# Service difficulty reports: N817US, cancelled May 21, 2004 A list on [N817US, cancelled May 21, 2004](https://openairdocs.org/deregistered/N817US-2004-05-21.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR USAAD01191](https://openairdocs.org/sdr/USAAD01191.md): Odor · detected · Dec 16, 2001 · N817US · Doug DC982 · Air Distribution System > ORD - PIT - FLT 1194 - THERE WAS A STRONG RUBBER SMELL IN THE AIRCRAFT DURING TAKEOFF. THE SMELL DISAPPEARED SHORTLY AFTER GEAR RETRACTION. MAINTENANCE NOTICED A SLIGHT TIRE RUBBER SMELL IN THE MAIN WHEEL WELLS. THE CONDITION OF THE MAIN WHEEL WELLS AND TIR - [SDR 2002F00000](https://openairdocs.org/sdr/2002F00000.md): Battery · discharged · Dec 12, 2001 · N817US · Doug DC982 · Emergency Lighting > IND - THE MAIN ENTRY EMERGENCY LIGHT AND THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE MAIN ENTRY EMERGENCY LIGHT ASSEMBLY AND THE LOW LEVEL EMERGENCY LIGHT BATTERIES. (M) - [SDR USAAD01189](https://openairdocs.org/sdr/USAAD01189.md): Light · inoperative · Dec 12, 2001 · N817US · Doug DC982 · Emergency Lighting > IND - THE MAIN ENTRY EMERGENCY LIGHT AND THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE MAIN ENTRY EMERGENCY LIGHT ASSEMBLY AND THE LOW LEVEL EMERGENCY LIGHT BATTERIES. (M) - [SDR USAAD01187](https://openairdocs.org/sdr/USAAD01187.md): Receiver · inoperative · Dec 8, 2001 · N817US · Doug DC982 · Emergency Lighting > PIT - THE CATWALK EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT RECEIVER. (M) - [SDR USAAD00133](https://openairdocs.org/sdr/USAAD00133.md): Fuel Control · leaking · Aug 16, 2000 · N817US · Doug DC982 · APU Engine Fuel and Control > FLL-PIT - FLT 1821 - FUEL SMELL IN PASSENGER CABIN AND COCKPIT. MAINTENANCE REPLACED THE APU FUEL CONTROL UNIT. (M) - [SDR USAAD00131](https://openairdocs.org/sdr/USAAD00131.md): Unknown · odor · Aug 14, 2000 · N817US · Doug DC982 · Air Distribution System > CLT-BOS - FLT 506 - 45 MINUTES AFTER TAKEOFF, THE SMELL OF JET FUEL WAS VERY STRONG. SMELL LASTED 15 MINUTES. MAINTENANCE RAN THE ENGINES, CHECKED THE AIR CONDITIONING COMPONENTS AND THE AIR CYCLE UNITS. THE WING AND WING PANELS WERE INSPECTED FOR SEEPAGE A - [SDR USAA000298](https://openairdocs.org/sdr/USAA000298.md): Skin · cracked · Feb 9, 2000 · N817US · Doug DC982 · Fuselage Main, Plate/Skin > PIT - FOUND TWO SKIN CRACKS BOTH.125 INCH LONG, AT STATION 1380 BETWEEN LONGERON 14R AND 15R. CUT OUT DAMAGED, INSTALLED FILLERS AND DOUBLERS PER SRM 53-04 FIG 18 SHT 1 PAGE 98A. (M) - [SDR USAA000299](https://openairdocs.org/sdr/USAA000299.md): Longeron · cracked · Feb 9, 2000 · N817US · Doug DC982 · Fuselage Main, Longeron/Stringer > PIT - FOUND LONGERON 1 INCH CRACK, STATION 160 LONGERON 4L. CUT OUT DAMAGED SECTION, INSTALLED NEW AND SPLICED PER SRM 53-02 FIG 18. (M) - [SDR