# Service difficulty reports: N824BX, cancelled May 16, 2006 A list on [N824BX, cancelled May 16, 2006](https://openairdocs.org/deregistered/N824BX-2006-05-16.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR IXXA0200002O](https://openairdocs.org/sdr/IXXA0200002O.md): Transmitter · defective · Jan 17, 2002 · N824BX · Doug DC871F · Hydraulic Quantity Indicator > WHILE ENROUTE FROM JFK TO BDL, THE FLIGHT CREW NOTICED THAT THE MAIN HYDRAULIC QUANTITY SYSTEM WAS DECLINING. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED TO BDL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND TRACED THE PROBLE - [SDR IXXA0200001O](https://openairdocs.org/sdr/IXXA0200001O.md): Transmitter · defective · Jan 17, 2002 · N824BX · Doug DC871F · Hydraulic Quantity Indicator > WHILE ENROUTE FROM JFK TO BDL, THE FLIGHT CREW NOTICED THAT THE MAIN HYDRAULIC QUANTITY SYSTEM WAS DECLINING. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED TO BDL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND TRACED THE PROBLE - [SDR 0100037O](https://openairdocs.org/sdr/0100037O.md): Warning System · activated · Jun 20, 2001 · N824BX · Doug DC871F · Engine EGT/TIT Indicating System > PRIOR TO ROTATION AIRCRAFT EXPERIENCED ABNORMAL EXHAUST GAS TEMPERATURE INDICATION. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO PARKING. NO FURTHER ABNORMALITIES OCCURRED. - [SDR IXXA0100016](https://openairdocs.org/sdr/IXXA0100016.md): Swivel · leaking · Apr 18, 2001 · N824BX · Doug DC871F · Hydraulic System, Main > AFTER TAKEOFF FROM TOL, THE FLIGHT CREW NOTICE A DECLINED IN THE MAIN HYDRAULIC QUANTITY SYSTEM. THE FLIGHT RETURNED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT LOCATING A RUPTURED LEFT AILERON SWIVEL GLAND. MAINTENANCE REPACKED THE - [SDR IXXA0000036](https://openairdocs.org/sdr/IXXA0000036.md): Uplock Roller · lack of lube · Oct 27, 2000 · N824BX · Doug DC871F · Landing Gear Position and Warning > EN ROUTE FROM IAH TO TOL, THE GEAR NOT LATCH LIGHT ILLUMINATED DURING THE LANDING GEAR UPLATCH CHECK. THE FLIGHT CREW CYCLED THE GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED - [SDR IXXA9800078](https://openairdocs.org/sdr/IXXA9800078.md): Plating · corroded · Oct 8, 1998 · N824BX · Doug DC871F · Fuselage Main, Plate/Skin > DURING ROUTINE PREFLIGHT INSPECTION, FOUND THE FUSELAGE EXTERNAL PLATING WITH CORROSION BULGE, TWO MISSING RIVET HEADS AND THREE CRACKS MIGRATING FROM ONE MISSING RIVET HEADS BETWEEN FUSELAGE STATION -21.0 TO 30.0 BETWEEN LONGERON 31 RIGHT AND 35 LEFT. THE A - [SDR IXXA9800067](https://openairdocs.org/sdr/IXXA9800067.md): Pressure Syst · malfunctioned · Aug 25, 1998 · N824BX · Doug DC871F · Cabin Pressure Control System > EN ROUTE AT FLIGHT LEVEL 35.0, THE