N811US, cancelled Oct 6, 2005
Service difficulty reports · 48
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 = 'N811US' AND deregistration_id = 'N811US-2005-10-06' 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.
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 = 'N811US' AND deregistration_id = 'N811US-2005-10-06' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR USAAD02016Battery · dischargedPIT - THE DOOR EXIT AND NUMEROUS FLOOR LEVEL EMERGENCY LIGHTS WILL NOT TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)SDR USAAD01184Battery · dischargedPIT - THE FORWARD OVERWING EXIT LIGHTS DID NOT ILLUMINATE WHEN THE AIRCRAFT POWER DROPPED OFF. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY. (M)SDR 2001F00647Battery · dischargedMCO - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS AND THE LEFT FORWARD EXIT IDENTIFIER LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. REF USAAD01176. (M)SDR USAAD01176Battery · dischargedMCO - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS AND THE LEFT FORWARD EXIT IDENTIFIER LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)SDR USAA011128Skin · crackedCLT - FOUND SKIN CRACKED, SKIN ON AFT ENTRANCE DOOR L2 AROUND HOLE OPEN HOOK CUTOUT. INSTALLED DOUBLER PER E NR 72317. (M)SDR USAAD01135Battery · dischargedCLT - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)SDR USAAD01115Battery · dischargedIND - THE LOW LEVEL EMERGENCY LIGHT FAILED TO TEST AT SEAT ROWS 1, 3, 6 AND 19. THE CEILING EMERGENCY LIGHTS AT SEAT ROWS 1 TO 3 AND THE RIGHT AFT EMERGENCY EXIT LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES, (P/N 9721055, AD4002SDR USAAD01090Battery · dischargedTPA - THE FLOOR TRACK EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)SDR USAAD01084Slide · unserviceableMCO - THE AFT SERVICE DOOR EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS LOW. MAINTENANCE REPLACED THE AFT SERVICE DOOR EVACUATION SLIDE. (M)SDR USAAD01086Battery · dischargedBOS - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)SDR USAAD00120Door · openCLT/BNA - FLT 2288 - ON TAKEOFF THERE WAS A VIBRATION FROM THE NOSE GEAR. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR DOORS OPEN. THE DOORS WERE INSPECTED AND CLOSED. (X)SDR USAAD99125Seal · failedMKE-CLT - FLT 751 - AFTER TAKEOFF AND CLIMBING THROUGH 17,000 FT THE AIRCRAFT WOULD NOT PRESSURIZE. THE AIRCRAFT DIVERTED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT AIR CYCLE MACHINE AND PERI-SEALS. (M)SDR USAAD99121Battery · dischargedPIT - THE FORWARD CABIN EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD CABIN EMERGENCY LIGHTS BATTERIES. (M)SDR USAAD99085Diode · failedTHE LOW LEVEL EMERGENCY LIGHTS REMAIN ON WHEN THE AIRCRAFT POWER IS TURNED OFF. MAINTENANCE RPELACED THE DIODE AT TERMINAL STRIP S3-389. (X)SDR USAA990610Beltframe · corrosionPIT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AT STATION 1322 STRINGER 27L TO 27 BELTFRAME. REMOVED AND REPLACED BELTFRAME. (M)SDR USAA990609Web · crackedPIT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK CANTED WEB AT STATION 1463 STRINGER 18R. CUTOUT DAMAGE AND INSTALLED DOUBLER PER TR 53-10-25. (M)SDR USAA990608Fitting · crackedPIT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK LEFT GROUND SPOILER SUPPORT FITTING LEG UPPER END. INSTALLED PART 5936838-505. (M)SDR USAA990607Skin · crackedPIT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .750 INCH CRACK AT FORWARD UPPER CORNER OF MED DOOR JAMB