main, Structure
  > RT WW SLANT PANEL AREA EDGE MEMBER CORRODED. REMOVED EDGE MEMBER SLANT PANEL. FABRICATED EDGE MEMBER IAW DWG AEA0449. INSTALLED NEW EDGE MEMBER IAW SRM 51-35-01, VOL II.
- [SDR FDEA201303190610](https://openairdocs.org/sdr/FDEA201303190610.md): Bulkhead · cracked · Mar 19, 2013 · N68052 · Doug MD1010F · Fuselage Floor Panel
  > RIGHT W/W HAS A 1 INCH CRACK INNER WALL 30 INCHES FORWARD OF BS 1521 & 2 FEET DOWN. REPAIR WAS ACCOMPLISHED AND INSTALLED REF EA 8-5310-157386, SEQ NR 255. EA 8-5310-157386 FINAL DRAFT SEQ 257 OF WO 58015 FOR MX PERFORMED.
- [SDR FDEA201303110609](https://openairdocs.org/sdr/FDEA201303110609.md): Web · cracked · Mar 11, 2013 · N68052 · Doug MD1010F · Fuselage Main, Bulkhead
  > WHEEL WELL LEFT BULKHEAD CRACKED 4 INCHES AFT OF BS 1381 AND 3 INCHES DOWN FROM UPPER BULKHEAD. REPAIRED AND INSTALLED IAW EA 8-5310-157385 SEQ 254.
- [SDR FDEA201102260778](https://openairdocs.org/sdr/FDEA201102260778.md): Module · failed · Feb 26, 2011 · N68052 · Doug MD1010F · Passenger Oxygen System
  > DON OXYGEN MASK HORN AND LIGHT TEST RESET LIGHT MODULE DOES NOT ILLUMINATE. RELAMPED NO HELP, TEMP SWAPPED LENS MODULES, PROBLEM MOVED. REQ LENS MODULE, CENTER PIN SPRING COLLAPSED. PARTS ORDERED. REMOVED AND REPLACED DON OXYGEN MASK TEST LIGHT MODULE PE
- [SDR FDEA201012274755](https://openairdocs.org/sdr/FDEA201012274755.md): Switch · no test · Dec 27, 2010 · N68052 · Doug MD1010F · Battery/Charger System
  > EMERGENCY POWER TEST FAIL DURING PRE-FLIGHT. RE-SELECTED BATTERY SWITCH AND FUEL SHUTOFF LEVERS EPT PASSED IAW-FIM-24-24. ACFT OK FOR SERVICE. RE-SELECTED BATTERY SWITCH AND FUEL SHUTOFF LEVERS EPT PASSED IAW FIM-24-24. ACFT OK FOR SERVICE. (CLOSED)
- [SDR FDEA201011284502](https://openairdocs.org/sdr/FDEA201011284502.md): Transmitter · failed · Nov 28, 2010 · N68052 · Doug MD1010F · Emergency Locator Beacon
  > ELT ON 121.5 FOLLOWED US, SUSPECT ACFT ELT IS ALERTING. FACT 28NOV10 19:44 MEM R R & R EMERGENCY LOCATOR TRANSMITTER IAW 23-25-00-4. OPS CHECK GOOD, OK FOR SERVICE. (CLOSED)
- [SDR FDEA201008112941](https://openairdocs.org/sdr/FDEA201008112941.md): Strut · failed · Aug 11, 2010 · N68052 · Doug MD1010F · Nose/Tail Landing Gear Strut/Axle
  > ON POST FLIGHT, FOUND NOSE GEAR COLLAPSED AND LOWER COLLAR OUT OF SHRUT. REMOVED AND REPLACED NOSE LANDING GEAR ASSY IAW WORK CARD 32T2701. OPS, LEAK & RIG CHECKS NORMAL.
