# Service difficulty reports: N413WN, cancelled Jun 5, 2026 A list on [N413WN, cancelled Jun 5, 2026](https://openairdocs.org/deregistered/N413WN-2026-06-05.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 · 307 reports - [SDR SWAA2025072393464](https://openairdocs.org/sdr/SWAA2025072393464.md): Lens · loose · Jul 20, 2025 · N413WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY EXIT LIGHT LENS LOOSE ROW 3 DEF, SECURED LENS WITH TAPE. OK TO CONTINUE PER MEL 3-15-02 SP-1B. REINSTALLED EMERGENCY LIGHT LENS AT ROW 3DEF PER AMM 33-51-03. OPS CHECK GOOD. - [SDR SWAA2025063086111](https://openairdocs.org/sdr/SWAA2025063086111.md): Floor Panel · cracked · Jun 27, 2025 · N413WN · Boeing 7377H4 · Fuselage Floor Panel > FWD CARGO BIN HAS FWD CRACK ON FLOOR<[01] PREFORMED REPAIR OF FWD CARGO AFT FLOOR PANEL (120CF) PER SRM 53-00-53-1A-1 TO BE REINSPECTED EVERY 400 CYCLE MUST REPLACE AT 4;000 CYCLES - [SDR SWAA2025063085969](https://openairdocs.org/sdr/SWAA2025063085969.md): Floor Panel · cracked · Jun 26, 2025 · N413WN · Boeing 7377H4 · Fuselage Floor Panel > FWD CARGO BIN HAS FWD CRACK ON FLOOR <[01]. OK TO CONTINUE AS PER MEL 25-16-01 SP1B AUTH NO 263657; [02] PERFORMED REPAIR ON FWD CARGO PIT AFT FLOOR PANEL 120CF PER SRM 53-00-53 SEE NON-ROUTINE TTG8Q013EBJT FOR CORRECTIVE ACTION AND TLD. - [SDR SWAA2025050767579](https://openairdocs.org/sdr/SWAA2025050767579.md): Girt Bar · out of adjust · May 5, 2025 · N413WN · Boeing 7377H4 · Emergency Equipment > AFT FLT ATT NDT REPORTS CAPT SIDE GIRT BAR CATCHING ON DOOR FRAME. ADJUSTED GIRT BAR IAW AMM 25-66-01. - [SDR SWAA2025041725075](https://openairdocs.org/sdr/SWAA2025041725075.md): Seat · loose · Apr 16, 2025 · N413WN · Boeing 7377H4 · Passenger Compartment Equipment > PASSENGER CABIN SEAT ROWS 1DEF; 2DEF; 3DEF; 5ABC; 8ABC AND 11DEF LOOSE IN SEAT TRACKS <[01]. ADJUSTED SEAT ROWS 1DEF; 2DEF; 3DEF; 5ABC; 8ABC; & 11DEF IN REF TO CMM 25-21-42. - [SDR SWAA2024121878927](https://openairdocs.org/sdr/SWAA2024121878927.md): Girt Bar · out of adjust · Dec 17, 2024 · N413WN · Boeing 7377H4 · Escape Slide > CAPT AFT DOOR OPENED FROM OUTSIDE WITH GIRT BAR ATTACHED<[01] INSPECTED AFT DOOR SLIDE ON CAPT SIDE IN REFERENCE TO AMM 25-66-00 NO FAULTS NOTED - [SDR SWAA2024090934916](https://openairdocs.org/sdr/SWAA2024090934916.md): Cover · out of adjust · Sep 6, 2024 · N413WN · Boeing 7377H4 · Escape Slide > AFT GALLEY SLIDE DOES NOT STOW PROPERLY<[01] READJUSTED AFT ENTRY DOOR SLIDE COVER PER SIP. NO OTHER DEFECTS NOTED. - [SDR SWAA2024072516217](https://openairdocs.org/sdr/SWAA2024072516217.md): Slide · dislodged · Jul 24, 2024 · N413WN · Boeing 7377H4 · Escape Slide > FLIGHT CREW LEFT GIRT BAR ARMED ON FWD SERVICE DOOR AND SLIDE CAME OUT AND PARTLY UNPACKED.<[01] REMOVED AND REPLACED FWD SERVICE DOOR SLIDE IAW AMM 25-66-01 AND MT 734-00-03. - [SDR SWAA2024050783114](https://openairdocs.org/sdr/SWAA2024050783114.md): Girt Bar · loose · May 6, 2024 · N413WN · Boeing 7377H4 · Emergency Equipment > AFT ENTRY SLIDE GIRT BAR LOOSE<[01] RE-ADJUSTED GIRT BAR AND AFT ENTRY SLIDE REF MT 725-61-06 - [SDR SWAA2023082490844](https://openairdocs.org/sdr/SWAA2023082490844.md): Rib · cracked · Aug 17, 2023 · N413WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > L/H HORIZONTAL STABILIZER REMOVABLE L/E; #4 (FROM I/B) UPPER RIB CRACKED. (MARKED)<[01] SRM 55-10-09-0I-1 IDENTIFICATION AND SRM 53-10-09-1A-1 ALLOWABLE DAMAGE ARE APPLICABLE.
