# Service difficulty reports: N867BX, cancelled Dec 20, 2005

A list on [N867BX, cancelled Dec 20, 2005](https://openairdocs.org/deregistered/N867BX-2005-12-20.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 · 51 reports

- [SDR IXXA0300011O](https://openairdocs.org/sdr/IXXA0300011O.md): Engine · worn · Feb 4, 2003 · N867BX · Doug DC863F · Powerplant System
  > AFTER DEPARTURE FROM KBFI ENROUTE TO KPDX CREW NOTICED OIL QUANTITY IN NUMBER 2 ENGINE DROPPED ABNORMALLY. AS A PRECAUTIONARY MEASURE THE #2 ENGINE WAS SHUTDOWN AND AIRCRAFT RETURNED TO KBFI FOR AN UNEVENTFUL LANDING. POSITIVE OIL PRESSURE WAS MAINTAINED THRU
- [SDR IXXA0300006O](https://openairdocs.org/sdr/IXXA0300006O.md): Mechanism · out of adjust · Jan 23, 2003 · N867BX · Doug DC863F · Door Warning System
  > AFTER TAKEOFF GEAR DOORS NOT LATCHED LIGHT ILLUM, AFTER GEAR RETRACTION. CREW PERFORMED UPLATCH CHECK DOORS NOT LATCHED CONTINUED TO BE ILLUM. CREW PERFORMED GEAR CYCLE, DOORS NOT LATCHED LIGHT CONTINUED TO REMAIN ILLUM. CREW NOTED NO BUFFET, YAW OR ABNORMA
- [SDR IXXA0300003O](https://openairdocs.org/sdr/IXXA0300003O.md): Uplock · lack of lube · Jan 7, 2003 · N867BX · Doug DC863F · Landing Gear Door Retract Section
  > AFTER DEPARTURE FROM FWA DURING GEAR RETRACTION DOORS NOT LATCHED LIGHT REMAINED ILLUMINATED. CREW CYCLED GEAR AND LIGHT REMAINED ILLUMINATED, APPROX 3 MINUTES LATER LIGHT EXTINGUISHED. CREW PROCEEDED TO LAX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED
- [SDR IXXA0200009O](https://openairdocs.org/sdr/IXXA0200009O.md): Connector · contaminated · Mar 7, 2002 · N867BX · Doug DC863F · Trailing Edge Flap Control System
  > AFTER TAKEOFF FROM PDX, THE TAKEOFF WARNING HORN SOUNDED WHEN THE LANDING GEAR AND FLAPS WERE RETRACTED AND COULD NOT BE SILENCED. THE FLIGHT RETURNED TO PDX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE FLAP LIMIT SWITCH C
- [SDR IXXA0200008O](https://openairdocs.org/sdr/IXXA0200008O.md): Striker · worn · Mar 6, 2002 · N867BX · Doug DC863F · Landing Gear Position and Warning
  > ENROUTE FROM BFI TO PDX, THE LANDING GEAR NOT LATCH LIGHT ILLUMINATED DURING THE GEAR UPLATCH CHECK. THE FLIGHT CREW CYCLED THE LANDING GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO PDX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPEC
- [SDR IXXA0200007O](https://openairdocs.org/sdr/IXXA0200007O.md): Warning Light · illuminated · Mar 5, 2002 · N867BX · Doug DC863F · Landing Gear Position and Warning
  > ENROUTE FROM TOL TO LAX, AFTER THE LANDING GEAR WAS RETRACTED THE DOOR UNSAFE LIGHT REMAINED ILLUMINATED. THE FLIGHT CREW CYCLED THE LANDING GEAR, PERFORMED A SUCCESSFUL GEAR UP LATCH CHECK, BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED T
- [SDR IXXA0000042](https://openairdocs.org/sdr/IXXA0000042.md): Control Valve · defective · Nov 23, 2000 · N867BX · Doug DC863F · Landing Gear Retraction/Extension System
