# Service difficulty reports: N68041, cancelled Sep 26, 2013

A list on [N68041, cancelled Sep 26, 2013](https://openairdocs.org/deregistered/N68041-2013-09-26.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 3 · 115 reports

- [SDR 22AA20081101](https://openairdocs.org/sdr/22AA20081101.md): Anti-Ice Valve · inoperative · Nov 18, 2008 · N68041 · Doug DC1010F · Cabin Cooling System
  > STRONG BURNING SMELL COMING FROM NR 1 AIR CONDITIONING PACK AFTER TAKEOFF AT HIGH POWER SETTINGS, PACK INLET & DISCHARGE TEMPERATURE NORMAL NR 1 AIR CONDITIONING PACK OPERATION NORMAL ON GROUND. REMOVED AND REPLACED WATER SEPARATOR CONICAL COALESCER IAW MM 21
- [SDR ARWA20080803](https://openairdocs.org/sdr/ARWA20080803.md): Windshield · shorted · Aug 29, 2008 · N68041 · Doug DC1010 · Windshield/Door Rain/Ice Removal
  > FIRST OFFICER`S WINDSHIELD STARTED ARCING, POWER REMOVED. OUTER PANEL CRACKED, CHECK LIST COMPLETED. REMOVED AND REPLACED FIRST OFFICER`S WINDSHIELD PANEL IAW DC-10 MM 56-11-00, OPERATIONAL CHECK NORMAL. REMOVED AND REPLACED RT WINDOW HEAT CONTROLLER IAW MM
- [SDR ARWA20080701](https://openairdocs.org/sdr/ARWA20080701.md): B-Nut · loose · Jul 17, 2008 · N68041 · Doug DC1010 · Rudder Control System
  > NR 1 HYDRAULIC SYSTEM LOSS PRESSURE AND QUANTITY ZERO. RUDDER STAND-BY POWER OFF, IGHT ON. REPAIRED LINE AND FOUND LOOSE B-NUT AT LT HORIZONTAL STABILIZER TRIM MOTOR. TIGHTENED B-NUT IAW DEIO M/M 20-10-0. PERFORMED OPERATIONAL CHECK, FOUND NORMAL IAW DEIO
- [SDR ARWA20080601](https://openairdocs.org/sdr/ARWA20080601.md): Transmitter · failed · Jun 4, 2008 · N68041 · Doug DC1010 · Trailing Flap Position Indicating System
  > DURING TAXI TAKEOFF CONFIGURATION TEST FAILED. REMOVED AND REPLACED LT OUTBOUND FLAPS POSITION TRANSMITTER IN ACCORDANCE WITH DC10-M/M 27-54-03, OPERATIONAL CHECK FOUND NORMAL IN ACCORDANCE WITH DC10 M/M 27-54-03. (A)
- [SDR ARWA20080404](https://openairdocs.org/sdr/ARWA20080404.md): Computer · malfunctioned · Apr 13, 2008 · N68041 · Doug DC1010 · Inertial Guidance System
  > ON TAXI, BOTH CAPTAIN AND FIRST OFFICER'S FMAS WENT TO G/A INSTEAD OF TAKEOFF. T/O WHEN G/A BUTTON PUSHED. SWAPPED BOTH NR 1 AND NR 2 PITCH GUIDANCE COMPONENT FOR DISPATCH IN ACCORDANCE WITH M/M 22-11-02. CHECK OK IN ACCORDANCE WITH M/M 22-10-00 AND M/M 34-
- [SDR ARWA20080301](https://openairdocs.org/sdr/ARWA20080301.md): Altimeter · intermittent · Mar 2, 2008 · N68041 · Doug DC1010 · Altimeter, Barometric/Encoder
  > FIRST OFFICER'S RADIO ALTIMETER HAS FLAG IN VIEW INTERMITTENT ON THE GROUND; OK IN FLIGHT. REMOVED AND REPLACED FIRST OFFICER'S ALTIMETER AND CHECK TEST FOUND NORMAL IN ACCORDANCE WITH M/M 34-42-02.
