# Service difficulty reports: N71CX, cancelled May 1, 2014

A list on [N71CX, cancelled May 1, 2014](https://openairdocs.org/deregistered/N71CX-2014-05-01.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 · 200 reports

- [SDR IXXA20130107001O](https://openairdocs.org/sdr/IXXA20130107001O.md): Transceiver · inoperative · Jan 7, 2013 · N71CX · Doug DC862F · HF Communications System
  > AFTER DEPARTURE, NR 1 HF RADIO TUNES, BUT IS WEAK AND UNREADABLE AND NR 2 HF RADIO WILL NOT CHANNELIZE OR TUNE. ACFT RETURNED TO PREVIOUS STATION. R & R CAPTAINS AUDIO SELECT PANEL IAW MM 23-50-1. AUDIO SELECTOR PANEL OPS CHECKS NORMAL IAW MM 23-50-0 AND NR
- [SDR IXXA20121210033O](https://openairdocs.org/sdr/IXXA20121210033O.md): Controller · inoperative · Dec 10, 2012 · N71CX · Doug DC862F · Windshield/Door Rain/Ice Removal
  > ACFT ENROUTE AND AIR RETURNED BACK TO DEPARTURE DUE TO F/O WINDSHIELD CRACKED AND ARCING. PILOT STATED F/O VISION IMPAIRED. R & R RT SIDE WINDSHIELD IAW MM 56-10-2 AND R & R RT WINDOW HEAT CONTROLLER IAW MM 30-41-0. OPS CHECKED NORMAL.
- [SDR IXXA20121001028O](https://openairdocs.org/sdr/IXXA20121001028O.md): Battery · inoperative · Oct 1, 2012 · N71CX · Doug DC862F · Emergency Equipment
  > F/A EMERGENCY FLASHLIGHTS FOUND INOPERATIVE. R & R THE RT EMERGENCY FLASHLIGHT AND BATTERIES IAW MM 16.02. OPS CHECK GOOD.
- [SDR IXXA20120907023O](https://openairdocs.org/sdr/IXXA20120907023O.md): Engine · stalled · Sep 7, 2012 · N71CX · Doug DC862F · Engine (Turbine/Turboprop)
  > DURING TAKEOFF ROLL, CREW EXPERIENCED A COMPRESSOR STALL ON THE NR 3 ENGINE. TAKEOFF WAS REJECTED AT 85 KIAS AND 1.96 EPR. RETURNED BACK TO GATE. MX PERSONNEL PERFORMED A VISUAL INSPECTION OF NR 3 ENGINE, NO DEFECTS OBSERVED. ACCOMPLISHED ENGINE RUN UP TO
- [SDR IXXA20120322009O](https://openairdocs.org/sdr/IXXA20120322009O.md): Ground Wire · damaged · Mar 20, 2012 · N71CX · Doug DC862F · Light System Wiring
  > PASSENGER COMPARTMENT FORWARD BULKHEAD EMERGENCY EXIT IDENTIFIER DOES NOT ILLUMINATE. REPAIRED GROUND WIRE TO IDENTIFIER IAW MM 20-50-1 AND RELAMPED SIGN. OPS CHECKS NORMAL IAW MM 33.01.1.
- [SDR IXXA1100770](https://openairdocs.org/sdr/IXXA1100770.md): Slide · low pressure · Nov 28, 2011 · N71CX · Doug DC862F · Escape Slide
  > LEFT HAND PASSENGER DOOR ESCAPE SLIDE PRESSURE LOW AND IN RED RANGE (2600 PSI AT 22 DEGREES CELCIUS) - DISCOVERED DURING POSTFLIGHT INSPECTION. MX R & R EMERGENCY ESCAPE SLIDE IAW MM 25-60-1.
