# Service difficulty reports: N953WN

A list on [N953WN](https://openairdocs.org/aircraft/N953WN.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 5 · 221 reports

- [SDR SWAA2026082402079](https://openairdocs.org/sdr/SWAA2026082402079.md): Isolator · cracked · Aug 19, 2026 · N953WN · Boeing 7377H4 · Escape Slide
  > AFT ENTRY DOOR UPPER FWD SLIDE MOUNT ISOLATOR CRACKED. R & R AFT ENTRY DOOR UPPER FWD SLIDE MOUNT ISOLATOR IAW SRM 51-40-02.
- [SDR SWAA2026082449279](https://openairdocs.org/sdr/SWAA2026082449279.md): Isolator · cracked · Aug 19, 2026 · N953WN · Boeing 7377H4 · Escape Slide
  > FWD SERVICE DOOR FWD LOWER SLIDE ISOLATOR IS CRACKED. R & R FWD SERVICE DOOR FWD LOWER SLIDE ISOLATOR IAW SRM 51-40-02.
- [SDR SWAA2026080470737](https://openairdocs.org/sdr/SWAA2026080470737.md): Light · inoperative · Aug 1, 2026 · N953WN · Boeing 7377H4 · Emergency Lighting
  > THE R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT IS INOPERATIVE. REPLACED THE R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT AND PERFORMED TEST IAW AMM 33-51-04-960-801. TESTED OK. TASK CARD COMPLETE.
- [SDR SWAA2026080565018](https://openairdocs.org/sdr/SWAA2026080565018.md): Support · cracked · Jul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ZEE, BS 887 - 907, RBL 21 IN THE AFT CARGO BAY. REPLACED THE SUPPORT ZEE AND FASTENERS IAW SRM 51-40-02, & DWG 147A7500, SHEET 37, REV-.
- [SDR SWAA2026080527935](https://openairdocs.org/sdr/SWAA2026080527935.md): Web · corroded · Jul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED SHIELD WEB, BS 767 - 794.3, WL 156, RBL 22 IN THE AFT CARGO BAY. REPLACED THE SHIELD WEB IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, AND DWG 146A0081, SHEET 43, REV -.
- [SDR SWAA2026080568771](https://openairdocs.org/sdr/SWAA2026080568771.md): Stringer Clip · corroded · Jul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CORRODED STRINGER CLIP BS 787, STR 26R, WL 152 IN THE AFT CARGO BAY. REPLACED THE STRINGER CLIP IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, AND DWG 146A1262, SHT 116, REV-.
- [SDR SWAA2026080501765](https://openairdocs.org/sdr/SWAA2026080501765.md): Support · corroded · Jul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED SUPPORT ZEE, BS 500A - 500D, STR 26R, WL 156.5 IN THE FWD CARGO BAY. REPLACED THE SUPPORT ZEE & FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 143A7500 SHEET: 71 AND REV-.
- [SDR SWAA2026080541643](https://openairdocs.org/sdr/SWAA2026080541643.md): Support · corroded · Jul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE BTWN BS 727B - 827, LBL 21, WL 156. ( 10 POINTS) IN THE AFT CARGO BAY. INSTALLED SUPPORT ZEE AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 146A7500, SHT 137, REV-.
- [SDR SWAA2026080519768](https://openairdocs.org/sdr/SWAA2026080519768.md): Angle · cracked · Jul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE BTWN BS 907 - 927, S25R - 27R IN THE AFT OF AFT CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, AND DWG 147A7221, SHEET 28, REV -.
- [SDR SWAA2026080517633](https://openairdocs.org/sdr/SWAA2026080517633.md): Support · corroded · Jul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED SUPPORT ZEE, BTW BS 727A - 767, RBL 21, WL 156 IN THE AFT CARGO BAY. REPLACED THE SUPPORT ZEE AND FASTENERS IAW SRM 51-40-02-0G-0, DWG 146A7500, SHEET 13, REV-, & DRAWING 146A7500, SHT 174, REV-.
- [SDR SWAA2026080551868](https://openairdocs.org/sdr/SWAA2026080551868.md): Support Angle · corroded · Jul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ANGLE, BS 500D, STR 26R - 26L AND WL 156.5 IN THE FWD CARGO BAY. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-10-02, ITEM 9, & DWG 143A7902, SHT 259, REV -.
- [SDR SWAA2026080501475](https://openairdocs.org/sdr/SWAA2026080501475.md): Web · corroded · Jul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SHIELD WEB BTWN BS 490 - 500A, STR 26R, WL 156.5 IN THE FWD CARGO BAY. REPLACED SHIELD WEB IAW SRM 51-40-02-0G-0, AND DWG 143A0080, SHT 41, REV-.
