N573US, cancelled Dec 13, 2006
Service difficulty reports · 94
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 = 'N573US' AND deregistration_id = 'N573US-2006-12-13' 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 = 'N573US' AND deregistration_id = 'N573US-2006-12-13' 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 PIDR2006041Frame · crackedFORWARD FRAME OF THE FORWARD CARGO DOOR CUTOUT (BS 440 FRAME) CRACKED AT LOWER FORWARD STOP FITTING. REPAIRED CRACK PER INSTRUCTIONS FROM MFG WITH FAA APPROVED 8100-9 DATED NOV.6, 2006.SDR PIDR2006039Skin · delaminatedDELAMINATION AT THE IB END OF THE LT OB FORE FLAP. REPAIRED DAMAGED AREA IAW SRM 51-70-10.SDR PIDR2006042Bear Strap · crackedCRACK INDICATION IN FASTENER HOLE JUST FORWARD AND BELOW THE L1 DOOR UPPER HINGE CUTOUT IN THE BEAR STRAP (SECOND LAYER) CONFIRMED BY HFEC. REPAIRED IAW MFG INSTRUCTIONS WITH FAA APPROVED 8100-9 DATED NOV 3, 2006.SDR PIDR2006038Fitting · crackedLT MLG FITTINGS CRACKED AT THE NR 2 HOLE. REPLACED FITTING IAW SB 737-57-1216.SDR PIDR2006035Beam · crackedLOWER LT AND RT INTERNAL BEAMS CRACKED. REPAIRED BEAMS SB 737-52A1079.SDR PIDR2006033Frame · crackedCRACK IN BS 616 FRAME RT SIDE BELOW FLOOR. REPAIRED DAMAGED AREA IAW SB 737-53-1182.SDR PIDR2006034Stringer · corrodedSTRINGER 28RT CORRODED BETWEEN BS 312 AND BS 328. REPLACED STRINGER SECTION IAW SRM 51-40-02.SDR SB05013Wire · openBWI - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT 4ABC INOPERATIVE. MAINTENANCE REPAIRED AN OPEN IN WIRING AT SEAT ROW 4ABC. OPERATIONAL CHECK GOOD.SDR USAA040339Skin · crackedCLT - FOUND SKIN CRACKED 1.5 INCHES LONG, STATION 727D PLUS 3 AT STRINGER 23 LEFT. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M)SDR USAASB04028Wire · inoperativeCLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT ON BULLNOSE AT SEAT ROW 6, RIGHT SIDE INOPERATIVE. MAINTENANCE REPAIRED WIRING AT D2912 AND REPLACED BLOWN FUSE, P/N 21031-0005, IN POWER SUPPLY M1135. OPERATIONAL CHECK GOOD. (M)SDR USAA040009Stringer · corrodedPIT - FOUND STRINGER WITH 5 INCH CORROSION, S25L AT STATION 356 VERTICLE LEG OF STRINGER. CORROSION LEVEL 2, TASK NR C53-201-01. REMOVED STRINGER DAMAGE, INSTALLED SPLICE SECTION PER EA 77521. (M)SDR USAA040100Skin · damagedPIT - FOUND SKIN WITH SCRIBE MARKS 260 INCHES IN LENGTH, STRINGER 10 LEFT BS 360-540. ACCOMPLISHED CUT-OUT AND INSTALLATION OF REPAIR DOUBLER PER EA 77471. (M)SDR USAASB03070Outflow Valve · leakingEN ROUTE FROM MCI TO CLT, AT FL290, THE CABIN BEGAN CLIMBING AT OVER 1,000 FEET PER MINUTE. BLEED PRESSURE WAS NORMAL AND THE OUTFLOW VALVE WAS CLOSED. CABIN STABILIZED ONCE AIRCRAFT DESCENDED TO FL240. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT ASDR USAA030020Skin · crackedCLT - FOND SKIN CRACKED 2 INCHES, 2.5 INCHES AFT OF 727D 23R. INSTALLED DOUBLER PER TR 53-60-03. (M)SDR USAASB02237Seal · failedTYS - FLT 1724 - EN ROUTE FROM ATL-PIT, WHILE CLIMBING TO FL250, THE AIRCRAFT LOST PRESSURIZATION. THE AIRCRAFT DESCENDED AND THE OXYGEN MASKS DEPLOYED. ALONG WITH THE PRESSURIZATION LOSS, THE PASSENGERS AND THE FIRST OFFICER NOTICED AN ODOR NOT PREVIOUSLY OSDR USAA020384Skin · crackedPIT - FOUND SKIN WITH THREE CRACKS, ONE AT .075 INCH, TWO AT .250 INCH, STATION 380 BL 0. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-30-07. (M)SDR USAASB02068Charger · failedPHL - DURING WEEKLY CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHT BATTERIES LOW. MAINTENANCE FOUND THE AFT RIGHT BATTERY CHARGER INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER ALONG WITH SEVEN BATTERY PACKS THAT WERE LOW. OPERATIONAL CHECK GOOD. (M)SDR USAA011183Mount · scoredPIT - FOUND MOUNT BEARING BORE SCORED, FORWARD ENGINE MOUNT. MACHINED BORE PER TYPICAL REPAIR 54-50-08 REV A. (M)SDR USAA010963Skin · crackedCLT - FOUND STAB LOWER SKIN CRACKED 1.5 INCH, RIGHT STAB, STAB STATION 66.5 TO 110. DAMAGE REMOVED, FILLER AND DOUBLER INSTALLED PER TYPICAL REPAIR 55-10-07 REV A. (M)SDR USAA001675Floorbeam · corrodedCLT - C-6, FLOORBEAM CORRODED, 34 INCHES, CORROSION LEVEL 1 C53-107-02, STA 344 BETWEEN STR 17L AND STR 17R. INSTALLED T-CAP AND SPLICE ANGLE PER SRM 53-10-51. (X)SDR USAA001593Frame · crackedCLT - Q-6, FRAME HAD .25 INCH CRACK AT STA 827, STR 9L. INSTALLED DOUBLER PER TR 53-10-14, EA 68097. (X)SDR USAA001592Intercostal · crackedCLT - Q-6, INTERCOSTAL HAD 1 INCH CRACK AT BS 179 WL 207 RBL 28. FABRICATED NEW INTERCOSTAL AND ANGLE PER SRM 51-10-02, SRM 51-10-08. (X)SDR USAA001591Angle · crackedCLT - DURING Q-5 INSPECTION, FOUND CRACKED INNER CHORD ANGLE .75 INCH AT BS 616 AND STR 16. (X)SDR USAASB00273Light · inoperativeORD - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE FORWARD ENTRY DOOR EXTERIOR EMERGENCY LIGHT, LEFT SIDE INOPERATIVE. MAINTENANCE CLEANED THE LIGHT SOCKET AND RELAMPED THE LIGHT (P/N 1619). OPS CHECK NORMAL. (M)SDR USAA001516Door Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, FORWARD SERVICE DOOR FORWARD FRAME AT OUTBOARD LOWER CORNER. REPLACED FRAME PER SRM 51-40-00 AND 51-10-2. (M)SDR USAA001515Web · crackedCLT - FOUND PRESSURE WEB CRACKED 1 INCH, PRESSURE FLOOR STATION 663, LBBL 24 PLUS 6. INSTALLED FILLER AND DOUBLER PER TR 53-60-04. (M)SDR USAA001514Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 294, 17L TO 17R. FABRICATED REPAIR PARTS PER SRM 53-10-51. (M)SDR USAA001502Beam · crackedCLT - FOUND VERTICAL BEAM CRACKED .250 INCH, BL 178, LBL 5.7, WL 184. INSTALLED REPAIR ANGLES, STRAPS AND FILLERS PER SRM 53-10-08 FIG 205. (M)SDR USAA001501Angle · crackedCLT - FOUND ANGLE CRACKED 2 INCHES, BOTTOM FORWARD CORNER SERVICE DOOR CUTOUT FRAME. REPLACED ANGLE PER 51-10-02 AND 51-40-00. (M)SDR USAA001500Frame · crackedCLT - FOUND FRAME CRACKED .75 INCH, FRAME 907 BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA001499Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED .5 INCH, BS 179, WL 207, LBL 28. REPLACED FABRICATED INTERCOSTAL PER SRM 51-10-02. (M)SDR USAA001484Bulkhead · crackedCLT - FOUND BULKHEAD SKIN CRACKED 1 INCH, STATION 178 PRESS BULKHEAD AFT SIDE WL 190, BL 0. INSTALLED EXT DOUBLER PER SRM 53-10-08 AND EA 67899. (M)SDR USAA001483Bulkhead · crackedCLT - FOUND BULKHEAD SKIN CRACKED .5 INCH IN TWO PLACES, AFT SIDE 178 PRESSURE