  > ENROUTE FROM TOL TO DFW, THE GEAR DOOR NOT LATCH LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE GEAR, BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO DFW FOR AN UNEVENTFUL LANDING. MAINTENANCE PERFORMED AN OP
- [SDR IXXA0000035](https://openairdocs.org/sdr/IXXA0000035.md): Harness · misrigged · Oct 7, 2000 · N867BX · Doug DC863F · Landing Gear Position and Warning
  > ENROUTE FROM DFW TO TOL, THE GEAR DOOR NOT LATCH WARNING LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT RETURNED TO DFW FOR AN UNEVENTFUL LANDING. MAINTENANCE PERFORMED A GEAR SWIN
- [SDR IXXA0000034](https://openairdocs.org/sdr/IXXA0000034.md): Uplock Target · loose · Oct 4, 2000 · N867BX · Doug DC863F · Landing Gear Position and Warning
  > EN ROUTE FROM TOL TO DFW, AFTER GEAR RETRACTION THE GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED. THE FLIGHT CREW CYCLED THE LANDING GEAR, THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO DFW FOLLOWING COMPANY PROCEDURES FOR AN UNEVENFUL LAN
- [SDR IXXA0000033](https://openairdocs.org/sdr/IXXA0000033.md): Rod · out of adj · Sep 28, 2000 · N867BX · Doug DC863F · Landing Gear Retraction/Extension System
  > EN ROUTE FROM TOL TO DFW, THE LANDING GEAR DOOR NOT LATCH LIGHT ILLUMINATED AFTER THE LANDING GEAR WAS RETRACTED. THE FLIGHT CREW CYCLED THE LANDING GEAR AND PERFORMED AN UNSUCCESSFUL UPLATCH CHECK. THE LANDING GEAR HANDLE WAS PLACED IN THE UP POSITION AND T
- [SDR IXXA0000027](https://openairdocs.org/sdr/IXXA0000027.md): Wire · broken · Jul 14, 2000 · N867BX · Doug DC863F · Landing Gear System Wiring
  > DURING DESCENT INTO TOL, WHEN THE LANDING GEAR WAS EXTENDED FOR LANDING THE NOSE LANDING GEAR DOWN AND LOCKED INDICATION LIGHT FAILED TO ILLUMINATE. THE FLIGHT CREW CYCLED THE GEAR. THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CREW FOLLOWED COMPANY P
- [SDR IXXA9900013](https://openairdocs.org/sdr/IXXA9900013.md): Indication · malfunctioned · Jul 7, 1999 · N867BX · Doug DC863F · Landing Gear Position and Warning
  > EN ROUTE FROM IAH TO TOL, THE MAIN LANDING GEAR NOT LATCHED LIGHT ILLUMINATED DURING THE UPLATCH CHECK, THE MAIN GEAR DOOR NOT LATCHED LIGHT REMAINED EXTINGUISHED. THE FLIGHT CREW CYCLED THE LANDING GEAR WITH THE WARNING INDICATION REMAINING THE SAME. THE FL
- [SDR IXXA9800069](https://openairdocs.org/sdr/IXXA9800069.md): Retract Mech · out of adjust · Sep 2, 1998 · N867BX · Doug DC863F · Landing Gear Door Retract Section
  > AFTER TAKEOFF WHEN THE LANDING GEAR WAS RETRACTED, THE FLIGHT CREW NOTICED A NOISE AND VIBRATION COMING FROM THE NOSE WHEEL WELL AREA. THE CREW CYCLED THE GEAR BUT THE VIBRATION CONDITION WAS STILL PRESENT. THE AIRCRAFT RETURNED TO TOL FOR AN UNEVENTFUL LAND