AIRCRAFT CABIN BEGAN TO CLIMB RAPIDLY, MANUAL CONTROL OF PRESSURIZATION WAS ATTEMPTED. PACK FLOWS WERE INCREASED TO 90 PERCENT CAPACITY WITH MINIMAL DECREASE IN CABIN. DESCENT INITIATED AND AT LEVEL OFF CABIN COULD BE MAIN - [SDR IXXA980004](https://openairdocs.org/sdr/IXXA980004.md): Engine · damaged · Feb 12, 1998 · N824BX · Doug DC871F · Engine (Turbine/Turboprop) > EN ROUTE FROM TOL TO ATL, DURING CRUISE THE FLIGHT ENGINEER NOTICED A MARKED DECLINE IN THE NUMBER ONE ENGINE OIL QUANTITY. THE CREW PERFORMED A PRECAUTIONARY INFLIGHT SHUTDOWN IAW COMPANY PROCEDURES, AND CONTINUED TO ATL MAKING AN UNEVENTFUL LANDING. MAINT - [SDR IXXA96118](https://openairdocs.org/sdr/IXXA96118.md): Hpt Blade · cracked · Jul 27, 1996 · N824BX · Doug DC871 · Turbine Section > DURING PRECAUTIONARY BORESCOPE INSPECTION OF THE NR 1 ENGINE, MAINTENANCE FOUND ONE HIGH PRESSURE TURBINE BLADE TRAILING EDGE TIP CORNER MISSING. MISSING MATERIAL WAS LOCATED AT THE TRAILING EDGE TIP, DOWNWARD TO THE FIRST AIR SLOT IN AREA B, CFMI MM 72-00-00 - [SDR IXXA96117](https://openairdocs.org/sdr/IXXA96117.md): Mec · leaking · Jul 27, 1996 · N824BX · Doug DC871 · Fuel Control/Turbine Engines > COMPRESSOR STALL ACCOMPANIED BY FLAMES EXITING THE EXHAUST NOZZLE REPORTED TO THE CREW BY THE CONTROL TOWER ON LANDING ROLL AT PDX, CREW SUSPECTED THE NR 2 ENGINE. MX BORESCOPED THE NR 2 ENGINE WITH NO FINDINGS. MX FOUND THE MEC SUSPECT OF CAUSING THE STALL - [SDR IXXA96120](https://openairdocs.org/sdr/IXXA96120.md): Control Cable · broken · Jun 26, 1996 · N824BX · Doug DC871 · Aileron Control System > ON TAXI OUT AND FLIGHT CONTROL CHECKS AT ATL, AILERONS FELT STIFF WITH VERY LITTLE SPOILER PRESSURE DROP. THE AIRCRAFT RETURNED TO RAMP. MAINTENANCE INSPECTED THE FLIGHT CONTROL CABLES AND FOUND THE LEFT AILERON BUS CABLE BROKEN. MAINTENANCE REPLACED THE BR - [SDR IXXA9683](https://openairdocs.org/sdr/IXXA9683.md): Fire Warning · shorted · May 30, 1996 · N824BX · Doug DC871 · Fire Detection > EN ROUTE FROM DEN-TOL - THE NR 4 ENGINE FIRE WARNING SHORT CIRCUIT LIGHT CAME ON INTERMITTENTLY, FOLLOWED BY A STEADY LIGHT. AFTER THREE MINUTES, THE SYSTEM WOULD NO LONGER TEST. SHORTLY THEREAFTER, THE FIRE WARNING LIGHT ILLUMINATED AND THE ENGINE WAS SHUT - [SDR IXXA9605](https://openairdocs.org/sdr/IXXA9605.md): Air Distr · odor · Jan 31, 1996 · N824BX · Doug DC871 · Air Distribution System > EN ROUTE BETWEEN MKE AND DEN, THE AIR CONDITIONING PACKS WERE PRODUCING A STRONG, UNIDENTIFIED ODOR. ON THE GROUND IN DEN, THE PACKS WERE OPERATIONALLY CHECKED AND FOUND NOT TO BE PRODUCING AND ODOR AT THAT TIME. A REVIEW OF THE FLIGHT SUGGESTED THAT A SMALL - [SDR IXXA9594](https://openairdocs.org/sdr/IXXA9594.md): Uplatch Cable · out of