# Service difficulty reports: N259WN A list on [N259WN](https://openairdocs.org/aircraft/N259WN.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 7 · 332 reports - [SDR SWAA2026092314330](https://openairdocs.org/sdr/SWAA2026092314330.md): Access Panel · cracked · Sep 19, 2026 · N259WN · Boeing 7377H4 · Leading Edge Devices > CRACKED ACCESS PANEL 524DB ON LEADING EDGE NR 2 SLAT, LT WING. REPLACED THE ACCESS PANEL 524DB IAW SRM 51-10-02, ITEM 9. - [SDR SWAA2026092335082](https://openairdocs.org/sdr/SWAA2026092335082.md): Web · cracked · Sep 11, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED WEB, BS 500B - 500C, LBL 21.80. REPLACED THE WEB AND FASTENERS, IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHT 81, REV-. - [SDR SWAA2026092374661](https://openairdocs.org/sdr/SWAA2026092374661.md): Fan Cowl · damaged · Sep 5, 2026 · N259WN · Boeing 7377H4 · Nacelle/Pylon, Main Frame > ELONGATED HOLE LOCATED ON OUTBOARD FAN COWL 0.500 INCH FROM FWD EDGE AND 3.375 INCH FROM LOWER EDGE AT ENGINE 1. EVALUATED HOLE LOCATED ON OTBD FAN COWL 0.500 INCH FROM FWD EDGE AND 3.375 INCH FROM LOWER EDGE AT ENGINE AND FOUND WITHIN LIMITS IAW CMM 71-13-3 - [SDR SWAA2026092313467](https://openairdocs.org/sdr/SWAA2026092313467.md): Web · cracked · Aug 25, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > WEB CRACKED AROUND FASTENER HOLE, BS 251+ 6 INCHES, RBL 5. PERFORMED A PERMANENT REPAIR BTWN BS 251 - 255, RBL 3.60 - 15.32 IAW SRM 51-40-02, & EA 26-153-02349. - [SDR SWAA2026092129407](https://openairdocs.org/sdr/SWAA2026092129407.md): Vapor Barrier · cracked · Aug 24, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, Bulkhead > CRACKED VAPOR BARRIER, BS 663.75, LBL 27. REPAIRED THE VAPOR BARRIER. THIS FAULT IS DOCUMENTED ON TTG8Q01DQ62J. - [SDR SWAA2026092188686](https://openairdocs.org/sdr/SWAA2026092188686.md): Vapor Barrier · cracked · Aug 24, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, Bulkhead > CRACKED VAPOR BARRIER, BS 663.75, LBL 27. REPAIRED THE VAPOR BARRIER, FAULT IS DOCUMENTED ON TTG8Q01DQ62J. - [SDR SWAA2026092119869](https://openairdocs.org/sdr/SWAA2026092119869.md): Vapor Barrier · cracked · Aug 24, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, Bulkhead > CRACKED VAPOR BARRIER BS 663.75 AND LBL 27 AT MAIN WHEEL WELL COMPARTMENT. REPAIRED VAPOR BARRIER BS 663.75 AND LBL 27 AT MAIN WHEEL WELL COMPARTMENT. - [SDR SWAA2026092176156](https://openairdocs.org/sdr/SWAA2026092176156.md): Vapor Barrier · cracked · Aug 24, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, Bulkhead > CRACK 4 VAPOR BARRIER BS 663.75 AND LBL 27 AT MAIN WHEEL WELL. REPAIRED VAPOR BARRIER BS 663.75 AND LBL 27 AT MAIN WHEEL WELL. - [SDR SWAA2026092167858](https://openairdocs.org/sdr/SWAA2026092167858.md): Vapor Barrier · cracked · Aug 24, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, Bulkhead > CRACKED VAPOR BARRIER, BS 663.75, LBL 27, IN THE MAIN WHEEL WELL. REPAIRED THE VAPOR BARRIER, FAULT DOCUMENTED ON TTG8Q01DQ62J. - [SDR SWAA2026092355100](https://openairdocs.org/sdr/SWAA2026092355100.md): Bracket · damaged · Aug 23, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > ELONGATED HOLE ON BRACKET, LBL 10, BS 663. EVALUATED AND FABRICATED A NEW BRACKET IAW SRM 51-40-05, & DWG 287A4413, SHEET 66, REV-. THE BRACKET INSTALLATION WILL BE ACCOMPLISHED IAW TTG8Q01DQJAM STEP 23. - [SDR