# Service difficulty reports: N41CX, cancelled Jan 30, 2021

A list on [N41CX, cancelled Jan 30, 2021](https://openairdocs.org/deregistered/N41CX-2021-01-30.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 10 · 494 reports

- [SDR IXXA201312040450](https://openairdocs.org/sdr/IXXA201312040450.md): Pressure Switch · malfunctioned · Dec 4, 2013 · N41CX · Doug DC862F · Engine Oil Pressure
  > AFTER TAKEOFF AT 1545Z NR 1 ENG LOW OIL PRESS LIGHT ILLUMINATED, PERFORMED APPROPRIATE CHECK LIST, LOW PRESS LIGHT STAYED ON SHUT ENG DOWN. R & R NR 1 LOW OIL PRESS SWITCH IAW 79-32-2, SYS OPERATIONS CHECKED NORMAL IAW DACO DC8 MM 79-32-0 & ATI ERH 70.01GMM 3
- [SDR IXXA201308180280](https://openairdocs.org/sdr/IXXA201308180280.md): Bleed Valve · malfunctioned · Aug 18, 2013 · N41CX · Doug DC862 · Compressor Bleed Valve
  > COMPRESSOR STALL AT APPROX 75 KNOTS. SUSPECT NR 1 AND 2 ENGINES. RAN NR 1 AND 2 ENGINES IAW ENGINE RUN HANDBOOK 70.01. FOUND NR 1 ENGINE PRESSURE RATIO BLEED CONTROL VALVE WILL NOT CLOSE ABOVE 64 PERCENT N1. R & R PRESSURE RATIO BLEED CONTROL VALVE IAW MM 75
- [SDR IXXA20130202002O](https://openairdocs.org/sdr/IXXA20130202002O.md): Link · inoperative · Feb 2, 2013 · N41CX · Doug DC862 · Landing Gear Retraction/Extension System
  > ON CLIMBOUT, AFTER A GOOD UPLATCH CHECK, HEARD A LOUD NOISE IN NOSE GEAR AREA. (SOUNDED LIKE A NOSE GEAR DOOR POPPED OPEN). R & R RT NLG DOOR FORWARD LINK ASSY IAW MM 32-22-1. OPS CHECKS GOOD ON NOSE GEAR SWING.
- [SDR IXXA2013020700006](https://openairdocs.org/sdr/IXXA2013020700006.md): Skin · cracked · Dec 5, 2012 · N41CX · Doug DC862 · Wing, Plate/Skin
  > RT WING UPPER SKIN CRACKED AT XRS 22.750 S17. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIGURE 8. TRIMMED OUT CRACK ON RT WING UPPER SKIN IAW SRM 57-2-1. FABRICATED DOUBLER 0.190", FILLER 0.200" IAW SRM 57-2-1. CLEANED, TREATED AND PRIMED FABRICATED PARTS AND
- [SDR IXXA2013020700005](https://openairdocs.org/sdr/IXXA2013020700005.md): Panel · damaged · Nov 23, 2012 · N41CX · Doug DC862 · Trailing Edge Flaps
  > RT WING OTBD FLAP LOWER PANEL WITH SEVERAL DENTS AND SCRATCHES XF 415 - 452. PERFORMED MAJOR REPAIR IAW SRM 57-7-1, FIG 4, TR 57-94. REMOVED OTBD FLAP LOWER PANEL IAW SRM 51-3-0. REMOVED EXISTING DAMAGED PANEL IAW SRM 51-1-21. FABRICATED NEW PANEL PLATING 0
- [SDR IXXA2013020700004](https://openairdocs.org/sdr/IXXA2013020700004.md): Fitting · corroded · Nov 12, 2012 · N41CX · Doug DC862 · Fuselage Main, Attach Fittings
  > AFTER CARGO COMPARTMENT - INTERIOR BATHTUB FITTING CORRODED AT STA 1530.000, L-32R (AFTER PART). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, NOV 15, 2012, DWG ED-5546 NOV 15, 2012. REMOVED CORRODED FITTING IAW SRM 51-1-20D, SRM 51-1-21. FABRICATED FITTING (