- [SDR IXXA110065O](https://openairdocs.org/sdr/IXXA110065O.md): Unknown · unknown · Oct 6, 2011 · N71CX · Doug DC862F · Nose/Tail Landing Gear
  > AFTER TAKEOFF, WHEN GEARS WERE BEING RETRACTED THE CREW A HEARD LOUD NOISE IN NOSE GEAR AREA. THEY CYCLED NOSE GEAR AND NOISE CONTINUED. THEY RETURNED TO WITHOUT FURTHER INCIDENT. ON POST FLIGHT INSPECTION BOTH DOORS WERE CLOSED AND LATCHED. MAINTENANCE IN
- [SDR IXXA110062O](https://openairdocs.org/sdr/IXXA110062O.md): Ground Wire · loose · Sep 25, 2011 · N71CX · Doug DC862F · Auto Flight System Wiring
  > AIR TURN BACK, DUE TO AUTO PILOT WILL NOT STAY ENGAGED WITH ELEVATOR SERVO ON. THE ACFT PITCHES UP AND DOWN AND DISENGAGED IN VERTICAL SPEED OR ALT HOLD MODES. MX TROUBLESHOT AND FOUND WEAK SHIELD GROUND AT GROUND STUD 1385, REPAIRED GROUND SHIELD AT STUD 138
- [SDR IXXA20110925001](https://openairdocs.org/sdr/IXXA20110925001.md): Fan · failed · Sep 25, 2011 · N71CX · Doug DC862F · Air Distribution Fan
  > DURING CRUISE, THE LT RECIRCULATION FAN HAS A SMELL OF SMOKE. THE CREW TURNED OFF LT RECIRCULATION FAN AND SMOKE, SMELL WENT AWAY. THEY LANDED WITHOUT FURTHER INCIDENT. MX PERFORMED OPS TEST ON BOTH LT AND RT RECIRCULATION FAN, NO SMOKE ODOR NOTED IAW MM 21-2
- [SDR IXXA110058O](https://openairdocs.org/sdr/IXXA110058O.md): Fan · odor · Sep 4, 2011 · N71CX · Doug DC862F · Air Distribution Fan
  > DURING CRUISE, THE OVERHEAD COCKPIT CLIMATE CONTROL UNIT EMITS A BURNING ODOR WHEN TURNED ON. THE CREW LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND CLEANED THE OVERHEAD CLIMATE CONTROL UNIT FAN. OPS CHECK GOOD IAW MM 21-02. ACFT WAS RETURNED TO SERVICE
- [SDR IXXA110059O](https://openairdocs.org/sdr/IXXA110059O.md): Battery · inoperative · Sep 3, 2011 · N71CX · Doug DC862F · Emergency Equipment
  > DURING PREFLIGHT INSPECTUIN, FOUND EMERGENCY FLASHLIGHT INOPERATIVE. MX REPLACED BATTERY IAW MM 33-50-0.
- [SDR IXXA110056O](https://openairdocs.org/sdr/IXXA110056O.md): Fan · failed · Sep 2, 2011 · N71CX · Doug DC862F · Air Distribution Fan
  > DURING CRUISE, WHEN THE CREW TURNED ON LT RECIRCULATION FAN IT EMITTED A BURNING SMELL. THEY TURNED THE LT RECIRCULATION FAN OFF AND SMELL WENT AWAY. THEY LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE LT RECIRCULATION FAN. OPS CHECKED GOOD IAW MM 21-21-1
- [SDR IXXA110054O](https://openairdocs.org/sdr/IXXA110054O.md): Controller · malfunctioned · Aug 19, 2011 · N71CX · Doug DC862F · Flight Controller
  > DURING CRUISE, 30 MIN INTO FLIGHT, AUTOPILOT DISCONNECTED AND WOULD NOT RECONNECT. THE CREW RETURNED. MX REPLACED AUTOPILOT CONTROLLER. OPS CHECKED GOOD IAW MM 22-10-2. ACFT RETURNED TO SERVICE.
