# Service difficulty reports: N826BX, cancelled Jan 6, 2014 A list on [N826BX, cancelled Jan 6, 2014](https://openairdocs.org/deregistered/N826BX-2014-01-06.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR IXXA0200004O](https://openairdocs.org/sdr/IXXA0200004O.md): Strut · cracked · Feb 7, 2002 · N826BX · Doug DC871F · Main Landing Gear Strut/Axle/Truck > EN ROUTE FROM TOL TO BDL, THE LANDING GEAR AND DOOR UNSAFE WARNING LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE LANDING GEAR BUT THE UNSAFE WARNING INDICATION REMAINED THE SAME. THE FLIGHT RETURNED TO TOL FOR AND UNEVENTFUL L - [SDR IXXAO200003O](https://openairdocs.org/sdr/IXXAO200003O.md): Uplock · lack of lube · Jan 29, 2002 · N826BX · Doug DC871F · Landing Gear Retraction/Extension System > EN ROUTE FROM MCI TO TOL, THE LANDING GEAR NOT LATCHED LIGHT ILLUMINATED DURING THE GEAR UPLATCH CHECK. THE FLIGHT CREW CYCLED THE LANDING BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPE - [SDR IXXA0100071O](https://openairdocs.org/sdr/IXXA0100071O.md): Connector · defective · Nov 10, 2001 · N826BX · Doug DC871F · Detection System > ENROUTE FROM TOL TO BFI, ON DESCENT THE NUMBER FOUR ENGINE FIRE WARNING SHORT CIRCUIT LIGHT ILLUMINATED. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND SECURED THE ENGINE. THE FLIGHT CONTINUED TO BFI FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE - [SDR IXXA0100036O](https://openairdocs.org/sdr/IXXA0100036O.md): Hinge Pin · worn · Jun 6, 2001 · N826BX · Doug DC871F · Landing Gear Position and Warning > IN ROUTE FROM RDU TO TOL AFTER GEAR RETRACTION LANDING GEAR DOOR UNSAFE LIGHT ILLUMINATED. FLIGHT CREW CYCLED THE LANDING GEAR, WARNING INDICATION REMAINED THE SAME. FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENACE INSPECTED THE LANDING GEAR WHICH - [SDR IXXA0100026](https://openairdocs.org/sdr/IXXA0100026.md): Door · out of rig · May 25, 2001 · N826BX · Doug DC871F · Landing Gear Door Retract Section > EN ROUTE FROM TOL TO BDL, THE LANDING GEAR DOOR UNSAFE WARNING LIGHT ILLUMINATED AFTER A SUCCESFUL GEAR UP LATCH CHECK WAS PERFORMED. THE FLIGHT RETURNED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE MAIN LANDING GEA - [SDR IXXA0100023](https://openairdocs.org/sdr/IXXA0100023.md): Warning System · malfunctioned · May 3, 2001 · N826BX · Doug DC871F · Landing Gear Position and Warning > EN ROUTE FROM SJC TO TOL, THE LANDING GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE LANDING GEAR AND THE GEAR DOOR WARNING LIGHT EXTINGUISHED. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANC - [SDR IXXA0100017](https://openairdocs.org/sdr/IXXA0100017.md): Uplock Sensor · dirty · Apr 24, 2001 · N826BX · Doug DC871F · Landing Gear Position and Warning > EN ROUTE FROM SJC TO TOL, THE LANDING GEAR UNSAFE AND DOOR WARNING LIGHTS ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE LANDING GEAR AND THE WARNING INDICATING LIGHTS EXTINGUISHED. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINT - [SDR IXXA0100009](https://openairdocs.org/sdr/IXXA0100009.md): Wire · broken · Mar 2, 2001 · N826BX · Doug DC871F · Landing Gear System Wiring > EN ROUTE FOR JFK TO TOL, THE GEAR DOOR WARNING LIGHT REMAINED ON DIM AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE LANDING GEAR AND THE WARNING LIGHT EXTINGUISHED. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT - [SDR IXXA0100007](https://openairdocs.org/sdr/IXXA0100007.md): Warning Light · illuminated · Feb 21, 2001 · N826BX · Doug DC871F · Landing Gear Position and Warning > EN ROUTE FROM TOL TO JFK, THE LANDING GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE LANDING GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO JFK FOR AN UNEVENTFUL LANDING. THE LANDIN - [SDR IXXA0100003](https://openairdocs.org/sdr/IXXA0100003.md): Switch · contaminated · Jan 9, 2001 · N826BX · Doug DC871F · Landing Gear Retraction/Extension System > EN ROUTE FROM TOL TO JFK, THE LANDING GEAR DOOR WARNING LIGHT ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE GEAR WITH THE WARNING INDICATION REMAINING THE SAME. THE FLIGHT CONTINUED TO JFK FOLLOWING COMPANY PROCEDURES. MAINTENANCE INSPECTED - [SDR IXXA0100001](https://openairdocs.org/sdr/IXXA0100001.md): Connector · loose · Jan 5, 2001 · N826BX · Doug DC871F · Landing Gear Retraction/Extension System > !ENROUTE FROM RDU TO TOL, THE GEAR DOOR WARNING LIGHT ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE LANDING GEAR AND THE WARNING INDICATION EXTINGUISHED. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE LANDING G - [SDR IXXA0000045](https://openairdocs.org/sdr/IXXA0000045.md): Connector · loose · Jan 5, 2001 · N826BX · Doug DC871F · Landing Gear Position and Warning > ENROUTE FROM RDU TO TOL, THE GEAR DOOR WARNING LIGHT ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE LANDING GEAR AND THE WARNING INDICATION EXTINGUISHED. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE LANDING GE - [SDR IXXA0000044](https://openairdocs.org/sdr/IXXA0000044.md): Uplock · lack of lube · Dec 12, 2000 · N826BX · Doug DC871F · Landing Gear Door Retract Section > ENROUTE FROM PDX TO TOL, AFTER T.O. THE GEAR DOOR WARNING LIGHT ILLUMINATED WITH THE GEAR RETRACTED. THE FLIGHT CREW CYCLED GEAR WITH THE DOOR WARNING INDICATION REMAINING THE SAME. THE FLIGHT RETURNED TO PDX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED T - [SDR IXXA0000043](https://openairdocs.org/sdr/IXXA0000043.md): Switch · misrigged · Dec 7, 2000 · N826BX · Doug DC871F · Landing Gear Door Retract Section > GEAR FAILED UPLATCH CHECK. CYCLED SEVERAL TIMES FOLLOWED ATI DOOR WARNING CHECKLIST. FOUND INDICATION PROBLEM AND CONTINUED ACCORDING TO ATI CHECKLIST. 30 MIN LATER LIGHT WENT OUT. CREW LANDED UNEVENTLY AT DESTINATION. MAINTENANCE PERFORMED GEAR SWING AND COUL - [SDR IXXA0000032](https://openairdocs.org/sdr/IXXA0000032.md): Filter · contaminated · Sep 13, 2000 · N826BX · Doug DC871F · Aircraft Fuel Filter/Strainer > EN ROUTE FROM TOL TO DFW, THE NUMBER ONE ENGINE EXPERIENCED A ROLL BACK AT THE TOP OF DESCENT. NO THROTTLE RESPONCE WAS MOMENTARILY NOTED THEN ALL ENGINE PARAMETERS RETURNED TO NORMAL. THE FLIGHT CONTINUED TO DFW FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPE - [SDR IXXA9800082](https://openairdocs.org/sdr/IXXA9800082.md): Connector · wet · Nov 10, 1998 · N826BX · Doug DC871F · Landing Gear Position and Warning > AFTER TAKEOFF, THE LANDING GEAR WAS RETRACTED, THE GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED. THE CREW CYCLED THE GEAR SEVERAL TIMES WITH THE WARNING INDICATION REMAINING THE SAME. THE CREW PERFORMED A SUCCESSFUL GEAR UPLATCH CHECK AND THE WARNING LIGHT E - [SDR IXXA9800062](https://openairdocs.org/sdr/IXXA9800062.md): Switch · defective · Jul 21, 1998 · N826BX · Doug DC871F · Landing Gear Position and Warning > ON APPROACH, DURING GEAR EXTENSION FOR LANDING,THE LEFT MAIN GEAR INDICATOR LIGHT FAILED TO ILLUMINATE IN THE DOWN POSITION, ACCOMPANIED BY AN ILLUMINATED GEAR UNSAFE WARNING LIGHT. THE CREW CYCLED THE GEAR BUT THE WARNING INDICATION REMAINED THE SAME. WHILE - [SDR IXXA9800056](https://openairdocs.org/sdr/IXXA9800056.md): Wire · chafed · May 1, 1998 · N826BX · Doug DC871F · Landing Gear System Wiring > EN ROUTE TOL TO DFW, DURING GEAR EXTENTION FOR LANDING THE LEFT MAIN LANDING GEAR INDICATOR LIGHT DID NOT ILLUMINATE IN THE DOWN POSITION. THE CREW CYCLED THE GEAR THREE TIMES PRIOR TO RECEIVING A DOWN AND LOCKED INDICATION. MAINTENANCE INSPECTED THE LEFT GE - [SDR IXXA96104](https://openairdocs.org/sdr/IXXA96104.md): Coalescer · loose · Jul 4, 1996 · N826BX · Doug DC871 · Humidity Control System > EN ROUTE FROM BNA-FLL AT FLT LEVEL 350, OIL SMOKE/MIST WAS NOTED IN THE COCKPIT. THE RIGHT PACK SYSTEM WAS SUSPECTED AND SHUT DOWN FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE FOUND AND SECURED A LOOSE CLAMP AT THE WATER SEPARATOR/COALESCER. OPERATIONALLY CH - [SDR IXXA96103](https://openairdocs.org/sdr/IXXA96103.md): Downlock Sw · intermittent · Jun 27, 1996 · N826BX · Doug DC871 · Landing Gear Position and Warning > ON DESCENT INTO SAN, LANDING GEAR UNSAFE LIGHT ILLUMINATED ACCOMPANIED BY THE WARNING HORN WHEN FLAPS SELECTED TO 50 DEGREES. GEAR CYCLED SEVERAL TIMES UNTIL SAFE INDICATION WAS OBTAINED. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE LEFT DOWNLOCK SWITCH - [SDR IXXA96102](https://openairdocs.org/sdr/IXXA96102.md): Downlock Sw · dirty · Jun 25, 1996 · N826BX · Doug DC871 · Landing Gear Position and Warning > UPON GEAR EXTENTION INTO TOL, LEFT GEAR INDICATION LIGHT ILLUMINATED IMMEDIATELY. ALL GEAR LIGHTS ILLUMINATED WITH GEAR UNSAFE LIGHT. GEAR WAS CYCLED, EXTENTION WAS NORMAL EXCEPT LEFT GEAR LIGHT CAME ON IMMEDIATELY. MAINTENANCE FOUND LEFT GEAR DOWNLOCK SWIT - [SDR IXXA9550](https://openairdocs.org/sdr/IXXA9550.md): Rib · cracked · Mar 27, 1995 · N826BX · Doug DC871 · Wing, Rib/Bulkhead > DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND AT XRS-6 RIB. THE RIB WAS REPAIRED IAW DRAWING HSE27-57-169, WHICH WAS FAA DER APPROVED, AND EO 57-DC8-151. (W) - [SDR IXXA9551](https://openairdocs.org/sdr/IXXA9551.md): Plating · cracked · Mar 24, 1995 · N826BX · Doug DC871 · Wing, Plate/Skin > DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND IN THE RIGHT WING LEADING EDGE, STUB WING, PLATING AT XRS 453. UPON DOUGLAS EVALUATION AND FAA DER APPROVAL THE CRACK WAS SUBJECTED TO ADDITONAL INSPECTION. INSPECTION RESULTS FOUND NO ADDITIONAL DAMAGE, A - [SDR IXXA9556](https://openairdocs.org/sdr/IXXA9556.md): Skin · corroded · Mar 16, 1995 · N826BX · Doug DC871 · Fuselage Main, Plate/Skin > DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS BLENDED BEYOND SRM