- [SDR ARWA20080103](https://openairdocs.org/sdr/ARWA20080103.md): Controller · malfunctioned · Jan 25, 2008 · N68041 · Doug DC1010 · Altitude Controller
  > ALTITUDE HOLD SLOW TO ENGAGE. PERFORMED ALTITUDE HOLD SYSTEM OPERATIONAL CHECK IN ACCORDANCE WITH M/M 22-00-03, FOUND NORMAL AT THIS TIME.
- [SDR ARWA20071203](https://openairdocs.org/sdr/ARWA20071203.md): Cadc · malfunctioned · Dec 15, 2007 · N68041 · Doug DC1010 · Airspeed/Mach Indicator
  > ABORTED AT 85 KTS DUE TO NO AIRSPEED INDICATION ON CAP SIDE. REMOVED AND REPLACED CADC IN ACCORDANCE WITH M/M 34-16-01. OPERATIONAL CHECK GOOD IN ACCORDANCE WITH M/M 34-16-00 AND M/M 34-11-00.
- [SDR ARWA20070902](https://openairdocs.org/sdr/ARWA20070902.md): Engine · flamed out · Sep 25, 2007 · N68041 · Doug DC1010 · Engine (Turbine/Turboprop)
  > NR 1 ENGINE FLAMED OUT; ENGINE FAILED/SHUTDOWN IN FLIGHT CHECKLIST COMPLETED (ENGINE VIBRATION STOPPED) SHUTDOWN O505Z; WINDMILLING O.P. 10 PSI. TROUBLESHOOT FUEL SYSTEM AND FOUND METAL DEBRIE IN FUEL FILTER. REMOVED AND REPLACED FUEL PACKAGE IN ACCORDANCE W
- [SDR ARWA20070803](https://openairdocs.org/sdr/ARWA20070803.md): Connector · damaged · Aug 22, 2007 · N68041 · Doug DC1010 · Ice/Rain Protection System Wiring
  > LEFT STATIC PORT HEAT AND RIGHT STATIC PORT HEAT AND LEFT ANGLE OF ATTACK C/B`S POPPED WITH LIGHT SMOKE FROM AROUND THE FIRE HANDLES. REMOVED AND REPLACED CONNECTOR FROM HEATER CONTROLLER IN ACCORDANCE WITH M/M 20-30-02, AND REMOVED AND REPLACED HEATER CONTRO
- [SDR ARWA20070601](https://openairdocs.org/sdr/ARWA20070601.md): Outflow Valve · lack of lube · Jun 4, 2007 · N68041 · Doug DC1010 · Pressure Regulator/Outflow Valve
  > WITH ALL 3 PACKS OPERATING, UNABLE TO MAINTAIN CABIN ALTITUDE BELOW 10,000. OUTFLOW VALVE FULL CLOSED (MANUALLY). FOUND THRUST RECOVERY VALVE LOCKED OPEN; LUBED OUTFLOW VALVE MECHANISM; CHECK MANUALLY OPERATION NORMAL ON GROUND IN ACCORDANCE WITH DC-10 M/M 2
- [SDR ARWA20070401](https://openairdocs.org/sdr/ARWA20070401.md): Hose · damaged · Apr 21, 2007 · N68041 · Doug DC1010 · Hydraulic System, Main
  > DEPARTING MNMG, LOST HYDRAULIC PRESSURE AND QUANTITY NR 3 SYSTEM; PERFORMED APPLICABLE CHECKLIST, AND CONTINUED TO MROC. REMOVED AND REPLACED RT MAIN LANDING GEAR TRIM CYLINDER HYDRAULIC HOSE ASSEMBLY IN ACCORDANCE WITH M/M 20-40-02; SERVICED NR 3 HYDRAULIC S
- [SDR ARWA20070304](https://openairdocs.org/sdr/ARWA20070304.md): Windshield · cracked · Mar 22, 2007 · N68041 · Doug DC1010 · Windshield/Door Rain/Ice Removal
  > DURING CRUISE RT WINDSHIELD CRACKED. REMOVED AND REPLACED RT WINDSHIELD PANEL IN ACCORDANCE WITH M/M 56-11-00. OPERATIONAL CHECK PERFORMED IN ACCORDANCE WITH M/M 30-41-00 AND M/M 30-42-00, FOUND NORMAL OPERATION.