- [SDR IXXA2013020700003](https://openairdocs.org/sdr/IXXA2013020700003.md): Fitting · corroded · Nov 12, 2012 · N41CX · Doug DC862 · Fuselage Main, Attach Fittings
  > AFTER ACCESSORY COMPARTMENT INTERIOR BATHTUB FITTING CORRODED AT STA 1530.000 L-34R (AFTER PART). PERFORMED MAJOR REPAIR IAW FORM 8110-3 DWG NR ED-5546 NOV 15,2012. REMOVED CORRODED FITTING IAW SRM 51-1-20D, SRM 51-1-21. FABRICATED FITTING AL 7075T651 IAW DW
- [SDR IXXA2013020700002](https://openairdocs.org/sdr/IXXA2013020700002.md): Skin · corroded · Nov 9, 2012 · N41CX · Doug DC862 · Rudder, Plate/Skin
  > RUDDER SKIN-LT PANEL SHOWS CORROSION FROM STA ZR 140.750 TO STA ZR 150.750. PERFORMED MAJOR REPAIR IAW SRM 55-6-1, FIG 1. REMOVED EXISTING DAMAGED PANEL IAW SRM 51-1-21, SRM 55-1-0. FABRICATED NEW PANEL PLATING 0.016" AND BONDED DOUBLER 0.016" BOTH FROM AL 2
- [SDR IXXA121109SMN026S](https://openairdocs.org/sdr/IXXA121109SMN026S.md): Longeron · cracked · Nov 9, 2012 · N41CX · Doug DC862 · Fuselage Main, Longeron/Stringer
  > LONGERON 24R, HORIZONTAL LEG CRACKED 2 INCHES AT FS 879.375. PERFORMED MAJOR REPAIR IAW SRM 53-2-2, FIG 5 TR 53-123. REMOVED FASTENERS FROM REPAIRED AREA IAW SRM 51-1-20D.
- [SDR IXXA121109SMN025S](https://openairdocs.org/sdr/IXXA121109SMN025S.md): Longeron · cracked · Nov 9, 2012 · N41CX · Doug DC862 · Fuselage Main, Longeron/Stringer
  > LONGERON 24L, HORIZONTAL LEG CRACKED 1 INCH AT FS 879.375. PERFORMED MAJOR REPAIR IAW SRM 53-2-2, FIG 5, TR 53-123.
- [SDR IXXA2013020700001](https://openairdocs.org/sdr/IXXA2013020700001.md): Skin · damaged · Nov 6, 2012 · N41CX · Doug DC862 · Wing, Plate/Skin
  > RT WING L/E NR 4 STUB WING CORRODED, XW 454 - XW 485. REMOVED FASTENERS FROM REPAIRED AREA IAW SRM 51-1-21. REMOVED CORROSION FROM DAMAGED AREA IAW SRM 51-1-8. TRIMMED OUT DAMAGED AREA IAW DWG ED-5545 NOV 14, 2012. FABRICATED DOUBLER 0.071" FILLER 0.063" BO
- [SDR IXXA20120618016O](https://openairdocs.org/sdr/IXXA20120618016O.md): Connector · dirty · Jun 18, 2012 · N41CX · Doug DC862F · Engine Indicating System Wiring
  > NR 1 EGT FLUCTUATED RAPIDLY AND THEN DROPPED TO ZERO DURING TAKEOFF ROLL. TAKEOFF ABORTED AT APPROX 40 KNOTS. ACFT RETURNED TO BLOCKS. INSPECTED THERMOCOUPLE HARNESS JUNCTIONS. NO DEFECTS NOTED. REMOVED, CLEANED AND INSPECTED EGT HARNESS PYLON CONNECTOR.
- [SDR IXXA20120605015](https://openairdocs.org/sdr/IXXA20120605015.md): Amplifier · failed · Jun 5, 2012 · N41CX · Doug DC862F · Attitude and Direction Data System
  > CAPTAINS HSI AND ADI FAILED AFTER TAKEOFF. RETURNED TO ORIGINATING STATION. PERFORMED OVERWEIGHT LANDING INSP IAW MM 5-50-0 AND MM 13.01.05. NO DISCREPANCIES NOTED. R & R INSTRUMENT AMPLIFIER IAW MM 34-23-00. OPS CHECKED GOOD.