LIMITS. THE EXTERIOR PLATING AT STATION 530-550 BETWEEN LONGERONS 33 RT AND 36. DAMAGE WAS REMOVED BY CUTOUT, ADDING A FILLER AND EXTERNAL DOUBLER. REPAIR ACCOMPLISHED IAW DRAWING HSE27-53- - [SDR IXXA9558](https://openairdocs.org/sdr/IXXA9558.md): Fitting · cracked · Mar 15, 1995 · N826BX · Doug DC871 · Cargo/Baggage Doors > DURING ROUTINE C-CHECK INSPECTION, AN AFT LOWER CARGO DOOR STOP FITTING WAS FOUND CRACKED. THE FITTING WAS MANUFACTURED IAW DRAWING HSE27-53-165, WHICH WAS FAA DER APPROVED AND EO 53-DC8-160. FITTING WAS INSTALLED IAW THE AIRCRAFT MM. (W) - [SDR IXXA9557](https://openairdocs.org/sdr/IXXA9557.md): Panel · corroded · Mar 15, 1995 · N826BX · Doug DC871 · Fuselage Main, Plate/Skin > DURING C-CHECK ROUTINE INSPECTION, FOUND LOADER DAMAGE AT THE FORWARD BASKET DOOR CUTOUT. THE FUSELAGE PLATING WAS ROUTED OUT AND AN EXTERNAL DOUBLER ADDED. REPAIR WAS ACCOMPLISHED IAW DRAWING HSE27-53-166, WHICH IS FAA DER APPROVED AND EO 53-DC8-158. (W) - [SDR IXXA9555](https://openairdocs.org/sdr/IXXA9555.md): Frame · corroded · Mar 15, 1995 · N826BX · Doug DC871 · Fuselage Main, Frame > DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND AT STATION 520, BETWEEN LONGERONS 33 AND 35 RIGHT. THE SECTION OF BELTFRAME WAS REMOVED MANUFACTURED AND REPLACED. REPAIR ACCOMPLISHED IAW DRAWING HSE27-53-163, WHICH IS FAA DER APPROVED AND EO 53-DC8-15 - [SDR IXXA9554](https://openairdocs.org/sdr/IXXA9554.md): Panel · corroded · Mar 15, 1995 · N826BX · Doug DC871 · Fuselage Main, Plate/Skin > DURING ROUTINE C-CHECK INSPECTION, LEVEL 2 CORROSION WAS FOUND AT FUSELAGE STATION 560-610. THIS AREA HAD A PREVIOUS REPAIR AND THE CORROSION FOUND IS ATTRIBUTED TO NOT REMOVING ALL CORROSION AT THAT TIME. REPAIR OF THE AREA REQUIRED TWO CUTOUTS OF BOTH THE - [SDR IXXA9553](https://openairdocs.org/sdr/IXXA9553.md): Frame · corroded · Mar 15, 1995 · N826BX · Doug DC871 · Fuselage Main, Frame > DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS NOTED AT THE BELTFRAME AT FUSELAGE STATION 1397, BETWEEN LONGERONS 34 LEFT AND RIGHT. THE LOCALIZED CORROSION WAS REMOVED BY CUT OUT, MANUFACTURE OF A NEW SECTION, ADDING A SPLICE CHANNEL, AND INSTALLING AN ORI - [SDR IXXA9552](https://openairdocs.org/sdr/IXXA9552.md): Panel · cracked · Mar 15, 1995 · N826BX · Doug DC871 · Wing, Plate/Skin > DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND IN THE LEFT WING LOWER PLATING. THE CRACK MEASURED 1.75 INCHES AND WAS LOCATED AT XW 441.5, BETWEEN STRINGERS 63 AND 64. REPAIR WAS ACCOMPLISHED BY REMOVAL OF THE CRACK, ADDING A FILLER, AND INSTALLING BOT - [SDR IXXA9549](https://openairdocs.org/sdr/IXXA9549.md): Panel · corroded · Jan 25, 1995 · N826BX · Doug DC871 · Fuselage Main, Plate/Skin > DURING ROUTINE C-CHECK, EXTERIOR CORROSION WAS NOTED AT FS 610, BETWEEN LONGERONS 34 LEFT AND RIGHT. THE CORROSION WAS REMOVED BY CUT OUT, ADDING A REPAIR FILLER, AND INSTALLING 2 EXTERNAL REPAIR DOUBLERS. REPAIR WAS ACCOMPLISHED IAW DRAWING HSE27-53-141, WH ## 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 = 'N826BX' AND deregistration_id = 'N826BX-2014-01-06' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N826BX-2014-01-06/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.