N803US, cancelled Feb 12, 2009

Service difficulty reports · 35

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 = 'N803US' AND deregistration_id = 'N803US-2009-02-12'
  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 USAAD01175Slide · unserviceablePIT - THE L2 SERVICE DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS LOW. MAINTENANCE REPLACED THE EMERGENCY EVACUATION SLIDE. (M)Oct 21, 2001 · N803US · Doug DC981 · Escape SlideSDR USAAD01146Receiver · inoperativeCLT - THE AFT OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMEREGNCY LIGHTS REMOTE RECEIVER. OPERATIONALLY CHECKED OK. (M)Aug 5, 2001 · N803US · Doug DC981 · Emergency LightingSDR USAA010682Skin · crackedPIT - FOUND SKIN CRACKED .125 INCH, STATION 1380 AT L14L. CUT OUT CRACK, INSTALLED FILLER AND DOUBLER PER SRM 53-01 FIG 2 SHT 3. (M)Jun 11, 2001 · N803US · Doug DC981 · Fuselage Main, Plate/SkinSDR USAAD01110Battery · dischargedTPA - THE LOW LEVEL EMERGENCY LIGHT AT SEAT ROW 11 AND THE EMERGENCY LIGHT AT THE AFT RIGHT SERVICE DOOR WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)May 19, 2001 · N803US · Doug DC981 · Emergency LightingSDR USA2001F00000Receiver · failedWOULD NOT TEST. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES AND THE TAILCONE EMERGEIND - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE AND THE TAILCONE EMERGENCY REMOTE RECEIVER NCY REMOTE RECEIVER. REF USAAD01095. (M)May 4, 2001 · N803US · Doug DC981 · Emergency LightingSDR USAAD01095Battery · dischargedWOULD NOT TEST. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES AND THE TAILCONE EMERGEIND - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE AND THE TAILCONE EMERGENCY REMOTE RECEIVER NCY REMOTE RECEIVER. (M)May 4, 2001 · N803US · Doug DC981 · Emergency LightingSDR 20010529SG004Regulator · failedMIA-CLT - FLT 1850 - AFTER TAKEOFF, THERE WAS A BURNING SMELL EMANATING FROM THE LEFT AIR CONDITIONING PACK. THE LEFT PACK WAS SHUTOFF AND THE ODOR WENT AWAY. THE AIRCRAFT CONTINUED TO ITS DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE LEFTMay 3, 2001 · N803US · Doug DC981 · Cabin Cooling SystemSDR USAAD01094Regulator Valve · failedMIA-CLT - FLT 1850 - AFTER TAKEOFF, THERE WAS A BURNING SMELL EMANATING FROM THE LEFT AIR CONDITIONING PACK. THE LEFT PACK WAS SHUTOFF AND THE ODOR WENT AWAY. THE AIRCRAFT CONTINUED TO ITS DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE LEFTMay 3, 2001 · N803US · Doug DC981 · Cabin Cooling SystemSDR USAAD01093Coupling · disconnectedCLT-MIA - FLT 895 - AFTER TAKEOFF THERE WAS A SLIGHT ODOR AND THE LEFT AIR CONDITIONING PACK TRIPPED OFF. WITH THE AIR CONDITIONING PACK OFF THE ODOR WENT AWAY. THE LEFT PACK WAS TURNED OFF FOR THE DURATION OF THE FLIGHT AND THE AIRCRAFT ARRIVED AT ITS DESTIMay 3, 2001 · N803US · Doug DC981 · Cabin Cooling SystemSDR USAAD01091Duct · contaminatedPIT-BUF - FLT 1120 - AFTER TAKEOFF, THE LAVATORY SMOKE DETECTORS ACTIVATED AND THERE WAS THE SMELL OF SMOKE IN THE CABIN. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE ISOLATED THE PROBLEM TO THE APU, AND PLACED THE APU ON MEL. May 1, 2001 · N803US · Doug DC981 · APU Cowling/ContainmentSDR USAAD01088Battery · dischargedMCO - THE LOW LEVEL EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)Apr 30, 2001 · N803US · Doug DC981 · Emergency LightingSDR USAAD01079Link · brokenCMH-DCA - FLT 835 - AFTER TAKEOFF, WITH THE LANDING GEAR HANDLE RAISED THE RIGHT GEAR RED UNSAFE LIGHT AND THE AMBER GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED. QRH PROCEDURES WERE FOLLOWED, ALL LIGHTS EXTINGUISHED WITH THE GEAR DOWN BUT NO CHANGE WITH THE GEAApr 9, 2001 · N803US · Doug DC981 · Landing Gear Retraction/Extension SystemSDR USAA001946Longeron · corrodedPIT - FOUND LONGERON CORRODED .75 INCH BY 30 INCHES, LONGERON 30 STATION 1309 TO 1324. CORROSION LEVEL 1. MFG LONGERON SECTION AND NEW LONG SPLICES PER SRM 53-02 FIG 14. (M)Nov 19, 2000 · N803US · Doug DC981 · Fuselage Main, Longeron/StringerSDR USAAD00172Transformer · failedMCO-PHL - FLT 1484 - DURING CRUISE, THERE WAS AN AC CROSS-TIE LOCKOUT AND A LEFT GENERATOR FEEDER FAULT. THE APU GENERATOR WAS BROUGHT ON LINE BUT FAILED AFTER 10 MINUTES AT 33,000 FT. THE AIRCRAFT DIVERTED TO CLT. DURING THE DIVERSION THE APU RESTARTED AT Nov 6, 2000 · N803US · Doug DC981 · AC Generation SystemSDR USAA002190Web · corrodedPIT - FOUND WEB CORRODED .032 INCH DEEP, STATION 1338 FROM LONGERON 27 LT TO 27 RT. WEBS AND DOUBLERS MADE FROM 7075T6 .040 PER TYPICAL REPAIR 53-30-10. (M)Oct 19, 2000 · N803US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA001943Former · corrodedPIT - FOUND SKIN FORMER CORRODED 36 INCHES LONG, STATION 1287 LONGERON 28 LT TO 28 RT. REMOVED OLD PART AND REPLACED WITH NEW PART PER SRM 53-03 FIG 3. (M)Oct 18, 2000 · N803US · Doug DC981 · Fuselage Main, FrameSDR USAA001944Longeron · corrodedPIT - FOUND LONGERON CORRODED .75 INCH WIDE BY 6 INCHES LONG, LONGERON 30 FROM STATION 1287 TO 1297. CORROSION LEVEL 1. NEW LONG SECTION INSTALLED WITH NEW LONG SPLICE PIECES PER SRM 53-02 FIG 14 AND 15. (M)Oct 18, 2000 · N803US · Doug DC981 · Fuselage Main, Longeron/StringerSDR USAA001945Skin · corrodedPIT - FOUND SKIN CORRODED TWO PLACES, .25 INCH DIAMETER AND .035 AND .047 DEEP, STATION 1287 AT LONGERON 28 RT. CORROSION LEVEL 1. REPAIRED WITH .025 (6 AL-4V TITANIUM) DOUBLER INTERNAL 8 INCHES BY 7.5 INCHES PER SRM 53-04 FIG 38 SHT 22. (M)Oct 18, 2000 · N803US · Doug DC981 · Fuselage Main, Plate/SkinSDR USAA001951Skin · crackedPIT - FOUND LEADING EDGE CRACKED 5.5 INCHES, LT WING FIXED L/E OUTBOARD OF NR 7 SLAT TRACK OPENING. REPAIRED WITH 4 INCH BY 5 INCH DOUBLER WITH BLIND FASTENERS, STOP DRILLED CRACK, PER SRM 57-06A FIG 1A. TEMP REPAIR EA 56594. (M)Oct 17, 2000 · N803US · Doug DC981 · Wing, Plate/SkinSDR USAAD98187Engine · failedBUF-PHL - FLT 1045 - UPON DESCENDING FROM CRUISE THE THROTTLES WERE RETARDED AND A SEVERE VIBRATION WAS FELT. THE RIGHT ENGINE VIBRATION METER WAS AT FULL SCALE. THE THROTTLES WERE MOVED TO IDLE AND THE VIBRATION SUBSIDED. REAPPLICATION OF POWER BROUGHT BACOct 18, 1998 · N803US · Doug DC981 · Engine (Turbine/Turboprop)SDR USAA980080Longeron · crackedPIT - DURING Q-4/C-3 INSPECTION, FOUND .5 INCH CRACK AT STATION 160 LONGERON 4 LEFT. SPLICED IN NEW SECTION OF LONGERON AND REPLACED END FITTING PER SRM 53-02 FIG 18 SHEET 1-6. (M)Feb 20, 1998 · N803US · Doug DC981 · Fuselage Main, Floor BeamSDR USAA990005Clip · crackedPIT - DURING C-4 CHECK, FOUND 2 INCH CRACK IN SKIN SLIP AT STATION 1437 LONGERON 2RT. REPLACED DEFECTIVE PART WITH IDENTICAL PART NUMBER. (M)Jan 8, 1998 · N803US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA990004Clip · crackedPIT - DURING C-4 CHECK, FOUND 2 INCH CRACK IN SKIN CLIP AT STATION 1437 LONGERON 2 LT. REPLACED DEFECTIVE PART WITH IDENTICAL PART NR. (M)Jan 8, 1998 · N803US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA990003Beam · crackedPIT - DURING C-4 CHECK, FOUND CRACK 2.625 LONG AT BEAM AND ANGLES AT