- [SDR FDEA201004031050](https://openairdocs.org/sdr/FDEA201004031050.md): Engine · flamed out · Apr 3, 2010 · N68052 · Doug MD1010F · Engine (Turbine/Turboprop)
  > ENGINE FLAMEOUT AT FL350. RESTART ATTEMPTED DURING DESCENT/DIVERT. DURING RESTART ATTEMPT, OIL PRESSURE WENT TO "0" (ZERO). "ENGINE FIRE, OR SEVERE DAMAGE" CHECKLIST ACCOMPLISHED. DIVERTED. TO PIT. CHECKED MAIN OIL FILTER CHIP DETECTOR. DETECTOR IS VERY C
- [SDR FDEA200812085111](https://openairdocs.org/sdr/FDEA200812085111.md): Probe · failed · Dec 8, 2008 · N68052 · Doug MD1010F · Fuel Indicating System
  > DEPARTING TPA RW 18R AT 392.2 TOGW BETWEEN 200 FT AND 3000 FT MSL IN A RT TURN TO 350' (FLAPS AND SLATS RETRACTED) LAT FUEL UNBALANCE ALERT CAME ON THE EAD. ALSO, FUEL QTY/USED CHK ALERT CAME ON. FUEL OFF SKED ALERT ILLUMINATED ABNORMAL NON ALERT FUEL LEAK.
- [SDR 08FDEA03490](https://openairdocs.org/sdr/08FDEA03490.md): Control Valve · failed · Aug 18, 2008 · N68052 · Doug MD1010F · Trailing Edge Flap Control System
  > LVL 2 FLAP DISAGREE AFTER TAKEOFF RAN QRH AND MADE NORMAL LANDING. CREW REPORTED IT TOOK 10 MINUTES FOR FLAPS TO EXTEND 35 DEGREES FOR LANDING. REMOVED AND INSTALLED I/B FLAP CNTL VALVE AND SECURED HYD LINES TO OTHER VALVES REF MD10-10 AMM 27-52-02-2. OPS
- [SDR 08FDEA01942](https://openairdocs.org/sdr/08FDEA01942.md): Check Valve · failed · May 21, 2008 · N68052 · Doug MD1010F · Trailing Edge Flap Control System
  > AFTER TAKEOFF, FLAPS UP GOT LEVEL 2 "FLAP DISAG". FLAPS INDICATED 8/7 (LEFT) AND 5/4 RIGHT WING. FLAP HANDLE BACK TO LAST POSITION AND FLAPS WOULD NOT MOVE. HANDLE BACK TO UP NO CHANGE, WHILE MANEUVERING TO LAND FLAPS INDICATED 3/1 AND UP. RETURNED TO MEM.
- [SDR 07FDEA04621](https://openairdocs.org/sdr/07FDEA04621.md): Fitting · corroded · Oct 17, 2007 · N68052 · Doug DC1010F · Fuselage Main, Attach Fittings
  > CTR CARGO COMPT RT TUNNEL SEVERE CORROSION WITH EXFOLIATION ON FITTING. ACCOMPLISHED EA NR 8-5310-111460.
- [SDR 07FDEA04620](https://openairdocs.org/sdr/07FDEA04620.md): Web · cracked · Oct 17, 2007 · N68052 · Doug DC1010F · Fuselage Miscellaneous Structure
  > LT MLG W/W FOUND CRACK ON VERTICAL WEB. REPAIRED WEB IAW SRM 53-00-01 FIG 10 VOL I.
- [SDR 07FDEA04619](https://openairdocs.org/sdr/07FDEA04619.md): Skin · cracked · Oct 17, 2007 · N68052 · Doug MD1010F · Horizontal Stabilizer, Plate/Skin
  > DURING U/S INSP FOUND PANEL P/N 7206-1 AND 7204-1 OF STAB LOWER SURFACE WITH CRACK IN FLYABLE LIMITS, SEE ATTACHED "INSP FINDING FORM" FOR DETAIL. ACCOMPLISHED EA NR 8-5510-111454.