- [SDR IXXA9800065](https://openairdocs.org/sdr/IXXA9800065.md): Mechanism · misrigged · Aug 12, 1998 · N867BX · Doug DC863F · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, WHEN THE FLIGHT CREW RETRACTED THE LANDING GEAR, THE CONTROL HANDLE WOULD NOT POSITION TO THE UP POSITION. THE CREW RETURNED THE GEAR HANDLE TO THE DOWN POSITION, RECEIVING THREE DOWN AND LOCK INDICATIONS. A SECOND ATTEMPT TO RETRACT THE GEAR
- [SDR IXXA9800095](https://openairdocs.org/sdr/IXXA9800095.md): Bulkhead Fitting · cracked · Jul 9, 1998 · N867BX · Doug DC863F · Fuselage Main, Bulkhead
  > DURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON AFT PRESSURE BULKHEAD LOWER SUPPORT FITTING AT FUSELAGE STATION 1744, LONGERON 36. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION A NEW FITTING IN ACCORDANCE WITH DOUGLAS
- [SDR 98ZZZX2958](https://openairdocs.org/sdr/98ZZZX2958.md): Spar Cap · cracked · Jul 9, 1998 · N867BX · Doug DC863F · Wing Spar
  > FOUND LT WING INBD LOWER AUXILIARY SPAR CAP CRACKED ON VERTICAL FLANGE AT XRS22. SUSPECT CAUSE OF THE CRACK WAS VIBRATION.
- [SDR 98ZZZX2957](https://openairdocs.org/sdr/98ZZZX2957.md): Plank · cracked · Jul 9, 1998 · N867BX · Doug DC863F · Nacelle/Pylon Structure
  > PYLON PLANK HAS CRACK LOCATED AT 19.5 INCHES AFT FROM YN190. SUSPECT CAUSE OF THE CRACK WAS VIBRATION.
- [SDR 98ZZZX2956](https://openairdocs.org/sdr/98ZZZX2956.md): Plank · cracked · Jul 9, 1998 · N867BX · Doug DC863F · Nacelle/Pylon Structure
  > PYLON PLANK CRACK LOCATED AT YN226. SUSPECT CAUSE OF THE CRACK IS VIBRATION.
- [SDR IXXA9800094](https://openairdocs.org/sdr/IXXA9800094.md): Plating · corroded · Jun 16, 1998 · N867BX · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON LOWER FUSELAGE EXTERNAL PLATING FROM FUSELAGE STATIONS 1752 AND 1766, BETWEEN LONGERONS 35 LEFT AND 35 RIGHT. REPAIR ACCOMPLISHED CORROSION REMOVAL IN ACCORDANCE WITH DOUGLAS FAX ACTION NUMBER 37266
- [SDR IXXA9800090](https://openairdocs.org/sdr/IXXA9800090.md): Angle · corroded · Jun 11, 1998 · N867BX · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED BETWEEN FUSELAGE STATION 380 AND 400, LONGERON 27 LEFT. REPAIR ACCOMPLISHED REMOVAL OF CORRODED ANGLE, FABRICATION AND INSTALLATION A NEW LONGERON ANGLE IN ACCORDANCE WITH FAA DER APPROVED DRAWING COO-
- [SDR IXXA9800071](https://openairdocs.org/sdr/IXXA9800071.md): Frame · corroded · Jun 10, 1998 · N867BX · Doug DC863F · Fuselage Main, Frame
  > DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE FRAME AT FUSELAGE STATION 70, BETWEEN LONGERON 32 AND 34 RIGHT. REPAIR ACCOMPLISHED CORROSION REMOVAL, FABRICATION AND INSTALLATION AN INTERNAL REPAIR ANGLE IN ACCORDANCE WITH THE DOUGL
- [SDR IXXA9800092](https://openairdocs.org/sdr/IXXA9800092.md): Doubler · corroded · Jun 8, 1998 · N867BX · Doug DC863F · Wing Miscellaneous Structure
  > DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON CENTER WING UPPER JOINT DOUBLER AT FUSELAGE STATION 816, STRINGER 6. REPAIR ACCOMPLISHED BLENDED OUT CORROSION IN ACCORDANCE WITH FAA DER APPROVED DRAWINGS, COO-SJO-98-0393DDAC, COO-SJO-98-0394DAC,
- [SDR IXXA9800088](https://openairdocs.org/sdr/IXXA9800088.md): Fitting · corroded · Jun 4, 1998 · N867BX · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON A FUSELAGE FITTING BETWEEN FUSELAGE STATION 70 AND 80, LONGERON 33 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING. FABRICATION AND INSTALLATION A NEW FITTING IN ACCORDANCE WITH DOUGLAS DRAWI
- [SDR IXXA9800091](https://openairdocs.org/sdr/IXXA9800091.md): Plating · cracked · Jun 3, 1998 · N867BX · Doug DC863F · Rudder, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON THE RUDDER RIGHT SIDE EXTERNAL PLATING AND STATION ZR208.625. REPAIR ACCOMPLISHED STOP DRILLING CRACK, FABRICATION AND INSTALLATION AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH FAA DER APPROVED DRAWI
- [SDR IXXA9800087](https://openairdocs.org/sdr/IXXA9800087.md): Plank · cracked · Jun 3, 1998 · N867BX · Doug DC863F · Nacelle/Pylon, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON NUMBER FOUR PYLON INTERMEDIATE OUTBOARD PLANK AT STATION YIP 241. REPAIR ACCOMPLISHED STOP DRILLING CRACK, FABRICATION AND INSTALLATION OF AN INTERNAL AND EXTERNAL REPAIR DOUBLERS IN ACCORDANCE WITH D
- [SDR IXXA9800075](https://openairdocs.org/sdr/IXXA9800075.md): Plating · cracked · May 31, 1998 · N867BX · Doug DC863F · Wing, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, A CRACK WAS FOUND ON THE RIGHT WING LOWER LEADING EDGE AT STATION XFS 304. REPAIR ACCOMPLISHED STOP DRILL CRACK, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH FAA DER APPROVED DRAWING COO-8-57
- [SDR IXXA9800085](https://openairdocs.org/sdr/IXXA9800085.md): Longeron · corroded · May 29, 1998 · N867BX · Doug DC863F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED BETWEEN FUSELAGE STATION 180 AND 220, LONGERON 31 LEFT. REPAIR ACCOMPLISHED CORROSION REMOVAL, FABRICATION AND INSTALLATION A NEW LONGERON SPLICE FITTING IN ACCORDANCE WITH FAA DER APPROVED DRAWINGS CO
- [SDR IXXA9800084](https://openairdocs.org/sdr/IXXA9800084.md): Plank · cracked · May 24, 1998 · N867BX · Doug DC863F · Nacelle/Pylon, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON NUMBER TWO PYLON OUTBOARD INTERMEDIATE PLANK PANEL AT STATION YN 190. REPAIR ACCOMPLISHED STOP DRILL CRACK, FABRICATION AND INSTALLATION AN INTERNAL AND EXTERNAL REPAIR DOUBLERS IN ACCORDANCE WITH FAA
- [SDR IXXA9800083](https://openairdocs.org/sdr/IXXA9800083.md): Plank · worn · May 22, 1998 · N867BX · Doug DC863F · Nacelle/Pylon, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, WEAR WAS DETECTED ON THE NUMBER FOUR PYLON UPPER INBOARD PLANK SIX INCHES FORWARD OF STATION YUS 297. REPAIR ACCOMPLISHED BLENDING, POLISH THE AFFECTED AREA IN ACCORDANCE WITH FAA DER APPROVED DRAWING COO-SJO-98-0351, FAX AC