- [SDR SWAA2026080546647](https://openairdocs.org/sdr/SWAA2026080546647.md): Web · corroded · Jul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED SHIELD WEB, BTW BS 847 TO 867, WL156, AND RBL 22 IN THE AFT CARGO BAY. REPLACED THE SHIELD WEB AND FASTENERS IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, AND DRAWING 146A0081, SHEET 43, REV-.
- [SDR SWAA2026080506407](https://openairdocs.org/sdr/SWAA2026080506407.md): Cargo Track · corroded · Jul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION TRACK RBBL 13.84 BTW STA 787 TO STA 847 AND WL 155 (5 POINTS) AT AFT CARGO COMPARTMENT. REPLACED TRACK AND FASTENERS, RBL 13.84 BTW BS 767 - 887 AND WL 155 AT AFT CARGO BAY IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, AND DRAWING 146A7500, SH
- [SDR SWAA2026080525167](https://openairdocs.org/sdr/SWAA2026080525167.md): Web · corroded · Jul 17, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION WEB BTW BS 747 TO 767, RBL 21, AND WL 156 AT AFT CARGO COMPARTMENT. REPLACED WEB BTW BS 747 TO 767 RBL 21 AND WL 156 AT AFT CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9 AND DWG 146A7502 SHEET: 49 REV -.
- [SDR SWAA2026080536416](https://openairdocs.org/sdr/SWAA2026080536416.md): Isolation Mount · deteriorated · Jul 16, 2026 · N953WN · Boeing 7377H4 · Emergency Exits
  > DETERIORATE ISOLATION MOUNTS, UPPER POSITION ON THE RT EMERGENCY EXIT, (2EA). REPLACED THE ISOLATION MOUNTS IAW SRM-51-10-02, ITEM 9, AND DWG:144A8111, SHT 61, REV-.
- [SDR SWAA2026080591590](https://openairdocs.org/sdr/SWAA2026080591590.md): Floor Panel · cracked · Jul 16, 2026 · N953WN · Boeing 7377H4 · Fuselage Floor Panel
  > CRACKED FLOOR PANEL 120BF IN THE FWD CARGO BAY. REPLACED FLOOR PANEL 120BF IAW SRM 51-10-02-0G-0, PARA 9, AND DWG 453A1610, SHT 7, REV C.
- [SDR SWAA2026080550087](https://openairdocs.org/sdr/SWAA2026080550087.md): Isolator · deteriorated · Jul 16, 2026 · N953WN · Boeing 7377H4 · Emergency Exits
  > DETERIORATED MOUNT ISOLATOR UPPER POSITION AT EMERGENCY EXIT LT SIDE (2EA). REPLACED MOUNT ISOLATOR UPPER POSITION AT EMERGENCY EXIT LT SIDE (2EA) IAW SRM-51-10-02, ITEM 9, AND DWG 144A8111, SHEET 61, REV -.
- [SDR SWAA2026080446399](https://openairdocs.org/sdr/SWAA2026080446399.md): Stringer · cracked · Jul 16, 2026 · N953WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER 25R, BS 540, FWD CARGO BAY, REPAIRED THE STRINGER 25R, BETWEEN BS 500C - 540 IAW SRM 53-00-03-2R-1, REPAIR 1.
- [SDR SWAA2026080585056](https://openairdocs.org/sdr/SWAA2026080585056.md): Access Panel · cracked · Jul 15, 2026 · N953WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > CRACKED LEADING EDGE RIB, ACCESS PANEL 331B HSS 114.55 LT HORIZONTAL STAB. REPLACED THE LEADING EDGE RIB ACCESS PANEL 331B IAW SRM 51-40-02-0G-0, AND DWG 186A1001, SHT 19, REV-.
- [SDR SWAA2026080555591](https://openairdocs.org/sdr/SWAA2026080555591.md): Angle · cracked · Jul 15, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE, BS 867, S26L, AFT CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, AND DRAWING 149A8102, REV A, SHT 19.
- [SDR SWAA2026080502837](https://openairdocs.org/sdr/SWAA2026080502837.md): Crossbeam · cracked · Jul 15, 2026 · N953WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACKED BRAKE PANEL FLOOR STRUCTURE BS 540 BTW LBL 24.82 TO BL 0. REPLACED THE BRAKE PANEL AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, STEP 9, & DWG 143A0060, SHT 58, REV A.