- [SDR ARWA20070301](https://openairdocs.org/sdr/ARWA20070301.md): Window · dislodged · Mar 8, 2007 · N68041 · Doug DC1010 · Flight Compartment Windows
  > ON TAKEOFF ROLL,F/O SLIDING WINDOW CAME OFF TRACK CAUSING LOW SPEED ABORT. PREFLIGHT INSPECTION OVER CENTER LOCKED AND NORMAL. LUBRICATED INSPECTED AND ADJ. SLIDING WINDOW CHECKED OPERATION SEVERAL TIMES AND FOUND NORMAL IAW DC-10 MM 56-12-00.
- [SDR ARWA20061103](https://openairdocs.org/sdr/ARWA20061103.md): Fitting · corroded · Nov 15, 2006 · N68041 · Doug DC1010 · Wing, Center Box
  > DURING AN "A" CHECK, THE FOLLOWING WAS FOUND; RT MAIN LANDING GEAR WHEEL WELL STATION 1381; SLANT PANEL PRESSURE BULKHEAD CAP ANGLE/STRUCTURAL FRAME HAS CORROSION ON BOTH INBOARD AND OUTBOARD LOWER CORNERS; WING CENTER SECTION REAR SPAR JOINT WITH RT PANEL, TH
- [SDR ARWA20061102](https://openairdocs.org/sdr/ARWA20061102.md): Frame · corroded · Nov 15, 2006 · N68041 · Doug DC1010 · Wing, Center Box
  > DURING AN "A" CHECK INSPECTION, THE FOLLOWING WAS FOUND; LT MAIN LANDING WHEEL WELL AT STATION 1381; SLANT PANEL PRESSURE BULKHEAD SHIMS INSTALLED AROUND CAP ANGLE/STRUCTURAL FRAME ARE DISPLACED DUE TO PRESENT CORROSION AND BROKEN RIVETS; FRAME STRUCTURE INBOA
- [SDR ARWA20061101](https://openairdocs.org/sdr/ARWA20061101.md): Engine · malfunctioned · Nov 3, 2006 · N68041 · Doug DC1010 · Engine (Turbine/Turboprop)
  > NR 1 ENGINE FAILED TO ACCELERATE PASS 80 PERCENT N1; ABORTED TAKEOFF AT 75 KTS. REMOVED AND REPLACED MAIN FUEL PUMP AND FUEL CONTROL ASSEMBLY IN ACCORDANCE WITH M/M 73-12-01; PERFORMED LEAK CHECK, NO LEAKS NOTED; PERFORMED ENGINE RUN AND TRIM IN ACCORDANCE WI
- [SDR ARWA20060801](https://openairdocs.org/sdr/ARWA20060801.md): Pump · unknown · Aug 2, 2006 · N68041 · Doug DC1010 · Fuel Control/Turbine Engines
  > NR 2 ENGINE WOULD NOT SPOOL UP ON THE RUNWAY. REMOVED AND REPLACED NR 2 ENGINE MEC/FUEL PUMP PACKAGE IN ACCORDANCE WITH M/M 73-45-01 AND M/M 73-20-01; FOUND NORMAL ON ENGINE RUN-UP IN ACCORDANCE WITH M/M 71-00-00.
- [SDR ARWA20060601](https://openairdocs.org/sdr/ARWA20060601.md): Engine · erratic · Jun 4, 2006 · N68041 · Doug DC1010 · Engine (Turbine/Turboprop)
  > DURING INITIAL CLIMBOUT OF MIAMI, ENGINE NR 1 EGT BECAME VERY ERRATIC AND FLUCTUATED INTO AN OVERTEMP CONDITIONS; RESET C/B, NO HELP. REMOVED AND REPLACED NR 1 ENGINE IAW ARROW AIR MSG-3 DC10 J/C 141R7101M. OPERATIONAL CHECK NORMAL IAW M/M 72-00-00.
- [SDR ARWA20060502](https://openairdocs.org/sdr/ARWA20060502.md): Antenna · failed · May 27, 2006 · N68041 · Doug DC1010 · Weather Radar System
  > BOTH RADARS INOPERATIVE, ANTENNA FAIL DISPLAYED ON BOTH RADAR SCREENS. REMOVED AND REPLACED WEATHER ANTENNA IAW MM 34-41-01 GROUND TEST (OPERATIONAL CHECK) NORMAL IAW MM 34-41-00.
