N808US, cancelled Jul 20, 2007

Service difficulty reports · 47

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N808US' AND deregistration_id = 'N808US-2007-07-20'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR USAAD01169Generator · failedBOS-CLT - FLT 323 - DURING CRUISE, THE RIGHT ENGINE DRIVEN GENERATOR BECAME INOPERATIVE. AS THE LEFT ENGINE GENERATOR WAS ALREADY INOPERATIVE AND RELEASED PER MEL PROCEDURES, THE AIRCRAFT DIVERTED AND LANDED AT RIC WITHOUT INCIDENT. MAINTENANCE REPLACED THE ROct 11, 2001 · N808US · Doug DC981 · AC Generator-AlternatorSDR USAA010951Doubler · crackedPIT - FOUND DOUBLER/ANGLE CRACKED .75 INCH, AFT PSG CABIN DOOR JAMB, LEFT UPPER FRAME. REMOVED DOUBLER, INSTALLED DOUBLER ANGLE PER SRM 53-05 FIG 30A. (M)Jul 28, 2001 · N808US · Doug DC981 · DoorsSDR USAAD01130Module · failedBOS-BWI - FLT 247 - THE LAST THREE ROWS OF LOW LEVEL EMERGENCY LIGHTS ILLUMINATED DURING FLIGHT. MAINTENANCE REPLACED THE AFT LOW LEVEL EMERGENCY LIGHT CONTROL MODULE. (M)Jun 25, 2001 · N808US · Doug DC981 · Emergency LightingSDR USA2001F00002Light · inoperativeIND - THE LOW LEVEL EMERGENCY LIGHTS DID NOT TEST. MAINTENANCE REPLACED THE CONTROL MODULE BATTERIES, THE LOW LEVEL LIGHT BATTERIES, AND THE OVERWING EXIT IDENTIFIER LIGHT ASSEMBLY. REF USAAD01102. (M)May 12, 2001 · N808US · Doug DC981 · Emergency LightingSDR USA2001F00001Battery · dischargedIND - THE LOW LEVEL EMERGENCY LIGHTS DID NOT TEST. MAINTENANCE REPLACED THE CONTROL MODULE BATTERIES, THE LOW LEVEL LIGHT BATTERIES, AND THE OVERWING EXIT IDENTIFIER LIGHT ASSEMBLY. REF USAAD01102. (M)May 12, 2001 · N808US · Doug DC981 · Emergency LightingSDR USAAD01102Battery · dischargedIND - THE LOW LEVEL EMERGENCY LIGHTS DID NOT TEST. MAINTENANCE REPLACED THE CONTROL MODULE BATTERIES, THE LOW LEVEL LIGHT BATTERIES, AND THE OVERWING EXIT IDENTIFIER LIGHT ASSEMBLY. (M)May 12, 2001 · N808US · Doug DC981 · Emergency LightingSDR USAAD01054Strut · lowEWR-PIT - FLT 557 - AFTER TAKEOFF, THE NOSE LANDING GEAR RED INDICATION LIGHT REMAINED ON AND THE NOSE LANDING GEAR RETRACTED INDICATION PIN WAS NOT VISIBLE. THE LANDING GEAR WAS EXTENDED AND THE AIRCRAFT DIVERTED TO LGA AND LANDED WITHOUT INCIDENT. MAINTENAMar 17, 2001 · N808US · Doug DC981 · Nose/Tail Landing Gear Strut/AxleSDR USAAD01048Piston · defectiveBOS-CLT - FLT 1045 - AFTER TAKEOFF, AS THE LANDING GEAR WAS BEING RAISED, A VIBRATION BEGAN AND THE INTENSITY INCREASED WITH AIRSPEED. THE LANDING GEAR WAS LOWERED, BUT THE NOSE GEAR UNSAFE LIGHT ILLUMINATED AND THE MECHANICAL INDICATOR SHOWED UNSAFE. QRH PRMar 13, 2001 · N808US · Doug DC981 · Nose/Tail Landing Gear Strut/AxleSDR USAAD01044Proximity Sensor · failedMSY-CLT - FLT 1278 - AFTER LANDING GEAR RETRACTION, THE RED NOSE GEAR INDICATION LIGHT REMAINED LIT. THE LANDING GEAR WAS CYCLED AND THE LIGHT WENT OUT BUT CAME BACK ON 5 MINUTES LATER. THE AIRCRAFT CONTINUED TO THE NEXT STATION AND LANDED WITHOUT INCIDENT. Mar 8, 2001 · N808US · Doug DC981 · Landing Gear Position and WarningSDR USAAD00178Slide · deflatedRSW - THE TAILCONE EMERGENCY EVACUATION SLIDE FAILED TO INFLATE WHEN DEPLOYED. MAINTENANCE REPLACED THE TAILCONE EVACUATION SLIDE ASSEMBLY. (M)Nov 17, 2000 · N808US · Doug DC981 · Escape SlideSDR USAAD00143Strap · brokenPIT - ONE TAILCONE EVACUATION SLIDE COVER HOLD DOWN STRAP WAS FOUND BROKEN. MAINTENANCE REPLACED THE STRAP. (M)Sep 6, 2000 · N808US · Doug DC981 · Escape SlideSDR USAAD00137Light · failedPIT - FOUND EMERGENCY LIGHTS TO BE INOPERATIVE