STATION 1429 BELTFRAME AT 2LT (LONGER). REPLACED BELTFRAME AND WEB PER DRAWING 9911840. (M)Jan 8, 1998 · N803US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA990002Former · crackedPIT - DURING C-4 CHECK, FOUND VERTICAL STABILIZER L/E FORMERS CRACKED ON AFT ENDS. SEE EA 49052 FOR DETAILS. REPLACED FORMERS ON VERTICAL STAB PER EA 49052. (M)Jan 8, 1998 · N803US · Doug DC981 · Vertical Stabilizer, Spar/RibSDR USAA970307Angle · crackedPIT - DURING C-2 CHECK, FOUND CRACK IN DRAG ANGEL (RT SIDE) AT STATION 1416 LONGERON 2 RT. DRAG ANGLE REMOVED AND REPLACED PER EO 5388XX223. (M)Oct 23, 1997 · N803US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA970306Frame · crackedPIT - DURING C-2 CHECK, FOUND 1.5 INCH CRACK EXTENDED INTO RADIUS AT TAIL COMPARTMENT, AFT LEFT SIDE OF CANTED FRAME 1388, VERTICAL STAB FRONT SPAR. REPLACED SRO 955003, -5, -7, -9, -3 7075-T6 ANGLES AND DOUBLERS PER SRM 55-02 FIG 26 PAGE 99-101. (M)Oct 23, 1997 · N803US · Doug DC981 · Vertical StabilizerSDR USAAD97090Gen Control · failedFLT 417 - FLL-PIT - CLIMBING THROUGH FL270, THE NR 2 GENERATOR WENT OFF LINE. TRIED TO BRING APU ONLINE, BUT FAILED DUE TO TWO OVERSPEEDS. DIVERTED TO CLT. REPLACED THE RIGHT GCU, AND RESET CROSSTIE LOCKOUT. (M)May 19, 1997 · N803US · Doug DC981 · AC RegulatorSDR USAAD97075Controller · failedCLT/PHL - FLT 2127 - AFTER TAKEOFF, AIRCRAFT WOULD NOT MAINTAIN PRESSURIZATION. RETURNED TO FIELD. REPLACED NR 2 PRESSURIZATION CONTROLLER. (X)Apr 27, 1997 · N803US · Doug DC981 · Cabin Pressure ControllerSDR USAAD96181Latch · looseFLT 1090 - BOS-CLT - AFTER TAKEOFF, ACCESS DOOR LIGHT CAME ON. RETURNED TO FIELD. RESECURED LOOSE LATCH. CHECKS GOOD. (M)Dec 15, 1996 · N803US · Doug DC981 · Accessory Compartment DoorsSDR USAAD96047Manifold · crackedFLT 842 - LAX-PIT - AFTER TAKEOFF, LEVEL AT 5000 FEET, LEFT FIRE WARNING AND BELL CAME ON. AS SOON AS CREW TURNED BELL OFF, THE LIGHT WENT OFF. RETURNED TO LEX. REPLACED LEFT ENGINE 13TH STAGE MANIFOLD AND SENSE LINE. (M)May 1, 1996 · N803US · Doug DC981 · Pneumatic Distribution SystemSDR USAAD96045Tube Assy · leakingFLT 254 - PBI-BWI - AT FL 330, MASTER CAUTION LIGHT CAME ON, LOW OIL PRESSURE LIGHT CAME ON, NOTICED LOSS OF ALL OIL QUANTITY, LOW OIL PRESSURE, AND RISING OIL TEMPERATURE. SHUT DOWN NR 1 ENGINE, DIVERTED TO SAV. REMOVED AND REPLACED NR 1 ENGINE OIL PRESSURE Apr 30, 1996 · N803US · Doug DC981 · Engine Oil PressureSDR USAA950783Air Distr · odorCLT - FLT NR 0207 - THE FLIGHT ATTENDANT REPORTED SMELLING SMOKE AND FUMES IN THE CABIN. THE CREW ELECTED TO DIVERT TO CLT. MAINTENANCE CHECKED ALL OVERHEAD PANEL LIGHTS, BALLASTS AND OXYGEN. RAN ENGINE AND APU AT POWER. MX CHECKED THE ACM OILS, TAIL COMPAAug 2, 1995 · N803US · Doug DC981 · Air Distribution SystemSDR USAA950648Brake Assy · faultyMCO - FLT NR 1136 - UPON TAXIING FOR DEPARTURE, THE LEFT BRAKE SEIZED. SUBSEQUENTLY, THE NR 1 TIRE WENT FLAT. CAPTAIN DECIDED TO RETURN TO THE GATE. MAINTENANCE REPLACED THE NR 1 BRAKE ASSEMBLY, AND THE NR 1 AND NR 2 MAIN WHEEL ASSEMBLIES P/N 32935. OPERATJun 29, 1995 · N803US · Doug DC981 · Landing Gear Brake SystemSDR 95ZZZM232Tire · blownMCO - FLT NR 1136 - UPON TAXIING FOR DEPARTURE, THE LEFT BRAKE SEIZED. SUBSEQUENTLY, THE NR 1 TIRE WENT FLAT. CAPTAIN DECIDED TO RETURN TO THE GATE. MAINTENANCE REPLACED THE NR 1 BRAKE ASSEMBLY, AND THE NR 1 AND NR 2 MAIN WHEEL ASSEMBLIES P/N 32935. OPERATJun 29, 1995 · N803US · Doug DC981 · Tire
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