# Service difficulty reports: N958WN

A list on [N958WN](https://openairdocs.org/aircraft/N958WN.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 4 · 158 reports

- [SDR SWAA2026062415452](https://openairdocs.org/sdr/SWAA2026062415452.md): Slide · out of position · Jun 24, 2026 · N958WN · Boeing 7377H4 · Escape Slide
  > L2 DOOR SLIDE ZEE FOLD HANGING DOWN. REINSTALLED L2 DOOR SLIDE IAW AMM 25-66-01 AND MT 725-61-01.
- [SDR SWAA2026033083734](https://openairdocs.org/sdr/SWAA2026033083734.md): Floor Panel · cracked · Mar 27, 2026 · N958WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 140BF IS CRACKED THRU AT SEVERAL FLOORBEAMS. REMOVED & REPLACED THE FLOOR PANEL 140BF IAW AMM 25-52-10, AND EA M-25-125-02433.
- [SDR SWAA2026033083733](https://openairdocs.org/sdr/SWAA2026033083733.md): Floor Panel · cracked · Mar 27, 2026 · N958WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD CARGO BAY FLOOR PANEL 120CF WAS CRACKED AT THE CENTER FLOOR BEAM 9 INCHES. REMOVED AND REPLACED THE FLOOR PANEL 120CF IAW AMM 25-52-10, AND EA M-25-125-02432.
- [SDR SWAA2026033083736](https://openairdocs.org/sdr/SWAA2026033083736.md): Battery Pack · no test · Mar 27, 2026 · N958WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY BATTERY PACK AT FWD ENTRY DOOR LEFT M1675 FAILED A CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2025081404149](https://openairdocs.org/sdr/SWAA2025081404149.md): Skirt · debonded · Aug 14, 2025 · N958WN · Boeing 7377H4 · Escape Slide
  > PASSENGER CABIN AFT SERVICE DOOR ESCAPE SLIDE SKIRT RUBBER DISBONDED AND FRAYED<[01] R&R PASSENGER CABIN AFT SERVICE DOOR ESCAPE SLIDE IAW AMM 25-66-01. REF.#TTG8Q00PLDJQ FOR PARTS INFO.;[02] INSPECTION C/W R&R PASSENGER CABIN AFT SERVICE DOOR ESCAPE SLIDE IAW
- [SDR SWAA2025051469707](https://openairdocs.org/sdr/SWAA2025051469707.md): Lens · loose · May 10, 2025 · N958WN · Boeing 7377H4 · Emergency Lighting
  > EXIT LIGHT LENS OVER FWD GALLEY SVC DOOR FELL OFF<[01] PERFORMED INTERIM REPAIR PER EA M-21-133-00720. SECURED WITH TAPE.
- [SDR SWAA2025051268746](https://openairdocs.org/sdr/SWAA2025051268746.md): Battery Pack · inoperative · May 7, 2025 · N958WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS INOP STA. 727C; STA. 952; AND STA. 322.<[01] REMOVED AND REPLACED 3 EA BATTERY PACKS M1670; M1673; AND M1674 AND OPS CHECK GOOD IAW SWA B737-700 AMM 33-51-06-960-805.;[02] REMOVED AND REPLACED 3 EA BATTERY PACKS M1670; M1673; AND M1674 AND OPS
- [SDR SWAA2025051255409](https://openairdocs.org/sdr/SWAA2025051255409.md): Stub Frame · cracked · Apr 23, 2025 · N958WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK FOUND R-1 DOOR UPPER FWD CUTOUT INTERNAL SURFACE JUST ABOVE SEAL DEPRESSOR MARKED AT.750' L TO END OF CUTOUT.<[01] REMOVED AND REPLACED 141A8371U7 STUB FRAME IAW B737-700 SRM 51-40-02 AND BAC DWG 141A8370;[02] VERIFIED REMOVED AND REPLACED 141A8371U7 ST