- [SDR ARWA20060101](https://openairdocs.org/sdr/ARWA20060101.md): Engine · stalled · Jan 11, 2006 · N68041 · Doug DC1010 · Turbine Engine Compressor Section
  > LOG PAGE NR 117483. NR 3 ENGINE COMPRESSOR STALLED. SHUTDOWN ENGINE. (SEE LOG PAGE NR 117486) REMOVED NR 3 ENGINE DUE TO COMPRESSOR STALLED AND REPLACED NR 3 ENGINE IAW ARROW AIR MM CHECK CARD NR 143-R7101; RUN UP CHECK GOOD. ACCOMPLISHED RED BORDER NR 18948
- [SDR ARWA20051203](https://openairdocs.org/sdr/ARWA20051203.md): Fitting · broken · Dec 21, 2005 · N68041 · Doug DC1010 · Landing Gear Door Retract Section
  > LOG PAGES NR 116686 AND NR 116688. ON SERVICE CHECK FOUND LT MAIN LANDING GEAR DOOR ROLLER ASSEMBLY LOWER SUPPORT FITTING BROKEN. REMOVED AND REPLACED LT MAIN LANDING GEAR DOOR IAW MM 32-14-01. OPERATIONAL CHECK NORMAL IAW MM 32-10-01.
- [SDR ARWA20050912](https://openairdocs.org/sdr/ARWA20050912.md): Cable · damaged · Sep 28, 2005 · N68041 · Doug DC1010 · Passenger/Crew Doors
  > MAIN CABIN L1 DOOR WITH DOOR OPEN, NO WARNING LIGHT. UPON INSPECTION OF DOOR MECHANISM FOUND DAMAGED CABLES AT AFT SECTION OF L1 DOOR. REMOVED DAMAGED SECTIONS IAW M/M 52-10-02; INSTALLED PASSENGER DOOR DRIVE CABLE IAW M/M 52-10-02. OPERATIONAL CHECK OK.
- [SDR ARWA20050911](https://openairdocs.org/sdr/ARWA20050911.md): Wire Harness · damaged · Sep 20, 2005 · N68041 · Doug DC1010 · Engine Indicating System Wiring
  > NR 2 EGT FAILED IN FLIGHT. REMOVED AND REPLACED EGT LEAD JUNCTION IN ACCORDANCE WITH M/M 77-21-02. SYSTEM TESTED IN ACCORDANCE WITH M/M 77-21-01 AND 77-21-00; FOUND NORMAL.
- [SDR ARWA2005050A](https://openairdocs.org/sdr/ARWA2005050A.md): Target · out of adjust · May 17, 2005 · N68041 · Doug DC1010 · Landing Gear Retraction/Extension System
  > AFTER GEAR RETRACTION LEFT GEAR; LIGHT REMAINED ILLUMINATED; PERFORMED CHECK LIST, NO HELP, OBSERVED SPEED LIMITS (GEAR). PERFORMED T/S FOUND TARGET SWITCH BROKEN. REMOVED AND REPLACED TARGET BRACKET IN ACCORDANCE WITH M/M 32-14-01. PERFORMED MAIN LANDING GEA
- [SDR ARWA20050501](https://openairdocs.org/sdr/ARWA20050501.md): Igniter · defective · May 1, 2005 · N68041 · Doug DC1010 · Spark Plug/Igniter
  > DURING ENGINE START NR 1 ENGINE IGNITION -A- INOPERATIVE; TRANSFER TO DMI NR 19182 AS PER MEL 74-1-1 CATEGORY-C. REMOVED AND REPLACED NR 1 ENGINE -A- IGNITOR IN ACCORDANCE WITH M/M 74-20-02; OPERATIONAL CHECK NORMAL.
- [SDR ARWA20050405](https://openairdocs.org/sdr/ARWA20050405.md): Line · leaking · Apr 27, 2005 · N68041 · Doug DC1010 · Hydraulic System, Main
  > ON POST FLIGHT, FOUND EVIDENCE OF HYDRAULIC LEAK AT RT WING ROOT AREA AT TOP OF RT MAIN LANDING GEAR AREA. CUT; FABRICATED; AND INSTALLED PERMANENT LINE AT RT WING ROOT AT TOP OF RT MAIN LANDING GEAR IN ACCORDANCE WITH M/M 20-10-01. NO LEAKS NOTED.
