N273AU, cancelled Dec 4, 2003
Service difficulty reports · 133
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 = 'N273AU' AND deregistration_id = 'N273AU-2003-12-04' 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 = 'N273AU' AND deregistration_id = 'N273AU-2003-12-04' 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 USAA011166Frame · crackedCLT - FOUND CHORD CRACKED .5 INCH, IN RADIUS OF LEFT SIDE CHORD BS 178 AT WL 196 AND WL 207. SPLICED IN ANGLE AND DOUBLER STRAP PER EO 5300V157. (M)SDR USAA011165Web · crackedCLT - FOUND WEB CRACKED 1 INCH, BS 179, WL 207, RBL 24. REMOVED AND REPLACED PART WITH NR 65-45833U40. (M)SDR USAA011164Web · crackedCLT - FOUND WEB CRACKED FIVE PLACES .25 INCH EACH, BS 178, WL 234, LBL 10. INSTALLED DOUBLER ON WEB, CRACK CUT OUT OF WEB PER EO 5300V153 AND SRM 53-10-08 FIG 209. (M)SDR USAA011163Frame · crackedCLT - FOUND SIDE CHORD CRACKED .5 INCH, BS 178 BULKHEAD, WL 207 AND WL 196, LEFT SIDE CHORD. INSTALLED NEW CHORD SECTION AND SPLICE PARTS. (M)SDR USAA011162Stiffener · crackedCLT - FOUND VERTICAL CHORD CRACKED .5 INCH AND .9 INCH, BS 178 BULKHEAD LBL 5-7 VERTICAL CHORD, WL 184. INSTALLED REPAIR DOUBLER PER EO NR 5300V155. (M)SDR USAA011161Web · crackedCLT - FOUND WEB CRACKED .5 INCH, BS 178 BULKHEAD WL 2.8, LBL 11.7. CUT OUT DAMAGE FABRICATED FILLER AND DOUBLER PER EA 85310 AND SRM 53-10-08 FIG 211. (M)SDR USAA011160Bulkhead · crackedCLT - FOUND WEB PRESSURE CRACKED .06 AND .08 INCH, BS 178 BULKHEAD WEB, LBL .5 AND RBL .5, WL 188. CUT OUT CRACKS AND INSTALLED DOUBLER PER EA 85310. (M)SDR USAA011159Web · crackedCLT - FOUND WEB CRACKED .6 INCHES, BS 178, WL 188 AT RBL .5 AND LBL .5 INCH. INSTALLED WEB REPAIR PER EA 85310, EO 5300V152. (M)SDR USAASB01176Battery Pack · dischargedBWI - THE LEFT OVERWING AN LEFT LOWER FUSELAGE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. (M)SDR USAASB01155Charger · failedLGA - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE OVERWING EMERGENCY EXIT LOCATOR LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY PACK M1052 (P/N 9008-3-5A). OPS CHECK GOOD. (M)SDR USAASB01110Power Supply · failedBWI - THE EXIT ROW OVERHEAD EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M)SDR USAASB01123Battery Pack · dischargedCLE - THE AISLE OVERWING EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. (M)SDR USAASB01122Battery Pack · dischargedIAD - THE CEILING EMERGENCY EXIT LIGHT AT SEAT ROW 10 WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. (M)SDR USAA200101172Compass · malfunctionedAFTER TAKEOFF, HDNG SYTM ON BOTH COMPASS SYTM BECAME UNRELIABLE. SYTM WAS APRX 30 TO 35 DEGREES OFF. CREW TRIED TO FLY DIRECT TO A VOR, COULD NOT NAVIGATE PROPERLY,SELECTED BOTH COMPASSES MULTIPLE TIMES, NO HELP. DID NOT SELECT DC IN ATTEMPT TO FIX HEADING. SDR USAASB00360Wire · chafedBWI - FLT 2706 - DESCENDING THROUGH 10,000 FEET, ON APPROACH TO BWI, THE WHEEL WELL FIRE WARNING LIGHT ILLUMINATED AND BEGAN FLICKERING. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND THE LIGHT EXTINGUISHED AND REMAINED EXTINGUISHED. FLIGHT LANDED WITSDR USAASB00193Hose · leakingFLL - FLT 2724 - AFTER TAKEOFF FROM FLL AND GEAR RETRACTION, CREW RECEIVED AND RED AND GREEN INDICATION FROM THE NOSE GEAR. THE MAINS INDICATED GREEN. CREW SELECTED GEAR DOWN AND RECEIVED THREE GREENS. FLIGHT RETURNED TO FLL AND LANDED WITHOUT FURTHER INCIDSDR USAASB00105Power Supply · failedMCO - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHT FAILED TO TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (PN 61-0478-9) AND POWER SUPPLY. OPERATIONAL CHECK GOOD. (X)SDR USAASB00102Battery Pack · dischargedSYR - MAINTENANCE FOUND THE EXTERIOR OVERWING EMERGENCY LIGHT, RIGHT SIDE, INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (X)SDR USAA991446Beam · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND NUTPLATE HOLES 12 EACH 1 INCH BY 1 INCH STATION 312 TO 328, RBL 11 T-SUPPORT BEAM. CORROSION LEVEL 2. REPAIRED T-CAP PER SRM 51-10-01. (M)SDR USAA991445Angle · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 5 INCH CRACK AT BS 294.5, STRINGER 17R SUPPORT ANGLE. REPLACED PART PER SRM 51-40-01. (M)SDR USAA991444Skin · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK LOWER AFT CORNER OF FORWARD ENTRY DOOR CUTOUT SKIN. INSTALLED DOUBLER AND TRIPLER PER EO 65C27257. (M)SDR USAA991429Fitting · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK BS 695 STRINGER 18A OUTBOARD VERTICAL FLANGE FORWARD FITTING. REPLACED FITTINGS PER EO NR 5391G625. (M)SDR USAA991428Skin · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK FORWARD CARGO DOOR ASSIST CABLE CUTOUT INTERIOR SKIN. RESKINNED DOOR PER BOEING DWG 65-46921 AND EA 66250. (M)SDR USAA991416Stringer · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 6 INCH BY 2 INCH AREA OF CORROSION STRINGER AFT CARGO STRINGER 27L STATION 941-947, CORROSION LEVEL 2. REMOVED AND REPLACED STRINGER SECTION