- [SDR IXXA110051O](https://openairdocs.org/sdr/IXXA110051O.md): Light · unsecure · Jul 26, 2011 · N71CX · Doug DC862F · Emergency Lighting
  > DURING PREFLIGHT INSP, FOUND GALLEY SERVICE DOOR EMERGENCY EXIT LIGHTING INTERMITTENT. MX RESECURED LIGHTING ASSY. OPERATIONAL CHECK GOOD IAW MM 33-50-0. ACFT RETURNED TO SERVICE.
- [SDR IXXA110050S](https://openairdocs.org/sdr/IXXA110050S.md): Stringer · delaminated · Jul 23, 2011 · N71CX · Doug DC862F · Nacelle/Pylon, Longeron/Stringer
  > DURING ROUTINE B-CHECK INSPECTION FOUND NR 1 ENGINE LOWER STRINGER DELAMINATED. R & R DAMAGED STRINGER IAW MM 78-10-2.
- [SDR IXXA110042O](https://openairdocs.org/sdr/IXXA110042O.md): Fan · defective · May 29, 2011 · N71CX · Doug DC862F · Air Distribution Fan
  > DURING CRUISE, THE LT RECIRCULATION FAN EMITTED A BURNED ELECTRICAL ODOR. THE CREW TURNED OFF THE LT RECIRCULATION FAN THE BURNED ODOR WENT AWAY. THEY LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE LT RECIRCULATION FAN. OPS CHECK GOOD IAW MM 21-21-1. ACFT
- [SDR IXXA110038O](https://openairdocs.org/sdr/IXXA110038O.md): Connector · shorted · May 4, 2011 · N71CX · Doug DC862F · Instrument System Wiring
  > WHILE INCREASING THE INTENSITY OF THE ENGINE INSTRUMENT LIGHTS, THE CREW SMELLED AN ELECTRICAL ODOR COMING FROM THE ENGINE INSTRUMENT LIGHT PANEL. THEY TURNED OFF THE RHEOSTAT TO THE ENGINE INSTRUMENT LIGHTS, THE ODOR WENT AWAY. THEY LANDED WITHOUT FURTHER INC
- [SDR IXXA110036O](https://openairdocs.org/sdr/IXXA110036O.md): Smoke Detector · defective · Apr 30, 2011 · N71CX · Doug DC862F · Smoke Detection
  > DURING CLIMBOUT, THE NR 2 CARGO SMOKE DETECTOR FLASHED ON MOMENTARLY SEVERAL TIMES WITH ASSOCIATED AUDIBLE WARNING. THE CREW INSPECTED THE CARGO COMPARTMENT FOR SMOKE OR FIRE AND NONE WAS NOTED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX IN
- [SDR IXXA1100330](https://openairdocs.org/sdr/IXXA1100330.md): Actuator · defective · Apr 18, 2011 · N71CX · Doug DC862F · Pressure Regulator/Outflow Valve
  > AT FL 320 CABIN PRESSURIZATION CONTROL WAS SET TO 340 FOR FOR A SELECTED CABIN 4,500 FT CABIN CLIMBED TO 8500 FT. CABIN PRESS CONTROL LEVER PHYSICALLY LIMITED TO 2" FROM FULL CLOSED. THE CREW RETURNED BACK TO DEPARTURE WITHOUT FURTHER INCIDENT. MX FOUND THE
- [SDR IXXA110032O](https://openairdocs.org/sdr/IXXA110032O.md): Fan · failed · Apr 13, 2011 · N71CX · Doug DC862F · Air Distribution Fan
  > DURING CRUISE THE RT RECIRCULATION FAN EMMITTING AN ELECTRICAL ODOR. THE CREW TURNED OFF FAN AND SMELL WENT AWAY. THE CREW LANDED WITHOUT FURTHER INCIDENT.