- [SDR SWAA2025051255380](https://openairdocs.org/sdr/SWAA2025051255380.md): Handle · loose · Apr 21, 2025 · N958WN · Boeing 7377H4 · Passenger/Crew Doors
  > ASSIST HANDLE LOOSE AT R2 DOOR LINER<[01] SECURED ASSIST HANDLE AT R2 DOOR LINER IAW B737-700 AMM 52-13-31-400-802 SUBTASK 52-13-31-020-008;[02] SECURED ASSIST HANDLE AT R2 DOOR LINER IAW B737-700 AMM 52-13-31-400-802 SUBTASK 52-13-31-020-008
- [SDR SWAA2025051255366](https://openairdocs.org/sdr/SWAA2025051255366.md): Service Door · corroded · Apr 20, 2025 · N958WN · Boeing 7377H4 · Fluid Service Doors
  > CR VB LAV SERVICE DOOR HAS SPOT OF CORROSION ON INNER SURFACE<[01] CR VB LAV SERVICE DOOR HAS SPOT OF CORROSION ON INNER SURFACE [TTG8Q00ZYZ5U];[02] REMOVED AND REPLACED LAV SERVICE DOOR IAW B737-700 AMM 52-49-07-400-801; 20-50-11-910-801; & AIPC 52-49-07-01;[
- [SDR SWAA2025032408354](https://openairdocs.org/sdr/SWAA2025032408354.md): Tire · burst · Mar 22, 2025 · N958WN · Boeing 7377H4 · Landing Gear System
  > LEFT MAIN LANDING GEAR TIRE FAILED ON DEPARTURE ROLL REJECTED TAKEOFF AT 130 KNOTS. 31.7M FT-LBS <[01] PREFORMED CONDITIONAL INSPECTIONS; HIGH ENERGY STOP; BRAKE SEIZURE INSPECTION AND TIRE TREAD LOSS/ TIRE BURST INSPECTION SEE TTG8Q00ZE4FT FOR WORK PREFORMED.
- [SDR SWAA2024111858670](https://openairdocs.org/sdr/SWAA2024111858670.md): Slide · delaminated · Nov 12, 2024 · N958WN · Boeing 7377H4 · Escape Slide
  > FWD PASSENGER DOOR ESCAPE SLIDE SKIRT RUBBER COVER WORN AND DELAMINATED<[01] R&R FWD ENTRY ESCAPE SLIDE IAW MT 725-61-06 FE REF:TTG8Q0F8KDU.;[02] INSPECTION C/W R&R FWD ENTRY ESCAPE SLIDE IAW MT 725-61-06 FE REF:TTG8Q0F8KDU
- [SDR SWAA2024071512427](https://openairdocs.org/sdr/SWAA2024071512427.md): Cover · broken · Jul 12, 2024 · N958WN · Boeing 7377H4 · Emergency Lighting
  > WHITE COVER FOR EXIT/SALIDA BROKEN OFF FROM ROW 11 ABC<[01] R&R OVER WING EXIT LIGHT COVER IAW AMM 33-51-01
- [SDR SWAA2024070810050](https://openairdocs.org/sdr/SWAA2024070810050.md): Start Valve · leaking · Jul 7, 2024 · N958WN · Boeing 7377H4 · Engine Start Valves/Controls
  > #2 ENGINE OVERHEAT ON CLIMB OUT. ENGINE OVERHEAT LIGHT EXTINGUISHED WITH THRUST LEVER AT IDLE AFTER TWO MINUTES.<[01] FOUND START VALVE LEAKING EXCESSIVELY R+R #2 ENG START VALVE PER AMM 80-11-03
- [SDR SWAA2023120527140](https://openairdocs.org/sdr/SWAA2023120527140.md): Girt Bar · out of adjust · Dec 3, 2023 · N958WN · Boeing 7377H4 · Emergency Equipment
  > CAPT SIDE AFT EMERGENCY SLIDE BUNCHED UP ON BOTTOM OF DOOR WHEN GIRT BAR ARMED<[01] ADJUSTED PER M.M 25-66-01; NO DEFECTS FOUND
- [SDR SWAA2023061257679](https://openairdocs.org/sdr/SWAA2023061257679.md): Light · inoperative · Jun 8, 2023 · N958WN · Boeing 7377H4 · Emergency Lighting
  > ROW 11 ABC WINDOW LIGHT INOPERATIVE. RELAMPED 11ABC WINDOW LIGHT IN REF. TO AMM 33-21-00. OPS CHECK GOOD.