RIB LE.STA 95.96 CRACKED; FOUND TO BE OUT OF LIMITS PER 55-10-09-1A-1 PARAGRAPH 4 - [SDR SWAA2023082490845](https://openairdocs.org/sdr/SWAA2023082490845.md): Rib · cracked · Aug 17, 2023 · N413WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > R/H HORIZONTAL STABILIZER REMOVABLE L/E; #2 (FROM I/B) LOWER RIB CRACKED. (MARKED)<[01] SRM 55-10-09-0I-1 IDENTIFICATION AND SRM 53-10-09-1A-1 ALLOWABLE DAMAGE ARE APPLICABLE.
RIB LE.STA 78.29 CRACKED FOUND TO BE OUT OF LIMITS PER 55-10-09-1A-1 PARAGRAPH 4. - [SDR SWAA2023082489571](https://openairdocs.org/sdr/SWAA2023082489571.md): Stiffener · cracked · Aug 14, 2023 · N413WN · Boeing 7377H4 · Horizontal Stabilizer Structure > REJECTED: L/H H-STAB RIB #7 STIFFENER #4 UPPER RADIUS CRACKED: SRM APPLICABILITY VALIDATION FOR REPAIR; AND NDT/VISUAL INSPECTIONS NOT PERFORMED AFTER DAMAGE REMOVAL.<[01] L/H H-STAB RIB #7 STIFFENER #4 UPPER RADIUS CRACKED: ACCOMPLISHED ON COSTUMER CARD TTG8Q - [SDR SWAA2023082487322](https://openairdocs.org/sdr/SWAA2023082487322.md): Support Bracket · cracked · Aug 9, 2023 · N413WN · Boeing 7377H4 · Wing Miscellaneous Structure > RT WING T/E PANEL 651FB FWD CENTER SUPPORT BRACKET IS CRACKED<[01] REMOVED AND REPLACED CRACKED FWD SUPPORT BRACKET ON PNL 651FB PER SRM 51-40-02-0G-0;[02] ADD REFERENCE SOPM 20-50-02;[03] VERIFIED CORRECTIVE ACTION #1. - [SDR SWAA2023082487069](https://openairdocs.org/sdr/SWAA2023082487069.md): Stringer · cracked · Aug 8, 2023 · N413WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > AREA AFT OF FORWARD CARGO BAY; STR 23R IS CRACKED AT AFT FASTENER BS 520+18<[01] PARTIAL STEP 1;[02] THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 (REPAIR 1) AND EA 23-153-02467';[03] TASK CARD COMPLETE - [SDR SWAA2023082487068](https://openairdocs.org/sdr/SWAA2023082487068.md): Stringer · cracked · Aug 8, 2023 · N413WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > AREA AFT OF FORWARD CARGO BAY; STR 26R IS CRACKED AT AFT FASTENER BS 520+18<[01] PARTIAL STEP 1;[02] REPAIRED AREA AFT OF FORWARD CARGO BAY; STR 26R FROM BS 500D+11 TO BS 540 IAW SRM 53-00-03-2R-1;[03] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE;[04] VE - [SDR SWAA2023082487066](https://openairdocs.org/sdr/SWAA2023082487066.md): Stringer · cracked · Aug 8, 2023 · N413WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > AREA AFT OF FORWARD CARGO BAY; STR 23L IS CRACKED AT AFT FASTENER BS 520+18<[01] COMPLETED STEPS 1;2;3 AND 5;[02] THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 (REPAIR 1) AND EA 23-153-02474;[03] VERIFIED CORRECTIVE ACTION #2.