- [SDR IXXA20120605014](https://openairdocs.org/sdr/IXXA20120605014.md): Gyro · failed · Jun 5, 2012 · N41CX · Doug DC862F · Attitude and Direction Data System
  > CAPTAINS HSI AND ADI FAILED AFTER INITIAL CLIMBOUT AND LEVEL OFF AT CRUISE ALTITUDE. RETURNED TO ORIGINATING STATION. R & R NR 1 FOG GYRO IAW MM 34-11-25. OPS CHECKED GOOD.
- [SDR IXXA20120228005O](https://openairdocs.org/sdr/IXXA20120228005O.md): Switch · leaking · Feb 28, 2012 · N41CX · Doug DC862F · Turbine Engine Oil System
  > NR 3 ENGINE STARTED SLOWLY LEAKING OIL. AT 1418Z WITH NR 3 OIL QUANTITY INDICATION OF 1 GALLON AND NR 3 OIL TEMP SLOWLY STARTING TO INCREASE, NR 3 ENGINE WAS SHUTDOWN AS A PRECAUTION. AFTER SHUTDOWN, NR 3 ENGINE OIL QUANTITY CONTINUED TO DECREASE TO ZERO WITH
- [SDR IXXA20120218003O](https://openairdocs.org/sdr/IXXA20120218003O.md): Battery · inoperative · Feb 18, 2012 · N41CX · Doug DC862F · Emergency Equipment
  > DURING PREFLIGHT INSPECTION, FOUND RT EMERGENCY FLASHLIGHT INOPERATIVE. MX REPLACED EMERGENCY FLASHLIGHT BATTERY. OPS CHECKED GOOD IAW MM 25-60-0.
- [SDR IXXA1100740](https://openairdocs.org/sdr/IXXA1100740.md): Fan · failed · Nov 2, 2011 · N41CX · Doug DC862F · Air Distribution Fan
  > DURING DESCENT, FLIGHT CREW SWITCHED ON RT RECIRCULATION FAN AND NOTICED A STRONG ELECTRICAL ODOR. FAN WAS SUBSEQUENTLY TURNED OFF AND ELECTRICAL ODOR DISSIPATED. MX TROUBLESHOT AND R & R RT RECIRCULATION FAN IAW MM 21-21-1.
- [SDR IXXA110069O](https://openairdocs.org/sdr/IXXA110069O.md): Transceiver · defective · Oct 13, 2011 · N41CX · Doug DC862F · Weather Radar System
  > DURING CLIMB OUT, THE WEATHER RADAR FAILED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED WEATHER RADAR TRANSCEIVER, OPS CHECK GOOD IAW MM 34-40-02. ACFT WAS RETURNED TO SERVICE.
- [SDR IXXA20110813001](https://openairdocs.org/sdr/IXXA20110813001.md): Skin · corroded · Aug 13, 2011 · N41CX · Doug DC862F · Vertical Stabilizer, Plate/Skin
  > DURING ROUTINE C-CHECK INSP, FOUND VERTICAL STABILIZER RT LATERAL SKIN CORRODED AT STA ZR 35.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IA
- [SDR IXXA20110812001](https://openairdocs.org/sdr/IXXA20110812001.md): Spar · corroded · Aug 12, 2011 · N41CX · Doug DC862F · Vertical Stabilizer, Spar/Rib
  > DURING ROUTINE C-CHECK INSP FOUND RT VERTICAL STABILIZER REAR SPAR CORRODED AT STA ZR 45.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED STRAP AND FILLER. CLEANED, TREATED, PRIMED AREA
- [SDR IXXA20110811001](https://openairdocs.org/sdr/IXXA20110811001.md): Skin · corroded · Aug 11, 2011 · N41CX · Doug DC862F · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSP, FOUND LT WING T/E UPPER SKIN CORRODED AT STA XW 761.695 - 736.500. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED REPAIR PARTS AS NEEDED. CLEANED, TREATED, PRIMED ARE
- [SDR IXXA20110810003](https://openairdocs.org/sdr/IXXA20110810003.md): Skin · cracked · Aug 10, 2011 · N41CX · Doug DC862F · Ailerons
  > DURING ROUTINE C-CHECK INSP, FOUND RT INBD AILERON UPPER SKIN CRACKED AT STATION XA 603.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARTS. PERFORMED RT INBD AILERON B