- [SDR ARWA20050401](https://openairdocs.org/sdr/ARWA20050401.md): Wire · broken · Apr 3, 2005 · N68041 · Doug DC1010 · Airspeed/Mach Indicator
  > DURING INITIAL TAKEOFF ROLL, NO AIR SPEED INDICATION ON CAPTAIN'S SIDE, ABORTED TAKEOFF AT 90 KNOTS. REPAIRED BROKEN WIRE AT CAPTAIN'S AIRSPEED INDICATION CONNECTOR (P1-102T) IN ACCORDANCE WITH M/M 20-30-00. PERFORMED DADC BITE TEST IN ACCORDANCE WITH M/M 34
- [SDR ARWA20050207](https://openairdocs.org/sdr/ARWA20050207.md): Switching Unit · malfunctioned · Feb 21, 2005 · N68041 · Doug DC1010 · Air Data Computer
  > AIRSPEED FLAGGED AT HOLDING POINT RUNWAY 9, BARBER POLE STUCK AT 250 IAS NEEDLE FLUCTUATES BETWEEN ZERO (O) AND SIXTY (60) KTS. REMOVED AND REPLACED CADC SWITCHING UNIT IN ACCORDANCE WITH MM 34-16-03. OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH MM 34-16-00.
- [SDR ARWA20050107](https://openairdocs.org/sdr/ARWA20050107.md): Door · unsecure · Jan 26, 2005 · N68041 · Doug DC1010 · Electrical/Electronic Compartment Doors
  > AFTER TAKEOFF UNABLE TO PRESSURIZE. SECURED AFT AVIONICS DOOR IN ACCORDANCE WITH MM 52-00-00 AND PRESSURIZED AIRCRAFT IN ACCORDANCE WITH MM 21-30-00. OPERATIONAL CHECK NORMAL.
- [SDR ARWA20050104](https://openairdocs.org/sdr/ARWA20050104.md): Engine · failed · Jan 16, 2005 · N68041 · Doug DC1010 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE FAILED ON ROTATION. ENGINE SHUTDOWN IN ACCORDANCE WITH CHECKLIST. AIRCRAFT RETURNED TO MSLP WITHOUT ANY FURTHER INCIDENT. ACCOMPLISHED RED BORDER 019056; REMOVED AND REPLACED NR 2 ENGINE IN ACCORDANCE WITH ARROW AIR DC-10 WORK CARD 142R7101M. P
- [SDR ARWA20050103](https://openairdocs.org/sdr/ARWA20050103.md): Adc · malfunctioned · Jan 13, 2005 · N68041 · Doug DC1010 · Airspeed/Mach Indicator
  > ABORTED TAKEOFF AT 75 KTS DUE TO NO AIRSPEED INDICATION AND FLAG ON FIRST OFFICER'S AIRSPEED INDICATOR. RESET ANALOGUE DIGITAL CONVERTER (ADC) AND PERFORMED TEST ACCORDING TO MM 34-130. OPERATIONAL CHECK NORMAL.
- [SDR RRXA001087](https://openairdocs.org/sdr/RRXA001087.md): Engine · failed · Dec 10, 2000 · N68041 · Doug DC1010F · Engine (Turbine/Turboprop)
  > AFT V1 NR 1 ENGINE EGT WENT TO 910 DEG, N1 FELL TO 82 PERCENT, N2 FELL TO 85 PERCENT, FUEL FLOW INCREASED TO ABOUT 15,000LBS PER HR. NO LIMITS OR RED LINES WERE APPROACH EWD. LEVELED OFF AT 18,000FT, EGT AND FUEL FLOW CONTINUED TO INCREASE. EVENTUALLY PULLE
- [SDR RRXA001065](https://openairdocs.org/sdr/RRXA001065.md): Actuator · failed · Oct 11, 2000 · N68041 · Doug DC1010F · Aileron Control System
  > AS ACFT SPEED INCREASES ACFT WANTS TO ROLL TO THE RIGHT FLAPS/SLATS RETRACTED. REMOVED AND REPLACED RIGHT INBOARD AILERON ACTUATOR IAW DC-10 MM 27-13-01 PAGES 401 - 407. OPS AND LEAK CHECKS GOOD.