- [SDR SWAA2023051747782](https://openairdocs.org/sdr/SWAA2023051747782.md): Light · inoperative · May 11, 2023 · N958WN · Boeing 7377H4 · Emergency Lighting
  > L/H OWE LOWER EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED BULB AND PERFORMED A GOOD OPERATIONAL TEST IAW AMM 33-51-04-960-801.;[02] CERTIFIED ACTION 1;[03] JOB COMPLETE.
- [SDR SWAA2023051747430](https://openairdocs.org/sdr/SWAA2023051747430.md): Light · inoperative · May 11, 2023 · N958WN · Boeing 7377H4 · Emergency Lighting
  > SEAT ROW 1 BULLNOSE BIN EMERGENCY LIGHT INOP<[01] REPLACED SEAT ROW 1 BULLNOSE BIN EMERGENCY LIGHT LAMP IAW AMM 33-51-03-960-801. LIGHT STILL INOP.;[02] VERIFIED CORRECTIVE ACTION 1;[03] VERIFIED ACTION 1 IS COMPLETE;[04] REPARED WIRE W0130-001-20 IN CONNECTOR
- [SDR SWAA2023051728501](https://openairdocs.org/sdr/SWAA2023051728501.md): Attach Angle · cracked · Apr 17, 2023 · N958WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > F.E.D MOPSILL FOUND TO BE CRACKED AT FWD ATTACH FASTENER COMMON TO BS 303.9 FRAME<[01] REMOVED GIRT BAR BRACKET FLOOR ATTACHMENTS AT BS 312 AND BS 344 FOR ACCESS TO MOPSILL PER SRM 51-40-02-0G-0<BR><BR>BEGAN REMOVING FASTENERS IN MOPSILL PER SRM 51-40-02-0G-0;
- [SDR SWAA2023051826337](https://openairdocs.org/sdr/SWAA2023051826337.md): Floor Panel · pulled · Apr 11, 2023 · N958WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242UF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4. F.REMOVED DAMAGED PLIES ON UPPER FACESHEET IN NUMEROUS LOCATIONS WITH THE LARGEST MEASURING 6' X 5.5'; THEN CLEANED IAW SRM 53-00-50-2R
- [SDR SWAA2023051826142](https://openairdocs.org/sdr/SWAA2023051826142.md): Rail · damaged · Apr 11, 2023 · N958WN · Boeing 7377H4 · Fuselage Internal Mounting Structure
  > AFT CARGO BAY - RAIL HAS A MECHANICAL DAMAGE BS 747+6 RBL 3.<OUT OF LIMITS IAW SRM 51-10-02 AND 53-00-53-1A-2 FIG 103;DETAIL D.<BR>USED TOOL:<BR>ID:ATS2827<BR>DATE:01/13/23<BR>DUE:01/31/24;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.;[03] CORRECTIVE ACTION FOR STE
- [SDR SWAA2023051826141](https://openairdocs.org/sdr/SWAA2023051826141.md): Rail · corroded · Apr 11, 2023 · N958WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY - RAIL HAS CORROSION RBL 3 BS 767+5.<OUT OF LIMITS IAW SRM 51-10-02 AND 53-00-53-1A-2 FIG 103;DETAIL E.<BR>USED TOOL:<BR>ID:NCX000336<BR>S/N:UNKNOWN<BR>DATE:06/2022<BR>DUE:06/2023;[02] VERIFIED CORRECTIVE ACTION 2.;[03] SRM 53-00-53-2R-3 IS FOUND
- [SDR SWAA2023051726330](https://openairdocs.org/sdr/SWAA2023051726330.md): Doubler · cracked · Apr 11, 2023 · N958WN · Boeing 7377H4 · Fuselage Main, Structure
  > L/H VAPOR BARRIER DOUBLER IS CRACKED BS 663; LBL 25 W/L 148<[01] UPDATED STEP 1-9;[02] UPDATED STEP 10;[03] UPDATED MEASUREMENTS TABLE;[04] FABRICATED DOUBLER IAW SRM 51-30-01-0G-0 AND DWG 111A1511-27 REV:A FROM 2024 T0 0.040' LOT. 1510004-1;[05] VERIFIED CORR