IN FIRST CLASS, THE VENTRAL STAIR AREA, AND THE EMERGENCY ESCAPE RAMP. MAINTENANCE REPLACED THE BATTERY PACK ASSEMBLIES IN THE FORWARD AND AFT POSITIONS, AND REPLACED THE INOPERATIVE LIGHT ASSEMBLY FOR THE EMERGEAug 19, 2000 · N808US · Doug DC981 · Emergency LightingSDR 20001129AP003Light · failedPIT - THE FORWARD SECTION OF THE PASSENGER CABIN OVERHEAD EMERGENCY LIGHTS AND THE VENTRAL STAIR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD PASSENGER CABIN OVERHEAD EMERGENCY LIGHT BATTERIES AND THE VENTRAL STAIR EMERGENCY LIGHT ASSEMAug 15, 2000 · N808US · Doug DC981 · Emergency LightingSDR USAAD00132Battery · dischargedPIT - THE FORWARD SECTION OF THE PASSENGER CABIN OVERHEAD EMERGENCY LIGHTS AND THE VENTRAL STAIR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD PASSENGER CABIN OVERHEAD EMERGENCY LIGHT BATTERIES AND THE VENTRAL STAIR EMERGENCY LIGHT ASSEMAug 15, 2000 · N808US · Doug DC981 · Emergency LightingSDR USAAD00077Battery · dischargedPIT - FOUND EMERGENCY LIGHTS WON''T TEST. MAINTENANCE REPLACED BATTERY PACKS. OPS CHECKED GOOD. (M)May 19, 2000 · N808US · Doug DC981 · Emergency LightingSDR USAAD00043Light · failedTPA - THE FORWARD ENTRY DOOR EMERGENCY EXIT IDENTIFIER LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE FORWARD ENTRY DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSEMBLY. (M)Mar 20, 2000 · N808US · Doug DC981 · Emergency LightingSDR USAA990944Skin · crackedPIT - DURING RON, FOUND 6 INCH CRACK AT LEFT WING, STATION XRS-214, OUTBOARD OF NR 7 SLAT TRACK AT L/E SKIN. INSTALLED DOUBLER PER SRM 57-068 FIG 4. (M)Aug 29, 1999 · N808US · Doug DC981 · Wing, Plate/SkinSDR USAAD98143Sensor · dirtyPHL - FLT 1622 - NOSE GEAR LIGHT WAS RED ON GEAR UP. CYCLED GEAR AND THE INDICATION WAS NORMAL. MAINTENANCE RESET PROX BOX AND PERFORMED BITE TEST, ALL NORMAL. CLEANED SENSORS A PRECAUTION. (M)Aug 14, 1998 · N808US · Doug DC981 · Landing Gear Position and WarningSDR USAAD98081Battery · dischargedROC - THE CEILING EMERGENCY EVACUATION LIGHTS FOR THE CENTER SECTION OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (X)May 6, 1998 · N808US · Doug DC981 · Emergency LightingSDR USAAD97167Controller · failedPIT - FL 2200 - AFTER TAKEOFF, CREW WAS NOT ABLE TO MAINTAIN PRESSURIZATION. THE FLOW LIGHT WAS ILLUMINATED. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPAIRED A LEAKING DUCT. SUBSEQUENTLY, THE PRESSURE SELECTOR ASSEMBLY WAS RSep 26, 1997 · N808US · Doug DC981 · Cabin Pressure ControllerSDR USAAD97149Battery · dischargedIND - FOUND FOUR CEILING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (X)Sep 4, 1997 · N808US · Doug DC981 · Emergency LightingSDR USAAD97089Retract Mech · lack of lubeFLT 2301 - BUF-DCA - ON APPROACH, DID NOT GET NOSE GEAR DOWN AND LOCKED LIGHT OR VISUAL INDICATION. SLOWED TO 160 KTS, CYCLED GEAR, GOT 3 GREENS. JACKED NOSE GEAR, INSPECTED. FOUND NEW GEAR NOT LUBED. LUBRICATED GEAR, CYCLED 20 TIMES, CHECKS GOOD. (M)May 19, 1997 · N808US · Doug DC981 · Landing Gear Retraction/Extension SystemSDR USAAD97014Windshield · crackedFLT 1706 - PIT-PWM - DURING CRUISE AT FL 370, OUTER PANE OF CAPTAINS WINDSHIELD SHATTERED. DIVERTED TO PHL. REPLACED CAPTAINS WINDSHIELD. (M)Jan 14, 1997 · N808US · Doug DC981 · Flight Compartment WindowsSDR USAAD96049Fuel Contl Unit · failedBOS - FL 478 - AT TOP OF CLIMB, FL 230, LEFT ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENT. OIL TEMPERATURE OF LEFT ENGINE WAS THIRTY TO THIRTY-FIVE DEGREES HIGHER THAN THE RIGHT