- [SDR IXXA9800093](https://openairdocs.org/sdr/IXXA9800093.md): Jamb · cracked · May 21, 1998 · N867BX · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C CHECK INSPECTION, A CRACKED FITTING WAS DETECTED AT UPPER TORQUE BOX FORWARD DOOR JAMB, AFT CARGO COMPARTMENT AT FUSELAGE STATION 1177 - X 68. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION A NEW FITTING IN ACCOR
- [SDR IXXA9800089](https://openairdocs.org/sdr/IXXA9800089.md): Plating · corroded · May 21, 1998 · N867BX · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED AT AFT ACCESSORY COMPARTMENT INTERNAL DOUBLER AT FUSELAGE STATION 1620, BETWEEN LONGERONS 24 AND 27 LEFT. REPAIR ACCOMPLISHED CORROSION REMOVAL, FABRICATION AND INSTALLATION REPAIR FILLERS, REPAIR DOUB
- [SDR IXXA9800086](https://openairdocs.org/sdr/IXXA9800086.md): Doubler · corroded · May 21, 1998 · N867BX · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON LOWER FUSELAGE, EIGHT EACH EXTERNAL FINGER DOUBLERS BETWEEN FUSELAGE STATIONS 1352 AND 1586.5. REPAIR ACCOMPLISHED TRIMMING OFF THE CORRODED FINGERS OF THE AFFECTED DOUBLERS IN ACCORDANCE WITH DOUGL
- [SDR IXXA9800072](https://openairdocs.org/sdr/IXXA9800072.md): Plating · corroded · May 21, 1998 · N867BX · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE EXTERNAL PLATING BETWEEN FUSELAGE STATIONS 1610 AND 1700, LONGERONS 31 LEFT AND 31 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA. FABRICATION AND INSTALLATION A NEW SECTION OF PLATIN
- [SDR IXXA9800074](https://openairdocs.org/sdr/IXXA9800074.md): Floor · corroded · May 20, 1998 · N867BX · Doug DC863F · Fuselage Floor Panel
  > DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON MAIN CABIN FLOOR PRESSURE PANEL BETWEEN FUSELAGE STATION 863 AND 878, BL +X4 TO -X5.50. REPAIR ACCOMPLISHED CORROSION BLEND OUT, FABRICATION AND INSTALLATION OF A REPAIR DOUBLER IN ACCORDANCE WITH F
- [SDR IXXA9800073](https://openairdocs.org/sdr/IXXA9800073.md): Plating · corroded · May 20, 1998 · N867BX · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON FUSELAGE EXTERNAL PLATING BETWEEN FUSELAGE STATION 301.5 AND 324, LONGERONS 33 AND 34 LEFT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA. FABRICATION AND INSTALLATION TWO INTERNAL FILLERS AND AN EXT
- [SDR IXXA980002](https://openairdocs.org/sdr/IXXA980002.md): Fire Warning · malfunctioned · Jan 7, 1998 · N867BX · Doug DC863F · Fire Detection
  > EN ROUTE, THE NUMBER FOUR ENGINE FIRE WARNING INTERMITTENTLY SOUNDED IN LIGHT TURBULENCE. THE FLIGHT CONTINUED TO TOL FOR AND UNEVENTFULL LANDING. MAINTENANCE INSPECTED THE ENGINE AND THE ASSOCIATED WIRING, WITH NO DISCREPANCIES NOTED. MAINTENANCE ACCOMPLIS
- [SDR IXXA9700146](https://openairdocs.org/sdr/IXXA9700146.md): Clamp · loose · Oct 24, 1997 · N867BX · Doug DC863F · Pneumatic Distribution System