- [SDR IXXA20110810002](https://openairdocs.org/sdr/IXXA20110810002.md): Skin · cracked · Aug 10, 2011 · N41CX · Doug DC862F · Ailerons
  > DURING ROUTINE C-CHECK INSP, FOUND RT OTBD AILERON LOWER SKIN CRACKED AT STA XA 610.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARTS. PERFORMED RT OTBD AILERON BALA
- [SDR IXXA20110810001](https://openairdocs.org/sdr/IXXA20110810001.md): Angle · cracked · Aug 10, 2011 · N41CX · Doug DC862F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C-CHECK, INSP FOUND NR 60 ACCESS DOOR BEAM AFT PRESS BULKHEAD CRACKED BOTTOM LINE-0. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED STOP HOLE AT CRACK END. FABRICATED ANGLES FORMED AND PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRI
- [SDR IXXA11SMN103S](https://openairdocs.org/sdr/IXXA11SMN103S.md): Skin · corroded · Aug 9, 2011 · N41CX · Doug DC862F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK, FOUND EXTERNAL SKIN CORRODED AT BS 902.00- 910.000 LONGERON 19 - 21RT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPANCIES FOUND. FABRICATED NEW SKIN, REPAIR DOUBLER AND FILLER
- [SDR IXXA20110809004](https://openairdocs.org/sdr/IXXA20110809004.md): Skin · corroded · Aug 9, 2011 · N41CX · Doug DC862F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND EXTERNAL SKIN CORRODED AT STA 1100.000 LONGERON 21 RT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, REPAIR DOUBLER AND FILLER. CLEANED, TREATED,
- [SDR IXXA20110809003](https://openairdocs.org/sdr/IXXA20110809003.md): Skin · corroded · Aug 9, 2011 · N41CX · Doug DC862F · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND LT WING UPPER SKIN CORRODED AT STATION XRS 358.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, REPAIR DOUBLER AND MACHINE TAPERED DOUBLER. CLEA
- [SDR IXXA20110809001](https://openairdocs.org/sdr/IXXA20110809001.md): Skin · corroded · Aug 9, 2011 · N41CX · Doug DC862F · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND LT WING UPPER SKIN AFT PART CORRODED AT STA XRS 70.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, REPAIR DOUBLER AND MACHINE TAPERED DOUBL
- [SDR IXXA20110808002](https://openairdocs.org/sdr/IXXA20110808002.md): Skin · corroded · Aug 8, 2011 · N41CX · Doug DC862F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND FORWARD CARGO COMPARTMENT INTERNAL SKIN CORRODED AT STA 600.000, LONGERON 36. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, REPAIR DOUBLER
- [SDR IXXA20110808001A](https://openairdocs.org/sdr/IXXA20110808001A.md): Skin · cracked · Aug 8, 2011 · N41CX · Doug DC862F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND FUSELAGE NOSE SECTION LOWER SKIN CRACKED AT STA 260.000, LONGERON 34 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, REPAIR DOUBLER AND F
- [SDR IXXA20110808001](https://openairdocs.org/sdr/IXXA20110808001.md): Skin · cracked · Aug 8, 2011 · N41CX · Doug DC862F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSP, FOUND NLG CORNER LOWER SKIN CRACKED AT STATION 208.000, LONGERON 33 LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR DOUBLER AND FILLER. CLEANED,
