# Service difficulty reports: Douglas DC-8-62F

A list on [Douglas DC-8-62F](https://openairdocs.org/model/douglas-dc-8-62f.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 24 · 1,163 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 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 IXXA20121121031O](https://openairdocs.org/sdr/IXXA20121121031O.md): Valve · stuck · Nov 21, 2012 · N799AL · Doug DC862F · Cabin Temperature Control System
  > ACFT RETURNED TO DEPARTURE, DUE TO NO HEAT IN THE PASSENGER COMPARTMENT. TROUBLESHOT AND FOUND NASI MIX VALVE STUCK IN THE FULL COLD POSITION. R & R MIX VALVE IAW MM 21.04.25. OPS CHECKED GOOD.
- [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 IXXA20120922027O](https://openairdocs.org/sdr/IXXA20120922027O.md): Control Valve · leaking · Sep 22, 2012 · N799AL · Doug DC862F · Hydraulic System, Main
  > DURING FLIGHT, HYDRAULIC QUANTITY LEVEL STARTED SLOWLY DECREASING. ACFT RETURNED TO ORIGINATING STATION. FOUND SLOT CONTROL VALVE LEAKING. R & R PACKING AND O-RINGS IAW MM 20-60-0 AND 27-80-4. SYS OPS AND LEAK CHECKS GOOD IAW MM 27-80-0. SERVICED HYD SYS
- [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 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 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 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 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 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 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 IXXA110055O](https://openairdocs.org/sdr/IXXA110055O.md): Oxygen Mask · torn · Aug 18, 2011 · N799AL · Doug DC862F · Emergency Equipment
  > DURING POST FLIGHT INSP, FOUND F/A DEMO KIT O2 MASK TORN. MX REPLACED O2 MASK IN F/A DEMO KIT IAW MM 16.02.
- [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 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 IXXA110041O](https://openairdocs.org/sdr/IXXA110041O.md): Fan · defective · May 18, 2011 · N799AL · Doug DC862F · Air Distribution Fan
  > DURING CRUISE, THE LT RECIRCULATION FAN EMITTED A BURNED ODOR. THE CREW SHUT OFF THE LT RECIRCULATION FAN AND BURNED ODOR WENT AWAY. THEY LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE LT RECIRCULATION FAN. OPS CHECK GOOD IAW MM 21-21-1. ACFT WAS RETURNED
- [SDR IXXA0041O](https://openairdocs.org/sdr/IXXA0041O.md): Fan · odor · May 18, 2011 · N799AL · Doug DC862F · Air Distribution Fan
  > DURING CRUISE, THE LT RECIRCULATION FAN EMITTED A BURNED ODOR IN COCKPIT. THE CREW SHUTOFF LT RECIRCULATION FAN AND ODOR WENT AWAY. OPEN
- [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 IXXA110034O](https://openairdocs.org/sdr/IXXA110034O.md): Fan · defective · Apr 20, 2011 · N799AL · Doug DC862F · Air Distribution Fan
  > DURING CRUISE, THE RT RECIRCULATION FAN EMMITTING A BURNING ODOR, TURNED OFF THE RT RECIRCULATION FAN AND ODOR WENT AWAY, LANDED WITHOUT FURTHER INCIDENT. MX REPLACED RT RECIRCULATION FAN. OPS CHECK GOOD IAW MM 21-21-1. ACFT WAS RETURNED TO SERVICE.
- [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 IXXA110030O](https://openairdocs.org/sdr/IXXA110030O.md): Csd · defective · Mar 22, 2011 · N799AL · Doug DC862F · AC Generator-Alternator
  > DURING CLIMB OUT, NR 4 GENERATOR BREAKER CYCLED OPEN AND CLOSED SEVERAL TIMES, GENERATOR WOULD NOT CARRY ITS OWN BUSS, VOLTS AND FREQUENCYS OK. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. NR 4 GENERATOR WAS DEFERRED IAW MEL 24-10-01. MX REPLACED

Next page: https://openairdocs.org/model/douglas-dc-8-62f/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 aircraft_model_key = 'DC862F'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/douglas-dc-8-62f/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.