- [SDR RRXA001061](https://openairdocs.org/sdr/RRXA001061.md): Floor Panel · damaged · Sep 30, 2000 · N68041 · Doug DC1010F · Fuselage Floor Panel
  > SEVERAL HOLES IN FLOOR CENTER OF POSITIONS 3R & 3L & AFT OF BALLMAT (FACING AFT). *S/D* INSTALLED NR 3 POS CENTER PNL IAW DC-10 M/M 25-50-67.
- [SDR RRXA001060](https://openairdocs.org/sdr/RRXA001060.md): Angle · broken · Sep 29, 2000 · N68041 · Doug DC1010F · Landing Gear Position and Warning
  > RIGHT LANDING GEAR RED LIGHT ON AFTER GEAR RETRACT. WHILE T/S FOUND DOOR STRIKER BROKEN OFF. REPLACED DOOR STRIKER, PERFORMED OPS CHECK IAW DC-10-10 M/M 32-34-03 ITEMS 17, 18, 19, 20, SYS OPS CHECKS GOOD.
- [SDR CALA9801320](https://openairdocs.org/sdr/CALA9801320.md): Motor · inoperative · Jul 21, 1998 · N68041 · Doug DC1010 · Passenger/Crew Doors
  > THE R-3 DOOR FAILED PNEUMATIC CHECK. THE R-3 DOOR AIR MOTOR WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD.
- [SDR CALA9801205](https://openairdocs.org/sdr/CALA9801205.md): Apu · malfunctioned · Jul 6, 1998 · N68041 · Doug DC1010 · Airborne Auxiliary Power Unit (APU) System
  > THE AIRCRAFT HAD A BRIEF HISTORY OF SMOKE APPEARING IN THE COCKPIT AND CABIN MOMENTARILY WHILE IN FLIGHT. THE SMOKE DISSIPATED QUICKLY ONCE THE EFFECTED PACK WAS TURNED OFF. THE APU WAS REMOVED AND REPLACED IAW MM 49-00-00, PAGES 401-415. OPERATIONAL CHECKS
- [SDR CALA9800849](https://openairdocs.org/sdr/CALA9800849.md): Floorbeam · corroded · May 13, 1998 · N68041 · Doug DC1010 · Fuselage Main, Floor Beam
  > INTERIOR LOWER LOBE AFT CARGO BILGE CORROSION ON FLOORBEAM STA 1841 UPPER SIDE ABOVE AND UNDER BETWEEN RBL 50 AND LBL 50. TRIMMED OUT CORRODED AREA. FABRICATED AND INSTALLED DOUBLER AND ANGLE PER SRM 57-60-01, 53-16-01, 51-20-00, 53-00-01.
- [SDR CALA9800821](https://openairdocs.org/sdr/CALA9800821.md): Latch · failed · May 11, 1998 · N68041 · Doug DC1010 · Passenger Oxygen System
  > OXYGEN COMPARTMENT DOORS DID NOT OPEN ABOVE THE FOLLOWING SEATS, 1A 1D 1E 2D 16A 16E AND 34G. REPLACED DOORS PER MM 35-20-00.
- [SDR CALA9800823](https://openairdocs.org/sdr/CALA9800823.md): Bulkhead Angle · cracked · May 9, 1998 · N68041 · Doug DC1010 · Fuselage Main, Bulkhead
  > AFT UPPER FUSELAGE AFT BULKHEAD LOWER LEFT ANGLE CRACKED. INSTALLED NEW ANGLE PER SRM 53-40-00 FIG 6 VOL 1.
- [SDR CALA9800822](https://openairdocs.org/sdr/CALA9800822.md): Skin · corroded · May 9, 1998 · N68041 · Doug DC1010 · Fuselage Main, Plate/Skin
  > OVERWING SECTION SWELLING ON UPPER SURFACE LBL 90 BETWEEN STA 1280 TO 1305. SWELLING SKIN TRIMMED OUT, REWORKED AREA, TREATED, PRIMED AND INSTALLED UPPER AND LOWER DOUBLER PER SRM 51-21-01 AND 51-31-01.