- [SDR SWAA2026080558809](https://openairdocs.org/sdr/SWAA2026080558809.md): Crossbeam · cracked · Jul 15, 2026 · N953WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACKED BRAKE PANEL FLOOR STRUCTURE BS540 AND BTW RBL24.82 TO BL0 AT PASSENGER CABIN. REPLACED BRAKE PANEL FLOOR STRUCTURE BS540 AND BTW RBL24.82 TO BL0 AT PASSENGER CABIN IAW SRM 51-40-02-0G-0 SRM 51-10-02-0G-0 ITEM 9 AND DWG:143A0060 SHEET:64 REV:-.
- [SDR SWAA2026080553996](https://openairdocs.org/sdr/SWAA2026080553996.md): Frame · cracked · Jul 14, 2026 · N953WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACKED FRAME, BS 312, S5L & 6L IN THE FWD GALLEY AREA. REPAIRED FRAME IAW M-22-153-01244, SEE TTG8Q01D738K. COMPLETED TASK.
- [SDR SWAA2026080502010](https://openairdocs.org/sdr/SWAA2026080502010.md): Web · cracked · Jul 14, 2026 · N953WN · Boeing 7377H4 · Nacelle/Pylon Miscellaneous Structure
  > CRACKED SUPPORT WEB, OTBD FAN COWL UPPER POSITION ON NR 2 ENGINE. REPLACED THE SUPPORT WEB AND FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, & 71-13-30.
- [SDR SWAA2026080535641](https://openairdocs.org/sdr/SWAA2026080535641.md): Angle · cracked · Jul 13, 2026 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE BS 400, STR 26L IN THE FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, AND DWG 143A7505, SHEET 117, REV-.
- [SDR SWAA2026080527872](https://openairdocs.org/sdr/SWAA2026080527872.md): Glowstrip · deteriorated · Jul 11, 2026 · N953WN · Boeing 7377H4 · Emergency Lighting
  > DETERIORATED PHOTOLUMINESCENT STRIP ALONG PAX CABIN. REPLACED AND PHOTOLUMINESCENT STRIP ALONG PAX CABIN IAW AMM 33-51-15-400-802, STEP 1.E (1) (3) (5), & DWG 33500007, REV 2.
- [SDR SWAA2026080546983](https://openairdocs.org/sdr/SWAA2026080546983.md): Access Panel · elongated · Jul 11, 2026 · N953WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLE ON ACCESS PANEL 561BB, LT WING. REPAIRED THE ACCESS PANEL 561BB IAW SRM 51-70-04-2R-9, REPAIR 9.
- [SDR SWAA2026080575921](https://openairdocs.org/sdr/SWAA2026080575921.md): Access Panel · damaged · Jul 11, 2026 · N953WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLE ACCESS PANEL 661BB AT RT WING. REPAIRED ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-04-2R-9, REPAIR 9.
- [SDR SWAA2026080540700](https://openairdocs.org/sdr/SWAA2026080540700.md): Skin · cracked · Jul 9, 2026 · N953WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK LOWER SURFACE OF RT WING LEADING EDGE SLAT 7 NOSE SKIN AT ACTUATOR LOCATION AROUND THE FASTENER. PERFORMED A REPAIR ON LOWER SURFACE OF LEADING EDGE SLAT 7 NOSE SKIN IAW SRM 57-42-01-2R, REPAIR 8, & DWG 114A5020, REV A, SHEET 38.
- [SDR SWAA2026080580743](https://openairdocs.org/sdr/SWAA2026080580743.md): Skin · cracked · Jul 9, 2026 · N953WN · Boeing 7377H4 · Leading Edge Devices
  > CRACKED LOWER SURFACE OF LEADING EDGE SLAT 6 NOSE SKIN AT THE ACTUATOR LOCATION. AROUND FASTENER. PERFORMED A REPAIR ON THE LOWER SURFACE OF LEADING EDGE SLAT 6 NOSE SKIN IAW SRM 51-40-02, AND SRM 57-42-01-2R-8, REPAIR 8, AND DWG 114A5030, REV A, SHEET 2.
- [SDR SWAA2025121551040](https://openairdocs.org/sdr/SWAA2025121551040.md): Support Fitting · corroded · Dec 9, 2025 · N953WN · Boeing 7377H4 · Wing, Landing Gear Attach Fittings
  > LEFT MAIN LANDING GEAR FWD TRUNNION SUPPORT FITTING, LOWER INBOARD LUG NR 4. OUTER FACE HAS EVIDENCE OF CORROSION. R & R LT MLG FWD TRUNNION SUPPORT FITTING; LOWER INBD LUG NR 4 PER EA. 1-A57-3246.