- [SDR SWAA2023051726130](https://openairdocs.org/sdr/SWAA2023051726130.md): Stringer Clip · corroded · Apr 11, 2023 · N958WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT OF CARGO COMPARTMENT - STRINGER CLIP HAS CORROSION BS 947 STR 26L<[01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS AFT CARGO COMPARTMENT STRINGER CLIP BS 947 STR 26 IAW SRM 51-10-02;[02] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR BY REPACEMENT IAW SRM
- [SDR SWAA2023051726129](https://openairdocs.org/sdr/SWAA2023051726129.md): Girt Bar · corroded · Apr 11, 2023 · N958WN · Boeing 7377H4 · Escape Slide
  > FOUND CORROSION ON R/H GIRT BAR FITTING AFT MOUNTING BRACKET FASTENER HOLE BS 986 WL 208 RBL 43<[01] UPDATED MEASUREMENT TABLE;[02] SRM 53-70-51-2R-6 FOUND TO BE APPLICABLER FOR 986 FLOOR BEAM REPAIR;[03] REMOVED DAMAGE ON 986 FLOOR BEAM AT RBL 43 WL208 GIRT B
- [SDR SWAA2023051726128](https://openairdocs.org/sdr/SWAA2023051726128.md): Girt Bar · corroded · Apr 11, 2023 · N958WN · Boeing 7377H4 · Escape Slide
  > FOUND CORROSION ON L/H GIRT BAR FITTING AFT MOUNTING BRACKET FASTENER HOLE BS 986 WL 208 LBL 43<OUT OF LIMITS PER B737-700 SRM 53-70-51-2R-6 REPAIR 6.REMOVED CORROSION DAMAGE AREA PER B737-700 SRM 53-70-51-2R-6 REPAIR 6; FIGURE 6. REQUIRE DETAIL INSPECTION ON
- [SDR SWAA2023051726334](https://openairdocs.org/sdr/SWAA2023051726334.md): Intercostal · cracked · Apr 11, 2023 · N958WN · Boeing 7377H4 · Fuselage Main, Structure
  > FOUND CRACK ON INTERCOSTAL COMMON TO FASTENER HOLE AT BS 353.5 WL 208 LBL 11<[01] UPDATED MEASUREMENT TABLE;[02] REMOVED INTERCOSTAL FOR ACCESS AT BS344-360 WL208.5 RBL2 PER SRM 51-40-02-0G-0;[03] REMOVED INTERCOSTAL AT BS 344-360 WL208 LBL11 PER SRM 51-40-02-
- [SDR SWAA2023051726335](https://openairdocs.org/sdr/SWAA2023051726335.md): Intercostal · cracked · Apr 11, 2023 · N958WN · Boeing 7377H4 · Fuselage Main, Structure
  > FOUND CRACK ON INTERCOSTAL COMMON TO FASTENER HOLE AT BS 284.5 WL 208 BL 0<[01] UPDATED MEASUREMENT TABLE;[02] REMOVED INTERCOSTAL AT 208 BL 0 BS 277-294.5 AND LOCATED AND DRILLED NEW INTERCOSTAL PN:141A5410U3AAR; NEED OK TO INSTALL;[03] CERTIFY;[04] VERIFIED
- [SDR SWAA2023051726336](https://openairdocs.org/sdr/SWAA2023051726336.md): Intercostal · cracked · Apr 11, 2023 · N958WN · Boeing 7377H4 · Fuselage Main, Structure
  > FOUND CRACK ON INTERCOSTAL COMMON TO FASTENER HOLE AT BS 321 WL 208 LBL 44<[01] UPDATED MEASUREMENT FIELD;[02] UPDATED MEASUREMENT TABLE;[03] CERTIFY;[04] REMOVED INTERCOSTAL AT WL208 LBL44 BS 312-328; LOCATED AND DRILLED NEW INTERCOSTAL PN:141A5410U12. NEED O
- [SDR SWAA2023051925556](https://openairdocs.org/sdr/SWAA2023051925556.md): Plate · cracked · Apr 10, 2023 · N958WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FOUND 2 EA AREAS OF CORROSION ALONG MOP SEAL THRESHOLD I/B ATTACH PLATE FED AT BS 313.4-316 WL 208 LBL 59 AND BS 334-336.5 WL 208 LBL 62.5<[01] VERIFIED APPLICABILITY FOR SRM 53-10-15-1A-1;[02] REMOVED CORROSION ALONG MOP SEAL THRESHOLD I/B ATTACH PLATE FED AT