- [SDR IXXA110028O](https://openairdocs.org/sdr/IXXA110028O.md): Fan · failed · Mar 13, 2011 · N71CX · Doug DC862F · Air Distribution Fan
  > DURING CRUISE, WITH THE RT RECIRCULATION FAN ON HAS A STRONG ELECTRICAL ODOR, WHEN TURNED OFF ODOR WENT AWAY. THE CREW LANDED WITHOUT FURTHER INCIDENT. MX DEFERRED THE RT RECIRCULATION FAN IAW MEL 21-16-01. MX REPLACED RECIRCULATION FAN. OPS CHECK GOOD IAW M
- [SDR IXXA110025S](https://openairdocs.org/sdr/IXXA110025S.md): Skin · damaged · Feb 28, 2011 · N71CX · Doug DC862F · Spoilers
  > DURING ROUTINE MAINTENANCE CHECK FOUND LEFT HAND WING NUMBER FOUR SPOILER PANEL DAMAGED. THE SPOILER WAS REPAIRED IAW DACO MAINTENANCE MANUAL 27-61-0.
- [SDR IXXA110013O](https://openairdocs.org/sdr/IXXA110013O.md): Pressure Switch · cracked · Feb 6, 2011 · N71CX · Doug DC862F · Engine Oil Pressure
  > DURING CRUISE, THE CREW SHUTDOWN NR 1 ENGINE DUE TO LOSS OF OIL QTY. THEY LANDED WITHOUT FURTHER INCIDENT. MX INPECTED NR 1 ENGINE AND FOUND OIL DIFFERENTIAL PRESSURE SWITCH HOUSING CRACKED. THEY REPLACED OIL DIFFERENTIAL PRESSURE SWITCH. OPS CHECK GOOD IAW
- [SDR IXXA100042O](https://openairdocs.org/sdr/IXXA100042O.md): Fan · odor · Aug 23, 2010 · N71CX · Doug DC862F · Air Distribution Fan
  > DURING CRUISE, THE LT RECIRCULATION FAN WHEN TURNED ON EMITTED A ELETRICAL ODOR. THE CREW TURNED OFF THE LT RECIRCULATION FAN AND CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE LT RECIRCULATION FAN. OPS CHECK GOOD IAW MM 21-21-1. ACFT WAS RET
- [SDR IXXA100041O](https://openairdocs.org/sdr/IXXA100041O.md): Fan · defective · Aug 20, 2010 · N71CX · Doug DC862F · Air Distribution Fan
  > DURING CRUISE, THE RIGHT HAND RECIRCULATION FAN WHEN TURNED ON EMITTED A ELECTRICAL ODOR. THE CREW TURNED OFF RIGHT RECIRCULATION FAN AND SMELL WENT AWAY. THEY LANDED IN KWRI WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT RECIRCULATION FAN. OPERATION
- [SDR 2010FA0000919](https://openairdocs.org/sdr/2010FA0000919.md): Beam · cracked · Jul 31, 2010 · N71CX · Doug DC862F · Fuselage Main, Structure
  > (SPUY) NR80 ACCESS DOOR - BULKHEAD BEAM CRACKED 4" AT STA 1606.000 L-19 ON RBL-2: TO LBL 2".
- [SDR 2010FA0000918](https://openairdocs.org/sdr/2010FA0000918.md): Skin · corroded · Jul 31, 2010 · N71CX · Doug DC862F · Fuselage Main, Plate/Skin
  > (SPUY) FUSELAGE SKIN CORRODED AT STA FS 1558.000 L-10L.
- [SDR 2010FA0000917](https://openairdocs.org/sdr/2010FA0000917.md): Skin · cracked · Jul 31, 2010 · N71CX · Doug DC862F · Wing, Plate/Skin
  > (SPUY) RT WING NR 4 STUB WING LWR SKIN CRACKED APPROX 1.5" (CORRECTING SOURCE DOCUMENT: INS-100R-5700).
- [SDR 2010FA0000916](https://openairdocs.org/sdr/2010FA0000916.md): Skin · dented · Jul 31, 2010 · N71CX · Doug DC862F · Trailing Edge Flaps
  > (SPUY) LT WING OTBD FLAP UPPER SKIN DENTED (STA XF 238.00 - 304.000).