  > EN ROUTE TOL TO BFI, THE NR 4 ENGINE FIRE WARNING SOUNDED WITH NUMBER 4 HIGH STAGE BLEED VALVE SELECTED TO HIGH. NR 4 BLEED VALVE WAS SELECTED TO LOW AND FIRE WARNING EXTINGUSHED. FLIGHT CONTINUED TO BFI FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE
- [SDR IXXA9700144](https://openairdocs.org/sdr/IXXA9700144.md): Wire · defective · Sep 10, 1997 · N867BX · Doug DC863F · Fire Detection
  > DURING APPROACH, THE NUMBER FOUR ENGINE FIRE WARNING SOUNDED. THE CREW SECURED THE ENGINE, FIRE WARNING EXTINGUISHED. MAINTENANCE INSPECTED THE ENGINE, NO EVIDENCE OF A FIRE WAS NOTED. MAINTENANCE PERFORMED AN INTENSIFIED INSPECTION OF THE WARNING SYSTEM WIR
- [SDR IXXA9700143](https://openairdocs.org/sdr/IXXA9700143.md): Fire Warning · malfunctioned · Sep 10, 1997 · N867BX · Doug DC863F · Fire Detection
  > ENROUTE, THE NUMBER FOUR ENGINE FIRE WARNING SOUNDED AND AN ENGINE SHUTDOWN WAS ACCOMPLISHED FOLLOWING COMPANY PROCEDURES. THE FIRE WARNING EXTINGUISHED SHORTLY AFTER THE SHUTDOWN. MAINTENANCE INSPECTED THE ENGINE AND FOUND NO EVIDENCE OF A FIRE. THE ENGI
- [SDR IXXA9700107](https://openairdocs.org/sdr/IXXA9700107.md): Ballast · burnt · Aug 9, 1997 · N867BX · Doug DC863F · Flight Compartment Lighting
  > AFTER TAKEOFF TOL, SMOKE EMANATED FROM FLIGHT ENGINEER'S PANEL IN THE VICINITY OF THE CABIN PRESSURE CONTROLLER AND THE HYDRAULIC SELECTOR CONSOLE. FLIGHT RETURNED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE FOUND THAT THE F/E'S INSTRUMENT WHITE LIGHTING B
- [SDR IXXA9700085](https://openairdocs.org/sdr/IXXA9700085.md): Electrical Syst · odor · Jul 2, 1997 · N867BX · Doug DC863F · Electrical Power System
  > EN ROUTE, CREW NOTICED HOT ELECTRICAL SMELL IN COCKPIT BELOW THE CIRCUIT BREAKER PANEL. SMELL DISSIPATED AFTER ABOUT 1 MINUTE. FOLLOWING AN UNEVENTFUL LANDING IN TOL, MAINTENANCE INVESTIGATED THE ORIGIN OF THE SMELL. NO CAUSE WAS FOUND AFTER A COMPLETE ENGI
- [SDR IXXA9700005](https://openairdocs.org/sdr/IXXA9700005.md): Uplatch Switch · unsecure · Jan 23, 1997 · N867BX · Doug DC863F · Landing Gear Position and Warning
  > ON CLIMBOUT, GEAR DOORS NOT LATCHED LIGHT WOULD NOT EXTINGUISH ON GEAR RETRACTION. LANDING GEAR WAS CYCLED AND THE DOORS LIGHT EXTINGUSHED. AFTER LANDING TOL, MAINTENANCE FOUND AND SECURED THE RIGHT HAND MAIN LANDING GEAR DOOR UPLATCH SWITCH. MAINTENANCE AC
- [SDR IXXA9700004](https://openairdocs.org/sdr/IXXA9700004.md): Wire · broken · Jan 22, 1997 · N867BX · Doug DC863F · Landing Gear System Wiring
  > AFTER TAKEOFF, GEAR UNSAFE LIGHT REMAINED ON AFTER RETRACTION. FLIGHT CREW CYCLED GEAR, LIGHT EXTINGUSHED, GEAR UPLATCH CHECK WAS NORMAL. THE FLIGHT CONTINUED TO TOL WITH AN UNEVENTFUL LANDING. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE AT THE LEFT MAIN L