- [SDR SWAA2023051825806](https://openairdocs.org/sdr/SWAA2023051825806.md): Floor Panel · damaged · Apr 10, 2023 · N958WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD CABIN FLOOR PANEL 222CF HAS A RIPPED OUT INSERT 3RD BACK FROM THE FWD EDGE ON L/H SIDE<OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.FABRICATED AND CLEANED HONEYCOMB CORE PLUGS USING BMS 8-124; C4; T05; G09 LOT: 1287137 IAW SRM 53-00-50-2R-6 PARA
- [SDR SWAA2023051825822](https://openairdocs.org/sdr/SWAA2023051825822.md): Seat Track · corroded · Apr 10, 2023 · N958WN · Boeing 7377H4 · Fuselage Internal Mounting Structure
  > CORROSION ON PASSENGER CABIN SEAT TRACK LBL45 BS727B+3; BS727B+20; BS727D+13; 747+2; 747+13; 767+14;787+6; 807+5; 827+16; 867+7. WL208.< OUT OF LIMITS PER SRM 53-00-52-1A-1. SEAT TRACK TO BE REPLACED.;[02] VERIFIED CORRECTIVE ACTIONS STEP 1;[03] REMOVED CABIN
- [SDR SWAA2023051825819](https://openairdocs.org/sdr/SWAA2023051825819.md): Seat Track · corroded · Apr 10, 2023 · N958WN · Boeing 7377H4 · Fuselage Internal Mounting Structure
  > CORROSION ON PASSENGER CABIN SEAT TRACK RBL45 BS727C+16; 766;787+10; 807; 827; 827+14; 847+11; 867+3 WL208.< OUT OF LIMITS PER SRM 53-00-52-1A-1. FIGURE 103; PG.11. SEAT TRACK TO BE REPLACED.;[02] VERIFIED CORRECTIVE ACTION 1<BR>VERIFIED MEASUREMENTS TABLE.;[0
- [SDR SWAA2023051825558](https://openairdocs.org/sdr/SWAA2023051825558.md): Shield · corroded · Apr 10, 2023 · N958WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > R/H FLOOR TO SIDEWALL SHIELD CORROSION; BS500+2; +6; +10; +14; RBL24; WL156; R/H FLOOR TO SIDEWALL SHIELD CORROSION BS500+2 +6 +10 +14 RBL24 WL156<[01] REMOVED CORROSION FROM 6 SPOTS ON PART 143A8126Y36. THE DEEPEST SPOT IS 1.00 X 1.50 DEPTH 0.015. ORDINAL THI
- [SDR SWAA2023051725820](https://openairdocs.org/sdr/SWAA2023051725820.md): Frame · cracked · Apr 10, 2023 · N958WN · Boeing 7377H4 · Fuselage Main, Frame
  > FRAME BS 312 CRACKED IN RADIUS; AT UPPER DOOR THRESHOLD STR 5 LH<[01] REMOVED DAMAGE IAW SRM51-10-02-OG.;[02] VERIFIED CORRECTION ITEM 1.;[03] REQUEST NDI FOR HFEC SERVICE SCAN TO VERIFY CRACK FREE CONDITION AT CUT OUT.;[04] HFEC INSPECTED CUTOUT AREA IAW 737
- [SDR SWAA2023051725560](https://openairdocs.org/sdr/SWAA2023051725560.md): Structure · corroded · Apr 10, 2023 · N958WN · Boeing 7377H4 · Fuselage Main, Structure
  > FCB SUB THRESHOLD CORROSION; BS460 +4; +5; +7; +10; +13; +16 2EA; +18; BS480+1; +11 MARKED;<[01] VERIFIED APPLICABILITY OF SRM 53-30-15-1A-1 ALLOWABLE DAMAGE 1 AND SRM 53-30-15-01-1 IDENTIFICATION 1.;[02] UPDATED MEASUREMENT TABLE.<BR>REMOVED CORROSION FROM BS
- [SDR SWAA2023051725559](https://openairdocs.org/sdr/SWAA2023051725559.md): Support Angle · corroded · Apr 10, 2023 · N958WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > R/H FLOOR TO SIDEWALL SUPPORT ANGLE CORROSION; BS500A +2; 6; 10; BS500B+10; +14; BS500C +7; +10; RBL24; WL156<[01] VERIFIED APPLICABILITY IAW SRM 53-30-53-01-2 AND SRM 53-00-53-1A-2;[02] REMOVED CORRSION AT<BR><BR>BS 500A+2 0.005'(OUT OF LIMIT) - THE DEEPEST D