- [SDR 2010FA0000915](https://openairdocs.org/sdr/2010FA0000915.md): Skin · corroded · Jul 31, 2010 · N71CX · Doug DC862F · Wing, Plate/Skin
  > (SPUY) RT WING OTBD L/E OUTER SECTION LWR SKIN CORRODED (XFS 710.000-760.000).
- [SDR 2010FA0000914](https://openairdocs.org/sdr/2010FA0000914.md): Longeron · corroded · Jul 31, 2010 · N71CX · Doug DC862F · Fuselage Main, Longeron/Stringer
  > (SPUY) AFT ACCY COMPT - L-23R INTERIOR CORRODED (STA 1380.000 - 1400.000).
- [SDR 2010FA0000913](https://openairdocs.org/sdr/2010FA0000913.md): Skin · corroded · Jul 31, 2010 · N71CX · Doug DC862F · Wing, Plate/Skin
  > (SPUY) RT WING UPPER SKIN CORRODED AT AROUND STA XRS 74.889.
- [SDR 2010FA0000912](https://openairdocs.org/sdr/2010FA0000912.md): Cargo Track · corroded · Jul 31, 2010 · N71CX · Doug DC862F · Fuselage, Seat/Cargo Attach Fittings
  > (SPUY) MAIN CARGO COMPT NR 6 TRACK CORRODED AT STA 372.000.
- [SDR 2010FA0000911](https://openairdocs.org/sdr/2010FA0000911.md): Skin · corroded · Jul 31, 2010 · N71CX · Doug DC862F · Elevator, Plate/Skin
  > (SPUY) LT HORZ STAB - ELEVATOR LWR SKIN CORRODED AT STA XE 195.313.149.000 AND 132.750.
- [SDR 2010FA0000910](https://openairdocs.org/sdr/2010FA0000910.md): Angle · corroded · Jul 31, 2010 · N71CX · Doug DC862F · Vertical Stabilizer, Attach Fittings
  > (SPUY) EMPENAGE - VERTICAL STAB TO FUSELAGE LT JOINT ANGLE CORRODED AT STA 1640.382.
- [SDR 2010FA0000909](https://openairdocs.org/sdr/2010FA0000909.md): Frame · corroded · Jul 31, 2010 · N71CX · Doug DC862F · Fuselage Main, Frame
  > (SPUY) LT MLG WW - FRAME FITTING CORRODED AT STA FS 879.000 L-24.
- [SDR 2010FA0000907](https://openairdocs.org/sdr/2010FA0000907.md): Structure · corroded · Jul 31, 2010 · N71CX · Doug DC862F · Wing Main, Frame Structure
  > (SPUY) RT WING INBD L/E OUTER SECTION UPPER PART CORRODED AT STA XW 257.000.
- [SDR 2010FA0000906](https://openairdocs.org/sdr/2010FA0000906.md): Skin · corroded · Jul 31, 2010 · N71CX · Doug DC862F · Fuselage Main, Plate/Skin
  > (SPUY) EXTERNAL FUSELAGE - LOWER SKIN PANEL BUTT SPLICE CORRODED AT STA 1480.000 L-11L.
- [SDR 2010FA0000905](https://openairdocs.org/sdr/2010FA0000905.md): Skin · corroded · Jul 31, 2010 · N71CX · Doug DC862F · Wing, Plate/Skin
  > (SPUY) LT WING - UPPER PANEL EXTERNAL SKIN CORRODED AT STA XRS 204.000 S-14.
- [SDR 2010FA0000904](https://openairdocs.org/sdr/2010FA0000904.md): Hook · cracked · Jul 31, 2010 · N71CX · Doug DC862F · Passenger/Crew Doors
  > (SPUY) AFT PAX DOOR- HOLD OPEN HOOKS (02EA) CRACKED 1", APPROX AT STA FS 1440.000L TO L-15L.