- [SDR 07FDEA04617](https://openairdocs.org/sdr/07FDEA04617.md): Skin · cracked · Oct 17, 2007 · N68052 · Doug DC1010F · Wing, Plate/Skin
  > RT WING OUTBOARD FLAP CRACK ON EXT SKIN UPPER SIDE. REPAIRED AREA IAW SRM 57-10-00 FIG 7 VOL I.
- [SDR 07FDEA04616](https://openairdocs.org/sdr/07FDEA04616.md): Skin · corroded · Oct 17, 2007 · N68052 · Doug DC1010F · Elevator, Plate/Skin
  > RT INBD ELEVATOR LWR SURFACE FOUND SEVERE CORROSION ON SKIN AND SUSPECT CORROSION UNDER SKIN. REPAIRED AREA IAW SRM 55-10-00 FIG 7 VOL I.
- [SDR 07FDEA04615](https://openairdocs.org/sdr/07FDEA04615.md): Skin · corroded · Oct 17, 2007 · N68052 · Doug DC1010F · Elevator, Plate/Skin
  > RT STAB, INBD ELEVATOR, MODERATE CORROSION BTWN UPPER SKIN AND RIB. REPAIRED AREA IAW SRM 55-10-00 FIG 7 VOL I.
- [SDR 07FDEA04549](https://openairdocs.org/sdr/07FDEA04549.md): Floorbeam · unknown · Oct 10, 2007 · N68052 · Doug DC1010F · Fuselage Main, Floor Beam
  > FOUND EXISTING REPAIR CTR CARGO COMPARTMENT FLOORBEAM. REPAIRED AREA IAW SRM 53-60-01 FIG 3 VOL I.
- [SDR 07FDEA04507](https://openairdocs.org/sdr/07FDEA04507.md): Rib · cracked · Oct 5, 2007 · N68052 · Doug DC1010F · Wing, Rib/Bulkhead
  > FOUND UPPER RIB CAP CRACKED ON RT WING PNL 634AT. REPLACED RIB IAW SRM 57-20-00 FIG 38 SHT 1-2-3 VOL I.
- [SDR 07FDEA04506](https://openairdocs.org/sdr/07FDEA04506.md): Rib · cracked · Oct 5, 2007 · N68052 · Doug DC1010 · Wing, Rib/Bulkhead
  > FOUND UPPER RIB CAP CRACKED ON LT WING PNL 534AT. REPLACED RIB IAW SRM 57-20-00 FIG 38 SHT 1-2-3 VOL I.
- [SDR 07FDEA04504](https://openairdocs.org/sdr/07FDEA04504.md): Longeron · corroded · Oct 5, 2007 · N68052 · Doug DC1010F · Fuselage Main, Longeron/Stringer
  > CTR CARGO COMPT BILGE, CORROSION WITH EXFOLIATION ON SPLICE AND LONGERON. REPAIRED AREA IAW SRM 53-10-00 VOL I FIG 5.
- [SDR 07FDEA04161](https://openairdocs.org/sdr/07FDEA04161.md): Skin · loose · Sep 21, 2007 · N68052 · Doug DC1010F · Wing, Plate/Skin
  > RT WING UPPER SURFACE OUTBD FLAP FOUND 180 EA LOOSE RIVETS ON SKIN. REPAIRED EFFECTED AREAS IAW SRM 57-20-00 VOL I FIG 11 AND WORK IN CONJUNCTION OF NRC N00468.
- [SDR 07FDEA04007](https://openairdocs.org/sdr/07FDEA04007.md): Seat Track · cracked · Sep 19, 2007 · N68052 · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BALLMAT AREA CRACKS ON SEAT TRACK. REPAIRED AREA IAW SRM 53-70-00 FIG 1 VOL I.
- [SDR 07FDEA04005](https://openairdocs.org/sdr/07FDEA04005.md): Seat Track · corroded · Sep 19, 2007 · N68052 · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SEVERE CORROSION WITH EXFOLIATION ON SEAT TRACK. REPAIRED SEAT TRACK IAW SRM 53-60-01 FIG 1 VOL I.