SWAA2026092147085](https://openairdocs.org/sdr/SWAA2026092147085.md): Support Frame · damaged · Aug 22, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, Structure > ELONGATED HOLE ON SUPPORT FRAME LOCATED ON VAPOR BARRIER LT SIDE BTWN BS 649 - 670, LBL 15 IN THE MAIN WHEEL WELL. EVALUATED & FABRICATED SUPPORT FRAME IAW SRM 51-40-05-0G-0, AND DWG 149A7214, SHEET 7 REV -. FRAME INSTALLATION WILL BE ACCOMPLISHED TTG8Q01DQ - [SDR SWAA2026092343474](https://openairdocs.org/sdr/SWAA2026092343474.md): Shear Angle · cracked · Aug 21, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED SHEAR ANGLE, BS 658 - BS638, LBL 40.875. FABRICATED & REPLACED THE SHEAR ANGLE & FASTENERS IAW SRM 51-10-02, ITEM 9, & DWG 110A0220, SHEET 2, REV-. - [SDR SWAA2026092352715](https://openairdocs.org/sdr/SWAA2026092352715.md): Bullnose · cracked · Aug 20, 2026 · N259WN · Boeing 7377H4 · Leading Edge Devices > LEFT WING, NR 2 KRUEGER FLAP, BULL NOSE CRACKED AT CENTER RIB. REMOVED AND REPLACED THE LT WING MID BULL NOSE KRUEGER FLAP NR 2 IAW CMM 57-56-44-NG. - [SDR SWAA2026092374461](https://openairdocs.org/sdr/SWAA2026092374461.md): Bracket · cracked · Aug 20, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED BRACKET ANGLE BTW BS 188 - 203, RBL 3, LOWER NOSE COMPARTMENT. REPLACED THE BRACKET ANGLE AND FASTENERS IAW SRM 51-40-02, AND DWG 141A9194, SHEET 4, REV D. - [SDR SWAA2026092142001](https://openairdocs.org/sdr/SWAA2026092142001.md): Floor Panel · delaminated · Aug 19, 2026 · N259WN · Boeing 7377H4 · Fuselage Floor Panel > DELAMINATED FLOOR PANEL 241FF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 241FF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-17-REPAIR 7 - [SDR SWAA2026092196832](https://openairdocs.org/sdr/SWAA2026092196832.md): Floor Panel · debonded · Aug 18, 2026 · N259WN · Boeing 7377H4 · Fuselage Floor Panel > DEBONDED FLOOR PANEL 241DF IN THE PAX CABIN. REPAIRED FLOOR PANEL 241DF IAW SRM 53-00-50-2R-1, REPAIR 1. - [SDR SWAA2026092169875](https://openairdocs.org/sdr/SWAA2026092169875.md): Doubler · cracked · Aug 18, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, Bulkhead > CRACK ON DOUBLER LOCATED ON RBL 54.21 TO RBL 72 AT VAPOR BARRIER RH SIDE UPPER POSITION. EVALUATED AND FABRICATED DOUBLER LOCATED ON BS 663 RBL 54.21 TO RBL 72 AT VAPOR BARRIER RH SIDE UPPER POSITION I.A.W SRM 51-20-01-0G-0 DWG: 111A1521 SHEET: 5 REV: -. - [SDR SWAA2026092156695](https://openairdocs.org/sdr/SWAA2026092156695.md): Doubler · damaged · Aug 18, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, Bulkhead > ELONGATED HOLE ON DOUBLER ON VAPOR BARRIER, RT SIDE UPPER POSITION BTWN RBL 40 - 45 IN THE MAIN WHEEL WELL. EVALUATED & FABRICATED A DOUBLER IAW SRM 51-40-05, DWG 111A1511, SHEET 16, REV-, PL 11A1511, ITEM 16, REV B, & DWG 111A1151, SHEET 6, REV-. - [SDR SWAA2026092313059](https://openairdocs.org/sdr/SWAA2026092313059.md): Nut Plate · cracked · Aug 17, 2026 · N259WN · Boeing 7377H4 · Wing, Attach Fittings > CRACKED NUT PLATE, OFSS 604, INTERNAL CAVITY LEADING EDGE, RT WING. REPLACED THE NUT PLATE BTWN OSS 362.51 - 384.24. IAW SRM 51-40-02, & DWG 112A4402, SHEET 14, REV-. - [SDR SWAA2026092332053](https://openairdocs.org/sdr/SWAA2026092332053.md): Doubler · damaged · Aug 17, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > ELONGATE HOLE ON DOUBLER ON REAR SPAR, RT VAPOR BARRIER BS 663 BTWN RBL12 - 27. FABRICATED A DOUBLER, & LOCATED IAW DWG 111A1512, SHT 