adjust · Jan 3, 1996 · N824BX · Doug DC871 · Landing Gear Retraction/Extension System > ON TAKEOFF FROM TOL TO ONT, THE CREW REPORTED AN UNSAFE GEAR AND DOOR LIGHT AFTER GEAR RETRACTION. THE AIRCRAFT RETURNED TO TOL FOR MAINTENANCE. THE AIRCRAFT WAS FERRIED TO A MAINTENANCE FACILITY FOR LANDING GEAR SYSTEM INSPECTION AND RIG CHECK. A RIG CHEC - [SDR IXXA9608](https://openairdocs.org/sdr/IXXA9608.md): Engine · flamed out · Jan 2, 1996 · N824BX · Doug DC871 · Engine (Turbine/Turboprop) > EN ROUTE FROM TOL TO SEA, THE NR 4 ENGINE FLAMED OUT AT 35,000 FEET. TWO UNSUCCESSFUL RESTART ATTEMPTS WERE MADE. THE ENGINE WAS SECURED AND THE AIRCRAFT DIVERETED TO MSO FOR MAINTENANCE. UPON ARRIVAL IN MSO, THE FLIGHT CREW REPORTED THEY SUMPED TANKS AND R - [SDR IXXA199589](https://openairdocs.org/sdr/IXXA199589.md): Connector · deteriorated · Oct 21, 1995 · N824BX · Doug DC871 · Landing Gear Position and Warning > WHEN THE LANDING GEAR UPLATCH CHECK WAS PERFORMED ON DEPARTURE OUT OF TOL, THE GEAR DOOR WARNING LIGHT REMAINED ON. THE AIRCRAFT ELECTED TO RETURN TO TOL FOR MAINTENANCE. TOL MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THAT THE ELECTRICAL CONNECTOR FOR - [SDR IXXA199587](https://openairdocs.org/sdr/IXXA199587.md): Flap Fitting · broken · Oct 13, 1995 · N824BX · Doug DC871 · Trailing Edge Flaps > AT MSP, IT WAS DISCOVERED THAT THE STATION 98 OUTBOARD FLAP BASE FITTING ON LEFT INBOARD FLAP SECTION HAD EXPERIENCED A TYPICAL FAILURE DUE TO A CRACK THAT ORIGINATED IN THE UPPER FLAP VANE ATTACH BOLT HOLE. THE OPPOSING BASE FITTING AT THAT STATION HAD RECIE - [SDR IXXA199585](https://openairdocs.org/sdr/IXXA199585.md): Uplatch Switch · failed · Oct 10, 1995 · N824BX · Doug DC871 · Landing Gear Position and Warning > ON DEPARTURE OUT OF BOS, THE LANDING GEAR FAILED THE UPLATCH CHECK. THE LANDING GEAR WAS CYCLED THREE TIMES WITH THE SAME RESULT, WITH THE LANDING GEAR LEVER IN THE UPLATCH CHECK POSITION, THE UNSAFE LIGHT WAS ILLUMINATED WITH NO APPARENT GEAR EXTENSION. INS - [SDR IXXA199579](https://openairdocs.org/sdr/IXXA199579.md): Uplock Switch · bent pin · Sep 22, 1995 · N824BX · Doug DC871 · Landing Gear Position and Warning > ORD/PDX - ON TAKEOFF, CREW REPORTED WITH LANDING GEAR HANDLE UP, LANDING GEAR UNSAFE LIGHT REMAINED ON. CREW RECYCLED GEAR HANDLE AND IT OPERATED NORMALLY. ON APPROACH TO PDX, GEAR EXTENDED NORMALLY. CREW DID OPS CK AND RETRACTED GEAR. WITH GEAR HANDLE UP, - [SDR IXXA199576](https://openairdocs.org/sdr/IXXA199576.md): Connector · contaminated · Sep 15, 1995 · N824BX · Doug DC871 · Landing Gear Position and Warning > ON TAKEOFF OUT OF ONT, THE LANDING GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED. CYCLING THE LANDING GEAR EXTINGUISHED