USAA000300](https://openairdocs.org/sdr/USAA000300.md): Longeron · cracked · Feb 9, 2000 · N817US · Doug DC982 · Fuselage Main, Longeron/Stringer > PIT - FOUND 2 INCH CRACK, STATION 160 LONGERON 2L. CUT OUT DAMAGED SECTION. INSTALLED NEW AND SPLICED PER SRM 53-02 FIG 18. (M) - [SDR USAA000301](https://openairdocs.org/sdr/USAA000301.md): Floorbeam · corroded · Feb 9, 2000 · N817US · Doug DC982 · Fuselage Main, Floor Beam > PIT - FOUND CORROSION, 1 INCH BY 20 INCHES, FLOORBEAM UPPER CHORD, STATION 1309. CUT OUT CORRODED SECTION. INSTALLED NEW AND SPLICED PER EA 54092. CORROSION LEVEL 1. (M) - [SDR USAA000302](https://openairdocs.org/sdr/USAA000302.md): Longeron · cracked · Feb 9, 2000 · N817US · Doug DC982 · Fuselage Main, Longeron/Stringer > PIT - FOUND 1.5 INCH CRACK AT STATION 160, LONGERON 3L. CUT OUT DAMAGED SECTION, INSTALLED NEW AND SPLICED PER SRM 53-02, FIG 18. (M) - [SDR USAA000303](https://openairdocs.org/sdr/USAA000303.md): Longeron · cracked · Feb 9, 2000 · N817US · Doug DC982 · Fuselage Main, Longeron/Stringer > PIT - FOUND 1 INCH CRACK AT STATION 160 LONGERON NR 1. CUT OUT DAMAGED SECTION, INSTALLED NEW AND SPLICED PER SRM 53-02, FIG 18. (M) - [SDR USAAD99012](https://openairdocs.org/sdr/USAAD99012.md): Battery · discharged · Jan 18, 1999 · N817US · Doug DC982 · Emergency Lighting > BUF - THE OVERHEAD EMERGENCY LIGHT AT SEAT ROW 30 AND BETWEEN THE AFT LAVATORIES WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) - [SDR USAAD98141](https://openairdocs.org/sdr/USAAD98141.md): Engine · malfunctioned · Aug 9, 1998 · N817US · Doug DC982 · Engine (Turbine/Turboprop) > PIT - FLT 365 - EN ROUTE BUF-CLT - CREW NOTED A RISE IN THE LEFT ENGINE OIL TEMPERATURE, EXCEEDING 165 DEGREES. THE ENGINE STARTED TO VIBRATE. CREW SECURED THE ENGINE. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE ENG - [SDR USAAD98135](https://openairdocs.org/sdr/USAAD98135.md): Filter · clogged · Aug 5, 1998 · N817US · Doug DC982 · Turbine Engine Oil System > PIT-TPA - FLT 219 - THE RIGHT ENGINE OIL FILTER CLOG LIGHT ILLUMINATED DURING CRUISE. AFTER ABNORMAL PROCEDURES FAILED TO EXTINGUISH THE LIGHT THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT DIVERTED TO CLT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLA - [SDR USAAD97180](https://openairdocs.org/sdr/USAAD97180.md): Retract Mech · malfunctioned · Oct 15, 1997 · N817US · Doug DC982 · Landing Gear Retraction/Extension System > PHL - FLT 531 - AFTER TAKEOFF, NOSE GEAR DID NOT RETRACT. CREW CYCLED THE GEAR. FLIGHT RETURNED TO PHL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE PERFORMED A GEAR SWING AND COULD NOT DUPLICATE THE FAULT. THE GEAR WAS LUBED AS A PRECAUTION. (X) - [SDR USAAD97045](https://openairdocs.org/sdr/USAAD97045.md): Downlock Ind · failed · Feb 24, 1997 · N817US · Doug DC982 · Landing Gear Position and Warning > FLT 1192 - PIT-BDL - WHEN GEAR WAS EXTENDED AT BDL, NOSEGEAR DOWN AND LOCKED LIGHT DID NOT ILLUMINATED. CYCLED GEAR AND LIGHT STILL DID NOT ILLUMINATE. DID TOWER FLYBY, AND LANDED NORMALLY AT BDL. RELAMPED DOWN AND LOCKED INDICATOR. (M) - [SDR USAAD96128](https://openairdocs.org/sdr/USAAD96128.md): Engine · failed · Sep 15, 1996 · N817US · Doug DC982 · Engine (Turbine/Turboprop) > FLT 984 - CLT-ORF - AFTER TAKEOFF, THE NR 2 OIL FILTER CLOGGING LIGHT ILLUMINATED. AT IDLE POWER, THE LIGHT REMAINED ILLUMINATED, ACCOMPANIED BY RISING OIL TEMPERATURE AND REDUCED FUEL FLOW. SHUT DOWN NR 2 ENGINE, AND RETURNED TO FIELD. 19 MINUTES SINGLE ENG - [SDR USAAD96124](https://openairdocs.org/sdr/USAAD96124.md): Comp Blades · fod damage · Sep 2, 1996 · N817US · Doug DC982 · Turbine Engine Compressor Section > FLT 1224 - ATL-PIT - LEFT ENGINE COMPRESSOR STALLS ON CLIMB-OUT FROM ATL. RETURNED TO FIELD. NO ENGINE SHUTDOWN. FOUND FOD DAMAGE TO 7TH STAGE COMPRESSOR BLADES. REPLACED ENGINE. (M) - [SDR USAAD96104](https://openairdocs.org/sdr/USAAD96104.md): Temp Sensors · failed · Jul 14, 1996 · N817US · Doug DC982 · Overheat Detection > FLT NR 1665 - PIT-FLL - 'TAIL COMPT TEMP HIGH' LIGHT ILLUMINATED DURING CLIMB. RETURNED TO FIELD. REPLACED WIRING BETWEEN TAIL COMPARTMENT TEMPERATURE SENSORS AND AFT PRESSURE BULKHEAD. (M) - [SDR USAAD96100](https://openairdocs.org/sdr/USAAD96100.md): Battery Pack · discharged · Jul 9, 1996 · N817US · Doug DC982 · Emergency Lighting > FIRST CLASS FLOOR TRACK LIGHTING INOPERATIVE. REPLACED BATTERY PACK. (M) - [SDR USAAD96085](https://openairdocs.org/sdr/USAAD96085.md): Circuit Breaker · failed · Jun 24, 1996 · N817US · Doug DC982 · Overheat Detection > FLT 765 - CLT-MSY - ON CLIMB, WHEEL WELL OVERHEAT CIRCUIT BREAKER POPPED. RETURNED TO FIELD. REPLACED CIRCUIT BREAKER. (M) - [SDR USAAD96073](https://openairdocs.org/sdr/USAAD96073.md): Cooling Screen · dirty · Jun 8, 1996 · N817US · Doug DC982 · AC Generator-Alternator > FLT 985 - BDL-TPA - WITH RIGHT GENERATOR ON MEL AND APU RUNNING FOR ELECTRICAL POWER, GOT APU OIL TEMP HI CAUTION LIGHT AT FL 350. DESCENDED TO FL 250, AND LIGHT WENT OUT. FLIGHT DIVERTED TO CLT DUE TO FUEL AND WEATHER CONSIDERATIONS AT NEW ALTITUDE. FOUND - [SDR USAA951244](https://openairdocs.org/sdr/USAA951244.md): Frame · corroded · Nov 22, 1995 · N817US · Doug DC982 · Fuselage Main, Frame > PIT - DURNG Q1/C6 INSPECTION, FOUND 2 INCH BY 1 INCH CORRODED AREA PREVIOUSLY REWORKED BELT FRAME, STA 1250, BETWEEN LONGERON 28R AND LONGERON 29R. CORROSION TASK REF C57-53300, LEVEL 1. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 53-14, FIGURE 5. - [SDR USAA951243](https://openairdocs.org/sdr/USAA951243.md): Fitting · corroded · Nov 22, 1995 · N817US · Doug DC982 · Fuselage Miscellaneous Structure > PIT - DURING Q1/C6 INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED, STA 180 - STA 200, RT SIDE BELOW FORWARD SERVICE DOOR IN FITTINGS AND CUSP ANGLE. CORROSION TASK NR C46-53305. SPLICED IN NEW SECTION OF CUSP AND FITTINGS PER SRM 53-03-5, CONF. J060 - [SDR USAA951242](https://openairdocs.org/sdr/USAA951242.md): Longeron · corroded · Nov 22, 1995 · N817US · Doug DC982 · Fuselage Main, Longeron/Stringer > PIT - DURING Q1/C6 INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED, LONGERON 28L SPLICE AT STA 228. CORROSION TASK NR C51-53300. ACCOMPLISHED SPLICE REPAIR PER SRM 53-02-14. (X) - [SDR USAA951241](https://openairdocs.org/sdr/USAA951241.md): Support Rail · corroded · Nov 22, 1995 · N817US · Doug DC982 · Fuselage Miscellaneous Structure > PIT - DURING Q1/C6 INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED, LT AND RT FLOOR SUPPORT RAILS, STA 218 - STA 541, FORWARD CARGO, CORROSION TASK NR C51-5330. INSTALLED SPLICE REPAIR PER USAIR TYPICAL REPAIR 53-20-09A. (X) - [SDR USAA951240](https://openairdocs.org/sdr/USAA951240.md): Skin · cracked · Nov 22, 1995 · N817US · Doug DC982 · Wing, Plate/Skin > PIT - DURING Q1/C6 INSPECTION, FOUND 4.75 INCH CRACK JUST OUTBOARD OF NR 7 SLAT TRACK CUT-OUT LEADING EDGE SKIN. INSTALLED INTERNAL AND EXTERNAL DOUBLERS PER SRM 57-06A, FIGURE 1, AND USAIR EA NR 31672. (X) - [SDR USAA951239](https://openairdocs.org/sdr/USAA951239.md): Longeron · corrosion · Nov 22, 1995 · N817US · Doug DC982 · Fuselage Main, Longeron/Stringer > PIT - DURING Q1/C6 INSPECTION, FOUND.50 INCH BY 9 INCH AREA OF LEVEL 1 CORROSION RESULT FROM UNIQUE EVENT, BROKEN WATER LINE. CORROSION TASK NR C57-53300. LONGERON 28L FROM STA 1315 - STA 1332. ACCOMPLISHED SPLICE REPAIR PER SRM 53-02-14 AND USAIR EA NR 31 - [SDR USAA951238](https://openairdocs.org/sdr/USAA951238.md): Skin · cracked · Nov 22, 1995 · N817US · Doug DC982 · Fuselage Main, Plate/Skin > PIT - DURING Q1/C6 INSPECTION, FOUND CRACK APPROXIMATELY 1 INCH LONG IN SECOND LAYER OF SKIN IN UPPER FORWARD CORNER OF M.E.D. IN FUSELAGE SKIN (X-RAY INSPECTION) SSI 53-11-015. CUT OUT CRACK AND INSTALLED FILLER AND DOUBLERS PER SRM 53-05, FIGURE 25A. (X) - [SDR USAA951237](https://openairdocs.org/sdr/USAA951237.md): Skin · cracked · Nov 22, 1995 · N817US · Doug DC982 · Fuselage Main, Plate/Skin > PIT - DURING Q1/C6 INSPECTION, FOUND.020 INCH CRACK IN LIGHTNING STRIKE AREA OF FUSELAGE EXTERIOR SKIN AT STA 380, LONGERON 6L AND LONGERON 7L. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR NR 53-30-11. (X) - [SDR USAA951236](https://openairdocs.org/sdr/USAA951236.md): Clip · corroded · Nov 22, 1995 · N817US · Doug DC982 · Fuselage Miscellaneous Structure > PIT - DURING Q1/C6 INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED AT STA 1060 BETWEEN LONGERON 29R AND LONGERON 30R SKIN CLIP. CORROSION TASK NR C57-53300. SPLICED IN SECTION OF SKIN CLIP PER SRM 53-03, FIGURE 3. (X) - [SDR USAA951234](https://openairdocs.org/sdr/USAA951234.md): Membrane · cracked · Nov 22, 1995 · N817US · Doug DC982 · Fuselage Miscellaneous Structure > PIT - DURING A Q-1 CHECK INSPECTION, FOUND.5 INCH CRACK IN CUSP MEMBRANE WEB STATION 1032 OUTBOARD OF RT SEAT TRACK. ACCOMPLISHED SPLICE REPAIR PER USAIR EA NR 315530A. (M) - [SDR USAA951212](https://openairdocs.org/sdr/USAA951212.md): Frame · cracked · Nov 14, 1995 · N817US · Doug DC982 · Fuselage Main, Frame > PIT - DURING Q-1/C-6 INSPECTION, FOUND.5 INCH CRACK AT CANTED FRAME 1485 AT LONGERON 7L. STOPPED DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-14-4 FIG 3. (M) - [SDR USAA951211](https://openairdocs.org/sdr/USAA951211.md): Skin · cracked · Nov 14, 1995 · N817US · Doug DC982 · Fuselage Main, Plate/Skin > PIT - DURING Q-1/C-6 INSPECTION, FOUND 1.09375 INCH CRACK AT STATION 821 AND LONGERON 17R IN EXTERIOR SKIN. CUTOUT DAMAGED AREA AND INSTALLED FILLER AND 6.5 INCH BY 8.5 INCH INTERNAL DOUBLER PER SRM 53-04 FIG 38 VIEW H. (M) - [SDR USAA951210](https://openairdocs.org/sdr/USAA951210.md): Clip · cracked · Nov 14, 1995 · N817US · Doug DC982 · Fuselage Miscellaneous Structure > PIT - DURING Q-1/C-6 INSPECTION, FOUND 1 INCH CRACK IN FRAME TO FUSELAGE CLIP AFT SIDE OF BS 1437 AT LONGERON 1. SPLICED IN NEW CLIP PER SRM 53-03 FIG 6. (M) - [SDR USAA951209](https://openairdocs.org/sdr/USAA951209.md): Cusp Membrane · cracked · Nov 14, 1995 · N817US · Doug DC982 · Fuselage Miscellaneous Structure > PIT - DURING Q-1/C-6 INSPECTION, FOUND.25 INCH CRACK RIGHT SIDE CABIN STATION 984 AND 1003 AT LONGERON 18 CUSP LINE MEMBRANE. MANUFACTURED CUSP MEMBRANE AND INSTALLED PER SRM 53-05 FIG 97. (M) - [SDR USAA950006](https://openairdocs.org/sdr/USAA950006.md): Clamp · leaking · Jan 4, 1995 · N817US · Doug DC982 · Cabin Cooling System > MCO - FLT 2382 - AFTER DEPARTING MCO, CREW RECEIVED AND OVERHEAT INDICATION IN THE TAIL SECTION. THE CREW FOLLOWED EMERGENCY PROCEDURES TO ISOLATE THE PROBLEM. THE LT PACK WAS SHUTDOWN, BUT THE CABIN PRESSURE COULD NOT BE MAINTAINED ON THE RIGHT PACK. THE C - [SDR USAA950009](https://openairdocs.org/sdr/USAA950009.md): Lines · loose · Jan 1, 1995 · N817US · Doug DC982 · Cabin Pressure Control System > CLT - FLT 1133 - A VIBRATION WAS REPORTED IN THE FLOOR OF THE ACFT AND AFT JUMPSEAT AREA. THE CREW DECIDED TO DIVERT TO CLT. FOUND SENSE LINES TO LT AUGMENTATION VALVE AND PILOT PRESSURE REGULATORS LOOSE. TIGHTENED LINES. (W) ## 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 = 'N817US' AND deregistration_id = 'N817US-2004-05-21' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N817US-2004-05-21/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.