- [SDR 07FDEA04004](https://openairdocs.org/sdr/07FDEA04004.md): Longeron · corroded · Sep 19, 2007 · N68052 · Doug DC1010F · Fuselage Main, Longeron/Stringer
  > AIR CONDITIONING COMPT LT SIDE FOUND SEVERE EXFOLIATION CORROSION. REPAIRED AREA IAW SRM 53-10-00 VOL I.
- [SDR 07FDEA03822](https://openairdocs.org/sdr/07FDEA03822.md): Skin · unknown · Sep 17, 2007 · N68052 · Doug DC1010F · Wing, Plate/Skin
  > RT WING L/E SKIN EXISTING DOUBLER. REPLACED DOUBLER IAW SRM 51-30-00 VOL II.
- [SDR 07FDEA03509](https://openairdocs.org/sdr/07FDEA03509.md): Web · cracked · Sep 10, 2007 · N68052 · Doug DC1010F · Fuselage Miscellaneous Structure
  > LT MLG W/W FOUND CRACKS ON VERTICAL WEB. REPAIRED WEB IAW SRM 53-00-01 FIG 10 VOL I.
- [SDR 07FDEA03508](https://openairdocs.org/sdr/07FDEA03508.md): Longeron · worn · Sep 10, 2007 · N68052 · Doug DC1010F · Fuselage Main, Longeron/Stringer
  > AIR CONDITIONING COMPT LT SIDE ON LONGERON FOUND DEEP WEAR OUT OF LIMITS IAW SRM 53-10-00. REPAIRED AREA IAW SRM 53-10-00 FIG 7 VOL I.
- [SDR 07FDEA03507](https://openairdocs.org/sdr/07FDEA03507.md): Longeron · corroded · Sep 10, 2007 · N68052 · Doug DC1010F · Fuselage Main, Longeron/Stringer
  > AIR CONDITIONING COMPT LT SIDE FOUND SEVERE EXFOLIATION CORROSION. REPAIRED AREA IAW SRM 53-10-00 FIG 6 VOL I.
- [SDR 07FDEA03506](https://openairdocs.org/sdr/07FDEA03506.md): Seat Track · cracked · Sep 10, 2007 · N68052 · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BALLMAT AREA CRACK ON SEAT TRACK. REPAIREED AREA IAW SRM 53-70-00 FIG 1 VOL I.
- [SDR 07FDEA03504](https://openairdocs.org/sdr/07FDEA03504.md): Skin · damaged · Sep 10, 2007 · N68052 · Doug DC1010F · Wing, Plate/Skin
  > RT WING LWR SURFACE OUTBD FLAP FOUND 30 EA LOOSE RIVETS ON SKIN. REPAIRED AREA IAW SRM 57-20-00 VOL I FIG 11.
- [SDR 07FDEA03372](https://openairdocs.org/sdr/07FDEA03372.md): Skin · cracked · Sep 5, 2007 · N68052 · Doug DC1010F · Leading Edge Devices
  > SLAT NR 5 RT: INSTALLING EXTEND CABLE ASSY FOUND NUT PLATE OF BOLT ASSY TRACK CABLE RETAINER ON TRACK SLAT, MISSING. REPAIRED SLAT SKIN IAW SRM 57-00-01 VOL I FIG 4 SHT 2.
- [SDR 07FDEA03213](https://openairdocs.org/sdr/07FDEA03213.md): Pan · cracked · Aug 29, 2007 · N68052 · Doug DC1010F · Cargo/Baggage Doors
  > CTR LOWER CARGO DOOR CRACK ON FWD JAMB DOOR PAN. REPAIRED AREA IAW SRM 52-00-01 FIG 7 SHT 2 VOL 1.
- [SDR 07FDEA03212](https://openairdocs.org/sdr/07FDEA03212.md): Skin · damaged · Aug 29, 2007 · N68052 · Doug DC1010 · Cargo/Baggage Doors
  > CTR LWR CARGO DOOR, LWR FWD CORNER OF SKIN DEFORMED. REPAIRED AREA IAW SRM 52-10-00 FIG 17 VOL 1.