PER SRM 53-10-3. (M)SDR USAA991415Skin · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND STRINGER REPAIR SKIN CUTOUT 18.25 INCH LENGTH BY 3 INCHES WIDE BY 23.75 INCHES IN LENGTH BY 8 INCHES WIDE CENTER LINE OF STRINGER 27L, BS 950 TO BS 991 SKIN. INSTALLED DOUBLER AND TRIPLER PER SRM 53-30-3 FIG 6 ASDR USAA991410Frame · crackedCLT - DURING Q-5 CHECK HFEC INSPECTION, FOUND A CRACK AT BS 727 STRINGER 18A LEFT CHORD. REPAIRED PER EA 66261 AND EO 5394G068. (M)SDR USAA991409Skin · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK LOWER AFT CORNER FORWARD SERVICE DOOR CUTOUT SKIN. INSTALLED TRIPLERS PER SRM 53-30-3 FIG 26. (M)SDR USAA991408Floorbeam · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION STATION 294.5 LBL 13 TO RBL 1 FLOORBEAM. CORROSION LEVEL 2. REPLACED T-CAP PER TR 53-10-04 B. (M)SDR USAA991381Stringer · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 3 INCH AREA OF CORROSION STRINGER 28R, STATION 313 TO 324.. CORROSION LEVEL 2. INSTALLED STRINGER SPLICE REPAIR AND CLIP PER SRM 53-10-3. (M)SDR USAA991380Door Frame · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 2 INCH AREA OF CORROSION ON SURFACE STATION 847, RBL 24, AFT CARGO DOOR CUTOUT AFT FRAME. CORROSION LEVEL 1. REPAIRED PER EA 66271. (M)SDR USAA991378Stiffener · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AFT SIDE 663 BULKHEAD, LBL 7, 16 FT UP FROM KEEL BEAM STIFFENER. REMOVED AND REPLACED STIFFENER PER EA 66242. (M)SDR USAA991377Beam · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK IN RADIUS OF FLOOR SUPPORT ANGLE STA 294.5 RBL 54. REMOVED AND REPLACED ANGLE PER SRM 51-40-1. (X)SDR USAA991376Floorbeam · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 4 INCH CRACK AT BS 663, BL ZERO FLOORBEAM. INSTALLED REPAIR SECTION OF FLOORBEAM PER TR 57-10-04. (X)SDR USAA991374Web · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 4 INCH BY 1 INCH DAMAGED FASTENER HOLE CUTOUT AT BS 294.5, WL 208, RBL 21-RBL 25 WEB. INSTALLED DOUBLER PER SRM 51-40-2. (X)SDR USAA991372Angle · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND NUTPLATE HOLES IN Z-ANGLE, STA 300 TO STA 333, RBL 55 TO RBL 60, WL 208.1 CREASE BEAM INNER CHORD ANGLE. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. INSTALLED NEW Z-ANGLE PER SRM 51-10-1.SDR USAA991371Floorbeam · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND NUTPLATES HOLES IN FLOORBEAM 6 EACH 1 INCH BY 1 INCH STATION 328, BL 0 TO RBL 35. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. REPLACED T-CAP SECTION PER TR 53-10-13. (M)SDR USAA991370Floorbeam · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION .5 INCH BY 5 INCH BY 15 INCHES AT BS 344, WL 208, BL 0 - LBL 15 FLOORBEAM. CORROSION LEVEL 2. CORROSION TASK NR C53-107-01. INSTALLED REPAIR STRAPS PER TR 53-10-13. (M)SDR USAA991369Stringer · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK LEFT STRINGER 18A SHELF, STATION 725 TO 727, 4 INCHES OF SKIN. INSTALLED NEW AFT SHELF SECTION PER SRM 51-10-1 AND 51-30-3. (M)SDR USAA991360Splice · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN STRINGER PRODUCTION SPLICE BS 908 STRINGER 4R. INSTALLED NEW STRINGER SPLICE PER SRM 51-10-01. (M)SDR USAA991359Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 4R STATION 767 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-01. (M)SDR USAA991358Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .0625 INCH CRACK AT STRINGER 2L STATION 727A TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-01. (M)SDR USAA991338Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .1875 INCH CRACK AT STRINGER 4L STATION 907 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-1. (M)SDR USAA991337Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .3125 INCH CRACK AT STRINGER 2L STATION 867 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-1. (M)SDR USAA991336Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STRINGER 5L STATION 847 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-30-2. (M)SDR USAA991335Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 2L STATION 827 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-1. (M)SDR USAA991334Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STRINGER 10L STATION 807 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-1. (M)SDR USAA991333Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 6R STATION 807 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-30-2. (M)SDR USAA991332Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 5R STATION 807 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-1. (M)SDR USAA991331Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 9L STATION 787 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-1. (M)SDR USAA991330Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 6R STATION 767 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-1. (M)
Back to N273AU, cancelled Dec 4, 2003