- [SDR IXXA20110801002](https://openairdocs.org/sdr/IXXA20110801002.md): Structure · misrepaired · Aug 1, 2011 · N41CX · Doug DC862F · Fuselage Main, Structure
  > DURING ROUTINE C-CHECK INSP, FOUND IMPROPER REPAIR AT STA FS 255 LONGERON 33.5 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR DOUBLER, FILLER, AND FINGER DOUBLERS. CLEANED
- [SDR IXXA201108SMN095S](https://openairdocs.org/sdr/IXXA201108SMN095S.md): Angle · cracked · Aug 1, 2011 · N41CX · Doug DC862F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSP, FOUND ANGLE CRACKED AT STA FS 975 LONGERON 24 LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR ANGLE. CLEANED, TREATED, PRIMED AREA AND REPAIR. INSTALLED NEW FASTENERS AND REPAIR ANGLE IA
- [SDR IXXA100059O](https://openairdocs.org/sdr/IXXA100059O.md): Coupler · defective · Dec 17, 2010 · N41CX · Doug DC862F · HF Communications System
  > DURING CRUISE, NR1 HF RADIO WILL NOT CHANNELIZE AND HAD NO RECEPTION, NR 2 HF RADIO WOULD NOT WORK. THE CREW RETURNED TO DEPARTURE WITH OUT FURTHER INCIDENT. MX REPLACED NR1 ACCESSORY COUPLER AND 2 COAX CONNECTORS ON THE NR2 ACCESSORY COUPLER. OPS CHECK GOOD
- [SDR IXXA100054O](https://openairdocs.org/sdr/IXXA100054O.md): Duct · disconnected · Oct 28, 2010 · N41CX · Doug DC862F · Pneumatic Distribution System
  > DURING CRUISE, NR 4 ENGINE GENERATOR UNPARALLEL LIGHT FOLLOWED BY GENERATOR DRIVE OIL LIGHT, MANIFOLD PRESSURE LIGHT ILLUMINATED WITH HIGH PRESSURE MANIFOLD AIR PRESSURE OVERTEMP LIGHT CAME ON, LOSS OF EGT INDICATION, ZERO FUEL FLOW AND ZERO EPR. THE CREW SHUT
- [SDR IXXA100052S](https://openairdocs.org/sdr/IXXA100052S.md): Skin · cracked · Oct 2, 2010 · N41CX · Doug DC862F · Fuselage Main, Plate/Skin
  > DURING INSP, FOUND SKIN CRACKED AT STA 255 BETWEEN LONGERONS 33 AND 34 RT SIDE. INSTALLED INTERIM REPAIR IAW REA D853-60270.
- [SDR IXXA090077O](https://openairdocs.org/sdr/IXXA090077O.md): O-Ring · damaged · Dec 21, 2009 · N41CX · Doug DC862F · Hydraulic System, Main
  > DURING CRUISE, ACFT LOST HYD FLUID TO THE STANDPIPE LEVEL. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MX INSPECTED THE HYD SYS AND FOUND THE O-RING ON THE NR 2 SYS HYD PUMP PRESSURE LINE LEAKING. THE O-RING WAS REPLACED, THE LEAK AND OPS CHECKS WERE GOOD AN
- [SDR IXXA090072O](https://openairdocs.org/sdr/IXXA090072O.md): Engine · power loss · Dec 14, 2009 · N41CX · Doug DC862F · Engine (Turbine/Turboprop)
  > DURING TAKEOFF FROM WSAP NR 4 ENG FAILED TO PRODUCE TAKEOFF PWR. THE CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX PERFORMED POWER RUN AND ACCELERATION CHECK. OPS CHECK GOOD IAW ERH 72.01.1. ACFT WAS RETURNED TO SERVICE.
- [SDR IXXA090068O](https://openairdocs.org/sdr/IXXA090068O.md): Prbc · dry · Nov 29, 2009 · N41CX · Doug DC862F · Turbine Engine Compressor Section
  > DURING CLIMB OUT, THE CREW HEARD A LOUD BANG, F/A REPORTED A FLASH ON LT SIDE. THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX INSPECTED BOTH NR 1 AND NR 2 ENGINE'S, LUBED THE PRBC'S. OPS CHECK GOOD IAW MM 72-00, ERH 70.01, ERH 75.01, AND MM 12-80-0.