- [SDR 07FDEA03142](https://openairdocs.org/sdr/07FDEA03142.md): Rib · cracked · Aug 27, 2007 · N68052 · Doug DC1010F · Wing, Rib/Bulkhead
  > LT WING INT L/E ON UPPER RIB FOUND CRACK 0.60" LONG. REPAIRED RIB IAW SRM 57-20-00 VOL 1 FIG 1.
- [SDR 07FDEA03084](https://openairdocs.org/sdr/07FDEA03084.md): Skin · deformed · Aug 24, 2007 · N68052 · Doug DC1010F · Wing, Plate/Skin
  > RT WING T/E LOWER SKIN OF ISLAND DEFORMATION. REPAIRED AREA IAW SRM 57-00-01 VOL 1 SHT 2 FIG 4.
- [SDR 07FDEA03030](https://openairdocs.org/sdr/07FDEA03030.md): Skin · unknown · Aug 22, 2007 · N68052 · Doug DC1010F · Wing, Plate/Skin
  > LT WING TIP EXTERNAL DOUBLER ON SKIN. ACCOMPLISHED EA NR 8-5760-112423.
- [SDR 07FDEA03029](https://openairdocs.org/sdr/07FDEA03029.md): Skin · unknown · Aug 22, 2007 · N68052 · Doug DC1010F · Wing, Plate/Skin
  > RT WING TIP EXTERNAL DOUBLER ON SKIN. ACCOMPLISHED EA NR 8-5760-112423.
- [SDR 07FDEA03028](https://openairdocs.org/sdr/07FDEA03028.md): Beam · corroded · Aug 22, 2007 · N68052 · Doug DC1010F · Fuselage Main, Structure
  > FWD CARGO COMPT BILGE AREA ON BEAM FOUND SEVERE EXFOLIATION CORROSION. REPAIRED AREA IAW SRM 53-60-01 VOL 1 FIG 3.
- [SDR 07FDEA02819](https://openairdocs.org/sdr/07FDEA02819.md): Rib · worn · Aug 10, 2007 · N68052 · Doug DC1010 · Wing, Rib/Bulkhead
  > LT WING L/E AT STA XOS 460 ON LOWER RIB AREA DOOR 513AB FOUND DEEP WEAR REPAIRED TEE IAW SRM 57-00-01 VOL I FIG 9. FABRICATED PARTS IAW SRM 57-00-01 FIG 9 VOL 1.
- [SDR 07FDEA02818](https://openairdocs.org/sdr/07FDEA02818.md): Seat Track · worn · Aug 10, 2007 · N68052 · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN DEEP WEAR ON SEAT TRACK AT STA 1497, X=-47 CUT DAMAGED SECTION OF SEAT TRACK FROM STA 1491 TO 1531. FABRICATED AND INSTALLED NEW SECTION REPAIR AND SPLICE IAW SRM 53-70-00 FIG 1 VOL 1.
- [SDR 07FDEA02672](https://openairdocs.org/sdr/07FDEA02672.md): Seat Track · worn · Jul 30, 2007 · N68052 · Doug DC1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK DEEP WEAR ON UPPER SIDE. REPAIRED IAW SRM 53-70-000 FIG 1 VOL 1.
- [SDR 07FDEA02669](https://openairdocs.org/sdr/07FDEA02669.md): Floorbeam · cracked · Jul 30, 2007 · N68052 · Doug DC1010F · Fuselage Main, Floor Beam
  > FWD CARGO COMPT BILGE AREA ON BEAM FOUND CRACK. REPAIRED BEAM IAW SRM 53-60-01 VOL 1 FIG 3 SHEET 1-2.

Next page: https://openairdocs.org/deregistered/N68052-2024-01-29/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 = 'N68052' AND deregistration_id = 'N68052-2024-01-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N68052-2024-01-29/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.