- [SDR SWAA2025111734914](https://openairdocs.org/sdr/SWAA2025111734914.md): Seal · cracked · Nov 14, 2025 · N953WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > R/H HORIZONTAL UPPER SLIDER IS CRACKED. R & R STABILIZER-TO-BODY FRONT SPAR UPPER SLIDING SEAL PER M/M 53-31-31.
- [SDR SWAA2025071590692](https://openairdocs.org/sdr/SWAA2025071590692.md): Lens · broken · Jul 12, 2025 · N953WN · Boeing 7377H4 · Emergency Lighting
  > EXIT LIGHT COVER LENS BY L1 DOOR BROKEN. R&R EXIT LIGHT COVER LENS IAW AMM 33-51-02
- [SDR SWAA2025021294868](https://openairdocs.org/sdr/SWAA2025021294868.md): Slide · dislodged · Feb 11, 2025 · N953WN · Boeing 7377H4 · Escape Slide
  > FWD ENTRY DOOR SLIDE FELL OUT OF SLIDE COMPARTMENT<[01] 01 - REMOVED AND REPLACED PER [AMM 25-66-01-400-804-NG (ESCAPE SLIDE PACK INSTALLATION (UNSCHEDULED) - PERMANENT)]
- [SDR SWAA2025011385281](https://openairdocs.org/sdr/SWAA2025011385281.md): Megaphone · loose · Jan 12, 2025 · N953WN · Boeing 7377H4 · Cargo Compartments
  > AFT MEGAPHONE HANDLE LOOSE.<[01] REMOVED AND REPLACED AFT MEGAPHONE PER AMM25-64-00.
- [SDR SWAA2024110554600](https://openairdocs.org/sdr/SWAA2024110554600.md): Fairing · cracked · Oct 29, 2024 · N953WN · Boeing 7377H4 · Trailing Edge Flaps
  > THE #8 FLAP TRACK FWD FAIRING (644AB) HAS A CRACK ON LOWER SURFACE<[01] REPAIRED CRACK ON #8 FWD FAIRING 644AB IAW SRM 51-70-05-2R-2;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. WITH STEPS 1-7
- [SDR SWAA2024110550016](https://openairdocs.org/sdr/SWAA2024110550016.md): Stiffener · cracked · Oct 18, 2024 · N953WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > VERTICAL STIFFENER IS CRACKED BS 663 LBL 26 WL 145<[01] CRACKED STIFFENER FOUND AT BS 663 LBL 26 WL 145; REMOVED AND INSTALLED NEW VERTICAL STIFFENER AT BS 663 LBL 26 WL 145 PER SRM 51-40-02-0G-0 AND DWG 111A1000 REV: A. FASTENERS COMMON TO VAPOR BARRIER WEB W
- [SDR SWAA2024110549346](https://openairdocs.org/sdr/SWAA2024110549346.md): Skate Angle · chafed · Oct 16, 2024 · N953WN · Boeing 7377H4 · Fuselage Main, Structure
  > CHAFED LH CROWN SKATE ANGLE AT BS1058 LBL11. WL308.5.<[01] REPAIRED LH CROWN SKATE ANGLE AT BS1058 LBL11. WL308.5 IAW SRM 53-80-71-2R-6.;[02] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2024110548973](https://openairdocs.org/sdr/SWAA2024110548973.md): Rib · cracked · Oct 16, 2024 · N953WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > R/H HORIZONTAL STABILIZER L/E 341B FIRST I/B RIB IS CRACKED (PANEL MARKED)<[01] REMOVED & REPLACED R/H HORIZONTAL STABILIZER L/E 341B FIRST I/B RIB I.A. W SRM 51-40-02 AND DWG 186A1301 LE STA 78.29;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2024110548977](https://openairdocs.org/sdr/SWAA2024110548977.md): Attach Bracket · cracked · Oct 16, 2024 · N953WN · Boeing 7377H4 · Wing, Attach Fittings
  > 651FB ATTACHING BRACKET (MARKED) IS CRACKED<[01] REMOVED AND REPLACED 651FB ATTACHING BRACKET; PER SRM 51-40-02-0G-0 AND BOEING DWG 115A2710 SHEET 2 REV.B;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE
- [SDR SWAA2024110549477](https://openairdocs.org/sdr/SWAA2024110549477.md): Web · cracked · Oct 16, 2024 · N953WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > LT WING FIXED T/E PANEL LOWER WEB HAS CRACK JUST IB OF DEFLECTION RIB ORSS 279. MARKED<[01] REMOVED; REPLACED; AND INSTALLED A NEW LT WING FIXED T/E PANEL LOWER WEB ORSS 279 IAW SRM 51-40-02 AND BOEING DWG 115A2512 SH 4.;[02] VERIFIED CORRECTIVE ACTION COMPLET
- [SDR SWAA2024110548945](https://openairdocs.org/sdr/SWAA2024110548945.md): Floor Panel · delaminated · Oct 15, 2024 · N953WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241KF TOP SURFACE IS DELAMINATED.<[01] COMPLETE STEP 1;[02] FABRICATED NEW 241KF FLOOR PANEL USING BMS4-17 TY6 LOT # 1569956-1; LIGHTLY SANDED EDGES; LOCATED; DRILLED AND UPSIZED ALL (32EA) THROUGH INSERT LOCATIONS IAW SRM 53-00-50-2R-0 PAR.