- [SDR SWAA2023051725808](https://openairdocs.org/sdr/SWAA2023051725808.md): Seat Track · corroded · Apr 10, 2023 · N958WN · Boeing 7377H4 · Fuselage Internal Mounting Structure
  > CORROSION ON PASSENGER CABIN SEAT TRACK LBL45 BS497; BS500A+4; WL208.<[01] SEAT TRACK TO BE REPLACED ON FAULT ID: TTG8Q00KCSLD;[02] VERIFIED CORRECTIVE ACTIONS 1.
- [SDR SWAA2023051725564](https://openairdocs.org/sdr/SWAA2023051725564.md): Plate · corroded · Apr 10, 2023 · N958WN · Boeing 7377H4 · Fuselage Main, Structure
  > FOUND 3EA AREAS OF CORROSION ALONG MOPSILL THRESHOLD ATTACH PLATE FSD AT BS 310-312.5 WL 208 RBL 56.5; BS 316-317.5 WL 208 RBL 58 AND BS 319.5-320.5 WL 208 RBL 58.75<[01] VERIFIED APPLICABILITY FOR SRM 53-10-15-1A-2.<BR>REMOVED CORROSION FROM FSD MOPSILL THRES
- [SDR SWAA2023051725217](https://openairdocs.org/sdr/SWAA2023051725217.md): Seal · cracked · Apr 9, 2023 · N958WN · Boeing 7377H4 · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL FRONT SPAR ATTACH LUG UPPER SLIDE SEAL IS CRACKED<[01] REMOVED L/H HORIZ STAB FWD SPAR ATTACH LUG UPPER SLIDE SEAL IAW AMM 53-31-31-000-801. STEP 2.;[02] INSTALLED L/H HORIZ STAB FWD SPAR ATTACH LUG UPPER SLIDE SEAL IAW AMM 53-31-31-400-802. ST
- [SDR SWAA2023051824736](https://openairdocs.org/sdr/SWAA2023051824736.md): Floor Panel · pulled · Apr 8, 2023 · N958WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD PANEL 221DF UPPER FACESHEET HAS MULTIPLE AREAS OF PULLED STRANDS.<EXCEEDS THE ALLOWABLE DAMAGE LIMITS PER SRM 53-00-50-1A-1 PARA 4. B. PERFORMED DAMAGE REMOVAL & SURFACE PREPARATION IAW SRM 53-00-50-2R-1 PARA 4 STEPS A-F.;[03] UPDATED MEASUREMENTS;[04] VAL
- [SDR SWAA2023051824737](https://openairdocs.org/sdr/SWAA2023051824737.md): Floor Panel · pulled · Apr 8, 2023 · N958WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD PANEL 221EF UPPER FACESHEET HAS MULTIPLE AREAS OF PULLED STRANDS.<EXCEEDS THE ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-50-1A-1 PARA 4 F.REMOVED 32EA THROUGH INSERTS THEN PERFORMED DAMAGE REMOVAL & SURFACE PREPARATION STEPS USING BMS5-28 TYPE 19 POTTING COMPO
- [SDR SWAA2023051824740](https://openairdocs.org/sdr/SWAA2023051824740.md): Floor Panel · pulled · Apr 8, 2023 · N958WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD PANEL 222AF UPPER FACESHEET HAS MULTIPLE AREAS OF PULLED STRANDS.<OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR>DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-1.<BR>REMOVED ALL INSERTS ON PANEL TO FACILITATE REPAIR; REMOVED ALL DAMAGED PLIES ON U
- [SDR SWAA2023051824741](https://openairdocs.org/sdr/SWAA2023051824741.md): Floor Panel · pulled · Apr 8, 2023 · N958WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD PANEL 222BF UPPER FACESHEET HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] IDENTIFIED PANEL MATERIAL IAW 53-00-50-0I-1 SHEET 1; FIGURE 2; TABLE 2;<BR>AND DWG DOC: 141A5810 ID: 0464<BR><BR>DAMAGE TO UPPER FACESHEET AREAS IS OUT OF ALLOWABLE LIMITS IAW SRM<BR>53