ENGINE TEMPERATURE. FLIGHT RETURNED TO BOS AND SHUT DOWN ENGINE ON FINAL APPROAMay 3, 1996 · N808US · Doug DC981 · Fuel Control/Turbine EnginesSDR USAA950830Belt Frame · crackedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND 2 CRACKS .25 INCH LONG IN BELTFRAME AT STATION 1322 AT LONGERON 17R. REPLACED SECTION OF FRAME AND INSTALLED DOUBLERS PER SRM 53-03 FIG 31. (M)Jul 12, 1995 · N808US · Doug DC981 · Fuselage Main, FrameSDR USAA950835Frame · corrodedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED ON BELTFRAME 1287 BETWEEN LONGERON 22L AND 23L (CORROSION TASK RED C57-53301). ACCOMPLISHED REPAIR TO BELTFRAME PER SRM 53-03 FIG 30. (M)Jul 11, 1995 · N808US · Doug DC981 · Fuselage Main, FrameSDR USAA950829Longeron · crackedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND A .25 INCH CRACK AT LONGERON ATTACH POINTS TO FRAME STATION 160 LONG 3L. ACCOMPLISHED SPLICE TYPE REPAIR PER SRM 53-02 FIG 2. (M)Jul 11, 1995 · N808US · Doug DC981 · Fuselage Main, Longeron/StringerSDR USAA950828Longeron · crackedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND CRACK .25 INCH LONG AT BOTH ATTACH POINTS STATION 160 LONG 4L. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2. (M)Jul 11, 1995 · N808US · Doug DC981 · Fuselage Main, Longeron/StringerSDR USAA950827Intercostal · crackedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .375 INCH CRACK IN FITTING AT STATION 988 INSIDE HEEL ABOVE AFT END OF DOOR HINGE. INSTALLED DOUBLER REPAIR PER SRM 53-01. (M)Jul 11, 1995 · N808US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA950826Cusp Membrane · crackedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND CUSP MEMBRANE CRACKED 1 INCH LONG STATION 1250 RIGHT SIDE. MFG CUSP MEMBRANE PER SRM 53-05 FIG 79. (M)Jul 11, 1995 · N808US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA950825Cusp Membrane · crackedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND CUSP MEMBRANE CRACKED IN 2 PLACES BOTH 1 INCH LONG AT STATION 1287 LEFT. MFG NEW CUSP MEMBRANE PER SRM 53-05 FIG 79. (M)Jul 11, 1995 · N808US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA950820Clip · crackedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND CRACK AT SKIN CLIP .375 INCH LONG AT STATION 1459 BETWEEN LONGERON 2L AND 3L. MFG NEW SKIN CLIP AND INSTALLED PER SRM 53-03 FIG 28. (M)Jul 11, 1995 · N808US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA950819Clip · crackedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .5 INCH CRACK IN SKIN CLIP STATION 1459 BETWEEN LONGERON 2R AND 3R. MFG NEW SKIN CLIP AND INSTALLED PER SRM 53-03 FIG 28. (M)Jul 11, 1995 · N808US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA950821Seat Track · corrodedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND LEVEL 1 CORROSION AT RIGHT INBOARD SEAT TRACK AT BOTTOM INBOARD FLOOR ATTACH ANGLE AT STATION FS-205 (PREVIOUSLY REWORKED) CORROSION TASK REF C46-53305. REMOVED CORROSION AND SPLICED IN NEW SECTION OF SEAT TRACK PJul 10, 1995 · N808US · Doug DC981 · Fuselage, Seat/Cargo Attach FittingsSDR USAA950824Fitting · corrodedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND 3 INCH BY 4 INCH AREA OF CORROSION (LEVEL 1) AT FITTING AT AFT LOWER CORNER OF AIR STAIR DOOR STATION 200 LONGERON 21L (PREVIOUSLY REWORKED). CORROSION TASK NR REF C45-53301. INSTALLED NEW FITTING P/N 109-7172. Jul 6, 1995 · N808US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA950823Angle · crackedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .5 