- [SDR CALA9800809](https://openairdocs.org/sdr/CALA9800809.md): Angle · cracked · May 7, 1998 · N68041 · Doug DC1010 · Wing Miscellaneous Structure
  > LT WING FUEL STA CRACK (2) AT RT FWD SIDE BETWEEN HI-LOCKS. CRACKED AREA TRIMMED AND BLENDED OUT. INSTALLED DOUBLER PER SRM 57-10-00 AND 51-33-01.
- [SDR CALA9800798](https://openairdocs.org/sdr/CALA9800798.md): Bulbs · failed · May 6, 1998 · N68041 · Doug DC1010 · Emergency Lighting
  > EMERGENCY LIGHTS INOP NEAR FLT ATTEND SEAT 2L, IVS CLOSET, B-ZONE SEATS 29K TO 36K, ABOVE 26K RT OF B-ZONE AND SEATS IN A ZONE. REPLACED BURNT BULBS PER MM 33-50-00.
- [SDR CALA9800775](https://openairdocs.org/sdr/CALA9800775.md): Support · corroded · May 5, 1998 · N68041 · Doug DC1010 · Fuselage Miscellaneous Structure
  > SUPPORT UNDER AFT GALLEY CORRODED STA 1884 TO 2007 RBL 24. REMOVED CORRODED PARTS, FABRICATED NEW PART, TREATED AND INSTALLED PER SRM 53-16-01, 53-60-01, 51-20-00, AND 51-31-01.
- [SDR CALA9800774](https://openairdocs.org/sdr/CALA9800774.md): Rib · cracked · May 5, 1998 · N68041 · Doug DC1010 · Leading Edge Devices
  > FOUND CRACK (2) IN SLAT NUMBER 1 RT. CRACKED RIB REMOVED, INSTALLED NEW RIB ARB1566-502 AS ORIGINAL PER SRM 51-31-01.
- [SDR CALA9800773](https://openairdocs.org/sdr/CALA9800773.md): Support · cracked · May 5, 1998 · N68041 · Doug DC1010 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CRACKED (2) UNDER AFT GALLEY STA 1921 LBL 20 RBL 20. REMOVED CRACKED SUPPORT SECTION. FITTED NEW SECTION PER SRM 51-20-00 AND 51-35-01.
- [SDR CALA9800772](https://openairdocs.org/sdr/CALA9800772.md): Angle · cracked · May 5, 1998 · N68041 · Doug DC1010 · Fuselage Miscellaneous Structure
  > CRACK ON VERTICAL ANGLE OF RIGHT MAIN L/G WHEEL WELL AFT BULKHEAD. REMOVED CRACKED ANGLE, FABRICATED, TREATED, PAINTED, AND INSTALLED NEW ANGLE PER SRM 53-53-01, 51-20-00 AND 51-31-01.
- [SDR CALA9800771](https://openairdocs.org/sdr/CALA9800771.md): Angle · cracked · May 5, 1998 · N68041 · Doug DC1010 · Fuselage Miscellaneous Structure
  > CRACK (2) IN VERTICAL ANGLE LEFT MLG WHEEL WELL AFT BULKHEAD. REMOVED CRACKED ANGLE, FABRICATED, TREATED, PAINTED, AND INSTALLED NEW ANGLE PER SRM 53-53-01, 51-20-00 AND 51-31-01.
- [SDR CALA9800770](https://openairdocs.org/sdr/CALA9800770.md): Angle · cracked · May 5, 1998 · N68041 · Doug DC1010 · Fuselage Miscellaneous Structure
  > CRACK (2) ON SUPPORT ANGLE OF AFT SIDE FITTING (AFT LONGERON) AT RIGHT MAIN LANDING GEAR WHEEL WELL. REMOVED CRACKED ANGLE, FABRICATED, TREATED, PRIMED, AND INSTALLED NEW ANGLE PER SRM 53-53-01, 51-20-00, AND 51-31-01.

Next page: https://openairdocs.org/deregistered/N68041-2013-09-26/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 = 'N68041' AND deregistration_id = 'N68041-2013-09-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N68041-2013-09-26/reports

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