VERIFIED MEASUREMENTS. - [SDR SWAA2023082486832](https://openairdocs.org/sdr/SWAA2023082486832.md): Stiffener · cracked · Aug 8, 2023 · N413WN · Boeing 7377H4 · Horizontal Stabilizer Structure > L/H H-STAB RIB #5 STIFFENERS 2 & 3 LOWER RADII ARE CRACKED.<[01] REMOVED THE DAMAGED PART AT LH HORIZONTAL STABILIZER STA 129.50 RIB 2ND AND 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4;[02] HFEC REQUEST ON THE CUT OUT EDGES; WEB AND EXISTING FASTENERS HOLES W - [SDR SWAA2023082486834](https://openairdocs.org/sdr/SWAA2023082486834.md): Stiffener · cracked · Aug 8, 2023 · N413WN · Boeing 7377H4 · Horizontal Stabilizer Structure > CRACK INDICATION ON L/H H-STAB RIB #7 STIFFENER #4 UPPER RADIUS.<[01] REJECTED: L/H H-STAB RIB #7 STIFFENER #4 UPPER RADIUS CRACKED: THE SRM APPLICABILITY VALIDATION FOR REPAIR; AND NDT/VISUAL INSPECTIONS NOT PERFORMED AFTER DAMAGE REMOVAL. GENERATED TTG8Q00MU - [SDR SWAA2023082486833](https://openairdocs.org/sdr/SWAA2023082486833.md): Stiffener · cracked · Aug 8, 2023 · N413WN · Boeing 7377H4 · Horizontal Stabilizer Structure > R/H H-STAB RIB 4 #3 STIFFENER LOWER RADIUS IS CRACKED.<[01] REMOVED THE DAMAGED PART AT RH HORIZONTAL STABILIZER STA 120.30 RIB 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4;[02] HFEC REQUEST ON THE CUT OUT EDGES; WEB AND EXISTING FASTENERS HOLES WITHIN THE REP - [SDR SWAA2023082387321](https://openairdocs.org/sdr/SWAA2023082387321.md): Scuff Plate · cracked · Aug 8, 2023 · N413WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > AFT CARGO BAY FORWARD CORNER SCUFF PLATE IS CRACKED<[01] WELDED CRACK ON AFT CARGO BAY FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARAGRAPH 4.B. (2) AND (4)
EQUIPMENT USED; WELDING MACHINE E10583; CALIBRATION DUE - [SDR SWAA2023082387067](https://openairdocs.org/sdr/SWAA2023082387067.md): Stringer · cracked · Aug 8, 2023 · N413WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > AREA AFT OF FORWARD CARGO BAY; STR 27R IS CRACKED AT AFT FASTENER BS 520+18<[01] PARTIAL STEP 1;[02] REPAIRED AREA AFT OF FORWARD CARGO BAY; STR 27R FROM BS 500D+11 TO BS 540 IAW SRM 53-00-03-2R-1;[03] VERIFIED CORRECTIVE ACTION 2 AND MEASUREMENT TABLE - [SDR SWAA2023082387065](https://openairdocs.org/sdr/SWAA2023082387065.md): Stringer · cracked · Aug 8, 2023 · N413WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > AREA