# Service difficulty reports: N247US, cancelled Apr 25, 2006 A list on [N247US, cancelled Apr 25, 2006](https://openairdocs.org/deregistered/N247US-2006-04-25.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 86 reports - [SDR USAA010573](https://openairdocs.org/sdr/USAA010573.md): Keel · corroded · May 20, 2001 · N247US · Boeing 737201 · Fuselage Main, Keel > CLT - 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 USAA010556](https://openairdocs.org/sdr/USAA010556.md): Shear Tie · corroded · May 18, 2001 · N247US · Boeing 737201 · Fuselage Structure (General) > CLT - 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 USAA010557](https://openairdocs.org/sdr/USAA010557.md): Web · cracked · May 18, 2001 · N247US · Boeing 737201 · Fuselage Main, Structure > CLT - FOUND WEB CRACKED 1 INCH, BS 712, LBL 24. INSTALLED REPAIR DOUBLER, REPLACEMENT WEB AND 4 VERTICAL STIFFENERS PER EA 69504. (M) - [SDR USAA010558](https://openairdocs.org/sdr/USAA010558.md): Floorbeam · cracked · May 18, 2001 · N247US · Boeing 737201 · Fuselage Main, Floor Beam > CLT - 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 USAA010559](https://openairdocs.org/sdr/USAA010559.md): Frame · cracked · May 18, 2001 · N247US · Boeing 737201 · Fuselage Main, Frame > CLT - FOUND CHORD CRACKED 1 INCH, BS 663, LBL 24, WL 203. INSTALLED REPAIR CHORD PER EA 69538 AND SB 737-53-1184. (M) - [SDR USAA010560](https://openairdocs.org/sdr/USAA010560.md): Web · cracked · May 18, 2001 · N247US · Boeing 737201 · Fuselage Structure (General) > CLT - 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 USAA010561](https://openairdocs.org/sdr/USAA010561.md): Frame · cracked · May 18, 2001 · N247US · Boeing 737201 · Fuselage Main, Frame > CLT - FOUND VERTICAL CHORD CRACKED 1.3 INCHES, BS 178, LBL 6, WL 198. INSTALLED REPAIR KIT PER EO 5300V155. (M) - [SDR USAA010562](https://openairdocs.org/sdr/USAA010562.md): Attach Fitting · corroded · May 18, 2001 · N247US · Boeing 737201 · Vertical Stabilizer, Attach Fittings > CLT - 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 USAA010563](https://openairdocs.org/sdr/USAA010563.md): Beam · cracked · May 18, 2001 · N247US · Boeing 737201 · Fuselage Structure (General) > CLT - FOUND BEAM CRACKED 3 INCHES, BS 663, BL 0. INSTALLED REPAIR ANGLES PER EA 69611. (M) - [SDR USAA010564](https://openairdocs.org/sdr/USAA010564.md): Skin · cracked · May 18, 2001 · N247US · Boeing 737201 · Fuselage Structure (General) > CLT - FOUND SKIN CRACKED.25 INCH, BS 345, AFT LOWER CORNER OF AIRSTAIR CUTOUT. REMOVED AND REPLACED REPAIR TRIPLER PER EA 69582. (M) - [SDR USAA010565](https://openairdocs.org/sdr/USAA010565.md): Skin · cracked · May 18, 2001 · N247US · Boeing 737201 · Fuselage Structure (General) > CLT - FOUND FUSELAGE SKIN CRACKED.25 INCH AFT ENTRY DOOR, UPPER HINGE CUTOUT. INSTALLED DOUBLER PER SRM 543-30-3, FIG 21A. (M) - [SDR USAA010566](https://openairdocs.org/sdr/USAA010566.md): Skin · corroded · May 18, 2001 · N247US · Boeing 737201 · Fuselage Structure (General) > CLT - FOUND FUSELAGE SKIN CORRODED, BS 468, BL 0. REMOVED DAMAGE, INSTALLED REPAIR DOUBLER PER SRM 51-20-4 AND 53-30-3. (M) - [SDR USAA010552](https://openairdocs.org/sdr/USAA010552.md): Frame · cracked · May 18, 2001 · N247US · Boeing 737201 · Fuselage Structure (General) > CLT - FOUND FRAME CRACKED.25 INCH, BS 639, STRINGER 17R. INSTALLED REPAIR DOUBLER PER SRM 51-40-2, FIG 1. (M) - [SDR USAA010553](https://openairdocs.org/sdr/USAA010553.md): Frame · cracked · May 18, 2001 · N247US · Boeing 737201 · Fuselage Structure (General) > CLT - 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 USAA010555](https://openairdocs.org/sdr/USAA010555.md): Doubler · cracked · May 18, 2001 · N247US · Boeing 737201 · Fuselage Structure (General) > CLT - FOUND DOUBLER CRACKED 2 INCHES, BS 676, BETWEEN LBL 24 AND RBL 24, WL 206. INSTALLED RE-INFORCEMENT CHANNELS PER EO 5791G632. (M) - [SDR USAA010525](https://openairdocs.org/sdr/USAA010525.md): Skin · cracked · May 10, 2001 · N247US · Boeing 737201 · Fuselage Main, Plate/Skin > CLT - 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 USAA010524](https://openairdocs.org/sdr/USAA010524.md): Frame · cracked · May 10, 2001 · N247US · Boeing 737201 · Fuselage Main, Frame > CLT - 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 USAA010523](https://openairdocs.org/sdr/USAA010523.md): Frame · cracked · May 10, 2001 · N247US · Boeing 737201 · Fuselage Main, Frame > CLT - FOUND FRAME CRACKED.25 INCH, BS 480 STRINGER 21L. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 51-40-3, FIG 1. (M) - [SDR USAA010522](https://openairdocs.org/sdr/USAA010522.md): Angle · cracked · May 10, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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 USAA010521](https://openairdocs.org/sdr/USAA010521.md): Stringer · cracked · May 10, 2001 · N247US · Boeing 737201 · Fuselage Main, Longeron/Stringer > CLT - FOUND STRINGER CRACKED.070 INCH, BS 380, STRINGER 2L. REMOVED DAMAGE SECTION, SPLICED IN NEW STRINGER SECTION PER SRM 53-10-3. (M) - [SDR USAA010518](https://openairdocs.org/sdr/USAA010518.md): Web · cracked · May 8, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - FOUND FLOOR STRUCTURE WEB CRACKED 1 INCH, BS 178, WL 207 AT LBL 24. REMOVED AND REPLACED WEB PER EO 5300V157. (M) - [SDR USAA010520](https://openairdocs.org/sdr/USAA010520.md): Pressure Panel · damaged · May 8, 2001 · N247US · Boeing 737201 · Fuselage Main, Bulkhead > CLT - 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 USAA010519](https://openairdocs.org/sdr/USAA010519.md): Frame · cracked · May 8, 2001 · N247US · Boeing 737201 · Fuselage Main, Frame > CLT - 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 USAA010497](https://openairdocs.org/sdr/USAA010497.md): Skin · corroded · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Plate/Skin > CLT - 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 USAA010496](https://openairdocs.org/sdr/USAA010496.md): Stringer · corroded · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Longeron/Stringer > CLT - 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 USAA010493](https://openairdocs.org/sdr/USAA010493.md): Floorbeam · corroded · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Floor Beam > CLT - 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 USAA010491](https://openairdocs.org/sdr/USAA010491.md): Floorbeam · corroded · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Floor Beam > CLT - 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 USAA010475](https://openairdocs.org/sdr/USAA010475.md): Angle · corroded · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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 USAA010474](https://openairdocs.org/sdr/USAA010474.md): Floorbeam · corroded · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Floor Beam > CLT - 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 USAA010473](https://openairdocs.org/sdr/USAA010473.md): Floorbeam · corroded · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Floor Beam > CLT - 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 USAA010503](https://openairdocs.org/sdr/USAA010503.md): Tie Clip · cracked · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - FOUND TIE CLIP CRACKED.125 INCH, BS 597, STRINGER 4R. INSTALLED NEW TIE CLIP PER EO 5393G227. (M) - [SDR USAA010502](https://openairdocs.org/sdr/USAA010502.md): Tie Clip · cracked · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - FOUND TIE CLIP CRACKED.125 INCH, BS 597, S5R. INSTALLED NEW TIE CLIP PER SRM 51-30-2. (M) - [SDR USAA010501](https://openairdocs.org/sdr/USAA010501.md): Tie Clip · cracked · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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 USAA010500](https://openairdocs.org/sdr/USAA010500.md): Tie Clip · cracked · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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 USAA010499](https://openairdocs.org/sdr/USAA010499.md): Tie Clip · cracked · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - FOUND TIE CLIP CRACKED.125 INCH, BS 663, S10R. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M) - [SDR USAA010498](https://openairdocs.org/sdr/USAA010498.md): Bulkhead · cracked · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Bulkhead > CLT - FOUND BULKHEAD CRACKED 1 INCH, BS 178, WL 234, RBL 11. INSTALLED DOUBLER AND FILLER PER SRM 53-10-11 FIG 1. (M) - [SDR USAA010495](https://openairdocs.org/sdr/USAA010495.md): Hinge Fitting · cracked · Apr 29, 2001 · N247US · Boeing 737201 · Ailerons > CLT - 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 USAA010494](https://openairdocs.org/sdr/USAA010494.md): Angle · cracked · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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 USAA010492](https://openairdocs.org/sdr/USAA010492.md): Tie Clip · cracked · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - FOUND TIE CLIP CRACKED.25 INCH, BS 360, S4L. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM 51-30-2. (M) - [SDR USAA010490](https://openairdocs.org/sdr/USAA010490.md): Stringer · cracked · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Longeron/Stringer > CLT - FOUND STRINGER CRACKED 1 INCH, BS 787, S16R. INSTALLED STRINGER SPLICE REPAIR PER SRM 53-30-3, 53-10-2. (M) - [SDR USAA010489](https://openairdocs.org/sdr/USAA010489.md): Intercostal · cracked · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - FOUND INTERCOSTAL CRACKED 1 INCH, BS 178, WL 195, RBL 24. REMOVED AND REPLACED INTERCOSTAL PER EO 5300V155. (M) - [SDR USAA010488](https://openairdocs.org/sdr/USAA010488.md): Stringer · cracked · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Longeron/Stringer > CLT - FOUND STRINGER CRACKED.5 INCH, BS 360, S15L. REMOVED AND REPLACED STRINGER SECTION PER RM 51-10-1. (M) - [SDR USAA010487](https://openairdocs.org/sdr/USAA010487.md): Skin · cracked · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Plate/Skin > CLT - 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 USAA010486](https://openairdocs.org/sdr/USAA010486.md): Stringer · cracked · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Longeron/Stringer > CLT - 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 USAA010485](https://openairdocs.org/sdr/USAA010485.md): Crease Beam · cracked · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Structure > CLT - FOUND CREASE BEAM WEB CRACKED.25 INCH, BS 637, RBL 70. REMOVED AND REPLACED WEB PER SRM 51-10-1. (M) - [SDR USAA010484](https://openairdocs.org/sdr/USAA010484.md): Stringer · cracked · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Longeron/Stringer > CLT - 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 USAA010483](https://openairdocs.org/sdr/USAA010483.md): Web · cracked · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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 USAA010482](https://openairdocs.org/sdr/USAA010482.md): Frame · cracked · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Frame > CLT - 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 USAA010481](https://openairdocs.org/sdr/USAA010481.md): Frame · cracked · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Frame > CLT - 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 USAA010480](https://openairdocs.org/sdr/USAA010480.md): Crease Beam · cracked · Apr 29, 2001 · N247US · Boeing 737201 · Fuselage Main, Structure > CLT - FOUND CREASE BEAM WEB CRACKED.25 INCH, BS 616-639, S17R. REMOVED AND REPLACED WEB PER SRM 51-30-10. (M) Next page: https://openairdocs.org/deregistered/N247US-2006-04-25/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N247US-2006-04-25/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.