N247US, cancelled Apr 25, 2006
Service difficulty reports · 86
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 = 'N247US' AND deregistration_id = 'N247US-2006-04-25' 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 = 'N247US' AND deregistration_id = 'N247US-2006-04-25' 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 USAA010573Keel · corrodedCLT - FOUND KEEL CHORD OUTBOARD FLANGE WITH 3 INCH AREA OF CORROSION, BS 727A, RBL 7, BELLY AREA. REMOVED DAMAGE, INSTALLED SPLICE REPAIR PER TR 53-10-24, EA 69672, SRM 51-20-1 FIG 10, 53-10-6 FIG 3. (M)SDR USAA010556Shear Tie · corrodedCLT - FOUND FRAME SHEAR TIE CORRODED 5 INCHES BY 1 INCH, BS 986 STRINGER 24R/25R. FABRICATED AND REPLACED SHEAR TIE PER BAC DRAWING 65-46564, SRM 51-10-0 AND 51-30-0. (M)SDR USAA010557Web · crackedCLT - FOUND WEB CRACKED 1 INCH, BS 712, LBL 24. INSTALLED REPAIR DOUBLER, REPLACEMENT WEB AND 4 VERTICAL STIFFENERS PER EA 69504. (M)SDR USAA010558Floorbeam · crackedCLT - FOUND FLOORBEAM T-CAP CRACKED, BS 520, RBL 25, WL 208. INSTALLED DOUBLER AND PIVOT LINK ASSY PER SB 737-53-1120 AND EA 69537. (M)SDR USAA010559Frame · crackedCLT - FOUND CHORD CRACKED 1 INCH, BS 663, LBL 24, WL 203. INSTALLED REPAIR CHORD PER EA 69538 AND SB 737-53-1184. (M)SDR USAA010560Web · crackedCLT - FOUND PRESSURE BULKHEAD WEB WITH CRACKS .125 INCH TO 1 INCH, BS 178, LBL 12 TO RBL 17, WL 188 TO WL 214. DAMAGED REMOVED, INSTALLED REPAIR DOUBLER PER EO 5300V153 AND EA 69493. (M)SDR USAA010561Frame · crackedCLT - FOUND VERTICAL CHORD CRACKED 1.3 INCHES, BS 178, LBL 6, WL 198. INSTALLED REPAIR KIT PER EO 5300V155. (M)SDR USAA010562Attach Fitting · corrodedCLT - FOUND FUSELAGE ATTACH LUGS CORRODED 3 SQUARE INCHES, VERT FIN, AFT OUTBOARD LEFT AND AFT OUTBOARD RIGHT ATTACH POINTS. CORROSION REMOVED AND LUGS REWORKED PER EA 69591 AND EO 5593G087. (M)SDR USAA010563Beam · crackedCLT - FOUND BEAM CRACKED 3 INCHES, BS 663, BL 0. INSTALLED REPAIR ANGLES PER EA 69611. (M)SDR USAA010564Skin · crackedCLT - FOUND SKIN CRACKED .25 INCH, BS 345, AFT LOWER CORNER OF AIRSTAIR CUTOUT. REMOVED AND REPLACED REPAIR TRIPLER PER EA 69582. (M)SDR USAA010565Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED .25 INCH AFT ENTRY DOOR, UPPER HINGE CUTOUT. INSTALLED DOUBLER PER SRM 543-30-3, FIG 21A. (M)SDR USAA010566Skin · corrodedCLT - FOUND FUSELAGE SKIN CORRODED, BS 468, BL 0. REMOVED DAMAGE, INSTALLED REPAIR DOUBLER PER SRM 51-20-4 AND 53-30-3. (M)SDR USAA010552Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 639, STRINGER 17R. INSTALLED REPAIR DOUBLER PER SRM 51-40-2, FIG 1. (M)SDR USAA010553Frame · crackedCLT - FOUND FRAME CRACKED .375 INCH, LATERALLY THROUGH EDGE OF FRAME BS 440, LBL 21. INSTALLED FORMED FRAME REPAIR DOUBLER PER SRM 51-40-3, FIG 1. (M)SDR USAA010555Doubler · crackedCLT - FOUND DOUBLER CRACKED 2 INCHES, BS 676, BETWEEN LBL 24 AND RBL 24, WL 206. INSTALLED RE-INFORCEMENT CHANNELS PER EO 5791G632. (M)SDR USAA010525Skin · crackedCLT - FOUND FUSELAGE SKIN WITH TWO CRACKS 1 INCH EACH, BS 727 PLUS 1 INCH AT STRINGER 17R AND BS 727A PLUS 6 INCHES AT STRINGER 19R. INSTALLED REPAIR DOUBLER. (M)SDR USAA010524Frame · crackedCLT - FOUND FRAME CRACKED 1.125 INCH, BS 277, STRINGER 16L. REMOVED DAMAGE, INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-40-2, FIG 1. (M)SDR USAA010523Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 480 STRINGER 21L. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 51-40-3, FIG 1. (M)SDR USAA010522Angle · crackedCLT - FOUND SUPPORT ANGLE CRACKED 1.5 INCH, BS 727, LBL 27, WHEEL WELL COMPRESSION CHORD. INSTALLED REPAIR STRAPS AND DOUBLER ANGLE PER BOEING DRAWING NR 691A0068 AND EA 69571. (M)SDR USAA010521Stringer · crackedCLT - FOUND STRINGER CRACKED .070 INCH, BS 380, STRINGER 2L. REMOVED DAMAGE SECTION, SPLICED IN NEW STRINGER SECTION PER SRM 53-10-3. (M)SDR USAA010518Web · crackedCLT - FOUND FLOOR STRUCTURE WEB CRACKED 1 INCH, BS 178, WL 207 AT LBL 24. REMOVED AND REPLACED WEB PER EO 5300V157. (M)SDR USAA010520Pressure Panel · damagedCLT - FOUND UNBEADED PRESSURE WEB APPROX 3 SQUARE FEET, BS 666 WL 55. REINFORCING ANGLES INSTALLED PER SB 737-57-1234 AND EA 69561. (M)SDR USAA010519Frame · crackedCLT - FOUND SIDE CHORD CRACKED .25 INCH, BS 178, WL 195 LEFT SIDE CHORD. DAMAGE REMOVED, SPLICED IN NEW CHORD SECTION PER EO 5300V157. (M)SDR USAA010497Skin · corrodedCLT - FOUND FUSELAGE SKIN CORRODED 2 INCH BY 3 INCH AREA, BS 468 BL 0. DAMAGED AREA CUTOUT, REPAIR DOUBLER INSTALLED PER SRM 53-30-3. (M)SDR USAA010496Stringer · corrodedCLT - FOUND STRINGER CORRODED 1 INCH BY 10 INCH AREA, BS 1006 TO 1016, S24R. REMOVED DAMAGE, FABRICATED NEW SECTION AND INSTALLED PER SRM 53-10-2. (M)SDR USAA010493Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORRODED .125 INCH, BS 967, RBL 42. DAMAGE REMOVED, SPLICED IN T-CAP REPLACEMENT PER SRM 53-10-9. (M)SDR USAA010491Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORRODED APPROX 13 SQUARE INCHES, BS 986.5, LBL 45 TO RBL 45. REMOVED AND REPLACED T-CAP PER TYPICAL REPAIR 53-60-01 REV ''A''. (M)SDR USAA010475Angle · corrodedCLT - FOUND AFT SERVICE DOOR Z-ANGLE CORRODED 40 INCHES BY .5 INCH, BS 947 TO 987, LBL 50. REMOVED AND REPLACED Z-ANGLE PER SRM 51-10-01. (M)SDR USAA010474Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORRODED 1 INCH BY .5 INCH AREA, BS 312, BL 0. DAMAGE REMOVED, SPLICED IN REPAIR ANGLES AND T-CAP SECTION PER TYPICAL REPAIR 53-10-13. (M)SDR USAA010473Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 3 INCHES, BS 1006, LBL 10. DAMAGE REMOVED, INSTALLED FILLER AND REPAIR ANGLES PER SRM 53-10-9 FIG 2. (M)SDR USAA010503Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 597, STRINGER 4R. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)SDR USAA010502Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 597, S5R. INSTALLED NEW TIE CLIP PER SRM 51-30-2. (M)SDR USAA010501Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, BS 344 S11R. FABRICATED AND INSTALLED NEW TIE CLIP PER BOEING DRAWING NR 69-38939 AND SRM 51-30-2. (M)SDR USAA010500Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, BS 706, S11R. FABRICATED NEW CLIP AND INSTALLED PER BLUEPRINT NR 69-45156 AND SRM 51-30-2. (M)SDR USAA010499Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 663, S10R. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M)SDR USAA010498Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED 1 INCH, BS 178, WL 234, RBL 11. INSTALLED DOUBLER AND FILLER PER SRM 53-10-11 FIG 1. (M)SDR USAA010495Hinge Fitting · crackedCLT - FOUND HINGE CASTING CRACKED .5 INCH, RT AILERON, NR 2 HINGE SUPPORT CASTING, LOWER OUTBOARD PANEL. REMOVED AND REPLACED CASTING PER BOEING DRAWING NR 65-63445-1. (M)SDR USAA010494Angle · crackedCLT - FOUND VERTICAL TIE ANGLE CRACKED .75 INCH AND 1 INCH, BS 360, BETWEEN S14L AND S15L. REMOVED DAMAGED ANGLE, FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-10-01, 51-40-3 AND 53-10-2. (M)SDR USAA010492Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, BS 360, S4L. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM 51-30-2. (M)SDR USAA010490Stringer · crackedCLT - FOUND STRINGER CRACKED 1 INCH, BS 787, S16R. INSTALLED STRINGER SPLICE REPAIR PER SRM 53-30-3, 53-10-2. (M)SDR USAA010489Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED 1 INCH, BS 178, WL 195, RBL 24. REMOVED AND REPLACED INTERCOSTAL PER EO 5300V155. (M)SDR USAA010488Stringer · crackedCLT - FOUND STRINGER CRACKED .5 INCH, BS 360, S15L. REMOVED AND REPLACED STRINGER SECTION PER RM 51-10-1. (M)SDR USAA010487Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED 1.7 INCH, RIGHT AFT GALLEY SERVICE DOOR CUTOUT, FORWARD LOW CORNER. DAMAGE CUTOUT, INSTALLED FILLER AND REPAIR DOUBLER, TEXAS PATCH, PER SRM 53-30-3 FIG 24. (M)SDR USAA010486Stringer · crackedCLT - FOUND STRINGER CRACKED .5 INCH, BS 358, S7L. FABRICATED WEB CLIP, REPLACED STRINGER AND TIE CLIP PER SRM 51-10-1 AND 51-30-0. (M)SDR USAA010485Crease Beam · crackedCLT - FOUND CREASE BEAM WEB CRACKED .25 INCH, BS 637, RBL 70. REMOVED AND REPLACED WEB PER SRM 51-10-1. (M)SDR USAA010484Stringer · crackedCLT - FOUND SHELF CRACKED .5 INCH, BS 727, S18A RIGHT, INBOARD FASTENER. REMOVED AND REPLACED SHELF PEER EA 69507 AND BAC DRAWING NR 65-46877-76. (M)SDR USAA010483Web · crackedCLT - FOUND WEB CRACKED .5 INCH, BS 639, 2.75 INCH INBOARD OF S16L. REMOVED DAMAGED WEB SECTION, INSTALLED NEW WEB DOUBLER AND FILLER PER SRM 51-40-02, FIG 1. (M)SDR USAA010482Frame · crackedCLT - FOUND FRAME CHORD ANGLE .25 INCH, BS 639, 2.75 INCH INBOARD OF STRINGER 16L. REMOVED AND REPLACED INNER CHORD ANGLE PER SRM 51-10-1. (M)SDR USAA010481Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 639, S17R. INSTALLED REPAIR DOUBLER PER SRM 51-40-2 FIG 1 AND SRM 51-30-00. (M)SDR USAA010480Crease Beam · crackedCLT - FOUND CREASE BEAM WEB CRACKED .25 INCH, BS 616-639, S17R. REMOVED AND REPLACED WEB PER SRM 51-30-10. (M)
Back to N247US, cancelled Apr 25, 2006