3, REV-. - [SDR SWAA2026092106314](https://openairdocs.org/sdr/SWAA2026092106314.md): Nut Plate · cracked · Aug 17, 2026 · N259WN · Boeing 7377H4 · Wing, Attach Fittings > CRACKED NUT PLATE, OFSS 404, INTERNAL CAVITY L/E OF LT WING. REPLACED THE NUT PLATE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 112A4402, SHEET 40, REV A. - [SDR SWAA2026092101997](https://openairdocs.org/sdr/SWAA2026092101997.md): Support Frame · damaged · Aug 17, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, Structure > ELONGATE HOLE ON FRAME ON RT VAPOR BARRIER BTWN BS 655 - BS 693, RBL 12. EVALUATED & FABRICATED THE FRAME IAW SRM 51-40-05-0G-0, & DWG 149A7214, SHEET 7, REV -. DOUBLER INSTALLATION WILL BE ACCOMPLISHED TTG8Q01DQJAS. - [SDR SWAA2026092127237](https://openairdocs.org/sdr/SWAA2026092127237.md): Nut Plate · cracked · Aug 17, 2026 · N259WN · Boeing 7377H4 · Wing, Attach Fittings > CRACKED RAIL NUT PLATE LOC OFSS 570, INTERNAL CAVITY LEADING EDGE OF RT WING. REMOVED THE NUT PLATE IAW SRM 51-40-01 AND PERFORMED VISUAL INSPECTION ON ADJACENT AREAS AND DID NOT FIND OTHER DAMAGE. REPLACED THE NUT PLATE IAW SRM 51-40-01, SRM 51-40-02, SRM - [SDR SWAA2026092130117](https://openairdocs.org/sdr/SWAA2026092130117.md): Nut Plate · cracked · Aug 17, 2026 · N259WN · Boeing 7377H4 · Wing, Attach Fittings > CRACKED RAIL NUT PLATE, OFSS 491 INTERNAL CAVITY LEADING EDGE IN THE RT WING. REPLACED RAIL NUT PLATE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 112A4402, SHEET 40, REV A. - [SDR SWAA2026092188030](https://openairdocs.org/sdr/SWAA2026092188030.md): Nut Plate · cracked · Aug 17, 2026 · N259WN · Boeing 7377H4 · Leading Edge Devices > CRACKED RAIL NUT PLATE, OFSS 385 INTERNAL CAVITY LEADING EDGE OF THE LT WING. REPLACED THE RAIL NUT PLATE IAW SRM 51-40-02, AND DWG 112A4402, SHEET 40, REV A. - [SDR SWAA2026092147620](https://openairdocs.org/sdr/SWAA2026092147620.md): Nut Plate · cracked · Aug 17, 2026 · N259WN · Boeing 7377H4 · Wing Miscellaneous Structure > CRACKED RAIL NUT PLATE, OFSS 337 INTERNAL CAVITY LEADING EDGE OF LT WING. REPLACED THE NUT PLATE IAW SRM 51-40-02, AND DWG 112A4402, SHEET 40, REV A. - [SDR SWAA2026092127663](https://openairdocs.org/sdr/SWAA2026092127663.md): Nut Plate · cracked · Aug 17, 2026 · N259WN · Boeing 7377H4 · Wing, Attach Fittings > CRACKED RAIL NUT PLATE, OFSS 588 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT PLATE IAW SRM 51-40-02-0G-0, & DWG 112A4402, SHEET 13, REV-. - [SDR SWAA2026092109501](https://openairdocs.org/sdr/SWAA2026092109501.md): Nut Plate · cracked · Aug 17, 2026 · N259WN · Boeing 7377H4 · Wing, Attach Fittings > CRACK RAIL NUT PLATE LOC OFSS 449 INTERNAL CAVITY LEADING EDGE AT RT WING. REPLACED THE NUT PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG:112A4402, SHEET 40, REV A. - [SDR SWAA2026092186645](https://openairdocs.org/sdr/SWAA2026092186645.md): Nut Plate · cracked · Aug 17, 2026 · N259WN · Boeing 7377H4 · Wing Main, Frame Structure > CRACKED RAIL NUT PLATE LOC OFSS 491 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT PLATE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 112A4402, SHEET 40, REV A. - [SDR SWAA2026092309524](https://openairdocs.org/sdr/SWAA2026092309524.md): Support · scratched · Aug 16, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > SCRIBE MARKS LOCATED ON SUPPORT ZEE BTW BS 400 - 488, LBL 21.8, IN THE FWD CARGO BAY. PERFORMED A