- [SDR IXXA090063O](https://openairdocs.org/sdr/IXXA090063O.md): Reservoir · low · Oct 25, 2009 · N41CX · Doug DC862F · Hydraulic Reservoir, Main
  > DURING CLIMB OUT FROM RJTY THE CREW NOTICE HYDRAULIC FLUID DROPPED TO STANDPIPE WITH RESERVOIR LOW PRESSURE LIGHT ON, THE CREW RETURNED TO RJTY WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED HYDRAULIC RESERVOIR. OPERATIONAL CHECK GOOD IAW MM 12-30-1, ERH 70.01
- [SDR IXXA090055O](https://openairdocs.org/sdr/IXXA090055O.md): Fan · defective · Sep 30, 2009 · N41CX · Doug DC862F · Air Distribution Fan
  > DURING C CHECK TEST FLIGHT FROM SPLP THE LEFT HAND RECIRCULATION FAN EMITTED ELECTRICAL ODOR. THE CREW TURNED OFF LEFT RECIRCULATION FAN. THEY RETURNED TO SPLP WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT HAND RECIRCULATION FAN. OPERATIONAL CHECK
- [SDR IXXA09SMN094S](https://openairdocs.org/sdr/IXXA09SMN094S.md): Skin · corroded · Aug 21, 2009 · N41CX · Doug DC862F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSP, FOUND FUSELAGE EXTERNAL SKIN CORRODED AT STA 960.000 LONGERON 18-19 RT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASETNERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. PERFORMED NDT INSP. NO CRACK OR CO
- [SDR IXXA09SMN093S](https://openairdocs.org/sdr/IXXA09SMN093S.md): Skin · dented · Aug 13, 2009 · N41CX · Doug DC862F · Ailerons
  > DURING ROUTINE C CHECK INSPECTION FOUND LEFT WING INBOARD AILERON UPPER SKIN DENTED AT STATION XA 515.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED,
- [SDR IXXA09SMN092S](https://openairdocs.org/sdr/IXXA09SMN092S.md): Skin · cracked · Aug 13, 2009 · N41CX · Doug DC862F · Ailerons
  > DURING ROUTINE C CHECK INSPECTION FOUND LT WING INBOARD AILERON UPPER SKIN CRACKED AT STATION XW 563.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED,
- [SDR IXXA09SMN091S](https://openairdocs.org/sdr/IXXA09SMN091S.md): Skin · corroded · Aug 13, 2009 · N41CX · Doug DC862F · Rudder, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION FOUND RUDDER LT SKIN CORRODED AT STATION ZR 238.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING SKIN. FABRICATED NEW SKIN AND BONDED DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, AND PRIMED AREA
- [SDR IXXA09SMN090S](https://openairdocs.org/sdr/IXXA09SMN090S.md): Fitting · cracked · Aug 13, 2009 · N41CX · Doug DC862F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION FOUND MAIN CARGO COMPARTMENT SUB FLOOR FITTING CRACKED AT STATION 798.000 LBL 24". REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA AND FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-0, DC8 SRM 51-1-8B
- [SDR IXXA09SMN089S](https://openairdocs.org/sdr/IXXA09SMN089S.md): Skin · corroded · Aug 11, 2009 · N41CX · Doug DC862F · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND RT WING L/E LWR SKIN CORRODED AT STA XFS 566.250. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACK OR CORROSION. FABRICATED DOUBLER, AND FILLER. CLEANED, TREATED, AND PRIMED AREA AN
- [SDR IXXA09SMN087S](https://openairdocs.org/sdr/IXXA09SMN087S.md): Spar Cap · corroded · Aug 11, 2009 · N41CX · Doug DC862F · Wing Spar
  > DURING ROUTINE C-CHECK INSP, FOUND RUDDER RT SIDE FRONT SPAR CAP CORRODED AT STA ZR 323.000. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED DAMAGED SPAR CAP. FABRICATED NEW SPAR CAP. CLEANED, TREATED, AND PRIMED AREA AND NEW SPAR CAP. INSTALLED NEW SPAR CAP
- [SDR IXXA09SMN088S](https://openairdocs.org/sdr/IXXA09SMN088S.md): Longeron · corroded · Aug 11, 2009 · N41CX · Doug DC862F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C CHECK INSPECTION FOUND MAIN CARGO COMPARTMENT CORROSION ON LONGERON 22 RT AT STATION 1530.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED LONGERON. CLEANED, TREATED, AND PRIMED AREA AND LONGERON. INSTALLED NEW LONGERON IAW SRM CHA
- [SDR IXXA09SMN086S](https://openairdocs.org/sdr/IXXA09SMN086S.md): Angle · corroded · Aug 11, 2009 · N41CX · Doug DC862F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C CHECK INSPECTION FOUND MAIN CARGO COMPARTMENT AFT RING ANGLE CORRODED AT STATION 1530.000 LONGERON 26-28 LT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR ANGLE. FABRICATED REPAIR ANGLE SPLICE. CLEANED, TREATED, AND PRIMED AR

Next page: https://openairdocs.org/deregistered/N41CX-2021-01-30/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 = 'N41CX' AND deregistration_id = 'N41CX-2021-01-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N41CX-2021-01-30/reports

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