BULKHEAD RBL 5.5, WL 201 AND 198. INSTALLED EXT DOUBLER PER SRM 53-10-08 AND EA 67899. (M)SDR USAA001482Bulkhead · crackedCLT - FOUND BULKHEAD SKIN CRACKED .5 INCH IN TWO PLACES, AFT SIDE STATION 178 BULKHEAD, RBL 1 AND LBL 1, WL 208. INSTALLED EXT DOUBLER PER SRM 53-10-08 AND EA 67899. (M)SDR USAA001481Bulkhead · crackedCLT - FOUND BULKHEAD SKIN CRACKED .25 INCH, AFT SIDE STATION 178 PRESS BULKHEAD, WL 201, RBL 7.5. INSTALLED EXT DOUBLER PER SRM 53-10-08 AND EA 67899. (M)SDR USAA001480Bulkhead · crackedCLT - FOUND BULKHEAD SKIN CRACKED .500 INCH, BULKHEAD 178, WL 213. INSTALLED EXT DOUBLER PER SRM 53-10-08 AND EA 67899. (M)SDR USAA001479Bulkhead · crackedCLT - FOUND BULKHEAD SKIN CRACKED .500 INCH IN TWO PLACES, AFT SIDE STATION 178 PRESS BULKHEAD LBL 5.5 WL 201 AND 198. INSTALLED EXT DOUBLER PER SRM 53-10-08 AND EA 67899. (M)SDR USAA001478Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .5 INCH BY 1 INCH, STATION 312, LBL 12. INSTALLED REPAIR PE SRM 53-10-51. (M)SDR USAA001477Floorbeam · corrodedCLT - FOUND T-CAP CORRODED 15 INCHES, STATION 270 AT BL 0. CORROSION LEVEL 1. REMOVED DAMAGE AND SPLICED IN REPAIR PART PER TR 53-20-08. (M)SDR USAA001476Support Bracket · corrodedCLT - FOUND ANT SUPPORT BRACKET 1 INCH BY 5 INCHES, BL 0 BETWEEN BS 500 AND 500A. CORROSION LEVEL 1 C53-208-01. REPAIRED PER SRM 51-10-02. (M)SDR USAA001417Stringer · crackedCLT - FOUND STRINGER 18A SHEAR BEAM CRACKED .5 INCH, STRINGER 18A SHEARBEAM WEB 1 INCH FORWARD STATION 727 LT SIDE. INSTALLED NEW SHELF PER SRM 51-10-2. (M)SDR USAA001416Stringer · crackedCLT - FOUND STRINGER CRACKED 1 INCH, BS 727 SHELF 18A RIGHT. REPAIRED PER SRM 51-10-02 AND 51-40-03. (M)SDR USAA001415Frame · crackedCLT - FOUND FRAME CRACKED 1 INCH, BS 616 BELOW STRINGER 17. INSTALLED DOUBLER PER TR 53-62-01. (M)SDR USAA001414Angle · crackedCLT - FOUND ANGLE CRACKED 1 INCH, FRAME TO INTERCOSTAL ATTACH ANGLES STATION 360 STRINGER 4L. INSTALLED FABRICATED ANGLE PER BOEING 65 58280. (M)SDR USAA001408Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .375 INCH, BS 328, RBL 24.50 TO SERVICE DOOR. INSTALLED ANGLES PER SRM 53-00-51. (M)SDR USAA001407Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 5 INCHES BY .25 INCH, BS 328M 11.5 INCHES IN FROM FORWARD SERVICE DOOR. INSTALLED REPAIR ANGLES, T-CAP PER SRM 53-00-51 FOG 201. (M)SDR USAA001411Stiffener · corrodedCLT - FOUND STIFFENER CORRODED 3 INCHES BY 1 INCH, AFT BULKHEAD STIFFENER STATION 1016 BETWEEN STRINGER 27L AND 27R. INSTALLED SECTION CHANNEL REPAIR PER RM 53-80-08 AND 51-70-11. CORROSION LEVEL 1. (M)SDR USAA001410Web · corrodedCLT - FOUND WEB CORRODED 1 INCH IN 18 AREAS, BS 440 TO BS 480 PLUS 12 BETWEEN STRINGER 25R AND 26R. REPLACED WEB PER SRM 51-10-02 FIG 201. (M)SDR USAA001409Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 3 INCHES, STATION 344, 14 INCHES LBL. CORROSION LEVEL 1 C53-107-01. INSTALLED T-CAP FLOORBEAM REPAIR PER SRM 53-10-51. (M)SDR USAA001406Frame · crackedCLT - FOUND FRAME CRACKED, FS 887 BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53-10-14. (M)
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