PERMANENT REPAIR ON THE SUPPORT ZEE IAW SRM 53-00-53-2R-6, REPAIR 6. - [SDR SWAA2026092374341](https://openairdocs.org/sdr/SWAA2026092374341.md): Bracket · damaged · Aug 16, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > ELONGATE HOLE ON BRACKET ASSY LOCATED AT RT VAPOR BARRIER BS 663, RBL 31. EVALUATED & FABRICATED BRACKET ASSY IAW SRM 51-40-05-0G-0, & DWG 287A9112, SHEET 13, REV. A. FOR INSTALLATION OF THE BRACKET, SEE TTG8Q01DQJA. - [SDR SWAA2026092192990](https://openairdocs.org/sdr/SWAA2026092192990.md): Strap · missing · Aug 16, 2026 · N259WN · Boeing 7377H4 · Emergency Equipment > MISSING STRAP ON LIFE LINE OF THE EMERGENCY DOORS LT & RT. INSTALLED THE STRAP ON LIFE LINE IAW SOPM 20-50-12, REV 56, & DWG 416A1500, REV-. - [SDR SWAA2026092135422](https://openairdocs.org/sdr/SWAA2026092135422.md): Web · cracked · Aug 16, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED WEB LOCATED BTWN BS 500D - 520, STR 28L IN THE FWD CARGO BAY. REPLACED THE WEB AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7902, SHEET 126, REV A. - [SDR SWAA2026092387797](https://openairdocs.org/sdr/SWAA2026092387797.md): Support · damaged · Aug 15, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > SCRIBE MARKS ON SUPPORT ZEE BTWN BS 727 - 847, LBL 21.80. REPLACED THE SUPPORT ZEE IAW SRM 51-40-02, AND DWG 146A7500, SHT 85, REV A. - [SDR SWAA2026092397570](https://openairdocs.org/sdr/SWAA2026092397570.md): Elec Connector · damaged · Aug 15, 2026 · N259WN · Boeing 7377H4 · Light System Wiring > CUT ON GALLEY 1 EMERGENCY EXIT LIGHT CABLE. REPLACED THE CONNECTOR ON WIRE W4142 D03658 IAW SWPM 20-30-12, AND PERFORMED EMERGENCY LIGHT OPS TEST IAW AMM 33-51-00-710-801. - [SDR SWAA2026092376151](https://openairdocs.org/sdr/SWAA2026092376151.md): Shield · corroded · Aug 15, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORRODED SHIELD WEB, BS 767 - 794.3, WL156, RBL 22. DRILLED DIAMETER FASTENERS HOLES (10 EA) TO ATTACH FLOOR PANEL TO SHIELD WEB. IAW SRM 51-40-05, & DWG 146A0081, SHT 46, REV -. DIAMETER HOLES IS 0.221 INCH. - [SDR SWAA2026092372218](https://openairdocs.org/sdr/SWAA2026092372218.md): Gusset · cracked · Aug 15, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED GUSSET, BS 500D, S19L. REPLACED THE GUSSET AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7902, SHEET 174, REV -. - [SDR SWAA2026092345565](https://openairdocs.org/sdr/SWAA2026092345565.md): Frame · dented · Aug 15, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, Frame > DENTED FRAME, BS 500B, STR 25L - 26L IN THE FWD CARGO BAY. MADE & DRILLED A REPAIR FOR FRAME BS 500B, STR 25L - 26L IAW SRM 53-30-07-2R-1, REPAIR 1, ALTERNATIVE 1. - [SDR SWAA2026092107956](https://openairdocs.org/sdr/SWAA2026092107956.md): Hook · corroded · Aug 15, 2026 · N259WN · Boeing 7377H4 · Emergency Equipment > CORROSION ON LEFT EMERGENCY EXIT DOOR LIFE LINE HOOK. REPLACED THE LIFE LINE HOOK IAW AMM 25-61-10-000-802, AND AMM 25-61-10-400-802. - [SDR SWAA2026092107556](https://openairdocs.org/sdr/SWAA2026092107556.md): Hook · corroded · Aug 15, 2026 · N259WN · Boeing 7377H4 · Emergency Equipment > CORROSION ON THE EMERGENCY EXIT DOOR LIFE LINE HOOK. REPLACED THE LIFE LINE HOOK IAW AMM 25-61-10-000-802, AND AMM 25-61-10-400-802. - [SDR SWAA2026092109333](https://openairdocs.org/sdr/SWAA2026092109333.md): Fastener · worn · Aug 15, 2026 · N259WN · Boeing 7377H4 · Emergency