- [SDR SWAA2023051824739](https://openairdocs.org/sdr/SWAA2023051824739.md): Floor Panel · pulled · Apr 8, 2023 · N958WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD PANEL 222CF UPPER FACESHEET HAS MULTIPLE AREAS OF PULLED STRANDS.<OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR><BR>WILL PERFORM REPAIRS IAW SRM 53-00-50-2R-1 REMOVED 40EA INSERTS TO FACILITATE REPAIR. REMOVED DAMAGED PLIES; CLEANED AND PREPAR
- [SDR SWAA2023051824742](https://openairdocs.org/sdr/SWAA2023051824742.md): Floor Panel · pulled · Apr 8, 2023 · N958WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD PANEL 222DF UPPER FACESHEET HAS MULTIPLE AREAS OF PULLED STRANDS.<OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR><BR>WILL PERFORM REPAIRS IAW SRM 53-00-50-2R-1<BR><BR>REMOVED 41EA INSERTS TO FACILITATE REPAIR. REMOVED DAMAGED PLIES; CLEANED AND
- [SDR SWAA2023051825794](https://openairdocs.org/sdr/SWAA2023051825794.md): Insert · damaged · Apr 8, 2023 · N958WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD PANEL 222DF HAS A RIPPED OUT INSERT ALONG THE O/B EDGE. (MARKED)<OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F. FOUND ADDITIONAL DAMAGE ON THE INBOARD EDGE. FABRICATED AND CLEANED 2E HONEYCOMB CORE PLUGS USING BMS 8-124; TYPE V; GRADE 9.0; CLASS 4
- [SDR SWAA2023051825027](https://openairdocs.org/sdr/SWAA2023051825027.md): Sidewall Support · corroded · Apr 8, 2023 · N958WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MULTIPLE AREA OF CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727E+9 TO BS 7847.<OUT OF LIMITS IAW SRM 53-00-53-1A-2. REPAIR BY REPLACEMENT<BR><BR>TOOL USED<BR>DEPTH GAUGE ID:ATS2678 CAL.DUE:02/29/2024 LOCATED AND DRILLED NEW AFT CARGO COM
- [SDR SWAA2023051825020](https://openairdocs.org/sdr/SWAA2023051825020.md): Tie Down · corroded · Apr 8, 2023 · N958WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY - TRACK-TIE DOWN HAS CORROSION RBL 13.75 BS 727D+8; BS 747; BS 767+5; BS 787+5; BS 787+8; BS 787+11; BS 787+15; BS 787+18.5<OUT OF LIMITS IAW SRM 51-10-02 AND SRM 53-00-53-1A-2.;[02] CORROSION ON TRACK IT'S OUT OF LIMITS WIIL BE REPAIRED BY REPLA
- [SDR SWAA2023051825023](https://openairdocs.org/sdr/SWAA2023051825023.md): Shield · corroded · Apr 8, 2023 · N958WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MULTIPLE AREA OF CORROSION ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 22 BS 767-787<[01] REMOVED CORROSION FROM 8 SPOTS ON PART 146A8172U12. THE DEEPEST SPOT IS 0.75 X 0.75 DEPTH 0.010. ORDINAL THICKNESS IS.040. PART HAS NO LIMITS FOR DAMAGE(OUT OF LIMITS). REPA

Next page: https://openairdocs.org/aircraft/N958WN/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 = 'N958WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N958WN/reports

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