- [SDR SWAA2024110548938](https://openairdocs.org/sdr/SWAA2024110548938.md): Floor Panel · delaminated · Oct 15, 2024 · N953WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241AF TOP SURFACE IS DELAMINATED.<[01] COMPLETE STEP 1;[02] FABRICATED NEW 241AF FLOOR PANEL USING BMS4-17 TY6 LOT # 1569956-1; LIGHTLY SANDED EDGES; LOCATED; DRILLED AND UPSIZED ALL (44EA) THROUGH INSERT LOCATIONS IAW SRM 53-00-50-2R-0 PAR.
- [SDR SWAA2024110548937](https://openairdocs.org/sdr/SWAA2024110548937.md): Floor Panel · delaminated · Oct 15, 2024 · N953WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 231XF TOP SURFACE IS DELAMINATED.<[01] UPDATED STEP 1;[02] REINSTALLED NEW SERVICEABLE CABIN FLOOR PANEL 231XF PER AMM 53-21-00-400-801;[03] REMOVED & REPLACED NEW SERVICEABLE CABIN FLOOR PANEL 231XF PER AMM 53-21-00-400-801 & AMM 53-21-00-00
- [SDR SWAA2024110548972](https://openairdocs.org/sdr/SWAA2024110548972.md): Stub Frame · cracked · Oct 15, 2024 · N953WN · Boeing 7377H4 · Fuselage Main, Frame
  > 2EA CRACKS ON R1 DOOR STUB FRAME INNER SURFACE; ONE ABOVE SEAL DEPRESSOR BS295+4 WL266 L: 0.8'; ONE EXTENDING FROM AFT EDGE BS295+5 WL266 L: 0.2'<[01] DO NOT INSTALL NEW PART; SEE INCOMPLETE SUB-STEP 4 FOR 'FINISH COAT' APPLICATION.;[02] PARTIAL SUB-STEP 4 VER
- [SDR SWAA2024110548932](https://openairdocs.org/sdr/SWAA2024110548932.md): Attach Angle · cracked · Oct 15, 2024 · N953WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > B.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 8 W.L. 164.<[01] REMOVED; REPLACED; AND INSTALLED NEW B.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE PER SRM 51-40-02-0G-0; AND DWG 111A1000 REV:-.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.
- [SDR SWAA2024110548943](https://openairdocs.org/sdr/SWAA2024110548943.md): Attach Angle · cracked · Oct 15, 2024 · N953WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > B.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 28 W.L. 164.<[01] CRACK FOUND TO BE OUT OF LIMITS AS PER SRM 57-10-10-1A-2. PART WILL BE REMOVED AND REPLACED ON FAULT TTG8Q00WF8Z9;[02] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2024110548568](https://openairdocs.org/sdr/SWAA2024110548568.md): Skin · debonded · Oct 15, 2024 · N953WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > PANEL 191D INNER SKIN HAS MULTIPLE DISBONDS. (MARKED)<[01] PANEL 191D WITH MULTIPLE DISBONDS ON INNER SKIN WAS REPAIRED IAW SRM 51-70-05-2R-2.
- [SDR SWAA2024110548569](https://openairdocs.org/sdr/SWAA2024110548569.md): Skin · debonded · Oct 15, 2024 · N953WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > PANEL 191HL OUTER SKIN IS DISBONDED. (MARKED)<[01] DISBOND ON OUTER SKIN OF PANEL 191HL WAS REPAIRED IAW SRM 51-70-05-2R-2.

Next page: https://openairdocs.org/aircraft/N953WN/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 = 'N953WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N953WN/reports

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