THE DOOR WARNING LIGHT. IN TOL, TROUBLESHOOTING REVEALED A HIGH RESISTANCE IN THE LEFT MLG DOOR UPLATCH SWITCH CIRCUIT CAUSED BY A CONTAMIN - [SDR IXXA199524](https://openairdocs.org/sdr/IXXA199524.md): Oil Cap · unlocked · Mar 31, 1995 · N824BX · Doug DC871 · Turbine Engine Oil System > OKC - ON DEPARTURE, FLIGHT CREW NOTICED THE NR 1 ENGINE OIL QUANTITY WAS DECREASING. THE ENGINE WAS PRECAUTIONARILY SHUT DOWN, AND THE AIRCRAFT RETURNED TO OKC FOR MAINTENANCE. SOME OIL QUANTITY WAS RETAINED, AND MINIMUM WINDMILLING OIL PRESSURE WAS MAINTAIN - [SDR IXXA9542](https://openairdocs.org/sdr/IXXA9542.md): Skin · cracked · Feb 17, 1995 · N824BX · Doug DC871 · Wing, Plate/Skin > DURING ROUTINE C-CHECK INSPECTION, EXTERNAL PLATING OF THE RIGHT WING EXHIBITED FOUR CRACKS. THE DAMAGE WAS AT WS XRS 74.8 BETWEEN STR 9 THROUGH STR 12. REPAIR OF THE AREA WAS ACCOMPLISHED BY CUTTING OUT THE CRACKS, INSTALLING FILLERS FOR THE REMOVED MATERIA - [SDR IXXA9541](https://openairdocs.org/sdr/IXXA9541.md): Belt Frame · corroded · Feb 14, 1995 · N824BX · Doug DC871 · Fuselage Main, Frame > DURING ROUTINE C-CHECK INSPECTION, STA 1120 BELT FRAME WAS FOUND CORRODED. DAMAGE WAS LIMITED TO ONE AREA JUST INBOARD OF LONGERON 35 RT AND APPROXIMATELY 1 INCH IN DIAMETER. THE DAMAGE WAS REPAIRED BY CUT-OUT, INSTALLING A FILLER, AND INSTALLING AN EXTERNAL - [SDR IXXA9540](https://openairdocs.org/sdr/IXXA9540.md): Belt Frame · corroded · Feb 14, 1995 · N824BX · Doug DC871 · Fuselage Main, Frame > DURING ROUTINE C-CHECK INSPECTION, LOCALIZED CORROSION WAS FOUND AT STA 1020 BELT FRAME. TWO AREAS, ONE AT LONGERON 34.5 RT AND ONE AT 34.5 LT, WERE 1 INCH BY 1 INCH AREAS. CORROSION REMOVAL WENT BEYOND SRM LIMITS. REPAIR OF THE BELT FRAME IAW DRAWING HSE27 - [SDR IXXA9538](https://openairdocs.org/sdr/IXXA9538.md): Drag Angle · cracked · Feb 12, 1995 · N824BX · Doug DC871 · Nacelle/Pylon Structure > DURING ROUTINE C-CHECK INSPECTION, A 2.200 INCH CRACK WAS FOUND IN THE NR 2 PYLON, INBOARD DRAG ANGLE. AFTER EVALUATION BY DOUGLAS AND FAA DER APPROVAL, THE AIRCRAFT WAS RETURNED TO SERVICE WITH FOLLOW-UP INSPECTIONS REQUIRED AT C-CHECK AND REPLACEMENT REQUIR - [SDR IXXA9539](https://openairdocs.org/sdr/IXXA9539.md): Hinge Fitting · cracked · Feb 2, 1995 · N824BX · Doug DC871 · Trailing Edge Flaps > DURING ROUTINE C-CHECK, THE LEFT OUTBOARD FLAP, INBOARD FLAP BASE HINGE FITTING WAS CRACKED IN HALF ON THE OUTBOARD HALF. THE FITTING WAS REPLACED IAW DOUGLAS SB 27-249 AND THE AIRCRAFT MM. (X) ## 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 = 'N824BX' AND deregistration_id = 'N824BX-2006-05-16' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N824BX-2006-05-16/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.