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.

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)May 20, 2001 · N247US · Boeing 737201 · Fuselage Main, KeelSDR 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)May 18, 2001 · N247US · Boeing 737201 · Fuselage Structure (General)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)May 18, 2001 · N247US · Boeing 737201 · Fuselage Main, StructureSDR 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)May 18, 2001 · N247US · Boeing 737201 · Fuselage Main, Floor BeamSDR 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)May 18, 2001 · N247US · Boeing 737201 · Fuselage Main, FrameSDR 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)May 18, 2001 · N247US · Boeing 737201 · Fuselage Structure (General)SDR USAA010561Frame · crackedCLT - FOUND VERTICAL CHORD CRACKED 1.3 INCHES, BS 178, LBL 6, WL 198. INSTALLED REPAIR KIT PER EO 5300V155. (M)May 18, 2001 · N247US · Boeing 737201 · Fuselage Main, FrameSDR 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)May 18, 2001 · N247US · Boeing 737201 · Vertical Stabilizer, Attach FittingsSDR USAA010563Beam · crackedCLT - FOUND BEAM CRACKED 3 INCHES, BS 663, BL 0. INSTALLED REPAIR ANGLES PER EA 69611. (M)May 18, 2001 · N247US · Boeing 737201 · Fuselage Structure (General)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)May 18, 2001 · N247US · Boeing 737201 · Fuselage Structure (General)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)May 18, 2001 · N247US · Boeing 737201 · Fuselage Structure (General)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)May 18, 2001 · N247US · Boeing 737201 · Fuselage Structure (General)SDR USAA010552Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 639, STRINGER 17R. INSTALLED REPAIR DOUBLER PER SRM 51-40-2, FIG 1. (M)May 18, 2001 · N247US · Boeing 737201 · Fuselage Structure (General)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)May 18, 2001 · N247US · Boeing 737201 · Fuselage Structure (General)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)May 18, 2001 · N247US · Boeing 737201 · Fuselage Structure (General)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)May 10, 2001 · N247US · Boeing 737201 · Fuselage Main, Plate/SkinSDR 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)May 10, 2001 · N247US · Boeing 737201 · Fuselage Main, FrameSDR USAA010523Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 480 STRINGER 21L. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 51-40-3, FIG 1. (M)May 10, 2001 · N247US · Boeing 737201 · Fuselage Main, FrameSDR 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)May 10, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous StructureSDR 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)May 10, 2001 · N247US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA010518Web · crackedCLT - FOUND FLOOR STRUCTURE WEB CRACKED 1 INCH, BS 178, WL 207 AT LBL 24. REMOVED AND REPLACED WEB PER EO 5300V157. (M)May 8, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous StructureSDR 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)May 8, 2001 · N247US · Boeing 737201 · Fuselage Main, BulkheadSDR 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)May 8, 2001 · N247US · Boeing 737201 · Fuselage Main, FrameSDR 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)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Plate/SkinSDR 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)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR 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)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Floor BeamSDR 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)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Floor BeamSDR 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)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous StructureSDR 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)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Floor BeamSDR 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)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA010503Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 597, STRINGER 4R. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010502Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 597, S5R. INSTALLED NEW TIE CLIP PER SRM 51-30-2. (M)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous StructureSDR 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)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous StructureSDR 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)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010499Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 663, S10R. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous StructureSDR 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)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, BulkheadSDR 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)Apr 29, 2001 · N247US · Boeing 737201 · AileronsSDR 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)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010492Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, BS 360, S4L. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM 51-30-2. (M)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010490Stringer · crackedCLT - FOUND STRINGER CRACKED 1 INCH, BS 787, S16R. INSTALLED STRINGER SPLICE REPAIR PER SRM 53-30-3, 53-10-2. (M)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA010489Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED 1 INCH, BS 178, WL 195, RBL 24. REMOVED AND REPLACED INTERCOSTAL PER EO 5300V155. (M)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010488Stringer · crackedCLT - FOUND STRINGER CRACKED .5 INCH, BS 360, S15L. REMOVED AND REPLACED STRINGER SECTION PER RM 51-10-1. (M)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR 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)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Plate/SkinSDR 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)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA010485Crease Beam · crackedCLT - FOUND CREASE BEAM WEB CRACKED .25 INCH, BS 637, RBL 70. REMOVED AND REPLACED WEB PER SRM 51-10-1. (M)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, StructureSDR 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)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR 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)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous StructureSDR 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)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, FrameSDR 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)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, FrameSDR USAA010480Crease Beam · crackedCLT - FOUND CREASE BEAM WEB CRACKED .25 INCH, BS 616-639, S17R. REMOVED AND REPLACED WEB PER SRM 51-30-10. (M)Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Structure
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