STATION 168 SKIN. REPAIRED PER SRM 53-05, FIG 26 CUT OUT DAMAGED AREA AND INSTALLED FILLER AND DOUBLER. (M)SDR USAAD96161Csd · failedFLT 741 - BWI-CLT - DURING CLIMB, LT CSD LOW OIL PRESSURE LIGHT ILLUMINATED. CAPTAIN BELIEVED CSD DID NOT DISCONNECT. RETURNED TO FIELD. MAINTENANCE FOUND THAT THE CSD FAILED, AND DID IN FACT DISCONNECT. A/C WAS RELEASED PER MEL 24-1A. THE CSD WAS LATER RESDR USAA950249Feeder Cable · chafedPIT - FLT 0992 - ON TAKEOFF, THE RIGHT GENERATOR OFF LIGHT ILLUMINATED FOLLOWED BY AC CROSSTIE LOCKOUT. CREW DECIDED TO RETURN TO PIT. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND STOWED LAV DUMP CABLE CHAFING ON GEN FEEDER CABLE. ACCOMPLISHED REPAIRS SDR USAA950250Csd · leakingPIT - FLT 0239 - AIRCRAFT RETURNED TO PIT DUE TO A GENERATOR PROBLEM. MAINTENANCE REPLACED THE RIGHT ENGINE CSD AND THE RIGHT ENGINE GENERATOR FOR TROUBLESHOOTING. OPERATIONS CHECKED GOOD. (W)SDR USAA950351Skin · dentedPIT - DURING Q-2 INSPECTION, FOUND DENT 1 INCH BY 1.75 INCH BY .75 INCH DEEP BETWEEN STATION 275 AND 294 LONGERON 23L AND 27L IN SKIN AREA. INSTALLED DOUBLER REPAIR PER SRM 53-04 SH 17 FIG 38. (W)SDR USAA950347Floor Beam · corrodedPIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION AT STATION 1322 FLOOR BEAM AFT RT LAV. CUT OUT DAMAGED AREA AND INSTALLED FILLER AND REPAIR ANGLE DOUBLERS PER SRM 53-10-19. (W)SDR USAA950346Splice · corrodedPIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION BETWEEN STATION 1193 AND 1212 LONGERON 29 LEFT. REMOVED AND REPLACED CORRODED SPLICE PER SRM 53-00 FIG 16. (W)SDR USAA950341Belt Frame · corrodedPIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION AT STATION 1309 BETWEEN LONGERON 28L AND 29R ON BELTFRAME 'J'. CLEANED AND TREATED CORRODED AREA AND INSTALLED REPAIR DOUBLER PER SRM 53-03 FIG 7. (W)SDR USAA950339Threshold · corrodedPIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION AFT CARGO DOOR THRESHOLD AT STATION 1155-1220 WEB AND STRAP. REMOVED AND REPLACED WEB AND STRAP PER DACO DWG NR 5936442. (W)SDR USAA950338Web · corrodedPIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION AT STATION 1338 AFT CARGO AREA BETWEEN LONGERONS 28L AND 28R. REMOVED CORROSION, CLEANED AND TREATED. INSTALLED REPAIR DOUBLERS PER SRM 53-03 FIG 3 PER USAIR TYPICAL REPAIR 53-30-10. (W)SDR USAA950337Door Jamb · corrodedPIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION AT FORWARD CARGO DOOR JAMB BETWEEN STATION 370 AND 427. REPLACED PAN AND SPLICED WITH REPAIR DOUBLERS PER SRM 53-05 FIG 44. (W)SDR USAA950336Angle · corrodedPIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION BETWEEN STATION 180 AND 203 FORWARD GALLEY AREA AND SERVICE DOOR THRESHOLD JAMB PAN, CUSP ANGLE LOWER CORNER OF SERVICE DOOR OPENING. (W)SDR USAA950335Membrane · crackedPIT - DURING Q-2 INSPECTION, FOUND A 1.75 INCH CRACK BETWEEN STATION 1287 AND STATION 1309 LEFT SIDE CUSP MEMBRANE. MANUFACTURED NEW SECTION OF CUSP MEMBRANE AND ACCOMPLISHED SPLICE REPAIR PER SRM 53-05 FIG 97. (W)SDR USAA950344Skin · corrodedPIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION AT STATION 807 LONGERON 29 LEFT SKIN. CLEANED AND TREATED CORRODED AREA AND INSTALLED REPAIR DOUBLER PER SRM 53-04 FIG 53. (W)SDR USAA950343Skin · corrodedPIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION SKIN AT STATION 769 LONGERON 28 RT. CLEANED AND TREATED CORRODED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 53. (W)SDR USAA950342Beam · corrodedPIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION AT STATION 1322 BETWEEN AFT GALLEY AND AFT LAV CENTER AISLE. REMOVED CORRODED AREA AND INSTALLED FILLER AND REPAIR ANGLE PER USAIR TYPICAL REPAIR 53-10-19. (W)SDR USAA950349Web · corrodedPIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION STATION 1338 RT SIDE UNDER LAV THRESHOLD FLOOR BEAM AREA. CUT OUT DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 53-05 FIG 72. (W)SDR USAA950345Splice · corrodedPIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION BETWEEN STATION 1193-1212 LONGERON 28L. REMOVED REPLACED SPLICE PER SRM 53-02 FIG 16. (W)SDR USAA950333Skin · gougedPIT - DURING Q-2 INSPECTION, FOUND GOUGE RT VERTICAL STAB SKIN PANEL. BURNISHED GOUGES AREA AND INSTALLED INTERNAL DOUBLER PER USAIR EA 29729 AND SRM 55-01 FIG 2 SHEET 2. (W)SDR USAA950329Longeron · crackedPIT - DURING Q-2 INSPECTION, FOUND .3125 INCH CRACK STATION 160 LONGERON 2 LEFT. CUT OUT DAMAGE SECTION OF LONGERON AND SPLICED IN NEW SECTION PER SRM 53-02 FIG 2. (W)SDR USAA950328Longeron · crackedPIT - DURING Q-2 INSPECTION, FOUND .25 INCH CRACK STATION 160 LONGERON 3 LEFT. CUT OUT DAMAGED SECTION OF LONGERON AND SPLICED IN NEW SECTION PER SRM 53-02 FIG 2. (W)SDR USAA950348Fitting · corrodedPIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION AT STATION 1338 RT SIDE UPPER TO LOWER FRAME ATTACH LONGERON 18R CUSP. REMOVED CORROSION, TREATED AND REPLACED FITTING PER DACO PRINT REF NR 5913700. (W)SDR USAA950340Skin · corrodedPIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION ON FUSELAGE LOWER SKIN BETWEEN 1155 AND 1174. CUT OUT DAMAGED SKIN AND INSTALLED REPAIR WITH EXTERNAL DOUBLER PER SRM 53-04 FIG 12B AND USAIR EA NR 29833. (W)SDR USAA950350Intercostal · corrodedPIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION REF C58-53301 AT STATION 1344 AFT LEFT GALLEY ATTACHMENT AT FLOOR BEAM 1338 TO AFT PRESSURE BULKHEAD AT FLOOR LEVEL. MANUFACTURED INTERCOSTAL AND REPLACED PER SRM 53-14. (W)SDR USAA950334Longeron · crackedPIT - DURING Q-2 INSPECTION, FOUND .25 INCH CRACK AT STATION 256 LONGERON 17 LEFT. CUT OUT DAMAGED SECTION AND SPLICED IN NEW SECTION OF LONGERON PER USAIR TYPICAL REPAIR 53-10-17. (W)SDR USAA950331Skin · dentPIT - DURING Q-2 INSPECTION, FOUND A 1 INCH BY 100 INCH DEEP DENT AT STATION 408 LONGERON 17 LEFT. INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIG 38 VIEW G. (W)SDR USAA950330Membrane · gougePIT - DURING Q-2 INSPECTION, FOUND GOUGE JUST AFT OF SERVICE DOOR CUSP MEMBRANE STATION 200 LONG 18R. CUT OUT CUSP MEMBRANE SECTION AND INSTALLED REPAIR SECTION PER SRM 53-05 FIG 9. (W)SDR USAA950327Longeron · crackedPIT - DURING Q-2 INSPECTION, FOUND .1250 INCH CRACK STATION 160 LONGERON 4 LEFT. CUT OUT DAMAGED SECTION AND ACCOMPLISHED SPLICE REPAIR PER SRM 53-02 FIG 02. (W)SDR USAA950332Skin · crackedPIT - DURING Q2 INSPECTION, FOUND CRACK .5 INCH LONG STATION 160 FORWARD AIR STAIR CUT OUT UPPER FWD CORNER SKIN. CUT OUT DAMAGED AREA AND INSTALLED FILLER AND EXTERNAL DOUBLER PER SRM 53-05 FIG 57A VIEW G. (W)SDR USAA950326Skin · crackedPIT - DURING Q-2 INSPECTION, FOUND .1250 INCH CRACK AT STATION 1437 LONGERON 3L IN SKIN. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER AND FILLER PER SRM 53-04 FIG 38 FIG 38 VIEW L. (W)SDR USAA950325Frame · crackedPIT - DURING Q-2 INSPECTION, FOUND CRACK .75 INCH LONG AT STATION 1463 CANTED FRAME WEB. CUT OUT DAMAGED SECTION OF WEB AND MANUFACTURED NEW WEB PER USAIR EA 27544. (W)
Back to N811US, cancelled Oct 6, 2005