- [SDR IXXA10SMN073S](https://openairdocs.org/sdr/IXXA10SMN073S.md): Skin · corroded · Jul 1, 2010 · N71CX · Doug DC862F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND EXTERNAL FUSELAGE SKIN CORRODED AT STA FS 1556.000 LONGERON 10 LT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, REPAIR DOUBLER, FILLER, AN
- [SDR IXXA10SMN072S](https://openairdocs.org/sdr/IXXA10SMN072S.md): Skin · cracked · Jun 19, 2010 · N71CX · Doug DC862F · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND RT WING NR 4 STUB WING LOWER SKIN CRACKED. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, EXTERNAL DOUBLERS AND INTERNAL DOUBLERS. PERF
- [SDR IXXA10SMN071S](https://openairdocs.org/sdr/IXXA10SMN071S.md): Skin · dented · Jun 19, 2010 · N71CX · Doug DC862F · Trailing Edge Flaps
  > DURING ROUTINE C-CHECK INSP FOUND THE LT WING OTBD FLAP UPPER SKIN DENTED AT STA XF 238.000 - 304.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW F
- [SDR IXXA10SMN070S](https://openairdocs.org/sdr/IXXA10SMN070S.md): Skin · corroded · Jun 19, 2010 · N71CX · Doug DC862F · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND RT WING OTBD L/E OUTER SECTION LOWER SKIN CORRODED AT STA XFS 710.000 - 760.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED NDT INSP. NO DISCREPAN
- [SDR IXXA10SMN069S](https://openairdocs.org/sdr/IXXA10SMN069S.md): Longeron · corroded · Jun 19, 2010 · N71CX · Doug DC862F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C-CHECK INSP FOUND AFT ACCESSORY COMPARTMENT LONGERON L-23 RT INTERIOR CORRODED AT STA 1380-1400. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABERCATED SPLICES. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW
- [SDR IXXA10SMN068S](https://openairdocs.org/sdr/IXXA10SMN068S.md): Skin · corroded · Jun 18, 2010 · N71CX · Doug DC862F · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSP, FOUND RT WING UPPER SKIN CORRODED AT STA XRS 38.000 -112.000. REMOVED CORROSION. FOUND OUT OF LIMITS. PERFORMED NDT INSP. NO DISCREPANCY FOUND. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. FABRICATED NEW SKIN, REPAIR DOUBLE
- [SDR IXXA10SMN067S](https://openairdocs.org/sdr/IXXA10SMN067S.md): Cargo Track · corroded · Jun 18, 2010 · N71CX · Doug DC862F · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT NR 6 TRACK CORRODED AT STA 372.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED SPLICES. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW TRACK SEGMENT AND RE
- [SDR IXXA10SMN066S](https://openairdocs.org/sdr/IXXA10SMN066S.md): Skin · corroded · Jun 17, 2010 · N71CX · Doug DC862F · Elevator, Plate/Skin
  > DURING ROUTINE C-CHECK INSP, FOUND LT HORIZ STABILIZER ELEVATOR LOWER SKIN CORRODED AT STA XE 195.313, 149.000, AND 132.750. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, FINGE
- [SDR IXXA10SMN065S](https://openairdocs.org/sdr/IXXA10SMN065S.md): Angle · corroded · Jun 17, 2010 · N71CX · Doug DC862F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSP, FOUND EMPENNAGE VERTICAL STABILIZER TO FUSELAGE LT JOINT ANGLE CORRODED AT STA 1640.382. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED ANGLE, FILLER AND TAPERED SHIMS. PERFORMED HEAT TREATMENT. CLEANED,
- [SDR IXXA10SMN063S](https://openairdocs.org/sdr/IXXA10SMN063S.md): Skin · corroded · Jun 17, 2010 · N71CX · Doug DC862F · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSP, FOUND RT WING INBD L/E OUTER SECTION UPPER PART CORRODED AT STA XW 257.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, REPAIR DOUBLER, AND FILLERS.

Next page: https://openairdocs.org/deregistered/N71CX-2014-05-01/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 = 'N71CX' AND deregistration_id = 'N71CX-2014-05-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N71CX-2014-05-01/reports

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