AFT OF FORWARD CARGO BAY; STR 24L IS CRACKED AT AFT FASTENER BS 520+18<[01] COMPLETED STEPS 1;2;3 AND 5;[02] REPAIRED AREA AFT OF FORWARD CARGO BAY; STR 24L FROM BS 500D+10 TO BS 540 IAW SRM 53-00-03-2R-1 REPAIR 1;[03] VERIFIED CORRECTIVE ACTION 2 AND MEA - [SDR SWAA2023082387064](https://openairdocs.org/sdr/SWAA2023082387064.md): Stringer · cracked · Aug 8, 2023 · N413WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > AREA AFT OF FORWARD CARGO BAY; STR 26L IS CRACKED AT AFT FASTENER BS 520+18<[01] COMPLETED STEPS 1;2;3 AND 7;[02] REMOVED DAMAGED SECTION OF STR 26L BETWEEN BS 500D+10 TO 540 AND INSTALLED HAT SECTION SPLICE AND NEW STRINGER SECTION IAW SRM 53-00-03-2R-1 (REPA - [SDR SWAA2023082486619](https://openairdocs.org/sdr/SWAA2023082486619.md): Panel · cracked · Aug 7, 2023 · N413WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > WING CENTER SECTION BREAK PANEL IS CRACKED AT BS 540; RBL 1; WL 208<[01] REMOVED AND INSTALLED NEW BREAK PANEL AT WING CENTER SECTION BS 540; PER SRM 51-40-02 AND DWG 143A0060.;[02] VERIFIED CORRECTIVE ACTION #1.
VERIFIED MEASUREMENTS. - [SDR SWAA2023082486620](https://openairdocs.org/sdr/SWAA2023082486620.md): Attach Angle · cracked · Aug 7, 2023 · N413WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > WING CENTER SECTION CABLE INTERCOSTAL LOWER ATTACH ANGLE IS CRACKED AT BS 685+7; RBL 24; WL 203<[01] VERIFIED CORRECTIVE ACTION PARTIAL ITEMS AND MEASUREMENT FIELDS; CARD COMPLETE; EXCEPT MISSING AMT SUMMARY OF WORK PER MPM.;[02] REMOVED AND REPLACED WING CENT - [SDR SWAA2023082486621](https://openairdocs.org/sdr/SWAA2023082486621.md): Attach Angle · cracked · Aug 7, 2023 · N413WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > WING CENTER SECTION CABLE INTERCOSTAL LOWER ATTACH ANGLE IS CRACKED AT BS 685+7; LBL 24; WL 203<[01] VERIFIED CORRECTIVE ACTION PARTIAL ITEMS AND MEASUREMENT FIELDS; CARD COMPLETE; EXCEPT MISSING AMT SUMMARY OR WORK PER MPM.;[02] TYPO: MISSING SUMMARY OF WORK. - [SDR SWAA2023082386622](https://openairdocs.org/sdr/SWAA2023082386622.md): Frame · cracked · Aug 7, 2023 · N413WN · Boeing 7377H4 · Fuselage Main, Frame > BS 312 FRAME IS CRACKED IN THE LOWER RADIUS AT FED HEADER SUPPORT<[01] REPAIRED BS 312 FRAME LOWER RADIUS IAW EA # M-22-153-01244;[02] VERIFIED MEASUREMENT TABLE.