INCH CRACK IN SUPPORT ANGLE LEFT OF CENTER UNDER RADAR SUPPORT SHELF STATION 37 BULKHEAD HORIZONTAL ANGLE. INSTALLED DOUBLER REPAIR PER SRM 53-01. (M)Jul 6, 1995 · N808US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA950822Skin · crackedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .25 INCH CRACK IN TEMPORARY REPAIR ON WING LE AT INBOARD AND OUTBOARD EDGE OF FUEL SERVICE PANEL IN SKIN. REMOVED TEMP REPAIR AND STOP DRILLED CRACKS. INSTALLED DOUBLER REPAIR PER SRM 57-06B. (M)Jul 6, 1995 · N808US · Doug DC981 · Wing, Plate/SkinSDR USAA950818Cusp Web · crackedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND 1 INCH CRACK IN STATION 825 TO 845 LONGERON 18R CUSP WEB. REPLACED SECTION OF CUSP WEB PER SRM 53-05 FIG 27. (M)Jul 6, 1995 · N808US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA950817Longeron · crackedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .125 INCH CRACK IN LONGERON 3L AT STATION 160. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2. (M)Jul 6, 1995 · N808US · Doug DC981 · Fuselage Main, Longeron/StringerSDR USAA950816Skin · damagedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND A LIGHTNING STRIKE LEAVING A .020 INCH PIT AT FUSELAGE SKIN STATION 636 BETWEEN LONGERON 9R AND 10R. REMOVED DAMAGE AND INSTALLED FILLER AND INTERNAL DOUBLER REPAIR PER SRM 53-04 FIG 38. (M)Jul 6, 1995 · N808US · Doug DC981 · Fuselage Main, Plate/SkinSDR USAA950815Angle · crackedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND A 1 INCH CRACK IN TOP KEEL BEAM 'T' ANGLE ON HORIZONTAL LEG AT STATION 985. SPLICED IN NEW SECTION OF ANGLE AND DOUBLER PER USAIR EA 30834. (M)Jul 6, 1995 · N808US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA950814Jamb · corrodedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND CORROSION IN MED STATION 200 BOTTOM LEFT AFT DOOR JAMB. CUT OUT CORRODED SECTION OF JAMB AND INSTALLED DOUBLER REPAIR PER USAIR EA 308 AND SRM 53-05 FIG 55. (M)Jul 6, 1995 · N808US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA950834Window Pan · crackedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .25 INCH CRACK STATION 888 LEFT WINDOW PAN. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-50-06. (M)Jun 30, 1995 · N808US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA950833Window Pan · crackedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .25 INCH CRACK STATION 929 LEFT SIDE WINDOW PAN. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-50-06. (M)Jun 30, 1995 · N808US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA950832Window Pan · crackedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .25 INCH CRACK STATION 948 LEFT SIDE WINDOW PAN. INSTALLED DOUBLER TYPE REPAIR PER USAIR TYPICAL REPAIR 53-50-06. (M)Jun 30, 1995 · N808US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA950831Le Web · crackedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND A .25 INCH CRACK RIGHT INBOARD WEB LEADING EDGE TO HORIZONTAL STABILIZER FROM SPAR. INSTALLED DOUBLER REPAIR IAW SRM 55-01 FIG 5. (M)Jun 30, 1995 · N808US · Doug DC981 · Horizontal Stabilizer StructureSDR USAA950813Frame · crackedPIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND 2 CRACKS ONE .0625 INCH AND ONE .1875 INCH IN FRAME STATION 1463 LEFT SIDE DORSAL FIN ATTACH ANGLE. INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 23B. (M)Jun 30, 1995 · N808US · Doug DC981 · Fuselage Main, Frame
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