Equipment > WORN HARDWARE ON GIRT BAR FITTING, AFT SERVICE & ENTRY DOORS. REPLACED THE HARDWARE IAW AMM 25-66-02-400-801. - [SDR SWAA2026092362109](https://openairdocs.org/sdr/SWAA2026092362109.md): Support · corroded · Aug 14, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORRODED LOWER SILL BTWN BS 794.5 - 847, RBL 23, WL 156. REMOVED CORROSION AND EVALUATED REWORKED AREAS LOWER SILL IAW SRM 53-60-15-1A-1. - [SDR SWAA2026092167397](https://openairdocs.org/sdr/SWAA2026092167397.md): Vapor Barrier · cracked · Aug 14, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, Bulkhead > CRACKED VAPOR BARRIER, BS 663.75, LBL 27. REPAIRED THE VAPOR BARRIER IAW SRM 51-70-04-2R-10, REPAIR 10. - [SDR SWAA2026092181079](https://openairdocs.org/sdr/SWAA2026092181079.md): Vapor Barrier · cracked · Aug 14, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, Bulkhead > CRACK VAPOR BARRIER BS 663.75 AND RBL 32 AT MAIN WHEEL WELL COMPARTMENT. REPAIRED VAPOR BARRIER BS 663.75 AND RBL 32 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. - [SDR SWAA2026092169457](https://openairdocs.org/sdr/SWAA2026092169457.md): Crossbeam · cracked · Aug 14, 2026 · N259WN · Boeing 7377H4 · Fuselage Main, Structure > CRACKED FLOOR CROSSBEAM, BS 540, BTWN BL 0 - RBL 24.75. REPLACED THE CROSSBEAM IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A0060, SHEET 46, REV -. - [SDR SWAA2026092105704](https://openairdocs.org/sdr/SWAA2026092105704.md): Support Angle · cracked · Aug 14, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED SUPPORT ANGLE, BS 663.75, RBL 7. INSTALLED A PERMANENT REPAIR TO THE SUPPORT ANGLE IAW SRM 57-10-10-2R-5, REPAIR 5, AND DWG 111A100, SHEET 226, REV A. - [SDR SWAA2026092132662](https://openairdocs.org/sdr/SWAA2026092132662.md): Fastener · worn · Aug 13, 2026 · N259WN · Boeing 7377H4 · Emergency Equipment > WORN HARDWARE ON GIRT BAR FITTING, FWD SERVICE & ENTRY DOORS. REPLACED THE HARDWARE IAW AMM 25-66-02-400-801. - [SDR SWAA2026092139517](https://openairdocs.org/sdr/SWAA2026092139517.md): Strap · corroded · Aug 12, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION STRAP RH SIDE LOCATED ON STR 25R BETWEEN BS 727 TO 727E AT AFT CARGO COMPARTMENT. EVALUATED CAPSTRIP LOC. ON RH SIDE STR 25R BETWEEN BS 727 TO BS 727E AT AFT CARGO COMPARTMENT AND NOT FOUND ALLOWABLE DAMAGE I.A.W B737-700 SRM 53-00-53-1A-2 CAPSTRIP - [SDR SWAA2026092146324](https://openairdocs.org/sdr/SWAA2026092146324.md): Strap · corroded · Aug 12, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORRODED STRAP, BTWN BS 767 - 847, STR 25L IN THE AFT CARGO BAY. EVALUATED CORROSION ON CAPSTRIP & DID NOT FIND ALLOWABLE DAMAGE IAW SRM 53-00-53-1A-2. REPLACED THE CAPSTRIP (STRAP) IAW SRM 51-10-02-0G, STEP 9, AND DWG 453A2600, SHEET 92, REV A. - [SDR SWAA2026092128302](https://openairdocs.org/sdr/SWAA2026092128302.md): Strap · corroded · Aug 12, 2026 · N259WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORRODED STRAP, STRINGER 25L, BS 727 - 727E IN THE CARGO BAY. EVALUATED THE CAPSTRIP & DID NOT FIND ALLOWABLE DAMAGE IAW SRM 53-00-53-1A-2. REPLACED THE CAPSTRIP (STRAP) IAW SRM 51-10-02-0G-0, ITEM 9, & DWG 453A2600, SHEET 92, REV A. Next page: https://openairdocs.org/aircraft/N259WN/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 = 'N259WN' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N259WN/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.