- [SDR IXXA96130](https://openairdocs.org/sdr/IXXA96130.md): Structure · vibration · Aug 23, 1996 · N867BX · Doug DC863F · Aircraft Structures
  > DURING APPROACH TO CLT, AIRCRAFT EXPERIENCED A SIGNIFICANT VIBRATION WITH FLAP 23 SELECTED. MAINTENANCE INSPECTED THE AIRCRAFT FLIGHT CONTROL SYSTEMS, LANDING GEAR SYSTEMS, WINGS, AND FUSELAGE WITH NO CAUSE FOUND. A SUBSEQUENT TEST FLIGHT WAS ACCOMPLOSHED WI
- [SDR IXXA96121](https://openairdocs.org/sdr/IXXA96121.md): Linkage · broken · Jun 27, 1996 · N867BX · Doug DC863F · Drag Control System
  > EN ROUTE BETWEEN ATL AND TOL, CREW NOTED SPOILER UNLOCK INDICATION LIGHT ILLUMINATED WITH STANDBY SPOILER PUMP OFF. FLIGHT CONTINUED WITH AN UNEVENTFUL LANDING AT TOL. MAINTENANCE FOUND AND REPLACED A BROKEN LEFT INBOARD SPOILER CRANK/LINKAGE IAW THE DOUGLAS
- [SDR CKSA6004](https://openairdocs.org/sdr/CKSA6004.md): Fire Loop · broken · Jan 19, 1996 · N867BX · Doug DC863F · Fire Detection
  > KTOL - FLT 71266 - NR 4 ENGINE FIRE WARNING CAME ON IN-FLIGHT DURING DESCENT. PERFORMED IN-FLIGHT SHUT DOWN AND DISCHARGED FIRE BOTTLE. LANDED WITHOUT INCIDENT. FOUND NR 4 ENGINE BOTTOM FIRE LOOP BROKEN. REPLACED LOWER FIRE LOOP. GROUND OPS CHECK GOOD IAW
- [SDR CKSA95167](https://openairdocs.org/sdr/CKSA95167.md): Ballast · failed · Dec 29, 1995 · N867BX · Doug DC863F · Flight Compartment Lighting
  > KTOL-KPHL - ELECTRICAL SMELL IN FRONT RIGHT SIDE OF COCKPIT. SUBMITTER STATES, SUSPECT RIGHT GLARESHIELD LIGHT, PULLED BREAKER. NO MORE SMELL, DEFERRED PER MEL 33-1 CAT C DMI NR 654. REPLACED LIGHT BALLAST TRANSFORMER ASSEMBLY. OPS CHECKED GOOD IAW DC-8 MM
- [SDR CKSA95062](https://openairdocs.org/sdr/CKSA95062.md): Fitting · corroded · Jun 28, 1995 · N867BX · Doug DC863F · Fuselage Miscellaneous Structure
  > KYIP - DURING B-CHECK INSPECTION, FOUND LONGERON 30L AT FS 1660, CORRODED. REPAIRED PER DC-8 SRM 53-2-2. REPLACED LONGERON END FITTING, STA 1660 LONGERON 30L. (X)
- [SDR CKSA95061](https://openairdocs.org/sdr/CKSA95061.md): Skin · corroded · Jun 28, 1995 · N867BX · Doug DC863F · Fuselage Main, Plate/Skin
  > KYIP - DURING B-CHECK INSPECTION, FOUND FUSELAGE SKIN BULGING FROM CORROSION AT STATION 1660, LONGERON 30L. REPAIRED FUSELAGE SKIN AT STATION 1660, LONGERON 30L IAW EA NR 95-178. (M)
- [SDR CKSA95018](https://openairdocs.org/sdr/CKSA95018.md): Wire · bare · Apr 11, 1995 · N867BX · Doug DC863F · Fire Detection
  > KTOL - ON SHORT FINAL NR 1 ENGINE FIRE WARNING CAME ON MOMENTARILY. REPAIRED BARE WIRE NEAR FIRE LOOP PLUG, CHECKS OK IAW MM CHAPTER 26. (W)

Next page: https://openairdocs.org/deregistered/N867BX-2005-12-20/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 = 'N867BX' AND deregistration_id = 'N867BX-2005-12-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N867BX-2005-12-20/reports

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