VERIFIED CORRECTIVE ACTION COMPLETE. CARD COMPLETE - [SDR SWAA2023082886355](https://openairdocs.org/sdr/SWAA2023082886355.md): Panel · pulled · Aug 6, 2023 · N413WN · Boeing 7377H4 · Wing, Plate/Skin > /R/W T/E PANEL 661CB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<[01] R/W T/E PANEL 661CB WITH SEVERAL PULLED FASTENER HOLE ON AFT END WAS REPAIRED IAW SRM 51-70-04-2R-9.;[02] DAMAGE WAS REPAIRED IAW SRM 51-70-04-2R-9.VERIFIED CURE TAPES UPLOADED.JOB - [SDR SWAA2023082886356](https://openairdocs.org/sdr/SWAA2023082886356.md): Panel · pulled · Aug 6, 2023 · N413WN · Boeing 7377H4 · Wing, Plate/Skin > R/W T/E PANEL 661BB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<[01] CONDUCTIVE COATED THE TOOLSIDE REPAIR SURFACE; CURED CONDUCTIVE COATING; AND PERFORMED A SATISFACTORY RESISTIVITY TEST WITH MULTIMETER ID:ATS1658 CAL DUE: 04/2024 IAW AMM 51-21-71-37 - [SDR SWAA2023082886357](https://openairdocs.org/sdr/SWAA2023082886357.md): Panel · pulled · Aug 6, 2023 · N413WN · Boeing 7377H4 · Trailing Edge Flaps > R/W T/E PANEL 661AB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<[01] R/W T/E PANEL 661AB WITH SEVERAL PULLED FASTENER HOLE ON AFT ENDWAS REPAIRED IAW SRM 51-70-04-2R-9.;[02] DAMAGE WAS REPAIRED IAW SRM 51-70-04-2R-9.VERIFIED CURE TAPES UPLOADED.JOB CO - [SDR SWAA2023082486362](https://openairdocs.org/sdr/SWAA2023082486362.md): Track · broken · Aug 6, 2023 · N413WN · Boeing 7377H4 · Horizontal Stabilizer Structure > L/H HORIZ STAB UPPER AFT SLIDE SEAL TRACK FOR IS BROKEN<[01] VERIFIED OK TO INSTALL L/H HORIZ STAB UPPER AFT SLIDE SEAL TRACK.;[02] REMOVED AND REPLACE L/H HORIZ STAB UPPER AFT SLIDE SEAL TRACK IAW AMM 20-50-11 AND AMM 51-21-99-300-801

TW ID: PER2271. C - [SDR SWAA2023082385853](https://openairdocs.org/sdr/SWAA2023082385853.md): Battery Pack · unknown · Aug 4, 2023 · N413WN · Boeing 7377H4 · Emergency Lighting > REMOVE AND REPLACE EMERGENCY EXIT LIGHT BATTERIES PRIOR TO AIRCRAFT DEPARTURE<[01] DOCUMENTATION OF INSTALLED PARTS;[02] ALL STEPS COMPLETE;[03] VERIFIED ALL PARTIAL STEPS COMPLETE; CARD COMPLETE; EXCEPT AMT MISSING FINAL ?SUMMARY OF WORK ACCOMPLISHED? PER MPM - [SDR SWAA2022093049110](https://openairdocs.org/sdr/SWAA2022093049110.md): Panel · damaged · Sep 29, 2022 · N413WN · Boeing 7377H4 · Aerodynamic Fairings > 193B MOUNTING HOLE LOCATIONS 1; 14; AND 19 HAVE ELONGATED OVERSIZED HOLES / [01] INSTALLED WASHERS AT HOLE LOCATIONS 1; 14; AND 19 PER EA 22-153-02942. - [SDR SWAA2022051908866](https://openairdocs.org/sdr/SWAA2022051908866.md): Lens · loose · May 17, 2022 · N413WN · Boeing 7377H4 · Emergency Lighting > 17ABC CLEAR LENS AT BULLNOSE LOOSE / [01] SECURED LENS IN PLACE WITH BIN TAPE
OK TO CONTINUE PER MEL 25-10-01 SP1B
AUTH 66639;[02] REINSTALLED AREA IGHT LENS AT ROW 17ABC IAW AMM 33-51-03 - [SDR SWAA2022010357368](https://openairdocs.org/sdr/SWAA2022010357368.md): Ballast · inoperative · Dec 31, 2021 · N413WN · Boeing 7377H4 · Emergency Lighting > RH EMERGENCY OVER WING EXIT SIDE WALL LIGHT OUT; FLORESCENT LIGHT ON THE EMERG DOOR. OK TO CONTINUE PER MEL 33-2-03 SP1B. R & R BALLAST IAW MM 33-21-00. - [SDR SWAA2021122254435](https://openairdocs.org/sdr/SWAA2021122254435.md): Cover · loose · Dec 18, 2021 · N413WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY LIGHT COVER AT 5DEF FELL OFF; / [01] SECURED LIGHT COVER AT 5DEF IAW AMM 33-51-03 OPS CHECK GOOD - [SDR SWAA2021121452162](https://openairdocs.org/sdr/SWAA2021121452162.md): Tie Rod · broken · Dec 12, 2021 · N413WN · Boeing 737 · Wing, Control Surfaces > SUPPLEMENTAL INFORMATION: L/H FIXED LOWER TE PANEL 551FB HAS BROKEN SUPPORT STUTS AT LEADING EDGE INBOARD SIDE.; / [01] R/R TWO BROKEN TIE RODS ON INBOARD FIXED TRAILING EDGE LOWER PANEL PER AMM 57-50-02 - [SDR SWAA2021112446110](https://openairdocs.org/sdr/SWAA2021112446110.md): Light · inoperative · Nov 21, 2021 · N413WN · Boeing 737 · Emergency Lighting > SUPPLEMENTAL INFORMATION: LEFT WING EMERGENCY EXIT DOOR OUTSIDE EMERGENCY LIGHT INOP; / [01] RELAMPED LEFT OVERWING EMERGENCY LIGHT IAW AMM 33-51-04 - [SDR SWAA2021102232413](https://openairdocs.org/sdr/SWAA2021102232413.md): None · cracked · Sep 27, 2021 · N413WN · Boeing 7377H4 · Escape Slide > GIRT TUBE END CRACKED OUT / [01] R&R GIRT TUBE IAW CMM 25-66-17.; [02] C/W - [SDR SWAA2021092018033](https://openairdocs.org/sdr/SWAA2021092018033.md): Door · out of adjust · Sep 16, 2021 · N413WN · Boeing 7377H4 · Passenger/Crew Doors > ON LANDING FWD ENTRY DOOR HANDLE POPPED UP A LITTLE AND FWD ENTRY LIGHT CAME ON. 2 OUT OF 3 LANDINGS. / [01] ADJUSTED FWD ENTRY DOOR OPS CHECK GOOD PER AMM 52-11-00 - [SDR SWAA2021091616781](https://openairdocs.org/sdr/SWAA2021091616781.md): Lamp · inoperative · Sep 12, 2021 · N413WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY LIGHT ROW 4ABL INOP.; / [01] RELAMPED EMERGENCY LIGHT AT ROW 4ABC PER B7373 AMM 33-51-03-960-801. INSTALLATION TEST; TESTED NORMAL.; [02] VERIFIED - [SDR SWAA2021091615326](https://openairdocs.org/sdr/SWAA2021091615326.md): Scuff Plate · cracked · Sep 8, 2021 · N413WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > AFT CARGO DOOR FORWARD CORNER SCUFF PLATE FOUND CRACKED.; / [01] LOCATED AND DRILLED NEW AFT CARGO DOOR FORWARD SCUFF PLATE IAW SRM 51-40-05-0G-0. SCUFF PLATE WILL BE INSTALLED ON CUSTOMER CARD #TTG8Q0035HUM.; [02] VERIFIED 1 - [SDR SWAA2021091614807](https://openairdocs.org/sdr/SWAA2021091614807.md): Battery Pack · inoperative · Sep 4, 2021 · N413WN · Boeing 7377H4 · Emergency Lighting > ASSOCIATED EMERGENCY LIGHTS BY LH OVER WING EXIT DOOR WITH BATTERY PACK M1668 ARE INOP.; OCIATED EMERGENCY LIGHTS BY LH OVER WING EXIT DOOR WITH BATTERY PACK M1668 ARE INOP. / [01] REPLACED BATTERY PACK AT M1668 L/H OVER WING AND PERFORMED OPS CHECK AS PER B7 - [SDR SWAA2021091613659](https://openairdocs.org/sdr/SWAA2021091613659.md): Support Bracket · broken · Aug 31, 2021 · N413WN · Boeing 7377H4 · Wing Miscellaneous Structure > RT WING AT LWR REAR SPAR NEAR OB FWD CORNER OF PNL 651BD HAS PNL SUPPORT BRKT BROKEN 8-98; / [01] REMOVED AND REPLACED SUPPORT BRACKET AT RT WING AT LOWER REAR SPAR IN IAW SRM 51-40-02-0G-0 P/N #115A5552U2; [02] VERIFIED 1 - [SDR SWAA2021091610592](https://openairdocs.org/sdr/SWAA2021091610592.md): Lug · corroded · Aug 23, 2021 · N413WN · Boeing 7377H4 · Horizontal Stabilizer Structure > CORROSION-- RH HORIZONTALSTABILIZER CENTER SECTION REAR SPAR LOWER CLEVIS E FWD LUG HAS CORROSION IN BORE.; / [01] ''PERFORMED EA 21-155-02335. REFER TO FAULT TTG8Q0065NR8''.; [02] VERIFIED STEP 1 - [SDR SWAA2021091610591](https://openairdocs.org/sdr/SWAA2021091610591.md): Lug · corroded · Aug 23, 2021 · N413WN · Boeing 7377H4 · Horizontal Stabilizer Structure > CORROSION-- RH HORIZONTAL STABILIZER CENTER SECTION REAR SPAR LOWER CLEVIS E AFT LUG HAS CORROSION ON FWD FACE.; / [01] ''PERFORMED EA 21-155-02335. REFER TO FAULT TTG8Q0065NR8''.; [02] VERIFIED STEP 1 - [SDR SWAA2021091609154](https://openairdocs.org/sdr/SWAA2021091609154.md): Spar · corroded · Aug 20, 2021 · N413WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > CORROSION FOUND ON RH REAR SPAR LOWER LUG K HAS CORROSION ON BOTH FACE OF THE LUG.; / [01] REPAIR ACCOMPLISHED PER EA 21-155-02337. REFER TO FAULT TTG8Q0065LLA.; [02] VERIFIED STEP 1 - [SDR SWAA2021091608697](https://openairdocs.org/sdr/SWAA2021091608697.md): Baffle · cracked · Aug 19, 2021 · N413WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > FWD CARGO RT SIDE PLATE BAFFLE CRACKED BTW STA 400 AND 420; / [01] REMOVED CRACKED BAFFLE OF FWD. CARGO COMP. STA. 400 TO 420. R/H.; [02] LOCATED AND DRILL NEW PLATE BAFFLE IAW. B-737-700 SRM. 51-40-05-0G-0; [03] VERIFIED 1-2. OK TO INSTALL NEW BAFFLE.; [04] - [SDR SWAA2021091607868](https://openairdocs.org/sdr/SWAA2021091607868.md): Fitting · corroded · Aug 16, 2021 · N413WN · Boeing 7377H4 · Vertical Stabilizer, Attach Fittings > LH O/B REAR SPAR FITTING OF VERTICAL STABILIZER(FTG-LH FWD MAIN)HAS PITTING CORROSION.; / [01] REMOVED LH O/B REAR SPAR FITTING OF VERTICAL STABILIZER - LH FWD MAIN IN IAW SRM 51-40-02-0G-0; [02] VERIFIED 1. OK TO LOCATE AND DRILL NEW FITTING.; [03] PARTIALLY - [SDR SWAA2021091606993](https://openairdocs.org/sdr/SWAA2021091606993.md): Clevis · corroded · Aug 14, 2021 · N413WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > **CORROSION** R/H HORIZONTAL STABILIZER REAR SPAR LOWER AFT CLEVIS 'E'; HAS CORROSION. DOT # 208-151; / [01] COMPLETED REPAIR OF RIGHT HORIZONTAL STABILIZER REAR SPAR LOWER AFT CLEVIS 'E' PER EA 21-155-02335 AND PER ENGINEERING WORK INSTRUCTIONS WIP1; WIP2. W Next page: https://openairdocs.org/deregistered/N413WN-2026-06-05/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 = 'N413WN' AND deregistration_id = 'N413WN-2026-06-05' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N413WN-2026-06-05/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.